Wednesday, 17 December 2014

WINGS - ACCESS PANEL INSTALLATION (Cessna Model T240)

CESSNA SEL-57-02

EFFECTIVITY

MODEL SERIAL NUMBERS                                              T240 2001 thru 2058

COMPLIANCE:     MANDATORY.

1. Special visual inspection as follows:

• During each preflight, the attachment screws for all under wing panels specified in the Accomplishment Instructions must be visually checked to make sure that they are not loose.

• If a loose screw is found, it must be tightened.
NOTE: The holder of a pilot certificate issued under 14 CFR Part 61 may perform the special inspections required by this service letter on any aircraft owned or operated by that pilot which is not used under part 14 CFR Part 121, 14 CFR Part 129, or 14 CFR Part 135.

2. The maintenance procedure specified in the Accomplishment Instructions Section of this service
letter must be accomplished within the next 100 hours of operation.

3. After the maintenance procedure specified in the Accomplishment Instructions Section of this service letter has been accomplished, the special visual inspections during preflight are no longer necessary.

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