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73 Cards in this Set

  • Front
  • Back
Max Ramp Weight
36,500 lbs.
Max Takeoff Weight
36,300 lbs.
Max Landing Weight
34,500 lbs.
Max Zero Fuel Weight (per STC)
32,400 lbs.
Min Structural Design Weight
21,400 lbs.
AFT ONE Cargo Compartment:

Max floor loading
125 lb/ft^2
AFT ONE Cargo Compartment:

Max permitted load
1,980 lbs.
AFT TWO Cargo Compartment:

Max floor loading
75 lb/ft^2
AFT TWO Cargo Compartment:

Max permitted load
980 lbs.
AFT ONE plus AFT TWO Cargo Compartment total load limit
1,980 lbs.
Maneuvering Limit Load Factors:

Flap Retracted G Limits
+2.5 to -1.0 g
Maneuvering Limit Load Factors:

Flap Extended G limits
+2.0 to 0.0 g
Maximum Lateral Asymmetry:

What is the maximum fuel imbalance between the contents of the main fuel tanks?
600 lbs. (In-flight limitation only).
Maximum Operating Altitude
25,000' ASL
Maximum Operating Altitude for Takeoff and Landing
10,000' ASL
Max Runway Slope for Takeoff and Landing
+-2%
What is the max tailwind for takeoff and landing?
20 kts.
What are the limitations for a takeoff and landing with a tailwind of 11-20 kts.?
Anti-skid must be operative.
Nosewheel steering must be operative.
Both ECU's must be operative.
Autofeather system must be operative.
Normal TO power must be used.
Bleeds must be OFF.
Flaps 15 used for takeoff.
Flaps 35 used for landing.
Max approach angle is 4 deg.
Condition levers 1200 for landing.
Runway must be uncontaminated.
Maximum Crosswind Component
36 kts. (Approved for takeoff/landing on a hard, dry or wet runway).
Max Operating Ambient Temperature
+48.9 C or ISA +35 C, whichever is lower.
Minimum Operating Ambient Temperature
-54 C
Max Operating Temperature for Landing with BLEEDs ON
41.9 C (107 F).
Flap Extended Speeds
Flaps 5 - 148
Flaps 15 - 148
Flaps 35 - 130
Maneuvering Speed
164 kts.
Max Landing Gear Operating Speed (Vlo)
158 kts.
Max Landing Gear Extended Speed (Vle)
172 kts.
Rough Air Speed
180 kts.
Alternate Gear Extension Speed
140 kts. (Speed is limited because all wheel well doors remain open after gear is fully down).
Engine Manufacturer / Model #
Pratt & Whitney / PW 123D
Maximum Altitude for Engine Airstart
20,000 ft.
How much additional power will the engine uptrim provide?
10% torque (nominal)
Minimum Torque for the Assumed OAT
88.5% (Per AFM supplement no. 13).
What is the Max Takeoff Power and when/how can it be set?
111%, rated for 5 minutes. Only set by uptrim via ECU. Crew shall not reduce setting until gear and flaps are retracted and a climb at Vse is established.
Max Torque for 1200 Np?

Max Torque for 1024 Np or lower?
97.5 in flight (99.5 for Takeoff)

105% (Commutair Limitation) 114.2% (AOM Limitation)
ITT Temp Limits
800-840 C - 20 Seconds
840-900 C - 12 Seconds
900-950 C - 5 Seconds

(Unless otherwise stated, transient limits are limited to 20 seconds).
Can normal takeoff ITT limits ever be exceeded during a takeoff?
No.
Minimum Flight Idle Nh
66%
Oil Pressure Limits
55 - 65 PSID: Normal
40 - 55 PSID: Allowed at engine speed below 75% Nh.
< 40 PSID requires engine shutdown with the exception of spool up during engine start.
Oil Temperature Limits
45 C - 115 C - Normal
115 C - 125 C - Time limited to 20 minutes.

