Honeywell EGPWS manuel d'utilisation

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Le mot vient du latin "Instructio", à savoir organiser. Ainsi, le manuel d’utilisation Honeywell EGPWS décrit les étapes de la procédure. Le but du manuel d’utilisation est d’instruire, de faciliter le démarrage, l'utilisation de l'équipement ou l'exécution des actions spécifiques. Le manuel d’utilisation est une collection d'informations sur l'objet/service, une indice.

Malheureusement, peu d'utilisateurs prennent le temps de lire le manuel d’utilisation, et un bon manuel permet non seulement d’apprendre à connaître un certain nombre de fonctionnalités supplémentaires du dispositif acheté, mais aussi éviter la majorité des défaillances.

Donc, ce qui devrait contenir le manuel parfait?

Tout d'abord, le manuel d’utilisation Honeywell EGPWS devrait contenir:
- informations sur les caractéristiques techniques du dispositif Honeywell EGPWS
- nom du fabricant et année de fabrication Honeywell EGPWS
- instructions d'utilisation, de réglage et d’entretien de l'équipement Honeywell EGPWS
- signes de sécurité et attestations confirmant la conformité avec les normes pertinentes

Pourquoi nous ne lisons pas les manuels d’utilisation?

Habituellement, cela est dû au manque de temps et de certitude quant à la fonctionnalité spécifique de l'équipement acheté. Malheureusement, la connexion et le démarrage Honeywell EGPWS ne suffisent pas. Le manuel d’utilisation contient un certain nombre de lignes directrices concernant les fonctionnalités spécifiques, la sécurité, les méthodes d'entretien (même les moyens qui doivent être utilisés), les défauts possibles Honeywell EGPWS et les moyens de résoudre des problèmes communs lors de l'utilisation. Enfin, le manuel contient les coordonnées du service Honeywell en l'absence de l'efficacité des solutions proposées. Actuellement, les manuels d’utilisation sous la forme d'animations intéressantes et de vidéos pédagogiques qui sont meilleurs que la brochure, sont très populaires. Ce type de manuel permet à l'utilisateur de voir toute la vidéo d'instruction sans sauter les spécifications et les descriptions techniques compliquées Honeywell EGPWS, comme c’est le cas pour la version papier.

Pourquoi lire le manuel d’utilisation?

Tout d'abord, il contient la réponse sur la structure, les possibilités du dispositif Honeywell EGPWS, l'utilisation de divers accessoires et une gamme d'informations pour profiter pleinement de toutes les fonctionnalités et commodités.

Après un achat réussi de l’équipement/dispositif, prenez un moment pour vous familiariser avec toutes les parties du manuel d'utilisation Honeywell EGPWS. À l'heure actuelle, ils sont soigneusement préparés et traduits pour qu'ils soient non seulement compréhensibles pour les utilisateurs, mais pour qu’ils remplissent leur fonction de base de l'information et d’aide.

Table des matières du manuel d’utilisation

  • Page 1

    Honeywell Electronics Honeywell Electronics Enhanced Ground Proximity Warning System (EGPWS): Flight History Data Flight History Data J im M u lkin s Ju s EGPWS Sr. Systems Engineer Honeywell Aerospace August 27, 2012[...]

  • Page 2

    EGPWS Flight History Data EGPWS Flight History Data was designed to: • EGPWS Flight History Data was designed to: - Provide detailed data on EGPWS alerts  to improve terrain database  to evaluate the performance of EGPWS algorithms in real-world operation • maximize CFIT protection • minimize nuisance alarms • EGPWS Flight History Dat[...]

  • Page 3

    EGPWS Flight History Data - Limitations EGPWS Flight History Data: • EGPWS Flight History Data: - Does NOT record Date & Time  EGPWS system time (hours:minutes:seconds) powered  Flight Leg (Leg 1 is most recent flight) - Is NOT environmentally protected or crashworthy  The EGPWS can be damaged beyond the ability to provide any data -[...]

  • Page 4

    EGPWS Units – Class A TAWS MK V & MK VII • MK V & MK VII - 2 MCU (2.5”W x 8”H x 13”D) - Found in  All Boeing  Most Airbus  Large and Medium business jets • MK VI & MK VIII & MK XXII - (3”W x 6”H x 10”D) - Found in  Medium and Small business jets  Turboprops  IFR Helico p ters 4 File Number p[...]

  • Page 5

    EGPWS Units – Class B TAWS • KGP560 & KGP860 & MK XXI - (2”W x 4”H x 6”D) Found in - Found in  Small business jets  Turboprops  VFR Helicopters  VFR Helicopters • KMH820 & KMH920 KMH820 & KMH920 - 4 MCU (4”W x 7”H x 13”D) - Earlier units are black Fd i - F oun d i n  Small business jets  Turboprop[...]

