Piper Aircraft Corporation Arrow IV PA-28RT-201 Information Manual Download

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Summary of Contents for Arrow IV PA-28RT-201

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Page 2: ...ARROW IV INFORMATION MANUAL Arrow IV PA 28RT 201 HANDBOOK PART NO 761 730...

Page 3: ...Published by PUR1 ICATIONS D E P A R I MEN 1 Piper Aircraft Corporation Issued September 14 1979 REPORT VB 1130 It...

Page 4: ...ane equipment Revision will be distributed whenever necessary a s complete page rrplacements or additions and shall be inserted into the handbook in accordance with the instruction given below I Hevib...

Page 5: ...he physical location olmaterial on a page will not bc identilicd ORIGINAI PAGES ISSllED The original pagcs issucd lor this handbook prior to rcvi ionarc givc i below Titlc ii through vii 1 1 through 1...

Page 6: ...Relocated itcms 103 and 105 to pg 6 24 Relocated items 103 and 105 from pg 6 23 Revised para 1 3 b Kevised para 1 7 c I 2 Reviscd para 2 7 d 1 2 4 5 2 7 e and 2 7 0 Itevised para 2 9 c Addcd placard...

Page 7: ...ed ilcnls 10 pg 6 33 addcd ilcms from pg 6 3 1 Rclocalcd items l o pg 6 34 addcd items from pg 6 32 I cloc itcd i crns10 pg 6 38 rcnutnbcrcd i c m s added itcnis from pg 633 Rclocated items to pp 6 39...

Page 8: ...6 48 and 6 49 renumbered items added items from pg 6 37 Relocated items to pg 6 50 renumbered items added i ems from pg 6 38 added new items 303 and 305 Relocated iterns to pgs 6 50 and 6 51 renumber...

Page 9: ...g relocated item from pg 6 46 added new iten 411 and 413 Added pg relocated and renumbered items from pg 647 added new item 4 15 Added pg relocated form from pg 6 48 Revised info Revised para 7 15 Rev...

Page 10: ...pgs added Supplemenl 7 ANS 351 Area Navigation Computer Added pgs added Supplemenl 8 Century 21 Autopilot Installation Added pgs added Supplemenl 9 Century 41 Autopilot Installation Added pgs added Su...

Page 11: ...itcrn 223 to pg 6 34 Rclocatcd item 223 from pg 633 Added item 292 Revised items 409 4 1 1 and 413 Rcvised item 4 15 movcd item 429 t o pg 6 57 Rclocatcd item 429 from pg 6 56 Rcvised fig 7 15 Rcvise...

Page 12: ...a 4 21 New pg relocaled para 4 23 from pg 4 19 and 4 20 Moved para 4 23 info to pg 4 19b Addrd note to para 4 29 moved info to pg 4 23 Relocated info from pg 4 22 moved para 4 33 to pg 4 24 Relocated...

Page 13: ...ig 5 31 Revised Table of Contents Revised para 6 1I Reviscd typo Rcvised itcm 299 rnovcd itcrns 307 and 309 to pg 6 43b Ncwpagc Ncw pagc rclocatctl itclns 307 and 309 from pg 643 rcloca editcm 3 1 1 r...

Page 14: ...ised para 4 9 Revised para 4 21 Kevisrd para 4 23 Revised para 4 25 Kcvised para 4 39 Kcvised para 4 4 I Revised example para 5 5 Rrvised fig 5 29 Revised fig 7 1 Revised para 7 1 1 and fig 7 3 ICeloc...

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Page 16: ...PROCEDURES SECTION 4 NORMAL PROCEDLIRES SECTION 5 PERFORMANCE SECTION 6 WEIGHT AND BALANCE SECTION 7 DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS SECTION 8 AIRPLANE HANDLING SERVICING AN...

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Page 18: ...AL Page No Introduction I I Engines 1 3 Propellers 1 3 Fuel 1 4 Oil 1 4 Maximum Weights 1 5 Standard Airplane Weights 1 5 Baggage Space 1 5 Specific Loadings 1 5 Symbols Abbreviations and Terminology...

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Page 20: ...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 fligh...

Page 21: ...RAL PIPER AIRCRAFT CORPORATION PA 28RT 201 ARROW IV Wing Arca sq TI 170 0 Min l urnirlg Radius f l from pivot point 10 wingtip 31 0 V 4 n 5 n J TliHEE VIEW F i g u r e 1 1 REPORT VB I130 1 2 ISSUED SE...

Page 22: ...1 5 PROPELLERS McCAULEY a Number of Propellers b Propeller Manufacturer c Blade Model d Number of Blades e Hub Model 0 Propcller Diameter in I Maximum 2 Minimum g Propeller Type ISSUED SEPTEMBER 14 1...

Page 23: ...Usable Fuel U S gal total c Fuel I Minimum Grade 2 Alternate Fuels 1 9 OIL a Oil Capacity U S qts b Oil Specification c Oil Viscosity REPORT VB 1130 1 4 100 Green or 100IdL Blue Aviation Grade Refer...

Page 24: ...num anding Weight Ibs c Maxiniu nW r i g h s in Ili ggage Ctrnlpartnicnt I clc l o 1 1gc11e6 5 lor tllr Standard Empty Weight and the Uselul I o rd I I l l p a r t n l c t Volunie cu it h lirltry W d...

Page 25: ...und Speed i s thc speed of an airplnr c relative to the ground Indicated Airspeed is thc specd of an aircraft as shown on the airspeed indicator when corrected for instrument error IAS values publishe...

Page 26: ...VNO Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air and then only with caution Stalling Speed or the minimum steady flight speed at which the airplane...

Page 27: ...meteorological sources adjustcd for instrument crror and co prcccihilily eCfccts Indicated Pressure The numbcr actually read from an Altitude altimeter when thc barometric su bsc le has beer1 sct to 2...

Page 28: ...mb to the horizontal distance traversed in the same time interval Demonstrated The demonstrated crosswind velocity is the Crosswind velocity of the crosswi d component for Velocity which adequate cont...

Page 29: ...cing the number of digits Center of Gravity The point at which an airplane would C G balance if suspended Its distance from the reference datum is found by dividing the total moment by the total weigh...

Page 30: ...tional equipment Weight of occupants cargo and baggage Difference between takeoff wcighl or ramp weight if applicable and basicempty weight Maximum weight approved for ground maneuver It includes weig...

Page 31: ...hermal Unit RTU centimctcrs cm centimctcrs of mercury at 0 C cm Hg centimeters per second cnii sec cubic centin eters cm REPORT VB 1130 1 12 T O O B 1 AIN ha sq ft sq rnl CIII He in l l g bar kg cn1 I...

Page 32: ...c feet per minute cu ft 1niin cub cinchrs cu in cmJ m 3 cu It n OZ 1 U S gal U S qt cubic meters mJ cu in cu yd cu ft U S gal cubic nlrters prr minute ml min cu ft min cubic yards cu yd cu ft m 3 U S...

Page 33: ...t 1 sec foot pounds ft lb foot pounds per minute ft lb min foot pounds per second It lb scc gallons Imperial In perial gal gallons 1J S dry U S gnl dry REPORT VB 1130 1 14 TO OBTAIN in yd rod ml N M m...

Page 34: ...eter slcm grams per cubic centimeter g crn3 hectares ha horsepower hp horsepower metric inches in ISSUED SEPTEMBER 14 1979 cu in cu ft cu yd cm3 m3 I Imperial gal n oz 0 00 1 kg 0 3527 oz avdp 2 205 x...

