Страница 1: ...restricled by lhe Arrn f port Control Act Title 22 U S C Sec 2751 et seo or the Exporl Adminislration Act o 1SiZg as amended Title 50 U S C App 2401 et r q Violalions ol lhese exporl laws are subiect...
Страница 2: ...hanges to illustrations are indicaled by miniaiure pointing hands Changes to wiring diagrams are indicated by shaded areas Dates ol issue for original and changed pages are Original 0 15 Sep90 Change...
Страница 3: ...Tech n ical Orde r lEq u ipment Co nf ig u ratio n Status Record T O 1T 41C 1 cl Cl Blank...
Страница 4: ...listing ol the current Flight Manuals Flight Crew Checklist Salety Supplements and Operalional Supplements lf you are missing any publications listed on this page see your Publications Distribution O...
Страница 5: ...1 Flight Manual Saf ety Supplement and Operational Supplement Status CUNREruT SUPPLEMENIS Number Date Short Title Flight Manual Pages Affected REP LAC E D RESCIN D ED S U P P LEM E VIS Number Date Dis...
Страница 6: ...s r r r r r r r r r 2 1 Emergency Procedures r r 3 l Crew Duties Not Applieable r 4 1 Opgrating Limitations r r r r r r r 5 1 Flight Characteristics r r 6 l All Wgathgr Operation 7 1 GLOSSARY r rr r r...
Страница 7: ...ced Landing Pattern Airspeed Limitations Gauge OilTemperaturecauge 5 2 Oil Pressure Gauge 5 2 Tachomeler 5 2 Fuel Flow lndicator 5 3 Fuel Quantitylndicator 5 3 Suction Gauge 5 3 Stalling Speeds 2200 P...
Страница 8: ...ing and Se rializatio n AIRQRAFT CODTNG D MODEL 69 7755 69 7756 All other airplanris are standard C models lndicales information that applies to D modified airplanes i l l 1 1 I I t I I I t i I 1 I I...
Страница 9: ...ription PERMISSIBLE OPERATIONS The Flight Manual takes a positive approach and nor mally stales only what you can do Usually operalions or conliguralions which excesd the limitations as specif ied in...
Страница 10: ...calions lo the llight crews immediately upon receipt SAFETY AND OPEBATIONAL SUPPLEMENTS Safety supplements are a rapid means ol lransmitting inlormation about hazardous condilions or saf ety problems...
Страница 11: ...ALL or WILL Used to express lhat the requiremenls are binding and mandatory SHOULD Used to express a non mandatory desire or prelerred method of ac complishment and shall be construed as a non mandato...
Страница 12: ...1T 41C l r 41c IilIX l 1 lj i ifilsffiffiilllrrrl rc6 rmrrl ffiffi g H llli ffiffiffiffiH FffiilFTII ffiffi 1 ffiffillHll ryffirrtrrr t Ilrrtrrrnrrli rrrrrrrrn fri Figure 1 The T 41C Aircraft ix x Bl...
Страница 13: ...apability of conver sion lo lour place seating On T 41D aircrafl lhe T 41D has the same characterislics as T 41C The T 41D has a variable pitch propeller which improves performance Dimensions The over...
Страница 14: ...is turning Do nol operate lhe starter molor more lhan a tolalol30 sec onds al one time ll lhe engine fails to start within 30 seconds ol cumulative cranking allow a 3 minute cooling period belore ree...
Страница 15: ...T SWITCH 7 LANDING TAXI LIGHT SWITCH B MANUAL PRIMER KNOB 9 IGNITION SWITCH 10 FUEL SHUTOFF KNOB 11 PARKING BRAKE 12 FLAP CIRCUIT BREAKER 13 CIRCUIT BREAKERS T O 1T 41 C 1 Figure 1 2 Lelt Lower Switch...
Страница 16: ...hISPONDER MAGNETIC COMPASS FREQUENCY PLACARD CARBON MONOXIDE DETECTOR RADIO FLAP INDICATOR FUEL FLOW INDICATOR FUEL OUANTITY INDICATOR 18 TACHOMETER 19 AMMETEB 20 SUCTION GAUGE 2 1 OIL TEMPERATURE IND...
