# Slingsby T67M-260 - Type: Aircraft model (FAA registry) - Registry code: 8323005 - Manufacturer (registry): SLINGSBY - Model: T67M-260 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A73EU](https://openairdocs.org/tcds/A73EU) (OpenAirDocs) - Holder: Slingsby Aviation Ltd. - Registered aircraft: 7 - Page: https://openairdocs.org/model/slingsby-t67m-260 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 2017-10-02](https://openairdocs.org/ad/2017-10-02): Flight Controls · Slingsby T67M260 and T67M260-T3A. Effective Jun 29, 2017 - [AD 2014-04-01](https://openairdocs.org/ad/2014-04-01): Stabilizers · Slingsby T67M260. Effective Apr 1, 2014 - [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 Effective Feb 23, 2005 Historical (superseded or no longer in force): - [AD 2015-11-01](https://openairdocs.org/ad/2015-11-01) (historical): Flight Controls · Slingsby T67M260 and T67M260-T3A. Effective Jun 16, 2015 ## Information bulletins (advisory) (7) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-06-24](https://openairdocs.org/saib/CE-06-24): . Issued Jan 26, 2006 - [SAIB CE-06-23](https://openairdocs.org/saib/CE-06-23): . Issued Jan 25, 2006 - [SAIB CE-04-12](https://openairdocs.org/saib/CE-04-12): . Issued Oct 28, 2003 - [SAIB CE-04-06](https://openairdocs.org/saib/CE-04-06): . Issued Oct 20, 2003 - [SAIB CE-04-05](https://openairdocs.org/saib/CE-04-05): . Issued Oct 20, 2003 - [SAIB CE-03-54](https://openairdocs.org/saib/CE-03-54): . Issued Sep 10, 2003 ## Registered aircraft (7) - [N123FR](https://openairdocs.org/aircraft/N123FR): [Royal Air Flying LLC](https://openairdocs.org/faa-owner/ROYAL%20AIR%20FLYING%20LLC), [Colorado Springs, CO](https://openairdocs.org/faa-place/CO/Colorado%20Springs), S/N 2250 - [N789FR](https://openairdocs.org/aircraft/N789FR): [Brookshire, TX](https://openairdocs.org/faa-place/TX/Brookshire), built 1996, S/N 2240, Registration pending, pending cancellation - [N833TE](https://openairdocs.org/aircraft/N833TE): [Eastern Shore Helicopters Inc](https://openairdocs.org/faa-owner/EASTERN%20SHORE%20HELICOPTERS%20INC), [Fort Denaud, FL](https://openairdocs.org/faa-place/FL/Fort%20Denaud), S/N 2260 - [N833UT](https://openairdocs.org/aircraft/N833UT): [Eastern Shore Helicopters Inc](https://openairdocs.org/faa-owner/EASTERN%20SHORE%20HELICOPTERS%20INC), [Fort Denaud, FL](https://openairdocs.org/faa-place/FL/Fort%20Denaud), S/N 2276 - [N833XT](https://openairdocs.org/aircraft/N833XT): [Schultz Clifford L](https://openairdocs.org/faa-owner/SCHULTZ%20CLIFFORD%20L), [Owens Cross Roads, AL](https://openairdocs.org/faa-place/AL/Owens%20Cross%20Roads), S/N 2270 - [N833YT](https://openairdocs.org/aircraft/N833YT): [Eastern Shore Hellicopters Inc](https://openairdocs.org/faa-owner/EASTERN%20SHORE%20HELLICOPTERS%20INC), [Fort Denaud, FL](https://openairdocs.org/faa-place/FL/Fort%20Denaud), S/N 2269 - [N964SM](https://openairdocs.org/aircraft/N964SM): [Matta Sam](https://openairdocs.org/faa-owner/MATTA%20SAM), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1996, S/N 2235 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR15FA021](https://openairdocs.org/ntsb/WPR15FA021), Oct 24, 2014: Slingsby T67M 260 (N456FR), Ridgecrest, CA, substantial damage, 2 fatal. Probable cause: The pilots' failure to recover from a spin for reasons that could not be determined based on available information. Contributing to the student's fatal injury was his delayed egress from the airplane… ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20141024021049A](https://openairdocs.org/incident/20141024021049A), Oct 24, 2014: Slingsby T67M-260 (N456FR), Randsburg, CA, Destroyed, 2 fatal. While performing spin training from an altitude of 11,200 fat, N456FR, operated by the national test pilot school, was unable to recover from the spin prior to… ## Service difficulty reports (76, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 98ZZZX3142](https://openairdocs.org/sdr/98ZZZX3142), Jul 1, 1998: FUEL HOSE. LOOSE. THE ENGINE QUIT WHILE PERFORMING AN ENGINE GROUND RUN-UP. DEFUELED AIRCRAFT AND OPENED FUEL TANK FOR INSPECTION. THE FUEL FLAP TUB WAS REMOVED FOR INSPECTION AN - [SDR 97ZZZX5178](https://openairdocs.org/sdr/97ZZZX5178), Dec 11, 1997: OIL FILTER. CRACKED. CRACKS WERE FOUND ON ENGINE OIL FILTERS (NEW FILTERS). THIS CRACK IS ON THE BASE FLANGE INSIDE OF BASE SEAL AND OUTBOARD OF INLET HOLES. SUSPECT CAUSE MIGHT BE - [SDR 97ZZZX3924](https://openairdocs.org/sdr/97ZZZX3924), Aug 11, 1997: STEERING COLLAR. CRACKED. DURING 100-HOUR INSPECTION, THE NOSE STEERING COLLAR ON NOSE STRUT WAS FOUND CRACKED. A ONE-TIME INSPECTION WAS PERFORMED FOR THE REST OF THE FLEET (57). EIGHTE - [SDR 97ZZZX3414](https://openairdocs.org/sdr/97ZZZX3414), Jul 15, 1997: BLADE. LOOSE. AFTER AEROBATICS, EXCESSIVE NOSE/PROPELLER VIBRATION WAS FELT, VERY ROUGH AND LOW AIRSPEED. ACFT LANDED SAFELY. FOUND NR 1 PROPELLER BLADE HAD EXCESSIVE PLAY. R - [SDR 97ZZZX2885](https://openairdocs.org/sdr/97ZZZX2885), Jun 13, 1997: SUMP. CRACKED. AFTER A PHASE INSPECTION AND AFTER ENGINE RUN-UP, THE ENGINE WAS CHECKED FOR OIL LEAKS BEFORE COWLING INSTALLED. A LEAK WAS NOTED BEHIND THE RIGHT REAR ENGINE M - [SDR 97ZZZX2891](https://openairdocs.org/sdr/97ZZZX2891), May 28, 1997: G SWITCH. FAILED. WHILE PERFORMING AN ANNUAL ELT INSPECTION, ELT SENSOR DID NOT COME ON. DORNE AND MARGOLIN, ELT NR TSOC91. - [SDR 97ZZZX4299](https://openairdocs.org/sdr/97ZZZX4299), May 27, 1997: SWITCH. MALFUNCTION. WHILE PERFORMING AN ANNUAL ELT INSPECTION, FOUND THE ELT SENSOR DID NOT COME ON. - [SDR 97ZZZX970](https://openairdocs.org/sdr/97ZZZX970), Feb 13, 1997: TANK. CRACKED. ON A PRE-FLIGHT INSPECTION, A FUEL STAIN WAS NOTICED ON BOTTOM OF LEFT WING. FURTHER INSPECTION FOUND A CRACK ON THE FWD INBOARD SIDE OF THE FUEL TANK. SUBMITTE - [SDR 97ZZZX969](https://openairdocs.org/sdr/97ZZZX969), Feb 13, 1997: BLADE. DELAMINATION. INSPECTION OF PROPELLER FOUND A PROPELLER BLADE WITH DELAMINATION AT BASE OF BLADE. (ONE INCH WIDE BY FOUR INCHES LONG). CAUSE UNKNOWN. AWAITING INFORMATION FRO - [SDR 97ZZZX753](https://openairdocs.org/sdr/97ZZZX753), Feb 4, 1997: WIRE. CHAFED. WIRE BUNDLE CHAFING ON INSTRUMENT MOUNT BRACKET BEHIND RADIOS. DISCREPANCY IS THE INTERCOM DOES NOT TRANSMIT CLEARLY. CUTS IN AND OUT. INSPECTED, FOUND A WIRE C - [SDR 97ZZZX893](https://openairdocs.org/sdr/97ZZZX893), Jan 1, 1997: BLADE. DELAMINATED. INSPECTION FOUND