Cessna 152 Service Manual D2064-1-13: 1978-1985

D2064-1-13 is the service-manual family for the 1978-1985 Cessna 152. Base Revision 1 is dated 2 October 1995. Later temporary revisions address specific maintenance subjects, so the base edition date is not the date of every instruction within an amended manual. Check the page and amendment lists for the manual being used, then match the relevant task to the aircraft and installed components.

Lower engine installation and nosewheel strut of a Cessna 152
The lower engine area of a Cessna 152 with the cowling removed, including the nosewheel strut assembly. Photo: Brian Burger from Victoria, Canada · Wikimedia Commons · CC BY 2.0. Resized, WebP.
Publication details
Issuing organizationCessna
Publication numberD2064-1-13
Document typeService Manual
Related aircraft and subjectsCessna 152

Cessna 152 manual coverage

The manual supports maintenance research rather than replacing the aircraft’s approved operating material. Engine publications, propeller instructions and airworthiness directives also retain their own scope. A 152 maintenance-manual title alone does not establish every instruction needed for a modified aircraft or provide missing certified limits for a Reims F152 or FA152.

This distinction is especially useful when records use abbreviated references such as a manual section or SID number. The publication family helps locate the subject, but the applicable revision and aircraft effectivity still need to be established. A document title is the beginning of the investigation, not the completion of it.

Cessna 152 nosewheel, tire and exposed nose strut
A close view of Cessna 152 nose landing gear. The tire, wheel and strut can be examined as separate visible components. Photo: Flohlateiner · Wikimedia Commons · CC BY-SA 3.0. Resized, WebP.

Structural inspection and corrosion revision history

TR5, dated 1 December 2011, adds SIDs, corrosion-prevention material and control-cable inspection. TR6, dated 1 April 2012, revises landing/taxi-light switch limits and adds a beacon-switch limit. These changes concern different maintenance subjects; they should not be compressed into a single undated claim that the base manual contains all later information.

TR7, dated 1 May 2013, is particularly important because it deletes SID 55-11-01, Horizontal Stabilizer Forward Attachment, and revises corrosion maps. That history shows why the continued presence of an inspection number in an older copy is not sufficient evidence of its position in later instructions. A deleted subject must not be silently carried forward by copying an older checklist.

TR8, dated 18 May 2015, addresses vertical-fin inspection requirements and revised corrosion maps. TR9, dated 1 August 2019, adds the rudder-horn inspection subject and related changes. TR10, dated 1 August 2020, addresses corrosion-prevention definitions, reporting and a vertical-fin inspection operation page. This is a historical sequence; check the current manual and amendments before maintenance use.

Applicability and practical use

Read each temporary revision with the base manual and any other applicable amendments. In particular, distinguish a changed inspection subject from a superseded page or a deleted SID. The presence of an older inspection number in a maintenance checklist does not establish that the checklist reflects later instructions. Identify the actual publication and revision cited by the work entry before comparing it with present maintenance requirements.

For an ownership or prebuy investigation, connect the aircraft’s actual identity, equipment and maintenance program with the appropriate publications. Structural, flap, fuel and component subjects can lead to different source sections and regulatory questions. A broad claim that the manual was followed is less useful than records identifying the work, instructions, findings and resulting action.

The correct publication path is particularly important when comparing U.S. and Reims aircraft or evaluating a modification. Shared systems descriptions do not automatically establish shared approved limitations or installation instructions. Follow the applicable authority and manufacturer material for the actual aircraft, leaving unsupported relationships unresolved rather than filling them from the nearest family reference.

Left side of a Cessna 150H Continental O-200-A engine
Left-side view of the Continental O-200-A in a Cessna 150H. The cowling is removed to expose the installation. Photo: YSSYguy at English Wikipedia · Wikimedia Commons · CC BY-SA 4.0. Resized, WebP.

Related Aircraft and Technical Guides

Related Documents

Browse all Cessna 150 and 152 technical documents.