# Rolls-Royce 0-200-A

- Type: Engine model (FAA registry)
- Registry code: 54532
- Manufacturer (registry): ROLLS-ROYC
- Model: 0-200-A
- Engine type: Reciprocating
- Power: 100 hp
- Data sheet: [TCDS E-252](https://openairdocs.org/tcds/E-252) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 11 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-0-200-a

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

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

- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [AD 98-01-06](https://openairdocs.org/ad/98-01-06): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Feb 13, 1998
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 96-12-06](https://openairdocs.org/ad/96-12-06): Engine Timing · Continental Motors O-200-A, O-200-B, RR O-200-A and 2 more. Effective Jul 18, 1996
- [AD 94-05-05 R1](https://openairdocs.org/ad/94-05-05-R1): Cylinder Rocker · Continental Motors C-125-1, C-125-2, C145-2 and 59 more. Effective Feb 13, 1996
- [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995
- [AD 93-22-05](https://openairdocs.org/ad/93-22-05): Carburetor Air Intake Housing Assemblies · Continental Motors C90-12F, C90-12FH, C90-12FJ and 22 more. Effective Dec 14, 1993
- [AD 93-19-04](https://openairdocs.org/ad/93-19-04): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Oct 18, 1993
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 93-11-03](https://openairdocs.org/ad/93-11-03): Incorrect Connecting Rod · Continental Motors O-200-A, O-300-A, O-300-C and 1 more. Effective Jul 13, 1993
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981
- [AD 81-07-06](https://openairdocs.org/ad/81-07-06): AC Fuel Pumps · Continental Motors A-65-1, A-65-12, A-65-12F and 60 more. Effective Apr 1, 1981
- [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980
- [AD 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969

Historical (superseded or no longer in force):

- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more

## Information bulletins (advisory) (5)

- [SAIB NE-18-27](https://openairdocs.org/saib/NE-18-27): POWERPLANT  Rocker Shaft Boss Inspection. Issued Sep 10, 2018
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-03-45](https://openairdocs.org/saib/NE-03-45): . Issued Jun 27, 2003
- [SAIB CE-98-21R1](https://openairdocs.org/saib/CE-98-21R1): . Issued Jun 10, 1998

## Registered aircraft (11)

- [N142MW](https://openairdocs.org/aircraft/N142MW): [Stefenelli Aviation N-Tr Inc Trustee](https://openairdocs.org/faa-owner/STEFENELLI%20AVIATION%20N-TR%20INC%20TRUSTEE), Attersee, S/N 0231
- [N150TV](https://openairdocs.org/aircraft/N150TV): [Plane Fun Inc Tr Trustee](https://openairdocs.org/faa-owner/PLANE%20FUN%20INC%20TR%20TRUSTEE), [Snellville, GA](https://openairdocs.org/faa-place/GA/Snellville), built 1975, S/N F15001165
- [N17342](https://openairdocs.org/aircraft/N17342): [Weber Worldwide LLC](https://openairdocs.org/faa-owner/WEBER%20WORLDWIDE%20LLC), [Cedar Rapids, IA](https://openairdocs.org/faa-place/IA/Cedar%20Rapids), built 1973, S/N 1045
- [N208TB](https://openairdocs.org/aircraft/N208TB): [Barker Terry G](https://openairdocs.org/faa-owner/BARKER%20TERRY%20G), [Purvis, MS](https://openairdocs.org/faa-place/MS/Purvis), built 1969, S/N 702
- [N208WC](https://openairdocs.org/aircraft/N208WC): [Plane Fun Inc Tr Trustee](https://openairdocs.org/faa-owner/PLANE%20FUN%20INC%20TR%20TRUSTEE), [Snellville, GA](https://openairdocs.org/faa-place/GA/Snellville), built 1965, S/N 580
- [N2904N](https://openairdocs.org/aircraft/N2904N): [Evolution Aircraft Inc](https://openairdocs.org/faa-owner/EVOLUTION%20AIRCRAFT%20INC), [Zephyrhills, FL](https://openairdocs.org/faa-place/FL/Zephyrhills), built 1947, S/N 13165
- [N31063](https://openairdocs.org/aircraft/N31063): [Qualitair LLC Trustee](https://openairdocs.org/faa-owner/QUALITAIR%20LLC%20TRUSTEE), Michelstadt, built 1973, S/N 0567
- [N40271](https://openairdocs.org/aircraft/N40271): [Larson Jeffrey A](https://openairdocs.org/faa-owner/LARSON%20JEFFREY%20A), [Eau Claire, WI](https://openairdocs.org/faa-place/WI/Eau%20Claire), S/N AV1062
- [N427KB](https://openairdocs.org/aircraft/N427KB): [Skorupa Anthony R](https://openairdocs.org/faa-owner/SKORUPA%20ANTHONY%20R), [Bridger, MT](https://openairdocs.org/faa-place/MT/Bridger), S/N 4
- [N624RW](https://openairdocs.org/aircraft/N624RW): [Wiles William Anthony](https://openairdocs.org/faa-owner/WILES%20WILLIAM%20ANTHONY), [Elkin, NC](https://openairdocs.org/faa-place/NC/Elkin), built 1970, S/N 1561
- [N6EW](https://openairdocs.org/aircraft/N6EW): [Thorne John S](https://openairdocs.org/faa-owner/THORNE%20JOHN%20S), [Woodland Hills, CA](https://openairdocs.org/faa-place/CA/Woodland%20Hills), built 1913, S/N WW6

