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Rockwell Commander 112 Service Manual

Rockwell Commander 112
293 pages
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Rockwell
Commander
112/B/Tc/TCA
REVISION
1: 23
APRIL
1977
CHANGED:
7
JANUARY
1980
MANUFACTURERSSERIALNO.
________________________
_
REGISTRATION
NO.
________________________________
_
For coordination
with
sales
and service
information,
Serial No.
126
thru
499
are
referred
to
as
Model
112A.
At
the
time
of
issue
of
this Maintenance Manual, the contents were,
to
the
best
of
Rockwell International's knowledge, adaquate
to
maintain the
aircraft
in a continued
airworthy
condition.
'!'
Rockwell International
General
Aviation
Division
5001
North
Rockwell Avenue
Bethany,
Oklahoma 73008
PIN M 112001-2
Copyright Commander Owners Group 2013 All Rights Reserved
**unofficial copy**
Includes Interim Change 4/1/86 and
Interim Change 2, 9/1/96

Table of Contents

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Rockwell Commander 112 Specifications

General IconGeneral
BrandRockwell
ModelCommander 112
CategoryAircrafts
LanguageEnglish

Summary

Interim Change Notice

Hydraulic Hoses Maintenance

Interim change notice regarding hydraulic hose maintenance instructions.

Interim Change Notice

Ground Contact Switch and Check

Interim change notice regarding ground contact switch adjustment and check procedures.

SECTION I GENERAL INFORMATION

GENERAL DESCRIPTION

Overview of the Rockwell Commander 112/B/TC/TCA aircraft and its design.

PRINCIPAL DIMENSIONS

Key physical dimensions and specifications of the aircraft.

AIRCRAFT STRUCTURES

Details on the fuselage, wing, and empennage construction.

POWER PLANT

Description of the engine and propeller systems, including specifications.

FUEL SYSTEM

Information on fuel storage, delivery, and system components.

LANDING GEAR, WHEELS AND BRAKES

Details on the tricycle landing gear, wheels, and brake systems.

SECTION II GROUND HANDLING, SERVICING, AIRFRAME MAINTENANCE

GENERAL DESCRIPTION

Standard procedures for ground handling, servicing, and airframe maintenance.

GROUND HANDLING

Procedures for towing, taxiing, parking, mooring, and jacking the aircraft.

GROUND EMERGENCY PROCEDURES

Steps to follow in case of engine or electrical emergencies on the ground.

GROUND OPERATION OF ENGINE

Procedures for operating the engine on the ground.

SYSTEM AND COMPONENT SERVICING

Maintenance actions performed with routine frequency.

AIRFRAME MAINTENANCE

Procedures for airframe sealing, fiberglass repair, and structural repair.

SECTION III HYDRAULICS

GENERAL DESCRIPTION

Overview of the aircraft's hydraulic system.

GENERAL MAINTENANCE PRACTICES

Essential cleanliness and practices for hydraulic system maintenance.

HYDRAULIC SYSTEM COMPONENTS

Details on key components like actuating cylinders and power packs.

FUNCTIONAL TEST PROCEDURE

Procedure for performing operational checks on the landing gear system.

HYDRAULIC POWER PACK

Description and servicing of the hydraulic power pack unit.

TROUBLE SHOOTING

Troubleshooting common issues in the hydraulic system.

SECTION IV POWER PLANT AND PROPELLER

GENERAL DESCRIPTION

Overview of the aircraft's engine and propeller.

IGNITION SYSTEM

Details on the ignition switch, operation, magnetos, and harness.

FUEL INJECTION SYSTEM

Description of the fuel injection system, including servo regulator.

OIL SYSTEM

Information on the engine oil system, cooler, and filters.

ENGINE CONTROLS

Description and rigging of throttle, mixture, and propeller controls.

PROPELLER

Information on propeller removal, installation, and governor.

SECTION V FUEL SYSTEM

GENERAL DESCRIPTION

Description of fuel storage in wing tanks and servicing ports.

MAINTENANCE PRECAUTIONS

Safety precautions for performing fuel system maintenance.

FUEL QUANTITY INDICATING SYSTEM

Components and calibration of the fuel quantity system.

AUXILIARY FUEL PUMP

Details on the electric auxiliary fuel pump and its function.

GASCOLATOR

Information on the gascolator, its screen, removal, and cleaning.

TROUBLE-SHOOTING

Troubleshooting common fuel system issues.

SECTION VI LANDING GEAR, WHEELS AND BRAKES

GENERAL DESCRIPTION

Overview of the tricycle landing gear, nose wheel steering, and brakes.

OPERATIONAL CHECK

Procedure for checking landing gear retraction and extension systems.

MAIN LANDING GEAR

Details on main landing gear removal, installation, and oleo servicing.

NOSE LANDING GEAR

Procedures for nose gear removal, installation, and shimmy dampener.

WHEELS AND BRAKES

Information on wheel assemblies, tires, and brake systems.

TROUBLE SHOOTING

Troubleshooting common issues related to landing gear, wheels, and brakes.

SECTION VII FLIGHT CONTROLS

GENERAL DESCRIPTION

Description of all-metal flight control surfaces and systems.

MAINTENANCE OF FLIGHT CONTROLS

Careful procedures for control system maintenance and rigging.

FLIGHT CONTROL SYSTEMS

Details on control column, ailerons, rudder, and elevator systems.

CONTROL SURFACE BALANCING

Procedures for balancing flight control surfaces for optimal performance.

TROUBLE SHOOTING

Troubleshooting common issues in the flight control systems.

SECTION VIII INSTRUMENTS

GENERAL DESCRIPTION

Overview of the standard equipment instrument installation.

INSTRUMENT SYSTEM MAINTENANCE

Field maintenance procedures for instruments and systems.

FLIGHT INSTRUMENTS

Description of magnetic compass, airspeed, altimeter, and gyros.

PITOT-STATIC SYSTEM

Details on the pitot-static system and its maintenance.

POWER PLANT INSTRUMENTS

Instruments monitoring engine operation and condition.

TROUBLE SHOOTING INSTRUMENTS

Troubleshooting common instrument malfunctions.

SECTION X ELECTRICAL

GENERAL DESCRIPTION

Overview of the aircraft's 14-volt DC electrical system.

POWER DISTRIBUTION

Description of electrical power sources and distribution.

ALTERNATOR SYSTEM

Details on the alternator, voltage regulator, and protection circuits.

CIRCUIT BREAKERS

Diagrams and identification of aircraft circuit breakers.

ELECTRICAL SYMBOLS

Key to schematic symbols used in wiring diagrams.

PART III DIAGRAMS

Electrical wiring diagrams applicable to specific aircraft serial numbers.