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钻石42飞机飞行手册 DA 42 Airplane Flight Manual(92)

时间:2011-10-28 13:17来源:蓝天飞行翻译 作者:admin
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Porous panel, center wing, LH  12102-23  CAV Aerospace 
Porous panel, center wing, RH  12102-24  CAV Aerospace 
Porous panel, horizontal tail, LH  12102-25  CAV Aerospace 
Porous panel, horizontal tail, RH  12102-26  CAV Aerospace 
Porous panel, vertical tail  12102-27  CAV Aerospace 
Inlet strainer  12121-02  CAV Aerospace 
 
Spray bar  12124-10  CAV Aerospace 
 
Metering pump 1  9513A-386  CAV Aerospace  4.180  1.896  40.160  1.020 
Metering pump 2  9513A-386  CAV Aerospace  4.180  1.896  40.160  1.020 
De-icing fluid tank  D60-3013-24-50  Diamond Aircraft  8.140  3.692  38.390  0.975 
Filter 1  F908  CAV Aerospace  0.680  0.308  40.160  1.020 
Filter 2  F908  CAV Aerospace  0.680  0.308  40.160  1.020 
Solenoid valve  FV158H-28V  CAV Aerospace  0.870  0.395  40.160  1020 
Solenoid valve  FV158H-28V  CAV Aerospace  0.870  0.395  40.160  1.020 

Doc. No. 7.01.05-E  Revision 5 15-Nov-2007  Page 6 - 26 

DA 42 AFM

Mass and Balance
Airplane Serial No.:  Registration:  Date:  Mass  Lever Arm 
Description  Type  Part No.  Manufacturer  S/N  inst‘d  lbs  kg  in  m 
High pressure switch  P041ED850  CAV Aerospace 
Proportioning unit, nacelle, LH  PU300DW142  CAV Aerospace 
Proportioning unit, nacelle, RH  PU300DW142  CAV Aerospace 
Tail bracket assembly  12132-03  CAV Aerospace  1.070  0.485  278.700  7.080 
Windshield pump 1  WP209A  CAV Aerospace  0.650  0.295  40.160  1.020 
Windshield pump 2  WP209A  CAV Aerospace  0.650  0.295  40.160  1.020 
De-ice control box  DAI-9030-00-01  Diamond Aircraft 
 

*) Refer to Service Bulletin SB 42-007 latest effective issue for approved ECU firmware and mapping
Place: ________________ Date: ____________________ Signature: __________________
Doc. No. 7.01.05-E
Revision 5 15-Nov-2007
Page 6 - 27
DA 42 AFM

Mass and Balance
Intentionally left blank.


CHAPTER 7
DESCRIPTION OF THE AIRPLANE
AND ITS SYSTEMS

Page
7.1 INTRODUCTION ........................................ 3

7.2 AIRFRAME ............................................. 3

7.3 FLIGHT CONTROLS ..................................... 4

7.4 INSTRUMENT PANEL ................................... 11
 
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