Страница 17: ...revolulion is small the number ol revolutions per minule is many the slipstream velocily is high and wilh the low airplane speed tlre lhrust is maximum T O 1T 41C 1 After lift ofl as lhe speed ol the...
Страница 18: ...by the throtile Fuel Flow lndicator Fuel llow is indicaled by llie right half of a dual indicating inslrument located on the righl side of lhe panet lt is a direct reading fuei pressure gauge calibra...
Страница 19: ...indicates detergent T O 1T 41C l oil An oil liller cap is located on the top side of the engine The oil dipstick is located on the lefi side of the engine just above lhe oil cooler Both the liller cap...
Страница 20: ...sTrcK OIL TEMPERATURE GAGE orL COOLER OIt SUMP ORAIN PLUG E orL CAP THERMOSTAT OIL PRESSURE RELIEF VALVE FILTER SCREEN PBESSURE ENGINE OIL PUMP FILTER SREEN sucTroN 1 8 ENGINE AND ACCESSOBY BEARINGS F...
Страница 21: ...T O 1T 41C 1 FUEL IANK SUMP OR IN PLUG IBEFI PLUG FIJEL ANO AIB THFOrILE UNII lffil pUGL Suppt y er rE C s8 FU L At ovAPoR M CIIANICAL lrxloE ELCSIBCAT FUEL NOZZLES 1 9 Figure 1 6 FuelSyslem Schemalic...
Страница 22: ...eir inputs from luel level lransmitters in each wing lank any time the master switch is ON NOTE Fuel quantity indicators are accurate only in stabilized straight and levetllight ELECTRICAL SYSTEM Elec...
Страница 23: ...witch panel ligure 1 2 On 1969 model aircrafl the master switch is a two piece split switch which should be used as one switch during normal operations NOTE On 1969 model aircrafl the split master swi...
Страница 24: ...N srAFrER SWrclr 10 wlNG FI AP POStnOil ftDTCATOR IO AUXILIAFY FUEL PUMP TO WilIG FI AP SYSI M TO IRANSPONOEF TO NAVtGAItON uoHT ctncLnr BRE X F TO NAVIGATION SYSTEM COOE t lo sTFroSE Lr6Ht3 ro vHF co...
Страница 25: ...are connected by me T O 1T 41C 1 chanical linkage to lhe pilot s brake pedals and pressure applied to the right seat pedals is trans mitted mechanically to lhe masler cylinders ll a sharper lurn is d...
Страница 26: ...e nosewheel and rudder syslem Exlernal gust locks are also provided lor allllight control surlaces lor use when slrong winds are expecled Crew members should be sure the control wheel is properly posi...
Страница 27: ...er The principal lunc lions ol lhe turn and slip indicalor are lo provide an alternale source of bank control and to indicate rudder coordination The turn needle driven by an electrical gyro indicates...
Страница 28: ...ween the microphone boom 1 16 and your mouth Headset volume should be set prior to adjusting radio volume Overhead Speaker System An overhead spoaker and hand held microphone are provided should the h...
Страница 29: ...s selecled T O 1T 41C 1 Transponder A Narco AT 150 lransistorized transponder pro vides positive radar idenlification lo ground agen cies and is capable of responding to interroga lions on any ol 4096...
Страница 30: ...3 Volume Control Frequency Selector Whole MHz Transmit lndicator Figure 1 9 VHF Radio Frequency Selector X MHz Frequency Selector OXX MHz Function Switch TO FBOM lndicator Frequency Selector Whole MH...
Страница 31: ...on the ground may damage lhe pro leclive lenses Strobe Lights A strobe light is located in each wingtip next lo the position light and on the top ol lhe vertical stabilizer The strobe lights produce...
Страница 32: ...depressing the button will cause internal damage lo the latch SEAT OPERATION The seats are lore and alt adjustable with manu ally operated reclining seat backs The lore and all adjustment levers are l...
Страница 33: ...any possible obstruction such as ground repair work lire exlinguishers on the ramp or other equipment that could cause a taxi accident The checklist outlines procedures bul never takes the place ol g...
Страница 34: ...inflalion culs or blisters and that the hub cap is secure ll any cord is showing the tire is worn beyond limits and should be changed 3 Brake Assembly CHECK brake pucks lor thickness minimum 3 32 inc...
