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 9810609102Battery · dischargedDURING LINE CHECK, FOUND FIRST CLASS SECTION PATHWAY EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR TWAA9813701Control Valve · failedWHEN LANDING THE RT BRAKE WAS INOPERATIVE WHEN THE RT HYD SYSTEM WAS SELECTED. BRAKING NORMAL WHEN LT HYD SYS SELECTED. REPLACED THE RT BRAKE CONTROL VALVE PER MAINT MANUAL 32-42-2. CHECK-C 7-6-98 STL.SDR 9809929101Boost Pump · failedAFTER TAKEOFF, THE RIGHT AC ELECTRICAL SYSTEM FAILED CAUSING MALFUNCTION OF SEVERAL SYSTEMS AND COMPONENTS. FLIGHT WAS RETURNED TO ICT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT AFT FUEL BOOST PUMP INOPERATIVE WHICH CAUSED TRIP OF A PHASE CIRCUIT BSDR TWAA9812701Light · looseTHE FIRST CLASS AND FWD SECTION OF COACH HAD EGRESS LIGHTING INOPERATIVE. FOUND POWER FEEDER LEAD LOOSE. RESECURED CONNECTOR. CHECK-C 3-12-98 STL.SDR ABXA9800645Frame · crackedWHILE COMPLYING WITH C INSPECTION, FOUND FUSELAGE FRAME 544 RIGHT CRACKED AT TRANSVERSE FLOORBEAM. REPLACED FUSELAGE FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9800643Floorbeam · corrodedWHILE COMPLYING WITH C INSPECTION, FOUND A FLOORBEAM CORRODED ALONG LOWER FLANGE AT FS801 AND LBL44. REPAIRED FLOORBEAM IAW ABX REA D953-24225MR.SDR ABXA9800642Bulkhead Bracket · crackedWHILE COMPLYING WITH 'C' INSPECTION, FOUND THE AFT FACE OF THE AFT PRESSURE BULKHEAD HAD A CRACKED BRACKET AT LOWER LEFT CORNER OF DOOR JAMB. REPLACED BRACKET IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR 9809829104Retract Mech · out of adjustAFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RETRACTED THE LANDING GEAR BY PUSHING THE LANDING HANDLE RELEASE BUTTON. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED THE ANTI-RETRACTION SDR ABXA9800649Web · crackedWHILE COMPLYING WITH C INSPECTION, FOUND A WEB CRACKED BETWEEN LONGERON 8L AND 9L AT FS206. REPAIRED WEB IAW ABX REA D953-24104.SDR MWEA98812Bracket · brokenON GEAR EXTENSION UPON LANDING, LEFT MAIN GEAR DOOR FREE SWUNG HITTING PAVEMENT. MTC FOUND BRACKET ON MAIN GEAR DOOR BROKE. REMOVED AND REPLACED DOOR.SDR ABXA9800650Spar · crackedWHILE COMPLYING WITH C INSPECTION, FOUND A CRACK IN THE RIGHT UPPER SPAR TEE CAP AT XCW 58. REPAIRED CRACK IAW ABX REA D957-24102MR.SDR ABXA9800648Spar · crackedWHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT WING UPPER FRONT SPAR CRACKED BETWEEN TWO SCREW HOLES 10 OUTBOARD OF XCW 58. REPAIRED CRACK IAW ABX REA D957-24108MR.SDR ABXA9800647Spar · corrodedWHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER UPPER REAR SPAR CORRODED AT XE 147. REPLACED SPAR SECTION IAW DC-9 SRM CHAPTER 55-02.SDR ABXA9800641Bulkhead Web · corrodedWHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD WEB CORRODED BETWEEN LONGERON 26L TO 30L. REPAIRED IAW ABX REA D953-24142MR.SDR ABXA9800620Panel · corrodedWHILE COMPLYING WITH C-CHECK, FOUND LEFT SLANT PANEL CORRODED. REPAIRED IAW DACO DWG 5956065, ABX DWG NR 4255 AND DC9 SRM 51-30-2.SDR ABXA9800619Shield · crackedWHILE COMPLYING WITH C-CHECK FOUND A CRACKED HEAT SHIELD IN THE RIGHT WING NR 1 LEADING EDGE SECTION. REPAIRED IAW ABX REA NR D957-24148.SDR ABXA9800618Doubler · corrodedWHILE COMPLYING WITH C-CHECK, FOUND STATION 