What it approves
Installation of Teledyne Avionics normalized angle of attack indicating 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.
FAA Form 8110-2(10-68) Page 1 of 2 Number SA1137SW This certificate issued to Aerosonic Corporation 1212 North Hercules Avenue Clearwater, FL 33765
Part 4b/25 of the Civil Air/Federal Aviation Regulations.
Original Product -- Type Certificate Number: A7EU Make: Avions Marcel Dassault
Model: Fan Jet Falcon, Fan Jet Falcon Series C, Series D, Series E Description of Type Design Change:
Installation of Teledyne Avionics Normalized Angle of Attack Indicating System in accordance with the data listed in Teledyne Avionics Drawing List No. D5232, Revision F, dated September 1, 1970, Revision G dated April 5, 1971, Revision H dated November 6, 1972, or Revision J dated September 21, 1976.
1. (a) Teledyne Avionics Airplane Flight Manual Supplement No. 1 for Avions Marcel Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D, FAA Approved September 14, 1970; or Supplement No. 2 for Avions Marcel Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan, Jet Falcon Series D, and Fan Jet Falcon E, FAA Approved November 17, 1972, is required.
(See STC Continuation Sheet Page 2)
Date of application: January 7, 1970
Date of issuance: April 3, 1970 Date reissued: January 7, 1972, November 17, 1972, July 1, 1976, March 8, 1993, August 14, 2007
Date amended: September 14, 1970, May 28, 1971 November 9, 1976By direction of the Administrator
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA1137SW Date of Reissue: August 14, 2007 Date of Amendment: November 9, 1976
Limitations and Conditions: (Continued):
(b) Teledyne Avionics Airplane Flight Manual Supplement for GAMD Falcon FAA Approved April 3, 1970, by Southwest Region is required with this installation of airplanes which are wired in accordance with Teledyne Avionics Drawing No. 112D103 Revision H in lieu of 112D19.
2. A Flight check in accordance with Automated Specialties Report No. SN 244 Revision A dated March 31, 1970 or Revision B dated November 6, 1972, is to be accomplished on each airplane modified by this STC.
3. The Installer must determine whether this design change is compatible with previously approved modifications.
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.
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ADs that name this STC · 0
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