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0
Q

What is the airplane minimum ambient temperature limit?

A

-54*C

FSM 1.1.2

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1
Q

What is the airplane maximum ambient temperature limit?

A

+50C or ISA + 35C, whichever is lower.

FSM 1.1.2

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2
Q

What is the maximum operating altitude?

A

25,000 ft ASL

FSM 1.1.2

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3
Q

What is the maximum operating altitude for takeoff?

A

10,000 ft ASL

FSM 1.1.2

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4
Q

What is the maximum speed for extension of the flaps to 5*?

A

195 KIAS

FSM 1.3.2

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5
Q

What is the maximum speed for extension of the flaps to 10*?

A

175 KIAS

FSM 1.3.2

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6
Q

What is the maximum speed for extension of the flaps to 15*?

A

165 KIAS

FSM 1.3.2

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7
Q

What is the maximum speed for extension of the flaps to 35*?

A

155 KIAS

FSM 1.3.2

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8
Q

What is the Landing Gear Operating Speed (VLO)?

Maximum speed at which it is safe to extend or retract the landing gear

A

195 KIAS

FSM 1.3.2

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9
Q

What is the Landing Gear Extended Speed (VLE)?

The maximum speed with the landing gear extended, doors closed

A

215 KIAS

FSM 1.3.2

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10
Q

What is the maximum airspeed for flight in severe turbulence?

A

210 KIAS

FSM 1.3.2

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11
Q

What is Maneuvering Speed?

A

204 KIAS

FSM 1.3.2

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12
Q

What is the maximum STRUCTURAL Landing Gear Operating Speed (VLO)?

A

200 KIAS

FSM 1.3.3

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13
Q

What is the engine maximum ambient temperature limit?

A

+50C or ISA +35C, whichever is lower.

FSM 1.4.1

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14
Q

What is the engine minimum ambient temperature limit?

A

-54*C

FSM 1.4.1

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15
Q

What is the definition of icing conditions on the ground?

taxi and takeoff roll to the point of lift-off

A

SAT is 10*C or below when precipitation in any form is present,
or fog with visibility of one mile or less;
also when operating on ramps, taxiways, or runways where surface snow, ice, slush, or standing water may be ingested by the engines or freeze on engines, nacelles, or engine sensor probes. FSM 1.5.1

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16
Q

What is the definition of icing conditions in flight?

after lift-off to landing

A

SAT is 5C or below and visible moisture is present in any form.
Ice accretion on aerodynamic surfaces is not considered to exist at temperatures of -40C or below.

FSM 1.5.1

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17
Q

Below what temperature is ice accretion on aerodynamic surfaces not considered to exist?

A

-40*C

FSM 1.5.1

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18
Q

What are the Engine Starter Cranking Limits?

A
  1. 70 seconds on, 2 minutes off.
  2. 70 seconds on, 2 minutes off.
  3. 70 seconds on, 30 minutes off.

FSM 1.4.6

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19
Q

What is the maximum crosswind component for takeoff or landing on a hard, dry or wet runway?

A

32 knots

FSM 1.6.1

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20
Q

What is the maximum tailwind component for takeoff?

A

20 knots

FSM 1.6.1

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21
Q

What is the minimum airspeed in severe icing conditions?

A

200 KIAS

FSM 1.3.1

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22
Q

What is the configuration for holding?

A

200 KIAS and clean (gear up, flaps 0*)

FSM 3.14.2

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23
Q

What is the maximum fuel imbalance between contents of main fuel tanks?

A

600 lbs (this is an inflight limitation only).

