| AD Number | 79-01-01 | Status | Active |
| Effective Date | January 08, 1979 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-3386 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small/Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | 100 200 35-B33 35-C33 35-C33A 56TC 58 58A 58P 58PA 58TC 58TCA 65-B80 70 95-A55 95-B55 95-B55A 95-C55 95-C55A 99 99A A100 A36 A99A B100 B90 B99 C90 D55 D55A E55 E55A E90 F33A F33C G33 V35B |
79-01-01 BEECH: Amendment 39-3386. Applies to the following models and serial number airplanes, certificated in all categories, except those that have previously complied with AD 74-13-02:
MODELS
SERIAL NUMBERS
ITEM NUMBERS
(Refers to Items in Table I)
F33A
CE-447 through CE-684
(1), (2)
F33A
CE-372
(2)
F33C
CJ-31 through CJ-128
(1), (2)
G33
CD-1292 through CD-1304
(1), (2)
35-C33
CD-970
(1), (2)
35-C33, 35-C33A
CD-1066 & CE-62
(2)
35-B33
CD-700
(2)
V35B
D-9478 through D-9480,
D-9482 through D-9531,
D-9533 through D-9536
and D-9539 through D-9968
(1)
A36
E-323
(2)
A36
E-441 through E-954
(1), (2)
D55 & D55A
TE-485, TE-615,
TE-703 and TE-710
(2)
E55 & E55A
TE-790, TE-911
(2)
E55 & E55A
TE-905, TE-923 through TE-937,
TE-939, TE-940, TE-942, and
TE-943 through TE-1084
(1), (2)
56TC
TG-78 and TG-83
(2)
58 & 58A
TH-49, TH-77, TH-114,
TH-180, TH-217, TH-324
(2)
58 & 58A
TH-145, TH-340 and
TH-343 through TH-779(1), (2)
58P & 58PA
TJ-2 through TJ-97
(1), (2)
58TC & 58TCA
TK-1 through TK-37
(1), (2)
65-B80
LD-441 through LD-511
(1), (3), (5), (6), (7)
70
LB-31 through LB-35
(1), (3), (5), (6), (7)
B90 & C90
LJ-500 through LJ-706
(1), (3), (5), (6), (7)
E90
LW-1 through LW-209
(1), (3), (5), (6), (7)
95-A55
TC-241
(1)
95-B55 & 95-B55A
TC-661 and TC-1510
(2)
95-B55 & 95-B55A
TC-1570 through TC-2011
(1), (2)
95-C55 & 95-C55A
TE-271
(2)
95-C55 & 95-C55A
TE-415
(1)
99, 99A, A99A, B99
U-134 through U-164
(1), (3), (4), (5), (6), (7)
100 & A100
B-61 through B-178,
B-180 through B-204
and B-206 through B-231
(1), (3), (4),
(5), (6), (7)
B100
BE-1 through BE-19
(1), (3), (4), (5), (6), (7)
200
BB-2 through BB-185,
& BB-187 through BB-199
(3), (4), (8),
(9), (10)
COMPLIANCE: Required as indicated unless already accomplished.
To assure continued structural integrity of certain screws in the airplane control system, in accordance with instructions set forth herein and in Beechcraft Service Instructions No. 0629- 150, Revision II or later approved revisions, accomplish the following:
A) Within 100 hours time-in-service after the effective date of this AD:
For affected models and serial numbers, determine those Item Numbers applicable thereto by referring to the column above entitled "Item Numbers". Next, determine the number, type and location of screws by referring to Table I of this AD (see below). Replace each screw at the specified location except that an existing screw need not be replaced if inspection shows that the head has at least one raised or depressed "X" mark. Replace the screws one at a time at the hinge brackets to retain original alignment of the bracket.
B) Any equivalent means of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
TABLE I
Item 1. Two AN502-10-10 screws securing each hinge bracket at leading edge of rudder or ruddervator.
Item 2. Two AN502-10-10 screws securing each hinge bracket at leading edge of elevator.
Item 3. Two AN502-10-12 screws securing elevator control cables to forward bellcrank under pilot's compartment left floorboard.
Item 4. Two AN503-8-8 screws securing elevator control cables to aft bellcrank in fuselage tail section.
Item 5. Two AN503-8-10 screws securing rudder control cables to forward bellcrank under pilot's compartment floorboard aft of left rudder pedals.
Item 6. Two AN503-8-6 screws securing rudder control cables to aft bellcrank in the fuselage tail section.
Item 7. Two AN503-8-6 screws securing aileron control cables to bellcrank under floorboard just forward of the rear spar.
Item 8. Two AN503-8-8 screws securing rudder control cables to forward bellcrank under pilot's compartment floorboard aft of left rudder pedals.
Item 9. Two AN503-8-8 screws securing rudder control cables to the aft quadrant assembly in the fuselage tail section.
Item 10. Two AN503-8-8 screws securing aileron control cables to bellcrank under floorboard just forward of the rear spar.
This AD supersedes AD 74-13-02, Amendment 39-1874 (39 FR 20784).
NOTE: Scheduling accomplishment of this Airworthiness Directive simultaneously with accomplishment of Airworthiness Directive No. 78-22-05 will result in a savings of man-hours.
This amendment becomes effective January 8, 1979.