N528FE

Service difficulty reports · 229

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 = 'N528FE' 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.

SDR 06FDEA03860Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL DIA: 1.240", FINAL DIA: 1.283", MAX ALLOWABLE DIA: 1.220". BUSHING FABRICATED AND INNov 3, 2006 · N528FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03859Hinge · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE), LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-408 AND FOUND WITHIN DAC ARC0503 LIMITS. ORIGINAL THK I/B: 0.474", O/B: 0.469", REMAINING THK I/B: 0.472", O/B: 0.467", MATERINov 3, 2006 · N528FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03858Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG 621-622. ORIGINAL DIA: 1.148", FINAL DIA: 1.152", MAX ALLOWABLE DIA: 1.150". BUSHING FABRACATED AND INNov 3, 2006 · N528FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03821Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE CORRODED. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 31, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03820Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 31, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03813Seat Track · corrodedFOUND SEAT TRACK AT STA 5-32 -5-123 X= -27.5 HAD SEVERAL PLACES CORRODED. DAMAGE SEAT TRACK REMOVED AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK , SPLICE HAT AND SPLICE PLATE FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I AND INSTALLED AS PER SRM 53-70-00 FIG Oct 30, 2006 · N528FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03812Seat Track · corrodedFOUND SEAT TRACK AT STA 1421- 5-12 X= 8.5 HAD SEVERAL PLACES CORRODED. DAMAGE SEAT TRACK REMOVED AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK , SPLICE HAT AND SPLICE PLATE FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I AND INSTALLED AS PER SRM 53-70-00 FIG 1 Oct 30, 2006 · N528FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03811Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-408 AND FOUND WITHIN DAC DWG ARC 0503 LIMIT. ORIGINAL THK I/B: 0.455", O/B: 0.462", REMAINING THK I/B: 0.453", O/B: 0.4Oct 30, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03810Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE ACTUATOR O/B BORE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-408. ORIGINAL DIA: 1.187", FINAL DIA: 1.2145", MAX ALLOOct 30, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03809Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE ACTUATOR I/B BORE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-408. ORIGINAL DIA: 1.187", FINAL DIA: 1.216", MAX ALLOWABLOct 30, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03808Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG 602-607 AND FOUND WITHIN DAC DWG ARC0502 LIMIT. ORIGINAL THK I/B: 0.465", O/B: 0.468" REMAINING THK I/B: 0.423", O/B: 0.432", MAOct 30, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03806Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PG 612-615 AND FOUND WITHIN DAC DWG ARC0502 LIMIT. ORIGINAL THK I/B: 0.383", O/B: 0.388", REMAINING THK I/B: 0.380", OOct 30, 2006 · N528FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03726Skin · crackedLT WING TELESCOPIC DUCT CUTOUT UPPER O/B CORNER FOUND CRACKED AS MARKED. LT WING TELESCOPIC DUCT CUTOUT UPPER O/B CORNER CRACK REPAIRED AS PER EA 1-5740- 104739, WING- LEADING EDGE AND LEADING EDGE DEVICES- LEFT- HEAD FIX LEADING EDGE SKIN REPAIR XORS= Oct 19, 2006 · N528FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03725Skin · crackedLT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER FOUND CRACKED AS MARKED. LT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER CRACK REPAIRED AS PER EA# 1-5740- 104739, WING- LEADING EDGE AND LEADING EDGE DEVICES- LEFT- HEAD FIX LEADING EDGE SKIN REPAIR XORS= Oct 19, 2006 · N528FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03724Skin · crackedRT WING TELESCOPIC DUCT CUTOUT UPPER O/B CORNER FOUND CRACKED AS MARKED. RT WING TELESCOPIC DUCT CUTOUT UPPER