# Socata Group Aerospatiale TB9

- Type: Aircraft model (FAA registry)
- Registry code: 8680752
- Manufacturer (registry): SOCATA GROUP AEROSPATIALE
- Model: TB9
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 7
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A51EU](https://openairdocs.org/tcds/A51EU) (OpenAirDocs)
- Holder: Daher Aerospace
- Registered aircraft: 1
- Page: https://openairdocs.org/model/socata-group-aerospatiale-tb9

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2018-21-06](https://openairdocs.org/ad/2018-21-06): Wings · SOCATA TB 10, TB 200 and TB9. Effective Dec 10, 2018
- [AD 2015-24-03](https://openairdocs.org/ad/2015-24-03): Stabilizers · SOCATA TB 10, TB 20, TB 200 and 2 more. Effective Jan 4, 2016
- [AD 2007-13-18](https://openairdocs.org/ad/2007-13-18): Nose Landing Gear (NLG) mounts · SOCATA TB 10, TB 200 and TB9. Effective Aug 10, 2007
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [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 2003-26-06](https://openairdocs.org/ad/2003-26-06): Safety Belts and Restraint Systems · Anjou Aeronautique Safety Belts and Restraint Systems, AS332C, AS332L and 14 more. Effective Feb 17, 2004
- [AD 2003-04-03](https://openairdocs.org/ad/2003-04-03): Aileron control gimbal joint · SOCATA TB 10, TB 20, TB 200 and 2 more. Effective Apr 7, 2003
- [AD 2001-23-05](https://openairdocs.org/ad/2001-23-05): Front Seats · SOCATA TB 10, TB 20, TB 200 and 2 more. Effective Jan 4, 2002
- [AD 2001-23-04](https://openairdocs.org/ad/2001-23-04): Lower Rudder Hinge Fitting · SOCATA TB 10, TB 20, TB 200 and 2 more. Effective Jan 4, 2002
- [AD 98-04-47](https://openairdocs.org/ad/98-04-47): Main Landing Gear Support Ribs · SOCATA TB 10, TB 200 and TB9. Effective Apr 3, 1998
- [AD 98-04-03](https://openairdocs.org/ad/98-04-03): Bolts and Spacers of the Upper Attachments of the Front Belts · SOCATA TB 10, TB 20, TB 200 and 2 more. Effective Mar 24, 1998
- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 91-15-10](https://openairdocs.org/ad/91-15-10): Horizontal Stabilizer Balance Weight Attachment Nuts · SOCATA TB 10, TB 20, TB 21 and 1 more. Effective Aug 10, 1991
- [AD 90-25-17](https://openairdocs.org/ad/90-25-17): Oil Cooler Inlet · SOCATA TB 10, TB 20, TB 21 and 1 more. Effective Jan 3, 1991
- [AD 90-02-18 R1](https://openairdocs.org/ad/90-02-18-R1): Fuel System · SOCATA TB 10, TB 20, TB 21 and 1 more. Effective Jun 13, 1990

Historical (superseded or no longer in force):

- [AD 98-16-03](https://openairdocs.org/ad/98-16-03) (historical): Wing Front Attachments · SOCATA TB 10 and TB9. Effective Sep 21, 1998

## Information bulletins (advisory) (3)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-04-09](https://openairdocs.org/saib/CE-04-09): . Issued Oct 23, 2003
- [SAIB CE-02-13](https://openairdocs.org/saib/CE-02-13): . Issued Feb 13, 2002

## Registered aircraft (1)

- [N513PC](https://openairdocs.org/aircraft/N513PC): [Baklanov Sergey I](https://openairdocs.org/faa-owner/BAKLANOV%20SERGEY%20I), [Whitestown, IN](https://openairdocs.org/faa-place/IN/Whitestown), S/N 1546

