AD 74-21-04

Airworthiness directive · Canopy Slats · Schweizer 269A, 269A-1, 269B and 1 more

Effective
April 4, 1975
Models
269A, 269A-1, 269B, 269C
Data sheet
TCDS4H12
Registered aircraft
330 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-1987

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.

On this page

The airworthiness directive

74-21-04 HUGHES HELICOPTERS: Amendment 39-1987 as amended by Amendment 39-2147. Applies to Hughes 269A, 269A-1, 269B, 269C Helicopters certificated in all categories, including military TH-55A equipped with canopy slat P/N 269A2297 or 269A2297-7.

Compliance required as indicated.

To detect possible cracks in canopy slat surfaces, and the condition and security of slat attachment hardware and canopy attachment areas, and provide for modification of the canopy slat, accomplish the following:

(a) On each day the helicopter is flown, conduct a close visual check by the pilot in command or an inspection by a certificated mechanic of the canopy slat surfaces over the entire length for cracks, slat attachment hardware and canopy attachment areas for condition and security. Note: The person who performs the check or inspection shall record it in the appropriate aircraft records per FAR 91.173.

(1) If cracks or other damage are found, replace prior to further flight with:

(i) P/N 269A2297 or 269A2297-7 modified in accordance with (b), below; or

(ii) P/N 269A2214; or

(iii) If the 50 hour limitation specified by (b), below, has not been exceeded, an unmodified part P/N 269A2297 or 269A2297-7 may be used, provided, it is modified at the time specified by (b), below; or

(iv) A part approved by Chief, Aircraft Engineering Division, FAA Western Region.

(b) Prior to the next 50 hours time in service after the effective date of this amendment, 39-2147, unless already accomplished, modify the canopy slat, P/N 269A2297 or 269A2297-7, in accordance with the instructions contained in Hughes Service Information Notice N-127, dated March 5, 1975, or later FAA-approved revisions, or equivalent procedure approved by the Chief, Aircraft Engineering Division, FAA Western Region.

(c) Upon installation of P/N 269A2297 or 269A2297-7 modified in accordance with (b), above, or P/N 269A2214 or other part approved by the Chief, AircraftEngineering Division, FAA Western Region, the daily visual check or inspection in accordance with (a) above may be discontinued.

Amendment 39-1987, was effective October 16, 1974, for all persons except those to whom it was made effective immediately by airmail letter dated September 23, 1974.

This Amendment 39-2147, to AD 74-21-04 becomes effective April 4, 1975.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 330

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Hughes207 aircraft
  • Schweizer120 aircraft
  • Schweizer RSG3 aircraft
By year built
19522025
Registered aircraft by year built: 242 aircraft
19521
19612
196210
196312
196417
196511
196612
19676
19688
19696
19703
19714
19733
19747
19752
19762
197710
19785
19797
19803
19814
19841
19852
19864
19873
19887
19896
19903
19916
19923
19932
19948
19953
19965
19977
19981
19993
20002
20015
20026
20032
20041
20052
20062
20073
20089
20094
20104
20231
20241
20251

88 with no year recorded

By model

Aircraft

See all 330 aircraft