NAVAIR 17-1-114.4.1 Load Test Items.pdf

NAVAIR 17-1-114.4.1

1 March 2022 Change 1 - 1 August 2023

TECHNICAL MANUAL

VOLUME4

INTERMEDIATE, AND DEPOT MAINTENANCE

WITH ILLUSTRATED PARTS BREAKDOWN

INSPECTION AND PROOFLOAD TESTING OF

LIFTING SLINGS FOR C-130 AIRCRAFT AND

RELATED COMPONENTS

This manual supersedes NAVAIR 17-1-114.4.1 dated 1 April 2017 with Change 1 dated 1 November 2019.

This manual is incomplete without NAVAIR 17-1-114.1.

DISTRIBUTION STATEMENT C. Distribution authorized to U.S. Government agencies and their contractors to protect publications required for official use or for administrative or operational purposes, determined on 1 March 2022. Other requests for this document shall be referred to Commanding Officer, Naval Air Systems Command (PMA 207), 46990 Hinkle Road, Unit 8, Bldg.

419, Patuxent River, MD 20670-1627.

DESTRUCTION NOTICE - For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

PUBLISHED BY DIRECTION OF THE COMMANDER, NAVAL AIR SYSTEMS COMMAND

0817LP0028305

NAVAIR 17-1-114.4.1 003 09

1 March 2022 Page 1 of 8

INTERMEDIATE AND DEPOT MAINTENANCE

SLING ASSEMBLY - REFRIGERATION UNIT INSTALLATION

WITH ILLUSTRATED PARTS BREAKDOWN

PART NUMBER 3402242-1

Reference Material

Number

Depot Level Rework Program for Support Equipment End Items ...... ... ... ..... .. ... ....... .. .... ... ... ..... .. ... ...... NAV AIRINST 13680.1 Inspection and Proofload Testing of Lifting Slings for Aircraft and Related Components .... .. .... .. .... .. .... .. NA VAIR 17-1-114.1

Alphabetical Index

Subject Page No.

Assembly, Refinishing and Lubrication Cleaning and Inspection Disassembly Illustrated Parts Breakdown (IPB) Introduction Notes Proofload Test Repair Usable On Codes

Record of Applicable Technical Directives

1. INTRODUCTION.

a. The refrigeration unit installation sling assembly is used to lift the refrigeration unit during installation.

Refer to figure 1 for application information.

PART NUMBER

CAGE :

NOMEN

CLATURE:

NSN:

SAFE

WORKING

LOAD:

APPLICATION:

3402242-1 (98897)

SLING

ASSEMBLY

REFIRGERATION

UNIT

INSTALLATION

l 730-01-006-0933

190LB

C/KC-130T/J

Figure 1. Application Information

None

2. DISASSEMBLY.

a. The refrigeration unit installation sling assembly, PIN 3402242-1 (98897), shall be disassembled in accordance with figure 2. General disassembly of sling components shall be accomplished in accordance with good shop practices.

3. CLEANING AND INSPECTION.

a. Clean sling as necessary in accordance with NAVAIR 17-1-114.1, Work Package (WP) 005 00 to remove dirt, oil, grease and other foreign matter.

b. Perform a detailed inspection of the entire sling assembly in accordance with NAVAIR 17-1-114.1, WP 005 00. Cracks are not acceptable. Leave paint intact and mark any suspect damaged areas. Remove paint from suspect areas and stress areas for Non-Destructive Inspection (NDI).

1299789680A Highlight

1299789680A Highlight

4. REPAIR.

a. Removal and replacement of hardware and readily available parts is permitted in accordance with applicable SM&R codes in figure 2. There is no repair for pins, screws and other common hardware. Damaged hardware shall be rejected and replaced with new hardware. All hardware shall be inspected prior to assembly. Refer to

NA VAIR 17-1-114.1, WP 005 00.

b. In general, surface defects on the sling's structural members, attachments, and fittings such as cracks, nicks and gouges, may be repaired by hand filing and blending with the surrounding area to remove the defect as long as 90 percent or more of the component cross sectional dimension/area is intact. Refer to NAVAIR 17-1-114.1, WP 005 00.

5. ASSEMBLY,

LUBRICATION.

REFINISHING

MATERIALS REQUIRED

Nomenclature

Epoxy Primer Polyurethane Coating

Specification/

Part Number

MIL-PRF-23377

MIL-PRF-85285

AND

HMWS

Index No.

a. The refrigeration unit installation sling assembly shall be assembled in accordance with figure 2. General assembly of sling components shall be accomplished in accordance with good shop practices.

Epoxy Primer, MIL-PRF-23377 1

b. Prime the refrigeration unit installation sling assembly where primer was removed for inspection or corrosion control purposes using epoxy primer, MIL-PRF-23377, corrosion inhibiting, lead and chromate free, Type II. There is no allowance for primer in holes or threaded areas.

( .. E;;r )[�J[• J[ :I; )

Polyurethane Coating, MIL-PRF-85285 2

c. Paint the refrigeration unit installation sling assembly where paint was removed for inspection or corrosion control purposes using polyurethane coating, 003 09

MIL-PRF-85285, untinted white (SAE-AMS-STD-595, 7925) or for USMC applications use green (SAE-AMS STD-595, 24052, 34052 or 34084). There is no allowance for paint in holes or threaded areas.

6. PROOFLOAD TEST.

MATERIALS REQUIRED

Nomenclature

Eye Nut Proofload Tag Swaging Sleeve Wire Rope

Specification/

Part Number

3019T16

MS51844-82

M83420/2-002

HMWS

Index No.

SUPPORT EQUIPMENT REQUIRED

Nomenclature

Proofload Adapter Proofload Adapter Proofload Adapter

Part Number

26E0257-1 26E0257-2 26E0257-3

a. Due to non-availability of proofload adapters, the proofload task for this sling is to be performed at a sling depot via NA V AIRINST 13680.1 procedures.

b. Perform proofload test of the refrigeration unit installation sling assembly at assigned depot by restraining at point IA!> and hang weights as shown in figure 3, view A and B.

c. Locally manufacture proofload tag in accordance with NAVAIR 17-1-114.1, WP 005 00. Attach proofload tag to the beam (2, figure 2) using six inches of wire rope (M83420/2-002) and one swaging sleeve (MS51844-82).

7. ILLUSTRATED PARTS BREAKDOWN (IPB).

a. Refer to figure 2. Refer to NAVAIR 17-1-114.1, WP 002 00 for instructions on how to use this IPB.

8. NOTES.

a. See figure 4, view A, for manufacturing details for Cable Assembly (3402242-25).

b. See figure 4, view B, for manufacturing details for Cable Assembly (3402242-35).

