BOMBARDIER
AIRCRAFT RECOVERY MANUAL
TRANSMITTAL LETTER
REVISION 3
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PSM 1−84−9 MASTER
Effectivity: ** ALL
Transmittal Letter Page 1
Nov 05/2014
AIRCRAFT RECOVERY MANUAL
PSM 1−84−9
BOMBARDIER INC.
Bombardier Aerospace Regional Aircraft
Customer Support
123 Garratt Blvd., Downsview, Ontario
Canada M3K 1Y5
Copyright© 1998 by Bombardier Inc. All rights
reserved. No part of this work may be reproduced or
copied in any form or by any means without written
permission of Bombardier Inc.
Initial Issue: Apr 30/1999
Revision 3: Nov 05/2014
The information, technical data and designs disclosed in this document (the "information") are either the exclusive property of Bombardier
Inc. or are subject to proprietary rights of others. The information is not to be used for design or manufacture or disclosed t o others
without the express prior written consent of Bombardier Inc. The holder of this document, by its retention and use, agrees to h old the
information in confidence. These restrictions do not apply to persons having proprietary rights in the information, to the exte nt of those
rights.
April 10, 1992
AIRCRAFT RECOVERY MANUAL
IMPORTANT MESSAGE TO USERS OF THIS DOCUMENT
The generalized recovery techniques and methods described in this document are intended only for
general planning purposes and to illustrate the use of special recovery equipment and procedures
for the Dash−8, Series 400 aircraft.
The data presented in this document was calculated for hypothetical aircraft conditions or for
specific conditions which have occurred in the past. Because every situation that requires recovery
is unique, the recovery method appropriate to a particular situation will depend on the
circumstances and the available recovery equipment.
DISCLAIMER
BOMBARDIER INC. MAKES NO WARRANTY OR GUARANTEE WHATSOEVER IN
CONNECTION WITH THE INFORMATION FURNISHED IN THIS DOCUMENT OR THE USE OR
IMPLEMENTATION OF SUCH INFORMATION, AND THE USER OF THIS DOCUMENT HEREBY
WAIVES, RELEASES AND RENOUNCES ALL WARRANTIES, OBLIGATIONS AND
LIABILITIES OF BOMBARDIER INC., AND RIGHT, CLAIMS AND REMEDIES OF THE USER
AGAINST BOMBARDIER INC., EXPRESS OR IMPLIED, ARISING BY LAW OR OTHERWISE,
WITH RESPECT TO ANY DEFECT IN ANY INFORMATION FURNISHED HEREIN, INCLUDING
BUT NOT LIMITED TO (A) ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS,
(B) ANY IMPLIED WARRANTY ARISING FROM COURSE OF PERFORMANCE, COURSE OF
DEALING OR USEAGE OF TRADE, (C) ANY OBLIGATION, LIABILITY, RIGHT, CLAIM OR
REMEDY IN TORT, WHETHER OR NOT ARISING FROM BOMBARDIER INC., NEGLIGENCE
ACTUAL OR IMPUTED, AND (D) ANY OBLIGATION, LIABILITY, RIGHT, CLAIM OR REMEDY
FOR LOSS OF USE, REVENUE OR PROFIT, OR FOR ANY OTHER DIRECT, INCIDENTAL OR
CONSEQUENTIAL DAMAGES.
Series: 400
Page 1
Apr 30/1999
AIRCRAFT RECOVERY MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK
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Oct 4/2013
AIRCRAFT RECOVERY MANUAL
Initial Issue
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AIRCRAFT RECOVERY MANUAL
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See Effective TR
See Effective TR
de Havilland Inc. Temporary Revision
PSM NO. 1---8---9 AIRCRAFT DASH 8 SERIES 100
PUBLICATION AIRCRAFT RECOVERY MANUAL TEMPORARY REVISION NO. 1
Insert facing 4---10---00, Page 1.
TOWING AIRCRAFT UTILIZING MAIN LANDING GEAR
REASON FOR ISSUE:
Following review of the existing procedures and equipment used in towing the Dash---8 aircraft in recovery
situations, it became apparent that further engineering investigation was required. The intent of this Temporary
revision is to remove from the Aircraft Recovery Manual all references to adapters and procedures utilizing the
main landing gear.
ACTION:
Pending further engineering investigation disregard the following:
1. Figure 1, 4---10---00, page 2.
2. Paragraph 3 on 4---20---00, page 1.
3. Figure 6 on 4---20---00, page 11.
4. Figure 7 on 4---20---00, page 12.
5. Paragraph 5, Line A on 4---30---00, page 1.
RECORDING INSTRUCTIONS:
This Temporary Revision will be rescinded following additional engineering investigation. At that time, new
towing procedures utilizing the main landing gear will be provided.
Record this Temporary Revision in the appropriate columns of the Temporary Revision Index at the front of this
manual. This Temporary Revision will be incorporated in a future revision to the Aircraft Recovery Manual.
Temporary Revision No. 1
Page 1 of 1
FEB 6/97
de Havilland Inc. Temporary Revision
PSM NO. 1---8---9 AIRCRAFT DASH 8 SERIES 100
PUBLICATION AIRCRAFT RECOVERY MANUAL TEMPORARY REVISION NO. 2
Insert with page 2 facing 04---20---00, Page 12.
MULTI-- VEHICLE TOWING ARRANGEMENT
REASON FOR ISSUE:
To update Multi---Vehicle Towing Arrangement illustration, Figure 7.
ACTION:
Replace the illustration in Figure 7 on page 04---20---00, page 12, with the following illustration on page 2 of TR 2.
RECORDING INSTRUCTIONS:
Record this Temporary Revision in the appropriate columns of the Temporary Revision Index at the front of this
manual. This Temporary Revision will be incorporated in a future revision to the Aircraft Recovery Manual.
Temporary Revision No. 2
Page 1 of 2
MAY 26/05
PSM 1---8---9 Temporary Revision No. 2 continued.
TRAILER GUIDE
AND TOW BRAKING
IF LOW BED TRAILER IS USED
FOR SUPPORTING NOSE OF
AIRCRAFT, SUPPORT SHOULD
SWIVEL TO ALLOW FOR
STEERING AND STRAPS TO
M.L.G. TO PREVENT ROCKING
ACTION
TOWING STRAP
P/N GSB0910007
TOWING STRAP
P/N GSB0910007--1
DIRECTION
OF TOW
TOWING VEHICLES
dar0420000_001.dg, kms, 02/03/05
IN TANDEM
MULTI-- VEHICLE TOWING ARRANGEMENT
FIGURE 6
Temporary Revision No. 2
Page 2 of 2
MAY 26/05
