AD 88-23-04

Airworthiness directive · AFM Changes -- Elevator · Cessna 650

Effective
February 21, 1989
Model
650
Data sheet
TCDSA9NM
Registered aircraft
201 matched by model
Product
Aircraft · Large airplane
Amendment
39-6133

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 May 30, 2024.

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The airworthiness directive

88-23-04 CESSNA: Amendment 39-6133. Final copy of Priority Letter AD which was effective November 16, 1988.

Applicability: Model 650 series airplanes; Serial Numbers 650-0094, 650-0096, 650- 0100 through 650-0103, 650-0105 through 650-0107, 650-0117, 650-0120, 650-0123, 650-0125 through 650-0129, 650-0131 through 650-0159, 650-0161, and 650-0162; certificated in any category.

Compliance: Required as indicated, unless already accomplished.

To prevent elevator flutter, accomplish the following:

A. Prior to further flight, incorporate the following into the Limitations Section of the FAA-approved Airplane Flight Manual (AFM). This may be accomplished by inserting a copy of this AD, or the Temporary AFM Change included as part of the Cessna Alert Service Letter SLA650-27-20, dated November 11, 1988, into the AFM:

"Enroute Operations Limits: 45,000 ft. Maximum Calibrated Operating Altitude."

B. Within the next 100 flight hours time-in-service or 60 daysafter the effective date of this AD, whichever occurs sooner, remove both elevators from the airplane and check for proper balance, in accordance with Cessna Alert Service Letter SLA650-27-20, dated November 11, 1988. Elevators not meeting proper balance specifications must be rebalanced, prior to further flight, in accordance with the Accomplishment Instructions of the service bulletin.

C. Accomplishment of the requirements of paragraph B., above, constitutes terminating action for the requirements of paragraph A., above, and the AFM revision may be removed.

D. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Wichita Aircraft Certification Office, FAA, Central Region.

E. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive may obtain copies of the applicable service information from Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, Kansas 67277. This material may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Wichita Aircraft Certification Office, FAA, Central Region, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas.

This AD was effective earlier to all recipients of Priority Letter AD 88-23-04 issued November 16, 1988.

This amendment (39-6133, AD 88-23-04) becomes effective February 21, 1989.

Affected TCDS · 1

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

Registered aircraft · 201

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
  • Cessna201 aircraft
By year built
19822000
Registered aircraft by year built: 179 aircraft
19821
19834
198422
198514
198613
19878
198810
19892
19908
19918
199211
199314
199413
199514
19968
19975
19986
199910
20008

22 with no year recorded

By model

Aircraft

See all 201 aircraft