Beechcraft Baron 95-B55 Page 276 Pilot Operating Handbook Download

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Summary of Contents for Baron 95-B55

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Page 292: ...m 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 Naviga...

Page 293: ...he 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 ...

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Page 308: ... 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 c...

Page 309: ...ropeller 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 the propeller deice system inoperative b Zero to 7 Amps If propeller deice system ammeter occas...

Page 310: ...be operated unless the need for propeller deice is urgent NORMAL PROCEDURES WARNING To minimize slip ring pitting do not operate the system with engines inoperative PREFLIGHT 1 With engines operating place propeller deice switch in 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 3...

Page 311: ...light and will 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 55 590000 51 ...

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Page 322: ...RATING HANDBOOKSAFFECTED 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 ...

Page 323: ...en the airplane has been modified by the installationof the Auxiliary Fuel Tank Annunciator Light in accordance with Beech Kit 96 9001 1 The information in this supplement supersedes or adds to the basic Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only as set forth within this docu ment Users of this manual are advised always to refer to the supplement for possibly supersedi...

Page 324: ...LIMITATIONS PLACARDS On instrument Panel ANNUNCIATOR LIGHT I WARNING TAKEOFF AND LANDING PROHIBITED EMERGENCY PROCEDURES No Change FAA Approved Issued November 1993 P N 96 590000 1 ...

Page 325: ...elected AUX TANK SE LECTED annunciator light CHECK ILLU MINATED Left Main Tank Selected AUX TANK SE LECTED annunciator light CHECK EXTIN GUISHED Right Aux Tank Selected AUX TANK SE LECTED annunciator light CHECK ILLU MINATED Right Main Tank Selected AUX TANK SELECTED annunciator light CHECK U TlNGUlSHED PERFORMANCE No Change WEIGHT BALANCE No Change FAA Approved Issued November 1993 P N 96 590000 ...

Page 326: ...y fuel tank annunciator light will illuminate if either one of the auxiliary fuel tanks is selected when the landing gear is extended Auxiliary fuel tanks are to be used during le vel flight only and not during takeoff or landing HANDLING SERVICING AND MAINTENANCE No Change FAA Approved Issued November 1993 P N 96 590000 1 ...

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