Page 35: ...nch pounds in lb kilograms kg m kg Ib 02 avdp g kilogram calories kg cal BTU ft lb m kg kilograms per cubic meter kg m3 Ib cu ft g cmJ kilograms per hectare kg ha kilograms per square centimeter kglcr...

Page 36: ...er kilogram m kg meters per minute m min ft sec R min kt mph m sec m min nautical mph ft sec statute mph km hr m sec 1000 cmj 61 02 cu in 0 0353 I cu rt 33 814 fl 02 0 264172 U S gal 0 2200 Imperial g...

Page 37: ...crons miles statute mi in ft k m m NM miles per hour mph cmlsec mlsec ft sec ft min km hr kt nliles per hour square m hr sq ft sec sq rnilli bars in Hg in in Hg millimeters mm millimeters of mercury a...

Page 38: ...es fluid per acre fl oz acre pounds Ib kg g slug pounds per acre lb acre pounds per cubic foot 1b l cu ft pounds per cubic inch Ib 1cu in Ib cu ft g cm3 in Hg kg m2 atm pounds per square foot Ib sq ft...

Page 39: ...rpm or rev miri revolutior s per second rev sec rod slug square centimeters cm2 square feet sq ft square inches sq in square kilometers km2 square meters mZ REPORT VB 1130 1 20 T O OBTAIN deg sec rev...

Page 40: ...ROW IV GENERAL MULTIPLY BY T O OBTAIN square miles sq mi 2 590 640 km2 acres square rods sq rods 30 25 sq yd square yards sq yd 0 8361 m2 9 sq ft 0 0330579 sq rods yards yd ISSUED SEPTEMBER 14 1979 0...

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Page 42: ...irspeed Indicator Markings 2 2 flower Plant l in itations 2 3 Power Plant lnstrurnent Markings 2 4 Weight Limits 2 4 C c n c r of Gravtty 1 imits 2 5 Maneuver Limits 2 5 Flight Load Factors 2 6 l ypes...

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Page 44: ...tems and equipment which require handbook supplements can be found in Section 9 Sirpplemel ts 2 3 AIRSPEED 1 IMITATIONS S P E E D KlAS KCAS Never Exceed Speed VNE Do not exceed this speed in any opera...

Page 45: ...08 I04 Maximum Landing Gear Extcnsion Spccd D o not excced this spccd when extending thc lariding gcar 130 130 Maxinlurn Lariding Gear Retraction Spccd 110 not excced this spcetl whcn retracting the l...

Page 46: ...0 e Oil Pressure Minimum red line 25 PSI Maximum red line 100 PSI I Fuel Pressure Minimum red line 14 PSI Maximum red line 45 PSI g Fuel minimum octane 100 or IOOLL Aviation Grade h Number of Propelle...

Page 47: ...ccn Arc No1n1 iI 0pc1 iti1ig1 11igc l c l I iuc bla x i i i i c Oil I ICTS IIC ICCI Arc No11ii 11 Opc ili ig 1 11igc Yellow Arc 1111io1i l i igc ldlc Ycllo A1 c ro1111tI V II 111 Ilp Itctl I i ic M i...

Page 48: ...en points given The datum used is 78 4 inches ahead of the wing leading edge at the intersection of the straight and tapered section It is the responsibility of theairplane owner and the pilot to insu...

Page 49: ...or F A R 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 2 5 gallo...

Page 50: ...able or unacceptable for operation at into or out of any airport The above statement otwitl sta lding the noise level stated above has been verified by and approved by the Federal Aviation Administrat...

Page 51: ...he pilot TAKEOFF CHECK LIST Fuel on Proper Tank Fasten Belts Harness Electric Fuel Pump On Flaps Set Engine Gauges Checked Trim Tab Set Alternate Air Closed Controls Frce Seat Backs Erect Doors Latche...

Page 52: ...ver aircraft equipped with backup gear extender I OVEKRI IE ENGAGED AUTO EXT OFF LOCK I IN O N S I D E T O E N G A G E OVERRIDE I ULl LEVER F U L L UP PUSH LOCK PIN T O RELEASE OVERRIDE 1 111 1 1 EVER...

Page 53: ...n inside of baggage cornpart rle lt door BAGGAGE MAXIMUM 200 LBS SEE WEIGIITAND BALANCE DATA FOR BAGGAGE LOADING BETWEEN 150 LBS AND 200 LBS Adjacent to fuel tank filler caps FUEL 100 OR IO0L L AVIAT...

Page 54: ...E M O X WIND 17 KTS V1 0 130 IN 109 111 V i 130 MAX 130 M A X In full v c w of pilot 0 1 1 COOL EK WINT EKIZATION PLATE TO BE R E M O V E D W l l E N A M B I E N T T E M P E R A T U R E EXCEEDS 50 F O...

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Page 56: ...r 3 9 Engine I owcr I oss Dtrring I akeofl 3 9 i11g111r I owrr 1 03s In t ligll 3 10 I owrr Off Landing 3 11 I irc 111 Flight 3 13 I 055 nl Oil i1rc5 ure 3 14 I oss of Fuel I rcss rte 3 15 lligh 011 T...

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Page 58: ...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 condition d...

Page 59: ...n and land straight ahead If area ahead is rough or if it is rlcccssary to clear obstructions Gear selector switch U I IEmergency gcar lever nircrnf cquippcd will1 backup gcar cxtcndcr latcl cdi r OVE...

Page 60: ...aircraft equipped with the backup gear extender lock emergcncy gear lever in OVERRIDE ENGAGED position before airspeed drops to 105 K IAS to prevent the landing gear from free falling 1 rim for 79 KIA...

Page 61: ...c airspeed FIRE IN FLIGIIT Source of fire clrcch Electrical fire smoke in cahin Master switch 01 F Vcnts opcrl Cabin heat 01 1 Land as soon as practicable Er pirre fire Fuel selector O1 1 Tl rottlc CI...

Page 62: ...required AI I swltch ON If puwcr not restored A1 T switch OFF 11 altrrnator output cannot bc restored reduce electrical loads and land as w o n as prac ical The battery is h r only rrniaining source o...

Page 63: ...n required by an electrical system failrrre If alternator loads are not reduced A L T switch 01 1 BAT switch as required Imr das soorl as possible Anticipate colnplctc electrical failure NO1E If the b...

Page 64: ...s still failed to lock down yaw the airplane abruptly from side to side with the rudder If tile nose gear will not lock down using the above proccdure slow the aircraft to the lowest safe speed attai...

Page 65: ...c door vill trail slightly open and iil spcctls illbc rctluccd slightly TO close the duor ill Ilipl t Slow airplarlc to 87 kl S Cabin vcnts close Storm vi lrln v O C I I If uppcr latch i s npcn I l rl...

Page 66: ...o the engine If the engine has started continue operating to try to pull the fire into the engine In rit hcr case above if fire continues more than a few seconds the fire should be extinguished by the...

Page 67: ...ed with thc Power Off Landing procedure refer to the emergency check list and Paragraph 3 13 3 11 ENGINE POWER 1 OSS IN FI IGHT Complete engine power loss i s usually caused by fuel flow interruption...

Page 68: ...105 KIAS to prevent the landing gear from inadvertently free falling on aircraft equipped with the backup gear extender Trim the aircraft for best gliding angle 79 KIAS Air Cond of0 and look for a sui...

Page 69: ...cr in thc OVERRIDE ENGAGED position before the airspeed drops to 105 KIAS to prevent tllc landing gcar from inadvertantly frce falling Touchdown sliould normally bc made at the lowcst possible airspee...

