ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

CHAPTER

11
PLACARDS
AND
MARKINGS
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4
CHAPTER 11

PLACARDS AND MARKINGS

LIST OF EFFECTIVE PAGES

CHAPTER/ REV.
SECTION PAGE DATE NO.
11-TITLE
11-LEP 1/2 NOV 30/08 19
11-CONTENTS 1/2 OCT 31/06 17
11-20-00 Fig. 1 0 NOV 30/08 19
1/2 NOV 30/08 19
11-30-00 Fig. 1 0 OCT 31/06 17
1 OCT 31/06 17
2 OCT 31/06 17
3 OCT 31/06 17
4 OCT 31/06 17
5 OCT 31/06 17
6 OCT 31/06 17

11 - LIST OF EFFECTIVE PAGES

Page 1/2
NOV 30/08
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4
CHAPTER 11

PLACARDS AND MARKINGS

TABLE OF CONTENTS

CHAPTER/
SUBJECT SECTION FIGURE

EXTERIOR PLACARDS 11-20-00 1

INTERIOR PLACARDS 11-30-00 1

11 - CONTENTS
Page 1/2
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

6
7

5A

4
3A

9
A
10
11

12
11

13

14
15

SLIDING DOOR
(TYPICAL)
NOTE

USED ON 76106−08050−043 DAMPER

RESERVOIR ASSEMBLIES.
CC0336_1B
SA

EXTERIOR PLACARDS /SHEET 1/

11-20-00 FIGURE 1
FIGURE 1 PAGE 0
NOV 30/08
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

MAX LOAD 600 LBS

SS9065−391
1
R

Model No.

EXIT HOOK LIMIT Serial No.

Type Cert. No.

3300 LBS Prod. Cert. No.

1496.88 KG SS9013−1530 Sikorsky

LIFT HANDLE A United Technologies Company

SS9013−1530 SS9026−2
TO OPEN SS9013−1447
12 xxxx−xxxxx

SS9013−1447 SS9026−1, SS9026−2

11 2

TO FILL LH AND RH FUEL TANKS FROM LH FILLER

JET A, JET A1, 1) OPEN LH FUEL FILLER CAP
2) PULL NYLON LANYARD FOR ACCESS TO PULL RING
JP5, OR JP−8 FUEL 3) LIFT RING UPWARDS THEN PULL OUTBOARD
(APPROXIMATELY 2 INCHES) LOWER ROD AND
FOR OPERATIONS BELOW SLOWLY ALLOW ROD TO MOVE INBOARD UNTIL
4OC (40O F) ANTI−ICE CAUGHT ON OPEN DETENT
ADDITIVE IS REQUIRED. 4) FILL BOTH TANKS TO DESIRED LEVEL BUT NOT
SEE FLIGHT MANUAL FOR LESS THAN 50 GALLONS PER TANK
SPECIFIC INSTRUCTIONS 5) LIFT RING UPWARDS UNTIL HOLD OPEN DETENT
SS9140−0155 SS9013−2653 LH RELEASES AND ROD COMMENCES TO MOVE
SS9013−2652 RH INBOARD
SS9140−0155 13 6) RELEASE RING
10 7) SECURE LH FUEL FILLER CAP

SS9013−2645
3
GROUND HERE
SS9065−054
SS9065−054

WINDOW JETTISON
9 FULL
PUSH BUTTON
OIL CAPACITY DRY: 1.0 LITERS (.26 GALS) LOW
DRAINABLE OIL: 1.0 LITERS (.26 GALS) TURN HANDLE UP
TYPE OF OIL: MIL−L−23699. MIL−L−21260.
OR DEXRON III 76106−08050−104
FOR TEMPERATURE LIMITS REFER TO 3A
SS9013−2651 (SEE NOTE)
MAINTENANCE MANUAL
33776−58901−101 14
33776−58901−101 LOCK
8 OIL CAPACITY DRY: 4.8 LITERS (1.27 GALS)
DRAINABLE OIL: 4.8 LITERS (1.27 GALS)
PITCH TYPE OF OIL: MIL−L−23699. OR MIL−L−7808
BEAM
FOR TEMPERATURE LIMITS REFER TO
END
MAINTENANCE MANUAL
UNLOCK 33776−58901−104

