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62 Cards in this Set
- Front
- Back
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What is the Maximum Permissible Operating Altitude?
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47,000 Feet
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What is Maximum Ramp Weight (Mod. M57 Installed)?
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36,700 lbs
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What is the Maximum Takeoff Weight?
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36,500 Pounds
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What is the Maximum Landing Weight?
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33,000 Pounds
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What is the Maximum Zero Fuel Weight?
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28,660 Pounds
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Maximum Flaps Extended (VFE ) for:
Slats Extended + 10° Flaps: Slats Extended + 20° Flaps : |
Slats Extended + 10° Flaps:
200 KIAS Slats Extended + 20° Flaps : 160 KIAS |
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What is the Maximum Landing Gear
Extended Speed (VLE / MLE)? |
245 KIAS / 0.75M
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What is the Maximum Landing Gear
Operating Speed (VLO / MLO)? |
190 KIAS / 0.70M
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What is VMCA (Minimum Control - Air)?
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90 KIAS
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What is VMCG (Minimum Control - Ground)?
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98 kias
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What is the Maximum Tire Ground Speed?
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195 kts
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What is the Maximum Operating Speed (VMO / MMO)?
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370 KIAS / 0.862M
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What is the Maximum Speedbrake Extension Speed?
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no limit
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Maximum Windshield Wiper Operating Speed?
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215 kias
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What is Maximum Direct Vision Window Opening Speed?
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215 kias
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What are Minimum & Maximum Airport
Pressure Altitudes for Takeoff and Landing? |
-1,000 / 10,000 Feet
(Paved / Hard-Surfaced Runways Only) |
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What is the Maximum Air Temperature
Approved For Takeoff and Landing? |
50°C @ Sea Level
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Is Anti-Skid Required for Takeoff?
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Anti-skid MUST be operational for takeoff
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Maximum Crosswind - Demonstrated?
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35 KTS
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Maximum Tailwind Component?
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10 KTS
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What is the Maximum Load Factor in Flight for Flaps UP?
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-1.0 to +2.64G
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What is the Maximum Load Factor in Flight for Flaps DOWN?
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0.0 to +2.0G
What |
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What is the Maximum Runway Slope?
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± 2.0%
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What is the Minimum Altitude for Autopilot Use?
Cruise: Non-Precision Approach: Coupled ILS: Radio Altimeter Radio Altimeter Inoperative: |
Cruise: 1,000 Feet AGL
Non-Precision Approach: 250 Feet AGL Coupled ILS: Radio Altimeter Operative: 70 Feet AGL Radio Altimeter Inoperative: 160 Feet AGL The autopilot must be OFF for takeoff and landing. |
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What is the Maximum In-Flight Generator Output?
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Stabilized – 400 Amps
Transient (5 Seconds) – 800 Amps Transient (40 Seconds) – 600 Amps Transient (160 Seconds) – 500 Amps |
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What is Maximum Voltage of the DC System?
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29.5 Volts
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What is the Maximum Generator Output On Ground?
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300 Amps
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What is the Maximum Differential Pressure?
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9.3 PSI
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What is the Maximum Negative Differential Pressure?
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-0.3 PSI
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The Total Usable Fuel Quantity Is:
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LH Wing + Half Center Wing Box: 906 gal ,6070 lbs
RH Wing + Half Center Wing Box: 906 gal 6085 lbs Airplane Total Capacity: 1,814 gal 12,155 lbs |
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What is the Minimum In-Tank Fuel
Temperature During Flight? |
≥ 3°C Above Freezing Point of Fuel Used
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What is the Maximum Fuel Dissymmetry for
Flight? |
2,200 Pounds
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What is the Maximum System Fueling
Pressure? |
50 PSI / 3.5 Bars / 350 KPa
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What Are the Approved Hydraulic Fluids?
