1A10C520110910.pdf

TO 1A-10C-5

TECHNICAL MANUAL

BASIC WEIGHT CHECKLIST AND LOADING

DATA

USAF SERIES A-10C AIRCRAFT

Prepared by HEBCO, INC.

FA8202-09-A-0001

THIS PUBLICATION SUPERSEDES TO 1A-10C-5 DATED 10 NOVEMBER 2010,

CHANGE 2 DATED 15 MARCH 2011.

DISTRIBUTION STATEMENT - E - Distribution authorized to DoD Components only for unclassified and clas-sified technical data. Direct Military Support - The document contains export-controlled technical data of such military significance that release for purposes other than direct support of DoD approved activities may jeop-ardize an important operational military advantage of the United States. Designation of such data is made by competent authority in accordance with DoD Directive 5230.25 (10 September 2011). Other requests for this document shall be referred to OO-ALC/GHAEJ, 6067 Box Elder Lane, Hill AFB, UT 84056-5811.

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. 2751 et seq.) or Executive Order 12470. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE - Handle in compliance with distribution statement and destroy by any method that will prevent disclosure of the contents or reconstruction of the document.

COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTION OF ALL

PERSONNEL CLEARED FOR OPERATION OF SUBJECT AIRCRAFT.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCE

10 SEPTEMBER 2011

LIST OF EFFECTIVE PAGES INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

NOTE: The portion of the text affected by the change is indicated by a vertical line in the outer margins of the page. Changes to illustrations are indicated by shaded or screened areas, or by miniature pointing hands.

Dates of issue for original and changed pages are:

Original ......... 0 ... 10 September 2011

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 142 CONSISTING OF THE FOLLOWING:

PAGE NO. *CHANGE NO. PAGE NO. *CHANGE NO. PAGE NO. *CHANGE NO.

Title A i - v vi Blank 1-1 - 1-50 2-1 - 2-83 2-84 Blank

*Zero in this column indicates an original page.

A USAF

TABLE OF CONTENTS

Chapter Page Chapter Page

LIST OF ILLUSTRATIONS ....................................... ii

LIST OF TABLES ....................................................... ii

INTRODUCTION ....................................................... iii

1 SAMPLE BASIC WEIGHT CHECKLIST

(CHART A) ................................................... 1-1

1.1 PURPOSE AND SCOPE ................ 1-1

1.2 WEIGHT AND BALANCE

SOFTWARE .............................. 1-1

1.3 BALLAST PLATE

PROCEDURES ......................... 1-1

1.3.1 Ballast Plate Marking ..................... 1-2

2 LOADING DATA .............................................. 2-1

2.1 PURPOSE AND SCOPE ................ 2-1

2.2 WEIGHING INSTRUCTIONS ...... 2-1

2.3 WEIGHING INTERVALS ............. 2-1

2.4 AIRPLANE WEIGHING

RECORD ................................... 2-1

2.5 AIRPLANE CONDITION ............. 2-1

2.5.1 Center of Gravity ............................ 2-1

2.5.2 Fixed Ballast ................................... 2-1

2.6 FUEL DRAINING

PROCEDURES ......................... 2-2

2.7 ENGINE OIL .................................. 2-4

2.8 WINDSHIELD WASH FLUID ...... 2-4

2.9 AMMUNITION LOADING .......... 2-4

2.10 PAINT ............................................. 2-4

2.11 WEIGHING, LEVELING,

AND MEASURING

PROCEDURES ......................... 2-4

2.12 OPERATIONAL LOADING

REQUIREMENTS ..................... 2-6

2.13 BALANCE REQUIREMENTS...... 2-6

2.14 GROSS WEIGHT

LIMITATIONS .......................... 2-7

2.15 CENTER OF GRAVITY

TABLE ....................................... 2-7

2.16 MISCELLANEOUS DATA ............ 2-7

i

LIST OF ILLUSTRATIONS

Number Title Page Number Title Page

1-1 32.0 lb Plate Fixed Ballast ....................... 1-1 1-2 Add Decimal ............................................ 1-2 1-3 Edit Item Number .................................... 1-2 1-4 Modified Plate Fixed Ballast ................... 1-2 1-5 Calculated Moment .................................. 1-2 1-6 Ballast Plate Marking .............................. 1-2 1-7 Equipment Locations ............................... 1-34 2-1 Typical Landing Gear Dimension Data ... 2-8 2-2 Loading Data Chart .................................. 2-9 2-3 Ballast Loading Table .............................. 2-12

2-4 Ammunition Loading Table ..................... 2-14 2-5 Store Loading Table ................................. 2-24 2-6 Chaff/Flare Loading Table ....................... 2-40 2-7 Fuel Loading Data ................................... 2-46 2-8 Center of Gravity Table ........................... 2-72 2-9 Typical Service Load Conditions ............. 2-79 2-10 CG Travel Diagram ................................. 2-80 2-11 Sample Weight and Balance Clearance

Form .................................................... 2-83

LIST OF TABLES

Number Title Page Number Title Page

1-1 Basic Weight Checklist Record ............... 1-3 2-1 Fuel Draining Procedure .......................... 2-2

2-2 Unusable Fuel Table ................................ 2-3 2-3 Weight and Moment Due to Paint ............ 2-5 ii

INTRODUCTION

PURPOSE AND SCOPE.

This manual contains a Sample Basic Weight Checklist (Chart A) (Refer to Table 1-1) and Loading Data (Figure 2-2 thru Figure 2-10). Refer to Figure 2-11 for assistance in computing Weight and Balance Data.

INVENTORY.

The Sample Basic Weight Checklist contained herein is to be used only as a guide in preparing checklists for insertion in the Weight and Balance Data, TO 1-1B-50 for A-10C aircraft. If no other Basic Weight Checklist is available, a complete inventory of all equipment in the aircraft must be made for a new checklist.

Check marks must be placed in the proper columns of the new checklist. The loading data is used to make appropriate entries in the Aircraft Weight and Balance Handbook and its computer generated forms. TO 1-1B-50 classifies the A-10C as Class 2 for loading control due to stores affecting the A-10C weight and balance as published in this manual.

MODELS NOT COVERED.

Unless specific modifications not covered by this Loading Data (Figure 2-2 thru Figure 2-10) have been made to any aircraft of this series, the Loading Data contained herein replaces every Loading Data for A-10C aircraft.

MAINTENANCE AND STORAGE.

The A-10C Weight and Balance Manual shall be maintained and stored in a location as determined by the Major Command.

YOUR RESPONSIBILITY - TO LET US KNOW.

Every effort is made to keep the manual current. Review con-ferences with operating personnel and a constant review of ac-cident and flight test reports assure inclusion of the latest data in the manual. We cannot correct an error unless we know of its ex-istence. In this regard, it is essential that you do your part. Com-ments, corrections, and questions regarding this manual or any phase of the flight manual program are welcomed. These should be forwarded through your command channels on AF Form 847 to: OO-ALC/GHAEJ, 6057 Box Elder Lane, Hill AFB, UT 84056.

iii

COCKPIT CONFIGURATION LAYOUT.

Cockpit configurations as depicted within this book are TYP- ICAL layouts only. For specific cockpit configuration layout based on aircraft modifications, refer to the following figure:

NOTE

Shadowed boxes indicate the changes from the previous configuration.

ARC2102-059-C1

Not modified by TCTO's 1A-10-1327 and/or 1A-10-1460 and/or

TCTO 1A-10C-509

Modified by TCTO 1A-10C-526

Modified by TCTO's 1A-10-1327 and/or 1A-10-1460

Modified by TCTO 1A-10C-509

Cockpit Configuration iv

RECORD OF TIME COMPLIANCE TECHNICAL ORDERS

The following list of Time Compliance Technical Orders (TCTOs) affect the technical content of this manual. Only current TCTOs are listed. A TCTO is deleted from this list when rescinded, superseded, or fully incorporated.

TCTO NUMBER TITLE DATE

1A-10-1327 Installation of Light Weight Airborne Recovery System (LARS), A/OA-10 Aircraft

24 Feb 93

1A-10-1460 Supplement to Basic Technical Order Installation of AN/ARS-6 Light Weight Airborne Recovery System (LARS) Capability, A/OA-10C Aircraft

1 Nov 2001

1A-10-1496 Installation of Precision Engagement Block Cycle A/OA-10 Aircraft 23 Oct 2006

1A-10-1509 Remove Color Airborne Video Tape Recorder (CAVTR), and replace with Digital Video Airborne Data Recorder (DVADR), on A-10A Air-craft

15 Nov 2005

1A-10-1510 Installation of AN/AAR-47 Missile Warning Set (MWS) capability A/OA-10 Aircraft

15 April 2007

1A-10C-509 Installation of Enhanced Position Location Reporting System (EPLRS)/Situation Awareness Data Link (SADL), AN/ARC-210 Secure Line of Sight (SLOS)/Beyond Line of Sight (BLOS) on A-10C Aircraft

10 Nov 2008

1A-10C-515 Installation of Improved Data Modem (IDM) on A-10C Aircraft 1 May 2009

1A-10C-518 Installation of Onboard Oxygen Generating System (OBOGS) on A-10C Aircraft

1 Aug 09

1A-10C-520 Replacement of Thin-Skinned Wing Assembly P/N 160D610001, with Enhanced Wing Assembly P/N 162D610001-1001, on A-10C Aircraft

1 Oct 2010

1A-10C-526 Installation of Second AN/ARC-210 (ARC-210-2) Radio System on A-10C Aircraft

31 Dec 2010 v/(vi blank)

CHAPTER 1

SAMPLE BASIC WEIGHT CHECKLIST (CHART A)

1.1 PURPOSE AND SCOPE.

Chart A (Table 1-1) contains a list of fixed equipment items with a definite location in the aircraft (Figure 1-7). These items are or may be installed in the aircraft, or can be an alternate instal-lation for standard equipment items. The weight, arm, and mo-ment/1000 are given for each item of equipment. The weights have been rounded to the nearest pound. The moments are cal-culated using rounded weights. Therefore, calculating a moment using the weight and arm data presented in Chart A will result in agreement with the moment presented in Chart A.

