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WEIGHT AND BALANCE CLEARANCE FORM F TRANSPORT (USE REVERSE FOR TACTICAL MISSIONS) Cross Reference AF Form 2870 CAF Form F. 115C 50M 5-51 (5797) FOR USE IN T.O. I-1B-40 & AN 01-1B-40 [[marginalia]] NOTE.–THIS TRANSPORT CLEARANCE FORM HAS RESULTED FROM TRIPARTITE AGREEMENT AND NO FURTHER CHANGES MAY BE MADE TO IT WITHOUT PRIOR CONSIDERATION BY TRIPARTITE AUTHORITIES [[/marginalia]] DATE 5 DEC 1957 AIRPLANE TYPE C47 FROM GANOSTUHL HOME STATION GANOSTUHL MISSION/TRIP/FLIGHT/NO. SPECIAL SERIAL NO. 43 48503 TO BERLIN PILOT DAVIS ^[[100%]] LIMITATIONS [[4 Columns]] CONDITION | TAKEOFF | LANDING | LIMITING WING FUEL 2. ALLOWABLE GROSS WEIGHT | 29000 | 26000 | 4824 TOTAL AIRPLANE WEIGHT (Ref. 11) | 23135 | - | - OPERATING WEIGHT PLUS ESTIMATED LANDING FUEL WEIGHT | - | 21635 | - OPERATING WEIGHT (Ref. 8) | - | - | 18311 ALLOWABLE LOAD (Ref. 12) (use SMALLEST figure) | 5865 | 4365 | - [[/4 columns]] 3 PERMISSIBLE C. G. TAKOFF FROM 11 TO (% M.A.C. or IN.) 28 4 PERMISSIBLE C. G. LANDING FROM 11 TO (% M.A.C. or IN.) 28 5 LANDING FUEL WEIGHT 3324 [[4 columns]] REF | ITEM | WEIGHT | 1 INDEX OR MOM/ 1 | BASIC AIRPLANE (From Chart C) | 17076 | 312 2 | OIL (^[[58]] Gal.) | 435 | 288 3 | CREW (No.) ^[[4 2a 2c]] | 800 | 125 4 | CREW'S BAGGAGE | - | - 5 | STEWARD'S EQUIPMENT | - | - 6 | EMERGENCY EQUIPMENT | - | - 7 | EXTRA EQUIPMENT | - | - 8 | OPERATING WEIGHT | 18311 | 125 9 | TAKEOFF FUEL (^[[804]] Gal.) | 4824 | 102 10 | WATER INJ. FLUID ( Gal.) | - | - 11 | TOTAL AIRPLANE WEIGHT | 25135 | 102 [[/4 columns]] 12 DISTRIBUTION OF ALLOWABLE LOAD (PAYLOAD) [10 columns]] COMPT | UPPER COMPARTMENTS PASSENGERS NO. | UPPER COMPARTMENTS PASSENGERS WEIGHT | UPPER COMPARTMENTS CARGO || COMPT | LOWER COMPARTMENTS PASSENGERS NO. | LOWER COMPARTMENTS PASSENGERS NO. | LOWER COMPARTMENTS CARGO || WEIGHT | 1 INDEX OR MOM/ A | - | - | - || - | - | - | - || - | - B | - | - | - || - | - | - | - || - | - C | - | - | - || - | - | - | - || - | - D | - | - | - || - | 2 | 400 | 1200 || 1600 | 43 E | - | - | - || - | - | - | 1200 || 1200 | 115 F | - | - | - || - | - | - | 1100 || 1100 | 278 G | - | - | - || - | - | - | - || - | - H | - | - | - || - | - | - | 125 || 125 | 316 I | - | - | - || - | - | - | - || - | - J | - | - | - || - | - | - | - || - | - K | - | - | - || - | - | - | - || - | - L | - | - | - || - | - | - | - || - | - M | - | - | - || - | - | - | - || - | - N | - | - | - || - | - | - | - || - | - O | - | - | - || - | - | - | - || - | - FWD | BELLY | - | - || - | - | - | - || - | - AFT | BELLY | - | - || - | - | - | - || - | - [[/10 columns]] CORRECTIONS [[4 columns]] COMPT | ITEM | CHANGES (+ or –) WEIGHT | CHANGES (+ or –) 1 INDEX OR MOM/ [[/4 columns]] TOTAL WEIGHT REMOVED | - | - TOTAL WEIGHT ADDED | + | + NET DIFFERENCE (Ref. 14) [[3 columns]] [[ITEM]] | WEIGHT | 1 INDEX OR MOM/ 13 TAKEOFF CONDITION (Uncorrected) | 27160 | 316 14 CORRECTIONS (If required) | - | - 15 TAKEOFF CONDITION (Corrected) | - | - 16 TAKEOFF C. G. IN % M. A. C. OR IN. | 20.8% 17 LESS FUEL | 1500 | - 18 LESS AIR SUPPLY LOAD DROPPED | - | - 19 MISC. VARIABLES | - | - 20 ESTIMATED LANDING CONDITION | 25660 | 350 21 ESTIMATED LANDING C. G. IN % M. A. C. OR IN. | 20.8% [[/3 columns]] COMPUTER BY SIGNATURE ^[[DAVIS]] WEIGHT AND BALANCE AUTHORITY SIGNATURE PILOT SIGNATURE ^[[B O D]] DD FORM 365F 1 SEPT 54 GPO: 1955 O-315288
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