Airplane Flight Manual
Reims-Cessna F177RG Cardinal · Flight Manual
Overview
This Airplane Flight Manual (AFM) is specifically designed for the Reims-Cessna F177RG Cardinal. It provides essential information for pilots operating this aircraft, including performance data, operating procedures, and safety guidelines. The manual serves as a comprehensive reference for both new and experienced pilots, ensuring safe and efficient operation of the F177RG. Key sections include limitations, emergency procedures, and performance charts, which are crucial for flight planning and execution.
- Maximum takeoff weight: 2,550 lbs
- Maximum landing weight: 2,500 lbs
- Stall speed in landing configuration: 55 knots
- Takeoff distance at sea level: approximately 1,200 feet
- Landing distance at sea level: approximately 1,000 feet
Document
Source
Originally published by bealefss.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 94
- File size
- 4.4 MB
- Publisher
- bealefss.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 945
- Engine (hp)
- 200
- Length (ft)
- 27
- Propeller
- Constant Speed
- Wingspan (ft)
- 35.6
- Engine model
- 10-360-A1B6D
- Empty weight (lb)
- 1,680
- Fuel capacity (gal)
- 61
- Rate of climb (fpm)
- 925
- Service ceiling (ft)
- 17,100
- Max takeoff weight (lb)
- 2,800
Performance
- Fuel burn (gph)
- 6
- Landing over 50ft
- 1,585
- Takeoff over 50ft
- 890
- Landing distance (ft)
- 730
- Takeoff distance (ft)
- 890
Weight & balance
- Useful load (lb)
- 1,120
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,680
- Max takeoff weight (lb)
- 2,800
Common. Rarer than 5% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Reims-Cessna F177RG Cardinal.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the F177RG Cardinal RG to your watchlist and track it in one place.
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In this document
Limitations
This section outlines the operational limitations of the Reims-Cessna F177RG Cardinal, including maximum takeoff weight, landing weight, and airspeed limits. The maximum takeoff weight is specified at 2,550 lbs, while the maximum landing weight is 2,500 lbs. Additionally, the stall speed in landing configuration is noted as 55 knots.
Emergency Procedures
Emergency procedures for the F177RG are detailed in this section, covering scenarios such as engine failure, electrical failure, and cabin fire. Pilots are instructed to follow specific checklists to ensure a systematic approach to handling emergencies.
Performance Data
Performance data includes takeoff and landing distances under various conditions, such as weight and altitude. For example, the takeoff distance at sea level on a standard day is approximately 1,200 feet, while the landing distance is around 1,000 feet.
Operating Procedures
This section provides standard operating procedures for preflight checks, engine start, and taxiing. It emphasizes the importance of thorough preflight inspections and checklist adherence to ensure safety.
Weight and Balance
Weight and balance calculations are crucial for safe flight operations. This section provides guidelines on how to calculate the center of gravity and ensure the aircraft is within weight limits for safe operation.
Safety notes
- Always adhere to weight and balance limits to ensure safe flight.
- Follow emergency procedures as outlined in the manual to handle in-flight emergencies effectively.
Full document text
Cessna. MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE AERO CLUB Cardinal RG 1975 IRONY 08 OWNER'S WORLD'S LARGEST PRO- DUCER OF GENERAL AVIATION AIRCRAFT SINCE 1956 MANUAL PERFORMANCE - SPECIFICATIONS GROSS WEIGHT SPEED, BEST POWER MIXTURE: Top Speed at Sea Level Cruise, 75% Power at 7000 ft Cardinal RG = 2800 lbs 180 mph 171 mph RANGE, EXTENDED RANGE MIXTURE: Cruise, 75% Power at 7000 ft 60 Gallons, No Reserve Maximum Range at 10,000 ft. 60 Gallons, No Reserve RATE OF CLIMB AT SEA LEVEL SERVICE CEILING TAKE-OFF: Ground Run Total Distance Over 50-Foot Obstacle LANDING: Ground Roll Total Distance Over 50-Foot Obstacle STALL SPEED: Flaps Up, Power Off Flaps Down, Power Off EMPTY WEIGHT: (Approximate) Cardinal