Douglas DC-9-32

Service difficulty reports · 12,755

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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"

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SDR 9900719985Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE SKIN AT FS 218 BETWEEN LONGERONS 23R AND 24R. INSTALLED REPAIR PER SRM 53-04, FIG 12B AND EA 99-163457.Feb 26, 1999 · N985US · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9903406Former · crackedDURING OP 15 MAINT CHECK, FOUND FORMER FOOT CRACKED AT STA 965, BETWEEN LONGERON 13, 14, 15 AND 16, LEFT SIDE. REPLACED FORMER FOOT PER MO 72514 AND PER DWG J060119, AND EMLR 69313.Feb 25, 1999 · N923L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9903405Skin · damagedDURING OP 15 MAINT CHECK, FOUND SKIN DAMAGED AND LONGERON 19L CRACKED AT STA 218. REPAIRED SKIN PER SRM 53-04 PAGE 218R. LONGERON REPAIRED PER SPM 6-70-01, PAGE 2.Feb 25, 1999 · N923L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9903404Floorbeam · corrodedDURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION BETWEEN MEMBRANE LAYERS AT STA 160 TO 165, RBL 43 TO 53. REMOVED CORROSION AREA BETWEEN MEMBRANE LAYERS AND FABRICATED ALUMINUM ALLOY REPAIR. PRIMED AND PAINTED AND INSTALLED PER SRM 53-01.Feb 25, 1999 · N923L · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9900194Wire · brokenTHE EMERGENCY AISLE PATH LIGHTS DID NOT ILLUMINATE WHEN ON POSITION WAS SELECTED DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A BROKEN WIRE ON SWITCH IN COCKPIT. THE SWITCH WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED.Feb 25, 1999 · N43537 · Doug DC932 · Light System WiringSDR AT9900286Bulkhead Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND AFT PIT BULKHEAD LINER SUPPORT ANGLE CORRODED AND GILLINER PANEL MISSING. FORMED SUPPORT ANGLE, CUT, DRILLED, TRIMMED ANGLE AND GILLINER PANEL, TREATED, PRIMED AND INSTALLED ANGLE TO GILLINER PANEL IAWFeb 25, 1999 · N813AT · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9900141Longeron · crackedDURING C-CHECK, FOUND LONGERON 2 LEFT, STATION 200 CRACKED. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.Feb 25, 1999 · N900AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA99080Adc · inopON TAKEOFF AT 20,000 FT THE FIRST OFFICER MAIN ALTIMETER FLAGGED AT 20,000 FT AND THE NEEDLE STUCK THERE. MTC REMOVED AND REPLACED NUMBER TWO AIR DATA COMPUTER.Feb 24, 1999 · N207ME · Doug DC932 · Air Data ComputerSDR AT9900356Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 209 BRACKET CORRODED. REMOVED AND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2.Feb 24, 1999 · N822AT · Doug DC932 · Wing Miscellaneous StructureSDR AT9900355Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 222 BRACKET CORRODED. REMOVED AND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2.Feb 24, 1999 · N822AT · Doug DC932 · Wing Miscellaneous StructureSDR AT9900354Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 238 BRACKET CORRODED. REMOVED AND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2.Feb 24, 1999 · N822AT · Doug DC932 · Wing Miscellaneous StructureSDR AT9900279Web · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT CUSP WEB AT BS 229 L-18 CORRODED. REMOVED CORRODED PORTION OF WEB, REMOVED SUPPORT FITTING FOR ACCESS AND FLOOR SUPPORT SECTION. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED NEW SECTION AND REFeb 24, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900184Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT TIEDOWN TRACK CORRODED ON BOTH SIDE AT BS 332 TO 465. REMOVED AND REPLACED TIEDOWN TRACK IAW DC9 SRM 51-10-3.Feb 24, 1999 · N822AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900142Cover · looseFOUND THE R-1 DOOR SLIDE COVER NEEDS TO BE SECURED AND INSPECTED FOR PROPER INSTALLATION. SECURED SLIDE COVER PER MM 25-60.Feb 24, 1999 · N805AT · Doug DC932 · Emergency EquipmentSDR 9900819985Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 26L BETWEEN FS 218 AND FS 229. SPLICED IN NEW LONGERON PER EA 99-163380.Feb 24, 1999 · N985US · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9900809985Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON SKIN UNDER FRAME 598 ON FORWARD SIDE ONE INCH BELOW LONGERON 18R. REPAIRED PER EA 99-165598.Feb 24, 1999 · N985US · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9903101Frame · crackedDURING OP 15 MAINT CHECK, THE TOP OF LT AFT EMERGENCY EXIT FRAME WAS CRACKED .5 INCH AT STA 667. INSTALLED REPAIR DOUBLER PER SRM 53-05, PAGE 79.Feb 23, 1999 · N923L · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA99081Valve · inopAIRCRAFT UNABLE TO PRESSURIZE, RETURNED TO MKE. MTC REMOVED AND REPLACED RIGHT AUGMENTATION VALVE.Feb 23, 1999 · N401ME · Doug DC932 · Cabin Pressure Control SystemSDR AT9900348Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE BRACKET AND PULLEYS BEARING ON THE NOSE LANDING GEAR WHEEL WELL AT BS 110 LBL17 CORRODED. REMOVED AND REPLACED FORWARD BRACKET AND PULLEYS, RIGGED AND OPS CHECKED GOOD IAW DC9 MM 20-16-0, AND 32-23-1.Feb 23, 1999 · N822AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900340Spar Web · crackedSCHEDULED INSPECTION AT AERO CORP, FL, DURING ACCOMPLISHMENT OF SB 57-200, FOUND A CRACK AT THE LOWER EDGE SPAR WEB OUTBOARD OF XCW 58 FITTING. REPAIRED AFT SPAR WEB LEFT SIDE AT XCW 58, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SB 57-200 AND DRAWING NR 5935Feb 23, 1999 · N822AT · Doug DC932 · Wing SparSDR AT9900339Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL, A CRACK ABOVE A REPAIR DOUBLER WAS FOUND IN THE LEFT WHEEL WELL OUTBOARD SIDE STRAP PANEL AT THE BS 718 FRAME. REMOVED AND REPLACED THE FRAME AT BS 718 IAW DC9 SRM 51-30-2, 51-10-0, 51-10-2, 51-10-5, 51-20-0, 51-30-5, ANFeb 23, 1999 · N822AT · Doug DC932 · Fuselage Main, FrameSDR AT9900213Fitting · chafedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING IN WHEEL WELL WITH A DEEP CHAFE MARK FROM A HYDRAULIC LINE RUBBING AT BS 699. BLEND AREA SMOOTH, HFEC VERIFY NO CRACKS NOTED. RESTORED ORIGINAL FINISHED, ALODFeb 23, 1999 · N815AT · Doug DC932 · Landing Gear Door ActuatorSDR AT9900141Cable · brokenFOUND THE R-1 DOOR SLIDE (LANYARD ASSEMBLY) PULL CABLE BROKEN. REMOVED AND REPLACED THE DOOR SLIDE CABLE LANYARD AND RETURNED THE AIRCRAFT TO SERVICE IAW MM 25-60.Feb 23, 1999 · N823AT · Doug DC932 · Escape SlideSDR TWAA9903103Angle · crackedDURING OP 15 MAINT CHECK, FOUND THE LT WING INBD AND OTBD SIDE OF OTBD HINGE CASTING INTERNAL ATTACH RIB ANGLE CRACKED AT ATTACH HOLES. RIBS AND HINGE CASTING REPLACED WITH NEW SERVICEABLE PARTS PER SRM 27-50-01.Feb 22, 1999 · N923L · Doug DC932 · Wing Miscellaneous StructureSDR TWAA9903102Angle · crackedDURING OP 15 MAINT CHECK, FOUND THE RT WING OTBD HINGE CASTING INTERNAL ATTACH RIB ANGLES CRACKED INBD AND OTBD SIDE. THE RIB AND HINGE CASTING WAS REPLACED WITH NEW SERVICEABLE PARTS PER SRM 27-50-01.Feb 22, 1999 · N923L · Doug DC932 · Wing Miscellaneous StructureSDR MWEA99075Slide · detachedFORWARD PASSENGER DOOR SLIDE FELL OFF DOOR. MTC REINSTALLED DOOR SLIDE.Feb 22, 1999 · N202ME · Doug DC932 · Emergency EquipmentSDR MWEA075Slide · detachedMCI - FORWARD PASSENGER DOOR SLIDE FELL OFF DOOR. MTC RE-INSTALLED DOOR SLIDE. (X)Feb 22, 1999 · N202ME · Doug DC932 · Emergency EquipmentSDR MWEA99074Battery Pack · dischargedMKE - THE RIGHT NACELLE