Piper ARCHER III Pilot Operating Handbook Download Page 66

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SECTION3

EMERGENCY PR

OCE

URES

PA-28-181, ARCHER III

3.1 GENERAL (continued)

Crew Alerting System (CAS) Messages

The following tables show the color and significance of the Warning,

Caution and Advisory messages which may appear on the Garmin G l 000

displays.

REPORT: VB-2749

3-2

ISSUED: December 22, 2017

•

Summary of Contents for ARCHER III

Page 1: ...PLANE REGIST NO __ N_2_3_2_T_F_ ERIC O D A 510 PTPER AfRCRAFT INC VERO BEACH FLORIDA FAA APPROVED 1N NORMAL AND UTILITY CATEGORIES BASED ON CAR 3 THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FUR...

Page 2: ...REPORT VB 2749 ii Published by TECHNICAL PUBLICATIONS Piper Aircraft Inc Issued December 22 2017 2017 2021 Piper Aircraft loc All Righis Reserved ISSUEU Uecember 22 2017 REVISED March 9 2021...

Page 3: ...RNING This handbook cannot be used for operational purposes unless kept in a current status ARNING Inspection maintenance and parts requirements for all non PIPER APPROVED STC installations are not in...

Page 4: ...n proper numerical order within each section 3 Insert page numbers followed by a small letter in direct sequence with the same common numbered page Il Identification of Revised MateriaJ Revised text a...

Page 5: ...5n 4 26 Revised Para 4 13 7 8 Revised Para 7 15 7 40 Revised Para 7 15 7 41 Revised Para 7 15 7 53 Revised Para 7 23 7 54 Revised Figure 7 9 7 55 Revised Figure 7 9 9 i Revised T O C 9 9 lhru Added S...

Page 6: ...Revised Para 2 25 Revised Para 3 5e Revised Para 3 5k Revised TAWS B alerts and for table additions Revised Supplement 6 Revised Supplement 6 Revised Supplement 6 Revised Supplement 7 July 3l 2018 Up...

Page 7: ...Added Rev 5 to TOC PRl90829 3 20 Revised Para 3 5d 3 25 26 Revised Para 3 5d 4 9 Revised Para 4 5c 4 13 Revised Para 4 5e 4 16 Revised Para 4 5h 7 36 Revised Databases 7 37 Revised Databases 7 42 Revi...

Page 8: ...5p Revised Para 7 17 Added pages 7 45a 7 45b Revised Para 7 23 Revised Figure 7 9 Revised Para 7 25 Revised Figure 7 11 Revised Para 8 19 Revised T O C Revised Supplement 6 Revised Supplement 8 Added...

Page 9: ...pdated copyright vi c vi d Added pages to L of R Added Rev 8 to L of R 1 6 Revised Para 1 11 2 15 Removed Para 2 29 Note 4 10 thru Revised Para 4 5d 4 12 7 2 Revised Para 7 7 8 13 Revised Para 8 19 9...

Page 10: ...PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 vi d ISSUED December 22 2017 REVISED March 9 2021...

Page 11: ...ROCEDURES SECTION 4 NORMAL PROCEDURES SECTION 5 PERFORMANCE SECTION 6 WEIGHT AND BALANCE SECTION 7 DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS SECTION 8 AIRPLANE HANDLING SERVICING AND M...

Page 12: ...PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 viii ISSUED December 22 2017...

Page 13: ...21 1 23 introduction 1 1 Notations 1 3 Engine 1 5 Propeller 1 5 Fuel Oil 1 5 1 6 Max _imumWeights 1 6 StandardAirplaneWeights 1 6 Baggage Space 1 7 SpecificLoadings 1 7 G1000 GNSS GPS SBAS Navigation...

Page 14: ...SECTION 1 GENERAL PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 I ii ISSUED December 22 2017...

Page 15: ...emainjng within the operating limitations as outlined by instrument markjngs placards and lrus handbook Although the arrangement of this handbook is intended to increase its in flight capabilities it...

Page 16: ...SECTION 1 GENERAL PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 1 2 ISSUED December 22 2017...

Page 17: ...recognition and corrective action ICAUTIONI Operating procedures or techniques which may result in damage to eq1 ipment if not carefully followed or the need for immediate crew awareness and possible...

Page 18: ...SECTION 1 GENERAL PA 28 181 ARCHER ill 14 12 10 48 i Min turning radius 30 ft from pivot point to wing tip 0 3 6 2 14 35 8 REPORT VB 2749 1 4 THREE VIEW Figure 1 1 ISSUED December 22 2017...

Page 19: ...361 0 8 5 I i Engine Type Four Cylinder Direct Drive Horizontally Opposed with Fuel lnjection 1 7 PROPELLER a Number of Propellers b Propeller Manufacturer c Model d Number of Blades e Propeller Diame...

Page 20: ...ding Weight lbs d Maximum Weights in Baggage Compartment lbs 1 15 STANDARD AIRPLANE WEIGHTS PA 28 181 ARCHER ill 8 Refer to latest revision of Lycoming Service Instruction 1014 Refer to latest revisio...

Page 21: ...is installed in accordance with AC 20 138D When all the equipment is operative the Garmin G1000 system has two independent GNSS long range navigation systems Failure of any of the above equipment or...

Page 22: ...erators require operational approval B RNAV Must have GNSS RNAV5 SBAS capability Europe and availability or GNSS RAlM FDE availability must be velified prior to ffight Maximum predicted RAIM FDE unava...

Page 23: ...for those routes requiring only one long range navigation sensor No time limit using GNSS as the primary navigation sensor Part 91 Pan 91 subpart K 121 125 and135 operators require operational approva...

Page 24: ...RNAV system is installed and meets the performance and functional requirements of AC 90 1 OOA CHG2 In accordance with AC 90 1 OOA CHG2 Part 91 operators except subpart K following the aircraft and tr...

Page 25: ...is installed and meets the performance and functional requirements of AC 90 lOOA CHG 2 In accordance with AC 90 I00A CHG 2 Part 91 operators except subpart K following the aircraft and training guidan...

Page 26: ...SBAS capability and availability or GNSS RAIM FDE availability must be verified prior 10 flight Maximum predicted RAI M FOE unavailabiliry is 5 minutes 1 In accordance with AC 90 1 0SA Part 91 operato...

Page 27: ...trument approach procedures that are retrieved from the current navigation database are authorired In accordance with AC90 105A Part91 operators except subpart K following the aircraft and training gu...

Page 28: ...PCH LNAV VNAV minima procedures Part 91 subpart K 121 125 129 and I 35 operators require operational approval This aircraft is not authorized to perform Barometric Based Vertical Guidance baro VNAV ap...

Page 29: ...dance with A C 90 107 Part 9I operators except subpart K following the operaIional considerations and training guidance inAC 90 107 are authorized to ny RNPAPCH LP minima procedures Part 91 SUbpart K...

Page 30: ...th AC90 107 Pan91 operators except subpanK following the aireraft and Lraining guidance in AC 90 107 are authorized to fly RNP APCH LPV minima procedures Part 9 I subpart K 121 125 129 and 135 operato...

Page 31: ...unctions ISSUED December 22 2017 REVISED JuJy 15 2020 Reference Documents FAA AC 20 138D ICAO Flight Plan Code Item I0a Item 18 Code PBN NIA NIA Notes B AV Hglding Supported RF Legs Not supported Para...

Page 32: ...ecision approach RAIM Also within Europe Europe s AUGER GPS RAIM Prediction Tool at hrtp augur ecacnav com augur app home Verification of FDE RAIM availability is not necessary if SBAS coverage is con...

Page 33: ...nots Ground Speed is the speed of an airplane relative to the ground Indicated Airspeed is the speed of an air craft as shown on the airspeed indicator when corrected for instrument error lAS values p...

Page 34: ...ain of altitude in the shortest possible horizontal distance Best Rate of Climb Speed is the airspeed which delivers the greatest gain in altitude in the shortest possible time b Meteorological Termin...

Page 35: ...itude measured from standard sea le el pressure 29 92 in Hg by a pressure or barometric altimeter It is the indicated pressure altitude corrected for position and instrument error In this handbook alt...

Page 36: ...System Crew Alerting System Evolution Backup Display Aspen standby instrument Engine Indication System Electronic Stability and Protection Fault Detection and Exclusion Fuel On Board Garmin Datalink G...

Page 37: ...h adequate control of the airplane during takeoff and landing was actually demonstrated during certification tests A part of a route Each end of that part is identified by I a geographical local ion o...

Page 38: ...ht of start taxi and run up fuel Maximum weight approved for the start of the takeoff run Maximum weight exclusive of usable fuel The product of the weight of an item multi plied by its arm Moment div...

Page 39: ...Limitations 2 13 Weight Limits 2 15 Center of Gravity Limits 2 17 Maneuver Linlits 2 19 Flight Load Factors 2 21 Types of Operations 2 23 Fuel Limitations 2 25 Gamlin GlOO0 Avionics System Limitations...

Page 40: ...SECTION 2 LIMITATIONS PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 2 ii ISSUED December 22 2017...

Page 41: ...operating limjtations stated in the form of placards and markings and those given in thjs section and trus complete handbook Limitations associated with those optional systems and equipment which req...

Page 42: ...ED Maximum Operating Maneuvering Speed Vo Do not make full or abrupt control movements above th is speed At 2550 lbs G W Al 1917 lbs G W Maximum Flaps Extended Speed VFE Do not exceed this speed with...

Page 43: ...el AVGAS ONLY minimum grade 6 Number of Propellers 7 Propeller Manufacturer 8 Propeller Model 9 Propeller Diameter Inches Minjmum Maximum l0 Propeller Tolerance ISA Conditions static RPM at maximum pe...

