Cessna 150F

Service difficulty reports · 47

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duckdb -csv -c "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 = '150F'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2022FA0000437Transmitter · defectiveTEST, 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. REMOVED FUEL QUANTITY TRANSMITTER FOR FUNCTIONAL TESTING. FOUND TWO RUB SPOTS ON FLOAT, REASON FOAug 8, 2022 · N8057F · Cessna 150F · Fuel Quantity SensorSDR 2022FA0000606Magneto · noneTOOKOFF ON RUNWAWY ALL PARAMETERS WERE NORMAL. AIRSPEED, RATE OF CLIMB, AND OIL PRESSURE PREFORMANCE CHECK GOOD. AFTER PASSING BETWEEN 1000 TO 1200 FEET, I SAW THE ENGINE HESITATED APPROXIMATELY 1 TO 2 SECONDS. AFTER THAT, THE ENGINE CUT OFF. PERFORMED AN EMEROct 17, 2021 · N8087S · Cessna 150F · Ignition SystemSDR 2021FA0000036Elt · false activationELT 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 ANFeb 7, 2021 · N6851 · Cessna 150F · Emergency Locator BeaconSDR 2012FA0000458Rod End · fracturedPOST ACCIDENT INSPECTION OF THE NOSE GEAR STEERING ASSY SHOWED THAT THE BEARING ROD END WAS BROKEN AT THE NUT. THE COLORING AT THE FRACTURE WAS 1 QUARTER SHINY AND 3 QUARTERS DULL DARK GREY. BOTH THE LT AND RT ROD ENDS FRACTURED UPON LANDING.Jul 5, 2012 · N524CC · Cessna 150F · Landing Gear Steering SystemSDR 2012FA0000244Seal · deterioratedFOUR NEW CYLINDER ASSEMBLIES WERE INSTALLED. AFTER GROUND RUNS AND 1 BREAK IN FLIGHT THE ENGINE WAS INSPECTED. DURING THE INSPECTION THE PUSHROD TUBE SEAL WERE FOUND TO HAVE LARGE CRACKS AND SPLITS. THE SEALS AND GASKETS WERE SUPPLIED WITH THE CYL KITS FROMMar 8, 2012 · N3132X · Cessna 150F · Reciprocating Engine Cylinder SectionSDR 2011FA0000167Bellcrank · brokenDURING ANNUAL INSP, FOUND ELEVATOR BELLCRANK PN 0411258 WITH A BEARING THAT CAME LOOSE FROM IT'S SWAGED MOUNTING. THE ONLY THING THAT KEPT IT FROM FALLING OUT COMPLETELY WAS THE FORK ROD THAT CONNECTS TO THE CONTROL COLUMN. ONCE THIS ROD WAS REMOVED THE BEARMar 10, 2011 · N3063X · Cessna 150F · Elevator Control SystemSDR 2010FA0001124Rod End · brokenON 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.Oct 8, 2010 · N3569L · Cessna 150F · Landing Gear Steering SystemSDR 2009FA0000465Tee Fitting · crackedDURING COMPLIANCE OF AD 2004-19-06, DETECT AND CORRECT FATIGUE CRACKING OR CORROSION OF THE FAIL SAFE STRAPS (S/B 767-53A0100) A CRACK WAS FOUND IN BOTH SIDES. THE RT T-FITTING WAS CRACKED FROM THE FWD SIDE OF THE BOLT HOLE APPROXIMATELY 22 DEGREES ABOVE HORIMay 1, 2009 · N6738F · Cessna 150F · Fuselage Miscellaneous StructureSDR CA090417001Control Cable · interferenceDURING DAILY PREFLIGHT INSPECTION RUBBING SOUNDS HEARD UNDER CABIN FLOOR WHEN MOVING CONTROL YOLK LEFT AND RIGHT (ROLL AXIX). INVESTIGATION OF SOUND REVEALED THAT TWO SCREWS (P/N S1021Z8-10) HOLDING STAINLESS STEEL SCUFFBOARD PLATE (P/N 04130264-4) TO CABIN FApr 16, 2009 · Cessna 150F · Aileron Control SystemSDR 2007FA0000479Seat · crackedSEAT PAN WAS FOUND CRACKED AT THE FORWARD END OF PILOTS OB SEAT RAIL STIFFENER, APPROXIMATELY 1 NR LONG ACROSS SCREW HOLES. STIFFENER PN 0411546-1 WAS ALSO CRACKED AT CUTOUT FOR FUEL LINE. TOTAL AIRFRAME TIME UNKNOWN, BUT GREATER THAN 1300 HOURS. THESE CRACKS May 16, 2007 · N8095S · Cessna 150F · Flight Compartment EquipmentSDR 2006F00013Cylinder Head · crackedECI CYLINDER NR 2 AND NR 6 CRACKED HEAD. NR 6 HAS HOLE BLOWN THROUGH BREAKING COOLING FINS AND BURNED BAFFLE. ROUGHLY 650 HOURS SINCE NEW ECI CYLINDERS INSTALLED ON OVERHAULED ENGINE, 2 OTHER ECI CYLINDERS WERE CHANGED AT 600 HOURS FOR SAME THING.Mar 8, 2006 · N8295S · Cessna 150F · Reciprocating Engine Cylinder SectionSDR CA060303014Stop Fitting · failedSDA AL-2000-04 CF-2000-20R2 SEB 01-1 COMPLETED, NO EVIDENCE OF JAMMING OR RUBBING ON EITHER RUDDER STOPS.Jan 31, 2006 · Cessna 150F · Rudder Control SystemSDR CA060203005Stop · failedNO JAMMING OR EVIDENCE OF SEE ON EITHER RUDDER STOPS.Jan 31, 2006 · Cessna 150F · Rudder Miscellaneous StructureSDR 2005FA0000350Exhaust Valve · stuckNR 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. Mar 9, 2005 · N6627F · Cessna 150F · Reciprocating Engine Cylinder SectionSDR 2004FA0000259Cylinder · brokenAIRCRAFT WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING AFTER TOTAL LOSS OF ENGINE POWER. INVESTIGATION SHOWED THE CYLINDER HAD COMPLETELY SEPARATED IN THE MIDDLE WHILE IN FLIGHT, CAUSING THE TOTAL LOSS OF POWER.Feb 7, 2004 · N8745S · Cessna 150F · Reciprocating Engine Cylinder SectionSDR 2003FA0001209Skin · corrodedLOWER 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 NNov 4, 2003 · N8006S · Cessna 150F · Fuel StorageSDR 2002FA0000411Magneto · failedINSTALLED NEW CONDENSER DURING MAGNETO INSPECTION. RUN-UP WAS NORMAL. FULL POWER DURING TAKE-OFF SHOWED ROUGH RUNNING ENGINE. FURTHER INSPECTION OF MAGNETO REVEALED THAT NEW M3064 CONDENSER HAD FAILED.Jan 15, 2002 · N3539L · Cessna 150F · Magneto/DistributorSDR 2001FA0000681Bulkhead · crackedSINCE MFG. WENT TO PLASTIC BULKHEAD, THEY CRACK ABOUT EVERY 200 HOURS.Nov 26, 2001 · N6937F · Cessna 150F · Fuselage