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Advisory Circular - Aircraft Weight and Balance Control

Beechcraft 99 Airliner · Other Documents

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Overview

This advisory circular provides updated methods and procedures for developing an approved weight and balance control system for small aircraft operating in the air taxi fleet under Federal Aviation Regulation (FAR) Part 135. It outlines the requirements for operators to ensure that their aircraft are loaded within the authorized weight and balance limitations. The document is intended for air taxi operators and provides guidance on establishing, monitoring, and adjusting empty weight and center of gravity, as well as creating loading schedules and load manifests. It emphasizes the importance of accurate weight and balance calculations to maintain safety during operations.

  • Average passenger weight is 160 lbs in summer and 165 lbs in winter.
  • Children aged 2-12 are averaged at 80 lbs for weight calculations.
  • Each piece of checked baggage averages 23.5 lbs, and hand baggage averages 5 lbs.
  • Aircraft must be reweighed if weight changes exceed 0.5% of empty weight or CG changes exceed 0.5% of the mean aerodynamic chord.
  • Loading schedules must ensure the aircraft remains within weight and balance limits throughout the flight.

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Source

Originally published by rosap.ntl.bts.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Other Documents
Year
1976
Pages
12
File size
399 KB
Publisher
rosap.ntl.bts.gov
Documentation completeness
3/7

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In this document

Purpose

The purpose of this advisory circular is to provide updated methods and procedures for developing an approved weight and balance control system for small aircraft operating in the air taxi fleet under FAR Part 135.

General Requirements

Operators may submit methods for ensuring their aircraft are properly loaded and do not exceed weight and balance limitations. The approval of these systems is based on evaluations of the proposed program and the operator's ability to implement it.

Establishing Initial Aircraft Status

Operators must determine the aircraft's empty weight and center of gravity before use in air taxi service. New multiengine aircraft may be placed into service without reweighing if previous reports have been adjusted for modifications.

Loading Schedule

Loading schedules must be simple and orderly, providing instructions on proper load distribution, including fuel and passenger seating restrictions. A copy of the loading schedule should be kept with the aircraft.

Load Manifest

A load manifest must be prepared by personnel responsible for supervising the loading of aircraft. It should include the weight of the aircraft, fuel, oil, cargo, passengers, and baggage, along with the maximum allowable takeoff weight.

Safety notes

  • Ensure all loading conditions are accounted for to prevent exceeding weight and balance limits.
  • Use calibrated scales for weighing aircraft and ensure they are checked regularly.

