Limitations Flashcards
(117 cards)
1
Q
max ramp weight
A
85800
2
Q
Max takeoff weight
A
85500
3
Q
Max Landing weight
A
74900
4
Q
max zero fuel
A
69,800
5
Q
fwd cargo weight
A
3306
6
Q
aft cargo weight
A
2535
7
Q
max headwind cat II
A
25 knots
8
Q
max crosswind dry
A
35 (Mark said 38)
9
Q
max crosswind less than 4000 and 3/4
A
15 (e)
10
Q
max crosswind takeoff (wet)
A
30 (e)
11
Q
max runway slope
A
+/- 2°
12
Q
max maneuvering load limits flaps up
A
-1.0 to +2.5
13
Q
Max maneuvering load limit flaps down
A
-0 to +2.0
14
Q
maximum operating altitude
A
41,000’
15
Q
Max T/O and LDG alt
A
8000
16
Q
MAX SAT FOR T/O LDG/ GND START
A
52C
17
Q
max alt with flaps extended
A
20,000
18
Q
max operating latitude
A
78N (E)
78S (E)
19
Q
Min SAT for T/O LDG and GND Start
A
-40C
20
Q
Max Crosswind Code 6 breaking action (-)
A
38 knots
21
Q
Max Crosswind Code 5 breaking action (good)
A
31
22
Q
Max Crosswind Code 4 breaking action (good to medium)
A
20
23
Q
Max Crosswind Code 3 breaking action (Medium)
A
15
24
Q
Max Crosswind Code 2 breaking action (medium to poor))
A
12
25
Max Crosswind Code 1 breaking action (Poor)
8
26
What are all winds based limits based on
Peak Gust Value
27
Min operating speed limit
Intentional operation below onset of stall warning (stick shaker) is prohibited unless specifically authorized for flight test.
28
Max Opp Airspeed
320
29
Max Mach
.82
30
Max RAT airspeed
Vmo Mmo
31
Turbulent Airspeed below 10,000
250
32
Turbulent Airspeed above 10,000
270/.76M
33
Tire Limit Groundspeed
195 knots
34
Max speed windshield wiper operation
"Hi"
-Jason Vandergriff (hahaha)
(250 knots)
35
Max speed windshield wiper failed not in non-parked position
320KIAS
36
MAX SPEED FLIGHT DECK WINDOW OPEN
160 KIAS
37
MAX GEAR (Retraction, extension, extended)
250 KIAS
38
Flaps 1 MAX SPEED
230
39
Flaps 2 MAX SPEED
215
40
Flaps 3 MAX SPEED
200
41
Flaps 4 MAX SPEED
180
42
Flaps 5 MAX SPEED
180
43
Flaps FULL MAX SPEED
165
44
Min Controllable Speed
Vapp +10, refer to QRH
45
Design Maneuvering Speed
Full application of rudder and aileron controls, as well as maneuvers that involve angles of attach near stall must be confined to speeds at or below 240 KIAS
46
Definition of Ice
OAT or TAT (in flight) of 10C or below AND:
- Visible moisture (precipitation or visibility of less than 1 mile)
- operating on surfaces covered in snow, ice, slush, or standing water
47
Engine and Wind Anti-Ice temp limit in Auto
There is no temperature limit in the AUTO position
48
Engine and Wing Anti-ice operations
must be set to "ALL" when 10C or below and icing conditions exist
49
Approved Fuels
