Common use of GUARANTEE CONDITIONS Clause in Contracts

GUARANTEE CONDITIONS. 5.1 The performance certification requirements for the Aircraft, except where otherwise stated, will be as stated in Section 02 of the Specification. 5.2 For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitation, no line-up allowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, and the use of speedbrakes, flaps, associated speeds, landing gear, center of gravity position and engines in the conditions liable to provide the best results will be assumed. 5.3 When establishing take-off performance no air will be bled from the engines for cabin air conditioning or anti-icing.

GUARANTEE CONDITIONS. 5.1 The performance certification requirements for the Aircraft, except where otherwise statednoted, will be as stated in Section 02 of the Specification. 5.2 For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitationlimitations, no line-up allowanceallowances, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, noted and the use of center of gravity position, speedbrakes, flaps, associated speeds, landing gear, center of gravity position gear and engines in the conditions liable to provide the best results will be assumed. 5.3 When establishing take-off performance and second segment performance, no air will be bled from the engines for cabin air conditioning or for anti-icingicing except if otherwise noted. 5.4 21-30.31 of the Specification. ***** 5.5 The engines will be operated using *****. 5.6 Where applicable, *****.

GUARANTEE CONDITIONS. 5.1 6.1 The performance and noise certification requirements for the Aircraft, except where otherwise statednoted, will be as stated in Section 02 of the Specification. 5.2 6.2 For the determination of FAR take-off and landing performance a hard dry level dry runway surface with no runway strength limitationlimitations, no line-up allowanceallowances, no obstacles, zero wind, atmosphere according to ISA, except as otherwise statednoted, and the use of speedbrakescentre of gravity positions, speed brakes, flaps, associated speeds, landing gear, center of gravity position gear and engines in the conditions liable to provide the best results will be assumed. 5.3 6.2.1 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. 5.1 The performance certification requirements for the A320 Aircraft, except where otherwise statednoted, will be as stated in Section 02 of the Specification. 5.2 For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitationlimitations, no line-up allowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, noted and the use of speedbrakes, flaps, associated speeds, landing gear, center of gravity position gear and engines in the conditions liable to provide the best results will be assumed. 5.3 5.2.1 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. 5.1 The performance certification requirements for the A319 Aircraft, except where otherwise statednoted, will be as stated in Section 02 of the Specification. 5.2 For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitationlimitations, no line-up allowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, noted and the use of speedbrakesspeed brakes, flaps, associated speeds, landing gear, center of gravity position gear and engines in the conditions liable to provide the best results will be assumed. 5.3 5.2.1 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. 5.1 6.1. The performance certification requirements for the Aircraft, except where otherwise stated, will be as stated in Section 02 of the Standard Specification. 5.2 6.2. For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitation, no line-up allowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, and the use of speedbrakes, flaps, associated speeds, landing gear, center of gravity position gear and engines in the conditions liable to provide the best results will be assumed. 5.3 6.3. When establishing take-off performance no air will be bled from the engines for cabin air conditioning or anti-icing.

GUARANTEE CONDITIONS. 5.1 6.1 The performance certification requirements for the Aircraft, except where otherwise stated, will be as stated in Section 02 of the Specification. 5.2 6.2 For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitation, no line-up allowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, and the use of speedbrakes, flaps, associated speeds, landing gear, center of gravity position and engines in the conditions liable to provide the best results will be assumed. 5.3 6.3 When establishing take-off performance no air will be bled from the engines for cabin air conditioning or anti-icing.

GUARANTEE CONDITIONS. 5.1 8.1 The performance certification requirements for the Aircraft, except where otherwise stated, will be as stated in Section 02 of the Specification. 5.2 8.2 For the determination of FAR take-off and landing performance a hard level dry runway surface with no runway strength limitation, no line-up allowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise stated, and the use of speedbrakes, flaps, associated speeds, landing gear, center of gravity position and engines in the conditions liable to provide the best results will be assumed. 5.3 8.3 When establishing take-off performance no air will be bled from the engines for cabin air conditioning or anti-icing.