Douglas DC9-15
Service difficulty reports · 926
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 = 'DC915' 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.
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 = 'DC915' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MWEA95354Frame · corrodedDURING CORROSION TASK INSPECTION OF AFT CARGO BAY, FOUND LIGHT CORROSION TO AFT FACE OF FRAME BETWEEN LONGERON 39R AND 29L, STA 786. MAINTENANCE INSTALLED REPAIR DOUBLER IAW SRM 53-03, AIRCRAFT RETURNED TO SERVICE.SDR MWEA95353Skin · chafedDURING CORROSION TASK INSPECTION OF VERTICAL STABILIZER, FOUND THE LEFT HAND FORWARD SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. MAINTENANCE REMOVED AND REPLACED SKIN IAW 55-01 PG 1, AIRCRAFT RETURNED TO SERVICE.SDR 9515389102Release Mech · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ADJUSTED AND LUBRICATED THE RELEASE MECHANISM, CHECKED OK.SDR 9514459104Fuel Sys · ventingAFTER TAKEOFF, FUEL BEGAN VENTING FROM LEFT WING. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PERFORMED BOOST PUMP CHECK VALVE BACKFLUSH PROCEDURE PER MM 28-20-0. FUEL TRANSFER CHECK WAS OK AND AIRCRAFT RETURNED TO SERVICE.SDR 9514769105Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR GRAA9542Clamp · looseON CLIMB-OUT FROM ENV, AIRCRAFT WOULD NOT HOLD PRESSURIZATION IN AUTO OR MANUAL. AIRCRAFT RETURNED TO ENV WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED A CLAMP HAD COME LOOSE ON THE WATER SEPARATOR CANNISTOR. MAINTENANCE RESECURED THE CLAMP AND PERFORMEDSDR 9514849104Angle · crackedDURING B-CHECK, FOUND A CRACK IN THE DORSAL FIN ATTACH ANGLE AT LONGERON 2L. REPAIRED ANGLE (P/N 5939711-1), PER EA 91-99249.SDR GRAA9544Current Limiter · failedAFTER TAKEOFF, MADE A CLIMBING RIGHT TURN THROUGH 2000 FEET MSC. THE AIRCRAFTS LEFT GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED THE LEFT GENERATOR POWER RELAY, PERFORMED OPERATIONAL CHECK ON THE AC CROSS-TIE SYSTEM, OPERATIONALLY CLEARED NORMAL. MAINSDR 95ZZZM633Seat Track · corrodedSTL - DURING OP-9, FOUND CORROSION IN NR 2 GALLEY RIGHT CABIN OUTBOARD SEAT TRACK MOUNT AREA, STATION 237. INSTALLED NEW SEAT TRACK PER SRM 53-05, FIGURE 4. (M)SDR GRAA9543Gen Contl Unit · malfunctionedSTS - UPON DESCENT, LT GENERATOR FEEDER FAULT, LT GENERATOR OFF, AND AC CROSS-TIE LOCKOUT ANNUNCIATOR LIGHTS ILLUMINATED. LOST LT SIDE ELECTRONICS. AIRCRAFT DIVERTED TO RNO. MAINTENANCE REPLACED LT GENERATOR CONTROL PANEL, LT BUSS PROTECTION PANEL, AND LT GSDR 95ZZZX6100Buss Prot Pnl · malfunctionedSTS - UPON DESCENT, LT GENERATOR FEEDER FAULT, LT GENERATOR OFF, AND AC CROSS-TIE LOCKOUT ANNUNCIATOR LIGHTS ILLUMINATED. LOST LT SIDE ELECTRONICS. AIRCRAFT DIVERTED TO RNO. MAINTENANCE REPLACED LT GENERATOR CONTROL PANEL, LT BUSS