9. USABLE ON CODES.

a. The usable on codes for the refrigeration unit installation sling assembly are as follows:

Usable On Code

A B

Units

1 thru 36 37 and up

1299789680A Highlight

34>·

//28 ®i~

6 18

Figure 2. Refrigeration Unit Installation Sling Assembly (3402242-1) (Sheet 1 of3)

003 09

Page4

UNITS USABLE

INDEX PART DESCRIPTION PER ON SM&R

NO. NUMBER 1 2 3 4 5 6 7 ASSY CODE CODE

3402242-1 SLING ASSEMBLY, REFRIGERATION ................................. REF PEOHH

UNIT INSTALLATION (98897)

1 LS35265B1 C2 IDENT PLATE (98897) ..................................................... 1 MDGZZ 3402242-3 FRAME ASSY (98897) ..................................................... 1 MDGZZ

2 3402242-5 BEAM (98897) ............................................................. 1 MDGZZ 3 3402242-7 LUG (98897) ............................................................... 2 MDGZZ 4 3402242-9 LUG (98897) ............................................................... 1 MDGZZ 5 3402242-11 LUG (98897) ............................................................... 1 MDGZZ 6 NAS 1335S3S05 PIN, QUICK RELEASE ................................................ 1 XBHZZ

MS17984C505 PIN, QUICK RELEASE (ALT FOR ............................... * PAHZZ

NAS 1335S3S05)

(ATTACHING PARTS)

7 3402242-33 CABLE (98897) ........................................................... 1 MDGZZ

M83420/2-004 WIRE ROPE 0.09 DIAX 12.00 (ALT FOR ................... * PAHZZ

3402242-33)

8 28-2G SLEEVE, SWAGING (76691) ...................................... 2 PAHZZ

9 3402242-39 CLIP (98897) ............................................................... 1 MDGZZ

3402242-31 HOIST BAR ASSY (98897) ............................................... 1 A AGGZZ 3402242-47 HOIST BAR ASSY (98897) ............................................... 1 B AGGZZ

10 3402242-13 BAR ASSY (98897) ..................................................... 1 A MDGZZ 3402718-1 BAR (98897) ............................................................... 1 B MDGZZ

11 3402242-41 SLIDE ASSY (98897) .................................................. 1 MDGZZ 12 NAS623-3-2 SCREW, MACHINE ..................................................... 2 PAHZZ

3402242-23 CLEVIS ASSY (98897) ..................................................... 1 AGGZZ 13 3402242-29 CLEVIS (98897) .......................................................... 1 A MDGZZ

3402720-1 CLEVIS (98897) .......................................................... 1 B MDGZZ 14 NAS 1334S3S08 PIN, QUICK RELEASE ................................................ 1 XBHZZ

MS17984C408 PIN, QUICK RELEASE (ALT FOR ............................... * PAHZZ

NAS 1334S3S08)

(ATTACHING PARTS)

15 3402242-33 CABLE (98897) ........................................................... 1 MDGZZ

M83420/2-004 WIRE ROPE 0.09 DIAX 12.00 (ALT FOR ................... * PAHZZ

3402242-33)

16 28-2G SLEEVE, SWAGING (76691) ...................................... 2 PAHZZ

3402242-25 CABLE ASSY (98897) ...................................................... 1 MGGZZ

17 3402242-27 CABLE (98897) ........................................................... 1 MGGZZ

M83420/2-006 WIRE ROPE 0.16 DIAX 5.00 (ALT FOR ..................... * PAHZZ

3402242-27) 18 NAS1435K5 TERMINAL-STRAP, CABLE ........................................ 2 PAHZZ

19 MS20664C5 BALL END, WIRE ROPE, SWAGING .......................... 2 PAHZZ

20 NAS1334S3S04 PIN, QUICK RELEASE ................................................ 1 XBHZZ

MS17984C404 PIN, QUICK RELEASE (ALT FOR ............................... * PAHZZ

NAS1334S3S04)

(ATTACHING PARTS)

21 3402242-33 CABLE (98897) ........................................................... 1 MGGZZ

M83420/2-004 WIRE ROPE 0.09 DIAX 12.00 (ALT FOR ................... * PAHZZ

3402242-33)

22 28-2G SLEEVE, SWAGING (76691) ...................................... 2 PAHZZ

3402242-35 CABLE ASSY (98897) ...................................................... 1 MGGZZ

23 3402242-37 CABLE (98897) ........................................................... 1 MGGZZ

M83420/2-006 WIRE ROPE 0.16 DIA X 6.00 (ALT FOR ..................... * PAHZZ

3402242-37) 24 NAS1435K5 TERMINAL-STRAP, CABLE ........................................ 2 PAHZZ

25 MS20664C5 BALL END, WIRE ROPE, SWAGING .......................... 2 PAHZZ

26 AN43B-15A EYE BOLT ................................................................... 1 XBHZZ

AN43B-15 EYE BOLT (ALT FOR AN43B-15A) ............................. * PAHZZ

(ATTACHING PARTS)

27 NAS623-3-7 SCREW, MACHINE ..................................................... 1 PAHZZ

Figure 2. Refrigeration Unit Installation Sling Assembly (3402242-1) (Sheet 2)

Pages

UNITS USABLE

INDEX PART DESCRIPTION PER ON SM&R

NO. NUMBER 1 2 3 4 5 6 7 ASSY CODE CODE

28 AN960-10 WASHER, FLAT .......................................................... 1 PAHZZ

NAS1149F0363P WASHER, FLAT (ALT FORAN960-10) * PAHZZ

29 MS21042-3 NUT, SELF-LOCKING ................................................. 1 PAHZZ 30 AN960-416 WASHER, FLAT ............................................................... 1 PAHZZ

NAS1149F0463P WASHER, FLAT (ALT FORAN960-416) * PAHZZ

31 AN315-4 NUT, PLAIN ...................................................................... 1 XBHZZ

AN315-4R NUT, PLAIN (ALT FORAN315-4) ..................................... * PAHZZ

32 NAS623-4-6 SCREW, MACHINE .......................................................... 1 PAHZZ 33 AN960-416 WASHER, FLAT ............................................................... 1 PAHZZ

NAS1149F0463P WASHER, FLAT (ALT FORAN960-416) * PAHZZ

34 MS21042-4 NUT, SELF-LOCKING ...................................................... 1 PAHZZ 35 NAS623-4-12 SCREW, MACHINE .......................................................... 1 PAHZZ 36 AN960-416 WASHER, FLAT ............................................................... 1 PAHZZ

NAS1149F0463P WASHER, FLAT (ALT FOR AN960-416) * PAHZZ

37 MS21042-4 NUT, SELF-LOCKING ...................................................... 1 PAHZZ

Figure 2. Refrigeration Unit Installation Sling Assembly (3402242-1) (Sheet 3)

