- Effective
- November 25, 1998
- Published
- October 22, 1998 · 63 FR 56547–56548
- Issued
- October 15, 1998
- Models
- PA-23-235, PA-23-250, PA-23-250 (Navy UO-1), PA-E23-250
- Data sheet
- TCDS1A10
- Registered aircraft
- 924 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-10852
- Docket
- 82-CE-36-AD
- Issued as
- Final rule; correction
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 118 KB | 66d9484c…9c4bfd6 | 98-28301.pdf on govinfo.gov |
| FAA DRS HTML | 53 KB | 790afe85…a872fdd | FAA DRS (API key needed) |
| Federal Register text | 14 KB | 10b2ad0b…2f83c85 | 98-28301.txt on federalregister.gov |
On this page
Summary
This amendment clarifies information contained in Airworthiness Directive (AD) 83-22-01, which currently requires inserting certain zero fuel weight limitations into the Limitations Section of the airplane flight manual (AFM) on certain The New Piper Aircraft, Inc. (Piper) Models PA-23-235, PA-23-250, and PA-E23-250 airplanes. The FAA has received reports that reference in the AD to two of the AFM reports contains incorrect information. In particular, reference to Report 1308, Revision B, contains the words "normally aspirated"; and reference to Report 1360, Revision B, contains the word "Turbocharged." These references should be removed. This document clarifies AD 83-22-01 by removing the words "normally aspirated" and "Turbocharged" from the reference to these reports. The actions specified in this AD are intended to continue to prevent possible wing structure damage caused by excessive fuel weight, which could result in loss of control of the airplane.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
Supplementary information
Discussion AD 83-22-01, Amendment 39-4758, currently requires inserting certain zero fuel weight limitations into the Limitations Section of the airplane flight manual (AFM) on The New Piper Aircraft, Inc. (Piper) Models PA-23-235, PA-23-250, and PA-E23-250 airplanes. These limitations are included in the following reports:
Airplane Model Serial Numbers Report PA-23-235 27-505 through 27-622 Report 1207, Rev. B PA-23-250 27-1 through 27-1999 Report 1036, Rev. B PA-23-250 27-2000 through 27-2504 Report 1204, Rev. C PA-23-250 27-2505 through 27-3836; and 27-3838 through 27-3943 Report 1308, Rev. B (4800 lbs. Gross weight) PA-23-250 27-2505 through 27-3836; and 27-3838 through 27-3943 Report 1360, Rev. B (5200 lbs. Gross weight) PA-23-250 27-3837, 27-3944 through 27-4425, and 27-4427 through 27-4523 Report 1520, Rev. B PA-23-250 27-4426, 27-4574 through 27-7554168 Report 1630, Rev. 17 PA-23-250 7654001 and up Report 1948,Rev. 13 PA-E23-250 27-2505 through 27-3836, and 27-3838 through 27-3943 Report 1378, Rev. B PA-E23-250 27-3837, 27-3944 through 7-4425; and 27-4427 through 27-4573. Report 1521, Rev. B PA-E23-250 27-4426 and 27-4574 through 27-7554168 Report 1631, Rev. B PA-E23-250 27-7654001 and up Report 2049, Amendment 5
Need for the Correction The FAA has received reports that reference in the AD to two of the AFM reports contains incorrect information. In particular, reference to Report 1308, Revision B, contains the words "normally aspirated"; and reference to Report 1360, Revision B, contains the word "Turbocharged." Both of these reports apply to both normally aspirated and turbocharged airplanes.
Consequently, the FAA has determined that there is a need to clarify AD 83-22-01 to eliminate any confusion concerning the particular report that the owners/operators of the affected airplanes need to incorporate into their AFM.
Correction of Publication This document clarifies the intent of AD 83-22-01 by eliminating reference to "normally aspirated" and "Turbocharged" in the applicable reports. This document also adds the amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).
Since this action only clarifies the intent of AD 83-22-01, it has no adverse economic impact and imposes no additional burden on any person than would have been necessary by the existing AD. Therefore, the FAA has determined that prior notice and opportunity for public comment are unnecessary.
List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39 - AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701.
39.13 [Amended] 2. Section 39.13 is amended by removing Airworthiness Directive (AD) 83-22-01, Amendment 39-4758, and by adding a new AD to read as follows:
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 924
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1953 | 1 |
|---|---|
| 1960 | 33 |
| 1961 | 13 |
| 1962 | 24 |
| 1963 | 31 |
| 1964 | 28 |
| 1965 | 45 |
| 1966 | 60 |
| 1967 | 31 |
| 1968 | 39 |
| 1969 | 49 |
| 1970 | 19 |
| 1971 | 24 |
| 1972 | 27 |
| 1973 | 44 |
| 1974 | 49 |
| 1975 | 36 |
| 1976 | 52 |
| 1977 | 35 |
| 1978 | 36 |
| 1979 | 46 |
| 1980 | 11 |
| 1981 | 10 |
| 1995 | 1 |
180 with no year recorded