# Service difficulty reports: Continental 0-200 series

A list on [Continental 0-200 series](https://openairdocs.org/engine/continental-0-200-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 69 reports

- [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 2024FA0000138](https://openairdocs.org/sdr/2024FA0000138.md): Door Latch · malfunctioned · Jan 31, 2024 · Cessna 162 · Passenger/Crew Doors
  > AT CRUISE CONFIGURATION, AFTER 30 MINUTES OF FLIGHT WITH NO ISSUES, THE RIGHT CABIN DOOR OPENED. THE FORCE OF THE EVENT BROKE THE GLASS OF THE DOOR AND DAMAGES THE ALUMINUM AND FIBERGLASS, LEAVING THE DOOR IN SUCH A CONDITION THAT RENDERED IT UNABLE TO CLOSE A
- [SDR 2021FA0000036](https://openairdocs.org/sdr/2021FA0000036.md): Elt · false activation · Feb 7, 2021 · N6851 · Cessna 150F · Emergency Locator Beacon
  > ELT ACTIVATED WITHOUT ANY LOAD PLACED ON AIRCRAFT AT 3:21AM,FEB 5,2021 AIRCRAFT WAS IN HANGAR HAVING ANNUAL ACCOMPLISHED. WORK ON AIRCRAFT STOPPED FOR THE DAY AT 4:30PM ON FEB 4,2021,THE DAY PRIOR. AFCC TRIED TO CALL OWNER AT 3:30AM FEB5 BUT OWNER DID NOT AN
- [SDR 2020FA0000374](https://openairdocs.org/sdr/2020FA0000374.md): Exhaust Valve · stuck · Aug 17, 2020 · N9891B · Bbavia 7EC · Reciprocating Engine Cylinder Section
  > ON JULY 14, 2020 12:15 CDT N9891B A CHAMPION 7EC LOST POWER TO THE ENGINE, AND LANDED IN A FIELD NEAR PORT O'CONNER, TX. THE AIRCRAFT MAIN LANDING COLLAPSED AND THE ENGINE WAS PARTIALLY TORN FROM THE ENGINE MOUNT. THE BROKEN CARBURATOR BEGAN LEAKING FUEL WHI
- [SDR 2019FA0000292](https://openairdocs.org/sdr/2019FA0000292.md): Adc · defective · Aug 29, 2019 · N6038K · Cessna 162 · Flight Management Computing Hardware System
  > GSU 73 AIR DATA COMPUTER STOPS GIVING ALTITUDE AND SPEED INFORMATION TO THE GDU 370 DISPLAY AFTER 40 MINUTES OF FLIGHT. DID THIS THE LAST THREE FLIGHTS. CALLED GARMIN AND THEY DID NOT OFFER ANY HELP.
- [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 2018FA0000088](https://openairdocs.org/sdr/2018FA0000088.md): Safety Wire · damaged · Jan 8, 2018 · N5942G · Cessna 150K · Emergency Equipment
  > WHEN CLEANING UP THE ACCESSORY CASE FOUND THAT THE SAFETY WIRE THAT SECURES THE OIL PUMP BOLTS PN 22537 WAS WORN THROUGH ON ALL 4 BOLTS. REMOVED THE SAFETY WIRE WITH MY FINGERS. THE WIRE WAS WORN WHERE IT ENTERED THE HOLES IN THE BOLT HEADS. THERE DOES NOT
- [SDR 2016FA0000417](https://openairdocs.org/sdr/2016FA0000417.md): Cylinder · separated · Sep 9, 2016 · N10770 · Cessna 150L · Reciprocating Engine Cylinder Section
  > AIRCRAFT WAS IN NORMAL CRUISE WHEN THE PILOT HEARD A LOUD BANG FROM THE ENGINE, RESULTING IN A PARTIAL LOSS OF POWER. FORCED LANDING OFF-AIRPORT. EXAMINATION OF THE ENGINE REVEALED THAT THE NR 2 CYLINDER HAS BROKEN IN THE BARREL AREA. ENGINE PART TT IS UNKN
- [SDR 2013FA0000490](https://openairdocs.org/sdr/2013FA0000490.md): Throttle Cable · failed · Aug 2, 2013 · N168JA · Cessna 162 · Power Lever
  > DURING TOUCH-AND-GOES, AND WAS PULLING THE THROTTLE BACK FOR PATTERN MANEUVERS. THROTTLE CABLE CAME COMPLETELY OUT OF THE HOUSING INTO COCKPIT. LANDED ACFT UNEVENTFULLY. DURING INSPECTION OF ASSY, CABLE HAD BROKEN ONE STRAND THAT WAS WRAPPED AROUND BASE OF
- [SDR 2012FA0000828](https://openairdocs.org/sdr/2012FA0000828.md): Leaf Spring · fractured · Dec 14, 2012 · N1901Z · Cessna 150C · Main Landing Gear
  > LEFT MAIN LANDING GEAR FRACTURED & FAILED ON LANDING AT MID-POINT OF LEAF SPRING. SEVERE CORROSION NOTED ON LEAF SPRING SURFACES. CORROSION PRESENT IN INNER SURFACE OF FRACTURE. LEAF SPRINGS COATED WITH INCORRECT PRIMER (ZINC CHROMATE) AND NOT PAINTED WITH
- [SDR 2012FA0000324](https://openairdocs.org/sdr/2012FA0000324.md): Latch · failed · May 9, 2012 · N60524 · Cessna 162 · Passenger/Crew Doors
  > LEFT DOOR FWD LATCH FAILED TO ENGAGE AND OPENED IN FLIGHT CAUSING DOOR TO FOLD IN HALF.
- [SDR AOU2012F00000](https://openairdocs.org/sdr/AOU2012F00000.md): Mount · broken · Feb 17, 2012 · N52040 · Cessna 162 · Engine Mount Section
  > ENGINE MOUNT BROKEN AT WELD IN FLIGHT. ACFT HAD PROPSTRIKE 450 HOURS PRIOR TO INCIDENT AND MOUNT WAS INSPECTED AT THAT TIME WITH NO DEFECTS NOTED. BELIEVE NEW DESIGN AND INFERIOR WELD WITH INSUFFICIENT PENETRATION WAS CAUSE OF PROBLEM. 4 WASHERS ARE WELDED
- [SDR 2010FA0001124](https://openairdocs.org/sdr/2010FA0001124.md): Rod End · broken · Oct 8, 2010 · N3569L · Cessna 150F · Landing Gear Steering System
  > ON TAKEOFF ROLL, LT FWD NOSE STEERING ROD END FAILED ALLOWING NOSE GEAR TO TURN FULL LT RESULTING IN LOSS OF CONTROL OF ACFT. ACFT DEPARTED RUNWAY EDGE AND FLIPPED OVER CAUSING SUBSTANTIAL DAMAGE.
- [SDR CA090407005](https://openairdocs.org/sdr/CA090407005.md): Axle · broken · Mar 30, 2009 · Amtr CUBYACROTNER · Main Landing Gear Strut/Axle/Truck
  > (CAN) GEAR USED PA 18 SUPER CUB INSTALLED AT TIME ACFT WAS BUILT. 1,284.00 ON HOMEBUILT 1.2500 AXLE IS FITTED INSIDE 1.5 GEAR TUBE AILED AT WHAT APPEARS LIKE ROSETTE WELDS OPERATING ON WHEEL SKIS GEAR WHEEL APPEARED MISALIGNED INSPECTED (JAKED UP) FOUND BROKEN
- [SDR 2008FA0000927](https://openairdocs.org/sdr/2008FA0000927.md): Hose · contaminated · Dec 1, 2008 · N8450M · Cessna A150K · Engine Air Intake System
  > BEGAN NORMAL LANDING CHECK LIST INCLUDING CHECKING CARB HEAT. AFTER PULLING CARB HEAT ON, ENGINE DIED. TURNED OFF CARB HEAT & ENGINE RESTARTED ON ITS OWN WITHOUT PILOT INPUTS. CONTINUED PATTERN & GRADUALLY REAPPLIED CARB HEAT ON BASE AND FINAL. ON SHORT FI
- [SDR 2008FA0000086](https://openairdocs.org/sdr/2008FA0000086.md): Spar · corroded · Feb 15, 2008 · Cessna 150G · Wing Spar
  > WINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSP OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE AN3-21A ATTACHMEN
- [SDR 2008FA0000087](https://openairdocs.org/sdr/2008FA0000087.md): Spar · corroded · Feb 15, 2008 · N3816J · Cessna 150G · Fuselage Main, Frame
  > WINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSPECTION OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE AN3-21A ATT
- [SDR 2007FA0001011](https://openairdocs.org/sdr/2007FA0001011.md): Drain · leaking · Oct 25, 2007 · N274AC · Bbavia 7EC · Reciprocating Engine Oil System
  > INSTALLED QUICK DRAIN VALVE (OIL) ON NEW AIRCRAFT/ ENGINE. AIRCRAFT FLEW APPROX 1 HR, INITIAL FLIGHT TEST. VERY MINUTE OIL LEAK WAS NOTED FROM OIL QUICK DRAIN VALVE. REMOVED VALVE TO FIND VALVE SNAP RING IN OIL DRAINED FROM ENGINE, ALSO FOUND O-RING SPLIT.
