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Nov 03/2015 OL0182-25397

AIRPLANE WEIGHT AND BALANCE

CONTROL AND LOADING MANUAL SUPPLEMENT

TO

AVIATION PARTNERS BOEING BLENDED WINGLET PROGRAM

FAA STC: ST01518SE SUPPLEMENT AIRPLANE WEIGHT AND BALANCE

CONTROL AND LOADING MANUAL

MODEL 757-200

With Precision Conversions Freighter Conversion This supplement for the above listed airplane must be attached to the Aviation Partners Boeing Supplement Airplane Weight and Balance Control and Loading Manual, Document No. AP57.2-0603-UAL1, which is attached to the basic Weight and Balance Control and Loading Manual (“Basic Manual”), Boeing Document No. D043N520-UAL1, when the aircraft is modified to a freighter configuration in accordance with Precision Conversions Freighter under Supplemental Type Certificate No. ST01529SE. The information contained herein supplements or supersedes the Aviation Partners Boeing Supplement or the Basic Manual only in those areas listed. For information not contained in this supplement, consult the Aviation Partners Boeing Supplement. For information not contained within the Aviation Partners Boeing Supplement, consult the Basic Manual.

WEIGHT AND BALANCE B757-200PCF CONTROL AND LOADING MANUAL SUPPLEMENT

Introduction Page 1 of 1 Nov 03/2015 OL0182-25397

INTRODUCTION The data presented in this supplement is in compliance with Federal Aviation Regulations. This data is provided for the purpose of establishing the 757-200 Precision Conversions Freighter Conversion aircraft weight and balance requirements. In addition, a revised Weight and Balance Control and Loading Manual Supplement, Chapter 2, Aircraft Weighing Report, is provided. To reiterate the Title page of this document, the information contained herein supplements or supersedes the FAA approved Aviation Partners Boeing Supplement or the FAA approved Basic Manual only in those areas listed. For information not contained in this supplement, consult the Aviation Partners Boeing Supplement. For information not contained within the Aviation Partners Boeing Supplement, consult the Basic Manual. DOCUMENT NUMBERING For all B757-200PCF (Precision Conversion Freighter) Chapter 1 Manuals, document numbering will use the following convention:

OL0182-[XXXXX] where [XXXXX] = Airplane Serial Number


List of Revisions Page 1 of 1 Nov 03/2015 OL0182-25397

LIST OF REVISIONS

REVISION DESCRIPTION BY DATE

IR Initial Release

Ole Leth Nov 03, 2015


List of Effective Pages Page 1 of 3 Nov 03/2015 OL0182-25397

LIST OF EFFECTIVE PAGES

SECTION PAGE REVISION TITLE PAGE IR INTRODUCTION 1 IR LIST OF REVISIONS 1 IR LIST OF EFFECTIVE PAGES 1 IR 2 IR 3 IR TABLE OF CONTENTS 1 IR 2 IR 3 IR AIRPLANE CONFIGURATION 1 IR 1-00-001 1 IR 1-00-042 1 IR 1-02-033 1 IR 2 IR 3 IR 1-04-001 1 IR 2 IR 1-09-003 1 IR 1-32-002 1 IR 1-34-002 1 IR 1-40-001 1 IR 1-44-034 1 IR 2 IR 1-60-005 1 IR 2 IR 1-60-021 1 IR 2 IR 3 IR 4 IR 1-60-041 1 IR 2 IR 3 IR 4 IR 5 IR 6 IR 7 IR 8 IR 9 IR 10 IR



LIST OF EFFECTIVE PAGES (Cont’d)

SECTION PAGE REVISION 1-60-061 1 IR 2 IR 3 IR 4 IR 5 IR 6 IR 7 IR 8 IR 9 IR 10 IR1-62-008 1 IR 1-62-010 1 IR 1-62-020 1 IR 1-62-042 1 IR 2 IR 3 IR 4 IR 5 IR 1-62-065 1 IR 2 IR 3 IR 4 IR 5 IR 1-62-101 1 IR 2 IR 3 IR 1-63-121 1 IR 2 IR 3 IR 1-68-101 1 IR 2 IR 3 IR 4 IR 5 IR 6 IR 7 IR 1-68-102 1 IR 2 IR 3 IR 4 IR



LIST OF EFFECTIVE PAGES (Cont’d)

SECTION PAGE REVISION 1-68-102 (cont’d) 5 IR 6 IR 7 IR 8 IR 9 IR 10 IR 11 IR 12 IR 13 IR 14 IR 15 IR 16 IR 17 IR 18 IR 19 IR 20 IR 21 IR 22 IR 23 IR 24 IR 25 IR 26 IR 27 IR 28 IR 29 IR 30 IR1-86-032 1 IR 1-90-001 1 IR


Table of Contents Page 1 of 3 Nov 03/2015 OL0182-25397

TABLE OF CONTENTS

TITLE CHP-SEC-SUB

PREFACE

INTRODUCTION

LIST OF REVISIONS

LIST OF EFFECTIVE PAGES

TABLE OF CONTENTS

AIRPLANE CONFIGURATION

GENERAL

GENERAL INFORMATION 1-00-001

Weight and Balance Definitions BALANCE REFERENCE SYSTEMS 1-00-042

Balance Arms / Body Stations CERTIFIED WEIGHT AND CENTER OF GRAVITY LIMITS 1-02-033

C.G. Limits – MTW 241000 LB, MLW 198000 LB, MZFW 185400 LB C.G. Limits – MTW 109315 KG, MLW 89811 KG, MZFW 84096 KG

AIRPLANE LATERAL IMBALANCE LIMITS 1-04-001

Fuel Imbalance Versus Lateral Cargo Moment ACE TELESCOPING CARGO SYSTEM – BALANCE EFFECT 1-09-003

Forward Cargo Compartment Aft Cargo Compartment

FLUIDS

POTABLE WATER SYSTEM 1-32-002

Galley Quantity and Location WASTE DISPOSAL SYSTEM 1-34-002

Lavatory Quantities and Locations

PERSONNEL

PASSENGER AND PERSONNEL WEIGHT ALLOWANCES 1-40-001

FAA Advisory Circular 120-27C Allowances INTERIOR ARRANGEMENT – MAIN DECK 1-44-034

Flight Deck Main Cabin – Arrangement



TITLE CHP-SEC-SUB

CARGO

CARGO COMPARTMENTS – LOAD LIMITS 1-60-005

Maximum Allowable Weights

CERTIFIED UNIT LOAD DEVICE POSITION 1-60-021

Unit Load Device Positions – Main Deck FORWARD BODY CUMULATIVE LOADS 1-60-041

Cumulative Load Check AFT BODY CUMULATIVE LOADS 1-60-061

Cumulative Load Check

CARGO COMPARTMENTS 1-62-008

General Location and Arrangement

CARGO HANDLING SYSTEM 1-62-010

Cargo Handling System Limitations

CRUSHABLE CARGO 1-62-020

Crushable Cargo Requirements

FORWARD CARGO COMPARTMENT 1-62-042

Forward Cargo Compartment Volumes Forward Cargo Compartment Cross Sections Cargo Door Dimensions and Allowable Package Sizes

AFT CARGO COMPARTMENT 1-62-065

Aft Cargo Compartment Volumes Aft Cargo Compartment Cross Sections Cargo Door Dimensions and Allowable Package Sizes