Jet-A and A-1
JP-8
QAV-1
When using JET-A with a temp below -30C, the fuel temp prior to flight must be verified to be above -29C
50
Fuel density
6.77 lbs/gal
51
Max fuel Capacity
10,392lbs per tank (20,734 total usable)
| 75lbs unusable fuel per tank
52
Min Fuel Temp
-37C
53
Max Fuel Imbalance
800lbs
54
Crossfeed Operation for Takeoff and Landing
Crossfeed OFF for Takeoff and Landing
55
APU Start Limit 1st/2nd cycle
60 seconds off per start
56
APU Start Limit 3rd cycle
5 minutes off
57
APU MIN/MAX temp for operation
-54C to ISA+35C
58
MAX APU START ALT
30,000
59
MAX APU OPERATION (ELECTRICAL)
33000
60
MAX APU OPERATION (BLEED)
15,000
61
MAX APU OPERATION (ENGINE START)
21,000
62
MAX APU ROTOR SPEED
108%
63
MAX APU EGT START
1032C
64
MAX APU EGT CONTINUOUS OPERATION
717
65
MAX SINGLE PACK ALT
31,000
66
MAX DIFF PRESSURE (UP TO 37,000)
7.8
67
MAX DIFF PRESSURE (ABOVE 37,000)
8.3
68
MAX DIFF OVERPRESSURE
8.7
69
MAX NEG DIFF PRESSURE
-0.5
70
MAX DIFF PRESSURE FOR T/O AND LDG
.2
71
OZONE CONCENTRATION LIMITS
REFER TO TABLE IN LIMITATIONS SECTION OF AOM 1
72
BRAKE TEMP limit for Takeoff
DO NOT TAKE OFF WITH BRAKE TEMPS IN THE AMBER.
73
FLAPS ENROUTE
ENROUTE USE OF FLAPS/SLATS IS PROHIBITED
74
MAX ALTITUDE WITH FLAPS/SLATS EXTENDED
20,000
75
AUTOPILOT MIN ALT
TAKEOFF- 400'
| LANDING- 50'
76
TCAS DEVIATIONS
DEVIATIONS FROM ATC CLEARANCES ARE AUTHORIZED TO COMPLY WITH TCAS RA
77
TCAS DEVIATIONS BASED SOLELY ON NAV DISPLAY
MANEUVERS MUST **NOT** BE BASED SOLELY ON INFORMATION PRESENTED ON NAV DISPLAY
78
IS COMPLIANCE WITH A TCAS RA REQUIRED
YES, UNLESS PIC DETERMINES DOING SO WOULD JEOPARDIZE SAFE OPERATION OF FLIGHT
79
CAN YOU NAVIGATE WITH EGPWS DISPLAY
NO, NAV MUST NOT BE PREDICATED ON EGPWS DISPLAY
80
ARE DEVIATIONS FROM ATC CLEARANCES PERMITTED TO COMPLY WITH EGPWS WARNINGS?
YES
81
WHEN SHOULD THE PILOT MANUALLY INHIBIT TERRAIN/OBSTACLE AWARENESS ALERTING?
WITHIN 15 MILES ON APPROACH TO AN AIRPORT NOT IN THE EGPWS AIRPORT DATABASE
82
HOW WILL CREWS KNOW AN AIRPORT IN NOT IN THE EGPWS DATABASE
IT WILL BE NOTED IN THE F4 MESSAGES OF THE RELEASE
83
BANK ANGLES ON FMS LNAV
THERE IS NOT AUTOMATIC BANK ANGLE PROTECTION FOR SINGLE ENGINE OPERATIONS WHEN IN FMS LNAV
84
TAS TAT AND SAT ARE ONLY VALID ABOVE WHAT AIRSPEED?
60 KNOTS
85
WHAT TYPE OF ENGINE DO WE HAVE
GE CF34-8E5
86
WHAT INFORMATION IS USED TO DETERMINE WHETHER WE ARE WITHIN ENGINE LIMITATIONS
THE MARKINGS ON THE EICAS
87
MAX AND MIN ENGINE LIMITATIONS ARE DEPICTED ON THE EICAS HOW?
IN RED
88
ENGINE CAUTION RANGE IS DEPICTED ON THE EICAS HOW?
AMBER
89
ENGINE NORMAL OPERATING RANGE IS DEPICTED ON THE EICAS HOW?
