# Schweizer RSG 269C

- Type: Aircraft model (FAA registry)
- Registry code: 8059498
- Manufacturer (registry): SCHWEIZER RSG LLC
- Model: 269C
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Reciprocating
- Seats: 3
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS 4H12](https://openairdocs.org/tcds/4H12) (OpenAirDocs)
- Holder: Schweizer RSG LLC
- Registered aircraft: 3
- Page: https://openairdocs.org/model/schweizer-rsg-269c

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 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2017-14-06](https://openairdocs.org/ad/2017-14-06): Main Rotor Drive System · Sikorsky 269A, 269A-1, 269B and 3 more. Effective Aug 25, 2017
- [AD 2015-23-01](https://openairdocs.org/ad/2015-23-01): Tail Rotor Drive · Sikorsky 269A, 269A-1, 269B and 3 more. Effective Dec 15, 2015
- [AD 2011-12-16](https://openairdocs.org/ad/2011-12-16): Rotorcraft Tailboom · Schweizer 269A, 269A-1, 269B and 2 more. Effective Jul 21, 2011
- [AD 2005-10-12](https://openairdocs.org/ad/2005-10-12): Lateral control trim actuator assembly · Schweizer 269C, 269C-1 and 269D. Effective Jun 2, 2005
- [AD 2003-13-15 R1](https://openairdocs.org/ad/2003-13-15-R1): Aft cluster fittings · Schweizer 269A, 269A-1, 269B and 1 more. Effective Aug 10, 2004
- [AD 2000-16-05](https://openairdocs.org/ad/2000-16-05): Tail Rotor Swashplate Shaft · Schweizer 269A, 269A-1, 269B and 3 more. Effective Sep 19, 2000
- [AD 98-18-11](https://openairdocs.org/ad/98-18-11): Main Rotor Blade · Schweizer 269A, 269A-1, 269B and 2 more. Effective Oct 7, 1998
- [AD 97-23-06](https://openairdocs.org/ad/97-23-06): Ring Gear Teeth Inspection · Schweizer 269A, 269A-1, 269B and 1 more. Effective Dec 10, 1997
- [AD 95-21-02](https://openairdocs.org/ad/95-21-02): Main Rotor Drive Shaft · Schweizer 269A, 269A-1, 269B and 1 more. Effective Nov 17, 1995
- [AD 95-03-12](https://openairdocs.org/ad/95-03-12): Clutch Control Spring Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective Mar 1, 1995
- [AD 94-16-04](https://openairdocs.org/ad/94-16-04): Tail Rotor Pedal support Structure · Schweizer 269A, 269A-1, 269B and 1 more. Effective Oct 5, 1994
- [AD 94-12-06](https://openairdocs.org/ad/94-12-06): Lower Pulley Bearings · Schweizer 269A, 269A-1, 269B and 1 more. Effective Sep 19, 1994
- [AD 94-13-04](https://openairdocs.org/ad/94-13-04): Clutch Control Spring Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective Sep 1, 1994
- [AD 93-05-11](https://openairdocs.org/ad/93-05-11): Fuel Pump Drain Tube Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective May 25, 1993
- [AD 91-05-18](https://openairdocs.org/ad/91-05-18): Tailboom · Schweizer 269C. Effective Mar 29, 1991
- [AD 89-20-03 R1](https://openairdocs.org/ad/89-20-03-R1): Tail Rotor Blades · Schweizer 269A, 269A-1, 269B and 1 more. Effective Feb 22, 1991
- [AD 90-09-07](https://openairdocs.org/ad/90-09-07): Cyclic Control Rod Assembly · Schweizer 269C. Effective Oct 3, 1990
- [AD 90-06-10](https://openairdocs.org/ad/90-06-10): Throttle Cable Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective Apr 6, 1990
- [AD 88-17-04](https://openairdocs.org/ad/88-17-04): Aft Cluster Fittings · Schweizer 269A, 269A-1, 269B and 1 more. Effective Aug 19, 1988
- [AD 88-12-02](https://openairdocs.org/ad/88-12-02): Tail Rotor Retention Strap · Schweizer 269C. Effective Jun 10, 1988
- [AD 82-15-01 R1](https://openairdocs.org/ad/82-15-01-R1): Main Transmission · Schweizer 269A, 269A-1, 269B and 1 more. Effective Oct 4, 1982
- [AD 82-15-03](https://openairdocs.org/ad/82-15-03): Rotor System · Schweizer 269A, 269A-1, 269B and 1 more. Effective Jul 16, 1982
- [AD 81-17-01](https://openairdocs.org/ad/81-17-01): Starting Vibrator Assemblies · Bendix Starting Vibrator Assemblies, B-2, B-2A and 49 more. Effective Aug 13, 1981
- [AD 79-23-03 R1](https://openairdocs.org/ad/79-23-03-R1): Tail Rotor Blades · Schweizer 269A, 269A-1, 269B and 1 more. Effective Nov 19, 1979
- [AD 78-26-04](https://openairdocs.org/ad/78-26-04): Tail Rotor Hub Assembly · Schweizer 269A, 269A-1, 269B and 6 more. Effective Dec 27, 1978
- [AD 78-25-04](https://openairdocs.org/ad/78-25-04): Pinion Assemblies · Schweizer 269A, 269A-1, 269B and 1 more. Effective Dec 18, 1978
- [AD 78-02-02](https://openairdocs.org/ad/78-02-02): Tail Rotor Control Pedals · Schweizer 269A, 269A-1, 269B and 1 more. Effective Jan 24, 1978
- [AD 77-07-01](https://openairdocs.org/ad/77-07-01): Clutch Actuator · Schweizer 269A, 269A-1, 269B and 1 more. Effective Apr 4, 1977
- [AD 76-10-02](https://openairdocs.org/ad/76-10-02): Lateral control · Schweizer 269A, 269A-1, 269B and 1 more. Effective May 21, 1976
- [AD 74-21-04](https://openairdocs.org/ad/74-21-04): Canopy Slats · Schweizer 269A, 269A-1, 269B and 1 more. Effective Apr 4, 1975
- [AD 75-08-12](https://openairdocs.org/ad/75-08-12): Actuator and Cover · Schweizer 269A, 269A-1, 269B and 1 more. Effective Mar 7, 1975
- [AD 73-11-01](https://openairdocs.org/ad/73-11-01): Idler Pulley Bearing Failure · Schweizer 269C. Effective May 21, 1973

