N682FE
Service difficulty reports · 299
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 = 'N682FE' 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 = 'N682FE' 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 FDEA202602040128Valve · faultedWHILE PERFORMING OPS CHECK OF ELCTROHYDRAULIC VALVE 3GA REPLACEMENT WRI 5-25/4268. THE NOSE GEAR RETRACTED.SDR FDEA202601310109Battery Pack · no testEMERGENCY LIGHT TEST SWITCH DOES NOT TEST. ENTRY AREA, RED EMER LT SWITCH DOES NOT ILLUMINATE EMERGENCY LIGHTS, SWITCH DOES ILLUMINATE RED. REMOVED & REPLACED THE EMERGENCY POWER SUPPLY BATTERY, OP TESTED GOOD.SDR FDEA202412241850Wire · detachedEMERGENCY ACCESS SWITCH AND MOMENTARY DOOR BELL BUTTON INOP. DURING T/S FOUND WIRE JMPR-22 BROKEN AT EMERGENCY ENTRY SWITCH TERM 1. RETERMINATED WIRE JMPR-22 AND 9005-20 AT EMERGENCY ENTRY SWITCH TERM 1 . OPS CHK REQ'D. ACCOMPLISHED OPS TEST OF COCKPIT DSDR FDEA202404070447Frame · crackedWINGS - BASIC WING STRUCTRUE - INSPECTION OF FR40 LOWER OUTBOARD RADIUS, LH SIDE, OUND CRACK AT AREA A STARTED FROM THE HOLE A LWR EDGE COMPILED WITH EO 6-5710-E0333575 D P5. REPAIRED THE CRACKED AREA A ON LH SIDE FR40 FWD FITTING LOWER OUTBOARD RADIUS. THSDR FDEA202404010429Web · crackedMAIN DECK FR47 BETWEEN -Y953 AND -Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN -Y953 AND -Y1456 UNDERFLOOR CRACKED WEB PER A300-600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A30SDR FDEA202404010428Web · crackedMAIN DECK FR47 BETWEEN Y953 AND Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y953 AND Y1456 UNDERFLOOR CRACKED WEB PER A300-600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-60SDR FDEA202404010427Web · crackedMAIN DECK FR47 BETWEEN Y0 AND -Y450 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y0 AND -Y450 UNDERFLOOR CRACKED WEB PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SDR FDEA202404010426Web · crackedMAIN DECK FR47 BETWEEN Y0 AND Y450 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y0 AND Y450 UNDERFLOOR CRACKED WEB PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRISDR FDEA202404010425Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR61, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR61 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS SDR FDEA202403050248Lug · corrodedL/H MLG RIB 5 FWD LUG SHOWS SIGNS OF CORROSION IN GREASE GROOVE. REPAIRED IAW AIRBUS REPAIR INSTRUCTIONS R57240425. SEE FINAL EA 6-5710-T0378283. TITLE: WINGS - LH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFT PINTLE FWD LUG BORE CORROSIION IAW AIRBUS RSDR FDEA202403050247Lug · corrodedR/H MLG RIB 5 FWD LUG SHOWS SIGNS OF CORROSION IN GREASE GROOVE REPAIRED R/H MLG RIB 5 FWD LUG PER AIRBUS R57240425 SEE JPF PAGES 1-2, ITEMS 1-16 FOR WORK COMPLETED, EA # 6-5710-T0378296 P1 TITLE: WINGS - RH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFTYSDR FDEA202312211950Engine · leakingENG 1 OIL LO PRESS. PRESSURE INDICATED NORMAL ON ENG PAGE AND GAUGE. HOWEVER, WE NOTICED OIL QUANTITY DECREASING. DECREASING APPROX 2 QUARTS PER 10 MINUTES. AFTER LANDING BACK AT KMEM WE HAD 5 QUARTS REMAINING. 