6410−30401−104 33776−58901−104
7 1 4
SS9013−1486 LH
OIL CAPACITY DRY: 0.9 LITERS (.246 GALS) SS9013−1587 RH
DRAINABLE OIL: 0.9 LITERS (.246 GALS) 15
TYPE OF OIL: MIL−L−23699. MIL−L−21260. IN CASE OF FIRE
OR DEXRON III
FOR TEMPERATURE LIMITS REFER TO
CAUTION ECU EXHAUST FIGHT FIRE HERE SS9067−0102
MAINTENANCE MANUAL SS9067−0102
33776−58901−102
SS9013−1266
5
33776−58901−102 SS9013−1266 CC0336_2C
6 5A SA

EXTERIOR PLACARDS /SHEET 2/

11-20-00 FIGURE 1
FIGURE 1 PAGE 1/2
NOV 30/08
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

22
21 21A 20 21
20 20
21A
19
18
17
16
23
15
21
14
20
57
12 24

11 30
10 28
9A
27
9
25
8
26
7
29
6
5 24
31
A 4
32
24
3 33 B
34
35
2 36
1 37
38
B
35
33
41
38 34 40 39

42
43
44
45
46
47

SLIDING DOOR
(TYPICAL)
CC0337_1D
SA

INTERIOR PLACARDS /SHEET 1/

11-30-00 FIGURE 1
FIGURE 1 PAGE 0
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

48 49 50
51 51
52 52
#2 ENG FIRE
#2 ENG OUT PRESS−TONE
OFF VNE PLACARD #1 ENG FIRE
MASTER CAUTION PRESS−TONE
OFF
PRESS−TONE #1 ENG OUT
#1 ENG OUT PRESS TO RESET OFF PRESS−TONE MASTER CAUTION
#1 ENG FIRE PRESS−TONE
OFF OFF PRESS TO RESET #2 ENG OUT
OFF
PRESS−TONE PRESS−TONE #2 ENG FIRE
OFF PRESS−TONE
OFF

96 98 96 98
95 95 TRIM VG RMT AP1 AP2 RAWS
75 75

55 100 55 100 FAIL ERECT TRIM CLTV DCPL ALT

#1 SERV0 #1 DC #1 ENG #1 ENG MAIN XMSN SMOKE DET #2 ENG #2 ENG #2 DC #2 SERVO
35 BV 35 BV
COMP FD SYSTEM GEN OIL PRESS FUEL PRESS OIL PRESS BAGGAGE FUEL PRESS OIL PRESS GEN SYSTEM
TRIM
MON CMD 15 15
COMP FD
FAIL RESET BARS BATT FEED #1 FUEL #1 ENG MAIN XMSN INT GB #2 ENG #2 FUEL ESS BUS ROTOR
BATT HOT FAULT LOW CHIP OIL HOT CHIP/HOT CHIP LOW VOLTS LOW BRAKE MON CMD
LOC VG2 DCL RESET BARS
AC NO. 2 #1 ENG MAIN XMSN TAIL GB #2 ENG ADELT LOC VG2 DCL
BATT OFF EMER PWR GOOD
GEN INV FAIL ANTI−ICE CHIP CHIP/HOT ANTI−ICE SAFE BRT
VG RMT AP1 AP2 RAWS
GS 20 20 T
20
SG ATT HDG BATTERY 180
COL REV REV BUS TIE AC GEN WINDSHEILD NO. 1 CPLT PITOT PLT PITOT E OFF ARM
TEST GS 20 20
ERECT TRIM ALT REV DAFCS DOOR OPEN S SG ATT HDG
CLTV DCPL OPEN BEARING HOT INV FAIL HEAT HEAT
T 160 COL
10 10 REV REV REV
#1 ENG NIGHTSUN ENG FLOTATION HOOK #2 ENG HOOK DIM
ANTI−ICE ON CPLT F/D N0T ST0WED BLEED AIR ARMED ARMED ANTI−ICE ON OPEN
5 7 5 7 40 10 10
3 9 3 9 140

KNOTS
1 11 1 11
20 10 10 0 120
180 60 10 10
9 1 0
160 20 9 1
20 M
100 80

40 20 20 M
DH 8 2 2
AGL FT/MIN X 100 DH
0 0 12 0 0 ALT
140 8 2
200 DH 150 RA 1

0 0 12 0 0 ALT
KNOTS
KNOTS SET 200 DH 150 RA
7 3
120 7 3
60 1
6 4 FUEL FLOW FUEL FLOW
100 80 2
5 0 6 4
3
RNAV WARN 10 5
120
ON OFF DR WPT
110 20
045 LBS/HR LBS/HR
DTRK CHMP2 LOR

2
MAN 30 DTRK CHMP2 045 LOR
076 1 NM TUNE 100
ENABLE

1
AUTO PERCENT 076 1 NM
0 6 TORQUE 40
3 90
10 E 2 3 6
120 1 CRT FAN 50 2
N

RANGE 80 E
33 3 FUEL FAIL ENG ENG 1

N
110 20 VERTICAL XFEED OIL OIL 70 60
.5
12
33

1 2
SPEED 3 .5 VERTICAL

30
33

6
3

12
33
T P T P
2

30 UP SPEED
100 0 3

30
UP
15
30

6
LH DOOR
1

PARK

27
PERCENT

9
0

15
30
DOWN BRAKE
90 TORQUE 40 3 RH DOOR ON VRM MNU X10 X10
.5 1000 FT PER MIN DOWN 3

27
W

9
12
.5 1000 FT PER MIN

24

W
50

S
80 LOR 24 21
VO
60 1

R
LOR 21

12
70 R

24
15 24

VO
2 21 CR TGT
8 VO #1 ENG #2 ENG 1
2

R
R 15

VO
HDG GSPD 21 OVSPD OVSPD
8
045 140 KTS HDG GSPD
HYD XMSN
TRB SCT 045 140 KTS
PRESS OIL

N2
1 2 T P
130 0 WX/RCT 1 PULL GAIN
+ BRT
DH GMAP TILT
120 10 HDG VS ALT VAR X10
DH
WX
N2
2 0 HDG VS ALT
ON ON ON 130 0
20 TST
ROTOR SBY − 120 10
MIN MAX OFF ON ON ON
1 2

NAV ILS DECEL

FULL APR GSPD
30 MAP HOV NAV LNAV 20
R

20 ARM CAP ARM GS ARM CAP NAV ILS DECEL ROTOR FULL APR GSPD
ARC HOV TTG 20
15 MAP HOV NAV LNAV

1 2
PERCENT SLV PULL FOR CLR ZONE MAIN
90 40 ARM CAP ARM GS ARM CAP ARC HOV TTG 15
RPM 10 RAD ALT FUEL 30

R
ARM CAP ON ARM CAP PULL FOR VAR BOTH 10
LNAV LNAV 5 .75 FUEL REMAINING
RAD ALT
DF 4 5
80 DF
3 2 1
50 ADF RAD BCN .50 1.00
PERCENT
ADF VDR APP IAS ALT PRE ARM CAP ON ARM CAP 90 40 LNAV LNAV 4
70 60 LBS RPM DF ADF DF 3 2 1
NAV1 NAV2
TEST MAX .25 1.25 . VDR APP IAS ALT PRE
ADF
TEST
ARM CAP ON ON 80 50
MIN AUTO LBSX100 NAV1 NAV2
OFF OFF OFF OFF 70 60
BRG EADI DH EMSI MX BRG BC SBY GA ARM CAP ON ON
BCN GAIN BCN CODE FUNCTION MISSED OFF OFF OFF OFF
APR PT SET BC SBY GA BRG EADI DH EMSI MX BRG
WC−701 BEACON CONTROLLER

RADIO TRANSMIT ICS

UHF VHF1 VHF2 M/FM L/FM HF POLICE C’PIT
55
60
5
TEST PANEL RADIO TRANSMIT ICS
UHF VHF1 VHF2 M/FM L/FM HF POLICE C’PIT
11
12
1
GEN 1 GEN 2 LDG GEAR 60
50 10 GND GND 55 5
10 2 FAULT FAULT AC GEN
COMM RECEIVER VOL 12
UNDER
UHF VHF1 VHF2 M/FM L/FM HF POLICE ICS VOLT L R 50
11 1
10 COMM RECEIVER VOL
45 9 3 15
N 10 2 UHF VHF1 VHF2 M/FM L/FM HF POLICE ICS

8 4 O UNLKD 45 9 3 15
40 20 F
NAV RECEIVE 7 5 F
6 OVER OVER
NAV1 NAV2 DME1 DME2 ADF EMG IN RADIO
VOLT VOLT EMER DN NORMAL 8 4 NAV RECEIVE
FLOOR

