N29124
Service difficulty reports · 89
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 = 'N29124' 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 = 'N29124' 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 CALA2022061501514Panel · arcedP-37 ARCHING FOUND AMONG EXISTING WIRING AT TERMINAL LUGS AND BR EAKERS. EA 4420-02847 REV C OP 014. REPORTED BY V931833 REPLACED WIRE W1272-006-12 AND W1272-0020-08 TERMINAL LUGS TO CB 02. NO ARCHING OR FIRE DAMAGE FOUND, EXCLUDING THE DAMAGE REFERE 3-26-00. SDR CALA2022061001477Structure · corrodedREF AMES NR 0100-0200 ALC DOOR CUTOUT SILL PLATE UNDERSIDE FOUND TO BE CORRODED @ STA. 1400-1410 WHILE ACC OMPLISHING REPAIR @ STA. 1390. REMOVED AND REPLACE ALC UPPER CORD AT DOOR THRESHOLD, WITH NEW P ART P/N: 146N8522-51 IAW BOEING DRAWLING: 146N8522-REV A SDR CALA2022052701361Skin · damagedREF AMES NR 0100-0224. DENT/GOUGE ON LEFT HAND SIDE FUSELAGE STA LINE 450 WATERLINE 167 REQUIRES REPAIR DUE TO OUT OF LIMITS. REPAIRED DAMAGED AREA AT WL 167 STA 457 L/H SIDE IAW AMES REA 47486REA03. ACCOMPLISHED BY V931857.SDR CALA2022051101207None · dentedREF AMES NR 0100-0224. DENT/GOUGE ON LEFT HAND SIDE FUSELAGE STA LINE 450 WATERLINE 167 REQUIRES REPAIR DUE TO OUT OF LIMITS. REPAIRED DAMAGED AREA AT WL 167 STA 457 L/H SIDE IAW AMES REA 47486REA03. ACCOMPLISHED BY V931857.SDR CALA2022050601157None · corrodedREF AMES NR 0100-0200 ALC DOOR CUTOUT SILL PLATE UNDERSIDE FOUND TO BE CORRODED @ STA. 1400-1410 WHILE ACC OMPLISHING REPAIR @ STA. 1390. REMOVED AND REPLACE ALC UPPER CORD AT DOOR THRESHOLD, WITH NEW P ART P/N: 146N8522-51 IAW BOEING DRAWLING: 146N8522-REV A SDR CALA2022050201110Beam · corrodedSTA 365BLO FLOOR SUPPORT STRUCTURE HAS CORROSION. REPORTED BY V9 21209 FOUND AREA ON FLOOR SUPPORT TO BE OUT OF LIMITS. REMOVED AND REP LACED FLOOR SUPPORT FROM STA 365B BLO IAW B757 SRM 51-40-02 PARA GRAPH 7. REF NON-ROUTINE 145078-0100-0161 FOR INFOSDR CALA2022041400989Angle · crackedREF AMES N/R 0100-0049 A SUPPORT ANGLE IS CRACKED AT B STA 1180, S-29R AT EXTERNAL LWR FUSELAGE. REMOVE AND REPALCED ANGLE PN 146N7528066 IAW B757 SRM 51-40-22 P ARA 7 51-31-01 SEE REVERSE FOR PARTIAL WORKSDR CALA2022041400988Floor Support · corrodedSTA 365BLO FLOOR SUPPORT STRUCTURE HAS CORROSION. REPORTED BY V9 21209 FOUND AREA ON FLOOR SUPPORT TO BE OUT OF LIMITS. REMOVED AND REP LACED FLOOR SUPPORT FROM STA 365B BLO IAW B757 SRM 51-40-02 PARA GRAPH 7. REF NON-ROUTINE 145078-0100-0161 FOR INFOSDR CALA2022040800911Skin · stainedFLOOR SUPPORT STRUCTURE BELOW AFT R/H LAV HAS BLUE WATER RESUIDU E AT STA 1620-1681 S29R - S29L. CLEANED FLOOR SUPPORT STRUCTURE BELOW RH LAV STA 1620-1681 S29R- 29L IAW SOPM 20-30-03 AND ECRA 2011-01000.SDR CALA2018041001139Fitting · crackedCRACK FOUND ON THE CABIN FLOORBEAM STABILIZATION STRAP IN THE FWD CARGO, BS 562, LBL 45. REPAIRED IAW SRM 53-00-51, REPAIR 12, FIG 201.SDR CALA2018031200882Slide · low pressureR1 DOOR SLIDE BOTTLE PRESSURE LOW PROCURED SERVICEABLE R1 DOOR SLIDE P/N D30654-122 S/N 1242, INSTALLATION ACCOMPLISHED ON CARD EA5210-01361 REV F SEQ 656. ROTABLE PARTS CHANGE WAS INDICATED - TT 1291971 SN OFF 0644 PARTS CHANGE FOR SLIDE WAS ACCOMPLISHED ON SDR CALA2018031200883Girt Bar · damagedR1 SERVICE DOOR GIRT BAR FAILED THE LEAF SPRING INSPECTION PROCURED. NEW R1 SERVICE DOOR GIRT BAR P/N 140N2762-26, INSTALLED, ACCOMPLISHED ON CARD EA2560-02123 REV D LOG PAGE 6425888 PARTS CHANGE ENTER IN ERROR SLIDE P/N D30654-122 S/N 1242 IS FOR PROCURED SERSDR CALA2018031200874Wedge · chafedRT WING SLAT 8 TE WEDGE HAS CHAFE MARKE ON INTERIOR SIDE AT FSS 464. REPAIRED RT WING SLAT NR 8 T/E WEDGE PER SRM 51-70-10.SDR CALA2018030500838Strap · brokenLT TUNNEL FLOORBEAM STABILIZER STRAP AT BS 365 FOUND BROKEN. REPAIRED IAW SRM 53-00-51, REPAIR 12.SDR CALA2018022800827Frame · dentedDENT ON AFT CARGO UPPER FRAME FLANGE AT BS 1440 ABOVE STRINGER 26L. FOUND DENT OUT OF LIMITS IAW SRM 53-00-07, FIG 101. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201.SDR CALA2018022400797Strap · crackedCRACKED STABILIZATION STRAP IN AFT CARGO CEILING AT STA 1380 RBL-45. ACCOMPLISHED REPAIR ON STABILIZATION STRAP ON AFT CARGO COMPT CEILING AT STA 1380 RBL 45 IAW SRM 53-00-51 REPAIR 12.SDR CALA2018020200437Light · inoperativeRIGHT FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED IAW WDM 33-51-12, OPS CHECKED OKSDR CALA2017080802511Mount · brokenFLT CONTROL YOKE LOCKED IN FULL LEFT POSITION DURING CHECK, NO RETURN TO CENTER. LATERAL TRIM CONTROL ACTUATOR MOUNTING BOSS ON AIRFRAME BROKEN OFF CAUSING THE LATERAL FEEL, CENTERING AND TRIM MECHANISM DRUM ASSEMBLY TO BIND. THE LATERAL CONTROL SUPPORT BOX CSDR CALA2017051201369Oven · odorGALLEY OVEN INOP AT 413. OVEN 413 LOUD NOISE AND BAD SMELL, UNUSABLE. AFTER RESET WORKS SATIS.SDR CALA2017051201358Oven · failedOVEN 413 POWERED ITSELF OFF. HAS ELECTRICAL BURNING ODOR AND TRIPS THE CIRCUIT BREAKER. REMOVED AND REPLACED THE OVEN IAW IFM 25-32-75. OPS CHECKED GOOD.SDR CALA2016010400025Windshield · crackedCAPTAIN FRONT WINDOWS, OUTSIDE PANEL SHATTERED IN FLIGHT. REPLACED L1 WINDOWS IAW MM 56-11-01-004-001 & EA 3040-01164 WINDOW CHANGE WIRE UPGRADE. OPERATIONS NORMAL ROTABLE PARTS CHANGE WAS INDICATED. TT 1470906, SN OFF 09429 WINDSHIELD, B75 OFF 19-5611-9-90SDR CALA2015020600084Angle · corrodedCORROSION AROUND FASTENERS L1 DOOR Z ANGLE. REPAIRED L1 DOOR SURROUND LOWER SILL ANGLE IAW ECRA 5300-02115.SDR CALA2014100601313Gcu · failedL EEC, L ENG LIMITER, & 'AUTO THROTTLE DISC AT LEVEL OFF FL 330. FOLLOWED QRH COMPLIED WITH FIM 73R-21 TASK 820. R & R UPPER DGCU A OPERATIONS CHECK OK. ROTABLE PARTS CHANGE WAS INDICATED TT 1622849 SN OFF 00755 CONTROL, POWER OFF 19-7321-9-0016 0755 ON 19SDR CALA2014070300864Transmitter · failed1.5 HOURS INTO FLIGHT LT ENG BLEED OFF LIGHT ILLUMINATED, FOLLOWED BY LT CTR FUEL PUMP LIGHT. FOLLOWED QRH CARRIED OUT T - S IAW MM 28-22-00-815-804 PG 1. DEFAULTED TO N3 HP TACHOMETER TRANSMITTER & REPLACED IAW MM 77-12-02-404-005-R-00. REPAIRED CONNECTOR SDR CALA2014051600604Bleed Air Sys · contaminatedDURING CRUISE LAVATORY SMOKE ANNUNCIATOR ILLUMINATED. LAVATORY DETECTORS IN LAVATORIES S2L+4L SOUNDED. RAN CHECKLIST, DIVERT & LAVATORY SMOKE ANNUNCIATOR LIGHT WHEN OUT. PERFORMED MM TASK 05-51-58-910-801C1 & TASK 21-00-01-002-001. FOUND CONTAMINATED DUCTS SDR CALA2014051300591Engine · malfunctionedAPPROXIMATELY 1:45 EN ROUTE FROM LAX TO KONA WE GOT THE LAVATORY SMOKE ADVISORY MSG. FIRST OFFICER RAN CHECKLIST. RETURNED TO LAX, APPROXIMATELY 30 MIN LATER WE NOTICED HIGH OIL TEMP & LOW OIL