MAULE M-7-235C User Manual

FAA APPROVED
FOR
MAULE M-7-235C
Airplane Serial No.__________________
Registration No.____________________
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
FAA APPROVED:
Manager, Aircraft Certification Office
Federal Aviation Administration
Atlanta, Georgia USA
DATE: October 10, 1995
Performance That Counts!
2099 Georgia Highway 133 South • Moultrie, GA 31788 •
(229) 985-2045 • Fax: (229) 890-2402 • www.mauleairinc.com

MAULE M-7-235C Specifications

General

Brand	MAULE
Model	M-7-235C
Category	Aircrafts
Language	English

Summary

SECTION I GENERAL

1.1 MAXIMUM WEIGHT

Specifies the maximum allowed weight for the aircraft.

1.2 CENTER OF GRAVITY LIMITS

Defines the acceptable range for the aircraft's center of gravity.

SECTION II LIMITATIONS

2.1 AIRSPEED LIMITS

Outlines the aircraft's airspeed indicator markings and their explanations.

2.2 POWER PLANT LIMITS

Specifies operating limits for the engine, propeller, and instruments.

SECTION III NORMAL PROCEDURES

3.1 PREFLIGHT INSPECTION

Provides a detailed checklist for inspecting the aircraft's interior and exterior.

3.2 OPERATING CHECK LISTS

Lists procedures for starting, engine checks, and before takeoff/landing.

C. ENGINE CHECK

Details the steps for performing a proper engine check.

D. BEFORE TAKEOFF

Lists pre-takeoff checks and settings for safe flight.

E. BEFORE LANDING

Outlines the procedures to follow before landing the aircraft.

F. ENGINE SHUT DOWN

Provides the correct procedure for shutting down the engine.

3.3 NORMAL FLIGHT OPERATIONS

Covers key flight phases like climbing, stalling, and crosswind operations.

SECTION IV EMERGENCY PROCEDURES

4.1 EMERGENCY BASIC RULES

Outlines fundamental rules for handling emergencies.

4.2 ENGINE EMERGENCY SHUT DOWN

Details the procedure for shutting down the engine in an emergency.

4.3 ENGINE FIRE DURING STARTING

Provides steps to take if an engine fire occurs during starting.

4.4 ENGINE FIRE AFTER STARTING

4.6 TAKEOFF ABORT

4.7 ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING

4.8 PARTIAL POWER FAILURE DURING FLIGHT OR AFTER TAKEOFF

4.9 COMPLETE POWER FAILURE DURING FLIGHT

4.10 ENGINE AIRSTART

4.11 ELECTRICAL FIRE

4.12 ENGINE FIRE DURING FLIGHT

4.15 RECOVERY FROM INADVERTENT SPINS

4.16 ALTERNATOR FAILURE

SECTION V WEIGHT AND BALANCE

5.1 WEIGHT AND BALANCE

CENTER OF GRAVITY RANGE

PROCEDURE

Calculations for determining weight, C.G. and moment

EXAMPLE OF WEIGHT AND BALANCE CALCULATION FOR LOADED AIRCRAFT