Exhibit 10.13(m)
AMENDMENT NUMBER 13 TO PURCHASE AGREEMENT GCT-025/98
This Amendment Number 13 to Purchase Agreement GCT-025/98, dated as of October
__, 2001 ("Amendment No. 13") relates to the Purchase Agreement GCT-025/98 (the
"Purchase Agreement") between EMBRAER - Empresa Brasileira de Aeronautica S.A.
("Embraer") and Solitair Corp. ("Buyer") dated June 17, 1998 as amended from
time to time (collectively referred to herein as "Agreement"). This Amendment
No. 13 is between Embraer and Buyer, collectively referred to herein as the
"Parties".
This Amendment No. 13 sets forth additional agreements between Embraer and Buyer
relative to the conversion of EMB-145 Aircraft into EMB-140 Aircraft (as defined
below), configuration changes for the EMB-140 Aircraft in order to comply with
the American Eagle ("AMR Eagle") configuration, and the Performance Guarantee
for the EMB-140 Aircraft, a change the name of Wexford Management LLC to Wexford
Capital LLC, and changes on the delivery schedule and Buyer's exercise of Option
Aircraft.
Except as otherwise provided for herein all terms of the Purchase Agreement
shall remain in full force and effect. All capitalized terms used in this
Amendment No. 13, which are not defined herein shall have the meaning given in
the Purchase Agreement. In the event of any conflict between this Amendment No.
13 and the Purchase Agreement the terms, conditions and provisions of this
Amendment No. 13 shall control.
WHEREAS, in connection with the Parties' agreements as described above, the
Parties have agreed to amend the Purchase Agreement as provided for below:
NOW, THEREFORE, for good and valuable consideration which is hereby acknowledged
Embraer and Buyer hereby agree as follows:
1. DEFINITIONS:
1.1 Article "1.b" shall be deleted and replaced with the following:
"b. Aircraft - shall mean the EMB-145 Aircraft and/or the EMB-140
Aircraft."
1.2 New Articles "1.b.1" and "1.b.2" shall be included as follows:
"b.1. EMB-145 Aircraft - shall mean the EMB-145 LR Firm Aircraft and
Option Aircraft or, where there is more than one of such Aircraft,
each of such Aircraft, manufactured by Embraer, for sale to Buyer
pursuant to this Agreement, according to the Technical Description
number TD-145/010, dated January 1998 (Appendix I), the Aircraft
Specific Configuration, Finishing and Registration Marks described
in Attachments 'A-1', 'A-2' and 'A-3', as applicable, and as may be
amended from time to time by Buyer at its expense as specified in
Article 11. The Aircraft is composed entirely of vendor parts and
parts manufactured by
Embraer and Embraer subcontractors, and the parts manufactured by
Embraer and Embraer subcontractors shall have Embraer part numbers.
b.2. EMB-140 Aircraft - shall mean the XXX-000, Xxxxx XXX-000 XX version
Firm Aircraft and New Option Aircraft, or, where there is more than
one of such Aircraft, each of such Aircraft, manufactured by
Embraer, for sale to Buyer pursuant to this Agreement, according to
Technical Description TD-140/002, dated April 2000, the Aircraft
Specific Configuration, Finishing and Registration Marks described
in Attachment 'A-4' as may be amended from time to time by Buyer at
its expense as specified in Article 11. The Aircraft is composed
entirely of vendor parts and parts manufactured by Embraer and
Embraer subcontractors, and the parts manufactured by Embraer and
Embraer subcontractors shall have Embraer part numbers."
2. SUBJECT: Article "2.a" shall be deleted and replaced with the following:
"a. Embraer shall sell and Buyer shall purchase and take delivery of
forty five (45) firm Aircraft ("Firm Aircraft"), and if Buyer so
elects, up to twenty-eight (28) option Aircraft ("Option Aircraft"),
upon the terms and conditions of this Agreement. Such Aircraft
quantity distribution shall be as follows:
a.1 Firm Aircraft: Thirty eight (38) EMB-145 Aircraft and seven
(7) EMB-140 Aircraft (also referred to as Aircraft #1 - #45);
a.2 Option Aircraft: eight (8) EMB-140 Aircraft and twenty (20)
EMB-145 Aircraft (also referred to as Aircraft #46 - #73)."
3. PRICE: Article "3.a.1" shall be deleted and replaced with the following:
"1. The per unit Aircraft Basic Prices for the Firm Aircraft shall be:
--------------------------------------------------------------------------------
Firm Aircraft
--------------------------------------------------------------------------------
"EMB-145 Aircraft # Aircraft Basic Price
--------------------------------------------------------------------------------
11 to 15 Such Aircraft have already been delivered for [*]
--------------------------------------------------------------------------------
16 and 17 Such Aircraft have already been delivered for [*]
--------------------------------------------------------------------------------
18 and 22 Such Aircraft have already been delivered for [*]
--------------------------------------------------------------------------------
23 to 27 Such Aircraft have already been delivered for [*]
--------------------------------------------------------------------------------
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28 and 29 Such Aircraft have already been delivered for a
Basic Price of US$16,796,182 (sixteen million,
seven hundred ninety six thousand, one hundred
eighty two United States dollars) in January 2000
economic conditions.
