Douglas DC-9-15F

Service difficulty reports · 851

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 = 'DC915F'
  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 K11A2014120400002Bulkhead Web · crackedLEFT MAIN GEAR WHEEL WELL UPPER LT SKIN HAS A CRACK.Jul 27, 2014 · N915CK · Doug DC915F · Fuselage Main, BulkheadSDR K11A201492291501Skin · crackedLEFT MAIN GEAR WHEEL WELL UPPER LT SKIN HAS A CRACK.Jul 27, 2014 · N915CK · Doug DC915F · Fuselage Main, Plate/SkinSDR K11A2014060591501Indicator · inaccurateALTIMETER DISCREPANCY WITH ATC ENROUTE FLYING AT 29.92 AT 35,000, ATC SHOWED AIRCRAFT AT 35,300 FT. REPLACED AIU, PERFORMED OP'S CHECK, OP'S CHECKED GOOD. AIRCRAFT IS RVSM COMPLIANT.Jun 5, 2014 · N915CK · Doug DC915F · Altimeter, Barometric/EncoderSDR K11A2014042291701Latch · out of adjustAFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR. NO EMERGENCY PROCEDURES TAKEN, RETURNED DEPARTURE. ADJUSTED LANDING GEAR ANTI-RETRACTION LATCH RIG AND OP'S CHECKED GOOD IAW AMM 32-23-1. PERFORMED LANG GEAR SWING OP'S CHECKED GOOD IAW AMM 32-30-00.Apr 22, 2014 · N917CK · Doug DC915F · Landing Gear Retraction/Extension SystemSDR Y2PA20140303002Gauge · unserviceableCREW REPORTED, DURING CLIMB THROUGH ABOUT FL230, LEFT OIL TEMPERATURE GAUGE ROSE TO A READING BEYOND THE RED RADIAL. COM PROCEDURE FOLLOWED AND CALL FOR PRECAUTIONARY ENGINE SHUTDOWN. EMERGENCY DECLARED WITH ATC AND RETURN TO DEPARTURE INITIATED. AS POWER LMar 2, 2014 · N195US · Doug DC915F · Engine Oil TemperatureSDR Y2PA20140226001Socket · damagedLEFT DOWNLOCK GEAR INDICATOR, GREEN, STAYS ILLUMINATED AFTER GEAR RETRACTION. CREW REPORTED THAT AFTER GEAR HANDLE PLACED UP, LT MAIN GEAR GREEN LIGHT REMAINED ILLUMINATED. GEAR APPEARED TO HAVE RETRACTED, ABSENCE OF WIND NOISE AND NO YAWING MOMENT. CREW REFeb 25, 2014 · N196US · Doug DC915F · Landing Gear Position and WarningSDR K11A2014012291502Stringer · corrodedCORROSION ON STRINGER 23L BS 766 - 786.Jan 6, 2014 · N915CK · Doug DC915F · Fuselage Main, Longeron/StringerSDR K11A2014012291501Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 786, LBL 28.Jan 6, 2014 · N915CK · Doug DC915F · Fuselage Miscellaneous StructureSDR MJYA201310150017Cabin Pressure · malfunctionedCLIMBING THROUGH APPROXIMATELY 14,000 FEET OBSERVED NO AIRFLOW COMING FROM THE AIR VENTS, CHECKED THE CABIN ALTITUDE AND IT WAS 9,000 FT AND CLIMBING 1,000 FPM. BEFORE PROCEDURES, CABIN PRESSURE AND MASTER WARNING LIGHTS ILLUMINATED DURING DESCENT THROUGOct 12, 2013 · N783TW · Doug DC915F · Cabin Pressure Control SystemSDR MJYA201309120016Light · inoperativeEMERGENCY LIGHTS INOPERATIVE.Sep 6, 2013 · N783TW · Doug DC915F · Emergency