Aircraft General Flashcards
The overall length of the CRJ 900 is:
118’ 10.7”
The CRJ 900 wing span is…
81’-6” EP
76’ 3”
The engine exhaust danger area for the CRJ 900 at idle thrust is:
100’
On the CRJ 900, the distance from the top of the vertical stabilizer to the ground is:
24’ 1”
The CRJ 900 max taxi and ramp weight is:
82,750 pounds
Maximum landing weight
73,500 pounds
Maximum zero fuel weight
70,000 pounds
Minimum flight weight
45,000 pounds
CRJ 700 turning radius
75’
The danger area in front of the CRJ 700/900 with the radar operating is:
2’
What is the max load capacity on the pax door:
1000# or four people
Maximum number of people allowed on the stairway
4
Which is not a plug type door on the CRJ:
Passenger door
A red door warning message on the EICAS would indicate that the
The passenger door is not locked properly
How many emergency exits are on the CRJ 900:
6
How many emergency exits are on the CRJ 700
5
CRJ 900 turning radius is
80’1”
Maximum passenger seats on 900
76-79 depends on configure
Max aft cargo capacity on 900
4375 pounds
Max forward cargo capacity in fwd and center compartments on 900.
1700 pounds, 850 lbs per compartment
Total fuel with pressure refueling on 900,
19,594 pounds
Left main tank and right main tank capacity with pressure refueling on 900.
7492 pounds.
Center fuel tank capacity with pressure refueling on 900.
4610 pounds
Horizontal stabilizer width on the 900.
28’4”
Distance maingear to maingear
13’6”
MMO
.85 Mach
MMO RVSM in 900.
.82 Mach
Flap 1/8
230
Flap 20
220
Flap 30
185
Flap 45
170
Max landing gear operation speed extension
220
Max landing gear operating speed retraction
200
Max speed with landing gear extended and locked.
220
Turbulence penetration speed
280/.75 whichever is lower
Max wiper operation speed
250
Max operating altitude
41,000 feet
Maximum airport pressure altitude takeoff and landing.
10,000 feet
Maximum demonstrated crosswind for takeoff/landing
22 kts dry runway
Maximum approved tailwind takeoff/landing
10 KTS
Maximum tire speed
195 KTS
Maximum altitude For extending flaps
15,000 feet
Maximum runway slope
+-2%
Maximum takeoff weight
82,500 Pounds
Max left main tank and right main tank fuel capacity with gravity refueling on 900.
7405 pounds
Total fuel capacity with gravity refueling.
14,810 pounds.
What is the max fuel load in pounds that can be in the center tank if the two main tanks are not fueled to at least 4,400 pounds each in the 900?
500 pounds
Max altitude for single pack operation in the 900.
25,000 feet.
Minimum fuel quantity in each tank for a go around in the 700/900.
600 pounds
The engine exhaust danger area for the CRJ 900 at maximum thrust is:
290 feet.
CRJ 700 max altitude for pressurized using one pack ?
31,000