Main, BulkheadSDR AUS20010609Cylinder · cracked(AUS) ENGINE CYLINDER ROCKER SHAFT SUPPORT CRACKED AND SEPARATED FROM CYLINDER HEAD.May 25, 2001 · Cessna 150F · Reciprocating Engine Cylinder SectionSDR CA010409019Bracket · cracked(CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS. ALSO SDA AV-2000-06. AFFTER REMOVAL OF BRACKET ALSO FOUND REAR SPAR REINFORCEMENT P/N 0432001-15 CRACKED (HOLES ARE ALSO ELONGATED) ALONG TOPSIDE, AFTER REMOVAL OF REAR SPAR. REINFORCEMENT BOTH LMar 21, 2001 · Cessna 150F · Horizontal Stabilizer StructureSDR AU001235Piston · cracked(AUS) NR 1, NR 2 AND NR 4 CYLINDER PISTONS CRACKED BETWEEN OIL HOLES. THEPISTONS ARE MANUFACTURED BY WELLWORTH CASTING NUMBER A470102 AND ARE DIFFERENT TO THE CONTINENTAL MANUFACTURED PISTON IN HAVINGTEN OIL HOLES UNDER THE OIL RING WHERE CONTINENTAL PISTONS Dec 29, 2000 · Cessna 150F · Reciprocating Engine Cylinder SectionSDR AU001234Gasket · misinstalled(AUS) NR 3 CYLINDER EXHAUST GASKET INCORRECTLY FITTED ON ONLY ONE STUD.DURING TIGHTENING OF THE EXHAUST THE FLANGE CRACKED AS WELL ASTHE WELD BETWEEN THE FLANGE AND THE PIPE. LT MUFFLER BAFFLE PIPEALSO ERODED.Dec 29, 2000 · Cessna 150F · Engine Exhaust SystemSDR AU000797Fitting · out of adj(AUS) AIRCRAFT MAIN PLANE ATTACHMENT FITTING CONCENTRIC BUSHES OUT OF ADJUSTMENT CAUSING AIRCRAFT TO ROLL TO THE LEFT. LEFT WING WAS UNABLE TO BE ADJUSTED AS THE BUSH WAS FOUND TO BE IN THE MAXIMUM POSITION. THE ADJUSTMENT HAD TO BE CARRIED OUT ON THE RIGHT WSep 4, 2000 · Cessna 150F · Wing, Attach FittingsSDR AU000796Damper · faulty(AUS) SHIMMY DAMPER LOW ON FLUID. ON FURTHER INVESTIGATION THE FOLLOWING COMPONENTS WERE FOUND TO BE DAMAGED: 1. HEAD BEARING P/N 0542102-3. 2. ROLL PIN P/N NAS 561P4-143. RING RETAINER P/N MS16625-1118. DAMPER WAS ATTACHED BY TWO FULLY THREADED METRIC Sep 4, 2000 · Cessna 150F · Shimmy DamperSDR AU000795Cap · cracked(AUS) ENGINE COWL NOSE CAP CRACKED. CRACK LENGTH 100 M (4 INCHES). NOSE CAP HAD BEEN ILLEGALLY REPAIRED USING A FIRE EXTINGUISHER DATE PLATE, POP RIVETS AND LIQUID NAILS. UNAPPROVED REPAIR. (X)Sep 4, 2000 · Cessna 150F · Engine Cowling SystemSDR AU000794Gauge · unserviceable(AUS) ARTIFICIAL HORIZON, DIRECTING GYRO AND CYLINDER HEAD TEMPERATUREGAUGE UNSERVICEABLE. UNSERVICEABLE INSTRUMENTS NOT PLACARDED IAW CAO 20.18.10. S TANDBY COMPASS HAD 23 DEGREES ERROR ON WEST. (X)Sep 4, 2000 · Cessna 150F · Attitude and Direction Data SystemSDR AU000793Seat · seized(AUS) PILOT AND COPILOT SEAT ROLLERS SEIZED. COPILOT''S SEAT RELEASE ROD BENT AND FOULING