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Piper Aircraft Corporation Cherokee Lance PA-32R-300, Руководство пользователя

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Piper Aircraft Corporation Cherokee Lance PA-32R-300 Скачать руководство пользователя страница 161

Содержание Cherokee Lance PA-32R-300

Страница 1: ...CHEROKEE LANCE INFORMATION MANUAL Cherokee Lance PA 32R 300 HANDBOOK PART NO 761 633...

Страница 2: ...Published by PUBLICATIONS DEPARTMENT Piper Aircraft Corporation Issued August 20 1976 REPORT VB 840...

Страница 3: ...s will replace only pages with the same page number 2 Insert all additional pages in proper numerical order within each section 3 Page numbers followed by a small letter shall be inserted in direct se...

Страница 4: ...i Revised para 4 33 page no 4 7 Added Caution to para 4 9 relocated material to page 4 8 4 8 Added relocated material from page 4 7 4 15 Added Note to para 4 31 relocated material to page 4 16 4 16 Ad...

Страница 5: ...47 6 47 Added items from pg 6 46 added new items relocated items to pg 6 48 6 48 Added items from pg 6 47 added new items 6 49 Revised item nos added new items revised item 273 6 53 Revised item nos...

Страница 6: ...Evans 8 11 Revised item 8 21 b Jan 25 1979 Rev 6 761 633 iii Revised aircraft serial number applicability PR800808 2 2 Revised para 2 5 4 5 Revised info Re eedd paa 4 c 6 3 Revised para 6 3 a 3 Ward E...

Страница 7: ...evised para 3 13 D H Trompler 3 10 Nov 26 1985 Rev 9 761 633 2 8 Revised para 2 25 PR870131 3 3 Revised para 3 3 3 4 3 7 Revised para 3 9 3 9 Revised para 3 13 3 10 3 12 Revised para 3 23 and 3 27 Add...

Страница 8: ...Approval Number and Pages Description of Revision Signature and Code Date Rev 11 761 633 3 4 Revised Emergency Landing Gear Extension PR900920 checklist 3 9 Revised para 3 13 g 3 12 Revised para 3 27...

Страница 9: ...NCYPROCEDURES SECTION 4 NORMAL PROCEDURES SECTION 5 PERFORMANCE SECTION 6 WEIGHTAND BALANCE SECTION 7 DESCRIPTION AND OPERATION OF THE AIRPLANE ANDITS SYSTEMS SECTION 8 AIRPLANE HANDLING SERVICINGAND...

Страница 10: ...BLANK PAGE...

Страница 11: ...ion 1 1 1 3 Engines 1 3 1 5 Propeller 1 3 1 7 Fuel 1 3 1 9 Oil 1 3 1 11 Maximum Weights 1 4 1 13 Standard Airplane Weights 1 4 1 15 Baggage Space 1 4 1 17 Specific Loading 1 4 1 19 Symbols Abbreviatio...

Страница 12: ...BLANK PAGE...

Страница 13: ...also responsible for remaining within the operating limitations as outlined by instrument markings placards and this handbook Although the arrangement of this handbook is intended to increase its in...

Страница 14: ...PER AIRCRAFT CORPORATION GENERAL PA 32R 300 CHEROKEE LANCE Wing Area sq ft 174 5 Min Turning Radius ft 37 75 frompivot point to wingtip 3ti it 118 07 THREE VIEW Figure 1 1 REPORT VB 840 ISSUED AUGUST...

Страница 15: ...del HC C2YK 1 F f Propeller Diameter inches 1 Maximum 80 2 Minimum 78 5 g Propeller Type Constant Speed Hydraulically Actuated 1 7 FUEL AVGAS ONLY a Fuel Capacity U S gal total 98 b Usable Fuel U S ga...

Страница 16: ...l Load lbs The difference between the Maximum Takeoff Weight and the Standard Empty Weight 1620 1 15 BAGGAGE SPACE FORWARD AFT a Compartment Volume cubicfeet 7 0 17 3 b Entry Width inches 16 0 48 0 c...

Страница 17: ...ndicated Airspeed expressed in Knots M Mach Number is the ratio of true airspeed to the speed of sound TAS True Airspeed is the airspeed of an airplane relative to undisturbed air which is the CAS cor...

Страница 18: ...ich the temperature is 56 5 C 69 7 F is 0 00198 C 0 003564 F per foot and zero above that altitude OAT Outside Air Temperature is the free air static temperature obtained either from inflight temperat...

Страница 19: ...rtion of a climb to the horizontal distance traversed in the same time interval Demonstrated Crosswind The demonstrated crosswind velocity is the velocity of the Velocity crosswind component for which...

Страница 20: ...e s individual moments and dividing the sum by the total weight C G Limits The extreme center of gravity locations within which the airplane must be operated at a given weight UsableFuel Fuel availabl...

Страница 21: ...PIPER AIRCRAFI CORPORATION SECTION 1 PA 32R 300 CIIEROKEE LANCE GENERAL THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 20 1976 REPORT VB 840 1 9...

Страница 22: ...SECTION 1 PIPER AIRCRAFT CORPORATION GENERAL PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 1 10...

Страница 23: ...cm 0 3937 in 0 7646 m3 0 032808 ft 202 U S gal centimeters of 0 01316 atm degrees arc 0 01745 radians mercury at 0 C 0 3937 in Hg cmHg 0 1934 lblsq in degrees per second 0 01745 radians sec 27 85 lbJ...

