Beechcraft Baron 95-B55 and 95-B55A Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement

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1 of 2 LOG OF SUPPLEMENTS Baron 95-B55 and 95-B55A Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual P/N 96-590011-25 September, 2011 FAA Supplement must be in the airplane for all flight operations when subject equipment is installed. PART NUMBER SUBJECT REV NO. DATE 130598 Landing Gear Safety System 3 1/83 *131262 Operation In The United Kingdom 1 8/03 131391 Manual Cowl Flaps (Kit 55-9017) 6/80 55-590000-51 Goodyear Electrothermal Propel- ler Deice 10/78 58-590000-49 Inside Cabin Door Handle With Open/Closed Placard 12/90 95-590014-47 Goodrich Reservoir Type Pneu- matic Deicing System 10/78 96-590000-1 Auxiliary Fuel Tank Annunciator Light (Kit 96-9001-1) 11/93 96-590010-19 King KN-74 Area Navigation 1 2/79 96-590010-21 Nickel-Cadmium Battery and Charge Current Detector 10/76 SA126CE Hartzell Propellers 4/1/69 Log Of Supplements (Cont’d) 96-590011-25 September, 2011 2 of 2 NOTE: Supplements applicable to equipment other than that installed may, at the discretion of the owner/operator, be removed from the manual. * Supplements marked with an asterisk will not be supplied with handbooks sold through Authorized Raytheon Outlets due to their limited applicability. If a document is required for your airplane, please order the document through normal channels. SA795CE Hartzell Propellers 2 2/13/76 PART NUMBER SUBJECT REV NO. DATE BEECHCRAFT LANDPLANES MODEL 9 5 - 5 5 SERIES PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT for the GOODYEAR ELECTROTHERMAL PROPELLER DEICE GENERAL The information in this supplement is FAA approved ma- terial and must be attached to the Pilot's Operating Hand- book and FAA Approved Airplane Flight Manual when the airplane is equipped with a Goodyear Electrothermal Pro- peller Deice System that has been installed in accordance with BEECHCRAFT FAA approved data. This document supersedes or adds to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual only where covered in the items contained herein. LIMITATIONS Do not operate the system unless engine is operating. Airplanes equipped with approved emergency static air source, surface deicing systems, pitot heat, heated stall warning, windshield defogging or storm windows, and ex- ternal antenna mast capable of withstanding ice load are considered to be equipped for flight into icing conditions as governed by operational practices of Bureau of Flight Standards Release No. 434. When not equipped ac- cordingly a placard as shown must be installed. FAA Approved Revised: October, 1 9 7 8 P/N 5 5 - 5 9 0 0 0 0 - 5 1 PLACARDS On Instrument Panel: WARNING THIS AIRCRAFT IS NOT FULLY EQUIPPED FOR FLIGHT I N ICING CONDITIONS EMERGENCY PROCEDURES 1. Loss of one generator, off-load unnecessary electrical equipment. Turn off the propeller deice system while operating the cabin heater blower or the landing gear motor. Monitor electrical loads so as not to exceed generator capacity. 2 . Abnormal Reading on Propeller Deice Ammeter a. Zero Amps Check propeller deice switch. If the circuit breaker in the switch has tripped, a wait of approximately 30 seconds is necessary before resetting the switch to the ON position. If ammeter reads 0 and switch has not tripped or if ammeter still reads 0 after the switch has been reset, turn the switch off and consider t h e propeller deice system inoperative. b. Zero to 7 Amps If propeller deice system ammeter occasionally or regularly indicates less than 7 amps, operation of the propeller deice system can continue unless serious propeller imbalance results from irregular ice throw-offs. FAA Approved Revised: October, 1 9 7 8 P/N 55-590000-51 c. 1 1 to 1 5 Amps If propeller deice system ammeter occasionally or regularly indicates 1 1 to 1 5 amps, operation of the propeller deice system can continue unless serious propeller imbalance results from irregular ice throw-offs. d. More than 15 Amps If the propeller deice system ammeter occasionally or regularly indicates more than 1 5 amps, the system should not be operated unless the need for propeller deice is urgent. NORMAL PROCEDURES WARNING To minimize slip ring pitting, do not operate the system w i t h engines inoperative. PREFLIGHT 1 . W i t h engines operating, place propeller deice switch i n the ON position. 2. Check propeller deice system ammeter for reading of 7 to I 1 amperes. 3. A small momentary deflection of the needle may be noticed approximately every 30 seconds: This is due to the switching action of the timer and is an indication of normal operation of the system. F A A Approved Revised: October, 1978 P/N 55-590000-51 IN FLIGHT 1. To place the system i n operation, move propeller deice switch to the ON position. The system may be oper- ated continuously i n flight and w i l l function au- tomatically until the switch is turned off. 2. Propeller imbalance may be relieved by varying rpm. Increase rpm briefly and return to desired setting, re- peating if necessary. PERFORMANCE - No change Approved: &J Chester A. Rembleske I Beech Aircraft Corporation DOA CE-2 FAA Approved Revised: October, 1978 P / N 5 5 - 5 9 0 0 0 0 - 5 1 BEECHCRAFT BARON LANDPLANES PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR THE AUXILIARY FUEL TANK ANNUNCIATOR LIGHT (BEECH KIT NO. 96-9001-1) PILOT'S OPERATING HANDBOOKS AFFECTED: Baron 95-55195-A55 (TC-1 thru TC-501 except TC-350 and TC-371) PIN 55-590000-65 . . . . . . . . . . . . . . . . . . . . . . . . . Baron 95-855195-B55A (TC-371 and TC-502 thru TC-1607) . . . . . . . . . . . . . . . . . . . . . . . . . . PIN 96-590011-25 Baron 95-C55195-C55A, D551D55A. E55lE55A (TC-350 and TE-1 thru TE-942 except TE-938) . . . . . . . . . . . . . . . . . . . . . . . . . PIN 96-590010-29 Airplane Serial Number: Airplane Registration Number: DOA CE-2 FAA Approved Issued: November, 1993 P/N 96-590000-1 1 of 5 CONTENTS GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . .Page 2