INCH-POUND

MIL-STD-2161C(AS)
7 February 2014
SUPERSEDING
MIL-STD-2161B(AS)
15 August 2008

DEPARTMENT OF DEFENSE
STANDARD PRACTICE

PAINT SCHEMES AND EXTERIOR MARKINGS

FOR U.S. NAVY AND MARINE CORPS AIRCRAFT

AMSC 9453 AREA MFFP

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 MIL-STD-2161C(AS)
FOREWORD

1. This military standard is approved for use by the Naval Air Systems Command,
Department of the Navy, and is available for use by all Departments and Agencies of the
Department of Defense.
2. In furtherance of the Defense Standardization Program and to provide a single point
of reference that gives clear and concise direction for the paint schemes and exterior markings
for United States (U.S.) Navy and Marine Corps aircraft, this document has been prepared to be
a readily available reference source to all concerned.
3. This standard contains integrated instructions for paint schemes and exterior marking
for U.S. Navy and Marine Corps aircraft. This document supersedes the previous version and
includes revised requirements. Paint schemes for aircraft no longer in the active inventory have
been deleted, paint schemes for new aircraft added, and certain paint schemes for existing
aircraft modified.
4. For additional guidance on the contents of this document, contact the Naval Air
Systems Command, Attention: (AIR 4.1.8), NAWC-AD/48110 Shaw Road, Building 2187 Unit
5, Patuxent River, Maryland 20670-1906 or the Naval Air Warfare Center Aircraft Division,
Lakehurst (at the address below).
5. Comments, suggestions, or questions should be addressed to: Commander, Naval Air
Warfare Center Aircraft Division, Code 4L8000B120-3, Highway 547, Lakehurst, NJ 08733-
5100, or email to michael.sikora@navy.mil. Since contact information can change you may
want to verify the currency of this address information using the ASSIST Online database at
https://assist.dla.mil.

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FOREWORD .......................................................................................................... ii

1 SCOPE .................................................................................................................... 1
1.1 General .............................................................................................................. 1
1.2 Purpose.............................................................................................................. 1
1.3 Foreign government aircraft ............................................................................. 1
1.4 Military aircraft used in research projects ........................................................ 1
1.5 Military aircraft attached to designated adversary squadrons........................... 1
1.6 Areas of responsibility ...................................................................................... 1
1.6.1 Cognizant authority........................................................................................... 1
1.6.2 Major vs. minor modification ........................................................................... 2
1.6.3 Squadron/Air Wing markings ........................................................................... 2

2 APPLICABLE DOCUMENTS .............................................................................. 2

2.1 General .............................................................................................................. 2
2.2 Government documents .................................................................................... 2
2.2.1 Specifications and standards ............................................................................. 2
2.2.2 Non-Government publications .......................................................................... 3
2.3 Order of precedence .......................................................................................... 3

3 DEFINITIONS........................................................................................................ 4
3.1 Arctic paint scheme........................................................................................... 4
3.2 High visibility paint scheme ............................................................................. 4
3.3 Tactical paint scheme ........................................................................................ 4

4 GENERAL REQUIREMENTS .............................................................................. 4

4.1 Paint schemes and insignia markings ............................................................... 4
4.2 Material ............................................................................................................. 4
4.2.1 Finishes ............................................................................................................. 4
4.2.2 Compatibility .................................................................................................... 4
4.2.3 Applicable limitation ........................................................................................ 5
4.2.4 Metal marking instruments ............................................................................... 5
4.2.5 External finish identification............................................................................. 5
4.2.5.1 Record of finish application .............................................................................. 5

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4.3 Drawings ........................................................................................................... 5

4.4 Service requirements ......................................................................................... 5
4.5 Foreign government aircraft ............................................................................. 6
4.6 Color and style of marking materials and paint schemes ................................. 6
4.6.1 Color standard ................................................................................................... 6

5. DETAILED REQUIREMENTS ............................................................................. 7

5.1 Aircraft paint schemes ...................................................................................... 7
5.1.1 High visibility color configurations .................................................................. 7
5.1.1.1 Application and color patterns .......................................................................... 7
5.1.2 Arctic paint scheme........................................................................................... 8
5.1.3 Tactical paint schemes ...................................................................................... 8
5.1.3.1 Tactical paint scheme materials ........................................................................ 8
5.1.3.2 Tactical paint scheme patterns .......................................................................... 8
5.1.3.2.1 Aircraft surfaces ................................................................................................ 8
5.1.3.2.2 Bottom surfaces ................................................................................................ 9
5.1.4 Paint scheme for drones .................................................................................... 9
5.1.5 Paint scheme for unmanned aerial vehicles (UAV) .......................................... 9
5.1.6 Paint scheme for target aircraft ......................................................................... 9
5.1.7 Solar heat reflection .......................................................................................... 9
5.1.8 Antiglare ........................................................................................................... 9
5.1.9 Glass fiber reinforced plastic assemblies ........................................................ 10
5.1.10 Landing gear ................................................................................................... 10
5.1.10.1 Fixed landing gear........................................................................................... 10
5.1.10.2 Retractable landing gear ................................................................................. 10
5.1.11 Speed brakes, wing flaps, etc. ......................................................................... 10
5.1.12 Wing leading edge slats .................................................................................. 10
5.1.13 Walkways and steps ........................................................................................ 10
5.1.14 External stores (including ordnance) .............................................................. 10
5.1.15 Radomes, antennae, and antennae covers ....................................................... 11
5.1.16 Helicopter blades, hubs, transmissions and rotor mechanisms ....................... 11
5.1.16.1 Rotor blades .................................................................................................... 11
5.1.16.2 Hubs of helicopters ......................................................................................... 11
5.1.16.3 Transmission and rotor mechanisms of helicopters ........................................ 11

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5.1.17 Jet air intake ducts........................................................................................... 11

5.1.18 Propeller assemblies........................................................................................ 11
5.1.18.1 Blades.............................................................................................................. 12
5.1.18.2 Spinners........................................................................................................... 12
5.1.18.3 Hubs and domes .............................................................................................. 12
5.1.19 Engine cowling interiors ................................................................................. 12
5.2 Aircraft exterior markings............................................................................... 12
5.2.1 Identification marking..................................................................................... 12
5.2.1.1 Letter and numeral (character) construction ................................................... 12
5.2.1.1.1 Fixed wing aircraft .......................................................................................... 13
5.2.1.1.2 Rotary wing aircraft (helicopters) ................................................................... 13
5.2.1.1.3 Research aircraft ............................................................................................. 13
5.2.1.1.4 Experimental aircraft ...................................................................................... 13
5.2.1.1.5 Target aircraft.................................................................................................. 13
5.2.1.1.6 Test and evaluation (T&E) aircraft ................................................................. 13
5.2.1.1.7 Unmanned aerial vehicles (UAV) ................................................................... 13
5.2.1.1.8 United States Naval Test Pilot School (USNTPS) Aircraft ............................ 13
5.2.2 Mandatory markings for U.S. Navy and Marine Corps aircraft ..................... 14
5.2.2.1 Changes ........................................................................................................... 14
5.2.2.2 Application...................................................................................................... 15
5.2.2.3 National star insignia ...................................................................................... 15
5.2.2.4 Branch of service marking .............................................................................. 15
5.2.2.4.1 Size.................................................................................................................. 15
5.2.2.4.2 Location .......................................................................................................... 15
5.2.2.5 Model designation and bureau airplane serial number (BUNO) .................... 15
5.2.2.5.1 Location .......................................................................................................... 15
5.2.2.5.2 Size.................................................................................................................. 16
5.2.2.6 Unit aircraft number (MODEX) ..................................................................... 16
5.2.2.6.1 Location .......................................................................................................... 16
5.2.2.6.2 Size.................................................................................................................. 16
5.2.2.7 Unit identifier .................................................................................................. 16
5.2.2.7.1 Location .......................................................................................................... 16
5.2.2.7.2 Size.................................................................................................................. 16
5.2.2.8 Station or unit name ........................................................................................ 16

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5.2.2.8.1 Location .......................................................................................................... 16
5.2.2.8.2 Size.................................................................................................................. 16
5.2.2.9 Call numbers ................................................................................................... 17
5.2.2.9.1 Location .......................................................................................................... 17
5.2.2.9.2 Size.................................................................................................................. 17
5.2.2.10 Mandatory safety markings............................................................................. 17
5.2.2.10.1 Jet engine intake warning chevrons and signs ................................................ 17
5.2.2.10.1.1 Application...................................................................................................... 17
5.2.2.10.1.2 Variations ........................................................................................................ 18
5.2.2.10.2 Jet engine blast warning .................................................................................. 18
5.2.2.10.3 Propeller, rotor, and turbine safety markings.................................................. 18
5.2.2.10.3.1 Main rotor blades ............................................................................................ 18
5.2.2.10.3.1.1 Matched sets.................................................................................................... 18
5.2.2.10.3.1.2 Unmatched sets ............................................................................................... 19
5.2.2.10.3.1.3 Static balance - preservation and maintenance ............................................... 19
5.2.2.10.3.1.4 Classification numbers .................................................................................... 19
5.2.2.10.3.2 Tail rotor blades .............................................................................................. 19
5.2.2.10.3.3 Helicopter tail boom - warning marking ......................................................... 20
5.2.2.10.3.4 Helicopter tail rotor - guards and stabilizers ................................................... 20
5.2.2.10.3.5 Propeller blades - warning markings .............................................................. 20
5.2.2.10.3.6 Fuselage propeller - warning stripe and signs................................................. 21
5.2.2.10.3.7 Staggered engines ........................................................................................... 21
5.2.2.10.4 Arresting hooks ............................................................................................... 21
5.2.2.10.4.1 Arresting hook warning marking .................................................................... 21
5.2.2.10.5 Loose and jettisonable equipment ................................................................... 21
5.2.2.10.6 Identification and markings of emergency escape system .............................. 21
5.2.2.10.6.1 Application...................................................................................................... 22
5.2.2.10.6.2 Location .......................................................................................................... 22
5.2.2.10.6.3 Lettering size ................................................................................................... 22
5.2.2.10.6.4 Cutout area marking ........................................................................................ 22
5.2.2.10.6.5 Exit control lever markings ............................................................................. 22
5.2.2.10.6.6 Fire access panel marking ............................................................................... 22
5.2.2.10.6.7 Explosive-actuated devices ............................................................................. 23
5.2.2.10.6.8 Axe and crowbar ............................................................................................. 23
5.2.2.10.6.9 Fire extinguishers ............................................................................................ 23

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5.2.2.10.6.10 First-aid kit ...................................................................................................... 23

5.2.2.10.6.11 Ejection seat markings .................................................................................... 23
5.2.2.10.6.11.1 Ejection seat markings for multiplace aircraft ................................................ 23
5.2.2.10.6.11.2 Other cartridge-actuated escape systems ........................................................ 24
5.2.2.10.6.12 Canopy release markings ................................................................................ 24
5.2.2.10.6.13 External exit emergency release ..................................................................... 24
5.2.2.10.6.14 Transport aircraft ............................................................................................ 24
5.2.2.10.6.14.1 Internal removable escape panels ................................................................... 24
5.2.2.10.6.14.2 Emergency exit marking ................................................................................. 24
5.2.2.10.6.14.3 Handles, releases, catches, and knobs for inside panels ................................. 25
5.2.2.10.6.14.4 External removable escape panels .................................................................. 25
5.2.2.10.6.14.5 Markings for forced emergency entry or exit ................................................. 25
5.2.2.10.6.14.6 Secondary openings ........................................................................................ 25
5.2.3 Tactical paint scheme markings ...................................................................... 26
5.2.3.1 Color of markings for aircraft with tactical paint schemes ............................. 26
5.2.3.1.1 Tactical paint scheme - general marking policy ............................................. 26
5.2.3.1.2 Color of MODEX numbers............................................................................. 26
5.2.3.2 Size of markings when used on aircraft with tactical paint schemes .............. 26
5.2.3.3 Paint scheme deviations approval ................................................................... 27
5.2.4 Marking material............................................................................................. 27
5.2.5 Exterior maintenance precautionary and warning markings .......................... 27
5.2.5.1 Aircraft and missile service point identification symbols and markings ........ 27
5.2.5.1.1 Application of service point identification symbols and markings ................ 27
5.2.5.1.2 Location .......................................................................................................... 27
5.2.5.1.3 Hydraulic system and landing gear/struts ....................................................... 28
5.2.5.2 Fuel nozzle jumper plug receptacles ............................................................... 28
5.2.5.3 Aircraft grounding points ................................................................................ 28
5.2.5.4 Storage batteries .............................................................................................. 28
5.2.5.5 Instrument static opening markings ................................................................ 28
5.2.5.6 Wing fold warning flag ................................................................................... 28
5.2.5.7 Markings for electrical connections ................................................................ 28
5.2.5.8 Markings for engine removal .......................................................................... 29
5.2.5.9 Markings for tank and filler areas ................................................................... 29
5.2.5.9.1 Tank ................................................................................................................ 29

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5.2.5.9.2 Filler caps ........................................................................................................ 29

5.2.5.10 Lift points, handgrips, caution legends, etc. ................................................... 29
5.2.5.11 Baggage compartment, life raft stowage, etc. ................................................. 29
5.2.5.12 Wing access panel latches and safety straps ................................................... 29
5.2.5.13 Actuating mechanism-warning signs .............................................................. 29
5.2.5.14 Recessed lubrication fittings ........................................................................... 30
5.2.6 Optional markings........................................................................................... 30
5.2.6.1 Ship names ...................................................................................................... 30
5.2.6.2 Squadron designation ...................................................................................... 30
5.2.6.3 Reserve aircraft markings - station names ...................................................... 30
5.2.6.4 Battle “E” ........................................................................................................ 30
5.2.6.5 Safety “S”........................................................................................................ 31
5.2.6.6 Hospital aircraft red cross ............................................................................... 31
5.2.6.7 Aircraft pilot and crew chief names ................................................................ 31
5.2.6.8 NAVAIR logo ................................................................................................. 31
5.2.6.8.1 Color ............................................................................................................... 32
5.2.6.8.2 Location .......................................................................................................... 32
5.2.6.8.3 Size.................................................................................................................. 32
5.2.6.8.4 Letter font........................................................................................................ 32
5.2.7 Special purpose marking for U.S. Navy aircraft ............................................. 32
5.2.7.1 Identification of American Legation U.S. Naval Attaché
(ALUSNA) aircraft ......................................................................................... 32
5.2.7.1.1 Fuselage marking ............................................................................................ 32
5.2.7.1.2 Naval attaché fuselage marking ...................................................................... 32
5.2.7.1.2.1 Location .......................................................................................................... 33
5.2.7.1.2.2 Size.................................................................................................................. 33
5.2.7.1.3 Naval attaché wing marking ........................................................................... 33
5.2.7.1.3.1 Location .......................................................................................................... 33
5.2.7.1.3.2 Size.................................................................................................................. 33
5.2.7.1.4 Naval attaché vertical stabilizer marking ........................................................ 33
5.2.7.1.4.1 Location .......................................................................................................... 33
5.2.7.2 Standard American flag sizes.......................................................................... 34
5.2.7.3 VIP helicopters................................................................................................ 34
5.2.8 Marking of foreign aircraft ............................................................................. 34

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5.2.9 Access panel identification ............................................................................. 34
5.2.10 Walkways and honeycomb panels .................................................................. 34
5.2.10.1 Walkways and steps ........................................................................................ 34
5.2.11 Honeycomb panels on airplanes ..................................................................... 34
5.2.12 Marking of loose and jettisonable equipment ................................................. 35
5.2.13 Dinghy (raft) release and flotation controls .................................................... 35
5.2.14 Workmanship .................................................................................................. 35

6. NOTES .................................................................................................................. 35
6.1 Intended use .................................................................................................... 35
6.2 Acquisition requirements ................................................................................ 35
6.3 Associated Data Item Descriptions (DIDs)..................................................... 35
6.4 Toxicity ........................................................................................................... 36
6.4.1 Personnel protective methods ......................................................................... 36
6.5 Subject term (key word) listing....................................................................... 36
6.6 International standardization agreement implementation ............................... 36
6.7 Changes from previous issue .......................................................................... 36

APPENDIX A STANDARD MARKING, EMERGENCY AND HAZARD WARNING

MARKINGS FOR AIRCRAFT

A.1 SCOPE .................................................................................................................. 37

A.1.1 Scope. .............................................................................................................. 37

A.2 APPLICABLE DOCUMENTS ............................................................................ 37

A.2.1 General ............................................................................................................ 37
A.2.2 Government documents. ................................................................................. 37
A.2.2.1 Specifications and standards. .......................................................................... 37
A.2.3 Order of precedence. ....................................................................................... 38

A.3 GENERAL REQUIREMENTS ............................................................................ 38

A.3.1 National insignia. ............................................................................................ 38
A.3.1.1 National insignia design.................................................................................. 38
A.3.1.1.1 Size.................................................................................................................. 38
A.3.1.1.2 Color ............................................................................................................... 38

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A.3.1.1.3 Application...................................................................................................... 39
A.3.1.2 Wing insignia. ................................................................................................. 39
A.3.1.3 Fuselage or hull insignia. ................................................................................ 39
A.3.1.4 Rotary wing aircraft insignia. ......................................................................... 39
A.3.1.5 Decalcomanias. ............................................................................................... 39
A.3.1.6 Decalcomania letter heights. ........................................................................... 40
A.3.1.7 Tactical paint scheme national insignia. ......................................................... 40
A.3.2 Aircraft markings. ........................................................................................... 40

APPENDIX B SERVICING, GROUND HANDLING, HAZARD WARNING MARKINGS,

AND ARMAMENT PLACARD FOR AIRCRAFT

B.1 SCOPE .................................................................................................................. 61

B.1.1 Scope. .............................................................................................................. 61

B.2 APPLICABLE DOCUMENTS ............................................................................ 61

B.2.1 General. ........................................................................................................... 61
B.2.2 Government documents .................................................................................. 61
B.2.2.1 Specifications and standards. .......................................................................... 61
B.2.2.2 Non-Government publications. ....................................................................... 63
B.2.3 Order of precedence. ....................................................................................... 64

B.3 GENERAL REQUIREMENTS ............................................................................ 64

B.3.1 Servicing and precautioning marking. ............................................................ 64
B.3.2 Servicing instructions...................................................................................... 64
B.3.3 Service warning markings............................................................................... 64
B.3.4 Printed information. ........................................................................................ 64
B.3.5 Colors. ............................................................................................................. 64

B.4 DETAIL REQUIREMENTS ................................................................................ 65

B.4.1 Aircraft markings and placard. ....................................................................... 65

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APPENDIX C PAINT SCHEMES AND MARKINGS FOR FIXED WING AIRCRAFT

C.1 SCOPE .................................................................................................................. 81

C.1.1 Scope. .............................................................................................................. 81
C.2 APPLICABLE DOCUMENTS ............................................................................ 81
C.3 GENERAL REQUIREMENTS ............................................................................ 81
C.3.1 Aircraft paint schemes. ................................................................................... 81

APPENDIX D PAINT SCHEMES AND MARKINGS FOR ROTARY WING AIRCRAFT

D.1 SCOPE ................................................................................................................ 150

D.1.1 Scope. ............................................................................................................ 150
D.2 APPLICABLE DOCUMENTS .......................................................................... 150
D.3 GENERAL REQUIREMENTS .......................................................................... 150
D.3.1 Aircraft paint schemes. ................................................................................. 150

APPENDIX E NATIONAL INSIGNIAS FOR FOREIGN AIRCRAFT

E.1 SCOPE ................................................................................................................ 179

E.1.1 Scope. ............................................................................................................ 179
E.2 APPLICABLE DOCUMENTS .......................................................................... 179
E.3 GENERAL REQUIREMENTS .......................................................................... 179
E.3.1 Foreign country national insignias. ............................................................... 179

TABLES

I FED-STD-595 standard colors used on U.S. Navy and Marine Corps aircraft. ..... 6
II Mandatory markings for U.S. Navy and Marine Corps aircraft ........................... 14

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FIGURES

APPENDIX A
A-1 National star insignia. ................................................................................................. 41
A-2 National star insignia on swept wing aircraft. ............................................................ 42
A-3 Arresting hook warning. ............................................................................................. 43
A-4(a) Form of letters and numerals (modified vertical block). ............................................ 44
A-4(b) Form of letters and numerals (open block – to be used for markings 2 inches high
or less) – Continued. ................................................................................................... 45
A-5 Color scheme for helicopter blades............................................................................. 47
A-6 Color scheme for reciprocating single and multi-engine aircraft propellers. ............. 48
A-7 Markings for fire access panel. ................................................................................... 49
A-8 Warning chevron and signs applied adjacent to jet engine intake and exhaust. ......... 50
A-9 Propeller warning stripes and signs. ........................................................................... 51
A-10 Canopy release location. ............................................................................................. 52
A-11 Warning decal. ............................................................................................................ 52
A-12 Helicopter tail boom markings.................................................................................... 53
A-13 Canopy release markings. ........................................................................................... 53
A-14 Tactical paint scheme – rescue arrow and arresting hook markings. ......................... 54
A-15 Tactical paint scheme – engine intake chevrons, access door warning and
branch of service markings. ........................................................................................ 55
A-16 Tactical paint scheme – ejection seat & warning and fuel nozzle port markings. ...... 56
A-17 Area cutout markings. ................................................................................................. 57
A-18 American flag dimensions shall be in accordance with DDD-F-416. ........................ 58
A-19 Geneva red cross. ........................................................................................................ 58
A-20 Placard installation-identification, emergency escape hatch. .................................... 59
A-21 NAVAIR logo ............................................................................................................. 60

APPENDIX B
B-1 Typical symbol dimensioning. .................................................................................... 66
B-2 Armament placard....................................................................................................... 66
B-3 NATO codes and markings-filling.............................................................................. 67
B-4 NATO codes and markings-filling, ground handling and hazards. ............................ 68
B-5 NATO code number cross-reference. ......................................................................... 69

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B-5 NATO code number cross-reference – Continued...................................................... 70

B-6 Typical NATO aircraft servicing markings. ............................................................... 71
B-7 Required markings and symbols. ................................................................................ 72
B-7 Required markings and symbols – Continued. ........................................................... 73
B-7 Required markings and symbols – Continued. ........................................................... 74
B-8 Decalcomania – ground here, international symbol. .................................................. 75
B-9 Samples of ground servicing and hazard markings (size and color). ......................... 76
B-9 Samples of ground servicing and hazard markings (size and color) – Continued. ..... 77
B-9 Samples of ground servicing and hazard markings (size and color) – Continued. ..... 78
B-9 Samples of ground servicing and hazard markings (size and color) – Continued. ..... 79
B-10 Record of finish marking. ........................................................................................... 80

APPENDIX C
C-1 AV-8B tactical. ..................................................................................................... 82
C-1 AV-8B tactical – Continued.................................................................................. 83
C-2 BQM-74C/E. ......................................................................................................... 84
C-2 BQM-74C/E – Continued. .................................................................................... 85
C-3 C-2A. ..................................................................................................................... 86
C-3 C-2A – Continued. ................................................................................................ 87
C-4 C-9B (Navy).......................................................................................................... 88
C-4 C-9B (Navy) – Continued. .................................................................................... 89
C-5 C-9B (Marine)....................................................................................................... 90
C-5 C-9B (Marine) – Continued. ................................................................................. 91
C-6 UC-12B/F/M Navy. .............................................................................................. 92
C-6 UC-12B/F/M Navy – Continued........................................................................... 93
C-7 UC-12B/F/M Navy Force Protection .................................................................... 94
C-7 UC-12B/F/M Navy Force Protection – Continued ............................................... 95
C-8 UC-12B/F/M Marines. .......................................................................................... 96
C-8 UC-12B/F/M Marines – Continued. ..................................................................... 97
C-9 UC-12B/F/M Marines tactical .............................................................................. 98
C-9 UC-12B/F/M Marines tactical – Continued.......................................................... 99
C-10 TC-12B high visibility. ....................................................................................... 100
C-10 TC-12B high visibility – Continued. .................................................................. 101
C-11 C-26D.................................................................................................................. 102

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C-11 C-26D – Continued. ............................................................................................ 103
C-12 C-26D (Navy Force Protection).. ........................................................................ 104
C-12 C-26D (Navy Force Protection).– Continued. .................................................... 105
C-13 C-40..................................................................................................................... 106
C-13 C-40– Continued. ................................................................................................ 107
C-14 KC-130T/J Tactical............................................................................................. 108
C-14 KC-130T/J Tactical – Continued. ....................................................................... 109
C-15 C-130T and KC-130 F/R. ................................................................................... 110
C-15 C-130T and KC-130 F/R – Continued. ............................................................... 111
C-16 E-2C. ................................................................................................................... 112
C-16 E-2C – Continued. .............................................................................................. 113
C-17 E-6A/B. ............................................................................................................... 114
C-17 E-6A/B – Continued. .......................................................................................... 115
C-18 EA-6B tactical..................................................................................................... 116
C-18 EA-6B tactical – Continued. ............................................................................... 117
C-19 F/A-18A/B/C/D tactical. ..................................................................................... 118
C-19 F/A-18A/B/C/D tactical – Continued. ................................................................ 119
C-20 F/A-18E/F and EA-18G tactical. ........................................................................ 120
C-20 F/A-18E/F and EA-18G tactical – Continued..................................................... 121
C-21 F-35 B. ................................................................................................................ 122
C-21 F-35 B – Continued............................................................................................. 123
C-22 F-35 C ................................................................................................................. 124
C-22 F-35 C – Continued............................................................................................. 125
C-23 P-3C. ................................................................................................................... 126
C-23 P-3C – Continued................................................................................................ 127
C-24 EP-3E, UP-3, VP-3 ............................................................................................. 128
C-24 EP-3E, UP-3, VP-3 – Continued......................................................................... 129
C-25 T-2C aircraft marking (high visibility). .............................................................. 130
C-25 T-2C aircraft marking (high visibility) – Continued........................................... 131
C-26 T-6 high visibility. .............................................................................................. 132
C-26 T-6 high visibility – Continued. .......................................................................... 133
C-27 T-34C aircraft marking (high visibility) ............................................................. 134
C-27 T-34C aircraft marking (high visibility) – Continued......................................... 135
C-28 T-38 ..................................................................................................................... 136
C-28 T-38 – Continued. ............................................................................................... 137

xiv

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 MIL-STD-2161C(AS)
CONTENTS
PARAGRAPH PAGE
C-29 T-39G/N high visibility....................................................................................... 138
C-29 T-39G/N high visibility - Continued................................................................... 139
C-30 T-44A high visibility........................................................................................... 140
C-30 T-44A high visibility – Continued. ..................................................................... 141
C-31 T-45A/C aircraft marking (high visibility) ......................................................... 142
C-31 T-45A/C aircraft marking (high visibility) – Continued..................................... 143
C-32 MQ-4C ................................................................................................................ 144
C-32 MQ-4C– Continued. ........................................................................................... 145
C-33 RQ-7B Shadow. .................................................................................................. 146
C-33 RQ-7B Shadow- Continued. ............................................................................... 147
C-34 P-8A (MultiMission Aircraft, MMA)(Proposed) ............................................... 148
C-34 P-8A (MultiMission Aircraft, MMA)(Proposed)– Continued. ........................... 149

