General Flashcards
Maximum tailwind approved for take-off and landing
10kts
Maximum slopes approved for take-off and landing
+2%(uphill)
-2%(downhill)
Maximum approved airport pressure altitude for take-off and/or landing
14500ft
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
Polar navigation is approved, provided:
TRUE heading is selected prior N73 and S60 deg latitude
Maximum operating altitude
51000 ft
Maximum operating altitude with yaw damper inoperative
45000 ft
Maximum operating altitude with single air-conditioning pack operating
48000 ft
Maximum operating altitude for extending or flying with landing gear extended
20000 ft MSL
Maximum operating altitude for extending landing flaps (39deg/down) or flying with flaps extended
20000 ft MSL
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
Minimum control speed, Air
112 KCAS
Minimum control speed, Landing
110 KCAS
Minimum control speed, Ground
107 KCAS - see level
86 KCAS - 15000 ft
(Rate 1 kt / 1000 ft)
Maneuvering speed (Va)
206 KCAS
Maximum flaps extended speeds - take-off (10deg)
250 KCAS
Maximum flaps extended speeds - take-off approach (20deg)
220 KCAS
Maximum extended speeds - Down (39 deg):
170 KCAS
Maximum landing gear extended speed
250 KCAS / 0.70 Mt
Maximum landing gear operation speed, normal operation
225 KCAS
Maximum landing gear operation speed, alternate operation
175 KCAS
Minimum holding speed
160 KCAS
Mach trim / electric elevator trim inoperative speed
0.80 Mt
Turbulence penetration speed
- altitude 10000 ft or above - 270 KCAS / 0.80 Mt
- below 10000 ft - 240 KCAS
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
- 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