SUPPLEMENT 3 11 APRIL CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL AND ON 510FM-S3-00 S3-1 U.S.
|
|
- Stephanie Woods
- 5 years ago
- Views:
Transcription
1 AND ON CITATION PERFORMANCE CALCULATOR (CPCalc) COPYRIGHT 2007 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 11 APRIL 2007 U.S. S3-1
2 CITATION PERFORMANCE CALCULATOR (CPCalc) Use the Log of Effective Pages to determine the current status of this supplement. Pages affected by the current revision are indicated by an asterisk (*) preceding the page number. Supplement Status Date Original 11 April 2007 LOG OF EFFECTIVE PAGES Page Number Page Status Revision Number Configuration Code S3-1 thru S3-8 Original 0 S3-AA S3-2 U.S. Configuration S3-AA
3 SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active. Number Title Airplane Serial Effectivity Revision Incorporated Incorporated in Airplane Configuration S3-AA U.S. S3-3
4 AIRPLANE CONFIGURATION CODES The following is a list of airplane configuration codes which appear at the bottom of each page of this supplement to the basic FAA Approved Airplane Flight Manual. The codes indicate page effectivity by serial number. This list contains only the configurations which have been incorporated into this supplement. Configuration Code S3-AA Effectivity by Serial Number Airplanes thru Incorporating SL and Airplanes and On using the Citation Performance Calculator (CPCalc). S3-4 U.S. Configuration S3-AA
5 CITATION PERFORMANCE CALCULATOR (CPCALC) INTRODUCTION This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual for Airplanes and On using performance information from the Citation Performance Calculator (CPCalc). The information contained herein supplements the information of the basic FAA Approved Airplane Flight Manual. For limitations, procedures and performance information not contained in this supplement, consult the basic FAA Approved Airplane Flight Manual. OPERATING LIMITATIONS GENERAL 1. The software version displayed on the main startup screen of the CPCalc must match the software version that corresponds with the applicable AFM revision as shown in the following table: OPERATIONAL APPROVALS The CPCalc provides FAA approved Section IV Takeoff and Landing performance information and provides Section VII Wet Takeoff and Landing performance information. 1. The CPCalc is approved for use as an alternative source to the takeoff and landing data presented in Section IV of the basic FAA Approved Airplane Flight Manual. 2. The CPCalc and AFM are each equally valid sources of performance data; however, the operator must use speed and distance data from only one of these sources. 3. Inputs with decimal values must be entered into CPCalc using the current decimal separator symbol selected in the Windows operating system regional control panel options. No other separator symbols are allowed as input values. OPERATING PROCEDURES The operating procedures are the same as the basic FAA Approved Flight Manual except as follows: EMERGENCY PROCEDURES No change. ABNORMAL PROCEDURES No change. NORMAL PROCEDURES No change. CPCalc Software Version AFM Revision Temporary Changes 1.X 4 None Configuration S3-AA U.S. S3-5
6 PERFORMANCE WARNING THE CPCALC PERFORMANCE THAT IS SHOWN IS FOR THOSE CONDITIONS AS SPECIFIED. ANY DEVIATION FROM THESE CONDITIONS WILL RESULT IN DIFFERENT PERFORMANCE. THERE CAN BE COMBINATIONS OF CONDITIONS (WEIGHT, ALTITUDE AND TEMPERATURE) THAT COULD RESULT IN PERFORMANCE OTHER THAN THAT WHICH WOULD NORMALLY BE EXPECTED: E.G., AS WEIGHT GETS LIGHTER, REQUIRED DISTANCES ARE LONGER. DEFINITIONS Climb Gradient Surface: Imaginary surface located 35 feet above the end of the available runway and inclined at a required gradient. NET TAKEOFF FLIGHT PATH METHODS The airplane is flown to Level Off Altitude per the Gross Takeoff Flight Path. Level Off Altitude is the sum of Airport Barometric Altitude and Takeoff Climb Increment. The Takeoff Climb Increment is based on Gross Takeoff Flight Path which is associated with Net Takeoff Flight Path meeting the requirements of one of the three methods the user specifies. CPCalc provides the level off altitude and the horizontal distances along the net takeoff flight path. The net takeoff flight path is used to plan obstacle clearance. CPCalc will reduce the gross weight, if necessary, to meet specific flight path performance requirements. CPCalc provides three methods for the user to specify net takeoff flight path performance. 1. The net takeoff flight path will level off at a fixed height 1500 feet above the takeoff surface. Figure S3-1 (Continued Next Page) S3-6 U.S. Configuration S3-AA
7 PERFORMANCE (Continued) 2. The net takeoff flight path may continue the 2 nd segment climb beyond 1500 feet to clear an obstacle located anywhere along the path by at least 35 feet. Figure S The net takeoff flight path may continue the 2 nd segment climb beyond 1500 feet until the aircraft reaches an assigned level off altitude. The net takeoff flight path is prevented from penetrating a defined climb gradient surface. Figure S3-3 Configuration S3-AA U.S. S3-7
8 DESCRIPTION SOFTWARE PROCEDURES The CPCalc software provides help with detailed information on how to use the CPCalc for calculating Takeoff and Landing performance information. 1. Operational landing distance factor requirements may be set under the menu selection Tools Options, or the keyboard shortcut CTRL+O. 2. Climb Gradient calculator is available under the menu selection Tools Climb Gradient Calculator, or the keyboard shortcut CTRL+G. 3. Help is available under the menu selection Help Contents. For help specific to the screen shown, press the F1 key. 4. The calculated performance data may be printed to a connected printer by selecting the Print All Takeoff or Print All Landing buttons on the appropriate output tabs. 5. Additional condition information is available from each output tab by selecting the Additional Conditions button or the keyboard shortcut Alt+C. SOFTWARE INFORMATION 1. The CPCalc software has been demonstrated to function with the following Microsoft Windows operating system versions: Microsoft Windows 98 SP1, 98SE, or ME Windows NT 4.0 SP4, SP6 Windows 2000 SP3 Windows XP SP1,SP2 Windows Vista 2. The CPCalc software has been demonstrated to work with the following personal computer processors: Pentium II Pentium III Pentium 4 Intel AMD K6 Athlon XP 3. It is recommended that CPCalc be installed on a system that meets the following system requirements: Microsoft Windows operating system (98, ME, NT, 2000, XP, Vista). Minimum CPU 300 MHz, recommended CPU 600 MHz or better (Intel or AMD ). Minimum memory 64 MB, recommended memory 128 MB or higher. 30 MB free disk space for installation. Desktop, laptop, or tablet PC with CD-ROM drive for installation. Input device (keyboard/mouse/pen). Display that supports a resolution of 800 x 600 at 96 DPI or, 1024 x 768 at 120 DPI. Administrative rights to install programs. Microsoft Data Access Components (MDAC) Version 2.5 or higher (included on installation CD). S3-8 U.S. Configuration S3-AA
SUPPLEMENT AUGUST CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL THRU FM-S51-00 S51-1 U.S.
MODEL 525 525-0001 THRU -0359 CITATION PERFORMANCE CALCULATOR (CPCalc) COPYRIGHT 2007 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 14 AUGUST 2007 U.S. S51-1 SECTION V - SUPPLEMENTS CITATION PERFORMANCE
More informationSUPPLEMENT OCTOBER CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL AND ON REVISION 8 68FM-S17-08
MODEL 680 680-0001 AND ON CITATION PERFORMANCE CALCULATOR (CPCalc) COPYRIGHT 2005 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 68FM-S17-08 REVISION 8 17 OCTOBER 2005 7 MARCH 2014 U.S. S17-1 SECTION V -
More informationSUPPLEMENT 9 EASA CERTIFIED AIRPLANES
EASA CERTIFIED AIRPLANES 680-0001 AND ON This Airplane Flight Manual Supplement is approved by the US Federal Aviation Administration (FAA) on behalf of the European Aviation Safety Agency (EASA). COPYRIGHT
More informationCESSNA MODEL 208B 867 SHP - GARMIN G1000 Serials 208B2197 and 208B5000 and On
CESSNA MODEL 208B 867 SHP - Serials 208B2197 and 208B5000 and On L-3 COMMUNICATIONS FA2100 COCKPIT VOICE AND FLIGHT DATA RECORDER SERIAL NO. REGISTRATION NO. This supplement must be inserted into Section
More informationCESSNA CITATION IIB PW JT15D-4 INTRODUCTION. Runway Analysis provides the means to determine maximum allowable takeoff and landing weights based upon:
CESSNA CITATION IIB PW JT15D-4 INTRODUCTION Runway Analysis provides the means to determine maximum allowable takeoff and landing weights based upon: Airport characteristics consisting of airport elevation,
More informationRunway Analysis User Guide
Runway Analysis User Guide The Runway Analysis & Weight and Balance functions are accessed by selecting Runway Analysis & Weight and Balance from the Flight Plan drop down menu. Select the tail to be used
More informationINSTRUCTIONS FOR USING THIS SAMPLE FLIGHT MANUAL SUPPLEMENT
INSTRUCTIONS FOR USING THIS SAMPLE FLIGHT MANUAL SUPPLEMENT 1. For those installations not installed in accordance with GDL 82 Mooney M20 Series STC SA02573SE, a flight manual supplement may be created
More informationMyTraveler User s Manual
MyTraveler User s Manual MyTraveler is the DataTraveler Elite tool that enables you to access and customize your DataTraveler Elite through the MyTraveler Console. Messages and prompts guide you through
More informationTRANSMITTAL SHEET. Concurrent Requirement Added G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016)
TRANSMITTAL SHEET This sheet transmits Revision A, dated, to Gulfstream G450 Aircraft Service Change 016, dated August 18, 2005, titled Aircraft General (ATA 00) Maximum Takeoff Gross Weight (MTOGW) Increase.