1.2 WEIGHT AND BALANCE SOFTWARE.

Weight and Balance (computer generated) Forms DD 365 Record of Weight and Balance Pesonnel, DD 365-1 Chart A Record, DD 365-2 Form B Aircraft Weighing Record, and DD 365-3 Chart C Basic Weight and Balance Record shall be maintained with the Automated Weight and Balance System (AWBS), Computer Program Identification Number (CPIN) 88Z-AWBS/DD365/PCSSE-F001-00A. Weight and Balance Flight Clearance Forms(s) F and DD 365-4 shall be main-tained with the Automatic Form F (AFF) for the A-10C, CPIN 88Z-AFF/A10/PCSSE-F001-00A. AWBS and A-10C AFF soft-ware can be ordered through your Technical Order Distribution Office (TODO), using the CPIN’s listed above or the software can be downloaded from the "https://awbs.hill.af.mil" website (OO-ALC/YPVT Hill AFB, Utah).

1.3 BALLAST PLATE PROCEDURES.

Ballast plates are weighed with the aircraft. The aircraft ba-sic weight accurately accounts for the ballast after a weighing.

When changes to ballast plates are made between weighings, the plates may not be consistently manufactured locally resulting in plates that weigh as much as three pounds off of the specification weights. To correct this error, the following ballast plate proce-dure will be used:

NOTE

All ballast plates are rounded to the nearest pound.

a. If the ballast plate is suspected of not reflecting the Chart A weight while being changed, then weigh the plate.

b. If a ballast plate does not reflect the Chart A - Plate Fixed Ballast ID Number weight within ±1 lb, the plate should be re-made.

c. If the plate cannot be re-made and is an operational ne-cessity, add it to the Chart A by the following:

(1) Choose a Plate Fixed Ballast whose weight is closest to the ballast in question.

(2) Add a line to the Chart A under the chosen Plate Fixed Ballast with a decimal point number.

(3) Give the plate a new Item Number with the cho-sen Plate Fixed Ballast Item Number the same up to the decimal point. Following the decimal point include a sequential number from the last modified plate Item Number.

(4) Name the plate the chosen Plate Fixed Ballast ID Number in the Item Description Field with the term MODIFIED next to it.

(5) Input the newly determined weight to the near-est pound and the appropriate H. Arm. The mo-ment will be calculated automatically.

d. EXAMPLE: For a ballast plate that weighed 34.5 lbs.

that is an operational necessity.

(1) Choose a 32.0 lb Plate Fixed Ballast (Figure 1-1).

Figure 1-1. 32.0 lb Plate Fixed Ballast

1-1

(2) Add a new line to the Chart A under the chosen plate adding a decimal point (Figure 1-2).

Figure 1-2. Add Decimal

(3) Give the plate a new Item Number with the cho-sen Plate Fixed Ballast Item Number the same up to the decimal point. Following the decimal point include a sequential number from the last modified plate Item Number (Figure 1-3).

Figure 1-3. Edit Item Number

(4) Name the plate the chosen Plate Fixed Ballast ID Number in the Item Description Field with the term MODIFIED next to it (Figure 1-4).

Figure 1-4. Modified Plate Fixed Ballast

(5) Input the newly determined weight to the near-est pound and the appropriate H. Arm. The mo-ment will be calculated automatically (Figure 1-5).

Figure 1-5. Calculated Moment

1.3.1 Ballast Plate Marking. Ballast plates are gen-

erally marked on the face of the plate with the ballast plate part number. During an inventory, each ballast plate must be verified.

This process is made easier by stamping ballast plate weights along the front edge of the ballast. In order to stamp the bal-last plates, weigh each plate IAW Paragraph 1.3, then stamp the weight, rounded to the nearest pound, on the leading edge of each ballast plate as follows (Figure 1-6):

Figure 1-6. Ballast Plate Marking

NOTE

Example: Assume a ballast plate has a weight of 32 lbs. The stamp on the front edge of the ballast plate should read, “32 lbs”. Make sure to include “lbs” in order to designate the units of weight.

1-2

Table 1-1. Basic Weight Checklist Record

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: * - NOTES

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

* -014.00 AIRCRAFT

MODIFIED BY

TO 1A-10-1327 OR

1A-10-1460, 1460C

& 1460D (LARS)

* -015.00 ONLY INSTALLED

WHEN

FULLY LARS

CONFIGURED FOR

CSAR MISSION

* -016.00 AIRCRAFT NOT

MODIFIED BY

TO 1A-10-1442

(IFFCC)

* -017.00 AIRCRAFT

MODIFIED BY

TO 1A-10-1442

(IFFCC)

* -018.00 AIRCRAFT NOT

MODIFIED BY

TO 1A-10-1491

(CADC)

* -019.00 AIRCRAFT

MODIFIED BY

TO 1A-10-1491

(CADC)

* -020.00 AIRCRAFT NOT

MODIFIED BY

TO 1A-10-1496(PRE-

CISION ENGAGE-

MENT)(PE)

* -021.00 AIRCRAFT

MODIFIED BY

TO 1A-10-1496

(PRECISION

ENGAGEMENT)

(PE)

1-3

Table 1-1. Basic Weight Checklist Record - Continued

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

* -022.00 AIRCRAFT

MODIFIED BY

TO 1A-10-1509

(DVADR)

* -023.00 AIRCRAFT

MODIFIED BY

SADL/EPLRS (509)

(SADL)

* -024.00 AIRCRAFT NOT

MODIFIED BY

ARC-210 RADIO

SYS. (509) (SLOS)

* -025.00 AIRCRAFT

MODIFIED BY

ARC-210 RADIO

SYS (509) (SLOS)

* -026.00 AIRCRAFT

MODIFIED BY

TO 1A-10C-501

(SCAN

CONVERTER)

* -027.00 AIRCRAFT

MODIFIED

BY BEYOND

LINE OF SIGHT

(TO 1A-10C-509)

(BLOS)

* -028.00 AIRCRAFT

MODIFIED BY

TO 1A-10A-501

(AAR-47)

* -029.00 AIRCRAFT

MODIFIED BY

TO 1A-10C-515

* -030.00 AIRCRAFT NOT

MODIFIED BY

TO 1A-10C-518

(OBOGS)

1-4

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

* -031.00 AIRCRAFT

MODIFIED BY

TO 1A-10C-518

(OBOGS)

* -32.00 Due to gun vibes ballast plate B-9 or B-10 and either B-11 or B-12 must be used when variable ballast is installed.

* -33.00 AIRCRAFT NOT

MODIFIED BY

TO 1A-10C-526

(ARC-210-2 RADIO

SYS)

* -34.00 AIRCRAFT

MODIFIED BY

TO 1A-10C-526

(ARC-210-2 RADIO

SYS)

1-5

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: A - NOSE COMPARTMENT - STA. 124 - 225/NLG WHEEL WELL

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment (Simp)

In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

A -000.00 FORWARD

FUSELAGE -

UPPER -VERTICAL

CENTERLINE

2000/05/08

A -001.00 UARRSI

2730526M5 or M13

82.0 170.00 13.9 2003/05/19

A -002.00 UARRSI

2760117-101 or 102

78.0 170.00 13.3 2003/06/02

A -003.00 ACCESS - HINGED

WINDSHIELD

2000/05/08

A -005.00 IFFCC COMPUTER

(NOTE 17)

20.0 199.00 4.0 2004/01/06

A -006.00 LASTE/IFFCC

COMPUTER

MOUNT

5.0 199.00 1.0 2004/01/06

A -007.00 TEMPERA-

TURE CON-

TROLLER-WIND-

SHIELD

2.0 198.00 0.4 2002/12/11

A -008.00 ELECTRICAL

EQUIP ACCESS

- F61

2000/05/08

A -009.00 BOX-BATTERY

BUS & RELAY

16.0 171.00 2.7 2002/12/12

A -009.01 INVERTER

MGH182-100A

2006/10/23

A -010.00 INVERTER

MS17406-1

BENDIX (ALT.

TO A-11)

18.0 173.00 3.1 2003/01/14

A -011.00 INVERTER

MS17406-1

AMF-LELAND

ELECTROSYSTEM

(ALT. TO A-10)

22.0 173.00 3.8 2003/01/24

1-6

Item Number Item Description Weight

H.