## NTSB investigations (3)

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 LAX98LA223](https://openairdocs.org/ntsb/LAX98LA223), Jul 5, 1998: Morane-Saulnier MS 880B (N55BF), Trinity Center, CA, destroyed, 1 fatal. Probable cause: The pilot's failure to maintain an adequate airspeed margin while maneuvering in a mountainous area at low altitude, which resulted in an inadvertent stall/spin.
- [NTSB LAX94LA142](https://openairdocs.org/ntsb/LAX94LA142), Feb 26, 1994: Weber Q200 (N89BW), Las Vegas, NV, substantial damage. Probable cause: THE TOTAL FAILURE OF THE TAILWHEEL ASSEMBLY. THE ROUGH/UNEVEN TERRAIN WAS A FACTOR IN THIS ACCIDENT.
- [NTSB CHI67F0275](https://openairdocs.org/ntsb/CHI67F0275), Oct 2, 1966: Cessna 120 (N2904N), Oxford, OH, substantial damage

## 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 19980705015649A](https://openairdocs.org/incident/19980705015649A), Jul 5, 1998: Socata MS880B (N55BF), Trinity Center, CA, Destroyed, 1 fatal. Acft crashed under unkn circumstances, pilot suffered fatal inj, acft was destroyed. Trinity Center, CA. (From .4) the aircraft impacted trees and terrain in a…

## Service difficulty reports (438, newest 50)

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

- [SDR 2026FA0000138](https://openairdocs.org/sdr/2026FA0000138), Jan 16, 2026: RETAINER. BROKEN. ON 1/16/26 AT APPROX 2030Z 2NM NE OF THE LAKE MURRAY DAM, ON A FLT FROM KCUB - KEOE AT 2000' MSL, ENGINE BEGAN EXPERIENCING SEVERE VIBRATION & RPM LOSS. ENG BEG
- [SDR 2026FA0000089](https://openairdocs.org/sdr/2026FA0000089), Oct 11, 2025: CYLINDER. FRACTURED. AFER TAKING ON FUEL AT BAF, THE AIRCRAFT DEPARTED FOR 47N. WHILE CLIMBING OUT THROUGH 2500 MSL, THE AIRCRAFT ENGINE SUFFERED CATASTROPHIC FAILURE OF CYLINDER NU
- [SDR 2025FA0000791](https://openairdocs.org/sdr/2025FA0000791), Aug 24, 2025: VOLT REGULATOR. DEFECTIVE. VOLTAGE REGULATOR FAILURE IN FLIGHT RESULTED IN OVERVOLTAGE CONDITION. CAUSED BATTERY OVERHEATING/SWELLING AND COMMUNICATION RADIO FAILURE. NO FIRE OR SMOKE NOT
- [SDR 2025FA0000265](https://openairdocs.org/sdr/2025FA0000265), Apr 12, 2025: MAGNETO. DEFECTIVE. LARGE MAG DROP ON RUNUP THAT WAS SIGNIFICANT ENOUGH TO ALMOST SHUT DOWN THE ENGINE. MAGNETO HAD 568.9 HOURS SINCE INSTALLATION ON THE ENGINE, AND WAS INSTALLED 
- [SDR 2023FA0000628](https://openairdocs.org/sdr/2023FA0000628), Sep 30, 2023: CYLINDER. DAMAGED. WE OVORNOULED LHLS ENGINE WITH FOUR (4), NEW CMI. (CONTINENTAL MOTORS INC) CY!NDER ASSEMBLIES. AL 112. 7 HO<N, WO HAD 10 REPLACE ALL FOUR CYLINDER AUEMBLIOS DUE
- [SDR 2022FA0000726](https://openairdocs.org/sdr/2022FA0000726), Nov 23, 2022: EXHAUST VALVE. STUCK. ENGINE ROUGH RUNNING DURING TAKE OFF RUN UP. COMPRESSION TEST FOUND #4 CYLINDER LOW. REMOVED CYLINDER FOUND EXHAUST VALVE STUCK OPEN. REMOVED VALVE, CLEANED GUI
- [SDR 2022FA0000727](https://openairdocs.org/sdr/2022FA0000727), Nov 23, 2022: EXHAUST VALVE. STUCK. ENGINE ROUGH RUNNING DURING PRE-TAKE OFF RUN UP. COMPRESSION TEST FINDS NONE IN #4 CYLINDER. DISASSEMBLED, FOUND EXHAUST VALVE STUCK DUE CARBON BUILD UP IN VALV
- [SDR 2022FA0000752](https://openairdocs.org/sdr/2022FA0000752), Nov 20, 2022: EXHAUST VALVE. DESTROYED. EXHAUST VALVE BROKE OFF AT BASE OF VALVE STEM, CAUSING DESTRUCTION OF CYLINDER COMBUSTION CHAMBER AND SUBSEQUENT ENGINE FAILURE.
- [SDR 2022FA0000437](https://openairdocs.org/sdr/2022FA0000437), Aug 8, 2022: TRANSMITTER. DEFECTIVE. TEST, TEST, TEST - AC LANDED SHORT OF RUNWAY AFTER ENGINE QUIT. AC HAD SUBSTANTIAL DAMAGE NO INJURIES. DETERMINED AC RAN OUT OF FUEL DUE TO FAULTY FUEL GUAGE. R
- [SDR 2020FA0000249](https://openairdocs.org/sdr/2020FA0000249), May 12, 2020: CRANKSHAFT. CRACKED. AIRCRAFT IN FOR ANNUAL INSPECTION, REMOVED SPINNER TO CHECK PROP HUB, S/N, MODEL. NOTICED CRANKSHAFT OIL PLUG MISSING, LOOKED INSIDE CRANKSHAFT BORED HOLE I NOT
- [SDR 20191204001](https://openairdocs.org/sdr/20191204001), Dec 4, 2019: BOLT. MISSING. THE AN3-6 BOLT WHICH CONNECTS THE ELEVATOR TRIM TAB CONTROL ROD TO THE TRIM ACTUATOR WAS MISSING AND WAS NOT ABLE TO BE LOCATED. FAILURE OF THE ITEM COULD NOT B
