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 CA000215035Indicator · malfunctioned(CAN) WHEN GEAR SELECTED UP NLG DID NOT RETRACT, A/C RETURNED. GEAR INDICATOR LIGHT REPLACED.Jan 22, 2000 · Doug DC932 · Landing Gear Position and WarningSDR AT0000190Cap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT MAIN TANK TEE CAP TO HAVE CORROSION BEYOND LIMITS FROM STRINGER 11 TO STRINGER 23. REMOVED AND REPLACED RIGHT TEE CAP IAW DC9 SB 57-98.Jan 22, 2000 · N836AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000051Frame · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND AFT PIT AT BS 965 LS 23 FRAME CORRODED. REMOVED AND REPLACED CORRODED SECTION OF FRAME WITH NEW FRAME AT BS 965 LS 23 IAW DC9 SRM 51-30-02, 51-30-05, 51-10-04, 53-03 FIG 2A, AND 51-30-01.Jan 22, 2000 · N836AT · Doug DC932 · Fuselage Main, FrameSDR AT0000035Warning Light · illuminatedFOUND DURING LANDING GEAR EXTENTION, GEAR DOOR OPEN AMBER LIGHT STAYED ON. RECYCLED GEAR BY EMERGENCY EXTENTION METHOD. LIGHT REMAINED ON. LANDED WITH ABNORMAL PROCEDURES. FERRIED AIRCRAFT TO ORLANDO (MCO).Jan 22, 2000 · N805AT · Doug DC932 · Landing Gear Position and WarningSDR 0000539612Frame · crackedCANTED FRAME CRACKED IN AFT ACCESORY COMPARTMENT AT BS 1143 UNDER ACTUATOR FOR AIRSTAIR. CUT OUT CRACKED AREA AND REPAIRED PER EA 98-16725.Jan 22, 2000 · N612NW · Doug DC932 · Fuselage Main, FrameSDR MWEA00025Window · contaminatedFLIGHT CREW REPORTED SMOKE OR STEAM COMING FROM BEHIND MOULDING ON RIGHT CLEARVIEW WINDOW. MAINTENANCE FOUND GLYCOL DEICING FLUID BEHIND RIGHT SIDEWALL PANEL AND AROUND CLEARVIEW WINDOW.Jan 22, 2000 · N401ME · Doug DC932 · Passenger Compartment WindowsSDR CA000209047Panel · missing(CAN) ON ARRIVAL FOUND RT ENG UPPER COWL OVERPRESSURE RELIEF PANEL MISSING. INSTALLED.Jan 21, 2000 · Doug DC932 · Engine Cowling SystemSDR TWAA0002007Panel · crackedDURING OP 16 MAINT CHECK, FOUND LT MLG WHEEL WELL LT TRAP PANEL AREA, A CRACK HAD MIGRATED BEYOND STOP DRILL AND WAS IN MOUNT BOLT HOLE. CONFIRMED BY HIGH FREQ EDDY CURRENT. REMOVED 718 CASTING AND INSTALLED NEW LT 718 PER SERVICE BULLETIN 53-131 AND SPM 6-7Jan 21, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000037Strut · dischargedFOUND AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE AND GEAR WOULD NOT COME UP. RETURNED TO BMI (BLOOMINGTON-NORMAL). STEERING IN AIR WOULD TURN. INSPECTED AIRCRAFT AND FOUND NOSE STRUT FLAT. SERVICED STRUT IAW DC9 MM 32-30.Jan 21, 2000 · N866AT · Doug DC932 · Nose/Tail Landing Gear Strut/AxleSDR MWEA00029Brace · inoperativeLANDING GEAR REQUIRES FREE-FALL EXTENSION CHECK. DURING CHECK, THE LANDING GEAR WOULD NOT OVER CENTER. MTC REMOVED AND REPLACED LOWER SIDE BRACE.Jan 21, 2000 · N207ME · Doug DC932 · Landing Gear Retraction/Extension SystemSDR TWAA0001602Stringer · crackedDURING OP 16 MAINT CHECK STRINGER 2L WAS CRACKED AT STA 200. INSTALLED NEW STRINGER FROM STA 149 TO 229, WITH RIVETS PER SRM 51-30-2 AND 51-30-5.Jan 20, 2000 · N921L · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA000069Warning Light · illuminatedON TAKEOFF, ON GEAR RETRACTION, RIGHT MAIN GEAR INDICATED UNSAFE. RECYCLED GEAR, UNSAFE LIGHT WENT OUT. CONTINUED FLIGHT WITH NO FURTHER PROBLEMS. CHECKED