Page 44: ...Band CautionRange Idle Yellow Band Ground Warm Up Red Line Minimum Red Line Maximum 2 11 SYSTEMS LIMITATIONS a Alternator b Emergency Battery Minimum 2 13 WEIGHT LIMITS a MaximumRamp lbs b Maximum We...

Page 45: ...arward Limit Inches Aft of Datum 93 0 93 0 Rearward Limit Inches Aft of Datum 93 0 93 0 Straight line variation between points given The datum used is 78 4 inches ahead of the wing leading edge at the...

Page 46: ...ormal 3 8 G 1 5 G Utility 4 4 G 1 7 G The airplane is approved for the following operations when equipped in accordance with FAR 91 or FAR 135 a Day V F R b Night Y F R c Day I F R d Night I F R e Non...

Page 47: ...Gannin also provides a detailed 01000 Pilot s Guide PIN 190 02130 02 latest appropriate revision This reference material is not required to be on board the aircraft but does contain a more in depth d...

Page 48: ...ase The GlOOO Navigation database must incorporate the current update cycle or each waypoint must be verified for accuracy with current approach chart data d Flight Plannjng In areas where GPS SBAS co...

Page 49: ...d or rerouted on a track where RAIM FDE requirements can be met For operations where the route requires oceanic remote area Class II navigation the aircraft s operator or flight crew must determine th...

Page 50: ...SECT1ON2 LIMITATIONS PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 2 8b ISSUED December 22 2017 REVISED March 27 2020...

Page 51: ...ical Guidance Advisory vertical guidance deviation information is only an aid to help pilots comply with altitude restrictions When using advisory vertical guidance the pilot must use the primary baro...

Page 52: ...raph 1 21 for approved GPS operations approaches 3 Non OPS Approaches The navigation equipment required to perform instrument approach procedures is indicated by the title of the procedure and notes o...

Page 53: ...g and attitude may occur near the poles but thls will not affect the GPS track NOTE In dual GPS installations only one GPS needs to be available for lFR operations h Terrain and Obstacle Display The G...

Page 54: ...m as installed in this aircraft supports approval of AC 120 76C Hardware Class 3 Software Type B Electronic Flight Bag EFB electronic aeronautical chart applications when using current FliteChart or C...

Page 55: ...ctronic approach charts must be used for situaLional awareness only Paper charts or other EASA approved electronically displayed information must be used as the primary source of aeronautical informat...

Page 56: ...e is not approved to replace any required or installed aircraft display equipment including navigation or traffic weather display equipment The data presented on the PED may not have the required inte...

Page 57: ...trument Heading l 1 2 l l l l l 0 I 0 2 2 0 0 0 0 3 0 3 0 3 1 2 OJ If the PFD is inoperative during DAY or NIGHT VFR the MFD must be operative 2l If the MFD is inoperative the PFD must be operative fo...

Page 58: ...pilot engagement limits a With enhanced AFCS features Pitch UP 50 Pitch DOWN 50 Roll 75 b Without enhanced AFCS features Pitch UP I6 Pitch DOWN 17 Roll 30 7 Autopilot approved for Category l precision...

Page 59: ...STATED IN THE fORN Of PLACARDS NARllNSS AMO MANUALS ALL NARKll S AND PLACARDS ON THIS AIRPLANE APPLY TO ITS OPERATIOI AS A UIILITY CATE ORY AIRPlAME FOR IORIIAL AND UTILITY CATHORY OPERATION REFER TO...

Page 60: ...verhead panel On lower left portion of instrument panel ALTERNATE STATIC SOURCE PULL AFT TO OPEN l All CABIN TS AND STORt t MNDOW t tUST BE QOSED HEATER AND DEFROSTER MUST BE ON OPEN FOR STATIC SY SlE...

Page 61: ...two placards on aft baggage compartment bulkhead BAGGAGE MAX 200 LBS UTILITY CATE GORY OPERA TION NO BAGGAGE OR AFT PASSENGERS ALLOWED NORMAL CATEGORY OPERATION SEE PILOT S OPERATING HANDBOOK WEIGHT A...

Page 62: ...tinued On the right side of Lbe fuselage aft of the wing EXTERNAL POWER 28 VOLTS O C TURN MASTER SWITCH AND ALL EQUIP OFF BEFORE INSERTING OR REMOVING PLUG Adjacent to the filler caps REPORT VB 2749 2...

Page 63: ...ire in Flight Electrical Fire in Flight EnginePowerLoss 3 1 3 2 3 6 3 7 3 7 3 8 3 8 3 8 3 8 3 9 3 10 3 11 3 11 3 12 3 13 3 14 3 14 3 15 3 16 3 17 3 18 3 5c 3 5d 3 5e EnginePowerLoss DuringTakeoff Engi...

Page 64: ...opilot Disconnect Electric PitchTrim Failure Electric Pitch Trim Runaway Autopilot Overspeed Recovery Autopilot Underspeed Recovery Autopilot Out Of Trim Abnormal Flight Director Mode Transitions Auto...

Page 65: ...procedure Pilots must familiarize themselves with the procedures given in this section and must be prepared to take the appropriate action should an emergency situation arise The procedures are offere...

Page 66: ...II 3 1 GENERAL continued Crew Alerting System CAS Messages The following tables show the color and significance of the Warning Caution and Advisory messages which may appear on the Garmin G l 000 disp...

Page 67: ...or more than 30 scconds Autopilot is engaged and the airspeed has fallen below the USP threshold or stall warning has activated Cause CAS Warnings with EIS Indications Propeller Overspecd Oil Temperat...

Page 68: ...UEL QTY RFUELQTY PITOT HEAT FAIL PITOT HEAT OFF CAS Message 3 41 CO level greater than or equal to 50 but less than 200 parts per million PPM NIA L FUEL QTY or R FUEL QTY less than or equal to 5 gals...

Page 69: ...visory l lessages Vhite Checklist CAS Message Page Cause CAS Advisories with Text Messages AVFANFAIL EMERGBATTON FUELIMBAL MFDFANFAIL PFDFANFAIL 3 31 One or more of the external avionics cooling fans...

Page 70: ...accompany PFD annunciations and alerts and no pilol action is required to acknowledge PFD annunciations and alerts See Gannin G 1000 Pilot s Guide for the Piper PA28 I 8I Archer G 1000 for additional...

Page 71: ...nt Timer Expired voice alert when countdown timer reaches zero If autopilot installed Autopilot disconnect Lone AIRSPEED voice alert when in a low airspeed condition Engaging Autopilot voice alert whe...

Page 72: ...CUT OFF THROTTLE OPEN FUEL PUMP OFF FUEL Selector OFF Abandon iffire continues Engine fires during strut are usually the result of overpriming If a fire is present before the engine has started move t...

Page 73: ...ceed with POWER OFF LANDING procedure The possibility of a fire in tlighL is extremely remote It is essential lhat the source of the fire be promptly identified through character of the smoke smell he...

Page 74: ...3 Sa Fire continued Electrical Fire In Flight EMERG BATT Switch VERIFY ARM BATT MASTR Switch OFF ALTR Switch OFF Vents OPEN HEAT DEP Defroster OFF Fire EXTINGUISH Emergency Descent Ifneeded TO A SAFE...

Page 75: ...structions If sufficient altitude has been gained to attempt a restart Airspeed MAINTAIN 76 KIAS FUEL Selector SWTTCH to tank containing fuel FUEL PUMP Check ON MIXTURE RICH ALT AIR OPEN If power is n...

Page 76: ...uption attempt to restore power by turning the fuel pump ON and selecting the other fuel tank Move the throttle and mixture control levers to different settings This may restore power if the problem i...

Page 77: ...tion off if installed and look for a suitable field If measures taken to restore power are not effective and if time permits check your charts for airports in the immediate vicinity If possible notify...

Page 78: ...sure regulating system and a landing should be made as soon as possible to investigate and prevent engine damage A complete loss of oil pressure indication may signify oil exhaustion or may be the res...

Page 79: ...d investigate the problem Prepare for power offLanding NOTE lf possible always retain glide capability to lhe selected landing area in case oftotal engine failure An abnormally high oil temperature in...

Page 80: ...Switch ON FUEL Selector SELECT OTHER TANK FULLEST FUEL PUMP Switch OFF If caused by engine driven fuel pump fai lure THROTTLE CLOSE FUEL PUMP Switch ON THROTTLE RE ESTABLISH as required MIXTURE RE EST...

Page 81: ...l quantity RFUELQTY FUEL Selector ON FULLEST TANK Land as soon as practical H both tanks have low fuel quantity FUEL Selector ALTERNATE TANKS TO MAINTAIN FUEL SUPPLY TO ENGINE Land as soon as possible...

Page 82: ...not reset any non essential circuit breakers in flight Alternator Failure Indication Master Warning Triple Chime ALTRFAJL I CAUTION The ALTR circuit breaker should not be opened manually when the alt...

Page 83: ...ry source of electrical power The only electrical bus that remains powered in this load shed configuration is the ESSENTIAL BUS All electrical items on the remaining buses will be inoperative See Figu...

Page 84: ...vely on the emergency bus as indicated by the PFD FAN FAIL and AV FAN FAIL advisory CAS messages EMERG BAIT Switch Verify ARM Standby Flight Instrument Verify OPERATIONAL Ain raft ConLrol Use PFD and...

Page 85: ...RES CHECK LIST continued 3 Sd Electrical Failures continued Emergency Battery Voltage Indication Master Warning Triple Chime Flashing Red E VOLTS Indication WARNING Complete electrical failure is immi...

Page 86: ...AV2 in DME TUNING Window Exit and avoid FR conditions as soon as practical NOTE If the PFD fails the MFD will remain in normal mode Pushjng the DISPLAY BACKUP button on the audio panel allows the MFD...

Page 87: ...on the MFD after the DlSPLAY BACKUP button is pressed It is the pilot s responsibility 10 compare these parameters lo verify accuracy GPS and VOR2 navigation as well as flight planning are available...

