Table Of Content

Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT DOCUMENT NUMBER 172059 FOR CESSNA 172R S/N _______________________REG._____________________ This supplement must be attached to the FAA Approved Airplane Flight Manual when STC SA2196CE, which increases the gross weight to 2550 lbs and STC SA4428SW, which installs an IO-360 Lycoming 180 HP engine, are installed. The information contained herein supplements the information of the basic Airplane Flight Manual. For limitations, procedures, and performance information not contained in this supplement, consult the basic Airplane Flight Manual. FAA APPROVED: ___________________ Margaret Kline Manager, Wichita Aircraft Certification Office FAA Central Region Wichita, KS DATE:_______________________ Original Date: 10/13/1999 172059 | FAA APPROVED Page 1 of 32 February 3, 2011 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com LOG OF REVISIONS REV PAGE DESCRIPTION APPROVED DATE Orig All Original Issue C.D. Riddle 10/13/1999 Corrections 4, 14 Added CG Limits and CG Kevin D. 1 27 & On 10/17/2000 Moment Envelope Graphs Campbell All Revised Page Numbering Added Logo Cover Tire Pressure Info Section 2 31 8 G.M Baker 04/12/2004 4 -9, 16 Changed Utility Category Wt. Changed Logo, Tire 3 1, 2,31 requirements 172059 | FAA APPROVED Page 2 of 32 February 3, 2011 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com TABLE OF CONTENTS SECTION 1: GENERAL ............................................................................... 4 SECTION 2: LIMITATIONS .......................................................................... 5 SECTION 3: EMERGENCY PROCEDURES ............................................... 9 SECTION 4: NORMAL PROCEDURES ..................................................... 16 SECTION 5: PERFORMANCE .................................................................. 21 SECTION 6: WEIGHT AND BALANCE / EQUIPMENT LIST ..................... 28 SECTION 7: AIRPLANE SYSTEMS AND DESCRIPTION ........................ 30 SECTION 8: AIRPLANE HANDLING , SERVICE & MAINTENANCE ........ 31 SECTION 9: SUPPLEMENTS ................................................................... 32 172059 | FAA APPROVED Page 3 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com SECTION 1: GENERAL INTRODUCTION This supplement contains the information that relates to changes related to STC SA2196CE and STC SA4428SW. For all other information refer to the FAA Approved Aircraft Flight Manual. DESCRIPTIVE DATA Number of Engines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: IO-360-L2A Engine Type:Normally aspirated, direct drive, air-cooled, horizontally opposed, fuel injected, four cylinder engine with 360 cu. In. displacement. Horsepower Rating and Engine Speed: 180 rated BHP at 2700 RPM. PROPELLER Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: 1A170/CFA7660 Number of Blades: 2. Propeller Diameter: 76 inches. Propeller Type: Fixed Pitch. PROPELLER (Alternate) Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: 1A170/JFA7658 Number of Blades: 2. Propeller Diameter: 76 inches. Propeller Type: Fixed Pitch. MAXIMUM CERTIFICATED WEIGHTS Ramp Weight ......... Normal Category: ................................. 2558 lbs. Utility Category: ................................... 2108 lbs. Takeoff Weight ....... Normal Category .................................. 2550 lbs. Utility Category: ................................... 2100 lbs. Landing Weight ...... Normal Category .................................. 2550 lbs. Utility Category: ................................... 2100 lbs. SPECIFIC LOADINGS Wing Loading: .............................................................1 4.7 lbs./sq. ft. Power Loading: ............................................................... 14.2 lbs./hp 172059 | FAA APPROVED Page 4 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com SECTION 2: LIMITATIONS AIRSPEED LIMITATIONS VNE Never Exceed Speed .................................. 160 KCAS ..... 163 KIAS VNO Maximum Structural Cruising ...................... 126 KCAS ..... 129 KIAS VA Maneuvering Speed 2550 Lbs. .................................................... 102 KCAS ..... 105 KIAS 2150 Lbs. ...................................................... 