  • Page 6

    EGPWS Flight History Data (Warning/Caution) • EGPWS records data 20 seconds before and 10 seconds after every EGPWS alert/warning  Used to determine a cause of the alert/warnin g and p ilot reaction gp 20 Seconds 10 Seconds Caution T errain 6 File Number[...]

  • Page 7

    EGPWS Flight History Parameters • List of parameters recorded in EGPWS Warning Flight History Data A l er t Type Ter r ai n D at abase El evat i on Engi ne Tor que Dat a #1 Ale r t Type T e rrain Da t aba se Elevat ion S y s t e m Op e r a tin g T im e GP S S a te llite s V is ib le C orr ect ed A l t i t ude G PS Satel l i t es Tracked Lat i t u[...]

  • Page 8

    EGPWS Flight History Data Does not record what is not input • Does not record what is not input - For example, no radio altitude on KGP or KMH Class B units • Data that is invalid is noted as such - For example, glideslope deviation when not ILS tuned • Data is recorded even when manually inhibited by pilot • Data can be exported to Excel s[...]

  • Page 9

    Flight History Retrieval Process • Flight History information is stored in the EGPWS in a specific area of the non-volatile memory Data can be downloaded via PCMCIA or CF card • Data can be downloaded via PCMCIA or CF card - Card must be programmed with special instruction file - Process similar to terrain database upload, requires < 5 minut[...]

  • Page 10

    S / Hawker 800 crash at Owatonna MN • NT S B AAR-11 / 01, 31 July 2008, – 8 Fatal - CVR, no FDR and none required - Crashed while attem p tin g late g o-around on runwa y 30 pg g y • EGPWS issued Bank Angle alert - Aircraft rolled 90 degrees after becoming airborne off rwy end Flight History download performed at Honeywell • Flight History [...]

  • Page 11

    S / f Cessna 560 crash at Pueblo, CO • NT S B AAR-07 / 02, 16 February 2005 – 8 f atal - CVR, no FDR and none required - Pueblo was a p lanned fuel sto p on cross-countr y fli g ht pp yg - Crashed 4 mi short of airport in freezing rain • EGPWS issued Bank Angle alert EGPWS destroyed in impact fire - EGPWS destroyed in impact , fire - Circuit [...]

  • Page 12

    Honeywell Electronics Non-Volatile Memory (NVM): An Increasin g Aide in Investi g ations Jay Eller gg Air Safety Investigator Honeywell Aerospace August 27, 2012 12 File Number[...]

  • Page 13

    Agenda What Data is What is the manufacturer ’s intended use of NVM data? What can we learn from data obtained from NVM? A vailable What can we learn from data obtained from NVM? Airframes and What types of equipment What types of airframes and Equipment have NVM data? have NVM data? Handling of Equipment Wh at co m p li cat i o n s a n d p r eca[...]

  • Page 14

    Mi t / T k i Intended Uses of NVM in Electronics • M a i n t enance /T rac ki ng - Logging of failures which require maintenance at next interval. - Logging of exceedances or failures which may require i di t tt ti i mme di a t e a tt en ti on. - Tracking of fleet such as EMS and Fire Fighting. • Trend anal y sis y - Engine performance over a p[...]

  • Page 15

    L Fid lit D t Various Levels of Data Available • L ow Fid e lit y D a t a: • Slow sample rates (greater than 1 sample per minute) • Minimal data precision (ie: Latitude, Longitude, altitude, etc) • Would show long term trending with little inability to show immediate behaviors/signatures. • Medium Fidelity Data: • Medium Fidelity Data: [...]

  • Page 16

    Example of Low Fidelity Data 16 File Number 16 Data points are on 4 minute increments.[...]

  • Page 17

    Example of Medium Fidelity Data T urn made but unable to determine accuracy during the turn. (1 minute data p oints ) p) 17 File Number 17[...]

  • Page 18

    Example of High Fidelity Data (1Hz Rate) 18 File Number 18[...]

  • Page 19

    Example of High Fidelity Data (1Hz Rate) Notice location precision as witnessed during taxi! taxi! 19 File Number 19[...]

  • Page 20

    Types of Equipment and Data Fidelity a l a ight w ard FDR EVXP HUMS Sky t a Retriev a Str a For w EGPWS ( Gen Av ) EGPWS (Air Transport) Sky Connect a se of Da t Somewhat Involved A PEX ACM S () Transport) EPIC Maintenance System Engine Controls reasing E a Smart Servo Inc Highly Involved Servo Radios 20 File Number 20 Increasing Fidelity of Data H[...]