Arm

H. Mo-ment (Simp)

In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

A -012.00 BATTERY

ACCESS- F65

2000/05/08

A -013.00 BATTERY

M81757/9-2 or

MS24498 (60 DAY)

80.0 192.00 15.4 2004/07/13

A -014.00 BATTERY

M81757/16-1 (1

YEAR)

78.0 192.00 15.0 2004/07/13

A -015.00 ADF ANTENNA &

GUN ACCESS

2000/05/08

A -016.00 ANTENNA -

UHF/ADF

7.0 181.00 1.3 2003/01/14

A -017.00 NOSE LANDING

GEAR WHEEL

WELL

2000/05/08

A -018.00 AMPLIFIER

DETECTOR (2) EA.

AM6639/ALR-69

(V)

7.0 158.00 1.1 2003/01/14

A -019.00 WINDSHIELD

WASH TANK

11.0 159.00 1.7 2001/06/19

A -020.00 UMBILICAL

DISPLAY UNIT

2.0 225.00 0.5 2002/12/12

1-7

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: B - GUN BAY COMPARTMENT - LEFT NOSE TO STA. 365

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

B -000.00 GUN REMOVAL

ACCESS - F3, F5,

F9, F15, F17, F19, F67

2000/05/08

B -001.00 MUZZLE CLAMP 14.0 121.00 1.7 2002/12/11

B -002.00 GUN BARREL

SEAL-NOSE

19.0 140.00 2.7 2001/06/19

B -003.00 GUN, MOUNTS &

CONTENTS

712.0 198.00 141.0 2003/03/12

B -004.00 CHUTING 123.0 238.00 29.3 2001/06/19

B -006.00 GUN DRIVE &

CONTENTS

104.0 254.00 26.4 2008/05/07

B -007.00 AMMO DRUM &

CONTENTS (NO

AMMO-1,174 RD,

SEP)

959.0 311.00 298.2 2003/01/28

B -008.00 GUN REMOVAL

ACCESS - F3

2000/05/08

B -009.00 BASE PLATE -

FIXED BALLAST

160D111011-41

(ALT TO B-10)

(NOTE 32)

32.0 183.00 5.9 2003/03/12

B -010.00 BASE PLATE -

FIXED BALLAST

160D111011-67

(ALT TO B-9)

(NOTE 32)

11.0 183.00 2.0 2003/03/12

B -011.00 PLATE-FIXED

BALLAST

160D111011-65

(ALT TO B-12)

(NOTE 32)

11.0 184.00 2.0 2003/05/05

1-8

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

B -012.00 PLATE-FIXED

BALLAST

160D111011-39

(ALT TO B-11)

(NOTE 32)

32.0 184.00 5.9 2003/05/05

B -013.00 PLATE-FIXED

BALLAST

160D111011-39

32.0 184.00 5.9 2003/02/24

B -014.00 PLATE-FIXED

BALLAST

160D111011-39

32.0 184.00 5.9 2003/02/24

B -015.00 PLATE-FIXED

BALLAST

160D111011-53

30.0 184.00 5.5 2003/02/24

B -016.00 PLATE-FIXED

BALLAST

160D111011-53

30.0 184.00 5.5 2003/02/24

B -017.00 PLATE-FIXED

BALLAST

160D111011-53

30.0 184.00 5.5 2003/02/24

B -018.00 WATER

SEPARATOR

(NOTE 31)

8.0 271.00 2.0 2006/08/18

1-9

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: C - COCKPIT COMPARTMENT - STA. 203 - 268

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

C -000.00 COCKPIT

FORWARD AREA

2000/05/08

C -001.00 PROJECTION

UNIT, HEADS-UP

DISPLAY

51.0 214.00 10.9 2003/06/24

C -002.00 RHAW-AZIMUTH

IND. AN/ALR-69

(V)

3.0 222.00 0.7 2003/02/27

C -004.00 CAMERA 2.0 222.00 0.4 2008/05/07

C -004.01 LEFT HAND

MULTI-FUNCTION

CONTROL/DIS-

PLAY UNIT (NOTE

21)

10.0 222.00 2.2 2005/04/07

C -004.02 RIGHT HAND

MULTI-FUNCTION

CONTROL/DIS-

PLAY UNIT (NOTE

21)

10.0 222.00 2.2 2005/04/07

C -005.00 STANDBY

ATTITUDE IND.

ARU-42/A-1

2.0 223.00 0.4 2001/06/19

C -006.00 ALTIMETER

AAU-34/A

4.0 223.00 0.9 2002/12/12

C -007.00 ATTITUDE

INDICATOR

ARU-2B/A

8.0 223.00 1.8 2001/06/19

C -008.00 LASTE OPTION

SELECT PANEL

(NOTE 20)

2.0 223.00 0.4 2005/04/07

C -008.01 UP FRONT

CONTROLLER

(NOTE 21)

2.0 223.00 0.4 2005/04/07

1-10

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

C -009.00 REMOTE FREQ.

IND - UHF-TYPE

ID-1961B/

ARC-164(V)

2.0 224.00 0.4 2002/12/12

C -009.01 REMOTE

FREQUENCY

INDICATOR

UHF-TYPE

ID-1961D/

ARC-164(V) (NOTE

6)

1.0 224.00 0.2 2007/08/01

C -010.00 AIRSPEED

INDICATOR

3.0 224.00 0.7 2001/06/19

C -011.00 RHAW-THREAT

DIS-

PLAY-AN/ALR-69(V)

(ALT TO C-11)

4.0 224.00 0.9 2001/06/19

C -012.00 CONTROL,

COUNTERMEA-

SURES SET

C-12546/ALQ-213

2.0 224.00 0.4 2008/05/07

C -013.00 DISPLAY

PANEL-FUEL/

HYD.SYSTEM

2.0 224.00 0.4 2002/12/12

C -014.00 HORIZONTAL

SITUATION IND.

AQU-6/A

7.0 224.00 1.6 2001/06/19

C -015.00 CONTROL

PANEL-ARMA-

MENT (NOTE 20)

9.0 224.00 2.0 2005/04/07

C -016.00 MAVERICK TV

MONITOR (NOTE

20)

15.0 224.00 3.4 2005/04/07

C -016.01 ARMAMENT/HUD

CONTROL PANEL

(NOTE 21)

2.0 225.00 0.5 2005/04/07

C -016.02 LT

MULTI-FUNCTION

COLOR DISPLAY

10.20 220.00 2.3 2006/10/23

C -016.03 RT

MULTI-FUNCTION

COLOR DISPLAY

10.20 220.00 2.3 2006/10/23

C -017.00 CONTROL PANEL

- LANDING GEAR

3.0 225.00 0.7 2003/01/27

1-11

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

C -018.00 PANEL - ENGINE

INSTRUMENTS

11.0 225.00 2.5 2003/01/27

C -019.00 CONTROL

PANEL-LASER

SPOT SEEKER

5.0 226.00 1.1 2003/01/24

C -020.00 PANEL ASSY.

ESSENTIAL

CIRCUIT

BREAKER

7.0 228.00 1.6 2002/12/12

C -021.00 COCKPIT

CONSOLE - LEFT

2000/05/08

C -022.00 CONTROL

PANEL - FUEL

MANAGEMENT

2.0 233.00 0.5 2003/01/27

C -023.00 CONTROL

PANEL-LIGHTING

2.0 241.00 0.5 2002/12/12

C -024.00 CONTROL

PANEL-IFF

TYPE C-6280(P)

APX-101(V)

3.0 245.00 0.7 2003/01/24

C -025.00 CONTROL

PANEL-VHF/AM

AN/ARC-186(V)

(NOTE 24)

2.0 246.00 0.5 2008/05/07

C -025.01 ARC-210 RADIO

CONTROL

C-12561A (NOTE

25)

5.0 248.00 1.2 2008/01/23

C -025.02 LARS CONTROL

DISPLAY UNIT

(ALT TO 26) (NOTE

4 AND 5)

3.0 246.00 0.7 2003/07/01

C -026.00 LARS CONTROL

DISPLAY UNIT

(NOTE 14 & 15)

3.0 246.00 0.7 2008/05/07

C -026.01 CONTROL

PANEL - VHF/AM

AN/ARC-186(V)

(ALT TO 25) (NOTE

9)

2.0 246.00 0.5 2003/07/01

C -027.00 CONTROL

PANEL-UHF -

AN/ARC-164(V)

(NOTE 24)

9.0 250.00 2.3 2008/01/23

1-12

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

C -027.01 CONTROL

PANEL-UHF -

AN/ARC-164(V)

(NOTE 25)

9.0 253.00 2.3 2008/01/23

C -028.00 CONTROL

PANEL-EMER-

GENCY

3.0 251.00 0.8 2002/12/12

C -029.00 CONTROL

PANEL-VHF/FM

AN/ARC-186(V)

(NOTE 24)

2.0 254.00 0.5 2008/01/03

C -030.00 CONTROL

PANEL-INTER-

COM TYPE C-3942

(P) ATC-18

4.0 256.00 1.0 2002/12/12

C -032.00 CONTROL PANEL

- KY-58 (NOTE 24)

2.0 256.00 0.5 2008/01/23

C -032.01 CONTROL PANEL

- KY-58 (NOTE 25)

2.0 259.00 0.5 2008/01/23

C -033.00 CONTROL

CONSOLE - RIGHT

2000/05/08

C -034.00 PROCESSOR,

COUNTERMEA-

SURE SIGNAL

CP-2385/ALQ-213

5.0 231.00 1.2 2008/05/07

C -036.00 CONTROL

PANEL-CAUTION

4.0 235.00 0.9 2008/05/07

C -037.00 OXYGEN REGU-

LATOR-CRU-73/A

(NOTE 30)

3.0 240.00 0.7 2001/06/19

C -037.10 OXYGEN

REGULATOR

(NOTE 31)

4.0 240.00 0.9 2006/08/18

C -037.20 OXYGEN

MONITOR (NOTE

31)

1.0 251.00 0.3 2006/08/18

C -039.00 CONTROL

DISPLAY UNIT

11.0 244.00 2.7 2008/05/07

C -040.00 AVIONICS AUX

PANEL

1.0 247.00 0.2 2008/05/07

1-13

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

C -043.00 CONTROL

PANEL-INT. & EXT.