APPENDIX D
D-1 AH-1W tactical. .................................................................................................. 151
D-1 AH-1W tactical – Continued. ............................................................................. 152
D-2 AH-1Z. ................................................................................................................ 153
D-2 AH-1Z – Continued. ........................................................................................... 154
D-3 UH-1N tactical. ................................................................................................... 155
D-3 UH-1N tactical – Continued. .............................................................................. 156
D-4 UH-1Y................................................................................................................. 157
D-4 UH-1Y – Continued. ........................................................................................... 158
D-5 HH/UH-1N non-combat SAR ............................................................................. 159
D-5 HH/UH-1N non-combat SAR – Continued. ....................................................... 160
D-6 HH-46E high visibility SAR ............................................................................... 161
D-6 HH-46E high visibility SAR – Continued. ......................................................... 162
D-7 CH-46E tactical................................................................................................... 163
D-7 CH-46E tactical – Continued. ............................................................................. 164
D-8 MH-53E Navy tactical ........................................................................................ 165
D-8 MH-53E Navy tactical – Continued .................................................................. 166
D-9 CH-53E Marine tactical ...................................................................................... 167
D-9 CH-53E Marine tactical – Continued. ............................................................... 168
D-10 TH-57B/C high visibility .................................................................................... 169
D-10 TH-57B/C high visibility – Continued. .............................................................. 170
D-11 SH-60B/F, CH-60S, MH-60 R/S and HH-60H tactical ...................................... 171

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 MIL-STD-2161C(AS)
CONTENTS
PARAGRAPH PAGE
D-11 SH-60B/F, CH-60S, MH-60 R/S and HH-60H tactical – Continued. ................ 172
D-12 SH-60F VIP transport ......................................................................................... 173
D-12 SH-60F VIP transport – Continued..................................................................... 174
D-13 MH-60S and SH-60F Search and Rescue (SAR) ............................................... 175
D-13 MH-60S and SH-60F Search and Rescue (SAR) – Continued. .......................... 176
D-14 MV-22 Tactical ................................................................................................... 177
D-14 MV-22 Tactical – Continued. ............................................................................. 178

APPENDIX E

E-1 National insignia of Portugal (flash and numbers). ............................................... 180

E-2 National insignia of Argentina. .............................................................................. 181
E-3 National insignia of Mexico (flash). ...................................................................... 182
E-4 National insignia of Great Britain. ......................................................................... 183
E-5 National insignia of Canada (roundel) marking I. ................................................. 184
E-6 National insignia of Canada (flash) marking II. .................................................... 185
E-7 National insignia of Netherlands (roundel) marking I. .......................................... 186
E-8 National insignia of Netherlands (flash) marking II. ............................................. 187
E-9 National insignia of France (cocarde) marking I (anchor superimposed when
planes are intended for French Navy.) ................................................................... 188
E-10 National insignia of France (flash) marking II. ..................................................... 189
E-11 National insignia of Australia (roundel) marking I................................................ 190
E-12 National insignia of Australia (flash) marking II................................................... 191
E-13 National insignia of Japan (roundel). ..................................................................... 192
E-14 National insignia of Japan (kanji characters). ........................................................ 193
E-15 National insignia of Uruguay (roundel). ................................................................ 194
E-16 National insignia of Uruguay. ................................................................................ 195
E-17 National insignia of Brazil (star) marking I. .......................................................... 196
E-18 National insignia of Brazil (flash) marking II........................................................ 196
E-19 National insignia of Federal Republic of Germany. .............................................. 197
E-20 National insignia of Federal Republic of Germany. .............................................. 198
E-21 National insignia of Italy (cocarde). ...................................................................... 199
E-22 National insignia of New Zealand (roundel) marking I. ........................................ 200
E-23 National insignia of New Zealand (roundel) marking II. ...................................... 201

CONCLUDING MATERIAL .................................................................................................... 202

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 MIL-STD-2161C(AS)

1. SCOPE

1.1 General. This military standard establishes the requirements for paint schemes and
markings to be applied to the exterior surfaces of U.S. Navy and Marine Corps aircraft, including
those procured for other government agencies and foreign countries under Navy contracts. The
requirements for paint schemes and markings include size, color, and approximate placement
locations, where applicable, as shown in Appendices A – E. This standard also provides a
mechanism to obtain approval for deviation from these requirements.

1.2 Purpose. The purpose of this document is to standardize paint schemes and
application of naval insignia and markings. In addition, this standard provides procedures to
obtain approval for deviations from these requirements.

1.3 Foreign government aircraft. The requirements for the insignia and markings for
foreign government aircraft procured under U.S. Navy contracts are as shown in the appendices
of this document except that the U.S. national insignia must be replaced by that of the purchasing
government, and U.S. Navy insignia must not be applied. Under certain circumstances,
temporary U.S. national insignias will be applied for ferrying the aircraft to the purchasing
country. Foreign insignia and flash insignia for vertical tail surfaces or rudders and markings are
shown in Appendix E. Foreign insignia not shown will be provided to the U.S. Navy contracting
activity by the foreign government procuring the aircraft. Paint schemes for foreign government
aircraft are as specified by that foreign government and, as such, are not contained in this
document.

1.4 Military aircraft used in research projects. The provisions of this standard are not
applicable to military aircraft research projects. The color and marking schemes of such aircraft
are subject to case-by-case approval by the Naval Air Systems Command (AIR 4.1.8).

1.5 Military aircraft attached to designated adversary squadrons. The provisions of this
standard with respect to paint schemes are not applicable to military aircraft attached to
designated adversary squadrons. However, provisions of this standard apply to aircraft attached
to squadrons, which have a secondary mission of adversary training.

1.6 Areas of responsibility.

1.6.1 Cognizant authority. The Naval Air Systems Command (AIR 4.1.8) is the
cognizant authority for all U.S. Navy and Marine Corps aircraft paint schemes and military
markings. Navy or Marine Corps activities requesting a change associated with paint schemes
and military markings must forward the request to AIR 4.1.8 for consideration. AIR 4.1.8 must
evaluate the request and assess its impact as either a minor or a major modification. AIR 4.1.8 is
cognizant of minor modifications and must provide final resolution to this type of change
request. In case of major modifications, AIR 4.1.8 must forward the change request, along with
recommendations, to the Commander Naval Air Forces (CNAF) (N421) for final assessment.

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 MIL-STD-2161C(AS)

1.6.2 Major vs. minor modification. Examples of minor modifications to

this standard include letter markings (such as size, position, etc.), temporary applications,
differences in paint schemes among variants of the same platform, or paint schemes and exterior
marking approvals associated with platforms of similar design but not included specifically in
this standard. Examples of major modifications requiring AIR 4.1.8 consultation with CNAF
(N421) include complete paint scheme conversions involving all assets within a given platform
or new platform designs. Major modifications must be approved by CNAF and their
implementation will be the responsibility of the appropriate Program Executive Officer (PEO).

1.6.3 Squadron/Air Wing markings. Squadron markings or logos, typically applied by

squadron staff on the tail section of aircraft, are the responsibility of the Type Command
(TYCOM) (e.g., AIRLANT, AIRPAC, CNATRA, etc.). AIR 4.1.8 can provide information and
recommendations to the TYCOMs concerning squadron markings.

NOTE: Unless special provisions are made to maintain the integrity of the specialty
coatings for the safe removal of aircraft markings, squadron/Air Wing markings cannot be
applied to aircraft with specialty coatings. Any such provisions must be approved by CNAF
(N421). CNAF Instruction 4790.2 must be consulted for policy regarding specialty coatings.

2. APPLICABLE DOCUMENTS

2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of
this standard. This section does not include documents cited in other sections of this
specification or recommended for additional information or as examples. While every effort has
been made to ensure the completeness of this list, document users are cautioned that they must
meet all specified requirements of documents cited in sections 3, 4, or 5 of this standard, whether
or not they are listed.

2.2 Government documents.

2.2.1 Specifications and standards. The following specifications and standards form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of
these documents are those cited in the solicitation or contract.

FEDERAL STANDARD

FED-STD-595 - Colors Used in Government Procurement

(Color numbers; 11136, 12197, 13538, 14187,
15044, 15045,16081, 16099, 16187, 16440, 16515,
17038, 17043, 17875, 17925,21136, 22190, 23538,
23655, 25237, 26231, 26492, 27925, 28915, 31136,
33538, 35044, 35237, 36081, 36099, 36118, 36170,
36231, 36320, 36375, 36440, 36495, 37038,
37925.)

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 MIL-STD-2161C(AS)

COMMERCIAL ITEM DESCRIPTION

A-A-59485 - Plastic Material, Pressure Sensitive Adhesive, for

Aerospace Identification and Marking

DEPARTMENT OF DEFENSE SPECIFICATIONS

MIL-PRF-23377 - Primer Coatings: Epoxy, High Solids

MIL-C-83413/9 - Connectors and Assemblies, Electrical, Aircraft
Grounding: Decalcomania for Grounding
Receptacle Identification, Decal
MIL-PRF-85285 - Coating: Polyurethane, Aircraft and Support
Equipment
MIL-PRF-85582 - Primer Coatings: Epoxy, Waterborne

DEPARTMENT OF DEFENSE STANDARDS

MIL-STD-7179 - Finishes, Coatings and Sealants, for the Protection

of Aerospace Weapons Systems
MS29525 - Cap-Pressure Fuel Servicing, Nominal 2-1/2 Inch
Diameter, Flush Type
MS90327 - Aircraft Markings, Access Numbering System

(Copies of these documents are available online at http://quicksearch.dla.mil or

https://assist.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue,
Building 4D, Philadelphia, PA 19111-5094.)

2.2.2 Non-Government publications. The following document forms a part of this

document to the extent specified herein. Unless otherwise specified, the issues of this document
are those cited in the solicitation or contract.

AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) INTERNATIONAL

ASTM-D4956 - Standard Specification for Retroreflective Sheeting

for Traffic Control. (DoD adopted)

(Copies of this document are available online at http://www.astm.org or from ASTM

International, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.)

2.3 Order of precedence. In the event of a conflict between the text of this document and
the references cited herein, and unless described as an exception, the text of this document takes
precedence. Exceptions to this order of precedence include aircraft detail specifications, aircraft

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 MIL-STD-2161C(AS)

drawings, and aircraft manuals. Nothing in this document, however, supersedes applicable laws
and regulations unless a specific exemption has been obtained.

3. DEFINITIONS

3.1 Arctic paint scheme. A paint scheme similar to the high visibility paint scheme
except that the top of the fuselage is painted engine gray (FED-STD-595, color number 16081)
instead of insignia white. This scheme is used for spotting downed aircraft against a snow
background.

3.2 High visibility paint scheme. A color scheme consisting of international orange
(FED-STD-595, color number 12197) and insignia white (FED-STD-595, color number 17925)
used to maximize the initial detection range of the aircraft.

3.3 Tactical paint scheme. A color scheme to reduce visual detection comprised of
shades of flat gray with exterior markings applied in a contrasting shade of gray.

4. GENERAL REQUIREMENTS

4.1 Paint schemes and insignia markings. Contractors and all U.S. Navy and Marine
Corps activities (including organizational level maintenance activities) shall apply all insignia
and markings (including identification plates for the aircraft and warning and instruction
markings) in accordance with this standard. The following markings are normally applied by
organizational level activities, but may be applied by Naval Aviation Depots and contractors,
when specified by the Program Managers or Type Commanders:

a. Unit identifier
b. Unit aircraft numbers (MODEX)
c. Station or unit name
d. Squadron markings
e. Radio call markings

4.2 Material.

4.2.1 Finishes. Unless otherwise specified by the Program Manager of a specific

aircraft, all U.S. Navy and Marine Corps aircraft shall be finished in accordance with
MIL-STD-7179. The standard primer coating shall be MIL-PRF-23377 Type I or
MIL-PRF-85582 Type I. MIL-PRF-23377 Type II or MIL-PRF-85582 Type II is required when
the use of tactical grays is specified. The standard topcoat shall be MIL-PRF-85285.

4.2.2 Compatibility. The coating material for insignias and markings shall be the same
material or material compatible with the finish on the surface to be marked.

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 MIL-STD-2161C(AS)

4.2.3 Applicable limitation. Paint or other markings shall not be applied to aircraft or
weapon systems when such application interferes with launching, operation, thermal reflection,
or aerodynamics.

4.2.4 Metal marking instruments. Sharp-pointed metal marking instruments shall not be
used in the layout of insignia or other markings on aircraft or weapon systems.

4.2.5 External finish identification. On all aircraft receiving paint finish coatings on the
exterior surfaces there shall be an identification of the finish system. The identification shall be
located on the starboard side of the fuselage, under or over the horizontal stabilizer, and contain
the following information:

a. Contractor or overhaul activity and location.

b. Month, day, and year of completion of paint application.
c. Identification by military specification number of all paint coating applied to the
exterior of the aircraft.

Lettering shall be a minimum of 1/2 inch (12.7mm) in height. Stencils or approved

decals may be used for this identification. Appendix B, Figure B-10, is a sample of this
identification.

Note: For paint materials not included in a military specification, identification of

material and name of manufacturer shall be listed.

4.2.5.1 Record of finish application. Complete information concerning the coating used,
identified by the applicable military specification, the preparation of the area to be coated, and
the touch-up or replacement procedure for the material used shall be included in the applicable
aircraft structural repair instruction(s) and T/M/S Corrosion Control manual.

4.3 Drawings. On all production contracts, the contractor shall submit for approval to
Commander, Naval Air Systems Command (AIR 4.1.8), via the contracting officer, three-
dimensional drawings, and any revisions thereof, showing paint schemes and the size and
location of the insignia and markings (except those markings specified in 4.1) prescribed in this
standard. Naval Aviation Depots shall submit for approval to Commander, Naval Air Systems
Command (AIR 4.1.8), copies of all paint scheme and marking drawings and revisions thereto.

4.4 Service requirements. Naval Aviation Activities, including Naval Aviation Depots
and organizational level maintenance activities, shall apply other markings that are not required
to be applied by the contractor. In addition, markings duplicating those specified herein, may be
applied to other areas of the aircraft at the discretion of cognizant commands as operational aids,
provided such markings are not prohibited by tactical paint scheme requirements or other
considerations, and do not conflict with the markings prescribed herein in the area selected.

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 MIL-STD-2161C(AS)

4.5 Foreign government aircraft. The exterior colors of aircraft procured for foreign
governments under naval contracts shall be as specified by that foreign government.

4.6 Color and style of marking materials and paint schemes. The color and gloss of
materials shall be as specified in 4.6.1. For non-tactical paint scheme aircraft, the marking
materials and decalcomania used shall be glossy, unless otherwise specified by the Program
Manager. Lusterless marking materials and decalcomania shall be used for aircraft with tactical
paint schemes, unless a deviation is authorized by Naval Air Systems Command (AIR 4.1.8).

4.6.1 Color standard. FED-STD-595 colors shall be used on U.S. Navy and Marine
Corps aircraft, except for specific vendor equivalent colors specified in Appendices C and D.
Table I lists the FED-STD-595 colors used on naval aircraft and weapon systems.

TABLE I. FED-STD-595 standard colors used on U.S. Navy and Marine Corps aircraft.

COLOR GLOSS SEMI-GLOSS LUSTERLESS

Insignia White (Untinted) 17925 27925 37925
Black 17038 37038
Blue 15045
Insignia Blue 15044 35044
Blue-Gray 25237 35237
Insignia Red 11136 21136 31136
International Orange 22190
12197
Orange-Yellow 13538 23538 33538
Gray 16081 36081
16099 36099
36118
36170
16187
26231 36231
36320
36375
16440 36440
26492
36495
16515
Gold 17043
Fluorescent Orange 28915
Light Green 14187
Yellow 23655
Glossy White 17875

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 MIL-STD-2161C(AS)

5. DETAILED REQUIREMENTS

5.1 Aircraft paint schemes. Paint schemes for fixed wing aircraft shall be in accordance
with Appendix C. Paint schemes for rotary wing aircraft shall be in accordance with Appendix
D. This standard does not apply to aircraft attached to designated adversary squadrons. These
aircraft may be painted in an appropriate scheme as determined by that squadron. For aircraft
attached to squadrons that have a secondary or split mission as adversary training, the
requirements of this standard apply. Deviation to this standard shall be submitted to NAVAIR
AIR-4.1.8 for approval.

5.1.1 High visibility color configurations. Aircraft in the training command (excluding
reserve training), target control, and search and rescue (SAR) functions (excluding helicopters in
combat SAR configuration) shall have a high visibility paint scheme in accordance with
Appendices C and D. Additionally, test and evaluation (non-production, prototype, research,
etc.) aircraft shall have a high visibility paint scheme. Transparent areas, antiglare areas, hinges,
openings, screens, and any part of the exhaust trail shall not be topcoated with a high visibility
coating. Request for utilization of high visibility color configuration on other types of aircraft
shall be submitted for approval to the Naval Air Systems Command (AIR 4.1.8) via the
appropriate Chain of Command.

5.1.1.1 Application and color patterns. Current platforms that follow high visibility
schemes are shown in Appendices C & D. For new platforms and platforms not included in this
standard , follow instruction described herein. General principles applicable to the placement of
high visibility paint schemes are as follows:

a. Wing tip markings are placed on the top and bottom of the wings, extending inboard
on the wings about one-third of the length of each wing, but extending inboard no less
than 4 feet or more than 8 feet. Unless specific dimensions are given, the strip shall
terminate at a natural break in the wing contour. Horizontal control surfaces are not
to be coated with high visibility paint.

b. The entire vertical tail section except control surfaces shall be painted to the zone
where the vertical stabilizer flares into the fuselage.

c. All aircraft, except transports and T-6, shall be painted on the bottom and sides on the
front portion of the fuselage starting from the radome, if any, and extending aft and
terminating at a line perpendicular to the forward edge of the front canopy. For
transports, the bottom and the sides on the front portion of the fuselage shall be
painted, starting from aft of the radome and extending aft 12 feet, or aft to a line
perpendicular to the most forward portion of the engines, whichever distance is less.
The customary insignia, markings, solar reflecting finish, antiglare, walkway
materials, rain erosion resistant finish, deicer boots, exhaust trail finish, etc., shall
retain the original color and these areas shall not be overpainted.

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 MIL-STD-2161C(AS)

d. Wing tip tanks on aircraft finished with the high visibility paint scheme shall be
painted international orange, FED-STD-595, color number 12197, except when these
tanks are part of the areas where antiglare or polishing is required.

e. High visibility paint schemes shall not be applied to any transparent or translucent
plastic, metal frames, fittings on windows, or painted nose sections having an area of
less than 2 square feet.

5.1.2 Arctic paint scheme. The high visibility paint scheme may be advantageous for
assisting in spotting downed aircraft against a snow background. Use of this paint scheme,
however, shall be in accordance with 5.1.1. Fuselage markings, such as branch of service, etc.,
shall not be overcoated or overlapped with the high visibility paint scheme. The national
insignia on the fuselage and the wings shall not be overcoated or overlapped by the high
visibility paint scheme. The national insignia, however, may be applied over the high visibility
paint scheme and shall not be altered in its size or location. The remainder of the aircraft shall
retain the paint scheme prescribed for the aircraft type, with the exception that upper surfaces of
the fuselage shall be painted gray, FED-STD-595, color number 16081, in place of insignia
white, FED-STD-595, color number 17925. On helicopters, international orange, FED-STD-
595, color number 12197, shall be applied overall, with the exception of areas requiring
extensive marking. These areas shall retain the basic aircraft paint scheme.

5.1.3 Tactical paint schemes. Tactical paint schemes are used for reduction of initial
detection range and/or to reduce the probability of visual or photographic detection (in flight or
on the ground). Tactical paint scheme patterns are based on optical principles that dictate certain
nonreflective colors, color configurations, and color proportions. Arbitrary application of
markings and color schemes, other than those prescribed in this standard, are prohibited.
Tactical paint schemes are comprised of single or multiple shades of gray or blue-gray with
exterior markings applied in a contrasting lusterless gray/blue-gray color (see 5.2.3).

5.1.3.1 Tactical paint scheme materials. The standard topcoat for the tactical paint
scheme and insignia markings is polyurethane (lusterless) coating conforming to
MIL-PRF-85285. Decals may be used in lieu of paint for insignia and markings that are a
maximum of 4 inches in height provided that they are made of a non-reflective decal material
meeting the gloss and color requirements of the coating system.

5.1.3.2 Tactical paint scheme patterns. Approved tactical paint scheme patterns shall be
in accordance with Appendices C and D.

5.1.3.2.1 Aircraft surfaces. The tactical paint scheme patterns shall be in accordance
with the specific aircraft illustrations included in Appendices C and D. These illustrations,
however, are intended only as guides. Minor variations in pattern are acceptable. Care shall be
taken that proportion and balance of the colors are approximately as shown in the illustrations.
Boundaries between colors shown in the illustrations shall be irregular and fade into each other
with no sharp lines of demarcation. A 6-inch blend line shall be used at all color boundaries.

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 MIL-STD-2161C(AS)

5.1.3.2.2 Bottom surfaces. Most tactical paint schemes use a single color on the
underside of the fuselage, wings, horizontal stabilizer, and control surfaces. The color on the
underside of the aircraft shall be brought up the sides of the fuselage to give the approximate side
view appearance in accordance with the application illustration of Appendices C and D. The
transition from the underside color to the upper surface pattern shall be an irregular, indistinct,
countershaded, 6-inch blend area. A sharp line and any regular repeating pattern (such as a
scallop pattern) may raise the risk of visual detection and compromise the overall effect. On
low-wing aircraft, the color on the bottom of the fuselage shall be brought into the wing root to
meet the color under the wing.

5.1.4 Paint scheme for drones. Drone exterior surfaces shall be painted orange,
FED-STD-595, color number 22190. See Appendix C, Figure C-2 for an example of the drone
paint scheme.

5.1.5 Paint scheme for unmanned aerial vehicles (UAV). Unless otherwise approved by
NAVAIR AIR-4.1.8 or CNAF (N421), UAVs shall have a tactical paint scheme applied to the
exterior surfaces. See Appendix C, Figure C-32 for an example of a UAV paint scheme.

5.1.6 Paint scheme for target aircraft. Exterior surfaces of target aircraft are typically
painted fluorescent orange (FED-STD-595, color number 28915), white or gray. Manufacturers
provide the color specifications for the white and gray colors. Examples of orange-color targets
include BQM-74C, BQM-74E, MA-31, BQM-74F (new replacement for BQM-74E), and BQM-
34S (orange-color body with black wing and vertical tail tips). Examples of targets painted with
colors other than orange include AQM-37C and GQM-163A. Follow manufacturer drawings for
the specific target aircraft colors. Appendix C, Figure C-2 provides the color scheme for BQM-
74C and BQM-74E.

5.1.7 Solar heat reflection. With the exception of where tactical paint schemes are
employed, the upper surfaces of the fuselage of all land-based cargo, transport, and utility planes
shall be painted insignia white, FED-STD-595, color number 17925. The white color shall begin
at the top, forward edge of the pilot’s enclosure, extending aft to include the vertical stabilizer
and elevator, and extending down each side of the fuselage to the bottom of the windows, in
accordance with Appendices C and D. Aircraft used in a VIP transport or staff capacity may
employ a stripe below the white area that runs forward to aft down the side of the fuselage and a
chevron on the nacelles for decorative purposes.

5.1.8 Antiglare. On all pilot-operated aircraft, nonspecular (lusterless) paint shall be

employed on all airframe surfaces that may produce glare in the pilot or copilot’s eyes, or induce
eyestrain due to excessive brightness. These areas shall be painted nonspecular (lusterless)
black, FED-STD-595, color number 37038, with the exception of aircraft painted with tactical
paint schemes. Aircraft painted with tactical paint schemes shall use nonspecular gray, FED-
STD-595, color number 36320, or blue, FED-STD-595, color number 35237.

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5.1.9 Glass fiber reinforced plastic assemblies. The color of assemblies fabricated of
glass-fiber reinforced plastic (such as radomes, radio antenna housings, noses, fairings, wing
tips, and intake ducts) for which rain-erosion-protective finishes are required, shall match the
color of adjacent surfaces.

5.1.10 Landing gear.

5.1.10.1 Fixed landing gear. Fixed landing gear shall be painted to match the prescribed
color scheme of the particular aircraft.

5.1.10.2 Retractable landing gear. Retractable landing gear, wheel well areas, wheel
assemblies, inner surfaces of landing gear well covers, hydroskis (including the strut and
trunnion doors) and nose gear doors (auxiliary, including the strut door), etc., shall be colored
insignia white, FED-STD-595, color number 17925. The edges of the landing gear door shall be
painted insignia red, FED-STD-595, color number 11136, without overcoating the white. The
outer surfaces of the well covers shall be painted to match the prescribed color scheme of the
aircraft.

5.1.11 Speed brakes, wing flaps, etc. Interior surfaces of speed brakes and wing flaps
shall be colored insignia red, FED-STD-595, color number 11136. Exterior surfaces of speed
brakes and wing flaps shall be colored to match the prescribed color scheme of the aircraft.
Wing flap areas, which are covered by the wing when they are in the retracted position, shall be
colored insignia red, FED-STD-595, color number 11136. Conformance to these requirements,
especially with respect to aircraft painted with a tactical paint scheme, shall be determined on a
case-by-case basis by the aircraft Program Manager in conjunction with the Naval Air Systems
Command (AIR 4.1.8). In case of hostility, fleet commanders have the authority to overpaint
these red areas for tactical advantage.