Page&

220 LBS

VIEWA

MATERIALS AND EQUIPMENT REQUIRED FOR PROOFLOAD TESTING

ITEM QTY DESCRIPTION PART NUMBER CAGE SM&R

& 1 PROOFLOAD ADAPTER 26E0257-1 96916 MDDZZ

& 1 PROOFLOAD ADAPTER 26E0257-2 96916 MDDZZ

& 1 PROOFLOAD ADAPTER 26E0257-3 96916 MDDZZ

& 2 NUT, EYE 3019T16 39428 PAHZZ

Figure 3. Proofload Test of Refrigeration Unit Installation Sling Assembly (3402242-1) (Sheet 1 of2)

1299789680A Highlight

1299789680A Highlight

1299789680A Highlight

1299789680A Highlight

Page7

160 LBS

220 LBS

VIEWB

Figure 3. Proofload Test of Refrigeration Unit Installation Sling Assembly (3402242-1) (Sheet 2)

1299789680A Highlight

1299789680A Highlight

1299789680A Highlight

1299789680A Highlight

TERMINAL-STRAP, CABLE, 2X NAS1435K5

CABLE, 3402242-33

SWAGING, SLEEVE, 2X 28-2G

BALL END, WIRE ROPE, 2X MS20664C5

-GS~:::::::Jio:ll)ID=====#-L2f~i:t!~~~ QUICK RELEASE PIN, NAS1334S3S04

1 ...... 1------7.75 -------■-

MANUFACTURE OF CABLE ASSEMBLY, P/N 3402242-25 (98897)

VIEWA

TERMINAL-STRAP, CABLE, 2X NAS1435K5

CABLE, 3402242-37 EYE BOLT, AN43B-15A

BALL END, WIRE ROPE, 2X MS20664C5

c··, SCREW, MACHINE, NAS623-3-7

WASHER, FLAT, AN960-10

NUT, LOCK, MS21042-3

MANUFACTURE OF CABLE ASSEMBLY, P/N 3402242-35 (98897)

VIEWB

Figure 4. Manufacture of Cable Assemblies (3402242-25 and 3402242-35)

003 09

NAVAIR 17-1-114.4.1 00310

1 March 2022 Page 1 of 6

INTERMEDIATE AND DEPOT MAINTENANCE

FIXTURE ASSEMBLY- FLIGHT STATION AIR CONDITIONING UNIT INSTALLATION AND REMOVAL

WITH ILLUSTRATED PARTS BREAKDOWN

PART NUMBER 3402244-1

Reference Material

Number

Depot Level Rework Program for Support Equipment End Items ...... ... ... ..... .. ... ....... .. .... ... ... ..... .. ... ...... NAV AIRINST 13680.1 Inspection and Proofload Testing of Lifting Slings for Aircraft and Related Components .... .. .... .. .... .. .... .. NA VAIR 17-1-114.1

Alphabetical Index

Subject Page No.

Assembly, Refinishing and Lubrication Cleaning and Inspection Disassembly Illustrated Parts Breakdown (IPB) Introduction Notes Proofload Test Repair Usable On Codes

Record of Applicable Technical Directives

1. INTRODUCTION.

a. Refer to figure 1 for application information.

PARTNUMBER

CAGE :

NOMEN

CLATURE:

NSN:

SAFE

WORKING

LOAD:

APPLICATION:

3402244-1 98897

FIXTURE

ASSEMBLY

FLIGHT

STATION AIR

CONDITIONING

UNIT

INSTALLATION

AND REMOVAL

l 730-01-006-0833

185 LB

C/KC-130T/J

Figure 1. Application Information

None

2. DISASSEMBLY.

a. The flight station air conditioning unit installation and removal fixture assembly, PIN 3402244-1 (98897), shall be disassembled in accordance with figure 2. General disassembly of fixture components shall be accomplished in accordance with good shop practices.

3. CLEANING AND INSPECTION.

a. Clean fixture as necessary in accordance with NAVAIR 17-1-114.1, Work Package (WP) 005 00 to remove dirt, oil, grease and other foreign matter.

b. Perform a detailed inspection of the entire fixture assembly in accordance with NAVAIR 17-1-114.1, WP 005 00. Cracks are not acceptable. Leave paint intact and mark any suspect damaged areas. Remove paint from suspect areas and stress areas for Non-Destructive Inspection (NDI).

1299789680A Highlight

a. Removal and replacement of hardware and readily available parts is permitted in accordance with applicable SM&R codes in figure 2. There is no repair for pins and other common hardware. Damaged hardware shall be rejected and replaced with new hardware. All hardware shall be inspected prior to assembly. Refer to

NA VAIR 17-1-114.1, WP 005 00.

b. In general, surface defects on the fixture's structural members, attachments, and fittings such as cracks, nicks and gouges, may be repaired by hand filing and blending with the surrounding area to remove the defect as long as 90 percent or more of the component cross sectional dimension/area is intact. Refer to NAVAIR 17-1-114.1, WP 005 00.

5. ASSEMBLY,

LUBRICATION.

REFINISHING

MATERIALS REQUIRED

Specification/ Nomenclature Part Number

Epoxy Primer Loctite Sealant Polyurethane Coating

MIL-PRF-23377

ASTMD5363

MIL-PRF-85285

AND

HMWS

Index No.

a. The flight station air conditioning unit installation and removal fixture assembly shall be assembled in accordance with figure 2. General assembly of fixture components shall be accomplished in accordance with good shop practices.

Epoxy Primer, MIL-PRF-23377 1

b. Prime the flight station air conditioning unit installation and removal fixture assembly where primer was removed for inspection or corrosion control purposes using epoxy primer, MIL-PRF-23377, corrosion inhibiting, lead and chromate free, Type II. There is no allowance for primer in holes or threaded areas.

00310

Polyurethane Coating, MIL-PRF-85285 2

c. Paint the flight station air conditioning unit installation and removal fixture assembly where paint was removed for inspection or corrosion control purposes using polyurethane coating, MIL-PRF-85285, untinted white (SAE-AMS-STD-595, 17925) or for USMC application use green (SAE-AMS-STD-595, 24052, 34052 or 34084).

There is no allowance for paint in holes or threaded areas.

Loctite Sealant, ASTM D5363

d. Apply sealing, locking, and reta1mng compound, ASTM D5363, (single-component), Grade A, to the mating threads of the shear bolt (14), self-locking nut (15), and turnbuckle (27) as required

6. PROOFLOAD TEST.

MATERIALS REQUIRED

Nomenclature

Proofload Tag Swaging Sleeve Wire Rope

Specification/ Part Number

MS51844-82

M83420/2-002

HMWS

Index No.

SUPPORT EQUIPMENT REQUIRED

Nomenclature

Proofload Adapter Proofload Stand

Part Number

26C0252-1 18E8178-1

a. Due to non-availability of proofload adapters, the proofload task for this sling is to be performed at a sling depot via NA V AIRINST 13680.1 procedures.

b. Perform proofload test of the flight station air conditioning unit installation and removal fixture assembly at assigned depot by attaching to proofload stand and hang weights as shown in figure 3. Fixture is to be proofload tested over the full length of the beam.

1299789680A Highlight

c. Locally manufacture proofload tag in accordance with NAVAIR 17-1-114.1, WP 005 00. Attach proofload tag to the snap hook (12, figure 2) using six inches of wire rope (M83420/2-002) and one swaging sleeve (MS51844- 82).

7. ILLUSTRATED PARTS BREAKDOWN UPB).

a. Refer to figure 2. Refer to NAVAIR 17-1-114.1, WP 002 00 for instructions on how to use this IPB.

8. NOTES.

a. The flight station air conditioning unit installation and removal fixture assembly is used to install or remove air conditioning unit.

9. USABLE ON CODES.

a. The usable on codes for the flight station air conditioning unit installation and removal fixture assembly are as follows:

Usable On Code Units

A 1 thru 5 B 6 and up C 1 thru 14 D 15 and up E 1 thru 36 F 37 and up

00310 Page3

18 17

00310 Page4

Figure 2. Flight Station Air Conditioning Unit Installation/Removal Fixture Assembly (3402244-1) (Sheet 1 of2)

INDEX

NO.

PART

NUMBER

3402244-1

LS35130E381

LS35265E181

MS21318-15

3402244-3 3402244-49 3402244-27 3402244-47 3402244-51

CF-3/4-SB

MS21042-6

NAS43HT6-23

17288 3402244-5 3402244-25 M84320/2-005

28-3-M G411-1/8 G3315-7/16 3402244-7 3402722-1

NAS1104-12

NAS6204-11

MS21042-4

3402244-11 3402723-1 3402244-41

MS20615-4MP9

3402244-55 3402244-13 3402244-39 3402244-9 3402244-15 3402244-21 3402244-29

NAS 1102-04-5

AN310-4

MS20426AD5-5

HG228-1/4-4

3402244-23

AN960-416L

NAS1149F0432P

MS21042-4

3402244-17

NAS 1102-4-24

AN960-416L

NAS1149F0432P

MS21042-4

3402244-17

DESCRIPTION

1 2 3 4 5 6 7

FIXTURE ASSEMBLY, FLIGHT STATION AIR

CONDITIONING UNIT INSTALLATION AND

REMOVAL (98897)

NAMEPLATE (98897)

NAMEPLATE (98897)

(ATTACHING PARTS)

SCREW, DRIVE

CARRIAGE ASSY (98897)

CARRIAGE ASSY (98897)

CARRIAGE PLATE (98897)

ANGLE (98897)

ANGLE (98897)

CAM, FOLLOWER (92563)

(ATTACHING PARTS)

NUT, SELF-LOCKING, HEXAGON

SPACER

LUBRICATION FITTING (95879)

CABLE ASSY (98897)

CABLE (98897)

WIRE ROPE 0.12 DIA X 35.0 (ALT FOR

3402244-25)

SWAGING, SLEEVE (76691)

THIMBLE, ROPE (75535)

HOOK, SNAP (75535)

JAW END FITTING (98897)

CLEVIS (98897)

(ATTACHING PARTS)

BOLT, SHEAR

BOLT, SHEAR (ALT FOR NAS1104-12)

NUT, SELF-LOCKING, HEXAGON

JAW END FITTING (98897)

LOCK ASSY (98897)

LOCK (98897)

(ATTACHING PARTS)

RIVET, SOLID

TURNBUCKLE ASSY (98897)

BEAM ASSY (98897)

BEAM (98897)

BRACKET ASSY (98897)

BRACKET (98897)

PIN (98897)

RETAINER (98897)

(ATTACHING PARTS)

SCREW, MACHINE

NUT, PLAIN, CASTELLATED

RIVET, SOLID

TURNBUCKLE (75535)

EYEBOL T (98897)

(ATTACHING PARTS)

WASHER, FLAT

WASHER, FLAT (ALT FOR AN960-416L)

NUT, SELF-LOCKING, HEXAGON

BLOCK (98897)

(ATTACHING PARTS)

SCREW, MACHINE

WASHER, FLAT

WASHER, FLAT (ALT FORAN960-416L)

NUT, SELF-LOCKING, HEXAGON

BLOCK (98897)

UNITS

PER

ASSY

REF

USABLE

ON

CODE

C D

A B A A B

E F

E F

00310 Pages

SM&R

CODE

PEOHH

XBHZZ

XBHZZ

PAHZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

XBHZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

MDGZZ

XBHZZ

PAHZZ

PAHZZ

MDGZZ

MDGZZ

MDGZZ

PAHZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

XBHZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

Figure 2. Flight Station Air Conditioning Unit Installation/Removal Fixture Assembly (3402244-1) (Sheet 2)

NAVAIR 17-1-114.4.1 00310

Page&

MATERIALS AND EQUIPMENT REQUIRED FOR PROOFLOAD TESTING

ITEM QTY DESCRIPTION PART NUMBER CAGE SM&R

& 1 PROOFLOAD STAND 18D8178-1 96916 MDDZZ

& 1 PROOFLOAD ADAPTER 26C0252-1 96916 MDDZZ

Figure 3. Proofload Test of Flight Station Air Conditioning Unit Installation/Removal Fixture Assembly (3402244-1)

1299789680A Highlight

1299789680A Highlight

NAVAIR 17-1-114.4.1 00311

1 March 2022 Page 1 of 6

INTERMEDIATE AND DEPOT MAINTENANCE

HOIST ASSEMBLY - UNIVERSAL CARGO COMPARTMENT REFRIGERATION UNIT

AND AUXILIARY POWER UNIT GENERATOR

WITH ILLUSTRATED PARTS BREAKDOWN

PART NUMBER 3402245-1

Reference Material

Title Number

Depot Level Rework Program for Support Equipment End Items ...... ... .... ........ .... .... .. .... .. .... ............. ... NAV AIRINST 13680.1 Inspection and Proofload Testing of Lifting Slings for Aircraft and Related Components ........................ NA VAIR 17-1-114.1

Alphabetical Index

Subject Page No.

Assembly, Refinishing and Lubrication Cleaning and Inspection Disassembly Illustrated Parts Breakdown (IPB) Introduction Notes Proofload Test Repair Usable On Codes

1. INTRODUCTION.

Record of Applicable Technical Directives

None

2. DISASSEMBLY.

a. Refer to figure 1 for application information. a. The universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly, PIN 3402245-1 (98897), shall be disassembled in accordance with figure 2. General disassembly of hoist components shall be accomplished in accordance with good shop practices.

