Piper ARCHER II Pilot Operating Handbook
  1. Manuals
  2. Brands
  3. Piper Manuals
  4. Aircrafts
  5. ARCHER II
  6. Pilot operating handbook

Piper ARCHER II Pilot Operating Handbook

Hide thumbs
Table of Contents

Advertisement

Quick Links

Download this manual
AIRPLANE
SERIAL NO. ________________________
PA-28-181
REPORT: VB-1120
DATE OF APPROVAL:
JULY 2, 1979
FAA APPROVED I N 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.
21.04.2018 added AFMS Fuel STC
05.07.2018 added AFMS G5 Instrument
30.04.2019 added GNS430W Upgrade
30.04.2019 added AFMS GFC500 Autopilot
28 - 8390087
FAA APPROVED BY: ________________________________
ARCHER II
OPERATING
HANDBOOK
AIRPLANE FLIGHT MANUAL
AIRPLANE
REGIST. NO. _____________________
WARD EVANS
D.O.A. NO. SO-1
PIPER AIRCRAFT CORPORATION
VERO BEACH, FLORIDA
PA-28-181
PILOT'S
AND
FAA APPROVED
OE-KBS

Advertisement

Table of Contents
loading
Need help?

Need help?

Do you have a question about the ARCHER II and is the answer not in the manual?

Questions and answers

Subscribe to Our Youtube Channel

Related Manuals for Piper ARCHER II

Summary of Contents for Piper ARCHER II

  • Page 1 ARCHER II PA-28-181 PILOT’S OPERATING HANDBOOK FAA APPROVED AIRPLANE FLIGHT MANUAL AIRPLANE 28 - 8390087 AIRPLANE OE-KBS SERIAL NO. ________________________ REGIST. NO. _____________________ PA-28-181 REPORT: VB-1120 FAA APPROVED BY: ________________________________ WARD EVANS D.O.A. NO. SO-1 DATE OF APPROVAL: PIPER AIRCRAFT CORPORATION...
  • Page 2 P I P E R M U S T PROPERLY INSERTED. Published by TECHNICAL PUBLICATIONS Piper Aircraft, Inc. Issued: July 2, 1979 © 1979–1986, 1988, 1990, 1993–1994, 1998, 2019 Piper Aircraft, Inc. All Rights Reserved REPORT: VB-1120 REVISED: APRIL 1, 2019...
  • Page 17 PILOT’S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision FAA Approved Number and Revised Description of Revisions Signature Code Pages and Date Rev. 14 vi-k Added log of revision page (PR930107) vi-l Added log of revision page Added Supplement 11 to T.O.C. 9-77 Added Supplement 11 W.
  • Page 18 PILOT’S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision FAA Approved Number and Revised Description of Revisions Signature Code Pages and Date REPORT: VB-1120 vi-l...
  • Page 91 PIPER AIRCRAFT CORPORATION SECTION 5 PA-28-181, ARCHER II PERFORMANCE 5.5 FLIGHT PLANNING EXAMPLE (a) Aircraft Loading The first step in planning the flight is to calculate the airplane weight and center of gravity by utilizing the information provided by Section 6 (Weight and Balance) of this handbook.
  • Page 92 SECTION 5 PIPER AIRCRAFT CORPORATION PERFORMANCE PA-28-181, ARCHER II (b) Takeoff and Landing After determining the aircraft loading, all aspects of takeoff and landing must be considered. Conditions of the departure and destination airport must be acquired, evaluated and maintained throughout the flight.
  • Page 118 TABLE OF CONTENTS SECTION 6 WEIGHT AND BALANCE Paragraph Page General ..................Airplane Weighing Procedure ..........Weight and Balance Data and Record........ Weight and Balance Determination for Flight ....Instructions for Using the Weight and Balance Plotter ..6-12a 6.11 *Equipment List ..............
  • Page 126 Weight and Balance Change Report Aircraft Type : PA28-181 Serial Number : 28-8390087 Registration : OE-KBS Date : 29.03.2022 : V20176/22 Description: Installation of Garmin GNC 255A WEIGHT MOMENT (kg) (kg m) BASIC WEIGHT AS OF 731,20 2,228 1628,927 30.04.2019 INSTALLED Garmin GNC 255A 2,88...
  • Page 162 Not implemented...
  • Page 164 Not implemented...
  • Page 175 PIPER AIRCRAFT CORPORATION SECTION 8 PA-28-181, ARCHER II HANDLING, SERV & MAINT BRAKE SYSTEM Figure 8-1 ISSUED: JULY 2, 1979 REPORT: VB-1120...

