Cessna 150G

Service difficulty reports · 49

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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 = '150G'
  ORDER BY difficulty_date DESC"

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SDR 2016FA0000404Bolt · looseLEFT ELEVATOR SEPARATED IN FLIGHT. BOLT CONNECTING ELEVATOR LOOSENED UP AND FELL OUT. ELEVATOR WAS DAMAGED AND APPEARED TO BE BENT FROM AERODYNAMIC FORCES. AIRCRAFT WAS DIFFICULT TO CONTROL. ANY CONTROL MOVEMENT CAUSED UNCONTROLLABLE PITCHING IN THE LATERAL Aug 13, 2016 · N3666J · Cessna 150G · Elevator StructureSDR CA150604020Coupling · 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 IN LOGS.May 17, 2015 · Cessna 150G · Vacuum Distribution SystemSDR CA150319006Muffler · cracked(CAN) CRACK IN THE INTERIOR OF THE RT MUFFLER FOUND DURING ANNUAL ENGINE INSPECTION. NEW MUFFLER TO BE INSTALLED.Oct 5, 2014 · Cessna 150G · Engine Noise SuppressorSDR CA130501003Wire · burned(CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT SAW SMOKE AND SHUT DOWN ELECTRICAL POWER TO AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND RING TERMINAL LAYING ON CABIN HEAT CONTROL. WIRE TRACED BACK AND FOUND CONNECTED TO AMMETER. THIS WIRE MUST BApr 30, 2013 · Cessna 150G · Heating SystemSDR 2013FA0000019Boss · crackedROCKER 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 INSPECTION, BUT 5 YEARS CALENDAR TIME. POSSIBLE MORE FREQUENT DYE CHECK ON ROCKER BOSSES FOR ADDec 6, 2012 · N2252J · Cessna 150G · Reciprocating Engine Cylinder SectionSDR 2012FA0000247Spark Plug · failedTESTED EIGHT REM38S SPARK PLUGS WITH 200 HRS TT AND FOUND THE RESISTORS HAD FAILED, NO RESISTANCE FOUND THROUGH THE SPARK PLUG.Mar 6, 2012 · N3038S · Cessna 150G · Spark Plug/IgniterSDR LC1R201202011501Skin · corrodedDURING A PRE-PURCHASE INSPECTION, HEAVY CORROSION WAS FOUND AT THE JOINT BETWEEN THE LT STABILIZER SKIN, PN 0432001-55 AND THE RT STABILIZER SKIN, PN 0432001-54 AT THE LOWER CENTER RIVET LINE WHICH HAD EATEN AWAY NUMEROUS RIVETS, LOOSENED THE SKIN JOINT AND BEFeb 1, 2012 · N2217J · Cessna 150G · Horizontal Stabilizer, Plate/SkinSDR 2008FA0000087Spar · corrodedWINGS 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 ATTFeb 15, 2008 · N3816J · Cessna 150G · Fuselage Main, FrameSDR 2008FA0000086Spar · corrodedWINGS 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 ATTACHMENFeb 15, 2008 · Cessna 150G · Wing SparSDR 2005FA0001283Carburetor · mismanufacturedENGINE HAD BAD HESITATION ON TAKEOFF ACCELERATION. SURGING OCCURRED DURING CLIMB WITH RPM FLUCTUATIONS OF +/- 50-75 RPM. AIRCRAFT