AD 48-32-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Timm Aircraft Corporation | N2T-1 | Airworthiness Directives; Timm Models N2T and PT-220-C Aircraft |
| aircraft | Timm Aircraft Corporation | PT-220-C | Airworthiness Directives; Timm Models N2T and PT-220-C Aircraft |
Unsafe Condition
Throttle quadrants pulling off the fuselage skin to which they were glued and nailed during manufacture.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect front and rear cockpit throttle quadrants for looseness immediately. Repair loose quadrants prior to next flight. Install four AN 3 bolts with washers or metal backing plates at each corner of the wood plate, and reinforce as described or equivalently by January 1, 1949.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Reinforcements must be installed not later than January 1, 1949.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Timm Aircraft Corporation Models N2T All Serial Numbers and PT-220-C Aircraft.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.