Full document text

^ Of Tlfcu. AC NO; 1 3 5 - i B DATE: 1 / 1 9 / 7 6 A D V I S O R Y C I R C U L A R DEPARTMENT OF TRANSPORTATION FEDERAL AVIATIOH ADMINISTRATION SUBJECT! A I R T A X I AIRCRAFT WEIGHT AND BALANCE CONTROL 1. PURPOSE. This advisory circular provides an updating of methods and procedures for developing an approved weight and balance control system for small aircraft operating in the air taxi fleet under Federal Aviation Regulation (FAR) Part 135. 2. CANCELLATION. Advisory Circular No. 135-lA, dated September 26, 1969, is cancelled. 3. BACKGROUND. a. Refer to FAR Section 91.31, Civil aircraft operating limitations and marking requirements. b. Under FAR Section 135.13, Application and issue of certificate and operations specifications, air taxi operators may be authorized to use an approved weight and balance control system based on average, assumed, or estimated passenger and baggage weights, to comply with applicable airworthiness requirements and aircraft operating limitations. c. Amendment 135-12, issued on November 26, 1969, added a new FAR Section 135.167. Paragraph (a) of that Section prohibits the operations of a raultiengine aircraft in Part 135 operations unless the current empty weight and center of gravity are calculated from values established by actual weighing of the aircraft within the preceding three years. The provision does not apply to either aircraft originally certificated for airworthiness within the preceding three years or aircraft under a weight and balance system approved in the operating specifications of the certificate holders. Initiated by: AFS-830 AC 135-lB 1 / 1 9 / 7 6 4. GENERAL. The operator may submit, for inclusion in the operations specifications, any method and procedure by which it can be shown that his aircraft will be properly loaded and will not exceed authorized weight and balance limitations during operation. The approval of such a weight and balance control system is based on an evaluation of the program presented for a particular aircraft, and of a particular operator's ability to implement that program. By whatever method used, account for all probable loading conditions whioh may be experienced in service, and show that the loading schedule developed will insure satisfactory aircraft loading, within the approved limits, throughout each flight. 5. CONTENTS. Weight and balance control systems encompass the following: a. Methods for establishing, monitoring and adjusting empty weight and empty weight center of gravity, in conjunction with the initial and periodic reweighing of each aircraft. b. A loading sohedule composed of charts, wherein the various balance conditions of an aircraft have been computed, based on current data in the individual aircraft weight and balance report, for use in loading that particular aircraft in a rapid and satisfactory manner. c. Procedures for using the loading schedule, to establish loaded con dition of the aircraft for which the sohedule was designed, thereby assuring that the aircraft is within safe operating limits. d. A load manifest to document the findings of personnel responsible for weight and balance control, together with procedures for its preparation. e. Procedures for crewmembers. cargo handlers, and other personnel con cerned with aircraft loading, giving complete details regarding distribution of passengers and fuel, the distribution and security of cargo, and restrictions to passenger movement during flight. 6. ESTABLISHING INITIAL AIRCRAFT STATUS. Include provisions in the aircraft weight and balance control system for determining the aircraft empty weight and empty weight center of gravity location as follows: a- Establishing empty weight before use in air taxi service. New production multiengine aircraft may be placed into service without reweighing, including those having a "computed" weight and balance report, if those reports have been adjusted for alterations or modifications to the aircraft. Used multiengine aircraft trans ferred from one operator to another need not be reweighed prior to utilization by the latter, unless 36-calendar months have elapsed since last weighing. Page 2 Par 4 1/19/76 AC 135-lB b. Individual aircraft weight and balance changes. Utilize the individual empty weight of each aircraft in the loading schedules when computing gross weight and balance of each aircraft at specified reweighing periods. A hew weight and balance should be reestablished whenever the accumulated weight change exceeds plus or minus one-half of one .percent of the aircraft empty weight or the cumulative change in'CG location exceeds one-half of one percent of the mean aerodynamic chord. c. Periodic reweighing. Aircraft operated under an approved weight and balance control system are normally reweighed in accordance with the provisions of the approved system a 3 indicated in the operator's operations specifications. d. Weighing prooedure. Use normal precautions, consistent with good practioes in the weighing .procedures, such as checking for the com pleteness of the aircraft and equipment, idetermining that fluids are properly accounted for, and that weighing is accomplished in an enclosed building to eliminate the possible effects of the slightest wind. Any acceptable scales may be used for weighing provided they are properly calibrated and used in accordance with the manufacturer's instructions. Use scales that have been calibrated by the manufacturer or other certifying agency within one year prior to weighing any air craft, unless evidence is presented which indicates a longer period between calibrations Is warranted. e. Fleet weights, establishment, and changes. For a fleet or group of aircraft of the same model and configuration, an average fleet empty weight may be utilized if the empty weights apd CG positions are within the limits established herein. The fleet empty weight will be calculated on the following basis: (1) An operator's fleet empty weight is usually determined by weighing

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aircraft according to the following data: For a fleet of one to three, weigh all aircraft; for a fleet of four to nine, weigh three aircraft plus at least 50 percent of the number over three; for a fleet of nine or over, weigh six aircraft plus at least ten peroent of the number over nine. (2) In choosing the aircraft to be weighed, the aircraft in the fleet having the highest time since last weighing should be selected. When the average empty weight and CG position have been determined for aircraft weighed and the basic fleet empty weight (winter and summer, if applicable) established, necessary data should be computed for aircraft not weighed, but which are considered eligible under such fleet weight. Par 6 Page 3 A C 1 3 5 - 1 B 1 / 1 9 / 7 6 ( 3 ) I F T H E E M P T Y W E I G H T O F A N Y A I R C R A F T W E I G H E D , O R T H E O A L O U L A T E D E M P T Y W E I G H T O F A N Y O F T H E R E M A I N I N G A I R C R A F T I N T H E F L E E T , V A R I E S B Y A N A M O U N T M O R E T H A N P L U S O R M I N U S O N E - H A L F O F O N E P E R C E N T F R O M T H E A V E R A G E F L E E T E M P T Y W E I G H T , O R T H E C G P O S I T I O N V A R I E S M O R E T H A N P L U S O R M I N U S O N E - H A L F O F O N E P E R C E N T F R O M T H E A V E R A G E F L E E T C G P O S I T I O N , T H A T A I R C R A F T S H O U L D B E O M I T T E D F R O M T H A T G R O U P ' A N D B E O P E R A T E D U S I N G I T S A C T U A L O R O A L O U L A T E D E M P T Y W E I G H T A N D C G P O S I T I O N . I F I T F A L L S W I T H I N T H E L I M I T S O F A N O T H E R F L E E T O R G R O U P , I T M A Y T H E N B E C O M E P A R T O F T H A T G R O U P . I N O A S E S W H E R E T H E A I R C R A F T I S W I T H I N T H E F L E E T E M P T Y W E I G H T T O L E R A N C E , B U T T H E C G P O S I T I O N V A R I E S I N E X C E S S O F T H E T O L E R A N C E A L L O W E D , T H E A I R C R A F T M A Y S T I L L B E O P E R A T E D U N D E R T H E A P P L I C A B L E F L E E T E M P T Y W E I G H T , B U T W I T H A N I N D I V I D U A L C G P O S I T I O N . ( 4 ) W H E N A N A I R C R A F T W I T H I N A F L E E T O R G R O U P H A S B E E N A L T E R E D ( W E I G H T O R C G C H A N G E S ) , T H A T A I R C R A F T ' S F L E E T E M P T Y W E I G H T O R C O R R E S P O N D I N G C G P O S I T I O N M A Y B E R E E S T A B L I S H E D B Y C A L C U L A T I O N B A S E D O N T H E O U R R E N T A V E R A G E E M P T Y W E I G H T O F A I R C R A F T W E I G H E D F O R F L E E T W E I G H T P U R P O S E S . ( 5 ) W E I G H I N G F O R R E E S T A B L I S H M E N T O F A L L F L E E T W E I G H T S I S N O R M A L L Y C O N D U C T E D O N A 3 6 - C A L E N D A R M O N T H B A S I S , U N L E S S O T H E R W I S E A P P R O V E D I N T H E O P E R A T O R ' S O P E R A T I O N S S P E C I F I C A T I O N S . 7 . L O A D I N G S C H E D U L E . D E S I G N L O A D I N G S C H E D U L E S A R E T O B E S I M P L E A N D O R D E R L Y , B A S E D O N S O U N D P R I N C I P L E S , T H U S R E D U C I N G T H E E L E M E N T O F H U M A N E R R O R . A C O P Y O F T H E L O A D I N G S C H E D U L E I S K E P T W I T H T H E A I R C R A F T A N D , I N S O M E C A S E S , F O R M S A P A R T O F T H E A I R P L A N E F L I G H T M A N U A L . I T I N O L U D E S I N S T R U C T I O N S O N T H E P R O P E R L O A D D I S T R I B U T I O N , S U O H A S F I L L I N G O F F U E L A N D O I L T A N K S , P A S S E N G E R S E A T I N G R E S T R I C T I O N S T O P A S S E N G E R M O V E M E N T , D I S T R I B U T I O N O F C A R G O , E T C . I T M U S T P R O V I D E F O R A R E D U C T I O N O F P A S S E N G E R S , F U E L A N D / O R B A G G A G E , E T C . , A S A P P R O P R I A T E T O R E M A I N W I T H I N T H E A I R C R A F T W E I G H T A N D B A L A N C E L I M I T A T I O N S . A . O T H E R M E A N S O F D E T E R M I N I N G S A F E L O A D I N G C O N D I T I O N S , S U O H A S T H E U S E O F G R A P H I O I N D E X , L O A D A D J U S T E R , E T C , A R E A O O E P T A B L E . B . P R O V I D E F O R C O M P U T I N G A S E P A R A T E L O A D I N G C O N D I T I O N W H E N T H E A I R C R A F T I S T O B E L O A D E D I N O T H E R T H A N A S S P E C I F I E D I N T H E L O A D I N G S C H E D U L E . 