Page 88: ...unctionality COM2 yellowx d but121 5MHzremains available NAV2 GPS2 GDL 69 SXM Garmin Datalink XM DME ADF ESP NOTE If the GFC700 au1opilo1 was engaged prior to MFD failure ii will remain engaged in its...

Page 89: ...removed course pointer straight up yeUow x s and amber text on all air data attitude and heading indicators System Messages Messages Softkey CONSIDER ADAHRS Circuit Breaker Row 2 Col 8 RESET If ADAHRS...

Page 90: ...VERIFY NO FAILURE INDICATIONS Attitude and Heading Use Standby Instrument I NOTE I The following features will become inoperative if there is a complete loss ofADAHRS functionality Autopilot includin...

Page 91: ...lever posiLion engine sound and speed 2 Monitor other indications to determine the health of the engine 3 Use known power settings from POH power setting tables for approximate fuel flow values 4 Use...

Page 92: ...perative 2 If a CAS message appears that is not expected treat it as if the condition exists 3 If an abnormal condition exists but the CAS system has not been activated use other available information...

Page 93: ...M2 Failure Indication Inability to communicate receive on COMl and COM2 NOTE If power is lost to the audio panel a fail safe communications path becomes available between the pilot s headset microphon...

Page 94: ...se the airplane symbol and magenta course line on the MAP display and the amber CDI on the HSI ARNING Information normally derived from GPS turns amber and becomes more inaccurate over time Amber CDI...

Page 95: ...moved from all maps The map will remain centered at the last know position NO GPS POSITION is shown in the center of the map TAWS and TAS are inoperative Avionics Cooling Fan Failures as required Indi...

Page 96: ...OTE I Electronic Stability Protection ESP will be inoperative following an autopilot failure Control Wheel GRASP FIR 1LY Allitude Indicators CROSSCHECK A P DISC Switch DEPRESS and HOLD Pitch Trim RETR...

Page 97: ...pect residual control forces upon disconnect The autopilot will not re engage after disconnect with failed pitch trim Autopilot DISCONNECT Electric Pitch Trim Runaway Indication An unexpected pitch de...

Page 98: ...vel light altitude to decelerate the airplane below the maximum approved autopilot operating speed The autopilot must be engaged for it to follow the pitch up commands of the night director Overspeed...

Page 99: ...If AIL or AIL annunciation Verify SLIP SKID INDICATOR centered If 1 ELE or 1 ELE annunciation Suspect elevator trim issue Control Wheel GRASP FIRMLY with both hands ICAUTIONI Be prepared to apply a s...

Page 100: ...e manually or execute missed approach Loss of selected lateral mode Autopilot Mode Controls SELECT ANOTHER LATERAL MODE If on an instrument approach Autopilot DISCONNECT if coupled and continue manual...

Page 101: ...is lost while the autopilot is tracking it the autopilot will roll U1e aircraft wings level and default to roll mode ROL Autopilot SELECT ANOTHER LATERAL MODE Nav Source SELECT AVALID NAV SOURCE Auto...

Page 102: ...OT HEAT Switch ON If Pitot Heat still inoperative Exit and Avoid Instrument Meteorological Conditions 3 Sg Starter Engaged Starter Engaged Indication Master Warning Triple Chime If on the ground START...

Page 103: ...nal spins are prohibited in this airplane 3 Si Open Door Open Door To close the door in night to recovery from dive Airspeed REDUCE to less than 87 KIAS Cabin vents CLOSE Storm window OPEN Upper latch...

Page 104: ...offlanding NOTE If possible always retain glide capabijjty to the selected landing area in case of total engine failure Engine roughness may be caused by blockage in the injector nozzles induction sys...

Page 105: ...conditioning or any other opening Lo the engine compartment Open a fresh air source immediately Don l smoke Land as soon as possible Be sure the source of the contamina1ion is corrected before funher...

Page 106: ...SECTION 3 EMERGENCY PROCEDURES PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 3 42 ISSUED December 22 2017...

Page 107: ...4 11 4 12 4 13 4 13 4 13 4 14 4 15 4 16 4 17 4 17 4 17 4 18 4 18 4 19 4 20 4 22 4 22 4 23 4 24 4 25 4 25 4 25 4 26 4 26 4 5f 4 5g 4 5h 4 5i 4 5j 4 5k 4 51 4 5m 4 5n 4 50 4 5p 4 5q 4 7 4 9 4 11 4 13 4...

Page 108: ...SECTION 4 NORMAL PROCEDURES PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 4 ii ISSUED December 22 2017...

Page 109: ...ith little emphasis on system operation These checklists should be used during normal ground and flight operations When appropriate additional information is provided immediately below the checklist p...

Page 110: ...equipment installed the condition of the engine airplane and equipment atmospheric conditions and piloting technique a Hest Rate of Climb Speed b Best Angle of Climb Speed 76 KIAS 64 KIAS c Maximum O...

Page 111: ...step NOTE Normal gear strut extension exposed area corresponds to that for the airplane under a normal static load empty weight of the airplane plus full fuel and oil COCKPIT Control Wheel RELEASE RES...

Page 112: ...tot Static Head CHECK WARM Stall Warning Horn CHECK All Lighting Switches OFF PITOT HEAT Switch OFF PITOT HEAT OFF CAS Message ILLUMINATED BATT MASTR Switch OFF Flaps EXTEND Primary Flight Controls PR...

Page 113: ...CAUTION When draining any amount offuel care should be taken to ensure that nofire hazard exists before starting engine Fuel Tank Sumps DRAIN AND CHECK FOR WATER SEDIMENT AND PROPER FUEL Tie Down and...

Page 114: ...leakage and that the cowling is secure The propeller and spinner should be checked for detrimental nicks cracks or other defects Check the tire for cuts wear and proper inflation LEFT WING Surface Co...

Page 115: ...E COVER HOLES CLEAR OAT Probe CHECK Wing Tip and Lights CHECK Aileron and Hinges NO DAMAGE or INTERFERENCE Flap and Hinges NO DAMAGE or INTERFERENCE Static Wicks CHECK SECURE FUSELAGE Antennas CHECK E...

Page 116: ...is not indicated within 30 seconds following an engine start stop the engine and determine the trouble In cold weather it will take a few seconds longer to get a positive oil pressure indication NOTE...

Page 117: ...trical Switches OFF DAY NIGHT Switch if installed SET BATT MASTR OFF AVION MASTER OFF I NOTE I TheEMERG BATTmay remain ON after checking for proper bus operation thereby allowing the displays to remai...

Page 118: ...nnel prior to further checks E VOLTS indication must not be less than 23 3 volts prior to flight Proceed to the appropriate ENGINE START checklist 4 Sd Engine Start Checklists NORMAL START COLD ENGINE...

Page 119: ...ONSIDER ANY ILLUMINATED Propeller CLEAR START Switch PRESS MIXTURE when engine starts ADVANCE THROTTLE ADJUST OiI Pressure CHECK ENGINE START FLOODED THROTTLE OPEN FULL BATT MASTR Switch ON i LTR Swit...

Page 120: ...M All Electrical Equipment OFF External Power APPLY THROTTLE 1 2 IN OPEN FUEL PUMP ON FIN STROBE Switch ON MIXTURE PRIME 3 5 seconds then IDLE CUT OFF CAS Messages CONSIDER ANY ILLUMINATED PFD Annunci...

Page 121: ...SYNC or ENTER MANUALLY CAS Messages CONSIDER ANY ILLUMINATED PFD Annunciations CONSIDER ANY ILLUMINATED System Messages Messages Softkey CONSIDER LightS AS REQUIRED Heater and Defroster AS DESIRED TA...

Page 122: ...in the fuel line resulting in rough idle operation To correct thjs condion see section 4 15 Before attempting 10 taxi the airplane ascertain that the propeller back blast and taxi areas are clear Pow...

Page 123: ...indication less than 23 3 VOLTS during BEFORE STARTING ENGINE Checklist EMERG BAIT Switch Verify ARM AVION MASTER Switch OFF ALTR Switch OFF BAIT MASTR Switch OFF E VOLTS Indication 23 3 VOLTS MINIMUM...

Page 124: ...RRECT Door LATCHED Air Conditioner if installed OFF NOTE TAS aural alerts will be muted when GPS altitude is lower than 400 FT AGL Takeoff should not be attempted with ice snow or frost on the wings T...

Page 125: ...or to application of power may be used SHORT FIELD OBSTACLE CLEARANCE Flaps 25 second notch Trim Slightly Aft of Neutral Brakes APPLY HOLD THROTTLE FULL POWER Brakes RELEASE Rotation Airspeed 55 K IAS...

Page 126: ...d in Section 5 Use of the mixture control in cruising flight reduces fuel consumption significantly especially at higher altitudes The mixture should be leaned during cruising operation above 5000 ft...

Page 127: ...ump should be normally OFF so that any malfunclion of the engine driven fuel pump is immediately apparent If signs of fuel starvation shoulci occur at any time during flight fuel exhaustion should be...

Page 128: ...pointer prior to i11itiating a VHF NAV approach COM NAV Radios Avionics CHECK SET Altimeter Standby Altimeter SET Seat Backs ERECT Seat Belts Harnesses FASTEN ADJUSTED Armrests STOWED FUEL PUMP ON FU...

Page 129: ...o around Full throttle operation with alternate air open can cause detonation The amount of flap used during landings and the speed of the aircraft at contact with the runway should be varied accordin...

Page 130: ...e handle followed immediately by the checklist shown above 4 So AfterLanding Checklist AFTER LANDING Clear of runway FLAPS RETRACT Air Conditioner if installed AS DESIRED FUEL PUMP OFF STROBE LIGHTS S...