- [SDR 2007FA0000891](https://openairdocs.org/sdr/2007FA0000891.md): Setscrew · mismanufactured · Sep 14, 2007 · N65LC · Amcnlg AL3 · Reciprocating Engine Cylinder Section
  > CHECKING ROCKER ARM SHAFT SET SCREWS AND TO ASSURE INTAKE AND EXHAUST ROCKER ARMS NOT SWITCHED IAW INFORMATION TO OWNERS FORM INTERNET OWNERS AIRCRAFT FORUM. CYLINDER NR 1, SN AC06HB070, SET SCREW AND ROCKER ARMS, OK. CYLINDER NR 2, SN AC06FA543, SET SCREW LO
- [SDR 2007FA0000842](https://openairdocs.org/sdr/2007FA0000842.md): Rocker Shaft · loose · Sep 7, 2007 · N977CC · Reciprocating Engine Cylinder Section
  > IAW OWNERS REQUEST, REMOVED ALL (4) ROCKER COVERS TO INSPECT THE ROCKER SHAFT AND SET SCREWS. AFTER REMOVING THE ROCKER COVERS. FOUND ALL(4) SET SCREWS LOOSE AND ALL (4) SHAFTS MOVED TOWARD THE INTAKE SIDE OF THE BOSSES. NONE HAVE CUT THE ROCKER COVERS YET,
- [SDR CA061018007](https://openairdocs.org/sdr/CA061018007.md): Piston · cracked · Oct 11, 2006 · Amtr CUBYACROTNER · Reciprocating Engine Power Section
  > (CAN) ENGINE WAS TORN DOWN FOR INSPECTION DUE TO SMALL AMOUNT NON FERROS METAL IN FILTER. ENGINE TIME 2,707 HOUR. FRONT BEARING SLIGHT WEAR AND FLAKING (NORMAL FOR HIGH TIME ENGINE). NR 1 PISTON SKIRT CRACKED AT 1,100 HOURS. NOTE: THIS IS THE 4TH PISTON T
- [SDR 2006FA0001009](https://openairdocs.org/sdr/2006FA0001009.md): Carburetor · failed · Sep 23, 2006 · N7870Z · Cessna 150C · Fuel Control/Reciprocating Engines
  > ENGINE STOPPAGE ON FINAL DUE TO CARBURATOR FLOODING, SUSPECT STUCK FLOAT. REMOVED UNIT AND SENT BACK TO MANUFACTURE FOR INSPECTION. THIS CARBURETOR WAS (FACTORY REBUILT) 1 YEAR EARLIER AND HAD LESS THAN 55 HOURS TT. FUEL WAS FOUND SPILLING OUT OF COWLING WH
- [SDR 2006FA0000757](https://openairdocs.org/sdr/2006FA0000757.md): Elt · inoperative · Aug 4, 2006 · N5896G · Cessna 150K · Emergency Locator Beacon
  > THIS IS ONE OF THE ELT`S THAT USES DATED FLASHLIGHT BATTERIES. THE BATTERIES ARE STILL IN DATE BUT OFTEN WE FIND THAT THE BATTERIES ARE LEAKING OR DEAD BEFORE THE EXPIRATION DATE. RECOMMEND THAT THE BATTERIES ARE CHANGED AT EACH ANNUAL TO CORRECT THIS PROBLE
- [SDR 2006FA0000072](https://openairdocs.org/sdr/2006FA0000072.md): Wire · shorted · Oct 15, 2005 · N601KF · Cndair CL6013A · Stabilizer System Wiring
  > WHILE TROUBLESHOOTING INTERMITTENT UPPER BEACON CIRCUIT BREAKER FAULT, DISCOVERED LT ELEVATOR CONTROL CABLE HAD TORN THROUGH WIRING CONDUIT IN VERTICAL STABILIZER. THE CABLE WORE THROUGH THE CONDUIT AND SHORTED OUT THE WIRING FOR THE UPPER BEACON. REPAIRED W
