What it approves
Installation of the Mark II performance system, including recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1085 dated November 16, 2010, or later FAA approved revision. 350 Knot Vmo authorized if equipped in accordance with Avcon Master Drawing No. 1085 dated November 16, 2010, or later FAA approved revision. An FAA approved Airplane Flight Manual Supplement is required for each model.
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.
This certificate issued to: AVCON Industries, Inc 714 N. Oliver Road Newton, KS 67114-9444
Part 25 of the Federal Aviation Regulations.
Original Product - Type Certificate Number: A10CE Make: Learjet, Inc Model: 24B, 24B-A, 24D, 24D-A, 24E, 24F, and 24F-A
Description of Type Design Change: Installation of the Mark II performance system, including recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1085 dated November 16, 2010, or later FAA approved revision. 350 Knot Vmo authorized if equipped in accordance with Avcon Master Drawing No. 1085 dated November 16, 2010, or later FAA approved revision. An FAA approved Airplane Flight Manual Supplement is required for each model.
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 a product, the holder must give the other person written evidence of that permission. A copy of this Certificate and Addendum No. SA841NW shall be maintained as part of the permanent records for the modified aircraft.
Date of application: July 15, 1979
Date of issuance: October 23, 1979
Date reissued: April 13, 2000; June 03, 2010;
November 16, 2010
Date amended: May 14, 2001
Original signed by Grant E. Youngdahl
( Signature) Grant E. Youngdahl Program Manager Wichita Airplane Certification Office
(Title)
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SA841NW Date of Issuance: October 23, 1979 Date Amended: May 14, 2001 Date Reissued: November 16, 2010
SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA841NW
The limitations noted in Type Certificate Data Sheet No. A10CE are applicable except as follows:
Section III
Airspeed Limits (CAS)
V mc (Minimum Control Speed) Air 97 Knots
V fe (Flaps Extended) Landing 150 Knots Flaps 20° 200 Knots Flaps 10° 250 Knots
V mo (Maximum Operating) 300 Knots
V mo (If equipped with Dwg. List 36) 300 Knots from Sea Level to 14,000 ft.
350 Knots 14,000 ft. to 23,900 ft.
Stabilizer Travel Limits
24B, 24B-A, 24D, 24D-A (If equipped with ECR 1514 or 1510 or 24E, 24F, 24F-A) Upper Limit –0 052’ to –108’ Lower Limit –8 030’ to –900’
--END--
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 7
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| November 16, 2010 | Reissued, current | Certificate |
| September 8, 2005 | Reissued, earlier issue | Certificate |