Page 131: ...ALTR Switch OFF THROTTLE CLOSED MIXTURE IDLE CUT OFF LEFT RIGHT MAG Switches OFF Interior Lights at night OFF Exterior Lights OFF BATI MASTR Switch OFF STANDBY INSTRUMENT VERIFY SHUTDOWN NOTE In case...

Page 132: ...e and then secure the tow bar on the aft bulkhead of the baggage compartment The aileron and stabilator controls should be secured by looping the safety belt through the control wheel and pulling it s...

Page 133: ...by turning the BATT MASTR switch ON lifting the detector and checking to determine if the Stall aural annunciation is actuated The BATT MASTR switch should be turned OFF after the check is complete 4...

Page 134: ...m the noise level is 75 3 dB A 4 15 RECOMMENDED PROCEDURES FOR ELIMINATION OF FUEL VAPOR Fuel vapor can occur in the fuel system during ground operations when high ambient temperatures are present The...

Page 135: ...OF CONTENTS SECTION 5 PERFORMANCE SECTION 5 PERFORMANCE Page No 5 1 General 5 1 5 3 Performance and Flight Planning 5 1 5 5 Flight Planning Example 5 3 5 7 Perfonnance Graphs 5 9 List of Figures 5 9 I...

Page 136: ...SECTION 5 PERFORMANCE PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 5 ii ISSUED December 22 2017...

Page 137: ...delerioralion of the aircraft This perfonnance however can be duplicated by following the staled procedures in a properly maintained airplane Effects of conditions not considered on the charts must be...

Page 138: ...SECTION 5 PERFORMANCE PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 5 2 ISSUED December 22 2017...

Page 139: ...ing Form Figure 6 11 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 After proper utilization of the information provide...

Page 140: ...anner using the existing conditions at the destination airport and when established the landing weight The conditions and calculations for the example flight are listed below The takeoff and landing d...

Page 141: ...onditions at lhe departure field to the graph Figure 5 17 Now subtract the values obtained from the graph for the field of departure condi tions from those for the cruise pressure altitude The remaini...

Page 142: ...the existing pressure altitude and temperature condjtions at the destination airport as variables to find the Lime distance and fuel values from the graph Figure 5 37 Now subtract the values obtained...

Page 143: ...e power setting from the information provided by the engine Operator s Manual The cruise Lime is found by dividing the cruise distance by the cruise speed and the cruise fuel is found by multiplying t...

Page 144: ...ight planning t xarnplc 1 Total Flight Time c 3 plus d l plus e 6 15 hr plus 17 hr plus 2 4 hrs g Total Fuel Required 2 7 hrs Determine the total fuel required by adding the fuel to climb the fuel to...

Page 145: ...off Performance 5 15 Flaps Up Takeoff GroundRoll 5 16 25 Flaps Takeoff Ground Roll 5 17 Climb Performance 5 18 Time Distanc e andFueltoClimb 5 19 Engine Performance 5 20 Engine CruisePerformance 55 5...

Page 146: ...SECTIONS PERFORMANCE PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 5 10 ISSUED December 22 2017...

Page 147: ...HER III 100 90 80 70 60 50 FAHRENHEIT 40 DEGREES 30 20 10 0 10 20 30 40 SECTION 5 PERFORMANCE 40 30 20 10 CELSIUS DEGREES 0 10 20 30 40 TEMPERATURE CONVERSION Figure 5 1 ISSUED December 22 2017 REPORT...

Page 148: ...0 100 10 IO 70 IO 80 40 AIRSPEED SYSTEM CALIBRATION 2550 LBS GROSS WEIGHT 40 1 1 API 40 80 eo 70 ao 10 100 110 120 130 140 1 0 eo 110 INDICATED AIRSPEED KIAS ZERO INSTRUMENT ERROR AIRSPEED SYSTEM CALI...

Page 149: ..._ AIR CONDITIONING OFF EXAMPLE _ Aircraft Weight 2 350 LB Angle of Bank 40 I 7 Flap Position UP Stall Speed 56 KIAS I 7 c 6 7 7 I 7 7 I I 25 24 23 22 21 20 0 10 20 30 40 50 WEIGHT LB x 100 ANGLE OF B...

Page 150: ...ross Weight 2 400 Lb Airspeed REFER TO TABLE AT RIGHT 2 450 58 lM Headwind 8Kt Propeller SENSENICH 76EM8S14 0 62 2 350 57 83 1907 Ft 2 250 56 e Takeoff Distance Flaps UP I 0 I I I z i 11 I J I I 0 __...

Page 151: ...I I I I I 1 I I ui al J N i f J w 1 1 _ _ LL w a __ 10 0 10 20 30 40 50 ClUfSU AIRTEM ERA1 JRE C TAKEOFF SPEEDS WT LIFTOFF 2 550 2 450 2 350 2 250 __ D i I 55 S5 53 50 _ I I KIAS SOFT se se 54 l L 1 C...

Page 152: ...l Tempeniture Gross Weight Headwind Takeoff Ground RoO 2 000 Fl 23 C 2 400 Lb 8 Kt 1073 Ft Flaps UP 2 250 56 o 2 800 z _ I I 1 1 S O 1 2 600 u s i f N Cl _ Jk y I r w 1 _ Ii z l w I i l s I mm 1 2 400...

Page 153: ...L IFTOFF cri l_ I 2 550 55 2 450 55 2 350 53 2 260 SO EXAMPLE Depart Airport Pressure Alt Terrperatl 1 8 G ossv kig t Hea Wncl T a eoff G olrld Roll 2 000 ft 2 f C 2 400lb 8K1 1 071 R ptj 1 1 5 I I I...

Page 154: ...CLIMB PERFORMANCE EXAMPLE Chmb Pressure Alt 4000 Ft I _ a x 8 f lll n _I 10 CJOO L _ I I I I I I Temperature 19 C Rate of Climb 487 FVMln E A _I I I I LE yEL PRESSURE 1 ALTITI JOE FT 90 ood II n a I l...

Page 155: ...takeoff EXAMPLE Depan Airport Press Aft 2000 FT Temperature Cruise Press Alt 8000 FT Cruise OAT Time to Climb 12 min mlnu 3 min 9 min Fuel to Climb 4 al minus 2 gal 2 gal Distance to Climb 17 n m min...

Page 156: ...RPM ISA Notes 1 Powers a e perrent of 180 BHP 2 Engine speeds applicable to both best power best economy mixtures 3 Propeller Sensenich 76EM6S14 0 62 _ I I I liJ 0 Q I I 0 5 10 15 2300 EXAMPLE Pressur...

Page 157: ...52 2280 ISA 10 21 70 2295 ISA 20 31 88 2305 ISA 30 41 106 2315 107 ISA 15 8 18 2285 106 ISA 7 45 2300 ISA 10 17 63 2315 ISA 20 27 81 2325 ISA 30 37 99 2335 108 ISA 15 12 10 2305 107 ISA 3 37 2320 ISA...

Page 158: ...31 88 2450 ISA 30 41 106 2465 ISA 15 8 18 2430 ISA 7 45 2450 ISA l0 17 63 2460 ISA 20 27 81 2475 ISA 30 37 99 2485 ISA 15 12 IO 2450 ISA 3 37 2470 ISA 10 13 55 2485 ISA 20 23 73 2495 ISA 30 33 91 2510...

Page 159: ...A 15 6 21 2535 ISA 9 48 2560 ISA 10 19 66 2580 ISA 20 29 84 2595 ISA 30 39 102 2615 ISA 15 8 18 2550 ISA 7 45 2575 ISA 10 17 63 2595 ISA 20 27 81 2610 ISA 30 37 99 2630 ISA 15 10 14 2565 ISA 5 41 2590...

Page 160: ...r SECTION 5 PERFORMANCE PA 28 181 ARCHER 1II Tms PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 5 24 ISSUED December 22 2017...

Page 161: ...65 K 7375 fl ISA 117 Knots _____ J_ l L 1 I I I I I I I I I I I 7 T r 1 I I I I I I I I 1 I I I I I I I I I I I 7 T r 1 I I I I I I I I _____J NOTE I I SUBTltACTl ICTASIF t WHEEL Pl NTS ARE I I REMOV...

Page 162: ...ENT DISTANCE 10000 9000 8000 7000 6000 5000 4000 3000 2000 1000 S L 500 510 I I c a 0 I w er I X 0 z 0 w I Cl UJ CJ R 0 I 520 I II 530 540 EXAMPLE Cruise Pressure All 6000 Ft Power 65 Best Economy Ran...

Page 163: ...0 C _ x S so o 75 BEST ECONOMY ly11 TURE 11 0 GPH I I I I I I I I I I 0 M ll 0 ll 0 0 0 0 CIO 0 0 co 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 O CIO O ll M N Cl l 33 1 On Lil 7 11 3tt0SS3t...

Page 164: ...o __ It Id 0 0 0 0 G 9 5 W W u E co 0 eE f o 0 lt i __ JS BEST 0 0 0 en 0 0 0 0 0 0 00 _ E CONOM Y M Tl RE 0 0 0 0 0 0 0 0 0 0 II 0 0 0 C ENDURANCE NO RESERVE Figure 5 33 It 11 0 GP _ 0 0 0 0 0 0 N 0...

Page 165: ...i J wm w oi j i uu z zw _ ffi l i3W 0 0 Z J ffi I I 1G E o 2 J O O _ E S _ sO o J G E 9 5 _ co 0 __ _ __ __ __ __ __ __ S o o 1 ll 0 11 0 GPH NOMY Ml TU E 75 BEST ECO I 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0...

Page 166: ...I II I I w 2 rr L L l 1SI 35 J t I f I I PA 28 181 ARCHER Ill I I I 11 7 I i I L L L L 0 I L a L 0 a I z uJ 0 I 0 LL i J L t a 0 0 0 ISi II I 111111 I I TIME DISTANCE AND FUEL TO DESCEND Figure 5 37 R...