ON THE STRUCTURE BENEATH THE SEAT PREVENTING THE SEAT FROM LOCKING. PILOT''S SEAT LEFT SEAT RAIL CRACKED AT INBOARDFORWARD ATTACHMENT SKIN. (X)Sep 4, 2000 · Cessna 150F · Flight Compartment EquipmentSDR AU000792Plate · inaccurate(AUS) ENGINE DATA PLATE NOT STAMPED FOR COMPLIANCE WITH AD/CON/75. (X)Sep 4, 2000 · Cessna 150F · Placards and MarkingsSDR AU000791Seal · deteriorated(AUS) FUEL STORAGE SYSTEM SEALS AND GASKETS DETERIORATED. SEALS AFFECTED: 1. FUEL TANK GASKETS DETERIORATED. 2. FUEL CAP SEALS DETERIORATED. 3. LEFT AND RIGHT FUEL TANK DRAIN VALVE SEALS DETERIORATED. (X)Sep 4, 2000 · Cessna 150F · Fuel StorageSDR AU000790Seal · damaged(AUS) WHEEL BEARING SEALS DAMAGED AND/OR FELT MISSING. WHEEL NUT SPLIT PIN TAILS NOT BENT OVER. (X)Sep 4, 2000 · Cessna 150F · Wheel/Ski/FloatSDR AU000789Brake Assy · corroded(AUS) BRAKE ASSEMBLY BACK PLATES P/N 74-10 AND PRESSURE PLATES P/N 73-11 BADLY CORRODED. BRAKE LININGS CRACKED. ONE BRAKE BLEEDER SCREW BROKEN AND BOTH BRAKER BLEEDER SEAT HEXAGONALS COMPLETELY ROUNDED. BRAKE SEALS LEAKING. (X)Sep 4, 2000 · Cessna 150F · Landing Gear Brake SystemSDR AU000787Seat Belt · misinstalled(AUS) LEFT AND RIGHT SEAT BELT OUTBOARD ATTACHMENT POINTS INCORRECT. THE BELTS WERE ATTACHED TO THE FORWARD BAGGAGE FLOOR WITH AN3 BOLTS INSTEAD OF TO THE CORRECT POSITION BELOW THE DOOR CUTOUTS USING 6.35 MM (0.25 INCH) HARDWARE AND BUSHES. UNAPPROVED PARTSSep 4, 2000 · Cessna 150F · Flight Compartment EquipmentSDR AU000786Hose · missing(AUS) CARBURETOR HEAT HOSE LOCATED BETWEEN FORWARD RIGHT ENGINE BAFFLE AND THE RIGHT MUFFLER MISSING. (X)Sep 4, 2000 · Cessna 150F · Engine Air Intake SystemSDR AU000785Pitot Line · leaking(AUS) PITOT/STATIC SYSTEM FAILED LEAK TEST. INVESTIGATION FOUND THE PITOT SYSTEM CONNECTOR LOCATED AT THE LEFT WING BREAK WAS CROSS-THREADED AND ONLY HOLDING BY ONE TURN. THE STATIC SYSTEM HAD BEEN REWORKED TO ACCOMMODATE THE ENCODED. THE EXISTINGPLUMBING HSep 4, 2000 · Cessna 150F · Pitot/Static SystemSDR AU000784Vhf Comm · inaccurate(AUS) AVIONICS FIT NOT RECORDED OR CERTIFIED IN AIRCRAFT LOG BOOK. ITEMS NOT ACCOUNTED FOR: 1. IC-A200 VHF SNO 139702. KT76A ATC TRANSPONDER SNO 117656. 