8 . C O M P U T I N G A I R C R A F T L O A D * A . P A S S E N G E R W E I G H T . T H E O P E R A T O R M A Y E L E C T T O U S E A V E R A G E P A S S E N G E R W E I G H T T O C O M P U T E P A S S E N G E R L O A D S O V E R A N Y R O U T E , E X C E P T I N T H O S E C A S E S W H E R E N O N S T A N D A R D W E I G H T P A S S E N G E R G R O U P S A R E C A R R I E D . E I T H E R M E T H O D M A Y B E U S E D I N T E R C H A N G E A B L Y , P R O V I D E D O N L Y O N E M E T H O D I S U S E D F O R A N Y F L I G H T F R O M B E G I N N I N G T O T E R M I N A T I N G P O I N T O F T H E P A R T I C U L A R T R I P O R F L I G H T I N V O L V E D . I N C O R P O R A T E P R O V I S I O N S W H I C H C L E A R L Y I N D I C A T E T O P E R S O N N E L T H E C I R C U M S T A N C E S U N D E R W H I C H A C T U A L O R A V E R A G E P A G E 4 P A R 6 1 / 1 9 / 7 6 AC 135-1B passenger weights are t o be used i n oomputing the passenger l o a d . ( 1 ) Average passenger w e i g h t . ( a ) An average weight of 160 pounds (sumner) may be used f o r a d u l t passengers during t h e calendar period from May 1 through October 3 1 . ( b ) An average weight of 165 pounds ( w i n t e r ) may be used f o r each a d u l t passenger during t h e calendar period from November 1 through A p r i l 3 0 . ( c ) An average of 80 pounds may be used f o r ohildren between t h e ages o f 2 and 1 2 . Children above 12 years of age are o l a s s i f i e d as a d u l t s f o r t h e purpose of weight and balance computations. Children l e s s than 2 years of age are considered "babes i n arms." (d) The above passenger weight inoludes minor items normally c a r r i e d by a passenger. ( 2 ) Actual passenger weight. Do not use the average passenger weight method i n the oase of f l i g h t s carrying passengers whose average weight o b v i o u s l y does not oonform with the normal standard weight. Use a c t u a l weights when a passenger load c o n s i s t s p a r t l y o f a t h l e t i c squads or other groups which are smaller or l a r g e r than the U . S . a v e r a g e . ( 3 ) Actual passenger weight may be determined by s c a l e weighing of each passenger p r i o r to boarding the a i r c r a f t , with such weight inoluding minor a r t i c l e s c a r r i e d on board by the passenger. I f such a r t i c l e s are not weighed, account f o r the estimated weight. The a c t u a l passenger weight may a l s o be determined by asking each passenger h i s weight and adding t h e r e t o a predetermined constant t o provide f o r hand-oarried a r t i c l e s and a l s o t o cover p o s s i b l e seasonal e f f e c t upon passenger weight due t o variance in o l o t h i n g w e i g h t . This constant may be approved f o r an operator on the b a s i s of a d e t a i l e d study by the operator over the p a r t i c u l a r routes involved and during the extreme seasons when a p p l i c a b l e . b- Crew Weight. For crewmembers, t h e f o l l o w i n g average weights may be u t i l i z e d : ( 1 ) Male oabin attendants 150 pounds, female cabin attendants 1 3 0 pounds. ( 2 ) A l l o t h e r crewmembers, 170 pounds. Par 8 Page 5 AC 135--1B 1/19/76 c. Passenger and Crew Baggage. Provide procedures which properly acoount for all baggage, including that carried on board by the passengers. If desired by the operator, a standard crew baggage weight may«be used. The following average passenger baggage weights may be 'used in lieu of actual weights: (1) For each piece of checked baggage, an average of not leas than 23.5 pounds; and (2) For each passenger boarding the aircraft, add an average of not less than 5 pounds for hand baggage whether or not such baggage is carried by the passenger. (3) Do not use average passenger baggafee weights in computing the weight and balance of charter flights and other flights in volving the carriage of special groups. 9, LOAD MANIFEST. Develop a form, to be prepared by personnel responsible for supervising the loading of aircraft, together with procedures for Its completion. Include the following Items on the load manifest: a. The weight of the aircraft, fuel, oil, cargo, passengers, mail, and baggage. b. The maximum allowable takeoff weight for that flight. c. The total weight as computed under the approved procedures. d. Evidence that the aircraft is loaded according to an approved schedule, which insures that the center of gravity is within limits, and will regain so throughout the proposed flight. 10. SYSTEM DEVELOPMENT. Consider the following details when developing weight and balance control procedures: a. Insure that the terms and descriptions used are readily understandable to prevent possible confusion and error. Chapter 13 of Advisory Circular No. 4^-13-1A provides a listing of recognized terminology. b. Mark all seats, compartments, and other loading stations using identification corresponding to the procedures established for computing the weight and balance of each aircraft. c. When the loading schedules require blocking-off seats or compartments in order to remain within center of gravity limits, provide effective means to assure that such seats or compartments are not occupied during operations specified. Page 6 Par 8 1 / 1 9 / 7 6 AC 1 3 5 - l B d . Include information r e l a t i v e t o maximum c a p a c i t i e s , and other p e r t i nent l i m i t a t i o n s , a f f e c t i n g the weight or balance of the a i r c r a f t i n these i n s t r u c t i o n s . e . Prepare and i s s u e s p e c i a l i n s t r u c t i o n s t o appropriate f l i g h t and ground personnel when i t i s p o s s i b l e t o exceed approved"aircraft CG l i m i t s by adverse d i s t r i b u t i o n or displacement of passengers, bag gage, or c a r g o . Center o f g r a v i t y during f l i g h t . F u l l y account f o r extreme v a r i a t i o n s i n center of g r a v i t y t r a v e l during f l i g h t caused by a l l or any combination of the following v a r i a b l e s : ( 1 ) The movement of passengers and cabin attendants from t h e i r normal p o s i t i o n In the a i r c r a f t cabin t o such l o c a t i o n s as a lounge or l a v a t o r y . I f the c a p a c i t y o f such compartment i s one, the movement of e i t h e r one passenger or one cabin attendant, whichever most adversely a f f e c t s the CG condition, w i l l be c o n s i d e r e d . Combine the v a r i o u s c o n d i t i o n s in such a manner t h a t the most adverse e f f e c t on the CG w i l l be obtained and accounted f o r In the development of the loading s c h e d u l e , t o assure that the a i r c r a f t i s loaded with the approved l i m i t s at a l l times during f l i g h t . ( 2 ) Landing gear r e t r a c t i o n . I n v e s t i g a t e and account for a p o s s i b l e change in CG p o s i t i o n due t o landing gear r e t r a c t i o n . ( 3 ) F u e l . Account f o r the e f f e c t of CG t r a v e l during a i r c r a f t f l i g h t due t o f u e l oonsuraed down t o the required reserve quantity or to an acceptable ^Inl-nuii reserve quantity e s t a b l i s h e d f o r a p a r t i c u l a r r o u t e . S* Weight o f f l u i d s . Describe the procedure t o be used f o r determining the q u a n t i t y of f l u i d s on board each a i r c r a f t operated. The t o t a l weights o f a l l f l u i d s may be e s t a b l i s h e d by c a l c u l a t i o n , using standard unit weights, such a s : 1 1 . RECORDS. Describe methods by which personnel w i l l maintain a complete, c u r r e n t , and continuous reoord of the weight and center of g r a v i t y o f each a i r c r a f t . Include the procedure f o r recording a l t e r a t i o n s and changes a f f e c t i n g e i t h e r weight or balance of the a i r c r a f t , together with a procedure f o r maintaining a complete and current equlp-nent l i s t . Gasoline Turbine f u e l . . Lubricating o i l 6 pounds per U . S . g a l l o n 6 . 