What it approves
The installation of an internal cargo pod lighting 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.
Part 23 of the Federal Aviation Regulations.
Description of Type Design Change: The installation of an internal cargo pod lighting system in accordance with document number DL1819M02, Data List – Installation Data, Cessna C-208 Series, Revision B dated November 7, 2012, or later FAA approved revision. Instructions for Continued Airworthiness (ICA) document number 02010000-ICA, Revision A dated May 8, 2012 or later FAA accepted revision must be available to the operator at the time of installation. Complete compliance data is contained in DL1819M00, Data List – Compliance Data, Cessna C-208 Series, Revision B dated November 7, 2012, or later FAA approved revision.
Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. 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.
Aircraft Structures International Corp.
Hangar 31 Enid Woodring Regional Airport, RR5, Box 41B Enid, OK 73701 A37CE Make : Cessna Model : 208 and 208B Date of application: December 14, 2011
Date of issuance: July 2, 2012
Date reissued: November 26, 2012
( Signature) C. Neil Hocker Lead ODA Administrator ODA-831473-SW
( Title)
Transfer the ownership of Supplemental Type Certificate Number
to (Name of transferee)
(Address of transferee) (Number and street)
(City, State, and ZIP code)
from (Name of grantor)(Print or type)
(Address of grantor) (Number and street)
(City, State, and ZIP code)
Signature of grantor (In ink):
United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Continuation Sheet
New 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 Cessna 208 and 208B airplanes modified by installation of an internal cargo pod lighting system is as follows:
a. The type certification basis for Cessna 208 and 208B airplanes is shown on TCDS A37CE for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of applications, December 14, 2011, is based upon part 23 as amended by Amendment 23-28:
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 this modification were determined to be:
Regulations at the latest amendment 23-0 through 23-62
23.23(b), 23.25, 23.307(a), 23.601, 23.605(a), 23.609(a), 23.619, 23.623, 23.625, 23.627,
23.1301(a)(b)(c)(d), 23.1359(a)(c), 23.1529.
Regulations at an intermediate amendment None
Regulations at the amendment level in TCDS A37CE
23.1, 23.301(a), 23.303, 23.305, 23.321, 23.341(a), 23.561(a)(b)(e), 23.603, 23.607, 23.611,
23.613(a)(b), 23.615(a), 23.621, 23.863(a)(b)(3), 23.867(b)(1), 23.1309(a)(c), 23.1351(a)(2),
23.1357(a)(c), 23.1365(a)(b), 23.1431.
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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 · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| November 26, 2012 | Reissued, current | Certificate |
| July 2, 2012 | Issued, earlier issue | Certificate |