LightingSDR MJYA201309120010Spar · crackedLT ELEVATOR SPAR FORWARD SPAR CRACKED BEYOND LIMITS.Sep 3, 2013 · N783TW · Doug DC915F · Elevator, Spar/RibSDR MJYA201309120014Structure · corrodedLEFT VERTICAL STAB HAS CORROSION.Sep 1, 2013 · N783TW · Doug DC915F · Vertical StabilizerSDR MJYA201309120015Floorboard · crackedMAIN DECK FLOORBOARD CRACKED SEVERAL PLACES.Aug 31, 2013 · N783TW · Doug DC915F · Fuselage Floor PanelSDR MJYA201309120012Skin · corrodedLT AFT SKIN CORRODED OUT OF LIMITS.Aug 31, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR MJYA201309120011Tee Fitting · corrodedCANTED BULKHEAD LOWER TEE CORRODED.Aug 31, 2013 · N783TW · Doug DC915F · Fuselage Main, BulkheadSDR K11A2014052791706Spar · corrodedCORROSION ON RT WING T/E FLAP REAR SPAR STA XRS 240.Aug 30, 2013 · N917CK · Doug DC915F · Trailing Edge FlapsSDR MJYA201309120013Skin · corrodedRT VERTICAL STABILIZER HAS CORROSION ON EXTERIOR SKIN.Aug 29, 2013 · N783TW · Doug DC915F · Vertical Stabilizer, Plate/SkinSDR MJYA201309120009Frame · corrodedCANTED FRAME AT BS 796 LT IS CORRODED OUT OF LIMITS.Aug 27, 2013 · N783TW · Doug DC915F · Fuselage Main, FrameSDR MJYA20130827008Frame · corrodedUPPER AND MID LT CANTED FRAME CORRODED AND FOUND TO BE OUT OF LIMITS AT BS 989.Aug 26, 2013 · N783TW · Doug DC915F · Fuselage Main, FrameSDR K11A2014052791705Spar · crackedRIGHT ELEVATOR CRACK INDICATION ON FRONT SPAR CHORD STA XE 109.Aug 19, 2013 · N917CK · Doug DC915F · Elevator, Spar/RibSDR K11A2014052791704Spar · crackedRIGHT ELEVATOR HAS A CRACK INDICATION ON THE FRONT SPAR CHORD STA XE 92.Aug 19, 2013 · N917CK · Doug DC915F · Elevator, Spar/RibSDR K11A2014052791703Frame · crackedFRAME STRUCTURE HAS TWO CRACKS AT STA 83 + 10 FROM CENTER VIEWED THROUGH LT WIPER MOTOR HOLE. ONE CRACK IN FLANGE RADIOUS ABOUT .5" & 1 CRACK AT FASTENERS 1 INCH LONG.Aug 15, 2013 · N917CK · Doug DC915F · Fuselage Main, FrameSDR K11A2014052791702Skin · corrodedRT ELEVATOR TOP SIDE INBD SKIN DAMAGED, STA XE 15.Aug 15, 2013 · N917CK · Doug DC915F · Elevator, Plate/SkinSDR K11A2014052791701Skin · corrodedEVIDENCE OF CORROSION ON UPPER OTBD END OF LT ELEVATOR, STA XE 209-233.Aug 14, 2013 · N917CK · Doug DC915F · Elevator, Plate/SkinSDR MJYA20130813007Structure · corrodedACFT LT SIDE REAR FUSELAGE, UN-PRESSURIZED AREA AFT OF VENT LOUVERS HAS CORROSION.Aug 12, 2013 · N783TW · Doug DC915F · Fuselage Main, StructureSDR MJYA20130813006Skin · crackedSKIN CRACKED AT BS 340 BETWEEN L17 - 18R.Aug 12, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR MJYA20130813005Skin · corrodedCORROSION ON OUTER SKIN AT BS 566 BELOW OVERWING EXITS.Aug 12, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR MJYA201308100002Window Frame · crackedRT NR 11 PASSENGER COMPARTMENT WINDOW CUTOUT HAS CRACK INDICATION LOWER AFT CORNER.Aug 7, 2013 · N783TW · Doug DC915F · Fuselage Main, StructureSDR MJYA201308100001Door Frame · crackedAFT PRESSURE BULKHEAD DOOR FRAME CRACKED APPROX 12 INCHES FROM BOTTOM FRAME.Aug 7, 2013 · N783TW · Doug DC915F · Fuselage Main, StructureSDR MJYA201308100003Bulkhead · corrodedAFT PRESSURE BULKHEAD EXTERNAL SIDE, SURFACE CORROSION FOUND UNDER ADHESIVE, 9 O`CLOCK POSITION APPROX 1.5' FROM DOOR FRAME LT BULKHEAD.Aug 6, 2013 · N783TW · Doug DC915F · Fuselage Main, BulkheadSDR MJYA201308090001Skin · crackedFUSELAGE SKIN CRACKED BS256 BETWEEN LONGERONS 4 & 5 LT.Aug 6, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR Y2PA20130508038Skin · damagedMX DISCOVERED .5" SKIN DAMAGE ON THE L1 DOOR CUT OUT UPPER EDGE OF FUSELAGE. MX REPAIRED IAW IAW DWG 53-13164-1 AND 8110-3.May 8, 2013 · N196US · Doug DC915F · Fuselage Main, Plate/SkinSDR Y2PA20130508037Structure · crackedMX DISCOVERED A 1" CRACK ON THE L1 DOOR TOP FLANGE 12" FWD OF AFT EDGE. FERRIED ACFT TO WHERE THEY REPAIRED THE DAMAGE IAW SRM 51-30-02 PGS, 1-4, 51-30-5 PGS, 1-22 AND 52-05, FIG 67.May 8, 2013 · N196US · Doug DC915F · Passenger/Crew DoorsSDR Y2PA20121001045Air Duct · crackedCREW REPORTED AFTER TAKEOFF UPON CLEANUP AND ACCELERATING IN CLIMB THEY NOTED A VIBRATION CHANGED THROTTLE SETTINGS/NO CHANGE. NO CONTROL ISSUES. CREW DECLARED AN EMERGENCY WITH APPROACH TO RETURN TO DEPARTURE. ACFT RETURNED TO POINT OF DEPARTURE AND LANDEDOct 1, 2012 · N196US · Doug DC915F · Air Distribution SystemSDR K11A2012091115001Csd · seizedIN CRUISE FLIGHT AUTOPILOT KICKED OFF AND SUBSEQUENTLY NOTICED A RIGHT GENERATOR OFF AND RIGHT CSD OIL PRESS LOW LIGHT ILLUMINATED ON THE OVERHEAD PANEL. PERFORMED CSD OIL LOW PRES CHECKLIST PER COM. INDICATION SHOWED VOLTS ON THE INDICATOR AND A HIGH TEMP RSep 9, 2012 · N915CK · Doug DC915F · Alternator-Generator DriveSDR 2012F00169Frame · gougedDURING INSPECTION, A DRILL GOUGE DAMAGE WAS FOUND IN STATION 585, FRAME.Aug 17, 2012 · N784TW · Doug DC915F · Fuselage Main, FrameSDR 2012F00168Frame · damagedDURING INSPECTION, RT STATION 817 FRAME WAS FOUND WITH DOUBLE-DRILLED HOLE FROM PREVIOUS INSTALLATION OF CARGO LINER.Aug 17, 2012 · N784TW · Doug DC915F · Fuselage Main, FrameSDR 2012F00167Skin · crackedDURING INSPECTION OF WINDOW BELT IAW AD 89-25-03, A 1" VERTICAL CRACK WAS DISCOVERED AT STA 447, ABOVE STRINGER L-15L.Aug 17, 2012 · N784TW · Doug DC915F · Fuselage Main, Plate/SkinSDR K11A2012071015001Structure · damagedDURING SERVICE CHECK FOUND DAMAGE TO MAIN DECK CARGO DOOR APPROX 9 INCHES FROM SILL AND 6 INCHES FORWARD