GUARANTEE CONDITIONS. 4.1 The performance certification requirements for the Aircraft, except where otherwise noted, will be as stated in Section 02 of the Standard Specification.
4.2 For the determination of JAR take-off and landing performance a hard dry level runway surface with no runway strength limitations, no line-up allowances, no obstacles, zero wind, atmosphere according to ISA, except as otherwise noted, and the use of speed brakes, flaps, landing gear and engines in the conditions liable to provide the best results will be assumed.
4.2.1 When establishing take-off and second segment performance no air will be bled from the engines for cabin air conditioning or anti-icing.
GUARANTEE CONDITIONS. All guaranteed performance data are based on the International Standard Atmosphere (ISA) and specified variations therefrom; altitudes are pressure altitudes.
GUARANTEE CONDITIONS. 5.1 All guaranteed performance data are based on the International Standard Atmosphere (ISA) and specified variations therefrom; altitudes are pressure altitudes.
5.2 The FAA Regulations (FAR) referred to in this Attachment are, unless otherwise specified, the 737-800 Certification Basis regulations specified in the Type Certificate Data Sheet A16WE, Revision 33, dated March 8, 2002.
GUARANTEE CONDITIONS. 4.1. The performance certification requirements for the Aircraft, except where otherwise stated, will be as stated in Section 02 of the Specification.
GUARANTEE CONDITIONS. 6.1 All guaranteed performance data are based on the International Standard Atmosphere (ISA) and specified variations therefrom; altitudes are pressure altitudes.
6.2 The Federal Aviation Administration (FAA) regulations referred to in this Attachment are, unless otherwise specified, Code of Federal Regulations 14, Part 25 amended by Amendments 25-1 through 25-128, subject to the approval of the Federal Aviation Administration.
6.3 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 as described in Paragraph 6.2, 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 Attachment will be appropriately modified to reflect any such change.
GUARANTEE CONDITIONS. 4.1 The performance certification requirements for the Aircraft, except where otherwise noted, will be as stated in Section 02 of the Standard Specification.
4.2 For the determination of JAR take-off and landing performance a hard dry level runway surface with no runway strength limitations, no line-up allowances, no obstacles, zero wind, atmosphere according to ISA, except as otherwise noted, and the use of speed brakes, flaps, landing gear and engines in the conditions liable to provide the best results will be assumed.
GUARANTEE CONDITIONS. 5.1. All guaranteed performance data are based on the ICAO International Standard Atmosphere (ISA) and specified variations therefrom; altitudes are pressure altitudes.
5.2. The FAA Regulations (FAR) referred to in this Attachment are, unless otherwise specified, the 747-400 Certification Basis regulations specified in the Type Certificate Data Sheet A20WE, Revision B, dated June 8, 1989.
5.3. Requirement, or in the interpretation of any such law, governmental regulation or requirement that affects the certification basis for the Aircraft as described in Paragraph 5.2, 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 79 Attachment to Letter Agreement No. 6-1162-DSF-082 CF6-80C2BIF Engines Page 15 Attachment shall be appropriately modified to reflect any such change.
5.4. The takeoff portion of the mission guarantees are based on hard surface, level and dry runways with no wind or obstacles, no clearway or stopway, 235 mph tires, with anti-skid operative, and with the Aircraft center of gravity at the most forward limit 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. The improved climb performance procedure will be used for takeoff as required.
5.5. The climb, cruise and descent portions of the mission guarantees include allowances for normal power extraction and engine bleed for normal operation of the air conditioning system. Normal electrical power extraction shall be defined as not less than a 100 kilowatts total electrical load. Normal operation of the air conditioning system shall be defined as pack switches in the "Normal" position, the temperature control switches in the "Auto" position that results in a nominal cabin temperature of 75 degrees F, and all air conditioning systems operating normally. This operation allows a maximum cabin pressure differential of 8.9 pounds per square inch, with a nominal Aircraft cabin ventilation rate of 5,600 cubic feet per minute including passenger cabin recirculation. The APU is turned off unless otherwise specified.
5.6. The climb, cruise and descent portions of the mission guarantees are based on an Aircraft center of gravity location of 20 percent of the mean a aerodynamic chord.
5.7. Performance, where applicable, is based on a fuel Lower Heating value (LHV) of 18,580 BTU...
GUARANTEE CONDITIONS. A. The obligation of Ex-Im Bank with respect to any Credit to issue a Lease Delivery Approval with respect to any Lease Delivery shall be subject to the delivery to Ex-Im Bank of the appropriate documents indicated below and to the fulfillment, in a manner satisfactory to Ex-Im Bank, of the conditions set forth below:
GUARANTEE CONDITIONS. 5.1 All guaranteed performance data are based on the International Standard Atmosphere (ISA) and specified variations therefrom; altitudes are pressure altitudes.
5.2 The Federal Aviation Administration (FAA) regulations referred to in this Attachment are, unless otherwise specified, the 737-900ER Certification Basis regulations specified in the Type Certificate Data Sheet A16WE, Revision 40, dated April 27, 2007.
5.3 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 P.A. No. PA-1951 AERO-B-BBA4-M12-0362C SS12-0153 Attachment to Letter Agreement Xx. XXX-XX-0000-XX-0000000 *** that affects the certification basis for the Aircraft as described in Paragraph 5.2, 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 Attachment shall be appropriately modified to reflect any such change.
5.4 The takeoff and landing guarantees, and the takeoff portion of the mission guarantees are based on hard surface, level and dry runways with no wind or obstacles, no clearway or stopway, *** mph tires, with Category P brakes and anti-skid operative, and with the Aircraft center of gravity at the most forward limit unless otherwise specified. The takeoff performance is based on no engine bleed for air conditioning or thermal anti-icing and the ***. Unbalanced field length calculations and the improved climb performance procedure will be used for takeoff as required. The landing performance is based on the use of automatic spoilers.
5.5 The enroute one-engine-inoperative altitude guarantee is based on engine bleed for air conditioning with one pack operating. No engine bleed for thermal anti-icing is provided unless otherwise specified. The APU is turned off unless otherwise specified.
5.6 The speed, altitude capability, and cruise range guarantees, and the climb, cruise and descent portions of the mission guarantees include allowances for normal power extraction and engine bleed for normal operation of the air conditioning system. Normal electrical power extraction shall be defined as not less than a *** kilowatts total electrical load. Normal operation of the air conditioning system shall be defined as pack switches in the “Auto” position, the temperature control switches in the “Auto” position that results in a nominal cabin temperature of ***°F, and ...
GUARANTEE CONDITIONS. 6.1. The performance certification requirements for the Aircraft, except where otherwise stated, will be as stated in Section 02 of the Standard Specification.
6.2. For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitation, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, and the use of speedbrakes, flaps, associated speeds, landing gear and engines in the conditions liable to provide the best results will be assumed.
6.3. When establishing take-off performance no air will be bled from the engines for cabin air conditioning or anti-icing.
