What it approves
Installation of provisions for side looking radar.
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.
4b of the Civil Air Regulations as annotated in Type Certificate 6A6
Installation of provisions for side looking radar and forward sensor mounting in accordance with FAA Approved ATS Drawing List Document Number 1818, Rev. “R,” dated June 27, 2012 or later FAA approved revision. General Dynamics Advanced Information Systems FAA Approved Airplane Flight Manual Supplement No. STC SA5002NM, dated April 23rd 2012, or later FAA Approved Revision is required as part of this installation.
1) A FAA approved oxygen system must be installed for the occupants of the operator seats.
2) Compatibility of this design change with previously approved modifications must be determined by the installer.
3) A copy of this certificate or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.
4) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
5) Continued on Page 3
General Dynamics, Advanced Information Systems 1200 Joe Hall Drive Ypsilanti, MI 48197 6A6 Make : Kelowna Flightcraft R & D Ltd.
Model : 340/440 Date of application : January 5, 1990
Date of issuance : September 18, 1990 Date reissued : October 12, 2011
Date amended : November 14, 1991, July 2, 2012
Original Signed By:
Karol Mordasiewicz ( Signature) Karol Mordasiewicz Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office
( Title)
FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES
Number
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SA5002NM Date of Issuance: September 18, 1990 Date Amended: July 2, 2012
Limitations and Conditions (Continued)
This approval is limited to aircraft modified in accordance with Supplemental type Certificate No.
SA4-110 and the following:
1. Weight Limitations
Maximum take-off weight 56,600 pounds Maximum landing weight 51,080 pounds Maximum zero fuel weight 45,000 pounds
To obtain gross weight limitation reduce the maximum weight permitted by the altitude and temperature of the airport by 1,556 pounds.
2. Center of Gravity Limits
Inches aft of datum
(378.1) to (398.8) at 56,600 pounds
(376.6) to (389.8) at 53,680 pounds
(371.5) to (389.8) at 45,000 pounds
(365.8) to (389.8) at 39,500 pounds
Straight line variation between points given
3. Flight into known icing conditions is prohibited.
4. Speed Limitations Pressure Altitude – Feet Maximum Operating Speed Vmo/Mmo Knots
CAS IAS Sea Level 270 271 8,000 ft. 270 271 15,000 ft. 238 239 25,000 ft. 193 194 -END-
FAA FORM 8110-2-1(10-69) PAGE 4 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 · 2
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| July 2, 2012 | Amended, current | Certificate |
| October 12, 2011 | Reissued, earlier issue | Certificate |