1953-1962 Cessna 150, 172, 175, 180, 182, and 185 Series Single-Engine Aircraft Service Manual (P/N D-138-13-GRIT)
Cessna Models Covered & Key Technical Specifications
Models: Cessna 150, 172, 175, 180, 182, 185
Sub-models / Variants: 150A, 150B, 172A, 172B, 172C, 175A, 175B, 175C, 180A, 180B, 180C, 180D, 180E, 182A, 182B, 182C, 182D, 182E, 185A
Trade Names: Skyhawk, Skylark, Skylane, Skywagon
Model Years: 1953–1962
Serial Numbers: 150: 17001 thru 15059351 & on; 172: 28000 thru 17248735 & on; 175: 55001 thru 17557003 & on; 180: 30000 thru 18051064 & on; 182: 33000 thru 18253599 & on; 185: 185-0001 thru 185-0238 & on
Technical Data:
- Engine oil capacities: 6 to 12 quarts depending on model
- Fuel capacities: 26 to 65 gallons
- Main wheel tire pressure: 23 to 35 psi
- Nose wheel tire pressure: 26 to 45 psi
- Engine models: Continental O-200-A, O-300-A/C/D, GO-300-A/C/D/E, O-470-A/J/K/L/R, IO-470-F
Cessna Manual Features & Content Preview
- Complete 508-page original OEM publication D-138-13-GRIT-1500, published February 1, 1962
- Covers 1953–1962 Cessna 150, 172, 175, 180, 182, and 185 single-engine aircraft
- Includes Skyhawk, Skylark, Skylane, and Skywagon variants
- Contains 47 exploded-view diagrams detailing airframe, landing gear, and cabin components
- Features 20 sections spanning general descriptions, ground handling, fuselage, and structural repair
Operational and Maintenance Coverage
This service manual documents factory procedures for ground handling, servicing, lubrication, and inspection. Mechanics can reference clear guidance for the entire 150 through 185 lineup. It details fuselage component teardowns, highlighting window installations, cabin doors, and seating mechanisms.
Sections four and five focus on airframe and landing gear maintenance. You will find comprehensive diagrams for wing structures, tail sections, and shock strut servicing. The documentation also outlines structural repair criteria alongside exterior painting requirements. This equips restoration shops with the exact factory references needed to maintain historic airframes.
Specification Highlights
Technical data covers aircraft weight, engine model variants, and wheel alignment parameters. Main gear positive camber ranges from 3° to 7°, depending on the specific model and serial number.
The manual lists precise torque values. Recommended fine-thread torque for 1/4-28 tension-type nuts is specified at 50–70 inch-pounds. Nose gear shock strut inflation sits at 35 psi for the Model 150 and 50 psi for the Model 182. Reference stations are provided in Section 1 to assist in precise positioning during maintenance. As with all historic aviation documents, the data shown in this overview is for reference only. Certified technicians must verify all procedures directly against the full OEM publication before initiating any hands-on shop work.
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