# N783SA: 2009 Learjet 60

- Status: Valid registration
- Airframe: [Learjet 60](https://openairdocs.org/model/learjet-60) (registry code 5170707, 11 seats)
- Engine: [Pratt & Whitney Canada PW305A](https://openairdocs.org/engine/pratt-whitney-canada-pw305a) (registry code 52190)
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE) (Learjet Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 368
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 12, 2025
- Certificate issued: October 1, 2025
- Expires: October 31, 2032
- Mode S code: AA9D3C
- Registered owner: [Sssi Inc](https://openairdocs.org/faa-owner/SSSI%20INC)
- Location: [Canonsburg, PA](https://openairdocs.org/faa-place/PA/Canonsburg)
- Owner type: Corporation
- Owner's area on the map: 40.2763° N, 80.1717° W: Placed by OpenAirDocs at the center of ZIP code 15317, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=783SA
- Page: https://openairdocs.org/aircraft/N783SA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 23 in force

### Matched by airframe (Learjet 60)

- [AD 2022-05-01](https://openairdocs.org/ad/2022-05-01): Spoilers · Learjet 35, 35A (C-21A), 36 and 5 more. Effective Mar 9, 2022
- [AD 2020-11-04](https://openairdocs.org/ad/2020-11-04): Engine Exhaust · Learjet 60. Effective Jun 25, 2020
- [AD 2019-17-01](https://openairdocs.org/ad/2019-17-01): Fuselage · Learjet 60. Effective Oct 2, 2019
- [AD 2018-19-04](https://openairdocs.org/ad/2018-19-04): TE Flap Control System · Learjet 28, 29, 31 and 9 more. Effective Oct 23, 2018
- [AD 2013-24-04](https://openairdocs.org/ad/2013-24-04): Fuel · Learjet 60. Effective Mar 14, 2014
- [AD 2013-13-09](https://openairdocs.org/ad/2013-13-09): Landing gear, Wings, Engine exhaust · Learjet 60. Effective Aug 6, 2013
- [AD 2012-08-16](https://openairdocs.org/ad/2012-08-16): Extinguishing system · Learjet 60. Effective May 29, 2012
- [AD 2010-11-11](https://openairdocs.org/ad/2010-11-11): Landing gear · Learjet 60. Effective Jul 13, 2010
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2001-12-02](https://openairdocs.org/ad/2001-12-02): Brake Valve · Learjet 55, 55B, 55C and 1 more. Effective Jul 18, 2001
- [AD 2000-23-18](https://openairdocs.org/ad/2000-23-18): Oxygen Tubing · Learjet 60. Effective Dec 26, 2000
- [AD 99-23-19](https://openairdocs.org/ad/99-23-19): Spoiler Actuator · Learjet 31, 31A, 35 and 2 more. Effective Dec 21, 1999
- [AD 99-16-03](https://openairdocs.org/ad/99-16-03): Horizontal Stabilizer Anti-Ice System · Learjet 23, 24, 24A and 22 more. Effective Sep 7, 1999
- [AD 98-16-18](https://openairdocs.org/ad/98-16-18): Brake Wear Dimension · Learjet 60. Effective Aug 24, 1998
- [AD 96-18-01](https://openairdocs.org/ad/96-18-01): Aft Core Cowl Nozzle of Engine Nacelles · Learjet 60. Effective Oct 2, 1996
- [AD 95-21-03](https://openairdocs.org/ad/95-21-03): Engine Fire Pull Switch Assembly · Learjet 31A and 60. Effective Oct 26, 1995
- [AD 94-01-06](https://openairdocs.org/ad/94-01-06): Traffic Alert and Collision Avoidance System II Processors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 176 more. Effective Feb 4, 1994
- [AD 93-23-12](https://openairdocs.org/ad/93-23-12): Heating Systems · Learjet 60. Effective Dec 15, 1993

