NAVIGATION AND PITOT-STATIC SYSTEMS
|
|
|
- Rosa Stevenson
- 5 years ago
- Views:
Transcription
1 NAVIGATION AND PITOT-STATIC SYSTEMS. GENERAL This chapter describes the navigation systems, units, and components which provide airplane navigational information. Included are pitot-static, gyros, compass, landing aids, global positioning system (GPS), and indicators. The subjects to be covered in this chapter are as follows: The Flight Environmental Data/Pitot Static Section describes systems which sense environmental conditions and use the data to influence navigation of the airplane. This includes components that depend on the pitot-static system such as vertical speed indicator, airspeed indicator, altimeter, air data computer, and MD30 Standby Attitude Module. (Refer to 34-0) The Attitude and Direction Section describes systems which use magnetic, gyroscopic and inertia forces. This includes gyros, magnetic compass, turn coordinator, attitude indicator, magnetometer, and GRS attitude and heading reference system. (Refer to 34-0) The Landing and Taxiing Aids Section describes systems which provide guidance during approach, landing, and taxiing. This includes components such as the glideslope and marker beacon systems. (Refer to 34-30) The Independent Position Determining Section describes systems which provide information to determine position from sources which are mainly independent of ground installations. This includes the optional Stormscope, SkyWatch, and Terrain Awareness and Warning Systems. (Refer to 34-40) The Dependent Position Determining Section describes systems which provide information to determine position from sources which are mainly dependent on ground installations. This includes the global positioning system (GPS), transponder, course deviation indicator, horizontal situation indicator, XM Weather system, automatic direction finder (ADF) receiver, distance measuring equipment (DME) receiver, and radio navigational aids. (Refer to 34-0) The Flight Management Computing Section describes systems which combine navigational data to compute or manage the aircraft's geographical position or theoretical flight path. This includes the GCU 48 Flight Management System (FMS) keyboard/controller. (Refer to 34-60) Navigational system instrument layout: (See Figure ) Pitot-Static system schematic: (See Figure ) Note: This chapter does not address specific instrument repair. Federal Aviation Regulations require malfunctioning instruments be sent to an approved instrument overhaul and repair station or returned to the manufacturer for servicing. All Page
2 I N L A S V M A P B R G NAV 84 SANDEL SN3308 SHFT SYNC 0 0 KT MAP OFF GPS A-B 30 3 V 6 U 0 E DTA BAR ALT ENT ALT ALR DH DH VS VS MAN INC PULL TENTHS AMMETER SELECT ALT ALT BATT CIRRUS AIRPLANE MAINTENANCE MANUAL FASTEN SEATBELTS FIRE EXTINGUISHER UNDER PILOT SEAT FRONT NO SMOKING ALTITUDE GPH SL MAX POWER FUEL FLOWS ALTIMETER nm A W N VERTICAL L R E E 6 0 SPEED Airspeed Indicator (34-0). Attitude Indicator (34-0) 3. Magnetic Compass (34-0) 4. Altitude Selector\Alerter (-). Altimeter (34-0) 6. Multi-Function Display (3-60). Audio Panel w/ Marker Beacon (34-30) 8. VOR/LOC (34-0) 9. Turn Coordinator (34-0) 0. HSI (34-0). Vertical Speed Indicator (34-0). Transponder (34-0) 3. System X Autopilot (-) 4. GPS/COM/NAV Receiver (34-0) Serials -000 thru -0434, -043 thru -080 w/o PFD. SR_MM34_39F Page Figure Navigation & Pitot-Static System - Serials -000 thru -080 w/o PFD (Sheet of 6) Serials -000 thru -080 w/o PFD
3 OFF R L START AMMETER SELECT ALT ALT BATT CIRRUS AIRPLANE MAINTENANCE MANUAL 3 6 FASTEN SEATBELTS FIRE EXTINGUISHER UNDER PILOT SEAT FRONT NO SMOKING ALTITUDE GPH SL MAX POWER FUEL FLOWS BOTH ACS L R Airspeed Indicator (34-0). Attitude Indicator (34-0) 3. Magnetic Compass (34-0). Altimeter (34-0) 6. Multi-Function Display (3-60). Audio Panel w/ Marker Beacon (34-30) 9. Turn Coordinator (34-0). Transponder (34-0) 3. System X Autopilot (-) 4. GPS/COM/NAV Receiver (34-0). Primary Flight Display (3-60) NOTE Mounted behind RH bolster. Serials -043 thru -080 w/ PFD, -08 thru -60, -603 thru -643, -64 thru -66. SR_MM34_60D Figure Navigation & Pitot-Static System - Serials -043 thru -080 w/ PFD, -08 thru -66 (Sheet of 6) Serials -043 thru -080 w/ PFD, -08 thru - 66 Page 3
