N528MC, cancelled Apr 30, 2013
Service difficulty reports · 63
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 = 'N528MC' AND deregistration_id = 'N528MC-2013-04-30' 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 = 'N528MC' AND deregistration_id = 'N528MC-2013-04-30' 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 UIEA200800281Relief Valve · leakingAT CRUISE NR 4 ENG HAD MULTPLE FIRE WARNINGS ON BOTH A&B. PERFORMED IN FLIGHT SHUT DOWN AND AIR TURNBACK. MAINTENANCE FOUND LEAKING PRESSURE RELIEF VALVE, WHICH WAS BLASTING HOT AIR ON THE DETECTORS. REPLACED OVER PRESSURE RELIEF VALVE PER 36-11-03, OPS CHESDR UIEA200800169Shear Pin · brokenAIR TURN BACK, SIDE CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. RETURNED TO BLOCKS PER FHB. FOUND OUTSIDE MASTER LATCH LOCK HANDLE SHEAR PIN BROKEN. REMOVED AND REPLACED SHEAR PIN PER AMM 52-32-06. OPS CHECKED OKAY.SDR UIEA200800163Regulator Valve · leakingNR 1 ENGINE FULL POWER TAKEOFF ON CLIMB-OUT BOTH A/B LOOPS REACHED 3.0. AFTER POWER REDUCTION BOTH LOOPS CAME BACK DOWN TO 2.0. REST OF FLIGHT WAS OK. OPENED COWL AND FOUND LEAKING PRV. REPLACED THE PRV IAW AMM 36-11-13. OPS AND LEAK CHECKED OK.SDR UIEA200800114Skin Panel · corrodedEVIDENCE OF CORROSION UNDER LAP JOINT STRINGER 46 RIGHT, BETWEEN STA 1737-1745. INTERIM REPAIR ACCOMPLISHED IAW SRM 53-30-03 FIG 17 TABLE LLL WITH INITIAL INSPECTION SCHEDULED AT 15000 FLIGHT CYCLES AFTER INTERIM REPAIR AND REPEAT INSPECTION THEREAFTER AT EVESDR UIEA200800113Skin · delaminatedRIGHT WING INBOARD SPOILER UPPER SURFACE HAS DELAMINATION WBL 235.150. REMOVED NR 7 GROUND SPOILER IAW MM 27-62-01. REPAIRED DELAMINATION IAW SRM 51-40-20. INSTALLED SPOILER AND OPS CHECKED OKAY PER 27-62-01.SDR UIEA200800042Radome · damagedAIRCRAFT WAS HIT BY LIGHTNING STRIKE. ENTRANCE AT THE RADOME. NO COMMUNICATIONS OR NAV FAILURES REPORTED BY CREW. FOUND RADOME DAMAGED BY LIGHTNING STRIKE. FOUND RIGHT HF ANTENNA DAMAGED BY LIGHTNING STRIKE. LIGHTNING STRIKE INSPECTION ACCOMPLISHED PER 5-SDR UIEA200700352Web · crackedOLEO 1450 FWD CRACKED JUST FWD OF NR 25 V/C FLAP UPPER FITTING. CARRY OUT REPAIR AS PER SRM 51-40-03.SDR UIEA200700349Nozzle · dentedNR 1 ENGINE EXHAUST NOZZLE DENTED AT 0300. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMITS AMM 78-11-01 PAGE 601.SDR UIEA200700347Web · crackedUPON L/E CAP REMOVAL OLES 1522, NR 26VC FLAP UPPER STOP FTG FWD WEB DOUBLER FOUND CRACKED. DOUBLER REPLACED IAW SRM 51-10-01.SDR UIEA200700346Frame · crackedR1 MED LOWER AFT CORNER FRAME CRACKED AT STA 490 RT S-25R TO S-26R AREA. C/OUT AS PER SRM 52-10-02 FIG 10.SDR UIEA200700345Door Frame · crackedM/D R4 MED FWD UPPER CORNER FRAME CRACKED AT STA 1670 S-16R TO S-17R AREA. CARRY OUT REPAIR AS PER SRM 52-10-02, FIG 10.SDR UIEA200700344Door Frame · crackedR3 DOOR FWD UPPER CORNER FRAME FOUND CRACKED. C/OUT AS PER SRM 52-10-02, FIG 10.SDR UIEA200700343Web · corrodedBULK CARGO BS 1980-2030 DOOR LOWER SILL FLOOR WEB, CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN ALLOWABLE LIMIT AS PER SRM 53-10-01.SDR UIEA200700342Panel · contaminatedRT WING I/B T/E PANEL FOUND WATER. REPLACE RHW I/B T/E PANEL AS PER SRM 51-10-01 AND SRM 51-30-02.SDR UIEA200700348Frame · crackedAFT REMOVAL OF L/E NOSE CAP FOUND THAT "D" SECTION CRACKED. CARRY OUT REPAIR AS PER SRM 57-20-03.SDR UIEA200700350Nozzle · dentedNR 3 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.SDR UIEA200700351Nozzle · dentedNR 4 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0700 TO 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.SDR UIEA200700336Access Panel · elongatedAIR COND, BAY ACCESS PANEL 192ER EXT SURFACE FOUND SKIN ELONGATION. AIR COND BAY ACCESS PANEL 192ER REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.SDR UIEA200700329Frame · crackedBS 800 S17 LT ONE FASTENER HOLE FOUND CRACK ON FWD INNER CHORD ANGLE. REPLACEMENT PER BOEING CONTROL NO PO24708.SDR UIEA200700337Access Panel · delaminatedAIR COND, BAY ACCESS PANEL 192HR EXT SURFACE FOUND SKIN DELAMINATION. AIR COND BAY ACCESS PANEL 192HR REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.SDR UIEA200700335Access Panel · erodedAIR COND, BAY ACCESS PANEL 191HL EXT SURFACE FOUND ERODED. AIR COND BAY ACCESS PANEL 191HL REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.SDR UIEA200700332Floorbeam · crackedFLOOR STRUCTURE BEAM WEB CRACKED. C/OUT AS PER BOEING MESSAGE NR 1-497681686-1.SDR UIEA200700338Torque Link · chafedNLG LOWER TORSION LINK FOUND CHAFING. BLEND OUT THE CHAFING AREA WITH MIN 20-1 BLEND-RATIO.SDR UIEA200700331Skin · dentedHORIZONTAL STAB RT I/B ELEVATOR L/E UPPER SKIN DENTED. REPAIRED IAW BOEING MESSAGE SR 1-514407012.SDR UIEA200700333Floorbeam · crackedFLOOR STRUCTURE BEAM WEB CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.SDR UIEA200700339Skin · dentedFX EXTERIOR SKIN DENT AS MARKED APPR, 1" SQ IN AT BS 780 S47-R. REINSTALLED A REPAIRED DOUBLER AS PER SRM 53-30-03 DETAILS AS PER SWS SHOWN.SDR UIEA200700334Pan · crackedCOCKPIT 2ND OBSERVER SEAT PAN CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.SDR UIEA200700340Hinge Fitting · crackedBS 2598 H/S RT RBL 40" REAR SPAR UPPER I/B OF HINGE FITTING OPEN HOLE. OVERSIZE TO 0.403", USED BACB30 US6K21Y BOLT. CARRIED OUT NDT TEST OF THE OPEN OVERSIZE HOLE FOUND SATISFACTORY.SDR UIEA200700330Panel · contaminatedLT WING T/E I/B PANEL FOUND WATER. REPLACE LHW T/E I/B FIXED PAL AS PER SRM 51-10-01 AND SRM 51-30-02, AND PANEL REPAIR IAW BOEING MESSAGE 