Page 70: ...instrument readings cliaracter of the smoke or other indications since the action to be taken differs somewhat in each case Check lor the source o l the fire first IIan electrical fire is indicated s...

Page 71: ...cither case proceed toward t l c rle lrcht airport and be prepared for a forced landing If the proble nis riot a pressure gauge rnalfunctio i the erigine may stop sudderilp Mairit i l altitude until s...

Page 72: ...echanic invest gale the problem Watch the oil prehsllrc gauge for a n accon panyir g loss of pressure 1 055 of ltrrni tor output is detected through zero reading on the arrlrllrtcr Ilcfore cxccuting t...

Page 73: ...lc 1lA l s vitcl OI F alld tllc arl lllctcrsllo lltldccrcasc Ilrrll IIC I j A I sw1fcl1 O N and c o r l t i r l e to n o r i o r the Irnlncter I f tllc altcrn ltor Lr pLr1tlocs 1101 decrease withill 5...

Page 74: ...NCY DOWN position If the gear has still failed to lock down yaw the airplane abruptly from side to side with the rudder I f the nosc gear will not lock down using the above procedure slow the airplane...

Page 75: ...l haidle to the latched position I f both latches are open close the side latch t len tllc top latch 3 33 ENGINE HOUCIINESS Engine rougl nessnlny be cnused by dirt in tlre il jcctori o l c s i r l d c...

Page 76: ...crlcral 4 12 I refligl t Chcch 4 12 Hciorc Starting lingrlrr 4 14a S a r n g Engine 4 15 Warm up 4 17 I rxrrng 4 17 iround Check 4 18 Ikiorc I akeofl 4 19 Takeoll 4 19b Climb 4 20 C r i s i n g 4 21 A...

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Page 78: ...iarize themselves with the procedures given in this xction in order to become proficient in the normal operations of the airplane h e first portion of this section consists ofa short formcheck list wh...

Page 79: ...mospheric condi ions and piloting technique a Rest Rate of Climb Spced gear up flaps up 87 KIAS gear down flaps up 76 KlAS b Ikst Anplc o l Climb Spccd gcar up Ilaps up 77 KlAS gear down flaps up 70 K...

Page 80: ...el release restraints Avionics OFF Parking brake set All switches OFF Mixture idle cut off Master switch ON F iel gaugcs check quantity Annunciator panel check Master switch OFF Primary flight control...

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Page 83: ...hrottle adjust Oil pressure check STARTING ENGINE WtIEN HOT Throttle 12 opcn Master switch ON Electric fuel pump ON Mixture idle cut ofC Starler engage Mixture advance Throttle adjust Oil pressure cl...

Page 84: ...est possible RPM External power plug disconnect from fuselage Master switch O N check ammeter Oil pressure check WARM UP Throttle 1400 to 1500 RPM TAXIING Chocks removed Taxi area clear Throttle apply...

Page 85: ...Electric fucl pump OFt Fucl prcssurc cllcck Ihrottlc rctnrd Master s vitcll ON Fligl l instrunients rl r c k Fuel selector proper tank Elcctric fucl pump O N Enginc gauges cl cck A I a I OSlil Prop s...

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Page 87: ...Belts ha rncss Casrc ltl j t r s r Elcctric Cucl pump ON Mixlurc 5ct Propeller 5c1 Gear down 130 K I A S Illax Flaps scl 108 K I A S I I I Air conditioner OIKl Trim to 75 KIAS STOPPING ENGINE Flaps rc...

Page 88: ...PIPER AIRCRAFT CORPORATION SECTION 4 PA 28HT 201 ARROW I V NORMAL PROCEDURES TtlIS PAGE INTENTIONALLY LEFT BLANK ISSUED SEPTEMBER 14 1979 REPOHT VB 1130 4 11...

Page 89: ...ring the control wheel turn O F F all avionics equipment and set the parking brake Insure that all electrical switches and the magneto switch arc O F F a n d the mixture is in idle cut off Turn ON the...

Page 90: ...a normal static load Check the tire forcuts wear and proper inflation Make a visual check of the brake block and disc Check that the fresh air inlet is clear of foreign matter NOSE SECTION Check the g...

Page 91: ...d operational interference and that thestatic wicks are firmly attached and in good condition FUSELAGE Check the condition and security of the antennas The empennage should be clear of ice frost snow...

Page 92: ...oper accessi bility to all controls includi lgfurl selrctor flaps tr1111 CIC while ma ntail inp adequate rrstralnl lor the occupdrtt If thc rtrrtiar r r l typr shoulder harnrss is installrd a pull tes...

Page 93: ...Sl l lON 4 l ll l lt A l l t ItAl 1 Olt l Olt I ION N O K h l Al 1 HOC L UHk S 1 A Z8H I ZOI AHRO V I I HIS AGE I N 1 E N I IONAI I Y I FfTI 111 A N K REPORT VB 1130 1 4 l4b...

Page 94: ...t hin five to ten seconds disengage tltc btarter and reprime b Starting Engine When tfot Open the throttle approximately 112 inch Turn ON the master bwitch and the electric fuel pump Move the mixture...

Page 95: ...sconnect the jumpcr cable from the aircraft Turn the master switch ON and chcck the alternator ammeter lor an indication of output 110 NOI ATTEMPT FLIGHT I F THERE IS NO INDICA7 ION OF ALTERNATOR OUTP...

Page 96: ...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 17 TAXIING Before attempting to taxi the airplane groun...

Page 97: ...full INCI ISASE r p r IOI takcoff 70 o b t a i maximum rpm pus11tllc pcdcstal n o t c d cor lrol f111Il forward on tllc instrument pancl D o not allow n d o p of r r rc t l i a 500 RPM during this cl...

Page 98: ...h is placed in the UP position Care should always be taken not to retract the gear prematurely or the aircraft could settle back onto the runway If the override lock is used for takeoff it should be d...

Page 99: ...t for the occupant I f the incrtia recl typc shouldcr harncss is installcd a pull test o l its locking restraint feature sl ould be performed I he mixture and propcller control leversshould be sct and...

Page 100: ...aft to climb attitude After breaking ground accelerate to 55 to 65 KIAS depending on aircraft weight and select gear up Continue to climb while accelerating to the flaps up rate of climb speed 87 KlAS...

Page 101: ...nded This incrcascd climb speed provides better engine cooling less engine wear reduced Cucl consumption lower cabin noise level and better forward visibility When reaching the desired altitude the el...

Page 102: ...ndicating that the lean mixture limit has been reached in the leanercylinders Then enrich the mixture by pushing the control towards the instrument panel until engine operation becomes smooth The fucl...

Page 103: ...fucl p u m p s l o u l d bc normally 01 1 so rliat III malfuncrion o f tllc cngirrc drivcn ftrcl pump is imnicdiatcly app rcnt 1fsig11s or fucl s arvation should occur lt any i n l c during Clight Cu...

Page 104: ...ectric fuel pump ON Reduce the speed during the flarcout and contact the ground close to the sralling speed After ground contact hold the nose wheel off as long as possible As the airplane slows down...

Page 105: ...ting and gentle pitching may also precede the stall l l e gross wcigl t stalling spced of the Arrow IV with powcr offa ld rull llaps is 53 KIAS With the flaps up this spced i s ir crcased 6 K TS Loss...

Page 106: ...unction and significance of the landing gear position indicators and warning lights l h e red gear warning ligh on the instrument panel and the horn operate simirltaneously in flight when the throttle...