More informationRevision Transmittal. June 11, Cessna Distributors and Authorized Service Facilities and CPC's
Revision Transmittal June 11, 2015 TO: Cessna Distributors and Authorized Service Facilities and CPC's SUBJECT: Multi-engine Service Bulletin, Pilot and Copilot Secondary Seat Stop Installation. REASON
More informationNUMBER 903 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE
NUMBER 903 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE June 9, 2005 PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE This service
More informationNUMBER 904 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE
NUMBER 904 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE October 27, 2005 PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE This service
More informationVideo Media Center - VMC 1000 Getting Started Guide
Video Media Center - VMC 1000 Getting Started Guide Video Media Center - VMC 1000 Getting Started Guide Trademark Information Polycom, the Polycom logo design, Video Media Center, and RSS 2000 are registered
More informationFAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
SUPPLEMENTAL TYPE CERTIFICATE NUMBER SA11103SC HALO 250 COMMUTER CATEGORY CONVERSION OF BEECHCRAFT KING AIR 200 SERIES AIRPLANES FAA APPROVED Airplane Serial No: This supplement must be attached to the
More informationSERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.
Citation TITLE SERVICE BULLETIN SB525B-25-01 EQUIPMENT/FURNISHINGS - PASSENGER SEAT GEAR AND BACKREST LATCH PIN REPLACEMENT EFFECTIVITY MODEL SERIAL NUMBERS 525B -0001 thru -0022 REASON The equivalent
More informationWeight and Balance User Guide
Weight and Balance User Guide Selecting the Weight and Balance tab brings up the Departure and Destination screen, used for initiating the process for a standalone WB report. Select the tail to be used
More informationCESSNA SECTION 5 PERFORMANCE
CESSNA SECTION 5 TABLE OF CONTENTS Page Introduction............................................5-3 Use of Performance Charts................................5-3 Sample Problem........................................5-4
More informationSERVICE LETTER REVISION
Citation Revision 1 SERVICE LETTER REVISION SL750-71-13 TRANSMITTAL SHEET This sheet transmits Revision 1 to SL750-71-13. A. Attaches the latest revision of the Rolls-Royce Notice To Operators (NTO) Number
More informationAIRCRAFT SERVICE CHANGE
AIRCRAFT SERVICE CHANGE NUMBER 909 SUBJECT INDICATING / RECORDING (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE DECEMBER 22, 2011 PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM
More informationSERVICE BULLETIN REVISION
Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to which: A. Removes the NOTE from the Effectivity section. B. Adds a NOTE to the Reason section. C. Changes SB750-76-06 to SB750-76-07
More informationAIRCRAFT SERVICE CHANGE
AIRCRAFT SERVICE CHANGE NUMBER 907 SUBJECT INDICATING / RECORDING (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE (SV-PFD) September 8, 2008 PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING
More informationSERVICE BULLETIN SERIAL NUMBERS
TITLE ENGINE INDICATING - ENGINE TREND MONITOR CALIBRATION EFFECTIVITY MODEL SERIAL NUMBERS 560 (Citation Ultra) -0387, -0392, -0404, -0410, -0415, -0420, -0426, -0452, -0456, -0462, -0468, -0472, -0495,
More informationBEARHHAWK Weight and Balance
BEARHHAWK Weight and Balance Author: Greg Hale -------- ghale5224@aol.com Rev. Date: 3/23/2008 5:14 PM The Bearhawk weight and balance program was designed for the Bearhawk aircraft. The program includes
More informationRV10 Weight and Balance
RV10 Weight and Balance Author: Greg Hale -------- ghale5224@aol.com Rev. Date: 4/15/2008 11:43:34 AM The RV10 weight and balance program was designed for the Van's RV10 aircraft. The program includes
More informationUSE OF TAKEOFF CHARTS [B737]
USE OF TAKEOFF CHARTS [B737] 1. Introducton This documentation presents an example of takeoff performance calculations for Boeing 737. It is called self-dispatch, primarily used by airline crew if that
More informationHawker 850XP. Supplement Pack