Historical (superseded or no longer in force):

- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 2011-01-52](https://openairdocs.org/ad/2011-01-52) (historical): Rotorcraft Tailboom · Schweizer 269A, 269A-1, 269B and 2 more
- [AD 2003-13-15](https://openairdocs.org/ad/2003-13-15) (historical): Tailboom Support Strut or Lug on Cluster Fitting · Schweizer 269A, 269A-1, 269B and 1 more. Effective Aug 12, 2003
- [AD 2001-25-52](https://openairdocs.org/ad/2001-25-52) (historical): Strut Clevis Lug on Center Frame Aft Cluster Fitting · Schweizer 269A, 269A-1, 269B and 1 more. Effective May 8, 2002
- [AD 99-17-10](https://openairdocs.org/ad/99-17-10) (historical): Shaft · Schweizer 269A, 269A-1, 269B and 3 more. Effective Sep 2, 1999
- [AD 93-17-13](https://openairdocs.org/ad/93-17-13) (historical): Lower Coupling Drive Shaft · Schweizer 269A, 269A-1, 269B and 1 more. Effective Oct 20, 1993
- [AD 76-18-01](https://openairdocs.org/ad/76-18-01) (historical): Tail boom support strut · Schweizer 269A, 269A-1, 269B and 3 more. Effective Sep 7, 1976

## Information bulletins (advisory) (5)

- [SAIB SW-17-29](https://openairdocs.org/saib/SW-17-29): Landing Gear Dampers Inspection. Issued Oct 10, 2017
- [SAIB SW-12-12](https://openairdocs.org/saib/SW-12-12): Conducting Engine Failure Simulation in Helicopters with Reciprocating Engines.. Issued Jan 12, 2012
- [SAIB SW-09-44](https://openairdocs.org/saib/SW-09-44): Cabin door. Issued Jul 28, 2009
- [SAIB NE-05-05](https://openairdocs.org/saib/NE-05-05): . Issued Oct 21, 2004
- [SAIB SW-04-13](https://openairdocs.org/saib/SW-04-13): . Issued Nov 7, 2003

