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 L1GA200000124Floorboard · crackedCRACK CABIN FLOOR SUPPORT FS 935 RBL 42.May 10, 2000 · N27509 · Doug DC932 · Fuselage Floor PanelSDR L1GA200000123Skin · corrodedLEVEL 2 CORROSION LWR RUDDER ACCESS HOLES.May 10, 2000 · N27509 · Doug DC932 · Rudder, Plate/SkinSDR L1GA200000122Stop · corrodedLEVEL 2 CORROSION AFT CARGO DOOR AFT STOPS.May 10, 2000 · N27509 · Doug DC932 · Cargo/Baggage DoorsSDR L1GA200000121Bracket · corrodedLEVEL 2 CORROSION FWD CARGO DOOR FWD/AFT HINGE BRACKETS AND HARDWARE.May 10, 2000 · N27509 · Doug DC932 · Cargo/Baggage DoorsSDR L1GA200000120Stop · corrodedLEVEL 2 CORROSION FWD CARGO DOOR STOP AND HARDWARE.May 10, 2000 · N27509 · Doug DC932 · Cargo/Baggage DoorsSDR L1GA200000119Fairing · brokenAFT LAV SERVICE DOOR OPENING UNDER PNL BROKEN OUT.May 10, 2000 · N27509 · Doug DC932 · Fuselage Miscellaneous StructureSDR L1GA200000118Floorboard · puncturedDENT AND PUNCTURE FLOOR PNL NR 82 FS 918 LBL 8.May 10, 2000 · N27509 · Doug DC932 · Fuselage Floor PanelSDR L1GA200000117Floorboard · puncturedDENT AND PUNCTURE FLOOR PNL NR 80 FS 908 LBL 52.May 10, 2000 · N27509 · Doug DC932 · Fuselage Floor PanelSDR L1GA200000116Pressure Panel · crackedCRACK FWD FLOOR PNL AFT EDGE VERT CLOSURE FWD OF CAPTAIN''S SEAT.May 10, 2000 · N27509 · Doug DC932 · Fuselage Main, BulkheadSDR L1GA200000076Floorbeam · crackedA CRACK WAS FOUND AT STATION 996 BL 28R FLOORBEAM WEB.May 10, 2000 · N27509 · Doug DC932 · Fuselage Main, Floor BeamSDR L1GA200000075Skin · crackedCRACK FOUND ON THE VERTICAL EDGE OF THE BRIEFCASE COMPARTMENT FOWARD O/B SIDE I/B EDGE.May 10, 2000 · N27509 · Doug DC932 · Fuselage Main, Plate/SkinSDR L1GA200000067Stringer · crackedONE CRACK ON STRINGER NUMBER 3 RT FS 520 TO 540.May 10, 2000 · N27509 · Doug DC932 · Fuselage Main, Longeron/StringerSDR L1GA200000073Door Frame · corrodedCRACKS AND CORROSION FOUND ON AFT BULKHEAD DOOR FRAME 10 INCHES OF CENTERLINE AT UPPER RADIUS.May 10, 2000 · N27509 · Doug DC932 · Fuselage Main, StructureSDR L1GA200000072Structure · corrodedCORROSION FOUND ON LEFT LEADING EDGE INBOARD SIDE TO OUTBOARD SIDE OF WING.May 10, 2000 · N27509 · Doug DC932 · Wing Main, Frame StructureSDR L1GA200000071Access Door · crackedTAIL CONE ACCESS DOOR WAS CRACKED ON THE FORWARD FRAME.May 10, 2000 · N27509 · Doug DC932 · Tail Cone DoorsSDR L1GA200000070Heat Exchange · crackedCRACKS AND CORROSION WERE PRESENT AT THE AFT LOWER EDGE AND FOWARD EDGE OF THE LEFT HAND HEAT EXCHANGER EXHAUST DUCT.May 10, 2000 · N27509 · Doug DC932 · Cabin Cooling SystemSDR L1GA200000069Floorboard · brokenFLOORBOARD PANEL NR 72 HAD CHAFED AREAS AND A BROKEN CORNER.May 10, 2000 · N27509 · Doug DC932 · Fuselage Floor PanelSDR L1GA200000068Floorboard · dentedDENT AND PUNCTURE FOUND ON NUMBER 50 FLOORBOARD PANEL.May 10, 2000 · N27509 · Doug DC932 · Fuselage Floor PanelSDR TWAA0007705Intercostal · crackedDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, FOUND INTERCOSTAL CRACKED 3.5 INCHES FROM FUSELAGE AND 7 INCHES FROM FRONT, BOTTOM AFT AREA OF PYLON. REPAIRED CRACK PER SRM 54-01 PAGE 97 EX D. INSTALLED FASTENERS PER 51-30 AND 51-10-4. SEALED PER 51-70-2.May 10, 2000 · N921L · Doug DC932 · Nacelle/Pylon StructureSDR TWAA0007602Floorbeam · crackedDURING OP 16 MAINT CHECK, FOUND STA 598, RBL 54 IN, HAD FLOOR MEMBRANE CRACKED. INSTALLED DOUBLER ON WEB PER SRM 53-01-9, FIG 2.May 10, 2000 · N921L · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA00436Frame · chafedAFT PART OF FRAME AT STATION 1168 WHERE TAIL CONE MATES WITH FRAME AT FOUR O''CLOCK AND SEVEN O''CLOCK POSITIONS IS CHAFED. MAINTENANCE REMOVED AND REPLACED FRAME SECTIONS.May 10, 2000 · N501ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00435Doubler · chafedFORWARD CARGO DOOR LOWER AFT STOP IS LOOSE AND IS CHAFING DOOR PAN DOUBLER. MAINTENANCE REMOVED AND REPLACED DOUBLER.May 10, 2000 · N501ME · Doug DC932 · Cargo/Baggage DoorsSDR AT0000246Skin · lightning strikeFOUND LIGHTNING STRIKE BLENDED BEYOND LIMITS AT RIGHT HAND WINDOW PANEL, BS 775 - 813. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW REO L00173.May 9, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000244Structure · misrepairedFOUND AFT CARGO CUT OUT LOWER SECTION HAS AN EXISTING REPAIR, NOT IAW DC9 SRM OR EO. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED PERMANENT REPAIR IAW TIMCO REO L-00161.May 9, 2000 · N825AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000243Doubler · crackedFOUND TEMPORARY REPAIR CRACKED AT BS 945. FABRICATED AND INSTALLED PERMANENT PEPAIR IAW TIMCO REO L-00161.May 9, 2000 · N825AT · Doug DC932 · Fuselage Miscellaneous StructureSDR L1GA200000066Shaft · shearedDURING POST FLIGHT WALK-AROUND INSPECTION AFTER THE COMPLETION OF FLIGHT NR 4, DAMAGE WAS NOTED TO PANEL 1242A RT WING. THE PANEL WAS REMOVED AND THE LOWER SLAT DRIVE CYLINDER WAS INSPECTED AND FOUND TO BE SHEARED.May 9, 2000 · N12508 · Doug DC932 · Leading Edge Slat ActuatorSDR TWAA0007704Rib · crackedDURING OP 16 MAINT CHECK ON LT HORIZ STAB LEADING EDGE ASSEMBLY, NUMBER 1 LEADING EDGE RIB, I/B END WAS CRACKED ON BOTTOM TRAILING EDGE, NUMBER 1 FROM I/B END. ACCOMP HIGH FREQ EDDY CURRENT ON END OF CRACK FOR CONTAINMENT PER 51-00-03 PART 6 OF NDT MANUAL. SMay 9, 2000 · N921L · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR TWAA0007703Skin · dentedDURING OP 16 MAINT CHECK ON LT WING, FOUND DENTS IN LEADING EDGE OF NUMBER 3 LEADING EDGE SLAT, DENT LOCATED 13 INCHES I/B FROM O/B END OF SLAT WAS 1 INCH WIDE BY 1 INCH LONG AND 0.050 INCH DEEP, DENT LOCATED 18 INCHES I/B FROM O/B END OF SLAT WAS .75 INCH LONMay 9, 2000 · N921L · Doug DC932 · Leading Edge DevicesSDR ABXA000248Window · out of adjCAPTAIN''S CLEARVIEW WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. ADJUSTED CAM FOLLOWER VERTICAL AND EXTENSION ADJUSTMENTS.May 9, 2000 · N939AX · Doug DC932 · Flight Compartment WindowsSDR CA000621039Controller · failed(CAN) TRANSFER LOCKOUT/STANDBY ON LIGHT ON, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT AND SYSTEM CAUSED SURGE AND LARGE CABIN RATE CHANGE, USING STANDBY LEVER HUNGTING +/- 2 INCHES. CHANGED NR 2 CABIN PRESSURE CONTROLLER AND OUTFLOW VALVE ACTUATOR.May 8, 2000 · Doug DC932 · Cabin Pressure ControllerSDR AT0000270Skin · corrodedFOUND FORWARD CARGO COMPARTMENT SKIN UNDER NR 2 DME ANTENNA CORRODED AT BS 427. CUT OUT CORRODED SKIN, REMOVED 2 SPLICES, SHEAR TIES AND FLAPPER VALVE. FABRICATED 2 DOUBLER REPAIRS, FABRICATED SHEAR TIE SPLICE AND INSTALLED IAW DC9 SRM 53-04 FIGURE 44, 53-08May 8, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000267Skin · lightning strikeFOUND LIGHTNING STRIKE AT BS 317 AND BS 323. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 53-04 FIGURE 38 AND 12B.May 7, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000264Door Frame · crackedDURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL, FOUND FORWARD ENTRANCE DOOR AFT TOP DOOR STOP BOLT HOLES CRACKED. INSTALLED REPAIR DOUBLER IAW RES 00-0408.May 7, 2000 · N816AT · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0007104Fitting · crackedDURING ROUTINE CHECK, FOUND RT WING SPAR TO TRAP FITTING WITH CRACK BETWEEN TRAP ATTACH BOLTS. REPLACED THE RT SPAR TO TRAP FITTING PER SRM 51-00, STANDARD PRACTICE AND EMLR 70740. CHECK-C 3-10-00 STL.May 7, 2000 · N926L · Doug DC932 · Wing Miscellaneous StructureSDR AT0000235Fuel Cap · missingON TAKEOFF, PASSENGER REPORTED FUEL COMING FROM RIGHT WING. FOUND FUEL CAP MISSING FROM RIGHT WING. REPLACED CAP.May 6, 2000 · N840AT · Doug DC932 · Fuel StorageSDR GTIA000194Light · inoperativeMLG - FLT 403 - EMERGENCY PATH LIGHTING FORWARD OF ROW 7 INOPERABLE. COULD NOT DUPLICATE INOPERATIVE PATH LIGHTING. SYSTEM OPS CHECKED NORMALLY IAW DC-9 MM 33-00. (X)May 4, 2000 · N941ML · Doug DC932 · Emergency LightingSDR AT0000234Actuator · malfunctionedRUN AWAY TRIM - PRIMARY LONGITUDINAL AXIS 15 MIN FROM BOS. AUTOPILOT WAS ENGAGED. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR, AND PRIMARY LONGITUDINAL TRIM CONTACTOR RELAY IAW DC9 MM 27-40, 27-40-04.May 4, 2000 · N845AT · Doug DC932 · Stabilizer ActuatorSDR AT0000266Skin · crackedFOUND FORWARD CARGO COMPARTMENT LOWER AFT DOOR JAMB CORNER WAS CRACKED AT FASTENER HOLE. CUT OUT CRACKED AREA, INSTALLED FILLERS, DOUBLERS AND TRIPLER IAW TIMCO SERVICE ORDER 151015-36912.May 2, 2000 · N825AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000242Angle · wornFOUND BOTTON ANGLE LEFT AFT SIDE OF VERTICAL PANEL WORN BEYOND LIMITS. REMOVED AND REPLACED ANGLE IAW TIMCO SERVICE ORDER 151015-38274.May 2, 2000 · N825AT · Doug DC932 · Horizontal Stabilizer, Tab StructureSDR AT0000241Skin · gougedFOUND TOP OF VERTICAL STAB PANEL DEEPLY GOUGED ALONG AFT LEFT SIDE, 2 EACH. REMOVED AND REPLACED SKIN IAW TIMCO SERVICE ORDER 151015-36905.May 2, 2000 · N825AT · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR AT0000262Keelbeam · crackedDURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL., FOUND KEEL BEAM WEB CRACKED AT BS 700 AFT OF GEAR DOOR ACTUATOR. INSTALLED REPAIR IAW RES 00-00441.May 2, 2000 · N816AT · Doug DC932 · Fuselage Main, KeelSDR GTIA000190Light · inoperativeMLB - FLT 718 - EMERGENCY FLOOR EXIT LIGHTS INOPERABLE. CLEANED CONNECTION AND BATTERY PACK AT STA 160. OPS CHECK OK IAW MM 33-00. (X)May 2, 2000 · N941ML · Doug DC932 · Emergency LightingSDR MWEA00405Angle · corrodedSTATION 160 LEFT SIDE SUBFLOOR PANEL SUPPORT BEAM JUST UNDER GENERATOR, RELAYS HAVE CORROSION ON IT. FABRICATED AND INSTALLED NEW SUPPORT BEAM AND ANGLE.May 2, 2000 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00404Fitting · corrodedFITTING INSIDE AFT CARGO DOOR CUTOUT AT STATION 917 LONGERON 28 RIGHT EXFOLIATED. FABRICATED AND INSTALLED NEW FITTING.May 2, 2000 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00403Longeron · corrodedSTATION 172 HAS CORROSION AROUND FASTENERS ON LONGERON 29 RIGHT SIDE. INSTALLED NEW LONGERON AND SPLICES.May 2, 2000 · N205ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00390Pan · corrodedAFT LEFT WASTE WATER PAN FORWARD BOTTOM CORNER HAS CORROSION ON IT. INSTALLED NEW PAN.May 1, 2000 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00389Angle · crackedRIGHT HAND TRAPEZOIDAL PANEL IS CRACKED BETWEEN FASTENERS NR 1 & 2 AND BETWEEN NR 5 AND 7. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE.May 1, 2000 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00388Fitting · corrodedLONGERON 20 LEFT END SHOVEL CLIP AT STATION 996 HAS MODERATE CORROSION. REMOVED AND REPLACED FITTING.May 1, 2000 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00387Longeron · corrodedLONGERON 20 LEFT AT STATION 996 - 968 HAS CORROSION. FABRICATED AND INSTALLED NEW SECTION OF 20 LEFT LONGERON.May 1, 2000 · N205ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00386Angle · crackedLEFT MAIN LANDING GEAR DOOR JAMB ANGLE CRACKED JUST BELOW HYDRAULIC RESERVOIR. FABRICATED AND INSTALLED REPAIR DOUBLER.May 1, 2000 · N205ME · Doug DC932 · Landing Gear Doors
Back to Douglas DC-9-32