Page 107: ...purposes the following changes must be made to the procedure to prevent the hydraulic pump frori activating during the procedure On aircraft equipped with the backup pcar extender the landing gear se...

Page 108: ...NTS SECTION 5 PERFORMANCE Paragraph No Page No 5 1 General 5 1 5 3 lnlroduction Performance and Flight Planning 5 1 5 5 Flight Planning Example 5 3 5 7 Performance Graphs 5 9 List of Figures 5 9 REPOR...

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Page 110: ...lc lly expanded for the various parameters of weight altitude IclllpcratLIrc ctc II I C perfornlancc charts are unfactored and do not make any allowance for v ryingdegrees of pilot proficiency or mech...

Page 111: ...detailed flight plan using the performance charts in this section Each chart includes its own example to show how it is used WARNINC P e r f o r m a n c e i n f o r m a t i o n derived by extrapolati...

Page 112: ...se the Weight and Balance Loading Form Figure 6 1 1 and the C G Range and Weight graph Figure 6 15 to determine the total weight of the airplane and the center of gravity position Use the information...

Page 113: ...ion airport and when established the landing weight The conditions and calculations for the example flight are listed below The takeoff and landing distances required for the example flight a r e belo...

Page 114: ...the flight plan corrected for field pressure altitude and temperature The following values were determined from the above instruc tions in our flight planning example I Cruise Pressure Altitude 6000 f...

Page 115: ...the Power Settirlg I able Figure 5 21 when selecting the cruisc powcr setting I Ilc established pressure altitude and temperature values and tile selected cruisc Dower should now be utili7cd to dctcr...

Page 116: ...g them to the cruise time The following flight time is required for the flight planning 1 example I Total Flight fime c 3 plus I plus eI 6 0 13 hrs plus 0 07 hrs plus 0 86 hrs 8 min plus 4 min plus 52...

Page 117: ...SECTION 5 PERFORMANCE I II EH AIRCRAFT CORI OHATION PA 28RT 201 A R R O W I V THIS PAGE INTENTlONA1 LY LEFT DLANK REPORT VB 1130 5 8 ISSUED SEPTEMBER 14 1979...

Page 118: ...ce car Down Climb Performance Furl Time and Distance to Cllmb I owcr Setting 1able Speed Power Performance Cruise Speed Power Economy Cruise Best I ower Range ISA Best I ower Range Non Standard Temper...

Page 119: ...SECTION 5 Pll ER AIR I AI T CORI ORA I ION PERFORMANCE PA 28RT 204 ARROIV IV TtllS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1130 5 10...

Page 120: ...PIPER AIRCRAFT CORPORATION SECTION 5 PA 28RT 201 ARROW 1V PERFORMANCE FAHRENHEIT DEGREES CELSIUS DEGREES TEMPERATURE CONVERSION Figure 5 1 ISSUED SEPTEMBER 14 1979 REPORT VB 1130 5 11...

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Page 123: ...0 Ibs AND FULL THROTTLE BEFO Surface wind 4 kts headwind Lift on speed 5 7 KlAS Speed at 5 0 ft 6 0 KlAS akeoii distance 1675 ft C 3ooo L I W 0 2500 5 2 0 L 2000 W Y 4 I 1500 loo0 40 20 0 20 40 2800 2...

Page 124: ...OUTSIDE AIR TEMPERATURE C WEIGHT POUNDS WIND COMPONENT KNOTS...

Page 125: ...OUTSIDE AIR TEMPERATURE C Xlz WEIGHT POUNDS W I N D COMPONENT KNOTS I 0...

Page 126: ...OUTSIDE AIR TEMPERATURE C WEIGHT POUNDS W I N D COMPONENT KNOTS...

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Page 128: ...0 R P M FULL THROlTLE MIXTURE FULL RICH GEAR D O W N FLAPS RETRACTED CLIMB SPEED 7 6 KlAS GROSS WEIGHT 2760 LBS I f i l i I I I j Example w b b i 7 Cltmb pressure altllude 6000 fi I j Outsde air tempe...

Page 129: ...M FULL T H R O I T L E M I X T U R E F U U R I C H G R O S S W E I G H T 4 0 3 0 ZO 1 0 0 1 0 2 0 3 0 4 0 0 10 2 0 3 0 M 5 0 6 0 7 0 8 0 O U T S I D E AIR TEMPERATURE C FUEL T l M E A N D D I S T A N...

Page 130: ...10000 5 F T 1 18 8 10000 l 1000 7 18 5 1 lo00 12000 9 18 2 12000 13000 I I 17 8 13000 14000 13 17 5 14000 T O maintain constant power corrcct manifold prcssurc approxirnatcly 0 16 H g f o r each 10 F...

Page 131: ...SECTION 5 I II EK Allt KAl T CUltPOltA LlON PERFORMANCE PA 28RT 201 ARROW I V THIS PAGE INTENTIONALzLY LEF1 BLANK R EI OH I VR 1 130 5 22...

Page 132: ...ude lmpe MK O rature...

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Page 134: ...Cru se oms de slr tempsrsture 3 C Range 776 u t mi with rsrarve 850 u t mi wnhom reserve RANGE NAUTICAL MILES INCLUDES CLIMB DESCENT DISTANCES...

Page 135: ...vc At 55 Powcr v o 2 k wl 1 fl U o wl o s fl Poucr Power 75 65 654 709 666 720 678 731 690 748 752 762 671 726 683 737 695 748 707 759 769 780 A 701 756 714 767 726 778 729 789 800 810 715 769 728 781...

Page 136: ...RANGE NALlTlCAL MILES INCLUDES C U M B DESCENT DISTANCE...

Page 137: ...Pressure Outside 45 Min Reserve No Reserve Altitude Air Temp At 55 Power Feet C Power Power 75 65 55 75 65 55 BEST ECONOMY RANGE NAIJTICALMI1 ES NON STANDARD TEMPERATURE EXPANSIOYJ IIARI Figure 5 33...

Page 138: ...X T U R E L E A N E D T O P E A K E G T t A GEAR UP FLAPS U P 72 GAL U S E A B L E FUEL C r u s e pressure alr rude 6000 f l 10000 8000 6000 E N D U R A N C E H O U R S I I N C L U D E S T I M E T O C...

Page 139: ...e u 6 01 l w n e u 8 v L S 1 puaasap 01 aauelsla v 1 uiw 2 snulw u w g p u a s a p 01 a w l 1 1e6 s snulw le6 s 1 puaasap 01 l a n j OZ a n l e a a w a l Jie ap slno u o e u s a a 4 0 0 6 L apnlille a...

Page 140: ...3 3 N V l S I O O 3 W 1 1 3 0 1 1 9 3 3 t l n l t l 3 d 3 1 M I V 3 0 1 5 l n 0 0 1 OC OL 0 L 0 0 1 0 c 0 2 OL 0 OL 02 OC 0 1 o w tneu 5 g I 1 w i n e u U I W 5 p...

Page 141: ...OUTSIDE AIR TEMPERATURE C WEIGHT POUNDS W I N D C O M P O N E N T 1 Cr 1 n I S I 2 I KNOTS 7 C Cr 1 2 X 2 1 e z...

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Page 144: ...E Paragraph No 6 1 General 6 1 6 3 Airplane Weighing Procedure 6 2 6 5 Weight and Balance Data and Record 6 5 6 7 Weigh1 and Balance Derermina ionTor Fligllt 6 9 6 9 Instructions Tor Using the Weigh1...

