Exhibit 10.1
FOIA CONFIDENTIAL
TREATMENT REQUESTED
SUPPLEMENT NO.
PA-0436-5
TO
MASTER PURCHASE AGREEMENT NO.
PA-0436
BETWEEN
BOMBARDIER
INC.
AND
HORIZON AIR INDUSTRIES,
INC.
This Supplement is part of the Master Purchase
Agreement No. PA-436 entered into between BOMBARDIER INC., a
Canadian corporation represented by Bombardier Aerospace, Regional
Aircraft having offices at 123 Garratt Boulevard, Downsview,
Ontario, Canada (“Bombardier”) and Horizon Air
Industries, Inc. (“Buyer”) dated the 21st day of
December, 1998 (the “Agreement”) and evidences our
further agreement with respect to the matters set forth
below.
The provisions of the Agreement shall apply to
the Bombardier products purchased and sold in accordance with this
Supplement PA 0436-5. All capitalized terms herein, unless defined
herein, shall have the same respective meanings as in the
Agreement. This Supplement PA 0436-5 is subject to the provisions
of the Agreement, all of which are incorporated herein, provided
that in the event of any inconsistency between the provision of the
Agreement and the provisions of this Supplement PA 0436-5, the
latter shall take precedence.
Article 1 below supplements Article 2 of the
Agreement.
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ARTICLE 1
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SUBJECT
MATTER OF SALE
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1.1
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Subject to the
provisions of the Agreement and this Supplement PA 0436-5,
Bombardier will sell and Buyer will purchase twelve
(12) additional Bombardier DHC-8Q Series 400 model DHC-8-402
aircraft manufactured pursuant to Detail Specification number
DS8-400 Rev. 1 Amend NC, Detail Specification for the DHC-8-402
dated April 2002, listed in Schedule 1 attached hereto, as same may
be modified from time to time in accordance with the Agreement and
this Supplement PA 0436-5 (the “Specification”) as
supplemented to reflect the incorporation of the Buyer selected
optional features (“Buyer Selected Optional Features”)
set forth in Schedule 2 hereto (individually or collectively the
“Aircraft”).
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Supplement No. PA-0436-5
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-1-
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Initials
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Buyer
Bombardier
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Article 2 below supplements Article 4 of the
Agreement.
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2.1
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(a
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The base price
for each of the Aircraft (excluding the Buyer Selected Optional
Features) for delivery in accordance with Article 4 hereof Ex Works
(Incoterms 1990) Bombardier’s facilities in Downsview,
Ontario is [***]* expressed in [***] US Dollars; and
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(b
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The base price of the Buyer Selected Optional
Features (Schedule 2) for the Aircraft is [***] expressed in
November 1, 2006 US Dollars.
The Aircraft base price shall be the
base price for the Aircraft as stated in paragraph (a), plus the
base price of the Buyer Selected Optional Features as stated in
paragraph (b) (the “Base Price”). The price of the
Aircraft shall be adjusted to the Delivery Date to reflect economic
fluctuations during the period from November 1, 2006 to the
Delivery Date of each Aircraft (“Aircraft Purchase
Price”). Such adjustments shall be based on the economic
adjustment formula attached hereto as Schedule 3 (“Economic
Adjustment Formula”) but when adjusted, the Aircraft Purchase
Price shall in no case be lower than the Aircraft Purchase Price,
as stipulated in Article 2.1 herein, and starting from the [***]
base year, escalated [***].
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Article 3.0 below supplements Article 5.0 of the
Agreement.
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3.1
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Bombardier has
previously received a deposit for certain of the Aircraft, as set
forth in Article 3.2.2 to this Supplement.