GREEN
90
NORMAL AND MAXIMUM TAKEOFF AND GO AROUND TEMPERATURES ARE LIMITED TO _____MINUTES DURING A ____ MINUTE PERIOD
5, 10
91
NORMAL TAKEOFF AND GO AROUND TEMP/TIME LIMIT
965 (2 MIN)
| 949 (3MIN)
92
MAX TAKEOFF AND GO AROUND TEMP/TIME LIMIT DURING WINDSHEAR OR OEI WITH THRUST LEVERS IN TOGA
1006 (2 MIN)
| 990 (3 MIN)
93
MAX CONTINUOUS ENGINE TEMP LIMIT
960
94
ENGINE START TEMP LIMIT
815
95
ENGINE N1 MAX RPM
100% N1
96
ENGINE N2 MAX RPM
100% N2
97
MAX ENGINE OIL TEMP (TIME)
163C FOR 15 MINUTES
98
MAX ENGINE OIL PRESSURE (TIME)
95PSI FOR 25 MIN
99
ENGINE START CYCLE LIMIT GROUND (1ST AND SECOND)
90 SEC ON, 10 SECONDS OFF
100
ENGINE START CYCLE LIMIT GROUND (3RD-5TH)
90 SEC ON, 5 MIN OFF
101
ENGINE START CYCLE LIMIT FLIGHT (1ST AND 2ND)
120 SEC ON ON, 10 SEC OFF
102
ENGINE START CYCLE LIMIT FLIGHT (3RD-5TH))
120 SEC ON, 5 MIN OFF
103
ENGINE MOTORING LIMIT (AIR AND GND) (1ST)
90 SEC ON, 5 MIN OFF
104
ENGINE MOTORING LIMIT (AIR AND GND) (2ND-5TH)
30 SEC ON, 5 MIN OFF
105
AFTER 5 MOTORINGS, HOW MUCH TIME BEFORE CYCLE CAN BE REPEATED
15 MIN
106
CAN WE GO AROUND AFTER DEPLOYING REVERSER
NO
107
CAN WE BACK UP WITH REVERSE THRUST
NO
108
CAN WE USE REVERSE THRUST IN THE AIR
NO
109
MIN SPEED FOR FULL REVERSE THRUST
60 KIAS
110
FUEL CIRCUIT BREAKER RESET (EVER?)
NO: "RESETTING A FUEL BOOST PUMP, OR FUEL INDICATING SYSTEM CIRCUIT BREAKER IS PROHIBITED."
"THERE IS NO OPERATIONAL SITUATION IN WHICH IT WOULD BE NECESSARY TO RESET A TRIPPED FUEL BOOST PUMP OR FUEL INDICATING SYSTEM CIRCUIT BREAKER"
111
MIN BATTERY TEMP FOR APU STARTING
-20C, THIS DOES NOT PROHIBIT STARTING THE APU VIA DC POWER IF A DC GPU IS AVAILABLE AND UTILIZED
112
WHEN MUST THE FLIGHT DECK DOOR ACCESS SYSTEM BE TESTED
PRIOR TO THE FIRST FLIGHT OF THE DAY
113
WHEN MUST THE ESCAPE SLIDES BE ARMED?
WHENEVER OCCUPANTS ARE IN THE CABIN, THE ESCAPE SLIDE MUST BE ARMED FOR TAXI, TAKEOFF, AND LANDING.
FOR DOOR ARMING REQUIREMENTS ON FERRY, TRAINING, AND CHARTER FLIGHTS, REFER TO FM-1 (E)
114
ALTIMETER TOLERANCES (STBY ALT)
STBY ALTIMETERS DO NOT MEET ACCURACY REQUIREMENTS OF RVSM
115
MAX ALLOWABLE IN FLIGHT DIFFERENCE BETWEEN CAPT AND FO ALTITUDE DISPLAY FOR RVSM?
200 FEET
116
length
width
height
104
94
32
117
certified operations
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day/night
VFR/IFR
ICING
CAT I
CAT II
RVSM
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