Страница 35: ...ation Lights CHECK 2 Aileron CHECK 3 Flap CHECK Righl Main Landing Gear Section 1 Chock REMOVE 2 Tire CHECK 3 Brake Assembly CHECK Right Fuselage Section 1 Static Port CLEAR Check visually only Rubbin...
Страница 36: ...appear secure but not hold the pilot securely The shoulder harness inertia reel should also be checked lor binding and proper operation 4 Heading lndicator CAGE 1968 models 5 Attitude lndicator CAGE 1...
Страница 37: ...ture FULL LEAN 2l Throttle IDLE 3 Aux Fuel PumP HIGH lor 5 10 seconds T O 1T 41C 1 4l Attempt normal starl NOTE ll the engine does not start during the lirst lew atlempts turn the ignilion and master...
Страница 38: ...s The aircralt need 2 6 nol be brought lo a complele stop to ad equately check the brakes 2 Turn and Slip lndicator CHECK the turn needle and balllor proper indication BEFORE TAKEOFF 1 Throttle 1800 R...
Страница 39: ...quarterlng lallwlnds require e ilrsmg cautlon Avold sudden bursts of the throttle or sharp braklng Use lull control delleclion when positioning the conlrol CODE wlND DtREcflON I 2 7 CONTBOL WHEEL LEFT...
Страница 40: ...ght oll the nose gear and hold aileron into the wind At 50 to 60 mph raise the nose smoothly to takeofl altitude Maintain this attitude and allow the aircralt to fly ofl lhe ground which will normally...
Страница 41: ...his operation may result in erratic control of RPM CLIMBS Normal climbs are accomplished with lull power and at a conslant airspeed ol95 mph When initiating a climb lrom level flight conlrolthe rate o...
Страница 42: ...CHECK Check total and balance lluirtrrr RtcH WARNING damage or possible luel slarvation and engine lailure 3 Flight lnstruments AS REQUIRED a Crosscheck the heading indicator wilh the magnetic compas...
Страница 43: ...AUTION AVOID WAKE TURBULENCE Throttle ldle slow to approach speed Flaps as required T O 1T 41C 1 THROTTLE IDLE SLOW TO APPROACH SPEED FLAPS AS REQUIRED Throttle as BASE LEG DOWNWIND LEG 105 mph 4f 45...
Страница 44: ...it a smooth reduc tion in power and gradual increase in pitch atti lude lor louchdown on the main wheels Attempl ing to touchdown at an excessive airspeed may result in a ihree point or nosewheel lirs...
Страница 45: ...ure Braking eflectiveness increases as lorward speed decreases Use the brakes as necessary to decel T O 1T 41 C 1 erate the aircrafl lo a safe taxi speed belore tur ing oll the runway NOTE Holding the...
Страница 46: ...eting the landing roll and clearing the runway proceed as lollows 1 VHF Radio SET 2 Lights Pitot Heat AS REQUIRED a Landing TaxiLighl OFF b Pitot Heat OFF c Strobe Lights OFF 3 Flaps UP 4 VOR OFF 5 Tr...
Страница 47: ...ts Air and Heat Knobs CLOSE 14 Trim SET lo TAKEOFF BEFOHE LEAVING AIRCRAFT ffiPFTE T O 1T 41C 1 2 Seat Belts FASTEN 3 Headsets PLACE ON SEATS 4 Chocks INSTALL 5 Tiedowns Grounding Wire pilot Tube Cove...
Страница 48: ...NTRODUCTION This section contains lhe recommended proce dures lor various emergency conditions No at tempt has been made to cover every conceivable malf unction or emergency A sound knowledge of these...
Страница 49: ...e leaving the aircralt WARNING While abandoning the aircralt use cau lion lor other aircraft spinning propellers and any other obslructions NOTE Since the right seal can be slid lurther aft than the l...
Страница 50: ...or uncontrollable rise in oil temperature sudden rise in oil pressure or llucluating RPM WARNING lf complete engine failure is accompanied by luellumes in the cockpit a reslart should not be attempte...
Страница 51: ...ed to maintain llight and proceed as lollows t ffi l rhe sride and make a rorced t i r ln T J n power t z ffleropeiler FULL NoREASE l s huerserecror B rH f I r SpEED 8s MpH tASl I tr UJ lrj g z E cr I...