4 Airspeed Indicator (34-0). Attitude Indicator (34-0) 3. Magnetic Compass (34-0). Altimeter (34-0) 6. Multifunction Display (3-60). Audio Panel w/ Marker Beacon (34-30) 9. Turn Coordinator (34-0). Transponder (34-0) 3. System X Autopilot (-) 4. GPS/COM/NAV Receiver (34-0). Primary Flight Display (3-60) NOTE Mounted behind RH bolster. Serials -60, -644, -663 thru -30, -306 & subs w/o Perspective Avionics. SR_MM34_98D Figure Navigation & Pitot-Static System - Serials -663 & subs w/o Perspective Avionics (Sheet 3 of 6) Page 4 Serials -663 & subs w/o Perspective Avionics
5 Airspeed Indicator (34-0). Attitude Indicator (34-0) 3. Magnetic Compass (34-0). Altimeter (34-0) 6. Multi-Function Display (3-60). Audio Panel w/ Marker Beacon (34-30). Primary Flight Display (3-60) 6. Flight Management System Controller (34-60). Automatic Direction Finder (34-0) 8. GFC 00 Autopilot (-) Figure Navigation & Pitot-Static System - Serials w/ Perspective Avionics & GFC 00 (Sheet 4 of 6) Serials w/ Perspective Avionics & GFC 00 SR_MM34_A Page
6 Magnetic Compass (34-0) 6. Multi-Function Display (3-60). Audio Panel w/ Marker Beacon (34-30). Primary Flight Display (3-60) 8. Flight Management System Controller (34-60) 9. Automatic Direction Finder (34-0) 0. GFC 00 Autopilot (-). MD30 Standby Attitude Module (34-0) Figure Navigation & Pitot-Static System - Serials -464 & subs, T-094, T-0963 & subs w/ MD30 (Sheet of 6) Page 6 SR0_MM34_363 Serials -464 & subs, T-094, T-0963 & subs w/ MD30
7 4 6 L R Airspeed Indicator (34-0). Attitude Indicator (34-0) 4. Magnetic Compass (34-0). Altimeter (34-0) 6. Multi-Function Display (3-60). Audio Panel w/ Marker Beacon (34-30) 9. Turn Coordinator (34-0) 3. System X Autopilot (-). Primary Flight Display (3-60) 6. Flight Management System Controller (34-60). Automatic Direction Finder (34-0) NOTE Mounted behind RH bolster. Figure Navigation & Pitot-Static System - Serials w/ Perspective Avionics & System X (Sheet 6 of 6) Serials w/ Perspective Avionics & System X SR_MM34_3033A Page
8 Serials -043 thru -080 w/ PFD, -08 thru -30, -306 & subs w/o Perspective Avionics. Serials -000 thru -0434, -043 thru -080 w/o PFD. PRIMARY FLIGHT DISPLAY AIRSPEED INDICATOR VERTICAL SPEED INDICATOR ALTIMETER ALTITUDE ENCODER ALTITUDE TRANSDUCER (OPTIONAL) ALTERNATE STATIC AIR SOURCE PITOT-STATIC WATER TRAPS PITOT MAST STATIC BUTTONS SR_MM34_838D Page 8 Figure Pitot-Static System Schematic - Serials w/o Perspective Avionics (Sheet of 3) Serials w/o Perspective Avionics
9 AIR DATA COMPUTER AIR DATA COMPUTER (optional) PFD Air Data AIRSPEED INDICATOR ALTIMETER PITOT-STATIC WATER TRAPS ALTERNATE STATIC AIR SOURCE PITOT MAST HEATER STATIC BUTTONS CURRENT SENSOR LOGIC Annunciation PITOT HEAT.A PITOT HEAT CB PITOT HEAT SW SR_MM34_6B Figure Pitot-Static System Schematic - Serials w/ Perspective Avionics (Sheet of 3) Serials w/ Perspective Avionics Page 9
10 AIR DATA COMPUTER AIR DATA COMPUTER (optional) PFD Air Data MD30 STANDBY ATTITUDE MODULE PITOT-STATIC WATER TRAPS ALTERNATE STATIC AIR SOURCE PITOT MAST HEATER STATIC BUTTONS Annunciation PITOT HEAT CURRENT SENSOR LOGIC.A PITOT HEAT CB PITOT HEAT SW ENGINE AIRFRAME UNIT SR_MM34_364 Figure Pitot-Static System Schematic - Serials -464 & subs, T-094, T-0963 & subs w/ MD30 (Sheet 3 of 3) Page 0 Serials -464 & subs, T-094, T-0963 & subs w/ MD30
CIRRUS AIRPLANE MAINTENANCE MANUAL
CIUS AIPANE MAINTENANCE MANUA MODE S NAVIGATION AND PITOT-STATIC SYSTEMS. GENEA This chapter describes the navigation systems, units, and components which provide airplane navigational information. Included
BEECHCRAFT SUPER KING AIR B200 Model: 1998 Crew: 2 pilots Passengers: 7