  • Page 176: Landing Gear Service

    Landing gear oleos on the Archer II should be serviced according to the instructions on the units. The main oleos should be extended under normal static load until 4.50 ±...
  • Page 187 --------------------------------------- 19 GFC500 Autopilot System...
  • Page 203 Piper PA28-181 OE-KBS 28-8390087...
  • Page 204 © Copyright 2017 Garmin Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or printed copy of this manual or revision must contain the complete text of...
  • Page 205 Garmin International, Inc Log of Revisions FAA Approved AIRPLANE FLIGHT MANUAL SUPPLEMENT SUPPLEMENTAL AIRPLANE FLIGHT MANUAL GARMIN G5 ELECTRONIC FLIGHT INSTRUMENT DATE OF PAGE NO(S) DESCRIPTION FAA APPROVED APPROVAL Robert Murray Original Issue 7/22/2016 ODA STC Unit Administrator Robert Murray Added information regarding...
  • Page 206 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page ii...
  • Page 207 Table of Contents Section 1 – General ....................1-1 Abbreviations and Terminology ......................1-2 Section 2 – Limitations ....................2-1 System Software Requirements ......................2-1 Use of Secondary Instruments ......................2-1 Kinds of Operations ..........................2-1 Section 3 – Emergency Procedures ................. 3-1 G5 Failure Indications ..........................
  • Page 208 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page iv...

  • Page 209: Section 1 - General

    SECTION 1 – GENERAL The G5 Electronic Flight Instrument can display the following information to the pilot depending on the installation and location of the G5 instrument. • Primary attitude • Primary slip and turn rate information • Primary heading •...

  • Page 210: Abbreviations And Terminology

    Abbreviations and Terminology The following glossary is applicable within the airplane flight manual supplement Attitude Direction Indicator AFMS Airplane Flight Manual Supplement Attitude Course Deviation Indicator Directional Gyro Dead Reckoning Federal Aviation Administration Global Positioning System GPSS GPS Roll Steering Heading Horizontal Situation Indicator Instrument Landing System...

  • Page 211: Section 2 - Limitations

    SECTION 2 – LIMITATIONS System Software Requirements The G5 must utilize the following or later FAA approved software versions for this AFMS revision to be applicable: Component Software Version G5 Electronic Flight Instrument 5.00 Use of Secondary Instruments The original type design approved instruments for airspeed, altitude and vertical speed remain the primary indications for these parameters.
  • Page 212 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 2–2...

  • Page 213: Section 3 - Emergency Procedures

    SECTION 3 – EMERGENCY PROCEDURES G5 Failure Indications If a G5 function fails, a large red ‘X’ is typically displayed over the instrument(s) or data experiencing the failure. Upon G5 power-up, certain instruments remain invalid as equipment begins to initialize. All instruments should be operational within one minute of power-up.

  • Page 214: Gps Failure

    GPS Failure If GPS navigation receivers and/or navigation information are not available or invalid, the G5 will display Dead Reckoning mode (DR) or Loss of Integrity mode (LOI) on the HSI in the lower left corner. If Alternate Navigation Sources (ILS, LOC, VOR) Are Available: 1.

  • Page 215: Loss Of Electrical Power To The Gad 29B (If Installed)

    Loss of Electrical Power to the GAD 29B (If Installed) In the event of a loss of aircraft electrical power to the optional GAD 29B, the heading and course datum will be unavailable to the autopilot and the autopilot may deviate from the intended path or may disconnect. GPS flight plan course information may be displayed on the HSI and VFR will be displayed in amber text on the HSI.
  • Page 216 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 3–4...

  • Page 217: Section 4 - Normal Procedures

    SECTION 4 – NORMAL PROCEDURES G5 Power Button and Knob The G5 display will power on with the application of aircraft power. The G5 power button is used to turn the display on and off. Press and hold the power button to turn the display off. The knob performs the following functions: Press to access the Menu.

  • Page 218: Autopilot Operations With The G5 Hsi

    Autopilot Operations with the G5 HSI The G5 and optional GAD 29B offer various integration capabilities dependent upon the type of autopilot installed in a particular aircraft. The G5 Electronic Flight Instrument installation in this aircraft provides the following autopilot functions (appropriate boxes will be checked): ...
  • Page 219 navigator. If the GPSS data is invalid (for example, if there is no active GPS leg) or the selected HSI source on the G5 HSI is not GPS, the annunciated GPSS text will be yellow and a zero turn command will be sent to the autopilot.
  • Page 220 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 4–4...

  • Page 221: Section 5 - Performance

    SECTION 5 – PERFORMANCE No change. 190-01112-13 Rev. 5 AFMS, Garmin G5 AML STC Page 5–1...
  • Page 222 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 5–2...

  • Page 223: Section 6 - Weight And Balance

    SECTION 6 – WEIGHT AND BALANCE See current weight and balance data. 190-01112-13 Rev. 5 AFMS, Garmin G5 AML STC Page 6–1...
  • Page 224 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 6–2...

  • Page 225: Section 7 - System Description

    SECTION 7 – SYSTEM DESCRIPTION Refer to Garmin G5 Electronic Flight Instrument Pilot’s Guide for Certified Aircraft, part number 190-01112-12 Rev A (or later approved revisions), for a description of the G5 electronic flight instrument. This reference material is not required to be on board the aircraft but does contain a more in depth description of all the functions and capabilities of the G5.
  • Page 226 The following table shows the meaning of each message. System messages are displayed in white text. Message Meaning External Power Lost Aircraft power has been removed from the G5. Critical battery fault! Battery has critical fault condition and the unit is about to power off to avoid Powering off damage to the battery.

This manual is also suitable for:

Pa-28-181

Table of Contents