1
Q
Weight Limitations
A
Ramp..........8730 lbs Takeoff.......8645 lbs Landing......8000 lbs ZFW............6750 lbs Max design fuel....2580 lbs
Takeoff limited by:
- max certified TO weight
- TO climb requirements
- TO field length
Landing limited by:
- Max LW
- Landing climb requirements
- landing distance
2
Q
TO and LDG
- Max altitude
- Max tailwind
- Max Xwind (without thrust reverser deployment)
- Max fuel imbalance
- Max ambient temp
A
- Max altitude…….. 14000’
- Max tailwind……. 10kt
- Max Xwind (without thrust reverser deployment)…….. 25kt
- Max fuel imbalance…. 200 lbs, 600lbs emerg.
- Max ambient temp….. refer AFM
3
Q
En Route Operations
- Max operating alt
- Max ambient temp
- Min ambient temp
- Max Alt flap extension
- Min temp for flap operation
- Yaw damper must be engaged
A
- Max operating alt…………. 41000’
- Max ambient temp………. 50 deg at 0ft P.alt
- Min ambient temp………..-54 deg 0ft P.alt
- Max Alt flap extension…. 18000’
- Min temp for flap operation… -40 deg
- Yaw damper must be engaged… >FL300
4
Q
RVSM OPS
- RVSM Levels
- Min speed RVSM airspace
- Min weight RVSM airspace
- Required equipment
- Altimeter requirement
A
RVSM OPS
- RVSM Levels…. FL290 - FL410
- Min speed RVSM airspace…. 110 KIAS
- Min weight RVSM airspace…. 6300 lbs
- Required equipment
- pilot and copilot altimeters
- autopilot
- altitude alerter
- ATCRBS Xpdr
- changes to pitot/static, ADC, AP, ALT Alert and xpdr should be assessed for impact on RVSM approval
- stby alt not approved for RVSM ops
- Both must read field elevation within 50’ and 75’ of each other on local QNH
5
Q
AIRSPEED LIMITATIONS
- Mmo (above 27120’)
- Vmo (SL to 27120’)
- Max AP speed
- Vturb
- TO/APP flaps (15 deg)
- LAND flaps (130 deg)
A
AIRSPEED LIMITATIONS
- Mmo (above 27120’)…. 0.63 M
- Vmo (SL to 27120’)…… 250 KIAS
- Max AP speed…………. 250 KIAS
- Vturb……………………… 160 KIAS
- TO/APP flaps (15 deg). 185 KIAS
- LAND flaps (130 deg).. 150 KIAS
6
Q
AIRSPEED LIMITATIONS
- VLE
- VLO (extending)
- VLO (retracting)
- Max tyre gnd speed
- Min speed in sustained icing (limit)
A
AIRSPEED LIMITATIONS
- VLE……………………. 250 KIAS
- VLO (extending)….. 250 KIAS
- VLO (retracting)….. 185 KIAS
- Max tyre gnd speed… 160 KIAS
- Min speed in sustained icing (limit) … 160 KIAS
7
Q
AIRSPEED LIMITATIONS
- Vmca (flap 0)
- Vmca (flap 15)
- Vmcg
- Vx (all engines, flap 15)
- Vy (all engines, flap 15)
A
AIRSPEED LIMITATIONS
- Vmca (flap 0)……….. 92 KIAS
- Vmca (flap 15)……… 81 KIAS
- Vmcg………………….. 73 KIAS
- Vx (all engines, flap 15).. 105 KIAS
- Vy (all engines, flap 15).. 150 KIAS
8
Q
PRESSURISATION
- Normal Max Differential
- Max Differential
A
- Normal Max Differential……. 8.3 psi
- Max Differential…………… 8.5 +/- 0.1 psi
9
Q
TO and LDG Operations
- Max Altitude
- Max TW component
- Max ambient temp
- Max demonstrated x-wind
A
- Max Altitude….. 14,000’
- Max TW component …… 10 kts
- Max ambient temp…… refer figures (50 deg at sea level)