MAIN DECK CARGO COMPARTMENT 1-62-101

Main Deck Cargo Compartment Volumes Main Deck Cargo Compartment Cross Section Door Dimensions

UNIT LOAD DEVICES – MAIN DECK 1-63-121

Allowable ULD Devices Engine Transport ULD Center of Gravity Center of Gravity Limits

MAIN DECK UNIT LOAD DEVICE RESTRAINTS 1-68-101

Missing and Inoperative Restraints Main Deck Cargo Lock Locations Main Deck Side Restraint Locations – Size Code ‘A’ ULD Main Deck Side Restraint Locations – Size Code ‘B’ ULD Main Deck Side Restraint Locations – Size Code ‘M’ ULD Main Deck Side Restraint Locations – Engine Pallets ENG 1 & ENG 2



TITLE CHP-SEC-SUB

MISSING AND/OR INOPERATIVE RESTRAINTS 1-68-102

Load Limits – Size Code ‘B’ Load Limits – Engine Transport Load Limits – Size Code ‘A’ and Size Code ‘M’

GROUND OPERATIONS

COMPONENT WEIGHTS AND BALANCE ARMS 1-86-032

Body Components

EXAMPLES

LOADING SCHEDULE DEVELOPEMENT 1-90-001

Ordering Instructions


Airplane Configuration Page 1 of 1 Nov 03/2015 OL0182-25397

AIRPLANE CONFIGURATION The engineering and FAA certification provided by this document are applicable and valid only for the airplane in its delivery configuration upon installation of the Precision Cargo Conversion. With respect to any other modifications, it shall be the responsibility of the buyer to obtain appropriate regulatory agency approval of the data provided by this supplement.


1-00-001 Page 1 of 1 Nov 03/2015 OL0182-25397

GENERAL INFORMATION WEIGHT AND BALANCE DEFINITIONS Balance Terms Lateral Imbalance

The offset of the airplane center of gravity from the airplane centerline. It is usually expressed as a moment (LB-IN. or KG-IN.) about the airplane centerline.

Cargo Terms and Definitions

Approved ULD A unit load device that has been manufactured in accordance to and received approval by the appropriate governmental airworthiness authority indicating the airplane ULD meets their safety requirements.

IATA ULD Technical Manual A document that provides essential data on the various types of unit load devices (ULDs) in use at present in air transportation.

Limit Loads Maximum loads to be expected in service. Limit loads must be supported without detrimental permanent deformation or interference with safe operation.

NAS 3610 A document which defines test conditions for approval of ULDs per TSO-C90c.

Non-Approved ULD A unit load device that has not received approval by the appropriate governmental airworthiness authority indicating the airplane ULD meets their safety requirement.

TSO-C90c Technical Standard Order for the approval of ULDs. NAS 3610 is the minimum performance standard.

ULD Unit Load Device. An assembly of components comprising an aircraft container or an aircraft pallet with nets. The purpose of the unit load device is to enable individual pieces of cargo to be assembled into a standardized sized unit to facilitate rapid loading/unloading onto aircraft having compatible handling and restraint systems which interface directly with the unit.

ULD Position A volume in the cargo compartment which is designated and equipped to be occupied, during flight, by a ULD of specified type.

Ultimate Load Load limits multiplied by the prescribed factors of safety.


1-00-042 Page 1 of 1 Nov 03/2015 OL0182-25397

BALANCE REFERENCE SYSTEM BALANCE ARMS / BODY STATIONS Longitudinal location of all airplane component centers of gravity identified throughout this addendum will be referred to as Balance Arms. The Balance Arm is a true measure in inches from the reference datum 159 inches forward of the airplane nose. Balance Arms are equivalent to Body Stations (B.S.).


1-02-033 Page 1 of 3 Nov 03/2015 OL0182-25397

CERTIFIED WEIGHT AND CENTER OF GRAVITY LIMITS CERTIFIED WEIGHT LIMITS – MTW 241000 LB (109315 KG) The Maximum Certified Gross Weights and Center of Gravity Limits are shown graphically on pages 2 & 3. These Center of Gravity Limits are for taxi, takeoff, flight and landing unless otherwise specified, and are the absolute limits which must not be exceeded by the airplane center of gravity in any taxi, takeoff, flight, or landing configuration. The maximum weight limits may be less if constrained by center of gravity limits. Reference should be made to the basic aircraft manual, including all supplements, to ensure that all current limits are observed.

CERTIFIED GROSS WEIGHTS LB KG

Maximum Taxi Weight (MTW) 241000 109315

Maximum Takeoff Weight (MTOW) 240000 108862

Maximum Landing Weight (MLW) 198000 89811

Maximum Zero Fuel Weight (MZFW) 185400 84096

Minimum Flight Weight (MFW) 122400 55520

LIMITATIONS The following limitations must be met in order to use the certified gross weight and center of gravity limits: The Maximum Zero Fuel Weight limit is only applicable with the APB winglets installed (-2 kit). For operations without the winglets installed (-1 kit) the Maximum Zero Fuel Weight is reduced by 1,400 LB (635 KG).


1-02-033 Page 2 of 3 Nov 03/2015 OL0182-25397

CERTIFIED WEIGHT AND CENTER OF GRAVITY LIMITS (Cont’d) C.G. LIMITS – MTW 241,000 LB, MLW 198,000 LB, MZFW 185,400 LB The following diagram represents the certified Center of Gravity Limits in English units:

WARNING REFER TO PAGE 1 OF THIS SUBJECT FOR LIMITATIONS TO THE C.G. LIMITS.


1-02-033 Page 3 of 3 Nov 03/2015 OL0182-25397

CERTIFIED WEIGHT AND CENTER OF GRAVITY LIMITS (Cont’d) C.G. LIMITS – MTW 109,315 KG, MLW 89,811 KG, MZFW 84,096 KG The following diagram represents the certified Center of Gravity Limits in Metric units:

WARNING REFER TO PAGE 1 OF THIS SUBJECT FOR LIMITATIONS TO THE C.G. LIMITS.


1-04-001 Page 1 of 2 Nov 03/2015 OL0182-25397

AIRPLANE LATERAL IMBALANCE LIMITS FUEL IMBALANCE VERSUS LATERAL CARGO MOMENT Airplane lateral imbalance is an allowance to account for the lateral imbalance loading of cargo and fuel. Cargo imbalance is permitted provided that the fuel imbalance as allowed per Section 1 of the FAA Approved Flight Manual is restricted per the following charts. ULD center of gravity limits are presented in CHP-SEC 1-63-121.


1-04-001 Page 2 of 2 Nov 03/2015 OL0182-25397

AIRPLANE LATERAL IMBALANCE LIMITS (Cont’d)


1-09-003 Page 1 of 1 Nov 03/2015 OL0182-25397

ACE TELESCOPING CARGO SYSTEM – BALANCE EFFECT This section does not apply to the B757-200 Precision Cargo Conversion aircraft. The ACE Telescoping Cargo System has been removed from the forward and aft hold during the installation of the Precision Cargo Conversion. Forward and Aft Cargo Compartment arrangement can be found in CHP-SEC 1-62-042 and CHP-SEC 1-62-065.


1-32-002 Page 1 of 1 Nov 03/2015 OL0182-25397

POTABLE WATER SYSTEM GALLEY QUANTITY AND LOCATION All passenger compartment galleys have been removed from the passenger aircraft and a self-contained hot water container with heater has been added to the flight deck. The following table identifies the quantity and weight of water the container can hold.

FLUID CATEGORY VOLUME/GALLEY WEIGHT/GALLEY

(Water) B.A. IN.

U.S. GAL. L LB KG Container, Max. Volume 2.0 7.6 16.6 7.5 275


1-34-002 Page 1 of 1 Nov 03/2015 OL0182-25397

WASTE DISPOSAL SYSTEM LAVATORY QUANTITIES AND LOCATIONS All passenger compartment lavatories have been removed from the passenger aircraft and a self-contained lavatory has been added to the flight deck. The following table identifies both the potable sink water, as well as the toilet fluid.

FLUID CATEGORY VOLUME/LAVATORY WEIGHT/LAVATORY B.A. IN. U.S. GAL. L LB KG

Sink Water 3.2 12.1 26.6 12.1 310 Chemical Toilet Fluid Precharge Capacity 2.0 7.6 16.6 7.5 310 Maximum Capacity 9.0 34.1 74.8 33.9 310


1-40-001 Page 1 of 1 Nov 03/2015 OL0182-25397

PASSENGER AND PERSONNEL WEIGHT ALLOWANCES FAA ADVISORY CIRCULAR 120-27E ALLOWANCES The following crew, passenger and baggage weights reflect the Federal Aviation Administration (FAA) Advisory Circular 120-27E, dated June 10, 2005. Flight Crew For flight crew members:

Flight crew member 190 LB (86.2 KG)

Pilot flight bag 20 LB (9.1 KG)

Crewmember roller bag 30 LB (13.6 KG)

Occupants For occupants:

Occupants 179 LB (81.2 KG) Carry-on baggage 16 LB (7.3 KG)

Baggage Typical baggage weight is 33 LB (15 KG) per person. However, a considerable variation will exist between various routes depending on such items as overnight stay requirements.


1-44-034 Page 1 of 2 Nov 03/2015 OL0182-25397

INTERIOR ARRANGEMENT – MAIN DECK FLIGHT DECK The flight crew balance arms are defined as 7 IN. in front of the Seat Reference Point (SRP). The SRP is defined as the intersection of the seat bottom and the seat back. The crew locations represent the crew seated at takeoff positions.

* Reference to 1st observer and/or 2nd observer only applicable when seat installed. ** Reference to Supernumeraries only applicable when seat installed.

FLIGHT CREW

LOCATION B.A. IN. Captain 248 First Officer 248 First Observer * 285 Second Observer * 286 Supernumeraries ** 322


1-44-034 Page 2 of 2 Nov 03/2015 OL0182-25397

INTERIOR ARRANGEMENT – MAIN DECK (Cont’d) MAIN CABIN - ARRANGEMENT This section does not apply to the B757-200 Precision Cargo Conversion aircraft. All passenger accommodations have been removed during the installation of the Precision Cargo Conversion. Main deck cargo arrangement can be found in CHP-SEC 1-62-008.


1-60-005 Page 1 of 2 Nov 03/2015 OL0182-25397

CARGO COMPARTMENTS – LOAD LIMITS MAXIMUM ALLOWABLE WEIGHTS This section provides main deck and lower deck cargo compartment loading. These values, when combined, are the maximum allowable loads that can be sustained by the basic monocoque structure. ULD sizes accommodated in the main deck cargo compartment are presented in CHP-SEC 1-63-121. The forward cargo compartment uses bulk loading. The aft cargo compartment uses bulk loading and contains an E6 rack. The four basic structural limitations that must be observed when loading payload are compartment loading, linear loading, floor loading, and cumulative loading limitations. Maximum allowable compartment loading, linear loading, and floor loading are provided for the main deck and lower deck in this section. See 1-60-041 and 1-60-061 for cumulative load limitations.

[a] Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft. [b] See 1-60-021 for pallet positions See NOTES below for additional restrictions

MAIN DECK MAXIMUM ALLOWABLE LOADS – ULD SIZE CODES ‘A’ AND ‘B’ [a]

BALANCE ARM (IN.) LINEAR LOADING FLOOR LOADING

LB/IN. KG/IN. LB/SQ FT KG/SQ FT 125” / 108” 125” / 108”

Sta. 346 to 900 74 33.6 85/98 38.6/44.5 Sta. 900 to 1180 107 48.5 123/142 55.8/64.4 Sta. 1180 to 1680 74 33.6 85/98 38.6/44.5

PALLET POSITION[b] LOAD PER POSITION LB KG 1 5988 2716 2 - 7 6500 2948 8 - 9 9400 4264 10 - 15 6500 2948 ENG 1 – ENG 2 10000 4536


1-60-005 Page 2 of 2 Nov 03/2015 OL0182-25397

CARGO COMPARTMENTS – LOAD LIMITS (cont’d) MAXIMUM ALLOWABLE WEIGHTS (cont’d)

MAIN DECK MAXIMUM ALLOWABLE LOADS – ULD SIZE CODE ‘M’ [a]

BALANCE ARM (IN.) LINEAR LOADING FLOOR LOADING LB/IN. KG/IN. LB/SQ FT KG/SQ FT Sta. 346 to 900 74 33.6 85 38.6 Sta. 900 to 1180 107 48.5 123 55.8 Sta. 1180 to 1680 74 33.6 85 38.6

PALLET POSITION[b] LOAD PER POSITION LB KG 1 6296 2856 2 - 5 7091 3216 6 - 7 10255 4652 8 - 13 7091 3216 ENG 1 – ENG 2 10000 4536

[a] Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft [b] See 1-60-021 for pallet positions See NOTES below for additional restrictions Notes:

1. Weight of ULDs must be considered as payload for computing allowable weight. 2. The “Floor Loading Limit” defines the load carrying capabilities of the individual

compartments; however, the cumulative load limits, maximum ULD load, and any other applicable load limits must still be observed.

3. The limits of this section do not reflect the strength of the ULDs or the loading system. 4. Maximum Pallet Loading assumes no observers or supernumeraries on aircraft.

Deductions in pallet loading must be made to Pallet Position 1 if observers or supernumeraries are on board.

LOWER HOLD MAXIMUM ALLOWABLE LOADS

COMPARTMENT TOTAL WEIGHT LINEAR LOADING FLOOR LOADING LB KG LB/IN KG/IN LB/SQ FT KG/SQ FT Forward Cargo Hold 10300 4672

B.A. 508 to B.A. 624 5445 2469 47.0 21.3 150.0 68.0 B.A. 624 to B.A. 845 10300 4672 47.0 21.3 150.0 68.0

Aft Cargo Hold 16300 7393 B.A. 1200 to B.A. 1377 8319 3773 47.0 21.3 150.0 68.0 B.A. 1377 to B.A. 1640 12361 5606 47.0 21.3 150.0 68.0


1-60-021 Page 1 of 4 Nov 03/2015 OL0182-25397

CERTIFIED UNIT LOAD DEVICE POSITION UNIT LOAD DEVICE POSITIONS – MAIN DECK The following diagrams illustrate the unit load device positions. For ULD centroid locations, see CHP-SEC 1-63-121 SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD POSITION DIAGRAM

ULD SIZE CODES ‘A’ AND ‘B’

ULD POSITION

FROM BALANCE ARM (IN.)

TO BALANCE ARM (IN.)

