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 TWAA9917602Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON CABIN FLOOR SUPPORT ANGLE AT BL 0, STA 216 TO 229. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SPM 6-70-01.Nov 10, 1999 · N925L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9917601Floorbeam · corrodedDURING OP 16 MAINT CHECK AT STA 160 TO 220 FOUND CABIN FLOOR PANEL ATTACH ANGLE WITH CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.Nov 10, 1999 · N925L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9917511Support · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR AT STA 197, LBL 0 TO 57 IN WITH CORROSION ON FLOOR PANEL ATTACH ANGLES. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.Nov 10, 1999 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9917510Floor Panel · corrodedDURING OP 16 MAINT CHECK,THE CABIN FLOOR AT STA 160 TO 200 HAD HEAVY CORROSION ON FLOOR PANEL ATTACH ANGLE RBL 45 IN. REMOVED AND REPLACED SUPPORT PER SPM 6-70-01.Nov 10, 1999 · N915L · Doug DC932 · Fuselage Floor PanelSDR TWAA9917508Floor Panel · wornDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR AT STA 160 TO 200, RBL 0 TO 50 IN, THE FLOOR PANEL MEMBRANE WITH A HEAVY WORN DEEP AREA IN MEMBRANE FROM FLOOR PANEL CHAFING WORN ALMOST THROUGH. REMOVED AND REPLACED MEMBRANE FROM STA 160 TO 200, RBL 0 TO 50, PER SNov 10, 1999 · N925L · Doug DC932 · Fuselage Floor PanelSDR TWAA9917409Stiffener · wornDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, THE SIDE COWL PANEL VERTICAL STIFFENER HAD WORN THROUGH AT REPAIR AND METAL HAD NOT BEEN ROUTED OUT TO PREVENT FURTHER CRACKING. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. REPAIRED PNov 10, 1999 · N925L · Doug DC932 · Nacelle/Pylon StructureSDR 9905059982Skin · crackedDURING LINE CHECK, FOUND FUSELAGE SKIN FS 996 BETWEEN LONGERONS 7 AND 8, 4 EA FASTENERS, BETWEEN LONGERONS 8 AND 9, 2 EA FASTENER HOLES CRACKED IN ROW NR 1. REPAIRED PER EA 99-169624.Nov 10, 1999 · N982US · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA99793Support · crackedFORWARD BAG PIT LEFT SIDEWALL SUPPORT AT STATION 332 IS CRACKE. MAINTENANCE FABRICATED AND INSTALLED SUPPORT REPAIR SECTION.Nov 9, 1999 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA99792Frame · crackedFUSELAGE FRAME 503 AT LONGERON 25 RIGHT IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER.Nov 9, 1999 · N602ME · Doug DC932 · Fuselage Main, FrameSDR MWEA99791Fitting · crackedFORWARD CARGO PIT AFT CARGO DOOR JAMB UPPER STRUT FITTING IS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW FITTING.Nov 9, 1999 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA99790Frame · corrodedLOWER LEG OF FUSELAGE FRAME 522 HAS CORROSION AT LONGERON 30. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLERS.Nov 9, 1999 · N602ME · Doug DC932 · Fuselage Main, FrameSDR AT9900829Battery Pack · dischargedFOUND AFT EMERGENCY CEILING LIGHTS DIM. REMOVED AND REPLACED BATTERY PACKS AND BATTERIES B5-28, B5-25, B5-26, B5-27 IAW 737 MM 33-53-0.Nov 9, 1999 · N811AT · Doug DC932 · Emergency LightingSDR MWEA99825Relay · failedMCI - FLT 580 - SMELLED ELECTRICAL SMOKE IN COCKPIT PRIOR TO DEPARTURE. MTC DEFERRED APU AND REMOVED AND REPLACED LEFT APU POWER