CIRRUS AIRPLANE MAINTENANCE MANUAL
|
|
- Patrick Phillips
- 5 years ago
- Views:
Transcription
1 MODEL SR0 INSTRUMENT AND CONTROL PANEL. DESCRIPTION Serials 00 thru 336, 337 thru w/o PFD: The airplane uses standard flight instruments arranged in the basic-six pattern. The airspeed indicator, attitude gyro, altimeter, turn coordinator, directional gyro or horizontal situation indicator, and vertical speed indicator are mounted in the instrument panel. Ignition switch is mounted on the LH console. Serials 68 thru w/o PFD: Ignition switch is mounted in a bolster plate located on the LH console. Serials 337 thru w/ PFD, 3 & subs w/o Perspective Avionics: An Avidyne FlightMax Entegra- Series Primary Flight Display (PFD) is mounted in the instrument panel. Backup instruments for airspeed, attitude, and altitude are mounted in a bolster plate located on the LH console. In airplanes with SRV configuration, the backup attitude indicator is not installed. The ignition switch is mounted in the instrument panel. Serials 06 & subs w/ Perspective Avionics: A Garmin Primary Flight Display (PFD) is mounted in the instrument panel. Backup instruments for airspeed, attitude, and altitude are mounted in a bolster plate located on the LH console. The ignition switch is mounted in the instrument panel. Serials 73 & subs w/ MD30 Standby Attitude Module: A Garmin Primary Flight Display (PFD) is mounted in the instrument panel. The MD30 Standby Attitude Module is a combined standby airspeed indicator, standby altimeter, and standby attitude indicator and is mounted in a bolster plate located on the LH console. The ignition switch is mounted in the instrument panel. A switch panel located in the bolster panel below the flight instruments contains the avionics power switch, pitot heat switch, lighting dimmer switches and the battery and alternator switches. Serials 886 & subs: The bolster panel switches are illuminated in the on position. An EL voltage inverter, located on the LH console strut converts DC power to AC power for the bolster switch panel backlight. The lights are powered by 8 VDC supplied through the -amp INST LIGHTS circuit breaker on Main Bus. A center console contains the avionics, flap control and position lights, power lever and mixture controls, fuel system indicator and controls, and audio controls. System circuit breakers, the alternate static source valve, alternate induction air control, and ELT panel switch are located on the left side of the console for easy access by the pilot. The parking brake actuation knob is mounted below the flight instruments on the left side of the center console. A friction knob for adjusting throttle and mixture control feel and position stability is located on the right side of the console. An accessory outlet, map compartment and audio controls are located in the console between the front seats. An hour meter, emergency egress hammer, and headset jacks are installed below the console armrest. All 3-0 Page Dec 0
2 MODEL SR0. MAINTENANCE PRACTICES A. Instrument Panel - Serials 00 thru 0, 06 & subs w/o Perspective Avionics (See Figure 3-0) () Removal - Instrument Panel (a) Disconnect battery. (Refer to -30) (b) Remove glareshield. (Refer to -0) (c) Remove MFD. (Refer to 3-60) (d) Remove annunciator panel. (Refer to 3-0) (e) Serials 00 thru 336, 337 thru w/o PFD: Remove altimeter. (Refer to 3-0) Remove attitude indicator. (Refer to 3-0) 3 Remove airspeed indicator. (Refer to 3-0) Remove outside air temperature/clock gage. (Refer to 3-0) Remove vertical speed indicator. (Refer to 3-0) 6 Remove horizontal situation indicator, if installed. (Refer to 3-0) 7 Remove turn coordinator/roll computer, if installed. (Refer to -0) 8 Remove turn coordinator, if installed. (Refer to 3-0) 9 Remove course deviation indicator, if installed. (Refer to 3-0) 0 Remove directional gyro, if installed. (Refer to 3-0) Remove remote GPSS switch, if installed. (Refer to -) Remove altitude selector/alerter, if installed. (Refer to -) (f) Serials 00 thru 67: Remove vacuum gage, if installed. (Refer to 37-0) (g) Serials 337 thru w/ PFD, 3 & subs: Remove PFD. (Refer to 3-60) Remove Fight Director switch assemblies, if installed. (Refer to -) 3 Remove TAWS control switches, if installed. (Refer to 3-0) Remove ignition switch. (Refer to 7-30) (h) Serials 00 thru 8: Remove ammeter select switch, if installed. (Refer to -30) Serials 00 thru 8 w/o Emax: Remove EGT/CHT gage. (Refer to 77-0) 3 Serials 00 thru 8 w/ Emax: Remove EGT/CHT insert. (Refer to 3-0) Remove tachometer. (Refer to 77-0) Remove volt/amp meter. (Refer to -30) 6 Remove oil pressure/temperature gage. (Refer to 79-30) 7 Remove manifold pressure/fuel flow gage. (Refer to 77-0) (i) Serials 8 & subs: Remove glove box. (Refer to -0) (j) Remove temperature control knobs. (Refer to -60) (k) Remove screws, washers, and spacers securing instrument panel to console. Remove instrument panel from airplane. () Installation - Instrument Panel (a) Position instrument panel to console and secure with screws, washers, and spacers. (b) Install temperature control knobs. (Refer to -60) (c) Serials 8 & subs: Install glove box. (Refer to -0) (d) Serials 00 thru 8: Install manifold pressure/fuel flow gage. (Refer to 77-0) Install oil pressure/temperature gage. (Refer to 79-30) 3 Install volt/amp meter. (Refer to -30) 3-0 Page Jun 00 Serials 00 thru 0, 06 & subs w/o Perspective Avionics
