TEXTRON CESSNA 336 MODIFICATIONS (124)

Installation of Grimes aviation white anti-collision strobe light system two...

Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail, P/N 30-0555-( ).

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Installation of the KMD 250 Multi-Function Display System with Optional...

Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.

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Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional...

Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2).

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Installation of drooped ailerons in flaps down mode, recontoured wing...

Installation of drooped ailerons in flaps down mode, recontoured wing leading edge, stall fences, aileron centering springs, and conical cambered wing tips.

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Installation of Hoskins Supplemental Position Light System which includes Model...

Installation of Hoskins Supplemental Position Light System which includes Model (A) Wing Tip Lights, Model 2 Fuselage Light used as a Tail Light or the Model L Tail Light.

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Installation of vortex generators on the leading edge of the...

Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.

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Automatic pilot AK140, pitch trim system AK141, and lateral guidance...

Automatic pilot AK140, pitch trim system AK141, and lateral guidance radio coupler AK123.

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Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction...

Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System

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Installation of Garmin AT Model GDL90 UAT Data Link System,...

Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.

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