Страница 24: ...l dry 1 556 x 10 cu ft at 0 C in Hg 0 4912 lb sq in 1 164 U S gal 70 73 lb sq ft 4 405 1 345 3 kg m2 2 540 cm Hg gallons U S liquid 231 cu in 25 40 mm Hg U S gal 0 1337 cu ft 4 951 x 10 3 cu yd inch p...

Страница 25: ...1 689 ft sec 1 467 ft lsec 1 1516 statute mph 88 ft min 1 852 km hr 1 6093 km hr 51 48 m sec 0 8684 kt liters 1 1000 cm miles per hour 2 151 ft lsec sq 61 02 cu in square m hr sq 0 03531 cu ft 33 814...

Страница 26: ...s per square 0 1414 in Hg foot lblsq ft 4 88243 kg m2 square kilometers 0 3861 sq mi 4 725 x 10 atm km2 pounds per square 5 1715 cm Hg square meters m2 10 76391 sq ft inch psior 2 036 in Hg 1 196 sq y...

Страница 27: ...ower Plant Limitations 2 2 2 9 Power Plant Instrument Markings 2 3 2 11 Weight Limits 2 3 2 13 Center of Gravity Limits 2 4 2 15 Maneuver Limits 2 4 2 17 Flight Load Factors 2 4 2 19 Types of Operatio...

Страница 28: ...BLANK PAGE...

Страница 29: ...149 Design Maneuvering Speed V Do not make full or abrupt control movementsabovethis speed At 3600 LBS G W 132 132 At 2170 LBS G W 106 109 CAUTION Maneuvering speed decreases at lighter weight as the...

Страница 30: ...el No IO 540 Kl G5D d Engine Operating Limits 1 Maximum Horsepower 300 2 Maximum Rotation Speed RPM 2700 3 Maximum Oil Temperature 245 F e Oil Pressure Minimum redline 25 PSI Maximum redline 100 PSI f...

Страница 31: ...nge 60 PSI to 90 PSI Yellow Arc Caution Range Idle 25 PSI to 60 PSI Yellow Arc Caution Range Start and Warm Up 90 PSI to 100 PSI Red Line Minimum 25 PSI Red Line Maximum 100 PSI d Fuel Pressure Green...

Страница 32: ...It is the responsibility of the airplane owner and the pilot to insure that the airplane is properly loaded See Section 6 Weight and Balance for proper loading instructions 2 15 MANEUVER LIMITS No ac...

Страница 33: ...er side each side having two interconnected tanks 2 23 FLIGHT WITH REAR CABIN DOOR OR REAR CABIN DOOR AND CARGO DOOR REMOVED The following limitations must be observed in the operation of this airplan...

Страница 34: ...SECTION 2 PIPER AIRCRAFT CORPORATION LIMITATIONS PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 2 6...

Страница 35: ...on Proper Tank Mixture Set Flaps Set Electric Fuel Pump On Propeller Set Trim Tab Set Engine Gauges Checked Fasten Belts Harness Controls Free Alternate Air Closed Doors Latched Seat Backs Erect Air...

Страница 36: ...gear lever Aircraft equipped with the backup gear extender OVERRIDE ENGAGED TO ENGAGE OVERRIDE LEVER UP LATCH DOWN TO RELEASE OVERRIDE LEVER FULL UP RELEASE On gear override latch Aircraft equipped w...

Страница 37: ...EOFF CLIMB PERFORMANCE On the inside of the forward baggage compartment MAXIMUM BAGGAGE THIS COMPARTMENT 100 LBS SEE THE LIMITATIONS SECTION OF THE PILOT S OPERATING HANDBOOK On aft baggage closeont M...

Страница 38: ...SECTION 2 PIPER AIRCRAFT CORPORATION LIMITATIONS PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 2 10...

Страница 39: ...Engine Power Loss During Takeoff 3 7 3 11 Engine Power Loss In Flight 3 8 3 13 Power Off Landing 3 9 3 15 Fire In Flight 3 10 3 17 Loss of Oil Pressure 3 11 3 19 Loss of Fuel Pressure 3 11 3 21 High O...

Страница 40: ...BLANK PAGE...

Страница 41: ...er of the section is devoted to amplified emergency procedures containing additional information to provide the pilot with a more complete understanding of the procedures These procedures are suggeste...

Страница 42: ...SECTION 3 PIPER AIRCRAFT CORPORATION EMERGENCY PROCEDURES PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 3 2...

Страница 43: ...RIDE landing approach ENGAGED position When field can easily be reached slow to 75 KIAS for shortest landing If sufficient altitude has been gained to attempt a restart Touchdowns should normally be m...

Страница 44: ...l pump ON whilefish tailing airplane Fuel selector check on full tank If landing gear still does not check down and locked HIGH OIL TEMPERATURE Emergency gear lever Hold emergency gear lever in the EM...

Страница 45: ...en and airspeeds will be reduced slightly To close the door in flight Slow airplane to 87 KIAS Cabin vents close Storm window open If upper latch is open latch If side latch is open pull on armrest wh...

Страница 46: ...SECTION 3 PIPER AIRCRAFT CORPORATION EMERGENCY PROCEDURES PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 3 6...

Страница 47: ...depend on the circumstances of the particular situation If sufficient runway remains to complete a normal landing leave the landing gear down and land straight ahead If the area ahead is rough or if i...

Страница 48: ...restored move the alternate air to the CLOSED position and turn OFF the electric fuel pump If the preceding steps do not restore power prepare for an emergency landing If time permits turn the ignitio...

Страница 49: ...her to attempt a landing with gear up or down depends on many factors If the field chosen is obviously smooth and firm and long enough to bring the plane to a stop the gear should be down If there are...

Страница 50: ...at the source of the fire be promptly identified through instrument readings character of the smoke or other indications since the action to be taken differs somewhat in each case Check for the source...