LIGHTS

6.0 255.00 1.5 2001/06/19

C -044.00 DVADR -

RECORDER &

MOUNT (NOTE 22)

8.5 267.00 2.3 2006/05/01

C -045.00 PILOTS SEAT AND

EQUIPMENT

2000/05/08

C -046.00 SURVIVAL KIT 23.0 249.00 5.7 2001/06/19

C -047.00 EJECTION

SEAT-PILOTS

122.0 254.00 31.0 2001/06/19

C -048.00 PARACHUTE 24.0 268.00 6.4 2001/06/19

C -049.00 EMERGENCY

OXYGEN

CYLINDER (NOTE

30)

3.0 275.00 0.8 2004/04/21

C -049.10 REOS CYLINDER

(NOTE 31)

11.0 263.00 2.9 2006/08/18

C -050.00 NOTE: PILOT’S

EJECTION SEAT

INCLUDES

ACTUATOR &

BALLISTICS

2000/05/08

C -050.01 SYSTEM, DATA

TRANSFER

6.0 279.00 1.7 2002/12/12

C -050.02 MOUNT ASSY,

DTU

4.0 279.00 1.1 2002/12/16

C -051.00 MISCELLANEOUS

- COCKPIT - AFT

LEFT

2000/05/08

C -052.00 UPGRADED DATA

TRANSFER UNIT

(UDTU)

6.0 279.00 1.7 2008/05/07

C -054.00 UDTU

ENCLOSURE

7.0 279.00 2.0 2008/05/07

C -054.01 EMI ENCLOSURE,

DTU

7.0 279.00 2.0 2002/12/16

C -055.00 LADDER

COMPARTMENT

- F69

2000/05/08

1-14

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

C -056.00 LADDER-CREW

BOARDING

(STAINLESS

STEEL)

23.0 246.00 5.7 2003/01/24

C -057.00 COCKPIT -

EXTERNAL -

RIGHT

2000/05/08

C -058.00 ADAPTER-PAVE

PENNY

16.0 236.00 3.8 2002/12/12

C -059.00 OXYGEN

CONVERTER

ACCESS - F2

2000/05/08

C -060.00 LIQUID OXYGEN

- 5 LITERS (NOTE

30)

13.0 261.00 3.4 2003/01/28

C -061.00 LOX CON-

VERTER-MB-5/A

(NOTE 30)

15.0 261.00 3.9 2001/06/19

C -062.00 OXYGEN

CONCENTRATOR

(NOTE 31)

35.0 261.00 9.0 2006/08/18

C -063.00 PLENUM (NOTE

31)

12.0 261.00 3.0 2006/08/18

1-15

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: D - EQUIPMENT COMPARTMENT-AVIONICS - STA. 268 - 365

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -000.00 ELECTRICAL

EQUIPMENT

ACCESS - F99

2000/05/08

D -000.01 GPS/EPLRS FILL

PANEL

1.45 269.38 0.401 2008/11/10

D -001.00 BLOS FILL PORT

AND CABLE

(NOTE 27)

2.0 270.00 0.5 2008/05/15

D -001.01 BLACK/RED FILL

PORTS

2.3 270.00 0.62 2008/11/10

D -002.00 CODER/DECODER

- FILL/KY-58

7.0 275.00 1.9 2008/05/07

D -003.00 PROGRAM-

MER-C1-286/ALE-40

(V) (ALT TO D-3)

3.0 279.00 0.8 2003/01/24

D -004.00 COUNTERMEA-

SURE SYSTEM

MUX 1 ASSY

2.0 279.00 0.6 2008/05/07

D -004.01 COUNTERMEA-

SURE SYSTEM

MUX 1 ASSY (ALT

TO D-2)

2.0 279.00 0.6 2003/01/24

D -005.00 TRANSPONDER

COMPUTER KIT

1C/T SEC

11.0 282.00 3.1 2002/12/12

D -006.00 ELECTRICAL

EQUIPMENT

ACCESS - F101

2000/05/08

D -007.00 GENERATOR

CONTROL UNIT,

#1 ENGINE

4.0 292.00 1.2 2003/08/08

D -008.00 RELAY Z-A1A-026 2.0 293.00 0.6 2001/06/19

1-16

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -009.00 CONTROLLER

(ROLL/TRIM)

1605T100

2.0 293.00 0.6 2003/03/20

D -010.00 BALANCE CONT

- INTERIOR

LIGHTING

8.0 300.00 2.4 2003/01/27

D -011.00 CONVERTER

MS27209 (NOTE

20)

9.0 300.00 2.7 2005/04/07

D -011.01 CONVERTER

MS28132 (NOTE

21)

18.0 300.00 5.4 2005/04/07

D -011.02 CONVERTER 17.0 300.00 5.1 2001/06/19

D -012.00 CONTACTOR

B-345

5.0 301.00 1.5 2001/06/19

D -013.00 ALPHA/MACH

COMPUTER

C-31206-4

9.0 309.00 2.8 2001/06/19

D -014.00 POWER DIODE 3.0 311.00 0.9 2001/06/19

D -015.00 AVIONICS ACCESS

- F103

2000/05/08

D -016.00 RECEIVER

TRAN VHF/FM

AN/ARC-186 (V)

(NOTE 33)

7.0 319.00 2.2 2004/01/23

D -016.01 ARC-210-2 RADIO

RT-1851A (C)

(NOTE 34)

11.0 318.7 3.51 2010/12/31

D -016.02 MOUNT,

ARC-210-2 (NOTE

34)

1.6 318.7 0.51 2010/12/31

D -016.03 ADAPTER PLATE,

ARC-210-2 RT

MOUNTING (NOTE

34)

0.67 318.7 0.22 2010/12/31

D -017.00 BOX - LIGHTING

TRANSFORMER

7.0 322.00 2.3 2008/05/15

D -017.01 BOX - LIGHTING

TRANSFORMER

(NOTE 27)

7.0 320.00 2.2 2008/05/15

D -018.00 RELAY

BOX-AVIONICS

7.0 326.00 2.3 2003/01/14

1-17

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -018.01 RELAY BOX -

AVIONICS (NOTE

27)

7.0 326.00 2.3 2008/05/15

D -019.00 MOUNT

MT-4682A/A

7.0 329.00 2.3 2003/01/24

D -020.00 ADAPTER

MX-9577/A

4.0 329.00 1.3 2003/01/24

D -021.00 TACAN

RCVR/XMTR

RT-1159A

25.0 329.00 8.2 2003/01/24

D -021.05 ARC-210 HPA

(NOTE 27)

9.0 333.00 3.0 2008/05/07

D -021.10 ARC-210 HPA

MOUNT (NOTE

27)

6.0 333.00 2.0 2008/05/07

D -022.00 RECEIVER TRANS.

RT1063A/APX-101

(V)

14.0 340.00 4.8 2002/12/12

D -022.05 RECEIVER TRANS.