7 pounds per U . S . g a l l o n 7 . 5 pounds per U . S . g a l l o n Par 10 Page 7 AC 135-1B 1/19/76 12- OPERATIONS SPECIFICATIONS. An approved weight and balance control system should be specified in the Operations Specifications shown on the examples of FAA Form 1014 (Operations Specifications) in Appendix 1, Pages 1, 2, and 3. J. A. FERRARESE, Acting Director Flight Standards Service Page 8 Par 12 " 1 9 / 7 6 AC 135-1B Appendix 1 APPENDIX 1. FAA FORM 1014, OPERATIONS SPECIFICATIONS Punn \|i|in»pi1. U N I T E D S T A T E S O F A M E R I C A uuJm iiun-au NO. W-IW;*. F E D E R A L A V I A T I O N A G E N C Y _ WASHINGTON EXAMPLE PART E O P E R A T I O N S S P E C I F I C A T I O N S EXAMPLE OPERATIONS SPECIFICATIONS AIRCRAFT WEIGHT AND BALANCE CONTROL The following procedures have been established to maintain control of weight and balance of A B C Air Taxi Aircraft operated under the terms of these specifications (identified below) and to insure that these aircraft are loaded within the gross weight a n d center of gravity limitations. Determination of Weight o f Passengers a n d Crew. Procedures by which either actual o r approved average passenger and crew weights m a y be used are provided in the operator's company manual. Section , Page . Determination of Weight o f Baggage. (a) W h e n computing the weight and balance of the aircraft, the average passenger baggage weights used are in accordance with the weight and balance section o f A B C A i r Taxi's company manual. Section , Page . (b) T h e average passenger baggage weights authorized in paragraph (a) shall n o t be used i n computing weight and balance involving carriage o f non-standard groups. Periodic Aircraft Weighing. A l t aircraft will be weighed in accordance with the procedures for establishing individual o r fleet aircraft weights as outlined i n weight a n d balance section o f A B C A i r Taxi company manual. Section , Page . Loading Schedules and Identification of Aircraft. The following loading schedules are used for routine operation: Aircraft Type Type Loading Schedule 1. Beech 99 Passenger and Cargo Tabular 2. Beech 18 Cargo Index Loading Instructions. Loading instructions relative to the above listed loading schedules are set forth in A B C A i r Taxi weight a n d balance section of the company manual. Section , Page . K N V r t i v i * Hnto Page 1 A C 1 3 5 - 1 B UW7S A p p e n d i x 1 A I R C R A F T W E I G H T A N D B A L A N C E C O N T R O L T h e o p e r a t o r i s a u t h o r i z e d t o u s e a v e r a g e p a s s e n g e r w e i g h t s t o c o m p u t e p a s s e n g e r l o a d s o v e r a n y r o u t e , e x c e p t I n t h o s e c a s e s w h e r e n o n s t a n d a r d w e i g h t p a s s e n g e r g r o u p s a r e c a r r i e d . E i t h e r m e t h o d m a y b e u s e d I n t e r c h a n g a b t y p r o v i d e d o n l y o n e m e t h o d I s u s e d f o r a n y f l i g h t f r o m b e g i n n i n g t o t e r m i n a t i n g p o i n t o f t h e p a r t i c u l a r t r i p o r f l i g h t i n v o l v e d . 1 * A v e r a g e P a s s e n g e r W e i g h t . a . A n a v e r a g e w e i g h t o f 1 6 0 p o u n d s ( s u n n i e r ) m a y b e u s e d f o r a d u l t p a s s e n g e r s d u r i n g t h e c a l e n d a r p e r i o d o f M a y 1 t h r o u g h O c t o b e r 3 1 . b . A n a v e r a g e w e i g h t o f 1 6 $ p o u n d s ( w i n t e r ) m a y b e u s e d f o r e a c h a d u l t p a s s e n g e r d u r i n g t h e c a l e n d a r p e r i o d f r o m N o v e m b e r 1 t h r o u g h A p r i l 30. c . A n a v e r a g e o f 8 0 p o u n d s m a y b e u s e d f o r c h i l d r e n b e t w e e n t h e a g e s o f 2 a n d 1 2 . C h i l d r e n a b o v e 1 2 y e a r s o f a g e a r e c l a s s i f i e d a s a d u l t s f o r t h e p u r p o s e o f w e i g h t a n d b a l a n c e c o m p u t a t i o n s . C h i l d r e n l e s s t h a n 2 y e a r s o l d a r e c o n s i d e r e d " b a b e s i n a r m s . " d . T h e a b o v e p a s s e n g e r w e i g h t i n c l u d e s m i n o r i t e m s n o r m a l l y c a r r i e d b y a p a s s e n g e r , s u c h a s h a n d b a g s a n d a t t a c h e c a s e s . e . D s c o f a v e r a g e p a s s e n g e r w e i g h t i s n o t a u t h o r i z e d i n t h e c a s e o f f l i g h t s c a r r y i n g p a s s e n g e r s w h o s e a v e r a g e w e i g h t o b v i o u s l y d o e s n o t c o n f o r m w i t h t h e n o r m a l s t a n d a r d w e i g h t . 2 . A c t u a l P a s s e n g e r W e i g h t . A c t u a l w e i g h t w i l l b e u s e d w h e n a p a s s e n g e r l o a d c o n s i s t s p a r t l y o r e n t i r e l y o f a t h l e t i c s q u a d s o r o t h e r g r o u p s w h i c h a r e l a r g e r o r s m a l l e r t h a n t h e a v e r a g e p a s s e n g e r w e i g h t a s s e t f o r t h i n I a b o v e , o r w h e n t h e p a s s e n g e r s * a v e r a g e w e i g h t o b v i o u s l y d o e s n o t c o n f o r m w i t h t h e a v e r a g e p a s s e n g e r w e i g h t . A c t u a l p a s s e n g e r w e i g h t m a y b e d e t e r m i n e d b y s c a l e w e i g h i n g o f e a c h p a s s e n g e r p r i o r t o b o a r d i n g t h e a i r c r a f t , w i t h s u c h w e i g h t i n c l u d i n g m i n o r a r t i c l e s c a r r i e d o n b o a r d b y t h e p a s s e n g e r . I f s u c h a r t i c l e s a r e n o t w e i g h e d , a c c o u n t f o r t h e e s t i m a t e d w e i g h t . T h e a c t u a l p a s s e n g e r w e i g h t m a y a l s o b e d e t e r m i n e d b y a s k i n g e a c h p a s s e n g e r h i s w e i g h t a n d a d d i n g t h e r e t o a p r e d e t e r m i n e d c o n s t a n t t o p r o v i d e f o r h a n d c a r r i e d a r t i c l e s a n d a l s o t o c o v e r p o s s i b l e s e a s o n a l e f f e c t u p o n p a s s e n g e r w e i g h t d u e t o v a r i a n c e i n c l o t h i n g w e i g h t . 3 . C r e w W e i g h t . F o r c r e w m e m b e r s , t h e f o l l o w i n g a v e r a g e w e i g h t s m a y b e u t i l i z e d : a . H a l e c a b i n a t t e n d a n t s I S O p o u n d s ; f e m a l e c a b i n a t t e n d a n t s 1 3 0 p o u n d s . b . A l l o t h e r c r e w m e m b e r s 1 7 0 p o u n d s . E f l V r t i v * - Ante P a g e 2 t'. if III A|'|«ut> ' U n i t e d S t a t e s o f A m e r i c a iiwibh tinnuM v . m u«: rCOCHAL A V I A T I O N A G E N C Y WASHING TON E x a m p l e P a r t E O P E R A T I O N S S I ' K C l F I X - A T I O N S 1 / 1 9 / 7 6 AC 135-1B Appendix 1 U N I T E D S T A T E S O F A M E R I C A F E D E R A L A V I A T I O N A G L N C V W A S H I N O T O N Exaii.pl e OPERATIONS SPECIFICATIONS AIRCRAFT WEIGHT AND BALANCE CONTROL 4, Passenger and C r n w Baggage. The following average passenger baggage weights may be used in lieu of actual weightst a. For each piece of check baggage, an average of not less than 23.5 pounds; and b. For each passenger boarding the aircraft, an average of not less than 5 pounds for hand baggage whether or not such baggage is carried by the passenger, c. Do not use average passenger baggage weights in computing the weight and balance of charter flights and 6Cher flights involving the carriage of special groups. LOAD MANIFEST. K load manifest must be prepared by the flight crew prior to departure from the Loading ramp and it shall include at least the following items: (1) The weight of the aircraft, fuel, oil, cargo, passengers, mail and baggage. (2) The maximum allowable weight for that flight. (3) The total weight as computed under the approved procedures. (4) Evidence that the aircraft 'is loaded according to an approved schedule which ensures that the center of gravity is within limits and will remain so throughout the proposed flight. IH ANY EVENT, REGARDLESS OF WHICH METHOD IS USED, THE AIRCRAFT MUST NOT EXCEED ALLOWABLE WEIGHT AND CENTER OF GRAVITY LIMITS * Uirlft ( lui'vu'i \ » in Part E Effwtivi* dnt*» Page 3 D E P A R T M E N T O P T R A N S P O R T A T I O N FEDERAL AVIATION ADMINISTRATION Washington, D.C. 20991 Official Business POSTA01 AHD FEES PAIS FtDBRAL AVIATION AO MX If I8TRATIO K DOT 515 PENALTY F O R PRIVATE USE. »0Q