35 25 40 20
OVER NAV1 NAV2 DME1 DME2 ADF POLICE EMG IN RADIO
30 7 5

FLOOR
VOLT 6
35 25
OUT ICS
FEEDER 30
FAULT UP OUT ICS
POLICE
UHF VHF1 VHF2 M/FM L/FM HF XMIT RCVR FLOATS TEST O POLICE
F N1/T5 FUEL
TEST F DIGITS GAGE UHF VHF1 VHF2 M/FM L/FM HF XMIT RCVR
DN TEST

WARN

NAV1 MB−1 NAV2 MB−2 DME1 DME2 ADF MB SENS NORM

1 TEST 2
HI
NAV1 MB−1 NAV2 MB−2 DME1 DME2 ADF MB SENS
LO HI

55 54
LDG GEAR UP RADIO CALL
LO
PUSH TO RESET
RADIO CALL LDG GEAR UP
PUSH TO RESET

56 INSTRUMENT PANEL 53
(TYPICAL)

A
STRUT
NOSE LANDING GEAR "X" DIM

STRUT SERVICING INSTRUCTIONS

CHECK STRUT EXTENSION:
FULLY COMP
25
+
− 12 IN
PRESSURE
+
− 10 PSIG

1540
1950
RESERVOIR
50 1260
1. IF STRUT IS FULLY COMPRESSED SEE 75 1060
MAINTENANCE HANDBOOK! 100 910
125 795
2. REMOVE AIR VALVE CAP AND ATTACH PRESSURE GAGE
150 705
3. LOOSEN SWIVEL NUT AND MEASURE AIR PRESSURE 175 635
4. CHECK CHART FOR CORRESPONDING "X" DIMENSION 200 575
IF MEASURED "X" VALUE IS NOT WITHIN + 225 525
− 25 PROCEED 250 486
WITH STEPS 5 THRU 11 (IN THIS SEQUENCE) 275 450
FOR PROPER SERVICING (IF STRUT IS WITHIN LIMITS 300 415 0
PERFORM STEP 10 ONLY) 350
400
365
325
THAN 0 C (32 F) & WINDSHIELD 0

SERVICING, (WEIGHT OF AIRCRAFT ON TIRES) 450 290

500 265
(BOTH FLUID & PRESSURE MUST CHECK TO PROPERLY 550 240
SERVICE STRUT)
5. REMOVE AIR VALVE CAP AND LOOSEN SWIVEL NUT TO 650
600

700
205
225

190
O−C−1901 (ISOPROPYL ALCOHOL)
SLOWLY BLEED OFF PRESSURE UNTIL STRUT BOTTOMS
IN FULLY COMPRESSED POSITION, THEN LOOSEN SWIVEL
NUT FULL OPEN (2 1/2 TURNS MAX) LEAVE OPEN.
750

850
800
180

160
170 MIXED WITH EQUAL PARTS WATER
0
6. REMOVE AIR VALVE FROM STRUT AND ATTACH FILLER HOSE
FILL STRUT WITH HYDRAULIC FLUID * TO LEVEL OF
950
900

FULLY EXT
140
150

135
FOR WEATHER BELOW 0 C (32 F). 0

SERVICE OPENING WAIT 5 MINUTES CHECK FLUID LEVEL

AND IF NECESSARY REFILL TO LEVEL OF SERVICE OPENING. SS9013−2231
7. REPLACE AIR VALVE AT TOP OF STRUT AND TIGHTEN TO
MAINTAIN PRESSURE
50−70 INCH LBS. SECURE WITH LOCKWIRE.
8. ATTACH HOSE FROM NITROGEN OR AIR BETWEEN 2700 PSI SS9013−2231
SOURCE WITH PRESSURE GAGE IN AIR LINE.
9. INFLATE SHOCK STRUT WITH NITROGEN OR AIR
SHOCK STRUT
AIR VALVE
AND 3200 PSI WITH
UNTIL DIMENSION "X" FROM CHART MEETS
CORRESPONDING PRESSURE READING.
SS9013−1804
10. TIGHTEN SWIVEL NUT 50−70 INCH LBS.
REMOVE HOSE AND REPLACE VALVE CAP FINGER
SS9082−300 3
TIGHT.
2
X DIM