RT1867B/APX-119

10.0 340.00 4.8 2008/01/09

D -023.00 RHAW-PROCES-

SOR CM479/ALR69

LESS MOUNT

25.0 340.00 8.5 2003/01/27

D -023.01 DATABUS

COUPLER

2313DBC03 (NOTE

34)

0.84 316.1 0.27 2010/12/31

D -023.02 DATABUS

COUPLER

2313DBC04 (NOTE

34)

0.84 316.1 0.27 2010/12/31

D -023.03 DATABUS

COUPLER

MOUNTING

BRACKET (NOTE

34)

0.35 315.3 0.11 2010/12/31

D -024.00 AVIONICS ACCESS

- F105

2000/05/08

D -025.00 COMPUTOR

- FLIGHT

DIRECTOR

CPU-80/A

4.0 347.00 1.4 2002/12/12

1-18

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -026.00 RECEIVER -

ILS-R-1871/ARN-108

7.0 350.00 2.5 2002/12/12

D -028.00 COMPASS SAIL

AMPLIFIER,

DETECTOR,

ALR-69

8.0 354.00 2.8 2008/05/07

D -029.00 RECEIVER

CONTROL

C10323/ALR69

21.0 356.00 7.5 2002/12/13

D -030.00 IMPEDENCE

COUPLER

CU2220/ALR-69

(ALT TO D-31)

3.0 359.00 1.1 2003/01/24

D -031.00 COUNTERMEA-

SURE SYSTEM

MUX 2 ASSY

(NOTE 20)

2.0 359.00 0.7 2008/05/07

D -031.01 DATABUS

COUPLER

9413DBC05

0.3 352.00 0.1 2006/10/23

D -031.02 DATABUS

COUPLER

9413DBC06

0.3 360.00 0.1 2003/01/14

D -032.00 RECEIVER

R2094/ALR-69

13.0 360.00 4.7 2002/12/12

D -033.00 SYSTEMS LOAD

CENTER ACCESS -

F75

2000/05/08

D -034.00 CIRCUIT

BREAKER BOX

12.0 333.00 4.0 2002/12/12

D -035.00 AVIONICS

ACCESS- F38

2000/05/08

D -036.00 RELAY BOX

- CANOPY

CONTROL

4.0 273.00 1.1 2002/12/12

D -037.00 RELAY BOX -

FUEL & ENGINE

CONTROL

14.0 281.00 3.9 2008/05/07

D -038.00 FUEL QUANTITY

INTERMEDIATE

DEVICE

5.0 281.00 1.4 2004/03/11

D -039.00 AVIONICS ACCESS

- F40

1-19

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -040.00 RELAY

BOX-FLIGHT

CONTROL

7.0 294.00 2.1 2002/12/12

D -040.01 RELAY BOX-1760

(NOTE 21)

13.0 294.00 3.8 2005/04/07

D -041.00 TRANSDUCER

TRU-164/A (VGH)

2.0 301.00 0.6 2003/03/31

D -042.00 RELAY

BOX-LANDING

GEAR

7.0 302.00 2.1 2002/12/12

D -044.00 RELAY

BOX-ARMAMENT

(NOTE 17)

8.0 303.00 2.4 2004/01/06

D -045.00 ALTITUDE

& AIRSPEED

SWITCH 1500P23

2.0 307.00 0.6 2002/12/12

D -046.00 RELAY BOX-MISC. 8.0 310.00 2.5 2002/12/12

D -047.00 TRANSCEIVER

VHF/AM

AN/ARC-186 (V)

(NOTE 24)

7.0 311.00 2.2 2008/01/03

D -047.01 ARC-210 RADIO

RT-1851A (C)

(NOTE 25)

11.0 311.00 3.4 2008/04/09

D -047.02 ARC-210 MOUNT

ASSEMBLY (NOTE

25)

7.0 311.00 2.2 2008/01/03

D -047.03 CRYPTOGRAPHIC

CABLE

ASSEMBLY (NOTE

25)

2.0 304.34 0.6 2008/01/03

D -048.00 AVIONICS ACCESS

- F42

2000/05/08

D -049.00 MASTER BUS

CONTROLLER

14.0 322.00 4.5 2002/12/12

D -050.00 GYRO - HARS 14.0 322.00 45 2003/01/24

D -050.10 EPLRS RADIO/EPA

(NOTE 23)

26.0 324.00 8.4 2008/04/09

D -050.15 EPLRS RADIO

MOUNTING TRAY

(NOTE 23)

4.0 324.00 1.3 2008/04/09

1-20

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -051.10 AIR DATA

COMPUTER (NOTE

19)

12.0 329.00 3.9 2005/04/07

D -051.15 AIR DATA

COMPUTER (NOTE

23)

12.0 333.00 4.0 2006/12/12

D -052.00 AMPLIFIER - HARS 9.0 332.00 3.0 2003/01/24

D -053.00 COMPUTER

294E415

11.0 340.00 3.7 2002/12/12

D -054.00 ELECTRONIC

PROCESSOR UNIT

12.0 337.00 4.0 2006/12/06

D -054.10 ELECTRONIC

PROCESSOR UNIT

(NOTE 23)

12.0 339.00 4.1 2006/12/12

D -054.20 SADL/ARC-210-2

DIPLEXER (NOTE

34)

3.0 315.00 0.95 2010/12/31

D -055.00 AVIONICS

ACCESS-F44

2000/05/08

D -056.00 EGI MOUNT 6.0 351.00 2.1 2008/05/07

D -058.00 EGI UNIT 26.0 351.00 9.1 2008/05/07

D -060.00 NAVIGATION

MODE RELAY

BOX

17.0 355.00 6.0 2008/05/07

D -061.00 GYRO SBU-13/A

(VGH)

3.0 358.00 1.1 2003/02/04

D -062.00 AVIONICS ACCESS

- F10

2000/05/08

D -063.00 ECU-68/A MULTI-

PLEXER/CONVTR

(VGH)

6.0 291.00 1.7 2003/01/27

D -064.00 ACCELEROME-

TER INDICATOR

ABU-15/A

5.0 292.00 1.5 2001/06/19

D -065.00 FUEL FLOW

SIGNAL

CONVERTER

5.0 292.00 1.5 2002/12/13

D -065.01 DC CONVERTER 17.0 300.00 5.1 2006/10/23

D -065.05 AAR-47 SMART

CABLE & CLAMPS

(NOTE 28)

5.0 297.00 1.5 2008/07/03

1-21

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -066.00 RELAY BOX - A.C.

POWER

3.0 301.00 0.9 2002/12/12

D -067.00 LARS RE-

CEIVER/TRANS-

MITTER (NOTE 14

& 15)

22.0 304.00 6.7 2003/05/07

D -068.00 MOUNT,

RECEIVER

TRANSMITTER,

LARS (NOTE 14)

2.0 304.00 0.6 2004/03/11

D -069.00 CMPT. DETECTOR

ADAPTER-PAVE

PENNY (INCL. MT)

24.0 305.00 7.3 2002/12/17

D -070.00 SIGNAL DATA

RECORDER (VGH)

19.0 308.00 5.9 2003/01/24

D -070.05 AAR-47 CPU &

BRACKET (NOTE

28)

17.0 311.00 5.3 2008/07/03

D -071.00 ELECTRICAL

EQUIPMENT

ACCESS - F12

2000/05/08

D -071.01 SIGNAL DATA

RECORDER

19.0 308.00 5.9 2003/01/24

D -072.00 POWER DIODE 3.0 318.00 1.0 2001/06/19

D -073.00 GENERATOR

CONTROL UNIT.

APU

2.0 320.00 0.6 2005/02/17

D -074.00 CONTACTOR -

APU B-345

5.0 320.00 1.6 2001/06/19

D -075.00 RELAY - BUS TIE

Z-A1A-026

2.0 325.00 0.7 2002/12/13

D -076.00 AUX. RIGHT

CIRCUIT

BREAKER BOX

2.0 332.00 0.7 2002/12/13

D -077.00 CONVERTER

MS27209 (NOTE

20)

9.0 332.00 3.0 2005/04/07

D -077.01 CONVERTER

MS28132 (NOTE

21)

18.0 332.00 6.0 2005/04/07

D -078.00 CONTACTOR

GENERATOR LINE

B-345

5.0 333.00 1.7 2003/01/28

1-22

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -079.00 CIRCUIT

BREAKER BOX

18.0 333.00 6.0 2002/12/13

D -080.00 POWER SUPPLY -

FLASHTUBE

6.0 339.00 2.0 2008/05/07

D -80.01 CURRENT

TRANSFORMER

2006/10/23

D -80.02 AVIONICS

ACCESS-F14

2000/05/08

D-081.00 GENERATOR

CONTROL UNIT,

#2 ENGINE

4.0 340.00 1.4 2003/08/04

D-082.00 ELECTRICAL

TEST PANEL

2.0 340.00 0.7 2002/12/13

D -083.00 ELECTRICAL

EQUIPMENT

ACCESS - F14

2000/05/08

D -084.00 ELECTRONIC

CONTROL

UNIT-GAU-8/A

7.0 348.00 2.4 2001/06/19

D -085.00 AUTOMATIC

VIDEO SWITCH

(NOTE 20)

2.0 348.00 0.7 2005/04/07

D -085.10 SCAN

CONVERTER AND

MOUNT (NOTE 26)

4.0 348.00 1.4 2008/07/23

D -086.00 CIRCUIT

BREAKER BOX

- ARMAMENT

6.0 351.00 2.1 2001/06/19

D -087.00 INTERSTATION

CONTROL UNIT

(NOTE 20)

29.0 353.00 10.2 2005/04/07

D -087.01 CENTRAL

INTERSTATION

CONTROL UNIT

(NOTE 21)

50.0 353.00 17.6 2005/04/07

D -088.00 DIGITAL DATA

PROCESSING

UNIT

9.0 355.00 3.2 2002/12/13

D -089.00 MISCELLANEOUS

- EXTERNAL

FUSELAGE

1-23

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

D -090.00 ANTENNA -

AS-1922 VHF/FM

(NOTE 33)

3.0 295.00 0.9 2002/12/13

D -091.00 ANTENNA

ADAPTER FRPA

2.0 355.00 0.7 2008/05/07

D -092.00 ANTENNA MT.