95 KCAS ....... 98 KIAS 1900 Lbs. ...................................................... 88 KCAS ....... 90 KIAS VFE Maximum Flap Extended Speed 10° Flaps ..................................................... 107 KCAS ..... 110 KIAS 10° to 30° Flaps ............................................ 85 KCAS ....... 85 KIAS Maximum Window Open Speed .............................. 160 KCAS ..... 163 KIAS AIRSPEED INDICATOR MARKINGS White Arc ........................................................................... 40 - 85 KIAS Green Arc ......................................................................... 48 - 129 KIAS Yellow Arc ....................................................................... 129 - 163 KIAS Red Line ................................................................................ 163 KIAS POWERPLANT LIMITATIONS Engine Manufacturer: Textron Lycoming. Engine Model Number: IO-360-L2A Maximum Power: 180 BHP rating Engine Operating Limits for Takeoff and Continuous Operations: Maximum Engine Speed ....................................................... 2700 RPM Note The static RPM range at full throttle is 2250 - 2400 RPM Maximum Oil Temperature .................................................... 245°F (118°C). Oil Pressure, ........ Minimum ................................................. 20 PSI Maximum ................................................ 115 PSI Fuel Grade: See Fuel Limitations. Oil Grade (Specification): Mil-L-8082 Aviation Grade Straight Mineral Oil Or Mil-L-22851 Ashless Dispersant Oil. Propeller Manufacturer: McCauley Accessory Division. Propeller Model: 1A170/CFA7660 Propeller Diameter: 76 inches. Propeller Manufacturer: McCauley Accessory Division. Propeller Model: 1A170/JFA7658 Propeller Diameter: 76 inches. 172059 | FAA APPROVED Page 5 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com POWERPLANT INSTRUMENT MARKINGS Tachometer Green Arc (Normal Operating) .................... 2100 - 2700 RPM Red Line (Maximum) .............................................. 2700 RPM Oil Temperature Green Arc (Normal Operating) ......................... 100° to 245° F Red Line (Maximum) .................................................... 245° F Oil Pressure Red Line (Minimum)..................................................... 20 PSI Green Arc (Normal Operating) ............................ 50 to 90 PSI Red Line (Maximum) .................................................. 115 PSI Fuel Quantity Red Line (Minimum)................................ 0 (1.5 Gal Unusable Each Tank) Fuel Flow Green Arc (Normal Operating) ............................ 0 to 11 GPH Suction Gage Green Arc (Normal Operating) ..................... 4.5 to 5.5 In. Hg. WEIGHT LIMITS Normal Category Maximum Ramp Weight ........................................... 2558 lbs. Maximum Takeoff Weight ........................................ 2550 lbs. Maximum Landing Weight ....................................... 2550 lbs. Maximum Weight in Baggage Compartment Baggage Area 1 - Station 82 to 108: ............... 120 lbs. Baggage Area 2 - Station 108 to 142: ............... 50 lbs. Note The maximum combined weight capacity for baggage areas 1 and 2 is 120 lbs. Utility Category Maximum Ramp Weight ........................................... 2108 lbs. Maximum Takeoff Weight ........................................ 2100 lbs. Maximum Landing Weight ....................................... 2100 lbs. Maximum Weight in Baggage Compartment: In the utility category, the baggage compartment must be empty and rear seat must not be occupied. 172059 | FAA APPROVED Page 6 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com CENTER OF GRAVITY LIMITS Normal Category Center of Gravity Range Forward: 35.0 inches aft of the datum at 1950 lbs or less, with straight line variation to 41.0 inches aft of datum at 2550 lbs. Aft: 47.3 inches aft of datum at all weights. Reference Datum: Lower portion of front face of firewall. Utility Category Center of Gravity Range Forward: 35.0 inches aft of the datum at 1950 lbs or less, with straight line variation to 37.5 inches aft of datum at 2100 lbs. Aft: 40.5 inches aft of datum at all weights. Reference Datum: Lower portion of front face of firewall. 