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Page 146: ...erformance i t will lave Center of gravity is a determining factor in flight cliarac eristics I f the C G is too far forward in any airplane it may bc difficult to rntatc for takeoff or landing I f th...

Page 147: ...e that the useful load includes usable fuel baggage cargo and passengers Following this is the metl od for con puting takeoff weight and C G 6 3 AIRPI ANE WEICIIING P R O C E D U R E At the time of de...

Page 148: ...osition and all control surfaces in the neutral position Tow bar should be in the proper location and a l l entrarlce and baggage doors closed 6 Weigh the airplane inside a closed building l o preveri...

Page 149: ...EIGtIING FORM Figure 6 I d Basic Empty Weight Center of Gravity I Tile following geometry applies to the PA 28RT 201 airplane when it is level Refer to Leveling paragraph 6 3 b Wing l eadi11g Iltlgt I...

Page 150: ...re 6 5 are for the airplane as delivered from the factory These figures apply only to the specific airplane serial number and registration number shown The basic empty weight of the airplane as delive...

Page 151: ...denlpty weight includes full oil capacity and 5 0 gallons of llllll lt lc IICI AIRI I ANE IJSEFIJI I OAD NORh IAI CAI EGORY OPERATION Gross Weight Basic Empty Weigllt Useful Load 2750 Ibs Ibs Ibs IIII...

Page 152: ...WEIGIIT AND BALANCE RECORD Figure 6 7 ISSUED SEPTEMBER 14 1979 R E P O I T vn 11 30 6 7...

Page 153: ...SECTION 6 I IPER AIRCRAFT CORPORATION WEI II r AN11 BALANCE I A 28HT 201 A R R O W 1V VI I II I ANL C AI ANCE ItE ORl colil 1 igurc 6 7 co111 REI OH I VB 1I30 ISSlJEL S E P T E M B E R 14 1979 6 8...

Page 154: ...envelope the loading meets the weight and balance requirements Arm Aft Weight Datt nl Moment I bs Inches In L bs Basic Empty Weight Pilot and Front Passenger 340 0 80 5 27370 Passengers Rear Seats 340...

Page 155: ...ion of 1 allcling Gear Total 1 oaded Airplane I otals rriust be within approved weight and C G limits I t is l l e responsi b i l i y o l tile airpla le owner and tile pilot to insurethat the airplane...

Page 156: ......

Page 157: ...SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT A N D BALANCE PA 28RT 201 ARROW IV WEIGHT VS C G ENVELOPE REPORT VB 1130 6 I2 ISSUED SEPTEMBER 14 1979 REVISED SEPTFblRER 5 1980...

Page 158: ...or in the baggage cornpartnients Brief instructions are given on the plotter itself 7 0 use it first plot a point on the grid to locate the basic weight and C G location This can be put on more or les...

Page 159: ...in the sale envelope a Place a dot on the plotter grid at 1600 pounds and 88 00 to represent the basic airplane See illustration b Slide the slotted plastic into position so that the dot is under the...

Page 160: ...PIPER AIRCRAFT CORPOHATION Sk fION 6 PA 28RT 201 ARROW IV WEIGIIT AND BAI ANCE WEIGHT VS C G ENVELOPE ISSUED SEPTEMBER 5 1980 REPORT VB 1130 6 1 2...

Page 161: ...SECTION 6 PIPER AIRCRAFT CORPORATION WElGliT AND BALANCE PA 28RT 201 ARROW IV REPORT VB 1130 L V7 l ISSlIFr SEPTEMBER 5 1980...

Page 162: ...m 7 3 Engine Corltrols 7 5 Landing Gear 7 4 Flight Controls 7 11 Fuel System 7 12 Electrical System 7 15 Vacuum System 7 18 Pitot Static System 7 19 Instrument Panel 7 22 Cabin Features 7 23 Baggagc A...

Page 163: ......

Page 164: ...A cargo door is installed aft of the rear scat The wing is of a conventional design semi tapcred and e ilploysa laminar flow NACA 652415 airfoil section l he main spar is located at approximately 40 o...

Page 165: ...I periocl he owner l r c r l t l c11cc L 111c I IIC I l y u o r i r g SCI VICC III IIUCI UII 111009 a1 I1i5 Piper tlc lcr 10i IIIC1 1 1 5 1IC L OIIIIIICII L over Iti1 11 pc 1iocl III I lor I I I addi1...

Page 166: ...meters fuel flow proportionally with airflow and maintains the mixture as manually set for all engine speeds The fuel flow divider receives metered fuel and distributes fuel toeach cylinder fuel nozz...

Page 167: ...SECTION 7 PIPER AIRCRAFT CORPORATION DESCRIFTION OPERATION PA 28RT 201 ARROW IV CONTROL QUADRANT AND CONSOLE Figure 7 1 REPORT VB 1130 7 6 ISSUED SEPTEMBER 14 1979 REVISEI JANUARY 31 1987...

Page 168: ...lo warn of an inadvertent gear up landing The propeller control lever is used to adjust the propeller speed from high RPM to low RPM The mixture control levcr is used to adjust the air to fuel ratio...

Page 169: ...e sr11si11gd e v c e in the systern w t i c l lowcls tllc gcal egardlcs o f gear clcctor position depending u p o n airsprrd i r l t l e g i r e power propeller slip trra l ear cxtenbior is dcslg lcd...

Page 170: ...ovcrride lever in the up position The lock is locatcd on tlie left side pallel ol the console below the level of the manual override Icvcr 1 0 lock tlic override lever in the up position raise the ov...

Page 171: ...I IIII C it1 cot tras to tllc t 111 w rnir g horn w l i c l ctnits a C IIII II I IIS hourrd IIlc IIOW gear is stcerable t l r o u g l a 30 degree arc each side of cer ter thro tgll 1he use o f t Ile r...

Page 172: ...KED POSIIION WITH s i f l u l s COMPRFSSED 8110 THROTTLE CLOSED 7 LIGHT LEGENO f l R E D L I G I I I I Y E L L O W L1GHl G GflEENLIGW1 W WIIITE LlGllT YO NORULLLT OPE 9 A l R c e n r l EOU PFCO 1 1 8...

Page 173: ...PUMP RESERVOIR flllfR 6118 UP CHICK HOTL I AIRCRAFT LQUlPPEO WITH BACKUP CEAR EXTEMOtR NOTE 2 AUTOMAllC GEAR OOWH AEFLAEHCL IS FOR AIRCRAFT LOUIPPEO WlTll BACKUP CEAR EXTEHOtR LANDING GEAR HYDRAULIC S...

Page 174: ...s the dual function of providing trimcontrol and pitch control forces The trirn function is controlled by a trim control wheel located on the control console bctwecn tlie two front seats Figurc 7 9 Ro...

Page 175: ...vo 111cl t rlrlrs o l c i l l c c l wing col t riniilg 38 5 I1 S iallolis givinga total c p c i y 01 77 gallorls ol wliicl 72 galloris irre us hlc Ilacli I I I is ciluippctl villi I I iIlcr icck ilid...

Page 176: ...T 201 ARROW IV DESCRIPTION OPERATION r N f l PRESSURE W 6 E 1UEl ilOW 6AU6i n t 61Ht DRIVtH N t L PUYP 3 4 ELtCTIIC i U t l PUYP y SUPPLYkH0 Lltit ORAM a d fIRtWAlL FUEL SYSTEM SCHEMATIC Figure 7 11 I...

Page 177: ...e tank which is supplyingfuel to theengine The valve also incorporates a safety latch which prevents inadvertently selecting the OFF position Normally fuel is supplied t o the engine through a n engin...

