N57862
Service difficulty reports · 70
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 = 'N57862' 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 = 'N57862' 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 CALA2026091019359Access Door · missingINSTALLED NEW STRUT ACCESS DOOR ASSEMBLY REF AMM 54-53-01SDR CALA2026070617568Wire · pulledEMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH, ROW 22C RED EMER LIGHT INOPERATIVE. WIRING PULLED OUT OF ELECTRICAL CONNECTOR. REPLACED SEAT 22 LIGHT ASSY AND HOUSING AND TESTED GOOD IAW AMM 33-51-11-403-036.SDR CALA2026063017478Hub Cap · missingDURING ETOPS CHECKS THE MECHANICS NOTICED NR 2 WHEEL WAS MISSING THE HUB CAP. FOUND A PIECE OF HUB CAP ATTACHED AT THE 6 O'CLOCK POSITION SUGGESTING THE HUB CAP BROKE OFF AT SOME POINT. NO DAMAGE NOTED AT AFFECTED AREA. HUBCAP WAS REPLACED AND AIRCRAFT WAS DISDR CALA2026040315062Girt Bar · fodR1 DOOR WILL NOT ARM, AND NOW WILL NOT DISARM COMPLETELY. FOUND DEBRIS INLINE WITH GIRT BAR ATTACHMENT POINTS. CLEARED THE SAME. OPERATED DOOR THRU ARMED/ DISARMED SEVERAL TIMES. OPS SATISFACTORY. NO FURTHER ACTION REQUIRED. OK TO CONTINUE.SDR CALA2025110610937Light · no discrepancyOVERHEAD LIGHTING AT L1 DOOR FOUND INOPERATIVE ON ARRIVAL AT GATE, PROBLEM WAS RESOLVED. OPERATED FWD GALLEY LIGHTS WITH SLIDE ARMED & DISARMED, AS WELL AS WITH FLIGHT DECK DOOR OPEN AND CLOSED. ALL WORKS PROPERLY. GOOD FOR SERVICE.SDR CALA2025102810673Skin · crackedACCOMPLISH INITIAL INSPECTION OF RT WING UPPER SKIN FASTENER HOLES #1-18 IAW PART 2C OF THE LATEST REVISION OF EC/RA 5720-03571 ON OR BEFORE THE AIRCRAFT REACHES 25,379 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 6,000 FSDR CALA2025102810671Skin · corrodedREPAIR ON THE FUSELAGE SKIN BETWEEN STA 1540 - 1560 AND STR 27R - 29R AT LAVATORY SERVICE DOOR CUTOUT PER THE LATEST REVISION OF EC/RA 5330-07636SDR CALA2025092209094Oil System · leakingWHILE RUNNING THE APU BLEED THERE IS A STRONG ODOR IN THE CABIN. TS APU FOR SOUCE OF ODOR/OIL LEAKS. ACCOMPLISHED AMM 21-00-01-002-001 REMOVAL OF OIL CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEMS. RAN PACK FOR SEVERAL HOURS. ODOR IS NO LONGER SDR CALA2025091909050Apu · odorACFT SMELLS OF VAPOR & BURNING OIL WITH APU & ENG BLEED. REPLACED RECIRCULATION FILTERS IAW 21-25-02/401. RAN APU AND BOTH ENGINES ONE AT A TIME. THE ODOR WAS ONLY NOTICEABLE WHEN USING THE APU BLEED. ENINE RUNS WERE NORMAL. SUGGEST PLACING APU BLEED ON SDR CALA2025091909047Cooling Fan · leakingCREW REPORTS AUTO SHUTDOWN OF APU AFTER CREW NOTICED & WAS INFORMED OF SMOKE & ODOR