STC ST00040SE

Number ST00040SE

This certificate, issued to Rockwell Collins, Inc.

27300 SW Parkway Ave Wilsonville, OR 97070

Part 25 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A16WE Make: Boeing Model: 737-300/-400/-500 Series

Description of the Type Design Change: Installation of the Model 2300 Head-Up Display Guidance System (HGS) in accordance with Flight Dynamics Installation Drawing List 9701-0861*.

* See Approved Model List (AML) No. ST00040SE for latest Federal Aviation Administration (FAA) approved revision levels and dates.

Limitations and Conditions: Approval of this change in type design applies to above model aircraft only. This modification has only been demonstrated to be acceptable for operations associated with Category (CAT) I and II Landing Minima as defined in FAA Advisory Circular (AC) 120-29 and CAT III Landing Minima as defined in FAA AC 120-28C. Acceptable demonstration for operations associated with Fail-Passive Rollout as defined in FAA AC 120-28D has been satisfactorily completed for properly equipped 737-400 aircraft. A copy of this certificate, continuation sheet, and the FAA-approved airplane flight manual supplement (AFMS) (listed on the continuation sheet) must be maintained as part of the permanent records for the modified aircraft. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of application: May 4, 1992 Date reissued: 6/15/04; 9/16/05; 3/7/12 Date of issuance: November 26, 1993 Date amended: 1/17/97; 5/23/97; 1/17/01; 4/16/03;

6/15/04

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

Number ST00040SE

Rockwell Collins, Inc.

Issued: November 26, 1993 Reissued: 6/15/04; 9/16/05; 3/7/12 Amended: 1/17/97; 5/23/97; 1/17/01; 4/16/03; 6/15/04

This installation is limited to Boeing 737-300/-400 series aircraft equipped with Electronic Flight Instrument Systems (EFIS), and Boeing 737-300/-500 series aircraft not equipped with EFIS (non-EFIS). The FAA AFMS, document number 9701-0978*, is applicable for the Boeing 737-300/-400 EFIS series aircraft. The FAA AFMS, document number 9701-0885*, is applicable for the Boeing 737-300/-500 Non-EFIS series aircraft. This installation shall be maintained in accordance with 2300 HGS Maintenance Manual referenced in the Installation Drawing List, 9701-0861*.

* See Approved Model List (AML) No. ST00040SE for latest FAA-approved revision levels and dates.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

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FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES