Douglas DC-9-32

Service difficulty reports · 12,755

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'DC932'
  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 MWEA010558Floorboard · crackedFLOORBOARD A-8 HAS 2 CRACKS AT FASTENER HOLES ON TOP SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER AND FAIRING.Apr 10, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010556Stringer · corrodedLEFT WING INTERNAL: LIGHT TO MODERATE CORROSION ON THE FORWARD LOWER HORIZONTAL LEG OF STRINGER 22 INBOARD END. APPROXIMATELY 3 INCHES FROM XCW 58. REMOVED AND REPLACED STRINGER.Apr 10, 2001 · N209ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA010555Spar · corrodedAFT SPAR SPLICE TEE REMOVED TO FACILITATE OTHER MAINTENANCE, STATION 111.5. FOUND CORROSION. FABRICATED AND INSTALLED SPLICE TEE.Apr 9, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010554Stiffener · tool damageREMOVED STIFFENER TO FACILITATE OTHER MAINTENANCE, LEFT WING STATION XRS 85. FOUND TOOL MARKS AND LIGHT CORROSION ON STIFFENER. FABRICATED AND INSTALLED STIFFENER.Apr 9, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010553Stiffener · corrodedREMOVED STIFFNER TO FACILITATE OTHER MAINTENANCE, STATION XRS 95. FOUND TOOLMARKS AND LIGHT CORROSION ON STIFFENER. FABRICATED AND INSTALLED STIFFENER.Apr 9, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010552Spar · corrodedRIGHT WING INTERNAL: LIGHT CORROSION ON OUTBOARD EDGE OF XCW 58 SPAR TEE LOWER LEG, FORWARD OF STRINGER 22. REMOVED CORROSION AND BLENDED AREA; WING TEE IS WITHIN SERVICEABLE LIMITS PER TELEX MWX-ORD-01-00200H DATED 07 MARCH 2001.Apr 9, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010551Spar · corrodedRIGHT WING INTERNAL: FOUR AREAS OF LIGHT TO MODERATE CORROSION ON XCW 58 TEE LOWER LEG BETWEEN STRINGEER 21 AND 22. REMOVED CORROSION AND BLENDED AREAS; WING TEE IS WITHIN SERVICEABLE LIMITS PER MWX-ORD-01-00200H DATED 07 MARCH 2001.Apr 9, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010550Spar · corrodedRIGHT WING INTERNAL: LIGHT TO MODERATE CORROSION ON XCW 58 SPAR TEE LOWER LEG FORWARD OF STRINGER 16. REMOVED CORROSION; WING TEE IS WITHIN SERVICEABLE LIMITS PER TELEX MWX-ORD-01-00200H DATED 07 MARCH 2001.Apr 9, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010533Floor Panel · crackedCABIN FLOOR PANEL B3 HAS TWO FASTENER HOLES CRACKED OUT. FABRICATED AND INSTALLED DOUBLERS AND FILLERS.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010549Spar · corrodedLEFT AUX SPAR WEB HAS INTERGRANULAR CORROSION. FABRICATED AND INSTALLED WEB.Apr 9, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010548Web · corrodedWEB SUPPORT ASSY AT STATION XRS 137 REMOVED TO FACILITATE OTHER MAINTENANCE. CORROSION PRESENT BY FASTENER HOLES. REMOVED AND REPLACED PART.Apr 9, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010547Spar · corrodedRIGHT WING INTERNAL: LIGHT CORROSION ON LOWER HORIZONTAL LEG OF FORWARD SPAR, STARTING 3 INCHES OUTBOARD OF XCW58 FOR A STRETCH OF APPROXIMATELY 12 INCHES OUTBOARD. REMOVED CORROSION AND BLENDED AREA ACCEPTABLE PER MWE/BOEING TELEX #MWX-ORD-01-00206H.Apr 9, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010546Floorboard · crackedFLOORBOARD B-8 HAS 2 EA CRACKED HOLES IN FORWARD END. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010545Floorboard · crackedFLOORBOARD B-2 HAS 3 EACH CRACKED HOLES IN FORWARD END. FABRICATED AND INSTALLED FLOOR BOARD REPAIR PARTS.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010544Floorboard · crackedCOCKPIT CENTER FLOORBOARD HAS A CRACK AT A FASTENER HOLE, LOCATED ON THE RIGHT SIDE TOWARDS THE FORWARD END. FABRICATED AND INSTALLED FLOOR BOARD AND HAT CHANNELS.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010543Floorboard · crackedLEFT FLOORBOARD B9 HAS SKIN CRACKS AROUND RIVITS WHICH SECURES CHANNELS AT ONE END. FABRICATED AND INSTALLED SKIN SPLICE AND FILLER.