Piper Cherokee Archer II Pilot Operating Handbook Download

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Summary of Contents for Cherokee Archer II

Page 1: ...D MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES AIRPLANE SERIAL NO _____________________________ AIRPLANE REGISTRATION NO ______________________ PA 28 181 REPORT VB 760 FAA APPROVED BY ________________...

Page 2: ...SUBSEQUENTLY REVISED IS VALID FOR USE WITH THE AIRPLANE IDENTIFIED ON THE FACE OF THE TITLE PAGE WHEN OFFICIALLY APPROVED SUBSEQUENT REVISIONS SUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE PROPERLY I...

Page 3: ...pages 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 direc...

Page 4: ...ed 8 7 a items I 2 and 3 lan 6 1976 Revised checklist Revised wording of 3 11 Revised 3 15 info Revised approach speed in 4 29 Revised takeoff perfonnance Added Fig 5 6 5 8 and 5 30 Revised Fig 5 5 Ad...

Page 5: ...dded info from pg 8 13 relocated info 10 pg 8 15 8 15 Added info from pg 8 14 1 3 Revised para 1 9 Item c 8 1 Revised para 8 t 8 3 Revised para 8 3 8 4 Revised para 8 5 8 1 J Revised para 8 19 Revised...

Page 6: ...ON 8 SECTION 9 SECTION 10 TABLE OF CONTENTS GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT AND BALANCE DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS AIRPLANE...

Page 7: ...n I I 1 3 Engines 1 3 1 5 Propellers 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 Loadings 1 4 1 19 Symbols Abbreviatio...

Page 8: ...is 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 i...

Page 9: ...CORPORATION PA 28 181 CHEROKEE ARCHER II t L Wing Area sq ft 170 0 Min Turning Radius ft 30 0 from pivot point to wingtip n nn 3 20 I L L_ li 1 1 _ 35 0 0 1 REPORT VB 760 1 2 1 1 10 U i 23 UI THREE VI...

Page 10: ...ity U S Quarts b Oil Specification SECTION 1 GENERAL Lycoming 0 360 A4M 180 2700 5 125 4 375 361 0 8 5 1 Four Cylinder Direct Drive Horizontally Opposed Air Cooled Sensenich 76EM8S5 0 60 2 76 76 Fixed...

Page 11: ...mpty Weight 1 15 BAGGAGE SPACE a Compartment Volume cubic feet b Entry Width inches c Entry Height inches 1 17 SPECIFIC LOADINGS a Wing Loading Ibs per sq ft b Power Loading lbs per hp PIPER AIRCRAFT...

Page 12: ...ratio of true airspeed to the speed of sound True Airspeed is the airspeed of an airplane relative to undisturbed air which is the CAS corrected for altitude temperature and compressability Maneuveri...

Page 13: ...e air static temperature obtained either from inflight temperature indications or ground meteorological sources adjusted for instrument error and compressibility effects The number actually read from...

Page 14: ...ate Stop Distance MEA Route Segment ISSUED AUGUST IS 1975 The demonstrated ratio of the change in height during a portion of a climb to the horizontal distance traversed in the same time interval The...

Page 15: ...e point at which an airplane wo uld balance if suspended Its distance from the reference datum is found by dividing the total momenl by the total weight of the airplane The arm obtained by adding the...

Page 16: ...PIPER AIRCRAFT CORPORATION PA 2S ISI CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975 SECTION I GENERAL REPORT VB 760 1 9...

Page 17: ...SECTION 1 GENERAL REPORT VB 760 1 10 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 18: ...Cll yards 35 1 eu ft 26 1 2 U S gal Cll yards 27 0 Cll ft 7 H6 x It 1 Cll melers 2 022 x 10 2 U S gal deg arc 1 745 x 1 2 radians ISSUED AUGUST 15 1975 MULTIPLY feel ftlmln ftlsec Mb ft Ihlmin ft lbls...

Page 19: ...SECTION I GENERAL REPORT VB 760 1 12 PIPER AIRCRAIT CORPORATION PA lI IIl CHEROKEE ARCHER 11 ISSUED AUGUST IS 1975...

Page 20: ...ians rev min 1 047 x 10 1 radians sec rod 16 5 ft 5 5 yd slug 32 174 lb sqcm 1 550 x 10 1 sq in 1 076 x 10 3 sq ft sq ft 929 0 sqcm 144 0 sq in 1 111 x 10 1 sq yards 2 296 x 10 5 acres sq in 6 452 sqc...

Page 21: ...SECTION 1 GENERAL REPORT VB 760 1 14 PIPER AIRCRAFI CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 22: ...5 Airspeed Indicator Markings 2 2 2 7 Power 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...

Page 23: ...ich require handbook supplements can be found in Section 9 Supplements 2 3 AIRSPEED LIMITATIONS SPEED Never Exceed Speed V Do not exceed this speed in any operation Maximum Structural Cruising Speed V...

Page 24: ...red line g Fuel Grade minimum octane h Number of Propellers i Propeller Manufacturer U Propeller Model k Propeller Diameter Minimum Maximum I Propeller Tolerance static RPM at maximum permissible thr...

Page 25: ...ellow Arc Caution Range Idle Red Line Minimum Red Line Maximum d Fuel Pressure Green Arc Normal Operating Range Red Line Minimum Red Line Maximum 2 11 WEIGHT LIMITS a Maximum Weight b Maximum Baggage...

Page 26: ...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 a Normal...

