Cessna Aircraft Compagny Manuel de vol SECTION 2 Winchita Kansas CESSNA 172S LIMITES D'EMPLOI

Transcription

1 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 Novembre 30 Mai

2 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS OPEATNG LMTATONS TABLE O CONTENTS Page ntroduction Airspeed Limitations Airspeed ndicator Markings Powerplant Limitations Powerplant nstrument Markings Weight Limits Normal Category Maximum Weight in Baggage Compartment - Normal Category. 2-8 Utility Category Maximum Weight in Baggage Compartment - Utility Category Center Of Gravity Limits Normal Category Utility Category Maneuver Limits Normal Category Utility Category light Load actor Limits Normal Category Utility Category Kinds Of Operations Limits Kinds Of Operations Equipment List uel Limitations lap Limitations System Limitations Aux Audio System V Power System G1000 Limitations Garmin GC 700 ACS (if installed) Terrain Awareness and Warning System (TAWS-B) Placards AA APPOVED 172SPHBUS-00 U.S. 2-1/2-2

3 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 30 Mai

4 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas Novembre 1998

5 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 Novembre 30 Mai

6 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas Novembre 1998

7 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 Novembre 30 Mai

8 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas Novembre 1998

9 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 Novembre Mai

10 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas Novembre 1998

11 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 30 Novembre Mai

12 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas Novembre 1998

13 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 Novembre 30 Mai

14 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas Novembre 1998

15 Cessna Aircraft Compagny Manuel de vol SECTON 2 Winchita Kansas CESSNA 172S LMTES D'EMPLO 1 Novembre 30 Mai

16 SECTON 2 Manuel de vol Cessna Aircraft Compagny LMTES D'EMPLO CESSNA 172S Winchita Kansas PAGE LASSEE BLANCHE NTENTONNELLEMENT Novembre 1998

17 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS KNDS O OPEATONS EQUPMENT LST System, nstrument, Equipment and/or unction PLACADS AND MAKNGS 1-172S Nav - GC 700 ACS POH/AM 2 - Garmin G1000 Cockpit eference Guide A CONDTONNG KND O OPEATON 1 - orward Avionics an PD an MD an Aft Avionics an COMMUNCATONS 1 - VH COM ELECTCAL POWE 1-24V Main Battery V Alternator V D AY V N G H T D AY N G H T COMMENTS Accessible to pilot in flight Accessible to pilot in flight. 3-24V Standby Battery 0 * * * * efer to Note Main Ammeter Standby Ammeter 0 * * * * efer to Note 1. NOTE 1. The European Aviation Safety Agency (EASA) requires the 24V Standby Battery and Standby Ammeter to successfully complete the pre-flight check before operating the airplane in V night, day, or night conditions in Europe. Correct operation of the 24V Standby Battery and Standby Ammeter is recommended for all other operations. (Continued Next Page) AA APPOVED 172SPHBUS-00 U.S. 2-13

18 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS KNDS O OPEATONS EQUPMENT LST (Continued) System, nstrument, Equipment and/or unction EQUPMENT AND UNSHNGS KND O OPEATON COMMENTS 1 - Seat Belt Assembly Each Seat Occupant 2 - Shoulder Harness ront Seat Occupants LGHT CONTOLS 1 - lap Position ndicator lap Motor Elevator Trim System Elevator Trim ndicator UEL SYSTEM 1 - Electric uel Pump uel Quantity ndicator - L Tank uel Quantity ndicator - Tank CE AND AN POTECTON 1 - Alternate Static Air Source Alternate nduction Air System NDCATNG/ECODNG SYSTEM 1 - Stall Warning System System Annunciator and Warning Displays LANDNG GEA V D A Y V N G H T D A Y N G H T Wheel airings emovable (Continued Next Page) 2-14 U.S. AA APPOVED 172SPHBUS-00

19 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS KNDS O OPEATONS EQUPMENT LST (Continued) System, nstrument, Equipment and/or unction LGHTNG KND O OPEATON 1 - PD Bezel Lighting V D A Y NOTE 2. PD backlighting is required for day V flight if MD backlighting has failed. Display backup mode must be active so engine indicators are shown. 3. MD backlighting is required for day V flight if PD backlighting has failed. Display backup mode must be active so flight instruments are shown. (Continued Next Page) COMMENTS 2 - PD Backlighting * *efer to Note MD Bezel Lighting MD Backlighting * *efer to Note Switch and Circuit Breaker Panel Lighting 6 - Standby Airspeed ndicator nternal Lighting 7 - Standby Altimeter nternal Lighting 8 - Non-stabilized Magnetic Compass nternal Lighting 9 - Standby Attitude ndicator nternal Lighting AA APPOVED 172SPHBUS-00 U.S V N G H T D A Y N G H T Cockpit lood Light Aircraft Position (NAV) Lights STOBE Light System BEACON Light TAX Light LAND (Landing) Light Operations for hire only.

