AD 93-17-01

Airworthiness directive · Leading Edge Fuel Cell Nipples · Textron B90, C90 and C90A

Effective
October 12, 1993
Models
B90, C90, C90A
Data sheet
TCDS3A20
Registered aircraft
525 matched by model
Product
Aircraft · Small airplane
Amendment
39-8671
Docket
93-CE-23-AD

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed January 21, 2026.

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The airworthiness directive

93-17-01 BEECH AIRCRAFT CORPORATION: Amendment 39-8671. Docket No. 93-CE- 23-AD.

Applicability: Models B90, C90, and C90A airplanes (serial numbers LJ-489 through LJ-1318), certificated in any category.

Compliance: Required within the next 150 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent failure of the leading edge fuel cell nipples caused by cracking and fuel leaks, which, if not detected and corrected, could result in an airplane fire, accomplish the following:

(a) Inspect the inboard nipple on the leading edge fuel cell for cracks or fuel leaks in accordance with Part I of the ACCOMPLISHMENT INSTRUCTIONS section of Beech Service Bulletin (SB) No. 2475, dated February 1993. If cracks or fuel leaks are found, prior to further flight, repair the fuel cells in accordance with procedures specified in the applicable maintenance manual.

(b) Replace the fuel interconnect tube assembly in accordance with Part II of the ACCOMPLISHMENT INSTRUCTIONS section of Beech SB No. 2475, dated February 1993.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) 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, FAA, 1801 Airport Road, 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 Aircraft Certification Office.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita Aircraft Certification Office.

(e) The inspection and replacement required by this AD shall be done in accordance with Beech Service Bulletin No. 2475, dated February 1993. 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, 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, 800 North Capitol Street, NW., suite 700, Washington, DC.

(f) This amendment becomes effective on October 12, 1993.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 525

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Beech370 aircraft
  • Raytheon155 aircraft
By year built
19682005
Registered aircraft by year built: 455 aircraft
196812
196911
19705
19714
19724
197313
19748
19759
197611
197712
197827
197924
198017
198114
198216
19836
198413
198512
19865
19878
19885
198915
199018
19917
19926
199310
199410
199514
199621
199719
199820
199919
200019
200117
20029
20031
20049
20055

70 with no year recorded

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