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49 Cards in this Set
- Front
- Back
- 3rd side (hint)
Airplane/Powerplant maximum operating ambient temperature |
+50C or ISA +35C (whichever is lower) |
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Airplane/Powerplant minimum operating temperature |
-54C |
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APU maximum operating ambient temperature |
+50C or ISA +35C (whichever is lower) |
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APU minimum operating ambient temperature |
-54C |
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Maximum operating altitude |
25,000 ASL |
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Maximum operating altitude for takeoff |
10,000 ASL |
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Maximum crosswind component for takeoff and landing (conditions: hard, wet, or dry runway) |
32 kts |
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Maximum ramp weight (MRW) |
65,400 lbs |
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Maximum takeoff weight (MGTOW) |
65,200 lbs |
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Maximum landing weight (MLW) |
62,000 lbs |
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Severe turbulence airspeed |
210 kts |
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Maneuvering speed (Va) |
204 kts |
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Maximum gear operating speed (VLE) |
215 kts |
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Maximum gear operating speed (VLO) |
195 kts |
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Structural landing gear operating speed |
200 kts |
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Define "icing conditions" (on ground) |
Static air temperature (SAT) is 10C 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. |
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Define "icing conditions" (in flight) |
Static air temperature (SAT) is 5C or below and visible moisture is present in any form. Ice accretion on aerodynamic surfaces is not considered to exist at temperature of -40C or below. |
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Flap VMIN, VMAX, and structural speeds for Flaps 0 |
VMIN - 180 kts VMAX - VMO Structural - Not Applicable |
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Flap VMIN, VMAX, and structural speeds for Flaps 5 |
VMIN - 160 kts VMAX - 195 kts Structural - 200 kts |
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Flap VMIN, VMAX, and structural speeds for Flaps 10 |
VMIN - 150 kts VMAX - 175 kts Structural - 181 kts |
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Flap VMIN, VMAX, and structural speeds for Flaps 15 |
VMIN - Solid or Open Bug VMAX - 165 kts Structural - 172 kts |
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Flap VMIN, VMAX, and structural speeds for Flaps 35 |
VMIN - Solid or Open Bug VMAX - 155 kts Structural - 158 kts |
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Maximum Fuel Capacity |
11,724 lbs |
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Maximum Fuel Imbalance - Inflight Only |
600 lbs |
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Tank 1 and Tank 2 Auxiliary Pumps |
On for Takeoff and Landing |
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Engine starter cranking limit |
70 seconds ON, followed by 2 min OFF |
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APU starter cranking limit |
60 seconds ON, followed by 5 min OFF 2nd attempt - 60 seconds ON, followed by MX Req'd. *30 minute minimum from 2nd start attempt before 3rd start attempt (after mx action) |
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Battery load prior to takeoff (main, aux, standby) |
0.1 |
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Min battery temperature prior to takeoff |
-20C |
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Maximum altitude for gear and flaps extended |
15,000 ASL |
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Miscellaneous Engine Operation Limitations (see hint, if needed)
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1. Setting power for takeoff prior to brake release with winds over 8 kts more than 45 deg off the nose is prohibited
2. Inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited 3. Engine intake bypass doors must be open for operation in icing conditions |
Three items.
1. What wind condition prohibits takeoff prior to break release? 2. Inflight operation aft of flight idle gate is allowed (T or F). 3. Bypass doors must be ___ for operation in icing conditions. |
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Air Conditioning Maximum Cabin Differential |
5.95 psi (in-flight) 0.5 psi (takeoff and landing) |
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When must bleed air be off for takeoff and landing? |
1. Windshear is suspected 2. Tailwind exceeds 10 kts 3. For takeoff - when conducted with MTOP selected 4. For landing only - when OAT exceeds 39C (100F) |
Four conditions. Two wind related, one power setting related, on temperature related. |
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What AHRS modes are prohibited for takeoff? |
BASIC mode and DG mode |
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Baggage compartment fire extinguishing operational requirement |
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. |
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What are the flight compartment communication settings when using the flight deck speakers? |
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. |
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APU Operating Requirements and Procedures
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1. APU is only approved for ground operation
2. APU shall be shutdown prior to takeoff 3. APU shall not be operated unattended with passengers on board 4. APU shall not be operated during gravity refueling 5. APU shall not be operated during refueling to maintain steady electrical state (QX SOP only) |
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During autopilot operation the pilot will be. . . . |
. . . seated at the controls with harness secured |
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Coupled autopilot and hand-flown FD approaches are approved for what glide slope angles? |
2.5 deg to 4 deg |
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When must the autopilot be disengaged? |
1. Severe icing 2. Severe or extreme atmospheric turbulence |
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What is the minimum height for autopilot engagement? |
1,000 AFE |
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Autopilot coupled approaches are approved to what minima? |
CAT 1 limits only |
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What flaps configurations are approved for autopilot coupled approaches? |
All flap configurations |
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At what flap setting(s) are autopilot coupled approaches prohibited with one engine inoperative? |
Flaps 35 |
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What is the demonstrated crosswind component for autopilot coupled approaches? |
18 kts |
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Autopilot shall be disengaged at or above 1,000 AFE for: |
1. HGS approaches flown in AIII mode 2. Approaches flown with an inoperative engine 3. Approaches flown with Flap 0 |
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What is the minimum altitude before the autopilot must be disengaged on a coupled approach?
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200 AFE
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Use of VOR without associated DME is prohibited in what mode? |
APP Mode |
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Reduced Np landings are prohibited when: |
1. Landings are accomplished at Solid Bug 2. Performance requires Bleeds OFF 3. Tailwind exceeds 10 kts. 4. Windshear is reported or suspected 5. Runway is contaminated or braking action is less than good 6. Landing performance is derived from the E&A Checklist "Adjusted Landing Speed and Distance Tables" |
Six items - mostly weather and performance related |