172059 | FAA APPROVED Page 7 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com FLIGHT LOAD FACTOR LIMITS Normal Category Flight Load Factors ( Maximum Takeoff Weight - 2550 lbs.): *Flaps Up: ......................................................... +3.8g, -1.52g *Flaps Down: ................................................................. +3.0g Utility Category Flight Load Factors ( Maximum Takeoff Weight - 2100 lbs.): *Flaps Up: ......................................................... +4.4g, -1.76g *Flaps Down: ................................................................. +3.0g *The design load factors are 150% of the above, and all cases, the structure meets or exceeds design loads PLACARDS The following placard is changed from the original Flight Manual 9. Near Airspeed indicator: Maneuvering Speed - 105 KIAS 172059 | FAA APPROVED Page 8 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com SECTION 3: EMERGENCY PROCEDURES AIRSPEEDS FOR EMERGENCY OPERATION Engine Failure After Takeoff: Wing Flaps Up ..................................................................... 70 KIAS Wing Flaps Down: ............................................................... 65 KIAS Maneuvering Speed: 2550 lbs: ........................................................................... 105 KIAS 2150 lbs: ............................................................................. 98 KIAS 1900 lbs ............................................................................. 90 KIAS Maximum Glide: ......................................................................... 68 KIAS Precautionary Landing with Engine Power ................................ 65 KIAS Landing Without Engine Power Wing Flaps Up: .................................................................... 70 KIAS Wing Flaps Down: ............................................................... 65 KIAS EMERGENCY PROCEDURES CHECKLIST ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF 1. Throttle - - IDLE 2. Brakes - - APPLY 3. Wing Flaps - - RETRACT 4. Mixture - - IDLE CUT OFF 5. Ignition Switch - - OFF 6. Master Switch - - OFF ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1. Airspeed - - 70 KIAS (flaps UP) 65 KIAS (flaps DOWN) 2. Mixture - - IDLE CUT OFF 3. Fuel Shutoff Valve - - OFF (Pull Full Out) 4. Ignition Switch - - OFF 5. Wing Flaps - - AS REQUIRED 6. Master Switch - - OFF 7. Cabin Door - - UNLATCH 8. Land - - STRAIGHT AHEAD 172059 | FAA APPROVED Page 9 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com ENGINE FAILURE DURING FLIGHT (Restart Procedures) 1. Airspeed -- 68 KIAS. 2. Alternate Air -- ON (pull control full out). 3. Fuel Shutoff Valve -- ON (push full in). 4. Fuel Selector Valve -- BOTH. 5. Auxiliary Fuel Pump Switch -- ON. 6. Mixture -- RICH (if restart has not occurred). 7. Ignition Switch -- BOTH (or START if propeller is stopped FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1. Passenger Seat Backs - - MOST UPRIGHT POSITION 2. Seats and Seat Belts - - SECURE 3. Airspeed - - 70 KIAS (flaps UP) 65 KIAS (flaps DOWN) 4. Mixture - - IDLE CUT OFF 5. Fuel Shutoff Valve - - OFF (Pull Full Out) 6. Ignition Switch - - OFF 7. Wing Flaps - - AS REQUIRED (30° recommended) 8. Master Switch - - OFF (when landing is assured) 9. Doors - - UNLATCH PRIOR TO TOUCHDOWN 10. Touchdown - - SLIGHTLY TAIL LOW 11. Brakes - - APPLY HEAVILY PRECAUTIONARY LANDING WITH ENGINE POWER 1. Passenger Seat Backs - - MOST UPRIGHT POSITION 2. Seats and Seat Belts - - SECURE 3. Airspeed - - 65 KIAS 4. Wing Flaps - - 20° 5. Selected Field - - FLY OVER, noting terrain and obstructions, then retract flaps upon reaching a safe altitude and airspeed. 6. Avionics Master Switch and Electrical Switches - - OFF 7. Wing Flaps - - 30° ( on final approach) 8. Airspeed - - 65 KIAS 9. Master Switch - - OFF 10. Doors - - UNLATCH PRIOR TO TOUCHDOWN 11. Touchdown - - SLIGHTLY TAIL LOW 12. Ignition Switch - - OFF 13. Brakes - - APPLY HEAVILY 172059 | FAA APPROVED Page 10 of 32 April 20, 2004

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Cessna 172 R. FAA Approved STC CESSNA 172R. S/N 1150. 1945. 1000. 940. 1600. 1010. 1720. 1090. 1850. 1170. 1990. 1260. 2135. 2000.
