N124DE, cancelled May 16, 2018

Service difficulty reports · 48

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N124DE' AND deregistration_id = 'N124DE-2018-05-16'
  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 DALA2015011200438Door Frame · corrodedLEFT FORWARD OVERWING EXIT DOOR FRAME IS CORRODED AT FORWARD LOWER CORNER. REMOVED AND FABRICATED NEW ANGLE.Jan 11, 2015 · N124DE · Boeing 767332 · Fuselage Main, StructureSDR DALA2014091805094Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED IAW ERA 528965-14.Sep 17, 2014 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DALA2014091805093Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED IAW ERA 528966-14.Sep 17, 2014 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DALA2014091805092Skin · damagedFUSELAGE SKIN GROUND DAMAGED. REPAIRED IAW ERA 528964-14.Sep 17, 2014 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DALA2014091705090Stringer · crackedRT SIDE FUSELAGE STRINGER 30R CRACKED BS 1530-1540. REMOVED STRINGER IAW SRM 53-00-01,. PERFORMED HFEC FOR DAMAGE CONTAINMENT, NO FINDINGS.Sep 16, 2014 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13028270124Floorbeam · crackedCABIN BS 347 FLOORBEAM UPPER TEE FOUND CRACKED AT RBL 2.0 AND RBL 8.0 & LBL 9.0. REPAIRED IAW 514023-14 (LP 0917476).Jun 7, 2013 · N124DE · Boeing 767332 · Fuselage Floor PanelSDR DALA13028260124Failsafe · crackedCRACK ON RT BULKHEAD FAIL SAFE STRAP AT BS 955. REPAIRED IAW PRI 514007-14AD, REV 0.Jun 7, 2013 · N124DE · Boeing 767332 · Fuselage Main, BulkheadSDR DALA13023700124Stringer · corrodedFWD CARGO -BS 412-434, STRINGER 38R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13023690124Stringer · corrodedFWD CARGO BS 412-434, STRINGER 36R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13023680124Stringer · corrodedFWD CARGO BS 412-434, STRINGER 34R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13023670124Stringer · corrodedFWD CARGO BS 412-434 STRINGER 27R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03 FIG 201, REPAIR 2, REV 92.00.May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13023660124Stringer · corrodedFWD CARGO BS 412-434 STRINGER 39R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13023650124Stringer · corrodedFWD CARGO BS 412-434, STRINGER 35R CORRODED, REPAIR CARRIED OUT IAW SRM 53-00-03 FIG 201, REPAIR 2, REV 92.00.May 21, 2013 · N124DE · Boeing 767332 · Fuselage Main, Longeron/StringerSDR DALA13023490124Frame · crackedDURING HFEC INSPECTION ON BS 1809, BULKHEAD LT FORWARD OUTER FRAME S6-7L FOUND CRACKED. REPAIRED FRAME.May 20, 2013 · N124DE · Boeing 767332 · Fuselage Main, FrameSDR DALA13028310124Structure · corrodedWING CENTER SECTION UPPER SURFACE BETWEEN BS 857 AND 859, LBL 88. REWORKED IAW PRI 514634-14, REV 0, REV 1, REV 2, REV 3 AND REV 4.May 8, 2013 · N124DE · Boeing 767332 · Fuselage Main, StructureSDR DALA13028300124Structure · corrodedWING CENTER SECTION UPPER SURFACE