Beechcraft Debonair & Bonanza 33 Series, CD-1 through CJ-148 1960-1989 Shop Manual (P/N 33-590011-1C)
Beechcraft Models Covered & Key Technical Specifications
Models: Beechcraft 33, Beechcraft A33, Beechcraft B33, Beechcraft C33, Beechcraft C33A, Beechcraft E33, Beechcraft E33A, Beechcraft E33C, Beechcraft F33, Beechcraft F33A, Beechcraft F33C, Beechcraft G33
Sub-models / Variants: Debonair 33 Series, Bonanza 33 Series
Model Years: 1960–1989
Serial Numbers: CD-1 through CD-1304, CE-1 through CE-771, CJ-1 through CJ-148
Technical Data:
- Engine models: Continental IO-470-J, IO-470-K, IO-470-N, IO-520-B, IO-520-BA, IO-520-BB
- Engine power: 225 hp to 285 hp
- Operating RPM: 2600 to 2700 rpm
- Landing gear tire sizes: 5.00-5 (nose), 6.00-6 and 7.00-6 (main)
- Aileron static balance: Must be nose-heavy by 0.2 to 1.5 inch-pounds
- Rudder static balance: 8.4 inch-pounds maximum
- Elevator static moment allowance (prior to CD-1023): 12.0 inch-pounds
- Elevator static moment allowance (CD-1023 and after): 7.8 inch-pounds
- Electrical systems: 14-volt or 28-volt configurations
Beechcraft Manual Features & Content Preview
- Covers 1960–1989 Beechcraft Debonair and Bonanza 33 Series airframes, including variants CD-1 through CJ-148.
- Official Beechcraft shop publication P/N 33-590011-1C (revised May 22, 1989).
- Features 175 technical illustrations, 12 electrical system schematics, and 8 comprehensive maintenance sections.
- Integrates all service bulletins and modification notes for the final production run of the 33 series line.
Manual Coverage
This 340-page publication serves as the core technical reference for the Beechcraft Debonair and Bonanza 33 series. It outlines major disassembly and maintenance parameters for both airframes and internal systems. Coverage begins with general aircraft information. From there, it progresses into detailed system breakdowns, major component overhaul outlines, and an extensive index of wiring diagrams. Shop planners will also find essential replacement schedules and periodic inspection requirements clearly documented to streamline workshop routines.
Specification and Reference Data
Inside this 1960–1989 manual, technicians will find precise station diagrams, skin plating thicknesses, and exact component adjustment values. Elevator static moment allowance, for example, is listed as 12.0 inch-pounds for airplane serials prior to CD-1023. Rudder static balance reaches a documented maximum of 8.4 inch-pounds. The 1989 revision is particularly useful for verifying Continental IO-470 and IO-520 series engine setups. It highlights critical torque values for wing bolts alongside landing gear motor installation settings. Aviation maintenance demands absolute precision and strict adherence to approved protocols. All service data referenced here provides an overview of the manual's contents; certified mechanics must consult the complete OEM documentation prior to executing any hands-on adjustments or repairs.
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