- [SDR 2005FA0001201](https://openairdocs.org/sdr/2005FA0001201.md): Rotor Shaft · sheared · Aug 13, 2005 · N18583 · Cessna 150L · AC Generator-Alternator
  > ALTERNATOR SHAFT SHEARED AT BEARING LOCATION. DRIVE GEAR, BUSHINGS, RETAINER AND COUPLING ASSEMBLY ROLLED BETWEEN ENGINE ACCESSORY CASE AND DRIVE GEAR. THE SHAFT HAD BEEN PREVIOUSLY CRACKED OVER 50 PERCENT PRIOR TO FAILURE. (K)
- [SDR 2005FA0000814](https://openairdocs.org/sdr/2005FA0000814.md): Piston · cracked · May 2, 2005 · N26DL · Cessna A185F · Reciprocating Engine Power Section
  > REMOVED CYLINDERS ON A FRESHLY OVERHAULED ENGINE PRIOR TO RUNNING AND FOUND A 3 INCH CRACK AROUND THE OIL RING LANDING. (K)
- [SDR 2005FA0000834](https://openairdocs.org/sdr/2005FA0000834.md): Float · bent · Apr 30, 2005 · N3691T · Tcraft F19 · Fuel Control/Reciprocating Engines
  > ENG QUIT DURING TAKEOFF AT APPROX 300-500 AGL. DURING EXAM OF ENG COMPONENTS, IT WAS NOTED ADVANCE POLYMAR FLOAT WAS BENT AWAY FROM THE FLOAT AT APPROX 45 DEGREE ANGLE. THIS CONDITION WOULD LEAD TO THE FLOW INTO THE CARBURETOR. PRECISION SIL MS-4 REV 1 ADDR
- [SDR 2005FA0000609](https://openairdocs.org/sdr/2005FA0000609.md): Mount · cracked · Apr 22, 2005 · N63581 · Cessna 150M · Engine Mount Section
  > 100 HOUR INSPECTION, RT LOWER ENGINE MOUNT TUBE CRACKED. CRACK LOCATED WITHIN 1 INCH OF NOSE WHEEL STRUT SUPPORT CRACK,.7500 INCH IN LENGTH AROUND CIRCUMFERENCE OF TUBE. REPLACED MOUNT. (K)
- [SDR 2005FA0000348](https://openairdocs.org/sdr/2005FA0000348.md): Bracket · inoperative · Mar 18, 2005 · N1918Z · Cessna 150C · Empennage Structure
  > (1) RIVET SHEARED AND BRACKET ROTATED, PARTIALLY. THIS WAS CAUSED BY FLAP CABLES BEING RIGGED TOO TIGHT. THIS CAUSED A TWIST IN THE CABLES ALLOWING (1) CABLE TO RIDE UP AND OVER THE OTHER CAUSING IT TO COME OFF AN210-2A PULLEY. THE PILOT REPORTED GREAT DIFF
- [SDR 2005FA0000350](https://openairdocs.org/sdr/2005FA0000350.md): Exhaust Valve · stuck · Mar 9, 2005 · N6627F · Cessna 150F · Reciprocating Engine Cylinder Section
  > NR 3 CYLINDER HAS A STUCK EXHAUST VALVE. UPON CYLINDER REMOVAL IT WAS FOUND THAT THE VALVE HEAD WAS MUSHROOMED AND THE ROCKER ARM WAS ALSO DAMAGED. THIS CAUSED CONCERN DUE TO THE FACT THAT THE CYLINDER ONLY HAD 174.1 TOTAL HOURS SINCE IT WAS PURCHASED NEW.