PROTECTION PANEL, AND LT GSDR 95ZZZX6099Power Relay · malfunctionedSTS - UPON DESCENT, LT GENERATOR FEEDER FAULT, LT GENERATOR OFF, AND AC CROSS-TIE LOCKOUT ANNUNCIATOR LIGHTS ILLUMINATED. LOST LT SIDE ELECTRONICS. AIRCRAFT DIVERTED TO RNO. MAINTENANCE REPLACED LT GENERATOR CONTROL PANEL, LT BUSS PROTECTION PANEL, AND LT GSDR 9514099102Transfer Relay · malfunctionedAFTER TAKEOFF, BOTH A AND B PHASE FUEL BOOST PUMP CIRCUIT BREAKERS POPPED, IN CONJUNCTION WITH LOSS OF SEVERAL AIRCRAFT COMPONENTS INCLUDING COMMUNICATIONS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED DC CROSSTIE RELAY (R2-27) AND NR 1 AND NSDR 95ZZZX5145Switch · malfunctionedSTL - FLT 582 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR AND DOOR LIGHT WAS SLOW TO EXTINGUISH. FOUND DEFECTIVE RIGHT MAIN LANDING GEAR DOOR SWITCH, MFG H14-6. REPLACED RIGHT MAIN LANDSDR MWEA95282Switch Washer · loosePILOT REPORTS, ON CLIMBOUT THE RIGHT GEAR RED UNSAFE LIGHT WOULD NOT EXTINGUISH, PERFORMED QRH PROCEDURES, RETURNED TO MKE. MAINTENANCE FOUND RIGHT UPLATCH SWITCH STRIKER WASHER LOOSE, STRIKER HAD JUMPED WASHER. SECURED WASHER, OPS CHECK GOOD. RETURNED A/C SDR MWEA95281Girt Bar Latch · dirtyCREW REPORTS, FORWARD ENTRANCE DOOR EVACUATION SLIDE GIRT BAR IS HARD TO REMOVE AND INSTALL. MAINTENANCE CLEANED AND LUBED GIRT BAR LATCHES. OPS CHECK GOOD, RETURNED A/C TO SERVICE.SDR 9513519105Skin · delaminatedDURING LINE CHECK, FOUND DELAMINATION IN THE RIGHT INBOARD SPOILER. REPLACED SPOILER PER CITEXT 90-2760-1-9901.SDR MWEA95280Pan · crackedPASSENGER DOOR PAN IS CRACKED APPROXIMATELY .6250 INCH ON AFT PORTION OF BEAM NR 8. REPAIRED CRACK IAW SRM 52-05 FIG 18A.SDR MWEA95279Frame · misdrilledFUSELAGE FRAME AT STATION 160 HAS A .75 INCH HOLE IN UPPER RADIUS, 3 INCHES OUTBOARD OF LONGERON 4R. INSTALLED REPAIR IAW DOUGLAS TELEX JSS DTD, 16 AUG 95 AND PDG DTD 17 AUG 95.SDR MWEA95278Seat Track · corrodedRIGHT INBOARD SEAT TRACK MODERATELY CORRODED AT STATION 200. REPAIRED IAW SRM 53-05 FIG 4, AT FACTORY SPLICE.SDR MWEA95277Seat Track · corrodedRIGHT OUTBOARD SEAT TRACK MODERATELY CORRODED AT STATION 200. REPAIRED IAW SRM 53-05 FIG 4, AT FACTORY SPLICE.SDR MWEA95276Skin · dentedFUSELAGE SKIN DAMAGED ON RIGHT SIDE OF FUSELAGE NEAR AOA VANE AT STATION 280. REMOVED DAMAGED SKIN AND SPLICED IN NEW SKIN ON RIGHT SIDE, PER XYX DRAWING 53-147 AND TELEX SVC-ORD-0151/PDG.SDR MWEA95275Skin · crackCRACK IN FUSELAGE SKIN APPROX 1.5 INCH LONG, AT PASSENGER DOOR UPPER FORWARD CORNER AT STATION 164. CUT OUT DAMAGE, FABRICATED AND INSTALLED PLUG, DOUBLER AND TRIPLER PER SRM 53-05 FIG 26.SDR MWEA95274Skin · dentedRIGHT SIDE OF FUSELAGE, STATION 256 AT LONGERON SKIN 25 IS SHARPLY DENTED 1.5 INCH LONG. INSTALLED REPAIR IAW SRM 53-04 FIG 38 SHEET 21.SDR MWEA95273Blkhd