COMING FROM VENTILATION SYS. CREW SHUTDOWN PACS & APU BLEED FOLLOWED BY APU AUTO SHUTDOWN. STARTED APU, TURNED ON APU BLEED, TURNED PACKS 1 & 2 ON, APU OIL 2197 SMELL & SMOKE SDR CALA2025091508946Unknown · odorCREW REPORTS HEAVY ELECTRICAL BURNING SMELL IN FLIGHT DECK AND THROUGH OUT THE CABIN WITH VISIBLE GREY SMOKE THROUGHOUT AIRCRAFT. LOCKING UNLOCKED WAS NOT AN ELECTRICAL SMELL. STARTED APU, TURNED ON APU BLEED, TURNED PACK 1 AND PACK 2 ON, APU OIL 2197 SMELL ANSDR CALA2025091108793None · noneBIRD STRIKE ON RADOM. PERFORMED BIRD STRIKE INSPECTION. AND INSPECTIONS, INCLUDING RADOME, NO DELAMINATION OR DAMAGE FOUND.OK TO CONTINUE.REF AMM TASK 05-51-18-212-001SDR CALA2025090508525Access Panel · missingACCESS PANEL 443JL IS MISSING FROM THE INBD SIDE OF NR 2 PYLON. INSTALLED ACCESS PANEL 443JL IAW MM 54-53-01. SECURED.SDR CALA2025082508097Warning Message · false activationR ENG OVHT AT FL360. WENT AWAY AFTER R EPR REDUCED BY .02. R OVH T DET STATUS ALSO. PER CREW ALSO GOT STRUT OVERHEAT EICAS MOMENTARILY ACP FIM 26-11 TASK 802 ENGINE FIRE/OVERHEAT DETECTION SYSTEM BITE . STEPS 1-6 COMPONENTS AND INTERFACE WIRING ARE CHECKING OKSDR CALA2025081907936Pcb · faultedR OVHT DET STATUS MSG FOLLOWED BY R ENG OVHT CAUTION. COMPLIED W ITH QRH. WENT AWAY WITH IDLE DEBRIEFED FLIGHT CREW, ADVANCED THROTTLES AT LANDING, MSG DID NOT REAPPEAR. HAS HISTORY REF LP 5883831. PERFORMED FLOWCHART 26-11 FAULT TREE 803. VERIFIED NO PRESSURESDR CALA2025081507823Cover · looseDOOR 2L SLIDE COVER LOOSE ADJUSTED 2L DOOR BUSSLE, INSTALLATION AND RIGGING NOT AFFECTEDSDR CALA2025080507292Unknown · unknownPOSSIBLE BIRD STRIKE OUT OF 10K, SOMTHING DID MAKE CONTACT WITH ACFT. ODOR DETECTED INSPECTED ACFT FOUND NO EVIDENCE OF A BIRDSTRIKE OR IMPACT OF SPECIFIED AREA IAW AMM TASK 05-51-18-212-001SDR CALA2025042804285Girt Bar · lack of lubeEMERGENCY POWER RESERVOIR CHECK PROCEDURE - INSTALLED SAFE DOOR PINS FOR DOOR SLIDE. INSTALLED EMARGENCY RESERVOIR SAFETY PINS L4 FOR GIRT BAR LUBE. REMOVED SAFE DOOR PINS AND RESERVOIR SAFETY PINS L4 VERIFIED SAFETY PINS ARE REMOVED ON L4 DOOR SLIDE AND POWERSDR CALA2025042304168Pseu · faultedGEAR DISAGREE EICAS ON TAKEOFF FROM DCA PER CREW GEAR DISAGREE EICAS ONTAKEOFF. RIGHT NOSE GEAR LIGHT ILLUMINATED W/GEAR IN UP/OFF POSITION. CREW DEBRIEF ON ARRIVAL AT IAD: AMBER GEAR TRANSIT/DISAGREE LIGHT ILLUMINATED WITH ASSOCIATED GEAR DISAGREE EICAS MESSASDR CALA2025030302546Warning Message · false activationR FWD ENT DOOR EICAS C THE RIGHT FORWARD ENTRY DOOR IS NOT LATCHED MOMENTARY CAUTION MSG AT FL330. PRESSURIZATION NO