- [SDR 2018FA0000314](https://openairdocs.org/sdr/2018FA0000314), Jul 31, 2018: CYLINDER. SEPARATED. CYLINDER NUMBER 3 SHOWING SIGNS OF HEAD SEPARATION FROM BARREL AT TT 115.3. PREVIOUSLY CYLINDERS NUMBER 1 AND NUMBER 2 WERE REMOVED FOR SAME REASON AT TT OF 47.
- [SDR 2018FA0000317](https://openairdocs.org/sdr/2018FA0000317), Jul 31, 2018: CYLINDER HEAD. SEPARATED. NR 1 CYLINDER SHOWING SIGNS OF HEAD SEPARATION FROM BARREL AT TT 47.6.
- [SDR 2018FA0000073](https://openairdocs.org/sdr/2018FA0000073), Feb 28, 2018: HOLDER. DETERIORATED. OLD FUSE HOLDERS DETERIORATED SO MUCH THEY FALL APART. SUGGEST AD TO REPLACE WITH "BUTTON HEAD" CIRCUIT BREAKERS SO AS TO BE ABLE TO FOLLOW AC ON EXERCISING OCC
- [SDR 2017FA0000319](https://openairdocs.org/sdr/2017FA0000319), Jun 12, 2017: JOURNAL. WORN. ENGINE RECEIVED FOR INSPECTION DUE TO EXCESSIVE CRANKSHAFT END PLAY. UPON DISASSEMBLY, THE CRANKSHAFT HAD EXCESSIVE WEAR FOR A 500 HR CRANK AND THE WEAR PATTERN
- [SDR XYZA20170228001](https://openairdocs.org/sdr/XYZA20170228001), Feb 12, 2017: CARBURETOR. CONTAMINATED. AFTER TAKEOFF AT APPROXIMATELY 200-250 FEET AGL THE ENGINE POWER DECREASED AND SUBSEQUENTLY WOULD NOT GO ABOVE IDLE. AIRCRAFT MADE AN EMERGENCY LANDING SAFELY P
- [SDR FAA2016FA0000602](https://openairdocs.org/sdr/FAA2016FA0000602), Nov 10, 2016: DIPSTICK. CRACKED. IMMEDIATELY AFTER TAKEOFF, THE PILOT OBSERVED SMOKE EMANATING FROM THE ENGINE. A MECHANIC FOUND THAT THE ENGINE OIL DIPSTICK CAP WAS NOT SECURELY LOCKED IN PLAC
- [SDR 2016FA0000323](https://openairdocs.org/sdr/2016FA0000323), Jul 11, 2016: MAGNETO. DAMAGED. BOTH MAGNETOS HAD INTERNAL DAMAGE. BOTH MAGNETOS REQUIRED NEW ROTORS, LT MAGNETO REQUIRED NEW ROTOR AND HOUSING DUE TO ROTOR BREAKING AND DAMAGING HOUSING.
- [SDR 2016FA0000143](https://openairdocs.org/sdr/2016FA0000143), Mar 25, 2016: CYLINDER HEAD. BROKEN. DURING CLIMB THE RPM DROPPED AND POWER WAS LOST FORCING THE AIRCRAFT TO LAND IN A FIELD. INSPECTING THE ENGINE ON CYLINDER NR 2, THE 3 ROCKER SHAFT RETAINING BO
- [SDR 2016FA0000094](https://openairdocs.org/sdr/2016FA0000094), Feb 24, 2016: HINGE. WORN. DURING ANNUAL INSPECTION, 2 MISSING PULL-TYPE RIVETS WERE FOUND MISSING ON THE LT OTBD ELEVATOR HINGE ASSY PN-0432165-1 ALONG WITH A WORN BUSHING, PN-0432003-1 
- [SDR 2016FA0000082](https://openairdocs.org/sdr/2016FA0000082), Feb 5, 2016: MAGNET. DEFECTIVE. REMOVED DEFECTIVE RT MAGNET, OWNER REPORTED DEAD MAG ON RUN UP. REMOVED COVER, BREAKING FACTORY TORQUE SEAL. APRON INSPECTION FOUND THE ROTATING MAGNET CRACKED 
- [SDR 2015FA0000658](https://openairdocs.org/sdr/2015FA0000658), Nov 2, 2015: VALVE. BURNED. REMOVED CYLINDERS NRS 1 AND 3 DUE TO NEAR ZERO COMPRESSIONS AND AUDIBLE LEAKING INTO EXHAUST SYS. BEGAN INVESTIGATION DUE TO LOW RPM AND VIBRATION ON TAKEOFF. E
- [SDR CA151002004](https://openairdocs.org/sdr/CA151002004), Oct 2, 2015: CAP. FAILED. (CAN) PILOT REPORTED ROUGH RUNNING ENGINE WITH SUBSEQUENT POWER LOSS AT CRUISE SETTING. FORCED LANDING IN FIELD UNEVENTFUL. INITIAL ENGINE INSPECTION REVEALED L
- [SDR CA150923010](https://openairdocs.org/sdr/CA150923010), Sep 22, 2015: CRANKSHAFT. DAMAGED. (CAN) END PLUG SEPARATED FROM CRANKSHAFT, FLOATED AROUND IN PROPELLER HUB. VIBRATION ONLY FELT BELOW 1200 RPM.