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (37)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2008FA0000544](https://openairdocs.org/sdr/2008FA0000544), Jul 30, 2008: ALTERNATOR. FAILED. ALTERNATOR WILL FAIL ABOVE 2500 RPM, LOW VOLTAGE LIGHT COMES ON AND THE VOLTMETER INDICATES BATTERY VOLTAGE. OPS CHECK DURING GROUND RUNS ARE NORMAL MAX RPM DUR
- [SDR 2006FA0001188](https://openairdocs.org/sdr/2006FA0001188), Dec 2, 2006: RIVET. LOOSE. DURING THE PRE-FLIGHT INSPECTION FOR A LOCAL TRAINING FLIGHT, THE BLIND RIVETS LOCATED HALFWAY UP VERTICAL FIN WERE FOUND TO BE MAKING ALUMINUM OXIDE (DIRT TRAI
- [SDR CA020917005](https://openairdocs.org/sdr/CA020917005), Sep 11, 2002: ROD END. BROKEN. (CAN) ON A SCHEDULED MAINTENANCE INSPECTION THE RT AILERON SWIVEL ROD END WAS FOUND STIFF. ON FURTHER INSPECTION THE BEARING RACE WAS FOUND BROKEN AND SOME OF T
- [SDR 97ZZZX2651](https://openairdocs.org/sdr/97ZZZX2651), May 14, 1997: MOUNT. CORRODED. NOSE GEAR MOUNT TUBE RUSTED FROM INSIDE OUT. SUBMITTER STATED RUSTED AREA 2ND ONE FOUND IN FLEET.
- [SDR 97ZZZX2792](https://openairdocs.org/sdr/97ZZZX2792), May 7, 1997: MOUNT. CORRODED. NOSE GEAR MOUNT CORRODED COMPLETELY THROUGH FROM INSIDE OUT. SMALL CRACK IN PAINT FOUND DURING INSPECTION. TUBE BROKE OFF DURING REMOVAL. CRACKED AREA.
- [SDR 97ZZZX1224](https://openairdocs.org/sdr/97ZZZX1224), Mar 18, 1997: CRANKSHAFT. CRACKED. THIS AIRCRAFT IS USED EXCLUSIVELY FOR FLIGHT TRAINING. ON PRE-FLIGHT, STUDENT AND INSTRUCTOR FOUND OIL ON THE COWLING. UPON INSPECTION, TWO CRACKS WERE FOUND ON
- [SDR AU970165](https://openairdocs.org/sdr/AU970165), Feb 20, 1997: TORQUE LINK. BROKEN. (AUS) LH MAIN LANDING GEAR LOWER TORQUE LINK BROKEN AT INBOARD ATTACHMENT LUG - OUTBOARD LUG CONTAINS A HAIR LINE CRACK - RH MLG TORQUE LINK CONTAINS SOME PITTI
- [SDR AU970107](https://openairdocs.org/sdr/AU970107), Feb 18, 1997: TORQUE LINK. BROKEN. (AUS) RH MAIN LANDING GEAR LOWER TORQUE LINK FAILED AT LOWER ATTACHMENT HOLES
- [SDR 96ZZZX6003](https://openairdocs.org/sdr/96ZZZX6003), Nov 12, 1996: SCISSORS. FAILED. THE LOWER SCISSORS ON THE LEFT MAIN GEAR CRACKED UPON TOUCH-DOWN, AND THE WHEEL TURNED CAUSING THE A/C TO SLIDE TO A STOP. INSPECTION REVEALED THE OUTBOARD SIDE
- [SDR 96ZZZX5110](https://openairdocs.org/sdr/96ZZZX5110), Sep 19, 1996: SUPPORT. CRACKED. DURING ROUTINE 100-HOUR INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE
- [SDR 96ZZZX5109](https://openairdocs.org/sdr/96ZZZX5109), Sep 19, 1996: SUPPORT. CRACKED. DURING ROUTINE 100-HOUR INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE SEVERE
- [SDR 96ZZZX5133](https://openairdocs.org/sdr/96ZZZX5133), Jul 19, 1996: SUPPORT. CRACKED. DURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FROMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE
- [SDR 96ZZZX5132](https://openairdocs.org/sdr/96ZZZX5132), Jul 19, 1996: SUPPORT. CRACKED. DURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE
- [SDR 96ZZZX5108](https://openairdocs.org/sdr/96ZZZX5108), Jul 19, 1996: SUPPORT. CRACKED. DURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE
- [SDR 96ZZZX5107](https://openairdocs.org/sdr/96ZZZX5107), Jul 19, 1996: SUPPORT. CRACKED. DURING ROUTINE 100-HOUR ANNUAL INSPECTION, FOUND BOTH RT AND LT YOKE SUPPORTS CRACKED IN RADIUS OF BEND WHICH FORMS AFT FLANGE OF SUPPORT. THE CRACKS WERE QUITE
- [SDR 96ZZZX1557](https://openairdocs.org/sdr/96ZZZX1557), Feb 21, 1996: TUBE. DETERIORATED. CARBURETOR HEAT TUBE ERODING DUE TO SUPER HEATED AIR FROM MUFFLER SHROUD. TUBE WIRE SUPPORT AND DEBRIS FROM TUBE COULD BE INJECTED DIRECTLY INTO CARB AND ENGINE
- [SDR 96ZZZX819](https://openairdocs.org/sdr/96ZZZX819), Jan 15, 1996: BAFFLE. CRACKED. BAFFLE OIL COOLER IS CRACKING AROUND OIL COOLER MOUNT POINT. SUBMITTER STATED BAFFLE NEEDS TO BE MADE FROM THICKER MATERIAL. THIS PROBLEM IS A COMMON OCCURRENCE
- [SDR 95ZZZX6388](https://openairdocs.org/sdr/95ZZZX6388), Oct 31, 1995: SUPPORT BAFFLE. BROKEN. DURING SCHEDULED MAINTENANCE (100-HOUR INSPECTION), THE OIL COOLER SUPPORT BAFFLE WAS FOUND BROKEN AT 2 OF THE 4 MOUNT POINTS AND SEVERELY CRACKED ON THE OTHER 
- [SDR 95ZZZX6567](https://openairdocs.org/sdr/95ZZZX6567), Oct 30, 1995: BAFFLE ASSY. BROKEN. DURING A 100-HOUR INSPECTION, THE OIL COOLER WAS FOUND SUPPORTED BY ONLY TWO BOLTS. THE OIL COOLER MOUNTING BAFFLE WAS COMPLETELY BROKEN AT TWO OF THE MOUNT HOL
- [SDR 95ZZZX6398](https://openairdocs.org/sdr/95ZZZX6398), Oct 27, 1995: SUPPORT BAFFLE. CRACKED. DURING A 100-HOUR INSPECTION, THE OIL COOLER MOUNT BAFFLE ASSY WAS FOUND SEVERELY CRACKED WITH PIECES MISSING. IF THE OIL COOLER BECOMES COMPLETELY DETACHED, IT
- [SDR 95ZZZX4185](https://openairdocs.org/sdr/95ZZZX4185), Jul 28, 1995: MOTOR. BURNED. INSPECTION OF MOTOR REVEALED INTERNAL WINDINGS FAILED DUE TO OVERHEATING OF MOTOR UNDER NORMAL FLYING CONDITIONS.
- [SDR 95ZZZX4268](https://openairdocs.org/sdr/95ZZZX4268), Jun 27, 1995: GUIDE. BROKEN. DURING CYLINDER REPAIR, A HALF-MOON SHAPED SECTION OF THE EXHAUST VALVE GUIDE THAT MEASURED APPROXIMATELY .3125 INCH X .25 INCH WAS FOUND MISSING FROM THE LOWER
- [SDR 95ZZZX4267](https://openairdocs.org/sdr/95ZZZX4267), Jun 27, 1995: GUIDE. BROKEN. DURING CYLINDER REPAIR, A RECTANGULAR SECTION OF THE EXHAUST VALVE GUIDE THAT MEASURED APPROXIMATELY .3125 INCH X .25 INCH WAS FOUND MISSING FROM THE LOWER PORT
- [SDR 95ZZZX4266](https://openairdocs.org/sdr/95ZZZX4266), Jun 27, 1995: GUIDE. CRACKED. DURING CYLINDER REPAIR, THE EXHAUST VALVE GUIDE WAS FOUND CRACKED AT BOTH THE TOP AND BOTTOM PORTIONS OF THE GUIDE. THE CRACKS WERE NOT CONNECTED.
