N18835, cancelled Jun 23, 2005

Service difficulty reports · 46

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N18835' AND deregistration_id = 'N18835-2005-06-23'
  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 CALA0400616Flange · crackedINSPECTION FOUND A 3 INCH CRACK IN THE AFT CARGO DOOR FORWARD LOWER STOP FLANGE. REPAIRED IAW ECRA 5232-01047.Aug 25, 2004 · N18835 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0400609Release Cable · out of rigTHE TAILCONE PULL CHECK FROM THE INTERIOR RELEASE HANDLE, FAILED. THE CABLES WERE ADJUSTED IAW MM 53-53-00.Aug 20, 2004 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CALA0400602Seat Track · corrodedINSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1007-1098, BL 0 TO LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.Aug 13, 2004 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0400601Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, BETWEEN LONGERON 13R AND 14R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 18.Aug 13, 2004 · N18835 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0400600Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, LONGERON 13L TO 14L. THE CRACKED AREA OF SKIN WAS CUT OUT AND FILLER AND A DOUBLER WERE INSTALLED IAW SRM 53-04, FIGURE 18 AND 51-10-3B.Aug 13, 2004 · N18835 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0400598Seat Track · corrodedINSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 200-218, RBL 22. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05.Aug 12, 2004 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0400596Seat Track · corrodedINSPECTION FOUND LT MID SEAT TRACK CORRODED FROM STA 1098-1201, LBL 30. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 12, 2004 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0400593Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1155 BETWEEN LT IB AND LT MID SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-5.Aug 6, 2004 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0300654Skin · corrodedINSPECTION FOUND RT WING LOWER T/E SKIN CORRODED AT REAR SPAR STA XRS 399-477. A SKIN DOUBLER WAS INSTALLED IAW ECRA 5731-01037.Nov 20, 2003 · N18835 · Doug DC982 · Wing, Plate/SkinSDR CALA0300653Spar · corrodedINSPECTION FOUND RT WING FORWARD SPAR CORRODED AT STA XRS 258-335. REPAIRED IAW ECRA 5731-01040.Nov 20, 2003 · N18835 · Doug DC982 · Wing SparSDR CALA0200467Web · corrodedINSPECTION FOUND AFT BAGGAGE BIN SUB FLOOR STRUCTURE PLATE(WEB) CORRODED BETWEEN STA 1211 AND 1231 ABOVE LONGERON 28L-27R. REPAIRED IAW ECRA 5311-01133.Sep 18, 2002 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200205Charger · failedTHE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 5-12 WERE FOUND INOPERATIVE DURING S CHECK INSPECTION. TROUBLESHOOTING IAW WDM 33-51-14 FOUND THE BATTERY CHARGER AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.Apr 15, 2002 · N18835 · Doug DC982 · Emergency LightingSDR CALA0001161Spacer · wornTHE NLG GEAR WOULD NOT FULLY RETRACT DURING TEST FLIGHT. MAINTENANCE FOUND THE NLG UPPER BEARING STRUT SPACER AND RING DAMAGED/WORN. THE NLG STRUT WAS REMOVED. THE SPACER AND NOSE STRUT SEALS WERE REPLACED IAW MM 32-21-02, PARAGRAPH 3A AND 3B. THE NLG STRUJul 27, 2000 · N18835 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA0001147Pan · crackedINSPECTION FOUND A 1 INCH CRACK IN SECOND FROM THE TOP MID CARGO DOOR AFT STOP PAD. A DOUBLER WAS INSTALLED ON DOOR PAN IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01565.Jul 24, 2000 · N18835 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001120Skin · damagedINSPECTION FOUND EXTERIOR FUSELAGE SKIN CREASED AT STA 256, LONGERON 18L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02978.Jul 21, 2000 · N18835 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001119Cable · frayedINSPECTION FOUND UPPER LEFT O/B AREA OF TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REPLACED AND TAIL CONE RELEASE MECHANISM WAS RIGGED IAW MM 53-53-00.Jul 21, 2000 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CALA0001086Pan · wornINSPECTION FOUND FORWARD CARGO DOOR AFT SIDE NR 1 STOP