Common use of GUARANTEE CONDITIONS Clause in Contracts

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. 4.1 4.1. The performance certification requirements for the Aircraft, except where otherwise notedstated, will be as stated in Section 02 of the Standard Specification. 4.2 4.2. For the determination of JAR take-off and landing performance a hard level dry level runway surface with no runway strength limitations, no line-up allowancesallowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise noted, stated and the use of speed brakesspeedbrakes, flaps, landing gear and engines in the conditions liable to provide the best results will be assumed. 4.2.1 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. 4.2.2. When establishing en-route one engine inoperative climb performance the air conditioning bleed shall be on but no air will be bled from the engines for anti-icing.

GUARANTEE CONDITIONS. 4.1 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 4.2. For the determination of JAR take-off and landing performance a hard level dry level runway surface with no runway strength limitationsobstacles, no line-up allowances, no obstaclesallowance, zero wind, atmosphere according to ISA, except as otherwise noted, noted and the use of speed brakesspeedbrakes, flaps, landing gear and engines in the conditions liable to provide the best results will shall be assumed. For take-off performance no special procedures have been considered if not otherwise specified. 4.2.1 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. 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 level dry level runway surface with no runway strength limitationsobstacles, no line-up allowances, no obstaclesallowance, zero wind, atmosphere according to ISA, except as otherwise noted, noted and the use of speed brakesspeedbrakes, flaps, landing gear and engines in the conditions liable to provide the best results will shall be assumed. For take-off performance no special procedures have been considered if not otherwise specified. 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. 4.2.2 For the purpose of the take-off elements of the guarantee the centre of gravity position providing the best results shall be assumed.

GUARANTEE CONDITIONS. 4.1 The performance certification requirements for the A321 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.. *** This information is subject to confidential treatment and has been omitted and filed separately with the Commission. A319/A320 – CSN – 01/04 CC-C 3370036/02

GUARANTEE CONDITIONS. 4.1 The performance certification requirements for the A319 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.. *** This information is subject to confidential treatment and has been omitted and filed separately with the Commission. A319/A320 – CSN – 01/04 CC-C 3370036/02

GUARANTEE CONDITIONS. 4.1 The performance certification requirements for the A320 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.. *** This information is subject to confidential treatment and has been omitted and filed separately with the Commission. A319/A320 – CSN – 01/04 CC-C 3370036/02

GUARANTEE CONDITIONS. 4.1 4.1. The performance certification requirements for the Aircraft, except where otherwise notedstated, will be as stated in Section 02 of the Standard Specification. 4.2 4.1. For the determination of JAR take-off and landing performance a hard level dry level runway surface with no runway strength limitations, no line-up allowancesallowance, no obstacles, zero wind, atmosphere according to ISA, except as otherwise noted, stated and the use of speed brakesspeedbrakes, flaps, landing gear and engines in the conditions liable to provide the best results will be assumed. 4.2.1 4.1.1. When establishing take-off and second segment performance no air will be bled from the engines for cabin air conditioning or anti-icing. 4.1.2. When establishing en-route one engine inoperative climb performance the air conditioning bleed shall be on but no air will be bled from the engines for anti-icing.

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. 4.1 The performance certification requirements for the A319 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. 4.1 The performance certification requirements for the A320 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. 4.1 5.1. The performance certification requirements for the Aircraft, except where otherwise noted, will be as stated in Section 02 of the Standard Specification. 4.2 5.2. For the determination of JAR take-off and landing performance a hard level 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, noted and the use of speed brakesspeedbrakes, flaps, landing gear and engines in the conditions liable to provide the best results will shall be assumed.. For take-off performance no special procedures and no line-up-allowance have been considered if not otherwise specified. LETTER AGREEMENT NO 6A 4.2.1 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. 4.1 7.1.1 The performance certification requirements for the Aircraft, except where otherwise noted, will shall be as stated in Section 02 of the Standard Specification. 4.2 7.1.2 For the determination of JAR JAR/FAR take-off and landing performance a hard level dry level runway surface with no runway strength limitationslimitation, no line-up allowances, no obstaclesobstacle, zero wind, atmosphere according to ISA, except as otherwise notedstated, and the use of speed brakesspeedbrakes, flaps, associated speeds, landing gear and engines in the conditions liable to provide the best results will shall be assumed. 4.2.1 7.1.3 When establishing take-off and second segment performance no air will shall be bled from the engines for cabin air conditioning or anti-icing, unless otherwise noted.

GUARANTEE CONDITIONS. 4.1 4.1. The performance certification requirements for the Aircraft, except where otherwise notedstated, will be as stated in Section 02 of the Standard Specification. 4.2 4.2. For the determination of JAR take-off and landing performance a hard level 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, stated and the use of speed brakesspeedbrakes, flaps, landing gear and engines in the conditions liable to provide the best results will be assumed. 4.2.1 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. 4.1 8.1.1 The performance certification requirements for the Aircraft, except where otherwise noted, will shall be as stated in Section 02 of the Standard Specification. 4.2 8.1.2 For the determination of JAR JAR/FAR take-off and landing performance a hard level dry level runway surface with no runway strength limitationslimitation, no line-up allowances, no obstaclesobstacle, zero wind, atmosphere according to ISA, except as otherwise notedstated, and the use of speed brakesspeedbrakes, flaps, associated speeds, landing gear and engines in the conditions liable to provide the best results will shall be assumed. 4.2.1 8.1.3 When establishing take-off and second segment performance no air will shall be bled from the engines for cabin air conditioning or anti-icing, unless otherwise noted.