AD 91-20-10

Airworthiness directive · Main Rotor Grip · Scotts-Bell 47 47G-2, 47G-2A, 47G-2A-1 and 11 more

Effective
November 14, 1991
Models
47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B-1, 47G-3B-2 and 8 more
Registered aircraft
354 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-8044
Docket
90-ASW-11

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

91-20-10 BELL HELICOPTER TEXTRON, INC.: Amendment 39-8044. Docket No. 90- ASW-11.

Applicability: All Model 47G2, 47G2A, 47G2A1, 47G3, 47G3B1, 47G3B2, 47G3B2A, 47G4, 47G4A, 47G5, 47G5A, 47J, 47J2, and 47J2A helicopters, certificated in any category, with main rotor (M/R) grip part number (P/N) 47-120-252-11, installed.

Compliance: Required within the next 50 hours' time in service after the effective data of this AD, unless already accomplished.

To prevent failure of the M/R grip, which could result in loss of control of the helicopter, accomplish the following:

(a) Visually inspect the M/R grip and determine if one of the following serial numbers is installed:

IT- 0251, 0253, 0254, 0255, 0256, 0257, 0260, 0261, 0262, 0263, 0264, 0265, 0267, 0268, 0270, 0271,0272, 0273, 0274, 0275, 0276, 0277, 0278, 0279, 0280, 0281, 0282, 0284, 0285, 0286, 0289, 0290, 0291, 0293, 0294, 0295, 0296, 0297, 0299, 0300, 0302, 0303, 0306, 0308, 0312, 0313, 0315, 0316, 0317,0319, 0323, 0324, 0326, 0327, 0328, 0329, 0330, 0333, 0334, 0335 ITM- 0005, 0007, 0022, 0046, 0077, 0096, 0109, 0112, 0114, 0115, 0125, 0128, 0133, 0155, 0161, 0165, 0166, 0167, 0168, 0170, 0171, 0178, 0182, 0183, 0185, 0187, 0189, 0191, 0192, 0194, 0197, 0198, 0202, 0204, 0211, 0212, 0218, 0234, 0235, 0236, 0237, 0238, 0239, 0240, 0241, 0242, 0243, 0244, 0245, 0246, 0248, 0249, 0250, 0251, 0252, 0253, 0255, 0256, 0257, 0258, 0259, 0261, 0262, 0263, 0264, 0265, 0266, 0267, 0269, 0270, 0271, 0272, 0273, 0274, 0275, 0276, 0277, 0278, 0279, 0280, 0281, 0282, 0283, 0284, 0286, 0287, 0288, 0289, 0290, 0291, 0292, 0293, 0294, 0295, 0296, 0297

(b) If one of the M/R grips listed in paragraph (a) is installed, remove and replace with a serviceable part.

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

NOTE: If any of the M/R grips identified in paragraph (a) are found, either installed or as spares, the FAA recommends that the parts be permanently marked or defaced so that they cannot be misconstrued as airworthy.

This amendment (39-8044, AD 91-20-10) becomes effective on November 14, 1991.

Affected TCDS · 3

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

Registered aircraft · 354

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
  • Bell347 aircraft
  • Bell-Huddleston And Wilson1 aircraft
  • Bell-Intermountain1 aircraft
  • Bell-K-Copter1 aircraft
  • Bell-Olympic Helicopters1 aircraft
  • Other makers33 aircraft
By year built
19482010
Registered aircraft by year built: 260 aircraft
19482
19511
19531
19541
19551
195610
195713
195816
19597
19608
19616
19628
196312
196416
196516
196632
196726
196820
196911
19708
197112
197213
197310
19744
19752
19761
19801
19811
20101

94 with no year recorded

By model

See all 20 models

Aircraft

See all 354 aircraft