Take-Off And Landing Pressure Altitude Limits

-1,000ft to 8,000ft

Take-Off and Landing Temperature Limits

-40 C to ISA+35C

Max. Presure Altitude

37,000ft

Max. Operating Temperature 

ISA + 35C 

Min. Operating Temperature 

-54C to 25,000Ft

-65 to 37,000Ft 

TAT in curise above 25,000Ft Limitation 

-45C 

Vlo (Retraction) 

200Kias 

Vlo (Extension) 

250KIAS 

Vle (Extended) 

250Kias 

Max. Operating Airspeed

Vmo/ Mmo 

0 to 8,000 : 250KIAS

10,000 to 26,000: 320KIAS

26,000 to 37,000: .78 Mach 

Va 

200KIAS 

Vfe 

Flaps 9:  250KIAS

Flaps 22:  200KIAS

Flaps 45:  145KIAS 

Tailwind Max 

10 Knots Max for Take-off and Landing 

Direct Vision Window Removal 

140KIAS 

Max. Operation for Windshield Wipers 

170KIAS 

Turbulent Air Penetration Max A/S 

At or below 10,000Ft : 200KIAS

Above 10,000Ft: 250KIAS / .63M

Whichever is lower 

Load Factor Limits 

Flaps Up: -1.00 G to 2.50 G

Flaps Down:  0 G to 2.0 G 

Maximum Ramp Weight

48,722 Lbs. 

Maximum Take-off Weight

48,501 Lbs. 

Maximum Landing Weight 

42,549 Lbs. 

Maximum Zero Fuel Weight 

39,462 Lbs 

Fuel Type 

JET A, Jet A-1, JP-8 

Fuel Tank Temperature Limits 

-40C to 52C 

Max. Imbalance Between Fuel Tanks 

800lbs 

Max. Usuable Quantity In Each Tank 

679.8 US Gal

(4,600 lbs) 

Usuable Quantity In Each Tank 

7.1 US Gal

(48lbs) 

Fuel Tank Notes: 

Unusuable fuel increases to 266 Lbs. in each tank if any of the associated electric fuel pumps is INOP.

Fuel Tank Notes:

When Performing pressure refueling, the usable fuel quantity in each tank may be reduced by 7.9 US Gal. 

APU Temperature Min.

40C11

-54C 

APU Altitude For Start 

40C11                                           40C14

Max: 25,000 or                       Max: 30,000ft

        30,000 (2)
 

Note 2: For airplanes post-mod or equipped with an equivalent modification factory incorportated. Min temp is -54C up to 30,000ft. 

APU Operational Altitude 

37,000Ft for Both C11 and C14 

APU Rotor Speed 

108% Max for both C11 and C14 

APU Start Temp. Max 

40C11                            40C14

884C (1)                         884C

Note 1: May be exceeded up to 925C above 25,000Ft during 10 Sec. 

APU Continious Temp. Max. 

40C11                                        40C14

680C (6)                                      680C(6)

 Note 6: The APU EGT may be exceed up to 717C for 5 Min max.

APU Starter Limits 

Cooling Period Between Each Attempt:

3 Consecutive Attempts: 1minute Off

Between 2 Series of 3 Consec. Attempts:   30 Min. Off

Engine Starter Limits 

On Ground:

Staring or Dry Motoring: Up to 5 on, 5 Min Off

Or

1st Through 4th Cycles: 1 min on, 1 Min Off

Following Cycles: 5 Min on, 5 Min Off

In Flight:

Maximum Cont. Operation Time: 5 Min On

(No cool down time is required should inflight attempt be required) 

ATTCS

Must be operative for ALT T/0-1 Mode 

Reversers 

Do NOT go-around after reverser deployment 

AE3007A1 (LR) N1 Max

Note: Any exceedance or peak must be monitered and logged by the crew. 