20 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS KNDS O OPEATONS EQUPMENT LST (Continued) System, nstrument, Equipment and/or unction NAVGATON AND PTOT- STATC SYSTEM KND O OPEATON 1 - G1000 Airspeed ndicator Standby Airspeed ndicator G1000 Altimeter Standby Altimeter G1000 Vertical Speed ndicator V D A Y V N G H T D A Y N G H T G1000 Attitude ndicator Standby Attitude ndicator G1000 Directional ndicator (HS) G1000 Turn Coordinator Non-stabilized Magnetic Compass 11 - VH Navigation adio (VO/LOC/GS) COMMENTS 0 0 A/ A/ As equired Per Procedure GPS eceiver/navigator 0 0 A/ A/ As equired Per Procedure Marker Beacon eceiver 0 0 A/ A/ As equired Per Procedure Blind Altitude Encoder A/ A/ 1 1 As equired Per Procedure Clock GC 700 ACS (if installed) (Continued Next Page) 2-16 U.S. AA APPOVED 172SPHBUS-00

21 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS KNDS O OPEATONS EQUPMENT LST (Continued) System, nstrument, Equipment and/or unction VACUUM 1 - Engine Driven Vacuum Pump KND O OPEATON V D A Y V N G H T D A Y N G H T Vacuum ndicator ENGNE UEL AND CONTOL 1 - uel low ndicator ENGNE NDCATNG 1 - Tachometer (PM) Cylinder Head Temperature (CHT) ndicator Oil Pressure ndicator Oil Temperature ndicator ENGNE OL 1 - Engine Crankcase Dipstick COMMENTS AA APPOVED 172SPHBUS-00 U.S. 2-17

22 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS UEL LMTATONS Total uel: U.S. GALLONS (28.0 GALLONS per tank) Usable uel (all flight conditions): U.S. GALLONS (26.5 GALLONS per tank) Unusable uel: U.S. GALLONS (1.5 GALLONS per tank) NOTE To ens ure m aximu m fuel capacity an d minimize crossfeeding when refueling, always park the airplane in a wings level, normal ground attitude and place the fuel selector in the LET or GHT position. efer to igure 1-1 for normal ground attitude definition. Takeoff and land with the fuel selector valve handle in the BOTH position. Maximum slip or skid duration with one tank dry: 30 seconds Operation on either LET or GHT tank limited to level flight only. With 1/4 tank or less, prolonged uncoordinated flight is prohibited when operating on either left or right tank. uel remaining in the tank after the fuel quantity indicator reads 0 (red line) cannot be safely used in flight. Approved uel Grades (And Colors): 100LL Grade Aviation uel (Blue) 100 Grade Aviation uel (Green) LAP LMTATONS Approved Takeoff ange: UP to 10 Approved Landing ange: up to ULL 2-18 U.S. AA APPOVED 172SPHBUS-00

23 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS SYSTEM LMTATONS AUX AUDO SYSTEM Use of the AUX AUDO N entertainment input is prohibited during takeoff and landing. Use of the AUX AUDO N entertainment audio input and portable electronic devices (PED), such as cellular telephones, games, cassette, CD or MP3 players, is prohibited under unless the operator of the airplane has determined that the use of the Aux Audio System and the connected portable electronic device(s) will not cause interference with the navigation or communication system of the airplane. 12V POWE SYSTEM The 12 Volt Power System (POWE OUTLET 12V - 10A) is not certified for supplying power to flight-critical communications or navigation devices. Use of the 12 Volt Power System is prohibited during takeoff and landing. Use of the 12 Volt Power System is prohibited under unless the operator of the airplane has determined that the use of the 12 VDC power supply and connected portable electronic device(s) will not cause interference with the navigation or communication systems of the airplane. AA APPOVED 172SPHBUS-00 U.S. 2-19