WARNING: RELEASE PRESSURE IN STRUT BOTTOM OF SIKORSKY

R

GLAND
BEFORE DISASSEMBLY PLATE
SIKORSKYR
* SEE SERVICE MANUAL FOR FLUID TYPE MANUFACTURED UNDER ONE OR MORE OF THE
VIEW LOOKING AFT FOLLOWING UNITED STATES PATENTS OWNED
BY UNITED TECHNOLOGIES CORPORATION
2070−76 D239,930 3,853,426
3,101,979 3,923,421
1 3,168,144
3,176,937
3,999,888
4,008,980
3,181,815 4,057,363
3,199,601 4,083,654
3,421,296 4,102,011
3,449,891 4,111,386
3,521,448 4,142,698
3,528,712 4,142,833
3,540,809 4,142,837
3,547,555 4,153,831
3,700,995 4,168,045
3,728,045 4,203,708
3,733,039 4,213,518
3,778,189 4,216,924
ON−DEPRESS TOE BRAKE 3,782,854 4,238,971
3,822,105 4,244,677
THEN PULL
OFF−DEPRESS TOE BRAKE AND OTHER PATENTS PENDING
S6126 61819 002 UNITED
TECHNOLOGIES
SIKORSKY
AIRCRAFT
S6126−61819−2 SS9002576

5 SS9002S76
4
CC0337_2A
SA

INTERIOR PLACARDS /SHEET 2/

11-30-00 FIGURE 1
FIGURE 1 PAGE 1
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

CARGO HOOK/HOIST
LIMITS LIFE VEST
ROTORCRAFT LOAD COMB
CLASS B
BELOW
NO PERSON MAY BE
CARRIED UNLESS DO NOT
HE IS A FLIGHT
CREWMEMBER
OBSTRUCT SS9013−1410
HE IS A FLIGHT
CREWMEMBER TRAINEE
THIS AREA SS9013−1410
HE PERFORMS AN 8
ESSENTIAL FUNCTION IN
CONNECTION WITH THE
76010−00105−113
EXTERNAL LOAD OPER
7
HE IS NECESSARY TO
THE ACCOMPLISHMENT
CAUTION
OF THE WORK ACTIVITY NORMAL ROTOR BRAKE STOPS ARE AUTHORIZED ONLY AT 65% Nr
DIRECTLY ASSOCIATED
WITH THAT OPER
OR LESS WITH BOTH ENGINES SHUTOFF,
OR ONE OR BOTH ENGINES AT IDLE.
SS9013−1622
6 SS9140−0053 LH
SS9140−0054 RH
9

FILL WITH OIL

SS9013−1352

TO TOP OF
FILLER NECK
SS9013−1352
NO STEP SS9065−269
19 604−04−3−003D
SS9065−269
20 OR
250−2AC / 3A
9A

−NOZZLE−
ENGINE WATER WASH NO HAND HOLD
SS9013−1647
SS9065−175
EXTINGUISHER

SS9013−1647 SS9065−175
18 21

NO STEP 76010−00105−107
OIL CAPACITY DRY: 11.5 LITERS (3.09 GALS)
DRAINABLE OIL: 10.4 LITERS (2.74 GALS)
TYPE OF OIL: MIL−L−23699, MIL−L−21260,
NO HANDHOLD 10
SS9067−0265
OR DEXRON III
FOR TEMPERATURE LIMITS REFER TO SS9067−0265 REAR SAS UNIT
MAINTENANCE MANUAL
21A MUST BE INSTALLED
33776−58901−103 UPPERMOST SS9013−1348

33776−58901−103 SS9013−1348
TO J1023 11
17 TOJ1013
NO.1 UP
Y SAS FRONT SAS UNIT
NO.2 MUST BE INSTALLED
MAINTAIN OIL Y SAS UPPERMOST
SS9013−1573 SS9013−1349
LEVEL IN CENTER
OF BULLSEYE
SS9013−1372
SS9013−1573 SS9013−1349
22 12
SS9013−1372
16

CAUTION
PHASE
ANGLE
ROTATE SLEEVE C’WISE TO STOP
BEFORE REMOVING STRAINER.
ROTATE SLEEVE C’C’WISE TO STOP
AFTER INSTALLING STRAINER.
EXIT
ALIGNMENT 76351−09102−101 604−04−3−003A
SS9013−1394 76351−09102−101 13
15 14 CC0337_3D
SA