RELAY. (X)Nov 8, 1999 · N206ME · Doug DC932 · AC Generation SystemSDR TWAA9915203Skin · crackedDURING CHECK-C MAINT, FOUND 2 CRACKS IN SKIN IN FWD UPPER CORNER OF THE RT SIDE FORWARD CABIN SERVICE DOOR JAM. CRACKS WERE .0625 IN AND .3125 IN LONG COMING OUT OF RIVETS, AND EDDY CURRENT SHOWED A CRACK THAT WAS UNDER .0625 INCHES IN LENGTH. CUT OUT CRACKNov 8, 1999 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900807Frame · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK OUT OF LIMITS IN MAIN FRAME AT BS 718 LEFT. REMOVED AND REPLACED MAIN FRAME AT BS 718 LEFT IAW DC9 SB 53-131.Nov 8, 1999 · N846AT · Doug DC932 · Fuselage Main, FrameSDR AT9900806Frame · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK OUT OF LIMITS IN MAIN FRAME AT BS 718 RIGHT. REMOVED AND REPLACED MAIN FRAME AT BS 718 RIGHT IAW DC9 SB 53-131.Nov 8, 1999 · N846AT · Doug DC932 · Fuselage Main, FrameSDR AT9900802Battery · dischargedEMERGENCY EVACUATION LIGHTS IN COCKPIT AND FORWARD PASSENGER CABIN INOPERATIVE. REMOVED AND REPLACED BATTERY IAW DC9 MM 33-40.Nov 8, 1999 · N848AT · Doug DC932 · Emergency LightingSDR AT9900801Handle · unserviceableTAILCONE UNSAFE LIGHT ON AFTER LANDING ROLL. RECONNECTED EXTERIOR HANDLE LINKAGE AND PERFORMED TAIL CONE DROP CHECK IAW DC9 MM 53-50-3.Nov 8, 1999 · N831AT · Doug DC932 · Door Warning SystemSDR AT9900800Emergency Lights · intermittentWITH EMERGENCY EXIT LIGHTS SELECTED OFF AND BATTERY SWITCH OFF. THE OVERWING EXIT LIGHTS REMAIN ILLUMINATED WITH SWITCH (BATT) ON ALL EMERGENCY EVAC LIGHTS ARE OUT/OFF. POWERED DOWN AIRCRAFT, THE REPOWERED EMERGENCY LIGHTS CHECKED NORMAL IAW DC9 MM 33-53.Nov 8, 1999 · N815AT · Doug DC932 · Emergency LightingSDR AT9900842Support · crackedFOUND FORWARD PIT FLOOR SUPPORT AT BS 389 HAS TWO EACH CRACKS. REMOVED, WEILDED AND REINSTALLED FLOOR SUPPORT IAW EA 12-5321-29-C1362 AND DC9 SRM 51-10-03, 51-30-2.Nov 6, 1999 · N838AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900835Longeron · corrodedFOUND LONGERON 20R AT BS 227 TO 285 CORRODED. CUT OUT CORRODED SECTION OF LONGERON. FABRICATED NEW LONGERON SECTION AND SPLICES. INSTALLED REPAIR IAW DC9 SRM 53-10-2, 51-30-2, 51-10-3 AND 51-10-4.Nov 6, 1999 · N802AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900816Frame · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND FRAME AT BS 617 RIGHT TO HAVE TEMPORARY REPAIR. REMOVED AND REPLACED FRAME AT BS 617 RIGHT IAW DC9 SRM 51-30-02 AND 51-30-05.Nov 6, 1999 · N802AT · Doug DC932 · Fuselage Main, FrameSDR MWEA99785Rib · crackedLEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION HAS A CRACK ON THE INBOARD RIB. MTC DRILLED UP AND INSTALLED NEW RIB WEB.Nov 5, 1999 · N202ME · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR AT9900847Web · corrodedFOUND RIGHT HAND AFT CABIN AT BS 908-965 RBL 50, FLOOR SUPPORT WEB WAS CRACKED AND CORRODED. REMOVED CORROSION, STOP DRILLED CRACK, FABRICATED, INSTALLED REPAIR IAW DC9 SRM 53-01, 51-10-3, 51-30-1.Nov 5, 1999 · N838AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900815Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND CORROSION AT BS 323-380 AND AT STATIC PORT TO BE OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER BS 323-380 IAW EO 99-1332 AND DC9 SRM 