BEECHCRAFT SUPER KING AIR B200 Model: 1998 Crew: 2 pilots Passengers: 7 AIRFRAME: 2996:09 Hours TSN Landings: 2314 ENGINES: Pratt & Whitney PW545A Left Engine: 2996:09 Hours TSN 2314 Cycles SN Right Engine:
AIRCRAFT AVIONIC SYSTEMS
AIRCRAFT AVIONIC SYSTEMS B-777 cockpit Package C:\Documents and ettings\administrato Course Outline Radio wave propagation Aircraft Navigation Systems - Very High Omni-range (VOR) system - Instrument Landing
A-VIATOR (AP68TP-600) STANDARD EQUIPMENT LIST
A-VIATOR (AP68TP-600) STANDARD EQUIPMENT LIST V13.04.16 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for
NAVIGATION INSTRUMENTS - BASICS
NAVIGATION INSTRUMENTS - BASICS 1. Introduction Several radio-navigation instruments equip the different airplanes available in our flight simulators software. The type of instrument that can be found
SD3-60 AIRCRAFT MAINTENANCE MANUAL
AMM 24.0.0.0FLIGHT DIRECTOR SYSTEM - DESCRIPTION & OPERATION 1. Description A. General Refer to Figure 1. Identical, left and right, systems are installed (one for each pilot); each provides information
Fokker 50 - Automatic Flight Control System
GENERAL The Automatic Flight Control System (AFCS) controls the aircraft around the pitch, roll, and yaw axes. The system consists of: Two Flight Directors (FD). Autopilot (AP). Flight Augmentation System
Description MFG P/N S/N STC Captains Instruments Audio Panel Autech 6608213-3 (2050-1) 175 ADI 84A Indicator Collins 622-3594-003 4 HSI Indicator Collins 622-4151-003 19 Emergency Gyro Jet 501-1105-04
LOG OF REVISIONS Rev 1 RFMS, Eurocopter EC130 B4 G500H System. Page Date Number Description FAA Approved.
Revision Number LOG OF REVISIONS Page Date Number Description FAA Approved 1 05/15/2014 All Complete Supplement See page 1 190-01527-16 Rev 1 RFMS, Eurocopter EC130 B4 G500H System Page 2 of 25 FAA APPROVED
CALL GULFSTREAM III PARTS FOR SALE
CALL 386-341-0423 GULFSTREAM III PARTS FOR SALE Part Number Serial Number Bleed Air Control 8606 38201 ANTENNA 10706 9757 ANTENNA 10706 9758 Ignition Exciter 43663 2149 Indidcator Dual Temperature 253682
Sikorsky S-76C++ N722JE S/N
Sikorsky S-76C++ N722JE S/N 760750 Sikorsky S-76C++ N722JE S/N 760750 OFFERED AT: Make Offer Entry into Service: March 17 th, 2010 Executive Cabin Interior Iridium Phone System Cabin Soundproofing XM Satellite
TITLE 14 OF THE CODE OF FEDERAL REGULATIONS (14 CFR) GUIDANCE MATERIAL
TITLE 14 OF THE CODE OF FEDERAL REGULATIONS (14 CFR) GUIDANCE MATERIAL Subject: INDEX OF AVIATION TECHNICAL STANDARD ORDERS Date: 10/10/00 Initiated by: AIR-120 AC No: AC 20-110L Change: 1. PURPOSE. This
CHAPTER NAVIGATION SYSTEMS
18--00--1 NAVIGATION SYSTEMS Table of Contents REV 3, May 03/05 CHAPTER 18 --- NAVIGATION SYSTEMS Page TABLE OF CONTENTS 18-00 Table of Contents 18--00--1 INTRODUCTION 18-10 Introduction 18--10--1 FLIGHT
Communication and Navigation Systems for Aviation
Higher National Unit Specification General information for centres Unit title: Communication and Navigation Systems for Aviation Unit code: F0M3 35 Unit purpose: This Unit is designed to allow candidates
This page is intentionally blank. GARMIN G1000 SYNTHETIC VISION AND PATHWAYS OPTION Rev 1 Page 2 of 27
This page is intentionally blank. 190-00492-15 Rev 1 Page 2 of 27 Revision Number Page Number(s) LOG OF REVISIONS Description FAA Approved Date of Approval 1 All Initial Release See Page 1 See Page 1 190-00492-15
Integrated Cockpit Display System ICDS 1000 Pilot Operation Handbook
Integrated Cockpit Display System ICDS 1000 Pilot Operation Handbook ICDS1000 Pilot Operating Handbook Revision 1.3 572-0540 page 1 Table Of Contents Electronic Attitude Direction Indicator (EADI)... 8
2010 EMBRAER LINEAGE 1000
HIGHLIGHTS AIRFRAME Engines on GE Onpoint No Damage History ADS-B Upgraded Fresh 96 Month Inspection Will Deliver With; Crew Training EASA / Isle of Man Certification Post Delivery; FANS-1/A & CPDLC Upgrade
SERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Removed the 4890307-2 Carpet from the -2 Kit and added the requirement to order it separately based on airplane color scheme.