PART

NUMBER

CAGE:

NOMEN

CLATURE:

NSN:

SAFE

WORKING

LOAD:

APPLIC

ATION:

3402245-1 (98897)

HOIST ASSEMBLY -

UNIVERSAL CARGO

COMPARTMENT

REFRIGERATION

UNIT AND

AUXILIARY POWER

UNIT GENERA TOR

1730-01-006-0931

200LB

C/KC-130T/J

Figure 1. Application Information

3. CLEANING AND INSPECTION.

a. Clean hoist as necessary in accordance with NAVAIR 17-1-114.1, Work Package (WP) 005 00 to remove dirt, oil, grease and other foreign matter.

b . Perform a detailed inspection of the entire hoist assembly in accordance with NAVAIR 17-1-114.1, WP 005 00. Cracks are not acceptable. Leave paint intact and mark any suspect damaged areas. Remove paint from suspect areas and stress areas for Non-Destructive Inspection (NDI).

1299789680A Highlight

a. Removal and replacement of hardware and readily available parts is permitted in accordance with applicable SM&R codes in figure 2. There is no repair for pins, washers and other common hardware. Damaged hardware shall be rejected and replaced with new hardware. All hardware shall be inspected prior to assembly. Refer to

NA VAIR 17-1-114.1, WP 005 00.

b. In general, surface defects on the hoist's structural members, attachments, and fittings such as cracks, nicks and gouges, may be repaired by hand filing and blending with the surrounding area to remove the defect as long as 90 percent or more of the component cross sectional dimension/area is intact. Refer to NAVAIR 17-1-114.1, WP 005 00.

5. ASSEMBLY,

LUBRICATION.

REFINISHING

MATERIALS REQUIRED

Nomenclature

Epoxy Primer Polyurethane Coating

Specification/ Part Number

MIL-PRF-23377

MIL-PRF-85285

AND

HMWS

Index No.

a. The universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly shall be assembled in accordance with figure 2. General assembly of hoist components shall be accomplished in accordance with good shop practices.

Epoxy Primer, MIL-PRF-23377 1

b. Prime the universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly where primer was removed for inspection or corrosion control purposes using epoxy primer, MIL-PRF-23377, corrosion inhibiting, lead and chromate free, Type II. There is no allowance for primer in holes or threaded areas.

00311

Polyurethane Coating, MIL-PRF-85285 2

c. Paint the universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly where paint was removed for inspection or corrosion control purposes using polyurethane coating, MIL-PRF- 85285, untinted white (SAE-AMS-STD-595, 17925) or for USMC applications use green (SAE-AMS-STD-595, 24052, 34052 or 34084). There is no allowance for paint in holes or threaded areas.

6. PROOFLOAD TEST.

MATERIALS REQUIRED

Nomenclature

Proofload Tag Swaging Sleeve Wire Rope

Specification/ Part Number

MS51844-82

M83420/2-002

HMWS

Index No.

SUPPORT EQUIPMENT REQUIRED

Nomenclature Part Number

Proofload Stand 18E8159-1

a. Due to non-availability of proofload adapters, the proofload task for this sling is to be performed at a sling depot via NA V AIRINST 13680.1 procedures.

b. Perform proofload test of the universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly at assigned depot by mounting it to the proofload stand and hang weight as shown in figure 3.

c. Locally manufacture proofload tag in accordance with NAVAIR 17-1-114.1, WP 005 00. Attach proofload tag to the hoist beam assembly (1, figure 2) using six inches of wire rope (M83420/2-002) and one swaging sleeve (MS51844-82).

7. ILLUSTRATED PARTS BREAKDOWN (IPB).

a. Refer to figure 2. Refer to NAVAIR 17-1-114.1, WP 002 00 for instructions on how to use this IPB.

1299789680A Highlight

8. NOTES.

a. The universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly is used to lift the cargo compartment refrigeration unit and auxiliary power unit generator.

9. USABLE ON CODES.

a. The usable on codes for the universal cargo compartment refrigeration unit and auxiliary power unit generator hoist assembly are as follows:

Usable On Code

A B C D E

Units

1 thru20 21 thru28 29 and up 1 thru 30 31 and up

00311

Figure 2. Universal Cargo Compartment Refrigeration Unit and Auxiliary Power Unit Generator Hoist Assembly (3402245-1) (Sheet 1 of2)

00311

NO.

PART

NUMBER

3402245-1

3402245-3

NO. 1000

NO. 5404

NO. 5414

3402245-5 3402245-11

CL-6-BLP-T-.8S

MS 17985C608

MS17984C608

3402245-13 M83420/2-004

28-2G

3402245-7 3402245-15 M83420/2-008

28-6X

MS20664C6

3402245-33 3402245-9

MS20220A1

MS20392-4C-43

MS24665-153

AN960C516

NAS1149C0563R

CL-6-BLP-T-1.0-S

3402245-13 M83420/2-004

28-2G

3402245-35 3402245-37 4002-8W 4002-0 R4G V8470-2 3402245-39

LS35265E1 C2

NO. 6122

6122, 1INIDX5.25L

DESCRIPTION

1 2 3 4 5 6 7

HOIST ASSEMBLY, UNIVERSAL CARGO

COMPARTMENT REFRIGERATION UNIT AND

AUXILIARY POWER UNIT GENERATOR (98897)

HOIST BEAM ASSY (98897)

TRAILER WINCH (16853)

TRAILER WINCH

TRAILER WINCH

EXTENSION BAR ASSY (98897)

EXTENSION BAR (98897)

BALL LOCK PIN (99862)

PIN, QUICK RELEASE (80205)

(ALT FOR CL-6-BLP-T-.8S)

PIN, QUICK RELEASE (ALT FOR

MS 17985C608)

(ATTACHING PARTS)

CABLE (98897)

WIRE ROPE 0.09 DIAx 12.00 (ALT FOR

3402245-13)

SLEEVE, SWAGING (76691)

CABLE ASSY (98897)

CABLE (98897)

WIRE ROPE 0.18 X 150.0

(ALT FOR 3402245-15)

SLEEVE, SWAGING (76691)

WIRE ROPE, BALL END

WASHER (98897)

STRUT (98897)

PULLEY, GROOVE

(ATTACHING PARTS)

PIN, STRAIGHT, HEADED

PIN, COTTER

WASHER, FLAT

WASHER, FLAT (ALT FOR AN960C516)

BALL LOK PIN (99862)

(ATTACHING PARTS)

CABLE (98897)

WIRE ROPE 0.09 DIAx 12.00 (ALT FOR

3402245-13)