817 FLOORBEAM WEB DOUBLER CORRODED. INSTALLED WEB DOUBLER IAW DACO DWG NR 9915561.SDR ABXA9800617Floorbeam · corrodedWHILE COMPLYING WITH C-CHECK FOUND STATION 817 FLOORBEAM WEB CORRODED. REPLACED WEB IAW DC9 SRM 51-10-2 AND 51-10-5.SDR ABXA9800646Bulkhead Jamb · crackedWHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER RIGHT CORNER CRACKED. REPAIRED IAW ABX REA D953-24119.SDR ABXA9800644Spar · corrodedWHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT WING FORWARD UPPER SPAR CAP CORRODED FROM XFS 410 TO 406. REPAIRED RIGHT WING FRONT SPAR CAP IAW ABX REA D957-24091MR.SDR ABXA9800613Housing · crackedWHILE COMPLYING WITH C-CHECK, FOUND MAIN ENTRY DOOR EXTERIOR HANDLE HOUSING CRACKED. REPLACED HOUSING IAW DC9 SRM 51-30-2.SDR ABXA9800612Spar Cap · corrodedWHILE COMPLYING WITH C-CHECK, FOUND CORROSION ON LEFT WING FRONT SPAR UPPER CAP AT STATION XRS 459. REPAIRED UPPER CAP IAW REA D957-24092.SDR ABXA9800611Longeron · crackedWHILE COMPLYING WITH C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT FUSELAGE STATION 786. REPLACED LONGERON 17 RIGHT SECTION AT STATION 786 IAW DC9 SRM.SDR ABXA9800610Structure · crackedWHILE COMPLYING WITH C-CHECK FOUND FORWARD SUB FLOOR CRACKED AT STATION 170 LBL 40. REPAIRED CRACKED SUB FLOOR IAW DC9 SRM 53-01.SDR 9809679105Controller · failedAT FL290, THE CABIN PRESSURE BEGAN CLIMBING 1500 FEET PER MINUTE. THE FLIGHT CREW CLOSED THE OUTFLOW VALVE, CHECKED FOR CLOSED CROSSFEED VALVES, FOLLOWED EMERGENCY CHECK LIST, AND INITIATED AN EMERGENCY DESCENT TO FL100. THE OXYGEN MASK AUTO DEPLOY SYSTEM OPSDR TWAA9810310Frame · crackedSTL - ON LT Z14 RADIAL OTBD LOWER HOLE ON THE FORWARD SIDE, A .25 INCH CRACK WAS INDICATED BY EDDY CURRENT IN THE ATTACH ANGLE. REPAIRED PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810309Frame · crackedSTL - FOUND LT Z14 RADIAL OTBD UPPER HOLE ON THE FORWARD SIDE WITH .3750 INCH CRACK INDICATION BY EDDY CURRENT. REMOVED AND REPLACED END CLIP PER SRM 51-30-5, AND ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810308Fitting · crackedSTL - FOUND UPPER END FITTING ON AFT PRESSURE BULKHEAD RT Z34 RADIAL CRACKED .1250 INCH AT TEE FITTING. REPAIRED PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810307Frame · crackedSTL - THE RT Z34 RADIAL WAS CRACKED ON END ABOUT 1 INCH. REPAIRED PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810306Frame · crackedSTL - THE RT Z34 RADIAL OUTBOARD LOWER HOLE ON FORWARD SIDE SHOWED CRACK INDICATION BY EDDY CURRENT. REPAIRED PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810315Bulkhd Fitting · crackedSTL - THE UPPER END FITTING ON AFT PRESSURE BULKHEAD LT Z24 RIB WAS CRACKED AT TEE FITTING. REMOVED AND REPLACED END FITTING PER ARA 15188. CHECK-C 3-12-98 STL. (X)SDR TWAA9810312Bulkhead Skin · crackedSTL - FOUND BULKHEAD SKIN CRACKED .25 INCH AT LT BULKHEAD AT Z24L, ON OTBD TOP SIDE, SECOND HOLE FORM END. REPAIRED SKIN PER ARA 15189. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810305Frame · crackedSTL - THE LT Z24 RADIAL, UPPER INBD HOLE ON THE FORWARD SIDE SHOWED CRACK INDICATION BY EDDY CURRENT. REMOVED AND REPLACED FITTING PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810311Frame · crackedSTL - ON THE LT Z34 RADIAL UPPER OTBD HOLE ON THE FORWARD SIDE, A CRACK INDICATION WAS SHOWN BY EDDY CURRENT. REPAIRED PER TWA ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR TWAA9810314Bulkhd Fitting · crackedSTL - THE LOWER END FITTING ON AFT PRESSURE BULKHEAD LT Z34 RIB HAD A .3750 INCH CRACK AT TEE FITTING. REPAIRED PER TWA ARA 15188. CHECK-C 3-12-98 STL. (X)SDR TWAA9810313Frame · crackedSTL - THE Z48 RADIAL FORMER RT SIDE WAS FOUND CRACKED 1 INCH LONG ON OTBD END. REPAIRED FORMER PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR MWEA98643Blkhd Stiffener · crackedFOUND CRACK IN AFT PRESSURE BULKHEAD RIGHT RADIAL 14 IN STIFFENER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR MWEA98642Skin · chafedFOUND RIGHT AND LEFT LOWER AFT SKINS ON CANOE FAIRING CHAFED BEYOND LIMITS. MTC REMOVED AND REPLACED SKIN.SDR MWEA98631Light · dimTHE PORTABLE EMERGENCY LIGHT FOUND DIM. MAINTENANCE INSTALLED SERVICEABLE PORTABLE EMERGENCY LIGHT.SDR TWAA9808603Battery Pack · dischargedSTL - FLT 404 - EMERGENCY EXIT SIGNS AT R1 AND L1 DOORS CAME ON IN FLIGHT. WOULD NOT RESET UNTIL SHORT FINAL. REPLACED FWD EMERGENCY EXIT SIGN BATTERY PACK. (M)SDR MWEA98582Power Supply · inoperativeTHE EMERGENCY LIGHTS AT LAST ROW OF SEATS CEILING REMAINED ON WHEN POWER TURNED OFF. MTC REMOVED AND REPLACED POWER SUPPLY.SDR 9808729101Valve · failedDURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR UNSAFE AND DOOR OPEN LIGHTS ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RECYCLED LANDING GEAR HANDLE, RETURNED TO MEM, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN LANDING GEAR CONTROL VALVSDR 9808719101Batteries · dischargedDURING LINE CHECK, FOUND SEVERAL FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE, EXIT LIGHTING WEAK OVER LEFT WING EXIT, AND EMERGENCY LIGHTING OUT OF SEQUENCE IN FIRST CLASS SECTION. MAINTENANCE REPLACED BATTERIES AND REARRANGED LIGHT ASSEMBLIES IN FIRST CLASSDR 9808609101Wire · chafedDURING CLIMB-OUT, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW PERFORMED UPLATCH CHECK. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRING AT RIGHT MAIN LANDING GEAR UPLOCK SWITCH. OPERATIONAL CHECK NORSDR 9808599106Roller · out of adjustDURING LANDING GEAR UPLATCH CHECK, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW RECYCLED THE LANDING GEAR HANDLE PER COM PROCEDURES AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDING GEAR DOOR ROLLERSSDR 9808469101Latch · out of adjustRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED RIGHT MAIN GEAR DOOR LATCH MECHANISM, OPERATIONAL CHECK NORMAL.SDR 9808339106Battery · dischargedDURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR MWEA98570Clip · crackedFOUND CRACKED LEFT WING RIB 111 MOST AFT LOWER SHEAR CLIP. MTC FABRICATED AND INSTALLED SHEAR CLIP.SDR MWEA98569Doubler · damagedREMOVED TCAS ANTENNA AND DOUBLER STATION 256 FRAME SHEAR CLIP FASTENERS IN SKIN LAP AT STATION 229, L27 LEFTHAND TO L28 RIGHT HAND TO FACILITATE OTHER MAINTENANCE. MTC REINSTALLED ANTENNA DOUBLER AND SHEAR CLIP.SDR MWEA98568Clip · damagedREMOVED CLIP FROM LEFT HAND WING AT STATION 69 STRINGER 11 TO FACILITATE OTHER MAINTENANCE. MTC FABRICATED AND INSTALLED STRINGER CLIP.
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