--------------------------------------------------------------------------------
30 and all subsequent US$16,794,145 (sixteen million, seven hundred
EMB-145 Aircraft ninety four thousand, one hundred forty five
United States dollars) in January 2000 economic
conditions."
--------------------------------------------------------------------------------
--------------------------------------------------------------------------------
EMB-140 Aircraft # Aircraft Basic Price
--------------------------------------------------------------------------------
All EMB-140 [*]
Aircraft
--------------------------------------------------------------------------------
4. DELIVERY SCHEDULE: The delivery schedule contained in Article "5.a" shall
be deleted and replaced with the following:
"
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A/C # AIRCRAFT DELIVERY MONTH A/C # AIRCRAFT DELIVERY MONTH
------------------------------------------------------------------------------------------------------------------
01 EMB-145 Apr-99* 24 EMB-145 Apr-01*
------------------------------------------------------------------------------------------------------------------
02 EMB-145 Jun-99* 25 EMB-145 Apr-01*
------------------------------------------------------------------------------------------------------------------
03 EMB-145 Aug-99* 26 EMB-145 May-01*
------------------------------------------------------------------------------------------------------------------
04 XXX-000 Xxx-00* 00 XXX-000 May-01*
------------------------------------------------------------------------------------------------------------------
05 EMB-145 Jan-00* 28 EMB-145 Jun-01*
------------------------------------------------------------------------------------------------------------------
06 EMB-145 Feb-00* 29 EMB-145 Jun-01*
------------------------------------------------------------------------------------------------------------------
07 XXX-000 Xxx-00* 00 XXX-000 Jul-01*
------------------------------------------------------------------------------------------------------------------
08 EMB-145 May-00* 31 EMB-145 Jul-01*
------------------------------------------------------------------------------------------------------------------
09 EMB-145 Jun-00* 32 EMB-145 Aug-01*
------------------------------------------------------------------------------------------------------------------
10 EMB-145 Jul-00* 33 EMB-145 Aug-01*
------------------------------------------------------------------------------------------------------------------
11 EMB-145 Aug-00* 34 EMB-145 Sep-01*
------------------------------------------------------------------------------------------------------------------
12 EMB-145 Aug-00* 35 EMB-145 Sep-01*
------------------------------------------------------------------------------------------------------------------
13 EMB-145 Sep-00* 36 EMB-140 22 Oct-01
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14 EMB-145 Oct-00* 37 EMB-145 20 Dec-01
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15 XXX-000 Xxx-00* 00 XXX-000 24 Oct-01
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16 XXX-000 Xxx-00* 00 XXX-000 26 Oct-01
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17 EMB-145 Dec-00* 40 EMB-140 26 Nov-01
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18 EMB-145 Dec-00* 41 EMB-145 14 Nov-01
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19 EMB-145 Jan-01* 42 EMB-140 29 Nov-01
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20 EMB-145 Jan-01* 43 EMB-140 10 Dec-01
------------------------------------------------------------------------------------------------------------------
21 EMB-145 Jan-01* 44 EMB-140 14 Dec-01
------------------------------------------------------------------------------------------------------------------
22 EMB-145 Feb-01* 45 EMB-140 19 Dec-01
------------------------------------------------------------------------------------------------------------------
23 EMB-145 Mar-01*
-------------------------------------------------
REMARKS: * Delivered to Buyer as of the date hereof.
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* Confidential
5. CERTIFICATION: The first line of Article "6" shall be deleted and replaced
with the following:
"On the Actual Delivery Date of Aircraft, the EMB-145 and EMB-140
Aircraft shall have valid and effective type certificates issued by
the CTA and FAA."