Page 178: ...ld check and monitor the applicable system gauge to determine when or if any necessary action is required Optional electrical accessories include navigation anti collision landing instrument and cabin...

Page 179: ...SECTION 7 PIPER AIRCRAFT CORPORATION DESCRIPTION OPERATION PA 28RT 201 ARROW IV ALTERNATOR AND STARTER SCHEMATIC Figure 7 15 REPORT VB 1130 7 1 6 ISSUED SEPTEMBER 14 1979 p l c r r r qr nrrr 7 fnrb...

Page 180: ...Strobe liglits shoultl not be s c t l in close proxilliity to tlic grou id s c l i as tlrtririg tirxiing takeoff or lalitling On airplanes with interlocked RA l and A1 T switclics the A1 T switch is m...

Page 181: ...I r c l i o l i r g properly Solenoids provided in the battery and starter circuits are used to control 11igl1 cllrrcnt d r i f c t i o n s rer lotelyTr ol the ci hill l l cvaculrrn syslem i s design...

Page 182: ...fl wing A n optioli ll Ilci Icd pilot Ilca l wllicli l l c v t c p o l l c r s wit11 icing or Ilcnvy rain is nvnilnhlc I Ilc s w i c l l for p i o 11c lt is Iocntctl OII t l c s w i l c l p ncl I II I...

Page 183: ...ERATION PA 28RT 201 ARROW IV 1 A1 IIMETEH 2 VEHTlC4L SPEED INDl AlOR 3 4lfl5PtEU INDICPIOH 4 P I I O I S l A l l C I l t P D b I I E A l t D I I O I 5 W I I I It IUPIIONALI 6 A1 IkIINAlk 5 1 4 1 1 O...

Page 184: ...1 16 TRANSPONDER 30 CLUSTER GAUGES 17 ADF 3 1 T A C H O M m R 18 CLIMATE CONTROL AREA 32 GEAR SELECTOR SWITCH 19 VACUUM GAUGE 33 GEAR INDICATOR LIGHTS 2 0 CIGAR UGHTER 34 CONTROL QUADRANT 21 MIKE JAC...

Page 185: ...11eradios are located in the center section of the panel and the circuit breakers are in the lower right corller ofthe panel An optional radio master switch is located near the top of the instr rrnent...

Page 186: ...sms which must be released before the rear seats can be removed Releasing the retainers is accon plishedby depressing the pIunger behind each rear leg Optional headrests reavailable A single strap adj...

Page 187: ...ous pockets o n the rear ofthe front seat backs armrests for the front occupants cabin or baggagc door locks and ignition lock The cabin door is double latched T o close the cabin door hold the door c...

Page 188: ...R INLET 3 FRESH AIR BLOWER 4 BULKHEAD ASSEMBLY 5 FRESH AIR DUCT 6 CABIN EXHAUST OUTLET 7 CABIN VENT 8 CONTROL PANEL 3 DEFROSTER CONTROL LINE 10 HEATER CONTROL LINE 1 1 CABIN HEAT DIVERSION CONTROL 12...

Page 189: ...erature of the cabin is regulated by the heater control located on the right side of the instrument panel Defrosting is accomplished by heat outlets located on the right and left side of the cowl cove...

Page 190: ...ccnnnnty si7c rprny cans of touch up paint are available from Pipcr 1 calcrs Arl op iorinl polyurethane finish i s available I 7 35 AIR CONDITIONING The air conditioning system is a recirculating air...

Page 191: ...IIIsuitcl i llowsopcr tio l of ttlc I I I will the air C U I I I I I I I C I U I 11cd 01 1 to 21d i l l ei bi r air circulation 1 0Ww or IIIGll call be selected to direct a flow oT air tl rorrght l e...

Page 192: ...t date is marked OII tllc trar sn ittcr II ct1111l1ly with F A A regulations the battery must he rcplaccd 011or bcforc t l i s d ltc The battery must also bc replaced i f tllc transmitter llas hccn r...

Page 193: ...1 arld tlren movirrg the switclr to At hl A pilot s rcnlotr switcl located orr the left side parrrl is provided to allow the transrnltter to be turned on from inside tlre cabin The pilot s rrnrotc swi...

Page 194: ...e Inspection Periods 8 2 Preventive Maintenance 8 3 Airplane Allerations 8 4 Ground Handling 8 5 Engine Air Filter 8 8 Rrake Service 8 8 Landing Gear Service 8 10 Propeller Service 8 11 Oil Requiremen...

Page 195: ......

Page 196: ...rvice Bulletins Scrvice Letters and Servicc Spares 1 etters relating to the aircraft Servicc Bulletins are of special importanccandsllor ld hc complied with promptly I hcsc are scnt to the latest rtgi...

Page 197: ...ued it is sell1 by the I AA to the latest registered owner of the affected aircraft and also to subscribers of their service The owrier should periodically check with his Piper dealer or A P l e c l a...

Page 198: ...internal condition of the engine For this system to be accurate oil sa nplcs must be sent in at regular intcrvals and induction air filters must hc cleanetl or changed regularly 8 5 PREVENTIVE MAINTE...

Page 199: ...by tl olocal FAA office Major al eri tions to the basic airfrirr rc or syhtcrtrs r i o t covcrc 1by A 43 17 2 ecluire a S pplcrllcl tiil l y p c e tiIIc tc I t c oultcr O I pilot is rcquircd to ascer...

Page 200: ...r o i i d by t l c rltc of tlic nosc wheel steering bar that is stowed ill t l crcar haggagc compartmcnt or by power equipment that will not tl irnnge or excessively strain tlie nose gear steeringass...

Page 201: ...If pcr sil lc s t i l i o a11crl sclver outside the airplarle 5 Wlle11taxiit g over unevcl gl ound avoid hole5 and ruts 6 I o I I O I operate tile engine at high RI M when r rrllli g up OI 1 1 riir g...

Page 202: ...control wheel and pt llingit snug 4 Block the wheels 5 Secure tiedown ropes to the wing tiedown rlngs and to the tail skid at approximately 45 degree angles to the ground When using rope of non synthe...

Page 203: ...2 I f tl efilter is excessively tli tyor hl ows I I I 1ii111 1ge icpl cc it ir tr edii tely 3 W p ct l clitter I o u s i g wit11 a clcall clot11 so rkcd irt l l c a d e d gasolil e Wllen the l o l s...

Page 204: ...EFT BRAKE AND RLIDDER PEDAL 4 RIGHT BRAKE CYLINDER 6 6 BRAKE LEFT BRAKE HANDLE CYLINDER 7 HANDLE LOCKING Birl loti B LINE INLET B CLEVIS PIN 10 MASTER CYLINDEH ASStMMl Y 11 BOLT ASSEMBLY 12 TORQUE rU8...

Page 205: ...excess air and oil to escapc With the strut still co rrprcsscd rcinscrt thc alvc strnr and pu rrp up thc strut as above I n jacking thc aircraft for landing gear or other service two Irydraulic jacks...

Page 206: ...hen necessary with flat black paint to retard glare To prevent corrosion tlle surface sliould be cleancd and waxed periodically 8 19 OIL REQUIREMENTS The oil capacity of the Lycoming 10 360 series eng...

Page 207: ...is hpecifird lor this airplane Since the use of lower grades can cause heriot15e lgir e darllagt in a short period ofti ne the engine warranty i 3 i validated by the use of lower octanes Refer to lat...

