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 ABXA9500242Bushing · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING FOR ATTACH ROD TO FOLLOW UP ROD WORN ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500240Rod End · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR ATTACH ROD END LOOSE IN ATTACH ROD. REPLACED ROD ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500241Bushing · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND WORN BUSHING IN ARM ASSEMBLY ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR 9504569759Skin · crackedDURING LINE CHECK, FOUND TWO 1.50 INCH CRACKS IN THE RIGHT FUSELAGE SKIN AFT OF ELEVATOR ACCUMULATOR SERVICE DOOR. REPAIRED PER EA 97-096492.SDR ABXA9500457Retract Mech · wornDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR DOOR BUSHINGS WORN IN ACTUATING ARM. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500468Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND FUSELAGE FRAME AT FS 1152 CRACKED AT LONGERON 14R. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500216Wire · burnedRIGHT GENERATOR DROPPED OFF LINE WITH CROSS-TIE LOCKOUT. SMOKE IN THE COCKPIT REPORTED. FOUND GENERATOR FEEDER CABLES OVERHEATED BEHIND THE GENERATOR CONTROL PANEL. REPLACED TERMINAL ON MAIN FEEDER CABLE. REPLACED CABLE FROM TERMINAL STRIP TO GENERATOR RESDR ABXA9500516Floorbeam · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND REPAIRS ON FLOORBEAM AT FS 1072, LBL 46 AND 48 NOT IAW THE SRM. REPAIRED FLOORBEAM IAW ABX REA D 953-11128-MR.SDR ABXA9500506Floorbeam · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND REPAIRS ON FLOORBEAM AT FS 1072, LBL 46 AND 48 NOT IAW THE SRM. REPAIRED FLOORBEAM IAW ABX REA D953-11128MR.SDR ABXA9500473Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FUSELAGE SKIN REPAIR AT FS 617 BETWEEN LONGERONS 28R AND 28L NOT IAW DC-9 SRM. REPAIRED FUSELAGE SKIN IAW ABX REA D953-11104-MR.SDR ABXA9500469Longeron · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 30 CORRODED FROM FS 908 TO FS 946 IN AFT BAG BIN. REPLACED LONGERON SECTION IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR 9504329751Switches · malfunctionedSTALL INDICATION FAILURE LIGHT AND STICK SHAKER ACTIVATED DURING SLAT RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED SLAT EXTEND SWITCHES. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500495Door Jamb · dentedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE SERVICE DOOR JAMB AFT STRUCTURE DENTED IN THE BAYONET AREA. REPAIRED RIGHT HAND SERVICE DOOR JAMB IAW DC-9 SRM 53-05 FIGURE 42.SDR 9504309754To Warning · soundedTAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL AT DTW. ABORTED TAKEOFF AND RETURNED TO GATE. DISCREPANCY COULD NOT BE DUPLICATED DURING OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE.SDR 9504269752Prbc Valve · failedDEPARTING FROM MSP, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AT APPROXIMATELY 3,000 FEET. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ENGINE WAS INSPECTED, NO DAMAGE NOTED. MAINTENANCE REPLACED THE PRBC AND P AND D VALVE. THE ENGINE WAS RUNSDR ABXA9500472Bushing · missingDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT MAIN LANDING GEAR FLYING DOOR HAD ONE MISSING BUSHNG IN THE HINGE LOBE. INSTALLED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500458Skin · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT VERTICAL SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. REPLACED SKIN IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500456Bushings · wornDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR ACTUATING ROD BUSHINGS WORN. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL.SDR ABXA9500147Prox Sw Box · defectiveNOSE GEAR UNSAFE LIGHT STAYED ON AFTER TAKEOFF OUT OF ELP. RECYCLED GEAR AND WENT THROUGH ABNORMAL, LIGHT STAYED ON. REPLACED PROXIMITY SWITCH BOX. PERFORMED SYSTEM CHECK. SYSTEM CHECKED NORMAL IAW DC-9 MM 32-60-01 PAGE 214 STEP 5A.SDR ABXA9500503Web · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE CUSP WEB CRACKED AT FS 218, LBL 55. REPLACED CUSP WEB FROM FS 218 TO FS 237 IAW DC-9 SRM 51-30-2.SDR ABXA9500502Intercostal · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN INTERCOSTAL CRACKED AT FS 180, LBL 42. REPAIRED INTERCOSTAL IAW DC-9 SRM SUPPLEMENTAL DRAWING NR K05195.SDR ABXA9500490Web · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT CUSP WEB AT FS 946 HAD LEVEL II CORROSION. REPLACED RIGHT CUSP WEB IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500489Fitting · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME TEE FITTING AT FS 1013 HAD LEVEL II CORROSION. REPLACED FUSELAGE FRAME TEE FITTING IAW DC-9 SRM 51-30-5.SDR ABXA9500488Fitting · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME TEE