cessna c-172 - TOPS Flying Club – Troy Oakland Pilots

Malfunctions, 3-8 excessive rate of charge, 3-9 insufficient rate of charge, 3-9 Electrical System, 2-3 ammeter, 2-5 circuit breakers and fuses, 2-6 ground service plug receptacle, 7-1 master switch, 2-4, 2-5 over-voltage sensor and warning light, 2-5 schematic, 2-4 Emergency Landing without Engine Power, 3-2 Emergency Let-Downs Through Clouds, 3-5 Emergency Locator Transmitter (ELT), 3-9 ELT operation, 3-11 Empty Weight, inside front cover Engine, before starting, 1-4 fire during start on grouni, 3-3 fire in flight, 3-1 Index-2 instrument markings, 4-3 oil, inside back cover operation limitations, 4-3 rough operation or loss of power, 3-7 starting, 1-4, 2-10 Engine Failure, 3-1 after take-off, 3-1 during flight, 3-1 Enroute Climb, 1-5, 2-15 Equipment, Cold Weather, 7-1 Excessive Rate of Electrical Charge, 3-9 Executing 180° Turn in Clouds, 3-5 Exterior Inspection Diagram, 1-2 Exterior Lighting, 2-6 F File, Aircraft, 5-5 Finish and Trim Plate, MAA Plate, 5-4 Fires, 3-3 electrical fire in flight, 3-4 engine fire during start on ground, 3-3 engine fire in flight, 3-4 Flight in Icing Conditions, 3-6 Flyable Storage, 5-6 Forced Landings, 3-2 ditching, 3-3 emergency landing without engine power, 3-2 precautionary landing with engine power, 3-2 Fuel System, 2-1 capacity, inside back cover fuel grade, inside back cover fuel quantity indicators, 4-4 long range fuel tanks, 2-3 quick-deain valves, 2-3 schematic, 2-2 Fuses and Circuit Breakers, 2-6 G Graph, Loading, 4-7 Gross Weight, inside front cover Ground Handling, 5-1 Ground Service Plug Receptacle, 7-1 H Handling Airplane on Ground, 5-1 Harnesses, Shoulder, 2-9 Headset-Microphone, 7-4 Heating, Ventilating and Defrosting System, Cabin, 2-8 Hot Weather Operation, 2-21 | Indicator, Fuel Quantity, 4-4 Indicator, True Airspeed, 7-5 Inspection Requirements, 5-6 Instrument Markings, Engine, 4-3 Instrument Panel Diagram, 1-8 Insufficient Rate of Electrical Charge, 3-9 Integrated Seat Belt/Shoulder Har- nesses With Inertia Reel, 2-9 Interior Care, 5-4 Interior Lighting, 2-7 Inertia Reel, Integrated Seat Belt/ Shoulder Harnesses, 2-9 Landings, 2-18 L after, 1-6 balked, 1-6, 2-18 before, 1-6 crosswind, 2-18 distance table, 6-5. forced, 3-2 normal, 1-6, 2-18 precautionary with power, 3-2 short field, 2-18 without engine power, 3-2 Landing Gear Servicing, inside back cover main/nose wheel tire pressure, inside back cover nose gear shock strut servicing, inside back cover Let Down, 1-6 Lighting Equipment, 2-6 exterior lighting, 2-6. interior lighting, 2-7 Limitations, Airspeed, 4-3 Limitations, Engine Operation, 4-3 Loading Arrangements Diagram, 4-5 Loading Graph, 4-7 Loading Problem, Sample, 4-6 Long Range Fuel Tanks, 2-3 Low Oil Pressure, 3-8 M MAA Plate/Finish Trim Plate, 5-4 Magneto Check, 2-12 Magneto Malfunction, 3-8 Maneuvers Normal Category, 4-1 Maneuvers Utility Category, 4-2 Markings, Airspeed Indicator, 4-3 Markings, Engine Instrument, 4-3 Master Switch, 2-4, 2-5 Maximum Glide Diagram, 6-6 Maximum Performance Take-Off, 1-5 Maximum Rate-Of-Climb Data Chart, 6-3 Microphone-Headsel, 7-4. Index-3 X ALPHABETICAL INDEX A After Landing, 1-6 Aircraft, file, 5-5 mooring, 5-1 securing, 1-7 Airspeed Correction Table, 6-2 Airspeed Indicator, True, 7-5 Airspeed Indicator Markings, 4-3 Airspeed Limitations, 4-3 Alternate Source Valve, Static Pressure, 7-2 Alternator Check, 2-13 Aluminum Surfaces, 5-3 Ammeter, 2-5 Authorized Operations, 4-1 B Balked Landing, 1-6, 2-19 Before Landing, 1-6 Before Starting Engine, 1-4 Before Take-Off, 1-4, 2-12 alternator check, 2-13 magneto check, 