Memory items Flashcards
Max Ramp Weight
40,750 lbs
Max T/O Weight
40,600 lbs
Max Landing Weight
34,150 lbs
Max Zero Fuel Weight
28,200 lbs
Minimum Flight Weight
24,800 lbs
Total Fuel
14,150 lbs
Total Fuel (gravity)
13,000 lbs
Honeywell HTF7350 (AS907-2-1A) takeoff thrust to ISA +15 C
7,323
Total fuel per side
7,075 lbs
Gravity fuel per side
6,500 lbs
Max baggage compartment
750 lbs
Minimum fuel for a go-around (per side)
Minimum altitude for spoilers
500
Emergency exit door weight
45 lbs
Minimum altitude for precision approach < 3.5*
80’
Minimum altitude precision approach 3.5 to 4.5*
160’
Minimum altitude visual, non-precision, AT off if Flaps <30* RA invalid
200’
Minimum height for autopilot engagement
700’
CABIN ALTITUDE - caution
8,500’
CABIN ALTITUDE - warning
(altitude)
9,400’
Max pressure altitude for takeoff and landing
10,000’
APU Max alt (ground), Emer depress altitude (auto mode)
14,000’
Cabin Altitude masks deploy
14,500’
Ditching switch only (below)
15,000’
Max Alt for flaps and gear
18,000’
APU Bleed Air for Engine start & ECS
20,000’
Max Alt for APU START (flight) & APU Gen
30,000’
Max Alt with YD inoperative
31,000’
APU max altitude
37,000’
Max Pressure Altitude
45,000’
Minimum speed for spoiler extension Vref +
8 KIAS
Max tailwind component
10 kts
Max crosswind TO
28 kts
Max crosswind Landing
24 kts
NWS Inop or one AHRS channel inop
15 kts
Max reverse available to
40 KIAS
Autothrottle engaged and thrust verified prior to
80 KIAS
Vmca flaps 10
110 KIAS
Vmcg flaps 20
114 KIAS
Vmcg, Vmcl flaps 10
115 KIAS
Vfe Flaps 30
175 KIAS
Tire limit speed
182 KIAS
Min airspeed for Dual engine flameout
185 KIAS
Vlo retract
200 KIAS
Vfe Flaps 10 and Flaps 20
210 KIAS
Vle, Vlo extension
250 KIAS
Turbulence
265 KIAS or M.75
Max airspeed for Apu start
285 KIAS
Vmo <8,000
300 KIAS
Vmo 8,000’ - 29,475’
320 KIAS
Mmo above 29,475’
M .83
Minimum temp for engine & apu start
-40 C
Minimum battery temperature for TO
-20 C
Max bulk fuel temp for TO, engine start
50 C
What is the automatic landing altitude return-to-base criteria (pressurization)?
6000’ or 10 minutes
How many feet are added to cabin altitude to readjust for a HAA caution light?
650’
How many feet are added to cabin altitude to readjust for a HAA warning light?
1550’
When must the PACK be operating on the ground?
When the aircraft electrical power is ON (Batt or external power) for more than 30 minutes w/ OAT >40 C
Where is Delta P displayed?
EICAS, Summary page, ECS synoptic
Half bank mode ON at altitude?
31,600
Can the pilot override the YD?
NO
What is required to erase the CVR?
Parking brake set and hydraulic system powered.
Audio control panel EMER/NORM switched to EMER position
Audio is routed directly to headphones, bypassing the radio
L (R) BATT OVERHEAT temp
70*C
IP & HP Bleed valves are closed when
Switch(s) is OFF
Fail closed
Fire push selected
Standby Instrument powered by
R ESS Bus
Standby Instrument receives info from
Nav 1
IP Air pressure regulated to
50 psi
HP Air regulated to
36 psi
How do you know an External Air Cart is connected?
psi displayed in the manifold on the ECS page
When will GRND spoilers Auto deploy?
WOW, RA > 7’, wheel speed > 16kts
Multi-function-spoilers
45, Ground 60
PSEU
Proximity Sensing Electric unit - WOW, TR pos, fuel door
BCU
Brake Control Unit
EPAV
Electrical Pneumatic Actuating Valve (brains for O2, compensator, etc.)
O2 min - max
700 liters (Oxy qty low CAS) - 5458 liters
Types of operation
Day, Night, VMC, IMC, Icing, Ditching
What is the purpose of the scavenge ejectors?
Transfer fuel from lowest inboard section of wing to the collector tank.
After crossing the holding fix in the FMS, what is displayed next to 6L
Exit Hold
What is the minimum width for an 180 degree turn with a 5’ safety margin?
58’
Load Factors
Flaps Up
Flaps Extended
Flaps Up +2.6 to -1.0 G
Flaps Extended + 2.0 to 0.0 G
Generator amp limits
Normal
Single gen flight
Transient
Normal 400a
Single gen flight 500a
Transient (5min) 600a
Pavement for 180* turn
58’
Aircraft dimensions
68’8” L x 69’ W x 20’ H
Nose wheel steering
Tiller
Pedals
Tiller 65*
Pedals 7*
What is the danger area distance for the Challenger 350 weather radar?
5 ft
What is the danger area distance for the Challenger 350 intake?
15 ft (4.5 m)
What is the danger area distance for the APU exhaust on the Challenger 350?
19 ft (5.8 m)
What is the danger area distance for the tailpipe of the Challenger 350?
200 ft (60.9 m)
Minimum fuel load for takeoff
2,800 lbs.
Minimum oil temp for takeoff?
+27C