## Registered aircraft (3)

- [N269AB](https://openairdocs.org/aircraft/N269AB): [Skyline Aviation Inc](https://openairdocs.org/faa-owner/SKYLINE%20AVIATION%20INC), [San Angelo, TX](https://openairdocs.org/faa-place/TX/San%20Angelo), built 2023, S/N S1982
- [N269AJ](https://openairdocs.org/aircraft/N269AJ): [Skyline Aviation Inc](https://openairdocs.org/faa-owner/SKYLINE%20AVIATION%20INC), [San Angelo, TX](https://openairdocs.org/faa-place/TX/San%20Angelo), built 2025, S/N S1983
- [N269CN](https://openairdocs.org/aircraft/N269CN): [N9660f LLC](https://openairdocs.org/faa-owner/N9660F%20LLC), [Grand Ledge, MI](https://openairdocs.org/faa-place/MI/Grand%20Ledge), built 2024, S/N S1981

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (118, newest 50)

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

- [SDR 2026F00166](https://openairdocs.org/sdr/2026F00166), Jul 28, 2026: SUPPORT FRAME. CRACKED. LEFT AFT AIRFRAME CLUSTER FITTING THAT ATTACHES TO REAR CROSSMEMBER, LANDING GEAR, AND TAIL-BOOM SUPPORT STRUT WAS FOUND CRACKED DURING A VISUAL PREFLIGHT INSPE
- [SDR BY8S2014092600566](https://openairdocs.org/sdr/BY8S2014092600566), Sep 13, 2014: MAGNETO. FAILED. COMPLETE RT MAGNETO IGNITION FAILURE/NO OUTPUT. MAGNETO FAILED PRIOR TO SCHEDULED HOUR INSPECTION.
- [SDR 2014FA0000546](https://openairdocs.org/sdr/2014FA0000546), Sep 13, 2014: MAGNETO. FAILED. COMPLETE RT MAGNETO IGNITION FAILURE WITH NO OUTPUT. MAGNETO FAILED PRIOR TO SCHEDULED INSPECTION.
- [SDR FAA20140910000001](https://openairdocs.org/sdr/FAA20140910000001), Aug 23, 2014: SENSOR. DETACHED. THE ENGINE STOPPED DUE TO LACK OF OIL. THE OIL TEMPERATURE SENSOR, AND CRUSH WASHER WERE FOUND HANGING BY ITS ELECTRICAL CONNECTOR INSIDE THE ENGINE COMPARTMENT
- [SDR 2011FA0000183](https://openairdocs.org/sdr/2011FA0000183), Mar 18, 2011: TAIL ROTOR. DAMAGED. ODOR OF BURNING LUBRICANT, EXCESSIVE VIBRATION, FORCED A SUCCESSFUL OFF AIRPORT LANDING. FOUND AFT "H" FRAME BEARING, PN 269A5050-56, SEIZED, OVERHEATED, DRIVES
- [SDR 2011FA0000027](https://openairdocs.org/sdr/2011FA0000027), Jan 14, 2011: THRUST BEARING. MISMANUFACTURED. (OG5S) DURING 800 HR, 12 AND 24 MONTH INSP, THE MAIN ROTOR DRIVE SHAFT WAS FOUND TO BE WORN JUST ABOVE THE MAIN ROTOR THRUST BEARING. UPON FUTHER INSP, THE WEAR
- [SDR 2010FA0001006](https://openairdocs.org/sdr/2010FA0001006), Sep 17, 2010: PIN. WORN. DURING 200 HR INSP WEAR MARKS WERE FOUND ON THE BOTTOM OF BOTH FUEL TANKS, CAUSED BY ATTACH PIN PN MS20392-2C47 USED ON STRAP ASSY. PN 269A8329-23. DETAILED INS
- [SDR 2010FA0000443](https://openairdocs.org/sdr/2010FA0000443), Apr 30, 2010: STRUT. BROKEN. (OG5S) DURING UNSCHEDULED MX THE LOWER DRIVE SUPPORT STRUT WAS FOUND TO BE CRACKED 90 PERCENT THROUGH THE TUBE WHERE THE UPPER ATTACH LUG IS WELDED. UPON REMOVA
- [SDR 2009FA0000920](https://openairdocs.org/sdr/2009FA0000920), Sep 29, 2009: GEARBOX. LEAKING. PILOT NOTE THE TAIL ROTOR GEARBOX WAS LEAKING. GEARBOX WAS CLEANED WITH SOLVENT AND AIR DRIED AND THEN GROUND RAN FOR 2-3 MIN. LEAKAGE AND CRACK WERE NOTED IN A
