# Service difficulty reports: Cessna 150M A list on [Cessna 150M](https://openairdocs.org/model/cessna-150m.md). Newest first. General aviation reporting is voluntary. Page 1 of 5 · 210 reports - [SDR 2026FA0000089](https://openairdocs.org/sdr/2026FA0000089.md): Cylinder · fractured · Oct 11, 2025 · N63079 · Cessna 150M · Reciprocating Engine Cylinder Section > 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 NUMBER 4. THE UPPER SECTION OF THE CYLINDER BARREL SEPERATED FROM THE LOWER SECTION APPROXIMATELY FOUR - [SDR 2024FA0000285](https://openairdocs.org/sdr/2024FA0000285.md): Pump · contaminated · Apr 4, 2024 · N1975T · Cessna 150M · Vacuum System > OVER LAST 12 YEARS AND 500 HOURS OPERATING TIME N1975T HAS EXPERIENCED 5 FAILURES OF THE PUMP PN RAP215CC-9. IN EACH CASE EXCEPT LAST INSTALLATION A PROPERLY LICENSED FAA TECH FAILED TO FOLLOW RAPCO INSTALLATION INSTRUCTIONS INCLUDED WITH PUMP. THIS LEAD - [SDR 2022FA0000363](https://openairdocs.org/sdr/2022FA0000363.md): None · detached · Jul 20, 2022 · N1975 · Cessna 150M · Elevator Control System > OUTBOARD ELEVATOR HINGE ON RIGHT ELEVATOR MISSING. APPEARED TO HAVE BEEN CUT OFF MOST LIKELY DURING IMPROPER REPAIR ABOUT 20 YEARS AGO.. - [SDR 2020FA0000505](https://openairdocs.org/sdr/2020FA0000505.md): Skin · damaged · Nov 16, 2020 · N704WR · Cessna 150M · Rudder, Plate/Skin > DURING ANNUAL INSPECTION IT WAS NOTED THAT THE LEFT SIDE UPPER RUDDER HINGE AREA SHOWED SIGNS OF DAMAGE AND THE RIGHT HAND SIDE SHOWED SIGNS OF CRACKING. RUDDER WAS REMOVED FROM AIRCRAFT FOR CLOSER DETAILED INSPECTION. B INSPECTION REVEALED MORE DAMAGE TO PR - [SDR 2020FA0000106](https://openairdocs.org/sdr/2020FA0000106.md): Fairlead · misinstalled · Jan 29, 2020 · N3882V · Cessna 150M · Rudder Control System > AIRCRAFT DUE FOR ROUTINE 100 HOUR / ANNUAL INSPECTION. FOUND RIGHT HAND RUDDER FAIRLEAD TO BE INSTALLED UPSIDE DOWN AT FUSELAGE STATION 95, FUSELAGE FORMER WAS NEARLY COMPLETELY SEVERED DUE TO WEAR FROM RUDDER CABLE. - [SDR CA190625009](https://openairdocs.org/sdr/CA190625009.md): Plate · cracked · Jun 14, 2019 · Cessna 150M · Propeller Spinner Section > (CAN) DURING GROUND RUN MAINTENANCE OBSERVED SPINNER NOT RUNNING TRUE. SPINNER REMOVED AND FOUND BACK PLATE CRACKED. BACK PLATE REPLACED. (TC# 20190625009) - [SDR 2018FA0000317](https://openairdocs.org/sdr/2018FA0000317.md): Cylinder Head · separated · Jul 31, 2018 · N704UT · Cessna 150M · Reciprocating Engine Cylinder Section > NR 1 CYLINDER SHOWING SIGNS OF HEAD SEPARATION FROM BARREL AT TT 47.6. - [SDR 2018FA0000316](https://openairdocs.org/sdr/2018FA0000316.md): Cylinder Head · separated · Jul 31, 2018 · N704UT · Cessna 150M · Reciprocating Engine Cylinder Section > NR 2 CYLINDER SHOWING SIGNS OF HEAD SEPARATION FROM BARREL AT TT 16.5. - [SDR 2018FA0000314](https://openairdocs.org/sdr/2018FA0000314.md): Cylinder · separated · Jul 31, 2018 · N704UT · Cessna 150M · Reciprocating Engine Cylinder Section > 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 47.6 AND 16.5 RESPECTIVELY. - [SDR 2018FA0000065](https://openairdocs.org/sdr/2018FA0000065.md): Transmitter · failed · Feb 5, 2018 · N55332 · Cessna 150M · Fuel Quantity Indicator > RIGHT FUEL QUANTITY INDICATOR SHOWED TANK EMPTY AFTER REFUELING. DURING COURSE