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.

SDR TWAA0003201Flange · crackedDURING OP 16 MAINT CHECK, IN RT WHEEL WELL FOUND UPPER FLANGE OF TRAPEZONDAL PANEL HAD A CRACK BETWEEN NUMBER 7 AND 8 HOLES. COMPLIED WITH SERVICE BULLETIN 53-182 PER EMLR 70245A.Feb 22, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000113Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON SKIN AT FORWARD CARGO COMPARTMENT AT BS 522 LONGERON 29R. REMOVED CORRODED SECTION AND INSTALLED DOUBLERS IAW DC9 SRM 51-20, 51-10-03, AND REO-L00064.Feb 22, 2000 · N847AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000105Frame · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LOWER FLANGE OF FRAME AT BS 832 IN AFT PIT CORRODED BEYOND LIMITS. REMOVED CORROSION AND INSTALLED REPAIR SPLICE IAW DC9 SRM 53-03 FIG 4J AND 51-10-03.Feb 22, 2000 · N847AT · Doug DC932 · Fuselage Main, FrameSDR ABXA000132Trim Motor · contaminatedUNABLE TO MOVE AILERON TRIM KNOB IN CRUISE FLIGHT. INSPECTED AILERON TRIM TAIL SYSTEM. FOUND AFT ACTUATOR TO HAVE WATER CONTAMINATION. CLEANED, INSPECTED AND LUBED LEFT AND RIGHT TRIM ACTUATOR AS PER DC9 O/H MANUAL 27-10-6. PERFORMED AILERON TRIM CONTROL CFeb 22, 2000 · N902AX · Doug DC932 · Aileron Control SystemSDR CA000320020Circuit Breaker · failed(CAN) VERY STRONG SMELL OF SMOKE AFTER TAKEOFF FROM GALLEY AREA. DECLARED EMER AND RETURNED TO GATE. FOUND NR 1 COFFEE MAKER 10 AMP CB AT FAULT AND REPLACED.Feb 21, 2000 · Doug DC932 · Buffet/GalleysSDR AT0000109Frame · corrodedDURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL, FOUND FRAME AT E/E COMPARTMENT BS 170 LONGERON 19R CORRODED BEYOND LIMITS. REMOVED AND REPLACED FRAME AT BS 170, LONGERON 19R IAW DC9 SRM 51-10-03, 53-03, AND 51-30.Feb 21, 2000 · N837AT · Doug DC932 · Fuselage Main, FrameSDR 20000427AP001Sensor · failedUPON TAKEOFF AND GEAR RETRACTION, OBSERVED NOSE GEAR UNSAFE LIGHT. RECYCLED AND THE SAME INDICATION WAS OBSERVED. DURING PERFORMANCE OF THE ABNORMAL CHECKLIST THE CREW REPORTED THE ILLUMINATION OF THE LEFT MAIN GEAR UNSAFE LIGHT. RETURNED AND LANDED UNDER NFeb 20, 2000 · N930BB · Doug DC932 · Landing Gear Position and WarningSDR MWEA00076Unknown · odorFLIGHT ATTENDANTS NOTICED BURNING SMELL AT ROW 8, ABOUT 5 MILES OUT. MAINTENANCE INSPECTED OVERHEAD FOR RESIDUAL SMELL, NONE NOTED. MAINTENANCE ALSO PERFORMED AN ENGINE RUN, AND RAN PACKS, NO BURNING SMELLS NOTED.Feb 18, 2000 · N212ME · Doug DC932 · Air Distribution SystemSDR TWAA0002908Pan · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON THE FORWARD SERVICE DOOR ENTRY WAY LOWER PAN AREA. REPLACED THE LOWER PORTION OF THE DOOR PAN PER SRM 53-05, FIG 55 SHEET 1 THROUGH 7, DRAWING JO 60288.Feb 17, 2000 · N921L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002907Structure · damagedDURING OP 16 MAINT CHECK, THE RT CABIN SERVICE DOOR ENTRY WAY PAN WAS DAMAGED AT STA 200, STRINGER 15R. INSTALLED DOUBLER PER SRM 53-05, FIG 42 SHEET 1 THROUGH 9.Feb 17, 2000 · N921L · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00075Cover · looseSPLIT PIN FOR FORWARD ENTRANCE DOOR EMERGENCY EVACUATION SLIDE COVER CAME OFF. MAINTENANCE REINSTALLED SLIDE COVER.Feb 17, 2000 · N203ME · Doug DC932 · Escape SlideSDR 0000489610Fire Detector · malfunctionedAFTER TAKEOFF, CARGO FIRE DETECTION SYSTEM A INDICATED A FIRE