Page 27: ...135 a Day V F R b Night V F R c Day I F R d Night I F R e Non Icing 2 21 FUEL LIMITATIONS a Total Capacity b Unusable Fuel The unusable fuel for this airplane has been determined as 1 0 gallon in each...

Page 28: ...SECTION 2 LIMITATIONS REPORT VB 760 2 6 PIPER AIRCRAFf CORPORATION PA l8 181 CHEROKEE ARCHER U THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 29: ...PERATIONS SPINS ARE PROHIBITED FOR BOTH NORMAL AND UTILITY CATEGORIES SECTION 2 LIMITATIONS In full view of the pilot the following takeoff and landing check lists will be installed Fuel on proper tan...

Page 30: ...GAGE AND AFT PASSENGER LIMITATIONS In full view of the pilot ROUGH AIR OR MANEUVERING SPEED 124 MPH UTILITY CATEGORY OPERATION NO AFT PASSENGERS ALLOWED DEMONSTRATED CROSS COMPONENT 20 MPH On the inst...

Page 31: ...mplified Emergency Procedures General Engine Fire During Start Engine Power Loss During Takeoff Engine Power Loss In Flight Power Off Landing Fire In Flight Loss of Oil Pressure Loss of Fuel Pressure...

Page 32: ...containing additional information to provide the pilot with a more complete understanding of the procedures These procedures are suggested as the best course of action for coping with the particular c...

Page 33: ...SECTION 3 EMERGENCY PROCEDURES PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 760 3 2 ISSUED AUGUST 15 1975...

Page 34: ...cated check tank selector position to be sure it is on a tank containing fuel When power is restored Carburetor heat OFF Electric fuel pump OFF ISSUED AUGUST 15 1975 REVISED NOVEMBER 12 1976 SECTION 3...

Page 35: ...h If lower latch is open open top latch push door further open and close rapidly Latch top latch A slip in direction of open door will assist latching All switch OFF ENGINE ROUGHNESS Reduce electrical...

Page 36: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II SECTION 3 EMERGENCY PROCEDURES THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975 REPORT VB 760 3 5...

Page 37: ...SECTION 3 EMERGENCY PROCEDURES PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 760 3 6 ISSUED AUGUST 15 1975...

Page 38: ...e fuel selector valves should be OFF and the mixture at idle cut off if an external fire extinguishing method is to be used 3 9 ENGINE POWER LOSS DURING TAKEOFF The proper action to be taken if loss o...

Page 39: ...ill be normal If engine failure was caused by fuel exhaustion power will not be restored after switching fuel tanks until the empty fuel lines are filled This may require up to ten seconds If power is...

Page 40: ...procedure given is general and pilot judgment should be the determining factor for action in such an emergency 3 17 LOSS OF OIL PRESSURE Loss of oil pressure may be either partial or complete A partia...

Page 41: ...uating an electrically powered device such as the landing light If no increase in the ammeter reading is noted alternator failure can be assumed The electrical load should be reduced as much as possib...

Page 42: ...ed or altitude If too much ice is allowed to accumulate restoration of full power may not be possible therefore prompt action is required Turn carburetor heat on See Note RPM will decrease slightly an...

Page 43: ...SECTION 3 EMERGENCY PROCEDURES PIPER AIRCRAFf CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 760 3 12 ISSUED AUGUST 15 1975...

Page 44: ...l 4 7 4 9 Preflight Check 4 7 4 11 Before Starting Engine 4 8 4 13 Starting Engine 4 9 4 15 Warm Up 4 11 4 17 Taxiing 4 11 4 19 Ground Check 4 11 4 21 Before Takeoff 4 12 4 23 Takeoff 4 12 4 25 CIimb...

Page 45: ...an action sequence for normal operations with little emphasis on the operation of the systems The remainder of the section is devoted to amplified normal procedures which provide detailed information...

Page 46: ...SECTION 4 NORMAL PROCEDURES REPORT VB 760 4 2 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 47: ...tank sumps drain Fuel vents open Main gear struts proper inflation 4 50 in Tires check Brake blocks check ISSUED AUGUST 15 1975 Pitot head remove cover holes clear Windshield clean Propeller and spinn...

Page 48: ...ammeter Oil pressure check WARM UP Throttle 800 to 1200 RPM TAXIING Chocks Removed Taxi area clear Throttle 1 2 open Throttle apply slowly Master switch ON Brakes check Electric fuel pump ON Steering...

Page 49: ...b past the obstacle Accelerate to best flaps up rate of climb speed 87 MPH lAS 76 KTS lAS ISSUED AUGUST 15 1975 REVISED MARCH 16 1979 SOFT FIELD SECTION 4 NORMAL PROCEDURES Flaps 25 second notch Accel...

Page 50: ...r OFF Radio s OFF Throttle full aft Mixture idle cut off Magnetos OFF Master switch OFF PARKING Parking brake set Control wheel secured with belts Flaps full up Wheel chocks in place Tie downs secure...

Page 51: ...switch should be returned to the OFF position after the check is complete The next step is to check the navigation lights The master switch must be ON for this check Return the master switch to OFF a...

Page 52: ...he cowling and check for any obvious fuel or oil leaks Check the oil level Make sure that the dipstick has properly seated after checking Secure the cowling and check the inspection covers Check the a...

Page 53: ...ON the master switch and turn OFF the electric fuel pump Move the mixture control lever to idle cut off and engage the starter by rotating the magneto switch clockwise and pressing in When the engine...