RG Cardinal RG II USEFUL LOAD: Cardinal RG Cardinal RG II BAGGAGE. WING LOADING: Pounds/Sq Foot POWER LOADING: Pounds/HP FUEL CAPACITY: Total OIL CAPACITY PROPELLER: Constant Speed, Diameter ENGINE: Lycoming Fuel Injection Engine 200 rated HP at 2700 RPM " 945 mi 5.6 hrs 170 mph 1210 mi 8.7 hrs 139 mph 925 fpm 17,100 ft 890 ft 1585 ft 730 ft 1350 ft 66 mph 57 mph 1680 lbs 1750 lbs 1120 lbs 1050 lbs 120 lbs 16.1 14.0 61 gal. 9 qts 78 inches 10-360-A1B6D *This manual covers operation of the Cardinal RG which is certificated as Model 177RG under FAA Type Certificate No. A20CE. The manual also covers operation of the Reims/Cessna Cardinal RG which is certificated as Model F177RG under French Type Certification. D1039-13-CPS-350-6/93 COPYRIGHT © 1993 Cessna Aircraft Company Wichita, Kansas USA CONGRATULATIONS Welcome to the ranks of Cessna owners! Your Cessna has been designed and con- structed to give you the most in performance, economy, and comfort. It is our de- sire that you will find flying it, either for business or pleasure, a pleasant and profitable experience. This Owner's Manual has been prepared as a guide to help you get the most pleasure and utility from your Cardinal RG. It contains information about your Cessna's equipment, operating procedures, and performance; and suggestions for its servic- ing and care. We urge you to read it from cover to cover, and to refer to it fre- quently. Our interest in your flying pleasure has not ceased with your purchase of a Cessna. World-wide, the Cessna Dealer Organization backed by the Cessna Service Depart- ment stands ready to serve you. The following services are offered by most Cessna Dealers: THE CESSNA WARRANTY It is designed to provide you with the most comprehensive coverage possible: No exclusions b. Coverage includes parts and labor c. Available at Cessna Dealers world wide d. Best in the industry Specific benefits and provisions of the warranty plus other important benefits for you are contained in your Customer Care Program book supplied with your aircraft. Warranty service is available to you at any authorized Cessna Dealer throughout the world upon presentation of your Customer Care Card which establishes your eligibility under the warranty. FACTORY TRAINED PERSONNEL to provide you with courteous expert service. FACTORY APPROVED SERVICE EQUIPMENT to provide you with the most efficient and accurate workmanship possible. A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you need them. THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING CESSNA AIRPLANES, since Cessna Dealers have all of the Service Manuals and Parts Catalogs, kept current by Service Letters and Service News Letters, published by Cessna Aircraft Company. We urge all Cessna owners to use the Cessna Dealer Organization to the fullest. A current Cessna Dealer Directory accompanies your new airplane, The Directory is revised frequently, and a current copy can be obtained from your Cessna Dealer. Make your Directory one of your cross-country flight planning aids; a warm welcome awaits you at every Cessna Dealer.. ï ii PRINCIPAL DIMENSIONS -6" MAX. 17.3" 27' 35.6" 7-10 8.7 MAX. "Maximum height of aircraft with nose gear depressed and all tires and nose strut properly inflated. **wing span of aircraft with optional strobe lights installed. TABLE OF CONTENTS SECTION I - OPERATING CHECKLIST Page = 1-1 SECTION II - DESCRIPTION AND OPERATING DETAILS 2-1 - EMERGENCY PROCEDURES 3-1 SECTION III SECTION IV SECTION V - - SECTION VI - OPERATING LIMITATIONS 4-1 CARE OF THE AIRPLANE…………………… 5-1 OPERATIONAL DATA..... SECTION VII- OPTIONAL SYSTEMS……………. ALPHABETICAL INDEX.... 