AD 88-23-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 650 | Airworthiness Directives; CESSNA Model 650 Series Airplanes |
Unsafe Condition
Elevator flutter due to improper balance of elevators.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Incorporate the enroute operations limit of 45,000 ft maximum calibrated operating altitude into the AFM. Remove both elevators and check for proper balance within 100 flight hours or 60 days after the AD's effective date, whichever comes sooner. Rebalance elevators not meeting specifications before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to further flight for AFM incorporation and elevator rebalancing. Within 100 flight hours time-in-service or 60 days after the effective date of this AD, whichever occurs sooner, for elevator balance check.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Model 650 series airplanes with specified 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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
AFM Changes -- Elevator
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_88-23-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-23-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model 650 Series Airplanes Subject: AFM Changes -- Elevator Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/21/1989 Make: Cessna Aircraft Company Model: 650 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 88-23-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6133 AD NUMBER: 88-23-04 SUBJECT HEADING: Airworthiness Directives; CESSNA Model 650 Series Airplanes ACTION: SUMMARY: DATES: Effective February 21, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 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 days after 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. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_88-23-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-23-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model 650 Series Airplanes Subject: AFM Changes -- Elevator Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/21/1989 Make: Cessna Aircraft Company Model: 650 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 88-23-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6133 AD NUMBER: 88-23-04 SUBJECT HEADING: Airworthiness Directives; CESSNA Model 650 Series Airplanes ACTION: SUMMARY: DATES: Effective February 21, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 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 days after 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. FOOTER:
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