Prior to unfeathering the prop and for power settings above flight idle, min oil temp is 0 deg. C.
What is the minimum oil temperature for adequate engine inlet anti-icing?
45 deg. C.
Reduced Torque Takeoff Limitations
(WARFARE TUMP)
Windshear not present/reported.
Anti-skid must be operative.
Runway not unpaved or gravel.
First flight of the day.
Autofeather must be operative.
Runway slope 2% or less.
ECU's must be operative.
Tailwind cannot exceed 10kts.
Uptrim must be armed and operational.
Min Torque for assumed temp is 88.5%.
Prohibited when special DP requires full power.
What is the lowest fuel tank temp?
-36 deg. C. (Must be at least 4 deg. C above the freezing point of Jet-A, which is -40 deg. C.).
Starter Cranking Limits
1: 1min on - 2 mins off
2: 1min on - 2 mins off
3: 1min on - 30 mins off
What does the red triangle signify on the ITT gauge?
Max temp during engine start.
Max Torque with the Prop Feathered
57%
Max Flight Idle Nh
66%
What is the prop prohibited range?
500 - 780 RPM.
Extended operation with prop RPM above 780 requires the aircraft to be oriented in what way?
Into the wind.
What can be expected if the power levers are operated aft of the flight idle gate in flight?
Propeller overspeed.
Possible engine failure.
May result in loss of aircraft control.
DC Generator Max Loadmeter
Ground 0.7
Flight 1.0

Note: The ground load may be exceeded for up to one minute during internal battery start.
TRUs Max Loadmeter
Ground/Flight - 1.0
AC Generators Max Loadmeter
Ground < 10 C - 1.0
Ground >= 10 C - 0.33
Flight - 1.0
Inverters Max Loadmeter
Ground/Flight - 1.0
Max altitude with landing gear and/or flaps extended
15,000 ft.
What is the maximum tire speed?
165 kts. groundspeed.
What is the normal cabin pressure differential?
5.5 psi. +- 0.3 psi.
What is the maximum cabin pressure differential?
5.95 psi.
What is the maximum cabin pressure differential during taxi, takeoff and landing?
0.5 psi.
What is the maximum cabin altitude?
8,000 ft.
According to the AOM, when do icing conditions exist on the ground?
SAT is 10 deg. C or less when precipitation in any form is present, or fog with vis 1 mile or less; also when operating on surfaces with snow, ice, slush or standing water may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
According to the AOM, when do icing conditions exist in flight?
SAT is 5 deg. C or less and visible moisture is present in any form.
When must the airframe deicing boots be turned on? When can they be turned off?
Wing and tail boots must be activated at the first sign of ice formation anywhere on the aircraft.

The wing and tail deice boots may be deactivated only after completion of an entire deicing cycle after leaving icing conditions. (Per AD).
What are the AFCS Limitations?
(DOG CHESS BEEF)
D-Use of NAV or APP not authorized with a VOR if associated DME is not available.
O-Do not overpower the autopilot.
G-Glideslope of 2.5 to 4 deg authorized. If greater than 3 deg, flaps 15 must be used.

C-CAT I approach mins only.
H-Harness must be worn at all times.
E-Engine failure, cannot commence or continue an approach.
S-Severe Icing not authorized.
S-Severe turbulence not authorized.

B-Backcourse apch not authorized.
E-Engagement altitude after T/O is 1,000 AGL.
E-Disengaged by 200 ft AGL unless on RNAV, then by 300 AGL.
F-Flaps 35 not authorized.
What are the AHRS limitations?
Takeoff in BASIC mode is prohibited.

Takeoff in DG mode is prohibited.

Takeoff with any advisory light illuminated on the AHRS control panel is prohibited.
What are the HGS limitations?
HGS takeoff in reduced visibility conditions requires that the PRI mode be selected.

HGS approaches are limited to PRI, IMC and AIII modes during CAT 1 approaches.
What are the EFIS limitations?
ILS and FMS based approaches are not permitted using composite EHSI/EADI display.
What is the usable fuel in each tank?
2,839 lbs.
What is the total usable fuel?
5,678 lbs.
Outside of E&A checklist usage, when should the TERR O-RIDE switch be inhibited?
When performing a takeoff or landing from an airport not contained in the EGPWS database. This applies to any airport not containing a hard surface runway at least 3,500' long with published coordinates.
What must be on for the Terrain Awareness and Display function (TAAD) to operate?
The IRS and the No. 1 FMS must be on.
What must be on for takeoff and landing per the limitations section?
Tank 1 and 2 aux pumps.
What is the upper and lower limit of the fuel heater outlet temperature?
11 deg. C. to 57 deg. C.
What is the rated horsepower for each engine under normal and uptrim conditions?
1950 HP - Normal
2150 HP - Uptrim