Piper PA-28-161 Pilot Operating Handbook
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Piper PA-28-161 Pilot Operating Handbook

Piper PA-28-161 Pilot Operating Handbook

Warrior ii
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See also: Maintenance Manual
REFERENCE ONLY
THIS ELECTRONIC VERSION
OF THE POH IS
NOT APPROVED TO
REPLACE ANY OPERATING
INFORMATION REQUIRED
BY THE REGULATIONS.
AirplAne
seriAl no.
pA-28-161
report: vb-1180 fAA Approved by:
dAte of ApprovAl:
August 13, 1982
faa approved in normal and utility categories based on car 3. this
handbook includes the material required to be furnished to the pilot
by car 3 and constitutes the approved airplane flight manual and must
be carried in the airplane at all times.
wArrior ii
AirplAne flight mAnuAl
AirplAne
regist. no.
wArd evAns
d.o.A. no. so-1
piper AircrAft corporAtion
vero beAch, floridA
pA-28-161
pilot's
operAting
hAndbook
And
fAA Approved

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  • Page 1 Approved by: wArd evAns d.o.A. no. so-1 dAte of ApprovAl: piper AircrAft corporAtion August 13, 1982 vero beAch, floridA faa approved in normal and utility categories based on car 3. this handbook includes the material required to be furnished to the pilot by car 3 and constitutes the approved airplane flight manual and must be carried in the airplane at all times.
  • Page 2 ExtrEmE carE must bE ExErcisEd to limit thE usE of this handbook to applicablE aircraft. this hand- book is valid for usE with thE airplanE idEntifiEd on thE facE of thE titlE pagE. subsEquEnt rEvisions suppliEd by pipEr aircraft corporation must bE propErly insErtEd. Published by PUBLICATIONS DEPARTMENT Issued: August 13, 1982 ©...
  • Page 4 APPLICABILITY Application of this handbook is limited to the specific Piper PA-28-161 model airplane designated by serial number and registration number on the face of the title page of this handbook. This handbook cannot be used for operational purposes unless kept in a current status.
  • Page 5 REVISIONS The information compiled in the Pilot’s Operating Handbook, with the exception of the equipment list, will be kept current by revisions distributed to the airplane owners. The equipment list was current at the time the airplane was licensed by the manufacturer and thereafter must be maintained by the owner.
  • Page 8 PIPER AIRCRAFT CORPORATION PA-28-161, WARRIOR II PIlOT’S OPERATING hANDBOOk lOG OF REVISIONS Revision FAA Approval Number and Revised Description of Revisions Signature and Code Pages Date Rev. 7 (cont) 2-3b Page added. Revised para. 7.5. Revised para. 8.5. D. H. Trompler Oct.
  • Page 9 PIPER AIRCRAFT CORPORATION PA-28-161, WARRIOR II ThIS PAGE INTENTIONAlly lEFT BlANk REPORT: VB-1180 ISSUED: AUGUST 13, 1982 vi-b...

  • Page 31: Placards

    PIPER AIRCRAFT CORPORATION SECTION 2 PA-28-161, WARRIOR II LIMITATIONS 2.25 PLACARDS In full view of the pilot: THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS AND MANUALS.
  • Page 32 SECTION 2 PIPER AIRCRAFT CORPORATION LIMITATIONS PA-28-161, WARRIOR II In full view of the pilot, in the area of the air conditioner control panel when the air conditioner is installed: WARNING — AIR CONDITIONER MUST BE OFF TO INSURE NORMAL TAKEOFF CLIMB PERFORMANCE.

  • Page 40: Loss Of Oil Pressure

    PIPER AIRCRAFT CORPORATION SECTION 3 PA-28-161, WARRIOR II EMERGENCY PROCEDURES LOSS OF OIL PRESSURE Land as soon as possible and investigate cause. Prepare for power off landing. LOSS OF FUEL PRESSURE Electric fuel pump ..................ON Fuel selector ................check on full tank HIGH OIL TEMPERATURE Land at nearest airport and investigate the problem.

  • Page 41: Spin Recovery

    SECTION 3 PIPER AIRCRAFT CORPORATION EMERGENCY PROCEDURES PA-28-161, WARRIOR II If alternator loads are reduced: Electrical load ..............Reduce to Minimum Land as soon as practical. NOTE Due to increased system voltage and radio frequency noise, operation with ALT switch ON and BATT switch OFF should be made only when required by an electrical system failure.

  • Page 48: High Oil Temperature

    PIPER AIRCRAFT CORPORATION SECTION 3 PA-28-161, WARRIOR II EMERGENCY PROCEDURES 3.21 HIGH OIL TEMPERATURE An abnormally high oil temperature indication may be caused by a low oil level, an obstruction in the oil cooler, damaged or improper baffle seals, a defective gauge, or other causes.

  • Page 49: Spin Recovery

    SECTION 3 PIPER AIRCRAFT CORPORATION EMERGENCY PROCEDURES PA-28-161, WARRIOR II Turn the BATT switch OFF and the ammeter should decrease. Turn the BATT switch ON and continue to monitor the ammeter. If the alternator output does not decrease within 5 minutes, turn the BATT switch OFF and land as soon as possible.
  • Page 138 PIPER AIRCRAFT CORPORATION SECTION 7 PA-28-161, WARRIOR II DESCRIPTION & OPERATION The annunciator panel includes alternator and low oil pressure indicator lights. When the optional gyro system is installed, the annunciator panel also includes a low vacuum indicator light. The annunciator panel lights are provided...
  • Page 139 SECTION 7 PIPER AIRCRAFT CORPORATION DESCRIPTION & OPERATION PA-28-161, WARRIOR II ALTERNATOR AND STARTER SCHEMATIC Figure 7-11 REPORT: VB-1180 ISSUED: AUGUST 13, 1982 7-12...

  • Page 157: General

    STC installations. WARNING Modifications must be approved in writing by PIPER prior to installation. Any and all other installations, whatsoever, of any kind will void this warranty in it’s entirety.
  • Page 158 HANDLING, SERV & MAINT PA-28-161, WARRIOR II 8.1 GENERAL (CONTINUED) WARNING Use only genuine PIPER parts or PIPER approved parts obtained from PIPER approved sources, in connection with the maintenance and repair of PIPER airplanes. Genuine PIPER parts are produced and inspected under rigorous procedures to insure airworthiness and suitability for use in PIPER airplane applications.
  • Page 159 Piper’s support systems. Piper takes a continuing interest in having owners get the most efficient use from their airplane and keeping it in the best mechanical condition. Consequently, Piper, from time to time, issues service releases including Service Bulletins, Service Letters, Service Spares Letters, and others relating to the airplane.

  • Page 160: Airplane Inspection Periods

    Appropriate forms are contained in the applicable Piper Service/Maintenance Manual, and should be complied with by a properly trained, knowledgeable, and qualified mechanic at a Piper Authorized Service Center or a reputable repair shop. Piper cannot accept responsibility for the continued airworthiness of any...

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