### Matched by engine (Pratt & Whitney Canada PW305A)

- [AD 2010-24-05](https://openairdocs.org/ad/2010-24-05): Failure of the impeller · Pratt & Whitney Canada PW305A and PW305B. Effective Jan 3, 2011
- [AD 2009-14-12](https://openairdocs.org/ad/2009-14-12): High Pressure Compressor (HPC) · Pratt & Whitney Canada PW305A and PW305B. Effective Aug 13, 2009
- [AD 2008-13-16](https://openairdocs.org/ad/2008-13-16): Fan blade · Pratt & Whitney Canada PW305A and PW305B. Effective Jul 10, 2008
- [AD 2001-04-10](https://openairdocs.org/ad/2001-04-10): Low Pressure Turbine (LPT) Disks · Pratt & Whitney Canada PW305 and PW305A. Effective Apr 6, 2001

### Historical (superseded or no longer in force)

- [AD 2017-11-09](https://openairdocs.org/ad/2017-11-09) (historical): Fuselage · Learjet 60. Effective May 30, 2017
- [AD 2017-08-07](https://openairdocs.org/ad/2017-08-07) (historical): Fuselage · Learjet 60. Effective May 22, 2017
- [AD 2003-19-11](https://openairdocs.org/ad/2003-19-11) (historical): Fuel crossflow tube · Learjet 60. Effective Nov 3, 2003
- [AD 95-14-09](https://openairdocs.org/ad/95-14-09) (historical): Fuel Crossflow Tube · Learjet 60. Effective Aug 3, 1995

## Information bulletins (advisory) (3 in force)

- [SAIB 2026-07](https://openairdocs.org/saib/2026-07): MAIN LANDING GEAR ATTACH SECTION, Trunnion Pins. Issued Mar 19, 2026
- [SAIB NM-12-25](https://openairdocs.org/saib/NM-12-25): Auto Flight: Altitude Controller. Issued Apr 16, 2012
- [SAIB 2024-04](https://openairdocs.org/saib/2024-04): Electronic Engine Control Units. Issued Oct 29, 2024

## NTSB investigations

None matched to N783SA.

## FAA accident and incident reports

None matched to N783SA.

## Reports on N783SA not matched to an aircraft (1)

They name N783SA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20120911025929I](https://openairdocs.org/incident/20120911025929I), Sep 11, 2012: Boeing 747-281F (N783SA), Anchorage, AK, Minor damage. At approximately 0115 local, a southern air B-747-200 aircraft, enroute from miami to Anchorage declared an emergency due to complete loss of electrical power.…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N783SA not matched to an aircraft (24)

They name N783SA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR Q2SA20120930197](https://openairdocs.org/sdr/Q2SA20120930197), Sep 30, 2012: BATTERY PACK. DISCHARGED. EMERGENCY FLOOR LIGHTING IN UPPER DECK INOP. REMOVED AND REPLACED BATTERY PACK CARTRIDGE IAW 3-51-04. SYS OPS CHECK NORMAL.
- [SDR Q2SA201209301](https://openairdocs.org/sdr/Q2SA201209301), Sep 30, 2012: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHT IN THE COCKPIT INTERMITTENT. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY IAW 33-51-07. SYSTEM OPS CHECK NORMAL.
- [SDR Q2SA2012091178305](https://openairdocs.org/sdr/Q2SA2012091178305), Sep 11, 2012: GENERATOR. FAILED. WHILE EN ROUTE FROM MIA TO ANC EXPERIENCED A NR 1 AND NR 3 GENERATOR FAILURE. THEREAFTER DISPATCH WAS NOTIFIED BY THE CREW, THE AIRCRAFT HAD LOST A THIRD GENERA
- [SDR TX9Y20111121010](https://openairdocs.org/sdr/TX9Y20111121010), Nov 18, 2011: ACCESS PANEL. DAMAGED. MAIN DECK MEC BAY ACCESS PANEL ASSY (P/N:65B11970-35) LOWER SURFACE WAS FOUND DENTS AND PUNCTURE HOLE, AND AT THE ACCESS PANEL (P/N:65B16167-14) CORNERS WAS FOU
- [SDR TX9Y20111116009](https://openairdocs.org/sdr/TX9Y20111116009), Nov 14, 2011: TENSION TIE. CRACKED. UPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS FOUND CRACK. UPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS REPAIRED PER SRM 51-40-03 FIG 2 REV 120
- [SDR TX9Y20111115008](https://openairdocs.org/sdr/TX9Y20111115008), Nov 14, 2011: TENSION TIE. CRACKED. UPPER DECK STA 800 LT & RT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 840 LT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 860 RT T
- [SDR TX9Y20111114007](https://openairdocs.org/sdr/TX9Y20111114007), Nov 11, 2011: STRUCTURE. DAMAGED. ONE ELONGATED HOLE WAS FOUND COMMON TO RT INBOARD FIXED TRAILING EDGE BEAM UPPER CHORD (P/N:65B11614) AT APPROX WBL 235.20. THE REPAIR WAS CARRIED OUT PER BOEIN
- [SDR TX9Y20111111006](https://openairdocs.org/sdr/TX9Y20111111006), Nov 8, 2011: DOUBLER. CORRODED. WATER SERVICE PORT EXTERIOR DOUBLER WAS FOUND CORROSION (BS 980-BS 1000, STR 44R-STR 46R). THE CORROSION WAS REMOVED AS PER SRM 51-10-01 REV 120. THE CORROSION 
- [SDR TX9Y20111111005](https://openairdocs.org/sdr/TX9Y20111111005), Nov 8, 2011: SHEAR TIE. CRACKED. WING CENTER SECTION FRONT SPAR LOCATION RBBL 33.89 SHEAR TIE (P/N:69B14267-9) WAS FOUND CRACK. A NEW SHEAR TIE WAS FABRICATED AS PER DRAWING 69B14267-9. THE REW
- [SDR TX9Y20111111004](https://openairdocs.org/sdr/TX9Y20111111004), Nov 8, 2011: PANEL. DAMAGED. ONE ELONGATED HOLE WAS FOUND COMMON TO DOOR PANEL (P/N:65B90719-86) OF NR 1 PYLON INBOARD TRAILING EDGE FAIRING DOOR ASSY (P/N:65B90717) AT APPROX STA 297.5. TH
- [SDR TX9Y20111108003](https://openairdocs.org/sdr/TX9Y20111108003), Nov 5, 2011: FLAP TRACK. CORRODED. FLAP TRACK NR 4 FORWARD END CLEVIS INBOARD LUG SURFACE FOUND CORROSION INDICATION ON INBOARD LUG INBOARD SURFACE. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NU
- [SDR TX9Y20111104002](https://openairdocs.org/sdr/TX9Y20111104002), Nov 1, 2011: STRUCTURE. CRACKED. CRACK INDICATIONS FOUND ON NR 2 PYLON STRUT STRUCTURE. REPAIRED PER MN TEC-SOF-11-0088, SRM 51-10-01 AND SRM 51-40-02.
- [SDR TX9Y20111104001](https://openairdocs.org/sdr/TX9Y20111104001), Nov 1, 2011: SPLICE PLATE. CRACKED. A FASTENER HOLE WAS FOUND CRACKED AT HORIZONTAL STABILIZER CENTER SECTION LT SIDE LOWER SPLICE PLATE. REPLACED PER MN TEC-SOF-11-0082 AND SRM 51-30-05.
- [SDR Q2SA783004](https://openairdocs.org/sdr/Q2SA783004), Sep 2, 2011: DUCT. CRACKED. NR 3 ENG FIRE WARNING LIGHT ILLUM WHILE ADVANCING POWER TO 88% RPM. BOTH NR 3 ENG NACELLE IND WERE AT 10 UNITS. EGT WAS RISING THRU 800 DEG CELCIUS WHILE OTHER 
- [SDR VGQY2010041300005](https://openairdocs.org/sdr/VGQY2010041300005), Apr 13, 2010: SKIN. DAMAGED. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.
- [SDR VGQY2010041400006](https://openairdocs.org/sdr/VGQY2010041400006), Apr 13, 2010: SKIN. DAMAGED. REQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 520 - 540 STR 38R - 42R IAW SRM 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 
- [SDR VGQY2010041400005](https://openairdocs.org/sdr/VGQY2010041400005), Apr 13, 2010: SKIN. DAMAGED. REQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 670-700 S37-42R IAW REP 783-024 PAGE 1 OF 4. REF: RAP 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN
- [SDR VGQY2010041400004](https://openairdocs.org/sdr/VGQY2010041400004), Apr 13, 2010: MOUNT. CORRODED. NR 4 ENG PYLON, LOWER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT LOWER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.
- [SDR VGQY2010041400003](https://openairdocs.org/sdr/VGQY2010041400003), Apr 13, 2010: MOUNT. CORRODED. NR 4 ENG PYLON, UPPER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT UPPER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.
- [SDR VGQY2010041300002](https://openairdocs.org/sdr/VGQY2010041300002), Apr 13, 2010: STRUCTURE. CORRODED. STA 1920 FRAME BULB TEE 65B04333-89 VERTICAL FLANGE IS FOUND CRACKED AND CHIPPED OFF AT RBL 6.30. COMPLIED WITH EN 1044-10, REPAIR FOR CRACKED 65B0433-89 BULB T
- [SDR VGQY2010041300001](https://openairdocs.org/sdr/VGQY2010041300001), Apr 12, 2010: STIFFENER. CORRODED. RIGHT HORIZONTAL STABILIZER REAR SPAR AT ELEVATOR STATION 206.8 STIFFENER LOWER END FOUND CORRODED. COMPLIED WITH EN 1048-10, ALTERNATIVE FABRICATION FOR HORIZO
- [SDR Q2SA783003](https://openairdocs.org/sdr/Q2SA783003), Oct 31, 2009: HYDRAULIC LINE. RUPTURED. AFTER TAKING OFF FROM KDOV, NR 1 HYDRAULIC SYSTEM QUANTITY DECREASED RAPIDLY, CREW RAN ABNORMAL CHECKLIST IN ACCORDANCE WITH B-747-200/300 QUICK REFERENCE HANDB
- [SDR Q2SA783002](https://openairdocs.org/sdr/Q2SA783002), Dec 15, 2008: PITOT LINE. BROKEN. ON DEPARTURE FROM KJFK, CAPTAIN'S POSITION LOST ALL PRIMARY INSTRUMENTS (AIRSPEED, ALTITUDE, IVSI INDICATORS). AIR TURN BACK TO KFJK, NO FUEL DUMP PERFORMED. CA
- [SDR Q2SA783001](https://openairdocs.org/sdr/Q2SA783001), Aug 14, 2008: SLIDE. UNWANTED DEPLOY. DURING MAINTENANCE ACTIVITY IN SBKP, ACFT DOOR OPENED WITH FLOOR MOUNTED ESCAPE SLIDE HANDLE IN "AUTO", WHICH INADVERTENTLY ACTIVATED RT SIDE UPPER DECK SLIDE. 