5.1.12 Wing leading edge slats. The interior (lower) surface and inboard end of wing
leading edge slats, and the wing area covered by the slat, when in a fully retracted position, shall
be colored insignia red, FED-STD-595, color number 11136, with the exception of new aircraft
to be delivered with a tactical paint scheme. On these new aircraft, the interior surface covering
color shall be determined by the Program Manager in conjunction with the Naval Air Systems
Command (AIR 4.1.8). Exterior surfaces of wing leading edge slats shall be colored to match
the required color scheme of the aircraft (see the applicable figures in Appendices C and D).

5.1.13 Walkways and steps. Where anti-skid material is applied, the color shall be as
follows: for conventionally painted aircraft, the color shall be gray, FED-STD-595, color number
36231, or black, FED-STD-595, color number 37038. For aircraft with tactical paint schemes,
the color shall match the color of adjacent areas.

5.1.14 External stores (including ordnance). External fuel tanks, pylons, rocket
launchers, missiles, pods, and other mounted equipment shall be colored to conform to the
aircraft paint scheme. For tactical paint schemes, gray, FED-STD-595, color number 36375,

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 MIL-STD-2161C(AS)

shall be used, with the exception of external stores peculiar to the SH-60 aircraft. For these
items, the color shall be gray, FED-STD-595, color number 36495. All other paint schemes shall
use FED-STD-595, color number 17925. Stores used on multiple aircraft with different color
schemes shall be painted to match the primary user. If temperature problems occur, the use of a
lighter shade of gray is acceptable upon approval of the Naval Air Systems Command (AIR
4.1.8). Safety color-coded markings shall be applied as specified in other directives.

5.1.15 Radomes, antennae and antennae covers. Blade type antennae, antenna mast,
antennae covers, and radomes shall be painted to match the color of adjacent areas, except where
prohibited by manufacturer’s direction.

5.1.16 Helicopter blades, hubs, transmissions and rotor mechanisms.

5.1.16.1 Rotor blades. Main and tail rotor blades shall be painted black, FED-STD-595
color number 37038, except when the tactical paint scheme is utilized. When the tactical paint
scheme is utilized, the color of the rotor blades shall be black, FED-STD-595 color number
37038, or gray. The gray color will depend on the aircraft model and shall match the tactical
color used on the upper surface of the aircraft. Marking of the main and tail rotor blades shall be
in accordance with 5.2.2.10.3.

5.1.16.2 Hubs of helicopters. Helicopter hubs shall be painted black, FED-STD-595,

color number 37038, except aircraft painted with the tactical paint scheme. For aircraft painted
with tactical paint scheme, the color of the hubs shall match the tactical paint scheme.

5.1.16.3 Transmission and rotor mechanisms of helicopters. Helicopter transmissions

and rotor mechanisms, other than blades and hubs, shall be painted black, FED-STD-595, color
number 37038, with the exception of aircraft painted with a tactical paint scheme. For aircraft
with a tactical paint scheme, the color of the transmission and rotor mechanisms shall match the
tactical paint scheme.

Note: When the same model/series aircraft is used in both the U.S. Navy and Marine
Corps and each service requires a different paint scheme, the transmission and rotor mechanisms
(including blades) on all aircraft for that branch of service shall be painted black, FED-STD-595,
color number 37038, or gray, respectively. The gray color number will depend on the aircraft
model and shall match the tactical color used on the upper surface of the aircraft. The decision
on which color to use will be based on which service has the most aircraft of this model series.

5.1.17 Jet air intake ducts. The color of the adjacent aircraft exterior shall be carried
around the lip of the duct and into the duct approximately 6 inches (except for the chevrons).
All remaining interior surfaces of the duct shall be painted insignia white, FED-STD-595, color
number 17925.

5.1.18 Propeller assemblies.

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5.1.18.1 Blades. Blades shall be painted black, FED-STD-595, color number 37038,
with the exception of aircraft with a tactical paint scheme. For aircraft with a tactical paint
scheme, the color of the blades shall match the tactical paint scheme. Markings shall be as
specified in 5.2.2.10.3 and 5.2.2.10.3.5.

5.1.18.2 Spinners. Spinners shall be painted black, FED-STD-595, color number 37038,
with the exception of aircraft with the tactical paint scheme. For aircraft with a tactical paint
scheme, the color of the spinners shall match the tactical paint scheme.

5.1.18.3 Hubs and domes. Hubs and domes shall be painted black, FED-STD-595, color
number 37038, with the exception of aircraft with tactical paint schemes. For aircraft with a
tactical paint scheme, the color of hubs and domes shall match the tactical paint scheme.

5.1.19 Engine cowling interiors. The interior of engine cowlings shall be painted gray,
FED-STD-595, color number 16440, unless a different color is specified by the engine technical
manual for the specific aircraft.

5.2 Aircraft exterior markings. Exterior markings for fixed wing aircraft shall be in
accordance with Appendix C. Exterior markings for rotary wing aircraft shall be in accordance
with Appendix D. Certain marking provisions of this standard are subject to international
standardization agreements and shall not be changed, except under emergency conditions,
without prior coordination with the North Atlantic Treaty Organization (NATO). Unless
otherwise specified, the height of all characters shall be chosen from the following sizes: 12, 16,
20, 24, 30 or 36 inches.

5.2.1 Identification marking. Identification markings for all U.S. Navy and Marine
Corps aircraft, with the exception of 5.2.1.1.3 through 5.2.1.1.6, shall be in accordance with 5.2.2
for mandatory markings and 5.2.6 for optional markings. Guidance is provided in 5.2.3 for
markings applied to aircraft with the tactical paint schemes.

5.2.1.1 Letter and numeral (character) construction. All letters and numerals (characters)
shall be constructed in a modified vertical block form with the exception that open block
lettering can be used for markings of 2 inches or less (see Appendix A, Figure A-4). All
characters shall be uniform in shape and size. The width of the characters, excluding the dash (-)
and the letters G, A, M and W, shall be 75 percent of the height of the character. The dash shall
be constructed in accordance with Appendix A, Figure A-4. The width of letters A and M shall
be 92 percent of its height. The width of the letter W shall be 108 percent of its height. The
width of the letter G, including the overhang on its right side, shall be 83 percent of its height.
All overhangs on letters C, G, S and numerals 2, 3, 4, and 9 shall be 1/12 of the character’s
height. The height of characters shall be a minimum of one inch. In areas where this is not
possible due to space limitation, the height of the characters may be reduced to 1/2 inch.
Decalcomania conforming to A-A-59485 may be used for application of markings. Only small
maintenance marking may be applied by decal to supersonic aircraft and in areas where it may
become dislodged and cause foreign object damage (FOD). Decals used shall perform as well or

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 MIL-STD-2161C(AS)

better than the standard topcoat in appearance and durability. Decals shall not be applied where
they may be deleterious to the surface to which they are applied. Decals shall not be applied
over brazier head rivets.

5.2.1.1.1 Fixed wing aircraft. The typical identification markings for fixed wing aircraft
shall be in accordance with applicable figures of Appendix C.

5.2.1.1.2 Rotary wing aircraft (helicopters). The typical identification markings for
rotary wing aircraft shall be in accordance with applicable figures of Appendix D.

5.2.1.1.3 Research aircraft. The markings of military aircraft used for research projects
are subject to Naval Air Systems Command (AIR 4.1.8) approval in each case.

5.2.1.1.4 Experimental aircraft. Experimental aircraft shall be marked as specified in

Appendix C and D, insofar as practicable. In addition, the marking “U.S. NAVY” shall be
applied on the upper surface of the right wing and on the bottom surface of the left wing, in a
similar location to the national insignia on the opposite wing. The height of the letters shall be
the largest possible size that can be accommodated on the aircraft, selected from 5.2.

5.2.1.1.5 Target aircraft. Target aircraft shall have the national insignia applied, in
accordance with Appendix A, and shall be marked as specified in Appendices C and D insofar as
is practicable. The size of the letters and numerals shall be as specified in Appendices C and D.
If there are space limitations, the size may be reduced proportionately.

Target aircraft shall also have the word “TARGET” applied along the port side of the
forward and aft sections of the fuselage, the starboard side of the midsection of the fuselage, the
top side of each wing assembly, inboard from the wing tips, the top side of each horizontal tail
surface (as applicable), inboard from the tips, and the starboard side of each vertical tail surface.

5.2.1.1.6 Test and evaluation (T&E) aircraft. Aircraft assigned to T&E activities shall
comply with the provisions of this standard to the extent that is practical. Deviations to meet
specific test objectives or safety of flight require Naval Air Systems Command (AIR 4.1.8)
approval.

5.2.1.1.7 Unmanned Aerial Vehicles (UAV). Unless otherwise approved by NAVAIR

AIR-4.1.8 or CNAF (N421), the typical identification markings for Unmanned Aerial Vehicles
shall be as shown on Figure C-32.

5.2.1.1.8 United States Naval Test Pilot School (USNTPS) Aircraft. These aircraft shall
comply with the provisions of this standard to the extent that is practical. USNTPS uses a wide
array of rotary and fixed wing aircraft to perform its function. This standard does not cover the
USNTPS paint scheme for each specific USNTPS aircraft. The intent, however, is to provide
general guidance for the "typical" USNTPS scheme. USNTPS aircraft typically maintain the
tactical paint scheme background color, as shown in Appendices C and D, or use a glossy white

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 MIL-STD-2161C(AS)

(FED-STD-595 color 17925) background. For fixed wing USNTPS aircraft, a gloss orange-red
(FED-STD-595 color 12197) stripe is applied along the length of the body, including the vertical
aft structure with the "USNTSP" marking applied inside the stripe on the vertical aft structure.
The USNTSP marking is either gloss black (FED-STD-595 color 17038) or gloss white (FED-
STD-595 color 17925). For rotary wing aircraft, the orange-red stripe is typically applied on the
main body of the aircraft and the vertical aft structure. Appendix C provides an example of a T-
38A aircraft painted with the USNTPS paint scheme. USNTPS provides guidance for the
specific paint scheme for the aircraft under its cognizance.

5.2.2 Mandatory markings for U.S. Navy and Marine Corps aircraft. The markings and
insignia contained in this section shall be applied to all U.S. Navy and Marine Corps aircraft, as
specified herein. Instructions concerning the size and color of markings and insignia for tactical
paint schemes are specified in 5.2.3. Appendix A reflects specific instructions, dimensions, etc.,
for the proper application of these markings and insignia. Table II lists the standard markings
and insignia for all aircraft.

TABLE II. Mandatory markings for U.S. Navy and Marine Corps aircraft.

GENERAL LOCATION
ITEM FIXED WING ROTARY WING
National star Wing and fuselage Fuselage
Branch of service Fuselage (carrier based) Fuselage
Wing and fuselage (other)
Model designation Fuselage Fuselage
Airplane serial number Fuselage Fuselage
(BUNO)
Unit aircraft number Fuselage Fuselage
(MODEX)
Unit identifier Vertical stabilizer Aft pylon or upper tail boom
Station or unit name Vertical stabilizer As specified
Call numbers Vertical stabilizer Aft pylon or upper tail boom
Warning markings As specified As specified

5.2.2.1 Changes. Dimensioned drawings, showing the size and location of the insignia
and markings applied to various types of aircraft, are prepared in accordance with applicable
Naval Air Systems Command (AIR 4.1.8) instructions. Any changes proposed to these insignia
and markings shall be coordinated with the Naval Aviation Depot (NADEP) that prepared the
service drawing and the Naval Air Warfare Center Aircraft Division, Systems Requirements
Department (Code 4L8000B120-3) Lakehurst, NJ, 08733-5100. Approval shall be obtained

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 MIL-STD-2161C(AS)

from the Naval Air Systems Command (AIR 4.1.8) and may require CNAF (N421) approval
depending on the magnitude of the change.

5.2.2.2 Application. All identifying information, except the national insignia, on the
under surface of the wing shall be applied so that it can be read from left to right when standing
in front of, and facing, the aircraft. On swept-back and variable sweep wings, all letters and
numerals shall be applied symmetrically along the 50 percent constant chord line, as is required
for application of the national insignia. Insofar as is practicable, all letters and numerals shall be
positioned on the fuselage and vertical tail surface so as to be perpendicular to the fuselage
reference line.

5.2.2.3 National star insignia. The national star insignia shall be applied to all aircraft as
delineated in Appendix A, Figure A-1.

5.2.2.4 Branch of service marking. The branch of service marking shall be applied to all
aircraft. On aircraft operated by the U.S. Navy and Naval Reserve, the branch of service
marking shall consist of “NAVY” or, on cargo/transport aircraft, “UNITED STATES NAVY,”
as specified in Appendices C and D. On aircraft operated by the U.S. Marine Corps and Marine
Corps Air Reserve, the branch of service marking shall consist of the word “MARINES” or, on
cargo/transport aircraft “UNITED STATES MARINES”, as specified in Appendices C and D.
On aircraft operated jointly by the U.S. Navy and Marine Corps, and/or their Reserve
components, the branch of service marking shall consist of “NAVY.” For tactical paint scheme
aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.2.4.1 Size. The size of the lettering of the branch of service marking shall be as large
as possible on the aircraft. The height of the letters shall be selected from 5.2. Special sizing
instructions for tactical paint scheme markings are contained in 5.2.3, and Appendix A, Figure
A-15. The last marking shown on Figure A-15 provides an example of the branch of service
marking.

5.2.2.4.2 Location. The location of the branch of service marking shall be both sides of
the fuselage, just forward of the empennage (aircraft tail) for all fixed and rotary wing aircraft
and on the underside of the left wing for non-carrier based fixed wing aircraft.

5.2.2.5 Model designation and bureau airplane serial number (BUNO). BUNO shall be
applied just below the model designation, in accordance with Appendices C and D. For tactical
paint schemes, the color requirements specified in 5.2.3 shall apply.

5.2.2.5.1 Location. BUNO shall be centrally located on both sides of the fuselage under
the horizontal stabilizer in the position shown in Appendices C and D. For transport (VR)
aircraft having twin booms, these markings shall be centrally located on the outboard side of
each main boom, between the insignia and the horizontal stabilizer. The BUNO shall be
symmetrically located 2 inches below the model designation.

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5.2.2.5.2 Size. Model designation numerals and letters shall be 2-inches high and the
BUNO shall be 4-inches high.

5.2.2.6 Unit aircraft number (MODEX). The unit aircraft number shall consist of
numbers only, to designate the number of the airplane within the unit. Numbers shall be applied
in black (FED-STD-595, color number 17038) for non-tactical paint scheme aircraft, and
contrasting gray (color number 35237, 37038, or 36375) or black (color number 37038) for
tactical paint scheme aircraft. See Appendices C and D for guidance to current aircraft.

5.2.2.6.1 Location. The unit aircraft number shall be located on the nose of the aircraft
and on both sides of the fuselage. The unit aircraft number may also be applied to the vertical
tail and wing flaps.

5.2.2.6.2 Size. Unit aircraft numbers shall be a minimum of 10-inches high for tactical
paint schemes and for other aircraft shall be the largest possible of the sizes specified in 5.2, not
to exceed 50 percent of the height of the projection of the fuselage side at the point of
application.

5.2.2.7 Unit identifier. The unit identifier is used on non shore-based (i.e. at sea
deployment) aircraft squadrons only. The unit identifier shall consist of letters only, to designate
the squadron or group of the airplane (letters are assigned in accordance with CNAF directives).
For tactical paint schemes, the color requirements specified in 5.2.3 shall apply.

5.2.2.7.1 Location. The unit identifier shall be applied to both sides of the vertical tail
surfaces centered on the vertical surfaces. On multiple tail surfaces, the marking shall appear on
the outboard sides only.

5.2.2.7.2 Size. Letters shall be a minimum of 10-inches high and shall be the largest
possible specified in 5.2. In case of double letters, the width of each letter may be reduced to
accommodate the letters to the shape of the tail surface, retaining maximum clarity, visibility,
and symmetry. The size of letters for tactical paint schemes is as specified in 5.2.3.

5.2.2.8 Station or unit name. Station or unit name marking is applied to shore-based
aircraft only. On shore-based aircraft, where no unit identifiers are assigned, this marking shall
consist of the name of the air station, e.g., North Island, Corpus Christi, etc., or abbreviation of
the unit’s title, e.g., AIRON-81, employed in lieu of the unit identifier. For tactical paint
schemes, the color requirements specified in 5.2.3 shall apply.

5.2.2.8.1 Location. On shore-based aircraft, the station or unit name is used instead of
the unit identifier and shall be applied on the vertical tail surfaces in the same locations specified
in Appendices C and D for the unit identifier.

5.2.2.8.2 Size. The size of the letters shall be such that the station or unit name can be
accommodated on the vertical tail surfaces in the specified location. If necessary due to space

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 MIL-STD-2161C(AS)

limitations, the station or unit name may be divided to occupy two lines. If two lines are used for
station names, the dash shall be omitted and the letters on the second line shall be centered below
those on the top line.

5.2.2.9 Call numbers. Aircraft shall have a call number painted on each side of the
vertical stabilizer surface or on each outboard side, as applicable. The call numbers shall consist
of at least the last four numbers of the bureau number. Arabic numbers shall be used when
applying call numbers. For tactical paint schemes, the requirements specified in 5.2.3 shall
apply.

5.2.2.9.1 Location. The call numbers shall be applied to both sides of the vertical
stabilizer and rudder assembly, or to each outboard side, as applicable. On rotary wing aircraft,
or if space limitations do not permit on other aircraft, these numbers shall be applied aft along
the fuselage, or aft along each side of the tail boom, as applicable.

5.2.2.9.2 Size. The height of the numbers shall be the largest size possible of the sizes
listed in 5.2. Under no circumstances shall the height of the characters be less than 12 inches
unless space prohibits application of 12-inch numbers. The numbers or designators shall be
discernible from a distance of 50 yards.

5.2.2.10 Mandatory safety markings. Mandatory standard safety markings are as

specified in 5.2.2.10.1 thru 5.2.2.10.6.14.6. For tactical paint schemes, refer to 5.2.3 for special
instructions.

5.2.2.10.1 Jet engine intake warning chevrons and signs. The areas of the leading edge
of the wing, the fuselage, or the nacelle or pod, or combination thereof, that are adjacent to the
sides of a jet engine intake, shall be marked with warning chevrons and signs, as specified in the
following subparagraphs. Not applicable to turboprop aircraft.

5.2.2.10.1.1 Application. The chevrons shall be applied such that the ends of their outer
sides contact the edge of the intake at points that are three-quarters of the diameter, or three-
quarters of the short axis, of the intake port. The outer points of the chevrons shall be located at
a distance of 4-feet outboard along the leading edge of the wing, or forward or aft, if applied on
the fuselage, or aft, if applied on the nacelle or pod, from the center of the intake. The chevrons
shall be 3 inches in width and shall be marked in insignia red, FED-STD-595, color number
11136, with the exception of tactical paint scheme aircraft. Superimposed on one side of a
chevron shall be the word “JET” and on the other side the word “INTAKE” in insignia white,
FED-STD-595, color number 17925 (see Appendix A, Figure A-8). The letters shall be 2 inches
in height. The word “DANGER” (with an arrow directed at the point of the chevron, see
Appendix A, Figure A-8) shall be applied along the leading edge of the wing, or on the fuselage,
nacelle, or pod, as applicable. The letters and arrows shall be insignia red, FED-STD-595, color
number 11136, and shall be superimposed on a stripe of insignia white, FED-STD-595, color
number 17925, 3 inches in width. The height of the letters and length of the arrows shall be 2

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inches. Aircraft painted with tactical paint schemes shall comply with the color requirements
specified in 5.2.3.

5.2.2.10.1.2 Variations. The dimensions specified in 5.2.2.10.1.1 shall be adhered to in

general. They may be varied, and the word “DANGER” (with the arrows pointing to the edge of
the intake) may be applied within the V of the chevrons if there are space limitations or other
considerations. The general outline and appearance of the warning chevrons shall conform to
Appendix A, Figure A-8.

5.2.2.10.2 Jet engine blast warning. The areas of the fuselage, nacelle or pod, or
combination thereof, which are adjacent to the sides of a jet engine exhaust shall be marked with
the words “Beware of blast” as shown in Appendix A, Figure A-8. Not applicable to turboprop
aircraft.

5.2.2.10.3 Propeller, rotor, and turbine safety markings. Application of safety markings
to statically balanced propellers and rotor blades shall be limited to new blades or to overhauled
blades, in accordance with 5.2.2.10.3.1.3. Only lusterless colors shall be used for propellers and
rotor blade identification danger zone marking, for antiglare purposes, unless otherwise noted
herein. Letters and numerals shall be 1 inch in height. If there are space limitations, letters and
numerals may be reduced in height to 1/2 inch. For tactical paint schemes, the use of
identification stripes on rotor blades is dependent upon whether they can be overpainted by field
units. If the provisions of 5.2.2.10.3.1.3 can be met, identification stripes shall be used. On all
other rotor blades, identification stripes shall be eliminated.

5.2.2.10.3.1 Main rotor blades.

5.2.2.10.3.1.1 Matched sets. For matched sets of main rotor blades, an individual
identification stripe shall be painted on both sides of the blade from the tip to 2 inches from the
tip. This stripe shall be insignia white, FED-STD-595, color number 17925, for one blade,
insignia red, FED-STD-595, color number 11136, for the second blade, and light green, FED-
STD-595, color number 14187, for the third blade. In addition, orange-yellow, FED-STD-595,
color number 33538, warning stripes shall be applied inboard of the 2-inch stripe on both of the
blades, and shall extend from the line 2 inches from the tip to a line 8 inches from the tip (see
Appendix A, Figure A-5). FOR TACTICAL PAINT SCHEMES, 5.2.2.10.3 SHALL APPLY.

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5.2.2.10.3.1.2 Unmatched sets. For unmatched sets of main rotor blades, orange-yellow
warning stripes, FED-STD-595, color number 33538, shall be applied to both sides of the blades
from the tip to 6 inches from the tip (see Appendix A, Figure A-5). FOR TACTICAL PAINT
SCHEMES, 5.2.2.10.3 SHALL APPLY.

5.2.2.10.3.1.3 Static balance - preservation and maintenance. Paint or other marking,

when applied to propellers, rotors, or statically balanced control surfaces for antiglare or
protective purposes, shall be applied only by the manufacturer or an authorized facility, except
when authorized by the Type Commanders. Between overhauls, when required, marking and
finishes shall be retained by a light maintenance touch-up. Touch-up shall be applied to all
surfaces in proportionate amounts for retention of proper balance.

5.2.2.10.3.1.4 Classification numbers. Classification numbers shall be stenciled on the

main rotor blades of all helicopters by any facility authorized to balance or alter the blade. These
numbers shall consist of three parts as follows:

a. The first shall be the weight in pounds of the blade, expressed in decimal form.

b. The second shall be the distance in inches from the center of rotation to the center of
gravity of the blade.

c. The third shall be the distance in percent mean aerodynamic chord (MAC) from the
leading edge of the blade to the center of gravity of the blade clockwise. For
example: 57.2-75.5-32.4, when the blade has a weight of 57.2 pounds with the center
of gravity 75.5 inches from the center of rotation and with the chordwise center of
gravity at 32.4 percent MAC.

Stenciling, 1/2-inch to 1-inch in height shall be accomplished with a paint that contrasts
well with the color of the blade. The classification numbers information shall be marked on the
flat surface on the groundside of each blade at the inboard or butt end of the main rotor blade.

5.2.2.10.3.2 Tail rotor blades. Tail rotor blades shall be finished as shown in Appendix
A, Figure A-5, starting from the tip and on both sides of the blade, as follows:

a. A 6-inch wide band of insignia red, FED-STD-595, color number 11136.

b. A 6-inch wide band of insignia white, FED-STD-595, color number 17925.

c. A 6-inch wide band of insignia red, FED-STD-595, color number 11136.

d. A nonspecular black band, FED-STD-595, color number 37038, to within 6 inches of

the hub.

e. A 6-inch wide band of insignia red, FED-STD-595, color number 11136.

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Note:

FOR TACTICAL PAINT SCHEMES, 5.2.2.10.3 SHALL APPLY.

5.2.2.10.3.3 Helicopter tail boom - warning marking. For helicopters having tail rotor
blade(s) revolving in the vertical plane, a warning sign shall be painted on both sides of the tail
boom, as shown in Appendix A, Figure A-12. This shall consist of a 33-inch wide band orange-
yellow, FED-STD-595, color number 13538, encircling the tail boom. Centrally superimposed
on this band shall be applied an insignia red arrow, FED-STD-595, color number 11136, of
appropriate size, with the arrow pointing aft as indicated in Appendix A, Figure A-12. Above
the arrow shall appear the word “DANGER” and below the arrow shall appear the words “KEEP
AWAY.” The letters shall be black, FED-STD-595, color number 17038, and shall be
approximately 2-inches in height. For tactical paint schemes, the color requirements specified in
5.2.3 shall apply.

5.2.2.10.3.4 Helicopter tail rotor - guards and stabilizers. On helicopters with tail rotor
guards and/or stabilizers, the tail rotor guard and/or stabilizer shall have warning markings
applied to prevent ground personnel from accidentally running into these components. The
markings shall consist of 2-inch wide alternating stripes of orange-yellow, FED-STD-595, color
number 13538, and bright red, FED-STD-595, color number 11136. For tactical paint schemes,
the color requirements specified in 5.2.3 shall apply.

5.2.2.10.3.5 Propeller blades - warning markings. Unless otherwise approved by

NAVAIR AIR-4.1.8 or CNAF (N421), blades shall be painted as shown in Appendix A, Figure
A-6. Propeller blades on multi-engine planes, including blades used on aircraft using a tactical
paint scheme, shall be painted on both sides from the tip to 3 inches from the tip with insignia
white, FED-STD-595, color number 17925, followed by a 6-inch strip of insignia red, FED-
STD-595, color number 11136, followed by another 3-inch strip of insignia white, FED-STD-
595, color number 17925. The remainder of the blade shall be colored black, FED-STD-595,
color number 37038. The black may be eliminated on blades where both the following
conditions are met:

a. Corrosion protection is not required and

b. The blades are so situated as to produce no brightness in the pilot’s or copilot’s eyes
(in cases where the blades rotate in a plane aft of the pilot’s seat).

If the blades are so situated as to produce glare or excessive brightness in the pilot’s or
copilot’s eyes, the insignia red, FED-STD-595, color number 11136, and insignia white,
FED-STD-595, color number 17925, shall be replaced by red, FED-STD-595, color number
31136, and white, FED-STD-595, color number 37925, respectively, on the rear face of the
blades only. Propeller blades on single engine planes shall be painted on the front side in the
same manner as for multi-engine blades; the rear face, however, shall be colored black,

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FED-STD-595, color number 37038, with a 4-inch band of orange-yellow, FED-STD-595 color
number 33538, at the tip for blades of less than 15 feet basic diameter or in a 6-inch band,
orange-yellow, FED-STD-595, color number 33538, for larger diameter blades.