6. OPTION AIRCRAFT:
6.1 The first paragraph, delivery table, and second paragraph in Article "24"
shall be deleted and replaced with the following:
"Buyer shall have the option to purchase the Option Aircraft, to be
delivered in accordance with the chart below, subject to the terms and
conditions of this Article:
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OPTION AIRCRAFT
--------------------------------------------------------------------------------------------------------------
A/C # AIRCRAFT DELIVERY MONTH A/C # AIRCRAFT DELIVERY MONTH
--------------------------------------------------------------------------------------------------------------
01 EMB-140 Jul 02 15 EMB-145 Feb 03
--------------------------------------------------------------------------------------------------------------
02 EMB-140 Jul 02 16 EMB-145 Feb 03
--------------------------------------------------------------------------------------------------------------
03 EMB-140 Aug 02 17 EMB-145 Mar 03
--------------------------------------------------------------------------------------------------------------
04 EMB-140 Aug 02 18 EMB-145 Mar 03
--------------------------------------------------------------------------------------------------------------
05 EMB-140 Sep 02 19 EMB-145 Apr 03
--------------------------------------------------------------------------------------------------------------
06 EMB-140 Sep 02 20 EMB-145 Apr 03
--------------------------------------------------------------------------------------------------------------
07 EMB-140 Oct 02 21 EMB-145 May 03
--------------------------------------------------------------------------------------------------------------
08 EMB-140 Oct 02 22 EMB-145 May 03
--------------------------------------------------------------------------------------------------------------
09 EMB-145 Nov 02 23 EMB-145 Jun 03
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10 EMB-145 Nov 02 24 EMB-145 Jun 03
--------------------------------------------------------------------------------------------------------------
11 EMB-145 Dec 02 25 EMB-145 Jul 03
--------------------------------------------------------------------------------------------------------------
12 EMB-145 Dec 02 26 EMB-145 Jul 03
--------------------------------------------------------------------------------------------------------------
13 XXX-000 Xxx 00 00 XXX-000 Aug 03
--------------------------------------------------------------------------------------------------------------
14 XXX-000 Xxx 00 00 XXX-000 Aug 03
--------------------------------------------------------------------------------------------------------------
"
6.2. Article "24.a" shall be deleted and replaced with the following:
"a. INITIAL DEPOSIT: A refundable deposit of [*] is due and payable
immediately after signature of this Amendment No. 13 and the
outstanding amount already paid [*]), regarding initial deposits
for the Option Aircraft shall be returned to Buyer promptly after
signature of this Amendment No. 13, and the interest on the initial
deposits of the cancelled Option Aircraft shall be paid in
accordance with Article "24.f" to the
Purchase Agreement. Interest
on the [*] returned portion of each non-cancelled Option Aircraft
deposit shall be due only if Buyer cancels such Option Aircraft. In
that case, Embraer shall pay [*] amount of the original Initial
Deposits for each such Option Aircraft in accordance with
Article "24.f" to the
Purchase Agreement, provided that interest
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* Confidential
shall stop accruing on the previously returned [*] as of the
date Embraer returned such amount to Buyer."
6.3. Article "24.b" shall be deleted and replaced with the following, as
applicable:
"b. [*], provided that such Option Aircraft be delivered to Buyer in
accordance with the chart above and in the same configuration,
specification and installations specified in Attachments 'A-1',
'A-2' and 'A-3', as such attachment is written on the date of
signature of this Amendment No. 13 unless otherwise modified by
the Parties and the costs for such changes shall be in addition
to the Basic Price."
b.1 [*] provided that such Option Aircraft be delivered to Buyer in
accordance with the chart above and in the same configuration,
specification and installations specified in Attachment "A-4",
as such attachment is written on the date of signature of this
Amendment No. 13 unless otherwise modified by the Parties and
the costs for such changes shall be in addition to the
Basic Price"
6.4. Article "24.d" shall be deleted and replaced with the following:
"d. DEPOSIT AND PROGRESS PAYMENTS: The payment of the price specified in
item "b" above, shall be made according to the following:
1. The initial deposit of [*] to be made by Buyer according to
Article 24.a., shall apply toward the price of the relevant
Option Aircraft.
2. A progress payment of [*] of the unit basic price defined in
item "b" above, per exercised Option Aircraft, less the
initial deposit of [*] per exercised Option Aircraft is due
and payable [*] prior to each exercised Option Aircraft
contractual delivery date.
3. A progress payment of [*] item "b" above is due and payable
[*] prior to each relevant exercised Option Aircraft
contractual delivery date.
4. A progress payment of [*] of the unit basic price defined
in item "b" above is due and payable [*]
5. The balance of each exercised Option Aircraft escalated price
is due and
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* Confidential
payable upon acceptance of each relevant Aircraft by Buyer.
6.5. Article "24.e" shall be deleted and replaced with the following:
"e. CONFIRMATION OF OPTION GROUPS: The Option Groups (of two Aircraft
each) shall be confirmed on or before the following dates:
First 4 Option Groups [*]
Next 4 Option Groups [*]
Next 2 Option Groups [*]
Next 2 Option Groups [*]
Last 2 Option Groups [*]
At the time of each such confirmation, the Initial Deposit with respect to
the Option Aircraft in such Option Group shall become non refundable. In
the event that Buyer fails to exercise its option with respect to any five
(5) Option Groups, Buyer shall lose its rights to said Option Groups, as
well as all remaining Option Groups."
7. ATTACHMENT A - CONFIGURATION CHANGES: Attachment A-4 to this Amendment
No.13 shall be included in the Purchase Agreement, reflecting the
configuration selected by Buyer for the EMB-140 Aircraft (to be delivered
under the AMR Eagle configuration).
8. ATTACHMENT B:
8.1. On item 2.0 of Section 2 to Attachment B, the reference to "EMB-145
Aircraft" shall be deleted and replaced with "EMB-145 and EMB-140
Aircraft".
8.2 EMB-140 Additional Technical Publications: The following operational and
technical publications to the EMB-140 Aircraft shall be supplied at no
cost to Buyer and a new item 3.1 shall be included to the Attachment "B"
to the Purchase Agreement as follows:
"3.1. LIST OF PUBLICATIONS (EMB-140 Aircraft)
As provided for in Article 15 of this Agreement, the technical
publications covering operation and maintenance for the EMB-140
Aircraft shall be delivered to Buyer in accordance with the
following list:
QTY
TITLE (COPIES)
----- --------
OPERATIONAL
1. Airplane Flight Manual (AFM)(*) [*]
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* Confidential
2. Quick Reference Handbook (QRH)(*) [*]
3. Supplementary Performance Manual (SPM)(*) [*]
MAINTENANCE
4. Aircraft Maintenance Manual (AMM) [*]
5. Illustrated Parts Catalog (IPC) [*]
6. Wiring Manual (WM) [*]
MAINTENANCE SUPPLEMENTARY SET
7. System Schematic Manual (SSM) [*]
(*) One extra copy on board each Aircraft
If Buyer elects not to take all or any one of the publications above mentioned,
or revisions thereof, no refund or other financial adjustment of the Basic Price
will be made since such publications are offered at no cost to Buyer as referred
to in Article 15.a of the Purchase Agreement.
10. ATTACHMENTS C, D, E, F, G AND I: All references to "EMB-145 Aircraft" on
Attachments C, D, E, F, G and I to Purchase Agreement shall be deleted and
replaced by "EMB-145 or EMB-140 Aircraft".
11. ATTACHMENT H AND NOTICES: All references to "Wexford Management LLC" on
Attachment H and Notices to Purchase Agreement shall be deleted and
replaced by "Wexford Capital LLC".
12. PERFORMANCE GUARANTEE FOR EMB-140 AIRCRAFT IN AMR EAGLE CONFIGURATION:
Attachment J-1 to this Amendment No.13 shall be included in the Purchase
Agreement, reflecting the Performance Guarantee for the EMB-140 Aircraft
to be delivered under the AMR Eagle configuration.
13. MISCELLANEOUS: All other provisions of the Agreement which have not been
specifically amended or modified by this Amendment No. 13 shall remain
valid in full force and effect without any change.
[The remainder of this page has been left blank intentionally.]
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* Confidential
IN WITNESS WHEREOF, EMBRAER and BUYER, by their duly authorized officers, have
entered into and executed this Amendment No. 13 to be effective as of the date
first written above.
EMBRAER - Empresa Brasileira de Solitair Corp.
Aeronautica S.A.
By /s/ Xxxxxxxxx Xxxxxx Curado By /s/ Xxx Xxxxxxxx
---------------------------- ---------------------------
Name: Xxxxxxxxx Xxxxxx Curado Name: Xxx Xxxxxxxx
------------------------ ------------------------
Title: E.V.P. Airline Market Title: V.P.
------------------------ ------------------------
By /s/ Xxxxxx Xxxxxx Date: 10/22/01
--------------------------- ------------------------
Name: Xxxxxx Xxxxxx Place: Greenwich, CT
------------------------- -----------------------
Title: Director of Contracts
------------------------
Date: 10/22/2001
------------------------
Place: Sao Xxxx dos Xxxxxx
------------------------
ATTACHMENT "A-4"
EMB-140 AIRCRAFT UNDER
AIRCRAFT SPECIFIC CONFIGURATION, FINISHING AND
REGISTRATION MARKS
1. STANDARD 140 AIRCRAFT
The Aircraft shall be manufactured according to the standard configuration
specified in Embraer's Technical Description TD-140/002 dated as of April
2000, Type Certification FAA, and including the following optional items:
2. OPTIONAL EQUIPMENT:
2.1 OPTIONS TO STANDARD AVIONICS CONFIGURATION
a) CAT II
b) 2nd DME
c) 2nd ADF
d) 2nd Transponder Mode S
e) Weather Radar with Independent Selection
f) 3rd VHF with 25 KHz spacing
g) Dual FMS+GPS (Universal)
h) ACARS (Unilink)
i) Printer
j) AFDAU
k) Single Potentiometer to control FA volume
2.2 OPTIONAL SYSTEM/OTHER EQUIPMENT
a) Thrust Reversers
b) APU Silencer
c) Cockpit Floodlight
d) External Painting with capability to be polished
e) LR Version
f) Service Door Sill Protection
g) Baggage Door Sill Protection
h) Baggage Door Light
i) Optional Main Door (without steps)
j) Floor Covering in Cargo Compartment - GE Lexan
k) Provisions for Antenna for In-Flight Phone (antenna to be
provided as loose item)
l) Steering Disengage Outside Cockpit
2.3 INTERIOR OPTIONAL ITEMS
a) Interior Option 3
b) Audio Entertainment
c) Aft Hand Set & Cradle
d) Blue Sterile Light
e) 3rd Oxygen Mask on RH
f) Passenger Seats Customized (P/N140-86006-401 seat installation
kit)
g) Baggage Restraint Net
h) Vertical Baggage Barrier Net
i) Provisions for Defibrillator
j) Emergency equipment items supplied by Buyer (BFE);
j.1) PBE 119003 Puritan Bennett
j.2) PBE brackets 119063-01 Puritan Bennett
j.3) Smoke goggles 322-70 Xxxxx Aviation
j.4) First Aid kit 70004-00 Xxxxx Aviation
j.5) Medical kit 4531 Medical Advisory Sys
j.6) Fire Extinguisher A352T HRD Aero Sys
j.7) Fire extinguisher bracket 817 HRD Aero Sys.
3. FINISHING
a. EXTERIOR FINISHING:
The Aircraft shall be painted according to Buyer's color and paint
scheme which shall be supplied to Embraer by Buyer on or before six
(6) months prior to the relevant Aircraft Contractual Delivery Date.
b. INTERIOR FINISHING:
Buyer shall inform Embraer on or before eight (8) months prior to
the relevant Aircraft Contractual Delivery Date of its choice of
materials and colors of all and any item of interior finishing such
as seat covers, carpet, floor lining on galley areas, side walls and
overhead lining, galley lining and curtain. The above mentioned
schedule for definition of interior finishing shall only be
applicable if Buyer selects its materials from the choices offered
by and available at Embraer. If Buyer opts to use different
materials and or patterns, such schedule shall be agreed between the
Parties at the time of signature of this Purchase Agreement.
4. REGISTRATION MARKS
The Aircraft shall be delivered to Buyer with the registration marks
painted on them, which shall be supplied to Embraer by Buyer no later than
ninety (90) days before each relevant Aircraft Contractual Delivery Date.
IF THERE IS ANY CONFLICT BETWEEN THE TERMS OF THIS ATTACHMENT "A-4" AND THE
TERMS OF THE TECHNICAL DESCRIPTION TD-140/002, DATED APRIL 2000, THE TERMS OF
THIS ATTACHMENT "A-4" SHALL PREVAIL.
ATTACHMENT J-1
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EMB 140 - AIRCRAFT PERFORMANCE GUARANTEE
ATTACHMENT "J-1" - AIRCRAFT PERFORMANCE GUARANTEE
1. GUARANTEES
Embraer, subject to the conditions and limitations hereby expressed, and
considering the Aircraft with a maximum takeoff weight of 46,517 pounds
(21,100 kg) and equipped with XXXXXXX xxxxxxxxx Xxxxx-Xxxxx Xxxxxxx XX
0000X0/0 engines, guarantees each Aircraft as follows:
a. On the Aircraft Actual Delivery Date, the Aircraft will comply with
the following performance:
a.1 CRUISE SPECIFIC AIR RANGE
The cruise specific air range at a gross weight of
40,000 pounds (18,144 Kg) in a standard day (ISA), at an
altitude of 35,000 feet, at 440 KTAS using not more than
maximum cruise thrust, shall not be less than the
guarantee value:
NOMINAL: .182 NAM/Pound
TOLERANCE: - .006 NAM/Pound
GUARANTEE: .176 NAM/Pound
a.2 MISSION PAYLOAD
a.2.1 The payload for a stage length of 1000 nautical miles in
still air, shall not be less than the guarantee value:
GUARANTEE: 10,506 Pounds (4,765 kg)
Note: The above guaranteed value is subject to the same tolerance
applicable to the MEW pursuant to Paragraph a.3 below.
The above guarantee is based on the following conditions
and operating rules:
Stage Length:
The stage is defined as the sum of the distances for
length climb, cruise and descent.
Takeoff:
The airport altitude is at SEA LEVEL.
The takeoff weight is not limited by the airport
conditions.
Maximum takeoff thrust is used for the takeoff.
Climbout Maneuver:
Following the takeoff to 35 feet, the EMB-140 Aircraft
accelerates to 245 KCAS while climbing to 1,500 feet
above the departure airport altitude and retracting
flaps and landing gear.