O/B CORNER CRACK REPAIRED AS PER EA 1-5740- 104740, WING LEADING EDGE AND LEADING EDGE DEVICES- RIGHT- HAND FIX LEADING EDGE SKIN REPAIR XORS= 4Oct 19, 2006 · N528FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA03723Skin · crackedRT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER FOUND CRACKED AS MARKED. RT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER CRACK REPAIRED AS PER EA 1-5740- 104740, LEADING EDGE AND LEADING EDGE DEVICES- RIGHT HAND FIX LEADING EDGE SKIN REPAIR XORS=464.00 THROct 19, 2006 · N528FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03722Access Panel · crackedRT WING LOWER L/E ACCESS PANEL NR 626FB I/B FLANGE FOUND CRACKED BETWEEN NR 14 AND NR 15 SLAT TRACK. REPAIRED AS PER SRM 57-10-00 FIG 18 VOL I. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 19, 2006 · N528FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03721Access Panel · crackedLT WING LOWER L/E ACCESS PANEL NR 526FB I/B FLANGE FOUND CRACKED BETWEEN NR 14 AND NR 15 SLAT TRACK. LT WING LOWER L/E CRACK AT ACCESS PANEL 526 FB I/B FLANGE BETWEEN NR 14 AND 15 SLAT TRACK REPAIRED AS PER SRM 57-10-00 FIG 18 VOL I. THIS REPAIR CLASSIFIED Oct 19, 2006 · N528FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03651Skin · unknownRT WING DROOP L/E UPPER SURFACE O/B TOP CORNER FOUND WITH EXISTING DOUBLER REPAIR. RT WING DROOP L/E UPPER O/B TOP CORNER EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 VOL II AND AREA REPAIRED AS PER SRM 57-10-00 FIG 26 VOL I. THIS REPAIR CLASSIFIED ASOct 17, 2006 · N528FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03670Rib · crackedLT WING L/E NR 16 TRACK I/B RIB FOUND CRACKED. LT WING L/E NR 16 TRACK I/B RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Rib/BulkheadSDR 06FDEA03669Rib · crackedRT WING L/E NR 16 TRACK I/B RIB FOUND CRACKED. RT WING L/E NR 16 TRACK I/B RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II AND CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Rib/BulkheadSDR 06FDEA03668Stringer · crackedCRACK FOUND FROM THE END OF STRINGER-12, APPROX 8" AT RT WING TANK AT XORS 642 DURING HFEC INSPECTION. RT WING TANK STR-12 END CRACK AT XORS 642 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03667Stringer · crackedCRACK FOUND FROM THE END OF STRINGER-44, APPROX 1/2 INCH AT LT WING TANK AT XORS 523 DURING HFEC INSPECTION. LT WING TANK STRINGER -44 END CRACK AT XORS 523 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 2 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03665Stringer · crackedCRACK FOUND FROM THE END OF STRINGER-42, APPROX 3.5" AT LT WING TANK AT XORS 629 DURING HFEC INSPECTION. LT WING TANK STRINGER-42 END CRACK AT XORS 629 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03664Stringer · crackedCRACK FOUND FROM THE END OF STRINGER 41 APPROX 1" AT LT WING TANK AT XORS 685 DURING HFEC INSPECTION. REPAIRED AS PER EA 1-5720.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03663Stringer · crackedCRACK FOUND FROM THE END OF STRINGER-11 APPROX 11" AT RT WING TANK AT XORS 704 DURING HFEC INSPECTION. RT WING TANK STRINGER -11 END CRACK AT XORS 704 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03661Stringer · crackedCRACK FOUND FROM THE END OF STRINGER-10 APPROX 2" AT RT WING TANK AT XORS 760 DURING HFEC INSPECTION. RT WING TANK STR-10 END CRACK AT XORS 760 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03660Stringer · crackedCRACK FOUND FROM THE END OF STRINGER-7, APPROX 4" AT RT WING TANK AT XORS, 952 DURING HFEC INSPECTION. RT WING TANK STRINGER -7 END CRACK AT XORS 952 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 17, 2006 · N528FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03647Skin · wornLT WING I/B T/E FLAP UPPER AFT I/B SKIN FOUND WITH EXISTING DOUBLER REPAIR. EXISTING REPAIR AT LT WING I/B T/E FLAP UPPER AFT I/B SKIN EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER SRM 57-10-00 FIG 34 VOL I EO 1-5100-7-5001A-PT1, TITLE: "REPAIR CATALOG-MD11Oct 16, 2006 · N528FE · Doug MD11 · Trailing Edge Flaps
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