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010542Floorboard · damagedFLOORBOARD F-4 AFT OUTBOARD CORNER IS MISSING, HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND AROUND SOME FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED SKIN FOR FLOORBOARD.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010541Floorboard · corrodedFLOORBOARD E-6 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE WITH SOME FASTENERS PULLED THROUGH SKIN AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. REMOVED AND REPLACED WITH FLOORBOARD REPAIR.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010540Floorboard · crackedFLOORBOARD B-1 HAS A SMALL CRACK IN TOP SURFACE WITH CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOOR PANEL.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010539Floorboard · corrodedFLOORBOARD B-8 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOOR BOARD REPAIR PARTS.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010538Floorboard · corrodedFLOOR BOARD F-2 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFTES AND CORROSION. FABRICATED AND INSTALLED TOP SKIN.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010537Floor Panel · crackedCABIN FLOOR PANEL A4, SKIN IS CRACKED AT FORWARD CORNER. FABRICATED AND INSTALLED FLOOR PANEL REPAIR PARTS.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010536Floor Panel · dentedCABIN FLOOR PANEL E15, SKIN IS DENTED AND A PIECE CRACKED OFF AT ONE EDGE. FABRICATED AND INSTALLED SKIN.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010535Floor Panel · corrodedCABIN FLOOR PANEL F9 HAS AREAS OF LIGHT CORROSION AND MISSING PAINT ON TOP SIDE. FABRICATED AND INSTALLED PATCH AND FILLER.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010534Floor Panel · misdrilledCABIN FLOOR PANEL B7 HAS MISDRILLED FASTNER HOLES AT ONE END. FABRICATED AND INSTALLED FLOOR PANEL REPAIR PARTS.Apr 9, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR ABXA010119Seat Track · corrodedSEAT TRACK LOCATED AT FUSELAGE STATION 160 LBL 44 WAS EXFOLIATED. MAINTENANCE INSPECTED AND REPLACED THE SEAT TRACK FROM FS 160 TO FS 218 IAW DC-9 SRM 51-30-1.Apr 9, 2001 · N984AX · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA010120Frame · crackedFUSELAGE FRAME AT STATION 737 LEFT SIDE WAS FOUND TO BE CRACKED. MAINTENANCE INSPECTED AND REPLACED THE MAIN FRAME AT STA 737 IAW ABX EA 53400325-001.Apr 9, 2001 · N984AX · Doug DC932 · Fuselage Main, FrameSDR ABXA010121Seat Track · corrodedSEAT TRACK AT FUSELAGE STATION 200 RBL 44 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE SEAT TRACK FROM FS 145 TO FS 200, IAW DC-9 SRM 51-30-1.Apr 9, 2001 · N984AX · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT0100162Door Frame · corrodedFOUND AFT STAIRWAY DOOR FRAME CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ATTACH ANGLE REPAIR IAW DC9 SRM 53-01 FIG 1, 51-30, 51-10-03, 51-10-02, 51-10-04 AND 51-30-01.Apr 8, 2001 · N803AT · Doug DC932 · Fuselage Main, StructureSDR AT0100154Coalescer Bag · dirtyHOT OILY SMELL NOTED AT 9000 FT. BOTH A/C TEMPS BELOW 25 DEGREES. REPLACED COALESCER BAGS AND SEALS.Apr 6, 2001 · N831AT · Doug DC932 · Humidity Control SystemSDR AT0100122Coalescer Bag · dirtyHOT OILY SMELL WAS NOTED AT 9000 FT. REPLACED COALESCER BAGS AND SEALS.Apr 6, 2001 · N831AT · Doug DC932 · Humidity Control SystemSDR MWEA010532Floor Panel · puncturedCABIN FLOOR PANEL B3 HAS A PUNCTURE HOLE IN SKIN AT FORWARD END. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010531Floor Panel · crackedCABIN FLOOR PANEL B9 HAS SKIN CRACKS AROUND RIVETS WHICH SECURE CHANNELS AT ONE END. FABRICATED AND INSTALLED PANEL REPAIR PART.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010530Panel · crackedCABIN FLOOR PANEL B9 HAS ONE FASTENER HOLE CRACKED OUT. FABRICATED AND INSTALLED PANEL REPAIR PARTS.