BASE FRPA

6.0 355.00 2.1 2008/05/07

D -093.00 LARS ANTENNA

SET (MATCHED

PAIR) (NOTE 14)

2.0 320.00 0.6 2003/01/07

D -094.00 ARC-210-1/SAT-

COM ANTENNA

(NOTE 27)

7.0 372.00 2.6 2008/05/15

D -094.01 ARC-210-1/SAT-

COM ANTENNA

ADAPTER HOUS-

ING (NOTE 27)

3.0 372.00 1.1 2008/05/15

D-095.00 IMPROVED DATA

MODEM (NOTE 29)

4.4 338.08 1.5 2008/03/31

1-24

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: E - FUEL COMPARTMENT - STA. 365 - 524.3

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

E -000.00 MISCELLANEOUS 2000/05/08

E -001.00 TRAPPED FUEL

(JP-5)

418.0 445.00 186.0 2003/01/14

E -002.00 DRAINABLE FUEL

(JP-5)

147.0 433.00 63.7 2003/01/14

E -003.00 TRAPPED

FUEL(JP-8)

412.0 445.00 183.3 2003/01/14

E -004.00 DRAINABLE FUEL

(JP-8)

144.0 433.00 62.4 2003/02/04

E -005.00 GRAY FUEL FOAM

FILLER

277.0 439.00 121.6 2002/12/13

1-25

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: F - AFT FUSELAGE COMPARTMENT - STA. 524.3 TO 761.0

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H Arm

H. Mo-ment

(Simp) In A/C

Man Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

F -000.00 HYDRAULIC

COMPARTMENT

ACCESS-F39

2000/05/08

F -001.00 HYDRAULIC

FLUID

RESERVE-LT SYS

17.0 534.00 9.1 2003/03/04

F -002.00 WATER

SEPERATOR

4.0 535.00 2.1 2003/01/28

F -003.00 AIR

CONDITIONING

ACCESS - F45

2000/05/08

F -004.00 REFRIGERATION

UNIT 751851

29.0 551.00 16.0 2001/06/19

F -005.00 ELECTRONIC

CONTROL BOX

APU

3.0 554.00 1.7 2003/01/28

F -006.00 AUXILIARY

POWER UNIT

(APU) ACCESS -

F47

2000/05/08

F -007.00 OIL COOLER-APU 3.0 572.00 1.7 2002/12/18

F -008.00 ALTERNA-

TOR-APU

24.0 572.00 13.7 2002/12/18

F -009.00 PALLET-APU 9.0 574.00 5.2 2001/06/19

F -010.00 AUX POWER UNIT

3800000-7

127.0 576.00 73.2 2003/01/14

F -011.00 HYDRAULIC

PUMP-APU

9.0 579.00 5.2 2002/12/18

F -012.00 HYDRAULIC

ACCESS - RIGHT

SYS - F51

1-26

Item Number Item Description Weight

H Arm

H. Mo-ment

(Simp) In A/C

Man Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

F -013.00 FIRE

EXTINGUISHER

(CHARGED)

13.0 595.00 7.7 2003/01/28

F -014.00 HYDRAULIC

FLUID RESER-

VOIR-RIGHT SYS-

TEM

17.0 618.00 10.5 2003/03/04

F -015.00 LOWER

FUSELAGE -

EXTERNAL

2000/05/08

F -016.00 AN-

TENNA-VHF/FM

(NOTE 33)

5.0 617.00 3.1 2002/12/18

F -017.00 AN-

TENNA-VHF/AM

(NOTE 24)

3.0 645.00 1.9 2008/04/09

F -017.01 SADL ANTENNA

(NOTE 25 & 33)

3.0 645.00 1.9 2008/04/09

F -017.02 SADL ANTENNA

ADAPTER PLATE

(NOTE 25 & 33)

2.0 645.00 1.3 2008/04/09

F -017.03 VHF/UHF/SADL

ANTENNA (NOTE

34)

3.0 617.00 1.85 2010/12/31

F -017.04 PLATE, COVER,

SADL ANTENNA

(NOTE 34)

0.66 645.00 0.42 2010/12/31

F -018.00 HYDRAULIC ACT.

LINKAGE ACCESS

- F57

2000/05/08

F -019.00 FIRE

EXTINGUISHER

(CHARGED)

13.0 645.00 8.4 2002/12/13

F -020.00 TAIL CONE

ACCESS - F59

2000/05/08

F -021.00 LASTE ALTIME-

TER/SWITCHING

UNIT

4.0 704.00 2.8 2003/03/04

F -022.00 AMPLIFIER

DETECTORS (2) EA

AM6639/ALR-69(V)

7.0 749.00 5.2 2003/01/14

1-27

Item Number Item Description Weight

H Arm

H. Mo-ment

(Simp) In A/C

Man Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

F -023.00 AAR-47 SENSOR &

BRACKET (NOTE

28)

6.0 745.00 4.5 2008/07/02

F -024.00 AAR-47 SENSOR &

BRACKET (NOTE

28)

6.0 752.00 4.5 2008/07/02

1-28

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: H - NACELLE COMPARTMENT

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

H -000.00 LEFT ENGINE

& ENGINE

MOUNTED ITEMS

2000/05/08

H -001.00 OIL - IDG SYSTEM 6.0 556.00 3.3 2001/06/19

H -002.00 OIL COOLER-HYD

LT SYS-10590F

(ALT TO H-4)(LOW

FIN)

6.0 556.00 3.3 2003/03/05

H -003.00 OIL COOLER-IDG

SYSTEM-11082-000

(HIGH FIN ONLY)

8.0 556.00 4.4 2003/03/05

H -004.00 OIL COOLER-HYD

LT SYS-11082-000

(ALT TO H-2)(HIGH

FIN)

8.0 556.00 4.4 2003/03/05

H -005.00 HYDRAULIC

PUMP & FLUID

65104-04

26.0 567.00 14.7 2003/01/16

H -006.00 AIR TURBINE

STARTER-3505188

25.0 567.00 14.2 2001/06/19

H -007.00 ENGINE OIL 13.0 568.00 7.4 2002/12/13

H -008.00 RESIDUAL

FLUIDS-ENGINE

OIL & FUEL (JP-5

OR JP-8 FUEL)

18.0 570.00 10.3 2002/12/18

H -009.00 INTERGRATED

DRIVE

GENERATOR (IDG)

79.0 570.00 45.0 2002/12/13

H -010.00 ENGINE

(TF34-GE-100A)

S/N: (SEE H-8

FOR RESIDUAL

FLUIDS)

1417.0 570.00 807.7 2008/04/08

1-29

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

H -011.00 RIGHT ENGINE

& ENGINE

MOUNTED ITEMS

H -012.00 OIL-IDG SYSTEM 6.0 556.00 3.3 2002/12/13

H -013.00 OIL COOLER-HYD

RT SYS-10590F

(ALT

TO H-15)(LOW

FIN)

6.0 556.00 3.3 2003/03/05

H -014.00 OIL COOLER-IDG

SYSTEM-11082-000

(HIGH FIN ONLY)

8.0 556.00 4.4 2003/03/05

H -015.00 OIL COOLER-HYD

RT SYS-11082-000

(ALT

TO H-13)(HIGH

FIN)

8.0 556.00 4.4 2003/03/05

H -016.00 HYDRAULIC

PUMP & FLUID

65104-04

26.0 567.00 14.7 2002/12/13

H -017.00 AIR TURBINE

STARTER-3505188

25.0 567.00 14.2 2002/12/13

H -018.00 ENGINE OIL 13.0 568.00 7.4 2002/12/13

H -019.00 RESIDUAL

FLUIDS-ENGINE

OIL & FUEL (JP-5

OR JP-8 FUEL)

18.0 570.00 10.3 2002/12/18

H -020.00 INTEGRATED

DRIVE

GENERATOR (IDG)

79.0 570.00 45.0 2002/12/13

H -021.00 ENGINE

(TF34-GE-100A)

S/N: (SEE H-19

FOR RESIDUAL

FLUIDS)

1417.0 570.00 807.7 2008/04/08

H -022.00 NOTE: Although the jet engine is listed in Chart A, changes will be shown in Chart C

1-30

CHART A - BASIC WEIGHT CHECKLIST RECORD

COMPARTMENT: J - WING COMPARTMENT

1. 6.

2. 7.

MDS: A-10 3. 8.

SERIAL NO: Sample-A-10 4. 9.

CONSTANT: 1000 5. 10.

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

J -000.00 WING

COMPARTMENT

- LEFT

2000/05/08

J -001.00 PANEL-FUEL

SYSTEM TEST

(LEFT POD)

4.0 368.00 1.5 2002/12/13

J -002.00 WEAPONS

PYLON-STATION 1

(BL 229.4)

99.0 417.00 41.3 2003/01/16

J -003.00 WEAPONS

PYLON-STATION 2

(BL 187)

95.0 431.00 40.9 2003/01/16

J -004.00 WEAPONS

PYLON-STATION 3

(BL 144)

129.0 427.00 55.1 2003/01/16

J-005.00 WEAPONS

PYLON-STATION 4

(BL 66)

133.0 428.00 56.9 2003/01/16

J -006.00 WEAPONS

PYLON-STATION 5

(BL 23) (ALT J-7)

131.0 431.00 56.5 2003/01/16

J -007.00 COVER (ALT

TO J-6)

4.0 437.00 1.7 2001/06/19

J -008.00 SEQUENCER SW.