AT BS 927, LBL 90. REPAIR CARRIED OUT IAW- PRI 514016-14, REV 0, REV 1, REV 2, REV 3, REV 4, REV 5 AND REV 6. AND COMPLIED WITH ER/A 514016-14, REV ORIGINAL.May 8, 2013 · N124DE · Boeing 767332 · Fuselage Main, StructureSDR DALA2015082707893Skin · crackedCRACK AT BS 687, STRINGER 36R AT CARRY THOUGH HOLE, RT AIRFONE BLANKING PLATE, 1/8TH INCH CRACK.Aug 14, 2012 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DALA1245820124Skin · crackedSKIN CRACKED ONE EIGTH INCH CRACK RT AIRFONE BLANKING PLATE INST STA 687 STR 36R AT CARRY THRU HOLE LOC MARKED REF ERA 389647-14 REV A. REPAIRED PER SRM B767-300 53-00-01 REPAIR 12.Aug 14, 2012 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DALA1102330124Skin · delaminatedRT WING OTBD FLAP LWR SURFACE MID INSPAR PANEL SKIN DELAMINATED AT APPROX 66"FROM INBD AND 24" FRM BOTTOM; CA: REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 57-53-01 OTIS. REPAIR PARTS BONDED IAW SRM 51-70-10 OTIS. DECAL INSTALLED ADJ TO REPAIR IAW PS 900-5-Jan 11, 2011 · N124DE · Boeing 767332 · Trailing Edge FlapsSDR DALA1102320124Wedge · delaminatedLT WING L/E NR2 SLAT WEDGE UPPER SURFACE FOUND DELAMINATED; CA: LT WING L/E NR2 SLAT WEDGE UPPER SURFACE, REPAIR FILLER AND DOUBLER FABRICATED IAW 51-70-10 OTIS. DECAL INSTALLED ADJ TO REPAIR IAW DELTA PS 900-5-1, NR 4.Jan 11, 2011 · N124DE · Boeing 767332 · Leading Edge DevicesSDR DALA1102060124Skin · dentedLT V-STAB EXTERIOR AROUND FS STA 270.784 FOUND DENT DURING HMV INSP AT SIN; C/A-DENTED SURFACE TRIMMED OFF. REPAIR PART FABRICATED IAW SRM 51-70-01, FIG 201, OT IS REPAIR PARTS BONDS IAW SRM 51-71-10.Jan 10, 2011 · N124DE · Boeing 767332 · Vertical Stabilizer, Plate/SkinSDR DL76S071392Indicator · malfunctionedAFTER TO, F/O AIRSPEED INDICATOR BECAME UNREADABLE AND ROSE STEADILY TO 400 KTS. NO FLAGS OR OTHER INDICATIONS, OTHER THAN OVERSPEED WARNING. ACTUAL AIRSPEED ON CAPTS IND NORMAL. FOUND QUICK DISCONNECT DAMAGED ON PITOT PRESS ON RT ADC. REPLACED SAME. LEAK Oct 27, 2007 · N124DE · Boeing 767332 · Airspeed/Mach IndicatorSDR DL76S071386Trunnion · corrodedLT AND RT NOSE LANDING GEAR TRUNNION FITTINGS CORRODED IN THE INNER DIAMETER. CORROSION CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED.Oct 24, 2007 · N124DE · Boeing 767332 · Fuselage, Landing Gear Attach FittingsSDR DL76S071046Mec · malfunctionedRTO DUE TO RT ENGINE WOULD NOT MAKE TAKEOFF POWER. REPLACED RT ENGINE MEC. AFTER RUNUP ENGINE MAKES TAKEOFF POWER.Aug 8, 2007 · N124DE · Boeing 767332 · Fuel Controlling SystemSDR DL76S070504Charger · missingEMERGENCY LIGHT EXIT SIGN INOP AT L1 AND R1 DOOR. INSTALLED NEW BATTERY AND CHARGER TRA, FOUND TRAY AND BATTERY PACK ASSY MISSING AT L1 POSITION.May 9, 2007 · N124DE · Boeing 767332 · Emergency LightingSDR DL76S060797Floorbeam · corrodedCABIN FLOORBEAM UPPER CHORD STA 287 CORRODED AT RBL 51 TO RBL 62 AND ALSO EXISTING SPLICE PLATE CORRODED AT RBL 10 TO RBL 15. REPAIRED PER SRM 53-00-51D FIGURE 