Page 54: ...e trouble In cold weather it wiJI take a few seconds longer to get an oil pressure indication If the engine has failed to start refer to the Lycoming Operating Handbook Engine Troubles and Their Remed...

Page 55: ...ven ground Do not operate the engine at high RPM when running up or taxiing over ground containing loose stones gravel or any loose material that may cause damage to the propeller blades 4 19 GROUND C...

Page 56: ...23 TAKEOFF The normal takeoff technique is conventional for the Cherokee Archer II The tab should be set slightly aft of neutral with the exact setting determined by the loading of the airplane AHow t...

Page 57: ...mixture control until the engine becomes rough indicating that the lean mixture limit has been reached in the leaner cylinders Then enrich the mixture by pushing the control towards the instrument pa...

Page 58: ...ind and airplane loading It is generally good practice to contact the ground at the minimum possible safe speed consistent with existing conditions Normally the best technique for short and slow landi...

Page 59: ...so precede the stall The gross weight stalling speed of the Cherokee Archer II with power off and full flaps is 61 MPH CAS 53 KTS CAS With the flaps up this speed is increased 7 MPH 6 KTS Loss of alti...

Page 60: ...speed to reduce the structural loads caused by gusts and to allow for inadvertent speed build ups which may occur as a result of the turbulence or of distractions caused by the conditions 4 39 WEIGHT...

Page 61: ...ABLE OF CONTENTS SECTIONS PERFORMANCE Page No 5 1 General 5 1 5 3 Introduction to Performance and Flight PJanning 5 1 5 5 Flight Planning Example 5 3 5 7 Performance Graphs 5 9 List of Figures 5 9 REP...

Page 62: ...s are unfactored and do not make any allowance for varying degrees of pilot proficiency or mechanical deterioration of the aircraft This performance however can be duplicated by following the stated p...

Page 63: ...SECTION 5 PERFORMANCE REPORT VB 760 5 2 PIPER AIRCRAFf CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFl BLANK ISSUED AUGUST 15 1975...

Page 64: ...xample The landing weight cannot be determined until the weight of the fuel to be used has been established refer to item g 1 J 1 Basic Empty Weight 2 Occupants 2 x 170 lbs 3 Baggage and Cargo 4 Fuel...

Page 65: ...values are the first variables to be considered in determining the climb components from the Time Distance and Fuel to Climb graph Figure 5 11 After the time distance and fuel for the cruise altitude...

Page 66: ...al distance to be traveled during 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...

Page 67: ...light planning example 1 Total Flight Time c 3 plus d l plus e 6 13 hrs plus 11 hrs plus 2 62 hrs g Total Fuel Required 2 86 hrs Determine the total fuel required by adding the fuel to climb the fuel...

Page 68: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975 SECTIONS PERFORMANCE REPORT VB 760 5 7...

Page 69: ...SECTIONS PERFORMANCE REPORT VB 760 5 8 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 70: ...14a 5 8 25 Flaps Takeoff Ground Roll 5 14b 5 9 Climb Performance 5 15 5 11 Time Distance and Fuel to Climb 5 16 5 13 Engine Performance 5 17 5 15 Speed Power Performance Cruise 5 18 5 17 Speed Power...

Page 71: ...SECTION 5 PERFORMANCE REPORT VB 760 5 10 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 72: ...APS 40 150 140 g 130 IE 120 e 110 Ii c 100 90 c u 80 II mID 10 u I I i V Ioeo 1 I IE c a 7 80 c u 6060 10 80 90 108 110 128 INDICATED AIRSPEED MPH INDICATED AIRSPEED KTS 60 70 10 SO 100 UI 120 130 130...

Page 73: ...POWlR Off 0 FlAI 25 FlAI 40 FUPS 2550 lIS ClOSS WDINT I CAlIIIUEOstU s G lenn SPUDS I I I I I I I I I I I I L 24 22 20 2 WEIGHT IOO LIS 4 REPORT VB 760 5 l2 I I I I l 20 STALL SPEEDS Figure 5 3 Iii Ir...

Page 74: ...P C r PAVED LEVEL DRY RUNWAY ex r r WT I liS r 2550 I 2450 2350 r 2250 2150 I I 12UO I I r r i f i i I 1 Irio f o r r r I t r f r I 1 0 i o r r r r r I r r 2550 2500 2400 i 2300 2200 G ROSS LBS Exampl...

Page 75: ...r l f i r r i tr r t r I i i r t r I i I I r o I t I 1 0 r I r l i r I 1 000 l i l t 1 000 I I 2550 2450 2350 2251 WEIGHT POUNDS Example Airport pressure altitude 200 ft Temperature 70 F Gross weight...

Page 76: ...50 4t 54 1 I I i i 2050 47 52 I 2100 ffj I I V f or i 218 J j r i i I t II I V I r _ f 9IIJ I r to I I 2400 1ft V V e I J J r 0 1 1 J f r 211 t 1 J 1 t r f _r I I I a J V r i I I 1 I I a I V r i i i o...

Page 77: ...LLV l r I l l It 4 m 1m ml mt Zlil aurSIDE AI TEll of I I I I I I I I I I i i i 11 t zo OOTSIDE TEIIP C CROSS WElCIfT lIS Example Airport pressure alliludc 200 fl Ibnpc ralurc 1 1 Gruss wdghl 2400 Ihs...