- [SDR 2015FA0000474](https://openairdocs.org/sdr/2015FA0000474), Aug 28, 2015: CYLINDER. CRACKED. ACFT DECLARED EMERGENCY DUE TO OIL LEAK AND EXCESSIVE VIBRATION. LANDED ON AIRFIELD WITHOUT FURTHER INCIDENT. INSPECTION REVEALED NR 3 CYLINDER BASE WAS CRACKED
- [SDR CA150604020](https://openairdocs.org/sdr/CA150604020), May 17, 2015: COUPLING. SHEARED. (CAN) VACUUM COUPLING FAILED. PROBLEM FOUND ON START UP AND FLIGHT ABORTED. REPLACED VACUUM PUMP WITH NEW UNIT. ALL WORK PERFORMED BY MAINTENANCE AND SIGNED OUT
- [SDR CA150223008](https://openairdocs.org/sdr/CA150223008), Feb 20, 2015: FITTING. CRACKED. (CAN) DURING ANNUAL INSPECTION, FOUND CORROSION ON THE FITTING HOLDING VERTICAL STAB TO HORIZONTAL STAB. WHEN CORROSION WAS REMOVED, FAINT LINES WERE NOTICED. U
- [SDR CA150225007](https://openairdocs.org/sdr/CA150225007), Feb 17, 2015: SPRING. BROKEN. (CAN) PILOT NOTICED RUDDER DEFLECTION TO RT WITH NOSE WHEEL STRAIGHT DURING PREFLIGHT INSPECTION. INSPECTION FOUND THE LT RUDDER CABLE TENSIONING SPRING BROKEN.
- [SDR 2014FA0000661](https://openairdocs.org/sdr/2014FA0000661), Nov 17, 2014: CYLINDER HEAD. CORRODED. BRAND NEW CYLINDERS WERE DISASSEMBLED AND INSPECTED PRIOR TO INSTALLATION, EXCESSIVE PITTING WAS FOUND ON BOTH INTAKE AND EXHAUST VALVE SEATS OF NEW, O-200 POWE
- [SDR CA150319006](https://openairdocs.org/sdr/CA150319006), Oct 5, 2014: MUFFLER. CRACKED. (CAN) CRACK IN THE INTERIOR OF THE RT MUFFLER FOUND DURING ANNUAL ENGINE INSPECTION. NEW MUFFLER TO BE INSTALLED.
- [SDR CA140407011](https://openairdocs.org/sdr/CA140407011), Apr 4, 2014: SPRING. MISSING. (CAN) UPON VISUAL INSPECTION OF THE CYLINDER ASSY IN QUESTION IT WAS FOUND THAT THE INTERMEDIATE EXHAUST VALVE SPRING, WAS NOT INSTALLED, AND AS VERIFIED BY WEA
- [SDR T22R2014051600001](https://openairdocs.org/sdr/T22R2014051600001), Feb 17, 2014: CYLINDER. CRACKED. AFTER ONE HOUR FLIGHT WITH LANDING. ON GROUND FOR 45 MINUTES, PREFLIGHT, CHECK OIL QTY, 5.8 QTS, STARTED ENGINE, TAXI TO RUN UP AREA, ENGINE RUN UP NORMAL, NORM
- [SDR CA140127003](https://openairdocs.org/sdr/CA140127003), Jan 17, 2014: MUFFLER. CRACKED. (CAN) DURING CF-90-03, INSPECTION A CRACK WAS FOUND AT FORWARD FLANGE. CRACK IS APPROXIMATELY 75 PERCENT AROUND THE CIRCUMFERENCE. THERE IS SEPERATION ALONG THE
- [SDR CA130819016](https://openairdocs.org/sdr/CA130819016), Aug 11, 2013: EXHAUST VALVE. FAILED. (CAN) ENGINE INSPECTED AFTER UNSCHEDULED LANDING, FOUND NR 1 CYLINDER WITH NO COMPRESSION, CYLINDER REMOVED AND FOUND EXHAUST VALVE BROKEN.
- [SDR CA131111017](https://openairdocs.org/sdr/CA131111017), Jun 14, 2013: TRANSMITTER. FAILED. (CAN) RIGHT FUEL TANK TRANSMITTER FOUND TO BE READING EMPTY ALL THE TIME. TROUBLESHOT PROBLEM TO BE THE RT FUEL TRANSMITTER PN MC04265171. RT FUEL TRANSMITTER R
- [SDR CA131111006](https://openairdocs.org/sdr/CA131111006), Jun 4, 2013: TRANSMITTER. FAULTED. (CAN) LT FUEL TRANSMITTER PN 0426517-1 REPORTED READING EMPTY WHEN FUEL TANK IS FULL. LT FUEL TRANSMITTER FOUND TO HAVE A HOLE IN FOAT. TRANSMITTER REPLACED WIT