31-516595696-1 TO 1-516595696-4.SDR UIEA200700260Unknown · odorAT DEPARTURE SMOKE AND BURNING ODOR IN COCKPIT, ELECTRICAL ODOR. PULLED C/BS FOR T/R UNITS, SMOKE AND ODOR STOPPED. WIRE BUNDLES AND AREA BELOW F/E PANEL (4) INSPECTED NO SIGN OF SHORTING OR CHAFING FOUND. PULLED T/R UNITS, PULLED AND INSPECTED FOUND NR 1 TSDR UIEA200700259Seal · looseL-3 WINDOW SEAL LIFTING IN THE WIND WITH EXCESSIVE COCKPIT NOISE. ALSO, DURING LEVEL FLIGHT APPROX TIME 1335Z FL 31.0 TEMP -09 TAT HEARD BANG AIRCRAFT SHOOK, POSSIBLE ENGINE STALL. AUTO THROTTLES TRIPPED OFF SEVERAL TIMES IN FLIGHT. RESECURED WINDOW SEAL ISDR UIEA200700255Panel · corrodedLOWER FUSELAGE CENTER PANELS 191HH AND 191JJ BETWEEN NR 1 AND NR 3 ACM'S HAVE AREA OF CORROSION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-02 FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 53-062007.SDR UIEA200700252Fairing · damagedRT WING, NR 8 FLAPTRACK FORWARD FIXED FAIRING HAS SEVERAL SMALL HOLES AT LEADING EDGE AREA. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09, FIG 6, TABLE I AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57-061907.SDR UIEA200700254Support · corrodedLOWER FUSELAGE AIR CONDITIONING ACCESS DOOR AREA, BELOW KEEL BEAM BOX, EXTERIOR CENTER PANEL SUPPORT EXTRUSION HAS CORROSION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-04, FIG 1. ALSO REFERENCE ATLAS AIR XEO NR 53-062007.SDR UIEA200700251Fairing · crackedRT WING NR 7 FLAP TRACK CANOE FAIRING DAMAGED AT LOWER SIDE, AFT OF ACCESS PANEL 667CB. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09, FIG 6 TABLE I AND 747-200 SRM 51-40-12. ALSO REFERENCE ATLAS AIR XEO NR 57-061907.SDR UIEA200700253Skin · delaminatedNR 4 ENGINE RT REVERSER AT NAC STATION 206.10 UPPER SIDEWALL SKIN DELAMINATED. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-03, REPAIR NR 13, REF: FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 78-062007.SDR UIEA200700148Skin · crackedFUSELAGE SKIN HAS 12" CRACK FROM STA 2650 TO 2658 ON RIGHT SIDE OF AIRCRAFT BETWEEN STRINGERS 11R AND 13R. FOUND CRACKED IN A SEMI-CIRCULAR SHAPE. REPAIRED PER SRM 53-30-03 FIG 1 DETAIL L AND XEO 53-04-06-07. (TIME LIMITED REPAIR)SDR UIEA200700068Altimeter · faultyCAPT ALT UNRESPONSIVE TO ALL CHANGE BOTH CADC/STBY MODES, PERFORMED CHECK DIFFERENCE BETWEEN ALT INDICATORS (3,34,7), CHANGE ALT LAGS IN DESCENT BY OVER 300' AND DIFFERS BY OVER 180' AT EL 290-310-MACH .84. T/S AND FOUND PIN NR 22 AT PLUG DN 101. CAPT ALT INSDR UIEA200700066Cadc · stickingDURING CLIMB CAPT ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNINGS, DON’T SINK WARNING AUDIBLES, ALTIMETER READ 37.0, ATC 36.8. PERFORMED STATIC SYSTEM LEAK CHECK NORMAL AS PER MM 34-11-00. FOUND NR 1 CADC DEFECTIVE. REMOVED AND REPSDR UIEA200700065Altimeter · stickingDURING CLIMB CAPT'S ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNING, DON'T SINK WARNING AUDIBLES. CAPT'S ALTIMETER REMOVED AND REPLACED, INDICATION AND LEAK CHECK CARRIED OUT, OK IAW MM 34-13-04.SDR UIEA200700026Panel · crackedLT WING PYLON GAP PANEL AT ILES 640.47 HAS A 3.