Page 78: ...j V II IJ J V V 20 0 20 40 10 10 100 OUTSIDE AIR TEMP OF it i i i t i 20 10 0 10 20 30 OUTSIDE AIR TEMP oC ISSUED AUGUST 15 1975 PA 28 181 I 1 FUU THROTTLE fLAPS UP 81 M P H 1 17 ITS U S J 1 1 I 2550...

Page 79: ...OKEE ARCHER II PA 28 181 20 0 20 40 60 80 100 0 5 10 15 20 25 30 35 40 45 50 55 60 TIME DISTANCE AND FUR TO ClIMB OUTSIDE AIR TEMP oF I 1 I I i i i f i 20 10 0 10 20 30 OUTSIDE AIR TEMP oC REPORT VB 7...

Page 80: ...I V 1 I I 1 jI 1 L I II I II J I I I I I I 1 I I I 5 JO J5 I I II I I J I I I I SECTIONS PERFORMANCE 1 i I FUEL flOW G P H I J V V 1 II I BEST POWU BEST ECONOMY I i V V V I 1 II I 1 1 I I V V I 1 IV 1...

Page 81: ...N PA 28 181 CHEROKEE ARCHER II PA 28 181 1 I I I BEST POWER llllURE II 2550 lIS GROSS IT J j MIXTURE L lICit AIOVE 75 WIIO 180 j t RICH OF PUI CT IELOW 75 POWEI II I I WHEEL FAIRIltIS IIISTAUlD I 1 SU...

Page 82: ...I PA 28 181 SECTION 5 PERFORMANCE j V I 1 v V T I I I j 1 V I V II j J V Y V V 1 V V 20 0 20 40 60 10 100 OUTSIDE AIR TEMP oF t i i I J j 20 10 0 10 20 30 OUTSIDE AIR TEMP oC SPEED POWER ECONOMY CRUIS...

Page 83: ...SER IilAOO 1I AT 55 POWf T 100 F IDI OF PEAl Eat I 85 WHEEL FAlla ISTAu D 85 48 8AL USABLE FUEL I 2550 PIIIeS ZERO WIND I I THIS UNII IG IIIES C1M i 75 AID DE CEIT DISTANCE I WII75 1 i I II l i 1 i I...

Page 84: ...II j II I 20 o 20 40 60 80 100 600 700 700 SECTIONS PERFORMANCE OUTSIDE AIR TEMP RANGE STATUTE MUS t t I i i J j i i i I 20 10 0 10 20 30 500 550 600 RANGE NAUTICAL MILES 600 50 OUTSIDE AIR TEMP oc IS...

Page 85: ...IR TEMP it i i i t i i t 20 10 0 to 20 30 OOTSIDE AIR TEMP 0 C REPORT VB 760 5 22 PIPER AIRCRAFT CORPORATION PA 8 181 CHEROKEE ARCHER II PA 28 181 IIfM QDOO fMCII 1 45 MIN RESERVE BEST E_MY IIX11JIE 1...

Page 86: ...Jj V L I I J lL II i I V L 1 V If lL Cnlis IL if v I V V i If II j v V I Ie 1 I I V 1 If LI L Il V v t IStilllti 1 J _ Altitude I V 1 1 I Co I r V r V y V V lL V V V L 1 V If I l IL Vi 20 0 20 40 50 1...

Page 87: ...1 v I V Vel v v j j V v V I V 1 o i 1 I V v I j j 1 1 VI 1 j J V V o i I j II y V V I PI V 1 v I j 1 V v V j 1 V 1V 20 0 20 40 0 80 tOO OUTSIDE AIR TEMP OF if i J i i i i I I 20 to 0 10 20 3D OUTSIDE...

Page 88: ...XIMUM BRAKING PAVED LEVEl DRY RUNWAY I 40 20 20 40 0 II 2sla 2500 2UG 2301 2200 OUTSIDE AIR TEMP OF I I I I i I I I i i i I I 40 20 0 20 OUTSIDE AIR TEMP C GROSS WEI6KT L8S Example Airport pressure al...

Page 89: ...20 OUTSIDE AIR TEMP C fULL STAlL TOUCHDOWN MAXIMUM BRAKING PAVED LEVEL DRY RUNWAY z I z O I GROSS WEIGHT LBS Example Airport pressure alt itude 2300 flo Temperature 70 F Gross weight 22M Ihs Wind 5 k...

Page 90: ...s d Electrical Equipment e Instruments f Miscellaneous g Engine and Engine Accessories Optional Equipment h Propeller and Propeller Accessories Optional Equipment i Landing Gear and Brakes Optional Eq...

Page 91: ...ed limit A properly loaded airplane however will perform as intended Before the airplane is delivered it is weighed and a basic empty weight and e G location is computed basic empty weight consists of...

Page 92: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 2 PIPER AIRCRAFT CORPORATION PA l8 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 93: ...g fuel is drained Operate engine on each tank until all undrainable fuel is used and engine stops Then add the unusable fuel 2 0 gallons total 1 0 gallons each wing CAUTION Whenever the fuel system is...

Page 94: ...t Main Wheel R Left Main Wheel L Basic Empty Weight as Weighed T Scale Reading WEIGHING FORM Figure 6 1 d Basic Empty Weight Center of Gravity Net Tare Weight l The following geometry applies to the P...

Page 95: ...nterline to the main wheel cenlerline 3 Obtain measurement B by measuring the distance from the main wheel centerline horizontally and parallel to the airplane centerline to each side of the nose whee...

Page 96: ...irplane serial number and registration number shown The basic empty weight of the airplane as delivered from the factory has been entered in the Weight and Balance Record Figure 6 7 This form is provi...

