Douglas DC-9-32
Service difficulty reports · 12,755
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 = 'DC932' 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 = 'DC932' 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 ABXA9700066Skin · crackedDURING C-CHECK INSPECTION, FOUND REPAIR ON FUSELAGE SKIN AT STATION 965, LONGERON 13 T0 14 LEFT TO BE BENT AND DISTORTED. INSTALLED DOUBLER REPAIR IAW REA DC953-18792-MR.SDR ABXA9700061Rib · crackedDURING C-CHECK INSPECTION, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS A CRACKED RIB ON LOWER AFT END SECOND RIB FROM INBOARD. REPAIRED CRACKED RIB IAW DC9 SRM 55-02.SDR ABXA9700060Rib · crackedDURING C-CHECK INSPECTION, FOUND TWO LEADING EDGE PANEL RIBS CRACKED. REPAIRED LEADING EDGE RIBS IAW DC9 SRM 55-01.SDR GTIA9700259Logo Light · missingMYR - FLT 1701 - RIGHT LOGO LIGHT DISCOVERED MISSING ON POST FLT INSPECTION. TRANSFERRED TO DMI NR 00292 PER MEL 33-23. CAT 'C'. BOS, INSTALLED LAMP, LOUVER AND CLIPS ON RT LOGO IAW DC-9 MM CHAPTER 33. OPS CHECK GOOD. CLEARS DMI NR 00292. (M)SDR CALA9700437Longeron · crackedINSPECTION FOUND A .75 INCH CRACK IN LONGERON 17L AT STA 980. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02.SDR CALA9700436Longeron · crackedINSPECTION FOUND A .75 INCH CRACK IN EACH OF THREE LONGERONS AT STA 965. THE CRACKS WERE FOUND IN LONGERON 16L, 17L AND 17R. THE LONGERONS WERE REMOVED AND REPLACED IAW SRM 53-02.SDR ABXA9700350Rib · crackedDURING C INSPECTION, FOUND THE RIGHT WING TRAILING RIB AT XRS 167, CRACKED AT AFT END. REPLACED TRAILING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9700336Tab · delaminatedDURING C INSPECTION, FOUND THE RIGHT ELEVATOR GEARED TAB DELAMINATED. REPLACED GEARED TAB IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-30-4.SDR 9705569919Press Switch · malfunctionedEN ROUTE MSP-HPN, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH TAIL DEICE SELECTED. RESET CIRCUIT BREAKER WITH NO HELP. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TAIL AIR PRESSURE SWITCH. OPERATIONAL CHECK SDR 9705649921Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD FORWARD ENTRY AND GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR 9705539985Battery Charger · failedDURING CRUISE TO LGA, NOTICED BATTERIES TAKING CHARGE OF 55-65 AMPS. PULLED AND RESET CIRCUIT BREAKER W-21. NO CHARGE WHEN RESET. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED SHIPS BATTERIES, BATTERY CHARGER, AND TEMPERATURE SENSOR. SYSTEMSDR MWEA97134Girt Bar Latches · dirtyDURING A-CHECK, FOUND GALLEY SERVICE DOOR EVAC SLIDE GIRT BAR DIFFICULT TO ENGAGE IN LATCHES. MAINT CLEANED AND LUBED GIRT BAR LATCHES.SDR MWEA97133Evac Slide · fell offCREW REPORTS, GALLEY DOOR ESCAPE SLIDE CAME OFF WHEN REMOVING GIRT BAR. MAINT REINSTALLED GALLEY DOOR ESCAPE SLIDE.SDR MWEA97132Girt Bar Latches · dirtyDURING INSPECTION, FOUND GALLEY DOOR EVAC SLIDE GIRT BAR LATCHES STICKING. MAINT CLEANED AND LUBED LATCHES.SDR GTIA9700247Tire · failedEWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REMOVED AND REPLACED MAIN SDR ABXA9701239Tab · delaminatedRUDDER TAB FOUND TO BE DELAMINATED. REMOVED AND REPLACED SKIN, HONEYCOMB CORE AND INTERNAL DOUBLERS, IAW DC-9 SRM.SDR ABXA9700343Fitting · corrodedDURING C INSPECTION, FOUND THE RIGHT WING FLAP HINGE ATTACH STUDS AND BRACKET CORRODED, AT XRS164. REPLACED HINGE FITTING AND STUDS IAW DC9 MAINTENANCE MANUAL CHAPTERS 57-40-1 AND 27-51-01.SDR ABXA9700341Studs · corrodedDURING C INSPECTION, FOUND THE RIGHT WING FLAP CENTER HINGE ATTACH STUDS NOT ENCAPSULATED AND CORRODED AT XRS267. REPLACED FLAP HINGE ATTACH STUDS IAW DC-9 MAINTENANCE MANUAL CHAPTERS 57-40-1 AND 27-51-01.SDR 97ZZZM485Tire · failedEWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REMOVED AND REPLACED MAIN SDR 9705429940Clip · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR GTIA9700234Air Data Comp · malfunctionedYIP - REF DME NR 00127 (MRR NR 97-01-27-003/GTIA9700147). AUTOPILOT PORPOISES IN ALL FLIGHT MODES (CLIMB, CRUISE, DESCENT, STABILIZED FLIGHT). FUNCTIONAL CHECK PERFORMED IAW DC-9 MM 22-10-0. READ WIRING TO PITCH CHANNELS. REMOVED AND REPLACED AIR DATA COMPSDR ABXA9700385Skin · excess blendoutDURING C INSPECTION, FOUND A DEEP BLENDOUT ON NR 1 SLAT DRIVE TRACK CUTOUT IN LEADING EDGE SKIN. REPAIRED IAW ABX REA D957-18774.SDR ABXA9700931Spoiler · corrodedLEFT OUTBOARD SPOILER CORRODED AND CRACKED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.SDR ABXA9700344Rib · crackedDURING C INSPECTION, FOUND A RIGHT WING LEADING EDGE RIB CRACKED, INBOARD OF NR 7 SLAT TRACK. REPAIRED RIB IAW ABX REA D957-18711 AND DC-9 SRM CHAPTER 57-06A FIGURE 5 SHEET 1.SDR ABXA9700068Frame · crackedDURING C-CHECK INSPECTION, FOUND SEVERE DENT AND CRACK AT STATION 945, LONGERON 5 RT. INSTALLED NEW FRAME SEGEMENT AT STATION 945 IAW DC9 SRM 51-30-02, 51-30-05.SDR VJ970173Skin · corrodedDURING DROP IN MAINTENANCE INSPECTION, FOUND CORROSION AROUND FLUSH MOUNTED ANTENNA AT F/S 395 AT 6 O'CLOCK POSITION WITH POPPED RIVET HEADS. CUT OUT DAMAGED AREA. REMOVED AND REPLACED ANTENNA DOUBLER, P/N 5911412-53N. FABRICATED FINGER DOUBLERS, FILLERS ANSDR CALA9700358Support · crackedINSPECTION FOUND A 2 INCH CRACK IN AFT PIT PANEL SUPPORT AT STA 870 BETWEEN LONGERON 29 AND 30R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5320-01263.SDR CALA9700357Support · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM PANEL SUPPORT IN AFT PIT AT STA 897, A/C CENTERLINE. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01-02.SDR CALA9700356Strap · corrodedINSPECTION FOUND CORROSION ON TOP OF BELT FRAME STRAP IN AFT PIT AT STA 897 BETWEEN LONGERON 27 AND 29L. THE STRAP WAS REPLACED IAW SRM 51-30-2.SDR ABXA9700352Bracket · crackedDURING C INSPECTION, FOUND A SUPPORT FORWARD OF CANTED FRAME, AT FS 1168, CRACKED AT 7 O'CLOCK POS. REPLACED SUPOORT BRACKET IAW DC-9 SRM CHAPTER 51-30-5.SDR 9705369920Control Unit · malfunctionedRIGHT ICE PROTECTION TEMPERATURE LOW LIGHT REMAINED ON AFTER TAKEOFF WITH AIRFOIL ICE PROTECTION SYSTEM ACTIVATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ELECTRONIC THERMAL CONTROL UNIT, LOW TEMPERATURE SENSOR, AND LOWSDR 9705339921Battery Pack · dischargedOVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR 9705289985Wire · looseTAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 20 KNOTS AND RETURNED TO GATE. MAINTENANCE REPAIRED LOOSE WIRE AT HORIZONTAL STABILIZER POSITION SWITCH IN FORWARD BAG BIN. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR CALA9700362Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN L-ANGLE AT STA 756, LONGERON 28R. ALSO, A .5 INCH CRACK WAS FOUND IN L-ANGLE AT STA 756, LONGERON 28L. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-0.SDR ABXA9700935Tab · delaminatedRIGHT ELEVATOR TAB FOUND TO HAVE SEVERE DELAMINATION, BOTH UPPER AND LOWER MID-SURFACE. REPLACED SKIN, HONEYCOMB CORE AND INTERNAL DOUBLERS.SDR ABXA9700353Longeron · crackedDURING C INSPECTION, FOUND LONGERON 3 CRACKED AT FS 160. REPLACED SECTION OF LONGERON AT FS 160 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5 ALSO 53-02 FIGURE 2.SDR ABXA9700349Web · crackedDURING C INSPECTION, FOUND THE RIGHT WING TRAILING EDGE AFT VERTICAL WEB CRACKED AT RIGHT OUTBOARD SPOILER REACTION ARM. REPAIRED CRACK IAW DC-9 SRM CHAPTER 57-01, FIGURE 3 SHEET 2.SDR ABXA9700301Skin · crackedDURING C INSPECTION, FOUND THE VERTICAL STABILIZER SKIN GOUGED, CRACKED AND PUNCTURED ON RIGHT SIDE NEAR THE JACK SCREW. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-10-8.SDR ABXA9700057Window · lack of lubeCAPTAIN'S SLIDING WINDOW VERY HARD TO OPEN AND GREASE ON LINKAGE. LUBED CAPTAIN'S CLEARVIEW WINDOW AND CHECKED RIG IAW DC-9 MM 56-10-3.SDR 9705199615Fitting · corrodedDURING M-CHECK AND PRIOR TO ENTERING SERVICE, FOUND CORROSION ON FLOOR SUPPORT FITTING AT FS 813 BETWEEN LONGERONS 27R AND 28R. REPLACED FITTING PER SRM 51-30-01.SDR 9705189615Fitting · corrodedDURING M-CHECK AND PRIOR TO ENTERING SERVICE, FOUND CORROSION IN FLOOR SUPPORT FITTING AT FS 813 BETWEEN LONGERONS 27L AND 28L. REPLACED FITTING PER SRM 51-30-01.SDR MWEA97126Coalescer Bag · dirtyPILOT REPORTS WITH RIGHT PACK RECEIVING AIR FROM APU THE SMALL OF HOT PLASTIC WAS DETECTED IN FWD GALLEY AREA. MAINTENANCE REMOVED AND REPLACED RIGHT WATER SEPARATOR SOCK, NO MORE SMELL NOTED.SDR GTIA9700246Switch · failedMDW - FLT 1704 - AFTER PUSH BACK AT MYR, SPOILER DEPLOYED LIGHT ILLUMINATED, ACCOMPLISHED PROCEDURE AS PER MEL 27-32, CONTINUED FLIGHT AS PER MEL. LIGHT EXTINGUISHED AFTER TAKEOFF AND NEVER RE-ILLUMINATED. TRANSFERRED TO DMI LOG NR 00252 IAW DC-9 MEL 27-32 CSDR GTIA9700231Warning Light · illuminatedMDW - FLT 1701 - AFTER PUSH-BACK AT MYR, SPOILER DEPLOYED, LIGHT ILLUMINATED. ACCOMPLISHED PROCEDURE PER MEL 27-32, CONTINUED FLIGHT PER MEL. LIGHT EXTINGUISHED AFTER TAKEOFF AND NEVER RE-ILLUMINATED. TRANSFERRED TO DMI LOG NR 00252 IAW DC-9 MEL 27-32 CAT 'SDR GTIA9700230Press System · malfunctionedBOS - FLT 248 - ON TAKEOFF, AUTO PORTION OF CABIN PRESSURIZATION DID NOT WORK. MANUAL WORKED WELL FOR REMAINDER OF FLIGHT USING FCOM PROCEDURES. DEFERRED PER MEL 21-24. MX CONTROL AUTHORIZED DMI NR 00250 CAT 'C'. (X)SDR GTIA9700166Connector · looseDTW - REPLACED ROLL COMPTER FOR AUTO-PILOT TROUBLESHOOTING. REPLACE PITCH COMPUTER CANNON PLUG FOR AUTO-PILOT SYSTEM TROUBLESHOOTING. REF DMI NR 00196 AUTO-PILOT WILL NOT ENGAGE WITH ELEVATOR SERVO ON. REMOVED AND REPLACED AUTO-PILOT ROLL COMPUTER, AUTO-PILSDR GTIA9700159Roll Computer · malfunctionedDTW - REPLACED ROLL COMPUTER FOR AUTO-PILOT TROUBLESHOOTING. REPLACE PITCH COMPUTER CANNON PLUG FOR AUTO-PILOT SYSTEM TROUBLESHOOTING. REF DMI NR 00196 AUTO-PILOT WILL NOT ENGAGE WITH ELEVATOR SERVO ON. REMOVED AND REPLACED AUTO-PILOT ROLL COMPUTER, AUTO-PISDR CALA9700435Intercostal · crackedINSPECTION FOUND A 1.75 INCH CRACK IN FORWARD BAGGAGE BIN INTERCOSTAL FROM STA 351 TO 370, LONGERON 29L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9700434Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FLOOR SUPPORT AT STA 446, LONGERON 26R. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.SDR CALA9700433Floor Support · crackedINSPECTION FOUND A .75 INCH CRACK IN FORWARD BAGGAGE BIN FLOOR SUPPORT AT STA 313, LONGERON 30. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01263.
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