| AD Number | 91-17-01 | Status | Active |
| Effective Date | November 25, 1991 | Issue Date | Not specified |
| Docket Number | 90-CE-71-AD | Amendment | 39-7099 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | 35-33 35-A33 35-B33 35-C33 35-C33A 36 45 (Military YT-34) 56TC 58 58A 58P 58PA 58TC 58TCA 95 95-55 95-A55 95-B55 95-B55A 95-C55 95-C55A A36 A36TC A45 (Military T-34A, B-45) A56TC B36TC B95 B95A D45 (Military T-34B) D55 D55A D95A E33 E33A E33C E55 E55A E95 F33 F33A F33C G33 T-34C |
91-17-01 BEECH: Amendment 39-7099. Docket No. 90-CE-71-AD.
Applicability: The following Model airplanes, certificated in any category:
Models
Serial Numbers
35-33, 35-A33, 35-B33,
CD-1 through CD-981 and
35-C33, E33, F33, G33
CD-983 through CD-1304
35-C33A, E33A, F33A
CE-1 through CE-235,
CE-249, CE-250, CE-256,
CE-260, CE-264 through CE-268, and
CE-270 through CE-1565
E33C, F33C
CJ-1 through CJ-179
36, A36
E-1 through E-2103, E-2105 through E-2110
A36TC, B36TC
EA-1 through EA-319, and EA-321 through
EA-388
T34C-1
GM-1 through GM-142
34C
GP-1 through GP-50
T-34C
GL-1 through GL-353
45
G-3 through G-6
A45
G-7 through G-156,
G-257 through G-306, G-696 through G-845,
CG-1 through CG-47, CG-58 through CG-60,
CG-68, CG-73, CG-75, CG-78, CG-79, CG-105,
CG-106, CG-108, CG-111 through CG-179,
CG-200 through CG-223, CG-279 through
CG-319
D45
BG-1 through BG-423
95
TD-2 through TD-302
B95
TD-303 through TD-452
B95A
TD-453 through TD-533
D95A
TD-534 through TD-707
E95
TD-708 through TD-721
95-55
TC-1 through TC-190
95-A55
TC-191 through TC-349, TC-351 through
TC-370, and TC-372 through TC-501
95-B55, 95-B55A
TC-371, TC-502 through TC-2456
95-C55
TC-350
95-C55A
TE-1 through TE-49, and TE-51 through TE-451
D55, D55A
TE-452 through TE-767
E55, E55A
TE-768 through TE-1201
56TC
TG-2 through TG-83
A56TC
TG-84 through TG-94
58, 58A
TH-1 through TH-1388, and TH-1390 through TH-1395
58P, 58PA
TJ-3 through TJ-435, and TJ-437 through TJ-443
58TC, 58TCA
TK-1 through TK-150
Compliance: Required the next time the elevator trim tab actuators are removed for any reason, but no later than 12 calendar months after the effective date of this AD, unless already accomplished.
To prevent loss of control of the airplane because of interchanging the right-hand and left-hand elevator trim tab actuators, accomplish the following:
(a)Paint a stripe on each stabilizer rear spar (right-hand black; and left-hand blue) in accordance with the Accomplishment Instructions of Beech Service Bulletin No. 2399, dated March 1991.
(b) Remove the cover over the actuator inspection hole on each stabilizer and paint the inspection hole ledges (right-hand black; and left-hand blue) in accordance with the Accomplishment Instructions of Beech Service Bulletin No. 2399, dated March 1991.
(c) Paint a stripe .50 by 1 inch on each actuator housing through the inspection holes (right-hand black; and left-hand blue) in accordance with the Accomplishment Instructions in Beech Service Bulletin No. 2399, dated March 1991. Actuators must not be removed to paint the .50 by 1 inch stripe on the housing.
NOTE: A left-hand trim tab actuator will have threads on its actuator screw that will rotate clockwise when screwed into the actuator assembly, and a right-hand trim tab actuator will have threads on its actuator screw that willrotate counterclockwise when screwed into the actuator assembly.
(d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a location where the requirements of this AD can be accomplished.
(e) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office.
(f) The modification required by this AD shall be done in accordance with Beech Service Bulletin No. 2399, dated March 1991. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from the Beech Aircraft Corporation, Commercial Service, Department 52, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 1100 L Street, NW, Room 8401, Washington, DC.
This amendment (39-7099, AD 91-17-01) becomes effective on November 25, 1991.