Page 97: ...eight Optional Equipmcm Basic Empty Weight The standard empty weight includes full oil capacity and 2 0 gallons of unusable fuel AIRPLANE USEFUL LOAD Gross Weight Basic Empty Weight Useful Load Normal...

Page 98: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 8 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFr BLANK ISSUED AUGUST 15 1975...

Page 99: ...Z t J 1 PA 28 l8l Serial Numher Item No Date Description of Article or Modil1cation In Out As Delivered Registration Number Page Number Weight Change Running Basic Added Removed Empty Weight Wt Arm M...

Page 100: ...umber Item No Weight Change Runni ng Basic Added Removed Empty Weight Date Description of Aniclc or Modificalion In Oul WI Arm Moment WI Ann Moment WI Moment Lh In 100 O h I n 100 Lb 100 As Delivered...

Page 101: ...C G envelope the loading meets the weight and balance requirements Arm Aft Weight Datum Moment Lbs Inches In Lbs Basic Empty Weight Pilot and Front Passenger 340 0 80 5 27370 Passengers Rear Seats 340...

Page 102: ...t be within approved weight and CO limits It is the responsibility of the airplane owner and the pilot to insure that the airplane is loaded properly The Basic Empty Weight CO is noted on the Weight a...

Page 103: ...300 0 I 250 W I V I I 7 Iv I I I V V 3 c 200 0 I 150 I V I I v V v V V V v 1 V V l 100 I l V V V I V v 50 0 C I V o 5 10 15 20 25 30 35 MOMENT 1000 POUNDS INCHES LOADING GRAPH Figure 6 13 ISSUED AUGUS...

Page 104: ...2000 I w 800 t 600 400 200 REPORT YB 760 6 14 V f 82 V 8 PIPER AIRCRAFT CORPORATION PA lI III CHEROKEE ARCHER n N RMAL CATEGORY V I UTILITY CATEGORY I I I I I I I I I I I I II 10 92 96 INCHES AFT OF D...

Page 105: ...PIPER AIRCRAFr CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975 SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 15...

Page 106: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 16 PIPER AIRCRAFT CORPORATION CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST IS 1975...

Page 107: ...lternate standard items and those required to be listed by the certificating authority FAA are presented Items marked with an X are those items which were installed on the airplane described below as...

Page 108: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 18 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 109: ...60 A4M Piper Dwg 62941 16 Cert Basis TC E286 13 Oil Filter Lycoming No 75528 AC OF5578770 Cert Basis TC E286 15 Oil Filter Lycoming LW 13743 Champion CH 48110 Cert Basis TC E286 ISSUED AUGUST 15 1975...

Page 110: ...SECflON6 WEIGHT AND BALANCE REPORT VB 760 6 20 PIPER A1RCRAFI CORPORATION PA 8 181 CHEROKEE ARCHER D THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 111: ...0 55 Cert Basis TSO C26a b Two Main 4 Ply Rating Tires 6 00 6 with Regular Tubes Cert Basis TSO C26b 29 One Nose Wheel a Cleveland Aircraft Products Wheel Assembly No 40 76B Less Brake Drum Cert Basis...

Page 112: ...SECTION6 WEIGHT AND BALANCE REPORT VB 760 6 22 PIPER AIRCRAFf CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 113: ...CRAFT CORPORATION PA 28 18I CHEROKEE ARCHER II Item No d Electrical Equipment Item ISSUED AUGUST IS 1975 Mark if Inst Weight Pounds SECflON6 WEIGHT AND BALANCE Arm In Aft Datum Moment Lb In REPORT VB...

Page 114: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 24 PIPER AIRCRAFT CORPORATION PA 18 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 115: ...Instruments Item 53 Airspeed Indicator Piper Dwg 63205 2 Cert Basis TSO C2b 55 Altimeter Piper Spec PS50008 2 or 3 Cert Basis TSO Cl Db ISSUED AUGUST IS 1975 Mark if Instl Weight Pounds SECTION 6 WEI...

Page 116: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 26 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 117: ...laneous Item 65 Forward Seat Belts 2 Piper Spec PS50039 4 2A Cert Basis TSO e22f 67 Rear Seat Belts 2 Piper Spec PS50039 4 3 Cert Basis TSO e22f ISSUED AUGUST IS 1975 Mark if Instl Weight Pounds SECTI...

Page 118: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 28 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 119: ...sis TC 2A13 81 Vacuum Pump Airborne Mfg Co Model 211ec and Drive PAC 79399 0 Cert Basis TC 2A 13 83 Low Vacuum Annunciator Light Cert Basis TC 2A 13 85 Vacuum Regulator Airborne Mfg Co 2H3 19 Cert Bas...

Page 120: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 30 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 121: ...ON PA 28 18I CHEROKEE ARCHER Item No h Propeller and Propeller Accessories Optional Equipment Item ISSUED AUGUST 15 1975 Mark if Inst Weight Pounds SECTJON6 WEIGHT AND BALANCE Ann In Aft Datum Moment...

Page 122: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 32 PIPER AlR CRAFf CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 123: ...ATION PA 28 I8I CHEROKEE ARCHER II Item No 0 Landing Gear and Brakes Optional Equipment Item ISSUED A UGUST IS 1975 Mark if Instl Weight Pounds SECfION6 WEIGHT AND BALANCE Arm In Aft Datum Moment Lb I...