OPERATION OF RIGHT MAIN LANDING GEAR AND CONTROLS. NO DEFECTS NOTED. LUBRICATED MAIN LANDING GEAR.Jan 20, 2000 · N900AX · Doug DC932 · Landing Gear Position and WarningSDR AT0100042Pan · corrodedFOUND C2 DOOR LOWER PAN CORRODED BEYOND LIMITS. REPLACED LOWER PAN IAW DC9 SRM 53-04 FIG 44, 51-10-03, 51-10-04, 51-30-02, AND 51-30-05.Jan 19, 2000 · N802AT · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0001406Floor Panel · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 23 HAD CORROSION. FABRICATED NEW FLOOR PANEL PER SRRM 53-00-104, PAGE 201.Jan 19, 2000 · N925L · Doug DC932 · Fuselage Floor PanelSDR AT0000050Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON PANEL NR 6402 OUT OF LIMITS. FABRICATED AND INSTALLED SKIN FOR PANEL NR 6402 IAW DC9 SRM 55-01 FIG 1, 51-70-02, AND 51-10-03.Jan 19, 2000 · N836AT · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR AT0000049Longeron · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LONGERON NR 30 CORRODED BETWEEN STATIONS 200 AND 218 AFTER REMOVAL OF CORROSION, FOUND LONGERON OUT OF LIMITS. CUT OUT DAMAGED AREA AND INSTALLED LONGERON SPLICE IAW DC9 SRM 51-10-03, 52-01 FIG 1, Jan 19, 2000 · N836AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000048Spar · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK ON RIGHT ELEVATOR SPAR AT ES 76-75. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLES AT ES 76-75 IAW EO 12-5520-29-B1092, DC9 SRM 51-20, 51-30-02, 51-20-03, AND 55-02.Jan 19, 2000 · N836AT · Doug DC932 · Elevator, Spar/RibSDR AT0000044Web · corrodedFOUND ELECTRICAL COMPARTMENT COCKPIT SUBFLOOR CORRODED AT BS 150-160. CUT OUT CORRODED AREA OF SUBFLOOR, FABRICATED FILLER/DOUBLER AND INSTALLED IAW DC9 SRM 51-30-2, 53-11-1, 53-01 FIGURE 4, 51-10-4, 51-10-3, 53-01.Jan 19, 2000 · N803AT · Doug DC932 · Fuselage Internal Mounting StructureSDR AT0000043Floorbeam · corrodedFOUND AFT PIT CABIN FLOORBEAM HAS EXFOLIATED CORROSION AT BS 996. REMOVED FLOORBEAM UPPER CAP, FABRICATED NEW CAP ANGLE, TREATED, PRIMED AND INSTALLED NEW CAP ANGLE IAW DC9 SRM 51-30-2, 51-30-5, 53-11-3 FIGURE 11, 51-10-4, 51-30-3.Jan 19, 2000 · N803AT · Doug DC932 · Fuselage Main, Floor BeamSDR 0000219982Wire · brokenDURING PERIODIC CHECK, FOUND CATWALK EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPAIRED WIRING AT AFT MOST CATWALK LIGHT. OPERATIONAL CHECK NORMAL.Jan 19, 2000 · N982US · Doug DC932 · Light System WiringSDR MWEA00022Cover · dislodgedFORWARD GALLEY DOOR SLIDE COVER CAME OFF. MTC REINSTALLED GALLEY DOOR SLIDE COVER.Jan 19, 2000 · N206ME · Doug DC932 · Escape SlideSDR MWEA00021Slide · dislodgedGALLEY DOOR EMERGENCY EVACUATION SLIDE PACK CAME OUT OF COVER. MAINTENANCE REINSTALLED SLIDE PACK.Jan 19, 2000 · N216ME · Doug DC932 · Escape SlideSDR TWAA0101020Longeron · crackedDURING CHECK-C MAINT, LONGERON 3R WAS CRACKED AT FORMER RING STA 639. INSTALLED NEW LONGERON SECTION AND SPLICE PER SRO9530128.Jan 18, 2000 · N995Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0001414Support · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL NUMBER 26, HAD SUPPORT RIB CRACKED. FABRICATED PANEL PER SSRM 53-00-104, PAGE 102.Jan 18, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0001203Support · crackedDURING OP 16 MAINT CHECK, THE VERTICAL SUPPORT WAS CRACKED AT STA 69, RBL 12 AT 1 O'CLOCK POSITION. INSTALLED NEW VERTICAL SUPPORT PN 9951860-6 PER DOUGLAS DRAWING 9957860 AND SPM 6-70-01, PAGE 3 PART 4B.Jan 18, 2000 · N921L · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000045Fitting · corrodedFOUND DURING REMOVAL OF WEB, FITTING WAS EXFOLIATED WITH CORROSION AT BS 996. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-01 FIGURE 1, 51-10-4, 51-30-5.Jan 18, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000035R1Bracket · looseFOUND DURING LANDING GEAR EXTENTION, GEAR DOOR OPEN AMBER LIGHT STAYED ON. RECYCLED GEAR BY EMERGENCY EXTENTION METHOD. LIGHT REMAINED ON. LANDED WITH ABNORMAL PROCEDURES. FOUND LOOSE GEAR DOOR ROLLER BRACKET ASSEMBLY, ON LEFT HAND GEAR DOOR. TIGHTENED BRJan 18, 2000 · N805AT · Doug DC932 · Landing Gear Retraction/Extension SystemSDR AT0000034Engine · failedFOUND LEFT ENGINE UNSPOOLED, AFTER TAKEOFF, WITH VIBRATION. ENGINE CHANGE IN PROGRESS.Jan 18, 2000 · N828AT · Doug DC932 · Engine (Turbine/Turboprop)SDR MWEA00020Slide · dislodgedFWD GALLEY DOOR EVACUATION SLIDE FELL OUT. MAINTENANCE REINSTALLED NEW SLIDE ASSEMBLY.Jan 18, 2000 · N401ME · Doug DC932 · Emergency EquipmentSDR TWAA0001413Floor Panel · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL MEMBER NUMBER 12 HAD CORROSION ON IT. REF CPCP TASK C46-53306 FWD GALLEY AREA. REMOVED CORROSION PER SPM 51-10-3 AND TREATED.Jan 17, 2000 · N925L · Doug DC932 · Fuselage Floor PanelSDR GTIA000029Terminal · shortACY - FLT 541 - COCKPIT EMERGENCY LIGHT ILLUMINATES WHEN CABIN ENTRY OR ATTENDANT LIGHT SWITCHES ARE ON. IF ENTRY OR HTT LIGHT SWITCHES ARE OFF, THEN CABIN EMERGENCY LIGHT LOCATED IN ENTRY LIGHT FIXTURE WILL NOT ILLUMINATE WHEN THE EMERGENCY LIGHT SWITCH IS IJan 17, 2000 · N12536 · Doug DC932 · Emergency LightingSDR AT0000047Doubler · corrodedFOUND CORROSION OUT OF LIMITS ON G-4 LEFT HAND GALLEY SIDEWALL. CUT OUT CORRODED AREA, FABRICATED FILLER/DOUBLER, AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2.Jan 17, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000017Battery Pack · dischargedFOUND BOTH RIGHT OVERWING EMERGENCY EXIT LIGHTS DIM AND FLICKERING. REMOVED AND REPLACED BOTH RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACKS IAW DC9 MM 33-53.Jan 17, 2000 · N840AT · Doug DC932 · Emergency LightingSDR ABXA000009Power Supply · dischargedDURING PREFLIGHT INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY.Jan 17, 2000 · N987AX · Doug DC932 · Emergency LightingSDR 2000ZZZM97Seal · failedAFTER T/O, THE FLT CREW EXPERIENCED PRESS DIFFICULTY. CAPT WAS NOTIFIED BY THE SENIOR F/A OF A LOUD SQUEAL COMING FROM LEFT FWD EMERGENCY EXIT DOOR. A DECISION WAS MADE TO LAND THE A/C. A/C WAS LANDED W/O FURTHER INCIDENT UNDER NORM CONDITIONS. AFTER LANDIJan 17, 2000 · N930BB · Doug DC932 · Emergency ExitsSDR GTIA000027Light · inoperativeACY - FLT 544 - CABIN EMERGENCY LIGHTS INOPERATIVE. COCKPIT EMERGENCY LIGHTS STAYS ON CONTINUOUSLY. FOUND EMERGENCY LIGHT AT L1 DOOR GROUNDED ON AIRFRAME. RELOCATED WIRE AND REPAIRED WIRE. CHECK NORMAL. (M)Jan 16, 2000 · N12536 · Doug DC932 · Emergency LightingSDR MWEA00015Skin · corrodedRIGHT