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3.2.1
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Buyer shall
make payment or cause payment to be made for each of the Aircraft
as follows:
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(a)
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[***] of the
net Aircraft Purchase Price upon execution of this Supplement PA
0436-5;
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(b)
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[***] of the
net Aircraft Purchase Price fifteen (15) months prior to its
Scheduled Delivery Date;
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(c)
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[***] of the
net Aircraft Purchase Price twelve (12) months prior to its
Scheduled Delivery Date;
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*
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Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
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Supplement No. PA-0436-5
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-2-
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Initials
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Buyer
Bombardier
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(d)
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[***]
* of the net Aircraft Purchase Price nine
(9) months prior to its Scheduled Delivery
Date;
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(e)
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[***] of the
net Aircraft Purchase Price six (6) months prior to its
Scheduled Delivery Date; and
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(f)
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the balance of
the Aircraft Purchase Price shall be received on or before the
Delivery Date of such Aircraft to Buyer.
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All payments referred to in
paragraphs (c) through (f) above are to be made on the
first day of the applicable month.
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3.2.2
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The sum of
[***] United States Dollars paid by Buyer pursuant to Supplement
No. PA 0436-1, as amended, and currently held by Bombardier against
the current [***] in Supplement No. MPA0436-1 and [***] in
Supplement No. MPA0436-3 thereunder, (the “Transfer
Deposit”), shall be transferred and retained by Bombardier
against the Aircraft purchased pursuant to this Supplement No. MPA
0436-5. The Transfer Deposit shall be applied against Buyer’s
obligations as they become due under this Agreement.
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3.3
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For the sole
purpose of the calculations set forth in Article 3.2.1
(a) through (f) above, the Aircraft Purchase Price shall
be the Aircraft Purchase Price [***].
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3.4
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Buyer shall
make all payments due under this Agreement in electronic funds
transfer by deposit on or before the due date to Bombardier’s
account in the following manner:
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(a)
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Transfer
to:
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[***]
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Account Name:
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[***]
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Account #:
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[***]
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Bank Name:
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[***]
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ABA#:
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[***]
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Please reference:
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Invoice # and/or Aircraft Serial #
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Article 4.0 below supplements Article 6.0 of the
Agreement.
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ARTICLE 4.0
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DELIVERY
PROGRAM
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4.1
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The Aircraft
shall be offered for inspection and acceptance to Buyer at
Bombardier’s facility in Downsview, Ontario during the months
set forth below: (the “Scheduled Delivery
Dates”).
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*
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Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
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Supplement No. PA-0436-5
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-3-
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Initials
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Buyer
Bombardier
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DELIVERY
SCHEDULE
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First
Aircraft
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December
2006
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Second
Aircraft
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December
2006
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Third
Aircraft
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January
2007
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Fourth
Aircraft
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February
2007
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Fifth
Aircraft
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February
2007
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Sixth
Aircraft
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March
2007
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Seventh
Aircraft
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April
2007
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Eighth
Aircraft
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April
2007
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Ninth
Aircraft
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May
2007
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Tenth
Aircraft
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June
2007
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Eleventh
Aircraft
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June
2007
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Twelfth
Aircraft
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July
2007
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Article 5.0 below supplements Article 7.0 of the
Agreement.
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ARTICLE 5.0
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BUYER
INFORMATION
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5.1
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Pursuant to
Article 7.1 of the Agreement, Buyer will provide the information
set forth in Article 7.1 of the Agreement as soon as practicable
following execution of this Supplement PA 0436-5.
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ARTICLE 6.0
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NON-EXCUSABLE DELAY
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Article 6.1 below supplements Article 14.1 of
the Agreement.
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6.1
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If delivery of
the Aircraft is delayed by causes not excused under Article 13.1 of
the Agreement (a “Non-Excusable Delay”), Bombardier
shall pay Buyer [***] for any such delayed Aircraft.
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Article 6.2 below supplements Article 14.3 of
the Agreement.
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6.2
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The period of
days referred to in Article 14.3 of the Agreement is sixty
(60) days.
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*
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Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
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Supplement No. PA-0436-5
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-4-
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Initials
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Buyer
Bombardier
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Article 8.0 below supplements Annex A, Article 4
of the Agreement.
