N512MC, cancelled Jun 6, 2011
Service difficulty reports · 118
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 = 'N512MC' AND deregistration_id = 'N512MC-2011-06-06' 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 = 'N512MC' AND deregistration_id = 'N512MC-2011-06-06' 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 UIEA200800345Skin · delaminatedLT WING OUTBOARD AILERON UPPER SURFACE HAS 3 AREAS WITH PREVIOUS REPAIRS DELAMINATING. DELAMINATION AT WBL 883.0 AREA IS 3.5 BY 2.0 INCHES, LOCATED 9.5 INCHES FROM T/E, WBL 991.0 AREA IS 4.0 BY 2.0 INCHES, LOCATED 8.5 INCHES FROM T/E AND AT WBL 1033 AREA IS 7SDR UIEA200800339Outflow Valve · failedAIR TURN BACK . ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. NR 1 PACK DEFERRED ALREADY. NR 3 PACK VALVE SWITCH OPEN. CABIN ALTITUDE WARNING HORN SOUNDED CABIN AT 10,000 FT. A/C MODE SELECT SWITCH IN AUTO. BOTH OUTFLOW VALVES CLOSED. DUCT PRESSURE 42 PSI, CABIN CSDR UIEA200800331Tire · blownINTO ANC NR 4 HYD SYSTEM QTY LOSS, COMPLIED WITH FHB, EDP SELECTED OFF AT 1612 HOURS. UPON INSPECTION ON THE GROUND FOUND NR 11 AND 12 TIRES BLOWN, 11 AND 12 BRAKES DAMAGED, NR 9 AND 10 TIRES DAMAGED AS WELL AS NUMEROUS BODY PANELS DAMAGED. ALSO FOUND THE RISDR UIEA200800309Frame · crackedMAIN DECK CARGO COMPARTMENT SIDEWALL FRAME AT BS 1780 AT S12R HAS A 6.0 INCH CRACK, TOTAL WIDTH OF FRAME. INTERIM REPAIR ACCOMPLISHED IAW SRM 51-30-02 EO NR 4753B208 AND FORM 8110-3. REQUIRES INITIAL AND REPEAT INSPECTIONS AT EVERY C-CHECK INTERVALS. (K)SDR UIEA200800308Skin · crackedLT WING LEADING EDGE KRUEGER FLAP LOWER IB SIDE PANEL AT WING STA 323.00 TO 330.00 HAS A 7.0 INCH COMPOSITE CRACK. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG 3, SHEETS 1, 4 AND 8, PREPEG 250 DEGREES F CURE IAW SRM 51-40-12. ALSO, REFERENCE EO NR 4757ASDR UIE2008F00044Isolation Valve · failedAIR TURN BACK. DURING CLIMB BOTH LT AND RT MANIFOLD PRESSURE WAS FLUCTUATING. DURING TROUBLESHOOTING AFTER CRUISE POWER SET 103.4, THE NR 1,3, AND 4 PYLONS VALVES WOULD NOT CLOSE. WITH LT AND RT ISOLATION VALVES CLOSED, IT WAS DETERMINED THAT THE NR 1 PYLON VASDR WRNA20080015Engine · malfunctionedBECAUSE OF HIGH HEAT AND HUMIDITY AT DUBAI, ENGINES WERE UNABLE TO MAKE TAKEOFF POWER, ABORTED TAKEOFF BEFORE 80 KNOTS AND RETURNED TO RAMP. PERFORMED MAIN ENGINE CONTROL TRIM ON NR 2 ENGINE IAW 71-00-00 PAGE 563 TEST 5. PERFORMED ENGINE PERFORMANCE RUN, OPSSDR