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ATR72-500 revised specific > THIRD PARTY DECK unverified > Flashcards

THIRD PARTY DECK unverified Flashcards

(72 cards)

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1
Q

What is the minimum flight crew requirement for the ATR 72-212A?

A

2 PILOTS

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2
Q

What is the maximum operating altitude for the ATR 72-212A?

A

25,000 FT

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3
Q

What are the maneuvering limit load factors for the ATR 72-212A with gear and flaps retracted?

A

+2.5 to -1 G

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4
Q

What are the maneuvering limit load factors for the ATR 72-212A with gear and/or flaps extended?

A

+2 to 0 G

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5
Q

What is the maximum takeoff weight for the ATR 72-212A?

A

49603 LB

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6
Q

What is the maximum landing weight for the ATR 72-212A?

A

49,273 LB

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7
Q

What is the maximum zero fuel weight for the ATR 72-212A?

A

45,194 LB

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8
Q

What is the minimum flight weight for the ATR 72-212A?

A

28,660 LB

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9
Q

What is the maximum operating speed (VMO) for the ATR 72-212A?

A

250 KT

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10
Q

What is the maximum Mach operating speed (MMO) for the ATR 72-212A?

A

0.55

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11
Q

What is the maximum design maneuvering speed (VA) for the ATR 72-212A?

A

175 KT

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12
Q

What is the maximum flaps extended operating speed (VFE) for flaps 15?

A

185 KT

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13
Q

What is the maximum flaps extended operating speed (VFE) for flaps 30?

A

150 KT

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14
Q

What is the maximum landing gear extended operating speed (VLE) for the ATR 72-212A?

A

185 KT

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15
Q

What is the maximum landing gear operating speed (VLO RET) for the ATR 72-212A?

A

160 KT

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16
Q

What is the maximum landing gear operating speed (VLO LOW) for the ATR 72-212A?

A

170 KT

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17
Q

What is the maximum rough air speed (VRA) for the ATR 72-212A?

A

180 KT

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18
Q

What is the maximum wipers operating speed (VWO) for the ATR 72-212A?

A

160 KT

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19
Q

What is the VMCL (CAS) at flaps 15 for the ATR 72-212A?

A

101 KT

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20
Q

What is the VMCL (CAS) at flaps 30 for the ATR 72-212A?

A

105 KT

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21
Q

What is the maximum tire speed for the ATR 72-212A?

A

165 KT (Ground Speed)

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22
Q

What is the tailwind limit for takeoff and landing for the ATR 72-212A?

A

15 KT

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23
Q

What is the maximum demonstrated crosswind for takeoff for the ATR 72-212A?

A

35 KT

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24
Q

What is the maximum demonstrated crosswind for landing with flaps 30° for the ATR 72-212A?