2-12 warm-up, 2-12 C Cabin Heating, Ventilating and Defrosting System, 2-8 Capacity, fuel, inside back cover oil, inside back cover Carburetor Air Temperature Gage, 4-4, 7-5 Carburetor Icing, 3-7 Care, interior, 5-4 propeller, 5-3 Center of Gravity Moment Envelope, 4-8 Cessna Customer Care Program, 5-7 Cessna Progressive Care, 5-7 Circuit Breakers and Fuses, 2-6 Climb, data, 2-15 enroute, 1-5, 2-15 maximum rate-of-climb data chart, 6-3 speeds, 2-15 Cold Weather Equipment, 7-1 ground service plug receptacle, 7-1 static pressure alternate source valve, 7-2 winterization kit, 7 Cold Weather Operation, 2-19 flight operations, 2-20 starting, 2-18 Correction Table, Airspeed, 6-2 Crosswind Landing, 2-18 Crosswind Take-Off, 2-14 Cruise Performance Chart, 2-15, 6-4 Cruising, 1-5, 2-16 Diagram, D electrical system, 2-4 ELT control panel, 3-10 exterior inspection, 1-2 fuel system, 2-2 Index-1 RAM AIRCRAFT MODIFICATIONS INC. CESSNA 1721, 172K, 172L and 172M SUPPLEMENTAL FLIGHT MANUAL III. PROCEDURES IV. No Change PERFORMANCE The performance of this airplane equipped with a Lycoming 0-320-D2G engine is equal to or better than the original F.A.A. approved performance. F.A.A. APPROVED: May 1, 1981 STC SA2375SW Page 3 of 3 pages: Waco-Madison Cooper Airport P.O. Box 5219 Waco, Texas 76708 817-752-83811 RAM AIRCRAFT MODIFICATIONS INC. AIRPLANE SUPPLEMENTAL FLIGHT MANUAL FOR LANDPLANE OR FLOATPLANE CESSNA MODELS 1721, 172K, 172L and 172M WITH LYCOMING 0-320-02G ENGINE INSTALLED Model Number 172 M Registration Number N64477 Serial Number 17265257 RAM AIRCRAFT MODIFICATIONS INC. CESSNA 1721, 172K, 172L, and 172M SUPPLEMENTAL FLIGHT MANUAL 1. GENERAL 1. ENGINE 2. FUEL 3. PROPELLER II. 4. PROPELLER (Seaplane only) LIMITATIONS 1. ENGINE LIMITS Lycoming 0-320-02G 100/130 Minimum Octane McCauley 1C160/CTM7557 or 1C160/DTM7557 McCauley 1A175/ETM8042 cr 1A175/ATM8042 This Supplemental Flight Manual is F.A.A. approved material and must be in the airplane for all operations when Lycoming 0-320-D2G engine is in- stalled in accordance with STC SA2375SW. The information contained herein supplements or supersedes the information in the form of placards, markings and manual material. For limitations, procedures and performance informa- tion not contained in this Supplemental Flight Manual consult the basic airplane placards, markings and manual material. F.A.A. APPROVED Date: May 1, 1981 Jack & Ovens for Don P. Watson, Chief Engineering & Manufacturing Branch FEDERAL AVIATION ADMINISTRATION Southwest Region Fort Worth, Texas 76101 ! S.T.C. NO. SA2375SW Page 1 of 3 pages. 2. PROPELLER LIMITS 3. PROPELLER LIMITS (Seaplane only) 4. ENGINE INSTRUMENT MARKINGS Maximum continuous: 150 HP-2650 RPM Take-off (5 minutes): 160 HP-2700 RPM Static RPM at maximum throttle setting: Not over 2400, not under 2280 Diameter: Maximum: 75.0 inches. Minimum: 74.0 inches Static RPM at maximum throttle setting: Not over 2570, not under 2470 Diameter: Maximum: 80.0 inches. Minimum: 78.5 inches Tachometer: Green Arc 2200 2650 RPM Yellow Arc 2650 Redline 011 Pressure: Redline 2700 RPM 2700 RPM 25 PSI Green Arc 60-90 PSI Redline 100 PST Cylinder Head Temperature (if installed): Green Arc 2250425° F. Redline 500° F. Waco-Madison Cooper Airport P.O. Box 5219 Waco, Texas 76708 817-752-8381 F.A.A. APPROVED: May 1, 1981 STC SA2375SW Page 2 of 3 pages Waco-Madison Cooper Airport P.O. Box 5219 Waco, Texas 76708 817-752-83811 United States of America Department of Transportation-Federal Aviation Administration Supplemental Type Certificate This certificate; issued to Number SA2375SW RAM Aircraft Modifications, Inc. P.O. Bax 5219 Waco-Madison Cooper Airport Waco, Texas 76708 cortifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part Regulations. 