What it approves
Installation of an headliner hanger and panel system
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Vnitecf States of }1.merica (J)epartment of <Transportation P ec£era[ Jl 1Jiation }la ministration Suppfementa[ 1ype Certifiate :Num6er: ST09878AC 11iis certificate issuecf to: BizJet International Sales& Support, Inc.
315 North Sheridan Road Tulsa, Ok 74115 certifies tnat tne cnange in tne type cfesign for tne fo{{owing procfuct witn tne £imitations ancf concfitions tnerefore as specifiea nereon meets tne airwortniness requirements of Part _25 __ of tne Federal Aviation Regulations.
Original Product - Type Certificate Number: Make: The Boeing Company Model:
Al6WE 737-800 Series Description of Type Design Change:
Installation of a headliner hanger and panel system in accordance with B izJ et data list 1446000001 revision AR dated 6/ 1/ 1 7 or later FM approved revision; Maintained in accordance with BizJet Instructions for Continued Airworthiness (ICA) RI 182S0601 Rev IR dated 9/19/16 or later F Maccepted revision.
The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to usethiscertificateto alter a product, the holder must give the other person written evidence of that permission.
(See continuation Sheet 3 of3) Certification Basis (See continuation Sheet 3 of 3) 11iis certificate ancf tne supporting cfata wnicn is tne 6asis for approva{ sna{{ remain in effect unti{ surrencferecf, suspenaecf, ana revof{ga or a termination aate is otnerwise esta6{isnea 6y tne }1.aministrator of tne Peaera{ }1.viation }I.cf ministration.
Date of Application: 8/26/2015 Date Reissued: l0/0 4/20I 3 Date oflssuance: 8/8/2017 Date Amended:
· FAA Form 8110-2 (5/14) Page 1 of 3
Vnitecf States of }lmerica <Department of <Transportation :
P eaerar JI. 'Viation Jiaministration I Suppfementa[ c_{ype Certifichte I (Continuation Sheet) :Num6er: ST09878AC Limitations and Conditions (Continued):
1. It must be demonstrated by test or combination of test and analysis that all occupants can be evacuated fro in the airplane in a time period not exceeding 45 seconds under the conditions specified in appendix J of part 25 amendment 25-72.
2. Operations involving the caniage of personsor property for compensation or hire are prohibited.
Certification Basis:
All regulations as the amendment levels identified in Type Certificate Data Sheet A16W Except for the following regulations have been complied with at a higher amendment level:
-14 CFR25.305 Amendment 25-86 -14 CFR25.571 Amendment 25-132 -14 CFR25.61 l Amendment 25-123 -14 CFR25.613 Amendment 25-112 -14 CFR25.856 Amendment 25-111 -14 CFR25.899 Amendment 25-123 This STC incorporates compliance to the following regulations by 14 CFR Part 25, Special Federal Aviation Regulations (SF AR) 109:
-14 CFR25.853(c) Amendment 25-72 ---END---
FAA Form 8110-2 (5/14) Page 3 of 3 ------·----------··-----·-----·------------------------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The Boeing Company | 737-800 Series | A16WE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 4, 2018 | Reissued, current | Certificate |
| August 8, 2017 | Issued, earlier issue | Certificate |