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DC-9 Landing Gear Repair Guide

This document provides information about landing gear doors for a DC-9-20 aircraft, including: 1) A description and illustrations of the nose and main landing gear doors, identifying materials used. 2) A table listing approved structural repairs for various door components like skin, honeycomb, and internal structures. 3) Detailed illustrations and material specifications for components of the nose and main landing gear doors.
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0% found this document useful (0 votes)
717 views6 pages

DC-9 Landing Gear Repair Guide

This document provides information about landing gear doors for a DC-9-20 aircraft, including: 1) A description and illustrations of the nose and main landing gear doors, identifying materials used. 2) A table listing approved structural repairs for various door components like skin, honeycomb, and internal structures. 3) Detailed illustrations and material specifications for components of the nose and main landing gear doors.
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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DOUGLAS

AIRCRAFTCO., INC.

STRUCTURALREPAIR MANUAL

LANDING GEAR - DESCRIPTION AND OPERATION (DC-9-20)

1. General

This section illustrates the doors used to enclose the landing gear
components. Types and gages of material used in construction of the doors
are identified within the illustrations.

° Repair Index

A. A list of structural components and the applicable repairs which may be


used to restore the structural integrity and appearance is presented as
follows:

Structural Component Approved Repairs

Skin Section 52-01, Figure l,


Sheets 2 and 3

Section 52-05, as applicable

Section 53-03, as applicable

Honeycomb Sectioz 52-02, as applicable

Section 52-01, Figure 2,


Sheet l; Figure 3, Sheet 1

Chapter 51, Repair Bonding


Section, as applicable

Internal structure Section 52-01, Figure l,


(frames, stiffeners, Sheet !; Figure 2, Sheet 4
etc.)
Section 52-05, Figures l, 2,
3, and 6 (nose gear door
only)

Section 52-05, Figure 5

NOTE: These repairs do not exclude other repairs, or variations


of repairs shown in the mRnual, that may also apply.

52-83-0
Mar l/T0 Page 1
Printed ,. U S A
DOUGLASAIRCRAFT CO,, INC.

STRUCTURAL REPAIR MANUAL

"3
2

2
1

14
].5

16
AFT
DOOR
21

19 20
17

18 21 19 I~/17

FORWARD SECTION A-A


DOOR
2O NOTE5:
1. 4iTEM 3 CHEM-MILLEO FROM.080 STOCK,
19 ANDVARIESTO .047 ± .007.
18 2. REFERENCE - DOUGLAS DRAWINGS5910086,
5914985 AND 5914984.
I ITEM NOMENCLATURE GAGE MATERIAL ITEM! NOMENCLATURE GAGE MATERIAL
1 PAN .050 CLAD 2024-T42 13 ATTACHFITTING 2.000 PLATE 7075-T651
2 COVER .O5O CLAD 2024-T3 14 RIB .063 CLAD 7075-T6
3 COVER .080 CLAD 7075-T6 15 RIB .071 CLAD 7075-T6
4 DOUBLER .063 CLAD7075-T6 16 HINGEHALF lx3 STL BAR4140
5 PAN .040 CLAD 2024-T42 17 ANGLE .O5O CLAD7075-T6
6 COVER .O25 CLAD 2024-T3 18 RIB .040 CLAD2024-T42
7 ATTACHFITTING 2 .75x 4 AL BAR 7075-Tb51 19 ’DOUBLER .050 CLAD7075-T6
8 HINGE AL FORGE7075-T6 2O RIB 3x4 ALBAR 7075-T651
9 FITTING 1.000; PLATE 7075-T651 "21 SKIN .040 CLAD 7075-T6
10 ANGLE .050 CLAD 2024-T42 22 SKIN .040 CLAD2024-T3
11 ATTACHFITTING 3x3 STL BAR 4130 23 RIB 1.750 PLATE20 24-T351
12 HINGEHALF 2955883

Nose Gear Door Plating and Structure -- Type C


52-83-0 Figure 1
Page 2 Dec 1/68
P¢,nled ,. U 5 A
DOUGLASAIRCRAFT CO., INC.