6-1 7-1 Index-1 This manual describes the operation and performance of the Cardinal RG and Cardinal RG II. Equipment described as "Optional" denotes that the subject equipment is optional on the Cardinal RG. Much of this equipment is standard on the Cardinal RG II. iii Section I OPERATING CHECKLIST One of the first steps in obtaining the utmost performance, service, and flying enjoyment from your Cessna is to familiarize yourself with your aircraft's equipment, systems, and controls. This can best be done by reviewing this equipment while sitting in the aircraft. Those items whose function and operation are not obvious are covered in Section II. Section I lists, in Pilot's Checklist form, the steps necessary to op- erate your aircraft efficiently and safely. It is not a checklist in its true form as it is considerably longer, but it does cover briefly all of the points that you should know for a typical flight. A more convenient plastic en- closed checklist, stowed in the map compartment, is available for quickly checking that all important procedures have been performed. Since vigi- lance for other traffic is so important in crowded terminal areas, it is important that preoccupation with checklists be avoided in flight. Proce- dures should be carefully memorized and performed from memory. Then the checklist should be quickly scanned to ensure that nothing has been missed. The flight and operational characteristics of your aircraft are normal in all respects. There are no "unconventional" characteristics or opera- tions that need to be mastered. All controls respond in the normal way
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within the entire range of operation. All airspeeds mentioned in Sections I, II and III are indicated airspeeds. Corresponding calibrated airspeed may be obtained from the Airspeed Correction Table in Section VI. 1-1 1-2 8 EXTERIOR 7 5 Refer to inside back cover of this manual for quantities, materials, and specifications | of frequently used service items. 4 1 3 INSPECTION 2 Note Visually check aircraft for general condition during walk-around inspection. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces. Also, make sure that control surfaces contain no internal accumulations of ice or debris. If a night flight is planned, check operation of all lights, and make sure a flashlight is available. 1 a. Check landing gear lever in DWN position. b. C. Check ignition switch OFF. d. e. Remove control wheel lock. Turn master switch ON; check fuel quantity indicators and landing gear DWN position indicator light (green) on; then turn master switch OFF. Check fuel selector valve handle in the BOTH position. Figure f. Before first flight of the day and after each refueling, pull forward on fuel reservoir drain lever (under pilot's seat) for about four seconds to clear fuel system of possible water and sediment. After draining, make sure that reservoir drains are closed. If water is observed in this check the system may contain additional water. Check the fuel tank sump quick-drain valves for presence of water, and remove the fuel vent line drain plugs (in wing roots just outboard of cabin doors) and the fuel selector valve drain plug to check for the presence of water. Check baggage door for security. g. 2 a. Remove rudder gust lock, if installed. b. Disconnect tail tie-down. C. 3 4 a. b. Check control surfaces for freedom of movement and security. Check aileron for freedom of movement and security. Check fuel tank vent opening (at wing tip trailing edge) for stoppage. Disconnect wing tie-down. a. b. Check main wheel tire for proper inflation. C. (5 (S) d. a. Before first flight of day and after each refueling, use sampler cup and drain small quantity of fuel from fuel tank sump quick-drain valve to check for water, sediment, and proper fuel grade. Visually check fuel quantity for desired level; then check fuel filler cap secure and vent unobstructed. Check engine oil level. Do not operate with less than six quarts. Fill to eight quarts for extended flight. b. Check propeller and spinner for nicks and security, and propeller for oil leaks. c. Check induction air filter for restrictions by dust or other foreign matter. d. Check landing and taxi lights for condition and cleanliness. jöö e. Check nose wheel strut and tire for proper inflation; nose wheel doors for security. f. g. Disconnect tie-down rope. Inspect flight instrument static source openings on side of fuselage for stoppage (both sides). 