5.2.2.10.3.6 Fuselage propeller - warning stripe and signs. That area of the fuselage
which is in the plane of the propeller path shall be marked with an insignia red stripe, FED-STD-
595, color number 11136, 3-inches wide extending completely around the fuselage, as shown in
Appendix A, Figure A-9. For aircraft having a solar reflective white paint, FED-STD-595 color
number 17925, on the top portion of the fuselage, the stripe shall only encompass the portion
around the fuselage that excludes this area. The word “Propeller” reading vertically from top to
bottom, on both sides, shall be superimposed on this stripe in insignia white, FED-STD-595,
color number 17925, letters 2 inches in height, at sufficiently frequent intervals to indicate the
dangerous area. The signs “DANGER” and “DANGER” shall be applied perpendicular to and
centered with respect to the word “PROPELLER,” one sign on each side thereof, with the arrow
pointing toward the stripe. The letters and arrows shall be insignia red, FED-STD-595, color
number 11136 and shall be superimposed on a stripe of white, FED-STD-595, color number
17925, 3 inches in width. The height of the letters and length of the arrows shall be 2 inches and
4 inches respectively. For tactical paint schemes, the color requirements specified in 5.2.3 shall
apply.

5.2.2.10.3.7 Staggered engines. On aircraft having engines staggered in the wing, a

marking similar to that described in 5.2.2.10.3.6 shall also be placed on the cowling of the next
inboard engine to mark the plane of rotation of the propeller disk.

5.2.2.10.4 Arresting hooks. Arresting hooks shall be painted with gloss black, FED-
STD-595, color number 17038, and insignia white, FED-STD-595, color number 17925, in
alternate bands 4-inches wide, to produce maximum visibility. For tactical paint schemes, the
arresting hook shall be painted in the surrounding gray/blue paint scheme. Paint shall not be
applied to the arresting hook point.

5.2.2.10.4.1 Arresting hook warning marking. For aircraft having arresting hooks, a
warning sign shall be painted on both sides of the fuselage (Appendix A, Figure A-3, and A-14)
and shall be located in proximity to the hook point when in the retracted position. The marking
shall be clearly visible to maintenance personnel.

5.2.2.10.5 Loose and jettisonable equipment. The following loose equipment shall be
marked in a contrasting color, using a stencil or other suitable marking, with the call numbers:
life rafts, tool kits peculiar to the airplanes, aircraft covers (engine covers, dust covers, etc.).

5.2.2.10.6 Identification and markings of emergency escape system. All exits to be used
in an emergency shall be identified by the words “EMERGENCY EXIT, RESCUE,
AUXILIARY EXIT” or other appropriate wording, followed by applicable instructions or
symbols. Painted insignia, letters, and markings shall be visible in the dark. Painting shall be

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 MIL-STD-2161C(AS)

compatible with finishes applied to adjacent surfaces. Decals shall conform to the requirements
specified herein and shall be edge-sealed with a clear finish (see Appendix A, Figure A-20).

5.2.2.10.6.1 Application. All surfaces to be lettered shall be prepared to ensure good

contrast between lettering and background. Standard application shall be black, FED-STD-595,
color number 17038, letters on an orange-yellow, FED-STD-595, color number 13538
background. In some applications, orange-yellow, FED-STD-595, color number 13538, lettering
on a black, FED-STD-595, color number 17038, background shall be specified. Other color
combinations shall not be used without approval of the procuring activity. The background
border shall extend 1/2 inch beyond the lettering. For tactical paint scheme aircraft the color
requirements specified in 5.2.3 shall apply.

5.2.2.10.6.2 Location. Lettering and marking of the emergency escape system shall be
placed so as to be easily readable.

5.2.2.10.6.3 Lettering size. All lettering shall be gothic type. Exit release signs shall
have 2-inch high lettering. The lettering of instruction shall be at least 1-inch high.

5.2.2.10.6.4 Cutout area marking. Each area of the aircraft intended to be cutout for
emergency rescue shall be marked with the wording “CUT HERE FOR EMERGENCY
RESCUE” and corner markings at the limits of the cutout area (see Appendix A, Figure A-17).
The horizontal and vertical lines of the corner marking shall be 3-inches long and 1-inch wide.
This marking scheme shall be applied to the interior and exterior of the aircraft at the intended
cutout point. The lettering shall be a minimum of 2 inches in height.

5.2.2.10.6.5 Exit control lever markings. Handles and levers used to actuate doors on
hatches shall be identified by alternating orange-yellow, FED-STD-595, color number 13538,
and black, FED-STD-595, color number 17038, stripes in a width ratio of 3 to 1, orange-yellow,
FED-STD-595, color number 13538, to black, FED-STD-595, color number 17038. The orange-
yellow stripes, FED-STD-595, color number 13538, shall be widths of 3/16-inch, 3/8-inch, or
3/4-inch; the black stripes, FED-STD-595, color number 17038, shall be corresponding widths of
1/16-inch, 1/8-inch, or 1/4-inch. Background striping shall be applied at a 45-degree angle from
the vertical, rotated clockwise. Small handles and levers shall be striped with alternate colored
rings with the above ratio and background. The striping shall not interfere with other types of
markings. If the handles or levers are visible in the aircraft’s clean flight configuration,
markings of aircraft with tactical paint schemes shall be in accordance with 5.2.3.

5.2.2.10.6.6 Fire access panel marking. A marking conforming to Appendix A, Figure

A-7 shall identify the fire access panel in the engine cowling. The words “FIRE PANEL” in red
letters shall be placed inside the rectangle. For tactical paint scheme aircraft the color
requirements specified in 5.2.3 shall apply.

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 MIL-STD-2161C(AS)

5.2.2.10.6.7 Explosive-actuated devices. Ejection seats and canopies, separable capsule

escape system, or encapsulated ejection seats, which are actuated explosively, shall be marked at
appropriate locations on the fuselage (see Appendix A, Figure A-1l and A-16).

5.2.2.10.6.8 Axe and crowbar. When an axe and/or crowbar are carried aboard the
aircraft, and are accessible from the outside of the aircraft, their positions shall be shown
externally by the words “AXE (CROWBAR) STOWED HERE” in 1-inch high letters. The
position of the axe and/or crowbar may be further identified by a silhouette. For tactical paint
schemes, the color requirements specified in 5.2.3 shall apply.

5.2.2.10.6.9 Fire extinguishers. When fire extinguishers are carried aboard the aircraft
and are accessible from the outside of the aircraft, their positions shall be shown by the words
“FIRE EXTINGUISHER STOWED HERE” and may be further identified by a silhouette of a
fire extinguisher. For tactical paint schemes, the color requirements specified in 5.2.3 shall
apply.

5.2.2.10.6.10 First-aid kit. When a first-aid kit is carried aboard the aircraft and is
accessible from the outside through an emergency exit or access panel, a red, FED-STD-595
color number 11136, Geneva cross on a white, FED-STD-595, color number 17925, background
shall be placed on the fuselage adjacent to this exit or panel (see Appendix A, Figure A-19). For
tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.2.10.6.11 Ejection seat markings. All parts of the ejection seat escape system shall
be marked with a triangle, colored insignia red, FED-STD-595, color number 11136. A triangle,
insignia red, FED-STD-595, color number 11136, shall be placed over each crew entrance to
indicate that the aircraft has such a system. The applicable words “EJECTION SEAT” or
“ESCAPE CAPSULE” shall be applied in 1-inch high letters under the triangle. Triangles shall
be located on each side of the fuselage at approximately the midpoint of the canopy for fighter,
fighter-trainer, and similar aircraft. The following warning shall be applied by using 3/4-inch
high painted or decal letters, on an orange-yellow, FED-STD-595, color number 13538,
background, beneath the triangles: “WARNING - THIS AIRCRAFT CONTAINS A
CARTRIDGE-ACTUATED EMERGENCY ESCAPE SYSTEM EQUIPPED WITH
EXPLOSIVE CHARGES” (see Appendix A, Figure A-11 and A-16). See Appendix A for
complete instructions. For tactical paint scheme aircraft, the color requirements specified in
5.2.3 shall apply.

5.2.2.10.6.11.1 Ejection seat markings for multiplace aircraft. If an aircraft is equipped

with cartridge-actuated escape provisions other than ejection seats, at certain crew stations, along
with ejection seats at other stations, the markings located on the exterior of the aircraft at each
crew entrance not equipped with ejection seats shall read “CARTRIDGE-ACTUATED
DEVICES” instead of “ESCAPE CAPSULE” or “EJECTION SEAT” under the triangle. In the
event all crewmembers use the same entrances, both notes shall be printed under the triangle
with the warning.

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 MIL-STD-2161C(AS)

5.2.2.10.6.11.2 Other cartridge-actuated escape systems. For aircraft equipped with

cartridge-actuated escape systems, such as hatch jettisoning systems, equipment stowage
systems, etc., but no means to forcibly separate crew members from the aircraft, the marking
shall read “CARTRIDGE-ACTUATED DEVICES.”

5.2.2.10.6.12 Canopy release markings. External canopy release access on aircraft shall
be painted orange-yellow, FED-STD-595, color number 13538. Release instructions from the
outside shall be painted in black, FED-STD-595, color number 17038. A reflective placard
applied near the canopy on the side of the flag opposite the canopy release shall show the
location of the release. For tactical paint scheme aircraft, the color requirements specified in
5.2.3 shall apply.

5.2.2.10.6.13 External exit emergency release. A “RESCUE” arrow applied on the

fuselage shall identify each external exit emergency release or handle. The arrow shall be in
accordance with Appendix A, Figure A-13, colored orange-yellow, FED-STD-595, color number
13538. Other markings (i.e., “STEP” or “ACCESS DOOR”) may be omitted to accommodate
this marking. For tactical paint scheme aircraft, the color requirements specified in 5.2.3 and
Figure A-14 shall apply.

5.2.2.10.6.14 Transport aircraft. The compartments of transport aircraft shall be marked

with individual compartment horizontal dimensional references, the compartment centroids, the
compartment letter designations, and the compartment maximum structural capacity in pounds.
Cargo compartments shall also be marked in inches from the horizontal reference datum at
20-inch intervals. This requirement does not apply to transport aircraft with executive interior
configurations.

5.2.2.10.6.14.1 Internal removable escape panels. Identification marking of escape

hatches, doors, and exits shall be colored orange-yellow, FED-STD-595, color number 13538, on
non-yellow surfaces. On yellow surfaces, the marking shall be colored black, FED-STD-595,
color number 17038. Retroreflective material, conforming to ASTM-D4956 shall be used for
this marking. An intermittent band, colored orange-yellow FED-STD-595, color number 13538,
shall identify the periphery of the escape panels. The segments of the band shall be a minimum
of 1-inch width and a maximum of 2-inch length, divided equally between the door mount and
the escape door. In locations where the door lining hides or covers the marking on the inside of
the aircraft, the marking shall continue onto the lining.

5.2.2.10.6.14.2 Emergency exit marking. The words “EMERGENCY EXIT” colored

orange-yellow, FED-STD-595, color number 13538, shall be painted or stenciled onto the escape
hatch, door or exit, or any covering thereof, in the most readily visible location. Letters shall be
a minimum of 2-inches high and shall not be less than 1-inch wide. For tactical paint schemes,
the color requirements specified in 5.2.3 shall apply.

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5.2.2.10.6.14.3 Handles, releases, catches, and knobs for inside panels. Handles,
releases, catches, and knobs for inside hatches, exit doors, and their soundproofing (or lining)
shall be painted orange-yellow, FED-STD-595, color number 13538. Suitable descriptive
wording, readily visible, shall be painted or stenciled on the door or structure of the aircraft,
whichever is nearer to the emergency release, to identify and explain its operation. This wording
shall be at least 1/2-inch high, using standard English terminology such as “PULL,” “PUSH,”
“TURN,” or “SLIDE.” Exits which are adequate for air, ground, and ditching escape shall have
the words “EMERGENCY EXIT” centered in the most visible location on the inside of the door
or hatch. Exits which are not adequate for the above three methods of escape shall be marked
“EMERGENCY EXIT,” and for specific usage, “GROUND USE ONLY,” “GROUND AND
DITCHING USE ONLY,” etc.

5.2.2.10.6.14.4 External removable escape panels. Markings identifying external

removable escape hatches, doors, and exits on the outside of aircraft shall be orange-yellow,
FED-STD-595, color number 13538. If the substrate is yellow, black, FED-STD-595, color
number 17038, shall be used. Retroreflective material conforming to ASTM-D4956 shall be
used for these markings to facilitate identification in the dark. Mark all external releases for
operation of emergency exit panels “EXIT RELEASE” on the outside of the aircraft to facilitate
identification. The writing that describes the operation of the exit release shall be standard
English terminology such as “PULL,” “PUSH,” “TURN,” or “SLIDE.” Letters shall be at least
1-inch high. For tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall
apply.

5.2.2.10.6.14.5 Markings for forced emergency entry or exit. Markings for aircraft
emergency entry or exit shall be orange-yellow, FED-STD-595, color number 13538. Black,
FED-STD-595, color number 17038, shall be used on yellow-orange backgrounds.
Retroreflective material conforming to ASTM-D4956 shall be used for these markings. For
tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.2.10.6.14.6 Secondary openings. Secondary openings, such as auxiliary exits,

windows, and navigator’s domes, are usually smaller than primary openings, making entrance or
exit more difficult. If the structure immediately surrounding secondary openings is free from
heavy structural members (such as bulkheads and the main longitudinal member), and from
oxygen, fuel and oil lines, and battery leads, it shall be marked with an orange-yellow,
FED-STD-595, color number 13538, broken band. The band shall be located at the extreme
boundary of the above-described area, both inside and outside of the fuselage. Segments of the
broken band shall be 1/2-inch wide, 1-inch long, and approximately 12-inches apart. Where the
band is covered with soundproofing, the soundproof (or lining) shall also be marked. “CUT
HERE FOR EMERGENCY RESCUE” shall be printed or stenciled inside of and parallel with
the broken band identifying the area on the exterior of the aircraft where forced entry can be
made for rescue purposes. Appendix A, Figure A-17, provides guidance for this marking. “CUT
HERE FOR EMERGENCY EXIT” shall be painted on a similar location inside the aircraft.
Letters shall be 1-inch high. If the area to receive the lettering is covered by soundproofing (or
lining), the letters shall also be stenciled on the soundproofing (or lining). Both exterior and

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 MIL-STD-2161C(AS)

interior markings shall be located inside of and adjacent to the broken band. For tactical paint
scheme aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.3 Tactical paint scheme markings. Unless otherwise approved by NAVAIR AIR-
4.1.8 or CNAF (N421), all markings specified in 5.2.2 and 5.2.5 are applicable to aircraft that
have a tactical paint scheme (TPS). Requirements for the colors of all the markings and the size
of some of the markings differ when applied to aircraft possessing the tactical paint scheme.
These differences in requirements are specified in 5.2.3.1 thru 5.2.4. Appendices C and D
include tactical paint schemes for US Navy and Marines aircraft systems.

5.2.3.1 Color of markings for aircraft with tactical paint schemes. All exterior markings
specified in 5.2.2 and 5.2.5 applied to aircraft possessing a tactical paint scheme shall be applied
in a contrasting shade of gray, the color of which is dependent on the gray colors used for the
specific tactical paint scheme and the location of the marking. See Appendices for examples.

5.2.3.1.1 Tactical paint scheme - general marking policy. Tactical paint schemes are
comprised of one, two, or three shades of gray. If the tactical paint scheme is comprised of only
one color, use another color of gray for the markings, which provides sufficient contrast. For
example, if the scheme is comprised of FED-STD-595, color number 36081, then use
FED-STD-595, color number 35237 for the markings. If the tactical paint scheme is comprised
of only two colors, the contrasting color specified is the color used in the scheme, which is not
located in the area where the marking is applied. If the tactical paint scheme is comprised of
three colors, the following guidelines apply:

a. If the background color is the darkest gray, medium gray is used for the marking.

b. If the background color is the medium gray, the darkest gray is used for the marking.

c. If the background color is the lightest gray, the medium gray is used for the marking.

5.2.3.1.2 Color of MODEX numbers. MODEX numbers applied to aircraft with the
tactical paint scheme shall be contrasting gray, FED-STD-595, color numbers 35237, or 36375
or black, FED-STD-595, color number 37038. See Appendices C and D for guidance on current
aircraft.

5.2.3.2 Size of markings when used on aircraft with tactical paint schemes. The size of
the markings when used on tactical paint scheme painted aircraft are the same sizes as specified
in 5.2.2 and 5.2.5 except that the branch of service marking, call number, and national insignias
shall follow those specified in Appendices A-D. For platforms not listed in Appendices A-D,
these markings shall be a maximum of 12-inches high on carrier based tactical paint scheme
aircraft.

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5.2.3.3 Paint scheme deviations approval. Deviations to paint schemes for one aircraft
per squadron may be approved by the Type Commander. Deviations for more than one aircraft
require prior approval by the Naval Air Systems Command (AIR 4.1.8). Additional approval
from CNAF (N421) may be required depending on the magnitude of the deviation(s), as
specified in 1.6.1.

5.2.4 Marking material. Marking materials shall conform to the gloss and IR
requirements of the coating used to apply tactical paint schemes. Decals may be used for small
markings (maximum of 4 inches) if all other requirements are met.

5.2.5 Exterior maintenance precautionary and warning markings.

5.2.5.1 Aircraft and missile service point identification symbols and markings. Service
point identification and precautionary warning markings shall be applied on all aircraft as
required (see Appendix B, Figures B-7, B-8, and B-9). All NATO markings, as referenced in
5.2, are required. The location of NATO markings are detailed in Appendix B, Figures B-3, B-4,
B-5, and B-6. The location of these markings may vary with airframe configuration and country
of interest. Each marking shall be displayed to provide the following:

a. Rapid identification of each required servicing point.

b. Identification of the type of ground servicing required.
c. Hazard warning of safety precautions, which will prevent injury to personnel or
damage to aircraft equipment.
d. Rapid entry or exit from vehicle under emergency conditions.

5.2.5.1.1 Application of service point identification symbols and markings. When

applying these symbols and markings, the instructions provided in Appendix B shall be adhered
to. The symbols shall not exceed 4 inches in width or height. Application may be accomplished
using paint or decals conforming to A-A-59485. When paint is used, stencils incorporating
capital letters and Arabic numerals not exceeding 1-1/4 inches in height shall be used; freehand
application is prohibited. When applied to a gray or white background, the marking shall be
black, FED-STD-595, color number 17038. On other backgrounds, the marking shall be white,
FED-STD-595, color number 17925. A decal similar to Appendix B, Figure B-6, shall be
located inside the nose wheel well, or nose wheel door, defining the location of service points.
For tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.5.1.2 Location. The location of each service point marking shall be based upon the
existing available space. They may be situated on the equipment concerned, directly below,
adjacent to, or on applicable access panels. In the event that the service point or marking is
concealed, arrows may be used to point out the location of the service point. The arrows shall
bear a brief identification of the purpose for which it is applied.

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5.2.5.1.3 Hydraulic system and landing gear/struts. Servicing instructions for hydraulic
systems, landing gear, and shock struts, shall be provided on metal instruction plates, or stenciled
in a permanent and legible manner, adjacent to charging points and test connections. For tactical
paint schemes, the color requirements specified in 5.2.3 shall apply.

5.2.5.2 Fuel nozzle jumper plug receptacles. Fuel nozzle plug receptacles shall be
marked in accordance with MIL-C-83413/9. For tactical paint schemes, the color requirements
specified in 5.2.3 shall apply.

5.2.5.3 Aircraft grounding points. All grounding points on all U.S. Navy and Marine
Corps aircraft shall be marked in accordance with Appendix B, Figures B-3, B-8, and B-9. For
tactical paint schemes, the color requirements specified in 5.2.3 shall apply.

5.2.5.4 Storage batteries. On all battery access doors, the word “BATTERY” shall be
painted in insignia red, FED-STD-595, color number 11136. The marking shall be in 1-inch
high letters. The lettering shall also be 1-inch high on aircraft with a tactical paint scheme and
the color shall be in accordance with 5.2.3. On the left side of the fuselage, as viewed from the
rear of the aircraft, there shall be a notation “BATTERY LOCATION __________.” The exact
location shall replace the line __________. The fore and aft positioning of the markings shall be
approximately in line with the trailing edge of the wings, and the vertical positioning 2 to 3 feet
above the bottom of the fuselage. For instances where there are windows, enclosures, etc., in
this position, the storage battery for marking shall be placed as near to the specified position as
possible. Where there are battery locations interior to the aircraft the word “BATTERY” or
“BATTERIES,” as applicable, shall be permanently and conspicuously affixed to the battery
casing or compartment. For tactical paint scheme aircraft, the color requirements specified in
5.2.3 shall apply.

5.2.5.5 Instrument static opening markings. Instrument static openings shall have no
finish applied within a 1-inch diameter circle around the opening. A red, FED-STD-595, color
number 31136, 1/2-inch wide circular band shall be applied around this area. The following
legend shall also be applied adjacent to the marking: “INSTRUMENT STATIC OPENING -DO
NOT COVER.” Aircraft painted with the tactical paint schemes shall be painted in accordance
with 5.2.3.

5.2.5.6 Wing fold warning flag. On aircraft having wing fold warning flags, the flags
shall be painted red, FED-STD-595, color number 31136.

5.2.5.7 Markings for electrical connections. The following caution note shall be placed
at points where it is necessary to break electrical connections when folding back or removing
wings, or removing tail surfaces, etc: “CAUTION, DISCONNECT ELECTRICAL WIRING
BEFORE REMOVING PART.” The color of the letters shall be black, FED-STD-595, color
number 17038.

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5.2.5.8 Markings for engine removal. All points of disconnect shall be painted either
black, FED-STD-595, color number 17038, or with contrasting gray for tactical paint schemes
(see 5.2.3).

5.2.5.9 Markings for tank and filler areas.

5.2.5.9.1 Tank. Aircraft tanks shall have notations indicating tank capacity, type of
liquid, and level restrictions. Tank markings shall be black, FED-STD-595, color number 17038.
Additional data, such as coolant mixture, water-alcohol mixture, and grade of liquid shall be
stenciled near the filler caps in letters 1/2-inch high in the same color as that used to indicate tank
capacity. Stenciling on the fuel tanks shall read: “USE ______ OCTANE FUEL OR BETTER,”
or “USE GRADE ______ OR BETTER,” as applicable. For tactical paint scheme aircraft, the
color requirements specified in 5.2.3 shall apply.

5.2.5.9.2 Filler caps. Filler caps for fuel and oil tanks and other external parts and
attachments for which identification is necessary and desirable shall be painted the color
assigned to the applicable fitting and shall be indicated by appropriate markings. Where flush-
type pressure fueling caps, conforming to MS29525 are installed, three radial black lines,
FED-STD-595, color number 37038, 3/8-inch wide by 1-inch long, shall be located as to form
extensions to the lines on the cap when the cap is in the locked position. Tactical paint scheme
aircraft shall be painted in accordance with 5.2.3. The type and grade of fuel to be employed in
the aircraft shall be indicated adjacent to the filler caps in accordance with Appendix B, Figures
B-3, and B-5.

5.2.5.10 Lift points, handgrips, caution legends, etc. Appropriate wording painted in
black, FED-STD-595, color number 17038, adjacent to the applicable location shall identify
these items. For tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall
apply. Appendix B, Figures B-4 and B-7 provide examples of this marking.

5.2.5.11 Baggage compartment, life raft stowage, etc. These shall be indicated by means
of appropriate signs painted in black, FED-STD-595, color number 17038, adjacent to the area.
For tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.5.12 Wing access panel latches and safety straps. On aircraft which have wing
access panel latches and safety straps, the inside lever and wing area under the latch safety strap
shall be painted insignia red, FED-STD-595, color number 11136, in such a manner that no red
color shall show when the latches and straps are properly secured.

5.2.5.13 Actuating mechanism-warning signs. A black warning sign, FED-STD-595,

color number 17038, shall be located adjacent to any actuating mechanism which can cause
damage to the weapon systems from improper or out-of-sequence operation. For tactical paint
scheme aircraft, the color requirements specified in 5.2.3 shall apply.

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5.2.5.14 Recessed lubrication fittings. Flush type (female receptacle) grease fittings,
recessed set screws, or depressed adjustments, such as may be found on rotor control and drive
shafts, but which require periodic servicing or inspection, shall be identified with a
circumscribed band of orange, FED-STD-595, color number 12197, not exceeding 1 inch in
width. For tactical paint scheme aircraft, the color requirements specified in 5.2.3 shall apply.

5.2.6 Optional markings.

5.2.6.1 Ship names. For carrier aircraft, the ship name may be applied to both sides of
the fuselage above the branch of service markings. If applied, the letters shall be a maximum of
6-inches high and applied in a contrasting shade of gray for tactical paint schemes and black for
conventional paint schemes.

5.2.6.2 Squadron designation. The squadron designation identifies with letters and
numerals of the squadron to which the aircraft is assigned. It shall be placed on both sides of the
fuselage, just forward of the empennage, and centered under the branch of service marking. If
this is not practical due to space limitations, the squadron designation shall be applied in an aft
location designated by the cognizant command. The squadron designation on low-wing
transports shall be applied along the centerline on both sides of the fuselage, just forward of the
empennage. On high-wing transports, if the branch of service marking is placed on the fuselage
either under the wing or aft of the trailing edge of the wing, the squadron designation shall be
centered symmetrically under the marking. If this is not practical, it shall be centered under the
marking, or placed aft, along the fuselage, below the centerline. Color of this marking shall be
black, FED-STD-595, color number 17038, except for tactical paint scheme aircraft. For these
aircraft the tactical paint scheme markings specified in 5.2.3 shall apply.

5.2.6.3 Reserve aircraft markings - station names. The name of the home station may be
placed on both sides of the fuselage just forward of the empennage and centered under the
branch of service marking. This shall be in addition to the station letter on both sides of the
vertical fin and rudder. On transport aircraft (VR), where the branch of service marking is
placed along the fuselage above the windows, the station name shall be placed along the
centerline on both sides of the fuselage, just forward of the empennage. This shall be in addition
to the station letter on both sides of the vertical fin and rudder. The letters used for reserve
station identification shall be one half the size of the branch of service marking. Color of this
marking shall be black, FED-STD-595, color number 17038, except for tactical paint scheme
aircraft, where the color requirements specified in 5.2.3 apply.