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Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT DOCUMENT NUMBER 172059 FOR CESSNA 172R S/N _______________________REG._____________________ This supplement must be attached to the FAA Approved Airplane Flight Manual when STC SA2196CE, which increases the gross weight to 2550 lbs and STC SA4428SW, which installs an IO-360 Lycoming 180 HP engine, are installed. The information contained herein supplements the information of the basic Airplane Flight Manual. For limitations, procedures, and performance information not contained in this supplement, consult the basic Airplane Flight Manual. FAA APPROVED: ___________________ Margaret Kline Manager, Wichita Aircraft Certification Office FAA Central Region Wichita, KS DATE:_______________________ Original Date: 10/13/1999 172059 | FAA APPROVED Page 1 of 32 February 3, 2011 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com LOG OF REVISIONS REV PAGE DESCRIPTION APPROVED DATE Orig All Original Issue C.D. Riddle 10/13/1999 Corrections 4, 14 Added CG Limits and CG Kevin D. 1 27 & On 10/17/2000 Moment Envelope Graphs Campbell All Revised Page Numbering Added Logo Cover Tire Pressure Info Section 2 31 8 G.M Baker 04/12/2004 4 -9, 16 Changed Utility Category Wt. Changed Logo, Tire 3 1, 2,31 requirements 172059 | FAA APPROVED Page 2 of 32 February 3, 2011 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com TABLE OF CONTENTS SECTION 1: GENERAL ............................................................................... 4 SECTION 2: LIMITATIONS .......................................................................... 5 SECTION 3: EMERGENCY PROCEDURES ............................................... 9 SECTION 4: NORMAL PROCEDURES ..................................................... 16 SECTION 5: PERFORMANCE .................................................................. 21 SECTION 6: WEIGHT AND BALANCE / EQUIPMENT LIST ..................... 28 SECTION 7: AIRPLANE SYSTEMS AND DESCRIPTION ........................ 30 SECTION 8: AIRPLANE HANDLING , SERVICE & MAINTENANCE ........ 31 SECTION 9: SUPPLEMENTS ................................................................... 32 172059 | FAA APPROVED Page 3 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com SECTION 1: GENERAL INTRODUCTION This supplement contains the information that relates to changes related to STC SA2196CE and STC SA4428SW. For all other information refer to the FAA Approved Aircraft Flight Manual. DESCRIPTIVE DATA Number of Engines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: IO-360-L2A Engine Type:Normally aspirated, direct drive, air-cooled, horizontally opposed, fuel injected, four cylinder engine with 360 cu. In. displacement. Horsepower Rating and Engine Speed: 180 rated BHP at 2700 RPM. PROPELLER Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: 1A170/CFA7660 Number of Blades: 2. Propeller Diameter: 76 inches. Propeller Type: Fixed Pitch. PROPELLER (Alternate) Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: 1A170/JFA7658 Number of Blades: 2. Propeller Diameter: 76 inches. Propeller Type: Fixed Pitch. MAXIMUM CERTIFICATED WEIGHTS Ramp Weight ......... Normal Category: ................................. 2558 lbs. Utility Category: ................................... 2108 lbs. Takeoff Weight ....... Normal Category .................................. 2550 lbs. Utility Category: ................................... 2100 lbs. Landing Weight ...... Normal Category .................................. 2550 lbs. Utility Category: ................................... 2100 lbs. SPECIFIC LOADINGS Wing Loading: .............................................................1 4.7 lbs./sq. ft. Power Loading: ............................................................... 14.2 lbs./hp 172059 | FAA APPROVED Page 4 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com SECTION 2: LIMITATIONS AIRSPEED LIMITATIONS VNE Never Exceed Speed .................................. 160 KCAS ..... 163 KIAS VNO Maximum Structural Cruising ...................... 126 KCAS ..... 129 KIAS VA Maneuvering Speed 2550 Lbs. .................................................... 102 KCAS ..... 105 KIAS 2150 Lbs. ...................................................... 