AD 60-07-02

Airworthiness directive · Tail Rotor Drive Shaft · Brantly International B-2, B-2A and B-2B

Models
B-2, B-2A, B-2B
Data sheet
TCDS2H2
Registered aircraft
53 matched by model
Product
Aircraft · Rotorcraft

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

60-07-02 BRANTLY: Amdt. 117 Part 507 Federal Register March 23, 1960. Applies to Model B-2 Helicopters.

Compliance required as indicated.

(a) Applies to Serial Numbers 1 through 31. Compliance required prior to next flight.

Failures of the tail rotor drive shaft through the cooling fan drive pulley bolt hole have occurred. These failures result in loss of directional control. To relieve stresses in this area and preclude recurrence of these failures, the tail rotor drive system must be modified to incorporate:

(1) New long tail rotor drive shaft P/N 108-31 incorporating 2 1/2-inch long plug pinned in forward end of shaft at support location for cooling fan drive pulley,

(2) Redesigned cooling fan drive pulley bearing support sleeve P/N 339-19,

(3) New cooling fan drive pulley P/N 339-4,

(4) New housing spacer P/N 339-18,

(5) New pin retainer P/N 339-17,

(6) New tail rotor shaft forward support bearing P/N 88505,

(7) New cooling fan attach bolt AN 173-14A with AN 960-10 washer and AN 365-1032 nut. (Brantly Service Bulletin No. 2 covers this same subject.)

Revised April 17, 1965.

Affected TCDS · 1

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

Registered aircraft · 53

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
  • Brantly53 aircraft
By year built
19591997
Registered aircraft by year built: 31 aircraft
19591
19601
19615
19622
19635
19646
19651
19664
19672
19682
19921
19971

22 with no year recorded

By model

Aircraft

See all 53 aircraft