Limitations Flashcards
1
Q
The airplane is certified in the transport category for day and night operations in the following conditions:
A
- VFR and IFR
- Landings with approach path angles no greater than 3.5°
- Flight in icing conditions up to FL350
2
Q
Maximum operating altitude
A
*41,000 feet
3
Q
Maximum airport pressure altitude for takeoff and landing?
A
*8,000 feet
4
Q
Crosswind limit for normal takeoff for airport elevations 7,000 feet MSL or below?
A
*30 Knots
5
Q
Crosswind limit for normal takeoff for airport elevations above 7,000 feet MSL?
A
*22 Knots
6
Q
Maximum tailwind component approved for takeoff and landing?
A
10 knots, or as restricted by Delta Company Pages
7
Q
Maximum crosswind component for engine start and ice shedding?
A
43 knots
8
Q
Maximum tailwind component for engine start and ice shedding?
A
18 knots
9
Q
Maneuver Limit Load Factors
Flaps retracted?
A
-1.0 to +2.5 G
10
Q
Maneuver Limit Load Factors
Flaps extended?
A
0 to +2.0 G
11
Q
Maximum ambient temperature approved for takeoff and landing is?
A
52.5°C (126.5°F)
12
Q
Minimum ambient temperature approved for takeoff and landing is?
A
-54°C (-65°F).
13
Q
Maximum ramp weight:
A220-100?
A
A220-100= 135,000 pounds
14
Q
Maximum ramp weight
A220-300?
A
A220-300=150,000 pounds
15
Q
Maximum takeoff weight A220-100?
A
134,000 pounds
16
Q
Maximum takeoff weight A220-300?
A
149,000 pounds
17
Q
Maximum landing weight A220-100?
A
115,500 pounds
18
Q
Maximum landing weight A220-300?
A
127,500 pounds
19
Q
Maximum zero fuel weight A220-100?
A
111,000 pounds
20
Q
Maximum zero fuel weight A220-300?
A
121,500 pounds
21
Q
Minimum flight weight A220-100?
A
77,000 pounds
22
Q
Minimum flight weight A220-300?
A
80,000 pounds
23
Q
Turbulence Penetration Speed
At or below 10,000 feet?
A
maintain 250 KIAS
24
Q
Turbulence Penetration Speed
Above 10,000 feet?
A
maintain 280 KIAS or 0.75 Mach, whichever is lower
25
Windshield Wiper Speed
| The maximum speed for operating windshield wipers is?
250 KIAS.
26
The tire limit speed is?
195 kts ground speed
27
Air Conditioning, Bleed, and Pressurization
The maximum positive differential pressure is?
8.8 psid.
28
Air Conditioning, Bleed, and Pressurization
The maximum negative differential pressure is?
-0.5 psid.
29
Air Conditioning, Bleed, and Pressurization
During initial landing (at touchdown), the pressure differential must not exceed?
1.0 psid.
30
Except for de-icing operations, all passenger and service doors should not be closed for more than ________ minutes when passengers are on board, the PACKs are OFF, and there is no ground conditioned air?
15 minutes
31
When OAT is above 40°C (104°F), operation without ECS or external cooling is limited to ________ minutes?
30
32
A220-300 PACK OFF takeoff is _________?
prohibited
33
The maximum allowable altimeter reading differences for RVSM operations are:
Captain or F/O and Field Elevation?
75 feet
34
The maximum allowable altimeter reading differences for RVSM operations are:
Captain and F/O In Flight?
200 feet
35
Autoflight
The minimum altitude for engagement of the autopilot is?
400 ft AGL
36
Autoflight
The minimum altitude for use of the autopilot is __________ ,unless using autoland.
80 ft AGL
37
Autoflight
During an approach and landing with autothrottle engaged, the approach speed must be increased by _______ ?
5 kts
38
Automatic Landing
| Maximum reported HEADWIND component to initiate approach and land using autoland?
25 knots headwind
39
Automatic Landing
| Maximum reported CROSSWIND component to initiate approach and land using autoland?
15 knots crosswind
40
Automatic Landing
| Maximum reported TAILWIND component to initiate approach and land using autoland?
10 knots tailwind
41
The maximum runway slope is ______ % upslope?
0.8% upslope
42
The maximum runway slope is _______% downslope.
1.0% downslope.
43
The minimum runway width is?
148 feet
44
The maximum glideslope angle is?
3.25°
45
The minimum glideslope angle is?
2.5°
46
Autoland is prohibited with the _____________ switchlight selected on?
AURAL WARN INHIB
47
Electrical
| Maximum AC generator load must not exceed __________ continuous
75 kVA
48
Electrical
The maximum permissible continuous load on TRU 1 and TRU 2 is ________?
350 amp
49
Electrical
The maximum permissible continuous load on TRU 3 is __________?
