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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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