Douglas DC-9-32

Service difficulty reports · 12,755

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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.

SDR AT0200048Slide · out of positionR1 DOOR SLIDE OFF. REINSTALLED R1 DOOR SLIDE PACK.Apr 10, 2002 · N867AT · Doug DC932 · Escape SlideSDR AT0200047Actuator · stickingFORWARD NOSE GEAR DOOR REMAINED OPEN ON DEPARTURE/BURNED DOWN FUEL, RETURNED TO BASE. FOUND NOSE GEAR DOOR MANUAL ACTUATOR STICKING, LUBED ACTUATOR AND MANUALLY OPERATION PERFORMED GOOD, AIRCRAFT GOOD TO CONTINUE IAW M/M 32-00 AND 12-90.Apr 9, 2002 · N866AT · Doug DC932 · Landing Gear Door ActuatorSDR 0201269611Pressure Panel · corrodedDuring Hck at ATL, corrosion was found on the APB WEB at L26R. The corrosion was found within Blue Print tolerance. Repaired per EA 96-188478.Apr 8, 2002 · N611NA · Doug DC932 · Fuselage Main, StructureSDR 0201259611Skin · corrodedDURING HCK IN ATL, CORROSION WAS FOUND ON THE LEADING EDGE OF LT WING. DAMAGE WAS TRIMMED OUT AND REPAIR WAS ACCOMPLISHED PER EA 96-188468.Apr 8, 2002 · N611NA · Doug DC932 · Wing, Plate/SkinSDR MWEA020224Skin · corrodedLEFT FLAP LOWER SKIN HAS A SMALL AREA OF CORROSION ABOUT 20 INCHES OUTBOARD OF INBOARD FLAP HINGE. FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLERS.Apr 8, 2002 · N501ME · Doug DC932 · Trailing Edge FlapsSDR AT0200046Duct · tornAIRCRAFT WOULD NOT MAINTAIN CABIN ALTITUDE/PRESSURE IN AUTOMATIC OR MANUAL MADE AT FL290. A/C DESCENDED LOWER TO ENABLE MANUAL PRESURIZATION; THUS NORMAL/OPTIMUM CABIN ALT/PRESSURE FOR CREW AND PASSENGERS. ALL MASKS FELL. CORRECTIVE ACTION: Apr 8, 2002 · N819AT · Doug DC932 · Cabin Pressure Control SystemSDR MWEA020222Angle · crackedVERTICAL STABILIZER LEADING EDGE TAIL TO FUSELAGE DORSAL INTERNAL ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET.Apr 8, 2002 · N206ME · Doug DC932 · Vertical Stabilizer Miscellaneous StructureSDR MWEA020223Web · out of toleranceREMOVAL AFT CARGO DOOR JAMB LOWER INNER WEB TO FACILITATE OTHER MAINTENANCE. -- OLD WEB FOUND OUT OF LIMITS. INSTALLED NEW WEB.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020221Former · crackedFORMER AT STATION 237 LONGERON 18 LEFT TO 17 LEFT IS CRACKED. -- FABRICATED AND INSTALLED SHIM TO ACHIEVE EDGE DISTANCE.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020219Web · misdrilledFORWARD CARGO DOOR JAMB WEB AND FRAME AT 427 HAS A DOUBLE DRILLED HOLE BETWEEN LONGERON 29 RIGHT AND LONGERON 28 RIGHT. -- FABRICATED AND INSTALLED REPAIR STRAP AND WEB REPAIR DOUBLER.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020217Angle · brokenCORROSION ON LOWER LEG FORWARD SIDE OF ELECTRONIC POWER CENTER PANEL SUPPORT FROM COCKPIT DOOR JAMB TO BANANA PANEL. FOUND ANGLE CRACKED OFF. REMOVED AND REPLACED ANGLE.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020216Skin · damagedFUSELAGE CLASS III DOUBLER NEEDS UPGRADE AT STATION 218 LONGERON 25 LEFT. REMOVED DOUBLER, VERIFIED AS NO CRACKS IN SKIN. INSTALLED DOUBLER. REPAIR PLACED ON WATCH ITEM 6712 FOR REINSPECTION PER SRM 53-04 FIGURE 12B.