5.2.6.4 Battle “E”. Squadrons selected for the battle “E” are entitled to display a white,
FED-STD-595, color number 17925, letter “E” on all assigned aircraft for the length of one
competitive cycle following the date of award. The “E” shall be painted on the starboard side of
the aircraft in the vicinity of the cockpit, in a rectangular block type letter not to exceed 8 inches
in height and proportional in width. Where the “E” is awarded to the same squadron for
consecutive competitive cycles, a service hash mark shall be painted under the letter. This hash
mark shall be the width of one stroke and of the same color as the “E.” The hash mark shall be

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30 degrees to the horizontal from the lower left hand of the “E.” When applied to aircraft with a
tactical paint scheme, the color of the “E” and hash mark shall be gray, FED-STD-595, color
number 36081 or color number 37038.

5.2.6.5 Safety “S”. Squadrons winning this award are authorized to display an “S” for
safety marking on their aircraft. Authorization shall extend through the calendar year subsequent
to the year for which the award was won. An appropriate hash mark is approved only for
squadrons who are repeat winners in consecutive years. The “S” for safety shall be white,
FED-STD-595, color number 17925, or black, FED-STD-595, color number 17038, and shall be
of an appropriate size not more than 8 inches in height. It is to be displayed under the squadron
insignia (when used) and shall not interfere with required markings. For tactical paint schemes,
the color of the “S” shall be gray, FED-STD-595, color number 36081. Lettering shall be in
accordance with 5.2.1.1. Consecutive year marking shall be accomplished in the same way as
the battle “E” hash mark (see 5.2.6.4).

5.2.6.6 Hospital aircraft red cross. When aircraft are assigned air evacuation or hospital
duty, this marking is mandatory. It shall be centered on both sides of the vertical tail surface,
above the horizontal stabilizer, in the space normally allotted to the unit identifier. It shall also
be placed on the upper surface of the right wing with the center of the marking at a distance from
the wing tip equal to one third of the distance from the fuselage to the wing tip, and in a similar
location to the national insignia of the opposite wing, and on the under surface of the right wing,
located symmetrically between the national insignia and fuselage. Hospital aircraft shall be
identified by a Geneva Red Cross consisting of a symmetrical glossy insignia red cross,
FED-STD-595, color number 11136, on a glossy white disc, FED-STD-595, color number 17925
(see Appendix A, Figure A-19). The insignia shall consist of five red squares arranged in the
form of a symmetrical cross, centered inside the white circumscribed circle. The length of the
red cross shall be 15/19 of the diameter of the circumscribed circle. The diameter of the
circumscribed circle shall be 2/3 of the mean chord of the vertical tail surface.

5.2.6.7 Aircraft pilot and crew chief names. The names of the regular aircraft pilot
and/or the aircraft crew chief may be applied to the fuselage side below the aircraft transparency
at the option of the Type Commander. Block lettering 2-inches high in black, FED-STD-595,
color number 17038, shall be used for these markings. For tactical paint schemes, the color
requirements specified in 5.2.3 shall apply.

5.2.6.8 NAVAIR logo. The application of this marking is a symbol of Naval Air
Systems Command’s commitment to support the Fleet. It will be displayed proudly to identify
the promise of delivering the world’s best technology to the Warfighter. The logo will be
displayed as a secondary, not mandatory, marking and as such is the responsibility of NAVAIR
to be applied during acquisition or at otherwise scheduled Depot inductions. It is not a
requirement to maintain the logo once it is introduced to the fleet. See Appendix A,
Figure A-21.

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5.2.6.8.1 Color. The lettering, the oval, and the lightning bolt shall be applied in black,
FED-STD-595, color number 17038. For tactical paint scheme aircraft, the color requirements
specified in 5.2.3 shall apply.

5.2.6.8.2 Location. Two inches, centrally located, above or below the external finish
specification, depending on aircraft configuration. Note: the logo shall be applied to the
starboard side of the aircraft only, similar to the external finish specification.

5.2.6.8.3 Size. The size of the letters shall be 1/2-, 1-, or 2-inches in height. The logo’s
aspect ratio is 12.45 inches in length per 1-inch letter height. The oval and lighting bolt shall be
proportionally larger than the letter height. This size also applies to aircraft with the tactical
paint scheme.

5.2.6.8.4 Letter font. The logo uses a Blank Gothic Md Bt – medium type font and has
set spacing between characters and therefore shall not follow 5.2.1.1. However, the logo shall
conform to 5.1.3.1 and 5.2.4.

5.2.7 Special purpose marking for U.S. Navy aircraft. Unless otherwise specified, the
dimensions, colors, and materials shall also apply to special purpose markings. Due to variance
in equipment configuration and restrictions in the uses of some markings, special purpose
markings may or may not be applicable to all aircraft. However, when applicable and authorized
for use, special purpose markings shall be applied in the dimensions, colors and locations as
specified herein.

5.2.7.1 Identification of American Legation U.S. Naval Attaché (ALUSNA) aircraft.

The marking for naval attaché also applies to naval mission. Either marking may be applied, as
applicable.

5.2.7.1.1 Fuselage marking. The U.S. Navy marking shall be located on the fuselage in
the same place as for the transport aircraft (see 5.2.2.4). The lettering shall be the largest
possible size that can be accommodated on the aircraft, selected from 5.2.

5.2.7.1.2 Naval attaché fuselage marking. ALUSNA markings may be deleted on the
basis of local, diplomatic, or other considerations. Fuselage markings for ALUSNA aircraft shall
consist of the following words: “UNITED STATES NAVAL ATTACHÉ TO (NAME OF
COUNTRY).” For the benefit of foreign personnel, the same wording in the language of the
country to which the attaché is accredited shall be placed approximately 2-inches below the
American wording. This foreign language inscription shall be applied under the supervision of
personnel who have a thorough knowledge of the foreign language involved. In the event that
there is more than one form of script of the foreign language, the selection shall be determined
by the foreign country. All letters shall be painted or stenciled in white on a dark background or
in black on a light background.

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5.2.7.1.2.1 Location. The attaché fuselage marking shall be forward on the aircraft,
approximately under the pilot’s cockpit, on both sides of the fuselage. For C-2A and larger
aircraft, the English language inscription shall be located above the centerline of the fuselage and
the foreign language inscription shall be located below the centerline of the fuselage. For
smaller aircraft, the English and foreign language inscriptions shall be located just below the
pilot’s window.

5.2.7.1.2.2 Size. For C-2A and larger aircraft, the lettering of the English and foreign
language inscription shall be 4-inches high. For smaller aircraft, the size of the lettering shall be
reduced proportionately.

5.2.7.1.3 Naval attaché wing marking. The wing marking for attaché aircraft shall
consist of an American flag, conforming to Appendix A, Figure A-18.

5.2.7.1.3.1 Location. The American flag shall be located on the underside of the left
wing, approximately under the national insignia on the topside of the left wing. The branch of
service marking shall not be used on the wing for ALUSNA aircraft. The flag shall be centered
and applied so that an observer on the ground, with airplane approaching, shall view the flag
with the blue field forward and to his left, and with the stripes extending outboard. If more
positive identification is required because of local conditions or other considerations, an
additional American flag may be applied to the topside of the right wing on an interim basis.
This flag shall be removed when local considerations permit. The flag size shall be the same as
that applied to the underside of the left wing and shall be located approximately over the national
insignia on the underside of the right wing.

5.2.7.1.3.2 Size. The flag markings shall use a length-to-height ratio of 1.9-to-1.0 (for
example, 36-inches long by 19-inches high), in accordance with standard American flag
requirements. In no case, however, shall the width exceed 75 percent of the distance between the
leading edge of the wing and the aileron cutout at the point of application. In all cases, the
largest size flag, which can be accommodated on the wing, shall be used.

5.2.7.1.4 Naval attaché vertical stabilizer marking. The vertical tail surface marking for
naval attaché aircraft shall consist of an American flag.

Note: At the discretion of cognizant commands, American flags, similar to the

configuration specified for ALUSNA aircraft, may be applied (except on tactical paint scheme
aircraft) on both sides, or on the two outboard sides of the vertical tail surface of transport
aircraft performing diplomatic missions, VIP missions, or for other important considerations.
Such markings shall be deleted after their purpose has been served.

5.2.7.1.4.1 Location. The American flag shall be positioned horizontally and in such a
manner that the union shall be uppermost on both sides of the vertical tail surfaces. For aircraft
having multiple vertical tail surfaces, the flag shall appear only on the two outboard sides. On
both sides of the aircraft, the flag shall be applied with the blue field forward and the stripes

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 MIL-STD-2161C(AS)

extending aft. The bars of the flag shall appear to be trailing at all times. The flag shall be
centered on the surface and placed above all other markings (see Appendix A, Figure A-18).

5.2.7.2 Standard American flag sizes. The following standard sizes (length by height)
are examples of American flag markings used on U.S. Navy aircraft (see Appendix A, Figure A-
18):

a. 36 x 19 inches
b. 40 x 21 inches
c. 48 x 25 inches
d. 60 x 31.4 inches

The flag or national insignia/emblem of any country, other than the United States of
America, shall not be displayed on any U.S. Navy or Marine Corps aircraft for any reason.

5.2.7.3 VIP helicopters. For layout and description of markings required on VIP
helicopters, refer to Appendix D, Figure D-12.

5.2.8 Marking of foreign aircraft. Aircraft procured by foreign countries through the
Department of Defense shall be marked in accordance with this standard, except that the U.S.
national insignia shall be replaced with the foreign country’s national insignia. National
insignias for various countries are provided in Appendix E.

5.2.9 Access panel identification. Exterior aircraft panels, plates, and access doors
which require opening or removal at the time of inspection or overhaul shall be identified by the
access numbering system in accordance with MS90327.

5.2.10 Walkways and honeycomb panels. Walkways and honeycomb panels shall be
marked as specified in 5.2.10.1 thru 5.2.11.

5.2.10.1 Walkways and steps. In cases where they do not contrast in color with adjacent
areas, walkway areas shall be bounded by a camouflage black line, FED-STD-595, color number
37038 for a light background or a camouflage white line, FED-STD-595, color number 37925
for a dark background, 1/2-inch wide, and marked with the word “WALKWAY” at sufficiently
frequent intervals to indicate the walkway area. Steps shall be suitably indicated at all points on
the aircraft. For exterior walkway areas on tactical paint scheme aircraft. the color requirements
of 5.2.3 shall apply.

5.2.11 Honeycomb panels on airplanes. Honeycomb panels (thin skin) for wing upper
surfaces shall be distinctly marked by a 1-1/2 inch wide stripe of hash marks; each hash mark
shall be 2-inches long, measured along the stripe with 2 inches between marks. The marks shall
slope 45 degrees. The markings shall be painted on, with a material that is compatible with the
finish on the aircraft, in the area of application. For exterior markings on honeycomb panels
used on tactical paint scheme aircraft, the color requirements of 5.2.3 shall apply.

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5.2.12 Marking of loose and jettisonable equipment. The following loose equipment
shall be marked in a contrasting color, using a stencil or other suitable marking, with the call
numbers: life rafts; tool kits peculiar to the airplanes; aircraft covers, (e.g., engine covers, dust
covers, etc.), equipment specifically calibrated for the airplane, such as drift meters, tuning units,
etc., and jettisonable equipment such as canopies, wing tanks, and ejection seats. Ejection seats
shall include abbreviation of the operator, such as PLT, CO-PLT, NAV. For tactical paint
schemes, the color requirements specified in 5.2.3 shall apply.

5.2.13 Dinghy (raft) release and flotation controls. Operating handles and levers shall be
striped orange-yellow and black alternating lines; the title and operating instructions shall be
orange-yellow. The letters of titles shall be at least 1-inch high and the letters of operating
instructions not less than 1/2-inch high. If the control is in the form of a switch, then the size of
the letters may be reduced to a size appropriate to the location. For tactical paint schemes, the
color requirements specified in 5.2.3 shall apply.

5.2.14 Workmanship. Insignia and markings shall be uniform in quality and shall be free
from irregularities, defects, or foreign material that could adversely affect performance,
reliability or durability. Insignia or markings not applied in accordance with acceptable level of
workmanship or not in accordance with the requirements of this standard shall be removed and
reapplied.

6. NOTES

(This section contains information of a general or explanatory nature that may be helpful,
but is not mandatory.)

6.1 Intended use. The purpose of this standard is to specify paint schemes and insignia
markings for all U.S. Navy and Marine Corps aircraft, including identification plates for the
aircraft and warning and instruction markings.

6.2 Acquisition requirements. Acquisition documents should specify the following:

Title, number, and date of this standard.

6.3 Associated Data Item Descriptions (DIDs). This standard has been assigned an
Acquisition Management Systems Control (AMSC) number authorizing it as the source
document for the following DID. When it is necessary to obtain the data, the applicable DID
must be listed on the Contract Data Requirements List (DD Form 1423).

Reference Paragraph DID Number DID Title Suggested Tailoring

4.3, 5.2.2.1 DI-SESS-81000E Engineering drawing Use contractor format

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The above DID was current as of the date of this standard. The ASSIST database should be
researched at http://quicksearch.dla.mil or https://assist.dla.mil to ensure that only current and
approved DIDs are cited on the DD Form 1423.

6.4 Toxicity. Some free isocyanate is released during the mixing and application of
multi-component polyurethane coatings. Released free isocyanates can produce a significant
irritation to the skin, eyes, and respiratory tract. Personnel exposed to free isocyanates may
develop an allergic pulmonary sensitization, particularly if there is an inhalation of the vapor and
mist produced during spray application. This sensitization may cause an asthmatic reaction with
wheezing, dyspnea, and cough. Once sensitized, further exposure cannot be tolerated. For this
reason, there is a restriction of the issuance and use of this material. Personnel exposed to free
isocyanates on a regular basis should receive a periodic medical exam in accordance with
OPNAVINST 5100.23 that includes a chest roentgenograph (X-ray), pulmonary function tests,
and an evaluation of any respiratory disease or history of allergy. Periodic testing of pulmonary
functions may aid in detecting the onset of pulmonary sensitization.

6.4.1 Personnel protective methods. Eye protection and appropriate clothing to prevent
repeated or prolonged skin contact should be worn while applying material that contains free
isocyanates. Refer to NAVAIR 01-1A-509 Aircraft Weapon Systems Cleaning and Corrosion
Control.

6.5 Subject term (key word) listing.

Aircraft color patterns

Emergency warnings
Hazard warnings
Identification
Insignias

6.6 International standardization agreement implementation. This standard implements

NATO STANAG 3230 “Emergency Markings On Aircraft”. When changes to , revision, or
cancellation of this standard are proposed, the preparing activity must coordinate the action with
the U.S. National Point of Contact for the international standardization agreement, as identified
in the ASSIST database at https://assist.dla.mil.

6.7 Changes from previous issue. Marginal notations are not used in this revision to
identify changes with respect to the previous issue due to the extent of the changes.

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 MIL-STD-2161C(AS)
APPENDIX A

STANDARD MARKING,
EMERGENCY AND HAZARD WARNING MARKINGS FOR AIRCRAFT

A.1 SCOPE

A.1.1 Scope. This appendix specifies the design of standard markings (including the
national insignia), emergency, and hazard warning markings for fixed wing and rotary wing
aircraft. This appendix is a mandatory part of this standard. The information contained herein is
intended for compliance.

A.2 APPLICABLE DOCUMENTS

A.2.1 General. The documents listed in this section are specified in section A.3 of this
standard. This section does not include documents cited in other sections of this standard or
recommended for additional information or as examples. While every effort has been made to
ensure the completeness of this list, document users are cautioned that they must meet all
specified requirements of documents cited in section A.3 of this standard, whether or not they are
listed.

A.2.2 Government documents.

A.2.2.1 Specifications and standards. The following specifications and standards form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of
these documents are those cited in the solicitation or contract.

FEDERAL SPECIFICATION

DDD-F-416 - Flag, National, United States of America,

and Flag, Union Jack

DEPARTMENT OF DEFENSE SPECIFICATION

MIL-F-18264 - Finishes, Organic, Weapons System, Application and

Control of

(Copies of these documents are available online at http://quicksearch.dla.mil or

https://assist.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue,
Building 4D, Philadelphia, PA 19111-5094.)

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APPENDIX A

A.2.3 Order of precedence. In the event of a conflict between the text of this document
and the references cited herein, and unless described as an exception, the text of this document
takes precedence. Exceptions to this order of precedence include aircraft detail specifications,
aircraft drawings, and aircraft manuals. Nothing in this document, however, supersedes
applicable laws and regulations unless a specific exemption has been obtained.

A.3 GENERAL REQUIREMENTS

A.3.1 National insignia.

A.3.1.1 National insignia design. The design of the national insignia shall conform to
the requirements of this standard. As illustrated in Figure A-1, it shall consist of an insignia-
white, five-pointed star inside an insignia-blue circumscribed circle. A white rectangle, one
radius of the blue circle in length and 1/2 radius of the blue circle in width, shall be located on
each side of the star. The top edges of the rectangle shall be placed to form a straight line with
the top edges of the horizontal two star points beneath the top star point. An insignia-red
horizontal stripe, 1/6 the radius of the star, shall be centered in the white rectangles at each end
of the insignia. A blue border, having a width of 1/8 the radius of the blue circle, shall outline
the entire design except that when the insignia is to be applied on a sea blue, dark blue, or black
background, the blue circle and border may be omitted. The inside edge of each interior
rectangle shall be concave, and shall have the same arc as the inside blue circle. The inside edge
of each outer rectangle shall not be depicted.

A.3.1.1.1 Size. The blue circle of the insignia for wing application, exclusive of border,
shall have a maximum diameter of 40 inches and a minimum diameter of 10 inches. Sizes may
vary by 5-inch increments in diameter. The blue circle diameter selected shall be the size that is
closest to, but does not exceed, 50 percent of the distance between the leading edge of the wing
and the aileron cutout at the point of application. For fuselage application the blue circle shall
have a maximum diameter of 40 inches and a minimum diameter of 10 inches. The diameter
selected for fuselage application shall be closest to but not exceeding that which is 50 percent of
the height of the projection of the fuselage or hull side. The most practical diameter shall be
selected for helicopters and tilt rotor aircraft.

A.3.1.1.2 Color. The standard colors of the national insignia are insignia red,
FED-STD-595, color number 11136, insignia white, FED-STD-595, color number 17925, and
insignia blue, FED-STD-595, color number 15044. Corresponding semi-gloss or lusterless
finishes of the above listed gloss colors may be used to match adjacent surfaces only when
specified by the procuring activity. For tactical paint schemes the color requirements specified
in 5.2.3 shall apply.

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APPENDIX A

A.3.1.1.3 Application. Application of the national insignia by painting shall be in

accordance with MIL-F-18264. When applying the national insignia by painting, a stencil shall
be used to produce a sharp outline. The insignia shall be applied with coatings compatible with
the finish applied to adjacent surfaces. Decals may be used in lieu of paint for application of the
national insignia (see A.3.1.5). The national insignia shall be so applied on horizontal surfaces
that, in the normal flight attitude of the aircraft, the top star point of the insignia points forward,
and a line through that point and the star’s center is parallel to the line of flight, except for the
swept wing or variable sweep wing configurations. On these aircraft, the national insignia shall
be placed so that it will not extend onto flaps, slats, or control surfaces (see Figure A-2). The
constant 50 percent chord line of the wing shall pass through the center of the star. For fuselage
application, the insignia shall be placed so that the top star point points upward, and a line
through that point and the star’s center is perpendicular to the line of flight.

A.3.1.2 Wing insignia. On fixed wing aircraft, the national insignia shall be applied to
the upper surface of the left wing, on the lower surface of the right wing, and on the fuselage, as
shown in the figures of Appendix C. The insignia shall be placed at a distance from the wingtip
equal to 1/3 of the distance from the fuselage to the wingtip, measured from the center of the
insignia. It may be moved inboard where impractical. The insignia shall not be applied to the
wings of research aircraft when interference with aerodynamics can result. The size selected
shall be that which is closest to, but does not exceed, 50 percent of the distance between the
leading edge of the wing and the aileron cutout at the point of application. The wing insignia or
other markings shall be omitted from the underside of wings or other surfaces on which thermal-
resistant finishes are applied.

A.3.1.3 Fuselage or hull insignia. On fixed wing aircraft, the national insignia shall be
applied to each side of the fuselage or hull. These locations are illustrated in the figures in
Appendix C. The fuselage or hull insignia may extend over doors and emergency exits, but shall
not extend over windows or openings used during combat. For aircraft with a tactical paint
scheme the insignia shall be 12 inches in diameter of a contrasting color, and placed as directed
by the applicable Naval Aviation Depot directive.

A.3.1.4 Rotary wing aircraft insignia. Four national star insignias shall be applied to
rotary wing aircraft, so as to be visible from either side and from above and below (see Appendix
D). If the configuration permits, an additional insignia may be applied to the nose of rotary wing
aircraft for frontal identification. Symmetry of size and location shall be maintained on all like-
model series aircraft.

A.3.1.5 Decalcomanias. Decals may be used for all small markings (4 inches or less in
size). For interior application, where they should not be affected by weather conditions, and for
exterior application on low-performance aircraft, decals may be applied. For exterior application
on high-performance aircraft and where subjected to extremes of temperature, speed, and
altitude, A-A-59485 shall apply. A-A-59485 decals may be furnished with perforation holes

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APPENDIX A

upon request. These decals may be applied only over the complete paint system. Decal
application shall not be deleterious to the aircraft surface. Decals shall not be applied over
brazier head rivets.

A.3.1.6 Decalcomania letter heights. Letter heights shall be as follows:

Small: 1, 2, 3, 4½, and 6-inches high

Medium: 9, 12, 15, 18, and 21-inches high
Large: 24, 30, 42, and 48-inches high

Decals larger than 48 inches in height may increase by 12-inch increments. Dimensions
for letters shall maintain a 1/3 ratio for height, width, and stroke.

A.3.1.7 Tactical paint scheme national insignia. See 5.2.3 and Figure A-1.

A.3.2 Aircraft markings. The following figures illustrate standard (including the
national insignia), emergency, and hazard warning for fixed wing and rotary wing aircraft.

***** NOTE: ACTUAL COLORS SHOWN ON ALL ILLUSTRATIONS IN

APPENDICES A-D ARE STRICTLY FOR ILLUSTRATIVE PURPOSE. SPECIFIC
FED-STD-595 COLOR DESIGNATIONS INDICATED ON THE ILLUSTRATIONS
SHALL BE USED. *****

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FIGURE A-1. National star insignia.

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FIGURE A-2. National star insignia on swept wing aircraft.

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FIGURE A-3. Arresting hook warning.

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FIGURE A-4(a). Form of letters and numerals (modified vertical block) (See notes
following Figure A-4(b).

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FIGURE A-4(b). Form of letters and numerals (open block – to be used for markings 2 inches
high or less) – Continued (See notes following this figure).

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NOTES FOR FIGURES A-4(a) AND A-4(b):

1. The width of all letters and numbers (characters) shall be measured between the
widest points of the characters.

2. The width of the characters is calculated as a percentage of the height. For example,
as on the previous page:

a. All letters and numerals are 6 blocks high and 4.5 blocks wide; therefore, the
width of letters and numerals shall be 75 percent of the height.
b. The width of letters A and M shall be 5.5 blocks wide therefore, 92 percent of
the letter’s height.
c. The width of the letter W shall be 6.5 blocks wide therefore, 108 percent of its
height.
d. The width of the letter G, including the overhang, shall be 5 blocks wide
therefore, 83 percent of its height.

3. To obtain the percentage of the height, divide the width of the character by its height.

4. The sides of the characters containing a corner wedge (e.g., B, C, D, G, 2, 3, etc.)

shall be made to include an angle of 30 degrees to the horizontal, as shown on the
previous page.

5. The spacing between characters shall be 1/6 of the height of the letter or numeral.
This spacing shall be measured from the point on each character nearest the other.
An exception to this requirement is when certain characters are coupled such as AV,
AW, AY, VA, WA, YA and 74.

6. The dash (-) character width is dictated by the height of the letters and shall be
vertically centered. Spacing of the dash and adjoining characters shall be 1/6 the
height of the adjoining characters.

7. All overhangs (letters C, G, S and numerals 2, 3, 4, 9) shall be 1/12 the character’s

height.

8. Gothic lettering may be utilized for markings less than 2 inches high.

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FIGURE A-5. Color scheme for helicopter blades.

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FIGURE A-6. Color scheme for reciprocating single and multi-engine aircraft propellers.

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FIGURE A-7. Markings for fire access panel.

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(NON-TPS)

FIGURE A-8. Warning chevron and signs applied adjacent to jet engine intake and exhaust.

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FIGURE A-9. Propeller warning stripes and signs.

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FIGURE A-10. Canopy release location.

FIGURE A-11. Warning decal.

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FIGURE A-12. Helicopter tail boom markings.

FIGURE A-13. Canopy release markings.

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FIGURE A-14. Tactical paint scheme – rescue arrow and arresting hook markings.

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SEE PARAGRAPH 5.2.3

SEE PARAGRAPH 5.2.3

SEE PARAGRAPH 5.2.3

FIGURE A-15. Tactical paint scheme – engine intake chevrons, access door warning and branch
of service markings.

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SEE PARAGRAPH 5.2.3

SEE PARAGRAPH 5.2.3 AND 5.2.2.10.6.7

FIGURE A-16. Tactical paint scheme – ejection seat & warning and fuel nozzle port markings.

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FIGURE A-17. Area cutout markings.

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FIGURE A-18. American flag dimensions shall be in accordance with DDD-F-416.

FIGURE A-19. Geneva red cross.

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FIGURE A-20. Placard installation-identification, emergency escape hatch.

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FIGURE A-21. NAVAIR logo.

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APPENDIX B

SERVICING, GROUND HANDLING, HAZARD WARNING MARKINGS,

AND ARMAMENT PLACARD FOR AIRCRAFT

B.1 SCOPE

B.1.1 Scope. This appendix specifies aircraft servicing markings and appropriate NATO
code number for cross servicing. Hazard warning markings for ground handling are included.
This appendix is a mandatory part of this standard. The information contained herein is intended
for compliance.

B.2 APPLICABLE DOCUMENTS

B.2.1 General. The documents listed in this section are specified in sections B.3 and B.4
of this standard. This section does not include documents cited in other sections of this standard
or recommended for additional information or as examples. While every effort has been made to
ensure the completeness of this list, document users are cautioned that they must meet all
specified requirements of documents cited in sections B.3 and B.4 of this standard, whether or
not they are listed.

