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ncea TITLE Raytheon Dressings RAS-67-9917 Rev IR Dated 11/05/99 Sundstrand Mk-VI Ground PrOXfftlity Warning Sys Note: This approval is for the Electrical aspects of the engineering design data only, and is not instaltabon approval. Approval tor aircraft S/Isi RK-244 only. Approval for GPWS is for on

3 (a) appendix F part 1(a) (1) (II) and FAR 25.85) (c) appendix F part II amendment 25-83. The flreblocking was accomplished in accordance with the Skandia, Inc. test plan #5880 Rev. new dated 04-13-00, , reference the form 8110-3 dated 04-13-00 approved by Judy Boggs, D.E.R. #DERY-405020-CE, structural speci

FAA approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systeme, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. Al 6SW Approvals are provided separately. 1. This approval 2. This approv

ne. PrOplber. etc) Airplane 5.NAME OF APPLICANT Constant Aviation-CLM LIST OF DATA 6,IDENTIFICATION 2.TITLE TP 22681 Rev A Dated 05/02/2013 Skandia, Inc. Flammability Oil Burner Testing and Vertical Notes: 1) Work accomplished under 2) Flammability test witnessing materials. Test Report Burner T

TION TITLE " Raytheon Drawings RAS-67.9917 Rev IR Dated 11/05/99 Sundstrand Mk-VI Ground Pro>amrty Warning Sys Note: This approval is for the Electrical aspects of the engineering design data only, and is not installation approval. Approval for aircraft SIN RK-244 only. Approval for GPWS is for onl

0-CE, for the flammability (1) (II) and FAR 25.85) (c) appendix F part II amendment 25-83. The fireblocking was accomplished in accordance with the Skandia, Inc. test plan #5880 Rev. new dated 04-13-00, , reference the form 8110-3 dated 04-13-00 approved by D.E.R. #DERY-405020-CE, structural special. Referenc