Frontier Airlines 2006 Annual Report Download - page 159

ATTACHMENT “H-1” - PERFORMANCE GUARANTEE EMBRAER 175
1. GUARANTEES
Embraer, subject to the conditions and limitations hereby expressed, and considering the Aircraft EMBRAER 175 LR version with a maximum takeoff
weight of 85,517 lb (38,790 kg), equipped with Embraer furnished General Electric CF34-8E5 engines, guarantees that each Aircraft on the relevant
Actual Delivery Date shall comply with the following performance:
1.1 CRUISE SPECIFIC AIR RANGE
The cruise specific air range(SAR) in a standard day (ISA), at the aircraft gross weights, pressure altitudes and Mach numbers
noted below shall not be less than the guarantee value:
***.
2. AIRCRAFT CONFIGURATION
2.1 The guarantees stated above are based on the Aircraft configuration as defined in the Technical Description PTD-175 Rev. 5 dated April 2005, plus
specific Buyer configuration options as defined at Attachment “A” to the Purchase Agreement, (hereinafter referred to as the “Detail Specification”). If
necessary, appropriate adjustment to this Aircraft Performance Guarantees shall be made for changes in such Detail Specification (including but not
limited to Buyer requests for changes, Proposal of Major Changes or any other changes mutually agreed upon between the Buyer and Embraer) 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 Aircraft, and as a result thereof, a change is made to the configuration and/or the performance of the
Aircraft in order to obtain certification, the guarantees set forth in this Aircraft Performance Guarantee shall be appropriately modified to reflect any such
change.
2.2 The performance guarantees of Article 1 of this Attachment shall be adjusted by Embraer for the following in its evidence of compliance with such
guarantees:
a. Changes to the Detail Specification including Major Changes or any other changes mutually agreed upon between the
Buyer and Embraer.
b. The difference between the weight allowances of optional items listed in 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) unless otherwise specified. Altitudes are pressure
altitudes.
3.2 The FAA Regulations referred to in this Attachment are, unless otherwise specified, the Certification Basis regulations specified in the Aircraft Type
Certificate Data Sheet.
3.3 The cruise specific air range 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 41 kW total electrical and
hydraulic loads. Normal operation of the air conditioning system
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***Confidential
Source: REPUBLIC AIRWAYS HOLDINGS INC, 10-K, March 15, 2007 Powered by Morningstar® Document Research℠