ARTICLE 8.0 - TECHNICAL DATA
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8.1
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Technical
Data Provided
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With each additional Aircraft
purchased hereunder, Bombardier will provide, at no additional
charge, one (1) copy of the Airplane Flight Manual, Quick
Reference Handbook, Airplane Operating Manual (“AOM”)
and Weight and Balance Manual. Such technical manuals/documents
will be prepared generally in accordance with revision 34 of ATA
Specification 100 and 2100.
The Technical Data and the
additional manuals provided with each Aircraft shall be in the
English language and shall provide information on items
manufactured according to Bombardier’s detailed design and in
those units of measure used in the Specification or as may
otherwise be required to reflect Aircraft instrumentation, as may
be mutually agreed.
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8.2
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List Of
Technical Data
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ITEM
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DOC
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CONF
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MEDIUM
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QTY
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REV
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DEL
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ATA
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REMARKS
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1
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Airplane Flight Manual
PSM 1-84-1A
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G
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1
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[***] *
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N
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ATD
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N
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2
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Quick Reference Handbook
PSM 1-84-1B
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G
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1
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[***]
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N
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ATD
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N
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3
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Weight and Balance Manual
PSM 1-84-8
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G
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1
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[***]
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Y
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ATD
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Y
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4
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Airplane Operating Manual (AOM)
PSM 1-84-1
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C
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1
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[***]
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N
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ATD
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N
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5
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*Aircraft Illustrated Parts Catalog
PSM 1-84-4
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G
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1
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[***]
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Y
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PTD
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Y
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6
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*Aircraft Maintenance Manual
PSM 1-84-2
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G
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1
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[***]
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Y
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PTD
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Y
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7
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*Wiring Diagrams Manual
PSM 1-84-2W
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G
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1
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[***]
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Y
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PTD
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Y
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Note: for items
5, 6, and 7, Bombardier may provide in electronic format, if
available at the time of delivery.
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Legend:
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CONF
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G = Generic
manual (contains information for all aircraft
configurations).
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C = Contains
information to for the operator fleet configuration.
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MED
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1 = Paper,
printed 2-sides.
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2 = Dynaweb on
DVD.
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3 = CD
ROM.
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4 = Laminated
Card.
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Optional ATA
specification 2100 (where applicable).
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*
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Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
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Supplement No. PA-0436-5
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-5-
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Initials
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Buyer
Bombardier
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QTY
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( number
) = Quantity per contract.
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( number
) PER = Quantity per delivered aircraft.
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A/R = As
Required.
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REV
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Y = Quarterly
Revision service (if purchased).
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N = Revisions
as required (if purchased).
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DEL
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ATD = Document
delivered at time of first aircraft delivery or subsequent aircraft
delivery (when ( number ) PER).
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PTD = Document
delivered 90 days prior to first aircraft delivery.
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ATA
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Y = Generally
in compliance with ATA 100 Revision 34.
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N = Bombardier
Standard.
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Except for the Airplane Flight
Manual, Quick Reference Handbook, Flight Crew Operating Manual, and
Weight and Balance Manual, which will be provided with each
Aircraft at time of delivery, all Technical Data provided hereunder
shall be shipped to Buyer Free Carrier (Incoterms)
Bombardier’s designated facilities.
Bombardier will provide Buyer with a
revision service, [***] * following the
Delivery Date of Buyer’s first Aircraft under this Supplement
PA 0436-5. This revision service shall apply to the Technical Data
for the Aircraft only. Subsequent to this [***] period, Buyer shall
be responsible for any revision services provided by Bombardier, at
Bombardier’s then current list prices.
Revisions to the Technical Data to
reflect the Aircraft configuration at delivery shall be provided to
Buyer within six (6) months following the Delivery Date of
each respective Aircraft.
Provided the revision service is
being supplied under the terms of this Agreement and applicable
Supplement or by subsequent purchase order, Bombardier shall
incorporate all applicable Bombardier originated Service Bulletins
into the appropriate Technical Data documents (in a regular
revision cycle), following formal notification by Buyer that such
Service Bulletins have been or shall be incorporated on
Buyer’s Aircraft. The Technical Data shall then contain both
the original and revised Aircraft configuration until Buyer advises
Bombardier in writing that one configuration is no longer
required.
