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AIRBUS SPECIFICATION CHANGE NOTICE (SCN) HAINAN AIRLINES COMPANY SCN Number CHH34D5311904S1C Issue 1 Dated 25-Nov-2009 Page 1 of 3 Title: Installation of dual ADF system - ROCKWELL COLLINS 900 Description Remarks / References Responds to RFC CHH34D5311904C Specification changed by this SCN A320-200 Aircraft Standard Specification Reference N° D 000 02000 Issue 07 Revision 00 Temporary Revision 00 dated 01-Mar-2007 This SCN requires prior or concurrent acceptance of the following SCN (s) : Price per aircraft Two ADF Receivers from ROCKWELL COLLINS (SERIES 900), in accordance with ARINC 712, a second loop and sense antenna shall be installed. Effect on weight Manufacturer’s Weight Empty Change : 11.5 Kg Operational Weight Empty Change : 11.5 Kg Allowable Payload Change : -11.5 Kg US DOLLARS: 44,500 (Foryty four thousand five hundred dollars) AT DELIVERY CONDITIONS : 01/2008 This change will be effective on CHH*C fleet AIRCRAFT MSN4412 and subsequent aircraft Provided approval is received by the 8 th December 2009 Buyer approval Seller approval By : By : Timothy BAUSOR Head of Customisation Date : Date : 25 November 2009

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Page 1: CHH34D5311904C_CHH34D5311904S1C_1.pdf

AIRBUS

SPECIFICATION CHANGE NOTICE

(SCN)

HAINAN AIRLINES COMPANY

SCN Number CHH34D5311904S1C Issue 1 Dated 25-Nov-2009 Page 1 of 3

Title: Installation of dual ADF system - ROCKWELL COLLINS 900 Description

Remarks / References Responds to RFC CHH34D5311904C

Specification changed by this SCN

A320-200 Aircraft Standard Specification Reference N° D 000 02000 Issue 07 Revision 00 Temporary Revision 00 dated 01-Mar-2007

This SCN requires prior or concurrent acceptance of the following SCN (s) :

Price per aircraft

Two ADF Receivers from ROCKWELL COLLINS (SERIES 900), in accordance with ARINC 712, a second loop and sense antenna shall be installed.

Effect on weight

Manufacturer’s Weight Empty Change : 11.5 Kg Operational Weight Empty Change : 11.5 Kg Allowable Payload Change : -11.5 Kg

US DOLLARS: 44,500 (Foryty four thousand five hundred dollars)

AT DELIVERY CONDITIONS : 01/2008 This change will be effective on CHH*C fleet AIRCRAFT MSN4412 and subsequent aircraft

Provided approval is received by the 8th December 2009 Buyer approval Seller approval By : By : Timothy BAUSOR Head of Customisation Date : Date : 25 November 2009

Page 2: CHH34D5311904C_CHH34D5311904S1C_1.pdf

AIRBUS

SPECIFICATION CHANGE NOTICE

(SCN)

HAINAN AIRLINES COMPANY

SCN Number CHH34D5311904S1C Issue 1 Dated 25-Nov-2009 Page 2 of 3

Specification repercussion :

After contractual agreement with respect to weight, performance, delivery, etc, the indicated part of the specification wording will read as follows :

34-53.01.00 Two (2) ADF receivers generally in accordance with ARINC 712 shall be installed in the avionics compartment.

34-53.02.00 The ADF receivers shall be tuned automatically by the FMGCs or manually on the MCDUs. 34-53.02.01 In the event of a dual FMS function failure, the ADF receivers may be tuned on the on side

RMP. 34-53.03.00 Two (2) combined loop and sense antennas shall be installed. 34-53.05.00 Test facilities shall be provided through the CFDS to enable the outputs of the ADF

receivers to be checked with the equipment installed. Key to Figure 23.00 shall be modified accordingly.

SFE changes: Qty Description

Part/Spec N°

Vendor Remarks

2 ADF receiver 822-0299-020

ROCKWELL COLLINS ADF 900

2 ADF antenna 615-2630-102

THALES AVIONICS SA

Page 3: CHH34D5311904C_CHH34D5311904S1C_1.pdf

AIRBUS

SPECIFICATION CHANGE NOTICE

(SCN)

HAINAN AIRLINES COMPANY

SCN Number CHH34D5311904S1C Issue 1 Dated 25-Nov-2009 Page 3 of 3

Scope of change (FOR INFORMATION ONLY)

This modification consists of : - installation of two (2) ADF receivers with associated mount in the Avionics Compartment, - installation of a second ADF loop and sense antenna, - installation of an additional circuit breaker and associated wiring, - modification of Display Management Computer (DMC), FMGC, RMP pin programming.