## STCs that may be installed (OpenAirDocs) (157, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Learjet 60)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST01984WI](https://openairdocs.org/stc/ST01984WI): Installation of Stores Carriage Provisions and Underwing Stores. Avcon Industries Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST04614CH](https://openairdocs.org/stc/ST04614CH): Installation of a SmartSky LITE System. Apcela IFC JV, LLC dba Apcela ATG
- [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12087CH](https://openairdocs.org/stc/ST12087CH): Installation replacement Cabin/Cockpit Handheld Fire Extinguishers. Avcon Industries Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST04743NY](https://openairdocs.org/stc/ST04743NY): Installation of ATI Oil Safety Cap. ATI Jet Inc
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST01138DE](https://openairdocs.org/stc/ST01138DE): Installation of MidContinent MD23 standby altimeter and/or attitude indicators. Butler National Corporation
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST02209AT-D](https://openairdocs.org/stc/ST02209AT-D): Installation of Composite Stang Fairings. Summit Aviation Inc
- [STC ST03996AT](https://openairdocs.org/stc/ST03996AT): Installation of a GDC64Tablet Aircraft Interface Unit (TAIU) in the Learjet Model 60 airplane. Summit Aviation Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST01742WI](https://openairdocs.org/stc/ST01742WI): Satcom Direct Router (SDR) Installation and Activation of WI-FI and Transmitting Portable Electronic Devices (T-PED), including Aircraft Tolerance Testing. Delta Engineering Corporation
- [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25. BHE & Associates Ltd
- [STC ST04208NY](https://openairdocs.org/stc/ST04208NY): Installation of LAI Windowshields. Lee Aerospace Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST02455SE](https://openairdocs.org/stc/ST02455SE): Installation of Dual GTX-3000 Transponders, GDL-88 Automatic Dependent Surveillance-Broadcast (ADS-B) (In) with Wide Area Augmentation System (WAAS) Global Positioning System (GPS) sensor and Flight Stream 210 Bluetooth Connectivity installed for ADS-B (Out) compliance. Butler National Corporation
- [STC ST01905LA](https://openairdocs.org/stc/ST01905LA): Installation of a Patient Loading and Utility System. LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA4999NM](https://openairdocs.org/stc/SA4999NM): Installation of lifeport patient loading and support system. LifePort LLC
- [STC SA01213CH](https://openairdocs.org/stc/SA01213CH): Install air ambulance conversion in accordance with Spectrum Aeromed Inc. Drawings as listed on AML SA01213CH, or later FAA approved revision. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC
- [STC ST00820DE](https://openairdocs.org/stc/ST00820DE): Installation of a Datalink Communications System supporting Air Traffic Services (ATS) using a Universal Unilink UL-801 Communications Management Unit (CMU). West Star Aviation LLC
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01794WI](https://openairdocs.org/stc/ST01794WI): Modification of Rockwell Collins TCAS II System Installation. Rockwell Collins Inc
- [STC ST02500SE](https://openairdocs.org/stc/ST02500SE): The installation of the Garmin GDL-88 with the Flight Stream 210 to allow ADS-B(In) Flight Information Service Broadcast (FIS-B), independent of the ADS-B(Out) solution compliance. Butler National Corporation
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC ST01795WI](https://openairdocs.org/stc/ST01795WI): Installation of an ADS-B Out TDR-94D Transponder. Learjet Inc
- [STC SA8105NM-D](https://openairdocs.org/stc/SA8105NM-D): Installation of dual universal UNS-1C flight management system. Learjet Inc
- [STC SA8106NM-D](https://openairdocs.org/stc/SA8106NM-D): Installation of Universal Avionics UL-600/UL-601 Unilink System. Learjet Inc
- [STC ST01596LA-D](https://openairdocs.org/stc/ST01596LA-D): Software Upgrade to the Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS) for the Runway Awareness and Advisory System (RAAS). Learjet Inc
- [STC ST02022LA-D](https://openairdocs.org/stc/ST02022LA-D): Installation of an AirCell Axxess II Satcom System. Learjet Inc
- [STC ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc
- [STC ST04233AT](https://openairdocs.org/stc/ST04233AT): Replacement of the inner aluminum barrel of the engine inlet cowl, with an inlet barrel of carbon graphite sandwich construction, to provide a solution for in-service corrosion. Quiet Technology Aerospace
- [STC ST01791WI](https://openairdocs.org/stc/ST01791WI): Installation of a Collins AHC-3000A Series Attitude Heading Computer. Butler Avionics, Inc

All 157: https://openairdocs.org/aircraft/N783SA/stcs.md

## Earlier aircraft with N783SA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N783SA before.

- [Cancelled 2004-03-12](https://openairdocs.org/deregistered/N783SA-2004-03-12): Cessna 172S, S/N 172S8601, built 2000. Exported to Denmark. Owner: [Suburban Aviation Inc](https://openairdocs.org/faa-owner/SUBURBAN%20AVIATION%20INC), [Ottawa Lake, MI](https://openairdocs.org/faa-place/MI/Ottawa%20Lake)

## Related

- Other Learjet 60 aircraft: https://openairdocs.org/model/learjet-60/aircraft.md
- The Pratt & Whitney Canada PW305A engine: https://openairdocs.org/engine/pratt-whitney-canada-pw305a.md

---
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