- [SDR CA130501003](https://openairdocs.org/sdr/CA130501003), Apr 30, 2013: WIRE. BURNED. (CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT SAW SMOKE AND SHUT DOWN ELECTRICAL POWER TO AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND RING TERMINAL
- [SDR 2013FA0000253](https://openairdocs.org/sdr/2013FA0000253), Apr 27, 2013: BULKHEAD. CRACKED. FUSELAGE TAILCONE BULKHEAD, FOUND TO BE CRACKED IN BEND RADIUS AT BOTH RUDDER STOP BOLT LOCATIONS. BULKHEAD REINFORCEMENT PLATE, PN 0412181-1, FOUND TO BE CRACK
- [SDR CA130429014](https://openairdocs.org/sdr/CA130429014), Apr 26, 2013: TUBE. LEAKING. (CAN) TUBE DEVELOPED SMALL HOLE AT MANUFACTURING SEAM LINE LIKE PREVIOUSLY FAILED TUBES.
- [SDR CA130422005](https://openairdocs.org/sdr/CA130422005), Apr 21, 2013: TUBE. FAILED. (CAN) TUBE DEVELOPED SMALL PIN HOLE AT SEAM JOINT. UPON LANDING THE TIRE WENT FLAT AND SHEARED THE STEM. DO NOT KNOW IF AIRPORT FOUND THE FOD. TUBE IN SERVICE F
- [SDR CA130419004](https://openairdocs.org/sdr/CA130419004), Mar 26, 2013: TUBE. FAILED. (CAN) TUBE DEVELOPS SMALL HOLE THEN EVENTUALLY IN LIFE CYCLE FINDS ITSELF FLAT.
- [SDR CA130406001](https://openairdocs.org/sdr/CA130406001), Mar 11, 2013: TUBE. PUNCTURED. (CAN) SMALL PIN HOLE FOUND. TIRE WENT FLAT MFG DEFECT.
- [SDR CA130406002](https://openairdocs.org/sdr/CA130406002), Mar 11, 2013: TUBE. FAILED. (CAN) SMALL PIN HOLE TOP OF TUBE BETWEEN 2 SEAMS. COMPONENT HAS 7.53 MONTHS IN SERVICE.
- [SDR CA130219004](https://openairdocs.org/sdr/CA130219004), Feb 19, 2013: HOUSING. CRACKED. (CAN) DURING UNSCHEDULED MAINTENANCE, AN OIL LEAK WAS DISCOVERED AT THE OIL SCREEN HOUSING. UPON REMOVAL OF THE HOUSING, A CRACK WAS FOUND FROM ONE SIDE TO THE 
- [SDR 2013FA0000098](https://openairdocs.org/sdr/2013FA0000098), Jan 10, 2013: MUFFLER. FAILED. PILOT OBSERVED SMOKE IN THE COCKPIT, DECLARED EMERGENCY AND LANDED NORMALLY. ON INSPECTION OF THE RT ENGINE COMPARTMENT, MUFFLER AFT WALL WAS MISSING AND EXHAUS
- [SDR CA130115016](https://openairdocs.org/sdr/CA130115016), Jan 10, 2013: TUBE. FAILED. (CAN) ON LANDING, THE TIRE WENT FLAT. NO FAULT FOUND WITH TIRE CAVITY, TUBE JUST DEVELOPED HOLE. CALENDAR TIME ON TUBE 7.5 MONTHS.
- [SDR 2013FA0000019](https://openairdocs.org/sdr/2013FA0000019), Dec 6, 2012: BOSS. CRACKED. ROCKER SHAFT BOSSES FOUND CRACKED WHEN CYLINDER REMOVED DUE TO FAILURE. LAST DYE CHECK WAS DONE IN 5/6/2007 (O/H DATE 1998). CYLINDER ONLY HAD 50 HRS SINCE LAST
- [SDR CA121212006](https://openairdocs.org/sdr/CA121212006), Nov 21, 2012: CONTROL CABLE. FRAYED. (CAN) RUDDER CABLES FOUND FRAYED AND STRETCHED, CABLE 0400107-49 FOUND FRAYED IN MIDDLE OF ITS CABLE RUN. CABLE 0400107-50 FOUND FRAYED AT AFT MOST PULLEY BOTH 
- [SDR CA121212003](https://openairdocs.org/sdr/CA121212003), Nov 20, 2012: BUSHING. WORN. (CAN) UPON INSPECTION CONTROL TEE LOWER PIVOT POINT RETAINING BUSHING FOR PIVOT BEARING FOUND TO HAVE COME LOOSE IN ITS CRIMP WITH BLACK FRETTING PRESENT AROUND
- [SDR CA121119008](https://openairdocs.org/sdr/CA121119008), Nov 17, 2012: EXHAUST VALVE. FAILED. (CAN) EXHAUST VALVE FAILURE, CYLINDER HEAD SEPARATION.