Hawker 85XP Supplement Pack The supplements contained in this supplement pack may not have been approved yet by foreign regulatory agencies. To determine approval status, view our web page at http://pubs.beechcraft.com
More informationSERVICE BULLETIN. SERIAL NUMBERS thru B0001 thru 208B5178
TITLE ICE AND RAIN PROTECTION - TKS ICE WARNING PLACARD REPLACEMENT EFFECTIVITY The airplanes that follow that are equipped with TKS with Fairing and the airplanes that follow that are equipped with TKS
More informationSection 7 Supplements. Miodel 400A SUPPLEMENTS
Miodel 400A SUPPLEMENTS Section 7 Supplements NOTE When a new airplane is delivered from the factory, the handbook delivered with it contains either an STC (Supplement Type Certificate) Supplement or a
More informationHAWKER BEECHCRAFT CORPORATION MODELS B300 AND B300C (C-12W) AIRPLANES
Page 1 2011-15-05 HAWKER BEECHCRAFT CORPORATION MODELS B300 AND B300C (C-12W) AIRPLANES Amendment 39-16752 Docket No. FAA-2011-0436; Directorate Identifier 2011-CE-009-AD PREAMBLE (a) Effective Date This
More informationAIRCRAFT SERVICE CHANGE
AIRCRAFT SERVICE CHANGE NUMBER 077 SUBJECT NAVIGATION (ATA 34) TCAS 7.1 INSTALLATION JUNE 12, 2012 PILOTS INFORMATION SHEET TCAS 7.1 INSTALLATION This service change upgrades TCAS 2000 or 3000SP systems
More informationSERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 525 (CJ1+) thru with GPS-4000S installed
SERVICE BULLETIN TITLE NAVIGATION - GPS-4000S SOFTWARE UPDATE EFFECTIVITY MODEL SERIAL NUMBERS 525 (CJ1+) -0600 thru -0701 with 822-2189-002 GPS-4000S installed 525A (CJ2+) -0300 thru -0518 with 822-2189-002
More informationSERVICE BULLETIN. The airplanes that follow that are equipped with the Garmin G1000 Nav III Avionics Option and the WAAS installed with SB
TITLE NAVIGATION - GARMIN G1000 ADS-B OUT INSTALLATION EFFECTIVITY The airplanes that follow that are equipped with the Garmin G1000 Nav III Avionics Option and the factory installed Wide Area Augmentation
More informationSERVICE LETTER REVISION
Revision 13 REVISION TRANSMITTAL SHEET This sheet transmits Revision 13 to, which: A. Updates the Accomplishment Instructions and the list of training agencies. B. Revises the expiration date to March
More informationType Acceptance Report
TAR 11/21B/5 Revision 2 AVIAT A-1 HUSKY Series Aircraft Certification Unit TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. STATE-OF-DESIGN TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE DETAILS
More informationUSE OF LANDING CHARTS [B737]
USE OF LANDING CHARTS [B737] 1. Introducton The landing stage of a flight is usually the path from 50 ft above the landing threshold and the place where an airplane comes to a complete stop. The 50 ft
More informationSERVICE BULLETIN REVISION
Revision 2 REVISION TRANSMITTAL SHEET This sheet transmits Revision 2 to, which: A. Removes JAA and replaces it with EASA. B. Adds the EASA Approval statement. NOTE: This revision replaces the original
More informationSUPERSEDED. [Docket No. FAA ; Directorate Identifier 2005-CE-08-AD; Amendment ; AD ]
[Federal Register: April 11, 2005 (Volume 70, Number 68)] [CORRECTIONS] [Page 18463] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr11ap05-186] DEPARTMENT OF TRANSPORTATION
More informationSERVICE BULLETIN TITLE NAVIGATION - GARMIN G1000 ENHANCED SEARCH AND RESCUE ENABLEMENT
TITLE NAVIGATION - GARMIN G1000 ENHANCED SEARCH AND RESCUE ENABLEMENT EFFECTIVITY The following G1000-equipped airplanes with system software version 0563.24 (or later) installed: MODEL 172R 172S 182T
More informationHawker 900XP. FAA Approved Airplane Flight Manual Supplement Pack
Hawker 900XP Supplement Pack The supplements contained in this supplement pack may not have been approved yet by foreign regulatory agencies. To determine approval status, view our web page at http://pubs.beechcraft.com
More informationThe following airplanes equipped with the Garmin G1000 Avionics system:
Single Engine Service Bulletin July 22, 2011 TITLE AVIONICS SWITCH INSPECTION AND REPLACEMENT EFFECTIVITY The following airplanes equipped with the Garmin G1000 Avionics system: Model Serial Numbers 172R
More informationSERVICE BULLETIN. NOTE: SL should be accomplished in conjunction with this service bulletin.
