Airworthiness directives › 99-13-04
AD 99-13-04 Airworthiness Directives; Cessna Aircraft Company Models 206H and T206H Airplanes
Makes named: cessna. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
The following airplane model and serial number airplanes, certificated in any category: ------------------------------------------------------------------------ Models Serial numbers ------------------------------------------------------------------------ 206H............................. 20608002 through 20608026. T206H............................ T20608002 through T20608015; T20608017 through T20608023; and T20608025 through T20608028. ------------------------------------------------------------------------ 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 (e) 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 as indicated in the body of this AD, unless already accomplished. To detect and correct loose aileron control bellcrank stop bolts, which could result in restricted movement of the aileron with possible partial or complete loss of aileron control, accomplish the following: (a) Within the next 10 hours time-in-service after the effective date of this AD or within the next 60 calendar days after the effective date of this AD, whichever occurs first, inspect the left and right wing aileron control bellcrank stop bolts and lock nuts for flush and tight contact with the surface of the threaded boss on each end of the yoke assemblies. Accomplish this inspection in accordance with the INSPECTION/MODIFICATION INSTRUCTIONS section of Cessna Special Service Project SSP99-27-02, dated May 18, 1999. (b) If the bolts and nuts are flush and tight, or loose but flush after tightening, prior to further flight, accomplish the following actions in accordance with the INSPECTION/MODIFICATION INSTRUCTIONS section of Cessna Special Service Project SSP99-27-02, dated May 18, 1999: (1) Loosen nuts; (2) Clean threads (bolt and nut); (3) Wick Loctite 290 into threads; and (4) Torque nut. (c) If the bolts and nuts are not flush, prior to further flight, accomplish the following actions in accordance with the INSPECTION/MODIFICATION INSTRUCTIONS section of Cessna Special Service Project SSP99-27-02, dated May 18, 1999: (1) Remove nut and stop bolt; (2) Spotface boss; (3) Clean threads (boss, bolt, and nut); (4) Apply Loctite 242; (5) Adjust stop bolt; and (6) Torque bolt. Note 2: Paragraphs (b) and (c) of this AD present a basic outline of the follow-on work to be accomplished. The detailed procedures to accomplish these actions are included in the INSPECTION/MODIFICATION INSTRUCTIONS section of Cessna Special Service Project SSP99-27-02, dated May 18, 1999. (d) 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. (e) An alternative method of compliance or adjustment of the compliance times 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. (f) The inspections and follow-on actions required by this AD shall be done in accordance with Cessna Special Service Project SSP99-27-02, dated May 18, 1999. 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 Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706. 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. (g) This amendment becomes effective on July 13, 1999. Issued in Kansas City, Missouri, on June 10, 1999. Michael K. Dahl, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 99-15220 Filed 6-17-99; 8:45 am] BILLING CODE 4910-13-P
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.
- Bring your existing list in from a spreadsheet Paste the rows straight out of Excel. Headers like C/W Date and N/A are read for you.
- A copy that works when this does not One file. No internet, no login, no this software running. For the morning something has to be produced and the computer is not cooperating.
- $5 a month, or $50 a year Up to 50 aircraft on either.
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