DELAMINATION AT BASE OF BLADE. SUBMITTER STATED CAUSE UNKNOWN. AWAITING INFORMATION FROM MANUFACTURER. - [SDR 97ZZZX887](https://openairdocs.org/sdr/97ZZZX887), Jan 1, 1997: BLADE. DELAMINATED. INSPECTION FOUND DELAMINATION AT BASE OF BLADE. SUBMITTER STATED CAUSE UNKNOWN. AWAITING INFORMATION FROM MANUFACTURER. - [SDR 96ZZZX5907](https://openairdocs.org/sdr/96ZZZX5907), Nov 7, 1996: SUPPORT BRACKET. CRACKED. ON ANNUAL INSPECTION THE INBD STBD RUDDER BAR SUPPORT BRACKET WAS FOUND CRACKED. PRESSURE APPLIED TO RUDDER PEDAL PUTS PRESSURE ON BRACKET CAUSING IT TO CRACK. - [SDR 96ZZZX5906](https://openairdocs.org/sdr/96ZZZX5906), Nov 7, 1996: MUFFLER. CHAFED. ON ANNUAL INSPECTION THE MUFFLER TAILPIPE WAS FOUND CHAFING ON FRAME NR 1 (FIREWALL). THE HEAT EXPANDS THE TAILPIPE WHICH CAUSED IT TO HIT THE BOTTOM OF FRAME N - [SDR 96ZZZX5293](https://openairdocs.org/sdr/96ZZZX5293), Oct 3, 1996: CRANK. CHAFING. WHILE PERFORMING AN ANNUAL INSPECTION, NOTICED LT RUDDER BAR CRANK WAS CHAFING ON RUDDER BAR WHEN BRAKE WAS APPLIED. SUSPECT RUDDER BAR CRANK WAS IMPROPERLY INS - [SDR 96ZZZX5294](https://openairdocs.org/sdr/96ZZZX5294), Sep 7, 1996: BRAKE CALIPER. LEAKING. DURING 100-HOUR INSPECTION, RT BRAKE CALIPER FOUND LEAKING THROUGH CASE, WHEN BRAKE WAS APPLIED. HYDRAULIC FLUID WAS SEEN LEAKING FROM CASE. SUBMITTER SUSPECTS - [SDR 96ZZZX4867](https://openairdocs.org/sdr/96ZZZX4867), Sep 5, 1996: SENDER. FAILED. AIRCREWS REPORT ENGINE OIL PRESSURE TOO LOW OR TOO HIGH DURING GROUND AND FLIGHT OPERATIONS. ERRONEOUS OIL PRESSURE GAUGE NEEDLE INDICATIONS HAVE CAUSED EMERGEN - [SDR 96ZZZX4836](https://openairdocs.org/sdr/96ZZZX4836), Aug 29, 1996: BRAKE DISC. WARPED. THE AIR CREW REPORTED THE AIRCRAFT BRAKES WERE SPONGY DURING BRAKING APPLICATION. THERE HAVE BEEN MANY REPORTS BY USAF PILOTS IN THE T-3A PROGRAM PERTAINING TO - [SDR 96ZZZX4835](https://openairdocs.org/sdr/96ZZZX4835), Aug 29, 1996: BRAKE DISC. WARPED. THE AIR CREW REPORTED THE ACFT BRAKES WERE SPONGY DURING BRAKING APPLICATION. THERE HAVE BEEN MANY REPORTS BY USAF PILOTS IN THE T-3A PROGRAM PERTAINING TO SPON - [SDR 96ZZZX4834](https://openairdocs.org/sdr/96ZZZX4834), Aug 29, 1996: FUEL PUMP. FAILED. THE AIR CREW REPORTED LOW OR NO FUEL PRESSURE INDICATION/RISE DURING PRE-FLIGHT CHECK. FURTHER INSPECTION BY UNC MAINTENANCE TECHNICIANS REVEALED THE FUEL PUMP - [SDR 96ZZZX4298](https://openairdocs.org/sdr/96ZZZX4298), Aug 15, 1996: PUSH ROD. BROKEN. THE AIRCREW DECLARED AN IN-FLIGHT EMERGENCY AFTER ACFT ENGINE WOULD NOT RESPOND TO THROTTLE APPLICATION FROM IP'S REMOTE THROTTLE HANDLE AND LINKAGE LOCATED ON - [SDR 96ZZZX4299](https://openairdocs.org/sdr/96ZZZX4299), Jul 10, 1996: PUSH ROD. BROKEN. THE AIRCREW DECLARED AN IN-FLIGHT EMERGENCY AFTER ACFT ENGINE WOULD NOT RESPOND TO THROTTLE APPLICATION FROM IP'S REMOTE THROTTLE HANDLE AND LINKAGE LOCATED ON - [SDR 96ZZZX4833](https://openairdocs.org/sdr/96ZZZX4833), Jul 9, 1996: MASTER CYLINDERS. FAILED. AIR CREWS HAVE REPORTED AIRCRAFT BRAKE PEDALS WERE SPONGY OR HAVE FADED/FAILED DURING BRAKING APPLICATIONS. AFTER 20,000 HOURS OF OPERATION AT THE USAFA, BRAKE - [SDR 96ZZZX3810](https://openairdocs.org/sdr/96ZZZX3810), Jun 25, 1996: ENGINE. STOPPAGE. ENGINE