What it approves
Installation of Light Emitting Diode (LED) based Position, Anticollision, Taxi, and Landing Light Systems with Single Mode (visible) or Dual Mode (visible plus infrared) options
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.
the Federal Aviation Regulations.
SA00301BO ATI Engineering Services, LLC 469 Airport Road, Hangar 9 Johnstown, Pennsylvania 15904 Part 23
A37CE Cessna 208, 208B
1. Flight with Night Vision Goggles (NVG) is not approved by this STC. NVG operational approval must be secured by other means. Infrared is prohibited from use in the NAS by AFMS limitation.
2. Operation must be in accordance with ATI Engineering Services Airplane Flight Manual Supplement (AFMS) Document No. FMS-100104, Revision 1, FAA approved on August 13, 2014, or later FAA approved revision.
(Limitations and Conditions continued on page 3 of 3) 01/04/2010 08/26/2019 08/05/2024 09/21/2010 Christina M. Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Installation of Light Emitting Diode (LED) based Position, Anticollision, Taxi, and Landing Light Systems with Single Mode (visible) or Dual Mode (visible plus infrared) options in accordance with ATI Engineering Services Installation/Manufacturing Drawing List, Document number IDL-100104, Revision 6, dated August 11, 2014, or later FAA approved revision.
11/26/2021
SA00301BO 08/05/2024 3
SA00301BO 08/05/2024 Limitations and Conditions continued:
The AFMS must be carried in the aircraft during all flights.
3. Maintenance must be in accordance with Instructions for Continued Airworthiness (ICA), ATI Engineering Services Document No. ICA-100104, Revision 1, dated May 14, 2013, or later FAA accepted revision.
The ICA must be made available to the operator at the time of installation.
4. Compatibility of this design with previously approved modifications must be determined by the installer.
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Cessna 208, 208B Caravan aircraft is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A37CE.
b. The modification certification basis for parts changed or affected by the change since the reference application date, March 06, 2013, is based upon part 23 as amended by Amendment 23-62 as follows:
Regulations at the latest amendment 23-0 through 23-62
23.1, 23.25(a), 23.773(a)(2), 23.777(a)(b), 23.867, 23.1301, 23.1309(a)(2)(c), 23.1351(a)
(1)(2)(i), 23.1357(a)(b)(c), 23.1359(a)(c), 23.1365(a)(b)(d), 23.1367, 23.1381 -23.1397,
23.1401, 23.1501, 23.1525, 23.1529, 23.1581, 23.1583, 23.1585(a)(j) Regulations at an intermediate amendment
23.853(a) at 23-49, 23.1309(a)(1)(2)(b)(c)(1)(d) at 23-49, 23.1431(a)(b) at 23-49 Regulations at the amendment level in TCDS A37CE None ------------------------------------------------------END-------------------------------------------------- 3 3 Add Page
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 5
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 5, 2024 | Reissued, current | Certificate |
| November 26, 2021 | Reissued, earlier issue | Certificate |
| August 26, 2019 | Reissued, earlier issue | Certificate |
| August 13, 2014 | Amended, earlier issue | Certificate |
| September 21, 2010 | Issued, earlier issue | Certificate |