FROM MANUAL AND UNLOCKING MECHANISM.Jul 10, 2012 · N915CK · Doug DC915F · Cargo/Baggage DoorsSDR Y2PA20120206004Lamp · inoperativeON PREFLIGHT MX, FOUND THE RT EXIT ROW GROUND EMERGENCY LIGHT INOPERATIVE. MX R & R THE RT EXIT ROW GROUND EMERGENCY LIGHT (LAMP) IAW THE INSTALLATION MANUAL, CHP. 33-21-27. THE SUBSEQUENT OPS CHECK WAS GOOD AND THE ACFT WAS RETURNED TO SERVICE.Feb 6, 2012 · N195US · Doug DC915F · Emergency LightingSDR K11A2012011391501Warning Light · inoperativeRIGHT LANDING GEAR (GREEN DOWN AND LOCK) LIGHT WILL NOT ILLUMINATE WHEN LEVER IS IN THE DOWN POSITION. CREW PERFORMED A GO-AROUND AND LANDED ON THE SECOND ATTEMPT. REPLACED LIGHT ASSY IAW SPWM 20-84-00, OPS CHECKED GOOD IAW DC9 AMM 32-60-1.Jan 13, 2012 · N915CK · Doug DC915F · Landing Gear Position and WarningSDR Y2PA2011112200028Probe · wrong partACFT STARTED WITH 13,500 LBS OF FUEL. AFTER 40-45 MINUTES OF FLIGHT FUEL QTY WAS 6,000 LBS. FUEL QTY CONTINUED TO DECREASE AT HIGHER RATE THAT FUEL BURN RATE. CAPTAIN DECLARED EMERGENCY. DIVERTED AND LANDED WITH FUEL INDICATING 3,050 LBS. DISCOVERED DURINNov 16, 2011 · N192US · Doug DC915F · Fuel Quantity SensorSDR MJYA20110831002Warning Light · illuminatedAFTER LANDING, GEAR "3 GREEN" WAS EXTENDED THE YELLOW DOOR OPEN LIGHT STAYED ILLUMINATED. FLIGHT CREW ACCOMPLISHED COM 32-17 "GEAR DOOR OPEN - MAIN GEAR EXTENDED" CHECKLIST. (INITIAL)Aug 31, 2011 · N784TW · Doug DC915F · Landing Gear Position and WarningSDR MJYA20110825001Wire · brokenRT MLG FAILED TO RETRACT. HYD QUANTITY AND PRESSURE NORMAL/GOOD. EMERGENCY DECLARED. LANDED IAW COM 32-17. FOUND WIRE BROKEN ON DOOR DOWN AND LOCK SWITCH. R & R SWITCH IAW AMM 32-60-01. RETRACTION CHECK OK IAW AMM 32-30-00. (FINAL)Aug 25, 2011 · N784TW · Doug DC915F · Landing Gear System WiringSDR K11A2011082491506Floorboard · corrodedFLOORBOARD CORROSION, 1X2 INCHES.Aug 2, 2011 · N915CK · Doug DC915F · Fuselage Floor PanelSDR K11A2011091504Keelbeam · crackedKEEL BEAM EVIDENCE OF 2 INCH CRACK.Jul 25, 2011 · N915CK · Doug DC915F · Fuselage Main, KeelSDR K11A20110991503Keelbeam · crackedKEEL BEAM EVIDENCE OF CRACK VERTICAL 3 INCHES.Jul 25, 2011 · N915CK · Doug DC915F · Fuselage Main, KeelSDR K11A2011082491505Cusp Web · corrodedCUSP WEB CORROSION, 2X6 INCHES.Jul 20, 2011 · N915CK · Doug DC915F · Fuselage Miscellaneous StructureSDR K11A2011082491504Cusp Web · corrodedCUSP WEB CORROSION, 2X6 INCHES.Jul 20, 2011 · N915CK · Doug DC915F · Fuselage Miscellaneous StructureSDR K11A2011082491503Seat Track · corrodedSEAT TRACK CORROSION, 2X6 INCHES.Jul 18, 2011 · N915CK · Doug DC915F · Fuselage, Seat/Cargo Attach Fittings
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