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Those Conforming to AIR 3520 Specifications
Those Conforming to MIL-H-5606 Specifications (NATO Codes H515 or H520) |
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When Must All Anti-Ice Systems Be Turned
ON? |
Operating in Visible Moisture
When TAT < +10°C |
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Continuous Use of the Supplemental Oxygen
System is Prohibited Above the Following CABIN Altitudes: |
Carrying Passengers: 25,000 ft
Crew Only: 40,000 ft EROS |
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Thrust Ratings (Uninstalled-Sea Level-ISA)
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Takeoff: 5,888 Pounds
Maximum Continuous: 5,613 |
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Which Engine Parameter Is Used For Setting
Thrust? |
N1
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Maximum N1 and N2:
Maximum Continuous Maximum / Normal Takeoff (5 Minutes Maximum) |
Maximum Continuous 96.7 104.9
Maximum / Normal Takeoff (5 Minutes Maximum) 96.7 106 |
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Engine Vibration Limits:
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N1 : 1.0 IN/SEC
N2 : 1.5 IN/SEC |
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Interstage Turbine Temperature (ITT) Limits (Starting):
Ground: Airstart: Restart Max Temperature: Windmilling Max Continuous: |
Ground Start: 815°C
Airstart: 890°C Restart Max Temperature: 150°C Windmilling: 970°C (10 Seconds Max) 1000 C (2 seconds max) |
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Starting Time Limits - Ground:
Start to Light-Off: After Reaching ?% N2 Light-Off to Idle: |
Start to Light-Off: 10 Seconds Maximum
After Reaching 22% N2 Light-Off to Idle: 60 Seconds Maximum |
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Starting Time Limits – Airstart (Light-Off to Idle):
assisted: windmilling |
Assisted: 60 Seconds Maximum
Windmilling: 180 Seconds |
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What is the APU Maximum Operating /
Starting Altitude? |
35,000
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APU
Max N1 EGT --starting --stabilized |
APU
Max N1 110% EGT --starting 974 C --stabilized 746 C |
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What is the APU Maximum Generator
Output? Transient (1 Minute Maximum): Amps 0 – 10,000 Feet: Amps 10,000 – 25,000 Feet: Amps 25,000 – 35,000 Feet: Amps |
Transient (1 Minute Maximum): 350 Amps
0 – 10,000 Feet: 300 Amps 10,000 – 25,000 Feet: 250 Amps 25,000 – 35,000 Feet: 200 Amps |
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Baggage Compartment
Limit lbs limit lb/sq ft |
1600 lbs
not to exceed 61.4 lb/sq ft |
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LH and RH coat compartment
not to exceed lb/sq ft |
not to exceed 81.9 lb/sq ft
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payload
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5990 lbs
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CG datum
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25% of MAC
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VA (maneuvering speed)
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198 kias
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landing light limit
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15 minutes ON / 45 minutes off
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Fuel types limit?
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use of JP-4 and Jet B flight altitudes limited to 23,000 ft after a low booster pump failure
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Pressure fueling system
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50 psi
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Fuel Control Computer
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FQMC must be operational for Takeoff
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Thrust
T/O MCT |
T/O 5888 lbs
MCT 5613 lbs |
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Oil Pressure Limits
Operating range Transient (minutes) Minimum (at idle) Cold Start |
Oil Pressure Limits
Operating range 60-85 psi Transient (3 minutes) 85 to 100 psi Minimum (at idle) 30 psi Cold Start oil to < 0. (2.5 min max) - 135 psi |
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Oil Temperature Limits
Max Min Transient Cold Start |
Oil Temperature Limits
Max 138 C Min 30 C Transient (3 min) 138 to 155 C Cold Start -40 C |
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Requirements to use TR
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Ground
All 3 wheels on ground down to 20 kts |
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Height
Wing Span Length Gear Width |
Height 23' 8"
Wing Span 63' 5" Length 66' 4" Gear width 14' 7" |
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Minimum Battery Voltage for start
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24V
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ITT limits
Maximum Takeoff (APR): Normal Takeoff: Maximum Continuous: |
Maximum Takeoff (APR): 890°C (5 Minutes Max)
Normal Takeoff: 864°C (5 Minutes Max) Maximum Continuous: 861°C |