B.2.2 Government documents.

B.2.2.1 Specifications and standards. The following specifications and standards form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of
these documents are those cited in the solicitation or contract.

INTERNATIONAL STANDARDIZATION AGREEMENT

NORTH ATLANTIC TREATY ORGANIZATION (NATO)

STANAG 1135 - Interchangeability Fuels, Lubricants and Associated

Products Used by the Armed Forces of the North Atlantic
Treaty Nations

FEDERAL SPECIFICATIONS

O-M-232 - Methanol (Methyl Alcohol)

SS-G-659 - Graphite, Dry (Lubricating)
TT-I-735 - Isopropyl Alcohol
VV-P-236 - Petrolatum, Technical

COMMERCIAL ITEM DESCRIPTION

A-A-58092 - Tape, Antiseize, Polytetrafluorethylene

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DEPARTMENT OF DEFENSE SPECIFICATIONS

MIL-DTL-4339 - Corrosion Preventive, Soluble Oil for Water Injection

Systems (NATO Code Number C-630)
MIL-DTL-5020 - Liquid, Compass, Aircraft
MIL-PRF-5606 - Hydraulic Fluid, Petroleum Base, Aircraft, Missile and
Ordnance
MIL-DTL-5624 - Turbine Fuel, Aviation, Grades JP-4 and JP-5
MIL-PRF-6081 - Lubrication Oil, Jet Engine
MIL-PRF-6083 - Hydraulic Fluid, Petroleum Base, for Preservation and
Operation
MIL-PRF-6085 - Lubricating Oil: Instrument, Aircraft, Low Volatility
MIL-PRF-6086 - Lubricating Oil, Gear, Petroleum Base (NATO O-153, O-
155)
MIL-C-6529 - Corrosion Preventive, Aircraft Engine
MIL-PRF-7808 - Lubricating Oil, Aircraft Turbine Engine, Synthetic Base
MIL-PRF-7870 - Lubricating Oil, General Purpose, Low Temperature
NATO O-142
MIL-PRF-8188 - Corrosion-Preventive, Aircraft Turbine Engine, Synthetic
Base
MIL-C-11796 - Corrosion Preventive Compound, Petrolatum, Hot
Application
MIL-PRF-16173 - Corrosion Preventive Compound, Solvent Cutback, Cold
Application
MIL-L-23398 - Lubricant, Solid Film, Air Cured, Corrosion Inhibiting,
NATO Code Number S-749
MIL-PRF-23699 - Lubricating Oil, Aircraft Turbine Engine, Synthetic Base,
NATO Code Number 0-156
MIL-PRF-23827 - Grease, Aircraft and Instrument, Gear and Actuator Screw
MIL-G-25013 - Grease, Aircraft, Ball and Roller Bearing, NATO Code
Number G-372, Metric
MIL-G-25537 - Grease, Aircraft, Helicopter, Oscillating Bearing, NATO
Code Number G-366, Metric
MIL-DTL-25681 - Lubricant, Molybdenum Disulfide, Silicone
MIL-PRF-81322 - Grease, Aircraft, General Purpose, Wide Temperature
Range, NATO Code G-395
MIL-PRF-81329 - Lubricant, Solid Film, Extreme Environment, NATO Code
Number S-1737
MIL-DTL-83133 - Turbine Fuel, Aviation, Kerosene Type, JP-8 (NATO F-
34), NATO F-35, and JP-8+100 (NATO F-37)

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APPENDIX B

MIL-PRF-83282 - Hydraulic Fluid, Fire Resistant, Synthetic Hydrocarbon

Base, Metric, NATO Code Number H-537
MIL-PRF-83363 - Grease, Transmission, Helicopter (NATO-G396)
MIL-DTL-85470 - Inhibitor, Icing, Fuel System, High Flash, NATO Code
Number S-1745

(Copies of these documents are available online at http://quicksearch.dla.mil or

https://assist.dla.mil/ or from the Standardization Document Order Desk, 700 Robbins Avenue,
Building 4D, Philadelphia, PA 19111-5094.)

B.2.2.2 Non-Government publications. The following documents form a part of this

document to the extent specified herein. Unless otherwise specified, the issues of this document
are those cited in the solicitation or contract.

AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) INTERNATIONAL

ASTM-D910 - Standard Specification for Aviation Gasolines

(Copies of this document are available from ASTM International, 100 Barr Harbor Drive,
West Conshohocken, PA 19428-2959 or online at http://www.astm.org.)

SOCIETY OF AUTOMOTIVE ENGINEERS (SAE) INTERNATIONAL

SAE-AMS1424 - Fluid, Deicing/Anti-icing, Aircraft, SAE Type I.

(DoD adopted)
SAE-AMS2518 - Thread Compound, Anti-Seize, Graphite-Petrolatum.
(DoD adopted)
SAE-AMS-G-4343 - Grease, Pneumatic System. (DoD adopted)
SAE-AMS-G-6032 - Grease, Plug Valve, Gasoline and Oil Resistant, NATO
Code Number G-363, Metric. (DoD adopted)
SAE-AMS-M-7866 - Molybdenum Disulfide, Technical, Lubrication Grade.
(DoD adopted)
SAE-AS8660 - Silicone Compound NATO Code Number S-736.
(DoD adopted)
SAE-J1899 - Oil, Lubricating, Aircraft Piston Engine (Ashless
Dispersant). (DoD adopted)
SAE-J1966 - Oils, Lubricating, Aircraft Piston Engine
(Nondispersant Mineral Oil). (DoD adopted)

(Copies of these documents are available from http://www.sae.org or from the Society of
Automotive Engineers, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)

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APPENDIX B

B.2.3 Order of precedence. In the event of a conflict between the text of this document
and the references cited herein, and unless described as an exception, the text of this document
takes precedence. Exceptions to this order of precedence include aircraft detail specifications,
aircraft drawings, and aircraft manuals. Nothing in this document, however, supersedes
applicable laws and regulations unless a specific exemption has been obtained.

B.3 GENERAL REQUIREMENTS

B.3.1 Servicing and precautioning marking. The servicing and precautionary markings
for aircraft shall be in accordance with the symbols shown and as specified herein. Symbols
shall be approximately 4 inches in the lowest dimension, except where otherwise specified.
However, smaller sized lettering which supplement the symbols may be used if required by the
item or area to be marked. Lettering which supplements the symbols shall be in the scale 1 to 4
in relation to the symbol (see figure B-1).

B.3.2 Servicing instructions. Servicing instructions for hydraulic systems, hydraulic

reservoirs, landing gear shock struts, wheels and tires, and pneumatic systems shall be provided
on instruction plates or in a permanent and legible manner adjacent to charging points and test
connections. Access doors or panels to servicing points shall be marked with the appropriate
servicing symbol(s).

B.3.3 Service warning markings. Service markings shall be used to give warning and
minimize possible errors in servicing, handling of aircraft and safety of flight. Symbols
approved by international agreement shall be displayed on all “in production” and “in service”
aircraft. These symbols shall be in accordance with those shown on figures B-6 and B-7.
Markings for trainer and liaison aircraft shall be included. Paint or decals may be used when
applying service point identification and precautionary service markings. Decalcomanias shall
be in accordance with ASTM-D4956 and plastic material per A-A-59485.

B.3.4 Printed information. Information required in connection with symbols shall be

printed in accordance with 5.2.5.1, unless specified by the procuring activity.

B.3.5 Colors. Colors for ground handling, hazard warning, filling and atomic flash
markings shall be as follows:

a. Ground handling: The servicing symbols used to mark ground handling servicing
points shall be orange yellow, FED-STD-595, color number 13538.

b. Hazard: Hazard symbols shall be insignia red, FED-STD-595, color number 11136.

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c. Filling points: The servicing symbols used to mark filling points shall be colored in
black, FED-STD-595, color number 17038 or insignia white, FED-STD-595, color number
17925, according to the background.

d. Atomic flash: Aircraft, which may be subjected to atomic flash, will have servicing
markings painted in suitable pale colors, having a reflectivity of at least 50 percent.

B.4 DETAIL REQUIREMENTS

B.4.1 Aircraft markings and placard. The following figures illustrate aircraft armament
placards, NATO codes and markings, ground handling and hazards and NATO code numbers for
cross servicing.

***** NOTE: ACTUAL COLORS SHOWN ON ALL ILLUSTRATIONS IN

APPENDICES A-D ARE STRICTLY FOR ILLUSTRATIVE PURPOSE. SPECIFIC
FED-STD-595 COLOR DESIGNATIONS INDICATED ON THE ILLUSTRATIONS
SHALL BE USED. *****

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FIGURE B-1. Typical symbol dimensioning.

FIGURE B-2. Armament placard.

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FIGURE B-3. NATO codes and markings-filling.

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FIGURE B-4. NATO codes and markings-filling, ground handling and hazards.

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APPENDIX B

NATO APPLICABLE
GENERAL TYPE OF PRODUCT NUMBER1 SPECIFICATION2
I. Piston engine fuels
II. Turbine engine fuels
Kerosene type, high flashpoint F-44 MIL-DTL-5624
Gasoline type, wide cut (JP-4) F-40 MIL-DTL-5624
Aviation, kerosene type (JP-8) F-34 MIL-DTL-83133
Kerosene type F-35 MIL-DTL-83133
III. Starter fuels
IV. Thrust augmentation fluids
Methanol S-747 O-M-232 Grade A
Soluble oil C-630 MIL-DTL-4339
V. Piston engine oils
Non-dispersant mineral oil 0-117 SAE-J1966 Grade 1100
Non-dispersant mineral oil 0-113 SAE-J1966 Grade 1065
Ashless dispersant 0-128 SAE-J1899 Type II
Ashless dispersant 0-123 SAE-J1899 Type III
VI. Turbine engine oils
Aircraft turbine lubricating oil 0-133 MIL-PRF-6081 Grade 1010
Synthetic type 3cSt 0-148 MIL-PRF-7808
Synthetic type 5cSt 0-156 MIL-PRF-23699
VII. Aviation greases
Grease, molybdenum disulfide, high and low G-353
temperatures G-382
General purpose3 G-359
High temperature3 G-359
Ball and roller bearing wide temperature range3 G-354 MIL-PRF-23827
Extreme pressure synthetic G-363 SAE-AMS-G-6032
Hydrocarbon resistant G-392 SAE-AMS-G-4343
Pneumatic system G-366 MIL-G-25537
Helicopter oscillating bearing G-372 MIL-G-25013
Extreme high temperature G-395 MIL-PRF-81322 Grade A
Aircraft, multipurpose G-396 MIL-PRF-83363
Aircraft, PTFE
VIII. Hydraulic fluids
Petroleum base H-515 MIL-PRF-5606
Fire resistant, synthetic H-537 MIL-PRF-83282
IX. Miscellaneous oils
Gear oil light (mineral type) O-153 MIL-PRF-6086 Grade L
Gear oil medium (mineral type) O-155 MIL-PRF-6086 Grade M
General purpose light oil O-142 MIL-PRF-7870
Synthetic oil instruments O-147 MIL-PRF-6085

FIGURE B-5. NATO code number cross-reference.

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NATO APPLICABLE
GENERAL TYPE OF PRODUCT NUMBER1 SPECIFICATION2
X. Specialty products
Liquid, compass, aircraft S-712 MIL-DTL-5020
Deicing and defrosting fluid S-742 SAE-AMS1424 Type I
Isopropanol S-737 TT-I-735 Grade B
Ethanol S-738
Petrolatum S-743 VV-P-236
Molybdenum disulfide lubricant (dry) S-740 SAE-AMS-M-7866
Antiseize graphite-petroleum S-720 SAE-AMS2518
Graphite S-732 SS-G-659
Electrical insulating and sealing compound S-736 SAE-AS8660
Lubricant, solid film airdrying S-749 MIL-L-23398
Molybdenum disulfide silicone base high temperature S-1735 MIL-DTL-25681
Antiseize compound, lead free S-716
Methanol, technical S-747 O-M-232
Fuel system deicing inhibitor S-748 MIL-DTL-85470
Antiseize aircraft oxygen systems S-1736 A-A-58092
Lubricant, solid film, extreme environment S-1737 MIL-PRF-81329
Fuel system icing inhibitor S-1745 MIL-DTL-85470
XI. Preservative compounds
Aircraft engine corrosion preventive oil concentrate C-608 MIL-C-6529 Type I
Aircraft piston engine corrosion preventive oil C-609 MIL-C-6529 Type II
Aircraft turbine engine corrosion preventive oil C-610 MIL-C-6529 Type III
Heavy oil or wax thickened type C-612
Corrosion preventive oil, gas turbine (synthetic base) C-638 MIL-PRF-8188
Hydraulic equipment corrosion preventive oil C-635 MIL-PRF-6083
Hard film cold application C-632 MIL-PRF-16173 Grade 1
Hard film hot application C-633 MIL-C-11796 Grade 1
Soft film cold application C-620 MIL-PRF-16173 Grade 2
Soft film hot application C-627 MIL-C-11796 Grade 3
Hydraulic fluid, rust inhibited, fire resistant, synthetic H-544
1
NATO Numbers are in accordance with STANAG 1135, Interchangeability Chart of NATO Standardized
Fuels, Lubricants and Associated Products.
2
Latest issues apply.
3
There is no U.S. implementing military document for this lubricant.

FIGURE B-5. NATO code number cross-reference – Continued.

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FIGURE B-6. Typical NATO aircraft servicing markings.

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FIGURE B-7. Required markings and symbols.

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FIGURE B-7. Required markings and symbols – Continued.

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FIGURE B-7. Required markings and symbols – Continued.

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FIGURE B-8. Decalcomania – ground here, international symbol.

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APPENDIX B

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

FIGURE B-9. Samples of ground servicing and hazard markings (size and color).

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BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

FIGURE B-9. Samples of ground servicing and hazard markings (size and color) – Continued.

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APPENDIX B

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

FIGURE B-9. Samples of ground servicing and hazard markings (size and color) – Continued.

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APPENDIX B

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

BLACK, COLOR NO. 17038, FOR CONVENTIONALLY PAINTED AIRCRAFT

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

FIGURE B-9. Samples of ground servicing and hazard markings (size and color) – Continued.

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APPENDIX B

OVERHAUL
PAINTED BY: ________________________ ACTIVITY OR
CONTRACTOR AND
THEIR LOCATION
DATE: ___ / ___ / ___
MONTH/DAY/YEAR
PRIMERS: ___________________________
MILITARY
TOPCOAT: __________________________ SPECIFICATIONS

BLACK COLOR NO. 17038 FOR CONVENTIONALLY PAINTED AIRCRAFT;

CONTRASTING GRAY (SEE 5.2.3.1.1) FOR AIRCRAFT WITH A TACTICAL SCHEME

FIGURE B-10. Record of finish marking.

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 MIL-STD-2161C(AS)
APPENDIX C

PAINT SCHEMES AND MARKINGS FOR FIXED WING AIRCRAFT

C.1 SCOPE

C.1.1 Scope. This appendix illustrates the different paint schemes for fixed wing
aircraft. This appendix is a mandatory part of this standard. The information contained herein is
intended for compliance.

C.2 APPLICABLE DOCUMENTS

N/A

C.3 GENERAL REQUIREMENTS

C.3.1 Aircraft paint schemes. The following figures illustrate aircraft finish and marking
specifications for fixed wing aircraft.

***** NOTE: ACTUAL COLORS SHOWN ON ALL ILLUSTRATIONS IN

APPENDICES A-D ARE STRICTLY FOR ILLUSTRATIVE PURPOSE. SPECIFIC
FED-STD-595 COLOR DESIGNATIONS INDICATED ON THE ILLUSTRATIONS
SHALL BE USED. *****

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Lower Vertical Stabilizer 7" 35237
Upper R.H. Wing 12" 35237
B. Model Designation, Lower Aft Fuselage 2" 35237
Acft BUNO 4"
C. National Star Fwd. Fuselage 20" 35237
Upper L.H. Wing 25"
35237
Lower R.H. Wing 25"
36118
D. Call Numbers Vertical Stabilizer 7" 35237
E. Intake Warning Engine Intake Nacelles See Para. 5.2.2.10.1 35237
F. Beware of Blast Engine Exhaust Nacelles 35237
G. Ejection Seat Warning Below Canopy Rail 8" 35237
H. Unit Identifier Upper Aft Fuselage 4" 35237
I. Unit Aircraft Numbers Fwd. Fuselage 12" 35237
J. Rescue Arrow R. H. and L.H. Sides of 24" 35237
Canopy

FIGURE C-1. AV-8B tactical.

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APPENDIX C

FIGURE C-1. AV-8B tactical– Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE *

A. NAVY Aft Fuselage 5" 17038/37038
Lower L. H. Wing 5" 17038/37038
Surface
B. Model Designation Aft Fuselage 2 ½" 17038/37038
(Decal 94743-17)
C. Drone Serial No. Center Fuselage Above 2" 17038/37038
Air Scoop (Decal 94743-18)
D. National Star Fwd. Fuselage NV-STD-158-8 17925/11136/15044
Lower R. H. Wing 17925/11136/15044
Surface 17925/11136/15044
Upper L. H. Wing
Surface
E. Target Air Scoop, Aft Fuselage, (Decal 32962-1) 17038
Upper R. H. & L. H.
Wing Tips, & Vertical
Stabilizer
F. No Lift Center of Tail Cone (Decal 32962-2) 17038

* NOTE: Follow paint scheme provided in manufacturer drawings for other targets, such as
BQM-34S, AQM-37C, GQM-163A and MA-31. See 5.1.6 for additional detail.

FIGURE C-2. BQM-74C/E.

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APPENDIX C

FIGURE C-2. BQM-74C/E – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES NAVY Center Fuselage 12" 17038

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Aft Fuselage 40" 17925/11136/15044

Upper L.H. Wing 40" 17925/11136/15044
Lower R.H. Wing 40" 17925/11136/15044

D. Call Numbers Mid Vertical 12" 17038

Stabilizer
(Outsides Only)

E. Propeller Tips N/A N/A Photoluminescent

F. Anti-Glare Nose & Propeller Hubs N/A 37038

G. Arresting Hook Marking Aft Fuselage Doors 13" 17038

H. Walkway Per Drawing Per Drawing 37038

I. Propeller Warning Band Fwd. Fuselage 3" 11136/17925

(See Figure A-9)

J. Rescue Arrow Fwd. Fuselage Toward 24" 17038

Pilot Compartment Door

K. Anti-Rain Erosion Coating Nose N/A 37038

L. Unit Aircraft Numbers Fwd. Fuselage Per Drawing 17038

M. Unit Identifier Vertical Fin Per Drawing 17038

Upper Right Wing Per Drawing

FIGURE C-3. C-2A.

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APPENDIX C

FIGURE C-3. C-2A – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES NAVY Fwd. Fuselage 16" 17038

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Engine Pod 28" 17925/11136/15044

Upper L.H. Wing 34" 17925/11136/15044
Lower R.H. Wing 34" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 16" 17038

E. Navy Lower L.H. Wing 36" 17038

F. Bare Metal Wing Leading Edge Cap Per Drawing N/A

(Slats); Engine Tail Pipe;
Forward Portion Flap Hinge
Fairings; Leading Edge,
Engine Pylons; Engine Fwd.
Nacelles; & Rub Area,
Horizontal Stabilizer

G. Gold Stripe Center Fuselage 6" Gold

H. Blue Stripe Center Fuselage 12" 15044

I. Unit Aircraft Numbers Wings 16" 17038

Fwd. Fuselage 16"

J. Anti-Glare Fwd. Of Cockpit N/A 37038

K. Unit Identifier Vertical Fin 36" 17038

Upper Right Wing 16" 17038
Lower Left Wing 16" 17038

L. Logo (Optional) Upper Fwd. Fuselage

M. Flag Upper Vertical 26" X 46" 11136

Fin 15044
17925

N. Erosion Boot Nose Per Drawing 17038

O. Activity Name Nose 3" 17038

P. Squadron Designation Forward Fuselage Per Drawing 17038

FIGURE C-4. C-9B (Navy).

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APPENDIX C

FIGURE C-4. C-9B (Navy) – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES Fwd. Fuselage 12" 17038

MARINES

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Engine Pod 25" 17925/11136/15044

Upper L.H. Wing 30" 17925/11136/15044
Lower R.H. Wing 30" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 10" 17038

E. Marines Upper R.H. Wing 17038

Lower L.H. Wing 30"

F. Bare Metal Engine Inlet Nacelle Per Drawing N/A

Engine Exhaust Cowling
Thrust Reverses
Passenger Windows Borders

G. Red Stripe Center Fuselage 6" 11136

H. Yellow Stripe Center Fuselage 12" 13538

I. Unit Aircraft Numbers Fwd. Fuselage 12" 17038

J. Anti-Glare Fwd. of Cockpit N/A 37038

K. Squadron Designation Fwd. Fuselage 6" 17038

L. Logo (Optional) Center Fuselage 34" IAW Squadron

Policy

M. Flag Upper Vertical 25" X 48" 11136

Stabilizer 17925
15044

N. Erosion Boot Nose Per Drawing 17038

FIGURE C-5. C-9B (Marine).

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APPENDIX C

FIGURE C-5. C-9B (Marine) – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE*

A. UNITED STATES NAVY Center Fuselage 8" 17038
NAVY Lower L.H Wing 20” 17038
B. Model Designation, Side Aft Fuselage 2" 17038
Acft BUNO 4"

C. National Star Aft Fuselage 20" 17925/11136/15044

Upper L. H. Wing 20" 17925/11136/15044
Lower R. H. Wing 20" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 12" 17038

Upper R.H. Wing 20” 17038

E. Station Identifier Aft of National Star 3” 17038

F. Accent Stripes Center Fuselage 6" each Upper 15045/Lower 17043
NAVY
G. Flag - United States Upper Vertical Stabilizer See Para. 5.2.7.2 11136/15044/17925

H. Anti-Glare Nose Fwd. of Wind Screen N/A 37038

Inside L. and R. Nacelles

I. Propeller Tips L. and R. Engine Propellers 3"/6"/3" See Fig. A-6 and 5.2.2.10.3.5

J. Propeller Warning Band Fwd. Fuselage 3" wide 11136/17925

K. Hubs Center of L. and R. Engines N/A Bare Polished Metal

L. Propellers L. and R. Engines N/A 37038, See P. A-6

* Equivalent Non- FED-STD-595 colors may be used by contractors painting the aircraft.

FIGURE C-6. UC-12B/F/M Navy.

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APPENDIX C

FIGURE C-6. UC-12B/F/M Navy – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE*

A. UNITED STATES NAVY Not applicable

B. Model Designation, Side Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Not applicable

D. Call Numbers Not applicable

E. Unit Identifier Not applicable

F. Accent Stripes Center Fuselage 6" each Upper 15045/Lower 17043

NAVY

G. Flag - United States Not applicable

H. Anti-Glare Nose Fwd. of Wind Screen N/A 37038

Inside L. and R. Nacelles

I. Propeller Tips L. and R. Engine Propellers 3"/6"/3" See Fig. A-6 and 5.2.2.10.3.5

J. Propeller Warning Band Fwd. Fuselage 3" wide 11136/17925

K. Hubs Center of L. and R. Engines N/A Bare Polished Metal

L. Propellers L. and R. Engines N/A 37038, See P. A-6

* Equivalent Non- FED-STD-595 colors may be used by contractors painting the aircraft.
Follow aircraft drawings for Navy Force Protection variant for specific markings directions.

FIGURE C-7. UC-12B/F/M Navy Force Protection.

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APPENDIX C

FIGURE C-7. UC-12B/F/M Navy Force Protection – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE*

A. UNITED STATES MARINES Center Fuselage 8" 17038

MARINES Lower L.H. Wing 20” 17038

B. Model Designation, Side Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Aft Fuselage 20" 17925/11136/15044

Upper L. H. Wing 20" 17925/11136/15044
Lower R. H. Wing 20" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 12" 17038

Upper R.H. Wing 20” 17038

E. Station Identifier Aft of National Star 3” 17038

F. Accent Stripes
MARINES Center Fuselage 6" each Upper 11136/Lower 17043

G. Flag - United States Upper Vertical Stabilizer See Para. 5.2.7.2 11136/15044/17925

H. Anti-Glare Nose Fwd. of Wind Screen N/A 37038

Inside L. and R. Nacelles

I. Propeller Tips L. and R. Engine Propellers 3"/6"/3" See Fig. A-6 and 5.2.2.10.3.5

J. Propeller Warning Band Fwd. Fuselage 3" wide 11136/17925

K. Hubs Center of L. and R. Engines N/A Bare Polished Metal

L. Propellers L. and R. Engines N/A 37038, See P. A-6

* Equivalent Non-FED-STD-595 colors may be used by contractors painting the aircraft.

FIGURE C-8. UC-12B/F/M Marines.

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APPENDIX C

FIGURE C-8. UC-12B/F/M Marines – Continued.

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 MIL-STD-2161C(AS)
APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE*

A. UNITED STATES MARINES Center Fuselage 8" 35237

MARINES Lower L. H. Wing 20” 35237

B. Model Designation, Side Aft Fuselage 2" 35237

Acft BUNO 4"

C. National Star Aft Fuselage 20" 35237

Upper L. H. Wing 20" 35237
Lower R. H. Wing 20" 35237

D. Call Numbers Vertical Stabilizer 12" 35237

Upper R.H. Wing 20” 35237

E. Station Identifier Aft of National Star 3” 17038

F. Accent Stripes
MARINES Center Fuselage 6" each Upper 35237/Lower 36320

G. Flag - United States N/A

H. Anti-Glare Nose Fwd. of Wind Screen N/A 37038

Inside L. and R. Nacelles

I. Propeller Tips L. and R. Engine Propellers 3"/6"/3" See Fig. A-6 and 5.2.2.10.3.5

J. Propeller Warning Band Fwd. Fuselage 3" wide 11136/17925

K. Propeller L. and R. Side Engine N/A 37038, See P. A-6

L. Hub Front of L. and R. Engine N/A Bare polished metal

* Equivalent Non- FED-STD-595 colors may be used by contractors painting the aircraft.

FIGURE C-9. UC-12B/F/M Marines tactical.

