N642FE
Service difficulty reports · 272
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 = 'N642FE' 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 = 'N642FE' 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 FDEA201306011166Indicator · malfunctionedCLOSING DOOR, PRIOR TO DEPARTURE THE L1 SLIDE LIGHT WAS ILLUMINATED STEADY. REMOVED AND REINSTALLED REMOTE PRESSURE INDICATOR, IAW AMM 25-61-04-4. PERFORMED ADJUSTMENT TEST IAW AMM 25-61-04-5, OPS CHECKED GOOD.SDR FDEA201305020896Light · inoperativeL1 DOOR SLIDE REMOTE PRESSURE PRESS TO TEST INOPERATIVE. REPLACED LIGHT ASSY IAW MM 25-61-04 AND TESTED IAW MM 25-61-04-5.SDR FDEA201208193079Battery · failedNR 2 EMERGENCY BATTERY TEST FAILED. R & R NR 2 EMERGENCY BATTERY REF AMM 33-51-01-4. OPS TESTED GOOD.SDR FDEA201207272719Engine · firePUSH CREW REPORTED NR 1 ENGINE EMITTING FLAMES ON START. START VALVE CLOSED AT 33 PERCENT N2, EARLY INDICATIONS 510 F/F, 168 EGT. CONTINUED TO MOTOR ENGINE WITH FUEL LEVER OFF FOR REJECTED START. FLAMES WERE REPORTED AT THIS TIME. TAILWIND OF 10 KTS. SUSDR FDEA201207242663Battery · dischargedRECEIVED A "EMERGENCY LIGHT BATTERY 1 LOW" LEVEL 1 ALERT DURING PREFLT TEST. CHECKED WIRING FROM RELAY R2-5700 PIN A3 TO EMERGENCY LIGHT BATTERY CONECTOR J1 PIN 6, ALL OPS CHECKED GOOD. CHECKED FOR POWER ON PIN A2 OF RELAY R2-5700 AND FOUND 115 VOLTS AC. RSDR FDEA201207022447Light · inoperativeON POST FLT CHECK, EMERGENCY LIGHT TEST FOUND ALERT "EMERGENY LIGHT BATTERY 1 LOW" STATUS IAW FIM 33-51-02-00 & FAULT. REPLACED EMERGENCY LIGHT IAW MM 33-51-01 & TESTED OK IAW MM 33-51-00.SDR FDEA201206112182Battery Pack · inoperativeWHILE PERFORMING EMERGENCY LIGHT TEST, RECEIVED "EMER LT BAT 1 LOW" STATUS MESSAGE. R & R EMERGENCY LIGHT BATTERY PACK IAW MM 33-51-01-4, OPS CHECKED NORMAL, OK FOR SERVICE.SDR FDEA201206042084Battery Pack · failedEMERGENCY LIGHT BATTERY 1 LOW ALERT DURING EMERG LT TEST. R & R EMERGENCY LIGHTS BATTERY PACK.SDR FDEA201204301686Power Supply · no testEMERGENCY LIGHTS FAILED BATTERY TEST DURING PRE-FLT TEST 'EMERG BATT LO' ALERT DISPLAYED. R & R EMERGNCY LIGHTS POWER SUPPLY IAW AMM 33-51-01-4-0 & OPS TESTED GOOD. ACFT OK FOR SERVICE.SDR FDEA201204161443Power Supply · failedEMERGENCY BATTERY 1 LOW ALERT ILLUMINATED ON EMERGENCY LIGHT TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW MD-11 33-51-01-4, ACCOMPLISHED SUCCESSFUL OPERATIONAL CK IAW AMM 33-51-01-5.SDR FDEA201203191021Battery Pack · inoperativeDURING PRE-FLIGHT CHECK, FOUND EMERGENCY LIGHT FAILED TEST. R & R THE EMERGENCY LIGHT BATTERY IAW MM 33-51-01-4, OPS TESTED NORMAL IAW MM 33-51-01-05.SDR FDEA201201150176Battery · inoperativeEMERGENCY LIGHT BATTERY LOW MESSAGE WHEN USING EMERGENCY LIGHT TEST. EMERGENCY LIGHTING POWER SUPPLY BATTERY R & R IAW MM 33-51-01-4. OPS CHECKED SATISFACTORY IAW MM 33-51-01-5.SDR FDEA201112115247Power Supply · failedEMERGENCY BATTERY LIGHT 1 LOW ON EMERGENCY LIGHT BATTERY TEST. R & R EMERGENCY LIGHT POWER SUPPLY IAW MM 33-51-01-4-0. OPS CHECKED GOOD IAW MM 33-51-01-5-0.SDR FDEA201112115241Power Supply · inoperativeEMERGENCY BATTERY 1 LOW ON EMERGENCY LIGHT BATTERY TEST. R & R EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-01-4-0. OPS