AD 2007-08-08 Airworthiness Directives; Raytheon Aircraft Company (The Beech Aircraft Company and BEECH previously held Type Certificate Nos. 3A15, 3A16, 5A3, and A-777) 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, V35A, V35B, 36, A36, A45 (T-34A, B45), D45 (T-34B), 95-55, 95-A55, 95-B55, 95-B

Makes named: beech, raytheon. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to the following airplane models and serial numbers (SNs) that are certificated in any category: (1) Group 1 (maintains the actions from AD 72-22-01):   Model SNs (i) 35-33, 35-A33, 35-B33, 35-C33, E33, F33, and G33 CD-1 through CD-1256. (ii) 35-C33A, E33A, and F33A CE-1 through CE-349. (iii) E33C and F33C CJ-1 through CJ-30. (iv) 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, and V35B D-1 through D-9287. (v) 36 and A36 E1 through E-283. (vi) A45 (T-34A, B45) and D45 (T-34B) All. (vii) 95-55, 95-A55, 95-B55, and 95-B55A TC-1 through TC-1402. (viii) 95-C55, 95-C55A, D55, D55A, E55, and E55A TE-1 through TE-846. (ix) 56TC and A56TC TG-1 through TG-94. (x) 58 TH-1 through TH-174. (xi) 95, B95, B95A, D95A, and E95 TD-2 through TD-721. (2) Group 2: Model 95-B55B (T-42A) airplanes, SNs TF-1 through TF-70.

To address this problem, you must do the following, unless already done:   Actions Compliance Procedures (1) Determine if each uplock roller is of the greasible type (one having a drilled and grooved inner race) (i) For Group 1 airplanes: Within 300 hours time-in-service (TIS) after October 25, 1972 (the effective date of AD 72-22-01) Follow Beechcraft Service Instructions No. 0448-211, Rev. I (undated), or Beechcraft Service Instructions No. 0448-211 (undated).   (ii) For Group 2 airplanes: Within 300 hours TIS after May 25, 2007 (the effective date of this AD). (2) Replace any nongreasible uplock roller (one having a solid inner race) with the greasible type (i) For Group 1 airplanes: Before further flight after the determination required by paragraph (e)(1)(i) of this AD (ii) For Group 2 airplanes: Before further flight after the determination required by paragraph (e)(1)(ii) of this AD. Follow Beechcraft Service Instructions No. 0448-211, Rev. I (undated), or Beechcraft Service Instructions No. 0448-211 (undated). (3) Install hollow zerk-ended mounting bolts on the uplock rollers (i) For Group 1 airplanes: Within 300 hours TIS after October 25, 1972 (the effective date of AD 72-22-01) (ii) For Group 2 airplanes: Within 300 hours TIS after May 25, 2007 (the effective date of this AD). Follow Beechcraft Service Instructions No. 0448-211, Rev. I (undated), or Beechcraft Service Instructions No. 0448-211 (undated). (4) Lubricate the uplock mechanism (i) For Group 1 airplanes: Initially within 300 hours TIS after October 25, 1972 (the effective date of AD 72-22-01). Repetitively lubricate thereafter at intervals not to exceed 100 hours TIS Follow Beechcraft Service Instructions No. 0448-211, Rev. I (undated), or Beechcraft Service Instructions No. 0448-211 (undated).   (ii) For Group 2 airplanes: Initially within 300 hours TIS after May 25, 2007 the effective date of this AD. Repetitively lubricate thereafter at intervals not to exceed 100 hours TIS. Alternative Methods of Compliance (AMOCs) (f) The Manager, Wichita Aircraft Certification Office, FAA, ATTN: Anthony Flores, Aerospace Engineer, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946-4174; facsimile: (316) 946-4107, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. (g) AMOCs approved for AD 72-22-01 are approved for this AD. Material Incorporated by Reference (h) You must use Beechcraft Service Instructions No. 0448-211, Rev. I (undated), or Beechcraft Service Instructions No. 0448-211 (undated), to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of Beechcraft Service Instructions No. 0448-211 (undated), and Beechcraft Service Instructions No. 0448-211, Rev. I (undated), under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html . Issued in Kansas City, Missouri, on April 6, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-7048 Filed 4-19-07; 8:45 am] BILLING CODE 4910-13-P

This AD results from a recent incident involving a Raytheon Aircraft Company (RAC) Model 95-B55B (T-42A) airplane where a seizure of the uplock rollers occurred. We are issuing this AD to decrease the possibility of gear-up landings caused by seizure of the uplock rollers.