RMAL. DOOR HAN DLE MOVING IN TURBULENCE DEBRIEF PILOTS AND FLIGHT ATTENDANT. PER WRITEUP NO PRESS ISSUES. ALSO PILOTS INDICATED THAT THE MESSAGSDR CALA2025012301983Unknown · odorUNNATURAL SMELL IN FLIGH T DECK DURING ALL PHASES OF FLIGHT. FAS ADVISE NO ODOR IN CABIN SUBMITTED FORM TO TOMC FOR SMELL IN FD. REF FIM TASK 21-00-01/301 FOUND NOTHING THAT PRODUCES AN ODOR IN FLIGHT DECK AND CREW STATED SMELL DID NOT SMELL LIKE ELECTRICAL ISDR CALA2024121701545Idg · faultedR GEN OFF EICASTALKED WITH CREW UPON ARRIVAL. THEY SAID THEY LOST AFT GALLEY POWER AND AFT LAV STOPPED WORKING. THEY THEN GOT THE R GEN CONT OFF LIGHT, THEN THEY GOT THE R GEN DRIVE LIGHT ALONG WITH THE R CTR FUEL PUMP OFF LIGHT ON. THEY DID NOT DISCONNECT THESDR CALA2024062100058Seal · damagedDOOR 1R EXCESSIVELY LOUD SQUEELATTACHED PHOTO'S TAKEN ON RIGHT SIDE OF AIRPLANE ABOVE DOOR 1 RIGHT. CREW DEBRIEF: F/O THOUGHT HE HEARD NOISE COMING FROM FWD LOWER DOOR AREA. DEADHEADING F/O WENT FWD TO HELP EVALUATE AND INDICATED NOISE WAS COMING FROM ABOVE GASDR CALA2024052301569Door · corrodedAPU DOOR INLET SURROUND STRUCTURE HAS CORROSION AT I/B FWD CORNE R, O/B FWD EXTENDING 10" I/B AND AFT O/B,SDR CALA2024052301568Strap · crackedFRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAMS BETWEEN F.S. 365.2 5 AND 377.7 AT LBL 25 (LEFT TUNNEL OF MEC) IS CRACKEDSDR CALA2024052001531Channel · crackedREF AMES NR 170224-0200-0211 GEN ITEM 53-5310-1-2626 CRACK FOUND THROUGH FASTENER ON FRAME IN UPPER CABIN R/H SIDE ST A 1580 FOR OVER HEAD BIN ATTACH BRACKET ABOVE STR 9 REPAIRED CRACK THROUGH FASTNER ON FRAME IN UPPER CABIN R/H SIDE STA 1580 ABOVE STRINGER 9 SDR CALA2024051301462Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1420-1440. REMOVED AND REPLACED FLOOR SUPPORT AT BS 1420-1440 BL0 IAW BOEIN G 757 SRM 51-40-02 PAR 4, SEE BACK FOR PARTIALLED WORK.SDR CALA2024051301461Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1320-1340 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1320-1370 AT BLO IAW BOEING 757 SRM 51-40-02 PAR 4. SEE BACK AND PARTIALLED WORKSDR CALA2024051301460Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1260-1300 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1260-1300BLO IAW BOEING 757 SRM 51-40-02 PAR 4. SEE BACK FOR PARTIAL WORK.SDR CALA2024051301459Floor Support · crackedCABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1500-1520 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED FLOOR SUPPORT IAW BOEING 757 SRM 51-40-02 P AR 4. SEE BACK AND PARTIAL WORK SHEET 40 FOR PARTIALLED WORK.SDR CALA2024051001423Bracket · crackedREF