CHECKED GOOD REF MM 33-51-01-5-0.SDR FDEA201112035136Battery Pack · dischargedEMERGENCY BATTERY LIGHT NR 1 LOW ON EMERGENCY LIGHT BATTERY TEST. R & R BATTERY PACK IAW MM 33-51-01-4, OPS CHECKED NORMAL.SDR FDEA201109304217Battery · dischargedDURING MX PREFLIGHT. EMERGENCY LIGHTS DISPLAYED: EMERGENCY LIGHT BATTERY 1 LOW ALERT. REF FIM 33-51-02-00, R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECK IS NORMAL.SDR FDEA201109053702Access Panel · crackedRT WING L/E XORS 797 UNDERWING ACCESS PANEL AREA FWD STRIP FOUND CRACKED. DOUBLER REPAIR CARRIED OUT IAW SRM 57-40-03, REPAIR 1, FIG 201, REV 47 AND SRM 51-33-01, REV47. REPAIR DOUBLER FABRICATED IAW SRM 57-40-03, REPAIR 1, FIG 201, REV 47 AND HOLES PICKEDSDR FDEA201109043660Skin · dentedFUSELAGE LEFT SKIN FOUND WITH DENT FWD OF ALTERNATE STATIC PORT AT STA 791.750 BETWEEN S37 AND S38. FUSELAGE LT SKIN AT STA 791.750 BETWEEN S37 AND S38 DENT MEASURED D=0.40", W=2.5", APPROX 6.8" FORWARD OF ALTERNATE STATIC PORT FOUND WITHIN LIMIT IAW SRM 53-00SDR FDEA201108283532Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL RT BULKHEAD FWD SIDE, FOUND DOUBLER CRACKED AT BS 1391. NEW DOUBLER INSTALLED PER SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.SDR FDEA201108213395Longeron · damagedCENTER CARGO STA 1812 TO 1853, LONGERON 46 RT FOUND WITH SEVERAL FASTENERS DRILLED CLOSE TO RADIUS. REPAIRED AS PER EA 1-5310-150779, PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.SDR FDEA201108153277Skin · misrepairedRT WING FIXED L/E SKIN SLAT TRACK CUTOUT AT STA XIS 286 MISREPAIRED. CORRECTED REPAIR IAW EA 1-5710-153404. CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201108153276Skin · misrepairedFUSELAGE SKIN STA 1821 TO 1853, LONGERON 41 TO 48 RT MISREPAIRED. REPAIRED IAW EA 1-5330-150765. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201108123233Skin · crackedRT WING L/E CAP SKIN CUTOUT FOUND CRACKED AT NR 12 SLAT TRACK AREA. SKIN TRIMMED, REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 51-40-02, REPAIR 7, FIG 201, REV 47. REPAIR PARTS INSTALLED IAW SRM 51-33-01, REV 47. HFEC SURFACE INSP CARRIED OUT IAW DAC NDT SPMSDR FDEA201108123232Floorbeam · corrodedCENTER CARGO COMPARTMENT ALONG STA 1841, BETWEEN LONGERON 45L AND LONGERON 48R, FLOORBEAM WEB AREAS FOUND SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-21-01, REV 47. FOUND EXCEEDED LIMIT IAW SRM 53-00-00, FIG 202, REV 47. R & R IAW SRM 51-35-01, REV 47SDR FDEA201108123231Floorbeam · corrodedAFT CARGO FLOORBEAM AT STA 1841 X=58.0 TO X=-58.0 FOUND CORROSION AT SEVERAL ANCHOR NUTS AREA. CORROSION REMOVED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-00, FIG 202, REV 47 AND NEW UPPER TEE INSTALLED IAW SRM 51-35-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMSDR FDEA201108083134Longeron · crackedLONGERON 4L FROM STA Y475 TO Y495, END FOUND CRACKED. REMOVED AND INSTALLED WITH NEW LONGERON END CLIP AS PER SRM 51-31-01, REV.47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.112.SDR FDEA201108073128Longeron · corrodedDURING REPAIR OF LONGERON 52 FOUND CORROSION AT LONGERON 51L AT STA 6-80. CORRODED LONGERON SECTION CUT AND REMOVED IAW SRM 