STRUCTURAL REPAIR MANUAL

STA STA
748 ,94

7 (TYP 15
PLACES)

3
6
6
4 8
3
2

38
3, 14
1.5
36
38 40
3
38
35
34 17
.18
32

33
2O

tt

30
STA
"23 694
24
29

NOTE: B, 25
19
FORSECTIONB-B ANDFOR
ITEM LIST OF MATERIALS, 26
SEESHEET2.
*28 26 STA 624
27
BB3-1591

Main Gear Inboard Door Structure -- Type C


Figure 2 (Sheet l) 52-83-o
Dec 1/68 Page 3
DOUGLASAIRCRAFT CO., INC.
DC-9
STRUCTURAL REPAIR MANUAL

.040 .071 • "28

smcnONB-B

NOTES:
1. STRIP MADEFROMCRESSHEETMIL-S-5059,
ANNEALED,COMP302, FINISH NO. 2D.
2. PRECOATED SAFETY WALK NON-PRESSURE
SENSITIVE, TYPE A, MEDIUMGRIT
3. *SKIN, ITEM 28, CHEMICALLY MILLED FROM.071
CLAD7075-1"6 STOCKANDVARIESTO .040.
4. RAMPASSEMBLY .750 OD X .083, 6061°T6 TUBE
WELDED TO .090, 6061-T6 ANGLES.
5. tl’BUMPER, ITEM 31, IS MADEFROMINVESTMENT
CASTINGBERYLLIUMCOPPER,MIL-C-22087,
COMP10, PONDB.
6. REFERENCE-DOUGLAS DRAWING5910161.

ITEMI NOMENCLATURE GAGE MATERIAL ITEM NOMENCLATURE GAGE MATERIAL


1 CHANNEL .040 CLAD 2024-T4 23 INTERCOSTAL .663 CLAD7075-1"6
,i
2 TUBE SEE NOTE4 24 FORMER .063 CLAD7075-T6
3 STRIP .032 SEE NOTE1 25 FORMER .080 CLAD7075-T6
4 COVER .040 CLAD 2024-T42 26 FORMER .040 CLAD7075-T6
S BUMPER .063 CLAD 2G14-T6 2? ANGLE .0(:~ CLAD 7075-T6
6 COVER .04O CLAD 7075-T6 w28 OUTERSKIN SEE NOTE3
7 SAFETY WALK SEE NOTE2 29 INTERCOSTAL .032 CLAD7075-T6
8 PLATE .080 CLAD 2024-T3 3O INTERCOSTAL .090 CLAD7075-T6
9 COVER .050 CL.AD 7075-T6 tt31 BUMPER/SKID SEE NOTE5
10 SHIM .063 CLAD 2024-T3 32 i .071 CLAD7075-T6
ANGLE
11 SUPPORT .750 PLATE7075-T651 33 ANGLE .125 CLAD7075-T6
12 CHANNEL .050 CLAD 7075-T6 34 FITTING 3.000 AL PLATE7075.-T651
13 HINGE 2926483 35 STIFFENER .050 CLAD7075-T6
14 COVER .071 CLAD 7075-T6 36 STEP .063 CLAD2024-T42
15 HINGE HALF 2916448 37 INNER PANEL .050 CLAD7075-T6
16 SCUFFPLATE .09C CLAD 7075-T6 38 COVER .040 CLAD 2024-T3
m
17 CLIP .080 CLAD 7075-76 39 S~lP .063 SEENOTE1
18 FORMER .O90 CLAD 7075-T6 4O COVER .090 CLAD7075-T6
|m
19 ANGLE 1642726 41 ANGLE 1249328
2O FITTING 5955992 b,L FORGING7075-T6
21 INTERCOSTAL .~71 CLAD 7075-T6
22 STRAP .125 CLAD7075-’1"6
BB3-1592A

Main Gear Inboard Door Structure -- Type C


52-83-0 Figure 2 (Sheet 2)
P~ge h Mar 1/69
Pr,nled ,n U 5 A
DOUGLASAIRCRAFT CO., INC.