  • Page 21

    Aircraft With Primus APEX High, Medium, and Low Fidelity Data V iking Air T win Otter 400 Pilatus PC-12 NG 21 File Number 21 T win Otter 400[...]

  • Page 22

    Aircraft With HUMS High, Medium, and Low Fid lit D t Fid e lit y D a t a Sikorsky S76C++ Health and Usage S Health and Usage Monitoring System HUM S = 22 File Number 22 Agusta A109E[...]

  • Page 23

    Aircraft with Primus EPIC (Medium and Low Fidelity) Dassault F7X Dassault F900EX/DX/LX Dassault F2000EX/LX Dassault F7X Gulfstream 450 Dassault F2000EX/LX Gulfstream 650 Gulfstream 550 Embraer 170/190 Cessna 680 Sovereign Cessna 680 Sovereign Hawker 4000 23 File Number 23 Agusta A W139[...]

  • Page 24

    Examples of Aircraft With Sky Connect EMS Helo Fleet Medium and Low Fidelity Data Charter Fleet 24 File Number 24 Agriculture Fleet Fire and Rescue Note: Aircraft models shown may not repr esent actual models containing Sky Connect[...]

  • Page 25

    Pi & R f P reservat i on & R ecovery o f Non-Volatile Memory (NVM) Evidence 25 File Number 25[...]

  • Page 26

    General Precautions • A ssu m e t h at t h e e l ect r o ni c co m po n e n t i s subject to e l ect r ostat i c Assume that the electronic component is subject to electrostatic discharge (ESD) damage. - Do not attempt to handle any electronic components using leather gloves. • Before cutting wires to components i nsure component does not • B[...]

  • Page 27

    If an accident has occurred in fresh or salt water… • Recovered electronic components should be placed in a container filled with 2 MOhm de-ionized water. - Bottled drinking water is acceptable, provided the water has been produced using a reverse osmosis (RO) process, as opposed to bottled spring water. - Do not use tap water, distilled water [...]

  • Page 28

    General Packing and Shipping Guidelines • Use hard plastic shipping containers when possible – avoid Styrofoam. • Wra p electronic com p onents with a la y er of electrostatic safe pp y material, such as “pink poly” (named for its color) or other ESD approved product. • Use packing materials that will not react with the contents or dete[...]

  • Page 29

    In Closing… • Monitoring Systems and NVM Data – What it is… and is not. - It is a tool for investigators to use - It is not a fli g ht data recorder g • Plus's and Minus’s Large volume of available data Not crashworthy High G-load tolerant plastic NVM Not fire tolerant Fire tolerant ceramic NVM Not G-load tolerant Easy to read data[...]

  • Page 30

    Honeywell Digital Engine Controls Honeywell Digital Engine Controls Incident Recorder Applicability to Accident Investigation Jim Allen Mf A i d t I t i t i M anager o f A cc id en t I nves ti ga ti on Honeywell Aerospace August 27, 2012[...]

  • Page 31

    Agenda • Introduction Applications • Applications • Use of Engine Control Data in Accident Investigation Use of Engine Control Data in Accident Investigation • Post Accident Precautions • Honeywell Support in Investigations • Questions 31 File Number[...]

  • Page 32

    Turbofan Engine Digital Control System • Honeywell Turbofan Engines utilize Digital Control with Engine Condition Trend Monitoring (ECTM) - Two g enerations of controls g  Generation One, Digital Electronic Engine Controls (DEEC) • TFE731-2/3/4/5 (New Production and Retrofit of older units) • TFE731-20/40/50/60 (All from Production)  Ge[...]

  • Page 33

    Examples of Data available via ECTM • Engine Statistics - Engine & Computer Information – Model, Part, and Serial Number - Performance Trending Performance Trending - Life Cycle Data – Engine Times, Cycle Counting, Landings, etc. • Engine Troubleshooting & Maintenance • Engine Troubleshooting & Maintenance - Engine & Compu[...]

  • Page 34

    TFE731 DEEC – Generation One (Gen 1) TFE731-2/3/4/5 N1 DEEC (Retrofit) TFE731-20/40/50/60 DEEC (P d ti ) (Retrofit) - Fuselage mounted - (P ro d uc ti on ) - Engine mounted*- TFE731-50 DEEC in Haw ker 900X P is fuselage mounted 34 File Number[...]

