Douglas DC-9-41
Service difficulty reports · 2,671
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 = 'DC941' 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 = 'DC941' 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 ABXA080177Battery · dischargedEMERGENCY EXIT PLANE EXIT LIGHTS FOUND INOPERATIVE ON PRE-FLIGHT. REPLACED EMERGENCY POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A)SDR NWAA082709751Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 13-15 OF THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND IMPROPER INSTALLATION OF THE BATTERIES. BATTERIES HAD BEEN INSTALLED BACKWARDS. REINSTALLED BATTERIES AND OPERATIONAL CHESDR ABXA080157Uplock Switch · malfunctionedSTA SWF, CPM GEAR RETRACTION, AFTER TAKEOFF, LEFT "GEAR UNSAFE" LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND NOTED THAT LEFT HEAR DOWN "GREEN LIGHT" ILLUMINATED WITHOUT DELAY. "NO CYCLE TIME" UPON RETRACTION ALL INDICATIONS WERE NORMAL. DEFERRED CLEARED DI 6SDR NWAA082679755Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE ATTEMPTED CORRECTION BY RELAMPING BUT ENDED UP REPLACING THE BATTERIES IN THE BATTERY PACK B5-28. THE LIGHTS RETURNED TO AN OPERATISDR ABXA080178Wire · burnedWHILE TROUBLE SHOOTING THE INOP LT INBO TAIL LIGHT AND THIS LT AFT WING TIP LIGHT FOUND WIRE L 26AH20N BURNT FROM R5-1051D TO GROUND STUD 713 IAW WDM 33-42-02. (A)SDR ABXA080182Bulkhead · crackedLT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB SKIN WAS CRACKED. CAN BE SEEN FROM CATWALK. REMOVED WALKWAY, REPAIRED AREA IAW REA D953-57424 MR. RE-INSTALLED WALKWAY IAW DC9 SRM 51-30-4. (A)SDR NWAA082979762Battery Pack · malfunctionedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 20-23 OF THE CABIN WERE INOPERATIVE. THE BATTERY PACK WAS "RESET" BY MAINTENANCE AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A)SDR ABXA080154Battery · dischargedCOCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A)SDR ABXA080140Battery · dischargedEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8.SDR NWAA081829752Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12 THROUGH 15 OF COACH SEATS IN THE CABIN HAD FAILED. MAINTENANCE REPLACED THE EMERGENCY PATHWAY LIGHT POWER SUPPLY AT THE OVERWING EXIT. INSTALLED NEW BATTERIES AND OPERATIONALSDR ABXA080139Seat · unlockedCAPTAIN'S SEAT BECAME UNLOCKED DURING ROTATION WHILE CAPTAIN WAS FLYING AND SLIDE TO REAR STOP. SEAT WAS VERIFIED LOCKED DURING PUSHBACK. INSPECTED CAPTAIN'S SEAT IN ALL LOCKING POSITIONS. NO DEFECTS FOUND. MOVED SEAT VIGOROUSLY IN ALL LOCKING POSITIONS ANSDR NWAA081769762Line · leakingWHILE IN CRUISE FLIGHT AT FL320, THE CABIN ALTITUDE BEGAN CLIMBING UNCONTROLLABLY. FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND BEGAN A RAPID DESCENT TO LOWER ALTITUDES. AT FL280 THE CREW WAS ABLE TO REGAIN CONTROL OF THE CABIN ALTITUDE AND RECEIVED CLEARASDR ABXA080148Intercostal · corrodedINTERCOSTAL FS 1060, LONGERON 27 LEFT WAS CORRODED. REMOVED AND REPLACED INTERCOSTAL AT FS 1060, LONGERON 27 LEFT IAW DC9 SRM.SDR ABXA080147Floorbeam · crackedFLOORBEAM CRACKED ON BOTH SIDES OF INTERCOSTAL AT STA 180, LEFT BUTT LINE 20. REPAIRED IAW DC9 SRM 53-05.SDR ABXA080124Bungee Cylinder · leakingRIGHT HYDRAULIC QUANTITY LOSS TO ZERO. FOUND LEFT MAIN LANDING GEAR HYDRAULIC BUNGEE CYLINDER LEAKING. REPLACED LEFT BUNGEE CYLINDER IAW DC9 AMM 32-32-03-2.SDR ABXA080146Pan · crackedMAIN ENTRY DOOR SWITCH STRIKER BRACKET LOWER ATTACH HOLE HAD A 3/8 INCH CRACK COMING FROM HOLE (MED PAN). REPAIRED AREA IAW DC9 SRM 52-03.SDR ABXA080142Floor Support · crackedLATERAL FLOOR SUPPORT CRACKED AT FS 677, RIGHT BUTT LINE 30 & 34. REPLACED SUPPORT IAW DC9 SRM.SDR ABXA080118Light · out of positionMAP & BRIEFCASE CIRCUIT BREAKER TRIPPED, SMOKE EXITING FROM FIRST OFFICER'S MAP LIGHT ON FIRST OFFICER'S CONTROL COLUMN. REPOSITIONED LIGHT ASSEMBLY. SYSTEM CHECKS GOOD IAW DC9 AMM 33-13-00.SDR ABXA080117Unknown · malfunctionedCABIN PRESSURIZATION WAS NORMAL OUT OF 10,000 MSL. APPROX 14,000 MSL, CABIN PRESSURIZATION ANNUNCIATOR & MASTER WARNING CAME ON. CHECKED CABIN PRESSURIZATION AND IT WAS APPROX 11K. DONNED OXYGEN MASKS AND PROCEEDED WITH ABNORMAL CHECKLIST. DURING THE ABNORSDR ABXA080136Frame · crackedPANEL 8105 FRAME CRACKED, LOWER PYLON BELOW AND FORWARD OF AFT ENGINE MOUNT. INSTALLED SPLICE REPAIR IAW DC9 DWG K05683.SDR ABXA080135Skin · crackedRIGHT WING UPPER SURFACE XRS 164.00, THE BONDED PANEL JUST INBOARD OF INBOARD SPOILER BOARD HAD 6 EACH SHEARED FASTENERS. REPAIRED CRACKED SKIN IN AREA OF LOOSE RIVETS IAW DC9 SRM 57-01, FIGURE 2.SDR NWAA081199762Web · crackedDURING "M" CHECK, FOUND CRACK IN WEB AT BS 110 FROM LBL 42 TO LBL 48. REPAIRED PER EA 97-212129.SDR ABXA080134Bracket · crackedINBOARD BULKHEAD FORWARD VERTICAL STIFFENER BRACKET FORWARD SIDE CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1.SDR ABXA080133Support Bracket · crackedLEFT REAR SUPPORT BRACKET FORWARD PATCH 2108 WAS CRACKED. REPAIRED CRACK IAW DC9 SRM 51-70-1.SDR ABXA080132Web · crackedSUB FLOOR WEB CRACKED AT STA 179, LEFT BUTT LINE 20. REPAIRED SUB FLOOR WEB IAW DC9 SRM 53-01, FIGURE 2.SDR NWAA081099759Fuse · failedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY FUSE. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE.SDR NWAA081079753Wire · damagedDURING LINE CHECK, MAINTENANCE FOUND THAT TWO OF THE EMERGENCY PATHWAY LIGHTS FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE FOUND OPEN WIRES IN THREE LOCATIONS AND REPAIRED THEM AND THEN RETURNED THE AIRCRAFT TO SERVICE.SDR NWAA080989760Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERWING EXIT SIGNS ON BOTH THE LEFT AND RIGHT SIDES WERE INOPERATIVE. AFTER INSTALLATION OF A NEW BATTERY PACK, MAINTENANCE OPERATIONALLY CHECKED SYSTEM AND AIRCRAFT RETURNED TO SERVICE.SDR ABXA080089Skin · corrodedDURING LINE MAINTENANCE, FOUND CORROSION OF FUSELAGE SKIN AROUND THE LEFT STATIC PORT PLATE. REMOVED LEFT STATIC PORT PLATE, FOUND FUSELAGE SKIN UNDER THE PLATE CORRODED BEYOND LIMITS. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 31, SHEET 1.SDR NWAA080799751Wire · disconnectedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR ROWS 5, 6, 7, 8, 14, AND 17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A DISCONNECTED WIRE AND RE-INSERTED IN THE CONNECTOR. THE AIRCRAFT RETURNED TO SERVICE.SDR ABXA080087Actuator · damagedUPON PUTTING GEAR HANDLE DOWN, HEARD LOUD BANG AND SHUTTER IN AIRCRAFT. NORMAL GEAR INDICATION. FOUND RIGHT MAIN LANDING GEAR ACTUATOR EYE BOLT PULLED OUT OF THE ACTUATOR. REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR IAW DC9 AMM 32-32-02.SDR NWAA080689756Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. THE BATTERY PACK AT THE FORWARD CABIN RIGHT DOOR WAS REPLACED. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