FSM 1.7.1

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24
When are Tank 1 and Tank 2 auxiliary pumps required to be on?
For takeoff and landing. FSM 1.7.1
25
The engine intake bypass doors shall be open in what condition?
They shall be open for engine operation in icing conditions. FSM 1.5.1
26
What is the maximum loadmeter reading for the Standby battery, Auxiliary battery and Main battery for takeoff?
0.1 FSM 1.8.1
27
What is the minimum battery temperature for takeoff?
-20*C FSM 1.8.1
28
What is the maximum altitude with the landing gear and/or flaps extended?
15,000 ft. FSM 1.8.1
29
What is the Takeoff Power Setting Limitation?
Setting takeoff power prior to brake release, with the nose of the airplane more than 45* out of wind, is prohibited for wind speeds greater than 8 knots. FSM 1.8.1
30
The use of MTOP (Max Takeoff Power) for takeoff is limited to how many minutes?
10 minutes. FSM 1.8.1
31
What are the Engine Airborne Operating Limitations?
Inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited. FSM 1.8.1
32
After exiting icing conditions, when is the aircraft considered aerodynamically clean?
The aircraft can only be considered aerodynamically clean when all ice is removed from the visible leading edges and wingtips. FSM 1.5.2
33
What is the maximum tire speed?
182 knots groundspeed. FSM 1.3.2
34
When are reduced NP landings prohibited?
Landings are accomplished at the Solid Bug - VREF (ICE). Performance requires Bleeds OFF. Tailwind component exceeds 10 knots. Windshear is reported or suspected. Runway is contaminated or braking action is less than good. When the landing performance is derived from an E/A Checklist. FSM 1.4.6
35
When are reduced torque takeoffs prohibited?
On IAFD (Initial Aircraft Flight of the Day). With a tailwind. If Windshear is present or suspected. On a contaminated runway. If deice/anti-ice fluids are applied to the aircraft. If Icing Conditions exist below acceleration height. FSM 1.4.6
36
What is the Maximum cabin pressure differential limit?
5.95 psi FSM 1.8.1
37
What is the Maximum cabin pressure differential limit during takeoff and landing?
0.5 psi FSM 1.8.1
38
What is the NORMAL cabin pressure differential limit?
5.46 +/- 0.1 psi FSM 1.8.1
39
When must the Bleed Air be off for Takeoff?
Tailwind component exceeds 10 knots Takeoff is conducted with maximum takeoff power (MTOP) selected Windshear is suspected (QX) FSM 1.8.2
40
When must the Bleed Air be off for Landing?
Tailwind component exceeds 10 knots Reported outside air temperature (OAT) exceeds 39*C (100*F) Windshear is suspected (QX) FSM 1.8.2
41
What is the AHRS (Attitude and Heading Reference System) limitation for takeoff?
Takeoff in BASIC mode is prohibited. Takeoff in DG mode is prohibited. FSM 1.8.2
42
What is the limitation regarding the Baggage Compartment Fire Extinguishing?
Unless the forward and aft baggage compartments are empty, the airplane shall not be operated farther than one hour flying time from a suitable airport for landing. FSM 1.8.3
43
What is the limitation regarding the Flight Compartment Communication?
HOT MIC select switches on the Captain and First Officer ARCDU shall be OFF, and the INT/RAD switch on the observer's Audio Control Panel shall be centered, when using the flightdeck speakers. FSM 1.8.3
44
What are the APU ambient temperature limits?
Upper: +50*C or ISA +35*C, whichever is lower Lower: -54*C Note: Prior to start, at temperatures below -35*C, the APU must be preheated in accordance with applicable maintenance procedures. FSM 1.8.3, and Bulletin 13-13
45
Are there any restrictions to operating the APU with passengers on board?
Yes, the APU must be attended. FSM 1.8.3
46
Is it permitted to operate the APU while gravity (over-wing) refueling?
No. FSM 1.8.3
47
Can we operate the APU during pressure refueling?
Yes (evidently there was an earlier prohibition on this, and has since been removed) FSM 1.8.3
48
The APU is approved for what kind of operations?
GROUND OPERATIONS ONLY. FSM 1.8.3
49
When does the APU need to be shutdown?
The APU shall be shutdown prior to takeoff. FSM 1.8.3
50
Can the APU be started during refueling?
No. To maintain steady electrical state, the APU shall not be started during refueling. FSM 1.8.3
51
What are the APU Starter Cranking Limits?
1. 60 seconds on 5 minutes off 2. 60 seconds on Maintenance action required FSM 1.8.3
52
What is a limitation regarding the APU Bleed Air?
The APU Bleed Air shall be selected off when the aircraft is being deiced/anti-iced. (QX) FSM 1.8.3
53
Can the APU be started during pressure refueling?
No. FSM 1.8.3, FOM 7.2.4
54
Use of VOR without associated DME is prohibited in which mode?
APP (Approach) mode. FSM 1.8.4
55
What are the 5 limitations regarding the Autopilot?
~ During autopilot operation, the pilot shall be seated at the controls with harness secured. ~ Autopilot (coupled) and Flight Director (manual) approaches are approved from a nominal glideslope angle of 2.5* to a max of 4*. ~ AFCS is approved for autopilot coupled approaches to CAT 1 limits only. ~ Autopilot coupled approaches are approved for all flap configurations. (However, use of Flaps 35*, autopilot coupled is prohibited with one engine inoperative). ~ Autopilot coupled approaches have been demonstrated in crosswind components up to 18 knots. This is not considered limiting. FSM 1.8.4
56
What is the minimum height for autopilot engagement?
After takeoff or go-around, the minimum height for autopilot engagement is 1,000 feet AFE. FSM 1.8.4
57
When shall the autopilot be disengaged?
~ The autopilot shall be disengaged at or above 1,000 feet AFE for: - HGS approaches flown in AIII mode - Approaches flown with an inoperative engine - Approaches flown with Flap 0* ~ For coupled approaches, the autopilot shall be disengaged at or above 200 feet AFE. ~ Autopilot shall be disengaged in severe icing. ~ Autopilot shall be disengaged in severe or extreme atmospheric turbulence. FSM 1.8.4
58
What is the definition of a wet runway?
Shiny surface, less than 1/8" water covering 100% of runway. (If there are dry spots showing on a drying runway with no standing water, the runway is not considered to be wet). FSM. 4.3.9
59
What is the definition of a contaminated runway?
A runway where more than 25% of the runway length, within the width being used, is covered by standing water or slush more than 1/8" deep, or that has an accumulation of snow or ice. A runway may also be considered contaminated with less than 25% coverage if the contaminant is located prior to the midpoint of the runway. FSM 4.3.9
60
What is the definition of a dry runway?
A runway that is neither wet nor contaminated. FSM 4.3.9
61
What items are on the IAC (Immediate Action Card)?
Fire / Smoke: Engine Fire/Fail (+Eng Oil Press / FADEC Fail Warn) APU Fire Aircraft Fire / Smoke Smoke Evacuation Emergency: Cabin Press Warning / Loss of Pressurization Emergency Descent Emergency Briefing Emergency Landing Engine Shutdown on Ground Emergency Evacuation (Others) Take Off Abort Uncommanded Roll Prop Ground Range Lights Cycling

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