Term
| Ambient Temperature Limits-Flight and Ground |
|
Definition
Maximum - +50 C or ISA +35 C, whichever is lower.
Minimum - -54 C |
|
|
Term
| Maximum Operating Altitude |
|
Definition
|
|
Term
| Maximum Operating Altitude for Takeoff |
|
Definition
|
|
Term
| Turbulence Penetration Speed |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max Flaps Extended Speed (Vfe) |
|
Definition
Flaps 5 - 195
Flaps 10 - 175
Flaps 15 - 165
Flaps 35 - 155 |
|
|
Term
| Landing Gear Operating Speed (Vlo) |
|
Definition
|
|
Term
| Landing Gear Extended Speed |
|
Definition
|
|
Term
| Engine Starter Cranking Limits |
|
Definition
| Start 1: 70 seconds max, 2 minutes off |
|
|
Term
|
Definition
|
|
Term
|
Definition
| 600 lbs. (In-Flight only) |
|
|
Term
|
Definition
| Must be on for takeoff and landing |
|
|
Term
| Max Loadmeter for takeoff |
|
Definition
| Standby, Aux, and Main battery max reading at takeoff is 0.1 |
|
|
Term
| Minimum Battery Temp @ Takeoff |
|
Definition
|
|
Term
| Maximum Altitude With Gear or Flaps Extended |
|
Definition
|
|
Term
| Takeoff Power Setting Limits |
|
Definition
| Setting takeoff power with prior to brake release, with the nose of the aircraft more than 45 degrees out of the wind, is prohibited for wind speeds greater than 8 knots. |
|
|
Term
| Engine Airborne Operating Limits |
|
Definition
| In flight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited. |
|
|
Term
|
Definition
|
|
Term
| Max Cabin Pressure Diff. for T/O and Landing |
|
Definition
|
|
Term
| When must bleed air be off for takeoff? |
|
Definition
-Tailwind component exceeds 10 knots
-Takeoff conducted with maximum takeoff power (MTOP)
-Windshear is suspected |
|
|
Term
| When must bleed air be off for landing? |
|
Definition
-Tailwind component exceeds 10 knots
-OAT greater than 39 C
-Windshear is suspected |
|
|
Term
|
Definition
-Takeoff in basic mode prohibited
-Takeoff in DG mode prohibited |
|
|
Term
| Baggage Compartment Fire Extinguishing |
|
Definition
| Unless forward and aft baggage compartments are empty, the airplane shall not be operated farther than one hour flying time from a suitable airport for landing. |
|
|
Term
|
Definition
-Approved for ground operations only
-APU shall be shut down prior to takeoff
-APU shall not be operated unattended with passengers on board.
-APU shall not be operated during gravity refuel.
-APU shall not be started during refueling. |
|
|
Term
|
Definition
+50 C or ISA +35 C, whichever is lower
-54 C |
|
|
Term
| APU Starter Cranking Limits |
|
Definition
Start 1: 60 Seconds ON, 5 minutes OFF
Start 2: 60 Seconds ON, Maintenence action required |
|
|
Term
|
Definition
| Use of VOR without associated DME is prohibited in APP mode. |
|
|
Term
|
Definition
-With autopilot engaged, pilot seated at controls with harness secured.
-Glideslope angle 2.5 degrees to max of 4 degrees
-AFCS approved for autopilot coupled approaches to CAT 1 limits only |
|
|
Term
|
Definition
| Approved for all flap configurations (Use of flaps 35, autopilot coupled approach prohibited with one engine inop) |
|
|
Term
|
Definition
| Autopilot coupled approaches demonstrated in crosswind components up to 18 knots. Not considered limiting. |
|
|
Term
|
Definition
| After takeoff or G/A, minimum height for autopilot engagement is 1000 ft. AFE. |
|
|
Term
|
Definition
Shall be disengaged at or above 1000 ft AFE for:
-HGS approaches flown in AIII mode
-Approaches flown with one engine inop
-Approaches flown with flaps 0 |
|
|
Term
| Autopilot Disengagement (continued) |
|
Definition
-Coupled approaches, AP shall be disengaged at or above 200 ft AFE
-Shall be disengaged in severe icing
-Shall be disengaged in severe or extreme turbulence |
|
|