All 438: https://openairdocs.org/engine/rolls-royce-0-200-a/reports.md

## STCs that may be installed (OpenAirDocs) (51, first 50)

Approved for this engine 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 SE04651CH](https://openairdocs.org/stc/SE04651CH): To allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22. Swift Fuels LLC
- [STC SE2932SW](https://openairdocs.org/stc/SE2932SW): Install carburetor air temperature indicator. Approved for Aircooled Motors (Franklin Engine Co.) equipped with float carburetors. Model eligibility included here may not be inclusive. Alcor LLC. Lists O-200 Series
- [STC SE208SO](https://openairdocs.org/stc/SE208SO): Installation of ice indicator in the carburetor. LegacySTC.com. Lists O-200 Series
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd
- [STC SE00145WI](https://openairdocs.org/stc/SE00145WI): Installation of B&C Specialty Products Model BC 320-( ) Engine Starter. B & C Specialty Products Inc
- [STC SE03232CH](https://openairdocs.org/stc/SE03232CH): Installation of Engine Preheat Kit p/n TA2925-1 for 115 volt application. Hartzell Propeller Inc
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp
- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc
- [STC SE00533SE](https://openairdocs.org/stc/SE00533SE): Installation of Real Gasket Corporation Continental Engine Pushrod Tube Modification. Real Gaskets Tennessee
- [STC SE7559SW](https://openairdocs.org/stc/SE7559SW): Install adapter to permit use of a spin-on oil filter. Stratus Tool Technologies LLC
- [STC SE10076SC](https://openairdocs.org/stc/SE10076SC): Modify engine by installation of C12ST2/S starter. Hartzell Engine Technologies, LLC
- [STC SE10129SC](https://openairdocs.org/stc/SE10129SC): Installation of rotocoil, valve springs, ni-resist valve guide, exhaust valve with chrome flash on stem, and rocker shaft with thrust buttons. Continental Motors, Inc
- [STC SE34WE](https://openairdocs.org/stc/SE34WE): Installation of Electro-Coatings, Inc., piston rings on Continental pistons. Continental Motors, Inc
- [STC SE4247SW](https://openairdocs.org/stc/SE4247SW): Regrind crankshaft to .020 undersize on crankpin and main journals. Continental Motors, Inc. Lists O-200 Series
- [STC SE8109SW](https://openairdocs.org/stc/SE8109SW): Installation of any or all parts identified by Drawing/Parts Application List AEC9109-2. Continental Motors, Inc
- [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings. Continental Motors, Inc
- [STC SE7562SW](https://openairdocs.org/stc/SE7562SW): Install adapter to permit use of a spin-on oil filter. Stratus Tool Technologies LLC
- [STC SE3330NM](https://openairdocs.org/stc/SE3330NM): Continental valve cover gasket. Real Gaskets Tennessee
- [STC SE09002SC](https://openairdocs.org/stc/SE09002SC): Regrind Teledyne Continental crankshafts, to .020-inch undersize on crankpin and main journals. Aircraft Specialties Services Inc
- [STC SE1780NM](https://openairdocs.org/stc/SE1780NM): Installation of Precise Flight standby vacuum system (SVS III). Precise Flight Inc
- [STC SE01943CH](https://openairdocs.org/stc/SE01943CH): Add the following approved fuels: unleaded automotive gasoline 87 minimum antiknock index, per ASTM Specification D-439 or D-4814 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227. Experimental Aircraft Association Inc
- [STC SE634GL](https://openairdocs.org/stc/SE634GL): Superseded by STC SE01943CH. Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index. EAA Aviation Foundation. Lists O-200 Series
- [STC SE154CH](https://openairdocs.org/stc/SE154CH): Engine oil pump repair/rework specifications and procedures. Harmony Machine Prod Inc
- [STC SE40CH](https://openairdocs.org/stc/SE40CH): Rebuilt modification of starter drive clutch assembly. Harmony Machine Prod Inc
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter. Aviation Development Corporation
- [STC SE8WE](https://openairdocs.org/stc/SE8WE): Installation of alternate oil sump. AD Aerospace, Inc