A

35 KT

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25
What is the maximum mean runway slope for the ATR 72-212A?
±2%
26
What is the maximum differential pressure for the ATR 72-212A?
6.35 PSI
27
What is the minimum height for autopilot engagement after takeoff for the ATR 72-212A?
100 FT
28
What is the minimum height for the use of either autopilot or flight director except during takeoff or approach?
1000 FT
29
What is the maximum load for a DC generator in the ATR 72-212A?
400 A
30
What is the maximum load for an ACW generator in the ATR 72-212A?
20 KVA CONTINUOUS 30 KVA 5 MINUTES 40 KVA 5 SECONDS
31
What is the maximum pressure for refueling the ATR 72-212A?
3.5 BARS (50 PSI)
32
What is the total quantity of usable fuel in each tank for the ATR 72-212A?
2500 kg (5510 lb)
33
What is the maximum fuel unbalance for the ATR 72-212A?
1609 LB
34
What is the maximum combined starter running time for the ATR 72-212A?
1 minute 30 seconds
35
What is the minimum oil temperature to ensure inlet strut de-icing for the ATR 72-212A?
45°C
36
What must be done if ground speed exceeds 165 kt for the ATR 72-212A?
All tires must be replaced
37
Is holding with any flaps extended allowed in icing conditions for the ATR 72-212A?
NO
38
What is the maximum time limit for takeoff power setting in the ATR 72-212A?
10 min
39
What is the maximum ITT during takeoff for the ATR 72-212A?
800°C
40
What is the maximum oil pressure range during takeoff for the ATR 72-212A?
55 to 65 PSI
41
What is the maximum oil temperature during takeoff for the ATR 72-212A?
125°C
42
What is the maximum transient time for engine parameters in the ATR 72-212A?
20 s
43
What is the maximum ITT during transient operation for the ATR 72-212A?
840°C
44
What is the maximum time limit for starting the engine in the ATR 72-212A?
90 SECONDS
45
What is the maximum freezing point for JET A fuel?
-40°C
46
What is the maximum freezing point for JET A1 fuel?
-47°C
47
What is the maximum freezing point for RT fuel?
-55°C
48
What is the maximum freezing point for TS-1 fuel?
-60°C
49
What is the maximum freezing point for JP 5 fuel?
-46°C
50
What is the maximum freezing point for JP 8 fuel?
-47°C
51
What is the maximum combined starter running time followed by off time for the ATR 72-212A?
1 minute 30 seconds, followed by 4 minutes off
52
What must be done before passengers boarding/disembarking in the ATR 72-212A?
The tail prop must be installed
53
Is the use of NP settings below 82% in icing conditions allowed for the ATR 72-212A?
No
54
What is the maximum demonstrated crosswind for landing in the ATR 72-212A?
35 KT
55
What should be done if smoke or fumes are detected in the cockpit?
Crew oxygen masks don / 100%
56
What is the maximum altitude for one bleed off operation?
20,000 FT
57
What action should be taken if fire persists after 10 seconds?
AGENT 1 (affected ENG) DISCH ## Footnote This refers to discharging the first fire suppression agent.
58
What action should be taken if fire persists 30 seconds after AGENT 1 DISCH?
AGENT 2 (affected ENG) DISCH ## Footnote This refers to discharging the second fire suppression agent.
59
What should be done in case of ENGINE 1(2) FIRE OR SEVERE MECHANICAL DAMAGE ON GROUND?
Stop aircraft, set parking brake, FTR THEN FUEL S.O., pull fire handle ## Footnote FTR stands for fuel throttle reduction.
60
What steps should be taken if there is a FLAME OUT AT TAKEOFF?
Check AUTOFEATHER, UPTRIM. If no UPTRIM, advance PL 1 + 2 to the ramp. When airborne, set LDG GEAR UP ## Footnote PL stands for power levers.
61
What should be done if icing conditions are present during FLAME OUT AT TAKEOFF?
Maintain FLAPS 15°, set PL (affected eng) FI, FTR THEN FUEL S.O. ## Footnote FI stands for fuel ignition.
62
What should be done if both engines flame out?
PF CAPT, ENG START selector CONT RELIGHT, PL 1+2 FI ## Footnote PF refers to the Pilot Flying.
63
What actions are necessary during an emergency descent?
Crew oxygen masks as required, initiate descent, PL 1+2 FI, CL 1+2 100% OVRD ## Footnote CL refers to the throttle or control lever.
64
What should IAS be during severe icing?
ICING BUG + 30 kt (or ICING BUG if FLAPS 15 extended) ## Footnote Icing bug refers to the indicated airspeed at which icing begins to affect performance.
65
What is the first action to take in case of a stall?
Push control column ## Footnote This action helps to reduce the angle of attack.
66
What should be done if there is an unreliable airspeed indication?
AP/YD OFF, FD STBY, maintain pitch and torque ## Footnote AP refers to autopilot and YD refers to yaw damper.
67
What should be done if there is a FLAPS UNLK before V1?
Abort takeoff ## Footnote V1 is the speed at which the takeoff should no longer be aborted.
68
What is the maximum IAS during a PITCH DISCONNECT?
180 kt ## Footnote This ensures safety during pitch disconnect scenarios.
69
What should be done if ROL, PIT, ATT, HDG cautions appear on EFIS?
Compare BOTH EADI/EHSI AND STBY INSTs to identify affected AHRS ## Footnote EADI stands for Electronic Attitude Director Indicator and EHSI stands for Electronic Horizontal Situation Indicator.
70
What should be done during a PEC 1(2) FAULT below 400 ft RA?
Perform go-around ## Footnote RA stands for Radio Altitude.
71
What action should be taken if ENGINE 1(2) FLAME OUT IN FLIGHT?
Set PL (affected ENG) FI; if NH drops below 30%, CL (affected ENG) FTR THEN FUEL S.O. ## Footnote NH refers to high-pressure turbine speed.
72
What should be done if there are ABNORMAL PARAMETERS DURING START?
CL (affected ENG) FUEL S.O.; ENG START selector OFF & START ABORT ## Footnote ITT refers to Interstage Turbine Temperature.

ATR72-500 revised specific (6 decks)

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