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SUPPLEMENT TO MASTER PURCHASE AGREEMENT

Purchase and Sale Agreement

SUPPLEMENT TO MASTER PURCHASE AGREEMENT | Document Parties: ALASKA AIR GROUP INC | BOMBARDIER INC.  | HORIZON AIR INDUSTRIES, INC. You are currently viewing:
This Purchase and Sale Agreement involves

ALASKA AIR GROUP INC | BOMBARDIER INC. | HORIZON AIR INDUSTRIES, INC.

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Title: SUPPLEMENT TO MASTER PURCHASE AGREEMENT
Date: 11/9/2005
Industry: Airline     Sector: Transportation

SUPPLEMENT TO MASTER PURCHASE AGREEMENT, Parties: alaska air group inc , bombardier inc.  , horizon air industries  inc.
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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.

 

ARTICLE 1

SUBJECT MATTER OF SALE

 

1.1

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”).

 

 

 

 

 

 

Supplement No. PA-0436-5

  

-1-

  

 

 

  

 

  

Initials

 

  

 

  

Buyer              Bombardier             


Article 2 below supplements Article 4 of the Agreement.

 

ARTICLE 2.0

PRICE

 

 

 

 

 

 

 

2.1

  

(a

)

 

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

 

 

 

 

  

(b

)

 

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 [***].

 

Article 3.0 below supplements Article 5.0 of the Agreement.

 

ARTICLE 3.0

PAYMENT

 

3.1

Bombardier has previously received a deposit for certain of the Aircraft, as set forth in Article 3.2.2 to this Supplement.

 

3.2

Payment Terms:

 

3.2.1

Buyer shall make payment or cause payment to be made for each of the Aircraft as follows:

 

 

(a)

[***] of the net Aircraft Purchase Price upon execution of this Supplement PA 0436-5;

 

 

(b)

[***] of the net Aircraft Purchase Price fifteen (15) months prior to its Scheduled Delivery Date;

 

 

(c)

[***] of the net Aircraft Purchase Price twelve (12) months prior to its Scheduled Delivery Date;


*

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

  

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Initials

 

  

 

  

Buyer              Bombardier             


 

(d)

[***] * of the net Aircraft Purchase Price nine (9) months prior to its Scheduled Delivery Date;

 

 

(e)

[***] of the net Aircraft Purchase Price six (6) months prior to its Scheduled Delivery Date; and

 

 

(f)

the balance of the Aircraft Purchase Price shall be received on or before the Delivery Date of such Aircraft to Buyer.

 

All payments referred to in paragraphs (c) through (f) above are to be made on the first day of the applicable month.

 

3.2.2

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.

 

3.3

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 [***].

 

3.4

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:

 

 

 

 

 

 

(a)

  

Transfer to:

 

[***]

 

 

 

 

  

Account Name:

 

[***]

 

  

Account #:

 

[***]

 

  

Bank Name:

 

[***]

 

  

ABA#:

 

[***]

 

  

Please reference:

 

Invoice # and/or Aircraft Serial #

 

Article 4.0 below supplements Article 6.0 of the Agreement.

 

ARTICLE 4.0

DELIVERY PROGRAM

 

4.1

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”).


*

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

  

-3-

  

 

 

  

 

  

Initials

 

  

 

  

Buyer              Bombardier             


DELIVERY SCHEDULE

 

 

 

 

First Aircraft

  

December 2006

 

 

Second Aircraft

  

December 2006

 

 

Third Aircraft

  

January 2007

 

 

Fourth Aircraft

  

February 2007

 

 

Fifth Aircraft

  

February 2007

 

 

Sixth Aircraft

  

March 2007

 

 

Seventh Aircraft

  

April 2007

 

 

Eighth Aircraft

  

April 2007

 

 

Ninth Aircraft

  

May 2007

 

 

Tenth Aircraft

  

June 2007

 

 

Eleventh Aircraft

  

June 2007

 

 

Twelfth Aircraft

  

July 2007

 

Article 5.0 below supplements Article 7.0 of the Agreement.

 

ARTICLE 5.0

BUYER INFORMATION

 

5.1

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.

 

ARTICLE 6.0

NON-EXCUSABLE DELAY

 

Article 6.1 below supplements Article 14.1 of the Agreement.

 

6.1

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.

 

Article 6.2 below supplements Article 14.3 of the Agreement.

 

6.2

The period of days referred to in Article 14.3 of the Agreement is sixty (60) days.

 

*

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

  

-4-

  

 

 

  

 

  

Initials

 

  

 

  

Buyer              Bombardier             


Article 8.0 below supplements Annex A, Article 4 of the Agreement.

 

ARTICLE 8.0 - TECHNICAL DATA

 

8.1

Technical Data Provided

 

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.

 

8.2

List Of Technical Data

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

ITEM


 

  

DOC


 

  

CONF


 

  

MEDIUM


 

  

QTY


 

 

REV


 

  

DEL


 

  

ATA


 

  

REMARKS


 

1

  

Airplane Flight Manual

PSM 1-84-1A

  

G

  

1

  

[***] *

 

N

  

ATD

  

N

  

 

2

  

Quick Reference Handbook

PSM 1-84-1B

  

G

  

1

  

[***]

 

N

  

ATD

  

N

  

 

3

  

Weight and Balance Manual

PSM 1-84-8

  

G

  

1

  

[***]

 

Y

  

ATD

  

Y

  

 

4

  

Airplane Operating Manual (AOM)

PSM 1-84-1

  

C

  

1

  

[***]

 

N

  

ATD

  

N

  

 

5

  

*Aircraft Illustrated Parts Catalog

PSM 1-84-4

  

G

  

1

  

[***]

 

Y

  

PTD

  

Y

  

 

6

  

*Aircraft Maintenance Manual

PSM 1-84-2

  

G

  

1

  

[***]

 

Y

  

PTD

  

Y

  

 

7

  

*Wiring Diagrams Manual

PSM 1-84-2W

  

G

  

1

  

[***]

 

Y

  

PTD

  

Y

  

 

 

*

Note: for items 5, 6, and 7, Bombardier may provide in electronic format, if available at the time of delivery.

 

Legend:

 

 

 

 

CONF

  

G = Generic manual (contains information for all aircraft configurations).

 

  

C = Contains information to for the operator fleet configuration.

MED

  

1 = Paper, printed 2-sides.

 

  

2 = Dynaweb on DVD.

 

  

3 = CD ROM.

 

  

4 = Laminated Card.

 

  

Optional ATA specification 2100 (where applicable).


*

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

  

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Initials

 

  

 

  

Buyer              Bombardier             


 

 

 

QTY

 

( number ) = Quantity per contract.

 

 

( number ) PER = Quantity per delivered aircraft.

 

 

A/R = As Required.

 

 

REV

 

Y = Quarterly Revision service (if purchased).

 

 

N = Revisions as required (if purchased).

 

 

DEL

 

ATD = Document delivered at time of first aircraft delivery or subsequent aircraft delivery (when ( number ) PER).

 

 

PTD = Document delivered 90 days prior to first aircraft delivery.

 

 

ATA

 

Y = Generally in compliance with ATA 100 Revision 34.

 

 

N = Bombardier Standard.

 

8.3

Shipment

 

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.

 

8.4

Revision Service

 

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.


*

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

  

-6-

  

 

 

  

 

  

Initials

 

  

 

  

Buyer              Bombardier             


8.5

Vendor Manuals

 

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.

 

ARTICLE 9.0 

WARRANTY

 

9.1

The period of months referred to in Annex B, Article 1.2.1 (a) of the Agreement is forty-eight (48) months.

 

9.2

The period of months referred to in Annex B, Article 1.2.1 (b) of the Agreement is forty-eight (48) months.

 

9.3

The period of months referred to in Annex B, Article 1.2.1 (c) of the Agreement is forty-eight (48) months.

 

9.4

The period of months referred to in Annex B, Article 1.2.1 (d) of the Agreement is forty-eight (48) months.

 

 

 

 

 

 

Supplement No. PA-0436-5

  

-7-

  

 

 

  

 

  

Initials

 

  

 

  

Buyer              Bombardier             


Article 10.0 below supplements Annex B, Article 3.7 of the Agreement.