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010529Floor Panel · corrodedCABIN FLOOR PANEL E10 HAS LIGHT CORROSION AROUND FASTENER HOLES BOTTOM SIDE AND MISSING SECTION OF CHAFE STRIP, LOCATED AFT LEFT CORNER. FABRICATED AND INSTALLED SECTION OF CHAFE STRIP.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010528Floor Panel · crackedCABIN FLOOR PANEL E10 FASTENER HOLE IS CRACKED OUT, LOCATED AT AFT END, LEFT SIDE. FABRICATED AND INSTALLED PANEL REPAIR.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010527Floor Panel · crackedCABIN FLOOR PANEL E10, FORWARD SIDE HAS CRACKS AROUND RIVETS WHICH SECURE CHANNELS AND FORWARD CORNER HOLE IS CRACKED OUT. FABRICATED AND INSTALLED FLOOR BOARD SKIN REPAIR.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010526Intercostal · corrodedCENTER FLOOR SUPPORT INTERCOSTAL IS EXFOLIATED AT THE FORWARD END UPPER CAP, LOCATED AFT OF STATION 237 APPROXIMATELY 3 INCHES. (REF NRI 4956). FABRICATED AND INSTALLED FLOOR SUPPORT AND SPLICE SET.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010525Floorbeam · gougedFLOORBEAM DEEPLY GOUGED AT STATION 917, 4 INCHES RIGHT OF CENTER. FABRICATED AND INSTALLED REPAIR DOUBLERS AND BUMPER.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA010524Intercostal · damagedINTERCOSTAL AT STATION 380 LONGERON 27 RIGHT AND 29 RIGHT HAS ELONGATED HOLES AND DAMAGE. FABRICATED AND INSTALLED INTERCOSTAL AND OUTBOARD TEE CLIP.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010523Intercostal · damagedINTERCOSTAL AT STATION 400, LONGERON 27 RIGHT AND 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED OUTBOARD TEE CLIP AND INSTALLED INTERCOSTAL.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010522Intercostal · damagedINTERCOSTAL AT STATION 409, LONGERON 27 RIGHT, 29 RIGHT AHS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTERCOSTAL.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010521Intercostal · damagedINTERCOSTAL AT STATION 419 LONGERON 27 RIGHT & 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTERCOSTAL.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010520Longeron · corrodedLONGERON 5 RIGHT HAS 2 OPEN HOLES WITH MODERATE CORROSION AT STATION 948. REMOVED AND REPLACED LONGERON AND 3 SPLICE.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010519Stiffener · crackedSTIFFENER 9911840-129 FOUND CRACKED WHILE COMPLYING WITH NRI 5469. LOCATED AT BOTTOM OF STATION FRAME 1087 AND LEFT AFT VENTRAL STAIR JAMB.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010518Frame · corrodedFRAME 996 RIGHT SIDE ABOVE FLOOR FITTING HAS CORROSION. REMOVED AND REPLACED FRAME REPAIR.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Main, FrameSDR MWEA010517Frame · crackedCRACK INDICATION FOUND ON RADIO GRAPH WHILE PERFORMING PCI 9228 ON CAPTAINS WINDOW RETAINER FRAME. (INDICATION IS AT UPPER AFT CORNER APPROXIMATELY 2 INCHES LONG.) FABRICATED FILLER AND REMOVED AND REPLACED EXTERNAL DOUBLER.Apr 4, 2001 · N209ME · Doug DC932 · Flight Compartment WindowsSDR MWEA010516Door Frame · corrodedFORWARD CARGO DOOR JAMB LOWER WEB HAS AREAS OF LIGHT CORROSION AND BARE METAL STATION 362 TO 434. ALSO ONE MISSING NUT PLATE AT STATION 412. REMOVED AND REPLACED WEB.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010515Door Frame · corrodedFORWARD CARGO DOOR JAMB AT STATION 427 BETWEEN LONGERON 28 AND 29 RIGHT, ONE NUTPLATE AND ONE BN FASTENER HAVE CORROSION AROUND THEM ON INNER SURFACE. FABRICATED AND INSTALLED STACKED ANGLE REPAIRS.Apr 4, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010514Skin · gougedGOUGE ON INNER AFT CARGO DOOR SKIN JUST BELOW FORWARD HINGE FITTING. FABRICATED AND INSTALLED REPAIR DOUBLER.Apr 4, 2001 · N209ME · Doug DC932 · Cargo/Baggage Doors
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