- [SDR CA090126006](https://openairdocs.org/sdr/CA090126006), Jan 26, 2009: BOLT. BROKEN. OPERATING A SCHWEIZER 269 C MODEL SERIAL NUMBER S1575 TSN 6449.5 THE CONICAL BRGS WERE REPLACE WITH NEW AT 6338.8 AND A NEW BOLT WAS INSTALLED AT THIS TIME P/N 
- [SDR GLQ2008F00000](https://openairdocs.org/sdr/GLQ2008F00000), Sep 11, 2008: NUT. DAMAGED. ROUTINE INSPECTION OF TRANSIENT ACFT REVEALED BOTH UPPER PULLEY FWD BEARING RETAINER CAP ATTACH BOLT NUTS LOOSE-APPROX Q.5 THREADS ONLY ENGAGED. THESE WERE SERV
- [SDR 2008FA0000271](https://openairdocs.org/sdr/2008FA0000271), Apr 3, 2008: LINE. LEAKING. FUEL LEAKING FROM GASCOLATOR INLET LINE, APPROX 5.0 HRS SINCE NEW. (K)
- [SDR CA080212005](https://openairdocs.org/sdr/CA080212005), Feb 8, 2008: LINK. DISCONNECTED. (CAN) THE COTTER PIN SECURING THE IDLE MIXTURE LINK BLOCK TO THE MIXTURE CONTROL ARM BECAME DISLODGED. THIS ALLOWED THE MIXTURE LINK BLOCK TO BECOME DISCONNECTE
- [SDR 2007FA0000697](https://openairdocs.org/sdr/2007FA0000697), Jul 11, 2007: CONDENSER. DISCONNECTED. SPRING CLIP ON TERMINAL WIRE CAME OFF ALLOWING WIRE TO DISCONNECT. (K)
- [SDR 2007FA0000688](https://openairdocs.org/sdr/2007FA0000688), Jul 10, 2007: BRACKET. LOOSE. ALTERNATOR BRACKET LOOSE AT ENGINE BOSS. BOLT CAUSES DAMAGE TO ENGINE CRANKCASE WHEN LOOSE. FRETTING OF ARM AND ENGINE CRANKCASE OCCURS. (K)
- [SDR 2007FA0000510](https://openairdocs.org/sdr/2007FA0000510), Jun 18, 2007: LOCK NUT. BACKED OUT. DURING GROUND RUNUP, PILOT NOTICED TAIL ROTOR NOT SPINNING. AIRCRAFT SHUTDOWN AND RETURNED TO HANGER. UPON DISASSEMBLY IT WAS NOTED THAT THE NUT PN 269A6029 THA
- [SDR 2007FA0000561](https://openairdocs.org/sdr/2007FA0000561), May 25, 2007: BUSHING. WORN. ENGINE MOUNTED THROTTLE LINKAGE BUSHINGS WORN. FOUND ON INSPECTION WITH EXCESSIVE PLAY. PROBABLY OCCURRED DUE TO EXCESSIVE VIBRATION OR LACK OF SUBRICATION. REC
- [SDR BS2R2120003](https://openairdocs.org/sdr/BS2R2120003), Nov 17, 2006: PULLEY BRACKET. BROKEN. ONE OF THE TWO BELT DRIVE CLUTCH ACTUATOR CABLE PULLEY BRACKETS BROKE CLEAN ACROSS BETWEEN THE FRAME MOUNT HOLE AND THE PULLEY MOUNT HOLE DURING ENGAGEMENT OF T
- [SDR 2006FA0001170](https://openairdocs.org/sdr/2006FA0001170), Nov 17, 2006: BRACKET. BROKEN. ONE OF THE BELT DRIVE CLUTCH ACTUATION SYSTEM CABLE PULLEY BRACKETS (1 OF 2 P/N 269A5472) BROKE CLEAN ACROSS BETWEEN THE PULLEY AND ITS FRAME MOUNT HOLES DURING
- [SDR AU510001955](https://openairdocs.org/sdr/AU510001955), Dec 9, 2005: SHAFT. LOOSE. (AUS) LATERAL CYCLIC CONTROL BELLCRANK LOOSE. DISASSEMBLY AND INVESTIGATION OF THE TRANSMISSION FOUND THAT THE BELLCRANK MOUNTING SHAFT ATTACHED TO THE TRANSMIS
- [SDR CA060303016](https://openairdocs.org/sdr/CA060303016), Nov 25, 2005: VALVE. INCORRECT. FUEL SYSTEM SENDER INCORRECT VALVE. REPLACED SENDER.
- [SDR CA050825001](https://openairdocs.org/sdr/CA050825001), Aug 17, 2005: RING. FAILED. (CAN) HEAVY OIL CONSUMPTION CYLINDER NR 3. OIL RING NOT PERFORMING ITS WORK. REMOVED AND SENT FOR REPAIR. REINSTALLED CYLINDER.