- [STC SE995GL](https://openairdocs.org/stc/SE995GL): Rebuilt modification of starter drive clutch assembly. Aerotech. Lists O-200 Series
- [STC ST00435AT](https://openairdocs.org/stc/ST00435AT): Overhaul/repair of the Delco starter adapter drive (P/N 1971890) used with Delco starters P/N's 11096656 and 1109660. Aerotech. Lists O-200 Series
- [STC SE09513SC](https://openairdocs.org/stc/SE09513SC): Installation and usage of Exxon 20W50 Multigrade aircraft engine oil conforming to Exxon Oil Formulation WS-3013. Exxon Company USA. Lists O-200 Series
- [STC SE1-201](https://openairdocs.org/stc/SE1-201): Installation of the Richter Aero Equipment Type B-4 or B-5 Temperature Probe. (O-360 SERIES (excl. A1C, C2B, C2D)). MidContinent Instru Co Inc. Lists O-200 Series
- [STC SE00164SE](https://openairdocs.org/stc/SE00164SE): Installation of Avglas components to modify carburetor air housing assemblies. McFarlane Aviation, Inc. Lists O-200 Series
- [STC SE01592AT](https://openairdocs.org/stc/SE01592AT): Modify the crankcase of the listed engines. Swords Don
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation
- [STC SE00262NY](https://openairdocs.org/stc/SE00262NY): Installation of Canadian Aero Manufacturing Pull Start Clutch, P/N 1971890-N or 1971890-M. Canadian Aero Manufacturing. Lists O-200 Series
- [STC SE977NE](https://openairdocs.org/stc/SE977NE): Installation of Canadian Aero Manufacturing Watson starter clutch P/N 641500-10, 641500-10-SO, 641500-15, 641500-15-SO, 641500-20, or641500-20-SO. Canadian Aero Manufacturing. Lists O-200 Series
- [STC SE154CE](https://openairdocs.org/stc/SE154CE): Engine oil pump repair/rework specifications and procedures. Allison James R. Lists O-200 Series
- [STC SE4315NM](https://openairdocs.org/stc/SE4315NM): Replacement of the original engine oil screen with an external mounted full flow oil adapter and spin-on filter. Timberman Allen E
- [STC SE8669SW](https://openairdocs.org/stc/SE8669SW): Installation of roller rocker arm. Performance Engineering
- [STC SE3208SO](https://openairdocs.org/stc/SE3208SO): Installation of replacement starter clutch assembly. Accessory Manufacture, Inc
- [STC SE2734CE](https://openairdocs.org/stc/SE2734CE): Continental P/N 530182, crankshaft is being replaced with crankshaft P/N AS530182 obtained by modification of Continental PC-60(Packette) engine crankshaft. Air Sports Inc
- [STC SE4768NM](https://openairdocs.org/stc/SE4768NM): Installation of a modified Marvel Model MA-3SPA carburetor. Hamilton David C
- [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP. Phillips Petroleum Co. Lists O-200 Series
- [STC SE1976SW](https://openairdocs.org/stc/SE1976SW): Manufacture of new cylinder barrels and rebarreling with original cylinder head. Gary Aerospace Corp. Lists O-200 Series
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines. Mattituck Airbase, Inc. Lists O-200 Series
- [STC SE2031CE](https://openairdocs.org/stc/SE2031CE): Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index and leaded autmotive gasoline, 88 minimum antiknock index(RON+MON)/2. Intermixing with aviation gasoline also approved. Petersen Aviation Inc
- [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines. ProTec. Lists O-200 Series
- [STC SE2791SW](https://openairdocs.org/stc/SE2791SW): Revised starter clutch. B C & J Enterprises. Lists O-200 Series
- [STC SE82WE](https://openairdocs.org/stc/SE82WE): Closing off of the oil outlet port of the main thrust bearing; installation of an O-200-B crank- shaft; modifying the front oil seal slinger flange; machining an already existing molded pad on the crankshaft to receive a side mounted fuel pump. Klein Harvey J
- [STC SE1396SW](https://openairdocs.org/stc/SE1396SW): Revise engine oil pick up system. Spinks M H Sr
- [STC SE44WE](https://openairdocs.org/stc/SE44WE): Use of Kling Aviation Oil, Specifications KL-100, KL-200 and KL-300 in Continental and Lycoming engines. Kling Oil Company

All 51: https://openairdocs.org/engine/rolls-royce-0-200-a/stcs.md

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