53-00-05, FIG 202, REV 47. NEW LONGERON SECTION FABRICATED AND REPAIR SPLICE FABRICATED IAW SRM 53-00-05, FIG 202, REV 47 AND INSTALLSDR FDEA201108073127Longeron · corrodedAFT CARGO - BILGE AREA AT STA 1952, LONGERON 51L, FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5310-150777, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201108053103Spar · corrodedRT WING REAR SPAR LOWER CHORD FOUND CORROSION LOCATED AT XORS 1042 -1070 AREA. CORROSION REMOVED AND PROTECTED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.060", MATERIAL REMOVED = 0.020" , REMAINED THICKNESS = 0.040", DIA. IS 27" X 1.25" FOUND EXCEEDED LSDR FDEA201108023066Seat Track · corrodedCABIN AT STA 1521 TO STA 5-11 X=-75.5 SEAT TRACK UPPER FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47, ORIGINAL THICKNESS = 0.085", REMAINED MATERIAL = 0.040" MATERIAL REMOVED = 0.045" FOUND EXCEEDED LIMIT IAW SRM 53-00-52, FIG 101, REV 47.SDR FDEA201108023062Seat Track · corrodedCABIN AT STA 5-11 TO STA 5-32 X=-108.75 SEAT TRACK BASE FOUND CORRODED. EXCEEDED LIMITS, REMOVED IAW SRM 51-31-01, REV 47 AND SRM 53-00-52, FIG 201, REV 47. CORROSION REMOVED IAW SRM 51-21-01, REV 47, ORIGINAL THICKNESS = 0.104", REMAINED MATERIAL = 0.050" SDR FDEA201107272997Frame · dentedFORWARD CABIN FRAME AT STA 655 RT BETWEEN LONGERON 11 TO 12 RT FOUND IMPACT DENT. DENTED AREA REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 47. COMPLIED IAW EA 1-5310-150789, PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201107272996Hinge · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) BARREL NUT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-150758, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201107272995Hinge · corrodedLT WING OTBD FLAP, INBD HINGE (WING SIDE) ACTUATOR OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.217", FINAL DIAMETER = 1.256", MAXIMUM ALLOWABLE DIAMETER = 1.220". REPAIR BUSHING AND WASHERS FASDR FDEA201107272994Hinge · corrodedLT WING OTBD, FLAP INBD HINGE (WING SIDE) ACTUATOR MOUNT FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.216", FINAL DIAMETER = 1.257", MAXIMUM ALLOWABLE DIAMETER = 1.220". REPAIR BUSHING AND WASHER FABRICSDR FDEA201107262951Skin · misrepairedSKIN REPAIR AT BS 859 LONGERON 35 RT, FOUND NOT ACCOMPLISHED IAW ANY APPROVED DATA. REPAIR REMOVED IAW SRM 51-35-01, REV 47. TRIMMED OUT AREA IAW SRM 53-00-01, FIG 201, REPAIR 1, REV 47. HFEC INSP CARRIED OUT IAW DAC NDT SPM REV 13, PART 06-10- 01.001 ON TSDR FDEA201107262956Hinge · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) FORWARD MOUNT FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.188", FINAL DIAMETER = 1.263", MAXIMUM ALLOWABLE DIAMETER =1.254". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201107262955Hinge · corrodedLT WING OTBD FLAP, INBD HINGE (WING SIDE) FORWARD MOUNT INBD HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.186", FINAL DIAMETER = 1.263", MAXIMUM ALLOWABLE DIAMETER =1.254". REPAIR BUSHING FABRICATESDR FDEA201107262954Hinge · corrodedLT WING OTBD FLAP, OTBD HINGE (WING SIDE) ACTUATOR. OTBD HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 70. ORIGINAL DIAMETER = 1.212", FINAL DIAMETER = 