WRNA20080008Engine · malfunctionedBECAUSE OF HIGH HEAT AND HUMIDITY AT DUBAI, ENGINES WERE UNABLE TO MAKE TAKEOFF POWER, ABORTED TAKE-OFF BEFORE 80 KNOTS AND RETURNED TO RAMP. PERFORMED MAIN ENGINE CONTROL TRIM ON NR 1 ENGINE IAW 71-00-00 PAGE 563 TEST 5. PERFORMED ENGINE PERFORMANCE RUN, OPSDR WRNA20080024Engine · malfunctionedBECAUSE OF HIGH HEAT AND HUMIDITY AT DUBAI, ENGINES WERE UNABLE TO MAKE TAKEOFF POWER, ABORTED TAKEOFF BEFORE 80 KNOTS AND RETURNED TO RAMP. PERFORMED MAIN ENGINE CONTROL TRIM ON NR 3 ENGINE IAW 71-00-00 PAGE 563 TEST 5. PERFORMED ENGINE PERFORMANCE RUN, OPSSDR WRNA20080027Frame · damagedDURING 'B' CHECK, FASTENERS WERE FOUND LOOSE AND MISSING RIGHT SIDE FRAME TO INTERCOSTAL AT STATION 2674 TO 2680 W/L 305. FABRICATED REPAIR DOUBLER ANGLES IAW SRM 51-40-03 FIGURE 01 AND INSTALLED IAW SRM 51-30-02.SDR WRNA20080026Longeron · gougedDURING B CHECK, A GOUGE WAS FOUND ON RT LONGERON AT STATION 2700 W/L 285. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW SRM 51-40-03 FIGURE 01 USING .100" 7075 T6 FORMED SECTION. INSTALLED REPAIR DOUBLER IAW SRM 51-30-02.SDR WRNA20080028Frame · damagedDURING B CHECK, FOUND MISSING FASTENER AND ELONGATED HOLE RIGHT SIDE OF FRAME AND INTERCOSTAL AT STATION 2662 W/L 305. FABRICATED REPAIR DOUBLER IAW SRM 51-40-03 FIGURE 01 AND INSTALLED DOUBLER IAW SRM 51-30-02.SDR UIEA200700416Frame · crackedFOUND MAIN DECK STA 1760 FRAME CRACKED AT STR 13R - 14R. REPAIRED PER BOEING MESSAGE 1-542767421-2.SDR UIEA200700415Spar · corrodedRIGHT WING STATION 1337 FRONT SPAR TO REAR SPAR HAS CORROSION EVIDENT. REMOVED CORROSION IAW SRM 51-10-01.SDR UIEA200700414Skin · delaminatedNR 1 SPOILER INBOARD EDGE DELAMINATED. REPAIR CARRIED OUT PER SRM 51-40-24.SDR UIEA200700413Skin · delaminatedNR 4 SPOILER OUTBOARD CORNER DELAMINATED. REPAIR CARRIED OUT PER SRM 51-40-24.SDR UIEA200700412Skin · delaminatedNR 2 SPOILER OUTBOARD EDGE DELAMINATED. REPAIR CARRIED OUT PER SRM 51-40-24.SDR UIEA200700411Spar · corrodedRIGHT WING AT WS 917- WS 1141 FRONT SPAR TO REAR SPAR HAS CORROSION EVIDENT. CORROSION REMOVED PER SRM 51-10-01.SDR UIEA200700409Skin · corrodedBS 1241 LBL 55- LBL 76 CTR SECTION UPPER SKIN CORROSION, LEVEL 1. BLENDED OUT IAW SRM 51-10-01 AND BOEING MESSAGE NUMBER 1-598402422-7.SDR UIEA200700408Skin · corrodedBS 1241 LBL 11- LBL 33 CTR SECTION UPPER SKIN CORROSION, LEVEL 1. BLENDED OUT IAW SRM 51-10-01 AND BOEING MESSAGE NUMBER 1-598402422-7.