Page 167: ...0 0 w w J o 0 a N 0 0 0 0 0 0 0 0 0 ci O l I i LU 0 I 0 0 0 0 0 0 0 0 0 co I D 111 0 0 0 0 0 0 0 0 0 If ri SECTION 5 PERFORMANCE 0 0 0 N 0 N IO 14 11 0 0 IO 0 0 133 t 30rllll1 t 3 lnSS d ISSUED Decem...

Page 168: ...nd Landing Olslance 2 500 FT 21 c 2 2 0 LB SKT 1 290 FT r _ I 0 L L ea v ti _ _lU _ t1 I lo_ 1 ti V y 1 y V l ll l e e Ir I _ 11 II I II I I II l Ll 0 IC IC i w z J u i i _ I I l I I r II 0 z N w z J...

Page 169: ...IM 0 32 3Nll 13 1 II I 0 0 0 I I I I I I 0 g I Ii I I J I 1 I IJ I J I II J J I I I sa oss l l rf1 x M 7Nn 13 II I y I rS C P ir 1 _ t _ Yt e 7 lo i I b __ _ __ o 1 t I a 1 1 I i i l I p J I 1 l I f C...

Page 170: ...SECTION 5 PERFORMANCE PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 5 34 ISSUED December 22 2017...

Page 171: ...TENTS SECTION6 WEIGHT AND BALANCE Page No 6 1 General 6 1 6 3 Airplane Weighing Procedure 6 2 6 5 Weight andBalance Data andRecord 6 5 6 7 Weight andBalance Determination for Flight 6 9 Equipment List...

Page 172: ...SECTION 6 WEIGHT AND BALANCE PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 6 ii ISSUED December 22 2017...

Page 173: ...e it will have Center of gravity is a determining factor in flight characteristics lf the C G is too far forward in any airplane it may be difficult to rotate for takeoff or landing If the C G is too...

Page 174: ...on and useful load Note that the useful load includes usable fuel baggage cargo and passengers Following this is the method for computing takeoff weight and C G 6 3 AIRPLANE WEIGHING PROCEDURE At the...

Page 175: ...the proper location and all entrance and baggage doors closed 6 Weigh the airplane inside a closed building to prevent errors in scale readings due to wind b Leveling I With airplane on scales block...

Page 176: ...181 airplane when it is level Refer to Leveling paragraph 6 3 b 2 The basic empty weight center of gravity as weighed including optional equipment full oil and unusable fuel can be determined by the...

Page 177: ...ber and registration number shown The basic empty weight of the airplane as certified at the factory has been entered in the Weight and Balance Record Figure 6 7 This form is provided to present the c...

Page 178: ...Optional Equipment 93 5 98 1829 9180 1 Basic Empty Weight 1731 2 88 9613 154007 1 The standar d empty weight includes full oil capacity and 2 0 gallons of unus able fuel AIRPLANE USEFUL LOAD Ramp Wei...

Page 179: ...22 i i z Tl 0 i z M 0 0 Se1ial Number 2881550 _ __ __ O Description of Article 0 l Q or Modification 0 0 o E l As licensed Registration Number N232TF Weight Change Wt Arm Moment Lb In 100 Page Number...

Page 180: ...E 0 bJ 0 w l 0 Q 0 so 0 0 E bJ 15 c s u 90 c i 8 z A 0 0 V 0 d Q pclAOUlclc PclPP v Q u g B 0 J5 A E 0 0 c o E z 0 V 0 C Q Q 0 Cl oN u1 i11 00 00 N Q C 0 0 PA 28 181 ARCHER HI WEIGHT ANDBALANCE RECOR...

Page 181: ...90 0 87 5 139125 Pilot and Front Passenger 340 0 80 5 27370 Passengers Rear Seats 340 0 i18 l 40154 Fuel 48 Gallon Maximum 288 0 95 0 27360 Baggage 200 Lbs Maximum 142 8 Ramp Weight 2558 Lbs Normal 21...

Page 182: ...m Inches 80 5 118 1 95 0 142 8 95 0 Moment In Lbs 760 Totals must be within approved weight and C G limits It is the responsibility of the airplane owner and the pilot to ensure that the airplane is l...

Page 183: ...250 7 200 V V 7 150 V I 100 V V I 0V 50 0 t 0 5 10 15 20 SECTION6 WEIGHT AND BALANCE I 0 I _ o I v S i7 v V Iv V 25 30 35 r1 l Ii I 40 45 50 MOMENT 1000 POUNDS INCHES LOADrNG GRAPH Figure 6 13 ISSUED...

Page 184: ...90 91 92 93 I I I 7 I I I I 2600 2400 2300 83 1 1 A r UTILITY CATEGORY 2200 2100 82 I 1 I I _ I 1 I I I I I I I 1 I I I 1 1 I I I 82 83 84 85 86 87 88 89 90 91 92 93 C G LOCATION INCHES AFT DATUM C G...

Page 185: ...Display Autopilot Optional Audio Panel GTX 335R Transponder Extended Squitter GTX 345R Transponder Option 7 17 Standby Instrument 7 19 Fuel System 7 21 Electrical System 7 23 Instrument Panel 7 25 Pit...

Page 186: ...SECTION7 DESCRIPTION OPERATION PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 7 ii ISSUED December 22 2017...

Page 187: ...to each side of the fuselage by insertion of the butt ends of the respective main spars into a spar box carry through which is an integral part of the fuselage structure providing in effect a continuo...

Page 188: ...low airflow into the engine in the event of blockage of the primary induction air source The air provided through the alternate air source is heated which will also provide induction system icing prot...

Page 189: ...PA 28 181 ARCHER ill 0 J i I ty __ SECTION7 DESCRIPTION OPERATION CONTROL QUADRANT AND CONSOLE Figure 7 1 ISSUED December22 2017 REPORT VB 2749 7 3...

Page 190: ...tle and mixture controls can be adjusted by using the friction adjustment lever on the right side of the control quadrant An alternate air control is located on the instrument panel right ofthe contJo...

Page 191: ...t seatS Figure 7 2 A rudder trim adjustment is mounted on the right side of the pedestal below the throttle quadrant and permits directional trim as needed in flight refer to Figure 7 1 The flaps are...

Page 192: ...SECTION7 DESCRIPTION OPERATION PA 28 181 ARCHER 111 REPORT VB 2749 7 6 fl f MAIN WHEEL ASSEMBLY Figure 7 3 Wheel fairing removed for clarity ISSUED December 22 2017...

Page 193: ...3 25 inches for the nose gear and 4 50 inches for the main gear The brake system consists of dual toe brakes attached to the rudder pedals and a hand brake lever located below behind and to the left o...

Page 194: ...ors and computers to process night and engine information for display to the pilot The system contains dual GPS SBAS receivers dual VOR ILS receivers dual VHF communications transceivers a transponder...

Page 195: ...ng information The PFD may also be used for flight planning and increased situational awareness via the Synthetic Vision and Pathways The following controls are available on the PFD clockwise from top...

Page 196: ...r is determined invalid by the internal monitors a red x is displayed over the invalid parameter If the AHRS becomes invalid a red x and amber ATTITUDE FAIL will be displayed on the attitude display T...

Page 197: ...ode for emergency use if the MFD display fails The DISPLAY BACKUP button on the audio panel should also be pressed In the composite mode the PFD will display the engine parameters typically reserved f...

Page 198: ...gratc d within SVS to provide visual and audible alerts of terrain threats relative to the projected flight path In addition to the standard TAWS or Terrain SYS alerts Terrain SYS offers a three dimen...

Page 199: ...ion These features are selected by use of the large FMS knob on the MFD The selection options disappear after IO seconds of inactivity and reappear by activating the large FMS knob Along the left side...

Page 200: ...SECTION7 DESCRIPTION OPERATION Multi Function Display continued EIS PAGE TYPICAL Figure 7 4 PA 28 181 ARCHER III REPORT VB 2749 7 14 ISSUED December 22 2017...

Page 201: ...y red on white CAS Warning text message located in the lower right area of the PFD Warnings are accompanied by a continuous triple chime which can be silenced by pressing acknowledging the Master WARN...

Page 202: ...ck annunciation CAS Caution text messages will persist until the initiating condition is removed If the Caution was initiated by a parameter whose indication appears on the Engine Indicating System EI...

Page 203: ...compass card with heading and course deviation the pilot selectable data fields transponder information and Gl000 system messages Autopilot annunciations will not be available on the MFD in the revers...

Page 204: ...of a TIS capable ground based terminal radar site Updates are available to the pilot in 5 second intervals Aircraft without a transponder are invisible to TIS and aircraft without altitude reporting...

Page 205: ...advisory and is considered to be potentially hazardous A yellow TRAFFIC annunciation is displayed al the top left of the attitude indicator on the PFD and an alert is heard in the cockpit advising Tr...

Page 206: ...rovides a system test mode to verify the TAS system is operating normally The test takes len seconds to complete When the system test is initiated a test pattern of traffic symbols appears on the Traf...

Page 207: ...ft without operating transponders The altitude difference between the requesting aircraft and other aircraft is displayed above below the traffic symbol in hundreds of feet If the traffic target is ab...

Page 208: ...1 o clock high three miles would indicate that the traffic is in front of and slightly to the left of the own aircraft above own altitude and approximately three nautical miles away A TA wiII be displ...

Page 209: ...h TSO C151b certification standards Terrain Proximity does not provide warning annunciations or voice alerts but it does provide color indications on map displays when terrain and obstacles are within...

Page 210: ...ition a yellow No OPS Position text will be displayed at the center of the Terrain Proximity Page and on the PFD inset map if terrain is selected If there is not a valid terrain obstacle database the...