24 SECTON 2 OPEATNG LMTATONS G1000 LMTATONS CESSNA MODEL 172S NAV GC 700 ACS The current Garmin G1000 Cockpit eference Guide (CG) Part Number and System Software Version that must be available to the pilot during flight are displayed on the MD AUX group, SYSTEM STATUS page. GPS based enroute, oceanic and terminal navigation is prohibited unless the pilot verifies the currency of the database or verifies each selected waypoint for accuracy by reference to current approved data. NAV/GPS instrument approaches must be accomplished in accordance with approved instrument approach procedures that are retrieved from the G1000 navigation database. The G1000 database must incorporate the current update cycle. Use of the NAVGATON MAP page for pilotage navigation is prohibited. The Navigation Map is intended only to enhance situational awareness. Navigation is to be conducted using only current charts, data and authorized navigation facilities. Use of the TAC MAP to maneuver the airplane to avoid traffic is prohibited. The Traffic nformation System (TS) is intended for advisory use only. TS is intended only to help the pilot to visually locate traffic. t is the responsibility of the pilot to see and maneuver to avoid traffic. Use of the TEAN POXMTY information for primary terrain avoidance is prohibited. The Terrain Proximity map is intended only to enhance situational awareness. t is the pilot s responsibility to provide terrain clearance at all times. Navigation using the G1000 is not authorized north of 70 North latitude or south of 70 South latitude due to unsuitability of the magnetic fields near the Earth's poles. n addition, operations are not authorized in the following two regions: 1. North of 65 North latitude between longitude 75 W and 120 W (Northern Canada). 2. South of 55 South latitude between longitude 120 E and 165 E (region south of Australia and New Zealand). (Continued Next Page) 2-20 U.S. AA APPOVED 172SPHBUS-00

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26 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS G1000 LMTATONS (Continued) TEAN AWAENESS AND WANNG SYSTEM (TAWS-B) Use of the Terrain Awareness and Warning System (TAWS-B) to navigate to avoid terrain or obstacles is prohibited. TAWS-B is only approved as an aid to help the pilot to see-and-avoid terrain or obstacles. TAWS-B must be inhibited when landing at a location not included in the airport database. Use of TAWS-B is prohibited when operating using the QE altimeter setting (altimeter indicates 0 feet altitude when the airplane is on the runway). The pilot is authorized to deviate from the current ATC clearance only to the extent necessary to comply with TAWS-B warnings. The geographic area of the TAWS-B database must match the geographic area in which the airplane is being operated U.S. AA APPOVED 172SPHBUS-00

27 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS PLACADS The following information must be displayed in the form of composite or individual placards. 1. n full view of the pilot: (The "DAY-NGHT-V-" entry, shown on the example below, will vary with installed equipment). 2. On control lock: (Continued Next Page) AA APPOVED 172SPHBUS-00 U.S. 2-23

28 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS PLACADS (Continued) 3. On the fuel selector valve: 4. Near both fuel tank filler cap: (Continued Next Page) 2-24 U.S. AA APPOVED 172SPHBUS-00

29 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS PLACADS (Continued) 5. On flap control indicator: 6. n baggage compartment: (Continued Next Page) AA APPOVED 172SPHBUS-00 U.S. 2-25

30 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS PLACADS (Continued) 7. A calibration card must be provided to indicate the accuracy of the magnetic compass in 30 increments. 8. Molded on the oil filler cap/dipstick: 9. Silk-screened on the instrument panel directly above the PD: (Continued Next Page) 2-26 U.S. AA APPOVED 172SPHBUS-00

31 CESSNA SECTON 2 MODEL 172S NAV OPEATNG LMTATONS GC 700 ACS PLACADS (Continued) 10. Silk-screened on the upper right instrument panel: 11. On auxiliary power plug door and second placard on battery box: 12. On the upper right side of the aft cabin partition: or (Continued Next Page) AA APPOVED 172SPHBUS-00 U.S. 2-27

32 SECTON 2 OPEATNG LMTATONS CESSNA MODEL 172S NAV GC 700 ACS PLACADS (Continued) 13. On the center overhead flood light control switch: 2-28 U.S. AA APPOVED 172SPHBUS-00