6 a. Check main wheel tire for proper inflation. b. C. (7) a. b. 8 a. b. Before first flight of the day and after each refueling, use sampler cup and drain small quantity of fuel from fuel tank sump quick-drain valve to check for water, sediment, and proper fuel grade. Visually check fuel quantity for desired level; then check fuel filler cap secure and vent unobstructed. Remove pitot tube cover, if installed, and check pitot tube opening for stoppage. Disconnect wing tie-down. Check fuel tank vent opening (at wing tip trailing edge) for stoppage. Check aileron for freedom of movement and security. 1-1. 1-3 BEFORE STARTING ENGINE. (1) Exterior Preflight -- COMPLETE. (2) Seats, Belts, Shoulder Harnesses (3) Fuel Selector Valve Handle -- ADJUST and LOCK. -- BOTH. -- OFF. (4) Radios, Autopilot, Electrical Equipment (5) Brakes -- TEST and SET. (6) Cowl Flaps -- OPEN (move lever out of locking hole to reposition). (7) Landing Gear Lever (8) Circuit Breakers -- STARTING ENGINE. -- DOWN. CHECK IN. (1) Mixture - - IDLE CUT-OFF. (2) Propeller -- HIGH RPM. (3) Throttle -- OPEN 1/4 INCH. ON. (4) Master Switch -- (5) Auxiliary Fuel Pump -- ON. (6) Mixture -- OFF. ADVANCE to 6 GAL/HR; then RETARD to IDLE CUT- NOTE If engine is warm, omit priming procedure above. (7) Propeller Area CLEAR. (8) Ignition Switch -- START (release when engine starts). (9) Mixture -- RICH (ADVANCE smoothly when engine fires). NOTE If engine floods, turn off auxiliary fuel pump, place mixture in idle cut-off, open throttle 1/2, and crank engine. When engine fires, advance mixture to full rich and retard throttle promptly. (10) Oil Pressure -- CHECK. (11) Auxiliary Fuel Pump -- OFF. BEFORE TAKE-OFF. 1-4 (1) Parking Brake -- (2) Cabin Doors (3) Flight Controls -->>> SET. CLOSED and LOCKED. -- FREE and CORRECT. (4) Stabilator and Rudder Trim (5) Fuel Selector Valve Handle (6) Throttle 1800 RPM. a. -- Magnetos -- -- -- TAKE-OFF. BOTH. - CHECK (RPM drop should not exceed 150 RPM on either magneto or 50 RPM differential between magnetos). CYCLE from high to low RPM; return to high b. Propeller RPM. -- Engine Instruments and Ammeter C. d. Suction Gage -- · CHECK. -- CHECK. (7) Flight Instruments and Radios -- - SET. (8) Navigation Lights, Flashing Beacon, and Optional Strobe Lights ON (as required). -- - (9) Throttle Friction Lock (10) Flaps -- 0° to 10°. TAKE-OFF. NORMAL TAKE-OFF. -- ADJUST. (1) Wing Flaps -- 0° to 10° (10° preferred). d See STC SA477CH (2) Power -- - `MAXIMUM (full throttle and 2700 RPM). -- (3) Mixture above 3000 feet). RICH (lean for field elevation per fuel flow placard (4) Aircraft Attitude -- LIFT NOSE WHEEL at 65 MPH. (5) Climb Speed (6) Brakes -- -- 75 to 85 MPH. APPLY momentarily when airborne. (7) Landing Gear (8) Wing Flaps -- -->> RETRACT in climb out. RETRACT (if extended). MAXIMUM PERFORMANCE TAKE-OFF. (1) Wing Flaps (2) Brakes (3) Power (4) Mixture -- -- -- -- 10°. APPLY. SeeSTC & SA477CH MAXIMUM (full throttle and 2700 RPM). RICH (lean for field elevation per fuel flow placard above 3000 feet). (5) Brakes -- RELEASE. (6) Aircraft Attitude -- LIFT NOSE WHEEL at 60 MPH. (7) Climb Speed 70 MPH until all obstacles are cleared. APPLY momentarily when airborne. (8) Brakes -- (9) Landing Gear (10) Wing Flaps -- -- - RETRACT after obstacles are cleared. RETRACT after reaching 80 MPH. 1-5 NOTE Do not reduce power until landing gear and wing flaps have been retracted. ENROUTE CLIMB. NORMAL CLIMB. (1) Airspeed (2) Power (3) Mixture -- -- -- 100 to 120 MPH. 25 INCHES Hg. and 2500 RPM. LEANED to 13 GAL/HR. (4) Cowl Flaps -- OPEN as required. MAXIMUM PERFORMANCE CLIMB. (1) Airspeed (2) Power (3) Mixture -- -- -- 95 MPH at sea level to 91 MPH at 10,000 feet. MAXIMUM (full throttle and 2700 RPM). (4) Cowl Flaps CRUISE. LEAN per fuel flow placard. -- FULL OPEN. See STC SA477CH (1) Power -- 75%). 