Page 211: ...d obstacle data in relationto the aircraft s current altitude withoutcluller from the basemap Aviation data airports VORs and other NAVAIDs can be displayed for reference Aircraft orientation on this...

Page 212: ...o confirm accuracy of the content per TSO C 151 b standards however the displayed information should never be understood as being all inclusive and data may be inaccurate WireAware database coverage i...

Page 213: ...tion Ifa valid 3 D GPS position solution and vertical accuracy requirements are not attained or the aircraft is out of the database coverage area aTAWS NIA annunciation will appear on theTAWS B Page a...

Page 214: ...Looking Tenain Awareness FLTA alerts RTC ITI ROC IOI RLC and ILI press the INHIBIT softkey on the TAWS B Page or depress theMENU key then select Inhibit TAWS or Enable TAWS depending on the current st...

Page 215: ...ted by the map range rings or arcs On all pages that display terrain data the obstacles and terrain are depicted with the following colors Red above or within 100 feet below the aircraft altitude Yell...

Page 216: ...SECTION7 DESCRIPTION OPERATION PA 28 181 ARCHER III THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 7 30 Reserved Table 7 1 ISSUED December 22 2017 REVISED June 17 2019...

Page 217: ...est angle of climb speed Vx until terrain or obstacle clearance is assured Only vertical maneuvers are recommended unless operating in VMC or the pilot determines after using all available information...

Page 218: ...weather information and associated text is displayed on the Multi Function Display MFD and the Primary Flight Display PFD Inset Map SiriusXM satellite weather operates in the S band frequency range a...

Page 219: ...the display is the elapsed time in minutes since the weather data provider compiled the weather product This age can be significantly different newer than the actual age of the weather contained with...

Page 220: ...OV SIGMETs AIRMETs Ill 60 12 SIG AIR METARs 90 12 City Forecast 60 12 CITY Sur1ace Analysis 60 12 SFC II Freezing Levels 60 12 FRZ LVU Winds Aloft Bl 60 12 WIND County Warnings iii 60 5 COUNTY Cyclone...

Page 221: ...NT key to select the option then press the FMS knob or the CLR key to return to the Weather Data Link Page with the changed settings Customizing Weather Data Link options is also available on the Navi...

Page 222: ...instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle and has no expiration dat...

Page 223: ...iew Database The Jeppesen JeppYiew electronic charts database contafos procedure charts for the coverage area purchased An own ship position icon will be displayed on these charts This database is upd...

Page 224: ...control wheel Commands nose up or nose down pitch trim when both halves of the switch are operated simu1taneously CWS Switch Control Wheel Steering switch located on the control wheel While this swit...

Page 225: ...in default ROL and PIT modes Pressing any key associated with a valid lateral or vertical mode activates that mode and the default mode in the opposing axis For example pressing the ALT key activates...

Page 226: ...on the control wheel The autopilot will disengage automatically under the following conditions which are indicated by a red flashing AP annunciation Internal autopilot system failure Total AHRS failur...

Page 227: ...ains engaged and the pilot must add power and reduce drag according to the Go Around checklist Section 4 Underspeed Protection Optional Underspeed Protection USP is a flight director function that pro...

Page 228: ...SP provides a control force feedback to deter the pilot from operating outside a defined envelope ESP functions only when the aucopilot is operable but is disengaged As the aircraft approaches the def...

Page 229: ...r beacon audio can be heard over the headsets or cockpit speaker In addition a clearance recorder records the last 2 minutes of received audio Lights above the audio panel selection buttons indicate w...

Page 230: ...llance EHS requirements Acquisition squitter which is a 24 bit identification address transmitted periodically to enable ground stations and aircraft equipped with a Traffic Avoidance System TAS to re...

Page 231: ...RUMENT The aircraft may be eyuippt tl witli either an Aspen standby instrument or Garmin GS standby instrument Both instruments are fully digital independent tlight instrument displays which provide a...

Page 232: ...ttery allowing approximately four hours of additional operation ln this occurrence the Gannin G5 standby instrument will display a battery status indicator showing battery endurance in hours and minut...

Page 233: ...ose the backlight page To select Auto mode from Manual mode I While the unit is turned on press the Power button 2 Press the Power button again to select Auto 3 Press the knob to close the backlight p...

Page 234: ...in each wing The signal corresponding to the position of the floats is sent to the Garmin Engine Airframe GEA interface unit where it is converted into fuel quantity The fuel quantity information is...

Page 235: ...hing tanks The pump switch is located in the switch panel above the throttle quadrant The fuel drain is provided at the lowest inboard corner of each wing lank An engine fuel strainer is accessible th...

Page 236: ...I Off Ollft Al Hit FIREWALL LEFT TANK DRAIN PA 28 181 ARCHER ill FUEL NOZZLE FUEL otSTRIBUTOR FUEL INJECTOR SERVO REGULATOR _ ELECTRIC FUEL PUMP f ____ FUEL SELECTOR VAJ VE RIGHT TANK DRAIN VENT FUEL...

Page 237: ...comes lhe primary source of electrical power for the aircraft The primary battery provides stored electrical power to back up lhe alternator During normal operations the battery is charged by the alte...

Page 238: ...o show which circuil it protects Standard electrical accessories include the starter electrical fuel pump the stall warning lift detector navigational lights anti collision lights landing lights and c...

Page 239: ...PA 28 181 ARCHER Ill SECTION7 DESCRIPTION OPERATION 7 21 ELECTRICAL SYSTEM continued ALTERNATOR AND STARTER SCHEMATIC Figure 7 7 Sheet 1 of 2 ISSUED December22 2017 REPORT VB 2749 7 51...

Page 240: ...ION7 DESCRIPTION OPERATION PA 28 181 ARCHER Ill 7 21 ELECTRICAL SYSTEM continued i al la Ji Sl18 1WN3SS3 ALTERNATOR AND STARTER SCHEMATIC Figure 7 7 Sheet 2 of2 REPORT VB 2749 7 52 ISSUED December 22...

Page 241: ...ches on the instrument panel the overhead flood lights and the lighting controls on the standby instrument The dimmer switches consist of three rheostats labeled SWITCH PANEL and AVIONICS The SWITCH d...

Page 242: ...00000000000 II 00 2 0 0 0 o0 o 0 P _ Da D3 D tt i il I r 0 l 0 1 0 I 1 11 hs 0 0 PA 28 181 ARCHER Ill s o o 0 0 0 0 0 0 0 ca 0 o 0 0 I I II O t ils 0 0 I J J C 0 C a 0 u 4 0 J O I N ii bO 0 ii 0 Cl u...

Page 243: ...panel 5 MFD 6 Cabin heater temp wnd shield defroster 7 Air conditioning temp controller 8 ELT switch 9 HOBSS meter Billing optional b Pirot heat c Ventilation fan d Air conditioner option 14 Dimmer r...

Page 244: ...CRIPTION OPERATION PA 28 181 ARCHER ill 7 23 INSTRUMENT PANEL continued 0 0 l N I QJ m liHI I I 0 0 r 11_ 1 _ l Jill m ill C 0 0 REPORT VB 2749 7 56 c 00 OVERHEAD SWITCH PANEL Figure 7 10 ISSUED Decem...

Page 245: ...PA 28 181 ARCHER Ill SECTION7 DESCRIPTION OPERATION THIS PAGE INTENTIONALLY LEFT BLANK ISSUED December22 2017 REPORT VB 2749 7 57...

Page 246: ...in vents must be closed and the cabin heater and defroster must be on during alternate static source operation The altimeter error is less than 50 feet unless otherwise placarded Both the pilot and st...

Page 247: ...ICLINE l J PITOTLINE 5 1 Standby Instrument Display 2 Alternate Static Valve 3 PitoVStatic Drain Valves 4 Air Data Attitude and Heading Reference System ADAHRS 5 Pilot Head PITOT STATIC SYSTEM Figure...

Page 248: ...SECTION7 DESCRIPTION OPERATION PA 28 181 ARCHER ill HEATING AND VENTILATING SYSTEM Figure 7 12 REPORT VB 2749 7 60 ISSUED December 22 2017...

Page 249: ...duct su1face becomes hot This could result i11 bums if arms or legs are placed coo close ro hear duc1 ou1lers or surface 7 29 CABIN FEATURES The Archer has four bucket style seats with adjustable bac...

Page 250: ...arply on the shoulder strap and checking that the reel will lock in place under sudden stress This locking feature prevents the strap from extending and holds the occupant in place Under normal moveme...

Page 251: ...located on the right side of the fuselage aft of the wing An external battery can be connected to the socket thus allowing the operator to crank the engine without having to gain access to the airpla...

Page 252: ...allow the transmiller to he armed or turned on from inside the cabin The switch is normally in ARM OFF position Moving the switch to ON will activate the transmitler A warning light located above the...

Page 253: ...heck by selecting 121 50 MHz on an operating receiver If a downward sweeping audio tone is heard the ELT may have been activated Set the remote switch to ON If there is no change in the volume of the...

Page 254: ...SECTION 7 DESCRIPTION OPERATION PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 7 66 ISSUED December 22 2017...

Page 255: ...25 8 27 8 29 General Airplane Inspection Periods Preventive Maintenance Airplane Alterations Ground Handling Engine Air Filter Brake Service Landing Gear Service Propeller Service Oil Requirements Fu...

Page 256: ...SECTION 8 HANDLING SERV MAINT PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 8 ii ISSUED December 22 2017...

Page 257: ...ion is incorporated on the airplane those portions of the airplane affected by the instaJJation must be inspected in accordance with the inspection program published by the owner of the STC Since non...

Page 258: ...ferent in fabrication techniques and materials and may be dangerous when instaUed in an airplane Additionally reworked or salvaged parts or those parts obtained from non PIPER approved sources may hav...

Page 259: ...tance and Piper considers compliance mandatory These are available on the Piper com website Depending on the nature of the release material and labor allowances may apply This information is provided...