SLEEVE, SWAGING (76691)

SUPPORT ASSY (98897)

PLATE (98897)

STUD (71286)

EYELET (71286)

RING, RETAINING (71286)

S-HOOK (14557)

S-HOOK (98897)

IDENT PLATE (98897)

GRIP, HANDLE (77969)

GRIP, HANDLE (77969) (ALT FOR NO. 6122)

UNITS

PER

ASSY

REF

Figure 2. Universal Cargo Compartment Refrigeration Unit and Auxiliary Power Unit Generator Hoist Assembly (3402245-1) (Sheet 2)

USABLE

ON

CODE

A B C

D E

00311 Pages

SM&R

CODE

PEOHH

MDGZZ

XBHZZ

XBHZZ

XBHZZ

AGGZZ

MDGZZ

PFHZZ

PBHZZ

PAHZZ

MDGZZ

PAHZZ

PAHZZ

MDGZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

MGGZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

PAHZZ

PAHZZ

AGGZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

XBHZZ

MDGZZ

MDGZZ

XBHZZ

PAHZZ

ITEM QTY

& 1

400 LBS

MATERIALS AND EQUIPMENT REQUIRED FOR PROOFLOAD TESTING

DESCRIPTION PART NUMBER CAGE

PROOFLOAD STAND 18E8159-1 96916

Figure 3. Proofload Test of Universal Cargo Compartment Refrigeration Unit and Auxiliary Power Unit Generator Hoist Assembly (3402245-1)

00311 Pages

SM&R

MDDZZ

NAVAIR 17-1-114.4.1 00312

1 March 2022 Page 1 of 8

INTERMEDIATE AND DEPOT MAINTENANCE

HOIST ASSEMBLY - AUXILIARY POWER UNIT INSTALLATION

WITH ILLUSTRATED PARTS BREAKDOWN

PART NUMBER 3402246-1

Reference Material

Number

Depot Level Rework Program for Support Equipment End Items ...... ... ... ..... .. ... ....... .. .... ... ... ..... .. ... ...... NAV AIRINST 13680.1 Inspection and Proofload Testing of Lifting Slings for Aircraft and Related Components .... .. .... .. .... .. .... .. NA VAIR 17-1-114.1

Alphabetical Index

Subject Page No.

Assembly, Refinishing and Lubrication Cleaning and Inspection Disassembly Illustrated Parts Breakdown (IPB) Introduction Notes Proofload Test Repair Usable On Codes

Record of Applicable Technical Directives

1. INTRODUCTION.

a. The auxiliary power unit installation hoist assembly is used to lift the auxiliary power unit. Refer to figure 1 for application information.

PART NUMBER

(CAGE):

NOMEN

CLATURE:

NSN:

SAFE

WORKING

LOAD:

APPLICATION:

3402246-1 98897

HOIST

ASSEMBLY,

AUXILIARY

POWER UNIT

INSTALLATION

l 730-01-006-

400LB

C/KC-130T/J

Figure 1. Application Information

None

2. DISASSEMBLY.

a. The auxiliary power unit installation hoist assembly, PIN 3402246-1 (98897), shall be disassembled in accordance with figure 2. General disassembly of hoist components shall be accomplished in accordance with good shop practices.

3. CLEANING AND INSPECTION.

a. Clean hoist as necessary in accordance with NAVAIR 17-1-114.1, Work Package (WP) 005 00 to remove dirt, oil, grease and other foreign matter.

b. Perform a detailed inspection of the entire hoist assembly in accordance with NAVAIR 17-1-114.1, WP 005 00. Cracks are not acceptable. Leave paint intact and mark any suspect damaged areas. Remove paint from suspect areas and stress areas for Non-Destructive Inspection (NDI).

1299789680A Highlight

a. Removal and replacement of hardware and readily available parts is permitted in accordance with applicable SM&R codes in figure 2. There is no repair for pins, washers and other common hardware. Damaged hardware shall be rejected and replaced with new hardware. All hardware shall be inspected prior to assembly. Refer to

NA VAIR 17-1-114.1, WP 005 00.

b. In general, surface defects on the hoist's structural members, attachments, and fittings such as cracks, nicks, and gouges, may be repaired by hand filing and blending with the surrounding area to remove the defect as long as 90 percent or more of the component cross sectional dimension/area is intact. Refer to NAVAIR 17-1-114.1, WP 005 00.

5. ASSEMBLY,

LUBRICATION.

REFINISHING

MATERIALS REQUIRED

Nomenclature

Primer, Epoxy Coating, Polyurethane

Specification/ Part Number

MIL-PRF-23377

MIL-PRF-85285

AND

HMWS

Index No.

a. The auxiliary power unit installation hoist assembly shall be assembled in accordance with figure 2. General assembly of hoist components shall be accomplished in accordance with good shop practices.

Epoxy Primer, MIL-PRF-23377 1

b. Prime the auxiliary power unit installation hoist assembly where primer was removed for inspection or corrosion control purposes using epoxy primer, MIL-PRF-23377, corrosion inhibiting, lead and chromate free, Type II. There is no allowance for primer in holes or threaded areas.

00312

Polyurethane Coating, MIL-PRF-85285 2

c. Paint the auxiliary power unit installation hoist assembly where paint was removed for inspection or corrosion control purposes using polyurethane coating, MIL-PRF-85285, untinted white (SAE-AMS-STD-595, 17925) or for USMC applications use green (SAE-AMS STD-595, 24052, 34052 or 34084). There is no allowance for paint in holes or threaded areas.

6. PROOFLOAD TEST.

MATERIALS REQUIRED

Nomenclature

Proofload Tag Swaging Sleeve Wire Rope

Specification/ Part Number

MS51844-82

M83420/2-002

HMWS

Index No.

SUPPORT EQUIPMENT REQUIRED

Nomenclature Part Number

Proofload Stand 18E8159-1

a. Due to non-availability of proofload adapters, the proofload task for this sling is to be performed at a sling depot via NA V AIRINST 13680.1 procedures.

b. Perform proofload test of the auxiliary power unit hoist assembly at assigned depot, by mounting it to the proofload stand and hang weight as shown in figure 3. The winch must be operated through a minimum of 1 foot of travel.

c. Locally manufacture proofload tag in accordance with 17-1-114.1, WP 005 00. Attach proofload tag to the frame assembly (1, figure 2) using six inches of wire rope (M83420/2-002) and one swaging sleeve (MS51844-82).

7. ILLUSTRATED PARTS BREAKDOWN (IPB).

a. Refer to figure 2. Refer to NAVAIR 17-1-114.1, WP 002 00 for instructions on how to use this IPB.