Страница 51: ...an off airport landing while power is still available particularly if other indications of actual oil pressure loss such as sudden increases in temperatures or oil smoke are apparent and an airport i...

Страница 52: ...w pitch If propeller overspeed should occur retard the throttle and check the oil pressure The propeller control should be moved to full DECREASE rpm and then set if any control is available Airspeed...

Страница 53: ...and airspeed will be reduced slightly To close the door in flight slow the airplane to 87 KIAS close the cabin vents and open the storm window If the top latch is open latch it If the side latch is op...

Страница 54: ...SECTION 3 PIPER AIRCRAFT CORPORATION EMERGENCY PROCEDURES PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 3 14...

Страница 55: ...flight Check 4 7 4 11 Before Startin g Engine 4 8 4 13 Starting Engine 4 9 4 15 Warm Up 4 11 4 17 Taxiing 4 1 1 4 19 Ground Check 4 1 1 4 21 Before Takeoff 4 12 4 23 Takeoff 4 13 4 25 Climb 4 13 4 27...

Страница 56: ...BLANK PAGE...

Страница 57: ...asis on the operation of the systems The remainder of the section is devoted to amplified normal procedures which provide detailed information and explanations of the procedures and how to perform the...

Страница 58: ...SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 4 2...

Страница 59: ...er free of ice snow frost inflation 2 60in Hinges check for interference Air inlets clear Wings free of ice snow frost Alternator belt check tension Stall warning check Tow bar and control locks stow...

Страница 60: ...HOT TAXIING Throttle l 2 open Master switch ON Electric fuel pump ON Chocks removed Mixture idle cut off Taxi area clear Starter engage Throttle apply slowly Mixture advance Prop high RPM Throttle ad...

Страница 61: ...e flapsup 92 KIAS Best rate 3600lb geardown flapsup 87 KIAS TAKEOFF Best angle 3600lb gearup flapsup 87 KIAS NORMAL Best angle 3600lb geardown flapsup 68 KIAS Flaps set En route 104 KIAS Tab set Elect...

Страница 62: ...t Gear down 129KIAS max Flaps set 106KIAS max Air conditioner OFF Trim to 75 KIAS STOPPING ENGINE Flaps retract Electric fuel pump OFF Air conditioner OFF Radio s OFF Propeller full INCREASE Throttle...

Страница 63: ...tional check of the stall warning system and navigation lights should now be made Turn the master switch ON Lift the detector while checking to determine if the horn is actuated and check that the nav...

Страница 64: ...oad The nose gear should be checked for 2 60 inches of strut exposure Check all tires for cuts and wear and insure proper inflation Make a lisual check of the brake blocks for wear or damage Remove th...

Страница 65: ...lever should be full OPEN Tum ON the master switch and tum OFF the electric fuel pump Move the mixture control lever to idle cut off and engage the starter by rotating the magneto switch clockwise Wh...

Страница 66: ...tch ON momentarily while the starter is engaged If cranking speed increases the ships battery is at a higher level than the extemal power supply When the engine is filing evenly advance the throttle t...

Страница 67: ...rd and apply the brakes to determine their effectiveness Taxi with the propeller set in low pitch high RPM setting While taxiing make slight turns to ascertain the effectiveness of the steering Observ...

Страница 68: ...RIDE ENGAGED position can be selected and latched before takeoff and the gear will then retract as soon as the gear selector switch is placed in the UP position Care should always be taken not to retr...

Страница 69: ...At lighter than gross weight these speed are reduced somewhat For climbing en route a speed of 104 KIAS is recommended This will produce better forward speed and increased visibility over the nose dur...

Страница 70: ...linders Then enrich the mixture by pushing the control towards the instrument panel until engine operation becomes smooth The fuel flow meter will give a close approximation of the fuel being consumed...

Страница 71: ...ue for short and slow landings is to use full flap and enough power to maintain the desired airspeed and approach flight path Mixture should be full RICH fuel on the fullest tank and electric fuel pum...

Страница 72: ...ffeting and gentle pitching may also precede the stall The gross weight stalling speed of the Cherokee Lance with power off and full flaps is 52 KIAS With the flaps up this speed is increased 5 KTS Lo...

Страница 73: ...ng light on the instrument panel and the horn will also operate simultaneously on the ground when the master switch is ON and the gear selector switch is in the UP position The three green lights on t...

Страница 74: ...SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 4 18...

Страница 75: ...TS SECTION 5 PERFORMANCE Paragraph Page No No 5 1 General 5 1 5 3 Introduction to Performance and Flight Planning 5 1 5 5 Flight Planning Example 5 3 5 7 Performance Graphs 5 9 List of Figures 5 9 REP...

Страница 76: ...BLANK PAGE...

Страница 77: ...proficiency or mechanical deterioration of the aircraft This performance however can be duplicated by following the stated procedures in a properly maintained airplane Effects of conditions not consid...

Страница 78: ...SECTION 5 PIPER AIRCRAFT CORPORATION PERFORMANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976...

Страница 79: ...determined until the weight of the fuel to be used has been established referto item g 1 1 Basic Empty Weight 2100 lbs 2 Occupants 6x 170 lbs 1020 lbs 3 Baggage and Cargo 60 lbs 4 Fuel 6lb gal x 50 30...

Страница 80: ...ature values are the first variables to be considered in determining the climb components from the Fuel Distance and Time to Climb graph Figure 5 19 After the fuel distance and time for the cruise pre...

Страница 81: ...the flight subtract the previously calculated distance to climb and distance to descend to establish the total cruise distance Refer to the appropriate Avco Lycoming Operator s Manual and the Power Se...