53-00.Nov 5, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900814Skin · crackDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 120-200 RIGHT. REMOVED AND REPAIRED CRACK AT BS 120-200 RIGHT IAW EO 99-1332.Nov 5, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900813Skin · dentedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE RIGHT FUSELAGE SKIN HAD NUMEROUS DENTS AT BS 227-408. REMOVED AND FABRICATED NEW SKIN IAW AT BS 227-408 EO 99-1328.Nov 5, 1999 · N802AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900774Cover · detachedCHECK RIGHT SLIDE PACK AND COVER. REINSTALLED RIGHT SLIDE COVER IAW DC9 MM 25-60.Nov 5, 1999 · N845AT · Doug DC932 · Emergency EquipmentSDR 9905019924Bulkhead · bulgedDURING LINE MAINTENANCE INSPECTION, FOUND BULGE IN LOWER FUSELAGE SKIN ADJACENT TO FS 604 BULKHEAD 'T' CAP. REPAIRED PER EA 99-153395.Nov 5, 1999 · N926NW · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9915103Skin · crackedDURING CHECK-C MAINT, TWO SKIN CRACKS WERE FOUND ON THE FORWARD CARGO DOOR, LOWER AFT CORNER, FUSELAGE STA 427 AND LONGERON 27R. CRACKS WERE 13/32 AND 5/32 IN LONG. REPAIRED PER SRM 53-05, FIG 105.Nov 4, 1999 · N995Z · Doug DC932 · Cargo/Baggage DoorsSDR AT9900811Doubler/Longeron · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK AT BS 230 LONGERON 21 LEFT. FABRICATED AND INSTALLED FILLER, DOUBLER, AND LONGERON SPLICE IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30, 51-30-02, 51-30-05, 25-52, AND EO 99-1335.Nov 4, 1999 · N846AT · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9917605Floor Panel · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR MEMBRANE AT STA 598, APPROX RBL 55 IN, WAS CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01, FIG 4, SHEET 3, PAGE 19.Nov 3, 1999 · N925L · Doug DC932 · Fuselage Floor PanelSDR TWAA9915001Doubler · crackedDURING CHECK-C MAINT, FOUND 3 CRACKS IN INTERNAL SKIN DOUBLER AT FWD ENTRY DOOR CUTOUT. CRACKS WERE 3 INCHES, 1.75 IN, AND .75 IN. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR PER SRM 53-05, FIG 25A AND ARA 16407.Nov 3, 1999 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA99782Controls · malfunctionedAT APPROX FL 200, ELEVATOR CONTROL ACTIVITY WAS LOST AND TRIM WAS USED TO SUSTAIN FLIGHT. MAINTENANCE REMOVED AND REINSTALLED PANELS 63084 AND 63104 ON HORIZONTAL STAB. INSPECTED FOR WATER AND DEBRIS BLOCKING DRAIN HOLES, NONE FOUND. OK FOR SERVICE AT THIS Nov 3, 1999 · N215ME · Doug DC932 · Elevator Control SystemSDR MWEA99779Slide · unlatchedGALLEY DOOR ESCAPE SLIDE CONTAINER WAS UNLATCHED AT BOTTOM. MAINTENANCE RELATCHED LANYARD ON GALLEY DOOR ESCAPE SLIDE.Nov 3, 1999 · N216ME · Doug DC932 · Emergency EquipmentSDR MWEA99771Beam · chafedLEFT LOWER CORNER OF AFT EXIT DOOR WAS CHAFED. MAINTENANCE FITTED AND INSTALLED NEW BEAM.Nov 3, 1999 · N602ME · Doug DC932 · Emergency ExitsSDR AT9900854Floor Panel · corrodedFOUND FLOOR PANEL CRACKED (HAT SECTION) AND CORRODED AROUND SCREW HOLE. FABRICATED PANEL REPAIR, FABRICATED 5 REPAIR HAT SECTIONS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED REPAIR AND HAT SECTIONS IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, AND DC9 MM 25-1Nov 3, 1999 · N838AT · Doug DC932 · Fuselage Floor PanelSDR TWAA9914905End