AD 80-17-05

Airworthiness directive · Tail Rotor Blades · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 2 more

Effective
September 10, 1980
Models
206A, 206A-1 (OH-58A), 206B, 206B-1, 206L
Data sheet
TCDSH2SW
Registered aircraft
867 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-3875
Docket
80-ASW-18

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.

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The airworthiness directive

80-17-05 BELL: Amendment 39-3875. Applies to Models 206A, 206B, 206A-1, 206B-1, and 206L helicopters equipped with tail rotor blades, P/N 206-010-750-005 and -007, certificated in all categories (Airworthiness Docket No. 80-ASW-18).

Compliance required as indicated.

To prevent possible failure of tail rotor blades, P/N 206-010-750-005 and -007, due to fatigue cracks, accomplish the following:

a. Before the first flight of each day after the effective date of this AD, visually check for chordwise cracks in the tail rotor blade skin surfaces in the area between Blade Station 7.1 and 11.1 using a three-power or higher magnifying glass. (Blade Station 0 is the center of the tail rotor yoke.)

b. Replace tail rotor blades having cracks before further flight.

c. Blades with 450 or more hours' time in service (as calculated in paragraph (e) below) on the effective date of this AD must be removed from service within the next 50 hours' time in service.

d. Blades with less than 450 hours' time in service (as calculated in paragraph (e) below) on the effective date of this AD must be removed from service prior to or on attaining 500 hours' time in service.

e. For purposes of this AD, hours' time in service is calculated by the following formula:

Time on 206A/B Series + Time on 206L = Calculated Time in Service 2.4

f. The check required by paragraph (a) of this AD may be performed by the pilot, providing the pilot's logbook has been endorsed by a properly rated mechanic stating that the pilot has been trained to conduct the daily check in accordance with this AD.

NOTE: For the requirements regarding the listing of compliance with this AD in the aircraft maintenance record, see FAR 91.173.

(Bell Helicopter Textron Operations Safety Notice No. 206-79-5/206L-79-2, dated December 4, 1979; Alert Service Bulletin Nos. 206-80-6 dated February 22, 1980, and 206L-80- 8, Rev. A, dated June 3, 1980; and Technical Bulletin Nos. 206-78-3 dated July 18, 1978, and 206L-79-38 dated September 28, 1979, pertain to this subject.)

This amendment becomes effective September 10, 1980.

Affected TCDS · 1

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

Registered aircraft · 867

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
  • Bell828 aircraft
  • Bell Helicopter Textron29 aircraft
  • Bell Helicopter Textron Canada10 aircraft
By year built
19542009
Registered aircraft by year built: 713 aircraft
19541
19661
19675
196816
196912
19707
197115
197222
197325
197439
197539
197635
197730
197840
197948
198047
198152
198227
19835
19847
19855
19865
19874
198811
198914
19907
19919
19926
199324
199438
199547
19964
19976
19985
19994
20006
200113
20027
20033
20042
20055
20066
20075
20083
20091

154 with no year recorded

By model

Aircraft

See all 867 aircraft