1 346.0 434.5 2 434.5 523.5 3 523.5 612.5 4 612.5 701.5 5 701.5 790.5 6 790.5 879.5 7 879.5 968.5 8 968.5 1057.5 9 1057.5 1146.5 10 1146.5 1235.5 11 1235.5 1324.5 12 1324.5 1413.5 13 1413.5 1502.5 14 1502.5 1591.5 15 1591.5 1680.0

NOTE: Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft.


1-60-021 Page 2 of 4 Nov 03/2015 OL0182-25397

CERTIFIED UNIT LOAD DEVICE POSITION (Cont’d) SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD POSITION DIAGRAM WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

SIZE CODES ‘A’ AND ‘B’ ULD W/ ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

ULD POSITION



1 346.0 434.5 2 434.5 523.5 3 523.5 612.5 4 612.5 701.5 5 701.5 790.5 6 790.5 879.5

ENG 1 904.5 1030.5 ENG 2 1030.5 1156.5

11 1235.5 1324.5 12 1324.5 1413.5 13 1413.5 1502.5 14 1502.5 1591.5 15 1591.5 1680.0



1-60-021 Page 3 of 4 Nov 03/2015 OL0182-25397

CERTIFIED UNIT LOAD DEVICE POSITION (Cont’d) SIZE CODE ‘M’ ULD POSITION DIAGRAM

SIZE CODE ‘M’ ULD

ULD POSITION



1 346.0 442.0 2 501.0 597.5 3 597.5 694.5 4 694.5 791.0 5 808.0 904.5 6 904.5 1001.5 7 1001.5 1098.5 8 1098.5 1195.5 9 1195.5 1292.5 10 1292.5 1389.5 11 1389.5 1486.5 12 1486.5 1583.5 13 1583.5 1680.0



1-60-021 Page 4 of 4 Nov 03/2015 OL0182-25397

CERTIFIED UNIT LOAD DEVICE POSITION (Cont’d) SIZE CODE ‘M’ ULD POSITION DIAGRAM WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

SIZE CODE ‘M’ ULD W/ ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

ULD POSITION



1 346.0 442.0 2 501.0 597.5 3 597.5 694.5 4 694.5 791.0 5 808.0 904.5

ENG 1 904.5 1030.5 ENG 2 1030.5 1156.5

9 1195.5 1292.5 10 1292.5 1389.5 11 1389.5 1486.5 12 1486.5 1583.5 13 1583.5 1680.0



1-60-041 Page 1 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS CUMULATIVE LOAD CHECK The cumulative total load profile is computed forward to aft in the forward body and must not exceed the load distribution limitations shown in the tables below. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft. MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD

LOCATION & LOADING

DIRECTION

BALANCE ARM (IN.) MAXIMUM COMBINED FWD CUMULATIVE LOAD FROM TO LB KG

Forward Body- Loading Forward

to Aft 297

434.5 5988 2716 523.5 9612 4360 612.5 17352 7871 701.5 25479 11557 790.5 30960 14043 879.5 35039 15893 968.5 39049 17712

MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

LOCATION & LOADING

DIRECTION



to Aft 297

434.5 5988 2716 523.5 9612 4360 612.5 17352 7871 701.5 25479 11557 790.5 30960 14043 879.5 35039 15893 1030.5 45039 20429

MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘M’ ULD

LOCATION & LOADING

DIRECTION



to Aft 297

442.0 6296 2856 597.5 16175 7337 694.5 24831 11263 791.0 30977 14051 904.5 36179 16411 1001.5 46546 21113


1-60-041 Page 2 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) CUMULATIVE LOAD CHECK (cont’d) MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘M’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

LOCATION & LOADING

DIRECTION



to Aft 297

442.0 6296 2856 597.5 16175 7337 694.5 24831 11263 791.0 30977 14051 904.5 36179 16411 1030.5 46179 20946

NOTES

1. The load limits above include the weight of cargo, main deck crew baggage, observers, supernumeraries, unit load devices, galley catering and main deck fluids.

2. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft.


1-60-041 Page 3 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) Allowable Cumulative Load The following charts show the allowable cumulative load in pounds. SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD

5988 LB atB.A. 434.5

9612 LB atB.A. 523.5

17352 LB atB.A. 612.5

25479 LB atB.A. 701.5

30960 LB atB.A. 790.5

35039 LB atB.A. 879.5

39049 LB atB.A. 968.5

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

200 300 400 500 600 700 800 900 1000

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 297.0



1-60-041 Page 4 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

5988 LB atB.A. 434.5

9612 LB atB.A. 523.5

17352 LB atB.A. 612.5

25479 LB atB.A. 701.5

30960 LB atB.A. 790.5

35039 LB atB.A. 879.5

45039 LB atB.A. 1030.5

0

5000

10000

15000

20000

25000

30000

35000

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45000

50000

200 300 400 500 600 700 800 900 1000 1100

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 297.0



1-60-041 Page 5 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD

6296 LB atB.A. 442.0

16175 LB atB.A. 597.5

24831 LB atB.A. 694.5

30977 LB atB.A. 791.0

36179 LB atB.A. 904.5

46546LB atB.A. 1001.5

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

50000

200 300 400 500 600 700 800 900 1000 1100BALANCE ARM - IN.

Max

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ulat

ive

Load

- LB

B.A. 297.0



1-60-041 Page 6 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

6296 LB atB.A. 442.0

16175 LB atB.A. 597.5

24831 LB atB.A. 694.5

30977 LB atB.A. 791.0

36179 LB atB.A. 904.5

46179LB atB.A. 1030.5

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

50000

200 300 400 500 600 700 800 900 1000 1100BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 297.0



1-60-041 Page 7 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) The following charts show the allowable cumulative load in kilograms. SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD

17712 KG atB.A. 968.5

15893 KG atB.A. 879.5

14043 KG atB.A. 790.5

11557 KG atB.A. 701.5

7871 KG atB.A. 612.5

4360 KG atB.A. 523.5

2716 KG atB.A. 434.5

0

2000

4000

6000

8000

10000

12000

14000

16000

18000

20000

200 300 400 500 600 700 800 900 1000

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 297.0



1-60-041 Page 8 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

20429 KG atB.A. 1030.5

15893 KG atB.A. 879.5

14043 KG atB.A. 790.5

11557 KG atB.A. 701.5

7871 KG atB.A. 612.5

4360 KG atB.A. 523.5

2716 KG atB.A. 434.5

0

5000

10000

15000

20000

25000

200 300 400 500 600 700 800 900 1000 1100

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 297.0



1-60-041 Page 9 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD

2856 KG atB.A. 442.0

7337 KG atB.A. 597.5

11263 KG atB.A. 694.5

14051 KG atB.A. 791.0

16411 KG atB.A. 904.5

21113 KG atB.A. 1001.5

0

5000

10000

15000

20000

25000

200 300 400 500 600 700 800 900 1000 1100

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 297.0



1-60-041 Page 10 of 10 Nov 03/2015 OL0182-25397

FORWARD BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

2856 KG atB.A. 442.0

7337 KG atB.A. 597.5

11263 KG atB.A. 694.5

14051 KG atB.A. 791.0

16411 KG atB.A. 904.5

20946 KG atB.A. 1030.5

0

5000

10000

15000

20000

25000

200 300 400 500 600 700 800 900 1000 1100

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 297.0



1-60-061 Page 1 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS CUMULATIVE LOAD CHECK The cumulative total load profile is computed aft to forward in the aft body and must not exceed the load distribution limitations shown in the table below. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft. MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD

LOCATION & LOADING

DIRECTION

BALANCE ARM (IN.) MAXIMUM COMBINED AFT CUMULATIVE LOAD FROM TO LB KG

Aft Body- Loading Aft to

Forward 1680

968.5 52355 23748 1057.5 48302 21909 1146.5 44318 20102 1235.5 40250 18257 1324.5 34685 15733 1413.5 26387 11969 1502.5 18164 8239 1591.5 7664 3476

MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

LOCATION & LOADING

DIRECTION



Forward 1680

1030.5 50250 22793 1235.5 40250 18257 1324.5 34685 15733 1413.5 26387 11969 1502.5 18164 8239 1591.5 7664 3476

MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘M’ ULD

LOCATION & LOADING

DIRECTION



Forward 1680

1001.5 50827 23055 1098.5 46467 21077 1195.5 42083 19089 1292.5 37634 17070 1389.5 28603 12974 1486.5 19640 8909 1583.5 8032 3643


1-60-061 Page 2 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) MAXIMUM CUMULATIVE LOADS – SIZE CODE ‘M’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

LOCATION & LOADING

DIRECTION



Forward 1680

1030.5 52083 23624 1195.5 42083 19089 1292.5 37634 17070 1389.5 28603 12974 1486.5 19640 8909 1583.5 8032 3643

NOTES

1. The load limits above include the weight of cargo and the unit load devices. 2. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate

engine transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft.


1-60-061 Page 3 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) Allowable Cumulative Load The following charts show the allowable cumulative load in pounds. SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD

7664 LB atB.A. 1591.5

18164 LB atB.A. 1502.5

26387 LB atB.A. 1413.5

34685 LB atB.A. 1324.5

40250 LB atB.A. 1235.5

44318 LB at B.A. 1146.5

48302 LB atB.A. 1057.5

52355 LB atB.A. 968.5

0

10000

20000

30000

40000

50000

60000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 1680.0



1-60-061 Page 4 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

7664 LB atB.A. 1591.5

18164 LB atB.A. 1502.5

26387 LB atB.A. 1413.5

34685 LB atB.A. 1324.5

40250 LB atB.A. 1235.5

50250 LB atB.A. 1030.5

0

10000

20000

30000

40000

50000

60000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 1680.0



1-60-061 Page 5 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD

8032 LB atB.A. 1583.5

19640 LB atB.A. 1486.5

28603 LB atB.A. 1389.5

37634 LB atB.A. 1292.5

42083 LB atB.A. 1195.5

46467 LB at B.A. 1098.5

50827 LB atB.A. 1001.5

0

10000

20000

30000

40000

50000

60000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 1680.0



1-60-061 Page 6 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

8032 LB atB.A. 1583.5

19640 LB atB.A. 1486.5

28603 LB atB.A. 1389.5

37634 LB atB.A. 1292.5

42083 LB atB.A. 1195.5

52083 LB atB.A. 1030.5

0

10000

20000

30000

40000

50000

60000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- LB

B.A. 1680.0



1-60-061 Page 7 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) The following charts show the allowable cumulative load in kilograms. SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD

23748 KG atB.A. 968.5

21909 KG atB.A. 1057.5

20102 KG at B.A. 1146.5

18257 KG atB.A. 1235.5

15733 KG atB.A. 1324.5

11969 KG atB.A. 1413.5

8239 KG atB.A. 1502.5

3476 KG atB.A. 1591.5

0

5000

10000

15000

20000

25000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 1680.0



1-60-061 Page 8 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘A’ AND SIZE CODE ‘B’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

22793 KG atB.A. 1030.5

18257 KG atB.A. 1235.5

15733 KG atB.A. 1324.5

11969 KG atB.A. 1413.5

8239 KG atB.A. 1502.5

3476 KG atB.A. 1591.5

0

5000

10000

15000

20000

25000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 1680.0



1-60-061 Page 9 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD

23055 KG atB.A. 1001.5

21077 KG at B.A. 1098.5

19089 KG atB.A. 1195.5

17070 KG atB.A. 1292.5

12974 KG atB.A. 1389.5

8909 KG atB.A. 1486.5

3643 KG atB.A. 1583.5

0

5000

10000

15000

20000

25000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 1680.0



1-60-061 Page 10 of 10 Nov 03/2015 OL0182-25397

AFT BODY CUMULATIVE LOADS (Cont’d) SIZE CODE ‘M’ ULD WITH ENGINE TRANSPORT PALLETS ENG 1 & ENG 2

23624 KG atB.A. 1030.5

19089 KG atB.A. 1195.5

17070 KG atB.A. 1292.5

12974 KG atB.A. 1389.5

8909 KG atB.A. 1486.5

3643 KG atB.A. 1583.5

0

5000

10000

15000

20000

25000

900 1000 1100 1200 1300 1400 1500 1600 1700 1800

BALANCE ARM - IN.

Max

imum

Cum

ulat

ive

Load

- K

G

B.A. 1680.0



1-62-008 Page 1 of 1 Nov 03/2015 OL0182-25397

CARGO COMPARTMENTS GENERAL LOCATION AND ARRANGEMENT The following airplane profile illustrates the main deck and lower hold cargo compartment locations.

Total volume and the volumetric centroid for the main deck are provided in CHP-SEC 1-62-101. The following table provides lower hold cargo compartment locations, usable volumes, and the corresponding volumetric centroid arms.

CARGO COMPARTMENT

LOCATION – B.A. USABLE VOLUME B.A. FROM TO CU FT IN.

Forward 508 845 667.7 690.9 Aft 1200 1640 1095 1406.0


1-62-010 Page 1 of 1 Nov 03/2015 OL0182-25397

CARGO HANDLING SYSTEM CARGO HANDLING SYSTEM LIMITATIONS The cargo handling system installed on this aircraft is identified in the following table, as defined by the Ancra Drawing Number of the same name: INSTALLED ANCRA SYSTEM ULD INSTALLATION VARIATIONS

83680-10 (15) 88x125 (ULD Size Code A) 83680-11 (15) 88x125 (ULD Size Code A) OR (15) 88x108 (ULD Size Code B)

83680-12 (15) 88x125 (ULD Size Code A) OR (13) 96x125 (ULD Size Code M)

83680-13 (15) 88x125 (ULD Size Code A) OR (13) 96x125 (ULD Size Code M)

83680-14 (15) 88x125 (ULD Size Code A) OR (15) 88x108 (ULD Size Code B)

83680-20 (15) 88x125 (ULD Size Code A) OR (15) 88x108 (ULD Size Code B) OR (13) 96x125 (ULD Size Code M) OR ENGINE TRANSPORT as (11) 88x125, (11)

88x108 or (10) 96x125 with (2) 88x125 longitudinal for engine transport

In addition to the loading limitations defined within the aircraft Weight and Balance Manual and this Supplement, the limitations of any applicable cargo loading manuals must be observed.


1-62-020 Page 1 of 1 Nov 03/2015 OL0182-25397

CRUSHABLE CARGO CRUSHABLE CARGO REQUIREMENTS Additional Requirements for ULD Positions Directly Behind the Safety Bulkhead Whenever practical or prudent (when gaps in ULD positions*), the ULD positions 1 or 2 directly behind the safety bulkhead shall be occupied by a ULD that is loaded to at least 70 percent of its volume with crushable-type cargo which may act as a buffer and load spreader. Definition of “Crushable Cargo” Crushable cargo must meet the following criteria:

No single large rigid piece of cargo. Any single-piece cargo must be deformable. Single pieces of cargo shall be larger than 24 inches (0.6096 meters). Smaller pieces of cargo must be consolidated into larger units which keep their integrity

but are deformable. Single cargo pieces shall have a density not greater than 15 lb/ft3 (240 Kg/meter3).