2007 BOMBARDIER CHALLENGER 605
2007 BOMBARDIER CHALLENGER 605 OVERVIEW AVIONICS Date of Manufacture: 10th January 2007 Entry Into Service: 22nd November 2007 EASA JAR OPS 1 Compliant One owner since new AIRFRAME Total Time: 2840 Hours
2007 bombardier challenger 605. serial number 5709 registration 9H-AFQ
2007 bombardier challenger 605 overview AVIONICS Date of Manufacture: 10th January 2007 Entry Into Service: 22nd November 2007 EASA JAR OPS 1 Compliant One owner since new AIRFRAME Total Time: 3022 Hours
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line II (Generic) Level I Operations & Flight Line Maintenance PREREQUISITES: Students should have basic knowledge of aircraft avionics systems and a working command of the English language
NAVIGATION INTRUMENTATION ADF
1. Introduction NAVIGATION INTRUMENTATION ADF The Automatic Direction Finding (ADF) equipment on-board of aircraft is used together with the Non Directional Beacon (NDB) transmitters installed on the ground.
P/N 135A FAA Approved: 7/26/2005 Section 9 Initial Release Page 1 of 10
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR GARMIN GNS 430 - VHF COMM/NAV/GPS Serial No: Registration No: When installing the Garmin GNS 430 - VHF COMM/NAV/GPS in the Liberty Aerospace XL2, this
G1000 Integrated Flight Deck
G1000 Integrated Deck Cockpit Reference Guide System Software 0719.03 or later Instruments ENGINE & AIRFRAME SYSTEMS Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures
RADIO SYSTEM DESCRIPTION The radio system consists of the following equipment:
COMMUNICATION SYSTEM RADIO SYSTEM DESCRIPTION The radio system consists of the following equipment: Radio tuning function located in MFD s Dual CDU s (for tuning - shared with FMS) Two VHF communication
Dash8-200/300 - Automatic Flight AUTOMATIC FLIGHT CONTROLS AND INDICATORS. Page 1
AUTOMATIC FLIGHT CONTROLS AND INDICATORS FLIGHT GUIDANCE MODE SELECTORS (alternate action) - Engages flight director modes of operation. - Flight director command bars display lateral and/or vertical guidance
SUPPLEMENT REVISION CESSNA MODEL 182T
SUPPLEMENT REVISION CESSNA MODEL 182T NAV III AVIONICS OPTION - Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875 PILOTS OPERATING HANDBOOK AND AIRPLANE FLIGHT MANUAL REVISION 1 1
Master Parts Inventory
ID Nomenclature Part Alternate P/N Manufacturer 44 Automatic Annunicator 103500 Sunstrand MTA 554 47 Tape Reproducer 108002 0004JL 980 9000 004 Sundtrand 201AACB 97 Tape Reproducer 108002 0004JL 980 9000
Operating Handbook. For. Gemini Autopilot
Operating Handbook For Gemini Autopilot TRUTRAK FLIGHT SYSTEMS 1488 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 www.trutrakap.com Table of Contents 1. Revisions... 5 2.
Cessna Citation XLS - Instrumentation & Avionics
INSTRUMENTATION The Citation XLS is equipped with a Honeywell Primus 1000 Control Display System which includes display, flight director guidance, autopilot, yaw damper and pitch trim functions. The system
G1000 Integrated Flight Deck
G1000 Integrated Deck Cockpit Reference Guide for the Beechcraft 200/B200 Series System Software 0985.00 or later Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures Features
Level I Operator & Flightline Maintenance
COURSE TITLE: PRO LINE II (Generic) Level I Operator & Flightline Maintenance EQUIPMENT TYPES: LRU DSP-8X DCP-8X MFD-85X MPU-85 DPU-8X EFD-8X PRE-8XX VSI-8X ALI-8X ASI/MSI-8X ADC 81, -82, -8X AHC-85/85E
G1000 Integrated Flight Deck. Cockpit Reference Guide for the Beechcraft 58/G58
G1000 Integrated Deck Cockpit Reference Guide for the Beechcraft 58/G58 FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV/COM/TRANSPONDER/AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT
A-VIATOR (AP68TP-600) STANDARD EQUIPMENT LIST
A-VIATOR (AP68TP-600) STANDARD EQUIPMENT LIST V15.05.18 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for
EMERGENCY AND ABNORMAL PROCEDURES...