(LG POD)

4.0 427.00 1.7 2002/12/13

J -009.00 SEQUENCER SW.

(LG POD)

4.0 428.00 1.7 2002/12/13

J.-010.00 CHAFF/FLARE

DISPENSERS (LG

POD FWD)

5.0 477.00 2.4 2002/12/13

J -011.00 CHAFF/FLARE

DISPENSERS (LG

POD AFT)

5.0 486.00 2.4 2002/12/13

1-31

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

J -012.00 SEQUENCER SW.

(WING TIP)

4.0 429.00 1.7 2002/12/13

J -013.00 SEQUENCER SW.

(WING TIP)

4.0 447.00 1.8 2002/12/13

J -014.00 CHAFF/FLARE

DISPENSERS

(WING TIP FWD)

5.0 441.00 2.2 2004/11/18

J -015.00 CHAFF/FLARE

DISPENSERS

(WING TIP AFT)

5.0 461.00 2.3 2004/11/18

J -016.00 WING

COMPARTMENT

- RIGHT

2000/05/08

J -017.00 COVER-(ALT

TO J-18)

3.0 427.00 1.3 2002/12/13

J -018.00 WEAPONS

PYLON-STATION

6 (BL 0) (ALT

TO J-17)

134.0 431.00 57.8 2003/01/16

J -019.00 WEAPONS

PYLON-STATION

7 (BL 23) (ALT

TO J-20)

131.0 431.00 56.5 2003/01/16

J -020.00 COVER-(ALT

TO J-19)

4.0 437.00 1.7 2004/01/06

J -021.00 WEAPONS

PYLON-STATION 8

(BL 66)

133.0 428.00 56.9 2003/01/16

J -022.00 WEAPONS

PYLON-STATION 9

(BL 144)

129.0 427.00 55.1 2003/01/16

J -023.00 WEAPONS

PYLON-STATION

10 (BL 187)

95.0 431.00 40.9 2003/01/16

J -024.00 WEAPONS

PYLON-STATION

11 (BL 229.4)

99.0 417.00 41.3 2003/01/16

J -025.00 SEQUENCER SW.

(LG POD)

4.0 427.00 1.7 2003/01/14

J -026.00 SEQUENCER SW.

(LG POD)

4.0 428.00 1.7 2003/01/02

1-32

Item Number Item Description Weight

H.

Arm

H. Mo-ment

(Simp) In A/C

Man.

Inv. Date 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

J -027.00 CHAFF/FLARE

DISPENSERS (LG

POD FWD)

5.0 477.00 2.4 2003/01/02

J -028.00 CHAFF/FLARE

DISPENSERS (LG

POD AFT)

5.0 486.00 2.4 2003/01/02

J -029.00 SEQUENCER SW.

(WING TIP)

4.0 429.00 1.7 2003/01/02

J -030.00 SEQUENCER SW.

(WING TIP)

4.0 447.00 1.8 2003/01/14

J -031.00 CHAFF/FLARE

DISPENSERS

(WING TIP FWD)

5.0 441.00 2.2 2003/01/14

J -032.00 CHAFF/FLARE

DISPENSERS

(WING TIP AFT)

5.0 461.00 2.3 2003/01/14

J -033.00 AAR-47 SENSOR

& BRACKET LEFT

WINGTIP (NOTE

28)

6.0 431.00 2.6 2008/07/09

J -034.00 AAR-47 SENSOR &

BRACKET RIGHT

WINGTIP (NOTE

28)

6.0 431.00 2.6 2008/07/09

1-33

Figure 1-7. Equipment Locations (Sheet 1 of 17)

1-34

BOG0167

A-015

ADF ANTENNA

B-002

GUN BARREL

NOSE SEAL

B-001

MUZZLE

CLAMP

B-009 OR B-010

AND

AND ANY OF B-011 THROUGH B-017

FIXED BALLAST PLATES

B-003

GUN, MOUNTS,

AND CONTENTS

B-004

CHUTING

B-006

GUN DRIVE

AND CONTENTS

B-007

AMMO DRUM

B-018.00

WATER SEPARATOR

Figure 1-7. Equipment Locations (Sheet 2)

1-35

Figure 1-7. Equipment Locations (Sheet 3)

1-36

E M E R

B R A K E

OFF

DIM

CHAN

STATUS

PRESET

GRDMNL

VOL

MAIN BOTH

ADFOFF

TEST

DISPLAY

TONE OFF ON

SQUELCH

SV0222

AIRCRAFT AFFECTED BY

TCTO 1A-10A-1327 OR

1A-10A-1460

C-022

C-026

C-027 OR

C-027.01

C-025

C-029 OR

C-029.01

C-031 OR

C-032.01

C-030

C-028

C-024

C-023

REFUEL STATUS

& INDEX ERLTS

DIM BRT

HARS/ SAS

OVERRIDE

WPNSTA

STATUS LTS

OFF BRT

SIGNAL

LIGHTS

LAMP TEST

FIRE DETECT

BLEED AIR

LEAK TEST

A

L

U X

T G

NORM

YAW SAS

ENGAGE

OFF

YAW TRIM

RL

L

MONITOR

TEST

OFF

ENGAGE

PITCH SAS

TAKEOFF

TRIM

T/O TRIM

REPLY TEST

EAC

ARM

OFF DIS

NRM

RDR

ALTM

AUTOPILOT

ENGAGE/

DISENGAGE

LASTE

PATH

ALT/HDG

ALT

MODE

OP

LD

RV

ON

3 4

FILL

DELAY

C/RAD

PLAIN

C/RAD

1 3 5

Z E R O I Z E

KY

R C U

INT

HM

HF

FM

IFF

VHF

ILS

UHF

TCN

CALLVOL

I N T E R

I N T E R

V H F

V O L S Q

I S

FM AM

MAN

PRE

LOAD

T O N E

EMER

D

PRESET

DF

TR

OFF

C O M M

75.7712

LIGHT COCKPIT UTILITY

AIRCRAFT

O R

ID

E

A R

M

S A

F E

T Y

S A

F E

C N

D

A N

T I-

G

V A

L V

E

T E

S T

S U

IT

EXT TKS

WING FUS

OFF OVERRIDE

OFFOFFCLOSE

BOOST PUMPS

WING LR

OFF

BOOST PUMPS FILL DISABLE

BRT

RCVR

LT

F

U

E

L

LINE

CHECK

SIG AMPL

NORM

C

L

O

S

E

RCVR

O

P

E

N

RWING

FILL DISABLE

L RMAINL RMAIN

OFF

CROSS

FEED

TK GATE

OPEN

ENG FUEL FLOW

L NORM R

UP

MVR

DN

FLAPS

IDLE

OFF

OFF

L/G WRN

SILENCE DECR

INCR

F R I C T I O N

LEFT CONSOLE

P I D D L E P A C K P A C K

(AIRCRAFT MODIFIED

BY TCTO 1A-10C-513)

IFF

UPPER

BOTH

LOWER

AUTO

UHF ANT

UPPER

LOWER

SPD BRK

EMER RETR

PITCH/ROLL TRIM

NORM

NOSE DN

L

WING

DN

R

WING

DN

NOSE UP

EMER

OVERRIDE

AILERON

EMER

DISENGAGE

L A I L

L R

R

A I L

L E L E V

ELEVATOR

EMER

DISENGAGE

E L E V

R

FLAP

EMER RETR

FLT CONT

NORM

MAN

REVERSION

CODE REPLY TEST MASTER

AUDIO

TEST RAD

TEST

MON

O N

OUT

MODE 1 MODE 3/A

MIC

O U T

IDENT

LIGHT

O U T

I F F

OUT OUT OUT

I F F

O U T

M-1 M-2 M 3 A M-C

OUT

ON

(AIRCRAFT MODIFIED

BY TCTO 1A-10C-509)

C-027 OR

C-027.01

C-029 OR

C-029.01

Figure 1-7. Equipment Locations (Sheet 4)

1-37

Figure 1-7. Equipment Locations (Sheet 5)

