Douglas DC-9-31

Service difficulty reports · 7,433

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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 = 'DC931'
  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 USAA000835Frame · crackedPIT - FOUND FRAME CRACKED 3 INCHES, STATION 1019, LONGERON 14. INSTALLED DOUBLER PER EA 55290. (M)Jun 3, 2000 · N934VJ · Doug DC931 · Fuselage Main, FrameSDR USA000834Skin · crackedPIT - FOUND TWO CRACKS .25 INCH AND .125 INCH, AT RIVET STATION 76.5 AT LONGERON 2L. INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND EA 55293. (M)Jun 3, 2000 · N934VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAAD00087Battery · dischargedIND - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE EMERGENCY LIGHT BATTERY. (M)May 31, 2000 · N925VJ · Doug DC931 · Emergency LightingSDR TWAA0008504Frame · crackedDURING CHECK-C, FOUND BELTING FRAME ABOVE STATION 408 CRACKED AT LONGERON 17 RT (TWO .375 INCH CRACKS). CUT OUT BELT RING AND REPAIRED PER SRM 5-3-03 FIG 32 AND ELMR 70752. CHECK-C 05-27-00 STL.May 27, 2000 · N982PS · Doug DC931 · Fuselage Main, FrameSDR TWAA0008503Skin · gougedDURING OP-9, FOUND RT ELEVATOR GOUGED APPROXIMATELY .125 INCH DEEP AND .25 INCH LONG ON THE UPPER SURFACE APPROXIMATELY 51 INCHES O/B FROM THE CENTERLINE. MADE A DOUBLER REPAIR PER DC9 SRM 55-01 FIG 2. BALANCED CALCULATED METHOD PER DC9 SRM 55-20-1. NEW BALMay 27, 2000 · N982PS · Doug DC931 · Elevator, Plate/SkinSDR TWAA0008502Frame · crackedDURING CHECK-C, FOUND BELT RING FRAME STATION 389 CRACKED AT LONGERON 17R .375 INCH CRACK. CUT OUT BELT RING AND REPAIRED PER SRM 53-03-FIG 32 AND ELMR 70752. CHECK-C 05-27-00 STL.May 27, 2000 · N982PS · Doug DC931 · Fuselage Main, FrameSDR USAAD00085Battery · dischargedDTW - THE FRONT SECTION OF THE OVERHEAD EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE FRONT SECTION OF THE OVERHEAD EMERGENCY LIGHTS. (M)May 26, 2000 · N965VJ · Doug DC931 · Emergency LightingSDR ABXA000286Angle · crackedDURING C-CHECK, FOUND THE LEFT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLEIAW DC9 SRM 51-30-2.May 26, 2000 · N947AX · Doug DC931 · Trailing Edge FlapsSDR ABXA000285Angle · crackedDURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2.May 26, 2000 · N947AX · Doug DC931 · Trailing Edge FlapsSDR ABXA000284Fitting · corrodedDURING C-CHECK, FOUND HORIZONTAL CENTER SECTION HINGE BORE CORRODED. REPAIRED IAW ABX REA D955-37167MR.May 26, 2000 · N947AX · Doug DC931 · Horizontal Stabilizer, Attach FittingsSDR ABXA000282Hinge Fitting · corrodedDURING C-CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION HINGE BORE CORRODED. REPAIRED IAW ABX REA D955-37167MR.May 26, 2000 · N947AX · Doug DC931 · Horizontal Stabilizer, Attach FittingsSDR ABXA000281Angle · crackedDURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE, OUTBOARD SUPPORT ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.May 26, 2000 · N947AX · Doug DC931 · Trailing Edge FlapsSDR ABXA000280Skin · crackedDURING C-CHECK, FOUND THE VERTICAL STABILIZER SKIN CRACKED UNDER PANEL NR 3804. REPLACED SKIN IAW DC9 SRM 51-30-1.May 26, 2000 · N947AX · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR ABXA000279Skin · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER SKIN CRACKED AT PANEL NR 3703. REPLACED SKIN IAW DC9 SRM 51-30-1.May 26, 2000 · N947AX · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR GTIA000206Light · inoperativeMYR - FLT 541 - EMERGENCY FLOOR PATH LIGHTING IN FRONT OF AIRCRAFT IS NOT WORKING. FOUND BROKEN WIRE. REPAIRED BROKEN WIRE AND OPS CHECK GOOD IAW 33-53-01. (M)May 25, 2000 · N928ML · Doug DC931 · Emergency LightingSDR ABXA000292Skin · delaminatedDURING C-CHECK, FOUND RUDDER TAB DELAMINATED. REPLACED RUDDER TAB IAW DC9 SRM 27-20-02.May 24, 2000 · N946AX · Doug DC931 · Rudder, Tab StructureSDR ABXA000291Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED, RIGHT SIDE FUSELAGE STATION 617. REPLACED CUSP WEB IAW DC9 SRM 51-30-1.May 24, 2000 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0008713Floorbeam · corrodedDURING CHECK-C MAINT IN AFT CABIN AT STA 965 JUST UNDER I/B RIGHT LAV WALL AT LOWER SIDE OF FLOORBEAM, FOUND SUPPORT STRAP CORRODED. INSTALLED NEW SECTION OF 9912243-52 CHORD PER ARA 16725.May 24, 2000 · N978Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0008712Floorbeam · corrodedDURING CHECK-C MAINT IN AFT CABIN AT LOWER FWD SIDE OF CABIN FLOORBEAM, STA 965 RBL 32 IN, HAD HEAVY CORROSION. INSTALLED DOUBLER AND STRAPS PER ARA 16725.May 24, 2000 · N978Z · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA000283Wire · brokenON GEAR EXTENSION AT LBB, RIGHT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. RECYCLED GEAR AND PERFORMED ABNORMAL PROCEDURES. LANDING WITHOUT INCIDENT. REPAIRED BROKEN WIRE NR 2G205C20 AT CANNON PLUG FOR RIGHT GEAR DOWN LIMIT SWITCH. OPS CHECKED GOOD.May 24, 2000 · N929AX · Doug DC931 · Landing Gear System WiringSDR USAAD00081Battery · dischargedIND - THE EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT ON THE SERVICE DOOR WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)May 23, 2000 · N967VJ · Doug DC931 · Emergency LightingSDR TWAA0008711Skin · crackedAT CHECK-C MAINT CHECK, FOUND APPROX 2 INCH CRACK IN OUTER SKIN AT STA 108, BETWEEN LONGERON 27L AND 28L. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6. CRACK WAS CONTAINED AT DRAIN HOLE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01May 23, 2000 · N978Z · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA000278Bulkhead · crackedDURING C-CHECK, FOUND SUPPORT ANGLE AFT SIDE OF STATION 37 BULKHEAD CRACKED IN 2 PLACES. REPLACED ANGLE IAW DC9 SRM 51-30-2.May 23, 2000 · N947AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA000277Angle · crackedDURING C-CHECK, FOUND THE OUTBOARD FLAP HINGE AFT FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.May 23, 2000 · N947AX · Doug DC931 · Trailing Edge FlapsSDR ABXA000276Attach Fitting · corrodedDURING C-CHECK, FOUND THE HORIZONTAL STABILIZER CENTER SECTION CENTER HINGE BOLT FITTING CORRODED INSIDE THE LEFT HINGE BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-30-1.May 23, 2000 · N947AX · Doug DC931 · Horizontal Stabilizer, Attach FittingsSDR USAAD00080Battery · dischargedDAY - THE AFT FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY LIGHT BATTERIES. (M)May 