1299789680A Highlight

8. NOTES.

Nomenclature

Rubber

MATERIALS REQUIRED

Specification/ Part Number

M6855/2

HMWS

Index No.

a. See figure 4 for manufacturing details for Pad (3402246-15).

9. USABLE ON CODES.

a. The usable on codes for the auxiliary power unit installation hoist assembly are as follows:

Usable On Code Units

A 1 thru 5 B 6 thru 52 C 29 thru 52 D 1 thru23 E 24 thru28 F 6 thru28 G 53 and up H 1 thru 67 I 68 and up J 1 thru 28 K 29 and up

00312

14 15

Figure 2. Auxiliary Power Unit Installation Hoist Assembly (3402246-1) (Sheet 1 of 2)

NO.

PART

NUMBER

3402246-1

3402246-3

NO. 1400

MODEL5407

MODEL 5417

DL1400

3402246-15 4002-8W

4002-0

R4G

3402246-23 3402246-39 3402246-41 3402246-45 3402246-25 3402246-43 M83420/2-008

MS20664C6

NAS1435-K6

3402246-17 3402246-19 M83420/2-004

28-2G

NAS 1335S3S05

MS17984C505

3402246-27

NAS602-6P

MS35335-38

3402246-35 3402246-37

MS20221A-1

MS20392-4C65

MS20392-4C74

MS20392-4C75

AN960-516

NAS1149F0532P

MS24665-283

LS35130D3C2

DESCRIPTION

1 2 3 4 5 6 7

HOIST ASSEMBLY, AUXILIARY POWER UNIT

INSTALLATION (98897)

FRAME ASSY (98897)

TRAILER WINCH (16853)

WINCH

WINCH

WINCH, DRUM, HAND OPERATED (72031)

PAD (98897)

STUD ASSY, TURN LOCK

FASTENER (71286)

EYELET, TURNLOCK FASTENER (71286)

(ATTACHING PARTS)

RING, RETAINING (71286)

CABLE ASSY (98897)

CABLE ASSY (98897)

CABLE ASSY (98897)

CABLE ASSY (98897)

CABLE 0.18 X 360.00 (98897)

CABLE 0.18 X 150.00 (98897)

WIRE ROPE (ALT FOR 3402246-43)

BALL END, WIRE ROPE

TERMINAL, WIRE ROPE, SWAGING

CABLE ASSY (98897)

CABLE (98897)

WIRE ROPE 0.09 X 12.0 (ALT FOR

3402246-19)

SLEEVE, SWAGING (76691)

PIN, QUICK RELEASE

PIN, QUICK RELEASE (ALT FOR

NAS1335S3S05)

GUARD ASSY (98897)

(ATTACHING PARTS)

SCREW, MACHINE

WASHER, LOCK

WASHER (98897)

WASHER (98897)

PULLEY, GROOVE

(ATTACHING PARTS)

PIN, STRAIGHT, HEADED

PIN, STRAIGHT, HEADED

PIN, STRAIGHT, HEADED (ALT FOR

MS20392-4C74)

WASHER, FLAT

WASHER, FLAT (ALT FOR AN960-516)

PIN, COTTER

IDENT PLATE (98897)

UNITS

PER

ASSY

REF

USABLE

ON

CODE

D E C G H

A F C G J K

A B

H I

Figure 2. Auxiliary Power Unit Installation Hoist Assembly (3402246-1) (Sheet 2)

00312 Pages

SM&R

CODE

PEOHH

MDGZZ

XBHZZ

XBHZZ

XBHZZ

XBHZZ

MGGZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

MDGZZ

PAHZZ

PAHZZ

PAHZZ

XBHZZ

XBHZZ

PAHZZ

PAHZZ

XBHZZ

PAHZZ

MDGZZ

PAHZZ

PAHZZ

MDGZZ

MDGZZ

PAHZZ

PAHZZ

XBHZZ

PAHZZ

PAHZZ

PAHZZ

PAHZZ

MDGZZ

Pages

800 LBS

MATERIALS AND EQUIPMENT REQUIRED FOR PROOFLOAD TESTING

ITEM QTY DESCRIPTION PART NUMBER CAGE SM&R

& 1 PROOFLOAD STAND 18E8159-1 96916 MDDZZ

Figure 3. Proofload Test of Auxiliary Power Unit Installation Hoist Assembly (3402246-1)

Page 7/(8 blank)

1.00_J L

NOTES

1. MATERIAL - RUBBER SHEET, PIN M6855/2, CLASS II , GRADE 60, 0.18 IN. THICK.

2. ALL DIMENSIONS ARE IN INCHES AND TOLERANCES ARE± 0.02 FOR 0J(X, UNLESS OTHERWISE SPECIFIED.

Figure 4. Manufacture of Pad (3402246-15)

NAVAIR 17-1-114.4.1 00314

1 March 2022

INTERMEDIATE AND DEPOT MAINTENANCE

SLING FITTING ASSEMBLY - REAR MOUNT

WITH ILLUSTRATED PARTS BREAKDOWN

PART NUMBER 3404003-1

Reference Material

Number

Depot Level Rework Program for Support Equipment End Items ......................................................... NAV AIRINST 13680.1 Inspection and Proofload Testing of Lifting Slings for Aircraft and Related Components ........................ NA VAIR 17-1-114.1

Alphabetical Index

Subject Page No.

Assembly, Refinishing and Lubrication Cleaning and Inspection Disassembly Illustrated Parts Breakdown (IPB) Introduction Notes Proofload Test Repair

Record of Applicable Technical Directives

1. INTRODUCTION.

a. Refer to figure 1 for application information.

PARTNUMBER

CAGE:

NOMENCLATlJRE:

NSN:

SAFE WORKING

LOAD:

APPLICATION:

3404003-1 (98897)

SLING FITTING

ASSEMBLY,

REARMOUNT

l 730-01-454-4216

1750 LB

CIKC-1301

Figure 1. Application Information

None

2. DISASSEMBLY.

a. The rear mount sling fitting assembly, PIN 3404003- 1 (98897), shall be disassembled in accordance with figure 2 . General disassembly of sling components shall be accomplished in accordance with good shop practices.

3. CLEANING AND INSPECTION.

a. Clean sling as necessary in accordance with NAVAIR 17-1-114.1, Work Package (WP) 005 00 to remove dirt, oil, grease and other foreign matter.

b. Perform a detailed inspection of the entire sling in accordance with NAVAIR 17-1-114.1, WP 005 00. Cracks are not acceptable. Leave paint intact and mark any suspect damaged areas. Remove paint from suspect and high stress areas for Non-Destructive Inspection (NDI).

a. Removal and replacement of hardware and readily available parts is permitted in accordance with applicable SM&R codes in figure 2. There is no repair for screws and other common hardware. Damaged hardware shall be rejected and replaced with new hardware. All hardware shall be inspected prior to assembly. Refer to

NA VAIR 17-1-114.1, WP 005 00.

b. In general, surface defects on the sling's structural members, attachments, and fittings such as cracks, nicks and gouges, may be repaired by hand filing and blending with the surrounding area to remove the defect as long as 90 percent or more of the component cross sectional dimension/area is intact. Refer to NAVAIR 17-1-114.1, WP 005 00.