OF TROUBLESHOOTING, REMOVED FUEL QUANTITY TRANSMITTER. FLOAT WAS FOUND TO BE FLOODED. FLOAT HAD PREVIOUSLY BEEN REPLACED WITH USED COMPONENT DURING PAST REPAIR TO WING. LEVER ARM - [SDR 2016FA0000143](https://openairdocs.org/sdr/2016FA0000143.md): Cylinder Head · broken · Mar 25, 2016 · N63507 · Cessna 150M · Reciprocating Engine Cylinder Section > 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 BOSSES WERE FOUND BROKEN AND THE INTAKE AND EXHAUST ROCKER'S WERE NO LONGER OPENING THE VALVES. THE - [SDR CA151002004](https://openairdocs.org/sdr/CA151002004.md): Cap · failed · Oct 2, 2015 · Cessna 150M · Reciprocating Engine Power Section > (CAN) PILOT REPORTED ROUGH RUNNING ENGINE WITH SUBSEQUENT POWER LOSS AT CRUISE SETTING. FORCED LANDING IN FIELD UNEVENTFUL. INITIAL ENGINE INSPECTION REVEALED LOW COMPRESSION ON CYLINDER 1, CONSISTENT WITH INTAKE VALVE LEAK. CYLINDER REMOVED AT NEXT OCCASION - [SDR CA150923010](https://openairdocs.org/sdr/CA150923010.md): Crankshaft · damaged · Sep 22, 2015 · Cessna 150M · Reciprocating Engine Power Section > (CAN) END PLUG SEPARATED FROM CRANKSHAFT, FLOATED AROUND IN PROPELLER HUB. VIBRATION ONLY FELT BELOW 1200 RPM. - [SDR CA150225007](https://openairdocs.org/sdr/CA150225007.md): Spring · broken · Feb 17, 2015 · Cessna 150M · Rudder Control System > (CAN) PILOT NOTICED RUDDER DEFLECTION TO RT WITH NOSE WHEEL STRAIGHT DURING PREFLIGHT INSPECTION. INSPECTION FOUND THE LT RUDDER CABLE TENSIONING SPRING BROKEN. - [SDR CA140407011](https://openairdocs.org/sdr/CA140407011.md): Spring · missing · Apr 4, 2014 · Cessna 150M · Reciprocating Engine Cylinder Section > (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 WEAR PATTERNS ON THE VALVE SPRING SEATS, HAD BEEN OPERATED WITHOUT THIS SPRING FOR SOME TIME. THE LACK - [SDR T22R2014051600001](https://openairdocs.org/sdr/T22R2014051600001.md): Cylinder · cracked · Feb 17, 2014 · N9173U · Cessna 150M · Reciprocating Engine Cylinder Section > 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, NORMAL TAKEOFF, APPROXIMATELY 100 METERS PILOT FELT SOME ENGINE VIBRATIONS, SMELLED OIL IN COCKPIT, SAW - [SDR CA131111017](https://openairdocs.org/sdr/CA131111017.md): Transmitter · failed · Jun 14, 2013 · Cessna 150M · Fuel Quantity Sensor > (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 REPLACED NEW, FUNCTION CHECKED SERVICEABLE. - [SDR CA131111006](https://openairdocs.org/sdr/CA131111006.md): Transmitter · faulted · Jun 4, 2013 · Cessna 150M · Fuel Quantity Indicator > (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 WITH SERVICABLE UNIT, FUNCTION CHECKED SERVICABLE. - [SDR CA130429014](https://openairdocs.org/sdr/CA130429014.md): Tube · leaking · Apr 26, 2013 · Cessna 150M · Tire Tube > (CAN) TUBE DEVELOPED SMALL HOLE AT MANUFACTURING SEAM LINE LIKE PREVIOUSLY FAILED TUBES. - [SDR CA130422005](https://openairdocs.org/sdr/CA130422005.md): Tube · failed · Apr 21, 2013 · Cessna 150M · Tire Tube > (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 FOR 5.4 MONTHS OR 195.9 HOURS, AVERAGE FLIGHT TIME IS 1 HR, THUS TUBE ONLY HAD 196 CYCLES ON IT. - [SDR CA130419004](https://openairdocs.org/sdr/CA130419004.md): Tube · failed · Mar 26, 2013 · Cessna 150M · Tire Tube > (CAN) TUBE DEVELOPS SMALL HOLE THEN EVENTUALLY IN