CTHIn ForceLegislation
AD/CESSNA 170/79 - Crew Seat Back Cylinder Lock Modification
Cessna 170, 172, F172, FR172 and 175 SerCessna 170, 172, F172, FR172 and 175 Series Aeroplanes
Start here
Get a plain-English read of Cessna 170, 172, F172, FR172 and 175 Ser
Turn the raw legal text into a practical explanation grounded in AD/CESSNA 170/79 - Crew Seat Back Cylinder Lock Modification.
Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes
| AD/CESSNA 170/79 | Crew Seat Back Cylinder Lock Modification | 5/2007 DM |
|---|
| Applicability: | Cessna 172R (Serial Numbers 17280001 through 17281262) and Cessna 172S (Serial Numbers 172S8001 through 172S9994). |
|---|---|
| Requirement: | 1) Aeroplanes that do not have Modification Kit MK172-25-10A or Modification Kit MK172-25-10B installed, for each crew seat (pilot and copilot), install Modification Kit MK172-25-10C or fabricate and install a steel lock rod/bar. Follow Cessna Single Engine Service Bulletin SB04-25-01, Revision 4, dated December 26, 2006, for installing Modification Kit MK172-25-l0C, or, follow Cessna Single Engine Service Bulletin SB04-25-02, Revision 1, dated October 17, 2005, or Revision 2, dated June 5, 2006, for fabricating and installing a steel lock rod/bar.2) Aeroplanes that have Modification Kit MK172-25-10A or Modification Kit MK172-25-10B installed:(i) For each crew seat (pilot and co-pilot), perform an installation inspection in accordance with Cessna Single Engine Service Bulletin SB04-25-01, Revision 4, dated 26 December 2006.(ii) If you do not find any discrepancies during the inspection required in paragraph (2)(i) of this AD, make a log book entry showing compliance with this AD and no further action is required.(iii) If you find discrepancies during the inspection required in paragraph (2)(i) of this AD, make all necessary corrective actions in accordance with Cessna Single Engine Service Bulletin SB04-25-01, Revision 4, dated 26 December 2006.Note: FAA AD 2007-05-10 Amdt 39-14971 and Cessna Service Bulletins SB04-25-01 and SB04-25-02 refer. |
| Compliance: | 1) For aeroplanes over 1,000 hours time-in-service (TIS) on the effective date of this AD, perform the action within the next 4 months after the effective date of this AD; orFor aeroplanes from 501 to 1,000 hours TIS on the effective date of this AD, perform the action within the next 8 months after the effective date of this AD; or |
| For aeroplanes from 0 to 500 hours TIS on the effective date of this AD, perform the action within the next 12 months after the effective date of this AD.2) For aeroplanes meeting Requirement 2:(i) Within the next 30 days after the effective date of this AD.(ii) Before further flight after the inspection required in paragraph 2(i) of this AD.(iii) Before further flight after the inspection required in paragraph 2(i) of this AD. |
|---|