3 of the Civil Air Original Product Type Certificate Number: 3A12 Make: Cessna Model 172D, 172E, 172F, 172G, 172H, 1721, 172K, 172L, 172M, 172N Description of Type Design Change: Installation of Lycoming 0-320-D2G, 0-320-D2J, or 0-320-E2D (as modified by STC SE3692SW) engine rated for 160 h.p. take-off and 150 h.p. METO for models 1721, 172K, 172L, and 172M according to RAM Dwg. R17201 Rev. F dated 12/9/86; or installation of Lycoming 0-320-D2G, 0-320-D2J, or 0-320-E2D (as modified by STC SE3692SW) engine rated for 160 h.p. take-off and 145 h.p. METO for models 172D, 172E, 172P, 172G, and 172H according to RAM Dwg. 17202, Rev. K dated 12/9/86; or installation of Lycoming 0-320-D2G, 0-320-D2J or 0-320-E2D (as modified by STC SE3692SW) engine (160 h.p., 2700 r.p.m) in model 172N according to RAM Dwg. 17203, Rev. L dated 12/9/86; or later FAA approved re See continuation sheet of this STC. Hitt! States of America Department of Transportation-federal Aviation Administration Supplemental Type Certificate Limitations and Conditions: (Continuation Sheet) Number SA2375SW Revision 8 1. The following appropriate FAA Approved Manual is required: Cessna Models 1721, 172K 172L, 172M Airplane Flight Manual for Landplane with Lycoming 0-320-D2G engine November 1, 1976 or June 10, 1977 172D, 172E, 172F, 172G, 172H or March 30, 1978. June 9, 1977 or 172N March 29, 1978 Not required Airplane Supplemental Airplane Supplementa Flight Manual for Land- Flight Manual for plane or Floatplane Landplane or Float- with Lycoming 0-320-D2G plane with Lycoming engine 0-320-D2J engine or 0-320-E2D (as modific STC SA3692SW) November 5, 1981. January 26, 1979 or May 1, 1981 or January 25, 1979 April 30, 1981. Not required or August 27, 1987 November 5, 1981 or August 27, 1987. Not required 2. For additional limitations see the applicable flight manual listed above. 3. Compatibility of this modification with other previously approved modifications must be determined by the installer. This certificate and the supporting data which is the basis for approval shall remain in effect until sur rendered, suspended, revoked, or a termination date is therwise established by the Administrater of the Federal Aviation Administration Late of application: September 7, 1976 Date of issuance November 1, 1976 FEDERAL AVIATION Dalessed 6/10/77; 3/30/78; 11/9/78; 1/26/79; 2/3/81; 9/28/81; 11/5/81; 8/28/87 Lale amended Revision 8 By direction of the Adininistrater L. B. Andriesen (Signature) Manager, Aircraft Certification Division Southwest Region (Tile) Any alteration of this certificate is punishable by a fine of not exceeding $1000, or imprisonment not exceeding 3 years, or both. FAA FOR 12-10-01 This certificate may be transferred in accordance with FAR 21.47. In reation of this restfrase is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or hik This entificate may be transferred in accordance with FAR 147 PAGE 2 OF 2 PAGES TAN FORM B10-2-110-591 United States of America Department of Transportation-Federal Aviation Administration Supplemental Type Certificate This certificate issued to certifies that the change in Number SA2375SW RAM Aircraft Modifications, Inc.. P.O. Bax 5219 Waco-Madison Cooper Airport Waco, Texas 76708 the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part 3 Regulations. of the Civil Air Original Product Type Certificate Number: 3A12 Make: Model: Cessna 172D, 172E, 172F, 172G, 172H, 1721, 172K, 172L, 172M, 172N Description of Type Design Change: Installation of Lycoming 0-320-D2G, 0-320-D2J, or 0-320-E2D (as modified by STC SE3692SW) engine rated for 160 h.p. take-off and 150 h.p. METO for models 1721, 172K, 172L, and 172M according to RAM Dwg. R17201 Rev. F dated 12/9/86; or installation of Lycaming 0-320-D2G, 0-320-D2J, or 0-320-E2D (as modified by STC SE3692SW) engine rated for 160 h.p. take-off and 145 h.p. METO for models 172D, 172E, 172F, 172G, and 172H according to RAM Dwg. 17202, Rev. K dated 12/9/86; or installation of Lycoming 0-320-D2G, 0-320-D2J or 0-320-E2D (as modified by STC SE3692SW) engine (160 h.p., 2700 r.p.m) in model 172N according to RAM Dwg. 17203, Rev. L dated 12/9/86; or later FAA moved revisiti See continuation sheet of this STC. 1 United States of America Department of Transportation-federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number Limitations and Conditions: SA2375SW Revision B 1. The following appropriate FAA Approved Manual is required: 2. Cessna Models 1721, 172K 172, 172M 172D, 172E, 172F, 172G, 172H 172N Airplane Flight Manual for Landplane with Lycoming 0-320-D2G engine November 1, 1976 or June 10, 1977 or March 30, 1978 June 9, 1977 or March 29, 1978 Not required Airplane Supplemental Flight Manual for Land- plane or Floatplane with Lycoming 0-320-D2G engine January 26, 1979 or May 1, 1981 January 25, 1979 or April 30, 1981. Not required Airplane Supplementa: Flight Manual for Landplane or Float- plane with Lycoming 0-320-D2J engine or 0-320-E2D (as modific STC SA3692SW) November 5, 1981 or August 27, 1987 or November 5, 1981 August 27, 1987 Not required For additional limitations see the applicable flight manual listed above. 3. Compatibility of this modification with other previously approved modifications must be determined by the installer. This certificate and the supporting date which is the basis for approval shall remain in effect until sur- rendered, suspended, revoked or a termination date is otherwise established by the oldministrater of the Federal Aviation Administration Date of application: September 7, 1976 Date of issuance November 1, 1976 EDERAL AVIATION RATION TOMINISTRAT Dated: 6/10/77; 3/30/78; 11/9/78; 1/26/79; 2/3/81; 9/28/81; 11/5/81; 8/28/87 Dale amended Revision 8 By direction of the Administrator fe Manager, Aircraft Certification Division L. B. Andriesen Southwest Region (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. 'AA Foo&110-210-8 This rtficate may be transferred in accordance with FAR 21.47. 4 In alteration of this certificate is punishable by a fine of not exceeding $1.000, or imprisonment not exceeding 3 years, b This emate may be transferred in accordance with FAR 217 PAGE 2 OF 2 PAGES TAX FORM 11021 10-699 US Depoime oooo Federal Aviation Administration MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification. INSTRUCTIONS: Print or type all entries. Sea FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 for subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S. C. 1421) Failure to report can result in a civil penalty not to exceed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft 2. Owner Make CESSNA Serial No. 172-65257 Name (As shown on registration certificate) TROY OAKLAND PLOTS Model 172-M Nationality and Registration Mark N64477 Address (As shown on registration certificate) 2672 INDUSTRIAL ROW Pp. Box 84307 TROY Hi 49099 FLYING CLUB INC. 3. For FAA Use Only NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. Description of Work Accomplished (If more space is required, attach additional shoals. Identity with aircralt nationality and registration mark and date work completed.) INSTALLED