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1 APPLICATION DASH NO. NEXT ASSY USED ON , , , , , , , , , , , , , , , , , , , , , TITLE SHEET INDEX SHEET NO. TITLE SHEET 1 REVISIONS 2 DOCUMENT 3 This document is an unpublished work. Copyright 2012 Honeywell International Inc. All rights reserved. This document and all information and expression contained herein are the property of Honeywell International Inc. and is provided to the recipient in confidence on a need to know basis. Your use of this document is strictly limited to a legitimate business purpose requiring the information contained therein. Your use of this document constitutes acceptance of these terms. Typed signatures constitute approval. Actual signatures on file at Honeywell in Redmond WA. CONTRACT NO DRAWN PRECIOUS METAL INDICATOR CODE: NA Robin W Halbert 09/03/98 Honeywell International Inc. Redmond, Washington PCMCIA CARD DOWNLOAD PROCEDURE CHECK ENGR MFG QA APVD Robin W Halbert 09/03/98 for EGPWS SIZE CAGE CODE DWG NO. REV Gill Gilliland 09/03/98 A D APVD SCALE: NONE SHEET 1 OF 8 ASF-2121/R3

2 REVISIONS SH REV DESCRIPTION DATE APPROVED 7 A Changed EGPWS MODEL: to MOD STATUS: 5,6 B Changed SOFTWARE SERIAL NUMBER: to SERIAL NUMBER: Added (if known) to TERRAIN DATABASE NUMBER: Reason: 01, Severity: 10 Section 2 and 4: Changed Air Transport & Regional, M/S 42 to Air Transport & Lighting, M/ S L2F Section 2 and 4: Added Attn: EGPWS Certification Group Section 2 and 4: Added Or the request to: robin.halbert@honeywell.com. Reason: 01, Severity: Aug Aug OCT OCT 99 R. Halbert J. Mulkins R. Halbert M. Shannon All C Update document to Honeywell format Added MK VI & MK VIII procedures Added new Figure 1, renumbered existing Figures 1, 2 03 OCT OCT 00 R. Halbert J. Mulkins Reason: 01, Severity: 10 All D Update document for latest EGPWS PNs 25 MAY 12 J. Mulkins 25 MAY 12 L. Matter Reason: 01, Severity: 10 ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV D SHEET 2

3 Table of Contents 1. INTRODUCTION DOWNLOAD PROCEDURE DECODING OF FLIGHT HISTORY DATA...5 TRANSCRIPTION REQUEST FORM...6 FIGURE FIGURES 2 & ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV D SHEET 3

4 1. INTRODUCTION This document provides the procedure for downloading the Flight History from an aircraft equipped with a Honeywell Enhanced Ground Proximity Warning System (EGPWS). This download procedure is applicable for the following Honeywell EGPWS part numbers: XX-XXX-XXX (MK V) XXX (Airbus MK V) XXX (Boeing MK V) XX-XXX-XXX (MK VII) XX-XXX (MK VI) XX-XXX (MK VIII) XX-XXX (MK XXII) To purchase the Flight History Download PCMCIA Card necessary for this procedure, contact: Honeywell Complete Customer Care Center Telephone: (800) (U.S.A.) Telephone: (602) (International) Fax: orders@honeywell.com For MK V and MK VII EGPWS request Flight History Download Card P/N For MK VI and MK VIII and MK XXII EGPWS request Flight History Download Card P/N Flight History Download cards have a special Honeywell programmed format that is required to initiate the download sequence and record the data. The Fight History Download cards (P/N and ) are not interchangeable. 2. DOWNLOAD PROCEDURE. 1.For the MK VI, MK VIII, or MK XXII, access and connect SmartCable P/N or -002 (see Figure 1) to Test Connector J3 on the EGPWS front panel. For the MK V or MK VII, access and open the front panel door (see Figure 2) on the EGPWS. 2. Apply power to the EGPWS. 3. Verify that the green COMPUTER OK LED is ON. If the red COMPUTER FAIL LED is ON, the integrity of the downloaded data cannot be assured. If the yellow EXTERNAL FAULT LED is ON, this will not interfere with the download process. 4. On the MK V/VII EGPWS front panel (see Figure 2), verify: IN PROG LED is extinguished. CARD CHNG LED is extinguished. XFER COMP LED is extinguished. XFER FAIL LED is extinguished. On the EGPWS SmartCable (see Figure 1), verify: POWER ON LED is illuminated ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV D SHEET 4