- [SDR 2005FA0000174](https://openairdocs.org/sdr/2005FA0000174.md): Nut Plate · worn · Feb 14, 2005 · N901SW · Cessna 150D · Rudder Structure
  > UPPER RUDDER PIVOT BOLT BACKED OUT OF SELF-LOCKING NUTPLATE AT UPPER RUDDER PIVOT ATTACH AND PIVOT POINT WHILE IN FLIGHT, RUDDER WAS RIPPED FROM THE LOWER BELLCRANK CONTROL AND DEPARTED AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. RUDDER WAS RECOVERED AND THE
- [SDR 2005FA0000363](https://openairdocs.org/sdr/2005FA0000363.md): Bolt · worn · Jan 17, 2005 · N901SW · Cessna 150D · Fasteners
  > TOP RUDDER HINGE BOLT LOOSENED FROM THE SELF LOCKING NUT PLATE AND CAME OUT CAUSING THE RUDDER ASSEMBLY TO DETACH FROM THE AC COMPLETELY DURING FLIGHT AT 2000 AGL. THIS BOLT SHOULD HAVE SOME TYPE OF RETAINING MECHANISM IN ADDITION TO THE SELF LOCKING NUT PLAT
- [SDR 2008FA0000716](https://openairdocs.org/sdr/2008FA0000716.md): Spar · delaminated · Sep 29, 2004 · N885CT · Diamon DA20C1 · Standard Practices/Structures
  > DURING THE 6000 HR INSPECTION, DELAMINATION FOUND IN THE TOP AFT CORNERS OF THE SPAR BRIDGE, BOTH SIDES. AFTER FURTHER INVESTIGATION BY FACTORY PERSONNEL, CRACKS WERE FOUND DOWN THROUGH THE DIFFERENT LAYERS OF GLASS NOT THROUGH THE CARBON FIBER. RECOMMEND THAT
- [SDR 2004FA0000751](https://openairdocs.org/sdr/2004FA0000751.md): Windshield · departed · Aug 3, 2004 · N4760X · Cessna 150G · Flight Compartment Windows
  > SECTION OF WINDSHIELD DEPARTED AIRCRAFT IN FLIGHT. WINDSHIELD HAD BEEN REPAIRED 7/15/00 IAW AC43.131B CHAPTER 3 SECTION 4, BUT NO REINFORCEMENT WAS EVIDENT ON PART REMAINING IN AIRCRAFT. HOW WINDSHIELD INSTALLED. THIS COULD HAVE BEEN PREVENTED IF NEW WINDSH
- [SDR CHQA000525](https://openairdocs.org/sdr/CHQA000525.md): Bulb · inoperative · Jul 27, 2004 · N281 · Emb EMB145ER · Emergency Lighting
  > THE LT SIDE OVERWING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-07. OPS CHECK IS GOOD.
- [SDR 2004FA0000369](https://openairdocs.org/sdr/2004FA0000369.md): Main Bearing · separated · Apr 29, 2004 · N2586J · Cessna 150E · Reciprocating Engine Power Section
  > AFT THRUST FACES OF BOTH FRONT MAIN BEARING HALVES WERE SEPARATED FROM BEARING. THIS IS A ONE PIECE STYLE THRUST/MAIN BEARING. PROBLEM FOUND DURING OVERHAUL, NO INDICATIONS OF FAILURE NOTED BEFORE DISASSEMBLY. NO DAMAGE TO CASE OR CRANKSHAFT.