IN THE FORWARD CARGO HOLD. THE AIRCRAFT HAD CARGO FIRE DETECTION SYSTEM B ON MEL, SO THE CREW DID NOT HAVE SECONDARY VERIFICATION CAPABILITY. THE CREW DISCHARGED THE FORWARD CARGO AREA FIRE EXTINGFeb 17, 2000 · N610NW · Doug DC932 · Fire DetectionSDR CA000320016Door · separated(CAN) CREW HEARD BANG ON CLIMB. SKIN DAMAGE ON LT HORIZONTAL STAB TIP FAIRING AND LT ENGINE OIL ACCESS DOOR TORN FROM HINGES. DOOR WAS FOUND DAMAGE ON PREVIOUS STOP AND TEMP REPAIR CARRIED OUT. REPLACED.Feb 16, 2000 · Doug DC932 · Fluid Service DoorsSDR TWAA0003014Spar · crackedDURING OP 16 MAINT CHECK, RT WING HAD APPROX .375 IN CRACK AT LOWER INBD HOLE ON SURFACE OF REAR SPAR AT INBD FLAP HINGE, STA XRS 164. STOP DRILLED CRACKS PER DAC DRAWING JO 60271. HIGH FREQ EDDY CURRENT ACCOMP PER 51-00-13, PART 6. REPAIRED CRACKED WING SPFeb 15, 2000 · N925L · Doug DC932 · Wing SparSDR TWAA0003013Structure · damagedDURING OP 16 MAINT CHECK, NECESSARY TO REPAIR HOLE DAMAGE IN FUSELAGE AT APPORX STA 608 TO 612, LONGERON 28L TO 28R. COMPLIED WITH ARA 16532.Feb 14, 2000 · N925L · Doug DC932 · Fuselage Main, StructureSDR TWAA0003012Skin · corrodedDURING OP 16 MAINT CHECK, LOWER FUSELAGE EXISTING REPAIR HAD CORROSION ON FUSELAGE SKIN AFT OF STA 604. REMOVED VISIBLE SURFACE CORROSION PER TWA STD PROCESSES 6-80-01. COMPLIED WITH ARA 16532..Feb 14, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA00071Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE COVER CAME LOOSE AT THE BOTTOM. MAINTENANCE REINSTALLED SLIDE COVER.Feb 14, 2000 · N602ME · Doug DC932 · Escape SlideSDR TWAA0005810Angle · crackedDURING OP 16 MAINT CHECK, THE LT WING FLAP WAS CRACKED IN UPPER SUPPORT ANGLE ON I/B SIDE OF O/B FLAP HINGE CASTING IN FLANGE. CRACKED ANGLE (P/N 9957600-7) WAS REMOVED AND REPLACED WITH NEW ANGLE PER SPM 6-70-01, PARA 4, SUBSECTION B SRM 51-6--0.Feb 11, 2000 · N925L · Doug DC932 · Trailing Edge FlapsSDR TWAA0003011Longeron · crackedDURING OP 16 MAINT CHECK, FUSELAGE STA 579 TO 604 AREA HAD A CRACK IN LONGERON 24L. REPLACED LONGERON 24L PER DAC PRINT 5910068.Feb 11, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0002708Longeron · brokenDURING OP 16 MAINT CHECK, LONGERON 25 LT& RT, LONGERON 29 LT STA 579 TO 604 WAS BROKEN OFF AT THE FWD END. REPLACED LONGERON AT EACH AREA AND INSTALLED PER PRINT 5910068.Feb 11, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00060Receiver · failedNUMBER 2 NAV VOR/LOC FLAG IS IN VIEW. MAINTENANCE REMOVED AND REPLACED NUMBER TWO NAVIGATION RECEIVER.Feb 11, 2000 · N216ME · Doug DC932 · Dependent Position Determining SystemSDR GTIA000095Light · obstructedACY - LAST ROW 24 D, E, F CARPET IS COVERING UP EMERGENCY TRACK LIGHTING. ADJUST CARPET ALONG EMERGENCY FLOOR TRACK LIGHT OPS CHECK GOOD PER DC9 MM 33-53-0. (M)Feb 10, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA000094Cover · displacedEMERGENCY TRACK LIGHTING COVER HAS MOVED EXPOSING THE FLOOR WIRES. SECURED FLOOR TRACK THAT SLID FORWARD. CHECKS GOOD PER DC-9 MM 33-53-0. (M)Feb 10, 2000 · N941ML · Doug DC932 · Emergency LightingSDR TWAA0002707Skin · corrodedDURING OP 16 MAINT CHECK, THE LOWER FUSELAGE HAD CORROSION COMING FROM MATING SURFACE OF FUSELAGE SKIN AND LONGERONS AT STA 604 TO 617, AND STRINGER 28L TO 29R. REPLACED FUSELAGE SKIN. INSTALLED SKIN PER DRAWING 5911418.Feb 10, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0002613Longeron · crackedDURING OP 16 MAINT CHECK, THE LOWER FUSELAGE, LONGERON 27L, AT STA 566 TO 585, WAS FOUND CRACKED AT THE FWD END. REPLACED CRACKED FITTING WITH (P/N 3920595-501). INSTALLED PER DRAWING 590068.Feb 9, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0002612Casting · crackedDURING OP 16 MAINT CHECK, THE RT WING TRAILING EDGE FLAP O/B HINGE CASTING ATTACH FRAME WAS CRACKED AT I/B AND O/B SIDES. REPLACED CRACKED FRAME PER SRM 51-10-01, PARAGRAPH C.Feb 9, 2000 · N925L · Doug DC932 · Trailing Edge FlapsSDR TWAA0002611Skin · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FUSELAGE SKIN AT STA 294, BETWEEN LONGERON 18L AND 19L. NO CRACK PER NDT HFEC PER 51-00-03 PART 6. BLENDED STATIC BURN AND REMOVED RIVET PER SRM 53-04 TABLE A PAGE 208. REPLACED RIVET PER SPM 6-70-01 PAGE 3 ANDFeb 9, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0002610Skin · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FUSELAGE SKIN AT STA 164, LONGERON 25L. NO CRACK PER PART 6, 51-00-03. REPLACED RIVET PER SPM 6-70-01 PAGE 3, AND SRM 51-30 AND 51-10-4.Feb 9, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0002609Rivet · damagedDURING OP 16 MAINT CHECK, ON RT FWD FUSELAGE FOUND RIVET BURN AT APPROX STA 446, 3.5 IN BELOW LONGERON 18R. NO CRACK PER PART 6, 51-00-03. REPLACED RIVET PER SPM 6-70-01 AND SRM 51-30 AND 51-10-4.Feb 9, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002608Rivet · damagedDURING OP 16 MAINT CHECK, THE RT FWD FUSELAGE APPROX STA 469 HAD A RIVET BURN 2.75 IN BELOW LONGERON 18R. REPLACED RIVET PER SPM 6-70-01, PAGE 3, SRM 51-30 AND 51-10-4. NO CRACKS PER NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6.Feb 9, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002509Skin · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION BETWEEN SKIN DOUBLERS AT FORWARD RT CABIN SERVICE DOOR ENTRYWAY, LOWER FWD CORNER. REMOVED CORROSION AND TREATED PER SRM 51-10-9. SPLICED IN NEW CUSP ANGLE PER SRM 53-05, FIG 55.Feb 9, 2000 · N921L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0002508Angle · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FORWARD RT CABIN SERVICE DOOR ENTRYWAY, LOWER FWD CORNER UPPER CUSP ANGLE. REMOVED CORROSION SECTION OF CUSP ANGLE. INSTALLED NEW SECTION PER SRM 53-05 FIG 55.Feb 9, 2000 · N921L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002507Angle · damagedDURING OP 16 MAINT CHECK, THE RT FORWARD SERVICE DOOR ENTRYWAY LOWER FWD CORNER AT STA 165, HAD STRINGER 18R CUSP ANGLE CUT. REPAIRED LOWER CUSP ANGLE PER SRM 53-05 FIG 55 AND ARA 16238A.Feb 9, 2000 · N921L · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000080Stringer · corrodedFOUND LEFT HAND WING STRINGER 15 CORRODED. INSTALLED STRAP REPAIR IAW DC9 SRM 51-30-5, 51-10-4, 57-08 FIGURE 2 METHOD 2, 51-22-1 TO -3.Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000079Stringer · corrodedFOUND LEFT HAND WING STRINGER 17 CORRODED. CUT AND SPLICED LEFT HAND WING STRINGER 17 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-10-3, 57-08 FIGURE 2.Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000078Stringer · corrodedFOUND LEFT HAND WING STRINGER 20 CORRODED. CUT AND SPLICED LEFT HAND WING STRINGER 20 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-10-3, 57-08 FIGURE 2.Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000077Stringer · corrodedFOUND LEFT HAND STRINGER 23 CORRODED. REMOVED AND REPLACED LEFT HAND STRINGER 23 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-30-1, 57-08.Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR L1GA200000308Brace · corrodedRIGHT MLG SIDE BRACE CORRODED 3 X 5 INCHES AND BOLT HOLE ELONGATED.Feb 8, 2000 · N14534 · Doug DC932 · Main Landing GearSDR L1GA200000306Door Frame · corrodedFWD CARGO DOOR FWD DOOR JAMB CORRODED 3 X 4 INCHES.Feb 8, 2000 · N14534 · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA000085Light · looseDTW - EMERGENCY TRACK LIGHTING STRIP LOOSE ON CAT WALK IN TAIL COMPARTMENT. RESECURED HARDWARE ON TRACK LIGHTING STRIP AS REQUIRED IAW DC9 MM 33-50. (M)Feb 8, 2000 · N133NK · Doug DC932 · Emergency LightingSDR GTIA000084Battery · inoperativeDTW - EMERGENCY LIGHTS ABOVE TAIL CONE SLIDE INOPERATIVE. TROUBLESHOT, RELAMPED, NO HELP. REMOVED AND REPLACED BATTERY POWER SUPPLY AND OPS CHECK PER MM 33-50-0. NO DEFECTS NOTED. (M)Feb 8, 2000 · N133NK · Doug DC932 · Emergency LightingSDR AT0000072Stringer · gougedFOUND AFT CARGO DOOR AT BS 937, LONGERON 23R - 25R WAS BENT AND GOUGED. FABRICATED, DRILLED AND INSTALLED REPAIR IAW TIMCO EO L00036.Feb 7, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00050Bracket · crackedFOUND ANGLE BRACKET ON LEFT ENGINE PYLON LOWER SIDE AT ACCESS PANEL 8105A CRACKED. MAINTENANCE FABRICATED AND INSTALLED BRACKET REPAIR.Feb 6, 2000 · N215ME · Doug DC932 · Nacelle/Pylon StructureSDR MWEA00049Web · crackedFOUND WEB ON LEFT ENGINE PYLON LOWER SIDE AT ACCESS PANEL 8105A CRACKED. MAINTENANCE FABRICATED AND INSTALLED WEB REPAIR.Feb 6, 2000 · N215ME · Doug DC932 · Nacelle/Pylon StructureSDR AT0000086Lanyard · disengagedFOUND ON TAXI OUT, R1 DOOR SLIDE LANYARD FELL OUT. STRAIGHTENED ARM AND ATTACHED PACK, REATTACHED PIN IAW DC9 MM 25-62-00.Feb 6, 2000 · N825AT · Doug DC932 · Escape SlideSDR MWEA00039Battery Pack · malfunctionedLEFT NACELLE LIGHT WOULD NOT GO OUT DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS. MAINTENANCE REPLACED LEFT NACELLE LIGHT BATTERY PACK.Feb 6, 2000 · N302ME · Doug DC932 · Emergency LightingSDR AT0000075Door Pan · corrodedFOUND CORROSION AT LOWER DOOR STOP AT AFT CARGO DOOR FRAME AT BS 917. REMOVED AND REPLACED AFT CARGO DOOR JAMB PAN SECTION IAW DC9 SRM 53-10-01 FIGURE 1, 51-10-3, AND 53-05 FIGURE 44.Feb 5, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous StructureSDR 0000349982Bulb · failedLANDING GEAR DOOR OPEN LIGHT FAILED TO ILLUMINATE ON APPROACH. FLIGHT CREW DECLARED YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RELAMPED GEAR DOOR OPEN LIGHT, OPERATIONAL CHECK NORMAL.Feb 5, 2000 · N982US · Doug DC932 · Landing Gear Position and WarningSDR TWAA0002406Channel · damagedDURING OP 16 MAINT CHECK FOUND CABIN AFT VAULT DOOR, WITH TORN METAL U CHANNEL BY RT SIDE OF DOOR JAMB. REPAIRED PER ARA 16326 AND INSTALLED.Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002405Angle · crackedDURING OP 16 MAINT CHECK FOUND CABIN AFT PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT, FWD T ANGLE CRACKED LT END. REMOVED OLD T ANGLE, MADE NEW ONE AND INSTALLED PER PRINT 9915565.Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous Structure
Back to Douglas DC-9-32