# AD 83-03-03: Tail Boom and Fin - Type: Airworthiness directive - Status: Current - Products: California Department of Forestry UH-1F, UH-1A, UH-1B, UH-1B, UH-1E, UH-1L, UH-1B and UH-1F - Effective: March 14, 1983 - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Rotorcraft - Amendment: 39-4556 - Registered aircraft: 2 may be affected, by airframe or engine model (OpenAirDocs) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C3DA0F0151E5885886256A4D0073B1AE.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/83-03-03 ## The airworthiness directive 83-03-03 GARLICK HELICOPTERS, HAWKINS & POWERS AVIATION, INC., WILCO AVIATION (BELL): Amendment 39-4556. Applies to Model UH-1 series helicopters certificated in restricted category. Compliance is required as indicated, unless already accomplished. To detect cracks and to prevent possible failure of the tail boom and fin, accomplish the following: Within the next 30 hours' time in service after the effective date of this AD: a. Conduct the following inspections: (1) Visually inspect the tail boom skin joint at tail boom Station 194 for fretting or cracking (inspect 10 inches forward and 10 inches aft of Station 194). (2) Visually inspect the vertical fin front spar cap at its intersection with the tail rotor gear box support fitting for cracks. (3) The areas to be inspected are shown in Figure 1. b. For aircraft found to have fretting or cracks by the inspections of paragraph a. above and for aircraft with more than 1,000 hours' time inservice, conduct a radiographic inspection of the tail boom Station 194 splice joint in accordance with Advisory Circulars 43-3 (Chapter 2) and 43-13-1A (paragraph 298) to MIL-STD-453 requirements, or FAA approved equivalent. c. After the initial inspections - (1) Visually inspect the tail boom skin and fin spar cap area in accordance with paragraph a. above, at intervals not to exceed 100 hours' time in service from the last radiographic inspection. (2) Radiographically inspect the tail boom skin in accordance with paragraph b. above at intervals not to exceed 500 hours' time in service from the last radiographic inspection. d. Replace cracked skin panels with serviceable panels. e. Replace cracked fin spar caps with serviceable parts. f. Any equivalent method of compliance with this AD must be approved by the Manager, Aircraft Certification Division, Southwest Region, Federal Aviation Administration. g. Upon request of the operator, an FAA maintenance inspector, subject to prior approval of the Manager, Aircraft Certification Division, FAA Southwest Region, may adjust the repetitive inspection intervals specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for that operator. h. In accordance with FAR 21.197, flight is permitted to a base where the inspections required by this AD may be accomplished. This amendment becomes effective March 14, 1983. ## Affected data sheets (2) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS H2NM](https://openairdocs.org/tcds/H2NM): California Department of Forestry; names 1 of 1 models: UH-1F - [TCDS H3SO](https://openairdocs.org/tcds/H3SO): Richards Heavylift Helo Inc.; names 1 of 4 models: UH-1A ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 2 (2 by airframe model, 0 by engine model) - Makers: Hawkins & Powers 2 Models with the most aircraft: - [Hawkins & Powers UH-1B](https://openairdocs.org/model/hawkins-powers-uh-1b): 2 aircraft (airframe model) All 1 models: https://openairdocs.org/ad/83-03-03/models.md Every aircraft: https://openairdocs.org/ad/83-03-03/aircraft.md Its text cites no advisory circulars or STCs. ## NTSB investigations that cite this AD (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB SEA96FA187](https://openairdocs.org/ntsb/SEA96FA187), Aug 12, 1996: Garlick UH-1H (N97NW), Coeur D'Alene, ID, substantial damage. Probable cause: Fatigue fracture of the left forward vertical stabilizer spar, resulting in loss of the vertical stabilizer and tail rotor and subsequent loss of control. A factor was insufficient applicability (by… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.