Climb:
The EMB-140 Aircraft climbs from 1,500 feet above the
departure airport altitude to 10,000 feet altitude at
245 KCAS.
The EMB-140 Aircraft then accelerates to a speed of 270
KCAS.
The climb continues at 270 KCAS until 16,000 feet is
reached.
The climb continues at 0.56 Mach number to cruise
altitude.
The temperature is ISA during the climb.
Maximum climb thrust is used throughout the climb.
Cruise:
The EMB-140 Aircraft cruises at an average speed of 0.76
Mach number.
The cruise altitude is 37,000 feet. The temperature is
ISA during cruise.
The cruise thrust is not to exceed maximum cruise
thrust.
Descent:
The EMB-140 Aircraft descends from the cruise altitude
at 250 KCAS.
The descent continues at 250 KCAS to an altitude of
1,500 feet.
The temperature is ISA during descent.
Approach and Landing Maneuver:
The EMB-140 Aircraft decelerates to the final approach
speed while extending landing gear and flaps, then
descends and lands.
The destination airport elevation is at sea level.
Fixed Allowances:
For the purpose of this guarantee and for the purpose of
establishing compliance with this guarantee, the
following shall be used as fixed quantities and
allowances:
Taxi-out fuel: 109 Pounds, equivalent to 9 minutes.
Takeoff and Climbout Maneuver fuel: 99 Pounds.
Approach and Landing Maneuver fuel: 101 Pounds.
Taxi-in fuel (shall be consumed from the reserve fuel):
97 Pounds, equivalent to 8 minutes of taxi.
The usable reserve fuel remaining upon completion of the
landing: 2,350 Pounds.
A.2.2 OPERATIONAL EMPTY WEIGHT BASIS
Operational empty weight (OEW) derived in accordance
with Paragraph a.2.3 shall be used as the basis for the
mission payload guarantees of Paragraph a.2.1.
A.2.3 EMB-140 WEIGHT SUMMARY
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ITEMS WEIGHT (KG) WEIGHT (LB)
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1 - M.E.W Std. EMB-140 Aircraft Configuration(*) 11,100 24,471
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2 - Option to std EMB-140 Aircraft (**) 677.7 1,495
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3 - M.E.W. Customer Configuration LR version 11,777.2 25,966
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4 - Operating Items 556 1,226
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a - Pilot and Copilot (180 Lb each) (***) 164.0 361.6
---------------------------------------------------------------------------------------------------
b - Stewardess (140 Lb each) (***) 64.0 141.1
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c - Engine oil 24.0 52.9
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d - Hydraulic Fluid 36.0 79.4
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e - Unusable Fuel 44.0 97.0
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f - Apu Oil 2.0 4.4
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g - Toilet Fluid 7.0 15.4
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h - Water 20.0 44.1
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i - Flight Kit 10.0 22.0
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j - Crew Baggage 20.4 45.0
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k - Catering Standard 160.0 352.7
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l - Pass. Serv. Equip. 4.5 9.9
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m - 2nd Attendant 0.0 0.0
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5 - O. E. W. Customer Configuration LR version 12,3334 27,191
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REMARKS:
(*) See Customer Options Table (Item a.5.4).
(**) In accordance with Advisory Circular No: 120-27C (U.S.
Depart. Of Transp./FAA)
a.2.4 CUSTOMER OPTIONS TABLE:
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ITEMS OPT WEIGHT WEIGHT
(KG) (LB)
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A) OPTIONS TO STD AVIONIC CONFIGURATION
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01. CAT-II Y 0.0 0.0
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02. DME (2nd) Y 1.5 3.3
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03. ADF (2nd) Y 8.0 17.6
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04. Transponder Mode S (2nd) Y 1.0 2.2
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05. Weather Radar w/ Independent Selection Y 1.0 2.2
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06. VHF (3rd) Y 6.0 13.2
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07. FMS+GPS Dual Universal Y 26.0 57.3
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08. Printer Y 5.0 11.0
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09. AFDAU Y 8.0 17.6
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10. Single Potentiometer to control FA volume Y 1.0 2.2
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11. ACARS Y 8.5 19.0
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B) OPTIONAL SYSTEM / OTHER EQUIPMENT
------------------------------------------------------------------------------------------------------------------
01. Thrust Reversers Y 173.0 381.4
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02. APU Silencer Y 13.0 28.7
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03. Cockpit Floodlight Y 2.5 5.5
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04. External Painting w/ capability to be polished Y 54.0 119.0
------------------------------------------------------------------------------------------------------------------
05. LR Version Y 172.0 378.4
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06. Service door sill protection Y 3.0 6.6
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07. Cargo door sill protection Y 3.5 7.7