- [SDR 95ZZZX4264](https://openairdocs.org/sdr/95ZZZX4264), Jun 27, 1995: ROCKER ARM. OBSTRUCTED. WHILE CLEANING THE ROCKER ARM, SOLVENT FLOW THROUGH THE OIL PASSAGE WAS FOUND TO BE RESTRICTED. INSPECTION REVEALED A BROKEN DRILL BIT TIP TO BE THE OBSTRUCTION
- [SDR 95ZZZX1801](https://openairdocs.org/sdr/95ZZZX1801), Mar 30, 1995: GUIDE. PART MISSING. DURING CYLINDER OVERHAUL, EXHAUST VALVE GUIDE FOUND MISSING APPROXIMATELY ONE-HALF OF THE LOWER PORTION OF THE GUIDE. THE WHOLE UPPER PORTION OF THE GUIDE THAT 
- [SDR 95ZZZX1708](https://openairdocs.org/sdr/95ZZZX1708), Mar 10, 1995: GUIDE. PART MISSING. DURING CYLINDER OVERHAUL, FOUND LOWER PORTION OF THE EXHAUST GUIDE WAS MISSING APPROXIMATELY ONE-HALF OF ITS MATERIAL. THE UPPER PORTION OF THE GUIDE THAT PROJE
- [SDR 95ZZZX1707](https://openairdocs.org/sdr/95ZZZX1707), Mar 10, 1995: GUIDE. CRACKED. DURING CYLINDER PRE-OVERHAUL INSPECTION, THE EXHAUST VALVE GUIDE WAS FOUND CRACKED IN THE LOWER PORTION.
- [SDR 95ZZZX1706](https://openairdocs.org/sdr/95ZZZX1706), Mar 10, 1995: GUIDE. CRACKED. DURING CYLINDER OVERHAUL, EXHAUST VALVE GUIDE WAS FOUND CRACKED IN THE LOWER PORTION.
- [SDR 95ZZZX1704](https://openairdocs.org/sdr/95ZZZX1704), Mar 10, 1995: GUIDE. CRACKED. DURING CYLINDER OVERHAUL, THE EXHAUST VALVE GUIDE WAS FOUND CRACKED IN THE LOWER PORTION.
- [SDR 95ZZZX1703](https://openairdocs.org/sdr/95ZZZX1703), Mar 10, 1995: GUIDE. CRACKED. DURING CYLINDER OVERHAUL, THE EXHAUST VALVE GUIDE WAS FOUND CRACKED IN THE LOWER PORTION.
- [SDR 95ZZZX1702](https://openairdocs.org/sdr/95ZZZX1702), Mar 10, 1995: GUIDE. CRACKED. DURING CYLINDER OVERHAUL, THE EXHAUST VALVE GUIDE WAS FOUND CRACKED IN THE LOWER PORTION.
- [SDR 95ZZZX1705](https://openairdocs.org/sdr/95ZZZX1705), Mar 8, 1995: GUIDE. CRACKED. DURING CYLINDER OVERHAUL, THE EXHAUST VALVE GUIDE WAS FOUND CRACKED IN THE LOWER PORTION.
- [SDR 95ZZZX1489](https://openairdocs.org/sdr/95ZZZX1489), Feb 28, 1995: LEVER ARM. RIVET BROKEN. DURING 100-HOUR INSPECTION, FOUND TOP RIVET CONNECTING THE STABILATOR LEVER ARM TO THE CONTROL PYLON BROKEN. LOOKED UP THE PROPER PART NUMBER TO REPLACE THE RIV
- [SDR 95ZZZX1716](https://openairdocs.org/sdr/95ZZZX1716), Feb 23, 1995: TORQUE LINK. CRACKED. UPON 500-HOUR TORQUE LINK INSPECTION WHEREAS TORQUE LINKS ARE TAKEN APART, CLEANED, INSPECTED AND LUBED, THEN ARE REINSTALLED. MECHANIC FOUND LMG LWR TORQUE LIN
- [SDR 95ZZZX1715](https://openairdocs.org/sdr/95ZZZX1715), Feb 23, 1995: TORQUE LINK. SPLIT. UPON 500-HOUR TORQUE LINK INSPECTION WHEREAS TORQUE LINKS ARE TAKEN APART, CLEANED, INSPECTED AND LUBED, THEN ARE REINSTALLED. MECHANIC FOUND LMG LWR TORQUE LIN
- [SDR 95ZZZX772](https://openairdocs.org/sdr/95ZZZX772), Feb 3, 1995: SCISSORS. CORRODED. INSPECTION OF LANDING GEAR FOUND LOWER SCISSORS WITH SEVERE CORROSION NEAR OUTBOARD BOLT HOLE.

