N526FE, cancelled Sep 4, 2012

Service difficulty reports · 84

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 = 'N526FE' AND deregistration_id = 'N526FE-2012-09-04'
  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 07FDEA04675Frame · dentedMAIN DECK CARGO COMPARTMENT, LEFT STA 1761 FRAME AT ABOUT STRINGER 12R AREA FOUND CRACKED. 11-07-07 MAIN DECK CARGO COMPARTMENT - LEFT HAND STA 1761 FRAME AT STRINGER 12L CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 3 VOLUME I. DUE TO CATEGORY B REPAIOct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, FrameSDR 07FDEA04674Frame · dentedMAIN DECK CARGO COMPARTMENT, RIGHT STA 1681 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTOct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, FrameSDR 07FDEA04673Frame · dentedMAIN DECK CARGO COMPARTMENT, RIGHT STA 1701 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPOct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, FrameSDR 07FDEA04672Frame · dentedMAIN DECK CARGO COMPARTMENT, RIGHT STA 1721 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIOOct 24, 2007 · N526FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA2637Structure · corrodedHORIZONTAL STABILIZER - INSPECT/REPAIR HORIZONTAL STABILIZER BARREL NUT HOLES. WORK ACCOMPLISHED AS PER EA 1-5510-94622 AIR WORTHINESS DIRECTIVE AD 2003-22-08- STABILIZERS - HORIZONTAL STABILIZER - EMBODIMENT OF HORIZONTAL STABILIZER S/B MD11-55-023 BARREL NUJul 20, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 06FDEA2491Skin · damagedFOUND RT WING NR 3 SLAT LE SURFACE FOUND DAMAGED. REPAIR CARRIED OUT ON RT WING NR 3 SLAT L/E SURFACE AS PER SRM 57-10-00 FIG.33 VOL.I.REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jul 10, 2006 · N526FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA2459Skin · crackedFOUND CRACKED FASTENER HOLE AT UPPER SURFACE OF RT WING DROOP LE SLAT. WORK CARRIED OUT AS PER E.A.1-5740-99695 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jul 4, 2006 · N526FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA2415Skin · crackedSNRM N02174: RT WING NR 7 SLAT INTERIOR SURFACE MID SECTION SUSPECT SKIN CRACK. REPAIRED AS PER SRM 57-10-00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.Jun 27, 2006 · N526FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA2045Skin Panel · unknownFOUND EXISTING FLUSH REPAIR FOUND AT RT FWD CORNER OF FUSELAGE CAC ACCESS DOOR CUTOUT (REF EO1-5100-7-5001). SKIN REPAIRED AS PER EA 1-5330-94701.May 28, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1932Longeron · crackedFOUND CRACKED LONGERON 7L ON INTERCOSTAL AT BS 518 RT. INTERCOSTAL REPLACED AS PER SRM 51-35-01 VOL2 AND DRAWING AFA3086.May 15, 2006 · N526FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 06FDEA1704Repair · unknownREPAIR REQUIRED AT UNUSED MOUNTING BASE HOLES OF ANTENNA (P/N S65- 5366-890L QTY 04 EACH) AFTER ITS REMOVAL AS PER EA1-2310-94626 STEP 18 REQUIREMENT, SNRM N01696: SKIN REPAIR AT BS 839-879 LONGERON 51L-51R AND INNER DOUBLER AT BS 859-879 LONGERON 51R-52. INMay 4, 2006 · N526FE · Doug MD11 · Standard Practices/StructuresSDR 06FDEA1678Bracket · crackedCRACK SUPPORT BRACKET FOR TAIL FUEL TRANSFER PIPE IN EMPERAGE.May 2, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer StructureSDR 06FDEA1677Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1676Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT BARREL NUT BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1675Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1674Attach Fitting · corrodedCORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1673Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1672Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) LOWER ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-605 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1671Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1670Attach Fitting · corrodedCORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.May 2, 2006 · N526FE · Doug MD11 · Wing, Attach FittingsSDR 06FDEA1615Spar · corrodedCORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 799-827. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.Apr 26, 2006 · N526FE · Doug MD11 · Wing SparSDR 06FDEA1614Spar · corrodedCORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 786-799. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.Apr 26, 2006 · N526FE · Doug MD11 · Wing SparSDR 06FDEA1613Spar · corrodedCORROSION LT WING REAR SPAR UPPER SURFACE BETWEEN BS 738-773. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.Apr 26, 2006 · N526FE · Doug MD11 · Wing SparSDR 06FDEA1606Web · damagedFLIGHT DECK OBSERVER SEAT DOUBLE FLANGE LIGHTENING HOLE LOCATED UNDERNEATH THE SEAT IN THE COCKPIT SUBFLOOR STRUCTURE FOUND DAMAGED.Apr 26, 2006 · N526FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 06FDEA1605Fitting · damagedLEFT INBOARD FLAP AFT UPPER ROLLER SUPPORT STRUCTURE CENTER BOLT HOLE FOUND DAMAGED.Apr 26, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1604Wedge · severedLT INBOARD FLAP TRAILING EDGE WEDGE ATTACH CHANNEL OUTBOARD REMOVABLE SEGMENT FOUND SEVERED AT THE OUTBOARD MOST 12 INCH (MATERIAL CLAD 2024-T42 SHEET 0.04 INCH).Apr 26, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1603Skin · dentedDENT FUSELAGE SKIN BETWEEN BS 1997-2015 AND S46L-47L. REPAIRED AS PER EA 1-5330-99714.Apr 26, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1602Attach Fitting · damagedLT INBOARD AILERON ATTACH LUG FOUND DAMAGED AT 2 LOCATION ON THE INBOARD SURFACE OF THE LUG AT UPPER AND LOWER CORNER.Apr 26, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer, Attach FittingsSDR 06FDEA1601Structure · damagedLT INBOARD AILERON INBOARD TRAILING EDGE FOUND AN IMPACT DAMAGED.Apr 26, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer StructureSDR 06FDEA1600Skin · damagedRIGHT HORIZONTAL STAB LEADING EDGE SECTION FOUND DAMAGED AT STA XFS91.2.Apr 26, 2006 · N526FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA1599Rib · damagedRIGHT HORIZONTAL STAB INBOARD ELEVATOR ASSY OUTER RIB FOUND DAMAGED.Apr 26, 2006 · N526FE · Doug MD11 · Elevator, Spar/RibSDR 06FDEA1595Bracket · dentedDENT AFT BRACKET AT DOOR 2R LOWER SIDE. REPLACED BRACKET AS PER DRAWING ADA3760 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).Apr 25, 2006 · N526FE · Doug MD11 · Passenger/Crew DoorsSDR 06FDEA1594Bracket · crackedCRACK FWD BRACKET AT DOOR 4R LOWER SIDE. REPLACED BRACKET AS PER DRAWING ADA3760 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).Apr 25, 2006 · N526FE · Doug MD11 · Passenger/Crew DoorsSDR 06FDEA1593Skin · damagedFUSELAGE EXTERIOR SKIN FOUND DAMAGED BETWEEN BS 1951-1961 LONGERON 38R-39R. REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK.0.068" REMOVED 0.006"X L=3"X W=3" REMAIN 0.062" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPApr 24, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1592Structure · crackedCRACK LOWER FWD CORNER OF AFT CARGO DOOR. REPAIRED AS PER SRM 52-10-00 FIG. 17 VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.Apr 24, 2006 · N526FE · Doug MD11 · Cargo/Baggage DoorsSDR 06FDEA1591Skin · dentedMULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE OUTBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.Apr 24, 2006 · N526FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA1590Skin · dentedMULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE INBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.Apr 24, 2006 · N526FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA1589Hinge · corrodedCORROSION PIVOT BORE AT RT WING INBOARD FLAP OUTBOARD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-07 PAGE 403-404 AND EA 1-5750- 94700.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1588Skin · dentedEXISTING DENT FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED 69 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).Apr 24, 2006 · N526FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA1587None · noneEXISTING REPAIR FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED ABOUT 76 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).Apr 24, 2006 · N526FE · Doug MD11 · Standard Practices/StructuresSDR 06FDEA1586Hinge · corrodedFOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-09 PAGE 402-407 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0503 AND REPAIRED AS PER CMM 57-44-09.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1585Hinge · corrodedFOUND CORROSION, LOWER ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1584Hinge · corrodedFOUND CORROSION, ACTUATOR ATTACHMENT OUTBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1583Hinge · corrodedFOUND CORROSION, ACTUATOR ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1582Hinge · corrodedFOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1581Hinge · corrodedFOUND CORROSION, LOWER ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-607 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1580Skin · dentedEXISTING DENT FOUND AT LT WING INBD FLAP ASSY UPP SURFACE LOCATED 37 INCH FROM INBD AND 30 INCH FROM AFT. FOUND EXCEED LIMIT AND REPAIRED AS PER SRM 57-10-00 FIG. 34 VOL.I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.Apr 24, 2006 · N526FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA1556Repair · unknownEXISTING FLUSH REPAIR FOUND AT FUSELAGE ADJACENT TO BS435 BILGE BETWEEN LONGERON 51L TO 51R (REF EO 1-5100-7-5001). SKIN REPAIRED AS PER SRM 53-20-00 FIG6 SHEET8 VOL1 CATB REPAIR-INITIAL INSPECTION AT 7500 CYCLES AND REPETITIVE INSPECTION AT 4750 CYCLES Apr 20, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1555Doubler · crackedFOUND CRACK-MACHINED DOUBLER LOCATED BETWEEN RT WALL (ADJACENT TO RT SPOILER MIXER OUTPUT ROD) AND RT WHEEL WELL CUTOUT OF CENTER LANDING GEAR WHEEL WELL. CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM Apr 20, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1554Doubler · crackedFOUND CRACK-MACHINED DOUBLER LOCATED BETWEEN LT WALL (ADJACENT TO LT SPOILER MIXER OUTPUT ROD) AND LT WHEEL WELL CUTOUT OF CENTER LANDING GEAR WHEEL WELL. CRACKED DOUBLER REMOVED AND REPLACED AS PER 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2Apr 20, 2006 · N526FE · Doug MD11 · Fuselage Main, Plate/Skin
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