LIFE CYCLE FINDS ITSELF FLAT. - [SDR CA130406002](https://openairdocs.org/sdr/CA130406002.md): Tube · failed · Mar 11, 2013 · Cessna 150M · Tire Tube > (CAN) SMALL PIN HOLE TOP OF TUBE BETWEEN 2 SEAMS. COMPONENT HAS 7.53 MONTHS IN SERVICE. - [SDR CA130406001](https://openairdocs.org/sdr/CA130406001.md): Tube · punctured · Mar 11, 2013 · Cessna 150M · Tire Tube > (CAN) SMALL PIN HOLE FOUND. TIRE WENT FLAT MFG DEFECT. - [SDR CA130219004](https://openairdocs.org/sdr/CA130219004.md): Housing · cracked · Feb 19, 2013 · Cessna 150M · Reciprocating Engine Oil System > (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 OTHER OF ONE OF THE MOUNTING EARS. THE HOUSING WAS REPLACED WITH AN INSPECTED USED SERVICEABLE HOUS - [SDR CA130115016](https://openairdocs.org/sdr/CA130115016.md): Tube · failed · Jan 10, 2013 · Cessna 150M · Tire Tube > (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 CA121212006](https://openairdocs.org/sdr/CA121212006.md): Control Cable · frayed · Nov 21, 2012 · Cessna 150M · Rudder Control System > (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 CABLES REPLACED NEW, ALONG WITH ASSOCATED PULLEYS, RETURN SPRINGS AND ATTACHING HARDWARE. - [SDR CA121212003](https://openairdocs.org/sdr/CA121212003.md): Bushing · worn · Nov 20, 2012 · Cessna 150M · Ailerons > (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 THE BUSHING. WITH SLIGHT FOR AND AFT MOTION OF THE CONTROL YOKE WITH ONE HAND WILL CAUSE ONE TO SE - [SDR CA121119008](https://openairdocs.org/sdr/CA121119008.md): Exhaust Valve · failed · Nov 17, 2012 · Cessna 150M · Reciprocating Engine Cylinder Section > (CAN) EXHAUST VALVE FAILURE, CYLINDER HEAD SEPARATION. - [SDR CA130115012](https://openairdocs.org/sdr/CA130115012.md): Starter · failed · Nov 8, 2012 · Cessna 150M · Engine Starter > (CAN) UPON START UP OF ENGINE, STARTER FAILED ON FIRST ATTEMPT. STARTER FAILURE TROUBLESHOT TO DETERMINE THE CAUSE AND PROBLEM OF FAILURE. FAILURE FOUND TO BE STARTER ITS SELF. STARTER REMOVED FROM ENGINE AND REPLACED NEW, WITH NEW STARTER, NEW STARTER FUCN - [SDR QXEA2012041800328](https://openairdocs.org/sdr/QXEA2012041800328.md): Stringer Splice · corroded · Apr 18, 2012 · N714QX · Cessna 150M · Fuselage Main, Longeron/Stringer > STRINGER 30P, STRINGER SPLICE BETWEEN STA X-39.00 AND X -18.250 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801. DAMAGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4456. ALODINED, PRIMED AND PAINTED I - [SDR CA120417004](https://openairdocs.org/sdr/CA120417004.md): Piston Pin · worn · Apr 17, 2012 · Cessna 150M · Reciprocating Engine Power Section > (CAN) WHILE PERFORMING 100 HRS INSPECTION, POST OPENING INSPECTION OF OIL FILTER REVEALED ALUMINUM CHIPS IN FILTER. AFTER CONSULTING WITH APPROVED REPAIR SHOP, NR 2 & NR 4 CYLINDERS WERE REMOVED AND PISTON PIN ENDS WERE FOUND WITH METAL MISSING. CYLINDER WALL - [SDR QXEA2012041400325](https://openairdocs.org/sdr/QXEA2012041400325.md): Threshold · corroded · Apr 14, 2012 · N714QX · Cessna 150M · Fuselage Miscellaneous Structure > STUB FRAME FLANGE ANGLE BELOW PAX DOOR THRESHOLD HAS CORROSION OTBD OF STRINGER 25P AT STA X9.00. REMOVED FLANGE ANGLE IAW SRM 51-42-05-02-01. MATCH DRILLED NEW ANGLE, ALODINED AND INSTALLED STUB FRAME FLANGE ANGLE IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND - [SDR CA130116011](https://openairdocs.org/sdr/CA130116011.md): Altimeter · reads low · Mar 21, 2012 · Cessna 150M · Altimeter, Barometric/Encoder > (CAN) ALTIMETER FOUND TO BE REPORTING LOWER, OUT OF TOLERANCE, ALTITUDE READINGS FOR THE ALTIMETER AND COULDN`T BE RECALIBRATED. ALTIMETER REMOVED AND SERVICABLE UNIT INSTALLED. ALL PARAMETERS CHECKED SERVICABLE - [SDR CA111118007](https://openairdocs.org/sdr/CA111118007.md): Cylinder Head · leaking · Nov 15, 2011 · Cessna 150M · Reciprocating Engine Cylinder Section > (CAN) CYLINDER NR 4 FOUND TO HAVE OIL LEAK AT THE CYLINDER HEAD TO BARREL THREADS ROUGH RUNNING. REPORTED ON GROUND RUN DURING TAXI, WHILE ENGINE WAS HOT FROM PREVIOUS FLIGHT. - [SDR CA110915006](https://openairdocs.org/sdr/CA110915006.md): Exhaust Valve · stuck · Sep 14, 2011 · Cessna 150M · Reciprocating Engine Cylinder Section > (CAN) POOR & ROUGH RUNNING ENGINE. COMPRESSION CHECK COMPLETED. CTLS 2 AND 4 - NO COMPRESSION. VISUAL INSP OF COMBUSTION CHAMBER(S) - FOUND EXHAUST VALVE STUCK OPEN. CTLS NR 2 AND NR 4 REPLACED WITH NEW. OIL SCREEN INSPECTED, CLEAR. GROUND RUN, OPERATIO - [SDR CA110826011](https://openairdocs.org/sdr/CA110826011.md): Mount · cracked · Aug 25, 2011 · Cessna 150M · Engine Mount Section > (CAN) ENGINE MOUNT TUBE CRACKED AT NOSE GEAR OLEO UPPER ATTACH POINT- RT SIDE DIAGONAL TUBE FROM RT LOWER ENGINE MOUNT, TOO UPPER NOSE GEAR ATTACH POINT, AND LT LOWER DIAGONAL TUBE FROM LOWER LT FIRE WALL ATTACH POINT TO LOWER NOSE GEAR ATTACH POINT. (CRACKED - [SDR CA110419003](https://openairdocs.org/sdr/CA110419003.md): Universal Joint · broken · Apr 14, 2011 · Cessna 150M · Control Column Section > (CAN) ON A 50 HR INSPECTION THE CO-PILOT CONTROL COLUMN UNIVERSAL JOUNT WAS LOOSE. WHEN THE RUBBER SLEEVE WAS REMOVED, 1 OF THE UNIVERSAL JOINT PINS WAS FOUND BROKEN. THE RUBBER SLEEVE DID ITS JOB AND KEPT THE U-JOINT FROM COMING APART. THE U-JOINT WAS REPLAC - [SDR CA090409003](https://openairdocs.org/sdr/CA090409003.md): Fuel Sys · low pressure · Apr 5, 2011 · Cessna 150M · Engine Fuel Distribution > (CAN) ENGINE FAILURE ON APPROACH REPORTED BY PILOT, SUSPECT LOW FUEL. INVESTIGATING IF OTHER FACTORS CONTRIBURTED TO LOW FUEL CONDITION. ACFT FUEL DELIVERY AND STORAGE SYS INSPECTED NO ABNORMALITIES FOUND. ACFT FUEL QUANTITY INDICATION SYS VERIFIED ACCURATE - [SDR CA110202001](https://openairdocs.org/sdr/CA110202001.md): Oil System · low pressure · Oct 27, 2010 · Cessna 150M · Reciprocating Engine Oil System > (CAN) IFSD RT ENGINE OIL PRESSURE INDICATION DROPPED TO THE YELLOW AREA. PILOT REDUCED POWER AND IT CONTINUED TOWARDS THE RED. THE PILOT SHUTDOWN ENGINE AND LANDED WITHOUT INCIDENT. TROUBLESHOOTING IS ONGOING. - [SDR CA100809009](https://openairdocs.org/sdr/CA100809009.md): Bracket · cracked · Jul 16, 2010 · Cessna 150M · Elevator Structure > WHILE PILOT COMPLETED PRE-FLIGHT WALK AROUND, HE NOTICED THE ELEVATOR CONTROL NOT RESPONDING NORMALLY. FOUND BRACKET CRACKED. - [SDR CA100702010](https://openairdocs.org/sdr/CA100702010.md): Switch · burned · Jun 30, 2010 · Cessna 150M · Exterior Lighting > SWITCH AND WIRE CLEARLY EXHIBITING HEAT DAMAGE, SWITCH CASING MELTED TO AN EXTENT WHICH ALLOWED BOTH CONTACTS TO TOUCH EACH OTHER. - [SDR