STOPPED. DURING TRAFFIC PATTERN STALL MANEUVERS WITH THE ENGINE AT APPROXIMATELY IDLE. STARTER WAS ENGAGED FOR A SUCCESSFUL RESTART. DURING LANDING THE E - [SDR 96ZZZX3001](https://openairdocs.org/sdr/96ZZZX3001), May 28, 1996: COOLER. LEAK. AFTER FIRST FLIGHT OF THE DAY, AIR CREW NOTICED OIL ON WING WALK. COWLING WAS REMOVED AND OIL WAS SEEN DRIPPING FROM OIL COOLER FINS. REMOVED AND REPLACED OIL C - [SDR 96ZZZX2985](https://openairdocs.org/sdr/96ZZZX2985), May 20, 1996: BLOWER MOTOR. FAILED. SUBMITTER REPORTS SEVERAL CONDENSER BLOWER MOTORS QUIT. SEVEN INSPECTED MOTORS FOUND BRUSHES COMPLETELY WORN. SUBMITTER STATES NO RECOMMENDATIONS AT THIS TIME. - [SDR 96ZZZX3811](https://openairdocs.org/sdr/96ZZZX3811), May 15, 1996: ENGINE. STOPPAGE. ENGINE STOPPED AFTER PILOT REDUCED POWER IN SPIN. SUCCESSFUL RESTART AND RETURN TO BASE WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL. USAF CONDUCTING INVEST - [SDR 96ZZZX3808](https://openairdocs.org/sdr/96ZZZX3808), May 10, 1996: ENGINE. STOPPAGE. ENGINE STOPPED DURING AEROBATIC MANEUVER. SUCCESSFUL RESTART AND RETURN TO BASE WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL. PRELIMINARY ASSESSMENT IS THAT - [SDR 96ZZZX2887](https://openairdocs.org/sdr/96ZZZX2887), May 1, 1996: ENGINE. FAILED. ENGINE STOPPED IN-FLIGHT AFTER POWER REDUCTION IN SPIN DURING POWER ON OF THE SPIN DEMONSTRATION SORTIE. ENGINE RESTARTED WITH START BUTTON. - [SDR 96ZZZX3809](https://openairdocs.org/sdr/96ZZZX3809), Apr 25, 1996: SENDER. FAILED. PILOT MADE AN EMERGENCY LANDING AT A SMALL AIRSTRIP. THE PILOT REPORTED LOW OIL PRESSURE AND RAISING OIL TEMPERATURE. A DOSS MAINTENANCE TEAM WAS SENT TO THE AI - [SDR CA960222039](https://openairdocs.org/sdr/CA960222039), Feb 13, 1996: CONTROL CABLE. FRAYED. (CAN)THE NEW CABLES WERE INSPECTED UNDER THE INSPECTION SCHEDULE OF 500 HOURS OR 12 MONTHS WHICHEVER COMES FIRST AS DIRECTED IN SERVICE BULLETIN 78. THE TWO AIR - [SDR CA960222016](https://openairdocs.org/sdr/CA960222016), Feb 13, 1996: CABLE. FRAYED. (CAN)THE NEW CABLES WERE INSPECTED UNDER THE INSPECATION SCHEDULE OF 500 HOURS OR 12 MONTHS WHICHEVER COMES FIRST AS DIRECTED IN SERVICE BULLETIN 78. THE TWO AI - [SDR 95ZZZX7029](https://openairdocs.org/sdr/95ZZZX7029), Nov 30, 1995: HOSE. DETACHED. PARTIAL ENGINE FAILURE, RPM DROPPED FROM 2700 RPM TO 2100 RPM AND BACK TO 27 RPM FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE RAN FOR APPROXIMATELY 4 TO 5 MINUTES W - [SDR 95ZZZX6608](https://openairdocs.org/sdr/95ZZZX6608), Oct 18, 1995: CANOPY. FAILED. EIGHTEEN MINUTES INTO FLIGHT THE CANOPY OPENED AND SHATTERED. OTHER THAN CANOPY, VERY MINOR DAMAGE DONE TO AIRFRAME. 15MM HOLE - STAB, RT SIDE TOP. 15MM HOLE - - [SDR 95ZZZX6005](https://openairdocs.org/sdr/95ZZZX6005), Oct 5, 1995: ALTERNATOR. DEFECTIVE. ALTERNATOR LIGHT CAME ON DURING FLIGHT. TESTED AND FOUND DEFECTIVE. - [SDR 95ZZZX6004](https://openairdocs.org/sdr/95ZZZX6004), Oct 5, 1995: ALTERNATOR. DEFECTIVE. ALTERNATOR LIGHT CAME ON DURING FLIGHT. TESTED AND FOUND DEFECTIVE. - [SDR 95ZZZX6003](https://openairdocs.org/sdr/95ZZZX6003), Oct 5, 1995: ATERNATOR. DEFECTIVE. ALTERNATOR LIGHT CAME ON DURING FLIGHT. TESTED ALTERNATOR AND FOUND TO BE DEFECTIVE. - [SDR 