2024年3月20日发(作者：吉范明)
Aircraft Weighing Report
Single Point Balancing
Aircraft Type
Mk
MOD Form 756A
(Revised Oct 93)
PPQ = 10
Serial Number
Last recorded figures from MOD Form 751 / RN A701
Weight
Moment
C of G
Certified that aircraft Surplus and Deficiency Form (MOD Form 756D) has been completed as per the Basic and Variable
Load Tables in the aircraft's AP, weight and C of G chapter:
Airframe
PropulsionElectrical
Weapons
(Enter AP details).
Air Radar
Air Comms
Flt SystemsSafety Equip
SNCO IC Aircraft
Certified that the MOD Form 756D has been completed and signed for by the required trades in the blocks above.
Name and Rank (Blk Caps)Signature
Unit
Date of Weight
Job Number
Weighing SNCO
Name and Rank (Blk Caps)Signature
Details of this report have been entered on MOD Form 751 / RN A701
Name (Blk Caps)Signature
Single Point Balancing
Serial No
Load
Reading
Latitude
Correction
Figure
Latitude
Corrected
Load
Zero
Error
Actual
Load
Weight of
Tackle at
Rotor Head
S
y
m
b
o
l
W
Added Weight (3):....
Distance from Weighing Datum Line to Centre Line of:or
Tail Reaction (3):....
Weight Added to bring Aircraft Longtitudinal Datum Line Level (3):....
or
Tail Reaction (3):............................................
Wt1
L
Fwd (3):...
Aft (3):.............
Aircraft Weight
As Weighed
Distance from Weighing Datum Line to C of G Datum Point
d
Fwd (3):...
Aft (3):.............
Distance from Weighing Datum Line to C of G Position = (Wt1) x (L)
(W)
a
Fwd (3):...
Aft (3):.............
Distance of C of G from C of G Datum Point As Weighed = d ± a
x
Fwd (3):...
Aft (3):.............
Aircraft Moment As Weighed = (W) x (x)
(+ If C of G Aft of Datum,
2024年3月20日发(作者：吉范明)
Aircraft Weighing Report
Single Point Balancing
Aircraft Type
Mk
MOD Form 756A
(Revised Oct 93)
PPQ = 10
Serial Number
Last recorded figures from MOD Form 751 / RN A701
Weight
Moment
C of G
Certified that aircraft Surplus and Deficiency Form (MOD Form 756D) has been completed as per the Basic and Variable
Load Tables in the aircraft's AP, weight and C of G chapter:
Airframe
PropulsionElectrical
Weapons
(Enter AP details).
Air Radar
Air Comms
Flt SystemsSafety Equip
SNCO IC Aircraft
Certified that the MOD Form 756D has been completed and signed for by the required trades in the blocks above.
Name and Rank (Blk Caps)Signature
Unit
Date of Weight
Job Number
Weighing SNCO
Name and Rank (Blk Caps)Signature
Details of this report have been entered on MOD Form 751 / RN A701
Name (Blk Caps)Signature
Single Point Balancing
Serial No
Load
Reading
Latitude
Correction
Figure
Latitude
Corrected
Load
Zero
Error
Actual
Load
Weight of
Tackle at
Rotor Head
S
y
m
b
o
l
W
Added Weight (3):....
Distance from Weighing Datum Line to Centre Line of:or
Tail Reaction (3):....
Weight Added to bring Aircraft Longtitudinal Datum Line Level (3):....
or
Tail Reaction (3):............................................
Wt1
L
Fwd (3):...
Aft (3):.............
Aircraft Weight
As Weighed
Distance from Weighing Datum Line to C of G Datum Point
d
Fwd (3):...
Aft (3):.............
Distance from Weighing Datum Line to C of G Position = (Wt1) x (L)
(W)
a
Fwd (3):...
Aft (3):.............
Distance of C of G from C of G Datum Point As Weighed = d ± a
x
Fwd (3):...
Aft (3):.............
Aircraft Moment As Weighed = (W) x (x)
(+ If C of G Aft of Datum,