## STCs that may be installed (OpenAirDocs) (133, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA1069NE](https://openairdocs.org/stc/SA1069NE): Installation of a Sensenich Model74DM6S8 fixed-pitch-metal propeller. Sensenich Propeller Company
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA00900WI-D](https://openairdocs.org/stc/SA00900WI-D): Installation of Bendix/King KMD 550 Multi-Function Display. Honeywell International Inc
- [STC SA00827WI-D](https://openairdocs.org/stc/SA00827WI-D): Installation of Bendix/King KMD 150 MFD Multi-Function Display. Honeywell International Inc
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04240NY](https://openairdocs.org/stc/SA04240NY): Installation of a new carbon spinner and back plate. Soci t DUC t/a DUC Helices Propellers Aerodrome De Villefranche-Tarare
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC

All 133: https://openairdocs.org/model/socata-group-aerospatiale-tb9/stcs.md

## PMA parts (OpenAirDocs) (254, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164594297520260806152310.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135648787420260806152404.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [066-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122711976720260723131535.0001): Rivet. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [RAP164-02601](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131654092620250829181752.0001): Brake Disc. Rapco Inc · PMA PQ2101CE · Replaces 164-02601 Cleveland · Aug 27, 2025
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166991847220250417183923.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137624527520240221143429.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [12-50009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196569787920231121213747.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50009 · Nov 20, 2023
- [12-50013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194615252420231121213800.0001): Assembly: saf-Tglo® Whiter Background Door Operation Signage. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50013 · Nov 20, 2023
- [SG8995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191492983420231121213645.0001): Flexible Overcarpet for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8995 · Nov 20, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182973973120231121213703.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Nov 20, 2023
- [12-50005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169967232120231121213732.0001): Assembly: saf-Tglo® Door Operation Sign. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50005 · Nov 20, 2023
- [12-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169285028920231121213718.0001): Assembly: saf-Tglo® Exit (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50001 · Nov 20, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168905257020231121213711.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Nov 20, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161564982620231121213654.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Nov 20, 2023
- [10-50011-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144262062820231121213637.0001): SSUL-X11 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50011-XFCCC · Nov 20, 2023
- [12-50007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137281535020231121213739.0001): Assembly: saf-Tglo® Supplemental Signage/Placard. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50007 · Nov 20, 2023
- [12-50011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130866806020231121213753.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50011 · Nov 20, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125261679120231121213620.0001): SSUL-X Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Nov 20, 2023
- [12-50003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107782691520231121213725.0001): Assembly: saf-Tglo® Exit (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50003 · Nov 20, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105060027420231121213612.0001): SSUL-X Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Nov 20, 2023
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100131158420231121213629.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Nov 20, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198071856820230707211349.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [EA-26000-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145218837920230105195548.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023
- [EA-26000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133441553820230105195526.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023
- [8000075](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183489636520221130202545.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Harrison P/N: 8526250 · Oct 21, 2022
- [AA4A2-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137191946020231018194107.0001): Electric Air Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces Airborne Electric Air Pump, 4A2-1 · Oct 7, 2022
- [APS66-10500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189746689120221020170308.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10500 · Aug 10, 2022
- [APS105-00200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144016163520221020170403.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 105-00200 · Aug 10, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124202264520220706160215.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197722606520240229155304.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190080838420240229155314.0001): Final Assembly KCP 100 Control Panel(Landscape). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177030264720240229155258.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158891984620240229155309.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID825500071820210921142609.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID363929608202107021752410.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID928479160520220125131428.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID728963452022012513145201.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID353616507820220125131514.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID344370491520220125131348.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID281101041020220125131405.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196378769202201251313310.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [W-2425-250](https://drs.faa.gov/browse/excelExternalWindow/DF18F8EF34688C51862583D300527F49.0001): SOCATA TB Windshield (.250 Clear). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB21 22000137 · Oct 11, 2018
- [SC-W/T-2425](https://drs.faa.gov/browse/excelExternalWindow/6F89E8EAE4194C02862583D300527F13.0001): SOCATA TB Windshield (Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB10 24030100, TB21 24001100, TB10… · Oct 11, 2018
- [W/T-2425-250](https://drs.faa.gov/browse/excelExternalWindow/5DA6DEB06E9C1C61862583D300527FA2.0001): SOCATA TB Windshield (.250 Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB21 22000137 · Oct 11, 2018
- [W/T-2425](https://drs.faa.gov/browse/excelExternalWindow/538E4F40792E5358862583D300527EBB.0001): SOCATA TB Windshield (Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB21 22000137 · Oct 11, 2018
- [SC-W/G-2425](https://drs.faa.gov/browse/excelExternalWindow/4FC78D4160F49C32862583D300527F2A.0001): SOCATA TB Windshield (Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB10 24030100, TB21 24001100, TB10… · Oct 11, 2018
- [SC-W/T-2425-250](https://drs.faa.gov/browse/excelExternalWindow/4E081507006E9F2F862583D300527FFA.0001): SOCATA TB Windshield (.250 Solar Control Green). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB10 24030100, TB21 24001100, TB10… · Oct 11, 2018
- [W-2425](https://drs.faa.gov/browse/excelExternalWindow/4B036AE4B5C6C2D9862583D300527E9F.0001): SOCATA TB Windshield (Clear). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB21 22000137 · Oct 11, 2018
- [SC-W/G-2425-250](https://drs.faa.gov/browse/excelExternalWindow/4857E791DC421651862583D30052803D.0001): SOCATA TB Windshield (.250 Solar Control Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB10 24030100, TB21 24001100, TB10… · Oct 11, 2018
- [W/G-2425-250](https://drs.faa.gov/browse/excelExternalWindow/293EA1D62EC266BE862583D300527FDF.0001): SOCATA TB Windshield (.250 Gray). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces TB21 22000137 · Oct 11, 2018

All of them: https://openairdocs.org/model/socata-group-aerospatiale-tb9/pma.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
