AIRWORTHINESS DIRECTIVES FINAL RULES: 72-22-01

CITATION: This information is not available.

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DOCKET NUMBER: Unknown

AMENDMENT: 39-1544

AD NUMBER: 72-22-01

SUBJECT HEADING: Airworthiness Directives; BEECH Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35TC, V35A, V35A-TC, V35B and V35B-TC, 36, A36, A45(T-34A), B45, D45(T-34B), 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 95, B95, B95A, D95A, and E95 Airplanes

ACTION:

SUMMARY:

DATES: Effective October 25, 1972.

ADDRESSES:

FOR FURTHER INFORMATION CONTACT:

SUPPLEMENTARY INFORMATION:

REGULATORY TEXT:
72-22-01 BEECH: Amendment 39-1544. Applies to the following:

Models	Serial Numbers
35-33, 35-A33, 35-B33, 35-C33, E33, F33, and G33	CD-1 thru CD-1256

35-C33A, E33A and F33A	CE-1 thru CE-349

E33C and F33C	CJ-1 thru CJ-30

35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35TC, V35A, V35A-TC, V35B and V35B-TC	D-1 thru D-9287

36 and A36	E-1 thru E-283

A45(T-34A), B45 and D45(T-34B)	All

95-55, 95-A55, 95-B55 and 95-B55A	TC-1 thru TC-1402

95-C55, 95-C55A, D55, D55A, E55 and E55A	TE-1 thru TE-846

56TC and A56TC	TG-1 thru TG-94

58	TH-1 thru TH-174

95, B95, B95A, D95A, and E95	TD-2 thru TD-721

Compliance: Required as indicated, unless already accomplished:

To decrease the possibility of gear-up landings caused by seizure of the uplock rollers, accomplish the following:

A) Within the next 300 hours' time in service after the effective date of this AD, determine if each uplock roller is of the greasible type (one having a drilled and grooved inner race) and replace any nongreasible uplock roller (one having a solid inner race) with the greasible type prior to further flight.

NOTE: This determination may be made by lubricating the uplock rollers and verifying that grease passes between the inner and outer races.

B) Within the next 300 hours' time in service after the effective date of this AD, install hollow zerk-ended mounting bolts on the uplock rollers in accordance with Beech Service Instructions No. 0448-211 or any FAA-approved equivalent.

C) Within the next 300 hours' time in service after the effective date of this AD, and thereafter at 100 hour intervals, lubricate the uplock mechanism in accordance with Beech Service Instruction No. 0448-211.

This AD supersedes AD 72-17-02 (Amendment 39-1501).

This amendment becomes effective October 25, 1972.

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