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*
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Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
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Supplement No. PA-0436-5
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-6-
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Initials
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Buyer
Bombardier
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Bombardier will, at no additional
charge, arrange to have one (1) set of the following manuals
shipped directly to Buyer from the applicable vendor:
(a) Engine Maintenance
Manual;
(b) Engine Illustrated Parts
Catalogue; and
(c) Propeller Maintenance
Manual.
In addition, Bombardier will ensure
that vendors ship directly to Buyer, all applicable vendor
Component Maintenance Manual information not contained in the
Bombardier issued Component Maintenance Manual.
The supply of revisions and
amendments to vendor manuals will be the subject of separate
agreements directly between Buyer and Bombardier’s
vendors.
Article 9.0 below supplements Annex B, Article
1.0 of the Agreement.
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9.1
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The period of
months referred to in Annex B, Article 1.2.1 (a) of the
Agreement is forty-eight (48) months.
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9.2
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The period of
months referred to in Annex B, Article 1.2.1 (b) of the
Agreement is forty-eight (48) months.
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9.3
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The period of
months referred to in Annex B, Article 1.2.1 (c) of the
Agreement is forty-eight (48) months.
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9.4
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The period of
months referred to in Annex B, Article 1.2.1 (d) of the
Agreement is forty-eight (48) months.
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Supplement No. PA-0436-5
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-7-
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Initials
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Buyer
Bombardier
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Article 10.0 below supplements Annex B, Article
3.7 of the Agreement.
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ARTICLE 10.0
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COVERED COMPONENTS
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10.1 WING
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(a)
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Upper and lower
wing skins and stringers between front to rear spars;
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(b)
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Wing spar caps,
webs and uprights;
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(c)
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Main box (front
spar to rear spar) wing ribs;
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(d)
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Main box splice
plates, fittings;
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(e)
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Wing to nacelle
structural attachments;
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(f)
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Wing to
fuselage structural attachments;
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(g)
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Support
structure in the wing to spoilers, spoiler actuators and
ailerons;
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(h)
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Main gear
support structure; and
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(i)
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Engine support
fittings.
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10.2 FUSELAGE
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(a)
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External
surface skins and doublers, stringers, circumferential frames
between forward pressure bulkhead and aft pressure dome, excluding
all systems, insulation, lining and decorative clips and
brackets;
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(b)
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Window and
windshield structure but excluding the windows and
windshields;
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(c)
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Primary
structure frames around body openings for passenger doors,
cargo/baggage doors and emergency exits;
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(d)
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Nose gear
support structure;
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(e)
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Floor beams and
supporting structure in the flight compartment and cabin including
the lavatory, excluding seat tracks in both areas;
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(f)
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Forward
pressure bulkhead and aft pressure dome; and
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(g)
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Floor beams and
supporting structure in the baggage compartment providing same is
not damaged through abusive handling of baggage or
cargo.
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10.3 VERTICAL TAIL (including
fuselage aft of aft pressure dome)
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(a)
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Fuselage
external surface skins, stringers and frames between aft pressure
dome and rear fin spar frame;
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(b)
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Fin skins and
stiffeners between front and rear spars;
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(c)
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Fin front,
centre and rear spar caps, webs and uprights;
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(d)
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Main box (front
spar to rear spar) fin ribs;
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(e)
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Fin hinge and
actuator support structure for rudder and elevator;
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(f)
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Fore rudder
structure and hinge and actuator brackets; and
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(g)
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Aft rudder
forward cell structure and hinge and radius rod
brackets.
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Supplement No. PA-0436-5
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-8-
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Initials
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Buyer
Bombardier
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10.4 HORIZONTAL TAIL
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(a)
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Tailplane skins
and stringers;
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(b)
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Tailplane spar
caps, webs and uprights;
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(c)
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Tailplane main
box (front spar to rear spar) ribs;
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(d)
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Tailplane hinge
support structure for elevator;
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(e)
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Elevator
forward cell structure and hinge and actuator brackets;
and
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(f)
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Horizontal tail
structure attachments.
