Mcdonnell Douglas DC-9-34
Service difficulty reports · 38
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 = 'DC934' 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 = 'DC934' 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 Y2PA20120921044Fuel Cell · damagedEXCESSIVE FUEL LOSS IN FLIGHT. LT FUEL LOW PRESSURE LIGHT CAME ON. CLIMBED TO FL270. AS ACFT LEVELED OFF CREW REALIZED THE LT WING FUEL GAUGE INDICATES ZERO. SHORTLY AFTER LT FUEL LOW PRESSURE LIGHT ILLUMINATED. COM 2.28.9 PROCEDURE PERFORMED, CROSSFEESDR Y2PA20120422019Battery · illuminatedTAIL COMPARTMENT EMERGENCY EXIT SIGN ON RT SIDE NEAR TAILCONE INOPERATIVE. MX R & R THE BATTERY IN THE POWER SUPPLY. SYSTEM OPS CHECKED GOOD IAW MM 33-53-0.SDR Y2PA20120422018Power Supply · inoperativeCABIN CEILING AND AFT F/A STATION EMERGENCY LIGHTS INOPERATIVE. MX R & R THE EMERGENCY EXIT POWER SUPPLY. SYSTEM OPS CHECKED GOOD IAW MM 33-50-0.SDR Y2PA20120422017Power Supply · inoperativeAFT OVER WING EMERGENCY EXIT LIGHTS INOPERATIVE. MX R & R THE EMERGENCY EXIT POWER SUPPLY. OPS CHECKED GOOD IAW MM 33-53-0.SDR Y2PA2011092000023Battery Pack · dischargedFORWARD AND MID SECTION EMERGENCY LIGHTS FOUND INOPERATIVE DURING INSPECTION. MX R & R EMERGENCY LIGHTING POWER PACKS AT 7 EACH POSITIONS IAW AMM 33-53-00. OPS CHECKED GOOD.SDR Y2PA2010112400031Battery · dischargedROW 12, LT & RT EMERGENCY EXIT SIGN FWD OF OVERWING HATCH IS INOPERATIVE. DISCREPANCY FOUND DURING SERVICE CHECK. MX RECHARGED THE BATTERY SUPPLY. SYS OPERATIONALLY CHECKED GOOD IAW THE MM 33-53-0. ACFT RETURNED TO SERVICE.SDR Y2PA2009051400002Pump · inoperativeDURING CLIMBOUT, RT ENGINE DRIVEN HYD PUMP PRESSURE DROPPED (INDICATED) "0" PRESSURE. (LT SYS NORMAL) PERFORMED COM PROCEDURE - RESTORED RT SYS PRESSURE WITH "AUX" PUMP. AT 18,000 FT APPROACH CHECKLIST ALTITUDE, DECLARED AN EMERGENCY WITH APPROACH AS A PRECSDR TWAA9911101Cable · failedTHE FIRST SECTION OF EGRESS LIGHTS IN THE COACH CABIN WERE INOPERATIVE. REPLACED THE FEEDER STRIP. CHECK-C 6-17-98 STL.SDR TWAA9907502Battery Pack · dischargedDURING PREFLIGHT CHECK, ROW 8-20 EGRESS LIGHTS WERE FOUND INOP. THE PROBLEM WAS LOW BATTERY PACKS. TWO PACKS WERE CHANGED. CHECK -C 06-17-98 STL.SDR TWAA9906601Power Supply · inoperativeTHE FORWARD OVERHEAD COACH EMERGENCY LIGHTS WERE DIM. REPLACED THE POWER SUPPLY FOR FORWARD OVERHEAD LIGHTS, AND SECURED THE GROUND STUD FOR LIGHT AT ROW 8. CHECK-C 6-17-98 STL.SDR TWAA9819801Fuel Control · malfunctionedTHE LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. THE LT ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO STL. REPLACED THE JFC, (P/N 743602-4), AND ENGINE FUEL PUMP, (P/N 378200). CHECK-C 3-22-98 STL.SDR TWAA9816102Duct · failedCOULD NOT MAINTAIN CABIN PRESSURIZATION AT ALTITUDE. DESCENDED TO 10,000 FT AND PRESSURIZATION NORMAL FOR REMAINDER OF FLIGHT. REPLACED THE LEFT WATER SEPARATOR DUCT. CHECK-C 6-17-98 STL.SDR TWAA9815001Actuator · wornNOSE GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED LANDING GEAR, NO HELP. RETURNED TO STL. REPLACED THE NLG RETRACT ACTUATOR. CHECK-C 1-4-98 STL.SDR TWAA9813901Tube · failedENGINE OIL PRESSURE AND QUANTITY DROPPED. LOW OIL PRESSURE LIGHT CAME ON. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND MADE UNSCHEDULED LANDING AT IND. NR 6 OIL BEARING LINE IN THE TAIL HAD FAILED. REPLACED LINE. CHECK-C 1-4-98 STL.SDR TWAA9812401Battery Pack · dischargedEMERGENCY EGRESS LIGHTS IN CABIN FLOOR WERE ILLUMINATED ALL THE TIME WITH THE SWITCH IN THE ARMED POSITION. REPLACED NR 4 BATTERY PACK FOR EMERGENCY LIGHTS. CHECK-C 3-22-98 STL.SDR TWAA9810702Battery · dischargedSTL - FLT 655 - EMERGENCY FLOOR LIGHTING INTERMITTENTLY ON DURING FLIGHT, ROW 9 AND AFT. CHARGED EGRESS POWER SUPPLY BATTERIES. CHECK-C 3-22-98 STL. (X)SDR TWAA9810701Connector · looseDFW - FLT 655 - THE ESCAPE PATH LIGHTS, ROW 10 TO ROW 14, ILLUMINATED DURING FLIGHT. RE-SEATED CANNON PLUG ON BATTERY PACK. CHECK-C 3-22-98 STL. (X)SDR TWAA9810601Light · inoperativeSTL - FLT 655 - AFT THIRD OF CABIN FLOOR ESCAPE PATH LIGHT INTERMITTENTLY CAME ON IN FLIGHT. RESEATED RIBBON ON FLOOR ESCAPE LIGHTS. CHECK-C 3-22-98 STL. (M)SDR TWAA9806801Computer · wornFLT 732 - CREW REPORTED VERY LITTLE RUDDER CONTROL AFTER TAKEOFF. THE NOSE WOULD HUNT BOTH SIDES. TURNED STAB AUG OFF WITH NO HELP. RETURNED TO STL. REPLACED THE STAB AUGMENTATION COMPUTER. (M)SDR TWAA9803003Wire · brokenSTL - FLT 433 - A BURNING SMELL WAS DETECTED IN REAR OF CABIN AT 300 FT AGL. REPAIRED BROKEN WIRE AT WIRE BUNDLE FOR LIGHTING BALLAST, ROW 19 RT SIDE. (M)SDR TWAA9801901Latch Assy · wornSTL - FLT 372 - ON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR AND NOSE GEAR UNSAFE LIGHT REMAINED ON BUT MAIN GEAR INDICATION NORMAL. PLACED GEAR HANDLE DOWN AND NORMAL INDICATION. RETURNED TO STL. REPLACED MAINTENANCE BYPASS HANDLESDR TWAA9714501Doubler · crackedSTL - DURING LAYOVER, MAINTENANCE FOUND .50 INCH CRACK IN DOUBLER NR 5910130-13 AT L1 DOOR UPPER AFT DOOR JAMB. REPAIRED PER ENGINEERING MAINTENANCE LIASION RECORD 65780 AND INSTALLED FASTENERS PER SRM 51-30-5. OP-15. 04/01-97. MCI. TOT. TIME: 46,511 HOSDR TWAA9712802Power Supply · inoperativeSTL - FLT 95 - DURING ROUTINE MAINTENANCE, THE TAIL CONE ESCAPE PATH LIGHTING WAS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY MFG P/N 5820-1 MANUFACTURED BY LUMINESCENT SYSTEMS. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9780001Clamps · looseSTL - FLT 467 - SHORTLY AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RE-TORQUED LOOSE CLAMPS ON THE AUGUMENTATION VALVE. OPS CHECK NORMAL. OP-16 - 12-31-96 - DAL. (X)SDR TWAA9757001Schrader Valve · leakingFLT 771 - STL - DURING CLIMB, NOSE GEAR FAILED TO RETRACT DUE TO LEAKING SHRADER VALVE. REMOVED AND REPLACED SCHRADER VALVE AND STRUT INFLATED PER CHART. OPS CHECK NORMAL. (M)SDR TWAA9806006Pan · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND THE AFT CARGO COMPT DOOR WITH 2 CRACKS IN DOOR PAN AT FWD LOWER DOOR PRESSURE STOP. FIRST CRACK WAS .5 INCH LONG IN RADIUS OF PAN, AND SECOND .5 INCH LONG IN PAN LIP. INSTALLED DOUBLER PER ARA 11688. (M)SDR TWAA9806005Pan · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO COMPT DOOR WITH A CRACK AND TEAR IN INNER PAN AND SEAL PAN AT FWD LOCK INTO PAN RADIUS. INSTALLED DOUBLER PER ARA 11688. (M)SDR TWAA9805508Skin · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN AFT LAV SKIN CRACKED AT RIVET LOCATED 6 INCHES FORWARD OF STATION 996, AND 2 IN BELOW LONGERON 15R. TWO EACH CRACKS. REPAIRED WITH TITANIUM DOUBLER PER SRM 53-04-41. (M)SDR TWAA9805502Skin · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT LOWER FUSELAGE SKIN BULGED AND RIVET HEADS POPPED AND PULLED FORWARD OF FS 996 LONGERON 27L. REMOVED CORROSION PER SRM 51-10-3 PARA 31-42. REPLACED LONGERON END PER SRM 53-02 IFG 2A PAGE 3, 51-30-0 AND 51-30-02SDR TWAA9805501Skin · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND THE AFT LOWER FUSELAGE SKIN BULGED AND RIVET HEADS POPPED AND PULLED FORWARD OF FS 996, LONGERON 28L. REMOVED CORROSION PER SRM 53-10-3 PARA 31-42. REPLACED LONGERON END PER SRM 53-02 FIG 2A PAGE 3, 51-30-0 AND 51-SDR TWAA9710003Actuator · slowSTL - FLT 647 - DURING CLIMB FOLLOWING GEAR RETRACTION, THE NOSE GEAR WAS SLOW TO RETRACT. REMOVED AND REPLACED THE NOSE GEAR RETRACT ACTUATOR, MFG P/N 3914738-5001, MANUFACTURED BY DOUGLAS AIRCRAFT COMPANY. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9614401Power Supply · inoperativeSTL - FLT 459 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 10 TO 15. FOUND MALFUNCTIONING POWER SUPPLY, MFG PN 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHTS OPERATION THEN CHECKED NORMAL. CHECK C - 4-10-96 - STL. (X)SDR 96ZZZM1205Power Supply · inoperativeSTL - DURING CRUISE EGRESS LIGHTS AT ROWS 8-12 ILLUMINATED. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL. (M)SDR 96ZZZM1196Seat Track · corrodedSTL - DURING OP-19, FOUND CORROSION ON LEFT INBOARD SEAT TRACK, STATION 200-206. REPLACED SEAT TRACK PER SRM 53-03, PAGE 10G, SHEET 1, FIGURE 4F. (M)SDR 96ZZZM906Battery Pack · dischargedSTL - FLT 501 - DURING CRUISE EMERGENCY EGRESS LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, OPERATIONAL CHECK NORMAL. (M)SDR 95ZZZM381Eel Cable · failedSTL - DURING CRUISE, EGRESS LIGHTS, FROM SEAT ROW 8 TO ROW 14, CAME ON. CYCLED EMERGENCY LIGHT SWITCH TO OFF, TO ARMED, EXTINGUISHED LIGHTS. FOUND OPEN FEEDER CABLE, MFG P/N 5853-1. REPLACED FEEDER CABLE AND LIGHT OPERATION CHECKED NORMAL. (M)SDR 95ZZZM294Fuel Control · failedDURING DESCENT SHUT DOWN RIGHT ENGINE, S/N 1605, DUE TO ENGINE DID NOT REDUCE TO IDLE WHEN THRUST LEVER WAS MOVED TO IDLE POSITION. FOUND FUEL CONTROL HAD INTERNAL MALFUNCTION. REPLACED FUEL CONTROL, MFG P/N 743602-5. ENGINE OPERATION CHECKED NORMAL. ENGINSDR 95ZZZW222Door Jamb · crackedSTL - DURING C-CHECK, FOND A .875 INCH CRACK IN UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD PASSENGER DOOR JAMB. STOP DRILLED CRACK AND REPAIRED PER S/B 53-137. TOTAL CYCLES 29,619.
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