- [SDR 2005FA0000418](https://openairdocs.org/sdr/2005FA0000418), Jan 7, 2005: SHAFT. WORN. DURING ANNUAL INSPECTION GREASE IN LOWER PULLEY SHAFT HAD A RUSTY (BROWN) COLOR (NOTE: ANDEROL GREASE IS BLACK). UPON INSPECTION PART HAS 414.2 HOURS SINCE NEW,
- [SDR CA041124003](https://openairdocs.org/sdr/CA041124003), Nov 22, 2004: ROTOR SHAFT. BROKEN. (CAN) ON RUN UP MAGNETO CHECK, FOUND LT MAG INOP. LT MAG REMOVED AND INSPECTED, ROTOR GEAR WAS FOUND SEPARATED FROM ROTOR SHAFT. RT MAGNETO WAS INSPECTED IN THE
- [SDR CA060303015](https://openairdocs.org/sdr/CA060303015), May 30, 2004: INDICATOR. FAILED. OIL PRESSURE UNSERVICEABLE. REPLACED CLUSTER ASSEMBLY.
- [SDR AUS20040413](https://openairdocs.org/sdr/AUS20040413), May 14, 2004: BOLT. SEPARATED. (AUS) GOVERNOR LINKAGE BOLT SEPARATED. LOSS OF ENGINE CONTROL RESULTED IN AUTO ROTATION AND HEAVY LANDING WITH SOME MINOR DAMAGE TO THE AIRCRAFT.
- [SDR H592004F00000](https://openairdocs.org/sdr/H592004F00000), Feb 28, 2004: SPLINE. SLIPPED. LEVEL FLIGHT, THE TAIL ROTOR DRIVESHAFT STARTED SLIPPING. TAIL ROTOR DRIVESHAFT SPLINES STRIPED. ON FRONT HALF OF SHAFT, STUDENT ENTERED AN AUTOROTATION AND AIR
- [SDR AUS20040136](https://openairdocs.org/sdr/AUS20040136), Feb 27, 2004: FUEL CONTROL. FAULTY. (AUS) ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND PRESSURE ON THE MIXTURE ARM CHANGED THE FUEL FLOW RATE CAUSING THE ENGINE TO STOP.
- [SDR AUS20040085](https://openairdocs.org/sdr/AUS20040085), Feb 8, 2004: SEAL. WORN. (AUS) ENGINE CRANKSHAFT SEAL LEAKING. INVESTIGATION FOUND SEAL HAD DISINTEGRATED AROUND THE SEALING LIP. THIS IS A REPLACEMENT SEAL AFTER THE SEAL FAILURE IN MD
- [SDR AUS20040084](https://openairdocs.org/sdr/AUS20040084), Feb 7, 2004: SEAL. WORN. (AUS) ENGINE CRANKSHAFT SEAL LEAKING. INVESTIGATION FOUND SEAL HAD DISINTEGRATED AROUND THE SEALING LIP.
- [SDR CA030703013](https://openairdocs.org/sdr/CA030703013), Jun 18, 2003: ENGINE. FLAMED OUT. (CAN) SUDDEN ENGINE FLAMES AND A CONTINUOUS LOSS OF SUBSTANTIAL POWER. EMERGENCY LANDING CARRIED OUT. THE ENGINE IS UNDER INVESTIGATION BY TSB. ADDITIONAL REPOR
- [SDR AUS20030615](https://openairdocs.org/sdr/AUS20030615), Jun 9, 2003: PINION GEAR. FAILED. (AUS) MAIN TRANSMISSION TAIL ROTOR DRIVESHAFT PINION FAILED IN AREA LOCATED JUST IN FRONT OF THE THREADED AREA ALLOWING THE TAIL ROTOR DRIVE TO SEPARATE. AIRCRA
- [SDR AUS20030521](https://openairdocs.org/sdr/AUS20030521), May 17, 2003: FRAME. CRACKED. (AUS) FUSELAGE FRAME RT CLUSTER CRACKED.
- [SDR AUS20020700](https://openairdocs.org/sdr/AUS20020700), Jul 12, 2002: CARBURETOR. FAULTY. (AUS) NEWLY FITTED ENGINE CARBURETTOR WAS UNABLE TO LEAN THE MIXTURE USING THE MIXTURE SCREW.
- [SDR AUS20020649](https://openairdocs.org/sdr/AUS20020649), Jun 17, 2002: BEARING. FAILED. (AUS) MAIN ROTOR TRANSMISSION OUTPUT SHAFT BEARING DISINTEGRATED. TAILROTOR DRIVESHAFT TWISTED UP AT TRANSMISSION END.