Страница 52: ...travel and adjust lor maximum RPM if power loss is a result ol governor lailure WARNING ll the loss ol power is a result ol governor lailure and control ol the propeller is regained proceed to the nea...
Страница 53: ...ents Open Pilot s Window As Required lf necessary the window may be opened to assist in clearing the smoke or lumes f rom the cabin WARNING Any time a crewmember or passenger experiences dizziness or...
Страница 54: ...lapr up glida rltitud lorg ln e no wind ritualion will bo approximetaly 6OO t cl por mil GLIOE Flrp Up 85 mph Flepr 2O 80 mph Flepr l0 75 mph LOw KEY soo ro t ooo FEET t o Figure 3 2 Typical Forced La...
Страница 55: ...ng the master switch oll removes all electrical power to aircraft components ll electrical power is essential the circuit malfunction may be isolated only in 1969 model aircraft by using only the batl...
Страница 56: ...ol travel NOTE ll after cycling the propeller control through lhe lull range ol travel control is not re gained conlinue with this checklist and land as soon as conditions permit ll control is regain...
Страница 57: ...climb in order to lower flaps below 100 7 mph Ftaps fuil down may be required to pre lf a main tire is llat land on the side of the a vent enEine overspeed lt it taits near idle and runway correspond...
Страница 58: ...must occupy lhe lett seal lfne minimum crew raquired lor this aircraft is one f ully qualif ied T 41D pilot When occupied by two squadron pilots both must be qualified in the T 41D Only designated lP...
Страница 59: ...eotts and go arounds never allow manifold pressure to exceed engine RPM WARNING At low pressure allitudes manilold pressure may exceed 25 during takeolls or go arounds Do not reduce throttle manifold...
Страница 60: ...ffi T O 1T 41C 1 Usable Fuel 51 gal 25 5 gal each tank levelllight Usable Fuel 46 gat 23 gal each tank all f light conditions Empty E ffi 3 gal unusable each tank Figure 5 6 Fuel Quantity lndicator uc...
Страница 61: ...lbs This aircraft is not designed for purely aerobatic flight However certain maneuvers are allowed when the aircraft is operated in the utility category ln the utility category the area behind the p...
Страница 62: ...irspeed llap setling power setting and coordination slips or skids Refer to ligures 6 1 and 6 2lor stall speeds When the aircraft approaches a stall lhe conlrol surfaces lose some il not all of their...
Страница 63: ...climb performance CLIMB PERFORMANCE The best rale of climb airspeed has been determined to vary with altitude At sea level the best rate of climb airspeed is 100 mph while at 10 000 leet MSL the airs...
Страница 64: ...of hydroplaning When landing on a wet runway expect a longer landing roll as braking elfectiveness is reduced Use caution as the pos sibility ol hydroplaning exists on a wet runway WARNING Crosswinds...
Страница 65: ...Primer lN and LOCKED 14 Engine lnstruments CHECK NOTE Below 0oF lhe oil pressure gauge should show a positive indication within 1 minule ol engine slart Engine Warmup ll the engine is cold soaked no i...
Страница 66: ...by Cessna with the aircrall and engine in good condition and using average piloting technique and best power mixture This data is a valuable aid lor llight planning A power setting selected from the r...
Страница 67: ...T O 1T 41C l Figure A1 1 Airspeed Conversion Charl A 2...
Страница 68: ...77 86 96 106 tt6 126 137 147 DOWN cAs 59 63 7t 80 88 98 a a a a a o lrj ttJ L U r o TU F g C z 180 170 160 150 140 130 120 1r0 100 90 80 70 60 50 Figure A1 2 Airspeed Correction Table 100 120 140 CAL...
Страница 69: ...oment lbs lb ins 1000 Weight Moment lbs lb ins 1 000 1 Licensed Empty Weight Sample Airplane 1443 54 1 2 Oil 10 pts Full oil may be assumed lnr rll linhrc t 19 o 4 19 o 4 3 4 5 Fuel 46 gal at 6 lbs ga...
Страница 70: ...05 110 115 LOADED ATRCRAFT MOMENT 1000 pOUND tNCHES CENTER OF GRAVITY MOMENT ENVELOPE NORMAL CATEGORY 10 15 20 25 MOMENT 1 000 POUND tNCtJES LOADING GRAPH PILOT AND FRONT PASSENGEB FUEL 46 cAL MAX er...