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APPENDIX C

FIGURE C-9. UC-12B/F/M Marines tactical – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE*

A. UNITED STATES NAVY Center Fuselage 8" 17038
NAVY
Lower L.H. wing 20" 17038
B. Model Designation, Side Aft Fuselage 2" 17038
Acft BUNO 4"
C. National Star Aft Fuselage 20" 17925/11136/15044
Upper L. H. Wing 20" 17925/11136/15044
Lower R. H. Wing 20" 17925/11136/15044
D. Call Numbers Vertical Stabilizer 12" 17038
Upper R.H Wing 20" 17038
E. Station Identifier Not applicable
F. Conspicuity Marking Per Drawing See Para. 5.1.1.1 12197
G. Anti-Glare Nose Fwd. of Wind N/A 37038
Screen
Inside L. and R. Nacelles
H. Propeller Tips L. and R. Engine 3"/6"/3" See Fig. A-6 and
Propellers 5.2.2.10.3.5
I. Propellers L. and R. Engines N/A 37038, See Fig. A-6
J. Propeller Warning Band Fwd. Fuselage 3" wide 11136/17925
K. Hub Front of L. and R. Engine N/A Bare polished metal

* Equivalent Non-FED-STD-595 colors may be used by contractors painting the aircraft.

FIGURE C-10. TC-12B high visibility.

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 MIL-STD-2161C(AS)
APPENDIX C

FIGURE C-10. TC-12B high visibility – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. Service Markings Center Fuselage 6 1/2" 17038

Lower L.H. Wing 12" 17038
Upper R.H. Wing 12" 17038

B. Aft BUNO Side Aft Fuselage 6" 17038

C. National Star L.H./R.H. Aft Fuselage 18" 17925/11136/15044

Upper L.H. Wing 18" 17925/11136/15044
Lower R.H. Wing 18" 17925/11136/15044

D. Call Number Vertical Stabilizer 10" 17038

E. Accent Stripe Center Fuselage 4" Upper 2” Navy Blue (15045) /

Lower 2” Gold (17043)

F. Flag -United States Upper Vertical Stabilizer 8" 11136/15044/17925

G. Anti-Glare Nose Fwd of Wind Screen N/A 37038

H. Propeller Tips L. and R. Engines 3"/6"/3" 17925/11136/17925 (See Fig A-6)

I. Propeller Warning Band Fwd. Fuselage 3" 11136 / 17925 (See Fig A-9)

J. Hubs* Center of L. and R. Engines N/A Bare Polished Metal

K. Propellers K. L. and R. Engines N/A 37038 (See Fig A-6)

L. Engine Nacelles L. and R. Engines N/A 17925

M. Engine Exhaust L. and R. Aft Engine Exhausts N/A 37038

N. Escape Hatches Outline Main Cabin Door and Over 2" 16440
Wing Escape

O. Engine Cowling L. and R. Forward Engine N/A 17038

Intake

*Wings are Bare Polished Metal

FIGURE C-11. C-26D.

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APPENDIX C

FIGURE C-11. C-26D – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY/MARINES Not Applicable

B. Aft BUNO Side Aft fuselage 4" 17038*

C. National Star Not Applicable

D. Call Number Not Applicable

E. Unit Identifier Not Applicable

F. Accent Stripe Center Fuselage 4" Upper 2” Navy Blue (15045)* /

Lower 2” Gold (17043)*

G. Flag -United States Not Applicable

H. Anti-Glare Nose Fwd of Wind Screen N/A 37038*
I. Propeller Tips L. and R. Engines 3"/6"/3" 17925/11136/17925* (See Fig
A-6)

J. Propeller Warning Band Fwd. Fuselage 3" 11136 / 17925* (See Fig A-9)
K. Hubs** Polished Metal

L. Propellers L. L. and R. Engines N/A 37038* (See Fig A-6)

M. Engine Nacelles L. and R. Fuselage, Empennage 17925*
N. Engine Exhaust L. and R. Aft Engine Exhausts 37038*
O. Escape Hatches Outline Main Cabin Door and Over 2" 16440*
Wing Escape

P. Engine Cowling L. and R. Forward Engine 17038*

Intake

*Equivalent Non-FED-STD-595 colors may be used by contractors painting the aircraft

** Wings and Wing Flaps are also polished metal

FIGURE C-12. C-26D (Navy Force Protection).

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APPENDIX C

FIGURE C-12. C-26D (Navy Force Protection) – Continued.

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 MIL-STD-2161C(AS)
APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES Upper Center Fuselage 20" 17038
NAVY
B. National Star Aft Fuselage 60" 17875/11136/15044
Upper L. H. Wing 34" 17875/11136/15044
Lower R. H. Wing 34" 17875/11136/15044
C. Call Numbers Vertical Stabilizer 16" 17038
D. NAVY Lower L. H. Wing 36" 17038
E. Gold Stripe Center Fuselage 2" 17043
F. Blue Stripe Center Fuselage 2" 15044
G. Unit Aircraft Forward Fuselage 16" 17038
Number Lower L. H. Wing 16" 17038
Upper R. H. Wing 16" 17038
H. Unit Identifier Vertical Fin 36" 17038
Lower R. H. Wing 36" 17038
Upper R. H. Wing 36" 17038
I. Flag - United States Upper Vertical Fin 24" x 45.6" 17875/11136/15044
J. Activity Name Forward Fuselage 4.8" 17038
K. Squadron Forward Fuselage 8" 17038
Designation

FIGURE C-13. C-40.

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APPENDIX C

FIGURE C-13. C-40 – Continued.

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 MIL-STD-2161C(AS)
APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES Center Fuselage 10" 35237

MARINES

B. Model Designation, Aft Fuselage 2" 35237

Acft BUNO 4"

C. National Star Aft Fuselage 40" 35237

Lower R.H. Wing 40" 36320
Upper L.H. Wing 40" 36320

D. Call Numbers Vertical Stabilizer 30" 35237

E. Propeller Tips1,2 N/A 3"/6"/3" 17925/11136/17925, See P.A-6

F. MARINES Lower L.H. Wing 30" 36320

G. Walkway Top of Wing & Fuselage Per Drawing 35237

H. Propeller Warning Band Fwd. Fuselage 3" 35237/36320

I. Unit Aircraft Numbers Fwd. Fuselage 24" 37038

Upper R.H. Wing 30"
Lower L.H. Wing 30"
J. Unit Identifier Lower R.H. Wing 30" 36320
Upper R.H. Wing 30" 36320
Vertical Stabilizer 36" 35237

K. Anti-Glare Nose Per Drawing 35237

L. Emergency Rescue Wing/Fuselage Joint, 2" 35237

Notice R.H. & L.H. Sides

M. Propellers C/KC-130 L. and R. Engines N/A Polished metal up to tip markings

KC-130J only L. and R. Engines N/A 37038
Note 1: C/KC-130F/R/T aircraft – A single 6-inch wide red (color 11136) or black (color 17038) stripe at the tip of each
propeller blade is allowed.
Note 2: KC-130J aircraft – One 3-inch wide white (color 17925) stripe at the tip of the blade and one 3-inch wide white (color
17925) stripe 9 inches inboard of the tip is allowed.

FIGURE C-14. KC-130T/J Tactical.

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APPENDIX C

FIGURE C-14. KC-130T/J Tactical – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES NAVY Center Fuselage 10" 26492

B. Model Designation L and R Aft fuselage 2" 26492
Acft BUNO 4" 26492

C. National Star Aft Fuselage 40" 26492

Lower R.H. Wing 40" 26492
Upper L.H. Wing 40" 26492

D. Call Number L and R Vertical Stabilizer 30" 26492

1
E. Propeller Tips Blade Tips 3"/6"/3" 17925/11136/17925 (See Fig A-6)
F. NAVY Lower L.H. Wing 30" 26492
G. Walkway Top of Wing and Fuselage Per Drawing 25237

H. Propeller Warning Band Fwd. Fuselage 3" 26492

I. Unit Aircraft Numbers Fwd. Fuselage 24" 26492
Upper R.H. Wing 30" 26492
Lower L.H Wing 30" 26492

J. Unit Identifier Lower R.H. Wing 30" 26492

Upper R.H. Wing 30" 26492
Vertical Stabilizer 30" 26492

K. Anti Glare Nose Per Drawing 25237

L. Emergency Rescue Notice Wing/Fuselage Joint 2" 26492

R.H. & L.H. Sides

M. Propellers: C/KC-130 L. and R. Engines Not applicable Polished metal up to tip marking

Note 1: C/KC-130 F/R/T aircraft – A single 6-inch wide red (color 11136) or black (color 17038) at the tip of each propeller blade is
allowed

FIGURE C-15. C-130T and KC-130 F/R.

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APPENDIX C

FIGURE C-15. C-130T and KC-130 F/R – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 20" 17038

B. Model Designation, Aft Fuselage 2"

Acft BUNO 4" 17038

C. National Star Aft Fuselage 40" 17925/11136/15044

Lower L.H. Wing 40" 17925/11136/15044
Upper R.H. Wing 40" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 12" 17038

E. Anti-Glare Fwd. of Cockpit N/A 37038

F. Beware of Blast Engine Exhaust Cowling 12" 17038

G. Arresting Hook Marking Aft Fuselage 7" 17038

H. Propeller Warning Band Fwd. Fuselage 3" 11136/17925

I. Walkway Top Horizontal Tail Surface N/A IAW Para. 5.1.13

Top Center of Wing

J. Unit Identifier Vertical Stabilizer 30"/36" 17038

K. Unit Aircraft Numbers Fwd. Fuselage 24" 17038

L. Propeller Tips N/A N/A Photoluminescent

M. Rescue Arrow L.H. Side Fuselage 24" 13538

Near Door
Top Fwd. Fuselage Aft 17038
of Cockpit

N. Anti-Rain Erosion Coating Nose N/A 37038

Inlet

FIGURE C-16. E-2C.

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APPENDIX C

FIGURE C-16. E-2C – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 16" 16515
B. Model Designation, Aft Fuselage 2" 17038
Acft BUNO 4" 17038
C. National Star Aft Fuselage 30" BAC-7067/11136/15044
Lower L.H. Wing 30" BAC-7067/11136/15044
Upper R.H. Wing 30" BAC-7067/11136/15044
D. Call Numbers Lower Vertical Tail 12" 17038
E. Intake Warning Engine Intake Nacelles See 5.2.2.10.1 IAW Figure A-15
BAC-7067/11136
F. Beware of Blast Aft Engine Nacelles 7" BAC-7067/11136
G. Rescue Arrows Fuselage (4) 24" 13538/17038
H. Anti-Glare Area Forward of Cockpit N/A 17038
I. Unit Aircraft Numbers Fwd. Fuselage 12" 17038

FIGURE C-17. E-6A/B.

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APPENDIX C

FIGURE C-17. E-6A/B – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 12" 35237, Figure A-15

B. Model Designation, Below National 2" 35237
Acft BUNO Star 4"
C. National Star Aft Fuselage 12" 35237
Lower L.H. Wing 12" 36320, Figure A-1
Upper R.H. Wing 12" 35237
D. Call Numbers Lower Vertical Stabilizer 12" 35237
E. Intake Warning Engine Intake Nacelles See 5.2.2.10.1 35237, Figure A-15
F. Beware of Blast Aft Engine Exhaust 15" 36320
Outlet
G. Arresting Hook Marking Aft Fuselage 13" 36320, Figure A-14
H. Ejection Seat Warning Below Canopy Rail 8" 35237, Figure A-16
I. Walkway Wings Next to Fuselage N/A IAW Para. 5.1.13
J. Unit Identifier Upper R.H. Wing 30" 35237
Vertical Stabilizer 30"
K. Unit Aircraft Numbers Forward Fuselage 12" 35237
Upper R.H. Wing 24"
L. Rescue Arrow R.H. & L.H. Sides of 24" 35237, Figure A-14
Fuselage Aft of Intake
Warning
M. Radome Top of vertical tail N/A 35237

FIGURE C-18. EA-6B tactical.

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APPENDIX C

FIGURE C-18. EA-6B tactical – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

(*See note below)

A. NAVY/MARINES L/R Aft Fuselage 10”/12” 35237 (See Figure A-15)

B. Model Designation, L/R Aft Fuselage 2" 35237 (See Figure A-15)
Acft BUNO L/R Aft Fuselage 4" 35237

C. National Star L/R Fwd. Fuselage 12" 35237 (See Figure A-1)
Lower R.H. Wing 12" 35237
Upper L.H. Wing 12" 35237

D. Intake Chevron & L/R Fwd Engine Intake Stripe width – 3" 35237 (See Figure A-15)
Warnings “Jet” marking – 2" 36375
“Danger” marking – 2" 36375
“Intake” marking – 2" 36375

E. Beware of Blast L/R Aft Fuselage 1" Letters 36375 (See Figure A-8)
4-1/2” x 8” Block 36320

F. Arresting Hook Marking L/R Aft Fuselage IAW Figure A-14 36375/36320 (See Figure A-14)
(T-Shaped Marking)

G. Ejection Seat Warning Upper Canopy Rail 0.5” W x 1.0" H Letters 36320/36375 (See Figure A-16)
8" x 9" Triangle

H. Walkway (non-skid) L/R LEX Not Applicable Not Applicable

I. Unit Identifier Outside Vertical Stabilizers 20" 35237

J. Unit Aircraft Numbers L/R Fwd. Fuselage 10" 37038

(MODEX) L/R T/E Flap 12" 37038
L/R Vertical Fin Cap 10" 37038

K. Arresting Hook Aft Lower Fuselage Per aircraft drawing Alternate bands of contrasting
grays per aircraft drawing

FIGURE C-19. F/A-18A/B/C/D tactical.

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APPENDIX C

FIGURE C-19. F/A-18A/B/C/D tactical – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY/MARINES L/R Aft Fuselage 10”/12" 35237 (See Figure A-15)

B. Model Designation, L/R Aft Fuselage 2" 35237 (See Figure A-15)
Acft BUNO L/R Aft Fuselage 4" 35237

C. National Star L/R Fwd Fuselage 15" 35237 (See Figure A-1)
Lower R/H Wing 15" 35237
Upper L/H Wing 15" 35237

D. Intake Chevron & L/R Fwd Engine Intake 3" Stripe 35237 (See Figure A-15)
Warnings ”Jet” Marking 2" 36375
”Danger” Marking 2" 36375
”Intake” Marking 2" 36375

E. Beware of Blast L/R Aft Fuselage 1" Letters 36375/36320 (See Figure A-8)
4-½" x 8" Block

F. Arresting Hook Marking L/R Aft Fuselage IAW Figure A-14 36375/36320 (See Figure A-14)

G. Ejection Seat Warning L/R Fwd Fuselage (below 0.5" W x 1.0” H Letters 36320/36375 (See Figure A-16)
canopy) 8" x 9" Triangle

H. Unit Aircraft Numbers L/R Fwd Fuselage 10" 37038

(MODEX) L/R T/E Flap 12" 37038
L/R Vertical Fin Cap 10" 37038

I. Unit Identifier O/B Vertical Stabilizers 20” 35237

J. Walkway coating L/R LEX N/A 36320

K. Arresting Hook Aft Lower Fuselage Per aircraft drawing Alternating bands of contrasting
grays per aircraft drawing

FIGURE C-20. F/A-18E/F and EA-18G tactical.

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APPENDIX C

FIGURE C-20. F/A-18E/F and EA-18G tactical – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES L/R Aft Fuselage 7" 36375 (See Figure A-15)

Top R/H & Bottom L/H Wing 7" 36375 (See Figure A-15)
B. Model Designation L/R Aft Fuselage 2" 36375 (See Figure A-15)
Acft BUNO L/R Aft Fuselage 4" 36375
C. National Star L/R Fwd Fuselage 15" 36375 (See Figure A-1)
Lower R/H Wing 15" 36375
Upper L/H Wing 15" 36375

D. Intake Chevron & L/R Fwd Engine Intake 3" Stripe 36375 (See Figure A-15)
Warnings ”Jet” Marking 2" 36375
”Danger” Marking 2" 36375
”Intake” Marking 2" 36375

E. Beware of Blast L/R Aft Fuselage 1" Letters 36375/36375 (See Figure A-8)
4-½" x 8" Block

F. Ejection Seat Warning L/R Fwd Fuselage (below 0.5"W x 1"H Letters 36375 (See Figure A-16)
canopy) 8" x 9" Triangle

G. Unit Aircraft Numbers L/R Fwd Fuselage 6" 36375

(MODEX) L/R T/E Flap 9" 36375
L/R Vertical Fin Cap 9" 36375

H. Unit Identifier O/B Vertical Stabilizers 14” 36375

I. Squadron Designator L/R Center Fuselage 6" 36375

FIGURE C-21. F-35B.

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APPENDIX C

FIGURE C-21. F-35B – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY L/R Aft Fuselage 7" 36375 (See Figure A-15)

B. Model Designation L/R Aft Fuselage 2" 36375 (See Figure A-15)
Acft BUNO L/R Aft Fuselage 4" 36375

C. National Star L/R Fwd Fuselage 15" 36375 (See Figure A-1)
Lower R/H Wing 15" 36375
Upper L/H Wing 15" 36375

D. Intake Chevron & L/R Fwd Engine Intake 3" Stripe 36375 (See Figure A-15)
Warnings ”Jet” Marking 2" 36375
”Danger” Marking 2" 36375
”Intake” Marking 2" 36375

E. Beware of Blast L/R Aft Fuselage 1" Letters 36375/36375 (See Figure A-8)
4-½" x 8" Block

F. Arresting Hook Marking L/R Aft Fuselage 2" 36375

G. Ejection Seat Warning L/R Fwd Fuselage (below 0.5"W x 1"H Letters 36375 (See Figure A-16)
canopy) 8" x 9" Triangle
H. Unit Aircraft Numbers L/R Fwd Fuselage 5" 36375
(MODEX) L/R T/E Flap 12" 36375
L/R Vertical Fin Cap 7.5" 36375

I. Unit Identifier O/B Vertical Stabilizers 14” 36375

FIGURE C-22. F-35C.

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APPENDIX C

FIGURE C-22. F-35C – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 24" 17038

Lower L.H. Wing 24"

B. Model Designation, Aft Fuselage Under 2" 17038

Acft BUNO Horizontal Stabilizer 4"

C. National Star Aft Fuselage 50" 17925/11136/15044

Upper L.H. Wing 50" 17925/11136/15044
Lower R.H. Wing 50" 17925/11136/15044

D. Anti-Glare Fwd. of Cockpit N/A 36440

E. Propeller Warning Band Forward Fuselage 3" 11136/17925

F. Walkway Top Surface of Wings N/A 16440

G. Rescue Arrows Fwd. Fuselage 24" 13538

Aft of Cockpit Windows
Mid Fuselage at Doors
Top of Fuselage Aft of Hatch

H. Call Numbers Vertical Stabilizer 12" 17038

I. Unit Aircraft Numbers Fwd. Fuselage 12" 17038

1 Blades on L. and R. Engines N/A 17925/11136/17925, see Figure A-6
J. Propeller Tips

K. Propellers L. and R. Side Engines N/A Bare metal until tip markings

Note 1: A single 6-inch wide red (color 11136) or black (color 17038) stripe at the tip of each propeller blade is
allowed.

FIGURE C-23. P-3C.

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APPENDIX C

FIGURE C-23. P-3C – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 24" 17038
Lower L.H. Wing 30"
B. Model Designation, Aft Fuselage Under 2" 17038
Acft BUNO Horizontal Stabilizer 4"
C. National Star Aft Fuselage 50" 17925/11136/15044
Upper L.H. Wing 50" 17925/11136/15044
Lower R.H. Wing 50" 17925/11136/15044
D. Anti-Glare Fwd. Of Cockpit N/A 36440
E. Propeller Warning Band Forward Fuselage 3" 11136/17925
F. Walkway Top Surface of Wings N/A 36440
G. Rescue Arrows Fwd. Fuselage Aft of 24" 17038/13538
Cockpit Windows
Mid Fuselage at Doors
Top of Fuselage Aft of
Hatch
H. Call Numbers Vertical Stabilizer 12" 17038
I. Unit Aircraft Numbers Fwd. Fuselage 12" 17038
1
J. Propeller Tips Blades on L. and R. Side N/A 17925/11136/17925, see
Engines Figure A-6
K. Propellers L. and R. Side Engines N/A Bare metal until tip
markings
Note 1: A single 6-inch wide red (color 11136) or black (color 17038) stripe at the tip of each propeller blade is
allowed.

FIGURE C-24. EP-3E, UP-3, VP-3.

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APPENDIX C

FIGURE C-24. EP-3E, UP-3, VP-3 – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY/MARINES Aft Fuselage 12"/10" 17038

Lower L.H. Wing 24"/16"

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Fwd. Fuselage 20" 17925/11136/15044

Lower R.H. Wing 30" 17925/11136/15044
Upper L.H. Wing 30" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 12" 17038

E. Intake Warning See Para 5.2.2.10.1 See Para 5.2.2.10.1 11136

F. Beware of Blast Aft Fuselage See Para 5.2.2.10.2 17925/11136

G. Arresting Hook Warning N/A 4" Alternating Stripes 17038/17925

H. Ejection Seat Below Canopy Rail See Para 5.2.2.10.6.11 IAW Para 5.2.2.10.6.11 (11136)

I. Walkway Wing Adjacent to Fuselage N/A 37038

J. Conspicuity Markings Per Drawing See Para 5.1.1.1 12197

K. Anti-Glare Fwd. of Cockpit N/A 37038

L. Unit Aircraft Numbers Fwd. Fuselage 12" 17038

Lower L.H. Wing 16"
Upper R.H. Wing 16"

M. Unit Identifier Vertical Stabilizer 20" 17038

Lower L.H. Wing 16"
Upper L.H. Wing

N. Rescue Arrow Fwd. Fuselage 24" 17038/13538

FIGURE C-25. T-2C aircraft marking (high visibility).

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APPENDIX C

FIGURE C-25. T-2C aircraft marking (high visibility) – Continued.

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APPENDIX C

1. MARKING1,2 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY/MARINES Aft Fuselage 6" 17038

Lower L.H. Wing 21" 17038
B. Model Designation, Aft Fuselage 2" 17038
Acft BUNO Aft Fuselage 4"
C. National Star Aft Fuselage 18" 17925/11136/15044
Lower R.H. Wing 24" 17925/11136/15044
Upper L.H. Wing 24" 17925/11136/15044
D. Call Numbers Vertical Stabilizer 5.5" 17038
E. Ejection Seat Below Canopy Rail 8” 17038/13538 see Figure A-16
F. Walkway Wing Adjacent to N/A 37038
Fuselage
G. Anti-Glare Fwd. of Cockpit N/A 37038
H. Unit Aircraft Numbers Fwd. Fuselage 6.5" 17038
Lower L.H. Wing 18" 17038
Upper R.H. Wing 21" 17038
I. Unit Identifier Vertical Stabilizer 12" 17038
Upper R.H. Wing 21" 17038
J. Propeller Center Body engine N/A 37038
K. Propeller Tips Propeller blades N/A 17925
L. Hub Center Body of engine N/A Bare polished metal
3
M. Wing/Unit Designator Aft Ventral Fin 4” minimum 17038, See Par. 1.6.3
Note 1: Color requirement established in paragraph 5.1.11 for the speed brake interior surface of the T-6 is
modified to allow use of orange color 12197, with a contrasting black border (color 17038) 3/4”-1” wide.

Note 2: Gloss white, FED-STD-595 color 17925, is the preferred color for the upper fuselage. However, gloss
white, FED-STD-595 color 17865, may be used as an alternate.

Note 3: Applied by Wing or Unit; for example TAW-###, VF-###, etc.

FIGURE C-26. T-6 high visibility.

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APPENDIX C

FIGURE C-26. T-6 high visibility – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 12" 17038

Lower R.H. Wing 24"

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Aft Fuselage 20" 17925/11136/15044

Lower L.H. Wing 20" 17925/11136/15044
Upper R.H. Wing 20" 17925/11136/15044

D. Call Numbers Lower Vertical Stabilizer 12" 17038

E. Propeller Tips N/A 3"/6"/3" 17925/11136/17925, see Figure A-6

F. Anti-Glare Propeller Spinner & Fwd. N/A 37038

& Aft of Cockpit Canopy

G. Walkway Per Drawing N/A 37038

H. Conspicuity Markings Engine Cowling, Wing Tips, Per Drawing 12197

& Vertical Stabilizer

I. "Rescue Other Side" L.H. Side Beneath Canopy Rail ½" Letters 17038

J. Rescue Arrow R.H. Side Beneath Canopy Rail 24" 17038/11136

K. Propellers Center Body of Engine N/A 37038

FIGURE C-27. T-34C aircraft marking (high visibility).

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APPENDIX C

J
G

F F

H C H

FIGURE C-27. T-34C aircraft marking (high visibility) – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY L/R Aft Fuselage 12" 17038

B. Acft BUNO L/R Aft Fuselage 4" 17038

C. National Star L/R Fuselage 18" 17925/11136/15044

Lower R/H Wing 18"
Upper L/H Wing 18" 17925/11136/15044
17925/11136/15044

D. Ejection Seat Warning L/R Fwd Fuselage (below 0.5"W x 1"H Letters
canopy) 8" x 9" Triangle

E. Station or unit name O/B Vertical Stabilizers 8” 17038

F. UNIT Air Craft Numbers L/R fwd fuselage 81/2” 17038

Bottom of fuselage

FIGURE C-28. T-38.

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APPENDIX C

FIGURE C-28. T-38 - Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 16" 17038

Lower L.H. Wing 20"

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Forward Fuselage 20" 17925/11136/15044

Upper L.H. Wing 30" 17925/11136/15044
Lower R.H. Wing 30" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 12" 17038

E. Intake Warning Fwd. Engine Nacelle See Para 5.2.2.10.1 11136/17925

F. Beware of Blast Aft Engine Nacelle See Para 5.2.2.10.2 17038

G. Anti-Glare Radome, Fwd. of Cockpit N/A 37038

H. Walkway Wings & Engine Mounts N/A 37038

Next to Fuselage

I. Conspicuity Markings Per Drawing See Para 5.1.1.1 12197

J. Unit Aircraft Markings Fwd. Fuselage 16" 17038

Lower L.H. Wing 16"
Upper R.H. Wing 20"

K. Unit Identifier Vertical Stabilizer 20" 17038

Lower R.H. Wing 16"
Upper R.H. Wing 24"

L. Rescue Arrow Fwd. Fuselage 24" 17038

Door 13538

M. Bare Metal & Polish Engine Intake Lip N/A N/A, Follow manufacturer
Engine Exhaust Shroud guidelines

FIGURE C-29. T-39G/N high visibility.

