METRO III – ICAO ANNEX 8 INTRODUCTION Section 7 of this manual contains supplements necessary for the safe operation of optional or new components that may be installed on the basic aircraft. Each supplement will normally cover a single system, device, or piece of equipment. Systems consisting of several components may have supplements for each component or the system as a whole depending on the scope of the change or addition. Some supplements may apply only to a specific, or limited number of, aircraft. Others may be applicable to all METRO III aircraft, but only if specific operators choose to take advantage of the optional equipment or information. The List of Supplements includes all currently available supplements which are prepared by Fairchild Aircraft and cannot include those supplements prepared by vendors for use with their optional equipment (e.g., an autopilot). It is the responsibility of the METRO III operator to ensure that appropriate supplements are filed with his basic AFM. Supplements which do not apply to your aircraft should not be included with the AFM. Pages in this section that are FAA approved are so identified.
MANUFACTURER'S DATA ISSUED: MAY 22/89 Revised: MAY 07/97
SUPPLEMENTS
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METRO III – ICAO ANNEX 8 LIST OF SUPPLEMENTS Suppl. No.
A-1 A-2 A-3 A-4 A-5 A-6 A-7 A-8 A-9 A-10 A-11 A-12 A-13 A-14 A-15 A-16
Description
Date
Takeoff with SRL Off/ Inoperative ................................................................ MAY 22, 1989 AC System with Three Inverters .................................................................. MAY 22, 1989 Flight Data Recorder (For AC-670B only) ................................................... MAY 22, 1989 Cockpit Voice Recorder (For AC-670B only) ............................................... MAY 22, 1989 Flight Data Recorder (For AC-692B only) ................................................... MAY 22, 1989 Cockpit Voice Recorder (For AC-692B only) ............................................... MAY 22, 1989 Flight Data Recorder ................................................................................... MAY 22, 1989 Cockpit Voice Recorder ............................................................................... MAY 22, 1989 Operation in Canada (Canadian Registration Only) .................................... MAY 22, 1989 Revised: MAY 7, 1997 200 Ampere Electrical System .................................................................... AUG 15, 1991 21-Inch Dowty Rotol Propeller Boots ............................................................. JUL 23, 1991 Increased Zero Fuel and Landing Weights .................................................. NOV 06, 1992 Aircraft Braking Systems (ABS) Anti-skid/Power Brake System (If installed in accordance with Fairchild Aircraft drawing number 27-85211) ................ AUG 12, 1994 14,500 Pounds MTOW Aircraft .................................................................... NOV 01, 1994 Revised: DEC 19, 1994 Reduced Viscosity Hydraulic Fluid .............................................................. DEC 19, 1994 Operation with Dual Bleed Air Flow Control .................................................. JUL 11, 2002
MANUFACTURER'S DATA ISSUED: MAY 22/89 Revised: JUL 11/02
SUPPLEMENTS
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MANUFACTURER'S DATA ISSUED: MAY 22/89