Skin · crackedCRACK IN AFT PRESSURE BULKHEAD SKIN AT 6 O'CLOCK POSITION BELOW PLUG DOOR JAMB 1.083 LONG. REMOVED EXITING REPAIR, VERIFIED LENGTH OF CRACK AND INSTALLED REPAIR IAW 51-30-2 AND 51-30-5.SDR MWEA95272Blkhd Skin · crackedTWO CRACKS IN AFT PRESSURE BULKHEAD SKIN AT RECEPTACLE HOLE, APPROXIMATLY 1 O'CLOCK POSITION .25 INCH AND .75 INCH LONG. STOP DRILLED CRACK AND INSTALLED REPAIR TO THE TWO CRACKS IAW SVC RWK 5934886-509.SDR 9513139102Circuit Breaker · failedDURING CLIMBOUT FROM DTW, AUTO-PILOT DROPPED OFF LINE, CAPTAIN'S RMI FLAGGED, FORWARD AND AFT FUEL BOOST PUMP CIRCUIT BREAKERS POPPED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT AC BUS PHASE A CIRCUIT BREAKER BROKEN AND REPLACED THE CIRCSDR ABXA9500889Bracket · cutDURING C-CHECK INSPECTION, FOUND A PULLEY BRACKET JUST FORWARD OF STA 110 CUT. REPAIRED IAW ABX REA D953-12626-MR.SDR ABXA9500844Bracket · cutDURING C-CHECK INSPECTION, FOUND A PULLEY BRACKET JUST FORWARD OF STA 110 CUT. REPAIRED IAW ABX REA D953-12626-MR.SDR ABXA9500831Spar · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 79-19-02, X-RAY INSPECTION INDICATED A CRACK IN THE RIGHT ELEVATOR SPAR. REPLACED ELEVATOR IAW DC-9 MM 27-30-2.SDR ABXA9500845Skin · damagedDURING C-CHECK INSPECTION, FOUND EXTERNAL DOUBLER DAMAGED AT STA 604 AND 585, LONGERON 17L. REPAIRED IAW ABX REA D953-12553-MR.SDR MWEA95247Eel Sign · detachedTHE EMERGENCY EXIT LIGHT SIGN CAME OFF THE WALL, NEXT TO THE FWD GALLEY SERVICE DOOR. MAINTENANCE INSTALLED NEW SIGN. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.SDR 9511579103Tear Strap · crackedDURING H-CHECK, FOUND A CRACK IN THE TEAR STRAP AT FS 700, LONGERON 1. REPAIRED PER EA 91-98412.SDR GRAA9538Engine · failedON 4TH OF JULY, 1995, AIRCRAFT N1064T EXPERIENCED A TAKEOFF ABORT FROM AMARILLO AIRPORT TEXAS. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. THE ABORT WAS PERFORMED DUE TO THE RIGHT ENGINE NOT BEING ABLE TO ACHIEVE FULL RATED TAKEOFF POWER. MASDR 95ZZZX4157Door Opening · crackedSTL - DURING SPECIAL CHECK, FOUND A ONE-INCH CRACK IN AFT CARGO BIN BOTTOM AT AFT CORNER OF DOOR OPENING, WHICH WAS ALSO BENT, STA 750. REPAIRED PER EMLR 65708. AIRCRAFT TOTAL TIME: 60,441 HOURS; 77,859 CYCLES.SDR GRAA9536Eel Batteries · dischargedDURING LINE MAINTENANCE, MECHANICS DISCOVERED THE CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES. THE EMERGENCY LIGHT SYSTEM WAS OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR ABXA9500599Link · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY AT FORWARD DOOR LINK. REPLACED DOOR LINK IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500598Shim · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR CROSS ARM AT DOOR END HAD EXCESSIVE PLAY. RE-SHIMMED CROSS ARM END IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500597Rod · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR LOOSE AT DRIVE LINK. REPLACED ATTACH ROD IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR MWEA95215Control Cable · separatedPILOT REPORTS ON LANDING IN OMA THE LEFT THRUST REVERSER WOULD NOT DEPLOY. THE UNLOCK LIGHT CAME ON BUT COULD NOT FEEL INTERLOCK STOP IN THROTTLE. MAINTENANCE FOUND LEFT THROTTLE CABLE SEPARATED AT SWIVEL JOINT NEAR ENGINE. REMOVED AND REPLACED CABLE. PERFSDR GRAA9535Skin · corrodedDURING C-CHECK, MAINTENANCE FOUND CORROSION IN THE FORWARD BAGGAGE BIN, FS 313, LONGERON 26 LEFT. REPAIRED PER FLIGHT VEHICALS, IAW ER NR DC-9-53-001. AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GRAA9534Skin · serviceableDURING C-CHECK, RUDDER TRAILING EDGE, RT SIDE, HAD 3 SURFACE CRACKS. ONE CRACK IS 3 INCHES LONG. ONE CRACK IS 1.50 INCHES LONG. ONE CRACK IS 5.25 INCHES LONG. RUDDER WAS REPAIRED PER FLIGHT VEHICALS IAW ER NR DC-9-55-001. AIRCRAFT WAS RETURNED TO SERVICE.SDR MWEA95208Switch · malfunctionedCREW REPORTED, AFTER GEAR RETRACTION, AND DURING CLIMB CHECK LIST, RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MKE. MAINTENANCE WAS UNABLE TO DUPLICATE PROBLEM. REMOVED AND REPLACED RIGHT MAIN GEAR UPLATCH SWITCH AS A PRECAUTIONARY. SDR MWEA95203Evac Slide · fell offCREW REPORTS, GALLEY DOOR EMERGENCY EXIT SLIDE CAME OFF DOOR. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE.SDR MWEA95202Skin · crackedDURING ROUTINE INSPECTION, THE AFT CARGO DOOR SKIN WAS FOUND CRACKED ON LOWER EDGE. MAINTENANCE INSTALLED REPAIR DOUBLER IAW SRM 52-05 FIG 4. RETURNED A/C TO SERVICE.SDR MWEA95201Skin · crackedDURING ROUTINE INSPECTION, THE FWD CARGO DOOR SKIN WAS FOUND CRACKED ON LOWER FWD CORNER. MAINTENANCE INSTALLED REPAIR DOUBLER IAW 52-05 FIG 4. RETURNED A/C TO SERVICE.SDR 9507729105Rib · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD SPOILER FITTING (RIB CAP). REPLACED RIB CAP.SDR MWEA95178Slide Cover · fell offCREW REPORTS, EVACUATION SLIDE COVER FELL OFF OF MAIN ENTRANCE DOOR. MAINTENANCE RE-INSTALLED EVACUATION SLIDE COVER. RETURNED A/C TO SERVICE.SDR 9506469103Connector · brokenLOSS OF CABIN PRESSURIZATION OCCURRED ON DESCENT INTO SYR. EMERGENCY DESCENT PROCEDURES WERE ACCOMPLISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BROKEN CANNON PLUG TO AUGMENTATION VALVE SOLENOID 'A'. ALSO, REPLACED FLOW CONTROL VALVE AND PILOT PRESSUSDR MWEA95174O-Ring · leakingPILOT REPORTS DURING CLIMBOUT AT MKE, NOTICED RIGHT HYDRAULIC QUANTITY DECREASING AND RETURNED TO MKE. MAINTENANCE FOUND O-RING ON NOSE STEERING ACTUATOR LEAKING. REPLACED O-RING, CYCLED SEVERAL TIMES AND NO LEAKS NOTED. OPS CHECK GOOD, RETURNED AIRCRAFT TO
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