Page 260: ...tains appropriate forms and all inspection procedures should be complied with by a properly trained knowledgeable and qualified mechanic at a Piper Authorized Service Center or a reputable repair shop...

Page 261: ...in preventive maintenance as defined in the FARs This maintenance may be perfo1med only on an aircraft which the pilot owns and operates and which is not used in air canier or air taxi commercial oper...

Page 262: ...t a To be displayed in the aircraft at all times I Aircraft Afrworthiness Certificate Form FAA 8100 2 2 Aircraft Registration Certificate Form FAA 8050 3 3 Aircraft Radio Station License if transmitte...

Page 263: ...d In the event towing lines are necessary ropes should be attached to both main gear struts as high up on the tubes as possible Lines should be long enough to clear the nose and or tail by not less th...

Page 264: ...rcraft When parking the airplane for any length of time or overnight it is suggested that it be moored securely J To park the airplane head it into the wind if possible 2 Sec the parking brake by pull...

Page 265: ...it snug 4 Block the wheels 5 Secure tie down ropes to the wing tie down rings and to the tail skid at approximately 45 degree angles to the ground When using rope of non synthetic material leave suf...

Page 266: ...requent attention 8 13 BRAKE SERVICE The brake system is filled with MIL PRF 5606 petroleum hase hydraulic brake fluid The fluid level should be checked periodically or al every 50 hour inspection and...

Page 267: ...EDAL 4 RIGHT BRAKE CYLINDER 5 LEFT BRAKE CYLINDER 6 BRAKE HANDLE 7 HANDLE RELEASE BUTTON 8 LINE INLET 9 CLEVIS PIN 10 MASTER CYLINDER ASSEMBLY 11 BOLT ASSEMBLY 12 TORQUE TUBE 13 COPILOT S RIGHT BRAKE...

Page 268: ...w that required refer to Maintenance Manual for servicing instructions 8 17 PROPELLER SERVICE The spinner and backing plate should be frequently cleaned and inspected for cracks Before each flight the...

Page 269: ...ge is not to exceed four 4 months NOTE Refer LO the latest revision of Lycoming Service Instruction 1014 Lubricating Oil Recom mendations for further information 8 21 FUEL SYSTEM a Servicing Fuel Syst...

Page 270: ...inant s such as water or sediment Each fuel tank is equipped with an individual quick drain located at the lower inboard rear corner of the tank The fuel strainer is equipped with a quick drain locate...

Page 271: ...urn counterclockwise to hold the drain open The remaining fuel in the system may be drained through tbe filter bowl Any individual tank may be drained by closing the selector valve and then draining t...

Page 272: ...allation Unbalanced wheels can cause extreme vibration in the landing gear therefore in the installation of new components it may be necessary 10 rebalance the wheels with the tires mounted When check...

Page 273: ...eaning Exterior Surfaces The airplane should be washed with a mild soap and water Harsh abrasives or alkaline soaps or detergents could make scratches on painted or plastic surfaces or could cause cor...

Page 274: ...surfaces apply a thin coat of hard polishing wax Rub lightly with a soft cloth Do not use a circular motion 5 A severe scratch or mar in plastic can be removed by rub bing out the scratch with jeweler...

Page 275: ...old carpet 8 29 COLD WEATHER OPERATION For cold weather operation a winterization plate is installed on the inlet openjng of the oil cooler duct on the left rear engine baffle This plate should be ins...

Page 276: ...SECTION 8 HANDLING SERV MAINT PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 8 20 ISSUED December 22 2017...

Page 277: ...DME 4 pages 9 19 Appareo Vision 1000 Unit 4 pages 9 23 Flightcom Model 403 Intercom 4 pages 9 27 Carbureted 0 360 Engine Installation 22 pages 9 31 I MSAFE Inflatable Seat Restraints STC SA02276AK 9...

Page 278: ...SECTION 9 SUPPLEMENTS PA 28 181 ARCHER Ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 9 ii ISSUED December 22 2017...

Page 279: ...en equipped with one or more of the various optional systems and equipment not approved with the standard airplane All of the supplements provided in this section are FAA Approved and consecutively nu...

Page 280: ...SECTION 9 SUPPLEMENTS PA 28 181 ARCHER Ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 9 2 ISSUED December 22 2017...

Page 281: ...ok and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedures and performance information not contained in this supplement consult the Pilot s Operating Handb...

Page 282: ...air conditioner must be turned OFF manually before the landing approach in preparation for a possible go around b Placards In full view of the pilot in the area of the air conditioner controls when th...

Page 283: ...Prior to takeoff the air conditioner should be checked for proper operation as follows a Check aircraft battery switch ON b Turn the air conditioner control switch to ON and the fan switch to one of...

Page 284: ...ompressor is operating continuously while the airplane is airborne This will be the case only in extremely hot weather a The decrease in true airspeed is approximately 4 KTS at all power settings b Th...

Page 285: ...ts located adjacent to each occupant The switches are located to the left of the the throttle quadrant and the temperature control is located on the right side of the instrument panel The temperature...

Page 286: ...d on the circuit breaker panel protects the air conditioning electrical system Whenever the throttle is in the full throttle position it actuates a micro switch which disengages the compressor and ret...

Page 287: ...ht Display PFD Indicator is installed per the Equipment List The information contained herein supplements or supersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in t...

Page 288: ...ory circuit no battery power required and displayed in self dimming gas discharge numer ics The active frequency is continuously displayed in the lef t window while the right window will display eithe...

Page 289: ...pit speaker 7 OFFNOL Control SET to desired volume level 8 ADF Bearing Display ADF bearing on PFD by selecting I be PFD soft key then pressing the BRGI or BRG2 softkey until ADP is displayed in the ap...

Page 290: ...desired time in the elapsed time display The small knob is pulled out to tune the I s The small knob is pushed in to tune the IO s The outer knob tunes minutes up to 59 min utes NOTE Selector knobs r...

Page 291: ...ening for station call letters Eleclrical S1orms ln the vicinity of electrical storms an ADF indicator pointer Lends to swing rrom the station tuned toward the center of the storm Night Effec1 This is...

Page 292: ...ICHT AND BALANCE PA 28 181 ARCHER ID Factory installed optional equipment is included in the certified weight and balance data in Section 6 or the Pilot s Operating Handbook and Airplane Flight Manual...

Page 293: ...ERATION 1 2 3 13 12 11 4 5 10 9 KR 87 Digital ADF 14 6 ADF Displays on Garmin PFD 8 SECTION 9 SUPPLEMENT 2 7 T REF T MSG DigiLal ADF Operating Controls and PFD Indicator Figure I ISSUED December 22 20...

Page 294: ...ed permits the carrier wave and associated morse code identifier broadcast on the carrier wave 10 be heard NOTE CW signals Morse Code arc unmodulated and no audio will be heard without use of BFO This...

Page 295: ...s audio level Audio mul ing causes the audio oulpul to be muted unless the receiver is locked on a valid station 9 Set Reset Bullon SET RST The set reset bullon when pressed resets the elapsed timer w...

Page 296: ...SECTION 9 SUPPLEMENT 2 PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 9 18 I0ofl0 ISSUED December 22 2017 REVISED May 7 2018...

Page 297: ...pment List The information contained herein supplements or supersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedure...

Page 298: ...required NOTE When the VORTAC or VOR DME frequency is selected the appropriate DME frequency is automatically channeled 2 DME 1DENTTFTCATION select DME button on audio panel audio 1D will always come...

Page 299: ...or HOLD as selected in the DME TUNING window 17 3 4 6NH 3 FREQUENCY Displays the fr equency of the VOR DME or VORTAC selected on the associated navigation radio or the frequency being held HOLD that w...

Page 300: ...to station which was last channeled when HOLD was selected and will continue to display information relative to this channel Allows both theNAV 1 and NAV 2 navigation receivers Lo be set to new opera...

Page 301: ...upersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedures and performance information not contained in this suppleme...

Page 302: ...s system does not require flighc crew imerface during aircraft operacion The flight crew need only ensure that an Appareo SD card is in the Vision 1000 prior to flight operations NOTE During low light...

Page 303: ...andverifyGreen LED SD card not formattedcorrectly format SD to NTSF verify Green LED GPS lock not received Allow 15 minutes to clear if problem persists contact Appareo 5 NO LED Not functioning Refer...

Page 304: ...ambient audio recording It will record the aircraft s airfr ame attitudes rates accelerations GPS position and record cockpit audio and images The Vision I000 system is protected via an in line fuse l...

Page 305: ...or supersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedures and performance information not contained in this sup...

Page 306: ...one plug but without a Mono setting will cause only one earphone to be active The Flightcom model 403 intercom does not have a dedicated circuit breaker but is protected via an in line fuse located be...

Page 307: ...noise levels NOTE If you set the squelch too high by turning the Squelch control knob counterclockwise your voice will be cut out unless you talk very loudly if you set the squelch too low by turning...

Page 308: ...AND OPERATION See Flightcom Model 403 Panel Mount Intercom Installation Operation Manual for a complete description of the Flightcom model 403 system www Flightcom net The Flightcom 403 panel mount i...

Page 309: ...dbook and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedures and performance information not contained in this supplement consult the Pilot s Operating Ha...

Page 310: ...ation contained within this supplement is to be used as described in conjunction with the complete handbook 1 5 ENGINES c Engine Model Number Carbureted i Engine Type SECTION 2 LIMITATIONS 2 7 POWERPL...

Page 311: ...unway remains Airspeed MAINTAIN SAFE AIRSPEED Flaps AS REQUIRED NOTE Make only shallow turns to avoid obstrnctions If sufficient altitude has been gained to attempt a restart Airspeed MAINTAIN 76 KIAS...