22, 2000 · N927VJ · Doug DC931 · Emergency LightingSDR GTIA000205Light · inoperativeDTW - FOUND 2 EMERGENCY LIGHTS WORKING ON FORWARD PART OF TRACK LIGHTING. REPAIRED WIRING AT FORWARD FLOOR TRACK AREA. SYSTEM OPS CHECKS GOOD IAW DC-9 MM 33-53-0. (M)May 21, 2000 · N928ML · Doug DC931 · Emergency LightingSDR ABXA000289Fitting · crackedDURING C-CHECK, FOUND AFT LOWER CARGO DOOR BEAM NR 2 AFT END FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.May 18, 2000 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000288Fitting · crackedDURING C-CHECK, FOUND AFT LOWER CARGO DOOR BEAM NR 4 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.May 18, 2000 · N946AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA000287Fitting · crackedDURING C-CHECK, FOUND AFT LOWER CARGO DOOR BEAM END FITTING CRACKED. REPLACED DOOR FITTING IAW DC9 SRM 51-30-5.May 18, 2000 · N946AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA000290Skin · crackedDURING C-CHECK, FOUND RIGHT SIDE VERTICAL STABILIZER CRACKED ABOVE TOP OF RUDDER, 4 INCHES LONG. REPAIRED IAW DC9 SRM 55-01.May 17, 2000 · N946AX · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR USAAD00076Warning System · activatedBHM/CLT - FLT 940 - DURING CRUISE AT 29,000 FEET, THE MASTER CAUTION LIGHT AND THE CABIN ALERT LIGHTS ILLUMINATED. DURING DESCENT TO A LOWER ALTITUDE, THE CABIN OXYGEN MASKS DEPLOYED AND AN EMERGENCY DESCENT WAS INITIATED. THE AIRCRAFT LANDED AT ITS DESTINATIMay 17, 2000 · N983VJ · Doug DC931 · Cabin Pressure Control SystemSDR TWAA0008309Airstair · bentDURING CC, FOUND IN THE AREA OF THE AFT STAIRS, FWD LOWER EDGE OF THE AIRSTAIR BENT AND HAS 2 CRACKS. LONGEST IS APPROXIMATELY ONE INCH. PERFORMED EDDY CURRENT FOR CRACK CONTAINMENT. STOP DRILLED AND INSTALLED AN EXTERNAL DOUBLER AS PER THE SRM 52-01 FIG 2.May 17, 2000 · N978Z · Doug DC931 · Entrance StairsSDR TWAA0008308Skin · crackedDURING CC, FOUND RT PYLON, UPPER SKIN CRACKED AT THE TOP OF THE PYLON ON THE WEDGE APPROXIMATELY 11 INCHES FROM THE FIXED COWL AFT EDGE, OUTBOARD EDGE OF THE SKIN. STOP DRILLED CRACKS, MADE DOUBLER SAME GUAGE THICKNESS AS SKIN AND INSTALLED WITH .125 INCH MS2May 17, 2000 · N978Z · Doug DC931 · Nacelle/Pylon, Plate/SkinSDR 0001839906Controller · failedBOTH AUTO AND MANUAL PRESSURIZATION FAILED TO OPERATE NORMALLY AT ALTITUDE. CABIN CLIMBED TO 15,000 FEET AND MASKS DEPLOYED. AN EMERGENCY DESCENT WAS INITIATED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER, REPACKED AIRSMay 17, 2000 · N956N · Doug DC931 · Cabin Pressure ControllerSDR USAAD00074Flashlight · failedPHL - THE PORTABLE RECHARGEABLE EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT. (X)May 16, 2000 · N966VJ · Doug DC931 · Emergency EquipmentSDR USAA000733Pan · crackedPIT - C-5 - PAN HAD LONG CRACK, 0.250 INCH, DOOR PAN AT CENTER AFT STOP. INSTALLED DOUBLER PER DC-9 SRM 52-15, FIG 51. (X)May 16, 2000 · N913VJ · Doug DC931 · Passenger/Crew DoorsSDR USAAD00071Light · inoperativeDTW - THE EMERGENCY EXIT LIGHT AT THE FORWARD FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE EMERGENCY LIGHT. (X)May 13, 2000 · N934VJ · Doug DC931 · Emergency LightingSDR USAAD00070Light · inoperativeDTW - THE AFT OVERHEAD SECTION OF EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE EMERGENCY LIGHTS. (X)May 12, 2000 · N970VJ · Doug DC931 · Emergency LightingSDR 0001779949Outflow Valve · failedAUTOMATIC CABIN PRESSURE CONTROL FAILED EN ROUTE PIT. FLIGHT DESCENDED TO 10,000 FEET AND PROCEEDED TO DESTINATION. MAINTENANCE REPLACED THE OUTFLOW VALVE, THERMOSTAT, AND ANTICIPATOR AS A PRECAUTION. NO FAULTS NOTED ON BITE TEST OF PRESSURE CONTROLLER. AIMay 12, 2000 · N8928E · Doug DC931 · Pressure Regulator/Outflow ValveSDR USAAD00073Slide · dischargedDAY - THERE WAS NO PRESSURE IN THE TAILCONE EMERGENCY EVACUATION SLIDE ASSEMBLY. MAINTENANCE REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)May 11, 2000 · N970VJ · Doug DC931 · Escape SlideSDR TWAA0007708Angle · misrepairedDURING OP 16 MAINT CHECK AT STA 996, THE CUSP ANGLE WAS GROUND BEYOND LIMITS ON LT SIDE. REPLACED DAMAGED CUSP ANGLE PER SRM 53-11-3, FIG 11 PAGE 22D, AND SRM 51-10 FIG 33 SHEET 11. REINSTALLED RIVETS PER SRM 51-30-2.May 11, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0007707Finger Doubler · crackedDURING OP 16 MAINT CHECK, FOUND 2 FINGER DOUBLERS CRACKED AT STA 983, ABOVE LONGERON 18L, 53 INCHES LBL, IN LT AFT LAV AREA. REPLACED FINGER DOUBLER WITH PART NUMBER S2912900-5-5000 DOUBLER. REINSTALLED RIVETS IN FINGER DOUBLER PER SRM 51-30-2.May 11, 2000 · N984Z · Doug DC931 · Fuselage Main, StructureSDR TWAA0007603Longeron · crackedDURING CHECK-C, MAINT FOUND LONGERON 5R AT STA 699, WAS CRACKED. INSTALLED NEW SECTION PER SRM 53-02, FIG 18.May 11, 2000 · N978Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR GTIA000196Light · misinstalledDTW - FOUND EMERGENCY FLOOR TRACK LIGHTING STRIP AT 1 EF IS HELD DOWN BY CARGO PIT TAPE. RESECURED TRACK IAW 33-50-00, NO DEFECTS NOTED. (M)May 10, 2000 · N934ML · Doug DC931 · Emergency LightingSDR USAAD00069Battery · dischargedIND - THE LEFT AND RIGHT EMERGENCY NACELLE LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)May 10, 2000 · N970VJ · Doug DC931 · Emergency LightingSDR 0001909966Bulkhead · crackedAPB CRACKS FOUND ON UPPER DOOR JAMB LEFT AND RIGHT SIDES. CUT OUT DAMAGE AND REPAIRED PER EA 99-172388, LOG PAGES 1437697, 1437694, 1437690.May 10, 2000 · N9330 · Doug DC931 · Fuselage Main, BulkheadSDR 0001899994Door Frame · crackedFWD CARGO DOOR JAMB UPPER CORNER CRACKED OUT FASTENER HOLE AS MARKED. REPAIRED PER EM 5330-01130-2B AND EA 99-176486.May 10, 2000 · N8979E · Doug DC931 · Fuselage Main, StructureSDR TWAA0007706Floorboard · corrodedDURING OP 16 MAINT CHECK, FOUND NUMBER 13 FLOOR PANEL WITH CORROSION ON BOTH SIDES OF PANEL SKIN. FABRICATED NEW PART PER SSRM 53-00-104 PAGE 102, SRM 51-10-3, PAGE 1 TO 12, AND SPM 6-70-01 PAGE 2.May 10, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0007506Skin · damagedDURING OP 16 MAINT CHECK, THE TAIL CONE MATING FRAME AND EXTERIOR SKIN HAD HOLE WORN THROUGH ON RT SIDE AT DRAIN CHANNEL, APPROXIMATELY 5 O''CLOCK POSITION. REPAIRED FRAME AND SKIN BY INSTALLING DOUBLERS PER SRM 53-01, PAGE 10, AND SRM 53-01 PAGE 18.May 8, 2000 · N984Z · Doug DC931 · Aerodynamic Fairings
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