Douglas DC-9-14

Service difficulty reports · 1,736

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 = 'DC914'
  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 MWEA020495Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 18&19 ALSO EXTENDING UNDER STRINGER 18 FORWARD AND AFT. -- FABRICATED AND INSTALLED SHIM.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020483Stringer · damagedREPAIR CLIPS REQUIRED BETWEEN STRINGERS 15&14 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020484Stringer · damagedREPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGERS 14&13 ON THE INBOARD AND OUTBOARD SIDE OF XCW 58 WING.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020485Stringer · damagedREPAIR CLIP REQUIRED INSTALL BETWEEN STRINGERS 13&12 ON THE INBOARD AND OUTBOARD SIDES OF XCW 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA02505Stringer · damagedREQUESTING BOEING AGREEMENT OF FASTENER PLACEMENT IN UPPER PORTION OF REPAIR CLIPS BETWEEN STRINGER 14,15&16 THERE ARE TWO CLIPS AND TWO FASTENERS PER CLIP. -- BOEING APPROVES OF THE PLACEMENT OF THE FASTENERS.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA02504Stiffener · damaged1 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD BETWEEN RADIAL STIFFENER 18&20 LEFT. -- REAMED HOLES AND INSTALLED BUSHING.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, StructureSDR MWEA020503Stiffener · damaged2 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD RADIAL STIFFNERS 2&6 LEFT. -- REAMED HOLE UP AND INSTALLED 2 EACH BUSHINGS.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, StructureSDR MWEA020500Angle · crackedAFT PRESSURE BULKHEAD RIGHT HAND RADIAL #2 LOWER ANGLE THAT ATTACHES TO JAMB GUSSET HAS A CRACKED ATTACH HOLE. -- FABRICATED AND INSTALLED ANGLE.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA020499Doubler · crackedAFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT UPPER RIGHT CORNER HAS A CRACK EMANATING FROM CUTOUT HOLE TO THE DOOR JAMB EDGE DOT 30. -- FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED 8 FASTENERS.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA020492Doubler · crackedAFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT LOWER LEFT CORNER HAS A CRACK EMANATING FROM CUT OUT HOLE TO DOOR JAMB EGDE DOT 31. -- FABRICATED AND INSTALLED DOUBLER.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA020491Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 14&15 ALSO EXTENDING UNDER STRINGER 14&15 AND ONE SPOT ON VERTICAL LEG. -- FABRICATED AND INSTALLED SHIMAug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020482Clip · crackedREMOVED LEFT FUEL TANK SHEAR CLIP AT 69 BULKHEAD BETWEEN STRINGER 12 & 13. DRILLED UP CLIP AND INSTALLED FASTENERS.Aug 14, 2002 · N800ME · Doug DC914 · Wing Miscellaneous StructureSDR MWEA020510Seal · crackedLEFT AND RIGHT AFT PRESSURE BULKHEAD SEAL RETAINERS ARE CRACKED. -- DRILLED UP AND INSTALLED SEAL RETAINERS.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, StructureSDR MWEA020509Stringer · damagedREPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGER 17&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020508Stringer · damagedREPAIRED CLIPS REQUIRED INSTALL BETWEEN STRINGER 15&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020507Stringer · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020494Stringer Clip · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 21&22 RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.Aug 14, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020493Stiffener · crackedSTIFFENER AFT SIDE OF AFT PRESSURE BULKHEAD AT RADIAL 20 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED STIFFENER.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA020488Fitting · crackedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 13 AND 14, ALSO EXTENDING UNDER STRINGER 14 AND 13. ALSO FOUND CRACK ON OUTBOARD LEG. BLENDED OUT CRACK AND REMOVED CORROSION AROUND AND UNDER STRINGER.Aug 13, 2002 · N800ME · Doug DC914 · Wing Miscellaneous StructureSDR MWEA020487Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 12 AND 13 ALSO EXTENDING UNDER STRINGER 12 AND 13. -- FABRICATED SHIMS FOR STRINGER AND REMOVED CORROSION.Aug 13, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020478Angle · crackedANGLE AT RADIAL 6 LEFT IS CRACKED. -- DRILLED UP ANGLE AND INSTALLED ANGLE.Aug 13, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA020486Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 11 AND 12 ALSO EXTENDING UNDER STRINGER 11. -- REMOVED CORRORION.Aug 13, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020480Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGERS 16 AND 17 ALSO EXTENDING UNDER STRINGERS 16 AND 17.Aug 13, 2002 · N800ME · Doug DC914 · Wing, Attach FittingsSDR MWEA020476Bracket · damagedSUPPORT BRACKET 5910163-191 LOCATED ON LEFT SIDE OF APB AT RADIAL 6 INBOARD END DAMAGED. -- LOCATED AND DRILLED INBOARD AND OUTBOARD END OF NEW 191 AND REMOVED AND INSTALLED BRACKET.Aug 13, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA020468Fastener · crackedSKIN CRACK INDICATION NOTED STATION 180 JUST RIGHT OF LONGERON ONE. -- REMOVED AND INSTALLED FASTENERS INTO FORMERS.Jul 30, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA020465Fitting · oversizedFORWARD CARGO DOOR FITTINGS HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED FITTINGS.Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA020464Angle · oversizedFORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND REPLACED ANGLE.Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA020470Doubler · crackedPER PCI 9274 FOUND SMALL SKIN CRACK INTO DOOR STOP ADJUST HOLE ON AFT SIDE OF DOOR 3RD HOLE FROM THE TOP (MARKED). -- FABRICATED AND INSTALLED DOUBLER.Jul 30, 2002 · N800ME · Doug DC914 · Fuselage Main, FrameSDR MWEA020469Finger Doubler · crackedSKIN CRACKED INDICATION NOTED STATION 525 JUST RIGHT OF LONGERON ONE (MARKED). -- FABRICATED AND INSTALLED SKIN PLUG AND FINGER DOUBLER.Jul 30, 2002 · N800ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA020467Angle · oversizedFORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED ANGLE.Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA020466Doubler · crackedFORWARD CARGO DOOR #2 OUTBOARD UPPER ATTACH HOLE IS CRACKED. -- FABRICATED AND INSTALLED DOUBLER.Jul 30, 2002 · N800ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA020456Intercostal · crackedINTERCOSTAL IS CRACKED AROUND FASTENER HOLES FORWARD CARGO DOOR BELOW #1 BEAM FORWARD END OF DOOR (DOT JH 23). -- REMOVED AND INSTALLED INTERCOSTAL.Jul 23, 2002 · N800ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA020455Clip · gougedSHOVEL CLIP JUST AFT OF APB LEFT 17 LONGERON IS GOUGED. -- REPAIRED GOUGE AND INSTALLED SHOVEL CLIP.Jul 23, 2002 · N800ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA020454Clip · crackedAPB RADIAL NR 16 LEFT END CLIP HAS A CRACK AROUND END FASTENER HOLE. FABRICATED AND INSTALLED CLIP.Jul 23, 2002 · N800ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA020451Splice Plate · crackedAFT PRESSURE BULKHEAD PLUG DOOR JAMB HAS A CRACK AT APPROXIMATELY THE 6 O'CLOCK POSITION IN THE SPLICE PLATE CONNECTION. REMOVED AND INSTALLED SPLICE PLATE.Jul 18, 2002 · N800ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA020447Oil SystemON DEPARTURE OUT OF MILWUAKEE RIGHT ENGINE OIL QTY INDICATION DECREASED TO ZERO. -- DEFERRED RIGHT ENGINE OIL QTY PER MEL 79-3Jul 13, 2002 · N500ME · Doug DC914 · Engine Oil QuantitySDR 0202349150Pump · malfunctionedWHILE