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 18 SHEET 5 AND SRM 51-40-12, ALSO REFERENCE ATLAS AIR EO 4757A342.SDR UIEA200700027Panel · crackedLT WING UPPER FIXED PANEL, 12 INCHES FROM FORWARD EDGE OF NR 5 SPOILER, WBL 421.00 HAS A 6.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 SHEET 5 AND SRM 51-40-12 AND ATLAS AIR EO 4757A342.SDR UIEA200600290Skin · puncturedNR 21 LEADING EDGE DEVICE FOLDING NOSE FOUND DAMAGED ON ARRIVAL. NOSE HINGE ARM FOUND BROKEN AND SKIN PUNCTURED. UNABLE TO CONCLUSIVELY DETERMINE THE REASON FOR THE FAILURE AND SUBSEQUENT DAMAGE. REPLACED NR 21 LEADING EDGE DEVICE ASSY.SDR UIEA200600158Duct · rupturedFOLLOWING TAKEOFF NR 4 ENG FIRE INDICATIONS NACELLE TEMPS A/B HIGH, THEN TO FIRE "F" AND FULL WARNING ENG NR 4 SHUTDOWN AS PER CHECKLIST. NR 4 ENG FIRE BOTTLE "A" DISCHARGED, FIRE WARNING EXTINGUISHED. FOUND 14TH STAGE BLEED AIR DUCT RUPTURE. REMOVED AND RESDR UIEA200700256Skin · dentedNR 4 ENGINE LT REVERSER HAS DENT ON UPPER SIDE OF TRANSLATING COWL AT NAC STATION 224.6. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-01, REPAIR 003. ALSO, REFERENCE ATLAS AIR XEO NR 78-062107.SDR UIEA200600131Hydraulic Line · crackedDURING CLIMB NR 4 HYD SYSTEM STARTED DECREASING AND LOW QUANTITY LIGHT CAME ON. FHB PROCEDURES C/W AND QUANTITY WAS STILL DECREASING. ENG PUMP SWITCH WAS POSITIONED TO "SUPPLY OFF" WITH ENGINE RUNNING. QUANTITY INDICATOR ZERO AT COMPLETION OF CHECKLIST. FOSDR UIEA200600136Start Valve · damagedNR4 ENGINE SHUT DOWN AT 1945Z DUE TO NR 4 START VALVE ENGINE LIGHT FLICKERING AND THEN COMING ON. REMOVED AND REPLACED NR 4 START VALVE AS PER AMM 80-11-04. PERFORMED GROUND OPS BY MONITORING SATISFACTORY.SDR UIEA200600121Seal · damagedACCOMPLISHED AIR TURNBACK DUE TO LOSS OF ALL OIL IN ENGINE NR 1, DURING CLIMBOUT. FOLLOWED SHORTLY BY A DROP IN OIL PRESSURE INTO THE MID TO LOWER AMBER BAND. FOUND NR 1 ENGINE HYD PUMP SHAFT SEAL CAVITY LEAKING OIL DURING IDLE RUN. HYD (EDP) PUMP SHAFT SEASDR UIEA200600127Relief Valve · leakingAT 3000 FT DURING CLIMBOUT FIRE DETECTION LIGHT ON PILOT'S CENTER ANNUNCIATOR PANEL ILLUMINATED, FOLLOWED SHORTLY BY A FIRE INDICATION ON NR 1 ENGINE. FIRE CAUSED SEVERE DAMAGE OR SEPARATION, CHECKLIST COMPLETE AS PER FHB 3.701. OVERWEIGHT LANDING AT 287.0 KSDR UIEA200600006Panel · missingON WALKAROUND FOUND NR 1 ENGINE LOWER ACCESS PANEL MISSING.
Back to N528MC, cancelled Apr 30, 2013