Страница 71: ...Maximum Any Direction 26 Knols 16 Knots Maximum Crosswind Componenls DUAL SOLO 0 20 Flaps 15 Knols I Knots Full Flaps 10 Knots exceed 26 knots Taxi Aircralt will not be moved without wing walkers when...
Страница 72: ...ase distance 10 for each 25 F above standard temperature for particular allitude For operation on a dry grass runway increase distance both ground run and total to clear 50 lt obstacle by 7Y ol the to...
Страница 73: ...2600 2500 2400 2300 68 62 57 51 46 41 138 133 126 118 107 90 10 4 OE 8 7 7 8 7 2 6 5 4 4 4 8 5 3 6 3 6 4 7 1 615 640 670 690 690 635 Figure 41 11 Cruise Range Performance Data LANDING DISTANCE TABLE...
Страница 74: ...u irrcl velocitl lcad vi ncl colnllolteltt jl OSs v irrcl conrpoltell l r i ll liriil i il ln il i ii lrrl lillFlnFl i I ilii I ii t I ii l r il rrl rlliifi 1lll ilElfrlr l l l ljliltrlTJFliEElE r r i...
Страница 75: ...650 450 285 I 105 825 585 NOTES 1 lncreasedistancelQY foreach25 Fabovestandardtemperatureforparticularaltitude 2 For operation on a dry grass iunway increase distance both ground run and total to clea...
Страница 76: ...24 23 22 78 73 69 64 139 136 132 128 11 8 11 1 10 5 9 8 3 9 4 l 4 4 4 7 540 565 580 605 2400 25 24 23 22 73 69 65 60 136 132 129 125 11 1 10 5 9 8 9 2 4 1 4 4 4 7 5 0 565 580 600 620 2300 25 24 23 22...
Страница 77: ...63 5B 138 134 130 125 11 0 10 3 9 6 8 9 4 2 4 5 4 8 5 2 580 600 620 645 2400 23 22 21 20 6B 63 59 55 134 130 126 121 10 3 9 7 9 0 8 4 4 5 4 8 5 1 5 5 600 620 640 660 2300 23 22 21 20 63 59 55 51 130 1...
Страница 78: ...d 75OO FEET Gross Weight 2550 LBS 46 cAL NO RESERVE ENDR HOURS RANGE MILES 10 5 9 8 9 1 8 4 605 625 650 675 10 1 9 4 8 7 8 0 8 9 8 3 7 7 7 1 660 675 690 700 21 20 19 1B 17 54 50 46 42 38 8 3 7 8 7 2 6...
Страница 79: ...4 8 5 2 5 6 6 2 645 670 690 705 2500 19 18 17 16 60 55 50 46 t32 126 118 110 9 2 8 5 7 8 7 l 5 0 5 4 5 9 6 4 660 680 700 710 2400 19 1B 17 16 56 52 47 43 127 121 113 105 8 6 8 0 7 4 6 8 5 3 5 7 6 2 6...
Страница 80: ...eading on panel instrument airspeed indicator IFF ldentification Friend or Foe interrogation communication equipment J K KHz Kilohertz Kilocycles per second KTS Knots L M MHz Megahertz Megacycles per...
Страница 81: ...ormance 6 2 Cruise Perlormance 10 0001t A 13 Cruise Perlormance 2500 ft A 10 Cruise Perlormance 5000 ft A 11 Cruise Perlormance 7500 t A 12 CylinderHeadTemperature 1 6 PaEe CylinderHeadTemperatureGaug...
Страница 82: ...13 o OilPressure Gauge 1 7 OilPressureGauge 5 2 lndex 2 Page OilSystemMallunction 3 8 Oilsyslem 1 7 OilTemperatureGauge 1 6 OilTemperatureGauge 5 1 OperatingLimitations 5 1 OptimumCruisePerformance A...
Страница 83: ...e A 4 i ThrottleApplication 2 12 WeightUmilations 5 4 Touch and goProcedures 2 14 WingFlapSystem 1 13 t Transponder 1 17 i Trim System 1 14 X TurbulenceandThunderslorms T 1 v Tum and Slip lndicator 1...
