What it approves
Incorporation of AeroAcoustics Payload Extender III System, manufactured
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.
Number SA01239SE
This certificate, issued to: AeroAcoustics Aircraft Systems, Inc.
9802 29th Avenue West, Hangar B-104 Everett, WA 98204
Part 23 of the Federal Aviation Regulations.
Original Product⎯Type Certificate Number: A37CE Make: Cessna Model: 208
Description of the Type Design Change: Incorporation of AeroAcoustics Payload Extender III System, manufactured in accordance with AeroAcoustics Document AA1680, Revision C, dated January 15, 2010, and installed and maintained in accordance with AeroAcoustics Document AA1679, Revision D, dated December 20, 2009, or later FAA-approved revisions to either of these documents.
Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.
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 relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. (See Continuation Sheet on Page 3)
A copy of this certificate and FAA-Approved Flight Manual Supplement (AFMS) AFMS-C208-25 (aircraft with PT6A-114 engine installed), or AFMS-C208-26 (aircraft with PT6A-114A engine installed), both dated March 26, 2010 or later FAA FMS, listed on Page 3 of the Continuation Sheet, must be maintained as part of the permanent records for the modified aircraft.
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.
Date of application: February 06, 2003 Date reissued: Xxxxxxx ##, #### Date of issuance: July 16, 2003 Date amended: April 13, 2010
(Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Original Signed by Ronald F. May
Number SA01239SE
AeroAcoustics Aircraft Systems, Inc.
Issued: July 16, 2003 Amended: April 13, 2010
This continuation sheet, which is part of STC SA01239SE, prescribes the conditions and limitations under which the product for which the STC was issued complies with the Federal Aviation Regulations.
Applicability: This modification is limited to the following landplanes only:
Model: Serial Number :
208 20800001 through 20800060 (Eligible only if modified with Cessna Kit SK-208-12) 208 20800061 and up
Limit Speeds (IAS): Maneuvering Speed at 8362 lbs. 143 Kt IAS
CG Range: Takeoff and Flight +175.68 inches to +184.35 inches at 8362 pounds +162.41 inches to +184.35 inches at 4200 pounds or less Straight line variation between the points given
Maximum Weights: Maximum Ramp Weight 8397 lb Maximum Takeoff Weight 8362 lb Maximum Landing Weight 8362 lb
Load Factor Flaps Up: +3.41, -1.36 Limits (g’s): Flaps Down (all settings) +2.00
Placards: On each side of nose strut fairing near tow limit marking:
“DO NOT JACK OR TOW THIS AIRCRAFT AT GROSS WEIGHTS ABOVE 8035 LB”
- END -
FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES
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 |
|---|---|---|
| Cessna Aircraft Company | 208 | A37CE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 13, 2010 | Reissued, current | Certificate |
| July 16, 2003 | Issued, earlier issue | Certificate |