5. ASSEMBLY,

LUBRICATION.

REFINISHING

MATERIALS REQUIRED

Nomenclature

Epoxy Primer Polyurethane Coating

Specification/ Part Number

MIL-PRF-23377

MIL-PRF-85285

AND

HMWS

Index No.

a. The rear mount sling fitting assembly shall be assembled in accordance with figure 2. General assembly of sling components shall be accomplished in accordance with good shop practices.

Epoxy Primer, MIL-PRF-23377 1

b. Prime spreader bar (1) and fitting (12) where primer was removed for inspection or corrosion control purposes using epoxy primer, MIL-PRF-23377, corrosion inhibiting, lead and chromate free, Type II. There is no allowance for primer in holes or threaded areas.

Polyurethane Coating, MIL-PRF-85285 2

c. Paint the spreader bar (1) and fitting (12) where paint was removed for inspection or corrosion control purposes using polyurethane coating, MIL-PRF-85285, 00314 untinted white (SAE-AMS-STD-595, 17925) or for USMC applications use green (SAE-AMS-STD-595, 24052, 34052, or 34084). There is no allowance for paint in holes or threaded areas.

6. PROOFLOAD TEST.

MATERIALS REQUIRED

Nomenclature

Proofload Tag Swaging Sleeve Wire Rope

Specification/ Part Number

MS51844-82

M83420/2-002

HMWS

Index No.

SUPPORT EQUIPMENT REQUIRED

Nomenclature

Proofload Adapter Proofload Adapter

Part Number

26D0358-1 26D0358-2

a. Due to non-availability of proofload adapters, the proofload task for this sling is to be performed at a sling depot via NA V AIRINST 13680.1 procedures.

b. Perform proofload test of sling at assigned depot by restraining at point l:Af> and apply load as shown in figure 3.

c. Locally manufacture proofload tag in accordance with NAVAIR 17-1-114.1, WP 005 00. Attach proofload tag to the link and jaw swivel (2, figure 2) using six inches of wire rope (M83420/2-002) and one swaging sleeve

(MS51844-82).

7. ILLUSTRATED PARTS BREAKDOWN UPB).

a. Refer to figure 2. Refer to NAVAIR 17-1-114.1, WP 002 00 for instructions on how to use this IPB.

8. NOTES.

a. The rear mount sling fitting assembly is used to support the engine turbine assembly during installation and/or removal of the rear engine mount without having to remove the engine from the aircraft.

1299789680A Highlight

Figure 2. Rear Mount Sling Fitting Assembly (3404003-1) (Sheet 1 of2)

00314

UNITS USABLE

INDEX PART DESCRIPTION PER ON SM&R

NO. NUMBER 1 2 3 4 5 6 7 ASSY CODE CODE

3404003-1 SLING FITTING ASSEMBLY, REAR .................................... .. REF PEOHH

MOUNT (98897)

1 3404003-3 SPREADER BAR, FITTING ASSY (98897) ...................... . 1 XDHZZ

2 G403-1-2 SWIVEL, LINK AND JAW (75535) .................................. .. 1 PAHZZ 3 NAS43HT8-8 SPACER .......................................................................... . 2 PAHZZ

3404003-9 CABLE ASSY, SLING (98897) ........................................ .. 1 AGGZZ 4 M83420/2-010 WIRE ROPE 0.25 DIA X 36.0 .................................... .. 1 PAHZZ 5 MS51844-88 SWAGING, SLEEVE ................................................. .. 2 PAHZZ 6 AN100-8 THIMBLE, ROPE ........................................................ . 2 PAHZZ

(ATTACHING PARTS)

7 G-215-3/8 IN SHACKLE (75535) ........................................................... . 1 PAHZZ 8 NAS43HT7-7 SPACER .......................................................................... . 2 XBHZZ

NAS43HT7-6 SPACER (ALT FOR NAS43HT7-7) .................................. . * PAHZZ

3404003-7 CABLE ASSY, SLING (98897) ........................................ .. 1 AGGZZ 9 M83420/2-010 WIRE ROPE 0.25 DIA X 36.0 .................................... .. 1 PAHZZ

10 MS51844-88 SWAGING, SLEEVE ................................................. .. 2 PAHZZ 11 AN100-8 THIMBLE, ROPE ........................................................ . 2 PAHZZ 12 3404003-5 FITTING (98897) ........................................................ . 1 XDHZZ

(ATTACHING PARTS)

13 G-215-3/8 IN SHACKLE (75535) ........................................................... . 1 PAHZZ 14 NAS43HT7-7 SPACER .......................................................................... . 2 XBHZZ

NAS43HT7-6 SPACER (ALT FOR NAS43HT7-7) .................................. . * PAHZZ

15 3404003-11 PIN, CLEVIS (98897) ...................................................... .. 2 XDHZZ

(ATTACHING PARTS)

16 CL-3-C-12.0 CABLE (99862) ............................................................... . 1 PAHZZ 17 CL-5-F FERRULE, WIRE ROPE (99862) .................................... .. 2 PAHZZ

18 3404003-13 PIN, SAFETY (98897) ...................................................... . 2 XDHZZ

90174A115 PIN, RETAINING (39428) (ALT FOR 3404003-13) .......... . * PAHZZ

(ATTACHING PARTS)

19 CL-3-C-12.0 CABLE (99862) ............................................................... . 1 PAHZZ 20 CL-5-F FERRULE, WIRE ROPE (99862) .................................... .. 2 PAHZZ

21 LS3534-3G 1 B 1 LABEL (98897) ................................................................ . 1 XDHZZ

(ATTACHING PARTS)

22 MS21318-15 SCREW, DRIVE ............................................................. .. 4 PAHZZ

Figure 2. Rear Mount Sling Fitting Assembly (3404003-1) (Sheet 2)

Page 5/(6 blank)

1750 LBS

1750 LBS

MATERIALS AND EQUIPMENT REQUIRED FOR PROOFLOAD TESTING

ITEM QTY DESCRIPTION PART NUMBER CAGE SM&R

& 1 PROOFLOAD ADAPTER 26D0358-1 96916 MDDZZ

& 1 PROOFLOAD ADAPTER 26D0358-2 96916 MDDZZ

Figure 3. Proofload Test of Rear Mount Sling Fitting Assembly (3404003-1)

1299789680A Highlight

1299789680A Highlight