Airworthiness Directive · Amendment 39-15770 · Cessna Model 560 Airplanes
Cessna Model 560 Airplanes
This AD applies to Cessna Model 560 airplanes, certificated in any category, serial numbers (S/Ns) 560-0001 through -0538 inclusive.
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Cessna Model 560 airplanes. That AD currently requires installing new minimum airspeed placards to notify the flightcrew of the proper airspeeds for operating in both normal and icing conditions. That AD also requires revising the airplane flight manual to provide limitations and procedures for operating in icing conditions, for operating with anti-ice systems selected "on" independent of icing conditions, and for recognizing and recovering from inadvertent stall. That AD also provides an optional terminating action for the placard installation. This new AD requires the previously optional terminating action. This AD results from an evaluation of in-service airplanes following an accident. The evaluation indicated that some airplanes might have an improperly adjusted stall warning system. We are issuing this AD to prevent an inadvertent stall due to the inadequate stall warning margin provided by an improperly adjusted stall warning system, which could result in loss of controllability of the airplane.
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Within 14 days after November 30, 2007 (the effective date of AD 2007-23-13), revise the Operating Limitations, Normal Procedures, Emergency Procedures, and the Approach and Landing sections of the AFM to include the information in the temporary changes (TCs) identified in Table 1 of this AD, as applicable, except as required by paragraph (k) of this AD. These TCs provide limitations and procedures for operating in icing conditions, for operating with anti-ice systems selected “on” independent of icing conditions, and for recognizing and recovering from inadvertent stall. Operate the airplane according to the limitations and procedures in the applicable TCs.
Note 1: This may be done by inserting a copy of the applicable TCs into the applicable AFM. When these TCs have been included in the general revisions of the AFM, the general revisions may be inserted into the AFM (in lieu of the applicable TCs), provided the relevant information in the general revision is identical to that in the applicable TCs.
| Airplanes | Applicable TC |
|---|---|
| Model 560 airplanes, S/Ns 560-0001 through -0259 inclusive | Cessna 560FM TC-R13-08, dated August 31, 2007, to the Cessna Model 560 Citation V AFM. Cessna 560FM TC-R13-09, dated August 31, 2007, to the Cessna Model 560 Citation V AFM. |
| Cessna 560FM TC-R13-10, dated August 31, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-12, dated August 31, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-13, dated August 31, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-14, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-15, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-16, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-17, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-18, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-19, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Cessna 560FM TC-R13-20, dated October 2, 2007, to the Cessna Model 560 Citation V AFM. | |
| Model 560 airplanes, S/Ns 560-0260 through -0538 inclusive | Cessna 56FMA TC-R11-16, dated August 31, 2007, to the Cessna Model 560 Citation Ultra AFM. Cessna 56FMA TC-R11-17, dated August 31, 2007, to the Cessna Model 560 Citation Ultra AFM. |
| Cessna 56FMA TC-R11-19, dated August 31, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-20, dated August 31, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-21, dated August 31, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-23, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-24, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-25, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-26, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-27, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-28, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-29, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. | |
| Cessna 56FMA TC-R11-30, dated October 2, 2007, to the Cessna Model 560 Citation Ultra AFM. |
Within 30 days after November 30, 2007, install new minimum airspeed placards to notify the flightcrew of the proper airspeeds for operating in normal and icing conditions, in accordance with the Accomplishment Instructions of Cessna Service Bulletin SB560-34-143, dated September 7, 2007, including Attachment and Service Bulletin Supplemental Data; or Cessna Service Bulletin SB560-34-143, Revision 1, dated November 21, 2007. As of the effective date of this AD, only Revision 1 may be used. The placards must be installed above or near the pilot and copilot altitude indicators or primary flight displays and must be in clear view of the pilot and copilot. The placards may be removed when the actions specified in paragraphs (i) and (j) of this AD have been accomplished.
Although Cessna Service Bulletin SB560-34-143, dated September 7, 2007, including Attachment and Service Bulletin Supplemental Data; and Cessna Service Bulletin SB560-34-143, Revision 1, dated November 21, 2007; referred to in paragraph (g) of this AD, specify to submit a maintenance transaction report to the manufacturer, this AD does not include that requirement.
(i) Within 6 months after the effective date of this AD, do a functional test of the angle-of-attack (AOA) system, and adjust the calibration settings of the AOA system as applicable, in accordance with Cessna Alert Service Letter ASL560-34-34 (for airplanes equipped with a single AOA system) or ASL560-34-35 (for airplanes equipped with a dual AOA system), both Revision 1, both dated October 2, 2007, both including Attachments, as applicable; or Cessna Alert Service Letter ASL560-34-34 or ASL560-34-35, both Revision 3, both dated March 6, 2008, both including Attachments, as applicable. As of the effective date of this AD, only Revision 3 may be used. Doing the functional test of the AOA system, adjusting the calibration settings of the AOA system as applicable, and submitting the AOA system test data as specified in paragraph (j) of this AD, terminates the placard installation required by paragraph (g) of this AD.
Note 2: Maintenance Manual Revision 24 of Cessna 560 Maintenance Manual 56MM has been changed to reflect the intent of the ASLs for the maintenance actions and periodic inspections of the AOA/Stall Warning System.
Submit the AOA system test data report for the functional test specified in paragraph (i) of this AD to Glenn Todd, Citation Customer Support Engineer, Department 572, P.O. Box 7706, Wichita, KS 67277-7706, e-mail: gatodd@cessna.textron.com, fax: 1-316-517-8500 or 1-316-206-2337. Submit the report at the applicable time specified in paragraph (j)(1) or (j)(2) of this AD. The report must include the AOA test data, the airplane serial number and registration number, and the number of landings and flight hours on the airplane. Under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has approved the information collection requirements contained in this AD and has assigned OMB Control Number 2120-0056.
(1) If the functional test was done after November 30, 2007: Submit the report within 30 days after doing the functional test.
(2) If the inspection was accomplished prior to November 30, 2007: Submit the report within 30 days after November 30, 2007.
For airplanes on which the actions required by paragraph (i) of this AD have been done: Within 30 days after doing the actions required by paragraph (i) of this AD or within 30 days after the effective date of this AD, whichever occurs later, revise the Limitations Section of the AFM by removing the following Warning statement:
“Warning: Stick Shaker May Not Activate Prior to Buffet/Roll-Off If Airspeed Is Reduced Below the Appropriate Minimum Speed.”
Cessna Alert Service Letters ASL560-34-34 and ASL560-34-35, both Revision 1, both dated October 2, 2007, both including Attachments; and Cessna Alert Service Letters ASL560-34-34 and ASL560-34-35, both Revision 3, both dated March 6, 2008, both including Attachments; specify to submit a maintenance transaction report to the manufacturer. This AD does not include that requirement.
Actions accomplished before the effective date of this AD in accordance with Cessna Alert Service Letter ASL560-34-34 or ASL560-34-35, both Revision 2, both dated January 11, 2008, both including Attachments, are considered acceptable for compliance with the corresponding action specified in paragraph (i) of this AD.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
Aircraft