95 KCAS ....... 98 KIAS 1900 Lbs. ...................................................... 88 KCAS ....... 90 KIAS VFE Maximum Flap Extended Speed 10° Flaps ..................................................... 107 KCAS ..... 110 KIAS 10° to 30° Flaps ............................................ 85 KCAS ....... 85 KIAS Maximum Window Open Speed .............................. 160 KCAS ..... 163 KIAS AIRSPEED INDICATOR MARKINGS White Arc ........................................................................... 40 - 85 KIAS Green Arc ......................................................................... 48 - 129 KIAS Yellow Arc ....................................................................... 129 - 163 KIAS Red Line ................................................................................ 163 KIAS POWERPLANT LIMITATIONS Engine Manufacturer: Textron Lycoming. Engine Model Number: IO-360-L2A Maximum Power: 180 BHP rating Engine Operating Limits for Takeoff and Continuous Operations: Maximum Engine Speed ....................................................... 2700 RPM Note The static RPM range at full throttle is 2250 - 2400 RPM Maximum Oil Temperature .................................................... 245°F (118°C). Oil Pressure, ........ Minimum ................................................. 20 PSI Maximum ................................................ 115 PSI Fuel Grade: See Fuel Limitations. Oil Grade (Specification): Mil-L-8082 Aviation Grade Straight Mineral Oil Or Mil-L-22851 Ashless Dispersant Oil. Propeller Manufacturer: McCauley Accessory Division. Propeller Model: 1A170/CFA7660 Propeller Diameter: 76 inches. Propeller Manufacturer: McCauley Accessory Division. Propeller Model: 1A170/JFA7658 Propeller Diameter: 76 inches. 172059 | FAA APPROVED Page 5 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com POWERPLANT INSTRUMENT MARKINGS Tachometer Green Arc (Normal Operating) .................... 2100 - 2700 RPM Red Line (Maximum) .............................................. 2700 RPM Oil Temperature Green Arc (Normal Operating) ......................... 100° to 245° F Red Line (Maximum) .................................................... 245° F Oil Pressure Red Line (Minimum)..................................................... 20 PSI Green Arc (Normal Operating) ............................ 50 to 90 PSI Red Line (Maximum) .................................................. 115 PSI Fuel Quantity Red Line (Minimum)................................ 0 (1.5 Gal Unusable Each Tank) Fuel Flow Green Arc (Normal Operating) ............................ 0 to 11 GPH Suction Gage Green Arc (Normal Operating) ..................... 4.5 to 5.5 In. Hg. WEIGHT LIMITS Normal Category Maximum Ramp Weight ........................................... 2558 lbs. Maximum Takeoff Weight ........................................ 2550 lbs. Maximum Landing Weight ....................................... 2550 lbs. Maximum Weight in Baggage Compartment Baggage Area 1 - Station 82 to 108: ............... 120 lbs. Baggage Area 2 - Station 108 to 142: ............... 50 lbs. Note The maximum combined weight capacity for baggage areas 1 and 2 is 120 lbs. Utility Category Maximum Ramp Weight ........................................... 2108 lbs. Maximum Takeoff Weight ........................................ 2100 lbs. Maximum Landing Weight ....................................... 2100 lbs. Maximum Weight in Baggage Compartment: In the utility category, the baggage compartment must be empty and rear seat must not be occupied. 172059 | FAA APPROVED Page 6 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com CENTER OF GRAVITY LIMITS Normal Category Center of Gravity Range Forward: 35.0 inches aft of the datum at 1950 lbs or less, with straight line variation to 41.0 inches aft of datum at 2550 lbs. Aft: 47.3 inches aft of datum at all weights. Reference Datum: Lower portion of front face of firewall. Utility Category Center of Gravity Range Forward: 35.0 inches aft of the datum at 1950 lbs or less, with straight line variation to 37.5 inches aft of datum at 2100 lbs. Aft: 40.5 inches aft of datum at all weights. Reference Datum: Lower portion of front face of firewall. 