INTERIOR PLACARDS /SHEET 3/

11-30-00 FIGURE 1
FIGURE 1 PAGE 2
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

MAIN
HARD POINT
FWD BAGGAGE RESTRAINT
SS9013-1439
RESERVE
SS9013-1439
24
AFT
BAGGAGE CAPACITY - 600 LBS. SS9065-612
PART NUMBER NOT ASSIGNED
23 SS9065-612
25

THE BAGGAGE COMPARTMENT

CAUTION MUST BE LOADED SYMETRICALLY
ROTATE SLEEVE C’C’WISE TO STOP
BEFORE REMOVING STRAINER. ABOUT BL 0.
ROTATE SLEEVE C’WISE TO STOP SS9013-1380
AFTER INSTALLING STRAINER.
76351-09102-101
SS9013-1380
76351-09102-101 26
31
CAUTION
BENT CONNECTOR PINS
ESSENTIAL FOR MATING.
STRUT DO NOT STRAIGHTEN
"X" DIM
+ PRESSURE SS9067-0652
- 12 IN
MAIN LANDING GEAR +
- 10 PSIG

STRUT SERVICING INSTRUCTIONS FULLY COMP 2310

SS9067-0652
52 1850
77 1460
CHECK STRUT EXTENSION: 102
127
1195
1005
27
1. IF STRUT IS FULLY COMPRESSED 152 865
SEE MAINTENANCE HANDBOOK! 177 755
2. REMOVE AIR VALVE CAP AND ATTACH PRESSURE GAGE 202 670
3. LOOSEN SWIVEL NUT AND MEASURE AIR PRESSURE 227 605
4. CHECK CHART FOR CORRESPONDING "X" DIMENSION 252 545
IF MEASURED "X" VALUE IS NOT WITHIN +
- 25 PROCEED 277 500
WITH STEPS 5 THRU 12 (IN THIS SEQUENCE).
FOR PROPER SERVICING IF STRUT IS WITHIN LIMITS
302
327
460
425
BAGGAGE MUST BE
PERFORM STEP 13 ONLY. 377 370

SERVICING: (WEIGHT OF AIRCRAFT ON TIRES)

427
477
527
325
290
265
SECURED PROPERLY.
(BOTH FLUID & PRESSURE MUST BE CHECK TO PROPERLY 577 240 SS9013-1382
SERVICE STRUT). 627 220
5. REMOVE AIR VALVE CAP AND LOOSEN SWIVEL NUT TO 677 205
SLOWLY BLEED OFF PRESSURE UNTIL STRUT BOTTOMS 727 190
IN FULLY COMPRESSED POSITION, THEN LOOSEN SWIVEL 777 175 SS9013-1382
NUT FULL OPEN (2 1/2 TURNS MAXIMUM) LEAVE OPEN. 827 165
6. REMOVE AIR VALVE FROM STRUT AND ATTACH FILLER HOSE FULLY EXT 160
28
FILL STRUT WITH HYDRAULIC OIL
*TO LEVEL OF
SERVICE OPENING WAIT 5 MINUTES CHECK FLUID LEVEL
AND IF NECESSARY REFILL TO LEVEL OF SERVICE OPENING.
7. REPLACE AIR VALVE AT TOP OF STRUT AND TIGHTEN TO
50-70 INCH LBS SECURE WITH LOCKWIRE.
SHOCK STRUT
AIR VALVE
8. ATTACH HOSE FROM NITROGEN OR AIR
SOURCE WITH PRESSURE GAGE IN AIR LINE..
9. INFLATE SHOCK STRUT WITH NITROGEN OR AIR UNTIL
THE MAXIMUM ALLOWABLE FLOOR
DIMENSION "X" FROM CHART IS APPROXIMATELY 4 INCHES
CLOSED AIR VALVE.
10. OPEN AIR VALVE SLIGHTLY AND READ PRESSURE WHILE
STRUT IS SLOWLY COMPRESSING.
LOADING FOR THE BAGGAGE COMPT
QUICKLY CLOSED AIR VALVE.
11. DETERMINE FINAL "X" DIMENSION FROM CHART
FOR PRESSURE INDICATED.
12. BLEED OFF NITROGEN OR AIR UNTIL FINAL "X" DIMENSION
X DIM IS 75 LB PER SQ FT FOR WEIGHTS UP
-+ 10 IS MET TIGHTEN SWIVEL NUT 50-70 INCH LBS.
13. REMOVE HOSE AND REPLACE VALVE CAP FINGER TIGHT.
BOTTOM OF
GLAND FLANGE
TO THE MAXIMUM COMPARTMENT
VIEW LOOKING AFT
* SEE SERVICE MANUAL FOR FLUID TYPE
CAPACITY OF 600 LB.
WARNING: RELEASE AIR IN STRUT BEFORE DISASSEMBLY
SS9013-1381

