N37882, cancelled Aug 15, 2003
Service difficulty reports · 58
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 = 'N37882' AND deregistration_id = 'N37882-2003-08-15' 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 = 'N37882' AND deregistration_id = 'N37882-2003-08-15' 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 CALA0100582Strut · deflatedTHE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHILE ENROUTE TO EWR. THE CREW FOLLOWED QRH PROCEDURES. WHEN THE GEAR WAS LOWERED ALL THREE GEAR INDICATED DOWN AND LOCKED. QRH PROCEDURES WERE CONTINUED AND WHEN CREW ATTEMPTED TO RAISE GEAR THE HANDLE WOULD NOT COME UP.SDR CALA0100030Strut · dischargedTHE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM BOS. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE NOSE GEAR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE THE FAILURE. THE STRUT PRESSURE WAS FOUND LOW. THE NOSE STRUT WASSDR CALA0001808Strut · dischargedTHE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM DTW. THE NOSE GEAR INDICATED UNSAFE AND A LOUD MECHANICAL CLUNKING NOISE WAS HEARD. THE GEAR WAS CYCLED WITH NO CHANGE IN RESULTS. THE GROUND CONTROL ALSO REVERTED TO THE GROUND MODE. THE AIRCRAFT WAS DIVERTED TSDR CALA0001173O-Ring · leakingTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM TPA. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SCHRADER VALVE O-RING LEAKING AND THE STRUT WAS FLAT. THE O-RING WASDR CALA0000277Support · crackedINSPECTION FOUND A 6 INCH CRACK IN FORWARD CARGO BAY GILL LINER SUPPORT FRAME AT FS 408, LONGERON 25L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-10-4.SDR CALA0000276Support · corrodedINSPECTION FOUND AFT CARGO LOWER AFT DOOR JAMB CORNER SUPPORT CORRODED AT LONGERON 27R. THE CORNER SUPPORT WAS REMOVED AND A NEW CORNER SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.SDR CALA0000269Skin · gougedINSPECTION FOUND LEFT VERTICAL STABILIZER SKIN GOUGED ALONG HORIZONTAL STABILIZER RUN LINE. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 51-30-5.SDR CALA0000268Skin · crackedINSPECTION FOUND A CRACK IN FORWARD LAV SERVICE DOOR LOWER AFT CORNER. THE DOOR WAS REMOVED AND A NEW DOOR WAS INSTALLED IAW SRM 51-30-2.SDR CALA0000267Door Pan · puncturedINSPECTION FOUND A PUNCTURE IN R-1 DOOR AT LOWER AFT INTERNAL PAN. A PLUG REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 1.SDR CALA0000266Angle · crackedINSPECTION FOUND A 3.5 INCH CRACK IN RT APU DOOR Z-ANGLE AT FS 1320, LONGERON 27R. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-10-04, AND 51-10-3.SDR CALA0000265Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN LEFT APU DOOR SKIN AT I/B EDGE, FS 1320, LONGERON 30. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 2 AND 51-30-2..SDR CALA0000264Angle · crackedINSPECTION FOUND A 4.2 INCH CRACK IN ANGLE IN AFT PIT AT FS 1250-1271, LONGERON 25L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-01, 51-30-1, AND 53-14-3.SDR CALA0000263Angle · crackedINSPECTION FOUND L-1 DOOR UPPER AND LOWER ATTACH ANGLES CRACKED. THE CRACKS WERE 0.75 LONG. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, 51-30-5, AND 51-30-7.SDR CALA0000262Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN AFT CARGO BAY GILL LINER SUPPORT FRAME AT STA 1309, LONGERON 23L. THE CRACK WAS STOP DRILLED IAW SRM 53-01-2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01-2.SDR CALA0000261Floorbeam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO BAY GILL-LINER FLOOR SUPPORT FRAME AT STA 503, LONGERON 25L. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.SDR CALA0000260Support · crackedINSPECTION FOUND MID CARGO BAY BULKHEAD VERTICAL SUPPORT CRACKED AT STA 541. THE VERTICAL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR CALA0000259Angle · crackedINSPECTION FOUND A 10 INCH CRACK IN HORIZONTAL STABILIZER RIGHT I/B LEADING EDGE I/B ANGLE AT XHR 9.652. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-04, AND 51-30-01.SDR CALA0000240Angle · crackedINSPECTION FOUND ANGLE CRACKED THROUGH LOWER ACCESS PANEL NR 7406 OF NR 2 ENGINE NOSE COWL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.SDR CALA0000237Skin · crackedINSPECTION FOUND RT WING LEADING EDGE SKIN CRACKED AT I/B END OF REFUELING DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 57-06B, FIGURE 3 AND 51-30-1.SDR CALA0000236Frame · crackedINSPECTION FOUND LT SIDE OF CANTED FRAME CRACKED JUST O/B OF LIGHT ASSEMBLY IN TAIL COMPARTMENT AT FS 1485. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, SHEETS 3 AND 4, 51-30-2, AND 51-30-5, PAGE 4.SDR CALA0000235Beam · corrodedINSPECTION FOUND AFT CARGO DOOR JAMB BEAM CORRODED. THE DOOR JAMB BEAM WAS REPAIRED IAW ECRA 5310-03027, SRM 51-30-2, AND 51-30-5.SDR CALA0000234Fitting · crackedINSPECTION FOUND LONGERON 25R END FITTING CRACKED IN AFT CARGO BAY AT STA 1220. THE FITTING WAS REMOVED AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.SDR CALA0000233Floorbeam · crackedINSPECTION FOUND FLOOR SUPPORT CRACKED IN AFT CARGO BAY AT STA 1271, L28L. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2 AND 51-10-4. REMOVED GUSSETS AND FASTENERS FROM INTERCOSTAL TO GAIN ACCESS TO TRAPPED FASTENER AND REINSTALLED IAW SRM 51-30-2 AND 51-10-SDR CALA0000228Skin · dentedINSPECTION FOUND RT WING L/E SKIN DENTED JUST FORWARD OF REFUELING DOOR. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 57-06B, FIGURE 5, 51-10-4, 51-10-3, 51-20-00, 51-30-2, AND 51-30-5.SDR CALA0000227Frame · crackedINSPECTION FOUND FLOOR SUPPORT FRAMES CRACKED IN AFT CARGO BAY AT STA 1250, L29L AND AT STA 1117, L27L. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.SDR CALA0000226Frame · crackedINSPECTION FOUND GILL-LINER SUPPORT FRAMES CRACKED IN AFT CARGO BAY AT STA 1060-1297, L24R TO L27R. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2.SDR CALA9900443Actuator · leakingWITH APU AIR ON AND PACKS ON, CABIN FILLS WITH SMOKE AND STRONG BURNING SMELL. FOUND LEFT GEAR RETRACT ACTUATOR IN TRANSIT LEAK. REMOVED AND REPLACED ACTUATOR PER MM 32-32-02. PERFORMED BURN OUT OF PNEUMATIC DUCT PER MM 21-20-02.SDR CALA990022Recepticle · wornTAIL CONE TOP FIVE ALIGNMENT PIN RECEPTICLES WORN. REPLACED TOP FIVE ALIGNMENT PIN RECEPTICLES.SDR CALA9900023Support · corrodedFLOOR SUPPORT HAT SECTION CORRODED STA 148 - 200. FABRICATED AND INSTALLED NEW HAT SECTION PER SRM 51-30-01.SDR CALA9800278Longeron · crackedINSPECTION FOUND A .4375 INCH CRACK T CAP AT STA 1338, LONGERON 14R. REPAIRED IAW EA 5310-01272.SDR CALA9800277Pan · crackedINSPECTION FOUND A 1.5 CRACK IN AFT ENTRY DOOR PAN AND A 1.5 CRACK IN INNER PAN ANGLE AT CENTER RT DOOR STOP PAD. REPAIRS WERE INSTALLED IAW ECRA 5220-01034.SDR CALA9800275Frame · gougedINSPECTION FOUND THAT THE LEFT HEAT VALVE HAD GOUGED THE FRAME INNER CAP AT STA 1380. A REPAIR STRAP WAS INSTALLED IAW ECRA 5311-01042.SDR CALA9800274Skin · chafedINSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR SKIN CHAFED IN SEVERAL PLACES BELOW LOCK HANDLE. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5230-01397.SDR CALA9800273Skin · oversize holesINSPECTION FOUND OVERSIZED HOLES IN FUSELAGE SKIN AT OUTER DORSAL FIN ATTACH ANGLE ON LEFT AND RIGHT SIDES. REPAIRED IAW ECRA 5340-01312.SDR CALA9800272Cusp Beam · corrodedINSPECTION FOUND CUSP BEAM CORRODED AT STA 200, LONGERON 18L. REPAIRED IAW ECRA 5310-03678.SDR CALA9800271Cusp Beam · corrodedINSPECTION FOUND CUSP BEAM CORRODED AT STA 229, LONGERON 18L. REPAIRED IAW ECRA 5310-03678.SDR CALA9800266Beltframe · corrodedINSPECTION FOUND BELTFRAME CORRODED ACROSS BOTTOM ON FRONT CENTER AND LOWER CHANNEL AT STA 1322 FROM LONGERON 28L TO 28R. A REPAIR WAS INSTALLED IAW SRM 53-03.SDR CALA9800257Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT FLOOR LEVEL AFT OF L-1 DOOR, STA 218 TO 256, LONGERON 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-01204.SDR CALA9800256Angle · crackedINSPECTION FOUND A .125 INCH CRACK IN MAIN CABIN DOOR ANGLE AT BAYONET CUTOUT. REPAIRED IAW SRM 52-05, FIGURE 33.SDR CALA9800255Beam · crackedINSPECTION FOUND A 1.25 INCH CRACK AT AFT END OF MAIN CABIN DOOR NR 7 BEAM AND A 1 INCH CRACK WAS LOCATED AT FORWARD END OF NR 7 BEAM. A 1 INCH CRACK WAS FOUND AT FORWARD END OF MAIN CABIN DOOR NR 8 BEAM. A .75 INCH CRACK WAS FOUND AT FORWARD END OF MAIN CABSDR CALA9800217Longeron · corrodedINSPECTION FOUND LONGERON 29R CORRODED UNDER FLANGE AT STA 1322. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR CALA9800214Pivot Plates · corrodedINSPECTION FOUND INBOARD AND OUTBOARD SET OF HINGE PIVOT PLATES CORRODED ON RT HORIZONTAL STABILIZER. THE OUTBOARD SET OF HINGE PIVOT PLATES WERE FOUND CORRODED ON LT HORIZONTAL STABILIZER. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW SRM 51-30-5.SDR CALA9800194Beam · corrodedINSPECTION FOUND MID BAGGAGE BIN DOOR JAMB BEAM CORRODED. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 63.SDR CALA9800150Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN PANEL D AND E AT STA 148 TO 160, FORWARD ENTRY AREA. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01, 51-10-3, AND 51-30-2.SDR CALA9700179Actuator · leakingTHE RT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO ACCOMPANIED BY THE RT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATING WHILE EN ROUTE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD FLAP ACTUATOR LEAKING. THE FLAP ACTUATOR WAS REPLACED IAW SDR CALA9601817Actuator · leakingTHE RT HYDRAULIC QUANTITY WAS LOST WHILE ON APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEAL LEAKING AT LEFT INBOARD FLAP ACTUATOR. THE LT INBOARD FLAP ACTUATOR CYLINDER WAS REPLACED IAW MM 27-52-02. THE FLAPS AND ALL OTHER FLIGHT CONSDR CALA9601055Bus Gen Cont · inoperativeBOTH GENERATOR OFF-LIGHTS ILLUMINATED AND ALL GENERATOR POWER WAS LOST DURING CLIMB AT 9,000 FEET. THE AC CROSSTIE LOCKOUT LIGHT ALSO CAME ON. THE GENERATORS WERE RESET AND OPERATION WAS NORMAL, BUT THE AC CROSSTIE LOCKOUT LIGHT REMAINED ILLUMINATED. THE FLSDR CALA9600871Ckt Breaker · failedTHE RT AC BUS 50 AMP CIRCUIT BREAKER, AFT CENTER AND LEFT FUEL BOOST PUMP CIRCUIT BREAKERS POPPED WHILE EN ROUTE. CREW ATTEMPTED TO RESET CIRCUIT BREAKERS WITHOUT SUCCESS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SDR CAL960424Strut · flatFLT NR 303 - EWR - THE N/G WOULD NOT RETRACT AFTER T/O FROM EWR. THE GEAR HANDLE WAS CYCLED SEVERAL TIMES, BUT WOULD NOT RAISE BEYOND HALFWAY POINT. THE AUTO SPOILER 'DO NOT' USE LIGHT WAS ON AND THE A/C WOULD NOT PRESSURIZE. THE A/C WAS RETURNED TO EWR WHESDR CAL960109Handle · lack of lubeFLT NR 1490 - CLE - THE FLAP/SLAT HANDLE WOULD NOT LOCK INTO THE SLAT RETRACT POSITION. WHEN HOLDING FLAP/SLAT HANDLE TO SLAT RETRACT POSITION THE SLAT DISAGREE LIGHT CAME ON AND BOTH LEFT AND RIGHT HYDRAULIC GAUGES DROPPED. THE DIAL-A-FLAP WAS MOVED SEVERAL
Back to N37882, cancelled Aug 15, 2003