Page 312: ...ruption attempt to restore power by turning the fuel pump ON and selecting the other fuel tank Move the throttle and mixture control levers to different settings This may restore power if the problem...

Page 313: ...t temperatures of 5 C to 20 C it is possible for ice to form in theinduction system Thisis due to the high air velocity through the carburetor venturi and the absorption of heat from this air by vapor...

Page 314: ...HECK LEFr RIGHT MAG Switches Individually Select OFF and ON If operation is satisfactory on either MAG continue on that magneto at reduced power and full RICH mixture to nearest airport Preparefor pow...

Page 315: ...STED and LOCKED IN POSITION Seat Belts and Harness FASTEN ADJUST CHECK INERTIA REEL FUEL Selector DESIRED TANK PARK BRAKE SET Circuit Breakers CHECK IN CARB HEAT OFF ALTERNATE STATIC SOURCE OFF All El...

Page 316: ...some time by the primary electrical system If E VOLTS is still less than 23 3 volts determine the cause and correct the issue prior to flight 4 5d Engine Start Checklists NORMAL START COLD ENGINE THRO...

Page 317: ...may form in the carburetor causing excessive fuel delivered to the intake resulting in increased chance of engine fire To minimize this it is recommended the aircraft be parked pointed into the wind w...

Page 318: ...rgency procedure for Engine Fire During Start THROTTLE OPEN FULL BATT MASTR Switch ON ALTR Switch ON LEFT MAG Switch ON FUEL PUMP OFF MIXTURE IDLE CUT OFF CAS Messages CONSIDER ANY ILLUMINATED PFD Ann...

Page 319: ...L RICH CAS Messages CONSIDER ANY ILLUMINATED PFD Annunciations CONSIDER ANY ILLUMINATED Propeller CLEAR START Switch PRESS RIGHT MAG Switch ON Oil Pressure CHECK BATT MASTR Switch ON THROTTLE LOWEST P...

Page 320: ...LTS indication less than 23 3 VOLTS during BEFORE STARTING ENGINE Checklist EMERG BATT Switch Verify ARM AYION MASTER Switch OFF ALTR Switch OFF BATT MASTR Switch OFF E VOLTS Indication 23 3 VOLTS MIN...

Page 321: ...r LATCHED Air Conditioner if installed OFF NOTE TAS aural alerts will be muted when GPS altitude is lower than 400 FT AGL Takeoff should not be attempted with ice snow or frost on the wings To achieve...

Page 322: ...xture control leaned as required Power response should be verified approximately every30seconds by partially opening and then closing the throttle clearing the engine When leveling off enrichen mixtur...

Page 323: ...The ARCHER Ill is powered by a four cylinder direct drive horizontally opposed engine rated at 180 horsepower at 2700 rpm It is furnished with a starter a 70 ampere 28 volt alternator a shielded igni...

Page 324: ...of the conLrol quadrant The conLrol displays two positions ON down OFF up 7 19 FUEL SYSTEM An electric engine priming system is provided to facilitate starting The primer switch is located right of tb...

Page 325: ...SELECTOR VALVE F lhdlc allon MULTIFUNCTION DISPLAY SECTION 9 SUPPLEMENT 6 FUEL PRIMER SOLENOID RIGHT MAIN TANK FUEL SYSTEM SCHEMATIC Carbureted Engine Figure 7 6 7 23 INSTRUMENT PANEL The instrument p...

Page 326: ...2749 9 48 18 of 22 g D 000 0 o o 000 0000000 00 0000000000 00 9_ o0 o 0 II I iii t0 lU I 0 0 0 PA 28 181 ARCHER III 0 s o o 0 0 0 0 0 0 0 0 0 0 0 N 0 0 ZJ I c Q c 0 0 t 0 O 0 c Q Q rn 0 INSTRUMENT PAN...

Page 327: ...temp controller 8 ELT switch 9 HOBSS meter Billing optional 10 HOBSS meter Maintenance optional 11 Circuit breakers 12 Carb heat 13 Electrical accessories L to R a Flight director autopilot switch opt...

Page 328: ...NT 6 PA 28 181 ARCHER III I 7 23 INSTRUMENT PANEL continued 0 0 1m1 m 0 0 rn m Jill 0 0 REPORT VB 2749 9 50 20 of 22 c co cl 0 I C oo C w OVERHEAD SWITCH PANEL Figure 7 10 ISSUED December 22 2017 REVI...

Page 329: ...NDLING SERVIClNG AND MAINTENANCE 8 21 FUEL SYSTEM a Servicing Fuel System At every 50 hour inspection the fuel screens in the strainer in the electric fuel pump and at the carburetor inlet must be cle...

Page 330: ...SECTION 9 SUPPLEMENT 6 PA 28 181 ARCHER ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 ISSUED December 22 2017 9 52 22 of 22...

Page 331: ...nclude the AMSAFE Inflatable Seal Restraints supplement in this location of the Pilot s Operating Handbook unless otherwise stated by AMSAFE The information contained in the AMSAFE Inflatable Seal Res...

Page 332: ...SECTION 9 SUPPLEMENT 7 PA 28 181 ARCHER Ill THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 9 54 ISSUED December 22 2017...

Page 333: ...nclude the Continental Aerospace Technologies diesel engine TAE 125 02 114 supplement in this location of the Pilot s Operating Handbook unless otherwise stated by Continental Aerospace Technologies T...

Page 334: ...SECTION9 SUPPLEMENT8 PA 28 181 ARCHER III TIDS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 I 9 56 ISSUED December 22 2017 REVISED August 29 2019...

Page 335: ...stalled per the Equipment List The information contained herein supplements or supersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in those areas listed herein For l...

Page 336: ...receives and displays angle of attack information from the lift transducer vane installed in the right wing of the aircraft SECTION 2 LIMITATIONS 1 The angle of attack system provides advisory inform...

Page 337: ...uminated not blank NOTE IfAoA indications aresuspected to not be accurate discontinue use of the AoA Indicator NOTE If the AoA Indicator screen turns off after the power on self test check that the AO...

Page 338: ...displays Angle of Attack AoA information from the lift transducer on the leading edge of the right wing The position of the lift transducer vane on the wing s leading edge is converted to AoA within t...

Page 339: ...minate giving the pilot awareness of where the reference marker is being set Holding the top button for four seconds mutes or unmutes the audio Holding the bottom bullon for two seconds dims or bright...

Page 340: ...erence marker can be set to a target angle of attack for the desired phase of flight During the takeoff roll as airflow increases over the wing the AoA indication will change to a representative in fl...

Page 341: ...then will illuminate a particular light segment on the display Note which light segments illuminated as this will aid in diagnosing the problem When contacting support have the following information a...

Page 342: ...SECTION9 SUPPLEMENT 9 PA 28 181 ARCHER lil THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 2749 I 9 64 s ors ISSUED December 22 2017 REVISED March 27 2020...

Page 343: ...The information contained herein supplements or supersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedures and perfo...

Page 344: ...quart marking as the minimum capacity indication SECTION 2 LIMITATIONS 9 The addition of a second oil cooler significantly increases the capability of the engine oil system to reject heat As a result...

Page 345: ...rature exceedance CAS Event Cylinder head temperature approaching limit CAS Message Checklist Page Cause CAS Warnings with Text Messages CYLHDTEMP 9 68 Cylinder head temperature on at least one cylind...

Page 346: ...REDUCING MIXTURE Consider ENRICHENING Airspeed Consider INCREASING If cylinder head temperatures continue to rise Indication Master Warning Triple Chime CYLHDTEMP THROTTLE MINIMUM REQUIRED MIXTURE RI...

Page 347: ...ht Manual SECTION 7 DESCRIPTION AND OPERATION 7 5 ENGINE AND PROPELLER A second oil cooler identical to the primary oil cooler is attached to the forward side of the firewall on the right side ofthe e...

Page 348: ...drain into the engine oil sump Continue to use the 8 quart marking on the oil dipstick as the maximum capacity indication and the 2 quart marking as the minimum capacity indication 8 29 COLD WEATBER O...

Page 349: ...The information contained herein supplements or supersedes the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only in those areas listed herein For limitations procedures and perfo...

Page 350: ...ITATIONS No change SECTION 3 EMERGENCY PROCEDURES No change SECTION 4 NORMAL PROCEDURES No change SECTION 5 PERFORMANCE No change SECTION 6 WEIGHT AND BALANCE No change REPORT VB 2749 I 9 12 2 or 4 PA...

Page 351: ...ctor valve and from there into the fuel tank that is selected to feed fuel to the engine This fuel selector valve controls both the fuel feed and fuel return selection with a single control Unlike the...

Page 352: ...FUEL INJECTION SERVO _ ENGINE DRIVEN FUEL PUMP _ AIRCRAFT ELECTRIC FUEL PUMP FILTER AND DRAIN FIREWALL _____ SUPPLY LINE TO ENGINE ___ FUEL SELECTOR VALVE OPTIONAL RETURN LINE SUPPLY LINE LEFT TANK DR...

Page 353: ...PA 28 181 ARCHER III TABLE OF CONTENTS SECTION 10 OPERATING TIPS SECTION 10 OPERATING TIPS Paragraph Page No No L0 l General 10 1 I0 3 Operating Tips I 0 1 ISSUED December 22 2017 REPORT VB 2749 10 i...

Page 354: ...SECTION 10 OPERATING TIPS PA 28 181 ARCHER Ill TIDS PAGE INTENTIONALLY LEFf BLANK REPORT VB 2749 10 ii ISSUED December 22 2017...

Page 355: ...ore extending the flaps The flap step will not support weight if the flaps are in any extended position The flaps must be placed in the UP position before they will lock and support weight on the step...

Page 356: ...ilots should obtain and study the safety related information made available in FAA publications such as regulations advisory circulars Aviation News AIM and safety aids i Prolonged slips or skids whic...

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