EMERGENCY BATTERY PACK INOPERABLE. MTC REMOVED AND REPLACED EMERGENCY BATTERY PACK. (X)Feb 21, 1999 · N202ME · Doug DC932 · Emergency LightingSDR AT9900343Support · crackedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT CARGO COMPARTMENT FLOOR SUPPORT ON AFT SIDE OF FRAME AT BS 775 BETWEEN L27-28R CRACKED. REMOVED FLOOR SUPPORT, WELDED REPAIR BY USING AMS 4951 FILLER WIRE AND REINSTALLED SUPPORT IAW DC9 SRM 51-30-2, 51-30-Feb 21, 1999 · N822AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900342Tie Down · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE G-2 GALLEY FLOOR MOUNTED TIE DOWNS AT BS 980 CORRODED. REMOVED AND REPLACED THE G-2 GALLEY FLOOR MOUNTS TIE DOWNS (4 EA) IAW DC9 MM 25-32-0.Feb 21, 1999 · N822AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900283Channel · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT COMPARTMENT LEFT HAND HAT CHANNEL ADJACENT TO THE LOWER BULKHEAD PRESSURE CAP CORRODED AT BS 996 ON THE LOWER END. REMOVED CORROSION, REMOVED AND REPLACED HAT CHANNEL, LOCATED, DRILLED AND INSTALLED IAW DC9 Feb 21, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900248Longeron · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND LONGERON IN THE FORWARD PIT AT BS 218L-23L CORRODED. REMOVED CUT OUT CORRODED SECTION, FABRICATED REPAIR LONGERON SPLICES AND INSTALLED IAW DC9 SRM 51-30-2, 51-30-5 AND 53-02 FIG 18.Feb 21, 1999 · N822AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9902803Skin · crackedDURING OP 15 MAINT CHECK, FOUND THE ADF LOOP ANTENNA AFT MOUNTING HOLES IN SKIN WITH CRACKS. STOP DRILLED THREE CRACKS AT MOUNT HOLES AND INSTALLED REPAIR PER SRM 53-04, FIG 29.Feb 20, 1999 · N923L · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA99077Battery Pack · dischargedMKE - THE FORWARD ENTRANCE EMERGENCY LIGHTS COME ON WHEN ALL AIRCRAFT POWER IS REMOVED. MTC REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. (X)Feb 20, 1999 · N602ME · Doug DC932 · Emergency LightingSDR AT9900294Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT FORWARD LOWER FLOOR PANEL BRACKET CORRODED AT BS 218 LBL 42. REMOVED BRACKET, CUT, DRILLED, TRIM, ALODINED, PRIMED, INSTALLED NUT PLATE ON BRACKET AND INSTALLED IAW DC9 SRM 51-30-2, 53-21-0 FIG 2D, 51-10-3 Feb 20, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900290Bracket · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE GILLINER ATTACH ANGLE CRACKED AT BS 237 L-24. PERFORMED HFEC TO VERIFIED CRACK. REMOVED CRACKED ATTACH ANGLE, WELDED REPAIR CRACK ON ANGLE IAW EA 12-5321-29-C1362 USING AMS 4951 FILLER WIRE AND INSTALLED ANGLE Feb 20, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900288Floorbeam · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND UPPER CAP CRACKED AND CORRODED ON FLOORBEAM WEB AT BS 996 RBL 54. REMOVED PULLEY TOWERS, REMOVED FLOOR UPPER BEAM CAP. LOCATED AND DRILLED NEW FLOORBEAM CAP, ALODINED, PRIMED, AND INSTALLED FLOORBEAM AND REINSTALLEFeb 20, 1999 · N813AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT9900287Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO COMPARTMENT FUEL SHUT OFF BRACKET AT BS 935 CORRODED. RELIEVED CABLE TENSION, REMOVED AND REPLACED BRACKET ASSEMBLY, RIGGED SYSTEM AND ALL OPS CHECKS GOOD IAW DC9 MM 20-18-0, 76-12-0 PG 206, 20-16-0, AFeb 20, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9902804Spar · crackedDURING OP 15 MAINT CHECK, FOUND LT WING TRAILING EDGE REAR SPAR CENTER UPPER FLAP ATTACH HOLES, I/B AND O/B WITH CRACKS. ACCOMP NDT HIGH FREQ EDDY CURRENT PER SRM 51-00-03, PART 6 CRACK CONTAINMENT. BLENDED AREA PER SRM 57-01, PG 5, FIG 1 SHEET 3. INSTALLEDFeb 19, 1999 · N923L · Doug DC932 · Wing SparSDR CA990330070Indicator · failed(CAN) FUEL SPILL FROM RIGHT WING VENT BOX DURING RE-FUELING, PASS AND CREW EVACUATED. LEFT WING FUEL QUANTITY INDICATOR NOT WORKING. REPLACED BOTH LUGS ON FUEL QUANTITY PROBE.Feb 19, 1999 · Doug DC932 · Fuel Quantity IndicatorSDR AT9900347Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND PULLEYS AND ATTACH BRACKET ON THE NOSE LANDING GEAR WHEEL WELL AT BS 69 LBL 28 CORRODED. REMOVED AND REPLACED BRACKET FOR GROUND SENSE ASSEMBLY WITH NEW HARDWARE AND TWO PULLEYS IAW DC9 20-16-0. RIGGED AND OPS CHEFeb 19, 1999 · N822AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900341Retainer · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THREE RETAINER RINGS CARGO TIE DOWN IN FORWARD PIT LEFT SIDE AT BS 218-332 CORRODED. REMOVED CORROSION, FABRICATED REPAIR RETAINER, TREATED, AND PRIMED IAW DC9 SRM 53-01 FIG 1, 51-10-2, AND 51-10-4.Feb 19, 1999 · N822AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900293Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SIDE ROLLER BEARING FITTING CORRODED ON THE INBOARD LEFT SIDE OF THE HORIZONTAL STABILIZER. REMOVED AND REPLACED LEFT HAND INBOARD BRACKET ON THE HORIZONTAL STABILIZER IAW DC9 MM 55-10-0.Feb 19, 1999 · N813AT · Doug DC932 · Horizontal Stabilizer StructureSDR AT9900285Floor · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE G-4 FLOOR PAN SKIN CORRODED. REMOVED FLOOR PAN HAT SECTION, FABRICATED NEW SKIN, TREATED, PRIMED, INSTALLED SKIN AND REINSTALLED HAT SECTION IAW DC9 SRM 51-30-2, 51-10-3 AND 51-10-2.Feb 19, 1999 · N813AT · Doug DC932 · Fuselage Floor PanelSDR AT9900193Support · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT IN THE FORWARD CARGO PIT AT BS 238 OVER L-28R CORRODED. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR, ALODINE, PRIMED, AND INSTALLED SUPPORT AND REPAIR IAW DC9 SRM 53-01-FIG 1, 51-10-3, AND 51-30-Feb 19, 1999 · N815AT · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9900919Skin · damagedTEMPORARY SKIN PANEL REPAIR AT STATION 218 TO 229 L-17 TO 18L. REMOVED SKIN AND REPLACED WITH FABRICATED SKIN AND DOUBLERS IAW DC9 SRM 53-04 FIG 47. ALL PARTS WERE FAY SURFACE SEALED AND INSTALLED WITH WET FASTENERS IAW DC9 SRM 53-04 FIG 47 HI-LOCK WERE INSTFeb 18, 1999 · N13512 · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900346Strap · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THREE ACCESS PANEL STRAPS IN THE FORWARD PIT AT BS 218-294 CORRODED. REPLACED STRAPS, FABRICATED, DRILLED, DEBURRED, TRIMMED TO FIT, INSTALLED CAMLOCKS, ALODINED, AND PRIMED IAW DC9 SRM 51-10-3, 51-10-4, 51-10-2, 5Feb 18, 1999 · N822AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900344Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, NOTED ON EXTERIOR OF SKIN AND FASTENERS AT BS 296 FORWARD OF EXISTING REPAIR CORRODED. DRILLED OUT FASTENERS AND REMOVED EXISTING REPAIR. CUT OUT SECTION OF SKIN AND REMOVED SHEAR TIE, FABRICATED REPAIR FILLER AND FINGEFeb 18, 1999 · N822AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900295Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHTNING STRIKES ON THE LEFT SIDE NOSE AT Y-69.550 AND RIGHT SIDE NOSE AT Y-69.550 AND Y-76.550. REMOVED E/E ACCESSORY DOOR, BULKHEAD VENT AND LIGHT BRACKET. CUT OUT LIGHTNING STRIKE AND FOUR FASTENER CRACKS. FOFeb 18, 1999 · N813AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900187Tie Down · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO PIT TIEDOWN TRACK AT BS 427-503 RIGHT SIDE CORRODED. ORDERED A NEW SECTION OF TRACK AND INSTALLED IAW DC9 SRM 51-10-4, AND 53-05 PG 1014.Feb 18, 1999 · N822AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
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