Cessna 172 Service Repair Manual 1969-1976 Cessna 172 Service Book

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🏷️ Basic Information Identification Make: Cessna Model: 172 Skyhawk Covered Years: 1969-1976 Generation: Pre-M (1969-1972) & M (1973-1976) 📋 Manual Details Documentation Manual Type: Service & Repair Manual Language: English...

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Tipo: Aircraft

Proveedor:

SKU: 27586

Etiquetas: 172 1969 1970 1971 1972 1973 1974 1975 1976 Aircraft Airplanes Cessna Other Vehicles

Variantes de producto

Descripción

🏷️ Basic Information

Identification

Make:

Cessna

Model:

172 Skyhawk

Covered Years:

1969-1976

Generation:

Pre-M (1969-1972) & M (1973-1976)

📋 Manual Details

Documentation

Manual Type:

Service & Repair Manual

Language:

English

Page Count:

Format:

Availability:

Instant Download

Printable:

Features

Illustrations:

Detailed Photos and Illustrations

Diagrams:

Exploded Diagrams and Drawings

Navigation:

Easy Identification of Procedures

⚙️ Engine Specifications

Powerplant 1969-1970

Engine Type:

Continental O-300

Displacement:

300 cu in (4.9 L)

Power:

145 hp (108 kW)

Powerplant 1968-1968 K

Engine Type:

Lycoming O-320-E2D

Power:

150 hp (112 kW)

Powerplant 1971-1972 L

Engine Type:

Lycoming O-320

Power:

150 hp (112 kW)

Powerplant 1973-1976 M

Engine Type:

Lycoming O-320

Power:

150 hp (112 kW)

🔧 Transmission

Propulsion

Type:

Fixed Pitch Propeller

Gears:

Direct Drive (Engine to Propeller)

📐 Dimensions

Airframe Weights 1969-1971

Max Gross Weight:

2,300 lb (1,043 kg)

Airframe Weights 1973-1976

Max Gross Weight:

2,400 lb (1,089 kg)

🔧 Maintenance

General

Focus:

Servicing, Repair, Preventative Maintenance

Objective:

Lower Repair and Maintenance Costs

📄 Model Specifics

Intro Year:

Initial Engine:

Continental O-300

Initial Power:

145 hp (108 kW)

Initial Gross Weight:

2,200 lb (998 kg)

Skylane Option:

Deluxe optional package for premium features

Gross Weight Increase:

2,250 lb (1,021 kg)

Design Change:

Omni-Vision rear window, one-piece windshield

Design Change:

Circuit breakers replaced fuses, redesigned instrument panel

Gross Weight:

2,300 lb (1,043 kg)

Design Change:

Electrically-operated flaps

Production Note:

Basis for USAF T-41A Mescalero trainer

Engine Upgrade:

Lycoming O-320-E2D (150 hp)

Instrument Panel:

Standard 'T' instrument arrangement

Landing Gear Change:

Tapered, tubular steel gear legs replace flat spring steel

Design Change:

Plastic fairing between dorsal and vertical fin

Wing Feature:

Drooped wing leading edge ('camber-lift' wing)

Optional Package:

'II' package with enhanced avionics

Designation Change:

Exclusively marketed as 'Skyhawk' from 1976