AND ENGINE FUEL SCREENS WERE REMOVED AND INSPECTED 3 TIMES IN THE LAST 50 HOURS WITH NO EVIDENCE OF CONTAMINATION. FUEL LINE TOSep 7, 2005 · Cessna 150G · Fuel Control/Reciprocating EnginesSDR 2004FA0000751Windshield · departedSECTION 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 WINDSHAug 3, 2004 · N4760X · Cessna 150G · Flight Compartment WindowsSDR 2003FA0000977Bushing · wornEIGHT ROCKER ARM BUSHINGS SHOWED INDICATIONS OF EXCESSIVE WEAR. THE PROBLEM WAS INDICATED AT THE FIRST OIL CHANGE (10 HOURS) AFTER ENGINE OVERHAUL AS BRONZE PARTICLES IN THE OIL FILTER. THE OVERHAULED ROCKER ARMS WERE INSTALLED IN NEW MFG CYLINDERS P/N 65381Aug 23, 2003 · N2698J · Cessna 150G · Reciprocating Engine Cylinder SectionSDR CA030517002Rudder · binding(CAN) INCORPORATION OF AD 2000-20R1 (CESSNA S/B SEB01-1) RESULTS IN BINDING BETWEEN NEW STOP BOLTS AND RUDDER STRUCTURE DUE TO THE INCREASED SIZE OF THE STOP BOLTS. BINDING WAS NOT APPARENT UNLESS PRESSURE WAS APPLIED TO BOTH RUDDER PEDALS.May 17, 2003 · Cessna 150G · Rudder Control SystemSDR AUS20030261Indicator · mismarked(AUS) AIR SPEED INDICATOR (ASI) LIMITS INCORRECTLY MARKED.Feb 7, 2003 · Cessna 150G · Airspeed/Mach IndicatorSDR AUS20021059Piston · broken(AUS) PISTON SIDE BROKEN AWAY. METAL CONTAMINATION OF OIL FILTER.Sep 18, 2002 · Cessna 150G · Reciprocating Engine Cylinder SectionSDR 2001FA0000286Magneto · inoperativeINSTALLED NEW LEFT AND RIGHT SIDE SLICK (UNISON) MAGNETOS AND IGNITION HARNESS. TEST RUN OK. ON FIRST FLIGHT AFTER 15 MIN. ENGINE POWER LOSS OCCURED. AFTER LANDING FOUND LEFT MAG INOP. REMOVED MAG AND FOUND THAT COIL INSULATION HAD BURNED THROUGH AND HIGH VOAug 25, 2001 · N2750S · Cessna 150G · Magneto/DistributorSDR 2001FA0000100Bellcrank · elongatedFOUND ELEVATOR BELLCRANKS CABLE ATTACH POINTS ELONGATED. RIGHT ATTACH WAS ELONGATED BY .215, LEFT ATTACH WAS ELONGATED BY .248, THE AN23-11 ATTACH BOLT IS .184. DRILLED OVERSIZE AND PUT NAS 75-3-004 STEEL BUSHING PRESSED IN, TO BRING BACK CORRECT TOLERANCE.Jun 18, 2001 · N3343J · Cessna 150G · Elevator Control SystemSDR 20010403CW019Bulkhead · damagedCORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTFeb 26, 2001 · N3232X · Cessna 150G · Fuselage Main, BulkheadSDR 20010403CW018Skin · damagedCORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTFeb 26, 2001 · N3232X · Cessna 150G · Vertical Stabilizer, Plate/SkinSDR 20010403CW017Spar · corrodedCORROSION FOUND EXFOLIATING (1) SPAR CUP ON RIGHT WING HEAVY CORROSION ON UPPER CABIN (2) CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTFeb 26, 2001 · N3232X · Cessna 150G · Wing SparSDR 20010403CW016Spar Cap · corrodedCORROSION FOUND EXFOLIATING SPAR CAP OR RIGHT WING HEAVY CORROSION ON UPPER CABIN CARRY THRU STRUCTURE. VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON CANTED BULKHEAD AT FUSLAGE STATION 20.5 BOTTOM FUSELAGE. AIRFeb 26, 2001 · N3232X · Cessna 150G · Wing SparSDR 20010403CW009Rudder Pedal · wornDURING ANNUAL INSPECTION PILOTS SIDE RUDDER PEDALS AND SHAFTS WERE FOUND TO BE BADLY WORN WHERE SHAFT PINS PASS THROUGH THE HOLES. IT IS EVIDENT THAT THIS ITEM IS OVERLOOKED.Feb 19, 2001 · N3057S · Cessna 150G · Rudder Control SystemSDR CA001207030Horn · bent(CAN) DURING ANNUAL INSP AND PER AD CF-2000-20, RUDDER CNTL SYS CLOSELY INSP. RT SIDE OF RUDDER HORN HAD NICKS ON LOWER OTBD EDGE AND CANTED UP SEVERAL DEGS. AT ROOT OF RT HORN WERE TEETH MARKS INDICATING PLIERS HAD BEEN USED TO ATTEMPT TO STRAIGHTEN HORN. Nov 3, 2000 · Cessna 150G · Rudder Control SystemSDR CA001018005Battery · wrong part(CAN) ELT WAS EQUIPPED WITH A NON-APPROVED BATTERY FOR THE ELT TYPE. REF: ANO B014 EDITION 4, NOVEMBER 20, 1998. (X)Sep 28, 2000 · Cessna 150G · Emergency Locator BeaconSDR AU000989Piston Pin · faulty(AUS) PISTON PIN FAULTY. LIMITED INFORMATION PROVIDED. (X)Sep 27, 2000 · Cessna 150G · Engine System WiringSDR AU991100Torque Link · cracked(AUS) NOSE LANDING GEAR UPPER TORQUE LINK CRACKED IN THREE PLACES IN THE LOWER WEB AREA. CRACK LENGTHS APPROXIMATELY 6.35MM (0.25 INCH).Oct 13, 1999 · Cessna 150G · Nose/Tail Landing Gear Strut/AxleSDR 99ZZZX2639Encoder · malfunctionedMODE C REPORTED AS INVALID. RETURNED DEFECTIVE ENCODER TO MANUFACTURER FOR REPAIR. PERFORMED BI-ANNUAL TESTS AND INSPECTIONS.May 15, 1999 · N2977J · Cessna 150G · Altimeter, Barometric/EncoderSDR CA981230034Valve · leaking(CAN) ONE FUEL DRAIN LEAKING AND THE OTHER STUCK. FOUND THE STUCK DRAIN HEAVILY CORRODED WITH CORROSION ON THE PLUNGER ON THE INSIDE OF THE TANK.Dec 8, 1998 · Cessna 150G · Fuel StorageSDR AU981527Pedestal · broken(AUS) NR 1 CYLINDER ROCKER PEDESTAL BROKEN.Nov 18, 1998 · Cessna 150G · Reciprocating Engine Cylinder SectionSDR 98ZZZX4591Stiffener · crackedSTIFFENER, P/N 0412521-3, WAS FOUND CRACKED IN 4 PLACES, .25 INCH TO .3750 INCH LONG. THIS CONDITION WAS CAUSED BY LOOSE BOLTS IN PLATE, P/N 0412010-1, FITTINGS, P/N 0432005-1, AND P/N 0432005-2. BOLTS AND BOLT HOLES WERE WORN EXCESSVIELY. THIS CONDITION CANov 1, 1998 · N3877J · Cessna 150G · Fuselage Miscellaneous StructureSDR 98ZZZX1605Angle · failedDURING ANNUAL INSPECTION, FOUND ANGLE WHICH MOUNTS FIREWALL TO FUSELAGE BUCKLED AND POORLY REPAIRED. DAMAGE EXTENDED FROM 