1401

Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401.

Aircraft: 180, 180A, 180B, 180C +67 more

Installation of Hoskins MK V B Anti-Collision Light System in accordance with FAA Sealed Hoskins Top Drawing No. 10-0051.1 This Anti-Collision Light System meets the requirements of FAR 25.1397, 25.1401 (b) (c) and (f), (400 effective candles minimum) effective August 11, 1971. Hoskins Inc., FAA approved AFM supplement Dated June 06, 1972, is required with this modification.

Aircraft: G-1159

Installation of Hoskins Model 700801Anti-Collision Light in accordance with FAA sealed Master Eligibility List No. SA2543WE. While the requirements of FAR 23.1401(a), (c), (d), (e) and (f) are met by this installation, the requirements of FAR 23.1401(b) are not met. Since the aircraft was type certificated under airworthiness regulations that contained no Anti-Collision Light Standards for intensity and field of coverage, this installation is accepted. Hoskins FAA approved AFM Supplement (see MEL SA2543WE) is required with this modification.

Aircraft: 95-A55, 58, E55, D55 +3 more

Installation of Hoskins (Pulstar TM) combined Position Anti-Collision Lighting System in accordance with FAA Sealed Hoskins Top Drawings No. 10-202186 or No. 10-202186-1. These Anti-Collision Lighting Systems have been found to meet the Anti-Collision Light Standards of FAR 23.1401, in effect of August 11, 1972. Hoskins FAA Approved AFM supplement dated December 27, 1972 or later FAA Approved Revision is required with this modification

Aircraft: 180

Install D Shannon Products, Ltd. 20-gallon fiberglass auxiliary wing-tip fuel tanks DLB1400, Rev. B dated May 14, 2009, in accordance with Installation Manual KB-1401-1, Rev. A, dated May 14, 2009, or later FAA Approved revision for 4010-lb gross weight normal category operation.

Aircraft: 36, A36, A36TC, G36