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62 Cards in this Set
 Front
 Back
What is the Maximum Permissible Operating Altitude?

47,000 Feet


What is Maximum Ramp Weight (Mod. M57 Installed)?

36,700 lbs


What is the Maximum Takeoff Weight?

36,500 Pounds


What is the Maximum Landing Weight?

33,000 Pounds


What is the Maximum Zero Fuel Weight?

28,660 Pounds


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 

What is the Maximum Landing Gear
Extended Speed (VLE / MLE)? 
245 KIAS / 0.75M


What is the Maximum Landing Gear
Operating Speed (VLO / MLO)? 
190 KIAS / 0.70M


What is VMCA (Minimum Control  Air)?

90 KIAS


What is VMCG (Minimum Control  Ground)?

98 kias


What is the Maximum Tire Ground Speed?

195 kts


What is the Maximum Operating Speed (VMO / MMO)?

370 KIAS / 0.862M


What is the Maximum Speedbrake Extension Speed?

no limit


Maximum Windshield Wiper Operating Speed?

215 kias


What is Maximum Direct Vision Window Opening Speed?

215 kias


What are Minimum & Maximum Airport
Pressure Altitudes for Takeoff and Landing? 
1,000 / 10,000 Feet
(Paved / HardSurfaced Runways Only) 

What is the Maximum Air Temperature
Approved For Takeoff and Landing? 
50°C @ Sea Level


Is AntiSkid Required for Takeoff?

Antiskid MUST be operational for takeoff


Maximum Crosswind  Demonstrated?

35 KTS


Maximum Tailwind Component?

10 KTS


What is the Maximum Load Factor in Flight for Flaps UP?

1.0 to +2.64G


What is the Maximum Load Factor in Flight for Flaps DOWN?

0.0 to +2.0G
What 

What is the Maximum Runway Slope?

± 2.0%


What is the Minimum Altitude for Autopilot Use?
Cruise: NonPrecision Approach: Coupled ILS: Radio Altimeter Radio Altimeter Inoperative: 
Cruise: 1,000 Feet AGL
NonPrecision 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. 

What is the Maximum InFlight Generator Output?

Stabilized – 400 Amps
Transient (5 Seconds) – 800 Amps Transient (40 Seconds) – 600 Amps Transient (160 Seconds) – 500 Amps 

What is Maximum Voltage of the DC System?

29.5 Volts


What is the Maximum Generator Output On Ground?

300 Amps


What is the Maximum Differential Pressure?

9.3 PSI


What is the Maximum Negative Differential Pressure?

0.3 PSI


The Total Usable Fuel Quantity Is:

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 

What is the Minimum InTank Fuel
Temperature During Flight? 
≥ 3°C Above Freezing Point of Fuel Used


What is the Maximum Fuel Dissymmetry for
Flight? 
2,200 Pounds


What is the Maximum System Fueling
Pressure? 
50 PSI / 3.5 Bars / 350 KPa


What Are the Approved Hydraulic Fluids?

Those Conforming to AIR 3520 Specifications
Those Conforming to MILH5606 Specifications (NATO Codes H515 or H520) 

When Must All AntiIce Systems Be Turned
ON? 
Operating in Visible Moisture
When TAT < +10°C 

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 

Thrust Ratings (UninstalledSea LevelISA)

Takeoff: 5,888 Pounds
Maximum Continuous: 5,613 

Which Engine Parameter Is Used For Setting
Thrust? 
N1


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 

Engine Vibration Limits:

N1 : 1.0 IN/SEC
N2 : 1.5 IN/SEC 

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) 

Starting Time Limits  Ground:
Start to LightOff: After Reaching ?% N2 LightOff to Idle: 
Start to LightOff: 10 Seconds Maximum
After Reaching 22% N2 LightOff to Idle: 60 Seconds Maximum 

Starting Time Limits – Airstart (LightOff to Idle):
assisted: windmilling 
Assisted: 60 Seconds Maximum
Windmilling: 180 Seconds 

What is the APU Maximum Operating /
Starting Altitude? 
35,000


APU
Max N1 EGT starting stabilized 
APU
Max N1 110% EGT starting 974 C stabilized 746 C 

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 

Baggage Compartment
Limit lbs limit lb/sq ft 
1600 lbs
not to exceed 61.4 lb/sq ft 

LH and RH coat compartment
not to exceed lb/sq ft 
not to exceed 81.9 lb/sq ft


payload

5990 lbs


CG datum

25% of MAC


VA (maneuvering speed)

198 kias


landing light limit

15 minutes ON / 45 minutes off


Fuel types limit?

use of JP4 and Jet B flight altitudes limited to 23,000 ft after a low booster pump failure


Pressure fueling system

50 psi


Fuel Control Computer

FQMC must be operational for Takeoff


Thrust
T/O MCT 
T/O 5888 lbs
MCT 5613 lbs 

Oil Pressure Limits
Operating range Transient (minutes) Minimum (at idle) Cold Start 
Oil Pressure Limits
Operating range 6085 psi Transient (3 minutes) 85 to 100 psi Minimum (at idle) 30 psi Cold Start oil to < 0. (2.5 min max)  135 psi 

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 

Requirements to use TR

Ground
All 3 wheels on ground down to 20 kts 

Height
Wing Span Length Gear Width 
Height 23' 8"
Wing Span 63' 5" Length 66' 4" Gear width 14' 7" 

Minimum Battery Voltage for start

24V


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 