3. AMER-KING ENCODER SNO 35243954. SPA-400 TSO SIGTRONICS CORP INTERCOM SNO 6055958. (X)Sep 4, 2000 · Cessna 150F · Communications SystemSDR AU000783Blade · corroded(AUS) PROPELLER BLADES CORRODED CAUSING PAINT TO LIFT. (X)Sep 4, 2000 · Cessna 150F · Propeller Blade SectionSDR AU000782Selector Valve · seized(AUS) FUEL SELECTOR VALVE SEIZED. (X)Sep 4, 2000 · Cessna 150F · Fuel Selector/Shut-Off ValveSDR AU000781Fuel Tank · unwanted(AUS) MOGAS USED IN AIRCRAFT WITHOUT AN STC. . (X)Sep 4, 2000 · Cessna 150F · Aircraft Fuel SystemSDR AU000780Filler · contaminated(AUS) FUEL TANK FILLER NECK CONTAMINATED WITH WASP NEST. (X)Sep 4, 2000 · Cessna 150F · Fuel StorageSDR CA000218004Cylinder · cracked(CAN) CYLINDERS FOUND CRACKED DURING 100-HOUR CHECK.Feb 10, 2000 · Cessna 150F · Reciprocating Engine Cylinder SectionSDR CA991027041Line · chafed(CAN) FUEL LINES FOUND CHAFED AGAINST IMPROPERLY INSTALLED HEADLINER RETAINER BOW. FUEL LINES CHAFED TO THE POINT WHERE MINOR CLEANING OF THE SUSPECT AREA CAUSED LEAKAGE.Oct 8, 1999 · Cessna 150F · Aircraft Fuel Distribution SystemSDR AU980703Carburetor · out of adjust(AUS) CARBURETOR OUT OF ADJUSTMENT.May 3, 1998 · Cessna 150F · Fuel Control/Reciprocating EnginesSDR 97ZZZX3813Valve Seat · carboned upFOLLOWING TAKEOFF, ENGINE LOST POWER. SAFE LANDING MADE. INVESTIGATION FOUND NR 2 CYLINDER LOST POWER DUE TO VALVE SEAT CARBON BUILD-UP CAUSING COMPRESSION LOSS AND BLOWBY TO OTHER CYLINDERS.Aug 3, 1997 · N6674F · Cessna 150F · Reciprocating Engine Cylinder SectionSDR 97ZZZX835Seat Frame · crackedFOUND BOTH PILOT AND COPILOT SEAT BACK FRAMES CRACKED DURING AN ANNUAL INSPECTION. IF LEFT UNDETECTED, POSSIBLE SEAT BACK FAILURE. THIS SHOULD BE INSPECTED CLOSELY DURING EACH INSPECTION. INSPECTION MAY REQUIRE PARTIAL REMOVAL OF UPHOLSTERY IN THIS AREA. TJan 4, 1997 · N8346G · Cessna 150F · Flight Compartment EquipmentSDR 96ZZZX3933Elt · failedELT SYSTEM INSTALLED AND INSPECTION IAW FAR 91.207.0. ELT SYSTEM CHECKED 60 DAYS LATER BY DEPRESSING TEST SWITCH. TEST LIGHT CAME ON, BUT NO AUDIO HEARD ON 121.5. ALSO 'G' SWITCH TURNS LIGHT ON, BUT NO AUDIO ON FREQUENCY.Jul 22, 1996 · N8749S · Cessna 150F · Emergency Locator BeaconSDR 95ZZZX6162Cylinder · fracturedALL ROCKER SHAFT BOSSES FRACTURED DUE TO FATIGUE ALLOWING ROCKER SHAFT AND ROCKER ARMS TO FALL AWAY FROM CYLINDER. ENGINE RAN EXTREMELY ROUGH AND EMERGENCY LANDING WAS COMPLETED WITHOUT INCIDENT.Sep 3, 1995 · N6495F · Cessna 150F · Reciprocating Engine Cylinder SectionSDR 95ZZZX566Brake Assy · crackedDURING AN INSPECTION, BOTH WHEEL BRAKE ASSEMBLIES WERE FOUND CRACKED AT THE ANCHOR BOLT BOSSES. THE CAUSE OF THE CRACK IS THE ANCHOR BOLT (PN 69-4) GETS RUSTY/DIRTY AND WOULD NOT SLIDE FREELY IN THE TORQUE PLATE (PN 75-37). SUBMITTER SUGGESTS DURING INSPECTIJan 13, 1995 · N6242R · Cessna 150F · Landing Gear Brake System
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