SDR UIEA200700407Skin · corrodedBS 1241 LBL 11- RBL 11 CTR SECTION UPPER SKIN CORROSION, LEVEL 1. BLENDED OUT IAW SRM 51-10-01 AND BOEING MESSAGE NUMBER 1-598402422-7.SDR UIEA200700410Seat Track · corrodedMAIN DECK BS 459 LBL 64 SEAT TRACK CORROSION, LEVEL 2. REPAIRED SEAT TRACK IAW SRM 53-10-05 FIG 1A.SDR UIEA200700406Fairing · damagedNR 3 ENGINE LT T/R AFT UPPER FAIRING FOUND TORN AND MATERIAL MISSING. REPAIRED PER EO4778A109.SDR UIEA200700404Floorbeam · corrodedMAIN DECK BS 1720 LBL 76- LBL 98 FLOORBEAM UPPER CHORD HAS LEVEL 2 CORROSION. REPAIRED PER SRM 53-10-07 FIG 2. RAM FORM AND CPCP SUBMITTED TO ENGINEERING.SDR UIEA200700403Skin · corrodedLEFT WING UPPER SURFACE WS 807 TO STR 516 SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700402Skin · corrodedLEFT WING UPPER SURFACE WS 353 TO WS 586 REAR SPAR HAS MINOR SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700401Spar · corrodedLEFT WING UPPER SURFACE MID SPAR WS 1112, WS 1280, WS 1330 AND WS 1392 HAS MINOR SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700405Bearing · corrodedRIGHT BODY GEAR RETRACT ACTUATOR LOWER END BEARING CORRODED. REMOVED CORROSION AS PER TEC - XMN-07-01832 PROPOSAL REF OHM 32-33-11.SDR UIEA200700400Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.5 TO WS 917 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700399Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.5 TO WS 917 BETWEEN MID SPAR AND REAR SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700398Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN MID SPAR AND REAR SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700397Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700396Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700395Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700394Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND REAR SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700377Seat Track · corrodedU/D BS 520 RBL 46 SEAT TRACK CORROSION. REPAIR SEAT TRACK IAW SRM 53-10-05 FIG 1A.
SDR UIEA200700393Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700381Spar · corrodedLHW UPPER SURFACE WS 353 TO WS 586 SPAR SURF CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700371Skin · corrodedSURFACE CORROSION EVIDENT AROUND HEAD FROM WS 724.50 TO WS 917.00 BETWEEN REAR SPAR AND MID SPAR. SURF, CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700382Skin · corrodedLHW UPPER SURFACE MID SPAR WS 1112 WS 1280 WS 1330 WS 1392 CORROSION EVIDENT. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700383Skin · corrodedSURF CORROSION EVIDENT AROUND HEAD FROM WS 528 TO WS 724.5 BETWEEN REAR SPAR AND MID SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700378Seat Track · corrodedBS 1960 LBL 99 SEAT TRACK FOUND CORROSION. BLEND OUT CORROSION IAW SRM 51-10-01 AND REPROTECTED IAW 51-10-02.SDR UIEA200700379Seat Track · corrodedBS 1980 RBL 90 SEAT TRACK FOUND CORROSION. BLEND OUT CORROSION IAW SRM 51-10-01 AND REPROTECTED IAW 51-10-02.
SDR UIEA200700380Skin · corrodedLHW UPPER SURFACE WS 807 STR S16 CORROSION EVIDENT. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700376Spar · corrodedWS 317 - WS 1141, FRONT SPAR TO REAR SPAR CORROSION EVIDENCED. SURFACE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700375Skin · delaminatedNR 2 SPOILER I/B EDGE DELAMINATION EVIDENCE. REPAIR CARRIED OUT IAW SRM 51-40-24.SDR UIEA200700374Skin · corrodedLHW SPOILER: NR 4 SPOILER O/B CORNER DELAMINATION EVIDENCE. REPAIR CARRIED OUT IAW SRM 51-40-24.SDR UIEA200700373Skin · corrodedLHW SPOILER: NR 1 SPOILER I/B EDGE DELAMINATION EVIDENCE. NR 1 SPOILER PNL REPLACED IAW AMM 27-61-02.SDR UIEA200700372Skin · corrodedRHW UPP SKIN PNL: WS1141-WS1337, FRONT SPAR TO REAR SPAR SEVERAL AREAS OF CORROSION EVIDENCED. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND SOPM 20-43-03.SDR UIEA200700370Skin · corrodedSURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.50 TO WS 917.00 BETWEEN FRONT SPAR AND MID SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
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