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APPENDIX C

FIGURE C-29. T-39G/N high visibility – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 16" 17038

Lower L.H. Wing

B. Model Designation, Side Aft Fuselage 2" 17038

Acft BUNO 4"

C. National Star Aft Fuselage 20" 17925/11136/15044

Upper L.H. Wing 20" 17925/11136/15044
Lower R.H. Wing 20" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 16" 17038

E. Unit Identifier Top Vertical Stabilizer 24" 17038

F. Conspicuity Markings Per Drawing See Para 5.1.1.1 12197

G. Anti-Glare Nose Fwd. of Windscreen N/A 37038

Inside of L&R Nacelles

H. Propeller Tips N/A 3"/6"/3" See Figure A-6 & Par.

5.2.2.10.3.5

I. Propeller Warning Band Fwd. Fuselage 3" Wide 17925/11136

J. Propeller N/A Up to Markings 37038

FIGURE C-30. T-44A high visibility.

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APPENDIX C

FIGURE C-30. T-44A high visibility – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 12"/10" 17038

Lower L.H. Wing 24"/16"

B. Model Designation, Aft Fuselage 2" 17038

Acft BUNO Aft Fuselage 4"

C. National Star Fwd. Fuselage 20" 17925/11136/15044

Lower R.H. Wing 30" 17925/11136/15044
Upper L.H. Wing 30" 17925/11136/15044

D. Call Numbers Vertical Stabilizer 12" 17038

E. Intake Warning See Para. 5.2.2.10.1 See Para. 5.2.2.10.1 11136/17925

F. Beware of Blast Aft Fuselage See Para. 5.2.2.10.2 17925/11136

G. Arresting Hook Warning N/A 4" Alternating Stripes 17038/17925

H. Ejection Seat Below Canopy Rail See Para. 5.2.2.10.6.11 11136

I. Walkway Wing Adjacent to Fuselage N/A 37038

J. Conspicuity Markings Per Drawing See Para. 5.1.1.1 12197

K. Anti-Glare Fwd. of Cockpit N/A 17038

L. Unit Aircraft Numbers Fwd. Fuselage 12" 17038

Lower L.H. Wing 16"
Upper R.H. Wing 16"

M. Unit Identifier Vertical Stabilizer 20" 17038

Lower L.H. Wing 16"
Upper R.H. Wing

FIGURE C-31. T-45A/C aircraft marking (high visibility).

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APPENDIX C

FIGURE C-31. T-45A/C aircraft marking (high visibility) – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. National Star Upper LH Wing, Lower RH Wing, 15” 37038/36099

Nacelle Both Sides
B. Navy Lower LH Wing, Upper RH Wing, 16" 37038
Center Fuselage-, Both Sides 10"
30378
C. Call Number V-Tail Both Sides Outbd Only 8" 30378
D. Walkway Border L and R Upper Wing 0.5" Stripe 36099

FIGURE C-32. MQ-4C.

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APPENDIX C

FIGURE C-32. MQ-4C – Continued.

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APPENDIX C

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Tail Boom 1" 17038

Center Fuselage 6" 17038
Lower L.H. Wing 6" 17038
Upper R.H. Wing 6" 17038

B. Acft BUNO Both Elerudders 4" 17038

C. National Star Center Fuselage 6" 37038/36099

Lower R.H Wing 6" 37038/36099
Upper L.H Wing 6" 37038/36099

D. Unit Aircraft Numbers Fwd. Fuselage 3" 17038

E. Unit Identifier Both Elerudders 4" 17038

F. Propeller Warning Tail Booms 2" 11136

Bands(Factory Applied)

G. Danger Propeller Marking Tail Booms 1" 17038

(Factory Applied)

FIGURE C-33. RQ-7B Shadow.

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APPENDIX C

FIGURE C-33. RQ-7B (Shadow) – Continued.

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APPENDIX C

1. MARKING1 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY L. and R. Aft Fuselage 36" 17038 (See Fig. A-4)
Lower Left Wing 30"
B. Model Designation, L. and R. Aft Fuselage 2" Letter & Number 17038 (See Fig. A-4)
(Under Hor. Stabilizer) Height
Bureau Number Aft fuselage (Centered 2” 4" Height 17038 (See Fig. A-4)
below Model Designation)
C. National Star L. and R. Aft Fuselage 40" Diameter Circle 11136/15044/17925
Upper Left Wing 40” Diameter Circle 11136/15044/17925
Lower Right Wing 40” Diameter Circle 11136/15044/17925
D. Anti-glare Upper Aircraft Nose N/A 36440 (BAC 707 Flat Gray)2
E. Engine Intake Warning L. and R. Side of Each 2" Letter Height 17925 (See Fig. A-8)
Engine Nacelle 3" Chevron Height 11136
F. Walkway Coating Fuselage @ Wing Root N/A 37875 (BAC 5705 Type I)2
G. No Step Aft Edge of Aileron 1" Letter Height 17038
Fwd Edge of Flapperons
H. Rescue Arrows Emergency Exit Locations 24" Long x 2" Ltr. Ht. 13638/17038
I. Beware of Blast Aft Engine Nacelle 2" Letter Height 11136/17925 (See Fig. A-8)
J. Unit Aircraft Numbers TBD TBD TBD

Note 1 – Proposed paint scheme; Final approval pending

Note 2 – BAC ### - Boeing Corporation’s color designation

FIGURE C-34. P-8A (MultiMission Aircraft, MMA) (Proposed).

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APPENDIX C

FIGURE C-34. P-8A (MultiMission Aircraft, MMA)(Proposed) – Continued.

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APPENDIX D

PAINT SCHEMES AND MARKINGS FOR ROTARY WING AIRCRAFT

D.1 SCOPE

D.1.1 Scope. This Appendix illustrates the different paint schemes and markings for
rotary wing aircraft. This appendix is a mandatory part of this standard. The information
contained herein is intended for compliance.

D.2 APPLICABLE DOCUMENTS

N/A

D.3 GENERAL REQUIREMENTS

D.3.1 Aircraft paint schemes. The following figures illustrate paint schemes for rotary
wing aircraft.

***** NOTE: ACTUAL COLORS SHOWN ON ALL ILLUSTRATIONS IN

APPENDICES A-D ARE STRICTLY FOR ILLUSTRATIVE PURPOSE. SPECIFIC
FED-STD-595 COLOR DESIGNATIONS INDICATED ON THE ILLUSTRATIONS
SHALL BE USED. *****

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES R.H. and L.H. of 10" 35237, Figure A-15

Tail Boom

B. Model Designation, Tail Boom 2" 35237

Acft BUNO R.H. and L.H. 4"

C. National Star R.H. and L.H. Side 15" 35237, Figure A-1

D. No Push R.H. and L.H. Side, Aft 35237

Tail Boom Fairing,
Fwd. and Aft of Elevators

E. Intake Warning Fwd. of Intakes 15" 35237, Figure A-15

F. Beware of Blast R.H. and L.H. Sides 5" 35237

G. Tail Rotor Warning Tail Boom 22" 35237

H. Walkway 24" X 6" 35237

I. Rescue Arrow R.H. and L.H. Side 2" 35237, Figure A-14
of Nose Section

J. Rescue Arrow Adjacent to Pilots ¾" 35237

and Gunners Door Handles

K. Unit Aircraft Numbers R.H. and L.H. of Nose Section 10" 35237

L. Unit Identifier R.H. and L.H. Side 10" 35237

FIGURE D-1. AH-1W tactical.

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APPENDIX D

FIGURE D-1. AH-1W tactical – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES R.H. and L.H. of 10" 35237

Tail Boom

B. Model Designation & R.H. and L.H. Vertical Tail 2" 35237
Acft BUNO 6"

C. National Star R.H. and L.H. Side Body 15" 35237

D. Intake Warning R.H. and L.H. Fwd. of Intakes 15" 35237

E. Beware of Blast R.H. and L.H. Sides Fwd of 5" 35237

Engine Exhaust

F. Tail Rotor Warning R.H. and L.H. Tail Boom 22" 35237

G. Walkway Coating Top of Winglets 24" X 60" 35237

Top of fuselage Per drawing

H. Rescue Arrow R.H. and L.H. Side Lower 6.5" 35237

Canopy

I. Unit Aircraft Numbers R.H. and L.H. of Nose Section 10" 35237

J. Unit Identifier R.H. and L.H. Side Upper 10" 35237, See Paragraph 5.2.2.7
Vertical Tail

FIGURE D-2. AH-1Z.

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APPENDIX D

FIGURE D-2. AH-1Z – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Tail Boom/ 8" 35237

Bottom Fuselage 35237, Figure A-15

B. Model Designation, Side 2" 35237

Acft BUNO Tail Boom 4"

C. National Star Aft Fuselage 15" 35237

Bottom Fuselage 15" 35237, Figure A-1

D. Walkway Top Fwd. Fuselage N/A 35237

E. Call Numbers Aft Tail Boom 12" 35237

F. Intake Warning Forward Intake 15" 35237

G. Beware of Blast Engine Exhaust Nacelle 5" 35237

H. Tail Rotor Warning Tail Boom 22" 35237

I. Unit Identifier Tail Boom 10" 35237

Bottom Fuselage

J. Rescue Arrow Fwd. Cockpit Door 24" 35237

FIGURE D-3. UH-1N tactical.

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APPENDIX D

FIGURE D-3. UH-1N tactical – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES R.H. and L.H. Tail Boom 10" 35237, Figure A-15

B. Model Designation, R.H. and L.H. Vertical Tail 2" 35237

Acft BUNO 6"

C. National Star R.H. and L.H. Aft Fuselage 15" 35237

Bottom Fuselage 15" 35237, Figure A-1

D. Walkway Top Fuselage Per drawing 35237

E. Call Numbers R.H. and L.H. Tail Boom 12" 35237

F. Intake Warning R.H. and L.H. Intake 15" 36375/35237

G. Beware of Blast R.H. and L.H. Engine Exhaust 5" 36375/35237

H. Tail Rotor Warning R.H. and L.H. Tail Boom 22" 35237

I. Unit Identifier R.H. and L.H. Vertical Tail 10" 35237

J. Rescue Arrow R.H. and L.H. Fwd. Cockpit 24" 35237

Doors

K. MODEX R.H. and L.H. Lower Side 10" 35247

Doors or Aft of cockpit & Nose

FIGURE D-4. UH-1Y.

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APPENDIX D

FIGURE D-4. UH-1Y – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY/MARINES Tail Boom/ 10" 17038

Bottom Fuselage

B. Model Designation, Side 2" 17038

Acft BUNO Tail Boom 4"

C. National Star Aft Fuselage 15" 17925/11136/15044

Top Fuselage 15" 17925/11136/15044
Bottom Fuselage 15" 17925/11136/15044

D. Intake Warning Forward Intake 15" 11136/17925

E. Beware of Blast Engine Exhaust Nacelle 5" 11136/17925

F. Tail Rotor Warning Tail Boom 22" 13538/31136/17038

G. Anti-Glare Fwd Fuselage N/A 37038

H. Walkway Top Fuselage N/A 37038

I. Unit Aircraft Numbers Mid Fuselage 10" 17038

Bottom Fuselage

J. Unit Identifier Tail Boom 10" 17038

Bottom Fuselage

K. Rescue Arrow Fwd. Cockpit Door 24" 13538/17925

L. Rescue Bottom Aft Fuselage 10" 17038

Top Fwd. Fuselage

M. Abandon Chute Bottom Fuselage 10" 17038

N. Conspicuity Markings Per Drawing N/A 12197

FIGURE D-5. HH/UH-1N non-combat SAR.

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APPENDIX D

FIGURE D-5. HH/UH-1N non-combat SAR – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Aft Fuselage (L. and R. Side) 10" 17925

Bottom Fuselage
R.H. Side 12"

B. Model Designation, Aft of Branch of 2" 17925

Aircraft BUNO Service Markings 4"

C. National Star Forward Lower Fuselage 20" 17925/11136/15044

Top Center Fuselage 20" 17925/11136/15044
Bottom Lower Fwd. Fuselage 20" 17925/11136/15044

D. Call Numbers Aft Pylon 9" 17038

E. Rescue Upper Fuselage 12" 17038

Lower Fuselage 12" 17038
Stubwing 8" 17925/17038
F. Abandon Chute (2 separate Lower Fuselage 12" 17925
lines, one word per line)
G. Walkway Top of Fuselage (both sides of N/A 37038
tunnel and in front of engine
intakes)
Top of Stubwing and Torque Box

H. Conspicuity Markings Per Drawing N/A 12197

I. Squadron Designation Aft Fuselage 6" 17925

Aft Pylon: Shadow Boxed 4” 17925/17038

J. Unit Aircraft Numbers Upper Center Fuselage 20" 17925

Nose Electronics
Compartment Door

K. Unit Identifier Top of Aft Pylon 24" 17925

L. Rescue Arrows Fwd. and Center of Fuselage 4”w x 18"l 17038/13538

Rescue Hatch (if installed)

FIGURE D-6. HH-46E high visibility SAR.

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APPENDIX D

FIGURE D-6. HH-46E high visibility SAR – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Aft Fuselage (L. and R. Side) 10" 35237

Bottom Fuselage 12" 35237, Figure A-15

B. Model Designation, Aft of MARINES Markings 2" 35237

Acft BUNO 4" 35237

C. National Star Forward Lower Fuselage 20" 35237

Top Center Fuselage 20" 36375
Bottom Lower Fwd Fuselage 20" 35237, Figure A-1

D. Walkway Top of Fuselage (both sides of tunnel N/A 35237

and in front of intakes)
Top of Stubwings and Torque Box N/A 35237

E. Call Numbers Aft Pylon 9" 35237

F. Unit Aircraft Numbers Upper Center Fuselage 20"

Nose Electronic 36375
Compartment Door

G. Unit Identifier Top of Aft Pylon 24" 35237

H. Squadron Designation Aft Fuselage 6" 35237

I. Rescue Arrow Fwd. & Center Fuselage 4"w x 18"l 35237, Figure A-14 for other
dimensions

FIGURE D-7. CH-46E tactical.

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APPENDIX D

FIGURE D-7. CH-46E tactical – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage (L.H. & R.H.) 20" 35237

B. Model Designation, Aft Fuselage (L.H. & R.H.) 2" 35237

Acft BUNO 4"

C. National Star Aft Fuselage (L.H. & R.H.) 20" 35237

Horizontal Stabilizer 20" 35237
Bottom Center Fuselage 20" 35237

D. Unit Aircraft Number Center Fuselage (L.H. & R.H.) 18" 35237
(MODEX) Nose 18” 35237

E. Call Numbers Upper Tail Boom (L.H. & R.H.) 6" 35237

F. Intake Warning Engine Intake Nacelles (L.H. & 2” Letters 35237

R.H.) 36” (Length)
4” Chevron

G. Beware of Blast Lower Aft Section of 2" Letters 35237

Engine Nacelles (L.H. & R.H.)

H. Tail Rotor Warning Aft Tail Boom (L.H. & R.H.) 24" 35237

I. Walkway Per Drawing N/A IAW Para 5.1.13

J. Keep Clear Exhaust Upper Fwd. Fuselage 1” Letters 35237

Between Exhaust Ducts 1-1/2” Arrows
L.H. Side

K. Rescue Arrow Fwd Fuselage (L.H. & R.H.) 24” 35237

L. Unit Identifier Tail Pylon (L.H. & R.H.) 22” 35237

M. Station or Unit Name Tail Pylon (L.H. & R.H.) 6” 35237, See Par. 5.2.2.8
(Shore-based A/C Only)

N. Squadron Designation Center Fuselage (L.H. & R.H.) 6” 35237, See Par. 5.2.6.2

FIGURE D-8. MH-53E Navy tactical.

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APPENDIX D

FIGURE D-8. MH-53E Navy tactical – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Aft Fuselage (L.H. & R.H.) 20" 35237, Figure A-15

B. Model Designation, Aft Fuselage (L.H. & R.H.) 2" 35237

Acft BUNO 4"

C. National Star Aft Fuselage (L.H. & R.H.) 20" 35237

Horizontal Stabilizer 20" 36375
Bottom Center Fuselage 20" 35237, Figure A-1

D. Unit Aircraft Number Center Fuselage (L.H. & R.H.) 18" 35237
(MODEX) Nose 18” 36375

E. Call Numbers Upper Tail Boom (L.H. & R.H.) 6" 35237

F. Intake Warning Engine Intake Nacelles (L.H. & 2” Letters 35237

R.H.) 36” (Length)
4” Chevron

G. Beware of Blast Lower Aft Section of 2" Letters 35237

Engine Nacelles (L.H. & R.H.)

H. Tail Rotor Warning Aft Tail Boom (L.H. & R.H.) 24" 35237

I. Walkway Per Drawing N/A 35237

J. Keep Clear Exhaust Upper Fwd. Fuselage 1” Letters 35237

Between Exhaust Ducts 1-1/2” Arrows
L.H. Side

K. Rescue Arrow Fwd Fuselage (L.H. & R.H.) 24” 35237

L. Unit Identifier Tail Pylon (L.H. & R.H.) 22” 35237

M. Station or Unit Name Tail Pylon (L.H. & R.H.) 6” 35237, See Par. 5.2.2.8
(Shore-based A/C Only)

N. Squadron Designation Center Fuselage (L.H. & R.H.) 6” 35237, See Par. 5.2.6.2

FIGURE D-9. CH-53E Marine tactical.

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APPENDIX D

FIGURE D-9. CH-53E Marine tactical – Continued.

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 MIL-STD-2161C(AS)
APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/COLOR

A. NAVY Tail Boom 6" 17038

B. Model Designation, Both Sides of 2" 17038

Acft BUNO Tail Boom 4"

C. National Star Aft Fuselage 10" 17925/11136/15044

Bottom Fuselage 10" 17925/11136/15044

D. Tail Boom Warning Tail Boom 22" 31136/37038

E. Anti-Glare 37038

F. Arctic As per Drawing 12197

Markings/Conspicuity

G. Unit Identifying Letters Tail Boom (IAW Para. 5.2.3) 17038

FIGURE D-10. TH-57B/C high visibility.

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APPENDIX D

FIGURE D-10. TH-57B/C high visibility – Continued.

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1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Aft Fuselage 12" 35237

B. Model Designation, Side 2" 35237

Acft BUNO Tail Boom Aft 4" 35237

C. National Star Mid Fuselage 12" 35237

Fwd. Top Fuselage 12" 36320
Aft Bottom Fuselage 12" 36320

D. Intake Warning Forward Intake Nacelle 20" Background 35237

2" Letters 36320

E. Beware of Blast Engine Exhaust Nacelle 1" Letters 35237

F. Tail Rotor Warning Tail Boom 33" 35237

G. Anti-Glare Fwd. of Cockpit N/A

H. Walkway Per Drawing N/A IAW Para 5.2.3

I. Unit Identifier Upper Tail Boom 12" IAW Para 5.2.3

J. Rescue Arrow Cockpit Door and 24" Background 35237

Center of Fuselage Letters 36320

Note 1. There are minor differences between aircraft models around the engine exhaust area
(marking “K”). Follow drawings for specific aircraft model for paint color configuration around
this area.

FIGURE D-11. SH-60B/F, CH-60S, MH-60 R/S and HH-60H tactical.

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FIGURE D-11. SH-60B/F, CH-60S, MH-60 R/S and HH-60H tactical – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. UNITED STATES NAVY Fuselage Tail Boom 8" 17925

B. Model Designation L.H. & R.H Side, Aft Lower Tail Rotor 2" 17925

Aircraft BUNO 4"

C. National Star Lower Center Fuselage 30" 17925/11136/15044

Upper Horizontal Tail 25" 17925/11136/15044

D. Wheel Wells N/A N/A 17925

E. Fleet Commander Stars L.H. & R.H. Avionics Access Panels 6" high stars 17925

F. Tail Rotor Warning L.H. & R.H. Side, Vertical Tail 29" x 9" (Per SH-60F VIP Paint See Fig. A-12 for colors
Scheme Deviation, dated 8 Nov
2005)

G. Flag L.H & R.H. Engine Work Plarforms 18" X 34" 11136
15044
17925

H. Unit Name L.H. & R.H. Side, Below Lower Stripe 6" 17925

I. Aircraft Side Number L.H. & R.H. Side, Float Bag Covers 6" 17925
Avionics Nose Door 8"

J. Unit Identifier L.H. & R.H. Side, Below Tail Rotor 12" 17925
Gear Box Access Panel

K. Accent Stripe -Upper Upper – Approx. 2” Above Avionics Stripe is made up of two ¾" 17925
lines separated by ½"
(See Aircraft Drawing)

L. Accent Stripe- Lower Lower – Along Bottom Edge of Pilot Stripe is made up of two ¾" 17925
Door lines separated by ½"
(See Aircraft Drawing)

I
H
D 17925

Drab Green*

*Non-FED-STD-595 color; refers to Raytheon Aircraft Services color J07902

FIGURE D-12. SH-60F VIP transport.

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APPENDIX D

I
88

17925

Drab Green*

FIGURE D-12. SH-60F VIP transport – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. NAVY Bottom Fwd (optional config.) 12" 12127

B. Model Designation, Side 2" 17038

Acft BUNO Tail Boom Aft 4" 17038

C. National Star Mid Fuselage 12" 17925/11136/15044

Fwd. Top Fuselage 12" 17925/11136/15044
Aft Bottom Fuselage 12" 17925/11136/15044

D. Intake Warning Forward Intake Nacelle 20" Background 11136

2" Letters 17925

E. Beware of Blast See Notes 1 and 2 See Notes 1 and 2

F. Tail Rotor Warning Tail Boom 22" 11136 (See Figure A.12)

G. Anti-Glare See Notes 1 and 2 See Notes 1 and 2

H. Walkway See Notes 1 and 2 See Notes 1 and 2

I. Unit Identifier See Notes 1 and 2 See Notes 1 and 2

J. Rescue Arrow Cockpit Door 24" Background 13538

Letters 17038

K. RESCUE Bottom Aft (optional config.) 10” 12197

Note 1: Follow Sikorsky drawing #96005-00117 for paint, decal, and stencil requirements not
shown in the figure for the MH-60S. For this aircraft, bulkhead area aft of engine exhaust is
painted flat black (as shown in schematic below).

Note 2: Follow Sikorsky drawing #7005-80201 for paint, decal, and stencil requirements not
shown in the figure for the SH-60F. For this aircraft, bulkhead area aft of engine exhaust is
painted white. Follow manufacturer drawing.

Engine exhaust
D bulkhead area

C
JE
T B
E
T AK
IN

RE
SC
UE
F

J
12197
17925

FIGURE D-13. MH-60S and SH-60F Search and Rescue (SAR).

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APPENDIX D

K
C

Optional bottom paint configuration (See Note 1)

FIGURE D-13. MH-60S Search and Rescue (SAR) – Continued.

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APPENDIX D

1. MARKING 2. LOCATION 3. SIZE 4. COLOR NO/CODE

A. MARINES Aft Fuselage 12" 35237

B. Model Designation, Aft Fuselage 2" 35237

Acft BUNO 4"

C. National Star Aft Fuselage 12" 35237

Lower R.H. Wing 12" 35237
Upper L.H. Wing 12" 36375

D. Rescue Arrow Forward Fuselage 24" 35237

Center Fuselage 24" 35237

E. Call Number Lower Vertical Tails 12" 35237

F. Intake Warning Engine Intake Nacelles 16" 35237

FIGURE D-14. MV-22 tactical.

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FIGURE D-14. MV-22 tactical – Continued.

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APPENDIX E

NATIONAL INSIGNIAS FOR FOREIGN AIRCRAFT

E.1 SCOPE

E.1.1 Scope. This Appendix illustrates insignias of foreign countries. This Appendix is
a mandatory part of this standard. The information contained herein is intended for compliance.

E.2 APPLICABLE DOCUMENTS

N/A

E.3 GENERAL REQUIREMENTS

E.3.1 Foreign country national insignias. The following figures illustrate national
insignias for foreign countries.

***** NOTE: FOR FOREIGN AIRCRAFT, MARKINGS SHALL BE

PROVIDED TO THE U.S. NAVY PROCURING ACTIVITY BY THE FOREIGN
COUNTRY PROCURING THE AIRCRAFT OF INTEREST.*****

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APPENDIX E

FIGURE E-1. National insignia of Portugal (flash and numbers).

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FIGURE E-2. National insignia of Argentina.

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APPENDIX E

FIGURE E-3. National insignia of Mexico (flash).

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FIGURE E-4. National insignia of Great Britain.

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APPENDIX E

FIGURE E-5. National insignia of Canada (roundel) marking I.

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APPENDIX E

FIGURE E-6. National insignia of Canada (flash) marking II.

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APPENDIX E

FIGURE E-7. National insignia of Netherlands (roundel) marking I.

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APPENDIX E

FIGURE E-8. National insignia of Netherlands (flash) marking II.

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APPENDIX E

FIGURE E-9. National insignia of France (cocarde) marking I (anchor superimposed when
planes are intended for French Navy).

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APPENDIX E

FIGURE E-10. National insignia of France (flash) marking II.

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APPENDIX E

FIGURE E-11. National insignia of Australia (roundel) marking I.

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APPENDIX E

FIGURE E-12. National insignia of Australia (flash) marking II.

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APPENDIX E

FIGURE E-13. National insignia of Japan (roundel).

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APPENDIX E

FIGURE E-14. National insignia of Japan (kanji characters).

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APPENDIX E

FIGURE E-15. National insignia of Uruguay (roundel).

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APPENDIX E

FIGURE E-16. National insignia of Uruguay.

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APPENDIX E

FIGURE E-17. National insignia of Brazil (star) marking I.

FIGURE E-18. National insignia of Brazil (flash) marking II.

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APPENDIX E

FIGURE E-19. National insignia of Federal Republic of Germany.

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APPENDIX E

FIGURE E-20. National insignia of Federal Republic of Germany.

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APPENDIX E

FIGURE E-21. National insignia of Italy (cocarde).

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APPENDIX E

FIGURE E-22. National insignia of New Zealand (roundel) marking I.

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APPENDIX E

FIGURE E-23. National insignia of New Zealand (roundel) marking II.

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 MIL-STD-2161C(AS)

CONCLUDING MATERIAL

Preparing activity:
Navy - AS
(Project MFFP-2014-002)

NOTE: The activities listed above were interested in this document as of the date of this
document. Since organizations and responsibilities can change, you should verify the currency
of the information above using the ASSIST Online database at https://assist.dla.mil.

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