- [SDR AUS20020610](https://openairdocs.org/sdr/AUS20020610), Jun 15, 2002: BOLT. BROKEN. (AUS) TAIL ROTOR FORK BOLT BROKEN IN HALF.
- [SDR AUS20011318](https://openairdocs.org/sdr/AUS20011318), Dec 11, 2001: BRACKET. CRACKED. (AUS) LOWER DRIVE PULLEY SUPPORT BRACKET CRACKED. ONE ATTACHMENT LUGSEPARATED.
- [SDR AUS20011251](https://openairdocs.org/sdr/AUS20011251), Nov 19, 2001: DAMPER. LOOSE. (AUS) LH REAR LANDING GEAR DAMPER UPPER CAP UNSCREWED AND SEPARATED FROM PISTON. SUSPECT CAUSED BY VIBRATION.
- [SDR AUS20011055](https://openairdocs.org/sdr/AUS20011055), Sep 30, 2001: FRAME. CRACKED. (AUS) FUSELAGE FRAME CRACKED AT LT CLUSTER. FOUND VISUALLY AND CONFIRMED USING DYE PENETRANT INSPECTION. AIRCRAFT HAD OPERATED FOR 192.2 HOURS SINCE AD/HU269/57
- [SDR CA010724035](https://openairdocs.org/sdr/CA010724035), Jul 10, 2001: BLADE. DAMAGED. (CAN) ON INSPECTION OF OPPOSITE TAIL ROTOR BLADE, THIS TAIL ROTOR BLADE WAS FOUND TO HAVE NO ABRAISON STRIP ON LEADING EDGE OF BLADE. FURTHER INSPECTION REVEALE
- [SDR CA010724034](https://openairdocs.org/sdr/CA010724034), Jul 10, 2001: BLADE. CRACKED. (CAN) ON DAILY INSPECTION OUTBOARD PART OF BLADE SKIN WAS FOUND TO BE CRACKED. CRACK IS FORMED AROUND TIP BLOCK ON BLADE. THE CRACK IS APPROX. 3 INCHES LONG, ST
- [SDR AUS20010479](https://openairdocs.org/sdr/AUS20010479), Apr 6, 2001: RETAINER. WORN. (AUS) THERMOFIT SLEEVE WORN ON RETAINER.
- [SDR AU001170](https://openairdocs.org/sdr/AU001170), Dec 8, 2000: KEY. DISINTEGRATED. (AUS) NO3 CYLINDER EXHAUST VALVE SPRING LOCKING KEYS SHATTERED BUT WERE STILL HOLDING THE SPRINGS IN PLACE. CAP PNO MS13998-3 ALSO HADSEVERAL CHIPS MISSING. THE
- [SDR CA000530017](https://openairdocs.org/sdr/CA000530017), May 18, 2000: BOOT. TORN. (CAN)WHILE PERFORMING A POST-FLIGHT INSPECTION, THE PILOT NOTED GREASE ON THE FAN HOUSING (SCROLL ASSY). INSPECTION SHOWED A TEAR ON BOOT 269A-5473 INSTALLED ON
- [SDR 20000505SH034](https://openairdocs.org/sdr/20000505SH034), Mar 29, 2000: SWASHPLATE. BINDING. INTERMITTENT T/R PEDAL BINDING. (X)
- [SDR CA991004031](https://openairdocs.org/sdr/CA991004031), Aug 31, 1999: CYLINDER. WORN. (CAN) POWER LOSS EXPERIENCED DUE TO STICKY VALVES.
- [SDR 99ZZZX2210](https://openairdocs.org/sdr/99ZZZX2210), May 12, 1999: PULLEY. DAMAGED. ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOLTS. INSTALLED NEW BOLTS AND ALTERNATOR. 
- [SDR 99ZZZX2160](https://openairdocs.org/sdr/99ZZZX2160), May 1, 1999: ALTERNATOR. DAMAGED. ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOLTS. INSTALLED NEW BOLTS AND ALTERNATOR. 
- [SDR 99ZZZX239](https://openairdocs.org/sdr/99ZZZX239), Nov 12, 1998: BEARING. FAILED. WHILE IN-FLIGHT, PILOT NOTICED SLIGHT VIBRATION COMING FROM THE ENGINE AND A DROP IN OIL PRESSURE STARTING TO OCCUR. PILOT OPTED FOR A PRECAUTIONARY LANDING. UP
- [SDR 99ZZZX237](https://openairdocs.org/sdr/99ZZZX237), Nov 9, 1998: STRUT. CRACKED. ONE INCH CRACK LOCATED AT UPPER PART OF DRIVE PULLEY FRAME STRUT ASSEMBLY. CRACK ORIGINATED AT WELD.

