# AD 51-15-02: Crankcase

- Type: Airworthiness directive
- Status: Current
- Products: Wytwornia Sprzetu Komunikacyjnego 6A4-165-B3
- Superseded by: Nothing supersedes this AD
- Product type: Engine
- Registered aircraft: 770 may be affected, by airframe or engine model (OpenAirDocs)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CDD17304E35B3D348625682B00618E6B.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/51-15-02

## The airworthiness directive

51-15-02 FRANKLIN: Applies to All Franklin 6A4-165-B3 Engines Serially Numbered 33046 and Below Incorporating Original Crankcase (Left Half No. 18305; Right Half No. 18306). These Two Parts Form Crankcase Assembly, P/N 18553. The Number of Each Crankcase Half is Located on Each Casting Below the Number 1 and 6 Cylinder Location. To be accomplished by July 15, 1951. Effective on and after this date, all applicable crankcases with 500 hours of operation since new or 250 hours since last overhaul should be inspected as follows: Remove crankcase cover and visually inspect the webbing near the main journal area for cracks. (1) Crankcases found to be free of cracks should be inspected at 250-hour intervals thereafter. In the event that the conditions described in (2) and (3) are detected, the provisions of (2) and (3) will apply. (2) Crankcases found with (a) surface indications, hairline cracks, or small wall cracks and (b) cracks starting at main bearing stud hole on the opposite side from main bearing support, may be operated further at the option of the owner. Such crankcases should be inspected at 50-hour intervals thereafter to determine progress of cracks. (3) Crankcases found fractured or with cracks that have progressed to the extent that they enter the main bearing supports (usually from back near (a) main bearing stud hole and (b) drilled oil hole) indicate that a complete break soon will occur. Such crankcases should be replaced with the reinforced crankcase assembly, P/N 18925, at which time no further inspection is required. Crankcase assembly P/N 18925 may be identified by casting No. 18905 appearing below No. 1 cylinder location and casting No. 18906 appearing below No. 6 cylinder location. (Franklin Service News No. 10 also covers this subject.)

## Affected data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS E-238](https://openairdocs.org/tcds/E-238): Franklin Sp. z.o.o.; names 1 of 7 models: 6A4-165-B3

## Registered aircraft it may apply to (OpenAirDocs)

Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment.

- Aircraft: 770 (0 by airframe model, 770 by engine model)
- Makers: Stinson 658, Universal Stinson 86, Bellanca 13, Cessna 5, Aeronca 4, Buck Robin F 1, Nord 1, Runyan 1, Temco 1

Models with the most aircraft:

- [Franklin 6A4165 series](https://openairdocs.org/engine/franklin-6a4165-series): 770 aircraft (engine model)

All 1 models: https://openairdocs.org/ad/51-15-02/models.md
Every aircraft: https://openairdocs.org/ad/51-15-02/aircraft.md

Its text cites no advisory circulars or STCs.

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