100% 

AE3007A1 (LR) N2 Max

102.4% (8)

Note: For airplanes pre-mod the N2 limit is 102.5% 

AE3007A1 (LR) ITT Start Max Temp.

800C 

AE3007A1 (LR) ITT Take-off Modes Temp. Max

948C (1)

Note 1: Takeoff Thrust is limited to 5 Min. 

AE3007A1 (LR) Continious Temp. Max.

901C 

AE3007A1 (LR) Oil Pressure Below 88% N2

Min:  34 PSI

Max:  110 PSI  (2) (7)

Note 2: May be exceeded during starts if oil temp. is below 21 C. The engine must remain at idle until the oil PSI is less than 110PSI

Note 7: Operation in oil pressure amber range111 and 115 psi is permitted in all opeational modes and time limited to 5 Minutes, Or between 116 and 155 PSI in all operational modes time limited to 2 minutes. Total time above 110 PSI may not exceed 5 Min.  

AE3007A1 (LR)  At or above 88% N2 Oil PSI.

Min: 50 PSI (9)

Max:  110 PSI (7)

Note 9: While this is an abnormal condition, operation between 50 and 34 PSI is permitted during takeoff and go around phases (AE3007A Only) 

Note 7: Operation in oil pressure amber range111 and 115 psi is permitted in all opeational modes and time limited to 5 Minutes, Or between 116 and 155 PSI in all operational modes time limited to 2 minutes. Total time above 110 PSI may not exceed 5 Min.  

AE3007A1 (LR) Fuel Temp Limits

-54C to +52C 

AE3007A1 (LR) Vibration Max.

LP Spool: 1.8 IPS (4)

HP Spool: 1.1 IPS (4)

Note 4: Vibration in the amber range below 2.5IPS is time limimted to 5 Min. during the takeoff or go-around phases or 10 sec. during the remainder of the flight phases. 

Engine Warm-Up

Engine Cool Down 

The engines must run for at least 1 minute at idle or taxi thrust before shutdown. 

Max Temp. for A/I Operation 

10C 

Min. Temp for Manual A/I Operation 

-40C 

Holding Configuration Icing Conditions 

Landing Gear- Up

Flaps-Up

Minimum Airspeed- 200Kias 

Single-Engine or Single Bleed In Icing Conditions 

Max Altitude- 15,000 Ft. 

Max Load on Main Generator 

400Amps 

Max Load on APU Generator 

400 Amps below 30,000Ft

300 Amps above 30,000Ft 

Max. Battery Temperature 

70 C 

Max Differential Pressure 

7.8 PSI 

Max Differential Overpressure 

8.1 PSI 

Max Differential Negitive Pressure 

-0.3  

Max Altitude to Extend Flaps 

20,000 Ft. 

Max Airspeed after Take-off/ During Climb without retrimming 

160KIAS 

Integrated Standby Instrument System 

Maximum duration of ISIS when operating on batteries is 40 Min.

Note: The max duration of battery power can be extended to 45 Min if the Pitot 3 Sensor Heating buttion is turned off when not operating in icing conditions.

Airplane must not be moved during power-up initialization. Do not cage attitude in turning flight. 

Electromechanical Gust Lock 

Each time electromechanical gust lock lever is set to unlocked position elevator movement must be checked. This check must be preformed at least 10 seconds after positioning the gust lock lever to the unlocked position by moving the control column from the full up stop to the full down stop and back to the full up stop position. 

ILS 

When crossing the outer marker on glideslope, the altitue must be verified with the published approach procedure. 

Min. Altitude Coupled to ILS 

200Ft 

Min. Autopilot engagement height after takeoff 

500 Ft. 

Single Engine Go-Around Autopilot

Prohibited 

Max Crosswind Dry Runway 

30Kts 

Max Crosswind Wet Runway 

30Kts 

Max Crosswind with Compacted Snow 

20 Kts 

Max Crosswind with Standing Water Or Slush 

20 Kts 

Max Croswind with Ice ( No Melting) 

10 Kts 

Max Operating Altitude when one bleed or one pack is closed 

25,000 Ft.