Страница 82: ...Flight Time c 3 plus d l plus e 6 ll hrs plus 17 hrs plus 66 hrs 6 5min plus 10 min plus 40 min 56 5 min g Total Fuel Required Determine the total fuel required by adding the fuel to climb the fuel to...

Страница 83: ...PIPER AIRCRAFT CORPORATION SECTION 5 PA 32R 300 CHEROKEE LANCE PERFORMANCE THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 20 1976 REPORT VB 840 5 7...

Страница 84: ...SECTION 5 PIPER AIRCRAFT CORPORATION PERFORMANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 5 8...

Страница 85: ...5 17 5 15 Gear Up Rate of Climb 5 18 5 17 Gear Down Rate of Climb 5 19 5 19 Fuel Distance and Time to Climb 5 20 5 21 Power Setting Table 5 21 5 23 Speed Power Performance Cruise 5 23 5 25 Speed Power...

Страница 86: ...SECTION 5 PIPER AIRCRAFT CORPORATION PERFORMANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 5 10...

Страница 87: ...PIPER AIRCRAFT CORPORATION SECTION 5 PA 32R 300 CHEROKEE LANCE PERFORMANCE SVM AIRSPEED SYSTEM CALIBRATION Figure 5 1 ISSUED AUGUST 20 1976 REPORT VB 840 REVISED AUGUST 19 1977 5 11...

Страница 88: ...SECTION 5 PIPER AIRCRAFT CORPORATION PERFORMANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 5 12 REVISED AUGUST 19 1977...

Страница 89: ...EE LANCE PERFORMANCE PA 32R 300 STALL 7 YsasusAWRE OF AM 100 90 0 FLAPS so 40 FLAPS 90 18 20 30 40 SO 60 ANGLE OFBANK DEGREES 50 p 30 0 FLAPS 40 FLAPS ID 20 39 40 50 80 ANGLE OFBANK DEGREES STALL SPEE...

Страница 90: ...1200 LIFT OFF BARRIER 3600 53 Si 1000 3200 49 56 2800 44 54 800 2400 40 52 ggg 4 20 0 20 40 60 80 100 120 3600 3400 3200 3000 2800 26002400 0 5 10 13 OUTSIDE AIR TEMP F GROSS WEIGHT LBS WIND KNOTS a i...

Страница 91: ...T4i O 40 2200 OH 2000 2 1800 1800 1400 STD TEMP 800 400 f 0 20 0 20 40 60 80 100 120 3600 3400 3200 30002800 2600 2400 0 5 10 l i OUTSIDE AIR TEMP F GROSS WEIGHT LBS WIND KNOTS fi 11111 40 20 0 20 40...

Страница 92: ...9 3800 3200 58 64 3400 g 3208 2000 o 2eoo 2400 Y STO TEMP 2200 2008 40 20 0 20 40 60 80 100 120 3600 34003200 3000 2800 24 0 5 10 t aan OUTSIDE AIR TEMP 4 F GROSS WEIGHT LBS WINB KNOTS 4 O 20 0 20 40...

Страница 93: ...00 sk STO TEMP 1200 o 1000 o see 600 400 0 20 0 20 40 00 80 100 120 3880 34003200 3000 2800 2600 2400 0 5 10 13 OUTSIDE AIR TEMP F GROSS WT LBS WINDKTS Illiti II 40 28 O 20 46 OUTSIDE AIR TEMP C Exa p...

Страница 94: ...ED 100 FtICN OF PEAK G T MIXRE FULL RICH 40 20 0 20 48 60 80 100 120 0 500 1000 1500 2000 OUTSIDE AIR TEMP F RATE OFCLIMB F P M I Illii 40 20 0 20 40 OUTSIDE AIR TEMP C Example Climb pressure altitude...

Страница 95: ...MIXTURE RICli 87KIAS 40 20 0 20 40 60 80 100 120 0 200 400 600 800 1000 OUTSIDE AIR TEMP F t i t I RATE OFCLIMB F P M 40 20 O 20 40 OUTSIDE AIR TEMP C Example Climb pressure altitude 8000 ft Outside a...

Страница 96: ...TEMP F FUEL DISTANCE AND TIME TOCLIMB EAIR MP C Example Departure airport pressure altitude 1200 ft Departure airport temperature 60 F Cruise pressure altitude 6000 ft Cruise OAT 42 F Time to climb 8...

Страница 97: ...5 25 6 24 6 Y 5 000 41 18 1 17 6 17 0 16 6 21 5 20 8 20 1 19 6 24 3 23 5 22 5 22 0 25 3 24 4 g 6 000 38 17 9 17 4 16 8 16 4 21 3 20 6 19 8 19 3 24 0 23 2 22 3 21 7 25 0 24 1 m 7 000 34 17 7 17 2 16 6...

Страница 98: ...SECTION 5 PIPER AIRCRAFT CORPORATION PERFORMANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 5 22...

Страница 99: ...T APPROX1MATE POWER FUEL CONS 75 18 GPH 65 16BPH p 55 14 GPH 4 I 55 85 15 2400RPM 4 20 O 20 40 60 80 100 120 120 130 140 150 160 1 0 OUTSIDE AIR TEMP F TRUE AIRSPEED KNOTS 40 28 O 20 40 OUTSIDE AIR TE...

Страница 100: ...WEIGHT APPROXWATE POWERFUEL CONS 75 16 0GPH 65 13 8 GPH 55 11 9 GPH I I I 4L 20 0 20 40 00 80 100 120 110 120 130 14 150 1 0 TRUE AIRSPEED KNOTS 40 20 20 40 OUTSIDE AIR TEMP C Example Cruise pressure...