SERVICE BULLETIN TITLE NAVIGATION - TDR-94D TRANSPONDER UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS 560 ( Encore+) -0751thru-0802 with diversity enhanced surveillance transponders The equivalent of this service
More informationApplicable to the following airplanes equipped with a Cessna Factory Installed Honeywell KT 76C Transponder.
Single Engine Service Bulletin February 27, 2006 TITLE HONEYWELL KT 73 MODE S TRANSPONDER INSTALLATION EFFECTIVITY Applicable to the following airplanes equipped with a Cessna Factory Installed Honeywell
More informationInstallation of ActiveModeler Avantage
Installation of ActiveModeler Avantage KAISHA-Tec Corporation January 2009 Overview 1. This document explains the procedure for the installation of ActiveModeler Avantage 2. The procedure has 3 main steps
More informationATTACHMENT. Company Name: Initial Shipping Address (if different from the Revision
Single Engine ATTACHMENT ELECTRONIC PILOT'S CHECKLIST REGISTRATION The NAV III Electronic Pilot s Checklist product enhancement provides the Pilot s Checklist to appear on the Multi-Function Display (MFD)
More informationPRE-SOLO KNOWLEDGE TEST Diamond Eclipse DA20-C1
PRE-SOLO KNOWLEDGE TEST Diamond Eclipse DA20-C1 Name Date 1 List the airspeeds and their definitions for your airplane. Visual Indication on the Definition Indicator (color) V SO V S1 V R V X T/O V X CRUISE
More informationAdvisory Circular. Regulations for Terrain Awareness Warning System
Advisory Circular Subject: Regulations for Terrain Awareness Warning System Issuing Office: Standards Document No.: AC 600-003 File Classification No.: Z 5000-34 Issue No.: 03 RDIMS No.: 10464059-V5 Effective
More informationPART 210 NOISE ABATEMENT AND RUNWAY PROCEDURES NOISE ABATEMENT AND PREFERENTIAL RUNWAY USE PROCEDURES
PART 210 NOISE ABATEMENT AND RUNWAY PROCEDURES 210.01 NOISE ABATEMENT AND PREFERENTIAL RUNWAY USE PROCEDURES 210.01-1 Establishment Of Procedures; FAA Guidelines This Rule establishes preferential runway
More information4 REPORTS. The Reports Tab. Nav Log
4 REPORTS This chapter describes everything you need to know in order to use the Reports tab. It also details how to use the TripKit to print your flight plans and other FliteStar route data. The Reports
More informationUVACARS User Guide Version 1.0
UVACARS User Guide Version 1.0 Effective 1 February 2015 Table of Contents List of Revisions... 3 Credits... 4 Introduction... 5 Installation... 6 Using UVACARS... 8 Getting Started... 8 Preparing UVACARS
More informationSERVICE LETTER TITLE EQUIPMENT/FURNISHINGS - AMSAFE AIRPLANE FLIGHT MANUAL SUPPLEMENT
Single Engine SERVICE LETTER TITLE EQUIPMENT/FURNISHINGS - AMSAFE AIRPLANE FLIGHT MANUAL SUPPLEMENT EFFECTIVITY MODEL SERIAL NUMBERS 172R 17281588 thru 17281615 172S 172S11092 thru 172S11176 182T 18282302
More information[Docket No. FAA ; Product Identifier 2017-NM-174-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 01/19/2018 and available online at https://federalregister.gov/d/2018-00657, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationCIVIL AVIATION AUTHORITY, PAKISTAN OPERATIONAL CONTROL SYSTEMS CONTENTS
CIVIL AVIATION AUTHORITY, PAKISTAN Air Navigation Order No. : 91-0004 Date : 7 th April, 2010 Issue : Two OPERATIONAL CONTROL SYSTEMS CONTENTS SECTIONS 1. Authority 2. Purpose 3. Scope 4. Operational Control
More informationValley Fliers 1402 Auburn Way North, #223 Auburn WA 98002
Valley Fliers 1402 Auburn Way North, #223 Auburn WA 98002 Instructor: Check Out Date: Phase 1: Pre-Flight Name: Certificate Number: Certificate Type: Ratings: Total Flight Time: Last 90 Days: Club check
More informationRunway Length Analysis Prescott Municipal Airport
APPENDIX 2 Runway Length Analysis Prescott Municipal Airport May 11, 2009 Version 2 (draft) Table of Contents Introduction... 1-1 Section 1 Purpose & Need... 1-2 Section 2 Design Standards...1-3 Section
More information1.- Introduction Pages Description 21.- Tutorial 22.- Technical support
FriendlyPanels Software WARNING This operating manual has been written to be used only with Microsoft Simulator. Flight FriendlyPanels www.friendlypanels.net fpanels@friendlypanels.net Table of Contents
More informationTo add airplane serial numbers thru and 172S0001 thru 172S9974 to the Effectivity section.