CA100621016](https://openairdocs.org/sdr/CA100621016.md): Switch · unserviceable · Jun 7, 2010 · Cessna 150M · Exterior Lighting > (CAN) UNKNOWN PART CYCLES, PART TSN AND PART TSO, HOWEVER THEY WERE CHANGED DUE TO AMENDED TIME CONTROL REQUIREMENT AS PER MANUFACTURER. SWITCH WELDED IN THE OFF POSITION, APPEARS SWITCH CANNOT HANDLE CIRCUIT REQUIREMENTS. SWITCH REPLACED WITH NEW. (TC# 2010 - [SDR CA091223006](https://openairdocs.org/sdr/CA091223006.md): Channel · cracked · Dec 11, 2009 · Cessna 150M · Service Doors > (CAN) DURING 200 HRS INSPECTED CRACK FOUND ON BOTH REAR DOOR POST CHANNEL LT P/N 0412533-3 2 CRACK AND RT P/N 0412533-4 1 CRACK, REST OF THE AREA INSPECTED NO OTHER DAMAGE FOUND. (TC NR 20091223006) - [SDR CA091019006](https://openairdocs.org/sdr/CA091019006.md): Cylinder · failed · Oct 12, 2009 · Cessna 150M · Reciprocating Engine Cylinder Section > (CAN) - STRONG SLOPE ALONG TAKEOFF (2000 RPM) - ASKED FOR PRIORITY LANDING - BURST VALVE EXHAUST CYL NR 2 WAS FOUND - REPLACED THE CYL NR 2 SAL0200-1A S/N 01344 WITH GASKET KIT AND NEW SPARK PLUG (2X) REM40E, RUN-UP CLOUT MAX RPM 2450 LEAK CHECK CLOUT AND OK, - [SDR 2009FA0000825](https://openairdocs.org/sdr/2009FA0000825.md): G Switch · inoperative · Sep 16, 2009 · N704FP · Cessna 150M · Emergency Locator Beacon > ELT G SWITCH, INOPERATIVE. (K) - [SDR CA090908005](https://openairdocs.org/sdr/CA090908005.md): Valve Stem · broken · Sep 8, 2009 · Cessna 150M · Reciprocating Engine Cylinder Section > DURING CRUISE UPON RETURN TO BASE ENG DROPPED ABOUT 300 RPM AND BEGAN TO RUN ROUGH, LANDING WITHOUT INCIDENT. UPON INVESTIGATION EXHAUST VALVE FACE HAD BROKEN INTO 2 PIECES AND VALVE STEM WAS BENT AND HAD BROKEN JUST BELOW THE TIP WITH ALL 3 PIECES BEING FOUND - [SDR CA090731004](https://openairdocs.org/sdr/CA090731004.md): Exhaust Valve · sticking · Jul 29, 2009 · Cessna 150M · Reciprocating Engine Cylinder Section > ENGINE RUNNING ROUGH, MISSING ETC. DP PERFORMED AND FOUND 0/80, FOUND STUCK VALVE IN OPEN POSITION. - [SDR CA090731003](https://openairdocs.org/sdr/CA090731003.md): Exhaust Valve · stuck · Jul 25, 2009 · Cessna 150M · Reciprocating Engine Cylinder Section > (CAN) EXHAUST VALVE STUCK IN OPEN POSITION. - [SDR CA090421008](https://openairdocs.org/sdr/CA090421008.md): Wire · melted · Apr 19, 2009 · Cessna 150M · Ice/Rain Protection System Wiring > (CAN) DURING ROLL AIR SPEED DID NOT BECOME ACTIVE, TAKEOFF ABORTED. CREW NOTICED PITOT HEAT ON WHEN THEY TOOK OVER THE ACFT. INVESTIGATION REVEALED THAT WIRING TO PITOT MAST (PWR FOR PITOT HEAT) HAD MELTED THE PITOT LINE. DAMAGED SECTION REMOVED AND PITOT LIN - [SDR CA090421007](https://openairdocs.org/sdr/CA090421007.md): Fuel Control · fire · Apr 16, 2009 · Cessna 150M · Fuel Control/Reciprocating Engines > (CAN) ENGINE EXPERIENCED BEFORE FIRE WHICH MELTED INDUCTION FILTER. FIRE EXTINGUISHING PROCEDURE UTILIZED CONTAMINATED INDUCTION SYS, INDUCTION SYS PULLED, CLEANED AND INSPECTED CORRECT. CARBURETOR REPLACED WITH SERVICEABLE UNIT AS A PRECAUTIONARY. ALL REASSEM Next page: https://openairdocs.org/model/cessna-150m/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '150M' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-150m/reports --- 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.