LYCOMING ENGINE L-1604-39A 0320-D2G SN PER ST2375-39A-REV#8 Unil Make 4. Unit Identification 5. Tyr Model Serial No. Repair Alteration AIRFRAME ************ (AS described in Item above) POWERPLANT PROPELLER Туре APPLIANCE Manufacturer x A. Agency's Name and Address WILLIAM HEGEDUS CAP 1745570 6. Conformity Statement B Kind of Agency US Canfcated Mechanic Foreign Certificated Mechanic Cartificated Repair Station Manufacturer C. Certificate No. 1745570 D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Avistion Regulations and that the information furnished nerein is true and correct to the best of my knowledge. Date 7-9-96 Signature of Authorized Individual W, Heyd 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item I was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is FAA FIL Standards Inspector BY FAA Designae Date of Approval or Rejection 7-9-96 FAA Form 337- Manufacturer Repair Station Certificate or Designation No. Al 1745570 APPROVED Inspection Authorization O REJECTED Other (Specify) Person Approved by Transport Canada Airworthiness Group Signature of Authorized Individual Willis I Haysever 7 Additional Sheets Are Attached AU.S.G.P.O. 1990-761-753 Cessna CUSTOMER CARE TAKE YOUR CESSNA HOME FOR SERVICE AT THE SIGN OF THE CESSNA SHIELD". Cessna MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE MODEL 172 AND 1975 172M 172-65267 Skyhawk CESSNA. AIRCRAFT COMPANY WICHITA, KANSAS Weg ORLD'S LARGEST PRO. DUCER OF GENERAL AVIATION AIRCRAFT SINCE 1956 OWNER'S MANUAL D. Nor Reive FROM HIRPLANE- LET-DOWN. (1) Mixture - RICH. (2) Power - AS DESIRED. (3) Carburetor Heat - AS REQUIRED (to prevent carburetor icing). SECURING AIRCRAFT. (1) Parking Brake - SET. -- (2) Radios, Electrical Equipment, Autopilot (3) Mixture - IDLE CUT-OFF (pulled full out). (4) Ignition Switch -- OFF. (5) Master Switch - OFF. (6) Control Lock INSTALL. BEFORE LANDING. (1) Fuel Selector Valve -- BOTH. (2) Mixture -- RICH. (3) Carburetor Heat ON (apply full heat before closing throttle). (4) Airspeed -- za 60 MPH (flaps UP). KTS (5) Wing Flaps -- AS DESIRED. (6) Airspeed 05-75 MPH (flaps DOWN). 57-65 KTS BALKED LANDING. (1) Throttle -- FULL. (2) Carburetor Heat - COLD. (3) Wing Flaps -- 20°. (4) Airspeed --65 MPH, 57 KTS (5) Wing Flaps -- RETRACT (slowly). NORMAL LANDING. (1) Touchdown -- MAIN WHEELS FIRST. (2) Landing Roll - LOWER NOSE WHEEL GENTLY. (3) Braking -- MINIMUM REQUIRED. AFTER LANDING. 1-6 (1) Wing Flaps -- UP. (2) Carburetor Heat - COLD. - OFF. BEACON 1-7 BEFORE STARTING ENGINE. (1) Exterior Preflight COMPLETE. (2) Seats, Belts, Shoulder Harnesses - ADJUST and LOCK. (3) Fuel Selector Valve -- BOTH. (4) Radios, Autopilot, Electrical Equipment (5) Brakes - TEST and SET. STARTING ENGINE. (1) Mixture -- RICH. (2) Carburetor Heat - COLD. (3) Master Switch -- ON. OFF. (4) Prime AS REQUIRED (2 to 6 strokes; none if engine is warm). (5) Throttle -- OPEN 1/8 INCH. (6) Propeller Area -- CLEAR. (7) Ignition Switch -- START (release when engine starts). (8) Oil Pressure - CHECK. 9 BEACON LIGHT 10 RADIOS ON BEFORE TAKE-OFF. (1) Parking Brake -- SET. ON (2) Cabin Doors and Window -- CLOSED and LOCKED. (3) Flight Controls FREE and CORRECT. (4) Elevator Trim -- TAKE-OFF. (5) Fuel Selector Valve -- BOTH. (6) Mixture - RICH (below 3000 ft.). (7) Throttle -- 1700 RPM. a. b. Magnetos CHECK (RPM drop should not exceed 125 RPM on either magneto or 50 RPM differential between magnetos). Carburetor Heat CHECK (for RPM drop). C. Engine Instruments and Ammeter -- CHECK. d. Suction Gage -- CHECK. (8) Flight Instruments and Radios -- SET. (9) Optional Autopilot - OFF. (10) Throttle Friction Lock -- ADJUST. (11) Wing Flaps -- UP. TAKE-OFF. NORMAL TAKE-OFF. (1) Wing Flaps -- UP. (2) Carburetor Heat - COLD. (3) Throttle FULL. 52KTS (4) Elevator Control -- LIFT NOSE WHEEL (at 86 MPH). (5) Climb Speed -- 75 to 8 MPH. KTS 6.5 74 MAXIMUM PERFORMANCE TAKE-OFF. SHORT FIELD (1) Wing Flaps - UP. (2) Carburetor Heat - COLD. (3) Brakes -- APPLY. (4) Throttle - FULL. (5) Brakes -- RELEASE. (6) Airplane Attitude -- SLIGHTLY TAIL LOW. (7) Climb Speed 8 MPH (until all obstacles are cleared). 