225 amp
50
APU
The minimum oil temperature for an APU start is _________?
-40°C.
51
APU
Maximum number of start attempts in 1 hour?
3 starts/start attempts with a 2 minute delay between start attempts.
52
APU
The altitude limit for APU bleed air extraction is __________?
23,000 ft.
53
If MCT is inadvertently selected above _________ , contact the MCC and make a logbook entry.
FL 290
54
Engine Start
After 3 start attempts, or after 4 minutes continuous cranking, a __________ cooling period is required.
30 minute
55
Engine Start
Do not engage the starter on ground if indicated N2 rpm exceeds ________%?
20%.
56
Thrust Reversers
Go-around is _________ after deployment of the thrust reversers?
prohibited
57
Derated and reduced engine thrust (FLEX) takeoffs are ___________ with the autothrottle system disengaged or inoperative.
not permitted
58
The engine must be operated at, or near idle for at least ____________ (cumulative) before shutdown?
3 minutes
59
Flight Controls
Maximum altitude with slats/flaps extended is ____________?
20,000 ft?
60
Flight Controls
Do not use flight spoilers below ________ feet AFE.
1000 feet AFE
61
Flight Controls
Minimum speed with flight spoilers manually extended is ____________?
VREF + 10 KIAS
62
Flight Controls
Use of MAX spoilers is __________ except in an emergency
prohibited
63
Fuel System
| The maximum permissible fuel imbalance between the contents of the left and right main tank is _______ lbs.
800 lbs
64
Fuel System
| Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is ___________?
not usable
65
Fuel System
The minimum fuel quantity for go-around is _______ lb per wing (with the aircraft level) and at a maximum aircraft climb attitude of ________° nose up.
* 975 lbs
| * 10°
66
Fuel System
Maximum bulk fuel temperature for starting and operating is __________°C?
52.5°C
67
Takeoff with bulk fuel temperature indications below_________°C is prohibited?
-37°C
68
Manual transfer and gravity crossflow must be_________ for takeoff.
off
69
Operation of the APU in an unattended mode is prohibited if either wing tank quantity is greater than _________ lbs.
6225 lbs
70
Max Usable Fuel Load
Left main tank or Right main tank A220-100?
6,775 pounds
71
Max Usable Fuel Load
Left main tank or Right main tank A220-300?
6,725 pounds
72
Max Usable Fuel Load
Center tank A220-100?
25,300 pounds
73
Max Usable Fuel Load
Center tank A220-300?
24,900 pounds
74
Max total Usable Fuel Load A220-100?
38,850 pounds
75
Max total Usable Fuel Load A220-300?
38,350 pounds
76
Fuel system
When operating on ground, the left engine must be started first if either wing tank fuel quantity is greater than ________ lbs.
6225 lbs
77
Fuel System
When operating on ground a manual fuel transfer must be done from the affected wing to the center tank to reduce affected wing quantity to less than 6225 lbs when:
* Either wing tank fuel quantity is greater than _______ lbs, and
* Center tank fuel quantity is less than _________ lbs
* 6225 lbs
| * 23,525 lbs
78
Landing Gear and Brakes
The maximum speed with landing gear extended is ________ KIAS
250 KIAS
79
Landing Gear and Brakes
BRAKE TEMP indications must be _______ prior to takeoff.
GREEN
80
Terrain Awareness Warning System
To avoid giving unwanted alerts, the TAWS, TERR switch must be selected to INHIB for takeoff or landing within _________ NM of an airport not contained in the TAWS database.
15 NM
81
Flight Management, Navigation
Use of the FPLN UPLINK function in flight. Any REQUEST PENDING must be __________ before takeoff.
cleared
82
Flight Management, Navigation
Use of the FMS as a primary navigation source beyond the FAF for ILS, LOC, LOC-BC, LDA, SDF and IGS approaches is ____________?
Prohibited
83
Flight Management, Navigation
Localizer approaches must be flown with ________ mode selected before the final approach fix (FAF).
NAV
84
Flight Management, Navigation
MAN SPD must be set and used when flying ________ in the final landing configuration.
VAPP
85
Engine Indications
Max takeoff Max EGT?
Max time limit?
1054°C
* 5 min time limit ** Time limit may be extended to 10 minutes for one-engine-inoperative
86
Engine Indications
Max continuous Max EGT?
* 1006°C
| * 1016°C (FADEC 2.11)
87
Engine Indications
Reverse thrust Max EGT?
1054°C
88
Engine Indications
Start Max EGT?
1054°C
89
Engine Indications
Oil Press Min/Max?
50.3/175.3 psi
90
Crosswind limit for the A220-100 for landing including gusts?
35 knots
91
Crosswind limit for the A220-300 for landing including gusts?
29 knots