1-38

RADAR

BEACON

SINGLE

DOUBLE

E M E R

B R A K E

OFF

DIM

A00.000A00.000

UU

HH

FF

CHAN

STATUS

PRESET

GRDMNL

VOL

MAIN BOTH

ADFOFF

TEST

DISPLAY

TONE OFF ON

SQUELCH

F01-007S06-R03

C-022

C-026

C-027 OR

C-027.01

C-030

C-028

C-024

C-023

REFUEL STATUS

& INDEX ERLTS

DIM BRT

HARS/ SAS

OVERRIDE

WPNSTA

STATUS LTS

OFF BRT

SIGNAL

LIGHTS

LAMP TEST

FIRE DETECT

BLEED AIR

LEAK TEST

A

L

U X

T G

NORM

YAW SAS

ENGAGE

OFF

YAW TRIM

RL

L

MONITOR

TEST

OFF

ENGAGE

PITCH SAS

TAKEOFF

TRIM

T/O TRIM

REPLY TEST

EAC

ARM

OFF DIS

NRM

RDR

ALTM

AUTOPILOT

ENGAGE/

DISENGAGE

LASTE

PATH

ALT/HDG

ALT

MODE

OP

LD

RV

ON

3 4

FILL

DELAY

C/RAD

PLAIN

C/RAD

1 3 5

Z E R O I Z E

KY

R C U

INT

HM

AIM

FM

IFF

VHF

ILS

UHF

TCN

CALLVOL

I N T E R

I N T E R

LIGHT COCKPIT UTILITY

AIRCRAFT

ORIDE

ARM

SAFETY

SAFE

CND

ANTI-GVALVE

TESTSUIT

EXT TKS

WING FUS

OFF OVERRIDE

OFFOFFCLOSE

BOOST PUMPS

WING LR

OFF

BOOST PUMPS FILL DISABLE

BRT

RCVR

LT

F

U

E

L

LINE

CHECK

SIG AMPL

NORM

C

L

O

S

E

RCVR

O

P

E

N

RWING

FILL DISABLE

L RMAINL RMAIN

OFF

CROSS

FEED

TK GATE

OPEN

ENG FUEL FLOW

L NORM R

UP

MVR

DN

FLAPS

IDLE

OFF

OFF

L/G WRN

SILENCE DECR

INCR

F R I C T I O N

LEFT CONSOLE

P I D D L E P A C K P A C K

SPD BRK

EMER RETR

PITCH/ROLL TRIM

NORM

NOSE DN

L

WING

DN

R

WING

DN

NOSE UP

EMER

OVERRIDE

AILERON

EMER

DISENGAGE

L A I L

L R

R A I L

L E L E V

ELEVATOR

EMER

DISENGAGE

E L E V

R

FLAP

EMER RETR

FLT CONT

NORM

MAN

REVERSION

CODE REPLY TEST MASTER

AUDIO

TEST RAD

TEST

MON

O N

OUT

MODE 1 MODE 3/A

MIC

O U T

IDENT

LIGHT

O U T

I F F

OUT OUT OUT

I F F

O U T

M-1 M-2 M 3 A M-C

OUT

ON

(AIRCRAFT MODIFIED

BY TO 1A-10C-526)

IFF ANT

UPPER

SAT ANT

HIGH

BOTH

LOWER LOW

EGI HQ TOD

ARC-210

ARC-164

OFF

C-032 OR

C-032.01

Figure 1-7. Equipment Locations (Sheet 6)

1-39

Figure 1-7. Equipment Locations (Sheet 7)

1-40

Figure 1-7. Equipment Locations (Sheet 8)

1-41

F01-007S09-R03

D-006

D-009

D-010 D-014

D-011

D-012 D-013

D-015

D-001

D-018

D-019

D-031

D-034D-030D-025

D-008

D-004

F-99 F-101

D-005 or

D-002

D-003

F-103

F-75

F-105

D-032 D-033 D-036

D-029 D-026 D-028

D-022

D-020

D-017

D-021

D-095

Figure 1-7. Equipment Locations (Sheet 9)

1-42

ARC2102-5-002-C1

D-006

D-010

D-014D-011

D-012 D-013

D-015

D-001

D-017

D-018

D-031

D-034 D-030D-22.05

D-008

D-004

F-99 F-101

D-005 or

D-002

D-003

F-103

F-75

F-105

D-032 D-033

D-036D-029D-023

D-028

D-021D-016.01

D-095D-21.05

D-016.02

D-23.01 & D-23.02

D-23.03

D-016.03

Figure 1-7. Equipment Locations (Sheet 10)

1-43

F01-007S11-R03

D-039 D-038

D-048 D-47.02

D-043D-046

D-47.01

D-044 D-045

D-042

F-40 F-38

D-052

D-060

D-062

F-44 F-42

D-055 D-058

D-50.10

D-50.15

D-061

D-054.20

Figure 1-7. Equipment Locations (Sheet 11)

1-44

D-094 & D-094.01

D-093

F01-007S12-R03

D-071 D-067

D-066

D-O68

D-069 or 070

OR D-066

LARS R/T

D-065

F-10

F-14 F-12

D-091 & D-092

D-089 D-086

D-081

D-085

D-080

D-078

D-079

D-076

D-075

D-082

D-077

D-074

D-088

D-087

Figure 1-7. Equipment Locations (Sheet 12)

1-45

Figure 1-7. Equipment Locations (Sheet 13)

1-46

Figure 1-7. Equipment Locations (Sheet 14)

1-47

ARC2102-5-005-C2

F-001 F-004 F-005 F-010 F-014

F-009

F-011

F-008

F-007

F-022 F-021

F-019

F-017.03 F-013 F-002

AIRCRAFT Modified by TO 1A-10C-526

F-017.04

Figure 1-7. Equipment Locations (Sheet 15)

1-48

Figure 1-7. Equipment Locations (Sheet 16)

1-49

Figure 1-7. Equipment Locations (Sheet 17)

1-50

CHAPTER 2

LOADING DATA

2.1 PURPOSE AND SCOPE.

The purpose of Chapter 2 is to provide the instructions and pro-cedures necessary to accurately complete the required weight and balance operations for the A-10C aircraft. The scope of Chapter 2 consists of providing the detailed instructions for per-forming the weight and balance function which include:

a. Weighing the Aircraft

(1) Time interval for weight to be performed

(2) Weighing form requirements and dissemination

(3) Condition of the aircraft for performing the weighing operation

b. Required Weight Procedures to include:

(1) Fuel drawing/ammunition unloading

(2) Establishing basic weighing for:

(a) Engine Oil

(b) Windshield Wash Fluid

(c) Paint

(3) Providing detailed weighing, leveling and mea-suring procedures

c. Loading Data Chart details (Figure 2-2)

d. Providing Sample Weight and Balance Clearance form data (Figure 2-11)

2.2 WEIGHING INSTRUCTIONS.

2.3 WEIGHING INTERVALS.

In order to ensure safe operation of the aircraft with weight and Center of Gravity (CG) within limits, the basic weight and mo-ment of the aircraft must be determined, tracked for changes, and recorded. Therefore, in addition to the requirements of TO 1-1B-50, each A-10C aircraft shall be weighed every 36 months. If more than 36 months elapses between weighing, the aircraft shall not be flown until weighing is accomplished.

Under exceptional circumstances, cognizant depot engineering authority may waive the requirements of this paragraph.

2.4 AIRPLANE WEIGHING RECORD.

After completing the aircraft AWBS computer-generated weighing record (DD 365-2, Form B) Airplane Weighing Record (DD Form 365B), forward one copy (noting the previ-ous calculated aircraft weight and % MAC before this weight in the remarks of the form) to: OO-ALC/GHAEJ,Weight & Balance Engineer, Building 1285, 6057 Box Elder Lane, Hill AFB, UT 84056-5811, or export the aircraft AWBS record through E-mail to the Weight & Balance Engineer (Hill.A10.Weight.Bal@Hill.af.mil).

2.5 AIRPLANE CONDITION.

2.5.1 Center of Gravity. The basic weight center of

gravity is established with the aircraft in the following condi-tions:

• Landing gear down

• Trailing edge flaps retracted

• Leading edge slats extended

• Speed brake closed

• All doors and panels closed

• Canopy closed

• UARRSI closed

• Hydraulic reservoirs full

• Engine oil full

• Aircraft boarding ladder retracted

• All pylons installed

2.5.2 Fixed Ballast. Include in the remarks section of

the Airplane Weighing Record (DD Form 365B), the FIXED BALLAST that is installed on the aircraft.

2-1

2.6 FUEL DRAINING PROCEDURES.

NOTE

Aircraft must be fueled to high level shutoff.

Drain fuel as follows:

a. Place aircraft (with normal operational serviced landing gear struts) wheels on a reasonably determined level tarmac/ramp area in ground attitude (zero degrees).

b. Defuel aircraft through single point receptacle by op-erating fuselage and wing tank boost pumps; pump fuel out of fuel tanks through the single-point fueling and de-fueling receptacle located in the left main landing gear pod. (IAW TO 1A-10C-2-12JG-1)

c. Open the drains noted in Table 2-1 and allow fuel to drain until flow rate becomes discontinuous. Fuel re-maining after draining is trapped fuel.

NOTE

Tanks with internal foam always retain some fuel that is not practical to drain. Therefore, draining should be terminated when flow rate becomes discontinuous.

d. In order to duplicate conditions that have been estab-lished by the manufacturer’s testing; the aircraft will be sequentially defueled, drained, and weighed within four hours of completion of the fuel drain process. This pro-cedure will ensure that trapped fuel is retained in the foam.

e. Establish the basic weight with unusable fuel (equiv-alent to the zero point of the fuel quantity indicator).

If the aircraft is weighed after draining the fuel, as outlined, add the drainable fuel weight and moment listed in Table 2-2 or to the as-weighed condition to obtain the basic weight. If the aircraft is weighed with a completely dry fuel system, add the total unusable fuel weight and moment listed in Table 2-2 to the as-weighed condition to obtain the basic weight.

Table 2-1. Fuel Draining Procedure

TO DRAIN NO. ACCESS DOOR DRAIN LOCATION

Forward tank 1 - FS 395.0 external below centerline

Aft tank 1 - FS 501.0 external below centerline

Wing tank 2 - FS 424.9 (±9) BL external below wing sump

Aerial…