95ZZZX6002](https://openairdocs.org/sdr/95ZZZX6002), Sep 28, 1995: VENT LINE. FUEL FUMES. AIR CREW REPORTED A STRONG SMELL OF FUEL WHEN FULL POWER WAS SET FOR TAKEOFF. FUEL TANK VENT LINES ARE ROUTED IN COCKPIT AND OUT THROUGH BELLY OF AIRCRAFT. SUSP - [SDR 95ZZZX6001](https://openairdocs.org/sdr/95ZZZX6001), Sep 28, 1995: VENT LINE. FUEL FUMES. AIR CREW REPORTED A STRONG SMELL OF FUEL WHEN FULL POWER WAS SET FOR TAKEOFF. FUEL TANK VENT LINES ARE ROUTED IN COCKPIT AND OUT THROUGH BELLY OF AIRCRAFT. SUSP - [SDR 95ZZZX5944](https://openairdocs.org/sdr/95ZZZX5944), Sep 1, 1995: MUFFLER. CHAFED. THE MUFFLER TAILPIPE IS CHAFING ON THE FIREWALL. A WEAR SPOT WAS FOUND ON INSPECTION. THE ENGINE WAS GROUND RUN AT OPERATING TEMPERATURE WHICH CAUSED THE MUFFLE - [SDR 95ZZZX5943](https://openairdocs.org/sdr/95ZZZX5943), Sep 1, 1995: MUFFLER. CHAFED. THE MUFFLER TAILPIPE IS CHAFING ON THE FIREWALL. A WEAR SPOT WAS FOUND ON INSPECTION. THE ENGINE WAS GROUND RUN AT AN OPERATING TEMPERATURE WHICH CAUSED THE MUF - [SDR 95ZZZX4557](https://openairdocs.org/sdr/95ZZZX4557), Aug 23, 1995: VALVE. LOOSE NUT. AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING ROUTINE TRAINING MISSION. SEVERAL AIRCRAFT IN THE FLEET HAD S - [SDR 95ZZZX4558](https://openairdocs.org/sdr/95ZZZX4558), Aug 21, 1995: VALVE. MALFUNCTIONING. AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING A ROUTINE TRAINING MISSION. OUTSIDE AIR TEMPERATURE WAS ABOVE - [SDR 95ZZZX4483](https://openairdocs.org/sdr/95ZZZX4483), Aug 15, 1995: SENSOR. DEFECTIVE. OIL PRESSURE SENDING UNIT FAILING TO GIVE CORRECT READINGS. SUBMITTER RECOMMENDS TRYING A DIFFERENT MANUFACTURER. SLINGSBY IPC, CHAPTER 55, FIGURE 5, ITEM NR 3. - [SDR 95ZZZX4482](https://openairdocs.org/sdr/95ZZZX4482), Aug 15, 1995: CONTROL CABLE. FRAYED. DURING AN ANNUAL INSPECTION, THE RT RUDDER CABLE WAS FOUND FRAYED BY AFT PULLEY. FRAYED AREA RUNS BACK AND FORTH ON PULLEY. NO RECOMMENDATION AT THIS TIME. SLIN - [SDR 95ZZZX4556](https://openairdocs.org/sdr/95ZZZX4556), Aug 7, 1995: VALVE. MALFUNCTIONING. AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING A ROUTINE TRAINING MISSION. OUTSIDE AIR TEMPERATURE WAS ABOVE - [SDR 95ZZZX4555](https://openairdocs.org/sdr/95ZZZX4555), Aug 7, 1995: VALVE. MALFUNCTIONING. AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING A ROUTINE TRAINING MISSION. OUTSIDE AIR TEMPERATURE WAS ABOVE - [SDR 95ZZZX4494](https://openairdocs.org/sdr/95ZZZX4494), Aug 1, 1995: SENSOR. DEFECTIVE. OIL PRESSURE SENDING UNIT GIVES FALSE READINGS ON INSTRUMENT GAUGE. READINGS ARE ALSO DIFFERENT WHEN TESTING WHILE UNIT IS OFF THE ENGINE. SUBMITTER RECOMMENDS - [SDR 95ZZZX3272](https://openairdocs.org/sdr/95ZZZX3272), Jun 23, 1995: SKIN. DEBONDED. A ONE-TIME INSPECTION FOUND LT AND RT WING SKIN DEBONDING FROM NR 2 RIB, 31 INCHES FROM CENTER LINE. - [SDR 95ZZZX3271](https://openairdocs.org/sdr/95ZZZX3271), Jun 23, 1995: SKIN. DEBONDED. A ONE-TIME INSPECTION FOUND LT AND RT WING SKIN DEBONDING FROM NR 2 RIB, 31 INCHES FROM CENTER LINE. All 76: https://openairdocs.org/model/slingsby-t67m-260/reports.md ## STCs that may be installed (OpenAirDocs) (48) 