8 QUARTS AFTER ENG SHUTDOWN. ADDED 12 QTS OISDR FDEA202312200245Fitting · corrodedLHRIB 5 FITTING HAS CORROSION REPAIRED PER AIRBUS REPAIR DRAWING R57240425SDR FDEA202312200244Fitting · corrodedRH RIB 5 FITTING HAS CORROSION. REPAIR PER AIRBUS REPAIR DRAWING R57240425SDR FDEA202312161943Unknown · unknownR1 SLIDE INDICATION NOT SHOWING ON ECAM WHEN DOOR IS CLOSED AND ARMED, ALL OTHER DOOR CLOSED AND LOCKED INDICATIONS ARE FINE. PERFORMED T/S FOUND NO R1" SLIDE" INDICATION ON ECAM. PERFORMED TEST OF AUTOMOMOUS STBY PWR UNIT AND R1 "SLIDE" INDICATION RETURSDR FDEA202304110624Idg · failedON DESCENT LOST GEN 2. GEN DID NOT RESET. REMOVED AND REPLACED #2 ENGINE IDG OPS CHECK GOOD AT THIS TIME REF A 300 AMM 24-11-11-04-01.SDR FDEA202211072737Meter · no test#4 COURIOUR O2 MASK FLOW METER BLINKER DOES NOT OPERATE DURING TEST. REPLACED #4 COURIER OXYGEN MASK STOWAGE BOX.SDR FDEA202201060018Transmitter · faultedON TAKE OFF ROLL @ 60 KNOTS RECIEVED ECAM ALERT FOR YELLOW SYSTEM LOW PRESSURE. REJECT THE TAKE OFF AND RETURN TO GATE (NOTE: CREW REPORTED SYSTEM PRESSURE RETURN TO NORMAL DURING TAXI IN) REMOVED AND REPLACED YELLOW SYSTEM HYD QTY TRANSMITTER. REF AMSDR FDEA202112233123Pressure Switch · failedPDIS 682 29-10 0412 23DEC21 MEM FACT U SHORTLY AFTER TAKEOFF, CLIMBING THRU 5000 FEET, ECAM DISPLAYED HYD LOW PRESSURE YELLOW SYSTEM. ECAM AND QRH WERE FOLLOWED AND AN UNEVENTFUL LANDING WAS MADE BACK TO RWY 18C KMEM. A300-600 AMM 29-24-00SDR FDEA202112220148Power Supply · inoperativeMDIS 682 33-50 0405 22DEC21 GSP FACT U EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY IS DEAD. R/I 22DEC21 01:03 GSP U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-31 POS: 3 SRL: 278291 SDR FDEA202112190147Power Supply · inoperativeMDIS 682 33-50 0400 19DEC21 MEM FACT U EMERGENCY LIGHTS NOT WORKING. R/I 19DEC21 20:26 MEM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL: 120148 TAG NBR: 28H905 SDR FDEA202110082521Web · crackedNO.2 ENG EXTERAL PYLON BOX (R/H) HAVE CRACK ON THE RIB8 REPLACED THE DAMAGED WEB WITH NEW ONE BY FASTENERS I.A.W. A300-600F SRM 51-72-10- 001, P. 2 AND 51-40-21-001, PARA. 6, P. 7B-23.SDR FDEA202110082520Web · crackedNO.1 PYLON BOX OUTSIDE SKIN HAS CRACKS ON THE RIB 8 BOTH SIDE. CRACKED RIB 8 WEB REPLACED NEW PART . INSTALLED WITH RIVETS AND FASTENERS I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001 ,PARA 6 PAGE 7B -PAGE 23SDR FDEA202110042505Stiffener · crackedRH PYLON FORWARD FAIRING STIFFENER CRACKED AT THE RIB JO0 FWD AREA REINFORCED REPAIR DOUBLER & ANGLE WORK INSTRUCTION I.A.W. A300-600F SRM 54-54-11- 201- 2, PARA. 5A, PAGE 201-207, FIG. 201.SDR FDEA202110022531Floor Panel · damagedTHE #232HG FLOOR PANEL OF MDC WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.SDR FDEA202110022530Floor Panel · damagedTHE 241BK PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.SDR FDEA202110022527Floor Panel · damagedTHE #252UH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.SDR FDEA202110012549Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR36 TO FR37,-Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-10SDR FDEA202110012548Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR30 TO FR31,-Y1456 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-1SDR FDEA202110012547Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR29 TO FR30,-Y953 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-10SDR FDEA202110012532Floor Panel · damagedTHE 251RH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.SDR FDEA202110012529Floor Panel · damagedTHE 251XG FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.SDR FDEA202110012528Floor Panel · damagedTHE 231FH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.SDR FDEA202110012506Access Door · crackedAFTER PAINT REMOVAL FOUND