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08. Cargo Door Light Y 1.0 2.2
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09. Optional Main Door (without steps) Y -8.0 -17.6
------------------------------------------------------------------------------------------------------------------
10. Gust Lock for Elevator Surfaces Y 2.6 5.7
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11. Floor Covering in Cargo Compartment - GE Lexan Y 3.3 7.3
------------------------------------------------------------------------------------------------------------------
12. Provisions for Antenna for In-Flight Phone (antenna to be
provided as loose item) Y 4.0 8.8
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13. Steering Disengage Outside Cockpit Y 0.2 0.5
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14. Floor Mat per AMR request Y 1.2 2.6
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C) INTERIOR OPTIONAL ITEMS
------------------------------------------------------------------------------------------------------------------
01. Interior Option 3 (1) Y 71.0 156.5
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02. Audio Entertainment Y 2.5 5.5
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03. Aft Hand Set & Cradle Y 2.5 5.5
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04. Blue Sterile Light Y 0.5 1.1
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05. 3rd Oxygen Mask Y 1.5 3.3
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06. Customized Passenger Seat AMR Leather Y 86 190.0
------------------------------------------------------------------------------------------------------------------
07. Baggage Restraint Net Y 8.0 17.6
------------------------------------------------------------------------------------------------------------------
08. Vertical Baggage Barrier Net Y 10.0 22.0
------------------------------------------------------------------------------------------------------------------
09. Provisions for Defibrillator Y 4.5 9.9
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SUB-TOTAL (OPTIONS STD A/C) 677.7 1,495
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(1) Galley inserts (Trolley, SU, Hot Jugs) and catering are not included
a.3 WEIGHT
a.3.1 The manufacturer's empty weight (M.E.W.), for
Customer configuration, is guaranteed to be:
NOMINAL: 25,966 POUNDS
TOLERANCE: 259 POUNDS
GUARANTEE: 26,225 POUNDS
2. EMB-140 AIRCRAFT CONFIGURATION
2.1 The guarantees stated above are based on the EMB-140 Basic Aircraft
configuration as defined in the Technical Description TD-140/002
dated April 2000, plus specific Buyer configuration options as
defined at Attachment "A" to the Purchase Agreement, (hereinafter
referred to as the Detail Specification). Appropriate adjustment to
the guarantees shall be made for changes in such Detail
Specification approved in writing by the Buyer and Embraer. Such
adjustments shall be accounted for by Embraer in its evidence of
compliance with the guarantees.
In the event a change is made to any law, governmental regulation or
requirement, or in the interpretation of any such law, governmental
regulation or requirement that affects the certification basis for
the EMB-140 Aircraft, and as a result thereof, a change is made to
the configuration and/or the performance of the EMB-140 Aircraft in
order to obtain certification, the guarantees set forth in this
EMB-140
Aircraft Performance Guarantee shall be appropriately modified to
reflect any such change.
2.2 The guarantee payloads of Paragraph 1.a.5 and the Manufacturer's
Empty Weight guarantee of Section 1.a.6 shall be adjusted by Embraer
for the following in its evidence of compliance with such
guarantees:
(1) Changes to the Detail Specification including Change Requests,
Master Changes, Change Orders or any other changes mutually
agreed upon between the Buyer and Embraer.
(2) The difference between the component weight allowances given
in the appropriate section of the Detail Specification and the
actual weights.
3. GUARANTEE CONDITIONS
3.1 All guaranteed performance data are based on the ICAO International
Standard Atmosphere (ISA) and specified variations there from;
altitudes are pressure altitudes.
3.2 The FAA Regulations (FAR) referred to in this Schedule are, unless
otherwise specified, the EMB-140 Certification Basis regulations
specified in the Type Certificate Data Sheet. The reference number
for the Certificate Data Sheet and its date of issue will be
provided to Buyer within fifteen (15) days of type approval.
3.3 The takeoff and landing guarantees are based on hard surface, level
and dry runways with no wind or obstacles, no clearway or stopway,
and with automatic anti-skid operative unless otherwise specified.
The takeoff performance is based on no engine bleed for air
conditioning or thermal anti-icing and the Auxiliary Power Unit
(APU) turned off unless otherwise specified. The improved climb
performance procedure will be used for takeoff as required. The
landing data is based on the use of automatic spoilers.
3.4 The cruise specific air range, speed and altitude capability, and
the climb, cruise and descent portions of the mission guarantees
include allowances for normal electrical power extraction and normal
operation of the air conditioning system. Normal power extraction
shall be defined as not less than a 37 kW total electrical and
hydraulic loads. Normal operation of the air conditioning system
shall be defined as operation in the automatic mode, with the
temperature control set to maintain a nominal cabin temperature of
75(DEGREE)F, and all air conditioning systems operating normally.
