Limitations Flashcards
0
Q
Nose wheel steering
A
Rudder pedals - 8 degrees
Tiller - 80 degrees
1
Q
Turning Radius
A
80’ 1”
2
Q
Max ramp weight
A
82,750 lbs
3
Q
Max T/O weight
A
82,500 lbs
4
Q
Max Landing weight
A
73,500 lbs
5
Q
Max Zero Fuel Weight
A
70,000 lbs
6
Q
Min flight weight
A
45,000 lbs
7
Q
Cargo weight limits
A
FWD - 850 lbs
CTR - 850 lbs
AFT - 4375
8
Q
Headset must be worn
A
Below FL180
9
Q
Max airport pressure altitude
A
10,000 feet
10
Q
Takeoff, landing, and operating limits (for pressure altitude above 8,000 feet and CABIN ALT WARN HI displayed.
A
One pilot must use oxygen from TO until message goes out, and landing until the airplane has vacated the runway after landing. The regulator should be set to the normal (N) position
11
Q
Max operating altitude
A
41,000 feet
12
Q
Max temp for T/O and landing
A
ISA + 35 C
13
Q
Min temp for takeoff
A
ISA - 40 C
14
Q
Engine type
A
GE CF34-8C5
15
Q
APR arms when thrust is within _____ of scheduled thrust setting
A
8%
16
Q
APR Activates on takeoff if:
A
Thrust levers are in TOGA detent
Either normal, flex or GA power is programmed
Engine fail (N1 rpm differ by 15%
17
Q
APR Activates on GA if:
A
OEO operations, or Engine failure (N1 RPM differ by 15%)
18
Q
Set OEO fuel scheduling for MCT by:
A
Placing thrust levers in the Max Power detent
19
Q
Engine thrust
A
APR - 14,750
Non-APR - 13,560
20
Q
Cold soaked definition:
A
- 30 degrees C (22 F) or below for more than 8 hours
21
Q
Cold soaked engine prep
A
Motored 60 seconds
Fan rotation observed
Thrust reversers cycles - 2 seconds or less
22
Q
Engine warm-up
A
IDLE - Normal operating range
Do not exceed 75% N1 for 2 minutes or until in normal operating range whichever is longer
23
Q
Engine ground start
A
ITT below 120 degrees C
24
Engine air start
ITT below 90 degree C
25
Do not accelerate engine until oil pressure has stabilized ???
Below 116 psi
26
Engine to engine N2 split?
Not be greater than 2% N2
27
If N2 is ______ or less with an OAT of _______ do not accelerate above idle
57%, - 20 degrees C
28
Min N2 for start
20%
29
Min N1 for start
Rotation
30
Min oil temp for start
- 40 degrees C
31
Min oil pressure min steady state
25 psi
32
When the engines are operating and oil quantity is below ______ or engines not operating and oil quantity is below ____ the L(R) OIL LEVEL LO status message is displayed
57%, 80%
33
Oil level is checked?
3 minutes - 2 hours after every engine shutdown
34
EICAS limit display status message colors
Green - Normal operating range
Amber - Caution range
Red - Max and min limitations
35
Continuos Ignition Must be used when:
T/O & LDG on contaminated runways
MDT or HVY rain
MDT or HVY turbulence
Vicinity of TS
36
Engine starter cracking limits:
1st & 2nd attempts - 90 seconds on, 10 seconds off
| 3rd - 5th attempts- 90 seconds on, 5 minutes off
37
Engine starter cracking limits (flight)
1st attempt - 120 seconds on, 10 seconds off
| 2 - 5 attempts - 60 seconds on, 5 minutes off
38
Engine dry motor cycle (ground)
1st attempt: 90 seconds on, 5 minutes off
| 2 - 5 attempts: 30 seconds on, 5 minutes off
39
Air start limits:
Windmill and starter assist 21,000 feet and below
| Rapid Relight: 10,000 feet and below
40
Max fuel imbalance between main tanks:
Takeoff - 300 lbs
| Flight - 800 lbs
41
Gravity fuel total:
14,810 lbs
42
Pressure refueling:
Total: 19,595 lbs
Mains: 7,492 lbs
Center: 4,610 lbs
43
Max fuel in center tank with less than ________ lbs in each main tank is _______ :
4,400 lbs, 500 lbs
44
Min fuel in each main tank for GA:
600 lbs
45
Min engine fuel temp limit for takeoff:
5 degrees C at engine inlet
46
Min temp for bulk fuel takeoff limit:
Jet A - 30 degrees C
47
Mixing of certain fuel types is permitted per CFM: T or F
True
48
APU Min temp cold soaked start:
- 40 degrees C
49
APU min battery voltage for start:
22 volts
50
APU max number of start attempts:
3 per hour
51
APU Min time between start attempts:
2 minutes
52
APU min time before pneumatic load:
2 minutes
53
APU max ops altitude
FL410
54
APU max starting altitude:
FL370
55
APU max altitude for bleed air:
FL250
56
APU ALT to use bleed air for engine starts:
FL250
57
APU max gen loading _____ KVA to _____:
40, FL410
58
APU max airspeed with door open & APU not running:
220 KTS
59
Ground icing requirements:
Cowl Anti-ice on in icing conditions or when OAT 10 degrees C or less and operating on RWY and/or TWY with snow, ice, slush, or standing water. Wing Anti-ice must be on when: OAT is 5 degrees C or below and visible moisture in any form is present (1sm vis) and/or OAT IS 5 degrees C or below and RWY is comtaimented with slush, snow, or standing water
60
In-flight icing:
Cowl Anti-ice on in icing conditions or ICE is annunciated by the ice detector system. Wing Anti-ice must be on when annunicated by the ice detection system or in icing conditions and IAS is less then 230 KTS
61
Holding in Super-cooled Large Droplet Icing conditions or operating in severe conditions is:
Prohibited
62
Continued operations in areas of super-cooled large droplet is:
Prohibited
63
Max RWY slope is:
+/- 2 degrees
64
Max tailwind component:
10 KTS
65
If cargo is in the cargo compartment the flight must be within ______ minutes of a suitable airport
60
66
Flap speeds:
1 & 8 degrees - 230 KTS
20 degrees- 220 KTS
30 degrees - 185 KTS
45 degrees - 170 KTS
67
Can flaps be used enroute?
