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 MWEA011112Splice · corrodedAFT CARGO STATION 899 FRAME SPLICE TOP PLATE HAS LIGHT CORROSION IN TWO SPOTS. FABRICATED AND INSTALLED NEW FRAME SPLICE.SDR MWEA011111Fitting · crackedAFT CARGO DOOR BEAM NR 4 AFT END FITTING IS CRACKED. REMOVED CRACKED BRACKET, LOCATED, DRILLED AND INSTALLED NEW BRACKET AND SHIM.SDR MWEA011110Seat Track · corrodedNR 3 SEAT TRACK CORRODED STATION 200-206. REMOVED CORROSION, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK.SDR MWEA011109Seat Track · corrodedNR 4 SEAT TRACK IS CORRODED AND HAS SOME TOOL MARKS STATION 218-237. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF SEAT TRACK.SDR 0103859612Floorbeam · crackedDURING AN HCK IN ATL, TWO CRACKS WERE FOUND IN THE VERTICAL WEB OF THE STA 237 FLOORBEAM. THE CRACKS ARE AT X=6 AND ARE APPROXIMATELY 1" LONG. THE CRACK ENDS ARE STOPPED DRILLED AND DOUBLER INSTALLED. 7075-T6511. REPAIRED PER EA 96-185017.SDR MWEA011097Transducer · failedWINDSHEAR AND STALL INDICATION FAILURE ANNUNCIATOR LIGHTS CAME ON WHEN AIRCRAFT WAS IN FLIGHT MODE. BOTH LIGHTS EXTINGUISHED AT GROUND SHIFT MODE. REMOVED AND REPLACE RIGHT, AND LATER LEFT, ANGLE OF ATTACK TRANSDUCERS.SDR MWEA011094Support Bracket · crackedRIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT BRACKET IS CRACKED. -- REMOVED SUPPORT BRACKET, INSTALLED NEW SUPPORT BRACKET.SDR MWEA011093Pan · tornFORWARD CARGO DOOR INNER PAN IS TORN BY A BN FASTENER AT THE AFT END AT BEAM #3. -- REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR. DOUBLER.SDR MWEA011092Longeron · crackedLONGERON 17 CRACKED AT STATION 965 LEFT SIDE VIEWABLE WITH MIRROR ON BOTTOM SIDE. -- REMOVED DAMAGED LONGERON SECTION, FABRICATED NEW SECTION AND LONGERON SPLICE, INSTALLED LONGERON ASSOCIATED ITEMS AND LONGERON SPLICE.SDR CA010906016Controller · failed(CAN) AT FL 330 "CABIN PRESURE" WARNING LIGHT ILLUMINATED. CABIN UNCONTROLLABLE, RAPID CABIN DESCENT CARRIED OUT. CABIN LIGHT WENT OUT THROUGH FL 200 BUT CABIN ALT SHOWING FL 300. ALSO, BOTH LAVATORIES DETECTORS CAME ON WITH NO VISIBLE SMOKE. CABIN RESSURE CONSDR 0103849612Elevator · crackedDuring Hck in Atl the RH elevator skin at XET=167 was found cracked at the outboard end where the gear tab fairing is attached . Doubler made of 2014-t6 elevator assembly 5910411-526 s/n 00397. Repaired per EA 96-185011.SDR 0103839612Frame · crackedDuring an Hck in Atl, a crack was found on the RH MLG door hinge support frame at sta 737. The crack stopped at a fastener hole and is .5" long. Material 7075-t6, repaired per EA 96-181352.SDR MWEA011079Shear Tie · crackedSHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 14 AND 15 RIGHT SIDE. -- REMOVED SHEAR TIE SECTION, FABRICATED NEW SECTION AND SHEAR TIE SPLICE, INSTALLED NEW SHEAR TIE SECTION AND SPLICE.SDR MWEA011078Rib · crackedLEFT WING #3 SLAT DRIVER OUTBOARD FITTING HAS A SMALL 1/8" CRACK ACROSS THE SIDE TO SIDE GUIDE ROLLER LOBE. -- REMOVED CRACKED RIB, LOCATED BOTH INBOARD AND OUTBOARD FITTING, INSTALLED RIB.SDR 0104979922Pan · crackedDuring M-ck in ATL, a crack was found at station 937 between longerons 26R and 27R. The crack was between marked holes "c" and "d" on the doorjamb pan. EA 99-181313SDR 0104549922Spar · corrodedDuring an Mck in ATL, Corrosion was found in the left and right upper beaver tails. The Beaver tails were removed to accomplish corrosion removal. After the beaver tail removal it was noted that 11 fasteners common to the pylon spar were elongated. Repaired peSDR 0104529922Pan · crackedDuring Mck in ATL, A crack was found between 2 fasteners in the aft cargo doorjamb pan at sta 937, between longerons 26r and 27r. Material .050" 2024-t42 AL, and .090"2024-t42 AL. Repaired per EA 99-181313.SDR 0103199922Skin · damagedDURING AN M-CHECK IN ATL, CORROSION WAS FOUND IN THE LEFT AND RIGHT UPPER BEAVER TAILS, P/N 5923937-501/502. THE BEAVER TAILS WERE REMOVED TO ACCOMPLISH CORROSION REMOVAL. AFTER THE BEAVER TAIL REMOVAL, IT WAS NOTED THAT 11 FASTENER HOLES COMMON TO THE PYLONSDR 0104989922Skin · crackedDuring MCK in ATL, a 1/4" long crack was found in the fuselage skin at staion 1019, between longerons 14L and 15L. The crack emanated from one fastener hole common to the upper attach angle and was removed using 1" diameter cut out. This EA provides instructioSDR 0104539922Skin · crackedDuring Mck in ATL a .25" crack was found in the fuselage skin at sta 1019, between longerons 14L and 15L. The crack emanated from one fastener hole common to the pylon upper attach angle and was removed using a 1" diameter cut out. Material .032 TI-6AI-4v. RepSDR MWEA011075Fitting · wornDURING CLIMB 17,000 FEET, GEAR DOOR LIGHT CAME ON, SO MAINTENANCE CONTROL DIVERTED AIRCRAFT TO MILWAUKEE MAINTENANCE BASE. REMOVED AND REPLACED LEFT AND RIGHT MAIN GEAR DOOR SENSORS, AND LEFT MAIN GEAR FITTING.SDR 0102609925Separator · malfunctionedAFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO MEM WITH AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE RIGHT WATER SEPARATOR. INSPECTED TAIL. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVISDR MWEA011066Fitting · crackedCRACK INDICATION ON OUT DOOR PAN UPPER SIDE OF #1 AFT DOOR STOP OF FORWARD CARGO DOOR. -- STOP DRILLED CRACK AND FABRICATED DOUBLER, LOCATED, DRILLED AND DEBURRED NEW STOP FITTING, INSTALLED STOP FITTING AND DOUBLER.SDR AT0100216Battery Pack · inoperativeFOUND EMERGENCY LIGHTS AT ROWS 18 AND 22 FAILED TEST. CORRECTIVE ACTION: REPLACED BATTERIES IN BATTERY PACK B5-26. IAW DC9 MM 33-50SDR 0104999922Door Frame · crackedDuring an MCK in ATL, a .8" crack was found while accomplishing inspection of the lower aft corner of the forward cargo door doorjamb. This EA. 99-181281 provides repair of area. Material .050" 2014-t6 and .090" 2014-t6.SDR 0104949917Angle · corrodedDuring Hck in ATL, corrosion was found on the horizontal flange of the fuselage cusp angle at station 120. Repair Material .071 7075-t6 Aluminum and .020" 7075-t6 Aluminum. Repaired per EA 99-181362.SDR 0104569922Door Frame · crackedDURING M-CK IN ATL, A .8 INCH CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-181281.SDR 0104519917Angle · corrodedDuring Hck in ATL, Corrosion was found on the horizontal flange of the fuselage cusp angle at sta 120. Due to depth of corrosion, it was elected to trim the flange to remove the damaged area. Material .071 7075-t6 AL, .020 7075-t6 Al. Repaired per EA 99-181362SDR 0104479922Door Frame · crackedDURING M-CK IN ATL, A .8 INCH CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-181281.SDR 0103099917Angle · corrodedDURING AN H CHECK IN ATLANTA, CORROSION WAS FOUND ON THE HORIZONTAL FLANGE OF THE FUSELAGE CUSP ANGLE AT STATION 120 (RT). DUE TO DEPTH OF CORROSION, IT WAS ELECTED TO TRIM THE FLANGE TO REMOVE THE DAMAGED AREA AND REPAIR ACCOMPLISHED PER EA 99-181362 LOG PAGSDR ABXA010405Actuator · brokenSPLIT FLAP INDICATION FROM 15 DEGREES TO ZERO DEGREES. MECHANICS FOUND THE LEFT OUTBOARD FLAP ACTUATOR WITH BROKEN MOUNTING EAR. REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IAW DC-9 AMM 27-52-02-2-0001. NO LEAKS NOTED.SDR AT0100215Battery Pack · inoperativeFOUND B5-28 FAILED TO OPERATE AFT ACCESSERY EMERGENCY LIGHTS. CORRECTIVE ACTION: REPLACED B5-28. IAW DC9 MM 33-50SDR 0103139922Spar · damagedDURING AN M-CHECK SHOP VISIT AT ATL MAINTENANCE BASE WHILE REMOVING THE FRONT SPAR FOR REPLACEMENT, SEVERAL FASTENER HOLES ON THE UPPER AND LOWER SKIN ASSEMBLY WERE FOUND TO BE DAMAGED (TOOLING DAMAGE). REPAIR TO DAMAGED SKIN ASSEMBLY WAS ACCOMPLISHED PER SECSDR MWEA011090Rib · gougedGOUGE ON INBOARD SLAT SUPPORT TRACK STATION 480.871. REMOVED AND REPLACED RIB.SDR MWEA011089Skin · crackedRIGHT WING SLAT DOOR CUT OUT BETWEEN NR 4 AND NR 5 SLAT SKIN IS CRACKED. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER.SDR MWEA011087Longeron · damagedLONGERON 6 RIGHT DAMAGED BETWEEN STATION 503 AND 522. BLENDED DAMAGED AND ATTACHED SPLICE PLATE OVER DAMAGE.SDR ABXA010406Control Rod · malfunctionedNR 1 THRUST REVERSER UNLOCKED BUT DID NOT DEPLOY. REPLACED THE NR 1 THRUST REVERSER UNLOCK CONTROL ROD ASSEMBLY. COMPLIED WITH ADJUSTMENT TEST OF NR 1 THRUST REVERSER SYSTEM IAW DC-9 MM. OPS CHECKED GOOD.SDR ABXA010404Power Supply · dischargedEMERGENCY OVERHEAD LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.SDR ABXA010401Rod End · brokenRIGHT WING LEADING EDGE SLAT ACTUATOR ROD END BROKEN. REPLACED THE RIGHT WING LOWER SLAT ACTUATOR ROD END IAW DC-9 MM 27-80-05-2-10. OPS CHECKED GOOD.SDR 0103129922Door Frame · damagedDURING M-CHECK AT ATL AND WHILE ACCOMPLISHING A DOORJAMB PAN SPLICE REPAIR PER SRM 53-05, FIG 44, EIGHT .1875 INCH DIA HOLES WERE FOUND WITH SHORT ON-CENTER DISTANCE IN THE VERTICAL FLANGE OF FRAME STA 896 P/N 9958214-29 AS SHOWN IN FIGURE 1. THE FASTENER HOLSDR MWEA011058Pump · inoperativeRIGHT ENGINE HYDRAULIC PUMP WOULD NOT PRODUCE OVER 1,500 PSI, RETURNED TO GATE. -- DEFERRED, REMOVED AND REPLACED PUMP.SDR MWEA011050Doubler · crackedAFT ACCESSORY COMPARTMENT SHEAR TIE DOUBLER AT FRAME STATION 1019 AT LONGERON 14 LEFT IS CRACKED. -- REMOVED SHEAR TIE DOUBLER, FABRICATED AND INSTALLED NEW SHEAR TIE DOUBLER.SDR MWEA011049Rib · corrodedRIGHT WING NR 1 SLAT INBOARD IDLER TRACK, OUTBOARD RIB HAS EXFOLIATION CORROSION AROUND TRACK DOOR FORWARD HINGE BOSS. REMOVED CORROSION, DRILLED NEW INBOARD AND OUTBOARD IDLER TRACK RIBS, INSTALLED NEW INBOARD AND OUTBOARD IDLER TRACK RIBS. LEVEL 2 CORROSION.SDR AT0100225Smoke Detector · malfunctionedFORWARD CARGO FIRE DETECTOR LIGHT ILLUMINATED WITH THE MASTER CAUTION LIGHT. EMERGENCY WAS DECLARED AND NR 2 FIRE BOTTLE WAS DISCHARGED AND AFT TAIL CONE SLIDE WAS DEPLOYED. INSPECTED THE FORWARD CARGO, E & E, FORWARD CABIN, AND COCKPIT AREAS FOR EVIDENCE OFSDR AT0100220Door · openLOUD RUMBLE AFTER TAKE-OFF. CORRECTIVE ACTION: INSPECTED NOSE LANDING GEAR DOOR LINKAGE, HINGES AND NO DEFECTES NOTED. CLOSED NOSE LANDING GEAR DOOR AND CONFIRMED LATCH CHECK. IAW DC9 MM 32-00, 52-00SDR 0104969922Spar · corrodedDuring Mck in ATL, corrosion was found in the left and right beaver tails. The beaver tails were removed to accomplish corrosion removal. After the beaver tail removal, it was noted that 11 fastener holes common to the pylon front spar were elongated on each sSDR 0103119922Frame · damagedDURING AN M1-CHECK IN ATL, STATION 579 FRAME REINFORCEMENT STRAPS 2800206-8 AND -9 WERE CUT FOR ACCESS AT LOCATION BETWEEN L-28 LT AND L-29 RT. ADDITIONAL DAMAGE WAS FOUND AT L-24 RT ON STRAP 2800206-8. THE EA 99-181344 (LOG PAGE 1640709) PROVIDES A SPLICE RSDR ABXA010384Switch · defectiveUPON GEAR RETRACTION, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR WAS RECYCLED PER ABNORMALS AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED WITH THE GEAR EXTENDED ALSO. REPLACED THE RIGHT MAIN LANDING GEAR DOOR SWITCH IAW DC-9 MM 32-60SDR CA010727026Transmitter · failed(CAN) STALL WARNING OCCURRED SEVERAL TIMES DURING APPROACH WITH SPEED ABOVE 220 KTS. REPLACED FLAP POSITION TRANSMITTER.SDR 0105019922Intercostal · crackedDuring MCK in ATL, a crack was found in the outboard end of intercostal 9923484-9 at sta 180 and at X=-20. Repaired per EA 99-1813231.
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