SDR NWAA080709751Oil System · overservicedTHE FLIGHT ATTENDANT AND PASSENGER BOTH REPORTED A BURNING ODOR IN THE CABIN. FLIGHT CONTINUED AS SCHEDULED AND LANDED AT MEM WITHOUT INCIDENT. MAINTENANCE INSPECTED EVERY POSSIBLE SOURCE OF FUMES ABOARD THE AIRCRAFT AND FOUND THE APU OIL OVER SERVICED. OILSDR ABXA080060Window Frame · crackedDURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND CENTER FRAME WITH MULTIPLE CRACKS. REPLACED CENTER FRAME SEGMENT IAW DC9 SRM 51-30-2 PER WO 600283624.SDR ABXA080058Window Frame · crackedDURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND RIGHT SIDE FRAME CRACKED LESS THAN 2.50 INCHES. REPAIRED IAW DC9 SRM 53-03, FIG 34 PER WO 600283624.SDR ABXA080057Intercostal · crackedDURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND FORWARD INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-10-4 PER WO 600283624.SDR ABXA080059Window Frame · crackedDURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND LEFT SIDE FRAME CRACKED LESS THAN 2.50 INCHES. REPAIRED IAW DC9 SRM 53-05, FIG 34 PER WO 600283624.SDR NWAA080389758O-Ring · failedIN CRUISE FLT AT FL310, THE RT HYD SYS FAILED. QTY AND PRESSURE WERE BOTH LOST REQUIRING CREW TO SECURE SYSTEM. FLT CONTINUED AS SCHEDULED AND THE EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED ON APPROACH. LANDING AT TPA INVOLVED THE GEAR DOORS MAKING CSDR ABXA080035Pin · dislodgedFIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER GUIDE PIN OUT OF CAM SLOT. RE-ALIGNED CAM PIN WITH CAM SLOT. CLEARVIEW WINDOW TEST GOOD IAW DC9 AMM 56-10-03-5.SDR ABXA080031Doubler · crackedDURING WINDOW FRAME MOD, FOUND WINDSHIELD WIPER DOUBLER CRACKED, 3 INCHES LONG LOCATED 10.5" FROM THE RIGHT OUTBOARD EDGE. REMOVED AND REPLACED DOUBLER IAW EA 53300036-010.SDR ABXA080030Window Frame · crackedDURING WINDOW FRAME MODIFICATION, FOUND COCKPIT WINDOW ENCLOSURE CENTER FRAME HAD MULTIPLE CRACKS AT BOTH ENDS EXCEEDING LIMITS. REPLACED FRAME IAW DC9 SRM 53-03, FIGURE 34 AND DC9 SRM 51-10-4, (3 CRACKS: 1.5 INCH, 1.25 INCH, AND 1INCH).SDR ABXA080027Battery · dischargedEMERGENCY EVAC LIGHTS WOULD NOT ILLUMINATE WITH SWITCH ON. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8.SDR ABXA080026Window Frame · crackedCENTER AND SIDE WINDSHIELD RIGHT ZEE P/N: 5912360-68 CRACKED. REPLACED RIGHT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.SDR ABXA080025Structure · crackedCENTER AND SIDE WINDSHIELD LEFT ZEE P/N: 5912360-67 CRACKED. REPLACED LEFT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.SDR ABXA080024Angle · crackedCOCKPIT WINDOW SILL LEFT ANGLE CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.SDR ABXA080023Angle · crackedCOCKPIT WINDOW SILL RIGHT ANGLE CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.SDR ABXA08026Angle · crackedCENTER AND SIDE WINDSHIELD RIGHT ZEE P/N: 5912360-68 CRACKED. REPLACED RIGHT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.SDR ABXA08025Angle · crackedCENTER AND SIDE WINDSHIELD LEFT ZEE P/N: 5912360-67 CRACKED. REPLACED LEFT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.SDR ABXA08024Angle · crackedCOCKPIT WINDOW SILL LEFT ANGLE P/N: 9957860-7 CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.SDR ABXA08023Angle · crackedCOCKPIT WINDOW SILL RIGHT ANGLE P/N: 9957860-8 CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.
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