Page 124: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 34 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 125: ...ght 27 2 Ibs Cert Basis TC 2A 13 119 Cabin Light Piper Owgs 66632 0 95229 0 Cen Basis TC 2A13 121 Cabin Speaker 58 1 5052 or 6EU 1937 Quincy Speaker Co Oakton Indiana Cert Basis TC 2A 13 123 Auxiliary...

Page 126: ...Piper Dwg 69041 7 Cert Basis TC 2A13 131 Instrument Panel Lights Cert Basis TC 2A13 133 Instrument Light Grimes 15 0083 7 eert Basis TC 2A13 REPORT V8 760 6 36 Mark If Instl PIPER AIRCRAFr CORPORATION...

Page 127: ...t Basis TC 2A13 155 Clock Cen Basis TC 2A 13 157 Tru Speed IndicalOr Piper Dwg 62 143 2 or 13 Cent Basis TSO C2b 159 Turn and Slip Indicator Piper Spec PS5OO30 2 or 3 eert Basis TSO C3b 161 Manifold P...

Page 128: ...or 7 Cert Basis TSO ClOb C88 167 Engine Hour Meter Piper Dwg 79548 0 Cert Basis TC 2A13 Mark if Instl PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER n Weight Arm In Moment Aft Datum Lb In 9 60 3...

Page 129: ...7 AutoFlite II Cert Basis STC SA3066SW D 179 AutoControl IllB Cert Basis STC SA3065SW D 181 Omni Coupler IC388 Cert Basis STC SA3065SW D ISSUED AUGUST 15 1975 Mark if Instl Weight Pounds 5 6 9 6 1 0 S...

Page 130: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 40 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFf BLANK ISSUED AUGUST 15 1975...

Page 131: ...ceiver 2nd King KN 77 VOR LOC Converter K ng KNI 520 VORlILS Indicator Cert Basis TSO C36c C37b C38b C40a 197 King KJ 201 VORl LOC Ind Cen Basis TC 2AI3 a Single b Dual 199 King KI 2 13 VORILOC GS Ind...

Page 132: ...TC 2A13 a Single b Dual 213 Narco Nav 12 VHF Receiver Cert Basis TC 2A13 215 Narco Nav 14 VHF Receiver Cert Basis TC 2A13 217 Narco Comm J 11 VHF Transceiver Cert Basis TSO C37b C38b a Single b Dual...

Page 133: ...227 Narco UGR 2A Glide Slope Receiver Cable Antenna Cable Antenna Cen Basis TC 2A 13 229 Narco UGR 3 Glide Slope Receiver Cable Antenna Cable Antenna Cen Basis TC 2Al 3 231 Narco MBT 12 R Marker Beac...

Page 134: ...KR S5 ADF Cert Basis TSO C41b a Audio Amplifier 243 King KR 86 ADF Cert Basis TC A3S0 a First b Second c Audio Amplifier 245 Narco ADF I40 Cert Basis TSO C4Jc a Single h Dual REPORT VB 760 6 44 Marl...

Page 135: ...r Cen Basis TSO C74b 255 Nav Receiving Antenna Cen Basis TC 2A13 a Antenna b Cable 257 Comm Antennas Cen Basis TC 2A 13 a 1 Antenna b 1 Cable c 2 Antenna d 112 Cable 259 Single ADF Sense Antenna and C...

Page 136: ...c Transmitter Piper Dwg 79761 4 d Antenna and Coax 265 Microphone Cert Basis TC 2A13 a Carbon Piper Dwg 68856 10 b Dynamic Piper Dwg 68856 11 c Dynamic Piper Dwg 68856 12 267 Headset Piper Owg 68856...

Page 137: ...PIPER AIRCRAIT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST IS 1975 SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 47...

Page 138: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 48 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST IS 1975...

Page 139: ...gs Piper Dwg 65237 Cen Basis TC 2A13 291 Vert Adj Front Seats Left Piper Owg 79591 0 Cert Basis TC 2A I3 293 Vert Adj Front Seal Right Piper Owg 79591 1 Cert Basis TC 2A13 295 Super Cabin Sound Proofi...

Page 140: ...g 35493 2 Cert Basis TC 2A13 Calibrated Alternate Static Source Placard Required Yes 307 Headrest 2 Front Piper Dwg 79337 18 Cert Basis TC 2A13 309 Headrest 2 Rear Piper Dwg 79337 18 Cert Basis TC 2A1...

Page 141: ...less Steel Control Cables Piper Dwg 79700 0 Cen Basis TC 2A 13 TOTAL OPTIONAL EQUIPMENT EXTERIOR FINISH Base Color____________ Trim COIOT _ _ _ _ _ _ _ _ _ _ __ Accent Color ___________ ISSUED AUGUST...

Page 142: ...SECTION 6 WEIGHT AND BALANCE REPORT VB 760 6 52 PIPER AIRCRAFI CORPORATION PA lII I81 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST IS 1975...

Page 143: ...trols 7 5 7 11 Engine Controls 7 6 7 13 Fuel System 7 8 7 15 Electrical System 7 10 7 17 Vacuum System 7 15 7 19 Instrument Panel 7 16 7 2t Pilot Static System 7 18 7 23 Heating and Ventilating System...

Page 144: ...which is an integral part of the fuselage structure providing in effect a continuous main spar with splices at each side of the fuselage There are also fore and aft attachments at the rear spar and a...