Revision Transmittal February 13, 2006 TO: Cessna Distributors, Single Engine Service Stations and CPC's SUBJECT: Single Engine Service Bulletin, Floorboard Bulkhead Rivet Inspection. REASON FOR REVISION
More informationAAIB Bulletin: 1/2017 G-EZFJ EW/C2016/04/01. None. 57 years
SERIOUS INCIDENT Aircraft Type and Registration: No & Type of Engines: Airbus A319-111, G-EZFJ 2 CFM CFM56-5B5/3 turbofan engines Year of Manufacture: 2009 (Serial no: 4040) Date & Time (UTC): Location:
More informationGULFSTREAM AEROSPACE CORPORATION
Page 1 2011-24-02 GULFSTREAM AEROSPACE CORPORATION Amendment 39-16866 Docket No. FAA-20110572; Directorate Identifier 2011-NM-009-AD. PREAMBLE (a) Effective Date This AD is effective January 3, 2012. (b)
More informationSERVICE LETTER TITLE AIR CONDITIONING - TRANSMIT KELLY AEROSPACE SERVICE BULLETIN KATS-SB
Single Engine SERVICE LETTER TITLE AIR CONDITIONING - TRANSMIT KELLY AEROSPACE SERVICE BULLETIN KATS-SB-16-001 EFFECTIVITY REASON All Cessna model 182T's and T206H's delivered from the factory with Kelly
More informationCommercial Pilot Practical Test Briefing
Commercial Pilot Practical Test Briefing 1. What certificates and documents must you have on board the aircraft prior to flight? 2. Locate the following inspections, as appropriate, in the airframe and
More informationThe following airplanes equipped with the Garmin G1000 Nav III Avionics Option: Serial Numbers
Single Engine Service Bulletin June 22, 2009 TITLE GARMIN G1000 SYNTHETIC VISION TECHNOLOGY (SVT) INSTALLATION EFFECTIVITY The following airplanes equipped with the Garmin G1000 Nav III Avionics Option:
More informationGarmin GNC 420 GPS Navigator with VHF COM
Cirrus Design Section 9 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Garmin GNC 420 GPS Navigator with VHF COM When a GARMIN GNC 420 GPS Navigator with VHF COM is installed
More informationultimate traffic Live User Guide
ultimate traffic Live User Guide Welcome to ultimate traffic Live This manual has been prepared to aid you in learning about utlive. ultimate traffic Live is an AI traffic generation and management program
More informationCOVER SHEET. Reduced Vertical Separation Minimum (RVSM) Information Sheet Part 91 RVSM Letter of Authorization
COVER SHEET Reduced Vertical Separation Minimum (RVSM) Information Sheet Part 91 RVSM Letter of Authorization NOTE: FAA Advisory Circular 91-85 ( ), Authorization of Aircraft and Operators for Flight in
More informationBF Goodrich Avionics Systems, Inc. SKYWATCH SKY497
Página 1 de 6 RGL Home Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [63 FR 66746 No. 232 12/03/98]
More informationSUPERSEDED. [Docket No. FAA ; Directorate Identifier 2008-NM-061-AD; Amendment ; AD ]
[Federal Register: April 23, 2008 (Volume 73, Number 79)] [Rules and Regulations] [Page 21811-21813] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr23ap08-2] DEPARTMENT
More informationREPORT A-024/2012 DATA SUMMARY
REPORT A-024/2012 DATA SUMMARY LOCATION Date and time Sunday, 1 July 2012; 08:45 UTC 1 Site La Juliana Aerodrome (Seville, Spain) AIRCRAFT Registration Type and model Operator HA-NAH SMG-92 Turbo Finist
More informationGAR-AERO WHEEL ADAPTERS & TIRES
FOUND FBA-2C2 SUPPLEMENT M400-S03 Transport Canada Approved Flight Manual Supplement For GAR-AERO WHEEL ADAPTERS & This supplemental manual is applicable to Gar-Aero Wheel Adapters & 8.50-10 tires equipped
More information[Docket No. FAA ; Directorate Identifier 2005-CE-34-AD; Amendment ; AD ]
[Federal Register: December 12, 2005 (Volume 70, Number 237)] [Rules and Regulations] [Page 73355-73358] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr12de05-4] DEPARTMENT
More informationDemonstration and. 4. Contact List. Federal Aviation Administration. Administration
Demonstration and Hands-On Training Presented to: VII ALACPA Airport Pavement Seminar & V FAA Airport Pavement Workshop By: David R. Brill, P.E., Ph.D. Date: Information on Disk 1. FAA Computer Programs
More informationFLIGHT AND OPERATING MANUAL SUPPLEMENT FMS305902, REVISION 1 SEAPLANES WEST INC.