PRESS BUT STILL IN AMBER. ALSO LOW OIL QTY APPROXIMATELY 10 QTS SDR CALA2012110600745Pressure Sensor · inoperativeENGINE SURGES WITH ANY POWER OTHER THAN IDLE. ALSO, WITH ENG ANTI-ICE ON IT SURGES AT IDLE WITH ENG ANTI-ICE ON. IAW FIM TEST 71-06-00-815-803-R-00 CHECKED P1 & P4 TUBES, IP/ HP SOLENOID PHYSICAL COND. PF RAKES FOUND NO ABNORM PERFORMED TEST NR 3 IAW 71-00-00SDR CALA2012051600354Anti-Ice Valve · malfunctionedLEFT ENG ANTI-ICE EICAS MESSAGE AND LT ENG DISAGREEMENT LIGHT ILLUMINATED IN FLIGHT. AIR RETURN WAS DONE. R & R LT ENGINE TAI VALVE IAW AMM30-21-03-404- 016, OPS AND LEAK CHECKS OK. ROTABLE PARTS CHANGE WAS INDICATED - TT 1537808, SN OFF 01011, VALVE, ANTI-ISDR CALA2012011600022Latch · dirtyOXYGEN MASK ABOVE ROW 27DEF DID NOT DEPLOY DURING CABIN ALTITUDE WARNING SWITCH FUNCTIONAL TEST. CHECKED DOOR AND LATCH MECHANISM FOR OPERATION. CLEANED LATCHES, REPACKED MASKS REF AMM 35-21-05 OPS. CHECK GOOD.SDR CALA2012011600021Latch · dirtyOXYGEN MASK LOCATED AT FLIGHT ATTENDENT STATION AT L2 DOOR DID NOT DEPLOY DURING THE CABIN ALTITUDE WARNING SWITCH FUNCTIONAL TEST. CHECKED DOOR AND LATCH MECHANISM FOR PROPER OPERATION. CLEANED LATCHES, REPACKED MASKS REF AMM 35-21-05, OPS CHECK GOOD.SDR CALA2012011600020Latch · dirtyOXYGEN MASK ABOVE SEAT ROW 23ABC DID NOT DEPLOY DURING THE CABIN ALTITUDE WARNING SWITCH FUNCTIONAL TEST. CHECKED DOOR AND LATCH MECHANISM FOR PROPER OPERATION. CLEANED LATCHES, REPACKED MASKS REF AMM 35-21-05 OPS. CHECK GOOD.SDR CALA2011021400090Fuse · blownAISLE PATH LIGHTING INOP AFT OF ROW 30 T/S IAW WDM33-51-22. FOUND BLOWN FUSE ON M736 & M737 REPLACED FUSE, CHECKED FOR FAULTS NONE NOTED, OPS CHECK NORMAL.SDR CALA2009072400393Computer · failedTCAS C/B POPPED DURING FLIGHT, TCAS EICAS MSG (ELECTRICAL ODOR OBSERVED) FOUND TCAS COMPUTER NOT TESTING AND WHEN TCAS TEST PERFORMED IN EITHER POSITION TCAS FAIL DISPLAYED. REMOVED AND REPLACED TCAS COMPUTER PER AMM 34-45-01, OPS CHECK GOOD. REPLACED C/B "TSDR CALA2009051900264Floorbeam · corrodedB757-53-3-0427 MAIN CABIN FLOOR, CORROSION ON FLOORBEAM AT STA 715 RBL 27, ABOVE AND BELOW FASTENER HOLE. DUPLICATE L/P CREATED FOR SCEPTRE AND ESFR REPORTING ONLY, DUE TO REV A OF ECRA. ECRA THAT WAS REVISED IS EC/RA 5310-04943 REV A. ALL WORK ACCOMPLISHEDSDR CALA2009050500238Pressure Panel · corrodedAFT CABIN FLOOR PRESSURE DECK AT STATION 1715, LBL 0 CORROSION PRESENT. CUT OUT DAMAGE, FABRICATED, INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-60-51, REPAIR 2, FIG 201.SDR CALA2009013000073Light · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED R-2 DOOR EXTERIOR EMERGENCY LIGHT LAMP HOLDER ASSY IAW AMM 33-51-06. OPS CHECKS NORMAL.SDR CALA0300640Skin · gougedINSPECTION FOUND RT TRAILING EDGE O/B MAIN FLAP NOSE SKIN GOUGED AT WBL 558. THE FLAP NOSE SKIN WAS REPAIRED IAW SRM 57-53-01 FIGURE 202.SDR CALA0300626Frame · puncturedINSPECTION FOUND AFT CARGO PIT FRAME PUNCTURED AT BS 1340, S25R. REPAIRED IAW SRM 51-70-11.SDR CALA9800492Bolt · shearedWHEN GEAR UP WAS SELECTED AFTER TAKEOFF, THE GEAR AND GEAR DOOR LIGHTS REMAINED ON WITH EICAS MESSAGE OF GEAR DOORS AND GEAR DISAGREE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A SHEARED BOLT IN NLG DOOR OPERATED SE
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