TABLE OF CONTENTS 1 GENERAL...5 1.1 SYSTEM OVERVIEW...5 2 LIMITATIONS...6 2.1 SOFTWARE VERSIONS...6 2.2 AIRSPEED LIMITATION...6 2.3 WEIGHT & CENTER OF GRAVITY...6 2.4 RSM GPS USAGE...6 2.5 GEOGRAPHIC LIMITATION...6
Flight Detector Indicator
Flight Detector Indicator Part No: 777-1224-003 Components Maintenance Manual No: 34-25-12 By Soumyadeep Das Raj shekhar Chatterjee Purpose of equipment: The flight detector indicator (FDI) is a part of
Module 13 Aircraft Aerodynamics, Structures and Systems
13.1 Theory of Flight (a) Aeroplane Aerodynamics and Flight Controls Operation and effect of: roll control: ailerons and spoilers, pitch control: elevators, stabilators, variable incidence stabilisers
G1000 Integrated Flight Deck
G1000 Integrated Deck Cockpit Reference Guide for the Cessna 350/400 System Software 0534.11 or later Instruments ENGINE INDICATION SYSTEM Transponder/Audio Panel Automatic Control System GPS Navigation
Dash8 - Q400 - Autoflight
12.3.1 Introduction The Automatic Flight Control System (AFCS), provides fail-safe operation of flight director guidance, autopilot, yaw damper and automatic pitch trim functions. 12.3.2 General The Automatic
SECTION 3 NAV/COM & TRANSPONDER G1000TM. cockpit reference guide for Cessna Nav III. Garmin G1000 Cockpit Reference Guide for Cessna Nav III
SECTION 3 NAV/COM & TRANSPONDER G1000TM cockpit reference guide for Cessna Nav III A COPYRIGHT Copyright 2004, 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation
G1000 Integrated Flight Deck. Cockpit Reference Guide for the DA42
G1000 Integrated Deck Cockpit Reference Guide for the DA42 Instruments ENGINE INDICATION SYSTEM Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures Annunciations & Alerts
Independent Position Determining
GENERAL Independent Position Determining 34-40: INDEPENDENT POSITION DETERMINING 1. General This section covers that portion of the system which provides information to determine position from sources
FOUND FBA-2C1/2C2 BUSH HAWK EQUIPPED WITH SINGLE GARMIN GNS-430 # 1 VHF-AM COMM / VOR-ILS / GPS RECEIVER
FOUND SUPPLEMENT M400-S11 Transport Canada Approved Flight Manual Supplement For FOUND BUSH HAWK EQUIPPED WITH SINGLE # 1 VHF-AM COMM / VOR-ILS / GPS RECEIVER Section 1 General is Unapproved and provided
G1000 Integrated Flight Deck. Cockpit Reference Guide for the DA42
G1000 Integrated Deck Cockpit Reference Guide for the DA42 FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV/COM/TRANSPONDER/AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES
SA4550. Pilot s Guide Effectivity and Errata
SA4550 Pilot s Guide Effectivity and Errata Insert this update ahead of the cover page of the above referenced Pilot s Guide. The environmental categories in the Technical Specifications contained in Section
Operating Handbook. For. Gemini Autopilot
Operating Handbook For Gemini Autopilot TRUTRAK FLIGHT SYSTEMS 1488 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 www.trutrakap.com Table of Contents 1. Revisions... 5 2.
GRT Autopilot User Guide. All GRT EFIS Systems
All GRT EFIS Systems Revision A 22-May-2014 Copyright 2014 3133 Madison Ave. SE Wyoming, MI 49548 (616) 245-7700 www.grtavionics.com Revision Notes Revision Date Change Description A 22-May-2014 Complete
DEPENDENT POSITION DETERMINING
DEPENDENT POSITION DETERMINING 1. DESCRIPTION This section covers that portion of the system which provides information to determine position from sources which are mainly dependent on ground installations.
G1000 Integrated Flight Deck. Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
G1000 Integrated Deck Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN FLIGHT INSTRUMENTS EIS NAV/COM/TRANSPONDER/AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES
SECTION 1 SYSTEM OVERVIEW
SECTION 1 1.1 DESCRIPTION This section is designed to provide an overview of the G1000 Integrated Flight Deck as installed in Cessna Nav III aircraft, which include the Cessna 172R, 172S, the normally
Pilot s Operating Handbook Supplement AS-21
SECTION 9 Pilot s Operating Handbook Supplement Mode S Transponder GARMIN GTX 335 / GTX 345 This supplement is applicable and must be inserted into Section 9 of the POH when a GARMIN GTX 335 or GTX 345
G1000 Integrated Flight Deck. Cockpit Reference Guide for the Beechcraft A36/G36
G1000 Integrated Deck Cockpit Reference Guide for the Beechcraft A36/G36 Instruments ENGINE INDICATION SYSTEM Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures Annunciations
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR. Trio Pro Pilot Autopilot
Page 1 480 Ruddiman Drive TRIO AP Flight Manual Supplement North Muskegon, MI 49445 L-1006-01 Rev D FOR Trio Pro Pilot Autopilot ON Cessna 172, 175, 177, 180, 182, 185 and Piper PA28 Aircraft Document
apply nose down control wheel force upon autopilot disconnect. Preflight system test has failed.