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In witness whereof this Supplement PA 0436-5 is
signed on the date written below:
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For and on
behalf of
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For and on
behalf of
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HORIZON AIR
INDUSTRIES, INC.
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BOMBARDIER
INC.
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Bombardier Aerospace
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Rudi Schmidt
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David MacNeil
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Vice President and Treasurer
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Senior Account Executive, Contracts
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Regional
Aircraft
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Date:___________________
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Date__________________
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Ross Gray
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Director, Contracts
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Regional
Aircraft
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Date:_______________
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Supplement No. PA-0436-5
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-9-
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Initials
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Buyer
Bombardier
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SCHEDULE 1 TO SUPPLEMENT NO.
PA-0436-5
DETAIL
SPECIFICATION
DS8-400 Rev. 1. Amend
NC,
for the DHC-8-402
April 16,
2002
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Supplement No. PA-0436-5
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-10-
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Initials
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Buyer
Bombardier
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SCHEDULE 2 TO SUPPLEMENT NO.
PA-0436-5
BUYER SELECTED OPTIONAL
FEATURES
PRICES AND
DESCRIPTIONS
CS: HRZ842207504
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CR Ref.#
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Option Descriptions
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Price in
Nov-06 U.S.
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803SO90021
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Increased
Tailwind Operation to 20 Knots (AFM Supplement #3)
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|
[***] *
|
|
|
|
|
|
803SO90027
|
|
High Gross
Weight (64,500 lb / 29,257 kg MTOW)
|
|
[***]
|
|
|
|
|
|
803SO90030
|
|
Reduced
Propeller RPM Landing (AFM Supplement #39)
|
|
[***]
|
|
|
|
|
|
803SO90036
|
|
2 X
Max.Take-Off Power (AFM Supplement #46)
|
|
[***]
|
|
|
|
|
|
803SO90037
|
|
AFM Supplement
- Cat 1 Coupled Flap 35 Approach (#75)
|
|
[***]
|
|
|
|
|
|
803SO90038
|
|
AFM Supplement
Take-off with bleed on - All flap settings (#61)
|
|
[***]
|
|
|
|
|
|
811CH00628
|
|
Exterior Paint
Scheme - S400 - Horizon Air
|
|
[***]
|
|
|
|
|
|
811CH00657
|
|
Max Load Labels
for Galleys, Baggage compartment and wardrobe inset -
Horizon
|
|
[***]
|
|
|
|
|
|
811CH00717
|
|
Exterior Paint
Scheme - Aluminized Paint Applied To Belly Of Aircraft
|
|
[***]
|
|
|
|
|
|
821SO90061
|
|
Ground Air
Conditioning Cart Connection
|
|
[***]
|
|
|
|
|
|
822SO90387
|
|
AFCS - Heading
Knobs Coupled Left & Right
|
|
[***]
|