FLIGHT AND OPERATING MANUAL SUPPLEMENT FMS305902, REVISION 1 AEROCET 3500/3500L FLOAT INSTALLATION ON CESSNA 182E THROUGH 182N AIRCRAFT AIRCRAFT MODEL: AIRCRAFT REGISTRATION: AIRCRAFT SERIAL NUMBER: TRANSPORT
More informationFlight Crew Operating Manual STANDARD OPERATING PROCEDURES
CONTENTS 9.00.01 P 2 9.00.01 CONTENTS... 2 9.01.01 CONFIGURE... 3 9.01.02 CONFIGURE... 4 9.02.01 START... 5 9.02.02 START... 6 9.03.01 REFUEL... 7 9.03.02 REFUEL... 8 9.04.01 STATUS... 9 9.05.01 FDR...
More informationDeveloping an Aircraft Weight Database for AEDT
17-02-01 Recommended Allocation: $250,000 ACRP Staff Comments This problem statement was also submitted last year. TRB AV030 supported the research; however, it was not recommended by the review panel,
More informationAdvisory Circular (AC)
Advisory Circular (AC) Certification of Transport Category Aeroplanes On Narrow Runways File No. 5009-6-525 AC No. 525-014 RDIMS No. 528471-V3 Issue No. 01 Issuing Branch Aircraft Certification Effective
More informationEMC Unisphere 360 for VMAX
EMC Unisphere 360 for VMAX Version 8.3.0 Installation Guide REV 01 Copyright 2014-2016 EMC Corporation. All rights reserved. Published in the USA. Published September 2016 EMC believes the information
More informationChapter 1. Draw Standard Departure Procedure
Chapter 1. Draw Standard Departure Procedure 1. Prior to drawing departure area consult the US Terminal Procedures book to determine if there are published take off special Take Off Minimums and (Obstacle)
More information[Docket No. FAA ; Product Identifier 2018-NM-131-AD] AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 12/26/2018 and available online at https://federalregister.gov/d/2018-27882, and on govinfo.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationAPPENDIX X: RUNWAY LENGTH ANALYSIS
APPENDIX X: RUNWAY LENGTH ANALYSIS Purpose For this Airport Master Plan study, the FAA has requested a runway length analysis to be completed to current FAA AC 150/5325-4B, Runway Length Requirements for
More informationTRAINING BULLETIN No. 1
TRAINING BULLETIN No. 1 Introduction: Hickok & Associates has provided a new charting legend Hickok & Associates Helicopter Instrument Approach and Departure Charts - Charting Format & Legend (Revision2),
More informationSITE ELEVATION AMSL...Ground Elevation in feet AMSL STRUCTURE HEIGHT...Height Above Ground Level OVERALL HEIGHT AMSL...Total Overall Height AMSL
******************************************** * Federal Airways & Airspace * * Summary Report * ******************************************** File: User Assigned File Name Latitude: NAD83 Coordinate Longitude:
More informationSERVICE LETTER COMMUNICATIONS - LINK CPDLC AND VHF ACARS CONFIGURATION VERIFICATION
TITLE COMMUNICATIONS - LINK 2000+ CPDLC AND VHF ACARS CONFIGURATION VERIFICATION EFFECTIVITY MODEL 525B (CJ3+) SERIAL NUMBERS -0451 thru -0517 with Link 2000+ CPDLC or VHF ACARS options REASON The equivalent
More informationSUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 40 NG. Integrated Avionics System Garmin G1000,
DA 40 NG AFM Garmin G1000, P-RNAV Operation SUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 40 NG Integrated Avionics System Garmin G1000, Doc. No. : 6.01.15-E Date of Issue : Design Change Advisory :
More informationOffice of Research and Engineering Safety Study Report: Introduction of Glass Cockpit Avionics into Light Aircraft Study Overview Joseph Kolly
Office of Research and Engineering Safety Study Report: Introduction of Glass Cockpit Avionics into Light Aircraft Study Overview Joseph Kolly NTSB Research Mandate Title 49 United States Code, Chapter
More informationDiamond Aircraft Industries GmbH N.A. Otto-Str.5 A-2700 Wiener Neustadt Austria
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A47CE Revision 12 DIAMOND DA 40 DA 40 F DA 40 NG FEB 21, 2014 TYPE CERTIFICATE DATA SHEET NO. A47CE This data sheet which is part of Type Certificate
More informationSERVICE BULLETIN TITLE NAVIGATION - ENHANCED SURVEILLANCE TRANSPONDER STRAPPING MODIFICATION
TITLE NAVIGATION - ENHANCED SURVEILLANCE TRANSPONDER STRAPPING MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 525B (CJ3) -0001 thru -0056, -0058 thru -0262, and -0264 thru -0293 equipped with TCAS I NOTE:
More informationPilot s Operating Handbook Supplement AS-04