201, AMM 32-41-00.Sep 28, 2006 · N124DE · Boeing 767332 · Fuselage Main, Floor BeamSDR DL76S060796Floorbeam · crackedCABIN FLOORBEAM AT STA 325 LBL 32 UPPER STRUCTURE BENT AND CRACKED IN RADIUS AS MARKED. REPAIRED PER SRM 53-00-51D FIGURE 201.Sep 28, 2006 · N124DE · Boeing 767332 · Fuselage Main, Floor BeamSDR DL76S060793Fitting · fatiguedDURING REWORK OF THE FORWARD UPPER SPAR FITTING PER SIP EO, CRACKING INDICATIONS WERE FOUND AT AFT OUTBOARD FASTENER LOCATIONS COMMON TO MIDSTRUT BULKHEAD FITTING ON EACH PYLON. HOLES WERE OVERSIZED AND BUSHED BACK TO DIAMETER.Sep 28, 2006 · N124DE · Boeing 767332 · Nacelle/Pylon, Attach FittingsSDR DL76S060792Fitting · fatiguedCRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRED SUBJECT HOLE TO BE OVERSIZED AND BUSHED BACK TO DIAMETER.Sep 28, 2006 · N124DE · Boeing 767332 · Engine Mount SectionSDR DL76S060791Frame · crackedFUSELAGE STATION 903.5 FRAME INNER CHORD FOUND CRACKED. ON BOTH LT AND RT AT TRANSITION BETWEEN CHORD FLANGES. AREA TRIMMED AND REPAIR INSTALLED.Sep 28, 2006 · N124DE · Boeing 767332 · Fuselage Main, FrameSDR DL76S060790Rib · corrodedRT WING RIB NR 8, LOWER OUTBOARD HOLE WAS FOUND WITH CORROSION PITTING. DAMAGE WAS REMOVED BY OVERSIZED HOLE, BUSHING INSTALLATION.Sep 28, 2006 · N124DE · Boeing 767332 · Wing, Rib/BulkheadSDR DL76S060695Linkage · misinstalledDURING INSPECTION OF THE LT OFF WING ESCAPE SLIDE PER JIC 6075 THE TECHNICIAN FOUND THAT THE INTEGRATOR LOCK HANDLE HAD TO BE FORCED INTO THE SAFETY POSITION. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT SLIDE DOOR OPENING ACTUATOR LINKAGE LEVER WAS INSTAAug 23, 2006 · N124DE · Boeing 767332 · Escape SlideSDR DL76S060467Skin · lightning strikeFUSELAGE SKIN WAS STRUCK BY LIGHTNING BETWEEN BS 257 AND 277 BELOW S-11L. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED.May 23, 2006 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S060140Bolt · missingNR 2 SLAT I/B ACTUATOR COVER DAMAGED. REINSTALLED MISSING HARDWARE, RAN SLATS, ALL OK.Feb 15, 2006 · N124DE · Boeing 767332 · Leading Edge Slat ActuatorSDR DL76S030503Skin · crackedMECHANIC FOUND 2 INCH CRACK IN FUSELAGE SKIN RT SIDE STA 1654.5 STR 3R. ALSO, FOUND STRINGER 3R AND 3L CRACKED AT SAME LOCATION. REPAIRED CRACK.Jun 2, 2003 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S020842Skin · dentedFUSELAGE / SKIN / FS 287-303 / STRG. 37R : DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT THE STRINGER 37R SKIN LAP JOINT BETWEEN FS 287 & 303. THE LAPJOINT WAS CUTOUT IN THE AREA TO REMOVE TJul 18, 2002 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S020565Power Supply · dischargedOVERHEAD AISLE LIGHTS FIRST CLASS LEFT SIDE INOP. REPLACED BATTERY PACK AND RACK.May 17, 2002 · N124DE · Boeing 767332 · Emergency LightingSDR DL76S020406Skin · crackedWHILE ACCOMPLISHING THE FS 1809.5 BULKHEAD OUTER CHORD MOD PER BAC S/B 767-53-0078 AND AD 2001-09-13, A CRACK WAS FOUND IN THE SKIN COMMON TO A