7 O'CLOCK TO 10 O'CLOCK POSITIONS. THE REPAIR CONSISTED OF AN ANGLE DOUBLER WITH RIVETS PASSING THROUGH BEND RADIUS AND ZERO EDGE DISTANMar 27, 1998 · N8311J · Cessna 150G · Nacelle/Pylon, Bulkhead/FirewallSDR 98ZZZX1604Strap · failedDURING ANNUAL INSPECTION, FOUND LEFT FUEL TANK AFT MOUNTING STRAP BROKEN. NOTIFIED OWNER.Mar 27, 1998 · N8311J · Cessna 150G · Fuel StorageSDR 98ZZZX1603Firewall · buckledFOUND FIREWALL BUCKLED HEAVILY ALL THE WAY ACROSS APPROXIMATELY 8 INCHES FROM BOTTOM. ALSO, BUCKLED AT ALL ENGINE MOUNT LOCATIONS. NOTIFIED OWNER.Mar 27, 1998 · N8311J · Cessna 150G · Nacelle/Pylon, Bulkhead/FirewallSDR 98ZZZX1602Screw · missingDURING ANNUAL INSPECTION, A SMALL HOLE WAS FOUND IN RIGHT SIDE OF FORWARD FUSELAGE BELOW WINDSHIELD. PER CESSNA SB SB 68-16, THIS BOLT IS FOR SCREW THAT SUPPORTS FORWARD END OF GLOVE BOX. THIS HOLE WAS PAINTED OVER SHOWING SCREEN HAD BEEN MISSING SINCE LAST Mar 27, 1998 · N8311J · Cessna 150G · Flight Compartment EquipmentSDR 98ZZZX1484Bracket · displacedFOUND LEFT LOWER ENGINE MOUNT BRACKET DISPLACED FROM NORMAL POSITION. THIS MAY HAVE OCCURRED DURING UNDOCUMENTED REPAIR IN AREA BY PERSONS UNKNOWN.Mar 27, 1998 · N8311J · Cessna 150G · Engine Mount SectionSDR AU980325Cylinder · worn(AUS) ENGINE CYLINDERS HAD LOW COMPRESSION. INVESTIGATION FOUND WORN EXHAUST VALVE GUIDES AND GLAZED AND OUT OF ROUND CYLINDER BORES.Mar 24, 1998 · Cessna 150G · Reciprocating Engine Cylinder SectionSDR AU980484Guide · worn(AUS) NR 3 CYLINDER WAS REMOVED FOR LOW COMPRESSION. THE EXHAUST VALVE GUIDE WAS FOUND TO BE WORN 0.483 MM (0.019 INCH). THE REMAINING CYLINDERS WERE THEN REMOVED AND ALL WERE FOUND TO BE IN A SIMILAR CONDITION. TIME IN SERVICE FOR THE CYLINDERS WAS 55 HRS.Mar 13, 1998 · Cessna 150G · Reciprocating Engine Cylinder SectionSDR AU980651Cylinder · worn(AUS) NR 2 CYLINDER WORN BEYOND LIMITS.Feb 4, 1998 · Cessna 150G · Reciprocating Engine Cylinder SectionSDR 98ZZZX978Attach Fitting · wornDURING AN ANNUAL INSPECTION, FOUND THE HORIZONTAL STABILZIER LOOSE AT THE REAR ATTACHMENTS. THE STABILIZER COULD BE MOVED UP AND DOWN ABOUT .25 INCH. THE REAR ATTACH FITTINGS WERE FOUND TO BE EXCESSIVELY WORN.Jan 28, 1998 · N8623J · Cessna 150G · Horizontal Stabilizer, Attach FittingsSDR AU971518Valve · sticking(AUS) NO4 CYLINDER EXHAUST VALVE STUCK OPEN. LOSS OF POWER AND ROUGH RUNNING RESULTED IN A FORCED LANDING IN THE BUSH.Nov 22, 1997 · Cessna 150G · Reciprocating Engine Cylinder SectionSDR 99ZZZX969Clutch · damagedTEETH ON PINION GEAR WERE GROUND OFF; METAL WAS FOUND IN THE OIL SUMP AND SCREEN. THIS PART WAS NEW. STC