说明案例讲稿to pa

1、Introduction to the Piper Warrior PA28Piper Warrior PA-28 CherokeeTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementThe PA-28 are all-metal, unpressurized, single engined, piston powered aircraft wit

2、h low-mounted wings and tricycle landing gear. The first PA-28 received its type certificate from the FAA in 1960 and the series remains in production to this day with over 32,000 aircraft built.TitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Pro

3、cedures Airmanship Threat and Error ManagementTo understand the design features of the PA28 Warrior.To learn the different cockpit layouts.OBJECTIVESTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error Management

4、The Piper Warrior was built in a number of variations including the two Moorabbin Flight Training Academy use;PA-28-151 (Cherokee)PA-28-161 (Warrior II and III)All Variations have different types of ing engines rated at different Horsepower.MFTA operate 6x PA-28-151 and 15x PA-28-161 Warriors for Ab

5、 Initio training.PIPER WARRIOR VARIATIONSTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementVH-LXP Engine: ing O-320-D3GROCKER COVERSENGINE OIL FILLER AND DIPSTICK ENGINETitleAimIntroductionObjectives

6、 Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementVH-LXP Engine: ing O-320-D3GENGINE MOUNTMAGNETOENGINETitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Th

7、reat and Error ManagementVH-LXP Engine: ing O-320-D3GEXHAUST MANIFOLDSINLET MANIFOLDSENGINETitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementVH-LXP Engine: ing O-320-D3GFUEL PRIMER FEED LINESPARK PLU

8、GSENGINETitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFUELThe Piper Warriors fuel is stored in both the LEFT and RIGHT wings. The fuel selector can be changed to draw fuel from the RIGHT “R” or L

9、EFT “L” at any one time. It can also be turned “OFF” in case of emergency.Total fuel capacity 181L useableEach wing holds approx. 90L useableFUEL CAPFUEL SELECTORTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Err

10、or ManagementFUELFuel “TABS” are used to assist pilots in estimating the fuel on board.If the fuel is at the same level as the metal “TAB” the pilot can estimate there is 64L left in the fuel tank (see POH for accurate figures)FUEL TABTitleAimIntroductionObjectives Revision DefinitionsThe Principles

11、 ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementENTRY AND EXITThe Warrior has one entry and exit located on the right hand side of the fuselage The smaller door is used for baggageTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsAp

12、plication Emergency Procedures Airmanship Threat and Error ManagementENTRY AND EXITGrab Handle and step for assistanceSTEP ONLY ON THE BLACK SURFACE ON THE WING- NOT THE FLAP!TitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship T

13、hreat and Error ManagementENTRY AND EXITStep 1- Rotate the Top Latch DOWN to “OPEN”Step 2- Hold the door closed and PULL the lever to OPEN, the door will now OPEN outwardsOPENING the door from the OUTSIDETitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emer

14、gency Procedures Airmanship Threat and Error ManagementENTRY AND EXITStep 1- Pull the door closed firmly and hold, PUSH down on the door lever to “LATCH”Step 2- Hold the handle at the top of the door and rotate the lever to “LATCH”CLOSING the door from the INSIDETitleAimIntroductionObjectives Revisi

15、on DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementENTRY AND EXITStep 1- Hold the door handle firmly, Rotate the top Latch “OPEN”Step 2- PULL the door lever upwards to OPEN and PUSH the door outwardsOPENING the door from the INSIDETitleA

16、imIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementENTRY AND EXITStep 1- Push the door closed firmly and hold, PUSH the door handle INStep 2- Hold the door closed at the top and rotate the latch CLOSEDClosi

17、ng the door from the outsideTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFLIGHT CONTROLSRotating the control YOKE left and right will manipulate the AILERONS on each wingYOKEAILERONSTitleAimIntr

18、oductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFLIGHT CONTROLSPulling back (CLIMBING) or pushing forward (DECENDING) on the control YOKE will manipulate the StabilatorYOKESTABILATORTitleAimIntroductionObjecti

19、ves Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFLIGHT CONTROLSTrim tabs are small surfaces connected to the trailing edge of a larger control surface, used to control the trim of the controls or to counteract aerodynamic fo

20、rces and stabilise the aircraft in a particular desired attitude without the need for the pilot to constantly apply a control force. TRIM TABTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFLIGHT C

21、ONTROLSTRIMS are used in flight to relieve the pressure on the pilotRUDDER TRIMTRIM WHEELTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFLIGHT CONTROLSLeft and Right Rudder pedals (LOWER) and diff

22、erential Brakes (UPPER)RUDDER PEDALSRUDDERBRAKESTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementFLIGHT CONTROLSFLAPS are used in flight to increase the lift to allow for slower flight FLAP LEVERFLA

23、PSTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementINSTRUMENTS Airspeed Indicator (ASI) Artificial Horizon (AH) Altimeter (ALT) Turn Coordinator (TC) Directional Gyro (DG) Vertical Speed Indicator (

24、VSI)TitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementSWITCHESSwitches in the Warrior are used to turn ON or OFF ancillary devices fitted to our aircraft.They include:BATTERY MASTER/ALTERNATOR (SPLIT

25、 SWITCH)SWITCHES AS PLACARDED ABOVENAV LIGHTSTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementCIRCUIT BREAKERSDesigned to protect an electrical circuit from damage caused by overload or short circui

26、t. Its basic function is to detect a fault condition and interrupt current flow to the electrical device.CIRCUIT BREAKERS- As PlacardedTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementENGINE INSTRUM

27、ENTS AND GAUGESGauges-Fuel quantity LEFT AND RIGHTEngine RPM (TACHOMETER)VDO (ENGINE TIME)FUEL GAUGES L&RTACHOMETERVDOTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementENGINE INSTRUMENTS AND GAUGESGa

28、uges-OIL TEMPERATUREOIL PRESSURE OIL PRESSUREOIL TEMPERATUREOIL PRESSUREFUEL PRESSURETitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplication Emergency Procedures Airmanship Threat and Error ManagementENGINE INSTRUMENTS AND GAUGESSwitches;MAGNETOSPrimer;FUEL PRIMERFUEL PRIMERMAGNETOSTitleAimIntroductionObjectives Revision DefinitionsThe Principles ConsiderationsApplicatio