|
|
|
|
|
823SO90100
|
|
Datalink -
UNILINK (UASC UL-701) with integral VHF comm and Half-size Printer
(Honeywell)
|
|
[***]
|
|
|
|
|
|
824CH00091
|
|
Batteries -
Three 40 Amp Configuration - Forward Fuse
|
|
[***]
|
|
|
|
|
|
825CH01366
|
|
Detail
Specification G2 Galley - Left Hand Aft Facing Galley -
S400
|
|
[***]
|
|
|
|
|
|
825CH01461
|
|
PAX Seats -
Deletion Of Ashtrays (Includes ‘No Smoking’
On)
|
|
[***]
|
|
|
|
|
|
825CH01596
|
|
G1 Galley -
Stowage Compartments and Two Driessen Hot Jugs - Horizon
|
|
[***]
|
|
|
|
|
|
825CH01624
|
|
Cabin - Soft
Materials Spec - Horizon
|
|
[***]
|
|
|
|
|
|
825CH01639
|
|
FWD Baggage
Compartment - Removable Shelf in Upper Aft Portion
|
|
[***]
|
|
|
|
|
|
825CH01644
|
|
PAX Seats -
Improved Seat Pan Cushions - Horizon
|
|
[***]
|
|
*
|
Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
|
|
|
|
|
|
|
|
Supplement No. PA-0436-5
|
|
-11-
|
|
|
|
|
|
|
|
Initials
|
|
|
|
|
|
Buyer
Bombardier
|
|
|
|
|
|
|
|
|
|
|
|
825CH01829
|
|
Cockpit -
Removal Of The Cockpit Door From Production Definition
|
|
[***] *
|
|
|
|
|
|
825CH02299
|
|
LOPA - Horizon
Air (74 PAX, 3 F/A, G1 modified, G2,91 CU FT and 411 CU FT baggage
compartments)
|
|
[***]
|
|
|
|
|
|
825CH02336
|
|
AFT Staggered
bulkhead with 2 F/A seats and without AFT stairs- Q400
|
|
[***]
|
|
|
|
|
|
825SO90115-03
|
|
Flight
Attendant Seats - Leather Dress Covers
|
|
[***]
|
|
|
|
|
|
825SO90150-74
|
|
Passenger Seats
- Leather Dress Covers
|
|
[***]
|
|
|
|
|
|
825SO90157
|
|
Flight
Attendant - 3rd Seat Installation
|
|
[***]
|
|
|
|
|
|
825SO90290
|
|
Passenger Seats
- In-Arm Meal Trays
|
|
[***]
|
|
|
|
|
|
825SO90302-74
|
|
Passenger Seats
- Additional Economy Passenger Seating (B/E Aero Model
925)
|
|
[***]
|
|
|
|
|
|
825SO90389
|
|
Galley -
Wardrobe Insert (Provisions for 1 Half Trolley and 1
S.U.)
|
|
[***]
|
|
|
|
|
|
831SO70185
|
|
FAR 121.344
Requirement - Q400 - 88 Parameter Installation
|
|
[***]
|
|
|
|
|
|
831SO90180
|
|
Enhanced GPWS
(Honeywell)
|
|
[***]
|
|
|
|
|
|
832CH00028
|
|
Cockpit - Nose
Gear Lock Indicator
|
|
[***]
|
|
|
|
|
|
833SO90188
|
|
Tail Logo
Lights
|
|
[***]
|
|
|
|
|
|
834CH00441
|
|
Single Cue
Command on EADI
|
|
[***]
|
|
|
|
|
|
834CH00559
|
|
VHF Comm -
Provisions for 3rd VHF Radio (With Level “A” Certified
Software)
|
|
[***]
|
|
|
|
|
|
834SO70216
|
|
Radio Altimeter
– Dual Collins ALT-4000
|
|
[***]
|
|
|
|
|
|
834SO90209
|
|
HGS - CAT IIIa
Partial Provisions For RCFDI STC
|
|
[***]
|
|
|
|
|
|
834SO90926
|
|
FMS - Dual with
GPS and TCAS II (Universal UNS-1E, SCN 802.2))
|
|
[***]
|
|
|
|
|
|
835CH00937
|
|
Emergency
Equipment - Increased Capacity Crew Fixed O2 Cylinder With Onboard
Charging
|
|
[***]
|
|
|
|
|
|
839SO90316
|
|
Alternate
Symbology Indication, Imperial (PFD & MFD Displays)
|
|
[***]
|
|
|
|
|
|
849SO90266
|
|
APU (Hamilton
Sundstrand APS-1000)
|
|
[***]
|
|
|
|
|
|
853CH00128
|
|
Cockpit -
Center Console Extension
|
|
[***]
|
|
|
|
Total Buyer Selected Optional
Features
|
|
[***]
|
|
|
|
|
|
|
|
Discounts
and Allowances
|
|
[***]
|
|
|
|
|
|
[***]
|
|
[***]
|
|
[***]
|
|
|
|
|
|
[***]
|
|
[***]
|
|
[***]
|
|
|
|
Total including Discounts and
Allowances
|
|
[***]
|
|
*
|
Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
|
ANAC - At No Additional Cost
STD - Standard
(Buyer may amend the Buyer Selected Optional
Features List via contract change order, subject to Bombardier
required lead times.)
|
|
|
|
|
|
|
Supplement No. PA-0436-5
|
|
-12-
|
|
|
|
|
|
|
|
Initials
|
|
|
|
|
|
Buyer
Bombardier
|
SCHEDULE 3 TO SUPPLEMENT NO.
