Learjet 35A User Manual

Gates Learjet 35A/36A
with
FC-200 Autopilot
FAA APPROVED AIRPLANE FLIGHT MANUAL
THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH THE
PRESCRIBED LIMITATIONS
IN SECTION 1 OF THIS MANUAL
___________________ NOTICE __________________ _
This
AFM is a revised issue of the original AFM dated 4-30-76. This
reissue replaces
all of the information in the original issue through
Change 13.
FM-102
SERIAL NO. ______ _
N ______________ __
for CHIEF, AIRCRAFT CERTIFICATION PROGRAM
FAA CENTRAL REGION
WlCHIT A, KANSAS
Copyright © 1983
GATES LEARJET CORPORATION
All rights reserved

Learjet 35A Specifications

General

Manufacturer	Learjet
Model	35A
Role	Business jet
First Flight	1973
Crew	2
Passenger Capacity	8
Length	48 ft 8 in (14.83 m)
Wingspan	39 ft 6 in (12.04 m)
Height	12 ft 3 in (3.73 m)
Engine Type	Garrett TFE731-2-2B turbofan
Service Ceiling	45, 000 ft (13, 716 m)
Max Takeoff Weight	18, 300 lb (8, 300 kg)
Thrust per Engine	3, 500 pounds-force (15.6 kN)

Summary

Gates Learjet 35A/36A with FC-200 Autopilot

Section I — LIMITATIONS

Weight and C.G. Limits

Details maximum ramp, takeoff, landing weights, zero wing/tip fuel weight, and CG envelope.

Airspeed/Mach Limits

Specifies maximum operating speeds (VMO/MMO), maneuvering speed (VA), and landing gear operating speeds.

Takeoff and Landing Operational Limits

Section II — NORMAL PROCEDURES

Before Starting Engines

Details pre-start checks including controls, oxygen system, battery, inverter, lights, and system switches.

Starting Engines

Section III — EMERGENCY PROCEDURES

Electrical

Covers complete AC power failure, battery overheat, current limiter failure, DC power loss, and dual generator failure.

Engine

Fire

Procedures for cabin/cockpit fire, smoke, or fumes.

Flight Controls

Landing — Both Engines Inoperative

Procedures for landing the aircraft with both engines inoperative.

Aborted Takeoff