13.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 13-5 AFCS System Status Annunciation
G1000 Integrated Flight Deck. Cockpit Reference Guide for the Cessna Citation Mustang
G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Citation Mustang FLIGHT INSTRUMENTS NAV/COM/TRANSPONDER/AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES
HAZARD AVOIDANCE. Displaying traffic on the Navigation Map. Displaying traffic information (PFD Inset Map):
HAZARD AVOIDANCE Displaying traffic on the Navigation Map 1) Ensure that the TAS system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is
Table of Contents. Introduction 3. Pictorials of the 40 and 50 Systems 4. List of Applicable Acronyms 6
Table of Contents Introduction 3 Pictorials of the 40 and 50 Systems 4 List of Applicable Acronyms 6 System 40 Modes of Operation 7 System 40 Functional Preflight Procedures 10 System 40 In Flight Procedures
SERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Changed the drawing number in the REFERENCES table from C190629 to CI90629. B. Changed the drawing number in the REFERENCES
AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS CHAPTER 4
TABLE OF CONTENTS CHAPTER 4 Page TABLE OF CONTENTS DESCRIPTION General Guidance Panel Autopilot System Autopilot Yaw Damper Autopilot Engage Autopilot Disengage PFD Annunciation Flight Director (FD) Flight
Page Chg
Page Chg Cover...0 Page #...2 TOC-1...2 TOC-2..2 1-1 2 1-2.2 1-3.2 1-4...2 1-5...2 1-6. 2 1-7. 2 1-8. 2 1-9. 2 1-10...2 1-11..2 1-12..2 1-13..2 1-14..2 1-15..2 1-16..2 1-17..2 1-18...2 2-1.0 2-2.0 2-3.2
SECTION 2-19 AUTOPILOT
AIRPLANE SECTION 2-19 Block General...2-19-05...01 Automatic Flight Control System...2-19-05...02 Flight Guidance System...2-19-05...04 Flight Director...2-19-05...04 Autopilot...2-19-05...04 Flight Director
G1000 Integrated Flight Deck
G1000 Integrated Deck Cockpit Reference Guide for the Cessna Caravan System Software 0767.02 or later Instruments EIS Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures
Advanced Avionics Workshop. Making the technology work for you
Advanced Avionics Workshop Making the technology work for you Presentation Outline GMA 340 Audio Panel Two-channel Monitoring ICS Isolation Split Comm GTX 330 Transponder Buttonology Basic Usage Advanced
EMBRAER 135/145 Autopilot
EMBRAER 135/145 Autopilot GENERAL The Primus 1000 (P-1000) Automatic Flight Control System (AFCS) is a fully integrated, fail passive three-axis flight control system which incorporates lateral and vertical
Page Chg
Page Chg Cover...0 Page #...4 TOC-1...3 TOC-2..3 1-1 2 1-2.3 1-3.3 1-4...3 1-5...3 1-6. 3 1-7. 3 1-8. 4 1-9. 4 1-10...3 1-11..4 1-12..4 1-13..3 1-14..3 1-15..3 1-16..3 1-17..3 1-18...3 1-19..3 2-1.0 2-2.0
Cirrus SR20/SR22/SR22T. Integrated Avionics System Cockpit Reference Guide
Cirrus SR20/SR22/SR22T Integrated Avionics System Cockpit Reference Guide Instruments EIS Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures Annunciations & Alerts Appendix
C I R R U S EMERGENCY DESCRIPTION A. Emergency Locator Transmitter (ELT)
EMERGENCY 1. DESCRIPTION A. Emergency Locator Transmitter (ELT) This airplane is equipped with a self-contained ELT. The ELT transmitter is installed immediately behind the aft cabin bulkhead. The ELT
G1000 Integrated Flight Deck. Cockpit Reference Guide for the Cessna Caravan
G1000 Integrated Deck Cockpit Reference Guide for the Cessna Caravan Instruments EIS Transponder/Audio Panel Automatic Control System GPS Navigation Planning Procedures Annunciations & Alerts INDEx Copyright
Digiflight II SERIES AUTOPILOTS
Operating Handbook For Digiflight II SERIES AUTOPILOTS TRUTRAK FLIGHT SYSTEMS 1500 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 Toll Free: 866-TRUTRAK 866-(878-8725) www.trutrakap.com
Operating Handbook For FD PILOT SERIES AUTOPILOTS
Operating Handbook For FD PILOT SERIES AUTOPILOTS TRUTRAK FLIGHT SYSTEMS 1500 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 Toll Free: 866-TRUTRAK 866-(878-8725) www.trutrakap.com
G1000TM. Cockpit Reference Guide for the Beechcraft A36/G36
G1000TM Cockpit Reference Guide for the Beechcraft A36/G36 Copyright 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0458.01 or
AIRPLANE FLIGHT MANUAL AQUILA AT01. Date of Issue A.01 Initial Issue (minor change MB-AT ) all March
0.1 LIST OF REVISIONS AND AMENDMENTS Revision Reason for Amendment/Revision Affected Pages Date of Issue A.01 Initial Issue (minor change MB-AT01-00297) all 2009 19. March 0.2 LIST OF EFFECTIVE PAGES Page
SECTION III INSTRUMENTATION AND AVIONICS CONTENTS
MODEL 750 SECTION III INSTRUMENTATION AND AVIONICS SECTION III INSTRUMENTATION AND AVIONICS CONTENTS Page INSTRUMENTATION................................................... 3-3 Pitot-Static System..................................................