- [SDR 2004FA0000159](https://openairdocs.org/sdr/2004FA0000159.md): Hinge Pin · broken · Dec 31, 2003 · N714MG · Cessna 150M · Passenger/Crew Doors
  > DURING A 100 HOUR INSPECTION, THIS BROKEN DOOR HINGE PIN WAS FOUND. FIND MANY OF THESE PINS BROKEN.(K) (NE01200402925)
- [SDR 2003FA0001279](https://openairdocs.org/sdr/2003FA0001279.md): Frame · cracked · Dec 19, 2003 · N1YU · Cessna 150M · Vertical Stabilizer
  > CRACKED FRAME AT TB/VERTICAL FIN SPAR JUNCTION. THIS IS THE SECOND SHIP WITH AN IDENTICAL CRACK THAT HAS BEEN SEEN IN THE LAST 90 DAYS. THE MFG SRM DETAILS THE REQUIRED REPAIRS. DETECTION IS POSSIBLE USING BRIGHT LIGHT AND MIRROR, OR BY DIRECT OBSERVATION. A
- [SDR 2003FA0001209](https://openairdocs.org/sdr/2003FA0001209.md): Skin · corroded · Nov 4, 2003 · N8006S · Cessna 150F · Fuel Storage
  > LOWER TANK SKINS CORRODED THROUGH IN STRAINER ASSEMBLY SUMP. CORROSION NOTED IN OTHER AREAS OF TANK LOWER SURFACE CONSISTENT WITH STANDING BEADS OF WATER. CORROSION NOTED AROUND FUEL DRAIN VALVE PAD. STRAINER ASSEMBLY SUMP IS LOW POINT IN THE TANK AND HAS N
- [SDR 2003FA0001178](https://openairdocs.org/sdr/2003FA0001178.md): Caliper · corroded · Oct 30, 2003 · N427JW · Cessna 150L · Landing Gear Brake System
  > LT BRAKE CALIPER REMOVED AND INSPECTION OF PART FOUND CORROSION AND PITTING ON CALIPER PISTON WALLS. PISTON WAS BINDING WHEN MOVED. THE PISTON WOULD NOT MOVE FREELY WITHIN CALIPER HOUSING.
- [SDR R142003F00002](https://openairdocs.org/sdr/R142003F00002.md): Caliper · corroded · Oct 30, 2003 · N427JW · Cessna 150L · Landing Gear Brake System
  > LEFT BRAKE CALIPER REMOVED AND INSPECTION OF PART FOUND CORROSION AND PITTING ON CALIPER PISTON WALLS. PISTON WAS BINDING WHEN MOVED. THE PISTON WOULD NOT MOVE FREELY WITNIN CALIPER HOUSING. INSTALLED NEW LEFT BRAKE CALIPER.
- [SDR 2003FA0000583](https://openairdocs.org/sdr/2003FA0000583.md): Line · corroded · May 5, 2003 · N73017 · Cessna 140 · Engine Oil Pressure
  > THE OIL INDICATOR LINE WAS WORN COMPLETELY THROUGH. THE CIRCUMSTANCES UNDER WHICH IT OCCURED, WAS DURING FLIGHT. PROBABLE CAUSE: OLD AND CORRODED. RECOMMENDATION TO PREVENT RECURRENCE: CLOSER INSPECTIONS OF ENGINE, AND ENGINE PARTS/ COMPONENTS.