Страница 101: ...A 32R 300 CHEROKEE LANCE PERFORMANCE I i Example Cruise pressure altitude 6000 ft Cruise OAT 42 F Power 65 Range withreserve 825 nautical miles Range noreserve 915 nautical miles RANGE Figure 5 27 ISS...

Страница 102: ...5 APPROX POWER FUEL CONS 75 16 0GPH 5 55 13 8 GPH 65 55 11 9GPH 45 MIN RESERVE AT45 POWER NORESERVE 75 75 43 28 0 20 4 60 80 100 120 5 6 7 5 6 1 OUTSIDE AIR TEMP F ENDURANCE HOURS 40 26 0 29 40 OUTSID...

Страница 103: ...AIR TEMP F FUEL DISTANCE AND TIME TO DESCEND 40 20 0 20 40 OUTSIDE AIR TEMP C Example Cruise pressure altitude 6000 ft Cruise OAT 42 F Destination airport pressure altitude 400 ft Destination airport...

Страница 104: ...LANCE O i I Example Cruise pressure altitude 8000 ft Cruise OAT 50 F Terrain pressure altitude 1200 ft Terrain temperature 70 F Glide Range ll nautical miles minus 2 5 nautical miles 8 5 nautical mil...

Страница 105: ...TION 5 PA 32R 300 CHEROKRP LANCE PERFORMANCE ci o BH 83188 8 BOG 53AO 33NVISIO BMIONV1 g se a co efl l if w Es gm REF LME m m a i i LANDING PERFORMANCE Figure 5 35 ISSUED AUGUST 20 1976 REPORT VB 840...

Страница 106: ...ULL STALL TOUCHDOWN MAXIMUM BRAKING AVEi LEVEL DRY RUNWAY 1500 1400 1300g 900 m STO TE IP 800 100 800 UN I I o 40 10 0 20 40 80 80 100 120 3600 3200 2800 2400 O 5 10 5 OUTSIDE AIR TEMPERATUREw F WEIGH...

Страница 107: ...o MAXIMUM BRAKING PAVED LEVEL DRY RUNWAY 21 1600 m 2 m STO TEMP 1500 1400 E 1300 E 1200 1100 I 1000 43 10 0 20 40 SO 80 100 120 3600 3400 3200 30002800 2600 2400 2200 0 5 10 15 OUTSIDE AIR TEMPERATURE...

Страница 108: ...EAR EXTENDED FULL STALL TOUCHOOWN MA IMUN BRAKitG PAVED LEVEL DRY RUNWAY 1400 800 STO T P 700 son 40 20 0 20 40 00 80 10 120 36003400 3200 30002800 2600 2400 2200 0 5 10 5 OUTSIDE AIR TEMPERATURE F GR...

Страница 109: ...WEIGHT AND BALANCE Paragraph Page No No 6 1 General 6 1 6 3 Airplane Weighing Procedure 6 3 6 5 Weight and Balance Data and Record 6 6 6 7 Weight and Balance Determination For Flight 6 11 6 8 Cargo Lo...

Страница 110: ......

Страница 111: ...operly loaded airplane however will perform as intended Before the airplane is licensed it is weighed and a basic empty weight and C G location is computed basicempty weight consists of the standard e...

Страница 112: ...SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 6 2...

Страница 113: ...ining fuel is drained Operate engine on each tank until all undrainable fuel is used and engine stops Then add the unusable fuel 4 0gallons total 2 0 gallons each wing CAUTION Whenever the fuel system...

Страница 114: ...in Wheel R Left Main Wheel L Basic Empty Weight as Weighed T WEIGHING FORM Figure 6 1 d Basic Empty Weight Center of Gravity 1 The following geometry applies to the PA 32R 300 airplane when it is leve...

Страница 115: ...AND BALANCE 2 The basic empty weight center of gravity asweighed including optional equipment full oil and unusable fuel can be determined by the following formula C G Arm N A R L B inches T Where T...

Страница 116: ...rial number and registration number shown The basic empty weight of the airplane as licensed at the factory has been entered in the Weight and Balance Record Figure 6 7 This form is provided to presen...

Страница 117: ...l Equipment Basic Empty Weight The standard empty weight includes full oil capacity and 4 0 gallons of unusable fuel AIRPLANE USEFUL LOAD NORMAL CATEGORY OPERATION Gross Weight Basic Empty Weight Usef...

Страница 118: ...SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 6 8...

Страница 119: ...Registration Number Page Number Item No Weight Change Running Basic Added Removed Empty Weight Date Description of Article or Modification In Out Wt Arm Moment Wt Arm Moment Wt Moment Lb In 100 Lb In...

Страница 120: ...er Registration Number Page Number Item No Weight Change Runn ng Basic 2 Added Removed Empt i Weight Date Description of Article or Modification 5 e In Out Wt Arm Moment Wt Arm Moment Wt Moment Lb In...

Страница 121: ...Arm Aft Weight Datum Moment Lbs Inches In Lbs Basic Empty Weight Pilot and Front Passenger 340 0 85 5 29070 Passengers Center Seats Forward Facing 118 1 Passengers Center Seats Aft Facing Optional 11...

Страница 122: ...llon Maximum 93 6 Baggage Forward 42 0 Baggage Aft 178 7 Moment due to Retraction of Landing Gear 819 Total Loaded Airplane Totals must be within approved weight and C G limits It is the responsibilit...

