FOR USE WITH T.O. 1-1B-40, NAVAIR
Form Approved
FORM B - AIRCRAFT WEIGHING RECORD
01-1B-40 AND TM-55-1500-342-23
OMB No. 0704-0188
The public reporting burden for this collection of information is estimated to average 10 minutes per response, including the time for reviewing instructions, searching existing
data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any
other aspect of this collection of information, including suggestions for reducing the burden, to the Department of Defense, Executive Services Directorate (0704-0188).
Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information
if it does not display a currently valid OMB control number.
DATE WEIGHED (YYYYMMDD)
MODEL/DESIGN/SERIES
SERIAL NUMBER
PLACE WEIGHED
WEIGHT AND BALANCE TECHNICIAN (Last, First, M.I.)
DUTY PHONE NO.
REACTION
SCALE
CORRECTIONS
NET WEIGHT
ARM
MOMENT
(Wheels, jackpoints, etc.)
LEFT MAIN
RIGHT MAIN
E
SUB-TOTAL
(Both main)
F
NOSE OR TAIL
TOTAL
(as weighed)
Not to be posted on Chart C
MEASUREMENTS
CORRECTIONS
B=
the distance from the jig point, to the center line of the main reactions.
NOSE
LEFT
RIGHT
Obtain by measurement.
OR
MAIN
MAIN
TAIL
the distance from the reference datum to the jig point of the aircraft, from which
I=
CALB
a plumb bob can be dropped to the ground. Obtain from the aircraft diagram in
CORR
Chart E.
SCALE
the distance from the reference datum to the center line of the main reactions.
CORR
1
E=
E = I+B
E = I - B (If the jig point is aft of the center line of the main reactions.)
TEMP
2
D=
the distance between the main and nose or tail reaction. Obtain by measurement.
EQUIP
the distance from the reference datum to the center line of the nose or tail
OTHER
1
F=
reaction.
F = E - D (for nose reaction)
F = E+D (for tail reaction)
TOTAL
DIAGRAMS FOR MEASURING VARIOUS TYPES OF REACTIONS TO DETERMINE ARM OF SUPPORT POINTS.
See Aircraft Chart E's for specific weighing instructions.
Check dimensions E and F against approximate dimensions listed on Chart E.
1
Enter temperature at time of weighing.
2
DD FORM 365-2, AUG 96
PREVIOUS EDITION MAY BE USED.
Reset
FOR USE WITH T.O. 1-1B-40, NAVAIR
Form Approved
FORM B - AIRCRAFT WEIGHING RECORD
01-1B-40 AND TM-55-1500-342-23
OMB No. 0704-0188
The public reporting burden for this collection of information is estimated to average 10 minutes per response, including the time for reviewing instructions, searching existing
data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any
other aspect of this collection of information, including suggestions for reducing the burden, to the Department of Defense, Executive Services Directorate (0704-0188).
Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information
if it does not display a currently valid OMB control number.
DATE WEIGHED (YYYYMMDD)
MODEL/DESIGN/SERIES
SERIAL NUMBER
PLACE WEIGHED
WEIGHT AND BALANCE TECHNICIAN (Last, First, M.I.)
DUTY PHONE NO.
REACTION
SCALE
CORRECTIONS
NET WEIGHT
ARM
MOMENT
(Wheels, jackpoints, etc.)
LEFT MAIN
RIGHT MAIN
E
SUB-TOTAL
(Both main)
F
NOSE OR TAIL
TOTAL
(as weighed)
Not to be posted on Chart C
MEASUREMENTS
CORRECTIONS
B=
the distance from the jig point, to the center line of the main reactions.
NOSE
LEFT
RIGHT
Obtain by measurement.
OR
MAIN
MAIN
TAIL
the distance from the reference datum to the jig point of the aircraft, from which
I=
CALB
a plumb bob can be dropped to the ground. Obtain from the aircraft diagram in
CORR
Chart E.
SCALE
the distance from the reference datum to the center line of the main reactions.
CORR
1
E=
E = I+B
E = I - B (If the jig point is aft of the center line of the main reactions.)
TEMP
2
D=
the distance between the main and nose or tail reaction. Obtain by measurement.
EQUIP
the distance from the reference datum to the center line of the nose or tail
OTHER
1
F=
reaction.
F = E - D (for nose reaction)
F = E+D (for tail reaction)
TOTAL
DIAGRAMS FOR MEASURING VARIOUS TYPES OF REACTIONS TO DETERMINE ARM OF SUPPORT POINTS.
See Aircraft Chart E's for specific weighing instructions.
Check dimensions E and F against approximate dimensions listed on Chart E.
1
Enter temperature at time of weighing.
2
DD FORM 365-2, AUG 96
PREVIOUS EDITION MAY BE USED.
Reset
INDEX OR
1
DESCRIPTION
NET WEIGHT
ARM
MOMENT
MOM/
TOTAL (As weighed)
(From front side)
TOTAL OF ITEMS WEIGHED BUT
_
_
NOT PART OF BASIC WEIGHED
(From Column I below)
TOTAL OF BASIC WEIGHT ITEMS
+
+
NOT IN AIRCRAFT WHEN WEIGHED
(From Column II below)
BASIC AIRCRAFT
(Post to Chart C)
COLUMN I
COLUMN II
ITEMS WEIGHED BUT
BASIC WEIGHT ITEMS
NOT PART OF
WEIGHT
ARM
MOMENT
NOT IN AIRCRAFT
WEIGHT
ARM
MOMENT
BASIC WEIGHT
WHEN WEIGHED
TOTAL
TOTAL
REACTIONS USED
TYPE SCALE
SERIAL NUMBER
CALIBRATION DATE (YYYYMMDD)
CALIBRATED ACCURACY
REMARKS
Enter constant used
1
DD FORM 365-2 (BACK), AUG 96
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