172059 | FAA APPROVED Page 7 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com FLIGHT LOAD FACTOR LIMITS Normal Category Flight Load Factors ( Maximum Takeoff Weight - 2550 lbs.): *Flaps Up: ......................................................... +3.8g, -1.52g *Flaps Down: ................................................................. +3.0g Utility Category Flight Load Factors ( Maximum Takeoff Weight - 2100 lbs.): *Flaps Up: ......................................................... +4.4g, -1.76g *Flaps Down: ................................................................. +3.0g *The design load factors are 150% of the above, and all cases, the structure meets or exceeds design loads PLACARDS The following placard is changed from the original Flight Manual 9. Near Airspeed indicator: Maneuvering Speed - 105 KIAS 172059 | FAA APPROVED Page 8 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com SECTION 3: EMERGENCY PROCEDURES AIRSPEEDS FOR EMERGENCY OPERATION Engine Failure After Takeoff: Wing Flaps Up ..................................................................... 70 KIAS Wing Flaps Down: ............................................................... 65 KIAS Maneuvering Speed: 2550 lbs: ........................................................................... 105 KIAS 2150 lbs: ............................................................................. 98 KIAS 1900 lbs ............................................................................. 90 KIAS Maximum Glide: ......................................................................... 68 KIAS Precautionary Landing with Engine Power ................................ 65 KIAS Landing Without Engine Power Wing Flaps Up: .................................................................... 70 KIAS Wing Flaps Down: ............................................................... 65 KIAS EMERGENCY PROCEDURES CHECKLIST ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF 1. Throttle - - IDLE 2. Brakes - - APPLY 3. Wing Flaps - - RETRACT 4. Mixture - - IDLE CUT OFF 5. Ignition Switch - - OFF 6. Master Switch - - OFF ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1. Airspeed - - 70 KIAS (flaps UP) 65 KIAS (flaps DOWN) 2. Mixture - - IDLE CUT OFF 3. Fuel Shutoff Valve - - OFF (Pull Full Out) 4. Ignition Switch - - OFF 5. Wing Flaps - - AS REQUIRED 6. Master Switch - - OFF 7. Cabin Door - - UNLATCH 8. Land - - STRAIGHT AHEAD 172059 | FAA APPROVED Page 9 of 32 April 20, 2004 Supplemental Airplane Flight Manual Cessna 172 R FAA Approved STC SA2196CE www.airplains.com ENGINE FAILURE DURING FLIGHT (Restart Procedures) 1. Airspeed -- 68 KIAS. 2. Alternate Air -- ON (pull control full out). 3. Fuel Shutoff Valve -- ON (push full in). 4. Fuel Selector Valve -- BOTH. 5. Auxiliary Fuel Pump Switch -- ON. 6. Mixture -- RICH (if restart has not occurred). 7. Ignition Switch -- BOTH (or START if propeller is stopped FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1. Passenger Seat Backs - - MOST UPRIGHT POSITION 2. Seats and Seat Belts - - SECURE 3. Airspeed - - 70 KIAS (flaps UP) 65 KIAS (flaps DOWN) 4. Mixture - - IDLE CUT OFF 5. Fuel Shutoff Valve - - OFF (Pull Full Out) 6. Ignition Switch - - OFF 7. Wing Flaps - - AS REQUIRED (30° recommended) 8. Master Switch - - OFF (when landing is assured) 9. Doors - - UNLATCH PRIOR TO TOUCHDOWN 10. Touchdown - - SLIGHTLY TAIL LOW 11. Brakes - - APPLY HEAVILY PRECAUTIONARY LANDING WITH ENGINE POWER 1. Passenger Seat Backs - - MOST UPRIGHT POSITION 2. Seats and Seat Belts - - SECURE 3. Airspeed - - 65 KIAS 4. Wing Flaps - - 20° 5. Selected Field - - FLY OVER, noting terrain and obstructions, then retract flaps upon reaching a safe altitude and airspeed. 6. Avionics Master Switch and Electrical Switches - - OFF 7. Wing Flaps - - 30° ( on final approach) 8. Airspeed - - 65 KIAS 9. Master Switch - - OFF 10. Doors - - UNLATCH PRIOR TO TOUCHDOWN 11. Touchdown - - SLIGHTLY TAIL LOW 12. Ignition Switch - - OFF 13. Brakes - - APPLY HEAVILY 172059 | FAA APPROVED Page 10 of 32 April 20, 2004

Description:
Cessna 172 R. FAA Approved STC CESSNA 172R. S/N 1150. 1945. 1000. 940. 1600. 1010. 1720. 1090. 1850. 1170. 1990. 1260. 2135. 2000.
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