TrackAD

Airworthiness directives › 99-09-10

AD 99-09-10 Airworthiness Directives; Raytheon Aircraft Company Models C90A, B200, B200C, B200T, B200CT, 300, B300, B300C, and A200CT Airplanes

1999-06-07
1999-04-26
39-11143
98-CE-104-AD
Airframe
—

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

Applicability*9

The following airplane models and serial numbers, certificated in any category: ------------------------------------------------------------------------ Models Serial numbers ------------------------------------------------------------------------ C90A......................... LJ-1063 through LJ-1482 B200......................... BB-1158, BB-1167, BB-1193 through BB- 1532, and all serial numbers with Beech Kit 101-8018 incorporated B200C........................ BL-113 through BL-117, BL-124 through BL- 140, and all serial numbers with Beech Kit 101-8018 incorporated B200T........................ BT-31 through BT-38, and all serial numbers with Beech Kit 101-8018 incorporated B200CT....................... BN-2, BN-3, and BN-4 that have Beech Kit 101-8018 incorporated B200CT....................... FG-1 and FG-2 300.......................... FA-1 through FA-230 300.......................... FF-1 through FF-19 B300......................... FL-1 through FL-138 B300C........................ FM-1 through FM-9 B300C........................ FN-1 A200C T (C-12D).............. BP-46 through BP-51 A200CT (C-12F)............... BP-52 through BP-63 A200CT (RC-12H).............. GR-14 through GR-19 A200CT (RC-12K).............. FE-1 through FE-9 A200CT (RC-12N).............. FE-10 through FE-24 A200CT (RC-12P).............. FE-25 through FE-31, FE-33, and FE-35 A200CT (RC-12Q).............. FE-32, FE-34, and FE-36 B200C (C-12F)................ BL-73 through BL-112 and BL-118 through BL-123 B200C (C-12F)................ BP-64 through BP-71 B200C (UC-12F)............... BU-1 through BU-10 B200CT (RC-12F).............. BU-11 and BU-12 B200C (UC-12M)............... BV-1 through BV-10 B200C (RC-12M)............... BV-11 and BV-12 B200C (C-12R)................ BW-1 through BW-19 ------------------------------------------------------------------------ [[Page 20155]] Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (c) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance

Required within the next 200 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished. Note 2: The service information referenced in this AD specifies 800-hour repetitive inspections. This AD does not require these inspections. To prevent the inability to extend the landing gear with the hand pump caused by debris entering the landing gear hand pump, which could result in passenger injury or damage to the airplane if manual operation of the landing gear failed, accomplish the following: (a) Install a filter element in the landing gear hand pump suction line, in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Raytheon Mandatory Service Bulletin SB 32-3073, Revision 1, Issued: March, 1998, Revised: July 1998. (b) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (c) 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 (ACO), 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO. Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. (d) The installation required by this AD shall be done in accordance with Raytheon Mandatory Service Bulletin SB 32-3073, Revision 1, dated July 1998. 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 Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC. (e) This amendment becomes effective on June 7, 1999. Issued in Kansas City, Missouri, on April 15, 1999. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 99-10171 Filed 4-23-99; 8:45 am] BILLING CODE 4910-13-U

Read the original on the Federal Register →

You just looked this one up by hand

TrackAD holds all 12,278 of them and matches them against the aircraft you actually look after — airframe, engine, propeller and appliances in one pass — then works out what falls due and when.

Look round a real shop first Start free

The demonstration shop is eleven real aircraft with a year of work behind them. No account needed.

The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1