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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [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 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 SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [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 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 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 SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 2](https://openairdocs.org/stc/SA01933LA-D%20PAGE%202): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC ST00961LA](https://openairdocs.org/stc/ST00961LA): Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated June 26, 2000, or later FAA approved revisions. AMETEK AMERON LLC d/b/a MASS Systems - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system. Champion Aerospace LLC - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. M-20 Oil Separators LLC - [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500. Garmin AT Inc - [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP. M-20 Oil Separators LLC - [STC SA02168AK](https://openairdocs.org/stc/SA02168AK): Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Avalaska Inc - [STC SA00765DE PAGE 1](https://openairdocs.org/stc/SA00765DE%20PAGE%201) (historical): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA01435DE](https://openairdocs.org/stc/SA01435DE) (historical): Installation of engines, modified with a Firewall Forward Technologies. Centri-Lube Technologies LLC - [STC SA02153LA](https://openairdocs.org/stc/SA02153LA) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin AT Inc - [STC SA01933LA](https://openairdocs.org/stc/SA01933LA) (historical): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc ## PMA parts (OpenAirDocs) (39) 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. - [RAP164-02000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160475727120250829181748.0001): Brake Disc. Rapco Inc · PMA PQ2101CE · Replaces 164-02000 Cleveland · Aug 27, 2025 - [APS105-00200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125110500720221020170432.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 105-00200 · Aug 10, 2022 - [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID240371565220210921142607.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID932536548020210702175239.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021 - [RA154-03000](https://drs.faa.gov/browse/excelExternalWindow/DD82997F649BC443862585E40035802A.0001): Molded Grease Seal. Rapco Inc · PMA PQ2101CE · Replaces Cleveland Wheels & Brakes 154-03000 · Sep 1, 2020 - [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/CB6B45C441A97D20862585510065ECA1.0001): SkyTrax 100B. Avidyne Corporation · PMA PQ4035CE · Replaces N/A · May 13, 2019 - [RA063-01200](https://drs.faa.gov/browse/excelExternalWindow/11AB135F1EE8766686257EE40073FC0A.0001): Pressure Plate. Rapco Inc · PMA PQ2101CE · Replaces Cleveland 063-01200 · Oct 13, 2015 - [9230-17003-01](https://drs.faa.gov/browse/excelExternalWindow/9DD900830DCF6B3D86257EBD005F60D4.0001): L-3 Detachable Configuration Module. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [9060-17250-01](https://drs.faa.gov/browse/excelExternalWindow/8511FE654B6B00B686257EBD005F5E3F.0001): L-3 Kit Installation NGT-1000/ NGT-2000/ NGT-2500. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [9060-17500-02 (right angle RF)](https://drs.faa.gov/browse/excelExternalWindow/76DD7CDEA34E5E2786257EBD005F5FFE.0001): L-3 Kit Installation NGT-9000R Panel Mount. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [9230-17003-01](https://drs.faa.gov/browse/excelExternalWindow/6F3D47AA7EA319D086257EBD005F606F.0001): L-3 Detachable Configuration Module. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [9060-17500-01 (straight RF)](https://drs.faa.gov/browse/excelExternalWindow/55A4F1B1D6B4109F86257EBD005F5F8E.0001): L-3 Kit Installation NGT-9000R Panel Mount. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [9060-17000-02 (right angle RF)](https://drs.faa.gov/browse/excelExternalWindow/525673C7552CD4A286257EBD005F5F2A.0001): L-3 Kit Installation NGT-9000 Panel Mount. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [9060-17000-01 (straight RF)](https://drs.faa.gov/browse/excelExternalWindow/4485A55F3E10F10B86257EBD005F5EC2.0001): L-3 Kit Installation NGT-9000 Panel Mount. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015 - [0118030-03](https://drs.faa.gov/browse/excelExternalWindow/CC160F31431510DE86257DFD00702763.0001): Restraint System. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 0118030-03 · Feb 18, 2015 - [0118018-01](https://drs.faa.gov/browse/excelExternalWindow/B4E977AACA4DB74E86257DFD007026EA.0001): Restraint System. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 0118018-01 · Feb 18, 2015 - [0118030-03](https://drs.faa.gov/browse/excelExternalWindow/A11571EA03E5F1FE86257E0E0062F680.0001): Restraint System. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces 0118030-03 · Feb 18, 2015 - [700-00188-XXX](https://drs.faa.gov/browse/excelExternalWindow/DA3A5EF9E847308186257D51004EEACA.0001): Tray, IFD5XX series. Avidyne Corporation · PMA PQ4035CE · Modification part · Aug 12, 2014 - [063-01200-OAA](https://drs.faa.gov/browse/excelExternalWindow/A8BE92F460426F1C86257C4A007619A5.0001): Pressure Plate. Omega Aircraft Articles LLC · PMA PQ4191CE · Replaces Cleveland Wheels and Brakes P/N… · Dec 19, 2013 - [B-00368-17](https://drs.faa.gov/browse/excelExternalWindow/DDB0DFFE740CAC7086257AB600748216.0001): Alternator Control, 28V. Lamar Technologies LLC · PMA PQ2242NM · Replaces B-00368-7 · Oct 28, 2012 - [B-00371-1](https://drs.faa.gov/browse/excelExternalWindow/373D5A16BFA4F97886257AB600748238.0001): Alternator Control, 14V. Lamar Technologies LLC · PMA PQ2242NM · Replaces B-00371-10 · Oct 28, 2012 - [B-00371-1](https://drs.faa.gov/browse/excelExternalWindow/E4F74873B6FB724086257AB60073238B.0001): Alternator Control, 14V. Lamar Technologies LLC · PMA PQ2242NM · Replaces B-00371-10 · Dec 14, 2010 - [B-00368-17](https://drs.faa.gov/browse/excelExternalWindow/A63A5EA697B52CD386257AB600732362.0001): Alternator Control, 28V. Lamar Technologies LLC · PMA PQ2242NM · Replaces B-00368-7 · Dec 14, 2010 - [C210988](https://drs.faa.gov/browse/excelExternalWindow/7E2C0ED71E151B16862572F10054DDAD.0001): Governor Assembly CSSA. ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 126-34-716 · May 14, 2007 - [G-243S](https://drs.faa.gov/browse/excelExternalWindow/366B9C1F221F02B48525704D0051E655.0001): Battery. Teledyne Battery Products · Replaces G-243 · Oct 30, 2003 - [Model 600 WP](https://drs.faa.gov/browse/excelExternalWindow/5682F8155CD6FB10852570490054D746.0001): Air/Oil Separator. M-20 Oil Separators LLC · Modification part · May 12, 2003 - [G-243](https://drs.faa.gov/browse/excelExternalWindow/40587578C85B59FE8525704D0051E5DA.0001): Battery. Teledyne Battery Products · Replaces RG24-11M · Feb 27, 2003 - [C210988](https://drs.faa.gov/browse/excelExternalWindow/0D21A12A1B05AD14852570490052CCA1.0001): Governor Assembly CSSA. ONTIC Engineering & Manufacturing Inc · Replaces 126-34-716 · Nov 3, 2002 - [APS105-0200](https://drs.faa.gov/browse/excelExternalWindow/412BF79D411D4C418525703C006B1579.0001): Rivet. Aviation Products Systems Inc · Replaces AP105-2, SB105-0200, ES-105-2, 0105-0200 · May 7, 2002 - [APS175-02000](https://drs.faa.gov/browse/excelExternalWindow/30BD277C4F6312888525703C006B159E.0001): Brake Disc- Stainless. Aviation Products Systems Inc · Replaces 75-20, 164-02000 · May 7, 2002 - [APS164-02000](https://drs.faa.gov/browse/excelExternalWindow/190C6B81F8E10A678525703C006B1580.0001): Brake Disc. Aviation Products Systems Inc · Replaces AA-20, SB164-02000, 164-02000 · May 7, 2002 - [0118018-01](https://drs.faa.gov/browse/excelExternalWindow/6C775D2C8C732D3585257046005B7530.0001): Restraint System. Pacific Scientific, HTL/Kin-Tech Div · Replaces 0118018-01 · Mar 28, 2000 - [0118030-03](https://drs.faa.gov/browse/excelExternalWindow/4529E3711277DD1785257046005B7531.0001): Restraint System. Pacific Scientific, HTL/Kin-Tech Div · Replaces 0118030-03 · Mar 18, 2000 - [SS-1002](https://drs.faa.gov/browse/excelExternalWindow/CD45EAE46AB59686862573E800758172.0001): Slick START Assembly. Unison Industries (formerly Slick Aircraft Products) · PMA PQ2050CE · Modification part · Apr 16, 1998 - [SS-1001](https://drs.faa.gov/browse/excelExternalWindow/C7E32203B0D0EC7E8525704C00570B73.0001): Slick START TM Installation. Slick Aircraft Products, Division of Unison Ind · Modification part · Dec 2, 1997 - [K-1001](https://drs.faa.gov/browse/excelExternalWindow/79670B8722A2299A8525704C00516146.0001): Slick START TM Installation. Slick Aircraft Products, Division of Unison Ind · Modification part · Dec 2, 1997 - [RA164-02004](https://drs.faa.gov/browse/excelExternalWindow/BA882EFDDD12680F8525704B004F43A1.0001): Brake Disc. Rapco Inc · Replaces Cleveland Wheels & Brakes 164-02004 · Oct 30, 1997 - [0118030-03](https://drs.faa.gov/browse/excelExternalWindow/735848446B81D60385257046005B72D3.0001): Restraint System. Pacific Scientific, HTL/Kin-Tech Division · Replaces Slingsby 0118030-03 · Apr 29, 1997 - [RG24-11M](https://drs.faa.gov/browse/excelExternalWindow/8A7B5858429A17E68525703F004DD191.0001): Battery. Concorde Battery Corp · PMA PQ1174NM · Modification part · Jul 2, 1996 ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Slingsby SLINGSBY T67M260](https://openairdocs.org/model/slingsby-slingsby-t67m260): 11 registered aircraft, registry code 8323050 --- 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.