- Max demonstrated x-wind ……. 25 kts
10
Q
Manoeuvring Speed
- consult chart
- 6000 lbs
- 8645 lbs
A
Manoeuvring Speed
*consult chart
- 6000 lbs…… 133 KIAS
- 8645 lbs…… 160 KIAS
11
Q
ELECTRICAL LIMITATIONS
Starter
Battery
A
Starter
- 3 starts in 30 mins
- 3 cycles with 60 seconds rest permitted
Battery
- on ground, idle…. 150 amps
- on ground, above idle….. 300 amps
- air <= 30000’ ….. 300 amps
- air >30000’ ……. 280 amps
12
Q
ENGINE
ITT LIMITS
- TO
- MCT
- MAX CRZ
- Transient (20 secs)
TO THRUST TIME LIMIT
A
ENGINE
ITT LIMITS
- TO…………… 830
- MCT………….. 830
- MAX CRZ ……830
- Transient (20 secs)..862
TO THRUST TIME LIMIT
5 mins per flight, 10 mins 1 inop
13
Q
ENGINE LIMITATIONS
N2
- Gnd idle
- Flt idle
- TO, CRZ, MCT
- Transient
N1
- TO, CRZ, MCT
- Transient
A
ENGINE LIMITATIONS
N2
- Gnd idle…….. 48.6
- Flt idle………. 56.8
- TO, CRZ, MCT.. 100
- Transient….. 102
N1
- TO, CRZ, MCT… 100
- Transient……….. 101
14
Q
ENGINE LIMITATIONS
Oil temps
- start
- gnd idle
- flt idle
- TO, CRZ, MCT
- Transient (90 secs)
A
ENGINE LIMITATIONS
Oil temps
- start…………… -40
- gnd idle………. -40 to 135
- flt idle…………. 22 to 135
- TO, CRZ, MCT … 22 to 135
- Transient (90 secs)… 135 to 141
15
Q
FUEL
- FUEL LO L-R CAS MSG
- Max approved imbalance
- max demonstrated emerg imbalance
- Min qty for TO per wing
A
FUEL
- FUEL LO L-R CAS MSG…… 170 lbs, turn boost pump on
- Max approved imbalance…. 200 lbs
- max demonstrated emerg imbalance…. 600 lbs
- Min qty for TO per wing…… 200 lbs
16
Q
FLIGHT CONTROLS
- Vortex generators, number installed, number required
Static wicks
- total missing
- wingtips and ailerons, installed, required
- rudder and tailcone, installed, required
- elevators, installed, required
A
FLIGHT CONTROLS
- Vortex generators, number installed, number required …… 16, 16
Static wicks
- total missing …… 2
- wingtips and ailerons, installed, required…. 3, 2 per side
- rudder and tailcone, installed, required….. 4, 3
- elevators, installed, required……. 6 (3/side), 5
17
Q
ICING
- prior to takeoff
- Min airspeed sustained flight in icing conditions
- configuration restrictions
- ENGINE ANTI ICE selected on when…?
- WING/STAB deice selected on when…?
A
ICING
- prior to takeoff….. airplane must be free of ice
- Min airspeed sustained flight in icing conditions…. 160 KIAS
- configuration restrictions…. only flaps up/ gear up unless during approach
- ENGINE ANTI ICE selected on when… +10 deg RAT or colder and in visible moisture
- WING/STAB deice selected on when… first sign of ice accretion anywhere on airplane
18
Q
AUTOPILOT
Minimum use heights
- TO and climb
- ENR and descent
- APRCH (GP or GS Mode)
- APRCH (FLC, VS, PIT, ALT mode) or APRCH MDA
A
AUTOPILOT
Minimum use heights
- TO and climb…. 700’ AGL
- ENR and descent …. 1000’ AGL
- APRCH (GP or GS Mode)…. 200’ AGL
- APRCH (FLC, VS, PIT, ALT mode) or APRCH MDA…. higher of 400’ AGL
Citation Mustang
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