3 MODEL SR0 Install tachometer. (Refer to 77-0) Serials 00 thru 8 w/o Emax: Install EGT/CHT gage. (Refer to 77-0) 6 Serials 00 thru 8 w/ Emax: Install EGT/CHT insert. (Refer to 3-0) 7 Install ammeter select switch, if installed. (Refer to -30) (e) Serials 337 thru w/ PFD, 3 & subs: Install ignition switch. (Refer to 7-30) Install TAWS control switches, if installed. (Refer to 3-0) 3 Install Fight Director switch assemblies, if installed. (Refer to -) Install PFD. (Refer to 3-60) (f) Serials 00 thru 336, 337 thru w/o PFD: Install remote GPSS switch, if installed. (Refer to -) Install altitude selector/alerter, if installed. (Refer to -) 3 Install directional gyro, if installed. (Refer to 3-0) Install course deviation indicator. (Refer to 3-0) Install turn coordinator, if installed. (Refer to 3-0) 6 Install turn coordinator/roll computer, if installed. (Refer to -0) 7 Install horizontal situation indicator, if installed. (Refer to 3-0) 8 Install vertical speed indicator. (Refer to 3-0) 9 Install outside air temperature/clock gage. (Refer to 3-0) 0 Install airspeed indicator. (Refer to 3-0) Install attitude indicator. (Refer to 3-0) Install altimeter. (Refer to 3-0) (g) Perform Functional Test - Pitot System Leak Test. (Refer to 3-0) (h) Perform Functional Test - Static System Leak Test. (Refer to 3-0) (i) Perform Functional Test - Altitude Encoder Calibration. (Refer to 3-0) (j) Install annunciator panel. (Refer to 3-0) (k) Install MFD. (Refer to 3-60) (l) Install glareshield. (Refer to -0) (m) Connect battery. (Refer to -30) (n) Perform Functional Test - Instrument Panel. (Refer to 3-0) (o) Perform Airplane Operational and Functional Checks. (Refer to 0-30) (3) Functional Test - Instrument Panel (a) Perform Operational Test - Multi-Function Display. (Refer to 3-60) (b) Perform Functional Test - Annunciator. (Refer to 3-0) (c) Serials 00 thru 336, 337 thru w/o PFD: Perform functional and operational tests. Perform Functional Test - Altimeter. (Refer to 3-0) Perform Operational Test - Attitude Indicator. (Refer to 3-0) 3 Perform Functional Test - Airspeed Indicator. (Refer to 3-0) Perform Functional Test - OAT Gage/Clock. (Refer to 3-0) Perform Functional - Vertical Speed Indicator. (Refer to 3-0) 6 Perform Operational Test - HSI. (Refer to 3-0) 7 Perform Operational Test - Turn Coordinator. (Refer to 3-0) 8 Perform Operational Test - Directional Gyro, if installed. (Refer to 3-0) (d) Serials 337 thru w/ PFD, 3 thru 0, 06 & subs w/o Perspective Avionics: Perform functional and operational tests. Perform Functional Check - Ignition Switch. (Refer to 7-30) Perform Functional Test - Flight Guidance Programmer/Computer. (Refer to -) Serials 00 thru 0, 06 & subs w/o Perspective Avionics 3-0 Page 3 Jun 00
4 MODEL SR0 (e) 3 Perform Operational Test - Flight Director, if installed. (Refer to -) Perform Operational Test - TAWS Processor, if installed. (Refer to 3-0) Serials 00 thru 8: Perform functional and operational tests. Perform Operational Test - Tachometer. (Refer to 77-0) Serials 00 thru 8 w/o EMax Engine Monitoring: Perform Operational Test - EGT/CHT Gage. (Refer to 77-0) 3 Perform Operational Test - MAP/Fuel Flow Gage. (Refer to 77-0) Perform Operational Test - Oil Pressure/Temperature Gage. (Refer to 79-30) Perform Operational Test - Volt / Amp Meter. (Refer to -30) 6 Perform Operational Test - Ammeter Select Switch. (Refer to -30) 3-0 Page Jun 00 Serials 00 thru 0, 06 & subs w/o Perspective Avionics
5 MODEL SR0 B. Instrument Panel - Serials 06 & subs w/ Perspective Avionics and -Inch Displays (See Figure 3-0) () Removal - Instrument Panel (a) Disconnect battery. (Refer to -30) (b) Remove glareshield. (Refer to -0) (c) Remove MFD. (Refer to 3-60) (d) Remove PFD. (Refer to 3-60) (e) Remove LH instrument panel. Remove clamp securing environmental duct to instrument panel. Remove ignition switch. (Refer to 7-30) 3 Remove Fight Director switch assemblies, if installed. (Refer to -) Remove screw, washer, and spacer securing instrument panel to bolster panel. Remove screws and washers securing instrument panel to support. (f) Remove center instrument panel. Remove reversionary switch. (Refer to 3-60) Remove screws and washers securing instrument panel to console. Remove instrument panel from airplane. (g) Remove RH instrument panel. Remove clamp securing environmental duct to instrument panel. Remove environmental control module. (Refer to -60) 3 Remove screw, washer, and spacer securing instrument panel to bolster panel. Remove screws and washers securing instrument panel to support. () Installation - Instrument Panel (a) Install LH instrument panel. Position instrument panel to bolster panel and secure with screw, washer, and spacer. Position instrument panel to support and secure with screws and washers. 3 Install ignition switch. (Refer to 7-30) Install Fight Director switch assemblies, if installed. (Refer to -) (b) Install center instrument panel. Position instrument panel to console and secure with screws and washers. Install reversionary switch. (Refer to 3-60) (c) Install RH instrument panel. Position instrument panel to bolster panel and secure with screw, washer, and spacer. Position instrument panel to support and secure with screws and washers. 3 Install environmental control module. Position environmental duct to instrument panel and secure with clamp. (d) Install PFD. (Refer to 3-60) (e) Install MFD. (Refer to 3-60) (f) Install glareshield. (Refer to -0) (g) Connect battery. (Refer to -30) (3) Functional test - Instrument Panel (a) Perform Operational Test - Multi-Function Display. (Refer to 3-60) (b) Perform Functional Check - Ignition Switch. (Refer to 7-30) (c) Perform Functional Test - Flight Guidance Programmer/Computer. (Refer to -) (d) Perform Operational Test - Flight Director, if installed. (Refer to -) Serials 06 & subs w/ Perspective Avionics and - Inch Displays 3-0 Page Jun 00