* Example: All ULD positions are occupied, except position 5.


1-62-042 Page 1 of 5 Nov 03/2015 OL0182-25397

FORWARD CARGO COMPARTMENTS FORWARD CARGO COMPARTMENT VOLUMES The following figure shows forward cargo hold compartment boundaries.

Volumes and centroids for the forward cargo hold are provided in the following table.

VOLUMES COMPARTMENTS 1A 1B 2 Forward Compartment Volumes [CU FT] 70.6 104.0 492.9

Total Forward Hold [CU FT] 667.7

Volumetric Centroids B.A. – IN. 534.5 592.4 734.0

Volumetric Centroid B.A. – IN. 690.9


1-62-042 Page 2 of 5 Nov 03/2015 OL0182-25397

FORWARD CARGO COMPARTMENTS (cont’d) FORWARD CARGO COMPARTMENT CROSS SECTIONS The figure below illustrates the general layout of the forward cargo compartments. The numbered labels and shaded panels correspond to the cross-sections provided on the following page.


1-62-042 Page 3 of 5 Nov 03/2015 OL0182-25397

FORWARD CARGO COMPARTMENTS (cont’d) The following cross-sections for compartments 1A, 1B and 2 can be used to determine ceiling clearances at various forward cargo compartment balance arms. The relative location of the cross-sectional cuts can be determined by correlating the cross-section number to the general layout on the previous page.

CROSS SECTION

NO. B.A. IN.

1 508.1 2 516.1 3 518.7 4 560.1 5 580.0 6 580.0 - 807.0 7 845.4


1-62-042 Page 4 of 5 Nov 03/2015 OL0182-25397

FORWARD CARGO COMPARTMENTS (cont’d) CARGO DOOR DIMENSIONS AND ALLOWABLE PACKAGE SIZES Package Size Illustration The following illustration shows package dimensioning used in the allowable package size tables.


1-62-042 Page 5 of 5 Nov 03/2015 OL0182-25397

FORWARD CARGO COMPARTMENTS (cont’d) Allowable Package Sizes The following tables apply to packages loaded aft of the forward cargo door (B.A. 590 IN.).


1-62-065 Page 1 of 5 Nov 03/2015 OL0182-25397

AFT CARGO COMPARTMENTS AFT CARGO COMPARTMENT VOLUMES The following figure shows aft cargo hold compartment boundaries.

Volumes and centroids for the aft cargo hold are provided in the following table.


1-62-065 Page 2 of 5 Nov 03/2015 OL0182-25397

AFT CARGO COMPARTMENTS (cont’d) AFT CARGO COMPARTMENT CROSS SECTIONS The figure below illustrates the general layout of the aft cargo compartments. The numbered labels and shaded panels correspond to the cross-sections provided on the following pages.


1-62-065 Page 3 of 5 Nov 03/2015 OL0182-25397

AFT CARGO COMPARTMENTS (cont’d) The following cross-sections for compartments 3 and 4 can be used to determine ceiling clearances at various aft cargo compartment balance arms. The relative location of the cross-sectional cuts can be determined by correlating the cross-section number to the general layout on the previous page. Compartment 3 Cross-Sections These cross-sections are for compartment 3 which is located in the forward end of the aft cargo hold.


1-62-065 Page 4 of 5 Nov 03/2015 OL0182-25397

AFT CARGO COMPARTMENTS (cont’d) CARGO DOOR DIMENSIONS AND ALLOWABLE PACKAGE SIZES Package Size Illustration The following illustration shows package dimensioning used in the allowable package size tables.


1-62-065 Page 5 of 5 Nov 03/2015 OL0182-25397

AFT CARGO COMPARTMENTS (cont’d) Allowable Package Sizes The following tables apply to packages loaded forward of the aft cargo door (B.A. 1410 IN.).


1-62-101 Page 1 of 3 Nov 03/2015 OL0182-25397

MAIN DECK CARGO COMPARTMENT MAIN DECK CARGO COMPARTMENT VOLUMES The following figure shows the main deck cargo hold compartment boundaries.

The following table provides the main deck cargo compartment location, usable volumes and the corresponding volumetric centroid arm.

CARGO COMPARTMENT

LOCATION – B.A. USABLE VOLUME CU FT B.A. IN. FROM TO

Main Deck 346 1680 6600 1013.0


1-62-101 Page 2 of 3 Nov 03/2015 OL0182-25397

MAIN DECK CARGO COMPARTMENT (Cont’d) MAIN DECK CARGO COMPARTMENT CROSS SECTION The following cross-sections for the main cargo compartment can be used to determine ceiling clearances at various main cargo compartment balance arm locations. Also shown are the intersection of the sidewalls with the ceiling and the top of the conveying surface on the floor.


1-62-101 Page 3 of 3 Nov 03/2015 OL0182-25397

MAIN DECK CARGO COMPARTMENT (Cont’d) DOOR DIMENSIONS The following figure provides the main deck cargo door dimensions.

The following figure provides the door opening and sill height.


1-63-121 Page 1 of 3 Nov 03/2015 OL0182-25397

UNIT LOAD DEVICES – MAIN DECK ALLOWABLE ULD DEVICES Bulk cargo loading is prohibited on the main deck. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See CHP-SEC 1-62-010 to determine which ULD size codes are applicable to this aircraft. Deflection limits shall be in accordance with Specification IATA ULD Technical Manual 50/4. Each pallet and net must be certified against the requirements of TSO-C90. ULD containers shall be maintained in an airworthy condition. To ensure a minimum of good condition, each ULD must also correspond to IATA Specification, Chapter 5, Standard Specification 50/0, Part II. The following table identifies the NAS3610 containers approved for use in container or pallet/net configuration:

SIZE CODE

BASE DIMENSIONS

(IN.) ULD TYPE NAS3610-

A 88 X 125

1A2 1A3 2A1 2A2 2A3 2A4 2A5 2A6

B 88 X 108

1B3 1B5 2B2 2B3 2B5 2B6

M 96 X 125 2M1 2M2 2M3

ULD numbering conforms to IATA recommendations. ENGINE TRANSPORT Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine transport. See CHP-SEC 1-62-010 to determine which ULD size codes are applicable to this aircraft. If the layout of the upper deck cargo compartment loading system as defined in CHP-SEC 1-62-010 allows for engine transport, reference CHP-SEC 1-60-021 for pallet positions. Pallets approved for engine transport are designated ENG 1 & ENG 2, and are Size Code A pallets only, installed longitudinally.


1-63-121 Page 2 of 3 Nov 03/2015 OL0182-25397

UNIT LOAD DEVICES – MAIN DECK (Cont’d) The upper deck cargo compartment is equipped with a NAS 3610 Class II restraint system approved for the transport of pallets. Engine pallets and restraint systems must be designed per NAS3610 standards. The pallet package may extend over the pallet width to the extent that the overhang of the package will not have an adverse effect on the cargo door and the cargo compartment lining. The minimum clearance to the ceiling and sidewall should be 2 inches (51 millimeters). Each engine pallet and engine stand shall be rigidly connected at least as required by NAS 3610, with respect to applicable gross weight and load factors. If a rigid pallet to engine stand connection is not possible, the package must be secured to the pallet by strap-nets type NAS 3610-2A2N, -2A3N or 2A6N. These nets must be adjustable in order to be compatible with the geometrical form of the cargo and their fittings must be fixed to the pallet rim so that loads are evenly distributed. The center of gravity locations and maximum center of gravity deviations are presented in the following paragraphs. Maximum allowable weights must comply with load limits presented in 1-60-005. ULD CENTER OF GRAVITY The following table identifies the centroids of the main deck ULD’s. Main deck ULD positions can be found in CHP-SEC 1-60-021.

