- Effective
- September 27, 1982
- Models
- EMB-110P1, EMB-110P2
- Data sheet
- TCDSA21SO
- Registered aircraft
- 13 matched by model
- Product
- Aircraft · Small/large airplane
- Amendment
- 39-4440
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 | 2aed66c0…5507001 | FAA DRS (API key needed) |
On this page
The airworthiness directive
82-18-01 EMBRAER: Amendment 39-4440. Applies to EMB-110P1 and EMB-110P2 models (S/Ns 110001 through 110329 and 110331 through 110339), airplanes certificated in any category.
Compliance: Required on or before December 31, 1982, unless previously accomplished.
To prevent leakage of water into the fuel tank, accomplish the following:
(a) Defuel the airplane in accordance with the EMB-110 maintenance manual.
(b) Remove the fuel filler neck components from each tank and install EMBRAER Kit S.B. 110-28-020 in accordance with the instructions contained in EMBRAER Service Bulletin 110-28-020, dated July 2, 1981.
(c) An equivalent method of compliance may be used, if approved by the Chief, Atlanta Aircraft Certification Office, ACE-115A, Federal Aviation Administration, P.O. Box 20636, Atlanta, Georgia 30320.
This amendment becomes effective September 27, 1982.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 13
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1964 | 1 |
|---|---|
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 2 |
| 1982 | 4 |
| 1983 | 1 |
2 with no year recorded