2071-34
SS9013-1381
30
29
CC0337_4
SA

INTERIOR PLACARDS /SHEET 4/

11-30-00 FIGURE 1
FIGURE 1 PAGE 3
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

COVER
LIFT DOOR LOCK PIN
THIS COMPARTMENT PULL HANDLE 76010-00105-103
34
76010-00105-106 LH
NOT TO BE OCCUPIED 76010-00105-105 RH
33 DOOR LOCK PIN
BY PASSENGERS OR CREW 76010-00105-104
35

SS9013-1422
32 PUSH FORWARD
THIS HELICOPTER MUST BE OPERATED IN ACCORD WITH THE OPERATING TO FOLD
LIMITS SPECIFIED IN THE FAA APPROVED ROTORCRAFT FLIGHT MANUAL. SS9013-1403
THE AIRWORTHINESS LIMITATIONS SECTION OF THE ROTORCRAFT SS9013-1403
MAINTENANCE MANUAL MUST BE COMPLIED WITH.
36
SS9013-1514
48
LIFT DOOR LOCK PIN
PULL HANDLE
SS9013-1506 76010-00105-105 LH
SS9013-1506 76010-00106-106 RH
37
47

PILOTS PERMISSION REQUIRED DOOR JETTISON

LIFT DOOR LOCK PIN
TO OPEN SLIDING DOOR. PULL COVER
LIFT RED HANDLE
INSURE THAT ALL PASSENGER PUSH HERE

SEATBELTS/HARNESS ARE FASTENED 76010-00105-101 LH

SS9013-1648 76010-00105-102 RH
38
SS9013-1648
46
ROTORCRAFT FLIGHT MANUAL STOWAGE
76010-00105-114
UNLOCKED 39

SS9013-2629
45
VENT
SS9065-267
40
LOCKED

NO STEP
SS9013-2628
44

SS9065-269

SS9065-269
41

WINDOW JETTISON
11
- 15

PULL RED HANDLE

SS9013

PUSH HATCH OUT

43
SS9013-2625 LH
SS9013-1511 LH SS9013-2626 RH
SS9013-1500 RH CC0337_5
42 SA

INTERIOR PLACARDS /SHEET 5/

11-30-00 FIGURE 1
FIGURE 1 PAGE 4
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

WHITE AREA ABOVE 10,000 FT HD

VNE (IAS) PWR ON 106-108% NR
VNE (IAS) PWR ON 106-108% NR
-35 -30 -20 -10 0 10 20 30 40 50 -35 -30 -20 -10 0 10 20 30 40 50
-1 OAT ~ OC -1
0 11,700 LB 150 0
1 155 KTS 149 143 1
2 148 142 137 2
WHITE AREA FOR USE ABOVE
3 154 148 141 136 130 3 10,000 DENSITY ALTITUDE FOR

PRESS ALT X 1000

PRESS ALT X 1000

4 154 147 141 135 129 123 4 A/C WEIGHTS 11,001 TO 11,700 LBS
5 154 147 141 134 128 122 117 5
6 152 153 154 147 140 134 127 121 115 109 6 68
8 134 135 136 133 126 120 114 107 101 95 8 66
10 118 118 118 119 112 105 99 92 86 80 10 64
12 99 99 99 104 97 90 84 77 12 62
14 80 92 92 89 82 76 14 60
11,000 LB
16 73 73 73 73 16 58
18 56 56 FLIGHT NOT ALLOWED 18 56 FLIGHT NOT ALLOWED

Vne POWER-ON Vne POWER-ON

FRONT BACK
49
76450-01501-042

COMPASS
SWUNG BY
TO FLY STEER TO FLY STEER TO FLY STEER
N 120 240
15 135 255
30 150 270
45 165 285
60 180 300
75 195 315
90 210 330
105 225 345 CAUTION

TURN OFF STROBE LIGHT WHEN TAXIING NEAR

AIRSPEED CALIB. OTHER AIRCRAFT OR WHEN FLYING IN FOG OR
CLOUDS. STANDARD POSITION LIGHTS MUST
IND CAL IND CAL IND CAL BE USED FOR ALL NIGHT OPERATIONS.

