Douglas DC-9-14

Service difficulty reports · 1,736

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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 MWEA95284Fairing · bentPILOT REPORTS ON WALK-AROUND IN ATLANTA, THE RIGHT OUTBD MOVEABLE VANE TRACK FAIRING WAS BENT UPWARD. MAINTENANCE IN ATL REMOVED FAIRING, AIRCRAFT WAS FERRIED TO MKE. NEW FAIRING WAS INSTALLED, A/C RETURNED TO SERVICE.Sep 5, 1995 · N800ME · Doug DC914 · Aerodynamic FairingsSDR MWEA 95296Eel Battery · dischargedDURING INSPECTION, THE EMERGENCY EXIT LIGHTS ABOVE RIGHT EMERGENCY EXIT AND THE COCKPIT EMERGENCY EXIT LIGHTS WERE VERY DIM DURING TEST. MAINTENANCE REPLACED BATTERIES IN FWD BATTERY PACK, OPS CHECK GOOD. RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Emergency LightingSDR 9513629161Door · damagedLANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED, RECYCLED GEAR WITH SAME RESULTS. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND FLIGHT RETURNED TO ATL, LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN INBOARD GEAR DOOR, RIGGED AND CYCLEDAug 31, 1995 · N8905E · Doug DC914 · Landing Gear DoorsSDR 9513119161Hyd Line · crackedON DESCENT INTO BHM, RIGHT HYDRAULIC SYSTEM PRESSURE BEGAN FLUCTUATING BETWEEN 1,500 AND 3,000 PSI AND QUANTITY WENT TO ZERO. PRECAUTIONARY COCKPIT OPERATING MANUAL PROCEDURES WERE ACCOMPLISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. DAMAGE TO LEFT MAIN GEAR DAug 26, 1995 · N8905E · Doug DC914 · Hydraulic System, MainSDR 9513269163Skin · crackedDURING H-CHECK, FOUND TWO CRACKS IN THE FUSELAGE SKIN AT THE MAIN CABIN DOOR CUTOUT FS 200 BETWEEN LONGERONS 12L - 14L. REPAIRED SKIN PER EA 91-102773.Aug 25, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9513259163Spar Web · crackedDURING H-CHECK, FOUND A CRACK IN THE RIGHT WING AFT SPAR WEB AT THE NR 2 STOP HINGE, LOWER INBOARD ATTACH STUD. REPAIRED PER EA 91-97631.Aug 25, 1995 · N8906E · Doug DC914 · Wing SparSDR 9513349163Skin · crackedDURING H-CHECK, FOUND FUSELAGE SKIN CRACKED AT FS 585, 623 AND 642 BETWEEN LONGERONS 1R AND 2R AT FASTENERS IN FRAME CLIP. FABRICATED AND INSTALLED DOUBLER PER EA 91-097634.Aug 24, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9513339163Bulkhead · corrodedDURING H-CHECK, FOUND AFT PIT FORWARD BULKHEAD LOWER CHORD CORRODED IN SEVERAL AREAS AT FS 642 BETWEEN LONGERONS 28L AND 28R. SPLICED IN NEW SECTION OF T-CHORD PER EA 91-097635.Aug 24, 1995 · N8906E · Doug DC914 · Fuselage Main, BulkheadSDR 9513329163Floorbeam · corrodedDURING H-CHECK, FOUND FLOORBEAM AT LEFT LAVATORY CORRODED AT FS 817. REPAIRED PER EA 91-102775.Aug 24, 1995 · N8906E · Doug DC914 · Fuselage Main, Floor BeamSDR 9513319163Skin · crackedDURING H-CHECK, FOUND FUSELAGE SKIN AT AFT SIDE OF FORWARD ENTRY DOOR CRACKED AT THIRD AND FOURTH DOOR STOPS. ACCOMPLISHED TEMPORARY REPAIR PER EA 91-102773.Aug 23, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9513039163Skin · crackedDURING H-CHECK, FOUND THREE SKIN CRACKS AT FS 585, FS 623 AND FS 642. REPAIRED PER EA 91-097634 SEC 1 AND SEC 2, PERMANENT REPAIR WILL BE ACCOMPLISHED IN ONE YEAR FROM 24 AUG 95.Aug 22, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9513029163Bulkhead · crackedDURING H-CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AROUND PERIMETER OF PLUG DOOR OPENING. STOP DRILLED CRACK AT LOWER LEFT RADIAL NR 16. REPAIRED RIGHT UPPER RADIAL PER SB 53-127.Aug 22, 1995 · N8906E · Doug DC914 · Fuselage Main, BulkheadSDR 9512969163Door Flange · crackedDURING H-CHECK, FOUND LEFT OVERWING EMERGENCY EXIT DOOR CRACKED AT AFT LOCKING PIN FLANGE. REPAIRED CRACK PER SRM 52-05 FIG 51 VIEW H. PERMANENT REPAIR WILL BE ACCOMPLISHED AT NEXT PERIODIC CHECK.Aug 19, 1995 · N8906E · Doug DC914 · Emergency ExitsSDR MWEA95270Evac Slide · fell offCREW REPORTS, FWD GALLEY DOOR EVACUATION SLIDE CAME OFF ITS MOUNT. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE.Aug 18, 1995 · N80ME · Doug DC914 · Emergency EquipmentSDR MWEA95267Bar Latch · dirtyCREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR LATCH SPRING IS BROKEN. MAINTENANCE FOUND SPRING OK, BUT LATCH WAS DIRTY. CLEANED AND LUBRICATED LATCH. OPS CHECK GOOD, RETURNED A/C TO SERVICE.Aug 18, 1995 · N600ME · Doug DC914 · Emergency EquipmentSDR MWEA95265Eel Power Supply · dischargedDURING SERVICE CHECK, WHEN BATTERY SWITCH SHUTOFF THE RIGHT AFT AND TAIL COMPARTMENT LIGHTS ILLUMINATE. MAINTENANCE REMOVED AND REPLACED AFT RT POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE.Aug 15, 1995 · N500ME · Doug DC914 · Emergency LightingSDR 9513649156Primary Trim · malfunctionedPRIMARY TRIM WOULD NOT OPERATE IN NOSE UP POSITION WITH YOKE SWITCHES, FUNCTIONED PROPERLY FROM SUITCASE HANDLES. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. OPERATIONAL CHECK WAS NORMAL ON GROUND. DISCREPANCY COULD NOT BE DUPLICATED, AIRCRAFT RETURAug 14, 1995 · N8915E · Doug DC914 · Stabilizer Control SystemSDR 9512289178Fence · separatedDTW-DSM - DURING DESCENT, THE LEFT WING LEADING EDGE FENCE SEPARATED FROM THE AIRCRAFT. NO ENGINE OR CONTROL DISCREPANCIES NOTED, LANDED DSM WITHOUT FURTHER INCIDENT. REPLACED AND RESEALED LEFT WING FENCE. INSPECTED NR 1 ENGINE AND LEFT WING TRAILING EDGE FAug 12, 1995 · N3310L · Doug DC914 · Wing Miscellaneous StructureSDR ABXA9500855Angle · dentedDURING C-CHECK INSPECTION, FOUND LEFT UPPER KEEL WEB ANGLE AT STRINGER 17 HAD A HI-LOCK THAT HAD DENTED THE ANGLE. REPAIRED IAW ABX REA D953-12409-MR.Aug 10, 1995 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95261Seat Track · wornDURING C-CHECK INSPECTION, THE CAPTAINS LEFT AND RIGHT AFT SEAT TRACKS WERE FOUND TO BE WORN AT THE LOCK PIN HOLES. MAINTENANCE INSTALLED STRAP REPAIR TO THE LEFT AND RIGHT SEAT TRACKS IAW SRM 53-05, FIG 28 AND RETURNED A/C TO SERVICE.Aug 9, 1995 · N500ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR 9512269160Clip · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. REPLACED AND ADJUSTED THE AFT CLIP, CHECKED OK.Aug 9, 1995 · N8903E · Doug DC914 · Aerodynamic FairingsSDR MWEA 95259Eel · inopDURING ROUTINE INSPECTION, THE EMERGENCY LIGHTING IN GALLEY WAS INOP. MAINTENANCE ADJUSTED LIGHT SOCKETS. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.Aug 8, 1995 · N400ME · Doug DC914 · Emergency LightingSDR ABXA9500854Door Jamb · misdrilledDURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR.Aug 8, 1995 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR ABXA9500853Door Jamb · misdrilledDURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR.Aug 8, 1995 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR ABXA9500852Door Frame · misdrilledDURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR.Aug 8, 1995 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR ABXA9500851Jamb · corrodedDURING C-CHECK INSPECTION, FOUND LOWER AFT CARGO DOOR JAMB CORRODED AT STA 718 TO 758. REPAIRED IAW ABX REA D953-12365-MR.Aug 8, 1995 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR ABXA9500846Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND RIGHT WING AFT SPAR LOWER CAP CORRODED AROUND NUTPLATES OUTBOARD OF AILERON. REPAIRED IAW ABX REA D957-12414-MR.Aug 8, 1995 · N925AX · Doug DC914 · Wing SparSDR ABXA9500843Bushing · wornDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND LEFT OUTBOARD GEAR DOOR BEARING ON FORK ASSEMBLY WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.Aug 8, 1995 · N925AX · Doug DC914 · Landing Gear Door Retract SectionSDR ABXA9500840Rod End · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT OUTBOARD GEAR DOOR FORWARD LONG ROD ASSEMBLY HAD A WORN EYEBOLT. REPLACED ROD END IAW DC-9 OHM 32-10-6.Aug 8, 1995 · N925AX · Doug DC914 · Landing Gear Door Retract SectionSDR ABXA9500850Skin · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON FUSELAGE SKIN FORWARD OF AFT BAG BIN. REPAIRED IAW ABX REA D953-12392-MR.Aug 7, 1995 · N925AX · Doug DC914 · Fuselage Main, Plate/SkinSDR ABXA9500848Blkhd Web · corrodedDURING C-CHECK INSPECTION, FOUND A GOUGE AND LEVEL I CORROSION IN TWO PLACES ON AFT PRESSURE BULKHEAD WEB FORWARD SIDE, BETWEEN FIVE-THIRTY AND SIX-THIRTY POSITIONS. REPAIRED IAW ABX REA D 953-12405-MR.Aug 7, 1995 · N925AX · Doug DC914 · Fuselage Main, BulkheadSDR ABXA9500849Fairing · corrosionDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ALONG THE PARAMETER OF THE LEFT AFT WING TO BODY FAIRING. REPAIRED IAW ABX REA D953-12379-MR.Aug 6, 1995 · N925AX · Doug DC914 · Aerodynamic FairingsSDR ABXA9500841Te Wedge · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 87-08-02, SB 55-23 REV 5, FOUND DEFECT IN RUDDER TRAILING EDGE PHENOLIC WEDGE DURING X-RAY INSPECTION. REPLACED PHENOLIC WEDGE IAW DC-9 SRM 51-30-2.Aug 3, 1995 · N925AX · Doug DC914 · Rudder StructureSDR ABXA9500847Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-8, FOUND LEFT UPPER PYLON ANGLE CRACKED ATSTA 860. REPAIRED IAW DC-9 SRM 54-04 FIG 10.Aug 2, 1995 · N925AX · Doug DC914 · Nacelle/Pylon StructureSDR 9512379160Skin · corrodedDURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 170 BETWEEN LONGERONS 28L - 28R. REPAIRED SKIN (P/N 5911401-1) PER EA 91-97109.Aug 2, 1995 · N8903E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9511849150Switch · failedTAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL AT 1.4 EPR. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED THE HORIZONTAL STABILIZER SWITCH (S1-141) AND FLAP SWITCH (S1-159). OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE.Aug 2, 1995 · N8908E · Doug DC914 · Central WarningSDR ABXA9500842Gear Door · bentDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND TRAILING EDGE OF LEFT OUTBOARD GEAR DOOR BENT. REPLACED SEAL IAW DC-9 SRM 51-30-2.Aug 1, 1995 · N925AX · Doug DC914 · Landing Gear DoorsSDR 9512349160Skin · crackedDURING H-CHECK, FOUND A ONE INCH CRACK IN THE FUSELAGE SKIN FS 490 AT LONGERON 29R. REPAIRED SKIN (P/N 5911418-1) PER EA 91-97105.Aug 1, 1995 · N8903E · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA95245Egt Bal Resistor · failedPILOT REPORTS ON CLIMBOUT FROM MKE, THE LEFT ENGINE EGT WENT DOWN TO 350 AND REMAINED FOR A SHORT TIME, THEN WENT DOWN TO 50 UNTIL