Document ID: chunk:federal_register_of_legislation:F2008L01387:body:0:p2
Version: federal_register_of_legislation:F2008L01387
Segment Type: other
Provision Reference: 
Character Range: 3020–6529

1 April 2008.

                   8. KAPS turbochargers, P/N 465930-0002 (TCM P/N 641672-2), installed on TCM GTSIO-520-M engines, with the turbocharger SNs listed in KAPS MSB No. 030, Revision A, dated 1 April 2008.

                   9. KAPS turbochargers, P/N 465680-0004 (Cessna P/N C295001- 0202), installed on Cessna P210 Pressurized Centurion airplanes with a TCM TSIO-520-AF or TSIO-520-P engine, with the turbocharger SNs listed in KAPS MSB No. 030, Revision A, dated 1 April 2008.

                   10. KAPS turbochargers, P/N 465930-0002 (TCM P/N 641672-2), installed on Cessna 404 Titan airplanes with a TCM GTSIO-520-M engine, with the turbocharger SNs listed in KAPS MSB No. 030, Revision A, dated 1 April 2008.

                   11. KAPS overhauled turbochargers, P/N 465930-9003, installed on TCM
                   GTSIO-520-L or GTSIO-520-N engines, with the turbocharger SNs listed in KAPS MSB No. 031, dated 28 February 2008.

                   12. KAPS overhauled turbochargers, P/N 409170-9001, installed on Lycoming Engines TIO-540-J2B; TIO-540-J2BD; TIO-540-N2BD, and LTIO-540-N2BD engines, with the turbocharger SNs listed in KAPS MSB No. 031, dated
                   28 February 2008.

                   13. KAPS overhauled turbochargers, P/N 465680-9005, installed on Lycoming Engines TIO-540-V2AD and TIO-540-W2A engines, with the turbocharger SNs listed in KAPS MSB No. 031, dated 28 February 2008.

                   14. KAPS overhauled turbochargers, P/N 465930-9002, installed on TCM
                   GTSIO-520-M engines, with the turbocharger SNs listed in KAPS MSB No. 031, dated 28 February 2008.

                   15. Also, the following KAPS turbochargers might have been overhauled or repaired by other than KAPS, that used a P/N 441977- 0023S or P/N 441977-0025S turbine housing sold as a spare part, through the Aviall Company.  These turbine housings have the date code of 1006 and might have been installed between October 2006 and 25 January 2008.  The turbocharger data plates might include manufacturer's information other than KAPS information, such as, Garrett:

                     (a) P/N 409170-0001; installed on Lycoming Engines TIO-540-J2B;
                     TIO-540-J2BD; TIO-540-N2BD; and LTIO versions of the noted engine models.

                     (b) P/N 465680-0004; installed on TCM TSIO-520-AF and TSIO-520P engines.

                   (c) P/N 465680-0005; installed on Lycoming Engines TIO-540-V2AD and
                   TIO-540-W2A engines.

                   (d) P/N 465930-0002; installed on TCM GTSIO-520-M engines.

                   (e) P/N 465930-0003; installed on TCM GTSIO-520-L and GTSIO-520-N engines.

                   (f) P/N 465448-0004; installed on TCM TSIO-520-CE engines.

                   (g) P/N 466412-0003; installed on TCM TSIOL-550-A and TSIOL-550-C engines.

                   (h) P/N 466412-0004; installed on engines modified by RAM.
Requirement:  Onetime Visual Inspection of Turbocharger

                 1. Carefully remove the "V'' band clamp from around the turbocharger turbine housing at the turbocharger exhaust outlet, taking care not to move the exhaust tube and tailpipe assembly.

                 2. Visually inspect the area that was captured by the "V'' band clamp.  Use a feeler gauge at the split line between the turbine housing flange and the exhaust tube flange all around the circumference.

                 3. The maximum gap must not exceed 0.005