PA-0436-5
AIRCRAFT
ECONOMIC ADJUSTMENT
FORMULA
|
1.
|
Economic
adjustment will be calculated using the following Economic
Adjustment Formula:
|
Pp = [***]*
Where:
|
|
Pp
|
= Aircraft
Purchase Price;
|
|
|
|
|
|
|
|
|
|
|
|
P O
|
|
=
|
|
Base Price;
|
|
|
|
|
|
LD
|
|
=
|
|
the Canadian labour index based upon arithmetic
the average of the indices for the fourth, fifth and sixth months
prior to the month of delivery of the relevant Aircraft;
|
|
|
|
|
|
LO
|
|
=
|
|
Being the arithmetic average of the Canadian
labour index for the months of May, June and July 2006;
|
|
|
|
|
|
ED
|
|
=
|
|
the U.S. labour index based upon the average of
the indices for the fourth, fifth and sixth months prior to the
month of delivery of the relevant Aircraft;
|
|
|
|
|
|
EO
|
|
=
|
|
Being the arithmetic average of the U.S. labor
index for the months of May, June and July 2006;
|
|
|
|
|
|
MD
|
|
=
|
|
the Material index based upon the average of
the arithmetic indices for the fourth, fifth and sixth months prior
to the month of delivery of the relevant Aircraft; and
|
|
|
|
|
|
MO
|
|
=
|
|
Being the arithmetic average of the Material
index which for the months of May, June and July 2006;
|
|
*
|
Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
|
|
|
|
|
|
|
|
Supplement No. PA-0436-5
|
|
-13-
|
|
|
|
|
|
|
|
Initials
|
|
|
|
|
|
Buyer
Bombardier
|
|
2.
|
For the purpose
of the Economic Adjustment Formula and the calculation of the
economic adjustment:
|
|
|
(a)
|
the Canadian
labour index shall be the North American Industrial Classification
System (N.A.I.C.S.) Code 3364 for Average Hourly Earnings
(including overtime) for Aerospace Products and Parts manufacturing
(Canada) published by Statistics Canada in Catalogue 72-002
“Employment Earnings and Hours”, Table 6;
|
|
|
(b)
|
the U.S. labour
index shall be the index published by the U.S. Department of Labor,
Bureau of Labor Statistics in the North American Industrial
Classification System (N.A.I.C.S.) Code 3364 for Average Hourly
Earnings of Production Workers for Manufacturing, Aerospace
products and parts (US).; (The U.S. labour index provided in the
Bureau of Labor Statistics (B.L.S.) Code 372 for Average Hourly
Earnings for Aircraft and Parts as published by the U.S. Department
of Labor, Bureau of Labor Statistics in “Employment and
Earnings” Table B-15, has been discontinued)
|
|
|
(c)
|
the material
index shall be the index provided in the Producer Price Index for
Code 10 Metals and Metals Products as published by the U.S.
Department of Labor, Bureau of Labor Statistics in “Producer
Prices and Price Indexes” Table 6;
|
|
|
(d)
|
the indices
used for the calculation of the Aircraft Purchase Price of each
Aircraft shall be the last indices received by Bombardier in the
month prior to the delivery of the relevant Aircraft;
and
|
|
|
(e)
|
in the event
that Bombardier shall be prevented from calculating the Aircraft
Purchase Price of each Aircraft due to any delay in the publication
of the required indices, Bombardier shall use the last
provisionally published indices, and in the event that provisional
indices are not available, Bombardier shall extrapolate from the
last three (3) months of published indices.
|
|
3.