A.S. A.S. A.S. A.S. A.S. A.S.

0 70 140 31-1601
10 80 150 50
20 90 150
30 100 170
40 0000 180
50 120 190
60 130 200

SS9083-01
51

CC0337_6
SA

INTERIOR PLACARDS /SHEET 6/

11-30-00 FIGURE 1
FIGURE 1 PAGE 5
OCT 31/06
 ILLUSTRATED PARTS CATALOG, SA 4047-76C-4

N1 TACHO CHECK TABLE −35 −30 −20 −10 0 10 20 30 40 50

OAT 0C
−1 134 OAT ~ OC
−3.5 +10 +25 +30 +35 +40 +45 +50
−1 0 131
102,7 102,7 102,6 102,5 102,3 102,1 101,8 1 129 134 VNE
+1 POWER OFF
2 126 132 136 KTS 115% NR
102,7 102,6 102,5 102,4 102,2 102,0 101,7 3 124 129 131 MAX
PRESS ALT x 1000

+3 4 122 127 130 124 WHITE AREA

102,7 102,6 102,4 102,3 102,1 101,9 101,7
5 120 125 134 135 129 123 118 ABOVE

PRESS ALT x 1000

+5
6 118 123 132 135 128 122 116 110 10,000 FT
102,7 102,4 102,3 102,2 102,0 101,8
+7
8 113 118 127 134 127 121 115 108 102 96 HD
102,6 102,3 102,2 102,1 101,9 10 109 114 121 120 113 106 100 93 87 79
+9 12 101 101 101 105 98 91 85 76
102,4 102,2 102,1 102,0 14 82 94 94 90 83 75
D
16 75 75 75 75 WE
+11 LO
102,1 102,1 102,0 18 48 48 FLIGHT NOT AL
+13
102,0 102,0
+15 Vne POWER−OFF
ALL WEIGHTS
0401−28−8350 LH 76450−01501−116
0401−28−8360 RH 53
52
CAUTION
ENG OPER WITH ROTOR
STOPPED LIMITED TO:
0
BLADES 45 TO LONG AXIS

FWD SS9013−2609
NO.1 R SAS NO. 2 R SAS 54

CAUTION
WITH USEABLE FUEL
TO J1024 TO J1014 PER TANK INDICATING 80
LBS OR LESS AVOID
SS9140−0651 SUSTAINED NOSE DOWN
57 PITCH ATTITUDES IN
EXCESS OF 5 0
(USED ON ALL OTHER AIRCRAFT)
SS9013−2241
55

50 40 30 20 10 0
−10 −20 −30 −35
OAT 0
C 134 −1
FWD
131 0
VNE
136 KTS 134 129 1

PRESS ALT x 1000

NO.1 R SAS NO. 2 R SAS POWER OFF
115% NR 132 126 2
MAX 131 129 124 3
WHITE AREA 124 130 127 122 4
ABOVE 118 123 129 135 134 125 120 5
10,000 FT 110 116 122 129 135 132 123 118 6
TO J1014 TO J1024 HD
96 102 108 115 121 127 134 127 118 113 8
79 87 93 100 106 113 120 121 114 109 10
SS9140−1275 76 85 91 98 105 101 101 101 12
57 FL 75 83 90 94 94 82 14
IGH
(USED ON AIRCRAFT EFFECTIVITIES TN 75 75 75 75 16
OT
0453, 0457, 0459, 0460, 0461, 0463, 0464, 0466, 0467, ALLOWED 48 48 18
0468, 0469, 0470, 0472, 0473, 0474, 0475, 0476, AND 0481)
76450−01501−115
Vne POWER−OFF
ALL WEIGHTS
56 CC0337_7B
SA

INTERIOR PLACARDS /SHEET 7/

11-30-00 FIGURE 1
FIGURE 1 PAGE 6
OCT 31/06