Cap · crackedDURING CHECK-C MAINT, FOUND LONGERONS R2 AND L2 WITH THE END CAPS CRACKED AT STA 1076, EACH WITH APPROXIMATELY A 1.5 INCH CRACK. REPLACED EACH LONGERON SECTION PER SRM 53-02, FIG 8.Nov 2, 1999 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900808Doubler · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND UPPER PRESSURE WEB DOUBLER AT BS 718 LEFT CORRODED BEYOND LIMITS. REMOVED, FORMED, AND INSTALLED NEW DOUBLER AT BS 718 LEFT IAW DC9 SRM 53-01 FIG 1, 51-10-02, 51-10-02A, 51-10-03, AND 51-10-04.Nov 2, 1999 · N846AT · Doug DC932 · Fuselage Miscellaneous StructureSDR 9904769917Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND AFT TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.Nov 2, 1999 · N967N · Doug DC932 · Emergency LightingSDR MWEA99759Doubler · crackedFUSELAGE SKIN HAD CRACK AT STATION 200 BETWEEN LONGERON 20 AND 21 COMING OUT OF THE AIRSTAIR COMPARTMENT OPENING LOWER AFT CORNER. MTC FABRICATED AND INSTALLED DOUBLER.Nov 1, 1999 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA99758Longeron · corrodedLIGHT CORROSION OF LONGERON 30 STATION 387. CORROSION WAS OUT OF LIMITS. MTC FABRICATED AND INSTALLED NEW LONGERON.Nov 1, 1999 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA99757Tab · damagedWATCH ITEM 3038 REPAIR LT AILERION CONTROL TAB, ORIGINAL REPAIR ACCOMPLISHED CORRECTLY. MTC REMOVED TAGGED AILERON. REMOVED DAMAGED AREA THEN FABRICATED AND INSTALLED DOUBLER.Nov 1, 1999 · N202ME · Doug DC932 · Aileron TabsSDR MWEA99756Skin · corrodidRIGHT HORIZONTAL STABILIZER HAD MODERATE CORROSION ON OUTBOARD HALF OF LEADING EDGE. CORROSION WAS OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER ON RIGHT STABILIZER.Nov 1, 1999 · N202ME · Doug DC932 · Horizontal Stabilizer, Plate/SkinSDR MWEA99755Panel · delaminatedRIGHT WING MOST INBOARD TRAILING EDGE PANEL (TRAP PANEL) HAD APPROX 120 SQUARE INCH OF DELAMINATION ON LOWER AFT SURFACE. MTC FABRICATED AND INSTALLED DOUBLER.Nov 1, 1999 · N202ME · Doug DC932 · Wing, Plate/SkinSDR MWEA99754Skin · chafedAFT CARGO DOOR HANDLE IS CHAFING INTO OUTER DOOR SKIN. MTC FABRICATED CHAFE DOUBLER. MTC INSTALLED CHAFE DOUBLER.Nov 1, 1999 · N202ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA755Vert Gyro · inopCAPTAIN'S HORIZON FAILIED ON CLIMBOUT. MTC NR 1 VERTICAL GYRO.Nov 1, 1999 · N501ME · Doug DC932 · Attitude Gyro and Indicating SystemSDR MWEA754Adi · inopCAPTIANS HORIZON FAILED ON CLIMBOUT. MTC REMOVED AND REPLACED CAPTIANS ADI AND INSTRUMENT AMP.Nov 1, 1999 · N501ME · Doug DC932 · Integrated Flight SystemSDR AT9900853Floor Panel · corrodedFOUND FLOOR PANEL NR 4692A WAS CORRODED. GAINED ACCESS, REMOVED HAT SECTIONS, FABRICATED NEW FLOOR PANEL, TREATED, PRIMED INSTALLED HAT SECTIONS AND PANEL IAW DC9 SRM 51-30-2, 57-10-2, 51-10-3, 51-70-2 AND DC9 MM 53-20-1.Nov 1, 1999 · N838AT · Doug DC932 · Fuselage Floor PanelSDR AT9900799Retract Mech · malfunctionedAFTER TAKEOFF AND UPON GEAR RETRACTION A FLUTTER NOISE CAME FROM THE NOSE GEAR AREA. FOUND RIGHT NOSE GEAR DOOR OPEN. VISUALLY INSPECTED NOSE GEAR DOORS AND WHEEL WELL. FOUND NOTHING ABNORMAL. CLOSED GEAR DOOR. OK FOR SERVICE PER MM 52-80.Nov 1, 1999 · N836AT · Doug DC932 · Landing Gear Door Retract Section
Back to Douglas DC-9-32