General Flashcards by Vladislav Stefanov

Maximum tailwind approved for take-off and landing

10kts

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Maximum slopes approved for take-off and landing

+2%(uphill)

-2%(downhill)

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Maximum approved airport pressure altitude for take-off and/or landing

14500ft

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Maximum speeds vs. altitude

300 KCAS             0-12000 ft
340 KCAS     12000-27860 ft
M 0.85           27860-32160 ft
M 0.885         32160-43500 ft
M 0.86           43500-51000 ft

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Polar navigation is approved, provided:

TRUE heading is selected prior N73 and S60 deg latitude

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Maximum operating altitude

51000 ft

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Maximum operating altitude with yaw damper inoperative

45000 ft

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Maximum operating altitude with single air-conditioning pack operating

48000 ft

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Maximum operating altitude for extending or flying with landing gear extended

20000 ft MSL

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Maximum operating altitude for extending landing flaps (39deg/down) or flying with flaps extended

20000 ft MSL

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Maximum operating altitude for extending flaps to 10 deg or 20 deg, or flying with flaps extended to 10 or 20 degrees

25000 ft MSL

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Minimum control speed, Air

112 KCAS

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Minimum control speed, Landing

110 KCAS

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Minimum control speed, Ground

107 KCAS - see level
86 KCAS - 15000 ft

(Rate 1 kt / 1000 ft)

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Maneuvering speed (Va)

206 KCAS

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Maximum flaps extended speeds - take-off (10deg)

250 KCAS

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Maximum flaps extended speeds - take-off approach (20deg)

220 KCAS

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Maximum extended speeds - Down (39 deg):

170 KCAS

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Maximum landing gear extended speed

250 KCAS / 0.70 Mt

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Maximum landing gear operation speed, normal operation

225 KCAS

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Maximum landing gear operation speed, alternate operation

175 KCAS

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Minimum holding speed

160 KCAS

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Mach trim / electric elevator trim inoperative speed

0.80 Mt

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Turbulence penetration speed

altitude 10000 ft or above - 270 KCAS / 0.80 Mt

- below 10000 ft - 240 KCAS

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Maximum tire speed

195 KCAS

Maximum speed with the emergency stabilizer trim armed, autopilot engaged and a jammed elevator

270 KCAS / 0.80 Mt

Flight load acceleration - flaps up (0 deg)

-1 - 2.5g

Flight load acceleration - flaps 10 or 20 deg

0 - 2.0g

Flight load acceleration - flaps Down (39 deg)

< MAX Landing weight - 0-2.0g | > MAX Landing weight - 0-1.5g

Maximum Zero Fuel Weight

52000 lb

Maximum Ramp Weight

91400 lb

Maximum Take-Off Weight

91000 lb

Maximum Landing Weight

75300 lb

Center of Gravity (ZFW)

Min 37.5% MAC | Max 45.0% MAC

Maximum fuel imbalance for take-off

1000 lb

Maximum fuel imbalance in-flight

2000 lb

The engine will run stable on suction fuel feed (no boost pumps) below:

20000 ft

Maximum Cabin Pressure Differential permitted:

10.48 psi

Maximum Cabin Pressure Differential permitted for take-off and landing

0.3 psi

Internal baggage door should be closed above:

40000 ft

If operating on a single ECS pack the access to the baggage compartment is allowed only at or below:

45000 ft

Time with the internal baggage door open above 40000ft is limited to:

5 minutes

Maximum Mmo with Mach Trim inoperative:

0.80 Mt

Single engine autopilot coupled go-around is:

Not approved

Autopilot minimum engage height:

200 ft

Autopilot minimum disengage height:

- ILS approach - min 60ft | - LNAV/VNAV approach - max 50 ft below MDA

Maximum demonstrated altitude loss in coupled Go-Around:

60 ft

Use of autothrottle during single engine approach is:

Prohibited

When Standby Electrical Power System (HMG) is in operation, speed brakes may be used, provided:

Operation is slow (approximately 3 seconds for full range movement)

Speed brakes extension with flaps at 39 deg or with landing gear extended in flight:

Not approved

Usable fuel capacity:

41300 lb

Red "Fuel Tank Temperature" CAS message, when:

- Fuel tank temperature of +54deg C or greater; or | - Fuel tank temperature is -37 deg C or less.

Amber "Fuel Tank Temperature" CAS message is displayed when

Fuel tank temperatures are -35 deg C to -36 deg C

Maximum hydraulic reservoir quantities (pressurized) are

- left hydraulic system: 4.8 gal | - right hydraulic system: 1.6 gal

Left and Right hydraulic system accumulator pre-charge is

1200 psi at 21 deg C, +/- 25 psi for each 5 deg C difference in temperature from 21 deg C

Automatic anti-ice is inhibited above:

35000 ft

Holding in icing condition is limited to ....... Flaps only.

0 deg (up)

All RA and TA aural messages (TCAS) are inhibited at a radio altitude of

Less than 500 ft +/- 100 ft climbing and descending.

The APU may be used for starter-assisted main engine starts below

30000 ft

Maximum permissible APU EGT:

- Start: 1050 deg C, | - Running: 732 deg C.

Maximum APU rotor speed

106%

APU starter limitations, when powered by airplane batteries

- max 3 consecutive start attempts; | - 1 hour cool down period.

APU starter limitations, when powered by an external DC cart

- max 3 consecutive start attempts; - 15 minutes cool down between start attempts; - 1 hour cool down perid.

The APU generator can deliver 100% (40 KVA) electrical power on the ground or in flight (altitude?)

Sea level to 45000 ft

APU is guaranteed to start at or below

39000 ft (possible start from 39000 ft to 43000 ft)

APU operations limitation (altitude)

45000 ft

Max TGT during powerplant ground start

700 deg C (momentary)

Max TGT during airstart (relight)

850 deg C (momentary)

Max TGT (powerplant) during take-off

900 deg C (5 min - all engines, 10 min - single engine)

Max continuous powerplant TGT

860 deg C (unrestricted)

Max powerplant overspeed

Max LP 101.5% Max HP 99.8% (20 sec)

Max powerplant TGT overtemperature

905 deg C (20 sec)

Max LP reverse thrust

Max LP 70.0% (30 sec) | Above 60 kts IAS

Maximum crosswind component for ground start

30 kts

Maximum tailwind component for engine ground start

20 kts

Prefered method of engine airstart

1. Automatic | 2. Manual starter assist / Windmill airstart

Take-off in alternate control mode:

Prohibited

Minimum engine fuel temperature

-40 deg C

Maximum engine fuel temperature

Unrestricted: +140 deg C. | Transient (15 min): +165 deg C.

Maximum fuel tank temperature

+54 deg C

Limitation on continuous (airstart) ignition

No limitation on duty cycle time

Minimum oil inlet temperature for starting

-30 deg C

Minimum oil inlet temperature for take-off power

+20 deg C

Maximum oil inlet temperature

+160 deg C

The engine must be shut down when oil pressure drops below

25 psi

Minimum engine oil pressure for power setting below 72.3 % HP

- for take-off - 35 psi; | - to complete the flight - 25 psi.

Minimum engine oil pressure with power setting above 90.0 % HP

- for take-off - 45 psi; | - to complete the flight - 35 psi.

Engine starter duty cycle:

- 3 start cycles with a max 3 min per start cycle; - 15 seconds delay between start cycles; - 15 min delay after 3 start cycles

The starter may be reengaged at HP RPM speeds up to

42% HP RPM