Page 208: ...re11 Il5 9 1 1 9 blue 2 0 100 110 g l c c n 10 115 145 p u r p l c 4 h The operation of the aircraft is approved with an an i icing additive in the fuel When an anti icing additive i s used i t must...

Page 209: ...sa rnaxirnum 0138 5 I1 S gallons I here I S rp roxin ately25 gallons i n the fucl tank when fuel Ievcl I CVCII WIIII tlic I c rtorn o f the filler rreck ilrdicator Wlrclr usic g less tlrarr 111e btand...

Page 210: ...I O I I C I I L S Y I C of27 pxi for I I I IIO C tire n11 1 3 0 p i f o 1I1cIII I II ti A l l t l ccl IIIII tiles IIC I I IIIC C I c f o c o l i g i l l i l IIISI I II II I I I IIic CI I IOII III 01...

Page 211: ...s and f i n i s l i l g with a rate o l two amperes l lle bi ttery s l o u l d he rernoved fro111 the airplane for charging and quick charges are not rccorl rr er ded 1Ile external power receptacle il...

Page 212: ...csircd Wlicrc I eavy grease and dirt deposits have collected it may be ncccssary t o brush areas that were sprayed i n order to clcan thcm 3 Allow the solvent t o rcmain o n tllc gear fronl five to te...

Page 213: ...l l I slraiglit back alld fort11 n otiori Do not rub Iiarsl ly 3 Rer ioveoil and greax with a clot11 oistcried with kcrose e 110 rlot usc gasolirir alcol ol belilene carbor t c t c l l r i d e tl ir...

Page 214: ...ry cleaning fluid Floor cnrpcts nlny be clcancd like any household carpet 8 29 WINTERIZATION For winter opcration a winteri7ation kit i s instnllctl on IIIC inlct opcning of the oil cooler outboard ch...

Page 215: ......

Page 216: ...1 7 llllrl IIIL I I A r l o p l l l II I III IIII II I 0 AIII OIIIIOI IIII AIIIOII III II I III III II 0 I I III IIIC Illc i1111 1liiIii1 II I I IIII II 0 It k N S XI N I ip 11io11 S ICI I 0 20 A N S...

Page 217: ......

Page 218: ...hen cquippctl w t h one or more of the various optional systems and cquiprncnt not provitlcd witlr h c standard airplnnc All of t11c Supplcrncnts providcd by this section arc f AA Ipprovc l and consec...

Page 219: ...SECTION 9 SUPPLEhlENTS PliJER AIHCIt AFT COHPOHA TION PA 28RT 201 ARROW IV I I I I S I A ifJ IN I EN PIONAI 1 Y I Ef I 1j1 A N K...

Page 220: ...al air conditioning systcm is installed a 1 0 ins rrc maximuni climb performnncc tlic air co Iitior cr rntrst be tr rncd OFF manually prior to takeoff to discngngc the compressor and retract the conde...

Page 221: ...s in the up pohition tl I f the AIR C O N L 1 OOR OI EN ligl t docs not rcspo ld as hpccilictl above an air conditioner system or indicator bulb n allul ction is indicated a l dI r t l e r investigat...

Page 222: ...remely hot weather a The decrease in true airspeed i s approximately 6 KIS at all powcr sc tings b The decrease in range nlay be as rnucll as 40 nautical rnilcs for tllc 72 galloll capacity The climb...

Page 223: ...SECTION 9 PIPER AIRCRAFT CORPORATION SUPP1 EMENTS PA 28RT 201 ARROW IV...

Page 224: ...n 2 of this Pilot s Operating tiandbook arc ncccssary for this supplcmcnt SECTION 3 EMERGENCY PROCEDURES Thc following information applies in casc of clcctric trim malfunction a In casc of malfunction...

Page 225: ...atii g the trirn control switch on the pilot scoillrol yoke 1o prevent excosive speed increase in the event of an electric trim run away malfu clion the systeni incorporates an automatic disconnect fe...

Page 226: ...nstalled SECTION 2 I IMITATIONS a Autopilot operatio lproliibited above 175 K IAS b Autopilot niirst be O F F for takeoff and landing SECTION 3 EMERGENCY PROCEDURES a I n case of malfunction depress i...

Page 227: ...r detent position 2 Autof lite I I nlaster switch ON b 1 isengagement I AutoFlite I I niaster switch OFF c I l s a d i g Cllar ges I Move trim knob on instrument for drift correction from a constarlt...

Page 228: ...cncitivity pocitior Col Io tIi7cr tri ckir g 111tl I l c i c t l lor O M N I racking e Mainlair1 directional rim during a11 atttopilot o p c i t i c r s SECTION 5 FERFORMANC E No changcs to the hasic...

Page 229: ...SECTION 9 PIPER AIRCRAFT CORPORATION SUPP1 EMENTS PA 28RT 201 ARROW IV 1 I l l s I A E I N 1 EN I IONAL 1 Y L E F T B L A N K...

Page 230: ...MITATIONS a Autopilot opcration prohibited ahove 175 KIAS b Autopilot OFF for takeoff and landing SECTION 3 EMERGENCY PROCEDURES a I n an clilcrgcncy tlrc a ltopilotcan he tlisco i icctctl by I I usli...

Page 231: ...ale till functional use card set to rotate card to aircraft l c a d i g for correct picture 4 Slaving I ailt re i e laillrre to srlf correct for gyro drift a Cl cck tllat gyro slavi lgswitcl is set t...

Page 232: ...g Engagc IiDG modc rockcr swi cll ncI rolntc I I O G hug right and left Aircraft col troi wllccl sl olrl l turn same direction as bug Grasp control wllcel l r l n a l r a l l y override servo both di...

Page 233: ...ired course with O B S tlSI Course Knob b Select OMNI mode on radio coupler c Sclcct I I I X mode on autopilot cor solcto engage couplcr Aircraft will turn to a 45 i ltcrceptangle to intercept the sel...

Page 234: ...ourse datum and therefore milst he set to match the desired VOR course as selected on tllc 0 n S I For VOR Intercepts and Tracking Select the desired VOR course and set the I1I h g to the same heading...

Page 235: ...SECTION 9 PIIDERAIRCRAFT CORPORATION SUIDPI EM KN I S PA 28RT 201 ARROW IV I I I I S I AGE IN I ENTIONAl LY I EFI BLANK...

Page 236: ...ing Conduct trim check prior to flight SCC 1 011 t o be installed in clear view of the pilot c A rtopilotO F F during takeoff and landing d During autopilot operation the pilot must he in his scat wit...

Page 237: ...bar 4 1 isconnccted by pushing the roll rocker switcl OFF b I t r 1111 rverlt uf a trinl t alfullction I L cpress and Ilold the hlaster l rin Ir tcrruptSwitch 2 I rllll Master Switcl OFF Retrim aircr...

Page 238: ...n Slnvcd NSD 360A I Appearance o C IIDG Flag a Check air supply gauge vacor pressurc Torarlccl atcair supply 4 in fig min h Check compass circuit hrcaker c Ohscrvc display for proper opcrntioli 2 1 0...

Page 239: ...l Itotate rull c u n n a l d knob Icll and right and obscrvc I I I Ico rtr ol wlleel descrihcs a correspontling left arid rig111 turll tl cnccr ter kl ob 2 Scl proper I leading or1 D G and I U I I I I...

Page 240: ...m systcrn fails any portiol o i thc proccdurc pull tlic trim circuit brcakcr out until tririi systcm is repaired Substitution o i any trim system coniponcrif for ariothcr modcl is not a t t l o r i c...

Page 241: ...n opera ti or llcsel to a k e o f lposiriol prior lo akeoff b C l cckalr prcshlrre o r vacuulll to ascertain 1Ila1 l l e direc ional gyro rlltl attit ldc g y o are receiving sufficien air e Roll S e c...

Page 242: ...CRS knob of H S I b Sclcct O M N l mode on Radio Couplcr c Select l l D G mode on autopilot consolc to engagl coupler Aircraft will turn to a 45 intcrccpt angle t i intercept the selected VOR course...

Page 243: ...S I For VOH Intercepts and Tracking Selcct the desired VOR Course and set the I1I X bug to the sante Ileading Select OMNI mode 011 the c o u p l e r a d eltgage Ill Inode on the autopilot console 2 or...

Page 244: ...scribed ill Sectiol 4 1 or g ahove and in Altitude Ilold mode b Inbound to L OM slow 10 90 to 100 KIAS ant1 lower flaps as desired c Automatic Glide Slope caplure will occur at l tlcSlope intercept i...

Page 245: ...utomatically drcouplc from Glide Slope Decoupling may be accomplished by any of the following means I Disengage Altitude Mode 2 Switch Radio Coupler to tIDG Mode 3 Disengage Autopilot SECI ION 5 I EHF...

Page 246: ...l l llc ir rorni tior c o t i c c l v i t I i i t l i s s p p l c i i c t i s 1 0l t LIS CI ill I I I I I I I I witli t l c c o l p l e l c Il rltlhook l liis supl lctiicnt II ISl c c n F A A Approvct...

Page 247: ...pe i ive llsl irlgof l l cVOI I utlol will cause lllc systclu lo ltcrnale hctwccl tllc VOIt and VOIC I Al lnodes wl ilcrepetitive pushing ol the ItNAV buttol causes the sysleni to IIel ni tc C I W C O...

Page 248: ...carryover occurs from the tens to hundreds place Rollover occurs from 1 17 to IOR Centcr knob varies frequency in 05 hi1I slcps rcgardlcss of whcther the switch is in its in or out position b Radial D...

Page 249: ...I COHYOHAI ION SUPP1 EMENTS PA 28RT 201 ARROW IV SECTION 5 PERFORMANCE N o changes to the basic performance provided by Section 5 of this Pilot s Operating Handbook are necessary for this supplement I...

Page 250: ...ion with the complete handbook This supplement has becn F 4 4 Approvedv as a permanent part of t h s handbook and must remain in this handbook at all times when the optiorial ANS 351 Area Navigation C...

Page 251: ...enyon ts or APPli al proachr modes of operation I n the rnroute mode CDI deviation is mileidot 5 rliiles full scale 1 1 approach CDI deflectioli is 1 4 r ile do 1 1 niiies full scale Waypoint Selecto...

Page 252: ...i o n ill rl uticalniilcs i r t o t I c d p l i y K o h s cor lrol i iforniatior IS lollows 1 arge knob Changcs d15l lily in 10 mile ncrenicnts Small knob puslicd iri C liarigcs tlr play I mile tr cr...

Page 253: ...e waypoint is at this point inactive Waypoint number 2 bearing and distance delinitions are then set into the ANS 351 c Set up the rest of thedesired waypoints as described above d Press the RTN retur...

Page 254: ...andbook and must rcmain in this handbook at all times when thc optional Century 21 Autopilot is installed SECTION 2 LIMITATIONS a Maximum airspeed for autopilot operation is 175 K lAS b Autopilot OFF...

Page 255: ...d NSD 360A a Appearance of HDG Flag 1 Check air supply gauge vac or pressure for adequate air supply 4 in Hg min 2 Check compass circuit breaker 3 Observe display for proper operation h l o disable he...

Page 256: ...s may remain out of view depending upon the design of the NAV converter used in the instal lation SECTION 4 NORMAL PROCEDURES Refer to Edo Aire Mitchell Century 21 Autopilot Operator s h l n l a l PIN...

Page 257: ...only slave and free gyro positions 2 Rotate card to center slaving meter check IIDG displayed with magnetic compass HDG 3 Perform standard VOR receiver check 4 Perform Steps I 7 in Section 4 item b ex...

Page 258: ...the complete handbook This supplement has been FAA Approved as a permanent part of this handbook and must remain in this handbook at all times when the optional Century 41 Autopilot or the Century 41...

Page 259: ...g t l cAl ON 01 1 switc11 0 1 1 t l c I I O I I I I I I C c I cp chsi g 111 1stcr I S U I I I I I I C Is w i c l 0 1 1 l i l j t h co11110l w11ccI 2 A I I I I I I I Inay Ilc tliscor l cctctl hy a I c...

Page 260: ...plays arc still lunction l usc card sct to rotatc ci rtlto aircraft heading lor correcl picturc d Slaving Failure i c failure l o scll corrcct lor gyro drift I Chcck gyro sl vingswitch is sct l o No...

Page 261: ...P OFF warning horn that will sound for approxi mately 4 seconds anytime the autopilot is disengaged This will be acco npa iied by ari A PWmessage flash on the autopilot remote annunciator for approxi...

Page 262: ...l P N 68S803 dated 1 79 for additional System Description and Nor nnl Operating Procedures b PREFI IGIIT PROCEDI IRES NOTE During system functional check the system must be provided adequate D C volta...

Page 263: ...ted systen self test circuit pro vided irr conjunction with a functional check describctl below will uncover internal failures that otherwise could remain undetected and thus compromise the fail safe...

Page 264: ...inltally 3 With TEST button on the Mode Annur cialors t i l l dcprcsscd verify Trim will not operate ineither direction with thc Control Wheel Switch 4 Release TEST pushbutton All lights exccpt 1iI C...

Page 265: ...rswitch ON 2 Adjust IIDG bug to aircraft I eadillgand select desircd pitch attitude by activation of the CWS Pitch S y l c l switcl or the nlodifier switch 1 Mancuver aircraft manually to satisfy the...

Page 266: ...ing the glide path or whcn passing the final approach fix FAF immediately lower tlic I lnding gcar and reduce the power for approximately 80 95 KIAS on the final approach segment Adjust powcr as ncccs...

Page 267: ...e ofclilrib is i itlicir ed then raise gear and Ilaps d I ilot rnay hand fly aircraft with reference to flight director stecring information e After aircraft is eslablishcd in climb gear a11d laps up...

Page 268: ...nt part of 11is handbook and mrlst remain in this handbook at all timcs w l i e IIIC optiorial Pipcr Control Wheel Clock is installcd SECTION 2 LIMITATIONS No changes to the basic limitations provided...

Page 269: ...oldthe time displayed At the time mark the ST SP button is pressed momentarily to begin the time cotrnting at the exact second I f t l e rninutes are not advanced when they are flashing in the set 11...

Page 270: ...1 ARI E O F CONTEN1 S SE TION I 0 SAFETY TII S Paragraph No I agc No 10 1 General 10 1 10 3 Safety Tips 10 1 REPORT VB 1130 10 1...

Page 271: ......

Page 272: ...s i t i s desirable to have the nirplal cat a slower speed before extending the flaps The flap step will not support weight i f the flaps are in any extendf ciposition 1 l e flaps must be placed in th...

Page 273: ...dcr pedals or opcra irlg 1 1 1 o e brilkes 11 1 1 1 it11 el1011l o i v o i l i c c i d c l s pilots sI1o111 l obtili11 i111 l 5111ily111c lcty 1c1 11cd i l o r l i t i o l III IC availablr 111 k AA p...

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