N124HQ
Service difficulty reports · 93
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 = 'N124HQ' AND registry_match = 'registration' 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.
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 = 'N124HQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR R61A201312141333Pin · damagedDURING HEAVY CHECK, LEFT MLG FWD PINTLE PIN HAS A LARGE PIECE OF MISSING PLATING AND RUST. MX R & R LT MLG FWD PINTLE PIN IAW AMM 32-11-01.SDR R61A201312141332Bracket · crackedDURING HEAVY CHECK, CO PILOTS AILERON CABLE PULLY BRACKET BETWEEN FRAMS 14,15 IS CRACKED ON AFT CORNER. MX FOR WORK ACCOMPLISHED SEE CONTINUATION CARD VP-041872-2013/623 C1,C2. REMOVED DAMAGED AREA IAW ETD 2013-170-068172, REV A, NDT (HFEC) OF DAMAGED REMOVSDR R61A201312141320Bolt · corrodedDURING HEAVY CHECK, LT HORIZONTAL STAB INTERNAL HINGE PIN IS CORRODED. MAINTENANCE R & R LT HORIZONTAL STAB HINGE PIN IAW AMM 27-41-03, PN NAS6314-74D, BOLT. AIRCRAFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.SDR R61A201312131341Line · degradedDURING HEAVY CHECK, LT WING FUEL VENT LINE HAS SURFACE DEGRADATION. MX R & R LT WING FUEL VENT LINE IAW AMM 20-10-13.SDR R61A201312131340Coupling · degradedDURING HEAVY CHECK, FUEL VENT COUPLINGS SHOW SIGNS OF DEGRADATION . MX R & R FUEL VENT COUPLING IN LT WING.SDR R61A201312131339Clamp · deterioratedDURING HEAVY CHECK, FUEL VENT CLAMPS, DETERIORATING IN LT WING. MX R & R ALL FUEL VENT CLAMPS IN LT WING IAW AMM 20-13-21.SDR R61A201312131327Nut · corrodedDURING HEAVY CHECK, LT MLG GLAND NUT CORROSION ON THREADS. MAINTENANCE R & R LT MLG GLAND NUT IAW AMM 32-11-04.SDR R61A201312121334Nut Plate · corrodedDURING HEAVY CHECK, FWD CARGO DOOR CUT OUT LOWER SILL HAS CORROSION AROUND NUT PLATES AND SILL ITSELF. MAINTENANCE BLENDED FWD CARGO DOOR CUT OUT LOWER BEAM FOUND TO BE WITHIN LIMITS, IAW ETD 2013-170-068305. REF CONTINUATION CARDS C1, C2, C3 FOR WORK STEPS DISDR R61A201312111344Nut · corrodedDURING HEAVY CHECK, AFT CARGO FWD LATCH FITTING FWD TOP NUT CORRODED. MAINTENANCE R & R AFT CARGO FWD LATCH FITTING FWD TOP NUT AND WASHER IAW AMM 20-10-01. PN MS21133-06, NUT, AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.SDR R61A201312111326Bolt · corrodedDURING HEAVY CHECK, RT ELEVATOR PCU LOWER MOUNT BOLTS HAVE CORROSION ON BOLT HEADS. MAINTENANCE R & R MOUNT BOLTS IAW AMM 27-32-01.SDR R61A201312111325Pan · crackedDURING HEAVY CHECK, SEAT PANS CRACKED AT SEATS 17D, 17F, 11F, 11D. MX R & R SEAT PAN IAW SRM 51-42-01, 51-40-02.SDR R61A201312111324Panel · crackedDURING HEAVY CHECK, LT FORWARD WHEEL WELL PANEL HAS CRACK IN THE WEB WHERE THE CABLES PASS THROUGH. MX R & R CRACKED RIB ON FWD SIDE OF LT WHEEL WELL IAW SRM 51-42-01, 51-40-02.SDR R61A201312111321Seat Track · corrodedDURING HEAVY CHECK, RT INBD SEAT TRACK FRAMES 85-90 CORRODED. MX R & R SEAT TRACK IAW SRM 51-40-02, 51-41-01, AND 51-43-03.SDR R61A201312111319Seat Track · corrodedDURING HEAVY CHECK, LT INBD SEAT TRACK FRAME 90 CORRODED. MX R & R IAW SRM 51-40-02, 51-41-02.SDR R61A201312111318Seat Track · corrodedDURING HEAVY CHECK, RT INBD SEAT TRACK EXTENSION TOP SHEAR CLIP AT FRAME 90 CORRODED. MX R & R SHEAR CLIP AT FRAME 90 RT IAW SRM 51-40-02, 51-41-02.SDR R61A201312111317Floor Support · corrodedDURING HEAVY CHECK, FLOOR SUPPORT FRAMES 87-88 CORRODED. R & R FLOOR SUPPORT IAW IAW SRM 51-40-02, 51-42-01.SDR R61A201312101342Attach Fitting · corrodedDURING HEAVY CHECK, AFT CARGO FLOOR PANEL 151CF PUCKS ARE CORRODED. MX R & R PUCKS IAW AMM 50-31-008.SDR R61A201312101316Seat Track · corrodedDURING HEAVY CHECK, LT SEAT TRACK HAS LIGHT CORROSION IN SPOTS AROUND FRAME 18. MX R & R SEAT TRACK IAW SRM 51-41-01, 51-41-02, & 51-43-01.SDR R61A201312101315Seat Track · corrodedDURING HEAVY CHECK, RT SEAT TRACK HAS LIGHT SPOTS OF CORROSION ON FRAMES 15, 16, 17. MX R & R RT SEAT TRACK IAW SRM 51-41-02, 51-40-02, & 51-23-06.SDR R61A201312091314Joint · corrodedDURING HEAVY CHECK, AFT GALLEY FWD AND AFT SPLIT JOINTS FOUND CORRODED. R & R DAMAGED SPLIT JOINTS IAW AMM 25-00-23, 25-00-05, & 20-10-01.SDR R61A201312081323Spacer · corrodedDURING HEAVY CHECK, PANEL 192BL HAS CORROSION AROUND SCREW HOLES ON THE SPACER. MX REMOVED SPACER MATCH DRILLED NEW SPACER INSTALLED SPACER RESTORED TOP COAT IAW SRM 51-40-02, 51-41-02, 51-43-06.SDR R61A201310111004Battery · inoperativeCREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE FORWARD F/A FLASHLIGHT BATTERY IAW AMM AND OPS CHECKED GOOD.SDR R61A201308200754Glowstrip · looseCREW REPORTED THAT THE PHOTO LUMINESCENT STRIP NEXT TO SEAT 1D WAS LOOSE. MX SECURED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD.SDR R61A201308010686Girt Bar · detachedCREW REPORTED THAT THE L2 DOOR GIRT BAR INDICATOR IS NOT SHOWING RED WHEN SLIDE IS ARMED. ON CALL, MX FOUND THE GIRT BAR UNHOOKED FROM ITS CLIP. MX REINSTALLED GIRT BAR IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.SDR R61A201307010566Glowstrip · inoperativeCREW REPORTED THAT THE PHOTOLUMINESCENT STRIP IN FRONT OF SEAT 1D NO LONGER GLOWS AND APPEARS TO HAVE HAD A DRINK SPILLED ON IT. MX REMOVED, CLEANED AND REINSTALLED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD.SDR R61A201305110457Flashlight · missingCREW REPORTED THAT THE FORWARD FLIGHT ATTENDANT FLASHLIGHT WAS MISSING. MAINTENANCE INSTALLED SERVICEABLE FLASHLIGHT PER EMB AMM AND OPS CHECKED GOOD.SDR R61A201304230400Mechanism · out of adjustCREW REPORTED THAT THE L2 DOOR ARMING LEVER IS STICKING AND HARD TO ARM & DISARM. MAINTENANCE ADJUSTED L2 DOOR CONTROL MECHANISM AND PERFORMED OPS CHECKS PER EMB AMM 52-12-52. OPS CHECKED GOOD.SDR R61A201303150279Seat Belt · brokenCREW REPORTED THAT THE DEMO SEAT BELT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED SEAT BELT PER EMB AMM AND OPS CHECKED GOOD.SDR R61A201303090263Handle · out of adjustCREW REPORTED THAT THE AFT L2 DOOR VENT HANDLE AND THE ARMING HANDLE ARE NOT COMING UP AT THE SAME TIME. MAINTENANCE PERFORMED DOOR ADJUSTMENT TEST PER EMB AMM 52-12-00 AND OPS CHECKED GOOD.SDR R61A201210230597Slide · partial deployCREW REPORTED THAT THE GIRT BAR WAS STILL ATTACHED TO THE FUSELAGE WHEN THE DOOR WAS OPENED CAUSING THE EMERGENCY EVACUATION SLIDE TO PARTIALLY BLOW. MAINTENANCE REPLACED THE SLIDE AND CABLE PER EMB AMM.SDR R61A201202010080Gusset · corrodedWHILE A/C WAS IN FOR HEAVY CHECK FOUND GUSSET ON FR 89 FOR