N478EV, cancelled Oct 29, 2013
Service difficulty reports · 85
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 = 'N478EV' AND deregistration_id = 'N478EV-2013-10-29' 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 = 'N478EV' AND deregistration_id = 'N478EV-2013-10-29' 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 EIAA20090028Seat Track · damagedMAIN DECK CARGO TRACK DAMAGED FROM STA 1880 TO 1980 AT LBL 33.99. REPAIRED PER SRM 53-10-05 FIG 1A.SDR EIA2007179Floorbeam · crackedMAIN DECK BS 380 FLOORBEAM LOWER CHORD CRACKED. MAIN DECK BS 380 FLOORBEAM LOWER CHORD REPAIRED PER EA-53-1183.SDR EIA2007069Drive Assy · malfunctionedNR 1 LT LEADING EDGE DRIVE FAILED TO RETRACT PNEU OR ELEC AFTER T/O FROM JFK AIRCRAFT RETURNED TO JFK. AWAITING CORRECTIVE ACTIONSDR EIA2006225Warning Light · illuminatedNR 4 ENGINE START VALVE OPEN LIGHT ILLUMINATED IN FLIGHT AT FL 310. SHUT NR 4 ENGINE DOWN IN FLT PER EIA ABNORMAL PROCEDURE.SDR EIA2006088Warning Light · false activationRED GEAR WARNING LIGHT ON WITH GEAR EXTENDED. ALL F/E LIGHTS INDICATED DOWN AND LOCK GEAR. TROUBLESHOT SYSTEM PER FIM 32-60-00 AND COULD NOT DUPLICATE OR TURN ON LIGHT. ALL GEAR TARGETS PHYSICALLY CHECKED FOR SECURITY. SYSTEM OPERATES NORMALLY.SDR EIA2006065Engine · oil consumptionAIRCRAFT NR 1 ENGINE HIGH OIL CONSUMPTION. SENT TO MZJ TO REPLACE ENGINE, 663076 OFF, 662500 ON.SDR EIA2006057Wire · brokenLT OUTBOARD FLAP INDICATION ERROR WITH ASYMMETRY LOCKOUT. FOUND LT O/B FLAP TRANSMITTER CABLE BROKEN AND TIE-IN BRACKET BROKEN, PARTS ORDERED. REPLACED FITTING AND MANUFACTURED CABLE PER BOEING STANDARD, INSTALLED PER MM 20-11-03. REMOVED AND REPLACED FLAP SDR EIA2006058Battery Pack · dischargedCREW SERVICE DOOR FRAME MOUNTED EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM33-51-04. OPS CHECKED GOOD PER SAME.SDR EIA2006076Battery Pack · dirtyRT UPPER DECK CREW SERVICE DOOR EXIT LIGHT WILL NOT TEST. REMOVED BATTERY PACK CLEANED BATTERY PACK ELECT CONTACTS. REINSTALLED BATTERY PACK, LIGHTS OPS CHECK GOOD.SDR EIA2006050Battery Pack · dirtyEMERGENCY "EXIT" LIGHT OVER CREW SERVICE DOOR INOP. REMOVED BATTERY PACK, CLEANED CONTACTS ON BATTERY PACK. REINSTALLED, LIGHT OPS CHECK GOOD PER MM 33-51-00 & 33-51-04.SDR EIA2006031Engine · oil consumptionDURING FLIGHT, NR 1 ENGINE WAS SHOWING EXCESSIVE OIL CONSUMPTION, REQUESTED TO RETURN TO DEPARTURE POINT FOR COMPANY CONVIENENCE. REPLACED NR 3 ENGINESDR EIA2006047Light · malfunctionedUPPER DECK CABIN EMERGENCY LIGHT ADJACENT TO FIRST ROW OF SEATING IS DIM. REPLACED LIGHT ASSEMBLY PER MM 33-51-07.SDR EIA2006025Spar · corrodedDURING B-CHECK, EXFOLIATION CORROSION ON LT WING FORWARD SPAR WEB AT LES 949 ON WEB AND STIFFENER. REMOVE DAMAGE, NDT AREA, FABRICATE AND INSTALL REPAIR PER ECRA 478-57-175-2.SDR EIA2006022Skin · corrodedDURING "B" CHECK, FOUND CORROSION ON THE RT WING LWR SKIN PNL AT WS 1371. REMOVED CORROSION TO RT LWR WING SKIN. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 CYCLES WHICHEVER COMES FIRST. WAITING FOR FINAL REPAIR INFORMATIONSDR EIA2006020Spar · crackedDURING B-CHECK, CRACK FOUND ON THE RT LWR FRONT SPAR CHORD FROM FSS 1387 - 1391 (LES 1422-1438). REMOVED AFFECTED AREA AND REPLACED WITH SPLICE. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 CYCLES WHICHEVER COMES FIRST, WAITING FOR FINAL REPAIR INFORMATIONSDR EIA2006019Skin · corrodedCORROSION FOUND ON THE LT WING BETWEEN WS 1044 (LES 1054). INSTRUCTS TO REMOVE CORROSION, ACCOMPLISH NDI INSPECTION, CUT OUT THE DAMAGED WING SKIN MATERIAL AND FABRICATE REPAIR. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 CYCLES WHICHEVER COMES FIRST.SDR EIA2006018Skin · corrodedCORROSION FOUND ON THE RT WING BETWEEN WS 1026 - 1057 (LES 1046 - 1078). ECRA 478-57-176-2 INSTRUCTS TO REMOVE CORROSION, ACCOMPLISH NDI INSPECTION, CUT OUT THE DAMAGED WING SKIN MATERIAL AND FABRICATE REPAIR. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 SDR EIA2006021Skin · corrodedDURING "B-CHECK", CORROSION FOUND ON THE RT WING AT WS 1280 (LES 1302) OUTBOARD OF JACKPAD LOCATION. INSTRUCTS TO REMOVE CORROSION, ACCOMPLISH NDI INSPECTION, FABRICATE AND INSTALL FORM FIT FILLERS AND THE SUBSTITUTION OF BACB30PT RADIUS LEAD IN BOLTS AND BACSDR EIA2005153Fuse · blownDOOR EMERGENCY EXIT LIGHT BY THE UPPER DECK ESCAPE SLIDE INOP. REPLACED FUSE IN BATTERY PACK.SDR EIA2005136Fuse · failedDOOR EMERGENCY EXIT LIGHT BY THE UPPER DECK ESCAPE SLIDE IS INOP. REPLACED FUSE ON THE BATTERY PACK.SDR EIA2005041Keelbeam · corrodedKEEL BEAM RIGHT LOWER CHORD CORROSION BS 1335-1345 WL 100 RBL 10. CORROSION REMOVED PER SRM 53-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005040Keelbeam · corrodedKEEL BEAM BS 1355-1365 LBL 10 WL 100 CORROSION. CORROSION REMOVED PER SRM 53-10-01, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005039Keelbeam · corrodedBS 1375-1380 WL 95-100 LBL 10 KEEL BEAM CORROSION. CORROSION REMOVED PER SRM 63-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005038Stringer · crackedBS 2260 STR 43R INNER CHORD CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005037Frame · crackedBS 1840 STR 11R FRAME CRACKED. DAMAGE REMOVED, FABBED AND INSTALLED REPAIR PER ECRA 478-51-173-1.SDR EIA2005036Keelbeam · corrodedBS 1360 KEEL BEAM LWR ANGLE UPPER SURFACE CORROSION WL 95, LBL 10. CORROSION REMOVED PER SRM 53-10-01, FABBED AND INSTALLED REPAIR PER SRM 51-10-01 AND 51-30-02.SDR EIA2005035Stringer Clip · crackedBS 820 LT TENSION TIE CRACKED STR 10AL - 10L. DAMAGE REMOVED, FABBED AND INSTALLED REPAIR PER ECRA 478-51-173-1.SDR EIA2005034Frame · crackedBS 1780 STR 13R FRAME CRACKED. DAMAGE REMOVED, REPAIR PARTS FABBED AND INSTALLED PER SRM 53-10-04.SDR EIA2005033Frame · crackedBS 880 LT STR 8L - 9L TENSION TIE FRAME CRACKED. DAMAGED AREA REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2005032Stringer Clip · crackedBS 800 STR 11L TENSION TIE CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.SDR EIA2004012Light · inoperativeMAIN CARGO DECK EMERGENCY EXIT LIGHT GOES OUT AFTER 10 SECONDS. REPLACED LIGHT ASSY.SDR EIA203172Lamp · malfunctionedL1 EMERGENCY AFT LIGHT DIM. DMI 33-13. RELAMPED 12-20-2003.SDR EIA2003170Power Supply · inoperativeBOTH EMERGENCY LIGHTS ON CREW SERVICE DOOR INOPERATIVE. R & R POWER SUPPLY, OPS CHECKED GOOD IAW MM 33-51-00.SDR EIA2003151Fire Warning · will not testFIRE WARNING TEST WILL NOT SOUND BELL. REMOVED AND REPLACED AURAL WARNING DEVICE IAW MM 31-26-02 PG 41. OPERATION CHECK GOOD IAW MM 31-26-00 PG 502SDR EIA2003150Light · inoperative1 CENTER ISLE EMERGENCY LIGHT INTERMITTENT. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD IAW MM 33-51-00.SDR EIA2003089Battery Pack · inoperativeCREW SERVICE DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AND EXIT SIGN OPS CHECKED IAW 33-53-00. AIRCRAFT IN MAINTENANCE FROM 6-19-03 TIL 06-24-03.SDR EIA2003086Flap Track · corrodedNR 1 FLAP TRACK FWD O/B SIDE FIRST 4 BOLT HOLES ARE CORRODED AND SOME CAD PLATING MISSING. REWORKED NR 1 FLAP TRACK O/B HOLES 1-4 PER SB 747-57-2256 PAGE 1-52.SDR EIA2003085Floorbeam · crackedUPPER DECK FLOORBEAM BS 380 RT BL 45 TO RT FRAME INTERFACE WEB HAS MULTIPLE CRACKS, ELONGATED HOLES AND DENTS. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-53-142-2.SDR EIA2003084Bulkhead · corrodedRIGHT WING GEAR W/W BS 1241 CANTED BULKHEAD WEB AND VERTICAL STIFFENER CORRODED RBL 55-75. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-53-143-2.SDR EIA2003083Attach Fitting · corrodedCORRSION ON UPPER SKIN TO STR ATTACH AREA IN RT HAND HORIZONTAL INTERIOR MAIN BOX 5 INCHES INBOARD OF RIB AT STAB STATION 235 ON 5TH STR AFT OF FWD SPAR ON FWD END. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-55-1582.SDR EIA2003082Stringer · crackedSTR 42A LEFT CRACKED AT STA 240. REMOVED DAMAGED Z-STRINGER, FABBED NEW PART AND INSTALLED PER B747 SRM 51-30-02, 51-20-01, SOPM 20-41-02 AND SRM 51-10-02.SDR EIA2003088Skin · corrodedSEVERAL SMALL AREAS OF SURFACE CORROSION ON LOWER SURFACE LT HORIZONTAL STAB APPROX STA 410 AT STR 7. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER B747 SRM 51-10-01, 51-20-01, 51-30-00, 51-10-02 AND SDR EIA2003087Flap Track · corrodedNR 1 FLAP TRACK FWD I/B SIDE BOLTS HOLES 1, 3 & 4 ARE CORRODED AND SOME CAD PLATING MISSING. REWORKED NR 1 FLAP TRACK I/B HOLES 1, 3 AND 4 PER SB 747-57-2256 PAGES 1-52.SDR EIA2003073Floorbeam · crackedSTA 440 RBL 52.0, FLOORBEAM WEB IS CRACKED RIGHT BELOW SEAT TRACK.SDR EIA2003072Stringer · corrodedCORROSION DAMAGED STRINGER S42L BS 585 IN FORWARD CARGO PIT AREA. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-03, PAGE 1-4.SDR 200200265Floorbeam · puncturedDURING B-CHECK A PUNCTURE WAS FOUND IN THE BS 380 FLOORBEAM WEB P/N 65B10929-506 AT APPROXIMATELY LBL 57. THE DAMAGE WAS TRIMMED OUT, HFEC INSPECTION PERFORMED AND DOUBLERS AND FILLERS FABRICATED AND INSTALLED PER ECRA 478-53-137-02.SDR 200200264Floorbeam · crackedDURING B-CHECK, A CRACKED FLOOR PANEL ATTACH HOLE COMMON TO THE BS 380 UPPER DECK FLOORBEAM UPPER CHORD WAS DISCOVERED P/N 65B10929-18 AT RBL 65.0. THE CRACKED UPPER CHORD IS BEING REPAIRED BY INSTALLING 2 STRAPS PER ECRA.SDR ERKR200100135Splice · corrodedLEFT AND RIGHT BS 1241 REAR SPAR- ANGLE SPLICE. THIS ECRA SPLICES IN A NEW SECTION OF 65B10821-1 ANGLE ON BOTH SIDES UP TO THE INBOARD EDGES OF THE BULKHEAD FITTINGS. REPAIR IS ACCOMPLISHED USING A SPLICE ANGLE AT LBL 80 AND RBL 80. ADDITIONALLY THE TAPERSHSDR ERKR200100134Beam · crackedCRACKED UPPER T-CHORD OF RT WING T/E BEAM AT WING 235.20. THE CRACK WAS FOUND IN THE UPPER T-WING TRAILING EDGE BEAM AT WBL 235.20. THE REPAIR WAS ACCOMPLISHED BY REMOVING AND REPLACING THE DAMAGED AREA OF THE CHORD WITH NEWLY FABRICATED CHORD, REPAIR STRAPSSDR ERKR200100133Shear Tie · crackedCRACKED SHEAR TIE AT LIGHTENING HOLES BETWEEN STA 340-STA 360, WL.199.80. THE CRACK WAS FOUND AT A LIGHTENING HOLE IN SHEAR TIE LOCATED BETWEEN STA 340 AND STA 360, WL 199.80. REMOVED AND REPLACED THE DAMAGED SHEAR TIE PER ECRA 478-53-125-2.
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