Страница 123: ...ATION SECTION 6 PA 32R 300 CHEROKEE LANCE WEIGHT AND BALANCE 600 450 400 250 200 150 100 50 0 5 10 15 20 25 30 35 40 45 50 55 60 MOMENT 1000 POUNDS INCHES LOADING GRAPH Figure 6 13 ISSUED AUGUST 20 19...

Страница 124: ...BALANCE PA 32R 300 CHEROKEE LANCE 3600 3400 3000 2600 2200 1800 1400 74 76 78 80 82 84 86 88 90 92 94 96 INCHES AFT OF DATUM Moment due to retracting landing gear 819 in lbs C G RANGE AND WEIGHT Figur...

Страница 125: ...ination Use the following chart to record the change in C G ITEM WEIGHT ARM MOMENT 1000 Right Front Seat 85 5 Jump Seat 118 1 3rd 4th Seats 118 1 each Forward Facing 3rd 4th Seats 119 1 each Aft Facin...

Страница 126: ...rea E Area F Aft Baggage Fuel Gal Total Weight Total Moment Ramp Weight CG Location Pilot s responsibility to determine actual arm of item loaded See Figure 6 19 for locations of loading areas CARGO W...

Страница 127: ...OADING CAPACITY AREA AREA FLOOR LOAD ALLOWABLE WEIGHT SQFT LBS SQ FT LBS A 5 15 19 0 100 B 4 16 46 5 193 C 6 56 84 0 544 D 3 75 49 0 183 E 3 75 49 0 183 F 4 22 24 0 100 MAXIMUM TIE DOWN CAPACITY Per B...

Страница 128: ...SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 6 16...

Страница 129: ...11 Landing Gear 7 6 7 13 Flight Controls 7 10 7 1 5 Fuel System 7 1 3 7 17 Electrical System 7 15 7 19 Vacuum System 7 19 7 21 Instrument Panel 7 21 7 23 Pitot Static System 7 21 7 25 Cabin Features...

Страница 130: ...BLANK PAGE...

Страница 131: ...flow NACA 652 415 airfoil section The main spar is located at approximately 40 of the chord aft of the leading edge The wings are attached to the fuselage by the insertion of the butt ends of the spar...

Страница 132: ...SECTION 7 PIPER AIRCRAFT CORPORATION DESCRIPTION AND OPERATION PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 7 2...

Страница 133: ...s located at the aft end of the induction scoop Access to the filter is gained through a detachable plate located on the outside of the lower cowl The intake air box incorporates a manually operated t...

Страница 134: ...to adjust the propeller speed from high RPM to low RPM The mixture control lever is used to adjust the air to fuel ratio The engine is shut down by the placing of the mixture control lever in the full...

Страница 135: ...TION AND OPERATION AIRCRAFT EQUIPPED WITH BACKUP GEAR EXTENDER CONTROL K B T BE PRESSED TO THE LEFT TO CLEAR THE RETAIN1NG GATE PRIOR TO SELECTING THE DESIREDPOSITION CONTROL QUADRANT AND CONSOLE Figu...

Страница 136: ...3 KIAS depending on power settings and altitude The device also prevents the gear from retracting at airspeeds below approximately 81 kts will full power though the selector switch may be in the up po...

Страница 137: ...raulic brake assemblies The nose wheel carries a 5 00 x 5 six ply tire and the main gear use 6 00 x 6 eight ply tires All three tires are tube type Two micro switches in the throttle quadrant activate...

Страница 138: ...ED AND THROTTLE CLOSED 2 LIGMT LEGENO P MOTOR R REDLIGMT T YELLOW LIGHT RESS G GREEN LIGHT W WHITE LIGMT PUMP SwiTCN 3 AUTOMATIC GEAR 00WN ACTUATOR 00 N UP L SWITCH SMOWNIN LOW AIRSPEED TO UP POSITION...

Страница 139: ...AND EMERGENCY FREE MANUAL FALLGEARVALVE FREEFALL NOTE2 EMERGENCY EXTEND NOSE MAIN GEAR MAINGEAR GEAR UP HYDRAUUC UP CYUNDER NOSE GEAR DIAPHRAGM NOTE 1 HYDRAUUC STATIC CYUNDER FROMPRESSUREHEAD ON FUSEL...

Страница 140: ...d pitch control forces The trim function is controlled by a trim control wheel located on the control console between the two front seats Figure 7 9 Rotating the wheel forward gives nose down trim and...

Страница 141: ...s To retract depress the button on the end of the handle and lower the control When extending or retracting flaps there is a pitch change in the aircraft This pitch change can be corrected either by s...

Страница 142: ...VENT A LINE ENGINE FUEL PUMP o FUEL INJECTOA FUEL FLOW g N GAUGE FUEL PRESSUAE GAUGE FILLER CAP SIGHT GAUGE SIGHT GAUGE FUEL NKS S NGEEE SAENLD L ER FSREEE G S AP OUTBOARD INBOAAD NBOARD OUTBOARD FUEL...

Страница 143: ...crews and nut plates and can be removed easily for service or inspection When using less than the standard 98 gallon capacity of the tanks fuel should be distributed equally between each side The fuel...

Страница 144: ...With full fuel tanks it will take approximately 6 seconds to drain all of the fuel from the line from either tank to the fuel strainer When the tanks are less than full it will take a few seconds long...

Страница 145: ...panel light is available as optional equipment The light is installed above the switch panel and is controlled by a rheostat switch mounted on the left side of the panel Two thumb wheel rheostat swit...

Страница 146: ...FILTER cApacitoa LAMP I TEST su ll li VAC 016 samm su se SW I OPTionAL l i I STARTER SWITCH I EXTERNAL POWER I t SOLENDIO I SATTERY n j sounoso svAnven a ace IS AMP EXTERNAL POWER RECEPTACLE STARTER...

