AD 92-13-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-34-200 | Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-34-200, Model PA-34-200T Airplanes |
| aircraft | Piper Aircraft Inc. | PA-34-200T | Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-34-200, Model PA-34-200T Airplanes |
Unsafe Condition
The inability to fully extend the nose landing gear due to an incorrectly installed or non-compliant clevis-head bolt (P/N 400-910) or a hex-head bolt, which could result in loss of control during landing operations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the nose gear centering spring assembly to determine bolt type. If a P/N 400-910 clevis-head bolt is installed, ensure correct installation per Piper SB No. 893 and incorporate placard P/N 582-943. If incorrectly installed or a non-compliant bolt is present, disassemble, reinstall, or replace with the correct bolt per SB No. 893 and install the placard.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 100 hours time-in-service after the effective date of this AD
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Affected Aircraft
Piper Aircraft Corporation Model PA-34-200 (serial numbers 34-7250001 through 34-7450220) and Model PA-34-200T (serial numbers 34-7570001 through 34-8170092)
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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