What it approves
Installation of Dual Rockwell Collins TDR-94D ADS-B Out Transponders with Gables Engineering G7614-() ATC/TCAS Control Panel for Flight ID input
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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.
FAA Form 8110-2 (5/14) Page 1 of 3
Number: ST04462AT
This certificate issued to: LB Aircraft Engineering, Inc.
6355 NW 36th St, Suite 510 Miami, Florida 33166
Part 25 of the Federal Aviation Regulations.
Original Product – Type Certificate Number: A6WE Make: Boeing Model: MD-81/-82/-83/-87/-88 Series
Description of Type Design Change: Installation of Dual Rockwell Collins TDR-94D ADS-B Out Transponders with Gables Engineering G7614-() ATC/TCAS Control Panel for Flight ID input, in accordance with LB Aircraft Engineering Master Data List LB-ADSB.MD80-MDL, Revision D, dated August 21, 2019, or later FAA approved revisions.
This modification installs ADS-B FAIL annunciator lights on each of the pilot and co-pilot instrument panels.
This modification removes and replaces the existing Mode-S ATC Transponders and ATC/TCAS Control Panel.
Limitations and Conditions: "The aircraft must be equipped with Dual Universal Avionics UNS-1()w Flight Management System with WAAS/GNSS sensors to provide High-Integrity GPS position Source to the TDR-94D.
FAA Approved Flight Manual Supplement, LB Aircraft Engineering LB-ADSB.MD80-AFM, Revision IR, dated October 3, 2019, or later FAA approved revisions, is part of this STC.
For maintenance and inspections, apply LB Aircraft Engineering Instructions for Continued Airworthiness LB-ADSB.MD80- ICA, Revision D, dated November 15, 2018, or later FAA approved revisions.”
Date of Application: November 28, 2016 Date Reissued:
Date of Issuance: October 10, 2019 Date Amended:
Signature Title (for) Christina M. Underwood Manager, Atlanta ACO Branch
FAA Form 8110-2 (5/14) Page 2 of 3
Transfer the ownership of Supplemental Type Certificate Number: ST04462AT
To (Name and address of transferee)
From (Name and address of grantor)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04462AT
FAA Form 8110-2 (5/14) Page 3 of 3
Date of Issuance: October 10, 2019 Date Reissued:
Limitations and Conditions (Continued): "This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications, will produce no adverse effect upon the airworthiness of that airplane.
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.”
Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Boeing B737 Series is as follows:
a. The type certification basis for Boeing MD-81/-82/-83/-87/-88 series airplanes is shown on TCDS A6WE for parts not changed or affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, November 28, 2016, is based upon 14 CFR Part 25 as amended by Amendment 25-142. Based on Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment than 25-0 thru 25-142:
§25.23 (a), Orig. §25.301 (a)(b), Amdt. 25-23 §25.303, Amdt. 25-23 §25.305, Amdt. 25-86 §25.307, Amdt. 25-72 §25.561 (c), Amdt. 25-91 §25.601, Orig. §25.603 (b)(c), Amdt. 25-46 §25.611, Amdt. 25-23 §25.771 (a), Amdt. 25-4 §25.773 (a)(2), Amdt. 25-72 §25.853 (a), Amdt. 25-116 §25.863 (a), Amdt. 25-46 §869 (a)(4), Amdt. 25-113 §25.1301, Amdt 25-123 §25.1309 (a)(b)(c)(e), Amdt. 25-123 §25.1322, Amdt. 25-131 §25.1351 (a)(1), Amdt. 25-72 §25.1353 (a)(c), Amdt. 25-123 §25.1363 (b), Orig. §25.1431 (a)(c)(d), Amdt. 25-113 §25.1529, Amdt. 25-54 §25.1541,Orig. §25.1555 (a), Orig.
§25.1581(a)(2)(d), Amdt 25-72 §25.1585 (a)(1)(2), Amdt. 25-105
14 CFR Part 26 regulations: Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections; as of the issuance date of this STC, compliance has been found for the following regulations: 14 CFR §§ 26.11(c) (Amdt 26-0).
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