Страница 147: ...will be indicating the amount of charging current demanded by the battery As each item of electrical equipment is turned on the current will increase to a total appearing on the ammeter This total inc...

Страница 148: ...SECTION 7 PIPER AIRCRAFT CORPORATION DESCRIPTION AND OPERATION PA 32R 300 CHEROKEE LANCE CIRCUIT BREAKER PANEL Figure 7 19 REPORT VB 840 ISSUED AUGUST 20 1976 7 18...

Страница 149: ...rease in pressure in a system that has remained constant over an extended period may indicate a dirty filter dirty screens possibly a sticking vacuum regulator or leak in system a low vacuum indicator...

Страница 150: ...RCONDITIONDOOR LIGHT 5 ATTITUDE GYRO 23 MASTERAND ACCESSORY 36 THROTTLEQUADRANT 6 GEARUNSAFELIGHT SWITCH PANEL 37 MICROPHONE BRACKET 7 DIRECTIONAL GYRO 24 AUTOPILOT 38 MIXTURE CONTROLLOCK 8 ALTIMETER...

Страница 151: ...wheninstalled Pitot and static pressure are picked up by the pitot head on the bottom of the left wing An optional heated pitot head which alleviates problems with icing or heavy rain is available Th...

Страница 152: ...SECTION 7 PIPER AIRCRAFT CORPORATION DESCRIPTION AND OPERATION PA 32R 300 CHEROKEE LANCE wg LU LULUTOI PITOT STATIC SYSTEM Figure 7 23 REPORT VB 840 ISSUED AUGUST 20 1976 7 22...

Страница 153: ...but not for the seventh seat The shoulder strap is routed over the shoulder adjacent to the windows and attached to the lap belt in the general area of the person s inboard hip The inertia reel should...

Страница 154: ...ALVE 3 DEFROSTER OUTLET 4 HEAT AND DEFROSTER AIR CONTROLS 5 OVERHEAD FRESH AIR DUCT 6 FRESHAIR OUTLET 7 OVERHEAD VENTBLOWER 8 FRESHAIR INLET 9 AIR BOX 10 CABINHEAT OUTLET 11 CABINAIR EXHAUST 12 DRAINT...

Страница 155: ...r at the top of the fire wall From this point it is ducted to the defroster outlets Fresh air inlets are located in the leading edge of each wing at the intersection of the tapered and straight sectio...

Страница 156: ...nditioning ON OFF switch are inboard of the temperature control The fan can be operated independently of the air conditioning however the fan must be on for air conditioner operation Turning either sw...

Страница 157: ...nit to the automatic position so that it will transmit only after impact and will continue to transmit until the battery is drained to depletion or until the switch is manually moved to the OFF positi...

Страница 158: ...have been activated and should be turned off immediately Reset to the ARM position and check again to insure against outside interference NOTE If for any reason a test transmission is necessary the te...

Страница 159: ...ods 8 3 8 5 Preventive Maintenance 8 4 8 7 Airplane Alterations 8 5 8 9 Ground Handling 8 6 8 11 Engine Air Filter 8 8 8 13 Brake Service 8 8 8 15 Landing Gear Service 8 10 8 17 Propeller Service 8 10...

Страница 160: ...BLANK PAGE...

Страница 161: ...ers in the United States U S and Piper Service Centers worldwide Depending on the nature of the release material and labor allowances may apply This information is provided to all authorized Piper Ser...

Страница 162: ...SECTION 8 PIPER AIRCRAFT CORPORATION HANDLING SERVICING AND MAINTENANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 8 2...

Страница 163: ...ed by the FAA A programmed Inspection approved by the Federal Aviation Administration FAA is also available to the owner This involves routine and detailed inspections to allow maximum utilization of...

Страница 164: ...r or air taxilcommercial operations service All other aircraft maintenance must be accomplished by a person or facility appropriately certificated by the Federal Aviation Administration FAA to perform...

Страница 165: ...n order and in the aircraft a To be displayed in the aircraft at all times 1 Aircraft Airworthiness Certificate Form FAA 8100 2 2 Aircraft Registration Certificate Form FAA 8050 3 3 Aircraft Radio Sta...

Страница 166: ...s seat to maintain control by use of the brakes b Taxiing Before attempting to taxi the airplane ground personnel should be instructed and approved by a qualified person authorized by the owner Engine...

Страница 167: ...s used to properly block the wheels d Mooring The airplane should be moored for immovability security and protection The following procedures should be used for the proper mooring of the airplane 1 He...

Страница 168: ...dirty or shows any damage replace it immediately 3 Wipe the filter housing with a clean cloth soaked in unleaded gasoline When the housing is clean and dry install the filter c Installation Of Engine...

Страница 169: ...9 CLEVISPIN 3 LEFT BRAKE AND RUDDER PEDAL 10 MASTER CYLINDER ASSEMBLY 4 RIGHT BRAKE CYLINDER 11 BOLT ASSEMBLY 5 LEFT BRAKE CYLINDER 12 TORQUE TUBE 6 BRAKE HANDLE 13 COPILOT SRIGHTBRAKE AND RUDDER PEDA...

Страница 170: ...uld be used At least 250 pounds of ballast should be placed on the base of the tail stand before the airplane is jacked up The hydraulic jacks should be placed under the jack points on the bottom of t...

Страница 171: ...of time the engine warrenty is invalidated by the use of unapproved fuels Refer to the latest issue of Lycoming Service Instruc tions 1070 for approved alternate grade fuels c Filling Fuel Tanks Obser...

Страница 172: ...ning fuel may be drained through the fuel strainer 8 23 TIRE INFLATION For maximum service from the tires keep them inflated to the proper pressures 35 psi for the nose gear and 38 psi for the main ge...

Страница 173: ...not recommended 8 27 CLEANING a Cleaning Engine Compartment Before cleaning the engine compartment place a strip of tape on the magneto vents to prevent any solvent from entering these units 1 Place...

Страница 174: ...cedure 1 Flush away loose dirt with water 2 Apply cleaning solution with a soft cloth a sponge or a soft bristle brush 3 To remove exhaust stains allow the solution to remain on the surface longer 4 T...

Страница 175: ...y cleaner suitable for the material Carefully follow the manufacturer s instructions Avoid soaking or harsh rubbing CAUTION Solvent cleaners require adequate ventilation 3 Leather should be cleaned wi...

Страница 176: ...SECTION 8 PIPER AIRCRAFT CORPORATION HANDLING SERVICING AND MAINTENANCE PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 8 16...

Страница 177: ...ent Page No No 9 1 General 9 1 1 Air Conditioning System Installation 9 3 2 AutoFlite II Autopilot Installation 9 7 3 AutoControl IIIB Autopilot Installation 9 9 4 AltiMatic IIIC Autopilot Installatio...

Страница 178: ...BLANK PAGE...

Страница 179: ...f the airplane when equipped with one or more of the various optional systems and equipment not provided with the standard airplane All of the Supplements provided by this section are FAA Approved and...

Страница 180: ...SECTION 9 PIPER AIRCRAFT CORPORATION SUPPLEMENTS PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 9 2...

Страница 181: ...IONS a To insure maximum climb performance the air conditioner must be turned OFF manually prior to takeoff to disengage the compressor and retract the condenser door Also the air conditioner must be...

Страница 182: ...hen the door is open and is off when the door is closed SECTION 5 PERFORMANCE Operation of the air conditioner will cause slight decreases in cruise speed and range Power from the engine is required t...

Страница 183: ...throttle position is selected When the full throttle position is not used or in the event of a nialfunction which would cause the compressor to operate and the condenser door to be extended a decreas...

Страница 184: ...SECTION 9 PIPER AIRCRAFT CORPORATION SUPPLEMENTS PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 9 6...

Страница 185: ...ion PRESS disconnect switch on pilot s control wheel b In case of malfunction overpower autopilot at either control wheel c AutoFlite II master switch OFF d In climb cruise or descent configuration a...

Страница 186: ...used for lesser turn rates d OMNI Tracker 1 Turn Command Knob move to center detent position and push IN to engage tracker Aircraft will track desired radial established on NAV 1 or as selected if equ...

Страница 187: ...ch OFF I b The autopilot can be overpowered at either control wheel c An autopilot runaway with a 3 second delay in the initiation of recovery while operating in climb cruise or descending flight coul...

Страница 188: ...Instrument Display Optional 1 VOR Navigation a Tune and identify VOR Station Select desired course with O B S H S I Course Knob b Select OMNI mode on Radio Coupler c Select HDG mode on autopilot conso...

Страница 189: ...he HDG bug to the same heading Select OMNI mode on the coupler and HDG Mode on the autopilot console 2 For ILS Front Course Intercepts and Tracking Tune the localizer frequency and place the HDG bug o...

Страница 190: ...SECTION 9 PIPER AIRCRAFT CORPORATION SUPPLEMENTS PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 9 12...

Страница 191: ...with a Master Disconnect Interrupt Switch on the pilot s control wheel When the switch button is depressed it will disconnect the autopilot When depressed and held it will interrupt all Electric Elev...

Страница 192: ...ured in approach configuration and operating either coupled or uncoupled EMERGENCY OPERATION WITH OPTIONAL HSI Non Slaved a Appearance of HDG Flag 1 Check air supply gauge vacor pressure for adequate...

Страница 193: ...aired Substitution of any trim system component for another model is not authorized For emergency interrupt information refer to Section 3 of this Supplement Command Electric Trim Switch The Command E...

Страница 194: ...e of climb or descent should be reduced to approximately 500 FPM prior to altitude hold engagement For accurate Altitude Holding below 95 KIAS lower flaps one or two notches NOTE Prior to disengaging...

Страница 195: ...e HDG bug on the inbound course heading to the airport Select LOC REV mode on the coupler and engage HDG mode on the autopilot console h Coupled Approach Operations 1 VOR or LOC a After arrival at the...

Страница 196: ...f the aircraft e Monitor localizer and Glide Slope raw data throughout approach Adjust power as necessary to maintain correct final approach airspeed All power changes should be of small magnitude and...

Страница 197: ...verpower the electric trim at either control wheel c Maximum altitude change with a 4 second delay in recovery initiation is 800 feet and occurs in the descent configuration Maximum altitude change in...

Страница 198: ...SECTION 9 PIPER AIRCRAFT CORPORATION SUPPLEMENTS PA 32R 300 CHEROKEE LANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 840 ISSUED AUGUST 20 1976 9 20...

Страница 199: ...TABLE OF CONTENTS SECTION 10 OPERATING TIPS Paragraph Page No No 10 1 General 10 1 10 3 Operating Tips 10 1 REPORT VB 840 10 i...

Страница 200: ...all radio switches light switches and the pitot heat switch are in the off position so as not to create an overloaded condition when the starter is engaged f Strobe lights should not be operating whe...

Страница 201: ...flow interruption may occur Prolonged slips or skids which result in excess of 2000 ft of altitude loss or other radical or extreme maneuvers which could cause uncovering of the fuel outlet must be a...

Страница 202: ...BLANK PAGE...

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