ULD

POSITION

SIZE CODE A SIZE CODE B

CENTROID BALANCE ARM

(IN.)

SIZE CODE M CENTROID

BALANCE ARM (IN.)

1 390.3 394.0 2 479.0 549.3 3 568.0 646.0 4 657.0 742.8 5 746.0 856.3 6 835.0 953.0 7 924.0 1050.0 8 1013.0 1147.0 9 1102.0 1244.0 10 1191.0 1341.0 11 1280.0 1438.0 12 1369.0 1535.0 13 1458.0 1631.8 14 1547.0 15 1635.8

ENG 1 967.5 967.5 ENG 2 1093.5 1093.5


1-63-121 Page 3 of 3 Nov 03/2015 OL0182-25397

UNIT LOAD DEVICES – MAIN DECK (Cont’d) CENTER OF GRAVITY LIMITS The following table identifies the allowable center of gravity range for the ULDs approved for use.

SIZE CODE ALLOWABLE CENTER OF GRAVITY RANGE

(IN.) VERTICAL LATERAL LONGITUDINAL

A 0 - 36 ± 12.5 ± 8.8 B 0 - 36 ± 10.8 ± 8.8 M 0 - 36 ± 12.5 ± 9.6

ENG 1 & ENG 2 0 - 36 ± 8.8 ± 12.5

Maximum vertical center of gravity is measured from the base of the ULD. Lateral and longitudinal ranges are measured from the geometric center of the ULD. Best judgment must be applied in evenly distributing the loading within the ULD. Airplane lateral imbalance limits are presented in CHP-SEC 1-04-001.


1-68-101 Page 1 of 7 Nov 03/2015 OL0182-25397

MAIN DECK UNIT LOAD DEVICE RESTRAINTS The main deck cargo restraint system is comprised of locks, side restraints, and stops (collectively referred to herein as restraints). The restraints are mounted at one or more floor track lateral locations. The tables found on the following three pages list all restraint installation locations. MISSING AND INOPERATIVE RESTRAINTS In the case of any missing or inoperative restraints, refer to CHP-SEC-SUB 1-68-102 of this Supplement.


1-68-101 Page 2 of 7 Nov 03/2015 OL0182-25397

MAIN DECK UNIT LOAD DEVICE RESTRAINTS (Cont'd) MAIN DECK CARGO LOCK LOCATIONS The following stations identify the locations of the main deck cargo locks. All locks are located laterally at the following five floor tracks locations: BL 0.0, LBL 24.75, RBL 24.75, LBL 45.50, and RBL 45.50.

ULD SIZE CODE 'A' ULD SIZE CODE 'B' BALANCE ARM (IN.)

ULD SIZE CODE 'M' BALANCE ARM (IN.)

345.95 345.95 434.45 441.95 523.45 500.45 612.45 597.45 701.45 694.45 790.45 790.95 879.45 807.95 968.45 904.45 1057.45 1001.45 1146.45 1098.45 1235.45 1195.45 1324.45 1292.45 1413.45 1389.45 1502.45 1486.45 1591.45 1583.45 1679.95 1679.95

Notes: 1. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine

transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft 2. To accommodate and restrain ENG 1 & ENG 2 pallets for engine transport, relocate 3 locks

from BA 1001.45 or 1057.45 to BA 1030.45. Also relocate 3 locks from BA 1146.45 or BA 1098.45 to BA 1156.45. Relocate the roller trays to removed lock locations.

3. Stations 345.95 and 1679.95 have stops installed in lieu of locks.


1-68-101 Page 3 of 7 Nov 03/2015 OL0182-25397

MAIN DECK UNIT LOAD DEVICE RESTRAINTS (Cont'd) MAIN DECK SIDE RESTRAINT LOCATIONS – ULD SIZE CODE 'A' The stations in the following table identify the locations of the main deck cargo side restraints. This table applies to the following floor track locations: LBL 62.5 and RBL 62.5.

SIDE RESTRAINT ULD SIZE CODE 'A'

LBL & RBL 62.5 BALANCE ARM (IN.)





364.95 779.95 1200.00 377.95 800.00 1219.95 394.95 819.95 1239.95 417.95 838.95 1259.95 439.95 859.95 1279.95 459.95 878.95 1300.00 479.95 900.00 1319.95 500.00 918.95 1339.95 519.95 938.95 1359.95 539.95 958.95 1379.95 559.95 978.95 1400.00 579.95 1000.00 1419.95 600.00 1018.95 1439.95 619.95 1039.95 1459.95 639.95 1059.95 1479.95 659.95 1079.95 1500.00 679.95 1100.00 1519.95 700.00 1119.95 1539.95 719.95 1139.95 1559.95 739.95 1159.95 1579.95 759.95 1179.95


transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft 2. For engine transport pallets ENG 1 & ENG 2 configurations, see following paragraph "MAIN

DECK SIDE RESTRAINT LOCATIONS - ENGINE PALLETS ENG 1 & ENG 2"


1-68-101 Page 4 of 7 Nov 03/2015 OL0182-25397

MAIN DECK UNIT LOAD DEVICE RESTRAINTS (Cont'd) MAIN DECK SIDE RESTRAINT LOCATIONS – ULD SIZE CODE 'B' The stations in the following table identify the locations of the main deck cargo side restraints installed on the right hand side, at RBL 62.5. .

SIDE RESTRAINT ULD SIZE CODE 'B'

RBL 62.5 BALANCE ARM (IN.)





364.95 779.95 1200.00 377.95 800.00 1219.95 394.95 819.95 1239.95 417.95 838.95 1259.95 439.95 859.95 1279.95 459.95 878.95 1300.00 479.95 900.00 1319.95 500.00 918.95 1339.95 519.95 938.95 1359.95 539.95 958.95 1379.95 559.95 978.95 1400.00 579.95 1000.00 1419.95 600.00 1018.95 1439.95 619.95 1039.95 1459.95 639.95 1059.95 1479.95 659.95 1079.95 1500.00 679.95 1100.00 1519.95 700.00 1119.95 1539.95 719.95 1139.95 1559.95 739.95 1159.95 1579.95 759.95 1179.95



DECK SIDE RESTRAINT LOCATIONS - ENGINE PALLETS ENG 1 & ENG 2" 3. The side restraint installation for Size Code 'B' at RBL 62.5 is the same as that of Size Code

'A' and Size Code 'M'.


1-68-101 Page 5 of 7 Nov 03/2015 OL0182-25397

MAIN DECK UNIT LOAD DEVICE RESTRAINTS (Cont'd) MAIN DECK SIDE RESTRAINT LOCATIONS – ULD SIZE CODE 'B' (Cont'd) The stations in the following table identify the locations of the main deck cargo side restraints installed on the left hand side, at LBL 45.5.


LBL 45.5 BALANCE ARM (IN.)