Page 145: ...SECTION 7 DESCRIPTION AND OPERATION REPORT VB 760 7 2 MAIN WHEEL ASSEMBLY Figure 7 1 PIPER AIRCRAFf CORPORATION PA 28 fin CHEROKEE ARCHER II ISSUED AUGUST 15 1975...

Page 146: ...er is included in the nose gear The three struts are of the air oil type with a normal extension of 3 25 inches for the nose gear and 4 50 inches for the main gear The standard brake system for this C...

Page 147: ...SECTION 7 DESCRIPTION AND OPERATION PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 760 7 4 ISSUED AUGUST 15 1975...

Page 148: ...rons are provided with a differential action which tends to reduce adverse yaw in turning maneuvers and which also reduces the amount of coordination required in normal turns A rudder trim adjustment...

Page 149: ...just the air to fuel ratio The engine is shut down by the placing of the mixture control lever in the full lean position In addition the mixture control has a lock to prevent inadvertent activation of...

Page 150: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II SECTION 7 DESCRIPTION AND OPERATION CONTROL QUADRANT AND CONSOLE Figure 7 5 ISSUED AUGUST 15 1975 REPORT VB 760 7 7...

Page 151: ...n case of failure of the engine driven pump The electric pump should be on for all takeoffs and landings and when switching tanks The pump switch is located in the switch panel above the throttle quad...

Page 152: ...II ElECTRIC fUEl PUMP ENGINE fUEL PUMP CARBURETOR fUEL PRESSURE GAUGE SECTION 7 DESCRIPTION AND OPERATION LEfT MAIN TANK FUEL TANK SELECTOR ALYE RIGHT MAIN TANK ISSUED AUGUST 15 1975 fUEL QUAHTnY GAUG...

Page 153: ...for radio and electrical equipment operation Since the alternator output is available at all times the battery will be charging for a greater percentage of use This will make cold weather starting eas...

Page 154: ...ar continuously under these flight conditions The amount of current shown on the ammeter will teB immediately if the alternator system is operating normally as the amount of current shown should equal...

Page 155: ...CEPTACI E I POWER SOLENOID I I L _______ __ J ALTERNATOR Fa O SA IN LINE WAIIN I IGHT AMMETER PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II 9 f t t t I l I 1 f WEi N j SOUItCE POWER R I AY E...

Page 156: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II ISSUED AUGUST 15 1975 CIRCUIT BREAKER PANEL Figure 7 13 SECTION 7 DESCRIPTION AND OPERATION REPORT VB 760 7 13...

Page 157: ...SECTION 7 DESCRIPTION AND OPERATION PIPER AIRCRAFT CORPORATION PA l8 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFf BLANK REPORT VB 760 7 14 ISSUED AUGUST 15 1975...

Page 158: ...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 light is provided in the annuncia...

Page 159: ...electrically operated A vacuum gauge is mounted on the far right side of the instrument panel A natural separation of the flight group and power group is provided by the placement of the flight group...

Page 160: ...3 r 0 t HH o tI l a III 15 ADF RECEIVER 16 DME RECEIVER 17 ENGINE HOUR METER 11 SUCTION GAUGE 1 g HEAT DEF ROST CONT ROL 20 CIGAR LIGHTER 21 MIKE JACK 22 PHONE JACK 23 AUTOPILOT 24 ENGINE INSTRUMENT C...

Page 161: ...de provides an alternate static source for the system when opened Both the pitot and static lines can be drained through separate drain valves located on the left lower side of the fuselage interior A...

Page 162: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II ISSUED AUGUST 15 1975 PITOT STATIC SYSTEM Figure 7 17 SECI ION7 DESCRIPTION AND OPERATION REPORT VB 760 7 19...

Page 163: ...SECTION 7 DESCRIYfION AND OPERATION PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II REPORT VB 760 7 20 HEATING AND VENTILATING SYSTEM Figure 7 19 I I v I oJ ISSUED AUGUST 15 1975...

Page 164: ...and pilot passenger comfort the front seats are adjustable fore and aft The back of the right front seat contains two latches an outboard latch which allows the seat to be moved forward or aft for eas...

Page 165: ...a small warning hom which is activated between five and ten miles per hour above stall speed Mild airframe buffeting and gentle pitching may also precede the stall Stall speeds are shown on graphs in...

Page 166: ...board of the temperature control is the fan speed switch and the air conditioning ON OFF switch The fan can be operated independently of the air conditioning However it must be on for air conditioner...

Page 167: ...the transmitter has been used in an emergency situation or if accumulated test time exceeds one hour The unit is equipped with a portable antenna to allow the locator to be moved from the airplane in...

Page 168: ...urn the transmitter OFF To activate the transmitter for tests or other reasons move the switch upward to the ON position and leave it in that position as long as transmission is desired 2 On other mod...

Page 169: ...SECTION 7 DESCRIPTION AND OPERATION PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 760 7 26 ISSUED AUGUST 15 1975...

Page 170: ...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 11...

Page 171: ...owners 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...

Page 172: ...SECTION 8 HANDLING SERVICING AND MAINTENANCE PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE LEFT BLANK REPORT VB 760 8 2 ISSUED AUGUST 15 1975...

Page 173: ...he FAA A Progressive 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 the ai...

Page 174: ...er or air taxilco l mercial operations service I All other aircraft maintenance must be accomplished by a person or facility appropriatily certificated by the Federal Aviation Administration FAA to pe...

Page 175: ...nd in the aircraft a To be displayed in the aircraft at all times I Aircraft Airworthiness Certificate Form FAA S 00 2 2 Aircraft Registration Certificate Form FAA S050 3 3 Aircraft Radio Station Lice...