15 to 25 INCHES Hg., 2100 to 2500 RPM (no more than (2) Mixture -- LEAN per Cessna Power Computer or Operational Data, Section VI. (3) Cowl Flaps -- CLOSED. LET-DOWN. (1) Power -- AS DESIRED. NOTE 1-6 Avoid continuous operation between 1400 and 1750 RPM with less than 10 inches Hg. (2) Mixture -- ADJUST for smooth operation. -- -- (3) Cowl Flaps (4) Wing Flaps below 110 MPH). (5) Landing Gear CLOSED. AS DESIRED (0° to 10° below 150 MPH, 10° to 30° -- AS DESIRED (do not extend above 140 MPH). BEFORE LANDING. (1) Seats, Belts, Harnesses (2) Fuel Selector Valve Handle (3) Landing Gear (4) Mixture -- -- RICH. ADJUST and LOCK. BOTH. -- EXTEND below 140 MPH. (5) Propeller -- HIGH RPM. (6) Airspeed - 80 to 90 MPH (flaps UP). (7) Wing Flaps AS DESIRED (0° to 10° below 150 MPH, 10° to 30° below 110 MPH). (8) Airspeed -- 70 to 80 MPH (flaps DOWN). (9) Stabilator and Rudder Trim BALKED LANDING. (1) Power -- -- ADJUST. MAXIMUM (full throttle and 2700 RPM). -- (2) Wing Flaps RETRACT to 20°. (3) Airspeed -- 75 MPH. (4) Wing Flaps -- RETRACT slowly. (5) Cowl Flaps -- OPEN. NORMAL LANDING. (1) Touchdown -- (2) Landing Roll -- MAIN WHEELS FIRST. LOWER NOSE WHEEL GENTLY. (3) Braking -- MINIMUM REQUIRED. AFTER LANDING. (1) Wing Flaps -- UP. (2) Cowl Flaps -- OPEN. SECURING AIRCRAFT. (1) Parking Brake -- SET. (2) Radios, Electrical Equipment -- OFF. (3) Mixture -- IDLE CUT-OFF (pulled full out). (4) Ignition and Master Switches (5) Control Lock (6) -- INSTALL. Fuel Selector Valve Handle -- OFF. LEFT or RIGHT. 1-7 -- INSTRUMENT PANEL 9 10 11 12 13 14 15 16 17 18 19 1 2 3 4 5 6 7 8 135.95 A35.93 30% 20 20 21 22 45 44 43 42 41 40 39 38 37 28 27 26 25 24 23 36' 29 30 35 34 -31 33. 32 1-8 1. Static Pressure Alternate Source Valve 2. Suction Gage (Opt.) 3. Economy Mixture Indicator (Opt.) 4. Marker Beacon Indicator Lights and Switches (Opt.) 5. Over-Voltage Warning Light 6. Cylinder Head Temperature, Left Fuel Quantity Indicator, Ammeter, and Oil Pressure Gage 7. Flight Instrument Group 8. Right Fuel Quantity Indicator and Oil Temperature Gage 9. Manifold Pressure/Fuel Flow Indicator 10. Radio Selector Switches (Opt.) 11. No. 1 LOC Reversed Indicator Light (Opt.) 12. No. 2 LOC Reversed Indicator Light (Opt.) 13. Rear View Mirror (Opt.) 14. Tachometer 15. Radios (Opt.) 16. Autopilot Control Unit (Opt.) 17. Flight Hour Recorder (Opt.) 18. ADF Bearing Indicator (Opt.) 19. Wing Flap Switch and Indicator 20. Map Compartment 21. ADF Radio (Opt.) 22. Right Cabin Air Control Knob 23. Circuit Breakers 24. Defroster Control Knob 25. Cabin Heat Control Knob 26. Mixture Control Knob 27. Propeller Control Knob 28. Rudder Trim Control Wheel 29. Ashtray 30. Cowl Flap Control Lever 31. Cigar Lighter 32. Microphone (Opt.) 33. Courtesy Light (Opt.) 34. Throttle 35. Landing Gear Lever 36. Stabilator Trim Control Wheel 37. Landing Gear Position Indicator Lights 38. Electrical Switches 39. Instrument and Radio Dial Light Rheostats 40. Parking Brake Handle 41. Ignition Switch 42. Auxiliary Fuel Pump Switch 43. Master Switch 44. Phone and Auxiliary Mike Jacks 45. Left Cabin Air Control Knob Figure 2-1. ፡ Section II DESCRIPTION AND OPERATING DETAILS The following paragraphs describe the systems and equipment whose function and operation is not obvious when sitting in the aircraft. This section also covers in somewhat greater detail some of the items listed in Checklist form in Section I that require further explanation. FUEL SYSTEM. Fuel is supplied to the engine from two integral fuel tanks, one in each wing. With the fuel selector valve handle in the BOTH position, the total usable fuel for all flight conditions is 60 gallons with the tanks completely filled. NOTE With heavy cabin loadings, it may be necessary to reduce the fuel load to keep the aircraft within the approved weight limits (refer to Section IV for weight and balance control procedures). To facilitate fueling to reduced fuel loads, a 22 gallon marker is provided inside each tank filler neck in the form of a series of small holes. Fuel from each wing fuel tank flows through a reservoir tank to the fuel selector valve, through a bypass in the electric auxiliary fuel pump to the fuel strainer, and then to the engine-driven fuel pump. From here fuel is distributed to the engine cylinders via a control unit and injector manifold. The auxiliary fuel pump is used primarily for priming the engine before starting. Priming is accomplished through the regular injection system. If the auxiliary fuel pump switch is accidentally placed in the ON po- sition (with master switch turned on and mixture rich) with the engine 2-1