SECTION 9 Pilot s Operating Handbook Supplement GPS and Multifunctional Display FLYMAP L This AFM supplement is applicable and must be inserted into Section 9 of the Airplane Flight Manual when the FLYMAP
More informationFAR and Military Requirements
FAR and Military Requirements W. H. Mason Advanced Conceps from NASA TM-1998-207644 slide 1 2/19/03 FAR and MIL STD Requirements Gov t requirements dictate some of the design requirements interest is safety,
More information[Docket No. FAA ; Directorate Identifier 2015-NM-006-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 99 (Monday, May 23, 2016)] [Rules and Regulations] [Pages 32227-32228] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No:
More informationTechnical Standard Order
Department of Transportation Federal Aviation Administration Aircraft Certification Service Washington, DC TSO-C145a Effective Date: 09/19/02 Technical Standard Order Subject: AIRBORNE NAVIGATION SENSORS
More informationCESSNA 400 EQUIPPED WITH GARMIN G1000
CESSNA 400 EQUIPPED WITH GARMIN G1000 After reading through the Information Manual, please complete this assignment. All answers can be found in the Information Manual in the section as noted in the right
More informationTechnology Briefing. Note: Changes since the last version of this document (Rev. 7 July 24, 2015) are highlighted.
Technology Briefing Subject: Version 7.1 (ACAS II Version 7.1) Date: December 22, 2015 Distribution: Citation, Beechcraft, and Hawker Operators Revision: 8 Note: Changes since the last version of this
More informationOperators may need to retrofit their airplanes to ensure existing fleets are properly equipped for RNP operations. aero quarterly qtr_04 11
Operators may need to retrofit their airplanes to ensure existing fleets are properly equipped for RNP operations. 24 equipping a Fleet for required Navigation Performance required navigation performance
More informationRevisions to this AML must be coordinated between the STC holder and the responsible Aircraft Certification Office (ACO), and require FAA approval.
For ADS-B Out & In Airworthiness 2. Introduction This document is the Federal Aviation Administration (FAA) Approved Model List (AML) for Supplemental Type Certificate (STC) Number ST00835DE, for installing
More informationSERVICE BULLETIN SB
TITLE NAVIGATION - ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) AUDIO INHIBIT WIRE INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 525 (CJ1+) -0615, -0623 REASON A wire was omitted that enables the EGPWS
More informationCHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS
CHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS General...2 Kinds of Operations...2 Structural and weight limitations...2 Maneuvering limitations...3 Flight load factor limitations...3 Power plant
More informationFAA Requirements for Engine-out Procedures and Obstacle Clearance
FAA Requirements for Engine-out Procedures and Obstacle Clearance Presentation to: CAAC Engine-out Procedures Seminar Name: Chuck Friesenhahn Date: 11/29/2005 Flight Standards Senior Advisor, Advanced
More information[Docket No. FAA ; Product Identifier 2017-CE-049-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 30 (Tuesday, February 13, 2018)] [Rules and Regulations] [Pages 6114-6118] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
More informationType Acceptance Report
TAR 13/21B/8 PIPER PA-20 Aircraft Certification Unit TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. ICAO TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE DETAILS 1 4. NZCAR 21.43 DATA REQUIREMENTS
More informationPlease read this guide carefully. It tells you how to prepare your cutting plotter for production use in a few easy steps.
OPERATING GUIDE for Secabo mini Cutting Plotter Congratulations on purchasing your Secabo mini cutting plotter! Please read this guide carefully. It tells you how to prepare your cutting plotter for production
More informationGARMIN Ltd. or its subsidiaries c/o GARMIN International, Inc E. 151st Street Olathe, Kansas U.S.A.
GARMIN Ltd. or its subsidiaries c/o GARMIN International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 U.S.A. EASA Approved AIRPLANE FLIGHT MANUAL SUPPLEMENT GTX 33X and GTX 3X5 Transponders for ADS-B
More information