AMES NR 170224-0100-00175 GEN ITEM EA 5100-02129 REV H OP 00 1 DURING AGING INSPECTION, FOUND L-BRACKET CRACKED FOR FUSELAGE FA IRING SUPPORT CRACKED, JUST AFT OF RWW RBL-12SDR CALA2024051001419Floor Support · crackedREF AMES NR 170224-0100-0149 GEN ITEM 53-5310-1-2606 FLC FS676 LBL24 SLOPE WALL FLOOR SUPPORT CRACKED. REPAIRED SLOPE WALL FLOOR SUPPORT FS676 LBL24 IN FLC IAW B757 SR M 51-70-0G-0 TABLE 1SDR CALA2024050701366Floor Panel · crackedREF AMES NR 170224-0100-0069 GEN ITEM EA 5100-02244 REV G OP 003 ALC FLOOR PANEL 153AF CRACKEDSDR CALA2024050701365Panel · crackedREF AMES NR 170224-0100-0068 GEN ITEM EA 5100-02244 REV G OP 003 ALC PANEL 151AF HAS A CRACKSDR CALA2024051001418Floor Support · crackedGENERATING ITEM B757-20-3-0065: FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAMS (LEFT TUNNEL OF MEC) BETWEEN F.S. 365.25 AND 377.7 AT BL 0 IS CRACKED (MARKED WITH STREAMER 70209). REPORTED BY V92 9433. REPAIRED FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAM BETWEEN SDR CALA2024050701358Support Rib · crackedFOUND CRACKED SUPPORT RIB AT STATION 365.25, JUST ABOVE WIRING B UNDLE #91177 REF AMES NR 170224-0100-0064SDR CALA2024032800901Fmc · failedRIGHT FMC FAIL LIGHT IS ON LP 7452038 MEL 3461AK WAS CLEARED. MUST REPLACE R FMC REF AMM34-61-01-024-001-002 UNLOCKED TO CLEAR WITH R FMC R&R FMC IN SFO WITH TT# 1524492 AC 0862 REF IPC EQUIPMENT AND SOFTWARE INSTL- MAIN ELECTRONICS EQPT CTR FMC REFERENCE: CYCSDR CALA2023012000164Reservoir · lowLT HYD QTY EICAS C, LEFT HYDRAULIC RESERVOIR QUANTITY IS LOW, HYD AUTO EVEN T RAN CHKLIST IAW QRH. AFT ER SECURING BOTH L PUMPS RUDDER RATIO DISPLAYED. QTY SLOWLY RETURNED NORMAL & LANDING WITH ALL MESSAGES & INDICATIONS RETURNING TO NORMAL. CREW STATED LT SDR CALA2021102901999Fuel Sys · noneABNORMAL FUEL INDICATION S CREW INFO: FUEL CONFIG LIGHT DISPLAYED. CROSS FEED CLOSED, NO DRIP STICKED FUEL TANKS AND THEY COINSIDE WITH COCKPIT FUEL IN CENTER TANK, ENG FUEL BURN WAS EQUAL, RIGHT WING FUEL INDICATIONS. LEVEL WAS GOING DOWN WHILE THE LEFT WING SDR CALA2021062500955Skin · dented(B757-06-3-0253) EXTERIOR FUSELAGE L/H SIDE, 3EACH DENTS ON THE FUSELAGE SKIN BTWN BS 740 AND BS 760 AND BTWN STRINGERS S-15L AN D S-17L. REF HAECO GSO NRC #9286611 REPAIR ACCOMPLISHED IAW HAECO REO-G23222 AND ECRA 5331-02232. PG 2, PART 1,ITEM 2 REQUIRES TO SDR CALA2021062500954Skin · damagedB757-06-3-0222, ZONE 100, LOWER HALF FUSELAGE, STA 1605, AFT OF WASTE DRAIN DOOR, SKIN IS DENTED FROM INSIDE HAECO/GSO LOG 9286586, V899290 2EA DENTS AT STA 1605 R/H SIDE AFT OF WASTE DR, GOUGE 0.018 DEEP