This operation nominally
allows a sea level cabin altitude to be maintained up to 19,500 feet
and a maximum cabin pressure differential of 7.8 pounds per square
inch at higher altitudes, with a nominal EMB-140 Aircraft cabin
ventilation rate of 1,100 cubic feet per minute at 35,000 ft
including passenger cabin recirculation (nominal recirculation is 42
percent not considering xxxxxx flow). The APU is turned off unless
otherwise specified.
3.5 The cruise specific air range, speed and altitude capability, and
the climb, cruise, and descent portions of the mission guarantees
are based on an EMB-140 Aircraft center of gravity location of 26
percent of the mean aerodynamic chord.
3.6 Performance, where applicable, is based on a fuel Lower Heating
Value (LHV) of 18,580 BTU per pound and a fuel density of 6.70
pounds per U.S. gallon.
4. PARTIES' OBLIGATIONS ACCORDING TO THIS GUARANTEE
RELATIVE TO THE GUARANTEES STATED IN PARAGRAPH 1.a above:
4.1 During the EMB-140 Aircraft acceptance to be performed by Buyer in
accordance with Article 7 of the Purchase Agreement, Buyer shall
check the EMB-140 Aircraft performance specified in paragraph 1.a of
this Schedule A, by using the EMB-140 Aircraft Flight Manual (AFM)
and by comparing the flight test data, at the atmospheric conditions
prevailing during the flight, with the information presented in the
EMB-140 Supplementary Performance Manual (SPM). All the performance
guarantee under this Schedule A are in accordance with both manuals
above mentioned, taking into consideration the established
tolerances.
4.2 Embraer's obligations in respect to the guarantees stated in
Paragraph 1.a of this Schedule A, are limited to Buyer's right to
terminate the Purchase Agreement in respect to the relevant EMB-140
Aircraft, pursuant to Article 22.d. should it be reasonably verified
that such EMB-140 Aircraft during the acceptance procedure specified
in Article 7 of the Purchase Agreement, cannot comply with the
performances guaranteed hereunder after Embraer has had a reasonable
opportunity to cure such deficiencies in accordance with Article 7.
4.3 In case during the above mentioned acceptance procedure, it is
proven that the EMB-140 Aircraft performance does not comply with
the performances specified in Paragraph 1.a of this Schedule A, but
Buyer considers it satisfactory by accepting delivery of such
EMB-140
Aircraft, then Embraer shall not be liable to any claim or demand
whatsoever from Buyer with respect to such performance guarantees.
4.4 Upon acceptance of the EMB-140 Aircraft by Buyer, all obligations of
Embraer regarding the Aircraft performance guarantees specified in
Paragraph 1.a, shall cease.
5. GUARANTEE COMPLIANCE
5.1 Compliance with the guarantees of Section 1.a shall be based on the
conditions specified in that section, the EMB-140 Aircraft
configuration of Section 2 and the guarantee conditions of Section
3.
5.2 Compliance with the takeoff, landing, and TOW Climb limit guarantees
shall be based on the FAA-approved Airplane Flight Manual for the
EMB-140.
5.3 Compliance with the cruise specific air range, speed, and the climb,
cruise and descent portions of the mission guarantees shall be
established by calculations based on the comparison mentioned in
Section 4.1 above.
5.4 The data derived from tests shall be adjusted as required by
conventional methods of correction, interpolation or extrapolation
in accordance with established engineering practices to show
compliance with provisions of Section 1.a.
5.5 Compliance with the Manufacturer's Empty Weight guarantee shall be
based on information in the appropriate approved weight and balance
manual, or associated document or report.
5.6 Compliance with the guarantees set forth in this Schedule does not
depend on the engine meeting the performance requirements contained
in the engine specification.
6. EXCLUSIVE GUARANTEES
6.1 The only performance guarantees applicable to the EMB-140 Aircraft
are those set forth in this document. The performance guarantees set
forth herein are established between Buyer and Embraer and may not
be transferred or assigned to others, unless by previous written
consent of Embraer.
6.2 THE GUARANTEES, OBLIGATIONS AND LIABILITIES OF Embraer, AND REMEDIES
OF Buyer SET FORTH IN THIS
PERFORMANCE GUARANTEE ARE EXCLUSIVE AND IN SUBSTITUTION FOR, AND
Buyer HEREBY WAIVES, RELEASES AND RENOUNCES, ALL OTHER RIGHTS,
CLAIMS, DAMAGES AND REMEDIES OF Buyer AGAINST Embraer OR ANY
ASSIGNED OF Embraer, EXPRESS OR IMPLIED, ARISING BY LAW OR
OTHERWISE, WITH RESPECT TO ANY ACHIEVED PERFORMANCE.
6.3 The terms and conditions of this Performance Guarantee do not alter,
modify or impair, in any way, the terms and conditions of Attachment
C (EMB-140 AIRCRAFT WARRANTY CERTIFICATE) to this Agreement.