|
In the
calculation of the Aircraft Purchase Price the following guidelines
in respect of decimal places shall apply:
|
|
|
(a)
|
All average
indices in the Economic Adjustment Formula shall be calculated to
the applicable one or two decimal places;
|
|
|
(b)
|
The Economic
Adjustment Formula shall be calculated to four decimal places;
and
|
|
|
(c)
|
The Aircraft
Purchase Price resulting from the Economic Adjustment Formula shall
be corrected to the nearest dollar.
|
|
4.
|
In the event
that any index referred to be discontinued or restated, or if the
methodology employed by the relevant authority in determining the
index is substantially revised, then a mutually agreed to index
will be substituted prior to delivery of the Aircraft.
|
|
|
|
|
|
|
|
Supplement No. PA-0436-5
|
|
-14-
|
|
|
|
|
|
|
|
Initials
|
|
|
|
|
|
Buyer
Bombardier
|
|
5.
|
Pursuant to
Article 4.2 of the Agreement, the Base Price of each Aircraft shall
be adjusted for economic fluctuations. Such adjustment shall be
based on the Economic Adjustment Formula (the
“Formula”) as defined in Article 4.2, and more
particularly set forth in this Schedule above.
|
|
|
|
|
|
|
|
Supplement No. PA-0436-5
|
|
-15-
|
|
|
|
|
|
|
|
Initials
|
|
|
|
|
|
Buyer
Bombardier
|
SCHEDULE 4 TO SUPPLEMENT NO.
PA-0436-5
CREDIT MEMORANDUM
|
1.0
|
Upon delivery
of and payment in full for each Aircraft, Bombardier will issue to
Buyer a credit memorandum in the amount of [***] *. Each credit memorandum shall be subject to
escalation to the date of delivery in accordance with the Economic
Adjustment Formula provided in Schedule 3 to this supplement [***]
and shall be used by Buyer to reduce the balance of the Aircraft
Purchase Price payable on delivery of each such
Aircraft.
|
|
2.0
|
Buyer
acknowledges that the amount of the credit memorandum referenced in
Article 1.0 above has been offered to Buyer [***].
|
|
3.0
|
In the event of
the termination of the Agreement, this Schedule shall become
automatically null and void.
|
|
4.0
|
The provisions
of this Schedule are personal to Buyer and shall not be assigned or
otherwise disposed of by Buyer without the prior written consent of
Bombardier.
|
|
5.0
|
This Schedule
constitutes an integral part of the Agreement and subject to the
terms and conditions contained therein.
|
|
|
|
|
|
|
|
HORIZON AIR
INDUSTRIES, INC.
|
|
|
|
BOMBARDIER
INC.
|
|
|
|
|
|
Bombardier Aerospace
|
|
|
|
|
|
|
|
|
|
|
|
Rudi Schmidt
|
|
|
|
David MacNeil
|
|
Vice President and Treasurer
|
|
|
|
Senior Account Executive, Contracts
|
|
|
|
|
|
Regional
Aircraft
|
|
Date: October ,
2005
|
|
|
|
Date: October ,
2005
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ross Gray
|
|
|
|
|
|
Director, Contracts, Americas
|
|
|
|
|
|
Regional
Aircraft
|
|
|
|
|
|
Date: October
, 2005
|
|
*
|
Indicates that
certain information contained herein has been omitted and filed
separately with the Securities and Exchange Commission.
Confidential treatment has been requested with respect to the
omitted portions.
|
|
|
|
|
|
|
|
Supplement No. PA-0436-5
|
|
-16-
|
|
|
|
|
|
|
|
Initials
|
|
|
|
|
|
Buyer
Bombardier
|
SCHEDULE 5 TO SUPPLEMENT NO.
PA-0436-5
PERFORMANCE
GUARANTEE
|
1.0
|
AIRCRAFT
CONFIGURATION
|
The guarantees contained in this
document are applicable to the DHC-8-402 aircraft to Detail
Specification No. DS8-400 Rev. 1, Amend. NC, dated April 16,
2002, equipped with 34-inch tires per ECR no. 4Q24060, with an
optional Maximum Take-off Weight of 64,500 pounds (29,257 kg) and
eq