AD 89-20-13

Airworthiness directive · Horizontal Stabilizer · Bell Helicopter Textron Canada 206L, 206L-1 and 206L-3

Effective
October 15, 1991
Models
206L, 206L-1, 206L-3
Data sheet
TCDSH2SW
Registered aircraft
318 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-8027
Docket
89-ASW-49

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

89-20-13 BELL HELICOPTER TEXTRON, INC. (BHTI): Amendment 39-8027. Docket No. 89-ASW-49. Final Rule of priority letter AD.

Applicability: All Model 206L, 206L-1, and 206L-3 helicopters, all serial numbers, certificated in any category.

Compliance: Required before further flight, unless already accomplished.

To prevent failure and separation of the horizontal stabilizer from the helicopter, which could result in a strike on the tail rotor, causing loss of control of the helicopter, accomplish the following:

(a) Visually inspect to determine if the horizontal stabilizer installed on the helicopter has the required raised external doubler. The doubler is visible on the top of the stabilizer surface extending approximately 4 inches outward from either side of the tailboom and covering the upper surface of the horizontal stabilizer from within one half inch of the forward leading edge to the trailing edge.

(b) If the horizontal stabilizer installed does nothave the required external doubler, remove and replace the stabilizer with an airworthy part before further flight. The addition of an external doubler to the Helicomb International part will not bring the horizontal stabilizer into conformity with the approved type design and will not provide an equivalent level of safety.

(c) Report the registration number of the affected helicopter and the serial number of the discrepant stabilizer if found. This report is to be made to the Manager, Rotorcraft Certification Office, ASW-170, Southwest Region, Federal Aviation Administration, Fort Worth, Texas 76193-0170, telephone (817) 624-5170, within l0 days of the inspection. (Reporting approved by the Office of Management and Budget under OMB No. 2120-0056.)

(d) An alternate method of compliance which provides an equivalent level of safety, may be used if approved by the Manager, Rotorcraft Certification Office, Southwest Region, Federal Aviation Administration, Fort Worth, Texas 76193-0170, telephone (817) 624-5170.

This amendment (39-8027, AD 89-20-13) becomes effective on October 15, 1991, as to all persons except those persons to whom it was made immediately effective by Priority Letter AD 89-20-13, issued October 4, 1989, which contained this amendment.

Affected TCDS · 1

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

Registered aircraft · 318

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
  • Bell165 aircraft
  • Bell Helicopter Textron149 aircraft
  • Bell Helicopter Textron Canada4 aircraft
By year built
19751999
Registered aircraft by year built: 262 aircraft
19751
19761
19772
19789
197921
198041
198126
198217
198323
19847
198510
19867
19872
19886
198910
199026
199135
199217
19991

56 with no year recorded

By model

Aircraft

See all 318 aircraft