CIRRUS AIRPLANE MAINTENANCE MANUAL
DEPENDENT POSITION DETERMINING 1. DESCRIPTION This section covers that portion of the system which provides information to determine position from sources which are mainly dependent on ground installations.
Pilot s Guide KI 825. Bendix/King Safety Display System Electronic Horizontal Situation Indicator For Units Having -2, -3 and -4 Softwa re
N Pilot s Guide KI 825 Bendix/King Safety Display System Electronic Horizontal Situation Indicator For Units Having -2, -3 and -4 Softwa re W A R N I N G The enclosed technical data is eligible for export
ENSTROM 480/480B OPERATOR S MANUAL AND FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN GNS 430W/530W NAVIGATION SYSTEM
ENSTROM 480/480B OPERATOR S MANUAL AND FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN GNS 430W/530W NAVIGATION SYSTEM * * * * * REPORT NO. 28-AC-055 HELICOPTER SERIAL NO. HELICOPTER REGISTRATION
KMD 550/850. Traffic Avoidance Function (TCAS/TAS/TIS) Pilot s Guide Addendum. Multi-Function Display. For Software Version 01/13 or later
N B KMD 550/850 Multi-Function Display Traffic Avoidance Function (TCAS/TAS/TIS) Pilot s Guide Addendum For Software Version 01/13 or later Revision 3 Jun/2004 006-18238-0000 The information contained
For Microsoft FSX and FS FriendlyPanels. All right reserved
FriendlyPanels Software (version 2.0) For Microsoft FSX and FS9 2007 FriendlyPanels. All right reserved FOURTEEN GAUGES FOR YOUR FSX and FS9 AIRCRAFT 1 1. Introduction. 2. Requirements 3. Installing the
SmartFly Cirrus Cirrus. Flight Trainer
SmartFly SmartFly Cirrus Cirrus Flight Trainer The new PX-Eco Professional BATD Flight Simulator was engineered from the bottom up with a robust mechanism and our new SIMSOFT USB Digital Hardware Controller.
SN3500 EHSI. Pilot s Guide Effectivity and Errata. Instructions
SN3500 EHSI Pilot s Guide Effectivity and Errata Insert this update ahead of the cover page of the Pilot s Guide referenced below. Date: Effectivity: 05-OCT-2018 SN3500 Software Version 4.05, A4.08 Pilots
Page Chg
Page Chg Cover...0 Page #...1 TOC-1...1 TOC-2..1 1-1.1 1-2.1 1-3.1 1-4...0 1-5...1 1-6. 1 1-7. 1 1-8. 1 1-9. 1 1-10...1 1-11..1 1-12..1 1-13..1 1-14..1 2-1.0 2-2.0 2-3.1 Page Chg 2-4.0 3-1.0 3-2.0 3-3.0
Page Chg
Page Chg Cover...0 Page #...1 TOC-1...1 TOC-2...1 1-1.1 1-2.0 1-3.1 1-4...1 1-5...1 1-6. 1 1-7. 1 1-8. 1 1-9. 1 1-10...1 1-11..1 1-12..1 1-13..2 1-14..1 1-15..1 1-16..1 1-17..1 1-18..1 2-1.0 2-2.0 Page
G1000TM. cockpit reference guide for the Diamond DA 40
G1000TM cockpit reference guide for the Diamond DA 40 Copyright 2004, 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0369.07 or
Instrument Flight Procedures - Glass Cockpits
Instrument Flight Procedures - Glass Cockpits The concepts contained here are general in nature and can be used by all however, they are targeted toward glass cockpits and, more specifically, integrated
CIRRUS AIRPLANE MAINTENANCE MANUAL
All GFC 700 AUTOMATED FLIGHT CONTROL SYSTEM (AFCS) 1. DESCRIPTION This section covers those systems and components which use inputs to the system to automatically control the flight path of the aircraft
SN3500 EHSI. Pilot s Guide Effectivity and Errata. (This page intentionally blank)
SN3500 EHSI (This page intentionally blank) Pilot s Guide Effectivity and Errata Insert this update ahead of the cover page of the Pilot s Guide referenced below. Date: Effectivity: 03-JUL-2014 SN3500
ENSTROM 480B OPERATOR S MANUAL AND FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN GTN 650 NAVIGATION SYSTEM