  • Page 35

    Gen 1 Incident Recorder Design Parameters • Design Features • Design Features - Records nine engine and aircraft parameters. - Records basic engine and aircraft information for approximately the last 1 1/2 hours of engine operation last 1 1/2 hours of engine operation . - Begins recording when the start initiates. - Stops recording after engine[...]

  • Page 36

    HTF7000 Family – Generation Two (Gen 2) HTF7000 F ADEC (Engine mounted, 2 units per engine) 36 File Number[...]

  • Page 37

    Gen 2 Incident Recorder Design Parameters • Design Features • Design Features - Records 36 engine and aircraft parameters. - Records enhanced engine and aircraft information for the last 60 minutes of operation minutes of operation . - Begins recording when the start initiates. - Stops recording after engine shutdown or 5 minutes after WOW is t[...]

  • Page 38

    TFE731 Applications – Gen 1 Civil DEEC (Retrofit) Cessna Citation III/VI/VII Raytheon Hawker HS1-731; 125-400-731/60 0-731/700/80 0/800XP North American Rockwell Sabreliner 65 Dassault Falcon 20- 5/200 Dassault Falcon 10/100 Dassault Falcon 50 / 50- 4 Dassault Falcon 900 Lockheed Jetstar / Jetstar IAI Westwind 1 124 Gulfstream G100 Lockheed Jetst[...]

  • Page 39

    TFE731 Applications – Gen 1 Military DEEC (Retrofit & Production) CASA 101AA / BB / CC “A viojet” AIDC A T -3 “ Tzu Chiang” 39 File Number Hongdu (Nanchang) A viation Industry Corporation K8 “Karakorum” (Production) FMA IA 63 “Pampa”[...]

  • Page 40

    TFE731 Applications – Gen 1 Civil DEEC (Production) Dassault Falcon 50E X Dassault Falcon 900EX / 900DX Hawker 900XP Hawker 900XP Gulfstream G150 Gulfstream 100 (Astra SPX) 40 File Number Learjet M45 Learjet M40[...]

  • Page 41

    HTF7000 Family Turbofan Applications – Gen 2 Civil FADEC (Production) Bombardier Challen g er CL 300 Bombardier Challen g er CL 300 g g Gulfstream 280 Gulfstream 280 41 File Number Embraer Legacy 450 and 500 Embraer Legacy 450 and 500[...]

  • Page 42

    Use of Incident Recorder Data in Accident Investigation • These are NOT Flight Data Recorders but, - The data can be very helpful in backing up FDR and CVR data. - Can be especially helpful if FDR data is not recoverable, wasn’t working, or the aircraft wasn’t equipped with one. • Units are not hardened and desi g ned for im p act and gp fi[...]

  • Page 43

    Generation 1 DEEC Plotted Data 43 File Number[...]

  • Page 44

    Generation 1 DEEC Plotted Data 44 File Number[...]

  • Page 45

    Generation 2 FADEC Plotted Data 45 File Number[...]

  • Page 46

    Post Accident Precautions • If the DEEC or FADEC appears intact: • If the DEEC or FADEC appears intact: - Do not attempt to power up the units. - Do not attempt to download the data with process used by operator and field service personnel operator and field service personnel .  This process automatically erases the data from the units as pa[...]

  • Page 47

    Post Accident Precautions (continued) • Use care when cutting wires and removing harness • If possible don ’ t allow any electronic debris to If possible , don t allow any electronic debris to freeze. • Do not flex or straighten a bent, broken or damaged circuit card circuit card . • Avoid exposure to magnetic fields such as large motors,[...]

  • Page 48

    Honeywell Support for Downloading and Analysis • Honeywell is best equipped to handle and download • Honeywell is best equipped to handle and download the data from our engine DEEC’s and FADEC’s after an accident or incident. Hi t i t d t i d l t - H ave appropr i a t e equ i pmen t an d t ra i ne d personne l t o properly analyze and prepa[...]

  • Page 49

    Example of Challenging Download • Engine mounted TFE731 DEEC was severely heat • Engine mounted TFE731 DEEC was severely heat and impact damaged during the accident sequence. • Incident Recorder chi p p was cleaned, removed, and copied. • The chip copy was then installed in a then installed in a slave unit and successfully downloaded. 49 Fi[...]

  • Page 50

    Accident Contact Information • For assistance with any Honeywell Aerospace • For assistance with any Honeywell Aerospace products involved in an Accident or Incident, Contact: Jim Allen M a n age r o f A cc i de n t Inv est i gat i o n aa g e o c c d et e s t g a t o Honeywell Product Integrity 1944 E Sky Harbor Circle Phoenix Arizona 85234 Pho[...]

  • Page 51

    Questions? 51 File Number[...]