OUTBOARD PUCK POSITION OF FLOOR PANEL 252ERF HAS CORROSION. MX REMOVED AND REPLACED GUSSET PLATE AT FR 89, AFT GALLEY FLOOR AREA REF IAW EMB 170 SRM 51-42-02. PN 170-91919-001. A/C REMAINS IN CMH FOSDR R61A201202010081Support Angle · crackedWHILE A/C WAS IN FOR HEAVY CHECK FOUND LEFT WHEEL WELL FORWARD BULKHEAD SUPPORT ANGLE CRACKED. MX REMOVED AND REPLACED ANGLE IAW EMB 170 SRM 51-41-01, 51-42-01, 51-40-02, 51-23-06, 51-21-05. ANGLE PN 170-30709-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETSDR R61A201202010079Gusset · corrodedWHILE A/C WAS IN FOR HEAVY CHECK FOUND GUSSET ON FR 90 FOR FLOOR PANEL 252ERF, AFT PUCK POSITION HAS CORROSION. MX REMOVED AND REPLACED GUSSET PLATE PN 170-60259-001 AT FR 90 IAW EMB 175 SRM 51-41-02. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.SDR R61A20110320Flap · out of adjustCREW REPORTED R-1 DOOR WAS DIFFICULT TO OPEN. MAINTENANCE ADJUSTED R-1 DOOR VENT FLAP PER EMB AMM, OPS CHECK GOOD.SDR R61A20110279Unknown · malfunctionedCREW REPORTED R-1 DOOR WAS DIFFICULT TO DISARM. MAINTENANCE PERFORMED OPS CHECK OF R-1 DOOR ARMING HANDLE PER EMB AMM, OPS CHECK GOOD.SDR R61A20110132Flap Track · lack of lubeCREW REPORTED R-1 VENT FLAP HANDLE DIFFICULT TO MOVE. MAINTENANCE LUBED R-1 DOOR VENT FLAP TRACK SYSTEM PER EMB AMM, OPS CHECK GOOD.SDR R61A20110087Warning System · false activationCREW REPORTED SLAT FAIL ON APPROACH INTO SAV, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND PERFORMED OPS CHECK OF SLATS/FLAPS PER EMB AMM. NO DEFECTS WERE NOTED, AND A/C WAS RETURNED TO SERVICE.SDR R61A20100452Sensor · failedCREW REPORTED SLAT FAIL ON APPROACH INTO PHL, CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT AND RT SLAT 3/4 HARNESSES AND BOTH LT O/B SKEW SENSORS PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.SDR R61A20100451Warning System · malfunctionedCREW REPORTED SLAT FAIL ON APPROACH, DECLARED EMERGENCY AND DIVERTED TO MHT. A/C LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PER EMB AMM AND PERFORMED FIM 27-81-00-810-805-A AND REPORTED FAULT WAS A TRANSITORY CONDITION OF SFACE 1 AND 2. A/C WAS THEN RSDR R61A20080033Wheel · vibrationCREW REPORTED VIA ACARS AFTER TAKE OFF THE CREW HAD A NOSE WHEEL VIABRATION AND A BURNING ODOR IN COCKPIT. CREW HAD TOWER VIRIFY NOSE GEAR HAD BOTH NOSE WHEELS INDY TOWER DECLARED A EMERGENCY AFTER A GO AROUND CRE LANDED ACFT WITHOUT INCIDENT AND PROCEEDED TO SDR R612008F00004Sensor · failedCREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO EVALUATE. MAINTENANCE REMOVED AND REPLACED LT HAND OUT BOARD SLAT SKEW SENSOR SYSTEM OPERATIONAL CHECK GOOD. AIRCSDR R612008F00000Sensor · failedCREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO EVALUATE. MAINTENANCE REMOVED AND REPLACED LT OB SLAT SKEW SENSOR SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURSDR R612008F00001Slat System · malfunctionedCREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH. DECLARED AN EMERGENCY AND LANDED AIRCRAFT WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO EVALUATE, CLEARED SF ACE INHIBITS SLAT FAIL MESSAGE CLEARED AND FLAP SLOW RATE MESSAGE APPEARED PLACED SL
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