STRUCTURAL REPAIR MANUAL

STA XW58
NOTE:
FORSECTIONE-E ANDF-F,
LIST OF MATERIALSAND
NOTES,SEESHEET2.

7 9 23 8
6 7
4 5
I 1
24
24
SECTION A-A 11

6
9
26

10
13
15 C

8 9 23 6

SECTION B-B
(TYP 3 PLACES) 13
25 12

SECTIONC-C 4 5 2 24 11 7

.... .....
SECTION D-D
8B3-1585A

Main Gear Outboard Door Plating


and Structure -- Type C
Figure 3 (Sheet l) 52-83-0
Mar 1/69 Page 5
Printed ,n U S A
DOUGLASAIRCRAFT CO., INC.

STRUCTURAL REPAIR MANUAL

16 20 21 t27 18

14 12 13 17
SECTION
E-E
18 V

1~14
SECTION
F-F
NOTES:

1. MADEFROM1.188 T X .125 HEX X .002 THICK ALUMINUM


FOIL HONEYCOMB,NON-PERFORATED.
2. MADEFROMTUNGSTEN BASE, HIGH DENSITYBAR
MIL-T-21014, TYPE2.
3. .003 ALUMINUM ALLOYLAMINATIONS.
4. GLASSCLOTHPHENOLIC,
5. CRESSHEET, MIL-S-5059, COND1/4H, COMP301,
FINISH 2B (OR EQUIVALENT).
6. CRESSHEET, MIL-S-SOS9, GOND1/2H, COMP301,
FINISH 2B ( OREQUIVALENT).
7. f USEDON FUSELAGE
NO. 488, 518 AND519 ONLY.
8’. * ITEM 3 MAYUSE 2.000 PLATE7075-T651 ON
FUSELAGENO. 286 AND SUBSEQUENT.
9. REFERENCE-DOUGLAS
DRAWING5910557.

ITEM NOMENCLATURE GAGE MATERIAL ITEM NOMENCLATURE GAGE MATERIAL L


1 HINGEHALF 2272677 14 OUTERSKIN .050 CLAD 7075-T6
2 BEAM 2923195 15 RUBSTRIP .O2O SEE NOTE6
"3 FITTING 3927055-3 FORGING7075-T6 16 PAN .040 CLAD2014-T’b
4 FITTING 2.000 PLATE 7075-T651 17 CORE SEE NOTE1
5 FITTING 3.500 PLATE 7075-T651 18 PAN .050 CLAD 2014-T6
6 CHANNEL .040 CLAD 2024-T3 19 WEIGHT SEE NOTE2
7 CHANNEL .063 CLAD 2024-T3 20 FITTING 1.500! PLATE 7075-T651
8 SEAL .012 SEE NOTE5 21 SEAL .062 SEE NOTE3
9 INNER
m
SKIN .040 CLAD 2024-T42 22 CLIP .063 CLAD20 24-T42
10 HINGEHALF 2913434 23 CLIP .063 CLAD2024-T3
l OUTERSKIN .040 CLAD 2024-T3 24 SHIM .032 SEE NOTE3
[2 BONDEDDOUBLER .063 CLAD 7075-T6 25 FILLER 1.250 SEE NOTE4
13 BONDEDDOUBLER .050 CLAD 7075-T6 26 SUPPORT .050 CLAD2024-T3
t27 DOUBLER .032 CLAD2024-T3

BB3-1586A
Main Gear Outboard Door Plating
and Structure -- Type C
52-83-0
Figure 3 (Sheet 2)
Page 6
Mar 1/69

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