FITTING HAD LEVEL II CORROSION AT FS 1005. REPLACED RIGHT FUSELAGE FRAME FITTING AT FS 1005 IAW DC-9 SRM 51-30-5.SDR ABXA9500487Fitting · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME FITTING AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT TEE FITTING IAW DC-9 SRM 51-30-5.SDR ABXA9500486Web · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT CUSP WEB AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT CUSP WEB FROM FS 973 TO 1041 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9500330Angle · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 FLAP OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE RIB ANGLE. REPLACED RIB ANGLE IAW DC-9 SRM 57-50-9.SDR 9503669760Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THE TAILCONE RELEASE MECHANISM OUT OF RIG. RE-RIGGED TAILCONE, CHECKED OK.SDR ABXA9500485Angle · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT HAND FLOOR BEAM ATTACH ANGLE CRACKED AT FS 655. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-5.SDR 9503489751Uplimit Switch · malfunctionedNOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DURING CLIMB-OUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR UPLIMIT SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500504Rib · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING NR 2 INBOARD SLAT TRACK FITTING CRACKED AT LOWER ATTACHMENT. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500499Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 2R CRACKED AT FS 718. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2.SDR ABXA9500491Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 2R CRACKED AT FS 718. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02 FIGURE 2.SDR 9503269758Bulkhead · corrodedDURING LINE CHECK, FOUND CORROSION ON THE CANTED BULKHEAD FS 729 AT LBL 40 BETWEEN THE LOWER CHORD AND WEB. REPAIRED PER EA 97-096744.SDR ABXA9500501Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 3R CRACKED AT FS 794. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2.SDR ABXA9500500Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 4R CRACKED AT FS 775. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2.SDR ABXA9500493Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 3R CRACKED AT FS 794. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02 FIGURE 2.SDR ABXA9500492Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 4R CRACKED AT FS 775. REPLACED LONGERON SECTON IAW DC-9 SRM 53-02 FIGURE 2.SDR ABXA9500484Longeron · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, WHILE COMPLYING WITH AD 94-03-01, FOUND LONGERON 17R CRACKED AT FS 408. REPAIRED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500494Door Jamb · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT MAIN ENTRY DOOR JAMB WEB CRACKED AT FS 207 AND LONGERON 11L AND 15L. REPAIRED IAW DC-9 SRM SUPPLEMENTAL DRAWING K05012.SDR 9503079760Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THAT THE LEFT AFT EMERGENCY OVERWING EXIT WOULD NOT OPEN FROM THE OUTSIDE. ADJUSTED THE OUTER HANDLE RELEASE MECHANISM PER MM 52-21-0.SDR ABXA95099Bushing · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR TO WING HINGE BUSHINGS WORN. REPLACED HINGE BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500101Pin · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR TO WING HINGE PINS WORN. REPLACED HINGE PINS IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500100Arm · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR ARM ASSEMBLY WORN. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500098Fitting · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR FITTING WORN. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500097Arm · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ARM ASSEMBLY WORN. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR 9502709753Stall Computer · malfunctionedSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER FLAP RETRACTION ON TAKEOFF AND REMAINED ON AT SPEEDS UP TO 340 KTS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. REPLACED BOTH NR 1 AND NR 2 STALLSDR 9502719760Retract Mech · malfunctionedA LOUD 'BANG' WAS HEARD ON INITIAL GEAR RETRACTION AFTER TAKEOFF. NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AND VIBRATION WAS EXPERIENCED. FLIGHT RETURNED TO DTW AND SUCCESSFUL OVERWEIGHT LANDING WAS ACCOMPLISHED. PERFORMED OVERWEIGHT LANDING INSPECTION PESDR 9502499756Track · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON RIGHT CARGO TRACK UPPER SURFACE IN THE AFT CARGO COMPARTMENT. REPLACED TRACK PER EA 97-096677.SDR 9502489756Jamb · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN FORWARD CARGO DOOR JAMB PAN AFT SIDE. REPAIRED PER EA 97-096686.
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