RETURN TO MKE. ALL OTHER PARAMETERS NORMAL. MAINTENANCE INSPECTED LEFT ENGINE EGT SYSTEM, TESTED WITH BARFIELD EGT TEST BOX. RJul 31, 1995 · N600ME · Doug DC914 · Engine Temperature Indicating SystemSDR 9511519150Epr Ind · malfunctionedNR 1 ENGINE EPR INDICATION WAS BELOW NORMAL ON TAKEOFF, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER, CHECKED THE PT7 SYSTEM FOR LEAKS AND THE INDICATOR FOR ACCURACY. SYSTEM OPERATION WAS NORMAL ON RUNUP. Jul 30, 1995 · N8909E · Doug DC914 · Engine Pressure Ratio (EPR)SDR 9511509150Epr Ind · malfunctionedNR 1 ENGINE EPR INDICATION WENT TO ZERO ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR. THE SYSTEM CHECKED OK, AIRCRAFT RETURNED TO SERVICE.Jul 28, 1995 · N8909E · Doug DC914 · Engine Pressure Ratio (EPR)SDR 9511449152Oil Press Sw · malfunctionedTHE NR 2 ENGINE FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE DIFFERENTIAL SWITCH AND OIL FILTER. THE REMOVED OIL FILTER WAS INSPECTED FOR CONTAMINANTS, NJul 26, 1995 · N9811E · Doug DC914 · Engine Oil PressureSDR MWEA 95258Angle · crackedDURING ROUTINE INSPECTION, THE EXTERIOR ANGLE AT STA 867 FUSELAGE TO VERTICAL STABILIZER ATTACH POINT WAS FOUND CRACKED 1.5 IN LENGTH. MAINTENANCE FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-09 FIG 23. RETURNED A/C TO SERVICE.Jul 25, 1995 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR 9512759160Stop Fitting · crackedDURING H-CHECK, FOUND LEFT OVERWING EMERGENCY EXIT DOOR UNSERVICEABLE. SHOP FOUND CRACKED INNER PAN AT STOP NR 14, CRACK AT STOP FITTING NR 1, AND UPPER INBOARD CORNER BETWEEN BEAMS NR 2 AND NR 3 GOUGED. REPAIRED PER NWA EA 99-098720 AND SRM 52-05 AND 52-01, Jul 25, 1995 · N8903E · Doug DC914 · Emergency ExitsSDR 9512309160Blkhd Web · crackedDURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD WEB AT FS 817 AT THE 3 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED WEB PER EA 91-101064.Jul 25, 1995 · N8903E · Doug DC914 · Fuselage Main, BulkheadSDR 9511479160Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 642 LEFT INBOARD AND OUTBOARD KEEL FITTINGS. REPLACED FITTINGS PER SRM 51-30-1, 51-30-5.Jul 25, 1995 · N8903E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9511469160Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE FS 642 RIGHT INBOARD AND OUTBOARD KEEL FITTINGS. REPLACED FITTINGS PER SRM 51-30-1, 51-30-5.Jul 25, 1995 · N8903E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9511199151Shutoff Vlv · leakingDURING INITIAL CLIMB, EXPERIENCED RIGHT HYDRAULIC SYSTEM FLUID AND PRESSURE LOSS. FLIGHT RETURNED TO ORIGIN WITHOUT FURTHER INCIDENT. THERE WAS NO FURTHER LOSS WITH GEAR EXTENDED. FOUND RUDDER HYDRAULIC POWER SHUTOFF VALVE LEAKING FROM VALVE BODY. REPLACEDJul 23, 1995 · N8909E · Doug DC914 · Rudder Control SystemSDR MWEA95257Floorbeam · corrodedDURING ROUTINE INSPECTION, THE FLOORBEAM AT STA 200 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE INSTALLED NEW SECTION OF EXTRUSION IAW SRM 53-01 FIG 2 AND 4. RETURNED A/C TO SERVICE.Jul 21, 1995 · N80ME · Doug DC914 · Fuselage Main, Floor BeamSDR 9511969150Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON LEFT WING STR 11 AT XRS 78 TO 88 AND RIGHT WING STR 14, 15, 17, AND 18 FROM XRS 65 TO 109. REPAIRED ALL PER EA 91-100821.Jul 21, 1995 · N8908E · Doug DC914 · Wing, Longeron/Stringer
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