When operating with APU bleed supplying PACK 1( Eng. 1 bleed closed) and engine 2 supplying Pack 2 ( Crossbleed Closed), Maximum operating altitude is 37,000Ft 

Windshear Prevention/Recovery 

Thrust Levers- Max

Go Around Buttions- Press 

Take Configuration Warning 

Do Not Take Off.

Airplane Configuration- Correct 

Battery Overtemperature 

Associated Battery- Off 

Cabin Fire or Smoke 

Crew Oxygen Masks- Don, Select 100%

Smoke Goggles or PBE- Don

Recirculation Fan- Off

Crew Communication- Eastablish 

Baggage Compartment Smoke 

Baggage Fire Extinguishing Button (If Installed)- Press 

APU Fire 

APU Shutoff Valve- Close 

Engine Fire, Severe Damage, or Seperation 

Identify Affected Engine.

Thrust Lever- Idle

Start/Stop Selector- Stop

Fire Extinguishing Handle- Pull (Do Not Rotate) 

Engine Low N1 

If during takeoff, below v1:

Rejected Takeoff Procedure- Accomplish 

Engine ATTCS No Margin 

During Take off, Below V1:

Rejected Takeoff Procedure- Accomplish 

ATTCS Failure 

Thrust Levers- Max 

Dual Engine Failure 

Airspeed- Minimum 260 KIAS

Altitude- Max 25,000 Ft

Oxygen Masks (If required)- Don

Engine Airstart Procedure- Accomplish 

Engine Reverser Failure 

During Take off, below V:

Rejected takeoff procedure- accomplish 

Engine Thrust Reverser Disagree 

During Takeoff, If below V1:

Rejected takeoff procedure- accomplish 

Rejected Takeoff (At or Below V1) 

Thrust Levers- Idle or Max Reverse 

Takeoff With Engine Failure Above V1 

Maximum Takeoff Thrust- Check

At Vr Rotate the airplane

With positive rate of climb

Landing Gear- Up

Airspeed- V2 

Pitch Trim Runaway 

Control Column- Hold Firmly

Below V1  Take off- Reject

Above V1 or in flight: Quick Disconnect Buttion- Press and hold 

Jammed Elevator 

Elevator Disconnect- Pull 

Aileron/Roll Trim Runaway 

Control roll attitude manually with control wheels and rudder.

Quick Disconnect Button- Press and Hold

Aileron Systems 1 and 2- Off 

Jammed Aileron 

Aileron Disconnect- Pull 

Inadvertent Spoiler Opening In Flight 

Control the airplane using thrust, elevator and stabilizer

Speed Brake- Close 

Rapid Cabin Depressurization 

Crew Oxygen Masks- Don

Crew Communication- Establish

Emergency Descent- As Required 

Emergency Descent 

Cabin Crew- Notify

Fasten Seat Belt Sign- on

Thrust Levers- Idle

Speed Brakes- On

Airspeed- 250 KIAS

Landing Gear- Down

Minimum Enroute Altitude- Check 

Abnormal Engine Start 

To abort start:

Associated Thrust Levers- Idle

Start/Stop Selector- Stop 

Engine Out 

If during takeoff, below V1:

Rejected Takeoff Procedure- Accomplish 

Rudder/Yaw Trim Runaway 

Quick Disconnect Button- Press

Rudder Systems 1 and 2- Off 

Steering System Inoperative or Uncommanded swerving on Ground 

Control the airplane using rudder command and differntial brakes.

Steering Handwheel- Do Not Use

If Unable to control the airplane, as an addiontional action:

 Steering Desengagement Buttion: Press

Consider the use of differential thrust reverser if serviceable 

Anti Icing Inoperative in Icing Conditons 

Below V1:

Takeoff- Reject