No
68
Max altitude for flap extension?
15,000 feet
69
When holding in icing conditions, flaps must be _______ ?
Retracted
70
Max speed for turbulence?
280 KTS, 0.75 MACH
71
Max gear extension?
220 KTS
72
Max gear operational speed?
220 KTS
73
Max gear retract speed?
200 KTS
74
Max tire speed on ground?
195 KTS
75
Max crosswind component?
700 - 27 KTS dry, 15 KTS slippery
| 900 - 22 KTS dry, 15 KTS slippery
76
ADG supplies power to:
ADG bus to AC Ess bus to ESS TRU to ESS BUSS and DC BATT bus ( thru ESS TIE), ACMP 3B, Flaps/slats, pitch trim are available, Stab ch 2
77
ADG deploy speed with no time limit:
Vmo/Mmo
78
Max speed for windshield wiper operations or parked in non-parked position?
250 KTS
79
Maneuvering Limit Load Factors?
Flaps up: -1.0 to 2.5 G
| Flaps down: 0.0 to 2.0 G
80
Max differential pressure is:
8.7 psi
81
Maximum negative differential pressure is:
- 0.5 psi
82
During taxi, takeoff and landing, the pressure differential must not exceed?
0.1 psi
83
The cabin must be completely depressurized prior to -____________ ?
Opening any doors
84
Max single pack operation altitude?
FL250
85
Autopilot use below 600 AGL is PROHIBITED, except?
Precision - 80 feet AGL
Single-engine precision - 110 feet AGL
Non-precision/Visual - 400 feet AGL
86
During RNAV departures and arrivals the autopilot must be -_______ ?
On
87
Using _______ sub mode during appr is not permitted?
DES
88
_________ mode use during VOR approaches is not permitted:
APPR
89
General load altitude limit (feet):
0-41,000 feet
90
Generator Load limitation each main:
40 KVA
91
General APU limitation:
40 KVA
92
TRU LOAD LIMIT:
120 amps
93
CRT display max time (ground) DC power only:
5 minutes
94
Wing and/or cowl anti-ice selection is _________ with the APU as a bleed source in manual mode:
Prohibited
95
Multi-function flight spoilers use Min altitude _______, Min Speed ________?
300 AGL, Vapp + 10 KTS
96
Min Multi-function flight spoilers altitude for stabilized approach:
1000 feet
97
Are thrust reversers approved to be used in flight?
No
98
By _______ KIAS reverse thrust must be reduced to idle?
60
99
Both stall protection systems switches must be _______ for all phases of flight:
ON
100
When on the ground and stationary, the taxi lights must be turned off after ________?
10 minutes
101
FMS is approved for use only during _______ and _____________ phases of flight:
Enroute, terminal, non-precision approach
102
Approaches prohibited using the FMS:
```
ILS
LOC/ LOC BC
VOR
LDA
SDF
MLS
```
103
What does the FMS message "NO APPR" mean when it is displayed on the PDF?
FMS must not be used past the FAF
104
Takeoff is prohibited with _________________ adhering to any critical surface:
Ice, snow, frost, and slush
105
Takeoff is permitted with a maximum of 1/8 inch of frost adhering to ____________ caused by ___________ in the wing:
The underside of the wing, cold-soaked fuel
106
RVSM required equipment?
1 operational autopilot
1 operational Altitude Alerting System
2 Altitude Reporting Transponders, 1 must be operational
2 operational ADC's
107
OAT above ________, delay WSHLD to LOW until after ________?
30 degrees C, takeoff
108
Max cruise MACH number during flight in RSVM airspace is ______?
0.82 MACH
109
Cross bleed start:
BLEED VALVES
Thrust lever Min ______ psi
Min _______ N2
Switch to AUTO
42 psi
80% N2
110
Engine start sequence: too many steps!!!!
Fuel pumps ON, Check boost pump INOP light out
Boost pump light ON, FUEL PUMP ON advisory message comes on
FUEL LO PRESS caution messages out, XFLOW INHIBIT not on
Engine - START, applicable START light on
Engine status - isolation valve opens, both pack valves close
Associated start valve opens, ATS engages,
50% - ATS Disengages, start valve closes, PAC/ISO valves previous
Settings
111
FUEL FEED CHECK VALVE TEST
Fuel pumps (both) OFF, observe FUEL LO PRESS caution on for. On-operating engine
FUEL LO PRESS caution (2 min max) displayed on the non-op engine
Dry motor non-operating engine max 30 seconds
Applicable FUEL LO PRESS caution should be displayed, if not-check valve failed
Fuel pumps (both) ON, L and R BOOST PUMP ON - lights come on
L and R BOOST PUMP INOP lights go out
L and R FUEL PUMP advisory message comes on
Applicable FUEL LO PRESS caution message goes out
112
SE taxi engine bleed
Only associated PACK
113
Bleeds may be transfer to APU when:
BLEED SOURCE - APU
ISOL - OPEN
BLEED VALVES - MANUAL
Automatic bleed operation restored by:
BLEED VALVE - AUTO
ISOL - CLOSED
BLEED SOURCE - BOTH ENG