- [SDR 2003FA0000199](https://openairdocs.org/sdr/2003FA0000199.md): Spinner · damaged · Feb 17, 2003 · N11418 · Cessna 150L · Propeller Spinner Section
  > PROP REMOVED TO FACILITATE REPLACEMENT OF ENG CRANKSHAFT SEAL. REMOVAL OF SPINNER, SEVERE WEAR AND FRETTING OF INNER SURFACE WAS NOTED WHERE FWD BULKHEAD (PN04500503) CONTACTS SPINNER. AFTER REMOVING PROP, PROP MOUNT BOLTS WERE OVERTORQUED, RESULTING IN DEFO
- [SDR H9Q2003F00000](https://openairdocs.org/sdr/H9Q2003F00000.md): Elt · misoverhauled · Feb 17, 2003 · N11418 · Cessna 150L · Emergency Locator Beacon
  > DURNG THE COURSE OF AN ANNUAL INSPECTION, ACCESS WAS GAINED TO THE ELT FOR TESTING AND BATTERY DATE VERIFICATION. THE FOLLOWING DISCREPANCIES WERE IMMEDIATELY OBVIOUS. THE UNIT HAD BEEN CONNECTED TO THE EXISTING SYSTEMS ANTENNA. THE REMOTE PANEL INDICATOR S
- [SDR Z372003F00000](https://openairdocs.org/sdr/Z372003F00000.md): Magneto · failed · Jan 23, 2003 · N4015J · Piper PA28181 · Magneto/Distributor
  > PILOT REPORTED DEAD MAGNETO IN RT POSITION. REMOVED RT MAGNETO FROM ENGINE. FOUND COIL SHAFT SEVERED AT CAM LIFTER LOBE POSITION. SUSPECT SOME METALLURGICAL DEFECT IN SHAFT. REPLACED MAGNETO WITH NEW. FUNCTIONALLY CHECKED GOOD.
- [SDR 2002FA0001208](https://openairdocs.org/sdr/2002FA0001208.md): Transistor · unapproved part · Oct 16, 2002 · N19255 · Cessna 150L · ATC Transponder System
  > TRANSPONDER FAILURE: IDENT PULSE PRESENT AND REPLY LAMP LIT WHEN UNIT HOT. (NOT COMMANDED) FOUND Q22 AND ASSORTED CIRCUIT VERY TEMPERATURE SENSITIVE. REPLACED COMPONENTS AND FOUND Q22 NOT STANDARD PART. PART INSTALLED AN ECG TPE 123. PART REPLACED WITH A
- [SDR CQ92002F00000](https://openairdocs.org/sdr/CQ92002F00000.md): Metering Valve · scored · Sep 20, 2002 · N714GM · Cessna 150M · Fuel Control/Reciprocating Engines
  > A/C WAS ON TRAINING FLIGHT, AT 4000 FT, INSTRUCTOR DEMONSTRATED LEANING PROCESS BY PULLING OUT MIXTURE CONTROL UNTIL ENGINE ROUGHNESS JUST OCCURRED. ENRICHENING MIXTURE HAD NO EFFECT, AND A EMERGENCY LANDING WAS MADE WITHOUT POWER. INITIAL INSP SHOWED THAT
- [SDR 2002FA0001238](https://openairdocs.org/sdr/2002FA0001238.md): Hinge · cracked · Sep 13, 2002 · N986CT · Diamon DA20C1 · Rudder Structure
  > DURING 100 HOUR INSPECTION MECHANIC DISCOVER THAT THE LOWER LEFT CORNER OF THE LOWER RUDDER HINGE SUPPORT TOWER HAD A CRACK. EVIDENCED BY LINE OF BROWN RUST RESIDUE VISIBLE AGAINST THE BLACK PAINT, AND ADJACENT TO THE WELD. PART WAS REPLACED.
- [SDR 2002FA0000884](https://openairdocs.org/sdr/2002FA0000884.md): Bulkhead · cracked · Jul 23, 2002 · N88808 · Cessna 150M · Fuselage Main, Bulkhead
  > CRACKS THROUGH BULKHEAD. TIE DOWN PROBLEMS/ LANDINGS TAIL LOW. REPETITIVE TAIL LOW LANDINGS.
- [SDR 2002FA0000356](https://openairdocs.org/sdr/2002FA0000356.md): Spar · damaged · Mar 18, 2002 · N9571S · Bbavia 7ECA · Wing Spar
  > WHILE RECOVERING WINGS FOUND NUMEROUS LOOSE RIBS THAT HAD RUBBED GROVES IN THE SPARS. SOME SMALL CRACKS ORIGINATING FROM THE NAIL HOLES. AIRPLANE HAD BEEN USED IN AEROBATICS. REPLACED ALL FOUR WING SPARS.

Next page: https://openairdocs.org/engine/continental-0-200-series/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 engine_model_key = 'O200'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/continental-0-200-series/reports

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