Page 176: ...fifteen feet and a qualified person should ride in the pilot s seat to maintain control by use of the brakes b Taxiing Before attempting to taxi the airplane ground personnel should be instructed and...

Page 177: ...ks 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 l H...

Page 178: ...mage replace it immediately 3 Wipe the filter housing with a clean doth and install the filter The usable Jife of the filter should be restricted to one year or 500 hours whichever comes first c Insta...

Page 179: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II ISSUED AUGUST 13 1975 SECTION 8 HANDLING SERVICING AND MAINTENANCE BRAKE SYSTDI Figure 8 1 REPORT VB 760 8 9...

Page 180: ...ut be extended a minimum of 10 inches the nose gear torque links need not be disconnected Do not allow the strut to extend more than 12 inches When air bubbles cease to flow through the hose compress...

Page 181: ...mended that single or multi viscosity aviation grade oils in accordance with latest issue of Textron Lycoming Service Instruction J014 be used The following seasonal aviation oil grades and seasonal a...

Page 182: ...SECTIONS HANDLING SERVICING AND MAINTENANCE PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK I REPORT VB 760 8 11a ISSUED JUNE 8 1990...

Page 183: ...ade 1001130 fuel The operation of the aircraft is approved with an anti icing additive in the fuel When an anti icing additive is used it must reflect the specification MlL J 27686 must be uniformly b...

Page 184: ...er left corner of the fire wall It is important that the fuel system be drained in the following manner I Open the easy drain valve with the fuel selector valve on one tank and allow fuel to nowfor a...

Page 185: ...of new components it may be necessary to rebalance the wheels with the tires mounted When checking tire pressure examine the tires for wear cuts bruises and slippage 8 25 BATTERY SERVICE Access to the...

Page 186: ...to remain on the gear from five to ten minutes Then rinse the gear with additional solvent and allow to dry 4 Remove the cover from the wheel and remove the catch pan 5 Lubricate the gear in accordan...

Page 187: ...re scratch or mar in plastic can be removed by rubbing OUI the scralch wi th jeweler s rouge Smooth both sides and apply wax e Cleaning Headliner S ide Panels and Seats I Clean headliner side panels a...

Page 188: ...SECTIONS HANDLING SERVICING AND MAINTENANCE PIPER AIRCRAFf CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 760 8 16 ISSUED AUGUST 15 1975...

Page 189: ...NTENTS SECTION 9 SUPPLEMENTS Page No 9 1 General 9 1 I Air Conditioning System Instal1ation 9 3 2 AutoFlite II Autopilot Installation 9 7 3 AutoControl IIIB Autopilot Installation 9 9 4 Piper Electric...

Page 190: ...of 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 a...

Page 191: ...SECTION 9 SUPPLEMENTS REPORT VB 760 9 2 PIPER AIRCRAFI CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE I TENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 192: ...IONS a To insure maximum climb performance the air conditioner must be turned OFF manually prior O takeoff to disengage the compressor and retract the condenser door Also the ai r conditioner must be...

Page 193: ...en 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 to...

Page 194: ...ll throttle position is selected When the full throttle position is not used or in the event of a malfunction which would cause the compressor to operate and the condenser door to be extended a decrea...

Page 195: ...SECTION 9 SUPPLEMENTS REPORT VB 760 9 6 PIPER AIRCRAFr CORPORATION CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 196: ...h on pilot s control wheel b Toggle switch on instrument panel OFF c Unit may be overpowered manually d In climb cruise or descent configuration a malfunction with a 3 second delay in recovery initiat...

Page 197: ...II I Center Turn Command Knob and push IN to engage Tracker 2 Trim Knob push IN for high sensitivity SECTION 5 PERFORMANCE No changes to the basic performance provided by Section 5 of this Pilot s Ope...

Page 198: ...Breaker 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 a climb cruise or descending flight cou...

Page 199: ...yro HDG knob in rotate bug to aircraft heading Push console heading rocker HDG switch to ON position To select a new aircraft heading push D G heading knob IN and rotate in desired direction of turn t...

Page 200: ...PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975 SECTION 9 SUPPLEMENTS REPORT VB 760 9 11...

Page 201: ...SECTION 9 SUPPLEMENTS REPORT VB 760 9 12 PIPER AIRCRAFT CORPORATION PA 28 181 CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFr BLANK ISSUED AUGUST 15 1975...

Page 202: ...er 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 the a...

Page 203: ...SECTION 9 SUPPLEMENTS REPORT VB 760 9 14 PIPER AlRCRAFf CORPORATION PA 28 181 CHEROKEE ARCHER n THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

Page 204: ...Paragraph No TABLE OF CONTENTS SECTION 10 SAFETY TIPS Page No 10 1 General 10 1 10 3 Safety Tips 10 1 REPORT VB 760 lO i...

Page 205: ...s since reflected light can produce spacial disorientation Do not operate strobe lights when taxiing in the vicinity of other aircraft g The rudder pedals are suspended from a torque tube which extend...

Page 206: ...SECTION 10 SAFETY TIPS REPORT VB 760 10 2 PIPER AIRCRAFI CORPORATION PA 28 ltll CHEROKEE ARCHER II THIS PAGE INTENTIONALLY LEFT BLANK ISSUED AUGUST 15 1975...

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Piper Cherokee Archer II, Pilot Operating Handbook

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Summary of Contents for Cherokee Archer II

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