N489EV, cancelled Jan 8, 2018
Service difficulty reports · 72
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 = 'N489EV' AND deregistration_id = 'N489EV-2018-01-08' 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 = 'N489EV' AND deregistration_id = 'N489EV-2018-01-08' 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 EIAA20120404037Battery Pack · dirtyEMERGENCY EXIT SLIDE LIGHTS UPPER DECK LEFT DOOR SILL INOPERATIVE. REMOVED BATTERY CLEANED BATTERY PACK X631 CONTACTS AND RE-INSTALLED PER B747 MM 33-51-04 PG 204-205, OPS CHECK GOOD.SDR EIAA20120404036Floorbeam · crackedUPPER DECK FLOORBEAM VERTICAL WEB CRACKED AT UPPER AND LOWER END BS 420 RBL 80. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER SRM 53-10-07 PG. 47-50A.SDR EIAA20120403035Access Panel · gougedNR 3 PYLON RT SIDE INSIDE ACCESS PANEL 473AR DEEP GOUGE JUST UNDER CUT OUT. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-020-2.SDR EIAA20120403034Skin · damagedNR 2 PYLON RT FRAMES STA 259 AND 234, RT SKIN BELOW LOUVER CUTOUT ARE HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.SDR EIAA20120403033Skin · damagedNR 4 PYLON RT BETWEEN FRAMES STA 248 AND 259, RT INTERNAL SKIN AT STIFFENER 2 TO 4 AND FRAMES HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.SDR EIAA20120403032Skin · damagedNR 2 PYLON RT BETWEEN FRAMES STA 259 AND 270, RT SKIN BETWEEN STIFFENERS 2 AND 3 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.SDR EIAA20120403031Skin · damagedNR 1 PYLON RT BETWEEN FRAMES STA 234 AND 270, RT INTERNAL SKIN BETWEEN STIFFENERS 2 AND 4 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.SDR EIAA20120403030Skin · damagedNR 3 PYLON RT BETWEEN FRAMES STA 234 AND 248, RT INTERNAL SKIN AT STIFFENER 3 AND STIFFENER HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.SDR EIAA20120402029Battery · dischargedTWO EA UPPER DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES WITH SERVICEABLE.SDR EIAA20120402028Skin · damagedNR 3 PYLON SKIN CAP DOUBLER MOST AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-023-2.SDR EIAA20120330027Skin · damagedNR 2 PYLON SKIN CAP DOUBLER AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-024-2.SDR EIAA20120330026Structure · crackedNR 4 PYLON O/B SIDE FWD ACCESS CUT OUT HAS CRACK IN UPPER FWD SIDE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2SDR EIAA20120327025Angle · damagedLT BS 800 FRAME STR 17L UPPER AFT HOLE IS MISMATCHED COMMON TO STRAP FRAME INNER CHORD AND DOOR STOP FITTING. REMOVED DAMAGE INNER CHORD ANGLE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-021-2.SDR EIAA20120327024Skin · crackedNR 4 PYLON I/B SIDE CRACK IN SKIN OF ACCESS CUT OUT, FWD UPPER CORNER NAC273. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2.SDR EIAA20120326022Floorbeam · damagedELONGATED HOLE IN UPPER CHORD OF UPPER DECK FLOORBEAM BS 780 LBL 27. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.SDR EIAA20120326020Strap · damagedRIGHT BS 800 FRAME STRAP AND STR 17R STRAP HAS 2 EACH HOLES WITH TOOL MARKS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ERCA 489-53-021-2.SDR EIAA20120326019Structure · damagedBS 2231 O/B CHORD ABOVE STR 19L HAS TOOL MARKS INSIDE HOLE AND HOLE ELONGATED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2.SDR EIAA20120326018Floorbeam · chafedLOWER CHORD OF UPPER DECK FLOORBEAM BS 560 LBL 87 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.SDR EIAA20120326017Floorbeam · chafedLOWER CHORD OF UPPER DECK FLOORBEAM BS 560 RBL 87.50 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.SDR EIAA20120326016Skin · chafedNR 4 PYLON CAP SKIN O/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION 17.SDR EIAA20120326015Skin · chafedNR 4 PYLON CAP SKIN I/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION NR 16.SDR EIAA20120326014Structure · damagedBS 2231 I/B CHORD BELOW STR 19L HAS DRILL START. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2SDR EIAA20120306012Skin · chafedNR 4 PLYON CAP SKIN I/B SIDE AT NAC 258 HAS CHAFING. REMOVED DAMAGED SECTION OF CAP SKIN, FABBED REPAIR PARTS AND INSTALLED PER EMC ENGINEERING DISPOSITION 3823 AND B747 SRM 54-31-03 PG 2 SHEET 1-4.SDR EIAA20120201009Floorbeam · crackedBS 360 FLOORBEAM LBL 54.50 FWD SIDE HAS CRACK. REMOVED DAMAGE FABBED AND INSTALLED REPAIR PER SB 747-53A2431 PART 3 FIG 9.SDR EIAA20120131008Floorbeam · crackedBS 340 FLOORBEAM LBL 13.25 AFT SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 TABLE 1 FIG 9.SDR EIAA20120131007Floorbeam · crackedBS 360 FLOORBEAM LBL 13.12 AND 14.65 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 PART 3 FIG 9.SDR EIAA20120131006Floorbeam · crackedBS 340 FLOORBEAM LBL 29.50 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-7471587-00 REV J, SB 747-53A2431 REV 2 TABLE 1 FIG 8.SDR EIAA20120131005Floorbeam · crackedBS 360 FLOORBEAM LBL 36.70 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J PART 3 FIG 9.SDR EIAA20120126004Reveal · crackedBS 2231 RT DOOR FRAME REVEAL HAS CRACK BETWEEN STR 16R AND 17R. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS PER B747 SRM 53-10-04 FIG 91.SDR EIAA20120101001Control Quadrant · lack of lubeON DESCENT THROUGH 8000 FT NR 2 THRUST LEVER SEIZED JUST FORWARD OF IDLE POSITION. CONFIRMED NR 2 THROTTLE SEIZED JUST FORWARD OF IDLE INSPECTED THROTTLE RUN FROM WING ROOT TO MEC NO OBVIOUS DEFECTS NOTED LUBRICATED QUADRANT AND INTERTOCK MECHANISM PER AMM 76SDR EIAA2011235Squib · no testDURING PREFLIGHT FLIGHT, ENGINEER DISCOVERED FIRE BOTTLE SQUIB 3B WOULD NOT TEST. REMOVED AND REPLACED 3B FIRE BOTTLE SQUIB.SDR EIAA2011229Sign · unknownEMERGENCY EXIT LIGHT LT CREW SERVICE DOOR WILL NOT STAY CLOSED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER B747 MM 33-51-02 PG 301-302 AND B747 SWPM 20-30-00 PG 2-3.SDR EIAA2011099Battery Pack · dischargedAFT EMERGENCY LIGHT AFT UPPER DECK INOP. REMOVED AND REPLACED BATTERY PACK - OPS CHECK OK PER MM 33-51-00 PG 501.SDR EIAA2011098Light · defectiveEMERGENCY LIGHT RIGHT UPPER DECK COCKPIT CLOSET IS ON AT ALL TIME WHEN A/C POWERS OFF. REMOVED AND REPLACED RIGHT UPPER DECK EMERGENCY LIGHT ASSY PER MM 33-51-00 PAGE 501.SDR EIAA2011097Warning System · false activationNR 3 ENGINE A LOOP FIRE DETECTION SYSTEM FAULT LIGHT ILLUMINATED, GAUGE NEEDLE FLUCTUATING. XFRD TO DMI 182 AS PER MEL 26-1 CAT C DUE 8/11/11. INSTALLED PLACARD. RESEATED AND SHOOK DOWN LOOP SENSOR AND CHECKED FOR CHAFING WIRES. NO FAULT FOUND. OPS CHECK SDR EIAA2011096Circuit Card · defectiveNR 3 ENGINE "A" LOOP FIRE DETECTION SYSTEM FAULT LIGHT ILLUMINATED. GAUGE FLUCTUATING. ITEM TRANSFERED TO DMI 181 PER MEL REF 26-1 CAT "C" DUE ON 8/7/11 PLACARDS INSTALLED. REPLACED NR 3 ENG "A" LOOP FIRE DETECT CARD IAW MM 26-10-00 PG 401 OPS CK OK IAW MM SDR EIAA2011094Circuit Card · malfunctionedNR 3 ENGINE "A" FIRE DETECTOR FLUCTUATES BETWEEN 2 AND 5 UNITS - SELECTED "B" LOOP - "B" LOOP TESTS OK. TRANSFERED TO DMI 177 PER MEL 26-1 CAT C DUE 7-31-11 2359Z PLACARD INSTALLED. RE-RACKED NR 3 FIRE WARNING AND DETECTOR CARD PER AMM 26-10-00. OPS CHECK OSDR EIAA2011042Connector · unsecureFOUND EMERGENCY LIGHT ABOVE UPPER DECK STAIR WELL INOPERATIVE. RESEATED CONNECTOR ON POWER SUPPLY OP'S CHECK OK PER MM 33-51-00/501SDR EIAA2011038Battery Pack · dischargedCREW SERVICE DOOR EMERGENCY EXIT SIGNS DO NOT TURN ON. REPLACED EMERGENCY LIGHT BATTERY PACK IN CREW CLOSET UPPER SHELF WALL PER B747 MM 33-51-040 PG 204.SDR EIAA2011037Light · inoperativeEMERGENCY LIGHT AT STA 470L UPPER DECK INOP. REPLACED EMERGENCY LIGHT IN CEILING PER B747 MM 33-51-07 PG 201-207.SDR EIAA2010065Pin · damagedUPPER DECK CEILING AFT EMERGENCY LIGHT INOP. REPAIRED CONNECTOR PIN 7 (DM335) GOING TO EMERGENCY POWER SUPPLY OP'S. CHECKED NORMAL PER MM 33-51-00 PAGE 501 REF WDM 33-51-12 PG 16.SDR EIAA2010043Frame · damagedUPON REMOVAL OF FASTENERS FROM TENSION TIE AT STA 920 RT FOUND 5 HOLES IN FRAME PLUGGED. REMOVED DAMAGE, NDT AREA, REPAIRED TENSION TIE AT BS 920 RT PER B747 SRM 53-10-11 FIG 2 PG 17-35 AND FRAME SECTION FROM STR 6R - 12R PER B747 SRM 53-10-04 FIG 137 PG 897 SDR EIAA2010042Frame · damagedUPON REMOVAL OF FASTENERS FROM TENSION TIE AT STA 920 RT FOUND 5 HOLES IN FRAME PLUGGED. REMOVED DAMAGE, NDT AREA, REPAIRED TENSION TIE AT BS 920 RT PER SRM 53-10-11 FIG 2 PG 17-35 AND FRAME SECTION FROM STR 6R - 12R PER SRM 53-10-04 FIG 137 PG 897-905.SDR EIAA2010018Relief Valve · defectiveNR 2 ENGINE FIRE WARNING INFLIGHT. A AND B LOOP NACELLE TEMP IN RED. PYLON VALVE WENT AUTOMATICALLY TO CLOSE, F/E SELECTED BLEED AIR TO OFF, FIRE BELL AND HANDLE LIGHT EXTINGUISHED. REMOVED AND REPLACED PRESSURE REL VALVE, OP'S CHECKED NORM PER MM 36-11-05.SDR EIAA2010006Wire · burnedAUTO PRESS CONTROL A/C CIRCUIT BREAKER TRIP, LEF OUT FLOW VALVE ON DMI. FOUND A LARGE BUNDLE OF WIRES SEVERELY DAMAGED (APPROXIMATELY 20-30) AT STA 2020-2040, ABOVE BULK CARGO BAY. REPAIRED WIRE BUNDLE TO LT OUTFLOW VALVE PER AMM 20 STANDARD WIRE PRACTICE, 3SDR EIAA200900128Indicator · defectiveON CLIMBOUT WHEN RETRACTING FLAPS, INBOARD FLAPS STOPPED AT 2 PERCENT. WHEN ALTERNATE RETRACT WAS ATTEMPTED LJ INBOARD FLAPS DID NOT MOVE AND RESULTED IN AN ASYMMETRIC LOCKOUT. FLAPS DISCREPANCY RECTIFIED WITH NEW INDICATOR.SDR EIAA200900126Pressure Switch · malfunctionedDURING CRUISE APPROX 7 HOURS INTO FLIGHT NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED FLASHING. RETARDED NR 2 THRUST LEVER, LIGHT CONTINUED TO FLASH. ACCOMPLISHED INFLIGHT ENGINE FAILURE AND SHUTDOWN PROCEDURE. FILTER BYPASS LIGHT REMAINED ON STEADY AFTESDR EIAA20090055Oil System · low pressureDURING CRUISE AT FL 310, NR 4 ENGINE OIL PRESSURE ILLUMINATED. CHECKED OIL QUANTITY GAUGE IT READ ZERO, AND OIL PRESSURE READ 10 PSI. SHUTDOWN ENGINE USING IN-FLIGHT FAILURE AN SHUT DOWN CHECKLIST. WINDMILL FOR 76 MIN, NOTIFY ATC AND DISPATCH, DUMPED FUEL ASDR EIA2007206Slide · disconnectedRT EMERGENCY DOOR SLIDE PACK INFLATION BOTTLE DEPLOYMENT CABLE DETACHED. DEPLOYMENT CABLE RE-ATTACHED IAW 25-60-00.SDR EIA2007205Skin · crackedNUMBER 2 PYLON PRECOOLER LOWER SKIN, TWO CRACKS FOUND AT AFT UPPER CORNER. REPAIR PER 54-50-35916. PERFORM DVI PER ECRA 489-54-010-1.
Back to N489EV, cancelled Jan 8, 2018