6 MODEL SR0 C. Instrument Panel - Serials 06 & subs w/ Perspective Avionics and 0-Inch Displays (See Figure 3-0) () Removal - Instrument Panel (a) Disconnect battery. (Refer to -30) (b) Remove glareshield. (Refer to -0) (c) Remove MFD. (Refer to 3-60) (d) Remove PFD. (Refer to 3-60) (e) Remove clamps securing environmental ducts to instrument panel. (f) Remove ignition switch. (Refer to 7-30) (g) Remove Fight Director switch assemblies, if installed. (Refer to -) (h) Remove reversionary switch. (Refer to 3-60) (i) Remove environmental control module. (Refer to -60) (j) Remove screws, washers, and spacers securing instrument panel to bolster panel. (k) Remove screws and washers securing instrument panel to supports. Remove instrument panel from airplane. () Installation - Instrument Panel (a) Position instrument panel to bolster panel and secure with screws, washers, and spacers. (b) Position instrument panel to supports and secure with screws and washers. (c) Install environmental control module. (d) Install reversionary switch. (Refer to 3-60) (e) Install Fight Director switch assemblies, if installed. (Refer to -) (f) Install ignition switch. (Refer to 7-30) (g) Position environmental ducts to instrument panel and secure with clamps. (h) Install PFD. (Refer to 3-60) (i) Install MFD. (Refer to 3-60) (j) Install glareshield. (Refer to -0) (k) Connect battery. (Refer to -30) (3) Functional Test - Instrument Panel (a) Perform Operational Test - Multi-Function Display. (Refer to 3-60) (b) Perform Functional Check - Ignition Switch. (Refer to 7-30) (c) Perform Functional Test - Flight Guidance Programmer/Computer. (Refer to -) (d) Perform Operational Test - Flight Director, if installed. (Refer to -) 3-0 Page 6 Jun 00 Serials 06 & subs w/ Perspective Avionics and 0- Inch Displays
7 MODEL SR0 D. Bolster Plate - Serials 68 thru 336, 337 thru w/o PFD (See Figure 3-0) () Removal - Bolster Plate (a) Disconnect battery. (Refer to -30) (b) Remove LH kick plate. (Refer to -0) (c) Remove nut securing ignition switch to bolster plate. (Refer to 7-30) (d) Remove screws and washers securing bolster plate to console. Remove bolster plate. () Installation - Bolster Plate (a) Install screws and washers securing bolster plate to console. (b) Install nut securing ignition switch to bolster plate. (Refer to 7-30) (c) Install LH kick plate. (Refer to -0) (d) Connect battery. (Refer to -30) Serials 68 thru 336, 337 thru w/o PFD 3-0 Page 7 Jun 00
8 MODEL SR0 E. Bolster Plate - Serials 337 thru w/ PFD, 3 & subs w/o MD30 Standby Attitude Module (See Figure 3-0) () Removal - Bolster Plate (a) Disconnect battery. (Refer to -30) (b) Remove airspeed indicator. (Refer to 3-0) (c) Remove attitude indicator, if installed. (Refer to 3-0) (d) Remove altimeter. (Refer to 3-0) (e) Remove screws, washers, and spacers securing bolster plate to console. Remove bolster plate. () Installation - Bolster Plate (a) Place bolster plate into position and secure to console with screws, washers, and spacers. (b) Install airspeed indicator. (Refer to 3-0) (c) Install attitude indicator, if installed. (Refer to 3-0) (d) Install altimeter. (Refer to 3-0) (e) Perform Adjustment/Test - Pitot System Leak Test. (Refer to 3-0) (f) Perform Adjustment/Test - Static System Leak Test. (Refer to 3-0) (g) Connect battery. (Refer to -30) 3-0 Page 8 Dec 0 Serials 337 thru w/ PFD, 3 & subs w/o MD30 Standby Attitude Module
9 MODEL SR0 F. Bolster Plate - Serials 73 & subs w/ MD30 Standby Attitude Module (See Figure 3-0) () Removal (a) Disconnect battery. (Refer to -30) (b) Remove MD30 Standby Attitude Module. (Refer to 3-0) (c) Remove center bolster trim. (Refer to -0) (d) Remove screws, washers, and spacers securing bolster plate to console. Remove bolster plate. () Installation (a) Place bolster plate into position and secure to console with screws, washers, and spacers. (b) Install center bolster trim. (Refer to -0) (c) Install MD30 Standby Attitude Module. (Refer to 3-0) (d) Connect battery. (Refer to -30) Serials 73 & subs w/ MD30 Standby Attitude Module 3-0 Page 9 Dec 0
10 MODEL SR0 G. EGT/CHT Gage Insert - Serials 3 thru 8 w/ EMax, 337 thru 8 w/ SRV (See Figure 3-0) () Removal - EGT/CHT Insert (a) Set BAT, BAT, and AVIONICS switches to OFF positions. (b) Remove glareshield. (Refer to -0) (c) Remove screws, washers, and nuts securing gage insert to instrument panel. () Installation - EGT/CHT Insert (a) Position gage insert to instrument panel and secure with screws, washers, and nuts. (b) Install glareshield. (Refer to -0) 3-0 Page 0 Dec 0 Serials 3 thru 8 w/ EMax, 337 thru 8 w/ SRV
11 MODEL SR0 7 BOLSTER PANEL (REF) Serials 68 thru w/o PFD before SB X Serials 00 thru 03. LOWER WINDSHIELD TRIM (REF) GLARESHIELD (REF) Serials 68 thru w/o PFD after SB X BOLSTER PANEL (REF) NOTE Serials 3 thru : Airplanes with engine monitoring. 3 Serials 00 thru 336, 337 thru w/o PFD. LEGEND. Screw. Washer 3. Instrument Panel. Spacer. Instrument Panel Support 6. Nut 7. Bolster Plate 8. EGT/CHT Gage Insert 9. Instrument Cover 0. Nutclip SR0_MM3_H Figure 3-0 Instrument Panel - Serials 00 thru 336, 337 thru w/o PFD (Sheet of ) Serials 00 thru 336, 337 thru w/o PFD 3-0 Page Dec 0
12 MODEL SR0 BOLSTER PANEL (REF) Serials 337 & subs w/ SRV. 6 Serials 337 thru w/ PFD, 3 thru 8. BOLSTER PANEL (REF) 3 Serials 8 & subs. NOTE 7 Serials 3 thru 8: Airplanes with engine monitoring. Serials 337 thru w/ PFD, 3 thru 0, 06 & subs w/o Perspective Avionics. LEGEND. Screw. Washer 3. Instrument Panel. Spacer. Instrument Panel Support 6. Nut 7. Bolster Plate 8. EGT/CHT Gage Insert SR0_MM3_8I Figure 3-0 Instrument Panel - Serials w/ PFD, 3-0, 06 & subs w/o Perspective Avionics (Sheet of ) 3-0 Page Dec 0 Serials w/ PFD, 3-0, 06 & subs w/o Perspective Avionics
13 MODEL SR BOLSTER PANEL (REF) Serials w/ MD30 Standby Attitude Module 7 LEGEND. Screw. Washer 3. Instrument Panel. Spacer. Instrument Panel Support 6. Nut 7. Bolster Plate. Fan Bracket Figure 3-0 Instrument Panel - Serials 06 & subs w/ Perspective Avionics and -inch Displays (Sheet 3 of ) Serials 06 & subs w/ Perspective Avionics and - inch Displays Serials 06 & subs w/ Perspective Avionics and -inch Displays. SR0_MM3_7B 3-0 Page 3 Dec 0
14 MODEL SR BOLSTER PANEL (REF) Serials w/ MD30 Standby Attitude Module 6 7 LEGEND. Screw. Washer 3. Instrument Panel. Spacer. Instrument Panel Support 6. Nut 7. Bolster Plate. Fan Bracket Serials 06 & subs w/ Perspective Avionics and 0-inch Displays. SR0_MM3_300B Figure 3-0 Instrument Panel - Serials 06 & subs w/ Perspective Avionics and 0-inch Displays (Sheet of ) 3-0 Page Dec 0 Serials 06 & subs w/ Perspective Avionics and 0- inch Displays
15 MODEL SR0 H. Circuit Breaker Panel () Removal - Circuit Breaker Panel (a) Disconnect battery. (Refer to -30) (b) Serials 00 thru 0, 06 & subs w/o Perspective Avionics: Remove screws securing circuit breaker panel to console. (Refer to -0) (c) Serials 06 & subs w/ Perspective Avionics: Remove turn studs securing circuit breaker panel to console. (d) Identify and disconnect all wire terminal connectors. Remove circuit breaker panel from airplane. () Installation - Circuit Breaker Panel (a) Place circuit breaker panel into position and connect all wire terminal connectors. (b) Serials 00 thru 0, 06 & subs w/o Perspective Avionics: Position circuit breaker panel to center console and secure with screws. (c) Serials 06 & subs w/ Perspective Avionics: Position circuit breaker panel to center console and secure with turn studs. (d) Connect battery. (Refer to -30) All 3-0 Page Dec 0
16 MODEL SR0 I. Bolster Switch Panel - Serials 00 thru 83 (See Figure 3-0) () Removal - Bolster Switch Panel (a) Disconnect battery. (Refer to -30) (b) Remove dimmer switch control knobs from bolster panel. (c) Remove screws, washers, and nut securing switch panel and finish panel to console. (d) Disconnect electrical connectors from switch panel. () Installation - Bolster Switch Panel (a) Connect electrical connectors to switch panel. (b) Position switch panel and finish panel to console and secure with screws, washers, and nut. (c) Install dimmer switch control knobs to bolster panel. (d) Connect battery. (Refer to -30) 3-0 Page 6 Dec 0 Serials 00 thru 83
17 MODEL SR0 J. Bolster Switch Panel - Serials 8 & subs (See Figure 3-0) () Removal - Bolster Switch Panel (a) Disconnect battery. (Refer to -30) (b) Remove screws securing bolster switch panel to console. (c) Disconnect electrical connectors from bolster switch panel. () Installation - Bolster Switch Panel (a) Connect electrical connectors to bolster switch panel. (b) Position bolster switch panel to console and secure with screws. (c) Connect battery. (Refer to -30) Serials 8 & subs 3-0 Page 7 Dec 0
18 MODEL SR0 K. EL Voltage Inverter - Serials 886 & subs (See Figure 3-0) () Removal - EL Voltage Inverter (a) Disconnect battery. (Refer to -30) (b) Remove LH kick plate. (Refer to -0) (c) Disconnect EL voltage inverter connector from bolster switch panel. (d) Remove screws, washers, and nuts securing EL voltage inverter to rib strut. () Installation - EL Voltage Inverter (a) Position EL voltage inverter to rib strut and secure with screws, washers, and nuts. (b) Connect EL voltage inverter connector to bolster switch panel. (c) Install LH kick plate. (Refer to -0) (d) Connect battery. (Refer to -30) 3-0 Page 8 Dec 0 Serials 886 & subs
19 MODEL SR0 BOLSTER PANEL (REF) 3 3 Serials 00 thru 7. BOLSTER PANEL (REF) Serials 8 thru BOLSTER PANEL (REF) LEGEND. Screw. Washer 3. Finish Panel. Switch Panel. Nut 6. Bolster Switch Panel Serials 8 thru 877, 879 thru 88. SR0_MM3_D Serials 00 thru 88 Figure 3-0 Bolster Switch Panel Installation - Serials 00 thru 88 (Sheet of ) 3-0 Page 9 Dec 0
20 MODEL SR0 6 7 LEGEND. Screw. Washer. Nut 6. Bolster Switch Panel 7. EL Inverter SR0_MM3_ Page 0 Dec 0 Figure 3-0 Bolster Switch Panel Installation - Serials 886 & subs (Sheet of ) Serials 886 & subs
CIRRUS AIRPLANE MAINTENANCE MANUAL
STALL WARNING SYSTEM 1. DESCRIPTION A. Stall Warning System - Serials 05 thru 2015, 2016 & subs w/o Perspective Avionics The airplane uses an electro-pneumatic stall warning system. As the angle of attack
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
ELECTRICAL LOAD DISTRIBUTION. DESCRIPTION The power distribution system for this airplane consists of the main distribution bus and the essential distribution bus in the MCU along with the associated buses
More informationINTEGRATED ENGINE INSTRUMENT SYSTEMS
All INTEGRATED ENGINE INSTRUMENT SYSTEMS. DESCRIPTION This section describes that portion of the engine indicating system which is used to analyze engine performance, temperature, and condition. Serials
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR FLIGHT ENVIRONMENTAL SYSTEMS. DESCRIPTION This section covers that portion of the system which senses environmental conditions and uses the data to influence navigation of the airplane. This includes
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 FLIGHT ENVIRONMENTAL SYSTEMS. DESCRIPTION This section covers that portion of the system which senses environmental conditions and uses the data to influence navigation of the airplane. This
More informationSTALL WARNING SYSTEM 1. DESCRIPTION A.
STALL WARNING SYSTEM 1. DESCRIPTION A. Stall Warning System - Serials w/o Perspective Avionics The airplane uses an electro-pneumatic stall warning system. As the angle of attack increases and the airplane
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
INDICATING 1. DESCRIPTION This section describes that portion of the oil system which is used to indicate the quantity, temperature, and pressure of the oil. Components included are the oil filler cap/dipstick,
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
ANALYZERS - ENGINE MONITORING. DESCRIPTION This section describes that portion of the engine indicating system which is used to analyze engine performance, temperature, and condition. Serials 00 thru 8
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
All ATTITUDE AND DIRECTION 1. DESCRIPTION This section contains information pertaining to those portions of the system which use magnetic, gyroscopic, and inertia forces. Included is the magnetic compass,
More information33-10 FLIGHT COMPARTMENT
FLIGHT COMPARTMENT. DESCRIPTION Flight compartment interior lighting consists of instrument lights, glareshield flood lights, overhead dome light, individual reading lights, pilot control lights, CAPS
More information24-00 ELECTRICAL POWER
ELECTRICAL POWER 1. GENERAL This chapter contains information on DC Generation, External Power, and Electrical Load Distribution. The airplane is equipped with a two-alternator, two-battery, 28-volt direct
More informationAttitude And Direction
CIRRUS AIRPLANE MAINTENANCE MANUAL Attitude And Direction CHAPTER 34-20: ATTITUDE AND DIRECTION GENERAL 34-20: ATTITUDE AND DIRECTION 1. General This section contains information pertaining to those portions
More informationSYSTEM LOAD CHARTS AND BUS SCHEMATICS
SYSTEM LOAD CHARTS AND BUS SCHEMATICS 1. GENERAL The airplane is equipped with a two alternator system, with each alternator operating continuously. Serials 22-0002 thru 22-1601, 22-1603 thru 22-1820,
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
All INDICATING. DESCRIPTION A. Fuel Quantity Serials 005 thru 885: A fuel quantity gage is installed in the center console directly forward of the fuel selector valve. The fuel quantity gage indicates
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
PASSENGER COMPARTMENT 1. DESCRIPTION This section covers the passenger compartment lighting. A. Passenger Eyeball Lights Individual eyeball-type reading lights are installed in the headliner above each
More information22-11 SYSTEM 55 AUTOPILOT
SYSTEM 55 AUTOPILOT 1. DESCRIPTION This section covers those systems and components which use inputs to the system to automatically control the flight path of the aircraft through adjustment to the pitch/roll
More informationA. Stall Warning System - Serials w/o Ice Protection
Stall Warning System GENERAL 27-31: STALL WARNING SYSTEM 1. General A. Stall Warning System - Serials w/o Ice Protection The airplane uses an electro-pneumatic stall warning system. As the angle of attack
More informationATTITUDE AND DIRECTION
All ATTITUDE AND DIRECTION 1. DESCRIPTION This section contains information pertaining to those portions of the system which use magnetic, gyroscopic, and inertia forces. Included is the magnetic compass,
More informationC I R R U S CONTROLLING DESCRIPTION
CONTROLLING 1. DESCRIPTION Serials 22-0002 & subs: An electric two-speed fuel pump provides boost (low speed) and prime (high speed) for the engine. A console mounted rocker switch located on the center
More informationSR22 Airplane Flight Manual (AFM) Temporary Change
Cirrus Design TPOH Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications:
More informationC I R R U S DISTRIBUTION DESCRIPTION
MODELS SR AND SRT DISTRIBUTION. DESCRIPTION This section contains information on the distribution system. The fuel distribution system consists of electric and mechanical (engine-driven) fuel pumps, fuel
More informationFlight Environmental Systems
CIRRUS AIRPLANE MAINTENANCE MANUAL Flight Environmental Systems CHAPTER 34-0: FLIGHT ENVIRONMENTAL SYSTEMS GENERAL 34-0: FLIGHT ENVIRONMENTAL SYSTEMS. General This section covers that portion of the system
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
POWER CONTROL. DESCRIPTION This section describes those components which furnish a means of controlling engine power. Engine controls for the airplane include the following: control quadrant, throttle
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
SYSTEM 55 AUTOPILOT 1. DESCRIPTION The S-TEC System 55 is a dual axis autopilot system that provides roll stability, heading hold, NAV/GPS tracking, altitude hold, vertical speed selection, automatic glideslope
More informationALT #2 fail light on but Alternator is still charging (MCU 100/120):
ALT #2 fail light on but Alternator is still charging (MCU 100/120): We have seen this happen a lot. The good news is there is probabl nothing wrong with the aircraft. Basic MCU Function: The MCU has a
More information33-40 EXTERIOR LIGHTING
EXTERIOR LIGHTING. DESCRIPTION This section covers that portion of the system which provides illumination outside of the aircraft. This includes the landing light, anti-collision strobe light, and recognition
More informationIndicating. 1. General. A. Fuel Quantity. B. Fuel Flow
Indicating GENERAL 28-40: INDICATING. General A. Fuel Quantity A dual reading fuel quantity indicator is displayed in the Fuel Qty block of the ENGINE page along calibrated vertical bars. The fuel quantity
More informationCessna Citation XLS - Electrical
GENERAL Electrical power for the Citation XLS comes primarily from DC sources originating with the starter/ generators, the Auxiliary Power Unit (APU) or the battery. A receptacle below the left engine
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 EXTERIOR LIGHTING. DESCRIPTION This section covers that portion of the system which provides illumination outside of the aircraft. This includes the landing light, anti-collision strobe light,
More informationThis chapter contains information on DC Generation, External Power, and Electrical Load Distribution.
CIRRUS AIRPLANE MAINTENANCE MANUAL Electrical Power CHAPTER 24-00: ELECTRICAL POWER GENERAL 24-00: ELECTRICAL POWER 1. General This chapter contains information on DC Generation, External Power, and Electrical
More informationC I R R U S PROPELLER GENERAL
PROPELLER 1. GENERAL The airplane employs a 3 blade, constant speed, non-feathering propeller. The blades (composite or aluminum) are mounted in an aluminum hub which contains the pitch changing mechanism
More informationCESSNA 172S NAV III VFR CHECKOUT POH EXAMINATION (Based on N1129K, serial no. 172S revised 10/05/06)
INTRODUCTION, POH CESSNA 172S NAV III VFR CHECKOUT POH EXAMINATION (Based on N1129K, serial no. 172S10315 - revised 10/05/06) 1. Rate of climb at sea level: 2. Service ceiling: 3. Takeoff performance,
More informationCHAPTER 13 INSTRUMENTS
CHAPTER 13 INSTRUMENTS Section Title Page 13.000 Description.............................................. 13.1 13.100 Pitot-Static System......................................... 13.3 13.200 Primary Instruments........................................
More informationVr V STANDARD EQUIPMENT LIST
Vr V5.02.09 STANDARD EQUIPMENT LIST IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for the purpose of generally
More informationCentral Warning Systems
CIRRUS AIRPLANE MAINTENANCE MANUAL Central Warning Systems CHAPTER 31-50: CENTRAL WARNING SYSTEMS GENERAL 31-50: CENTRAL WARNING SYSTEMS 1. General This section describes the Indicating/Recording Systems
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
ELEVATOR AND PITCH TRIM SYSTEM 1. DESCRIPTION This section describes that portion of the flight control system which controls the position and movement of the elevator. Included are; elevator system torque
More informationCESSNA SECTION 4. Unless otherwise noted, the following speeds are based on a maximum weight of 2550 pounds and may be used for any lesser weight.
CESSNA SECTION 4 INTRODUCTION Section 4 provides procedures and amplified instructions for normal operations using standard equipment. Normal procedures associated with optional systems can be found in
More informationLOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual
LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Revision A12 - May, 2015 Title Page LOEP LOR Section 1 All Reformatted to
More informationDC Generation. 1. General. A. DC Generation
CIRRUS AIRPLANE MAINTENANCE MANUAL DC Generation CHAPTER -0: DC GENERATION GENERAL -0: DC GENERATION 1. General (See Figure -0-1) This section covers the systems to generate, regulate, control, and indicate
More informationCHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
FLIGHT CONTROLS 27-00 General 1 Troubleshooting 2 AILERON AND ROLL TRIM SYSTEM 27-10 Aileron System Cables 2 Removal - Aileron System Cables 2 Installation - Aileron System Cables 2 Adjustment/Test - Aileron
More information53-40 ATTACH FITTINGS
ATTACH FITTINGS. DESCRIPTION Attach fittings are provided for attachment of the seats (Refer to -0), baggage straps (Refer to -0), rear seat harnesses (Refer to -0), cargo net straps (Refer to -0), cabin
More informationCHAPTER 24 - ELECTRICAL POWER TABLE OF CONTENTS
ELECTRICAL POWER 24-00 General 1 Electrical Power - Serials w/o Perspective Avionics 1 Electrical Power - Serials w/ Perspective Avionics 1 Troubleshooting 2 DC GENERATION 24-30 Description 1 DC Generation
More informationP68 Observer 2 STANDARD EQUIPMENT LIST V
P68 Observer 2 STANDARD EQUIPMENT LIST V9.03.12 P68 OBSERVER 2 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
PROPELLER 1. GENERAL The airplane employs a 3 blade, constant speed, non-feathering propeller. The blades (composite or aluminum) are mounted in an aluminum hub which contains the pitch changing mechanism
More informationCHAPTER 13 INSTRUMENT SYSTEM
CHAPTER 13 INSTRUMENT SYSTEM Section Title 13-00 Description............................................... 13.1 13-10 Pitot-Static System......................................... 13.3 13-20 Primary Instruments.........................................
More informationC I R R U S BRAKES DESCRIPTION
BRAKES. DESCRIPTION The brake system consists of a single disc brake assembly on each main landing gear wheel, master cylinder for each rudder pedal, hydraulic fluid reservoir, parking brake, and associated
More informationCHAPTER 95 INSTRUMENT SYSTEM
Section Title CHAPTER 95 INSTRUMENT SYSTEM 95-00 Description............................................... 95.1 95-10 Pitot-Static System......................................... 95.3 95-20 Primary Instruments.........................................
More informationVr (P68R) STANDARD EQUIPMENT LIST V
Vr (P68R) STANDARD EQUIPMENT LIST V15.04.16 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for the purpose
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
CENTRAL WARNING SYSTEMS 1. GENERAL This section describes the Central Warning Systems which consists of a Crew Alerting System (CAS) and related sensors and switches. A. Crew Alerting System Aircraft annunciations
More informationAIRPLANE FLIGHT MANUAL AQUILA AT01 AIRPLANE FLIGHT MANUAL - SUPPLEMENT AVE28 GLASS COCKPIT. equipped with ASPEN EFD1000 PFD
SECTION 9 AIRPLANE FLIGHT MANUAL - SUPPLEMENT AVE28 GLASS COCKPIT equipped with ASPEN EFD1000 PFD This AFM supplement is applicable and must be inserted into Section 9 of the Airplane Flight Manual when
More informationFLIGHT SIMULATOR SYSTEMS
FLIGHT SIMULATOR SYSTEMS 1. GENERAL This section describes systems required for simulator operation. This equipment includes the Cirrus Landing Gear Simulator (CLGS). 2. DESCRIPTION The intent of the CLGS
More informationElmendorf Aero Club Aircraft Test
DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 172 For the following questions, you will need to refer to the Pilots Information Manual for the C-172R (180hp). The bonus
More informationPilot's Operating Handbook Supplement AS-03
POH / AFM SECTION 9 Pilot's Operating Handbook Supplement ASPEN EFD1000 PFD This supplement is applicable and must be inserted into Section 9 of the POH when the Aspen Avionics Evolution Flight Display
More informationElmendorf Aero Club Aircraft Test
DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 182 For the following questions, you will need to refer to the Pilots Information Manual for the C-182R. The bonus questions
More informationSECTION 3 EMERGENCY PROCEDURES
SECTION 3 TABLE OF CONTENTS Page Introduction... 3-3 Airspeeds for Emergency Operation... 3-5 CHECKLISTS Engine Failures... 3-6 Engine Failure During Takeoff Run... 3-6 Engine Failure Immediately After
More informationcertified aircraft GENERAL PRICE LIST 2018 P2008JC mkii P TwentyTen cs-23 - FAR 23 P2002JF
certified P92JS cs-vla P2002JF cs-vla P2008JC mkii aircraft cs-vla P TwentyTen cs-23 - FAR 23 p2006t cs-23 - FAR 23 GENERAL PRICE LIST 2018 CS-23 FAR 23 & CS-VLA 18040312 T1001 STANDARD ANALOGUE IFR RETRACTABLE
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
SCHEDULED MAINTENANCE 1. DESCRIPTION These inspections meet the intent of 14 CFR 91.409 and Part 43, Appendix D. In addition to the inspections prescribed by this schedule, the altimeter instrument and
More informationNORMAL CHECKLIST ATTENTION!
Avion Training CHECKLIST Normal Checklist CESSNA 172R / TC-STS Cessna 172 R TC-STS NORMAL CHECKLIST ATTENTION! DO NOT STOW THIS CHECKLIST IN DIRECT SUNLIGHT Avion Training - Doc.nr. 212 Revision 1 / 02022018
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
AIR INTAKES 1. DESCRIPTION This section describes that portion of the power plant which directs mass air flow to the engine. Induction air enters the engine through a filter mounted on the left, forward
More informationFINAL EXAM. 3. Name the items on the control shift in the unmodified aircraft (non ASC-36).
FINAL EXAM Name 1. Total usable fuel is 177 gallons 2. Proper fuel(s) specification for the T-28 is (are): XX (a) 100/130 alternate 100LL (b) 115/145 and 100/130 alternate (c) 115/145 and 100/130 emergency
More information24 ELECTRICAL DC ELECTRICAL SYSTEM DESCRIPTION
24 ELECTRICAL DC ELECTRICAL SYSTEM DESCRIPTION The Direct Current electrical system provides power to most equipment through an electrical bus system. The power may be supplied from one of three sources:
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
BRAKES. DESCRIPTION The brake system consists of single disc brake assembly on each main landing gear wheel, master cylinder for each rudder pedal, hydraulic fluid reservoir, parking brake, and associated
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T CHAPTER 28-00: FUEL GENERAL. Fuel 28-00: FUEL. 1. General
CIRRUS AIRPLANE MAINTENANCE MANUAL Fuel CHAPTER 28-00: GENERAL 28-00: 1. General This chapter contains information on the storage, distribution, and indicating components of the fuel system. The engine
More informationCessna 172RG WARNING. Maximum Demonstrated Crosswind. Takeoff or landing..15 KTS
Cessna 172RG INTRODUCTION: This aircraft checklist contains information from the original manufacturer s Pilot Information Manual. Normal procedures associated with optional systems can be found in Section
More informationCHAPTER 22 AUTOPILOT
Section Title CHAPTER 22 AUTOPILOT 22-00 Description............................................... 22.1 22-10 (Pitch) Servo Assembly...................................... 22.3 22-20 (Roll) Servo Assembly.......................................
More informationBasic Ice Protection System
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Basic Ice Protection System When the Ice Protection System is installed on the aircraft, this POH
More informationJump to Table of Contents
Jump to Table of Contents PIPER AIRCRAFT CORPORATION PA-28R-201, CHEROKEE ARROW III SECTION 3 EMERGENCY PROCEDURES 3.3 EMERGENCY PROCEDURES CHECK LIST ENGINE FIRE DURING
More informationCARENADO COPYRIGHTS. Normal & Emergency Checklist
NORMAL PROCEDURES CHECKLIST PREFLIGHT CHECK Control wheel -- RELEASE BELTS Avionics -- OFF Master Switch -- ON Fuel quantity gauges -- CHECK Master switch -- OFF Ignition -- OFF Exterior -- CHECK FOR DAMAGE
More informationAUTOPILOT SELECTION GUIDE & PRICE LIST. The NEW
AUTOPILOT SELECTION GUIDE & PRICE LIST The NEW February 1, 2001 TABLE OF CONTENTS How To Use This Selection Guide... 2 Rate Based vs. Attitude Based Autopilots... 2 S-TEC s Building Block Design Philosophy...
More informationDO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test. Cessna - 182
DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 182 For the following questions, you will need to refer to the Pilots Information Manual for the C-182R. The bonus questions
More informationP2010. twenty ten. Specifica on & Descrip on INTRODUCTION
P2010 twenty ten Specifica on & Descrip on INTRODUCTION This document is published for the purpose of providinggeneral information for the evaluation of design, performance and equipment of the Tecnam model
More information2007 A119 Koala Price: Make an Offer
2007 A119 Koala Price: Make an Offer Aircraft Details Manufacture Date: 2007 Hours: 87hrs Airframe: Aluminium alloy & bonded panel fuselage Semimonocoque aluminium alloy tail boom Skid type landing gear
More informationVso 61. Vs1 63. Vr 70. Vx 76. Vxse 78. Vy 89. Vyse. 89 (blue line) Vmc. 61 (radial redline) Vsse 76. Va 134) Vno 163
PA34-200T Piper Seneca II Normal procedures V-speeds Knots Vso 6 Vs 63 Vr 70 Vx 76 Vxse 78 Vy 89 Vyse Vmc 89 (blue line) 6 (radial redline) Vsse 76 Va 2-36(@4507lbs 34) Vno 63 Vfe 38 (0*)/2(25*)/07(40*)
More informationSECTION 7 AIRPLANE AND SYSTEMS DESCRIPTION
FOUND SECTION 7 SECTION 7 AIRPLANE AND SYSTEMS DESCRIPTION TABLE OF CONTENTS Page Introduction... 7-5 Airframe... 7-5 Flight Controls... 7-7 Aileron Control System... 7-7 Elevator Control System... 7-7
More informationPASSENGER AND CREW DOORS
MODELS SR AND SRT PASSENGER AND CREW DOORS. DESCRIPTION AND OPERATION Serials -000 thru -00: The two crew/passenger doors incorporate a flush-mount outside door handle, key-operated door lock, and a conventional
More informationC I R R U S BRAKES DESCRIPTION
BRAKES. DESCRIPTION The brake system consists of a single disc brake assembly on each main landing gear wheel, master cylinder for each rudder pedal, hydraulic fluid reservoir, parking brake, and associated
More informationEMERGENCY PROCEDURES TABLE OF CONTENTS
CESSNA SECTION 3 TABLE OF CONTENTS Page Introduction............................................3-5 Airspeeds For Emergency Operations........................3-5.........................3-6 ENGINE FAILURES.....................................3-6
More informationService Bulletin No.: DAC Rev. 2 Date Issued: 28 January 2013 Title: Installation of backup Artificial Horizon Indicator
Page: 1 of 18 1. ATA Code: 3420 2. Effectivity: All DA20-C1 Aircraft equipped with the Garmin G500 system. 3. General: This Service Bulletin (SB) provides the installation instructions for installing a