364.95 859.95 1300.00 377.95 890.45 1313.45 394.95 918.95 1339.95 417.95 938.95 1359.95 459.95 958.95 1379.95 479.95 984.45 1400.00 510.95 1011.45 1424.45 539.95 1026.45 1439.95 559.95 1045.45 1459.95 579.95 1067.45 1475.45 619.95 1087.45 1519.95 639.95 1110.45 1539.95 659.95 1135.45 1559.95 679.95 1158.95 1572.45 719.95 1184.45 1600.00 739.95 1205.45 1620.00 759.95 1219.95 1640.00 779.95 1245.45 1661.00 819.95 1259.95 838.95 1279.95



DECK SIDE RESTRAINT LOCATIONS - ENGINE PALLETS ENG 1 & ENG 2"


1-68-101 Page 6 of 7 Nov 03/2015 OL0182-25397

MAIN DECK UNIT LOAD DEVICE RESTRAINTS (Cont'd) MAIN DECK SIDE RESTRAINT LOCATIONS – ULD SIZE CODE 'M' The stations in the following table identify the locations of the main deck cargo side restraints. This table applies to the following floor track locations: LBL 62.5 and RBL 62.5.

SIDE RESTRAINT ULD SIZE CODE 'M'






364.95 779.95 1200.00 377.95 800.00 1219.95 394.95 819.95 1239.95 417.95 838.95 1259.95 439.95 859.95 1279.95 459.95 878.95 1300.00 479.95 900.00 1319.95 500.00 918.95 1339.95 519.95 938.95 1359.95 539.95 958.95 1379.95 559.95 978.95 1400.00 579.95 1000.00 1419.95 600.00 1018.95 1439.95 619.95 1039.95 1459.95 639.95 1059.95 1479.95 659.95 1079.95 1500.00 679.95 1100.00 1519.95 700.00 1119.95 1539.95 719.95 1139.95 1559.95 739.95 1159.95 1579.95 759.95 1179.95



DECK SIDE RESTRAINT LOCATIONS - ENGINE PALLETS ENG 1 & ENG 2" 3. The side restraint installation for the Size Code ‘M’ ULDs is the same as the installation for the

Size Code ‘A’ ULDs.


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MAIN DECK UNIT LOAD DEVICE RESTRAINTS (Cont'd) MAIN DECK SIDE RESTRAINT LOCATIONS – ENGINE PALLETS ENG 1 & ENG 2 The stations in the following table identify the locations of the main deck cargo side restraints for use on pallets ENG 1 & ENG 2 as engine transport pallets. This table applies only to the floor tracks for use on pallets ENG 1 & ENG 2 at the locations noted. All other floor tracks designated in previous paragraphs also apply at other pallet locations.

SIDE RESTRAINT ENG 1 & ENG 2 PALLETS


SIDE RESTRAINT ENG 1 & ENG 2 PALLETS


914.45 918.95 934.45 938.95 954.45 958.95 984.45 984.45 1014.45 1011.45 1045.45 1026.45 1066.45 1045.45 1087.45 1067.45 1110.45 1087.45 1133.45 1110.45

1135.45 Notes: 1. Not all ULD size codes are applicable to all aircraft, and not all aircraft accommodate engine

transport. See 1-62-010 to determine which ULD size codes are applicable to this aircraft


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MISSING AND/OR INOPERATIVE RESTRAINTS This Subject provides procedures for ULD loading when there are missing and/or inoperative restraints. The maximum allowed ULD loading listed in Section 60 assumes that all equipment is installed and operating correctly. When certain equipment is missing and/or inoperable, these loading limits may be reduced. The following equipment malfunctions do not require a load limit restriction:

Jammed or missing sill rollers Jammed or missing balls in a caster tray/panel Jammed or missing rollers in a roller unit

LOAD LIMITS – SIZE CODE ‘B’ In the case of any missing and/or inoperative restraints, the corresponding ULD position(s) cannot be used. LOAD LIMITS – ENGINE TRANSPORT In the case of any missing and/or inoperative restraints, engine transport in the corresponding position(s) is not allowed. LOAD LIMITS – SIZE CODE ‘A’ AND SIZE CODE ‘M’ The following guidelines must be followed in order to determine allowable loads for a ULD position with restraint irregularities.

The operator determines the number of restraints available for each ULD position. Two or more missing and/or inoperative restraints in the same direction are not allowed

(e.g. two side restraints or two vertical restraints may not be missing or inoperative). Also, two restraints adjacent to a common corner cannot be missing and/or inoperable. If either of these conditions exists, the allowable weight of that ULD position is 0 LB (0 KG).

Restraint systems fall into four categories: side restraints, side/vertical restraints, forward/aft restraints and forward/aft/vertical restraints. Each restraint direction is considered separately when missing and/or inoperative restraint equipment exists (i.e. forward, aft, side left, side right and vertical loading.) When a missing and/or inoperative restraint condition exists, the allowable weight is determined by considering each restraint direction separately and using the most limiting resultant allowable weight determined from the following tables (Note - restraint ‘R1’ corresponds to a forward left position).

An empty ULD can be carried in any position, provided that at least one restraint is operable in each (forward, aft, left and right) direction. In addition, one vertical restraint on each edge (forward, aft, left and right) is required to be operable.


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CAUTION CARE MUST BE EXERCISED DURING LOADING AND UNLOADING OF UNIT LOAD DEVICES WHEN EQUIPMENT IS MISSING AND/OR INOPERATIVE TO PREVENT DAMAGE TO AIRPLANE STRUCTURE. IT IS ADVISABLE THAT MALFUNCTIONING EQUIPMENT BE REPAIRED OR REPLACED IMMEADIATELY IN ORDER TO PREVENT DAMAGE TO OPERATIVE EQUIPMENT.


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MISSING AND/OR INOPERATIVE RESTRAINTS (Cont’d) ULD POSITION 1 LOAD LIMITS – SIZE CODE ‘A’

MISSING RESTRAINT

NUMBER

MAXIMUM ULD ALLOWABLE LB KG

R1 2451 1112 R2 3871 1756 R3 5014 2275 R4 3871 1756 R5 2451 1112 R6 2380 1080 R7 3911 1774 R8 4482 2033 R9 1581 717 R10 2451 1112 R11 3871 1756 R12 5014 2275 R13 3871 1756 R14 2451 1112 R15 1581 717 R16 4482 2033 R17 3911 1774 R18 2380 1080


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ULD POSITION 2 LOAD LIMITS – SIZE CODE ‘A’

MISSING RESTRAINT

NUMBER


R1 2661 1207 R2 4202 1906 R3 5443 2469 R4 4202 1906 R5 2661 1207 R6 2587 1173 R7 4271 1937 R8 5363 2433 R9 4279 1941 R10 2709 1229 R11 2661 1207 R12 4202 1906 R13 5443 2469 R14 4202 1906 R15 2661 1207 R16 2709 1229 R17 4279 1941 R18 5363 2433 R19 4271 1937 R20 2587 1173

MISSING AND/OR INOPERATIVE RESTRAINTS (Cont’d)


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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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ULD POSITION 1 LOAD LIMITS – SIZE CODE ‘M’

MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING RESTRAINT

NUMBER





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MISSING

RESTRAINT NUMBER


R1 2907 1318 R2 4591 2082 R3 5946 2697 R4 4591 2082 R5 2907 13

airplane weight and balance control and loading … · 2017. 6. 16. · conversion aircraft weight...

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