AD 63-10-01

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Model C-82A and C-82A Jet Packet Aircraft

AD Number
63-10-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Steward-Davis Incorporated C-82A Airworthiness Directives; Fairchild Model C-82A and C-82A Jet Packet Aircraft
aircraft Steward-Davis Incorporated C-82A Jet Packet Airworthiness Directives; Fairchild Model C-82A and C-82A Jet Packet Aircraft

Unsafe Condition

Premature wear in the bushings of the original rear heavyweight crankshaft vibration dampers in R-2800 'C' Series engines reduces crankshaft damping characteristics, causing propeller blade vibration stresses above safe limits. Flight operations at gross weights over 36,500 pounds with unmodified 6491-0 propeller blades also impose excessive vibration stresses.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Install a placard on the instrument panel and apply red arc tachometer markings to avoid 1,550-1,650 r.p.m. operations. Replace crankshaft assemblies with P/N 326054 or engines with CA/CB crankshafts within specified time limits. Modify or replace 6491-0 propeller blades and rework propeller hub components per specified procedures, or revise operating limitations to restrict gross weight and power.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Compliance required as indicated in the AD: (a) within 100 hours' time in service after June 6, 1963; (b) within 300 hours' time in service after June 6, 1963 (or prior to 650 hours since new/overhaul for engines with <350 hours as of June 6, 1963); (c) and (d) within 300 propeller hours' time in service after June 6, 1963; (e) no time specified but must be done prior to propeller modifications if choosing weight/power restrictions.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Steward-Davis Incorporated C-82A and C-82A Jet Packet aircraft with Pratt & Whitney R-2800 C, CA, or CB Series engines and Hamilton Standard 33E60/6491-0 or 33E60/6801-0 propellers.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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