HAND AILERON ON INBOARD SKIN IS CORRODED UNDER CHAFE PLATE IN SEVERAL AREAS. MTC FABRICATED AND INSTALLED FILLER AND DOUBLER.Jan 16, 2000 · N203ME · Doug DC932 · AileronsSDR MWEA00014Pressure Switch · defectiveEN ROUTE TO MKE, LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED. FOLLOWED QRH AND DIVERTED TO CLE. MTC REMOVED AND REPLACED DIFFERENTIAL PRESSURE SWITCH.Jan 16, 2000 · N216ME · Doug DC932 · Engine Oil PressureSDR GTIA000028Light · inoperativeDTW - FLT 570 - CABIN EMERGENCY LIGHTS OVERHEAD INOPERATIVE. REPAIRED WIRE ON LIGHT ASSEMBLY AT FORWARD PASSENGER ENTRANCE DOOR. OPS CHECKED GOOD IAW DC-9 MM. (M)Jan 15, 2000 · N12536 · Doug DC932 · Emergency LightingSDR TWAA0001412Support · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 25 SUPPORT RIBS CRACKED. FABRICATED NEW FLOOR PANEL WITH NEW RIBS PER SPM 6-70-01, PAGES 2 AND 3, AND SSRM 53-00-102 PAGE 201.Jan 14, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0001411Floor Panel · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 35 HAD CORROSION. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201.Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor PanelSDR TWAA0001410Support · damagedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 40C SUPPORT RIBS DAMAGED. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.Jan 14, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0001409Floor Panel · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL SCREW HOLES CRACKED IN SEVERAL PLACES, PANEL 48. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor PanelSDR TWAA0001408Floor Panel · damagedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 77, HAD THE END OF THE PANEL BROKEN OUT. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor PanelSDR TWAA0001407Floor Panel · damagedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 42 HAD BOTTOMSIDE IN CHANNEL. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201..Jan 14, 2000 · N925L · Doug DC932 · Fuselage Floor PanelSDR TWAA0001405Support · crackedDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL 40A SUPPORT RIBS CRACKED. REPLACED SUPPORT RIBS WHILE FABRICATING NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201. PICKED UP HOLES ON PANEL 40A.Jan 14, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000028Floor Board · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT SIDE CABIN FLOORBOARD CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOORBOARD IAW DC9 SRM 53-01 FIG 1, 51-10-03, 51-10-04, AND 51-30-02.Jan 14, 2000 · N836AT · Doug DC932 · Fuselage Floor PanelSDR ABXA000084Panel · crackedUPPER OUTBOARD FLANGE OF LEFT TRAP PANEL CRACKED IN AREA OF HYDRAULIC LINES. VERIFIED WITH EDDY CURRENT INSPECTION. REPLACED LEFT TRAP PANEL IAW REA NR D953-35095-MR AND DC9 SERVICE BULLETIN 53-182.Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000083Intercostal · crackedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000082Fitting · crackedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND RIGHT WHEEL WELL KEEL TO FLOORBEAM ATTACH FITTING CRACKED AT STA 718. REPLACED FITTING IAW DC9 SRM 51-30-5.Jan 14, 2000 · N980AX · Doug DC932 · Fuselage Miscellaneous Structure
Back to Douglas DC-9-32