IN CRUISE FLIGHT WITH THE ENGINE DRIVEN HYDRAULIC PUMPS IN LOW, THE RIGHT HYDRAULIC SYSTEM WENT TO ZERO PRESSURE FOR 3-5 SECONDS THEN RETURNED TO NORMAL 1500 PSI. THIS OCCURRED TWICE AND THE RIGHT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS Jul 8, 2002 · N8908E · Doug DC914 · Hydraulic Pump (Electric/Engine), MainSDR 0202359140Duct · disconnectedAT 14,000 FEET, THE CABIN PRESSURE ANNUNCIATOR ILLUMINATED. CABIN ALTITUDE WAS 10,000 FEET. VERY SOON AFTER THE WARNING LIGHT CAME ON AND CABIN WENT TO 15,000 FEET AND MASKS DEPLOYED. COMPLIED WITH COM PROCEDURES AND PRESSURE CONTROLLER WAS FULL FORWARD. FLIGHJun 24, 2002 · N930RC · Doug DC914 · Cabin Cooling SystemSDR 0201579150Indicator · malfunctionedRIGHT HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. RIGHT HYDRAULIC QUANTITY WENT TO 10 QUARTS FROM 7-8 THAT WAS SHOWING AT TAKEOFF. COMPLIED WITH COM AND LANDED AT MSP WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED TO THE GATE FROM THE TAXIWAY. MAINTENANCE TESTED THEMay 13, 2002 · N8908E · Doug DC914 · Hydraulic Pressure IndicatorSDR MWEA020321Oven · shortedF/A REPORTED SEEING AN ORANGE FLASH ABOVE AND BEHIND GALLEY OVEN. -- NWA MTC INSPECTED LEFT AND RIGHT OVENS. FOUND OVEN GROUND WIRE SHORTED. PULLED AND COLLARD LEFT AND RIGHT OVEN CIRCUIT BREAKERS. DEFERRED OVENS PER MEL 25-12. REMOVED AND REPLACED OVENS DMIMay 5, 2002 · N500ME · Doug DC914 · Equipment/Furnishings WiringSDR MWEA020290Arm · failedPASSENGER DOOR HAS STRUCTURAL DAMAGE (CRACK) TO INTERCOSTAL LOCATED WHERE CRANK ARM PASSES THROUGH. DAMAGED CAUSED BY CRANK ARM FAILURE. REMOVED AND REPLACED INTERCOSTAL.Apr 25, 2002 · N700ME · Doug DC914 · Passenger/Crew DoorsSDR MWEA020292Beam · elongatedREMOVED DAMAGED INTERCOSTAL AND SUPPORT AND FOUND PAX DOOR BEAM #5 TO HAVE AN ELONGATED HOLE. -- FABRICATED AND INSTALLED REPAIR DOUBLER.Apr 25, 2002 · N700ME · Doug DC914 · Passenger/Crew DoorsSDR MWEA020291Support · elongatedINTERCOSTAL SUPPORT WAS REMOVED TO FACILITATE OTHER MAINTENANCE AND WAS FOUND TO HAVE ELONGATED HOLES AFTER REMOVAL. -- REPLACED WITH NEW SUPPORT.Apr 25, 2002 · N700ME · Doug DC914 · Passenger/Crew DoorsSDR 0201189152Insulation · out of positionJUST PRIOR TO THE FLIGHT LEVELING OFF AT FL290, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN ALTITUDE WAS 10,500 FEET WITH THE DIFFERENTIAL AT 5 PSI. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND RETURNED TO DTW. NO MENTION OF COM COMPLIANCEApr 18, 2002 · N8911E · Doug DC914 · Passenger Compartment EquipmentSDR 0201309151Door · crackedDuring shop visit in ATL, the 2 aft cargo door assy webs were found cracked at aft end. Repaired per EA 99-189648.Apr 11, 2002 · N8909E · Doug DC914 · Cargo/Baggage DoorsSDR MWEA020207Stiffener · elongatedVERTICAL STIFFENER IN FORWARD ELECTONIC POWER CENTER HAS ELONGATED HOLES. -- REPAIRED VERTICAL STIFFENER IAW SRM 53-01 FIGURE SHEET 4.Apr 2, 2002 · N500ME · Doug DC914 · Fuselage Main, StructureSDR ABXA010776Stiffener · crackedOUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM.Mar 4, 2002 · N925AX · Doug DC914 · Wing Miscellaneous StructureSDR MWEA020158Stiffener · crackedLEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER.Mar 2, 2002 · N700ME · Doug DC914 · Nacelle/Pylon, Attach FittingsSDR ABXA010775Skin · crackedRIGHT MAIN LANDING GEAR DOOR INNER SKIN CRACKED JUST AFT OF THE FORWARD HINGE FITTING. REPAIRED CRACKED AREA IAW DC-9 SRM 52-01.Feb 28, 2002 · N925AX · Doug DC914 · Landing Gear DoorsSDR ABXA010774Frame · crackedAUXILIARY SUPPORT FRAME CRACKED IN AFT ACCESSORY COMPARTMENT FLOOR SUPPORT, FORWARD OF MAIN FRAME AT STATION 908. REPLACED FRAME IAW DC-9 SRM DWG 505159 AND DC-9 SRM 51-30-2.Feb 27, 2002 · N925AX · Doug DC914 · Fuselage Main, Frame
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