FASTENER HOLE FOR THE OUTER CHORD ON THE LT SIDE. THE HOLE WAS OVERSIZED IN THE SKIN ASSY ONLY AND A BUSHING INSTALApr 4, 2002 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S011920Battery Pack · dischargedLEFT FORWARD OVERHEAD EMERGENCY LIGHTS INOP IN CABIN. REMOVED AND REPLACED BATTERY PACK FOR LEFT FORWARD OVERHEAD EMERGENCY LIGHTS, CHECKS GOOD.Dec 10, 2001 · N124DE · Boeing 767332 · Emergency LightingSDR DL76S011516Engine · unserviceableON CLIMB OUT RIGHT ENGINE STALLED. ACCOMPLISHED POM "ENGINE SURGE OR STALL" PROCEDURE. THROTTLE REDUCED TO IDLE. ENGINE SHUT DOWN AFTER LANDING. EGT MAX 895 FOR 1.4 SECONDS. FOUND METAL IN EXHAUST. REPLACED ENGINE.Sep 10, 2001 · N124DE · Boeing 767332 · Engine (Turbine/Turboprop)SDR DL76S010388Probe · malfunctionedRTB FOR INSP. DUE TO SMOKE COMING FROM LT NOSE AREA OVER RADOME. J/C VISUAL INSPECTION OF NLG AREA, FWD AND MAIN E/E COMPARTMENTS. ALSO VISUALLY INSPECTED OF LT / RT ACM AREAS AND RADAR ANTENNA AREA. NO ANOMALIES NOTED-ALL HYD QTYS NORMAL, NO HYD LEAKS FOUNMar 10, 2001 · N124DE · Boeing 767332 · Flight Environment DataSDR DL76S010170Frame · corrodedCORROSION WAS FOUND ON THE FWD FRAME AT THE CUTOUT FOR THE FWD LT PASSENGER DOOR. THE CORROSION WAS LOCATED ON THE AFT SURFACE OF THE FRAME WEB SURROUNDING THE GIRT BAR HOLE (JUST ABOVE CABIN FLOOR LEVEL). REPAIRED DAMAGE PER ER/A 396699-14.Jan 26, 2001 · N124DE · Boeing 767332 · Fuselage Main, FrameSDR DL76S010171Skin · dentedFUSELAGE SKIN WAS DENTED DUE TO NOSE TIRE BLOWOUT. THE DENTS WERE APPROVED FOR INTERIM SERVICE PER ER/A 269377-14. THE DAMAGE WAS PERMANENTLY REPAIRED PER ER/A 269377-14 AT OVERHAUL MTC VISIT. REPAIRED DAMAGE PER ER/A 269377-14.Jan 25, 2001 · N124DE · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S992442Light · inopFOUR AISLE EMERGENCY LIGHTS INOP AFT RIGHT SIDE. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL.Nov 4, 1999 · N124DE · Boeing 767332 · Emergency LightingSDR DL76S990692Mask · fellTHE O2 MASK ZONE C HANGING DOWN. REINSTALLED MASK AND SECURED PANEL.Mar 29, 1999 · N124DE · Boeing 767332 · Passenger Oxygen SystemSDR DL76S981698Skin · corrodedCORROSION WAS FOUND ON THE WING CENTER SECTION. DAMAGE LOCATED ON AFT SKIN PANEL, FWD EDGE ON THE LT OUTBD END. REPAIRED PER ERA 331990-14.Aug 12, 1998 · N124DE · Boeing 767332 · Wing, Plate/SkinSDR DL76S981265Power Supply · inoperativeON L/O, FOUND ZONE EMERGENCY TRACK LIGHTS INOP BOTH AISLES. REPLACED PWR SUPPLY M9010. LIGHTS OPS NML.Jun 15, 1998 · N124DE · Boeing 767332 · Emergency LightingSDR DL76S971347Skin · delaminatedTHE NR 9 LE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 3.5 DIAMETER SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED IN THE CENTER OF THE SLAT WEDGE FWD/ AFT AND INB'D/OUTB'D. THE DAMAGED SECTION WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201.Jul 1, 1997 · N124DE · Boeing 767332 · Leading Edge Devices
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