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020215Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND-OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER.Apr 8, 2002 · N206ME · Doug DC932 · Horizontal Stabilizer, Plate/SkinSDR MWEA020214Skin · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER.Apr 8, 2002 · N206ME · Doug DC932 · Horizontal Stabilizer, Plate/SkinSDR MWEA020213Intercostal · crackedFORWARD CARGO DOOR, INTERCOSTAL CRACKED, LOWER AFT AREA OF DOOR. -- REMOVED AND REPLACED INTERCOSTAL.Apr 8, 2002 · N206ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020212Doubler · blownAFT CARGO COMPARTMENT DOUBLER AROUND THE SUGAR SCOOP IS BLOWN OUT ON THE BOTTOM AFT AREA AT STATION 965 ABOVE LONGERON 22 LEFT. -- REMOVED DOUBLER. DRILLED UP AND TRIMMED DOUBLER TO FIT IAW SRM 51-10-4 DAC DRAWING 5914558. INSTALLED DOUBLER.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020211Longeron · blownAFT CARGO COMPARTMENT HAS A LONGERON BLOWN OUT IN THE CENTER OF LONGERON 23 LEFT AT STATION 945. -- FABRICATED AND INSTALLED STRAP.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020210Panel · damagedREMOVED CABIN FLOOR PANEL B-5 TO FACILITATE OTHER MAINTENANCE. -- FORWARD END OF PANEL IS DAMAGED. FABRICATED NEW SKIN AND REINSTALLED CABIN FLOOR PANEL.Apr 8, 2002 · N206ME · Doug DC932 · Fuselage Floor PanelSDR 0201119925Wheel · failedTHE LEFT OUTBOARD ANTI-SKID LIGHT ILLUMINATED DURING TAKEOFF ROLL AT FAR. CLIMBOUT AND GEAR RETRACTION WERE NORMAL. LANDING WAS UNEVENTFUL AT MSP BUT CREW THOUGHT THE AIRCRAFT WAS A LITTLE HARD TO TAXI. SUSPECTED A FLAT TIRE OR A DRAGGING BRAKE. NO TIRE WAApr 7, 2002 · N925US · Doug DC932 · Wheel/Ski/FloatSDR MWEA020209Connector · dirtyLOCALIZER FLAGS ON BOTH NAV 1 AND NAV 2 FROM TWO DIFFERENT APPROACHES WITH TWO DIFFERENT FREQUENCYS. DISCONNECTED NR 1 AND 2 NAV ANTENNAS AND CLEANED. PERFORMED OPS CHECK OF FLIGHT DIRECTOR SYSTEM WITH LOCAL FREQUENCY AND WITH NAV TESTER. SYSTEM OPERATIONS Apr 7, 2002 · N602ME · Doug DC932 · Localizer/VOR SystemSDR AT0200057Skin · crackedLT ELEVATOR UPPER SKIN IS CRACKED AT I/B END. STOP DRILLED ENDS OF CRACK, LT ELEVATOR UPPER SKIN AT I/B END AS PER DC9 SRM 55-03. ACCOMPLISHED HFEC ON CRACK PER NDT SPM 06-00-07; CRACK CONTAINED. INSTALLED REPAIR DOUBLER AS PER DC9 SRM 55-03, FIGURE 15.Apr 5, 2002 · N834AT · Doug DC932 · Elevator, Plate/SkinSDR 0201249611Pressure Panel · crackedDuring an Hck in ATl, three cracks were found in the flight compartment pressure panel at station 105. The cracks are located at x=25 1.5" long x=35 2.3" long and x=-35 2.4" long. Repaired per EA 96-188455.Apr 5, 2002 · N611NA · Doug DC932 · Fuselage Main, StructureSDR AT0200045Rod End · out of adjustAFTER TAKEOFF NOSE LANDING GEAR FAILED TO RETRACT. ADJUSTED NOSE LANDING GEAR RETRACT CYLINDER ROD END AND PERFORMED LANDING GEAR SYSTEM RETRACT AND EXTENSION TEST PER DC9 MM 32-32-6 AND 32-30-0. ALL INDICATIONS AND OPERATIONS NORMAL.Apr 5, 2002 · N832AT · Doug DC932 · Landing Gear Retraction/Extension SystemSDR AT0200059Skin · corrodedEXTERIOR FUSELAGE SKIN IS BULGED JUST FORWARD OF STA 996 AT STR 25L AND 23L. REMOVED FASTENERS AND TIE FITTING 25L AT STA 996. REMOVED CORROSION, OUT OF LIMITS. REMOVED TIE FITTING 25L. REMOVED CORROSION. REMOVED SHIM BELOW FITTING 25L. SHIM CORRODED OUTApr 4, 2002 · N834AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0200056Bulkhead · corrodedAFT CARGO COMPARTMENT, AFT PRESSURE BULKHEAD LOWER T-CHORD CORROSION BETWEEN STR 29 LEFT TO STR 29 RIGHT BS 996. REMOVED STIFFENER AT LONG 28 RIGHT AND LEFT FOR ACCESS AND REMOVED LEFT ANGLE BS 996 LONG 29R TO 29L. CUT OUT VERTICAL WEB STA 996 (INTERIOR) FORApr 4, 2002 · N834AT · Doug DC932 · Fuselage Main, BulkheadSDR AT0200044Cylinder · malfunctionedNOSE GEAR INDICATED NO RETRACTION AFTER TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR CYLINDER, OPS AND LEAK CHECK GOOD IAW DC-9 MM 32-3-6.Apr 4, 2002 · N832AT · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA010816Rod · out of adjustCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER HOOK NOT CLEARING TO ALLOW WINDOW TO OPEN. ADJUSTED UPPER ROD WINDOW IAW DC-9 MM, OPS CHECKED GOOD.Apr 4, 2002 · N939AX · Doug DC932 · Flight Compartment WindowsSDR AT0200043Battery Pack · burnedDURING CRUISE AN ELECTICAL SMELL WAS REPORTED IN AFT CABIN, SMELL DISIPATED BUT STILL PRESENT. CORRECTIVE ACTION: AFT RIGHT LAVATORY EMERGENCY BATTERY PACK OVERHEATED. REMOVED AND REPLACED BATTERY PACK. OPS CHECK O.K. IAW MM 33-00.Apr 4, 2002 · N823AT · Doug DC932 · Emergency LightingSDR AT0200058Door Frame · crackedFORWARD CARGO DOOR CUTOUT BETWEEN LOWER DOOR STOP FITTINGS HAS CRACKS ON FLANGE OF VERTICAL FRAME AND HAS BULGING (EVIDENCE OF CORROSION). REMOVED FASTENERS AND CORROSION, MATERIAL LOSS BEYOND LIMITS. REMOVED LOWER PAN AT FORWARD CARGO DOOR. REMOVED LOWER DApr 3, 2002 · N834AT · Doug DC932 · Fuselage Main, StructureSDR ABXA010817Jackscrew · corrodedVISUAL INSPECTION OF THE JACKSCREW ASSEMBLY THREADED AREA SHOWED PITTING ALONG TOP FLANGE OF THREADS. REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01-4-001.Apr 2, 2002 · N981AX · Doug DC932 · Stabilizer Control SystemSDR MEX2002092A/C Pack · malfunctionedFLT 115 - HMO-MEX - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF PRESSURIZATION PROBLEMS. BOTH AIR CONDITIONING PACKAGES FAIL DURING FLIGHT, RECOVERING LEFT PACKAGE DURING DESCENT. CHECKED THE OPERATION OF THE PRESSURIZATION CONTROL VALVE AND CONTROLLERS Mar 30, 2002 · N1003P · Doug DC932 · Cabin Cooling SystemSDR GTIA020273Adc · faultyFLT 616 - ACY - AUTO PILOT PITCH CONTROL PORPOISES DURING CLIMB AND DESCENTS AND WILL NOT HOLD ALTITUDE ALL OTHER FUNCTIONS OK FLT 616. REMOVED AND REPLACED AIR DATA COMPUTER PERFORMED PITOT STATIC LEAK CHECK. GROUND CHECK OK AT THIS TIME. (M)Mar 30, 2002 · N12536 · Doug DC932 · Air Data ComputerSDR 0201089919Line · looseWHILE CRUISING AT FL260 WITH ENGINE AND AIRFOIL ANTI-ICE ON, THE CABIN BEGAN A 500 FPM CLIMB. PACK SUPPLY PRESSURE INDICATED 25 PSI ON BOTH PACKS. TURNING OFF THE ANTI-ICE SYSTEM, RESETTING PACK TO MANUAL, AND CLOSING THE OUTFLOW VALVE DID NOT STOP THE PRESSURMar 30, 2002 · N941N · Doug DC932 · Cabin Cooling SystemSDR 0200949602Spar Cap · crackedDuring Hck in ATL, the L/H wing spar revealed corrosion in the lower spar cap at the inbd and outbd attach holes for the flap hinge fitting. A .625 crack was found at the inboard hole. Repaired per EA 96-188409.Mar 27, 2002 · N602NW · Doug DC932 · Wing SparSDR MWEA020194Panel · damagedDENT DAMAGE ON RUDDER LEADING EDGE STRUCTURE AT STATION ZR70 RIGHT SIDE. MEASURES APPROX 4 INCHES IN LENGTH. FABRICATED AND INSTALLED REPAIR.Mar 27, 2002 · N206ME · Doug DC932 · Rudder, Plate/SkinSDR MWEA020195Gusset · corrodedGUSSET AT STATION 580 IS CORRODED ON INTERCOSTAL. -- FABRICATED AND INSTALLED GUSSET.Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020193Fitting · misdrilledFITTINGS MISDRILLED AT STATION 207 (INTERCOSTAL ATTACH CLIP). -- FABRICATED AND INSTALLED NEW FITTING. LOCATED AND PRIMED AND INSTALLED PARTS.Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020192Fitting · damagedREMOVED FLOOR BEAM END FITTING AT CUSP, STATION 218 LEFT SIDE TO FACILITATE OTHER MAINTENANCE. -- FITTING DAMAGED UPON REMOVAL. INSTALLED NEW FITTING.Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020191Angle · corrodedCORROSION ON CELING IN E&E BAY FROM STATION 200 TO 218 JUST BELOW THE CUSP LINE NEAR LONGERON 18 LEFT. REMOVED DAMAGED SECTION OF UPPER CUSP ANGLE. FABRICATED AND FORMED -3 REPAIR SPLICE. INSTALLED CUSP ANGLE AND SPLICE.Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020190Intercostal · improperFORWARD PIT INTERCOASTAL LOCATED BETWEEN LONGERON 28 RIGHT AND 27 RIGHT AND FRAMES 560-579 HAS SEVERAL DIVETS IMPROPERLY BACKED. -- FABRICATED AND INSTALLED AFT FLANGE. FOUND CRACKS ON INTERCOSTAL LOWER ATTACH HOLES. FABRICATED AND INSTALLED INTERCOSTAL .Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020188Bracket · corrodedCORROSION ON ANGLE BRACKET FOR FLOOR SUPPORT AT STATION 367 RIGHT SIDE. REMOVED AND REPLACED BRACKET.Mar 27, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0200042Odor · detectedSTRONG ACIDIC SMELL FROM GALLEY AREA, COFFEE MAKER ON FORWARD SIDE OF AIRCRAFT RIGHT. TURNED GALLEY POWER OFF, SMELL DISSIPATE. REMOVED ALL 3 COFFEE MAKERS AND INSPECTED WIRING TO EACH, NO DISCREPANCIES NOTED. INSPECTED ALL WIRING INSIDE FORWARD GALLEY, NO Mar 26, 2002 · N846AT · Doug DC932 · Buffet/GalleysSDR AT0200040Slide · unserviceableDURING SERVICE CHECK FOUND TAIL CONE EVACUATION SLIDE PRESSURE LOW. REMOVED AND REPLACED EVACUATION SLIDE IAW DC9 MM 25-62.Mar 26, 2002 · N847AT · Doug DC932 · Escape SlideSDR AT0200039Wire · cutCONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK, EMERGENCY PATH LIGHT WIRES WERE CUT OFF. REPAIRED WIRES L9045-20, L9054-20N, L9049-20 AND L9057-20N AT CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK EMERGENCY PATH LIGHT IAW WDM 33-51-03 AND MM 20-5Mar 23, 2002 · N816AT · Doug DC932 · Light System WiringSDR GTIA020242Controller · faultyACY - FLT 8012 - A/P WILL NOT STAY ENGAGED. REMOVED AND REPLACED AUTOMATIC PILOT CONTROLLER. OPERATIONAL CHECK NORMAL IAW DC9 MM 22-10-2. (M)Mar 22, 2002 · N12536 · Doug DC932 · Autopilot SystemSDR MWEA020187Splice · crackedLONGERON 28 LEFT SPLICE AT STATION 560 IS CRACKED OUT AFT HOLE. -- REMOVED LONGERON SPLICE FITTING. MATCH DRILLED FITTING. FABRICATED AND INSTALLED SHIMS TO SPLICE AND INSTALLED SPLICE TO LONGERONS.Mar 22, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020186Panel · corrodedLEFT FLAP TRAILING EDGE PANEL NR 3 HAS MODERATE TO HEAVY CORROSION AROUND FINGER DOUBLERS IN SEVERAL BAYS. FINGER DOUBLERS LOOSE IN SEVERAL AREAS. FABRICATED AND INSTALLED LOWER AND UPPER PANELS.Mar 22, 2002 · N206ME · Doug DC932 · Trailing Edge FlapsSDR ABXA010813Panel · corrodedLEVEL I CORROSION UNDER 8 EACH LOWER FLOATING NUT PLATES ON THE RIGHT SLANT PANEL. REMOVED AND REPLACED THE RIGHT SLANT PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-20-0.Mar 21, 2002 · N986AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA010812Panel · corrodedLEVEL I CORROSION UNDER 10 EACH LOWER FLOATING NUT PLATES ON LEFT SLANT PANEL. REMOVED AND REPLACED THE LEFT SLANT PANEL IAW DC-9 SRM 51-30-1.Mar 21, 2002 · N986AX · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0200041ApuAFTER TAKE OFF BOTH LAVATORY SMOKE DETECTORS ACTIVATED. WITH WHITE SMOKE IN AFT CABIN. CORRECTIVE ACTION: FOUND APU TO BE PRODUCING OIL INTO PACK SYSTEMS FROM INTERNAL LEAK. REMOVED AND REPLACED APU ASSY PER AMM 49-10, FUNCTIONAL CHECK NORMAL.Mar 21, 2002 · N837AT · Doug DC932 · Smoke Detection
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