5 If power was applied to the EGPWS at the time the SmartCable was connected, all LEDs may illuminate until the data transfer begins. 5. For card PN ONLY, verify that the PCMCIA Card has its Write Protect selector in the OFF position (see Figure 3). The PCMCIA Card Write Protect selector is fragile and should be moved only with the minimum amount of force. 6. Insert the Flight History Download card into the PCMCIA card slot. For the MK V or MK VII, ensure the L-shaped notch on the bottom of the PCMCIA card is in the down position and the U-shaped notch on the top of the PCMCIA card is the up position (See Figure 2). Push the card in carefully until the PUSH TO EJECT button on the front Panel is fully extended. This will be when the card is fully inserted, and the face of the PUSH TO EJECT button is nearly level with the rear of the inserted PCMCIA card. For the MK VI or MK VIII or MK XXII, the label on the card and on the Smart Cable should both be oriented in the same direction. The PCMCIA card will only insert about half the card length. CAUTION: Excessive force will damage the internal connector. 7. While loading is in progress, the amber IN PROG LED illuminates and the green COMPUTER OK LED turns OFF. 8. When loading is complete, the amber IN PROG LED will turn OFF and the green XFER COMP LED will turn ON. This operation should require no more than 10 minutes. If the red XFER FAIL LED turns ON instead of the green XFER COMP LED, verify proper position of the Write Protect switch (PN only, see Figure 3). If this checks OK, it may be necessary to obtain a different Flight History Download PCMCIA card from Honeywell for the data download. 9. Remove the PCMCIA Card. For the MK V or MK VII, depress the PUSH TO EJECT button on the EGPWS front panel. For the MK VI or MK VIII or MK XXII, carefully grasp the card and pull it out of the SmartCable. The EGPWS should automatically return to its normal operating mode within 1 minute of removal of the card. 10. Verify that the green COMPUTER OK LED illuminates (allow up to 3 minutes for this step). 11. Procedure is complete. Close the EGPWS front panel door or disconnect the SmartCable as appropriate. Flight History Download Cards can only be used once. After inserting them into an EGPWS, do not insert them into another EGPWS or the data stored may become unreadable. 3. DECODING OF FLIGHT HISTORY DATA For decoding of Flight History data, complete the request form on Sheet 6) and fax/ it to: Honeywell Technical Operations Phone (Toll Free) or (Direct), select Option 5 then 3 Fax: aerotechsupport@honeywell.com Technical operations will make arrangement to receive the card or accept the data contents via . ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV D SHEET 5

6 Honeywell PCMCIA CARD TRANSCRIPTION OF FLIGHT HISTORY REQUEST FORM Company Name: Company Address: Contact Person: Phone Number: Fax Number: Aircraft Type: Aircraft Tail Number: Aircraft Serial Number: Honeywell Contact Person: EGPWS Part Number: (16 Digit Part Number) EGPWS Mod Status: EGPWS Serial Number: Terrain Database Number: (If known) ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV D SHEET 6

7 MK VI / MK VII / MK XXII Smart Cable FIGURE 1 ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV D SHEET 7

8 WHEN THE PCMCIA CARD IS CORRECTLY INSERTED INTO THE EGPWS, THIS L-SHAPED NOTCH IS ON THE BOTTOM PINS WRITE PROTECT "ON" POSITION WRITE PROTECT "OFF" POSITION MK V / MK VII EGPWS FRONT PANEL FIGURE 2 PCMCIA CARD FIGURE 3 ASF-2121/R2 CAGE CODE: SCALE: NONE SIZE: A DWG NO REV: D SHEET 8