ENSTROM 480B OPERATOR S MANUAL AND FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN GTN 650 NAVIGATION SYSTEM * * * * * REPORT NO. 28-AC-064 HELICOPTER SERIAL NO. HELICOPTER REGISTRATION NO. * *
SN4500. Pilot s Guide. Primary Navigation Display. Reversionary Attitude Mode. with. (This page intentionally left blank)
SN4500 Primary Navigation Display with Reversionary Attitude Mode (This page intentionally left blank) Pilot s Guide 82009-PG, REV D1 SANDEL SN4500 PILOT S GUIDE PAGE II Pilot information Publication Date:
Integrated Flight Deck. Cockpit Reference Guide. Cessna 350/400
Integrated Flight Deck Cockpit Reference Guide Cessna 350/400 SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV/COM/TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING
G5 Electronic Flight Instrument Pilot's Guide for Certified Aircraft
G5 Electronic Flight Instrument Pilot's Guide for Certified Aircraft Blank Page SYSTEM OVERVIEW FLIGHT INSTRUMENTS AFCS ADDITIONAL FEATURES INDEX Blank Page 2017 Garmin Ltd. or its subsidiaries. All rights
Flight Management, Navigation Chapter 11
Flight Management, Navigation Chapter 11 Controls and Indicators Section 10 11.10 Flight Management, Navigation-Controls and Indicators Flight Management System Control Display Unit (CDU) [Option Liquid
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line 21 King Air C90GTi Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC 3000 822-1129-001 IAPS Environmental Controller
Operations Manual. Caution: Preliminary
Operations Manual Caution: Preliminary This manual is incomplete at this time. Most, but not all of the data within the manual is accurate, although it is all subject to change and may not match the software
11 Traffic-alert and Collision Avoidance System (TCAS)
11 Traffic-alert and Collision Avoidance System (TCAS) INSTRUMENTATION 11.1 Introduction In the early nineties the American FAA stated that civil aircraft flying in US airspace were equipped with a Traffic-alert
AP OLLO S L15M Audio Control Panel and Marker Beacon Receiver
SkyRentals INFO FOR VH-VMA Insert to SECTION 7 MODEL 182Q (1977) Audio Control Panel & Marker Receiver AP OLLO S L15M Audio Control Panel and Marker Beacon Receiver Audio Panel & Marker components 1A Apollo
GFC 700 AUTOMATED FLIGHT CONTROL SYSTEM (AFCS)
All GFC 700 AUTOMATED FLIGHT CONTROL SYSTEM (AFCS) 1. DESCRIPTION This section covers those systems and components which use inputs to the system to automatically control the flight path of the aircraft
GFC 700 Automated Flight Control System
CIRRUS AIRPLANE MAINTENANCE MANUAL CHAPTER 22-10: GFC 700 AUTOMATED FLIGHT CONTROL SYSTEM GENERAL GFC 700 Automated Flight Control System 22-10: GFC 700 AUTOMATED FLIGHT CONTROL SYSTEM 1. General (See
Flying Club - Archer III For Microsoft Flight Simulator X Steam Edition
Piper Archer III 1 Flying Club - Archer III For Microsoft Flight Simulator X Steam Edition Pilot s Guide CONTENTS INTRODUCTION... 3 INSTALLATION... 3 SETTING UP FLIGHT SIMULATOR FOR FLYING CLUB... 4 HOW
ARMY MODEL UH-1H/V HELICOPTERS
OPERATOR S MANUAL ARMY MODEL UH-1H/ HELICOPTERS This manual supersedes TM 55-1520-210-10 dated 1 December 1986, including all changes. HEADQUARTERS, DEPARTMENT OF THE ARMY 15 FEBRUARY 1988 TECHNICAL MANUAL
G1000 Integrated Flight Deck
G1000 Integrated Deck Cockpit Reference Guide for the Piper PA-46 Mirage/Matrix System Software 0720.10 or later Instruments EICAS Transponder/Audio Panel Automatic Control System GPS Navigation Planning