FLIGHT SAFETY CITATION EXCEL
LIMITATIONS. EXAM 2025/2026
QUESTIONS AND ANSWERS 100% PASS
Maximum Design Ramp Weight - ANS 20,200 lbs
Maximum Design Takeoff Weight - ANS 20,000 lbs
Maximum Design Landing Weight - ANS 18,700 lbs
Maximum Design Zero Fuel Weight - ANS 15,000 lbs
Minimum Flight Weight - ANS 12,400 lbs
Maximum Tailcone Baggage Weight - ANS 700 lbs
Minimum Oil Temperature for ground engine startin - ANS -40C (AM, AX, AY) or -20C (AV)
(CONFIG BF ONLY) L and R IGNITION must be selected of ___ Prior to reducing power to less
than ____ N2 - ANS On, 70%
1 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED
, Starter Limitation - ___ engine starts per _____ with ___ second rest period between cycles -
ANS 3, 30 minutes, 90 seconds
Battery Limitation - ___ engine starts per _____ - ANS 3, 1 hour
If battery limitation is exceeded, a _________ including a ________ must be accomplished -
ANS deep cycle, capacity check
How many generator assisted cross starts are equal to one battery start? - ANS 3 (each 1/3
of a battery start)
How many battery starts does one external power start count as? - ANS 0
External power source must be ____ VDC, and between ____ amps and ____ amps - ANS 28
VDC, 800-1000 amps
APU Starter Limitation - ___ APU starts per _____ with ___ second rest period between cycles -
ANS 3, 30 minutes, 90 seconds
APU Battery Limitation - ___ APU starts per _____. An APU counts as ___ of a normal engine
battery start - ANS 9, 1 hour, 1/3
___ Battery cycle is counted when starting the APU from a ground power unit - ANS No
Continuous engine ground static operation up to and including ___ minutes at takeoff thrust is
limited to ambient temperatures not to exceed ____ - ANS 5 minutes, 39C above ISA
Limit ground operation of pitot/static heat to ___ minutes - ANS 2 minutes
2 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED
LIMITATIONS. EXAM 2025/2026
QUESTIONS AND ANSWERS 100% PASS
Maximum Design Ramp Weight - ANS 20,200 lbs
Maximum Design Takeoff Weight - ANS 20,000 lbs
Maximum Design Landing Weight - ANS 18,700 lbs
Maximum Design Zero Fuel Weight - ANS 15,000 lbs
Minimum Flight Weight - ANS 12,400 lbs
Maximum Tailcone Baggage Weight - ANS 700 lbs
Minimum Oil Temperature for ground engine startin - ANS -40C (AM, AX, AY) or -20C (AV)
(CONFIG BF ONLY) L and R IGNITION must be selected of ___ Prior to reducing power to less
than ____ N2 - ANS On, 70%
1 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED
, Starter Limitation - ___ engine starts per _____ with ___ second rest period between cycles -
ANS 3, 30 minutes, 90 seconds
Battery Limitation - ___ engine starts per _____ - ANS 3, 1 hour
If battery limitation is exceeded, a _________ including a ________ must be accomplished -
ANS deep cycle, capacity check
How many generator assisted cross starts are equal to one battery start? - ANS 3 (each 1/3
of a battery start)
How many battery starts does one external power start count as? - ANS 0
External power source must be ____ VDC, and between ____ amps and ____ amps - ANS 28
VDC, 800-1000 amps
APU Starter Limitation - ___ APU starts per _____ with ___ second rest period between cycles -
ANS 3, 30 minutes, 90 seconds
APU Battery Limitation - ___ APU starts per _____. An APU counts as ___ of a normal engine
battery start - ANS 9, 1 hour, 1/3
___ Battery cycle is counted when starting the APU from a ground power unit - ANS No
Continuous engine ground static operation up to and including ___ minutes at takeoff thrust is
limited to ambient temperatures not to exceed ____ - ANS 5 minutes, 39C above ISA
Limit ground operation of pitot/static heat to ___ minutes - ANS 2 minutes
2 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED
