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 9803389916Wire · brokenDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRING IN WIRE BUNDLE, OPERATIONAL CHECK NORMAL.Feb 26, 1998 · N949N · Doug DC932 · Light System WiringSDR VJ9800036Skin · corrodedEXTERNAL FUSELAGE SKIN BELOW FORWARD CARGO DOOR LOWER SILL PLATE HAS CORROSION. GROUND OUT LIMITS, FABRICATED AND INSTALLED DOUBLER REPAIR IAW EO 98-794. REPAIR DOUBLER FABRICATED 2024 T3 .071 THICKNESS TIMES 69 BY 21 BY 7.50 TIMES 52.75 BY 21 INCHES.Feb 25, 1998 · N901VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800029Fitting · elongatedOUTBOARD LOWER MAIN BOLT HOLE ELONGATED ON LEFT HAND MAIN LANDING GEAR, FOUND DURING COMPLIANCE INSPECTION OF AD 96-01-05 PER EO 12-5740-29-B1049 INSPECTION REQUIREMENT. REWORKED OUTBOARD LOWER MAIN LANDING GEAR FITTING IAW EO 12-5740-29-C1397 AND AERCORP EO Feb 25, 1998 · N937VV · Doug DC932 · Main Landing GearSDR VJ9800026Cover · looseR1 DOOR EMERGENCY SLIDE COVER BECAME DISLODGED. REPLACED COVER AND PERFORMED REQUIRED INSPECTIONS.Feb 25, 1998 · N907VJ · Doug DC932 · Emergency EquipmentSDR MWEA98214Skin · dentedA DENT WITH AERODYNAMIC FILLER WAS FOUND AT FS 218 LONGERON 16R TO 17R INVESTIGATION REVEALED THE DENT TO BE OUT OF LIMITS. REMOVED AND REPLACED SECTION OF SKIN.Feb 25, 1998 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98213Skin · damagedSTATIC DISCHARGE DAMAGE WAS FOUND ON EXTERNAL FUSELAGE SKIN FS 718 LONGERON 2R. FABRICATED AND INSTALLED REPAIR DOUBLER.Feb 25, 1998 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98212Support · corrodedTHE FS 965 FLOORBEAM LEFT SUPPORT STRUT FOUND WITH NUMEROUS AREAS OF CORROSION. REPAIRED DAMAGED SECTION OF SUPPORT STRUT.Feb 25, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98211Support · corrodedFLOORBEAM SUPPORT STRUT AT FS 965 FOUND CORRODED OVER A LARGE AREA. REMOVED AND REPLACED STRUT.Feb 25, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800135Link · crackedDURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5.Feb 25, 1998 · N988AX · Doug DC932 · Engine Thrust ReverserSDR ABXA9800134Link · crackedDURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE LOWER RIGHT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5.Feb 25, 1998 · N988AX · Doug DC932 · Engine Thrust ReverserSDR ABXA9800133Frame · crackedDURING C-CHECK, FOUND FRAME CRACKED AT LONGERON 17R AND STATION 980. REPAIRED FRAME IAW DC9 SRM 53-03.Feb 25, 1998 · N988AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9800132Longeron · crackedDURING C-CHECK, FOUND LONGERON 13R CRACKED AT STATION 965. REPAIRED FRAME IAW DC9 SRM 53-02.Feb 25, 1998 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800131Longeron · crackedDURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED CRACKED LONGERON IAW DC9 SRM 53-02.Feb 25, 1998 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800130Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.Feb 25, 1998 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800129Shear Tie · crackedDURING C-CHECK, FOUND SHEAR TIE CRACKED AT LONGERON 17R AND STATION 965. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.Feb 25, 1998 · N988AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800128Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 237. REPAIRED LONGERON IAW DC9 SRM 53-02.Feb 25, 1998 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800035Skin · dentedDENT, 2.035 IN DEPTH, CROSSING 3 BAYS ON FUSELAGE SKIN STRETCHING FROM FS 242 TO FS 304 OUT OF LIMITS IAW DC9 SRM 53-04, FIG 38. FABRICATED DOUBLERS 14.75 TIMES 7.125 INCHES, 17 BY 7 INCHES AND 135 BY 8.7 INCHES USING TITANIUM .025 IAW EO 98-800; PRIMED IAW DFeb 24, 1998 · N901VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98210Angle · crackedGALLEY SERVICE DOOR A DOUBLER ANGLE ON THE AFT END OF NR 1 HORIZONTAL BEAM WAS FOUND CRACKED. REMOVED CRACKED ANGLE AND FAB. REPLACEMENT ANGLE IAW SRM 5301. INSTALLED FAB ANGLE IAW SRM 5130.Feb 24, 1998 · N212ME · Doug DC932 · Galley DoorsSDR MWEA98209Skin · misrepairedPREV REPAIR FOUND AT L1 MAIN CABIN ENTRANCE DOOR FWD UPPER CORNER OF CUTOUT, REPAIR IS NOT PER THE SRM. REMOVED OLD REPAIR FAB FILLER AND DOUBLER IAW SRM 5305 FIG 26. INSTALLED FILLER DOUBLER IAW SRM 5130.Feb 24, 1998 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98208Web · crackedGALLEY DOOR INNER WEB WAS FOUND CRACKED BELOW THE BAYONET. REMOVED DAMAGED SECTION FABRICATED DOUBLER IAW SRM 520. INSTALLED DOUBLER IAW SRM 5130.Feb 24, 1998 · N212ME · Doug DC932 · Galley DoorsSDR MWEA98207Beam · crackedGALLEY SERVICE DOOR NR 4 HORIZONTAL BEAM FOUND CRACKED AT FWD END ADJACENT TO OUTER SKIN. STOP DRILLED CRACK FAB REPAIR ANGLE IAW SRM 5205 FIG 25. INSTALLED REPAIR ANGLE IAW SRM 5130.Feb 24, 1998 · N212ME · Doug DC932 · Galley DoorsSDR MWEA98205Longeron · corrodedLONGERON 20L FOUND CORRODED BY THE AFT PRESSURE BULKHEAD FS 996. REMOVED DAMAGED SECTION LONGERON FABRICATED REPLACEMENT SECTION OF LONGERON IAW SRM 5311. INSTALLED REPLACEMENT LONGERON IAWSRM 5130.Feb 24, 1998 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98204Skin · damagedSTATIC DISCHARGE DAMAGE FOUND ON EXTERNAL FUSELAGE SKIN AT STATION 1121.225 BETWEEN LONG 4R AND 6R IAW SRM 53-04 FIG 4. MAINTENANCE REPAIRED SRM 53-10.Feb 24, 1998 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98203Fitting · corrodedLONGERON ATTACH FITTING AT FS 996 LONGERON 24R FOUND CORRODED OUT OF LIMITS. FITTING REMOVED NEW ONE PROCURED REPLACEMENT INSTALLED IAW SRM 51-30.Feb 24, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98202Longeron · corrodedCORROSION FOUND ON LONGERON 28R FROM FS 945 TO 996. DAMAGE SEC OF LONGERON REMOVED, A REPLACEMENT SECTION OF LONGERON WAS FABRICATED IAW SRM 5311. INSTALLED SECTION OF LONGERON IAW SRM 5130.Feb 24, 1998 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98201Skin · crackedCRACK FOUND ON EXTERNAL FUSELAGE SKIN AT FS 313 APPROX 2.5IN BELOW LONGERON 16R. REMOVED DAMAGED SEC SKIN FAB REPAIR FILLER, DOUBLERS IAWSRM 5304 FIG 38. INSTALLED RREPAIR FILLERS, DOUBLERS IAW SRM 51-30.Feb 24, 1998 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9800124Switch · shortedLEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE UP. RECYCLED GEAR, NO CHANGE. REPAIRED SHORTED PIN NR 6 ON THE LEFT MAIN LANDING GEAR DOWN LOCK LIMIT SWITCH. OPS CHECKED GOOD ON GEAR SWING.Feb 24, 1998 · N939AX · Doug DC932 · Landing Gear Position and WarningSDR VJ9800130Floor · corrodedFLOOR PANEL, FS 130 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01. REMOVED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-2 AND 51-30-1.Feb 23, 1998 · N905VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800073Angle · corrodedFLOOR SUPPORT AT FS 996, BL 32 LT, CORRODED BEYOND LIMITS. REMOVED CORROSION IAW DC9 SRM 51-10-3. FABRICATED AND TREATED SHIM AND ANGLE IAW DC9 SRM 53-05, FIG 20A.Feb 23, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98200Fitting · crackedFORWARD END FITTING ON THE GALLEY SERVICE DOOR 4 HORIZONTAL BEAM WAS FOUND CRACKED. REMOVED DAMAGED PART ORDERED NEW PART, INSTALLED IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Galley DoorsSDR MWEA98199Beam · crackedGALLEY SERVICE DOOR WAS FOUND TO HAVE A CRACK IN THE NR 2 BEAM AT THE FORWARD END. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER IAW SRM 52-05 FIG 25, INSTALLED DOUBLER IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Galley DoorsSDR MWEA98198Skin · crackedEXTER FUSE SKIN WAS FOUND CRACKED AROUND A FASTENER FS 965, 3 INCHES ABOVE LONG 14R. REMOVED DAMAGED SEC OF SKIN, FABED FILLER AND REPAIR DOUBLER IAW SRM 53-04, INSTALLED FILLER AND DOUBLER IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98197Floorbeam · chafedFLOORBEAM AT FS FOUND WITH CHAFE MARKS FROM FLOORBOARDS RBL 20 - LBL 20. BLENDED AREA OF BEAM, FAB REPAIR STRAP IAW SRM 5305 FIG 20, INSTALLED REPAIR STRAP IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA98196Floorbeam · chafedFLOORBEAM AT FS 916 WAS FOUND CHAFED FROM THE FLOORBOARDS FROM RBL 20 - LBL 20. BLENDED AREA OF BEAM, FABRICATED REPAIR STRAP IAW SRM 53-05 FIG 20, INSTALLED STRAP IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA98195Bulkhead Web · crackedRIGHT HAND LOWER WEB OF THE BULKHEAD AT FS 965 WAS FOUND CRACKED IN SEVERAL PLACES. REMOVED DAMAGED SEC OF WEB, FAB REPAIR PARTS IAW SRM 53-03 FIG 19, INSTALLED REPAIR PARTS IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98194Skin · misrepairedPREVIOUS FLUSH REPAIR WAS FOUND RUDDER RIB 22 REPAIR DOES NOT CONFORM TO SRM. REMOVED PREVIOUS REPAIR AND FAB DOUBLER IAW SRM 55-03 FIG 11, INSTALLED REPAIR DOUBLER IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Rudder, Plate/SkinSDR MWEA98193Bulkhead Web · crackedWEB ATTACHED TO RADIAL STIFFENER APB FOUND CRACKED AT THE O/B END LONG14R. STOP DRILLED CRACK, FABED REPAIR ANGLES IAW DRAW J060110, INSTALLED REPAIR ANGLES IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98192Tee · corrodedRT HAND WING T-CAP WAS FOUND TO BE EXCESSIVELY CORRODED WING STA XCW 58. T-CAP AT STA XCW 58 WAS REMOVED AND REPLACED IAW DOUGLAS SERVICE BULLETIN 57-98 REV 8.Feb 23, 1998 · N212ME · Doug DC932 · Wing Miscellaneous StructureSDR CALA9800321Latch Mech · wornTHE LT GEAR UNSAFE LIGHT REMAINED ILLUMINATED ATER GEAR RETRACTION (REPEAT PROBLEM - LANDING GEAR SWITCH PREVIOUSLY CHANGED). THE CHECKLIST WAS COMPLETED WITH NO CHANGE. THE FLIGHT WAS CONTINUED TO CLE WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCEFeb 23, 1998 · N12507 · Doug DC932 · Landing Gear Door Retract SectionSDR 9803369941Fitting · crackedDURING M-CHECK, FOUND CRACK IN LONGERON 30 END FITTING AT FS 575. REPLACED FITTING PER DWG 5911412 AND SRM 51-30-5.Feb 23, 1998 · N3324L · Doug DC932 · Fuselage Miscellaneous StructureSDR 9803269609Battery Pack · dischargedEMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 23, 1998 · N609NW · Doug DC932 · Emergency LightingSDR VJ9800072Floor Track · corrodedAFT PIT FLOOR TRACK, TOP AND BOTTOM, CORRODED BEYOND LIMITS. REPLACED FLOOR TRACK IAW DC9 SRM 51-10-4 AND 51-30-1.Feb 22, 1998 · N905VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800071Angle · corrodedFLOOR SUPPORT FS 980, BL 42 RT CORRODED BEYOND LIMITS. REMOVED CORROSION AND NUT PLATES IAW DC9 SRM 53-05, PG 31, FIG 20A AND FABRICATED REPAIR ANGLE AND SHIM PER FIG 20A, VIEW AA.Feb 21, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800070Angle · corrodedFLOOR SUPPORT FS 980, BL46 LT CORRODED BEYOND LIMITS. REMOVED CORROSION, FABRICATED, TREATED AND PRIMED ANGLE, FILLER ANDS SHIM IAW DC9 SRM 53-05, PG 31.Feb 21, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9802603Lamp · failedJAX - FLT 494 - FORWARD GALLEY OVERHEAD FLOURSCENT WORK LIGHT, RT OUTBOARD, WAS SMOKING SHORTLY AFTER TAKEOFF. THE LIGHT WAS TURNED OFF. AT JAX THE LIGHT WAS DEACTIVATED BY PULLING THE CIRCUIT BREAKER. CORRECTION WAS DEFERRED. ON LAYOVER, THE WIRING AND SEFeb 21, 1998 · N920L · Doug DC932 · Passenger Compartment LightingSDR MWEA98191Skin · corrodedINSPECTION FOUND CORROSION UNDER THE LEFT WING FINGER DOUBLERS ON LOWER SKIN INSIDE TRAILING EDGE PANEL. REPLACED SKIN IAW EA NR 57-006.Feb 20, 1998 · N203ME · Doug DC932 · Wing, Plate/SkinSDR MWEA98185Frame · crackedTHE FRAME AT FS 965 WAS FOUND CRACKED AT THE INTERSECTION OF THE FORWARD LOWER PYLON SPAR. FABRICATED REPAIR PARTS IAW SRM 53-03 FIG 13.Feb 20, 1998 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98184Bulkhead Clips · crackedWEB ATTACHED TO THE RADIAL STIFFENER ON THE APB WAS FOUND CRACKED ON THE OUTBOARD END. INSTALLED REPAIR CLIPS IAW SRM 51-30 AND DRAWING J060110.Feb 20, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98183Skin · misrepairedPREVIOUS REPAIR WAS NOTED ON THE LT ELEVATOR BETWEEN NOSE RIBS 8 AND 9 FROM OUTBOARD TIP REPAIR NOT IAW SRM. FABRICATED REPAIR DOUBLER IAW SRM 55-02.Feb 20, 1998 · N212ME · Doug DC932 · Elevator, Plate/SkinSDR MWEA98182Pan · crackMAIN CABIN DOOR A CRACK WAS FOUND ON THE UPPER FORWARD SECTION OF PAN ABOVE STOP F1. INSTALLED NEW PAN SECTION IAW SRM 51-30 AND 52-05.Feb 20, 1998 · N212ME · Doug DC932 · Passenger/Crew Doors
Back to Douglas DC-9-32