# STC SA3-506

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sabreliner Aviation LLC, United States
- Description: Installation of weather radar antenna mount and radar nose.
- Applied: May 13, 1960
- Status date: March 7, 2014
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-793](https://openairdocs.org/tcds/A-793)
- Certificate PDF: https://openairdocs.org/files/sha256/da/44/da44e895d5cbf203994514538f43894af1dc1a3b230e3198afc41fd50b44f858
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B80F138C7788C4E586257E65006EA94F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3-506

## ADs that name it (0)

None.

## Approved models (1)

- Kelowna Flightcraft R & D Ltd. 240 Series ([TCDS A-793](https://openairdocs.org/tcds/A-793))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA3-506 Sabreliner Aviation, LLC.

1390 Highway H Perryville, MO 63775 4b 3 Civil Air Regulations A-793 240 Installation of Weather Radar Antenna Mount and Radar Nose. Data Required: Remmert-Werner Drawing No's.

SK-10331 and SK-10113, or later FAA approved revision.

General Dynamics (Convair) October 1, 1970; March 25, 1981; June 30, 1983;

March 7, 2014 9/9/60; 10/27/60; 4/19/61; 7/19/61; 9/14/62;

9/8/66 May 13, 1960 May 13, 1960 Grant E. Youngdahl Program Manager Wichita Aircraft Certification Office

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SA3-506

FAA Form 8110-2 (5/14) Page 3 of

3 Limitations and Conditions: (continued from page 1)

Placard forward baggage compartments either per Strato Engineering Co., Drawing ACE-9101 (for Model 240-5 only) or essentially as follows:

"Upper, 500 lb. maximum; Lower, 1100 lb. maximum. Total on both upper and lower, 1100 lb. maximum."

Optionally, cabin interior may be altered per STC SA3-500, SA3-580, SA3-582, SA3-583, SA3-645, or SA3-735.

Except as indicated above, this approval should not be extended to other specific aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

-------------------- END -------------------- SA3-506

## Every issue (1)

- March 7, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/da/44/da44e895d5cbf203994514538f43894af1dc1a3b230e3198afc41fd50b44f858)

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