All 118: https://openairdocs.org/model/schweizer-rsg-269c/reports.md

## STCs that may be installed (OpenAirDocs) (110, 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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [STC SR00004DE](https://openairdocs.org/stc/SR00004DE): Installation of an SX-5 searchlight. Dart Aerospace Company
- [STC SR00006DE](https://openairdocs.org/stc/SR00006DE): Installation of Inframetics IRTV-445G infrared imaging system. Dart Aerospace Company
- [STC SR00152DE](https://openairdocs.org/stc/SR00152DE): Installation of a FLI-MAP (fast laser imaging - mapping airborne platform) terrain mapping equipment system using an organic tissue eye-safe laser beam. (269C S/N 1704 only). Dart Aerospace Company
- [STC SR00364DE](https://openairdocs.org/stc/SR00364DE): Installation of Video Tracker System. Dart Aerospace Company
- [STC SH2726NM](https://openairdocs.org/stc/SH2726NM): Installation of a cabin heater. Dart Aerospace USA Inc
- [STC SH5248NM](https://openairdocs.org/stc/SH5248NM): Installation of external pod, camera mount, and 12 volt power provision. Dart Aerospace USA Inc
- [STC SH4036NM](https://openairdocs.org/stc/SH4036NM): Installation of door actuators. Dart Aerospace USA Inc
- [STC SR00038DE](https://openairdocs.org/stc/SR00038DE): Installation of supplemental lubrication kit for lower drive shaft. Dart Aerospace USA Inc
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SR01838AT](https://openairdocs.org/stc/SR01838AT): Installation of Cyclic Friction Release Levers. Thoroughbred Aviation Maintenance Inc. Lists 269 Series
- [STC SR00711SE](https://openairdocs.org/stc/SR00711SE): Fabrication of Onboard Systems Model 200-244-00 cargo hook kit. Onboard Systems International
- [STC SH1152NW](https://openairdocs.org/stc/SH1152NW): Installation of the Automatic Flagman Model 135 Control Stick Grip. Air Products & Parts LLC
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SH2334SO](https://openairdocs.org/stc/SH2334SO): Installation of a cabin heater/defroster. Schweizer RSG LLC
- [STC SH7WE](https://openairdocs.org/stc/SH7WE): Fabrication of Precision Helicopters Model 4887 Cargo Rack System. Schweizer RSG LLC
- [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc
- [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights. Whelen Aerospace Technologies
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SH444NE](https://openairdocs.org/stc/SH444NE): Installation of Whelen Strobe Lights. Schweizer RSG LLC
- [STC SH445NE](https://openairdocs.org/stc/SH445NE): Installation of Engine Idle Overspeed Control System. Schweizer RSG LLC
- [STC SH586EA](https://openairdocs.org/stc/SH586EA): Installation of Hartzell Anti-Overspeed kits (D-3520-1 and D-3520-2). Schweizer RSG LLC
- [STC SH1065NE](https://openairdocs.org/stc/SH1065NE): Installation of Airwolf Model AFC-500 full flow engine oil filter P/N AFC-500. Airwolf Filter Corporation
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC
- [STC SR02470AK](https://openairdocs.org/stc/SR02470AK): Installation of the L-3 Communications NGT -1000/2000/2500 ADS-B System. ADS-B Technologies, LLC
- [STC SR02471AK](https://openairdocs.org/stc/SR02471AK): Installation of the L-3 Communications NGT -9000/9000R ADS-B System. ADS-B Technologies, LLC