More informationAIRSPEEDS FOR EMERGENCY OPERATIONS
INTRODUCTION Section 3 provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight
More information1974 Mitsubishi MU-2K N462MA Serial Number 302
1974 Mitsubishi MU-2K N462MA Serial Number 302 Avionics Chelton Synthetic Vision System (3 Displays) with latest Software (SBAS/WAAS/LPV/VNAV) Updated Next Generation ADAHRS (Combined AHRS and ADC) Remote
More informationCessna 172P PPL Checklist Page 1
Cessna 172P PPL Checklist 06-08-2017 Page 1 Cessna 172P PPL Checklist 06-08-2017 Page 2 Checklist Items Informational Items Critical Memory Items PREFLIGHT COCKPIT CHECK (DO-LIST) Pitot Cover -- REMOVE
More informationCHAPTER 77 ENGINE INDICATING
FBA-C, FBA-C CHAPTER 77 ENGINE INDICATING 77-00 Page July 4, 0 FBA-C, FBA-C List of Effective Pages Chapter / Section Page No. Date Chapter / Section Page No. Date 77-00 Jul 4, 0 Jul 4, 0 77-05 Jul 4,
More informationCOLUMBIA 350 EMERGENCY PROCEDURES
COLUMBIA 350 EMERGENCY PROCEDURES TABLE OF CONTENTS EMERGENCY PROCEDURES LANDING AND TAKEOFF Engine Failure During Takeoff...1 Engine Failure Immediately After Takeoff...1 Engine Failure During Climb to
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
1. GENERAL This chapter contains information on the storage, distribution, and indicating components of the fuel system. The engine is supplied with fuel drawn out of the left or right integral fuel tank
More informationIn-Flight Entertainment System
GENERAL In-Flight Entertainment System 44-20: IN-FLIGHT ENTERTAINMENT SYSTEM 1. General This chapter describes the systems, units, and components which provide entertainment to the passengers with music,
More informationN123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIONS. Best Rate of Climb (gear up, flaps up)
N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIS Best Rate of Climb (gear down, flaps up) Best Rate of Climb (gear up, flaps up) Turbulent Air
More informationAutopilot Selection Guide
Autopilot Selection Guide TABLE OF CONTENTS How To Use This Selection Guide...2 Rate Based vs. Attitude Based Autopilots...2 The S-TEC Autopilot Building Block Design Philosophy...2 The S-TEC Autopilot
More informationCESCOM 20 - Projected Maintenance Due
Date Average Projected Days Months Overdue Maintenance Tasks Position Description Drawing # / Task # City 51211 PHASE 11 051211 051208 : L RIGHT 051208 : R Scheduled Maintenance Tasks Mod Lvl Part Number
More information57-50 FLIGHT SURFACES
FLIGHT SURFACES 1. DESCRIPTION The flaps are mounted to the trailing edge of each wing between the inboard end of the ailerons and the fuselage. The ailerons are located near the wing tips and hinge to
More informationLOG OF REVISIONS. Description of Revisions Initial Release. Add underspeed
LOG OF REVISIONS Revision Number 00 Revised Pages ALL Description of Revisions Initial Release FAA Approval Robert G. Mann Date 18 Jun 10 01 4, 20, 23, 24, 27, 28, 29, 30, 31 Add underspeed Robert G. Mann
More informationC I R R U S CABIN 1. DESCRIPTION A. Cabin Seats B. Radio Module Assembly
CABIN. DESCRIPTION This section covers cabin compartment seats, seat harnesses, trim, cabin headliner, floor covering, sunvisors, grab handles, headset hooks, coat hooks, drink holders, storage pockets,
More informationDocument No. ST-931-RFM-0001
275 Palos Verdes Dr. North Document No. ST-931-RFM-1 FAA APPROVED Rotorcraft Flight Manual Supplement to the Robinson R44 Pilot s Operating Handbook and FAA Approved Rotorcraft Flight Manual HeliSAS Aircraft
More information2011 DAHER-SOCATA TBM850 S/N569 D-FRAS Garmin 1000 Avionics / MT 5-blade propeller
2011 DAHER-SOCATA TBM850 S/N569 D-FRAS Garmin 1000 Avionics / MT 5-blade propeller If you want to stay in your comfort zone, but while cruising at 31,000 feet and with an approach speed slow enough to
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
POWER PLANT 1. GENERAL This chapter describes maintenance practices for the airplane systems which provide the means to induce and convert fuel-air mixture into power such as the engine, baffling, cowling,
More informationCessna 172S Skyhawk. AFTER LANDING CHECK RPM CHECK 2. Flaps UP 3. Transponder STANDBY 4. Strobes OFF 5. Contact Ground as Required. 121.
PRE-LANDING CHECK 1. ATIS/AWOS/ASOS OBTAIN 2. Seat Belts CHECK 3. Autopilot OFF 4. Master Switch ON 5. Ignition BOTH 6. Circuit Breakers ALL IN 7. Landing Light AS REQ. 8. Mixture (Push) RICH 9. Fuel Selector
More informationWelcome to Orange County Flight Center
Welcome to Orange County Flight Center e POH Summary for the airplane you ll be flying is attached. Please study it and then review areas of concern using the Pilot s Operating Handbook/Airplane Flight
More informationCessna 152 Checklist
Cessna 152 Checklist This checklist covers the operation of the model 152. Use at your own risk, the author nor the publisher is responsible for any damage or accidents resulting from the use of this checklist.
More informationBest Glide 75 kias (Max Gross)
CESSNA 172XP CHECKLIST PREFLIGHT (Interior) 1. ACFT DOCS / INSPECTIONS--------CHECK 2. TACH TIME-----------------------------RECORD 3. CONTROL LOCK---------------------REMOVE 4. ELEVATOR / RUDDER TRIM------------
More informationPA28R ARROW CHECKLIST
PA28R ARROW CHECKLIST 2300.11.0112 1 Normal Procedures Initial PREFLIGHT CHECK General Appearance... CHECKED Position & Taxi Path... CHECKED Tie Downs, Locks, Chocks & Covers... REMOVED Cockpit Controls...UNLOCKED
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 All PASSENGER AND CREW DOORS. DESCRIPTION AND OPERATION Serials 005 thru 4: The two crew/passenger doors incorporate a flush-mount outside door handle, key-operated door lock, and a conventional
More information