- Effective
- May 11, 1964
- Models
- D-16, D-16A
- Data sheet
- TCDS2A1
- Registered aircraft
- 10 matched by model
- Product
- Aircraft · Small airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 20 KB | 6681c7ea…cfdff9a | FAA DRS (API key needed) |
On this page
The airworthiness directive
64-08-04 UNIVERSAL: Amdt. 712 Part 507 Federal Register April 8, 1964. Applies to All Models Temco D-16 and D-16A Aircraft. Compliance required within 50 hours' time in service after the effective date of this AD. As a result of instances of cracking of nose gear support braces (Navion P/N 145-34161) and channel drag brace supports (Navion P/N 145-34204) installed on D-16 and D-16A aircraft accomplish the following: (a) On D-16 aircraft, visually inspect Navion P/N 145-34161 for cracks. If cracks are found, replace cracked part with a new part of the same number. In all cases, add Temco P/N 5531A cap nose gear drag brace or FAA approved equivalent, and replace Navion P/N 145-34204 with Universal P/N TN 5980A or FAA approved equivalent. Perform this rework in accordance with Temco Drawing TN 5505 or FAA approved equivalent. (b) On D-16A aircraft, replace Navion P/N 145-34204 with Universal P/N TN 5980A or FAA approved equivalent. (Universal Aircraft Service Bulletin No. 14 covers the same subject.) This directive effective May 11, 1964.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 10
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1946 | 1 |
|---|---|
| 1947 | 3 |
| 1948 | 3 |
3 with no year recorded