1.250", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING FABRICATED ASDR FDEA201107262952Hinge · corrodedLT WING OTD FLAP, OTBD HINGE (WING SIDE) ACTUATOR INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 70. ORIGINAL DIAMETER = 1.212", FINAL DIAMETER = 1.250", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING FABRICATED AND ISDR FDEA201107222892Longeron · corrodedCTR CARGO COMPARTMENT BETWEEN STA 1681 AND STA 1691, LONGERON NR 52 FOUND CORRODED. CORRODED AREA REPAIR CARRIED OUT EA 1-5310-150780, PT1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201107212878Seat Track · damagedCABIN AT STA 806 TO STA 879 X=27.5 SEAT TRACK FOUND ELONGATED HOLES. REMOVED IAW SRM 51-31-01, REV 47. NEW REPAIR SEAT TRACK SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, FIG 201, REV 47. NEW REPAIR SEAT TRACK SECTION AND SPLICE INSTALLED IAW SRM 51-31-01SDR FDEA201107212877Hinge · corrodedRT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.206", FINAL DIAMETER = 1.250", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING AND WASHER FABRSDR FDEA201107212876Hinge · corrodedRT WING OTBD FLAP, INBD HINGE (WING SIDE) ACTUATOR INBD HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.206", FINAL DIAMETER = 1.255", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING AND WASHER FABSDR FDEA201107202837Seat Track · corrodedCABIN SEAT TRACK FLANGE FASTENER HOLES, FOUND ELONGATED HOLES FROM STA 959 TO STA 979, X= 27. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 47. NEW REPAIR SEAT TRACK SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 47, FIG 201. NEW REPAIR SEAT TRACK SECTIOSDR FDEA201107202836Seat Track · corrodedCABIN SEAT TRACK CROWN AT STA 1406 TO STA 1409, X= -75 FOUND CORRODED. CORROSION ON SEAT TRACK FLANGE AND CROWN REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.103 IN AND 0.085 IN RESPECTIVELY. MATERIAL REMOVED = 0.028 INCH AND 0.045 INCH; MATERIASDR FDEA201107202835Seat Track · corrodedCABIN SEAT TRACK FLANGE AND CROWN AT STA 1309 - STA 1327, X= -75 FOUND CORRODED. CORROSION ON SEAT TRACK FLANGE AND CROWN REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.085 INCH AND 0.103 INCH RESPECTIVELY. MATERIAL REMOVED = 0.045 INCH AND 0.053SDR FDEA201107202834Seat Track · corrodedCABIN - CORROSION FOUND ON SEAT TRACK FLANGE LOWER SURFACE AT STA 695, X = -25. CORROSION REMOVED SRM 51-21-01, REV 47. FOUND EXCEEDED LIMITS IAW SRM 53-00-52, REV 47, FIG 101. SEAT TRACK REMOVED IAW 51-31-01 REV 47. NEW SEAT TRACK SECTION AND REPAIR SPLISDR FDEA201107192799Seat Track · corrodedCABIN AT STA 1661 TO STA 1665, X= 75 SEAT TRACK UPPER FLANGE FOUND CORRODED. REMOVED CORROSION IAW SRM 51-21-01 REV 47. FOUND EXCEEDED LIMITS IAW SRM 53-00-52, REV 47, FIG 101. REMOVED SEAT TRACK IAW 51-31-01, REV 47. NEW SEAT TRACK SECTION AND REPAIR SPLSDR FDEA201107172769Skin · misrepairedREPAIR AT LT WING INBD FLAP LOWER SKIN INBD SIDE XIFH 201 TO XIFH 207 EVALUATED AND FOUND PREVIOUSLY NOT ACCOMPLISHED IAW APPROVED DATA. REPAIR REMOVED IAW SRM 51-35-01, REV 47. NEW REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-00-01, FIG 201, REPAIR 1,
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