Aircraft Manifest and Weight and Balance ___________________
Date of Flight: __________
Manifest Serial #: __________
Aircraft:____________ / CE-501
From: _________________________________________
Via: ________________
To: ___________________________________________
Distance: ____________
Example Only
CREW/PAX
WEIGHT
AIRCRAFT STATUS
PIC: __________________________
______________
Calendar Event:
______
SIC/Pax:_______________________
______________
Tach Event:
______
Pax: __________________________
______________
Pax: __________________________
______________
Altimeter System:
______
Pax: __________________________
______________
ATC XPDR Due:
______
Pax: __________________________
______________
ELT Insp. Due:
______
Pax: __________________________
______________
Pax: __________________________
______________
BAGGAGE
______
WEIGHT
____________
Baggage: ___________________
Example Only
FLIGHT (WEATHER) BRIEFING:
FAA FLIGHT PLAN
1. TYPE OF
FLIGHT PLAN
2. A/C
IDENT.
3. A/C TYPE/
SPEC. EQUIP.
4. TRUE
AIRSPEED
5. DEP.
POINT
6. DEP. TIME (Z)
PROP.
ACTUAL
7.
CRUISING
ALTITUDE
VFR
IFR
C500 /
DVFR
KTS
FT
8. ROUTE OF FLIGHT
9. DESTINATION- NAME OF
AIRPORT AND CITY (ID)
10. EST. TIME
ENROUTE
HOURS
12. FUEL ON
BOARD
13. ALTERNATE AIRPORT(S)
11. REMARKS
MINUTES
14. PILOT’S NAME, ADDRESS & TELEPHONE
NO., AIRCRAFT HOME BASE
Example Only
HRS
15.
NUMBER
ABOARD
MINS
17. DESTINATION CONTACT/TELEPHONE (Opt.)
16. COLOR OF
AIRCRAFT
CLOSE VFR FLIGHT PLAN WITH _______________ FSS UPON ARRIVAL
Preflight inspection completed. Maintenance discrepancies cleared or MEL-deferred. I have
checked this manifest, including the weight and balance data and calculations. I have found
the manifest and all associated data and calculations, as shown, to be complete and correct.
Date _________________ Time __________ PIC Signature __________________________
COPYRIGHT © 2013 by FlightComp Systems and its licensors. All rights reserved. DISCLAIMER: FlightComp Systems accepts no liability of any kind for any loss(es) or damage(s) caused, or alleged to be caused,
directly or indirectly, as a result of using this manifest form.
WARNING: This form is based only on “generic” references including TCDS No. A22CE as published online in the FAA Regulatory & Guidance Library
(RGL). This form cannot be used for actual weight and balance control purposes unless it is first checked and modified in accordance with information contained in the aircraft’s official FAA-approved Airplane Flight Manual
(AFM). Any use of this form constitutes unconditional acceptance of the above standards and policies by the person(s) or other legal entity(s) using it.
Page 2 - Manifest Serial #: _________
Cessna CE-500/501 (Cessna Citation I ) - Weight and Balance
( Serial Numbers 500-0303 to 500-0689 (and 500-0001 to 500-0302 with Cessna Service Bulletin upgrades )
Aircraft ____________ (i.e., N12345)
Weight
(Lbs.)
Arm
(In.)
Moment
(In-lbs.)
TCDS No. A22CE
Typical Empty Weight: 7084 Lbs.
Basic Empty Weight - Weighing Due ________
Pilot-in-Command
131.0
Second-in-Command
131.0
Seat #3 Occupant
207.0
Seat #4 Occupant
207.0
Seat #5 Occupant
241.0
Jet A / A-1
6.75 PPG
Seat #6 Occupant
241.0
JET B / JP-4
6.5 PPG
Seat #7 Occupant
267.0
JP-5
6.8 PPG
Seat #8 Occupant
267.0
JP-8
6.7 PPG
Nose Baggage Compt. - 350 Lbs Max
74.0
Aft Cabin Baggage Compt. - 650 Lbs Max
286.3
Example Only
Approximate Fuel Densities @ 15E C
AVGAS 100LL
AVGAS 100 / 80
6 PPG
5.8 PPG
Zero-Fuel Weight - 8400 Lbs Max
FUEL TANKS (Ramp)
Gals
256.0
Max. Useable Fuel: 564 Gallons
Ramp Gross Weight - 12,000 Lbs Max
Example Only
FUEL TANKS (Takeoff)
Gals
256.0
Fuel to Taxi: 209 Lbs. every 10 Mins.
Gals
256..0
Fuel used, Takeoff to Landing:
Takeoff Gross Weight - 11,850 Lbs Max
FUEL TANKS (Landing)
Landing Gross Weight - 11,350 Lbs Max
CE-500/501 - Center of Gravity Limits vs. Gross Weight
Gross Weight (Lbs)
[ C.G. Range (Gear Extended): 11,850 Lbs: +250.0 to +255.9 / 7,500 Lbs or less: +246.4 to +255.9 ]
(Straight line variation between points given).
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
11850 Lbs. +
250.0 >
<2 55.9
Max Takeoff Weight: 11850 Lbs.
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
11250 Lbs. +
249.5 >
< 255.9
Max Landing Weight: 11350 Lbs.
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
10650 Lbs. +
249.0 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + ..
10050 Lbs. +
248.5 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
9450 Lbs. +
248.0 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
8850 Lbs. +
247.5 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
8250 Lbs. +
247.0 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
7650 Lbs. + 246.5 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
7050 Lbs. + 246.4 >
< 255.9
+ . + . + . + . + . + . + . + . + . + . + . + . + . + . + .
244
246
248
250
252
254
256
258
Center of Gravity - Inches Aft of Datum
Example Only
EXTREME CARE MUST BE EXERCISED TO ENSURE THAT THIS DATA IS EXACTLY APPLICABLE TO ANY AIRCRAFT FOR WHICH IT IS TO BE USED.
COPYRIGHT © 2013 by FlightComp Systems and its licensors. All rights reserved. DISCLAIMER: FlightComp Systems accepts no liability of any kind for any loss(es) or damage(s) caused, or alleged to be caused,
directly or indirectly, as a result of using this manifest form.
WARNING: This form is based only on “generic” references including TCDS No. A22CE as published online in the FAA Regulatory & Guidance Library
(RGL). This form cannot be used for actual weight and balance control purposes unless it is first checked and modified in accordance with information contained in the aircraft’s official FAA-approved Airplane Flight Manual
(AFM). Any use of this form constitutes unconditional acceptance of the above standards and policies by the person(s) or other legal entity(s) using it.