SE00262NY CANADIAN AERO MANUFACTURING.Nov 17, 1997 · N3856J · Cessna 150G · Engine StarterSDR 97ZZZX1707Bulkhead · crackedSPINNER BULKHEAD CRACKED. SUSPECT FROM PUSHING ON SPINNER WHEN MOVING A/C AND OR PUTTING TOO MANY SHIMS ON FORWARD BULKHEAD; THUS, HAVING TO PUSH TOO HARD TO GET SCREW IN. SECOND TIME THIS BULKHEAD WAS REPLACED.Apr 1, 1997 · N4044J · Cessna 150G · Propeller Spinner SectionSDR CA970310005Blade · corroded(CAN) PROPELLER WAS SENT FOR 5 YEAR INSPECTION. CORROSION WAS FOUND PAINTED OVER. PROP HAD NOT BEEN INSPECTED SINCE 1970.Mar 6, 1997 · Cessna 150G · Propeller Blade SectionSDR 96ZZZX5892Dampener · failedAIRCRAFT LANDED, RAN OFF RUNWAY PUSHING NOSE GEAR UNDER FUSELAGE. OWNER SAID PLANE DEVELOPED SHIMMY AND HE COULDN'T KEEP ON RUNWAY. CHECKED SHIMMY DAMPENER AND FOUND ONE-HALF AIR IN IT. SUBMITTER STATED SHOULD MAYBE CHECK SHIMMY DAMPENER MORE OFTEN FOR FLUIOct 31, 1996 · N2951J · Cessna 150G · Shimmy DamperSDR 96ZZZX3433Control Cable · chafedDURING A 100-HOUR INSPECTION, THE FOLLOWING DEFECTS WERE FOUND: THE AILERON CONTROL CABLE WAS SCRAPING THE PRIMER LINE(S) LOCATED IN THE FIREWALL AND A CRACK IN THE CONTROL CABLE SUPPORT BETWEEN THE INSTRUMENT PANEL AND THE FIREWALL ON THE PILOT'S SIDE.Jun 6, 1996 · Cessna 150G · Aileron Control SystemSDR AU960972Seat Belt · wrong part(AUS) SEAT BELTS CONTAINED NON APPROVED HARDWARE AND WEBBING - UNAPPROVED PART - PERSONNEL/MAINTENANCE ERRORMay 1, 1996 · Cessna 150G · Flight Compartment EquipmentSDR AU960443Crankshaft · worn(AUS) ENGINE SUFFERED TWO CRANKSHAFT MAIN BEARING EXCESSIVE WEAR INCIDENTS IN APPROXIMATELY 50 HOURS OPERATION: 1. FIRST OCCURRENCE WAS AT 8.5 HOURS AFTER INSTALLATION FOLLOWING OVERHAUL - ENGINE WAS INSPECTED/CHECKED, NEW BEARINGS AND A USED SERVICEABLE CRANMar 8, 1996 · Cessna 150G · Reciprocating Engine Power SectionSDR 96ZZZX1084Cylinder · crackedPILOT REPORTED A ROUGH ENGINE AND A PARTIAL LOSS OF POWER. A PRECAUTIONARY LANDING MADE ON A COUNTY ROAD. NO DAMAGE TO AIRCRAFT, PERSONNEL, OR PROPERTY. FOUND NR 4 CYLINDER CRACKED AFTER CYLINDER REMOVED. CRACK WENT THROUGH VALVE GUIDE BOSS ALLOWING GUIDE Jan 1, 1996 · N3824J · Cessna 150G · Reciprocating Engine Cylinder SectionSDR 96ZZZX5905Strap · brokenWHILE REPLACING RUSTY LEFT FUEL TANK COVER SCREWS, FOUND REAR INBOARD TANK STRAP BROKEN AT BEND-WEAR MARKS ON TOPS OF TANK AND TANK COVER-INDICATIONS ARE TANK COVERS HAD NEVER BEEN REMOVED SINCE MANUFACTURE-FOUND SAME PROBLEM WITH RIGHT TANK STRAP 2-9-94 AT 27Nov 17, 1995 · N2974S · Cessna 150G · Fuel Storage
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