- [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC
- [STC SH1839NM](https://openairdocs.org/stc/SH1839NM): Installation of Skytronics, Part No. 7150T-300-1 Alternators. Hartzell Engine Technologies, LLC
- [STC SR03281CH](https://openairdocs.org/stc/SR03281CH): Installation of Garmin G500H Flight Display System, including GDU 620 PFD/MFD, GTN 650 Control and Display, GRS 77H AHRS, GMU 44 Magnetometer, GTP 59 Temperature Probe and Midcontinent Instrument MD302 Standby Attitude Module. University Aerospace Foundation
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SH202WE](https://openairdocs.org/stc/SH202WE): Installation of controls for pilot-in-command on right side. Allen J Gerbino, Gerbino Flight Systems
- [STC SH249WE](https://openairdocs.org/stc/SH249WE): Installation of a searchlight kit. Allen J Gerbino, Gerbino Flight Systems
- [STC SH258WE](https://openairdocs.org/stc/SH258WE): Installation of MCT-10 mounting rack. Allen J Gerbino, Gerbino Flight Systems
- [STC SH259WE](https://openairdocs.org/stc/SH259WE): Installation of utility compartment. Allen J Gerbino, Gerbino Flight Systems
- [STC SH286WE](https://openairdocs.org/stc/SH286WE): Installation of Tayburn antenna deployment system. Allen J Gerbino, Gerbino Flight Systems
- [STC SH290WE](https://openairdocs.org/stc/SH290WE): Installation of a 'T' instrument console. Allen J Gerbino, Gerbino Flight Systems
- [STC SH152WE](https://openairdocs.org/stc/SH152WE): Installation of Hoskins Model 700801 Anti-collision light system. BF Goodrich Aerospace
- [STC SH152AWE](https://openairdocs.org/stc/SH152AWE): Installation of Hoskins Model 700801 Anti-collision light system in accordance with Hoskins Drawing No. 10-201969, Rev D. Dated August 14, 1972. BF Goodrich Aerospace
- [STC SH1099CE](https://openairdocs.org/stc/SH1099CE): Installation of cabin heater and engine exhaust tail pipe extension. Kinzie Industries Inc
- [STC SH1138CE](https://openairdocs.org/stc/SH1138CE): Installation of engine exhaust tail pipe extension. Kinzie Industries Inc
- [STC SR09562RC](https://openairdocs.org/stc/SR09562RC): Installation of Night Vision Goggle Compatible Interior Lighting System. Aero Dynamix Inc
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc
- [STC SA4172NM](https://openairdocs.org/stc/SA4172NM): Installation of Aviation Development oil filter. Aviation Development Corporation
- [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 SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc
- [STC ST02481CH](https://openairdocs.org/stc/ST02481CH): Installation of camera quick disconnect mounting. NASS-EAC
- [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development Corporation

All 110: https://openairdocs.org/model/schweizer-rsg-269c/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Schweizer 269C](https://openairdocs.org/model/schweizer-269c): 115 registered aircraft, registry code 8059502
- [Hughes 269C](https://openairdocs.org/model/hughes-269c): 74 registered aircraft, registry code 4470504
- [Schweizer HUGHES 269C](https://openairdocs.org/model/schweizer-hughes-269c): 4 registered aircraft, registry code 8059500
- [Sikorsky 269C](https://openairdocs.org/model/sikorsky-269c): 0 registered aircraft, registry code 8140301

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