59 KTS ENROUTE CLIMB. (1) Airspeed 70 78 --80 to 90 MPH. KTS NOTE If a maximum performance climb is necessary, use speeds shown in the Maximum Rate-Of-Climb Data chart in Section VI. (2) Throttle -- FULL. (3) Mixture FULL RICH (mixture may be leaned above 3000 feet)., CRUISE. (1) Power 2200 to 2700 RPM (no more than 75%). (2) Elevator Trim - ADJUST. (3) Mixture -- LEAN. 1-4 1-5 8 Refer to inside back cover of this manual for quantities, materials, and specifications of frequently used service items. (2 3 4 a. Remove rudder gust lock, if installed. b. Disconnect tail tie-down. C. Check control surfaces for freedom of movement and security. 4 a. a. b. c. d. Check aileron for freedom of movement and security. Disconnect wing tie-down. Check main wheel tire for proper inflation. 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; then check fuel filler cap secure. Check oil level. Do not operate with less than six quarts. Fill to eight quarts for extended flights. Before first flight of the day and after each refueling, pull out strainer drain knob for about four seconds to clear fuel strainer of possible water and sediment. Check strainer drain closed. If water is observed, the fuel system may contain additional water, and further draining of the system at the strainer, fuel tank sumps, and fuel selector valve drain plug will be necessary. Check propeller and spinner for nicks and security. 5 a. EXTERIOR INSPECTION b. 1-2 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 night flight is planned, check operation of all lights, and make sure a flashlight is available. a. Remove control wheel lock. b. Check ignition switch OFF. C. Turn on master switch and check fuel quantity indicators; then turn off master switch. d. Check fuel selector valve handle on BOTH. e. Check baggage door for security. Lock with key if children are to occupy child's seat. C. d. Check landing light(s) for condition and cleanliness. e. Check carburetor air filter for restrictions by dust or other foreign matter. f. Check nose wheel strut and tire for proper inflation. g. Disconnect tie-down rope. h. Inspect flight instrument static source opening on side of fuselage for stoppage (left side only). 6 a. Check main wheel tire for proper inflation. 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, then check fuel filler cap secure. C. a. Remove pitot tube cover, if installed, and check pitot tube opening for stoppage. 238 b. Check fuel tank vent opening for stoppage. c. Check stall warning vent opening for stoppage. d. 8 a. Disconnect wing tie-down. Check aileron for freedom of movement and security. Figure 1-1. : 1-3 .... : s Section 1 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 enclosed checklist, stowed in the map compartment, is available for quickly checking that all important procedures have been performed. Since vigilance for other traffic is so important in crowded terminal areas, it is important that preoccupation with checklists be avoided in flight. Procedures 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 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. 7_1