GOUGE''S NOT ALLOWED. OUT OF LIMITS PER SRM 53-00-01. CSDR CALA2021042600549Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M11490 INOP REPLACED EMERGNCY LIGHT BATTERY PACK M11490 AS PER AMM 33-51-07-902-005-002. OPS CHECKS GOOD.SDR CALA2021042600547Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M11489 INOP REPLACED EMERGNCY LIGHT BATTERY PACK M11489 AS PER AMM 33-51-07-902-005-002. OPS CHECKS GOOD.SDR CALA2019100501698Transmitter · malfunctionedFLAP ASYMMETRY EICAS INDICATION AFTER FLAP RETRACTION ON TAKEOFF. RH FLAP NEEDLE STUCK WITH NO FLIGHT CHARACTERISTICS NOTICED. FLAPS INDICATION DID RETURN TO NORMAL ON FLAP EXTENSION FOR LANDING USING NORMAL FLAPS. REMOVED AND REPLACED FLAP POSITION IND. NO JOSDR CALA2019072401241Wire · openFOUND FOWARD EXIT SIGN AT DOOR 3 RIGHT INOP REMOVED CEILING PANEL ABOVE DOOR 3 RIGHT FOR TROUBLESHOOTING AND REMOVED DADO PANEL JUST AFT OF DOOR 3 RIGHT RANG OUT BOTH WIRES ON LIGHT FORWARD FOR DOOR 3 RT AND FOUND AN OPEN ON GROUND WIRE REF AWD 33-51-22, PG 90SDR CALA2019051300755Skin · damagedSUBSTASK:B757-53-3-0569: MAIN CABIN, R4 DOOR, ABOVE THE LOWER GATE HAS CUT MARKED SAA-072/61 OFF AIRCRAFT. REF ON REF N/R 0053913. ACCOMPLISHED REPAIR AT MAIN CABIN, R4 DOOR INNER SKIN BETWEEN 165 8.31 TO STA 1652.19 PER EC/RA 5210-03021. WORK WAS ACCOMPLISHEDSDR CALA2019051300760Gate · corrodedREMOVED CORROSION AT R2 DOOR LWR GATE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE R-2 DOOR LWR GATE ASSY P/N 19-5211-3-0 709 IAW SRM 52-10-02 FIG 101 AD 1 AND 51-40-02 PARAG 4. WORK ACCOMPLISHED, EA 5210-01363 REV F: R2 DOOR LWR GATE HAS CORROSION. MARSDR CALA2019050700698Support Fitting · corrodedSUBTASK ZONE 200 OPEN, LAV A SUPPORT FITTING AT STA 340 B/L 0 IS CORRODED. REF N/R 0053993 REMOVED AND REPLACED NEW FITTING P/N 65N57839U2, BATCH 000347007 6, PO NO:SAG7990580 AT MAIN CABIN FWD LAVATORY FLOOR AT STA 340, PER SRM 51-40-02. WORK WAS ACCOMPLISHEDSDR CALA2019050700697Fitting · corrodedSECONDARY FINDING ZONE 200 OPEN, FWD GALLEY FLOOR FITTING AT STA 365 IS CORRODED AND PITTED. REF N/R 0053994 REMOVED AND REPLACED NEW FITTING P/N 415N4007-11, BATCH 00034697 25, PO NO:SAG1900502 AT MAIN CABIN FWD GALLEY FLOOR AT STA 365 PER SRM 51-40-02 AND AMSDR CALA2019050700696Crossbeam · corrodedSECONDARY FINDING ZONE 200 OPEN, FLOOR CROSSBEAM AT STA 395 HAS SEVERAL AREAS OF CORROSION, 22-87. REF NR 0053995. REMOVED DAMAGED CROSSBEAM IAW SRM 51-40-02, FABRICATED NEW SUPPORT FLOOR CROSSBEAM IAW DWG 141N5162, INSTALLED NEW SUPPORT CROSSBEAM, P/N 141N516
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