 

ARTICLE 10.0

 COVERED COMPONENTS

 

10.1 WING

 

 

(a)

Upper and lower wing skins and stringers between front to rear spars;

 

 

(b)

Wing spar caps, webs and uprights;

 

 

(c)

Main box (front spar to rear spar) wing ribs;

 

 

(d)

Main box splice plates, fittings;

 

 

(e)

Wing to nacelle structural attachments;

 

 

(f)

Wing to fuselage structural attachments;

 

 

(g)

Support structure in the wing to spoilers, spoiler actuators and ailerons;

 

 

(h)

Main gear support structure; and

 

 

(i)

Engine support fittings.

 

10.2 FUSELAGE

 

 

(a)

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;

 

 

(b)

Window and windshield structure but excluding the windows and windshields;

 

 

(c)

Primary structure frames around body openings for passenger doors, cargo/baggage doors and emergency exits;

 

 

(d)

Nose gear support structure;

 

 

(e)

Floor beams and supporting structure in the flight compartment and cabin including the lavatory, excluding seat tracks in both areas;

 

 

(f)

Forward pressure bulkhead and aft pressure dome; and

 

 

(g)

Floor beams and supporting structure in the baggage compartment providing same is not damaged through abusive handling of baggage or cargo.

 

10.3 VERTICAL TAIL (including fuselage aft of aft pressure dome)

 

 

(a)

Fuselage external surface skins, stringers and frames between aft pressure dome and rear fin spar frame;

 

 

(b)

Fin skins and stiffeners between front and rear spars;

 

 

(c)

Fin front, centre and rear spar caps, webs and uprights;

 

 

(d)

Main box (front spar to rear spar) fin ribs;

 

 

(e)

Fin hinge and actuator support structure for rudder and elevator;

 

 

(f)

Fore rudder structure and hinge and actuator brackets; and

 

 

(g)

Aft rudder forward cell structure and hinge and radius rod brackets.

 

 

 

 

 

 

Supplement No. PA-0436-5

  

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Initials

 

  

 

  

Buyer              Bombardier             


10.4 HORIZONTAL TAIL

 

 

(a)

Tailplane skins and stringers;

 

 

(b)

Tailplane spar caps, webs and uprights;

 

 

(c)

Tailplane main box (front spar to rear spar) ribs;

 

 

(d)

Tailplane hinge support structure for elevator;

 

 

(e)

Elevator forward cell structure and hinge and actuator brackets; and

 

 

(f)

Horizontal tail structure attachments.

 

In witness whereof this Supplement PA 0436-5 is signed on the date written below:

 

 

 

 

 

 

For and on behalf of

 

 

 

For and on behalf of

 

 

 

HORIZON AIR INDUSTRIES, INC.

 

 

 

BOMBARDIER INC.

 

 

 

 

Bombardier Aerospace

 

 

 

 

 

 

 

 

Rudi Schmidt

 

 

 

David MacNeil

Vice President and Treasurer

 

 

 

Senior Account Executive, Contracts

 

 

 

 

Regional Aircraft

Date:___________________

 

 

 

Date__________________

 

 

 

 

 

 

 

 

 

 

 

 

Ross Gray

 

 

 

 

Director, Contracts

 

 

 

 

Regional Aircraft

 

 

 

 

Date:_______________

 

 

 

 

 

 

Supplement No. PA-0436-5

  

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Initials

 

  

 

  

Buyer              Bombardier             


SCHEDULE 1 TO SUPPLEMENT NO. PA-0436-5

 

DETAIL SPECIFICATION

 

DS8-400 Rev. 1. Amend NC,

for the DHC-8-402

 

April 16, 2002

 

 

 

 

 

 

Supplement No. PA-0436-5

  

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Initials

 

  

 

  

Buyer              Bombardier             


SCHEDULE 2 TO SUPPLEMENT NO. PA-0436-5

 

BUYER SELECTED OPTIONAL FEATURES

PRICES AND DESCRIPTIONS

CS: HRZ842207504

 

 

 

 

 

 

CR Ref.#


 

  

Option Descriptions


 

  

Price in

Nov-06 U.S.


 

803SO90021

  

Increased Tailwind Operation to 20 Knots (AFM Supplement #3)

  

[***] *

 

 

 

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

  

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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


 
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