EQUIPMENT COMPARTMENT ACCESS DOOR 1 EA CRACK AT AFT UPPER LATCH CUTOUT AREA. CUT OUT THE DAMAGED AREA. FABRICATED THE REPAIR DOUBLER AND INSTALLED THEM WITH RIVETS I.A.W. A300-600F SRM 52-41-12-201, PARA. 5, FIG. 201, P. 202-205SDR FDEA202109272553Skin · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON LH WING LWR L/E PANEL 513AB CUTOUT FWD O/B POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SDR FDEA202109272552Skin · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRMSDR FDEA202109272551Skin · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON FUSELAGE SKIN BTW FR101 TO FR103 AND STR-2L TO STR-5L POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATSDR FDEA202109272550None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.20 AND NO.21 FASTENER COUNTED FROM LOWER SIDE. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERSDR FDEA202109252467Stiffener · bentAGING AIRCRAFT RECORDS REVIEW:AT THE TIME OF RECORDS REVIEW THE FOLLOWING WAS IDENTIFIED ON W/O 67250,SNRM N00580, PRIMARY STRUCTURE REMOVED AND REPLACED, PRIMARY STRUCTURE LOCALLY FABRICATED, SEE JPF ITEM 5, AND TRAVELER T16/1235154, SNRM BLOCK 16 NOT ISDR FDEA202109242488Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB 26AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364452 P1, TITLE: WING-FLIGHT SURFACES-LH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB26 AT STRINGERS 2.8-ALI 575306-0SDR FDEA202109212526Floor Panel · damagedFWD CARGO COMPT #131KG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B FIG. 203 SHEET 1, P. 209-211.SDR FDEA202109212525Floor Panel · damagedFWD CARGO COMPT #131LG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B FIG. 203 SHEET 1, P. 209-211.SDR FDEA202109212524Floor Panel · damagedFWD CARGO COMPT #131QG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202109182358Floor Panel · damagedTHE #147CF KEEL BEAM FLOOR WAS FOUND SOFTEN AND CAUSE BY HYD FLUID CONTAMINATION FABRICATED FLOOR PANEL #147CF I.A.W FEDEX DWG SRZ-25-005 REV.RSDR FDEA202106081471Isolation Valve · leakingPDIS 682 29-10 9603 08JUN21 JFK OPEN U AT FL 240 RECEIVED ECAM WARNING FOR YELLOW HYD SYSTEM LO PRESSURE. AFTER ANALYZING WE FOUND LOSS OF ALL YELLOW HYDRAULIC FLUID. RAN QRH, DECLARED EMERGENCY AND LANDED. AMM: 27-14-21-04 REMOVED AND REPLASDR FDEA2019121323235Manifold · crackedABOUT 15-20 MINS AFTER LEVEL OFF AT 350FL WE NOTICED THAT THE GREEN HYD LEVEL WAS LOW. 10 MINS LATER WE GOT A GREEN LOW FLUID LEVEL ON THE ECAM. FOLLOWED PROCEDURES AND SECURED THE GREEN SYSTEM. DURING THE REST OF THE FLIGHT WE RECIEVED MANY GREEN LOW LEVELSDR FDEA2019032760731Floor Panel · damagedMAIN CARGO FLOOR PANEL 252VF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 252VF ON VT MAE TRAVELER T19/1403082 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIRSDR FDEA2019032760729Floor Panel · damagedMAIN CARGO FLOOR PANEL 252GF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 252GF ON VT MAE TRAVELER T19/1403192 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIRSDR FDEA201903260733Floor Panel · damagedMAIN CABIN FLOOR PANEL 231QG IS BROKEN FABRACATED NEW FLOOR PANEL 231QG ON T19/1403671 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.SDR FDEA201903260732Floor Panel · damagedMAIN CABIN FLOOR PANEL 261XF AFT INBD INSERT PULLED THROUGH PANEL. FABRICATED NEW FLOOR PANEL 261XF ON T19/1403254 IAW DWG SRZ-25-005 MAJOR REPAIR.
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