PAD AND FORWARD SIDE NR 5 STOP PAD WORN. REPAIRED IAW ECRA 5230-01540.Jul 17, 2000 · N18835 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001085Door Frame · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB CORRODED. REPAIRED IAW SRM 53-05, FIGURE 44.Jul 17, 2000 · N18835 · Doug DC982 · Fuselage Main, StructureSDR CALA0001082Spacer · corrodedINSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR Z-BEAM SPACER CORRODED AT STA 1155 - 1212. THE LOWER DOOR Z-BEAM SPACER WAS REMOVED AND REPLACED IAW SRM 51-10-2.Jul 17, 2000 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001092Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 BELOW LONGERON 16L AFT OF MAIN CABIN DOOR. THE DENT WAS COLD WORKED AND A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.Jul 14, 2000 · N18835 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001067Skin · dentedINSPECTION FOUND EXTERIOR SKIN DENTED AT STA 237, LONGERON 17L TO 18L. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-02445.Jul 14, 2000 · N18835 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001060Longeron · bentINSPECTION FOUND LONGERON 16R BENT FROM STA 250 - 252. A LONGERON SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18.Jul 12, 2000 · N18835 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0001031Seat Track · corrodedINSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 200 - 245. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, SHEETS 1, 9 AND 10.Jul 11, 2000 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900819Battery Charger · inoperativeINSPECTION FOUND TAIL CONE EMERGENCY AISLE PATH LIGHTING INOPERATIVE. THE BATTERY CHARGER AT AFT SERVICE DOOR OVERHEAD PANEL WAS REMOVED AND REPLACED IAW MM 33-50.Jul 13, 1999 · N18835 · Doug DC982 · Emergency LightingSDR CALA9801156Clips · out of adjustTHE TAIL CONE RELEASE HANDLE INSIDE TAIL COMPARTMENT PULLED HIGH FROM CLIPS AT 45 POUNDS. THE CLIPS WERE ADJUSTED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-50-00.Jun 23, 1998 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CALA9801155Cables · out of adjustTHE TAIL CONE PULL FROM INTERIOR RELEASE HANDLE, EXTERIOR RELEASE HANDLE, AND AFT ENTRY DOOR WAS LOW. THE TAIL CONE CABLES WERE RIGGED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-53-00.Jun 22, 1998 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CALA9801154Rail · corrodedINSPECTION FOUND LT TIE DOWN RAIL HAD EXFOLIATED CORROSION AT ATTACH FASTENER AND BELTFRAME AT STA 1022 WITH LIGHT TO MODERATE CORROSION AT STA 1003 TO 1221. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jun 22, 1998 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9801145Pivot Plates · corrodedINSPECTION FOUND VERTICAL FIN RIGHT SIDE INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED IN SLEEVE BORE. THE INBOARD AND OUTBOARD SET OF PIVOT PLATES WERE REMOVED AND REPLACED IAW SRM 51-30-5.Jun 19, 1998 · N18835 · Doug DC982 · Vertical StabilizerSDR CALA9801132Skin · dentedINSPECTION FOUND A DENT IN RT FUSELAGE SKIN AT STA 282. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38.Jun 19, 1998 · N18835 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9801128Jamb · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT DOOR JAMB Z-ANGLE BEAM CORRODED AT STA 1155-1211, LONGERON 26R. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63.Jun 19, 1998 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9801127Intercostal · crackedINSPECTION FOUND THE MAIN CABIN DOOR INTERCOSTAL JUST AFT OF LOCK MECHANISM HAD A 1/2 CRACK AT EXTERNAL HANDLE RECESS. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.Jun 18, 1998 · N18835 · Doug DC982 · Passenger/Crew DoorsSDR CALA9801126Beam · crackedINSPECTION FOUND A 1.5 CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.Jun 17, 1998 · N18835 · Doug DC982 · Service DoorsSDR CALA9801123Beam · crackedINSPECTION FOUND A 1/2 CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW SRM 51-30, 51-30-2, 51-30-5.Jun 17, 1998 · N18835 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800844Slide · failedTAIL CONE DEPARTED AIRCRAFT AND SLIDE FAILED TO COMPLETELY DEPLOY. REPLACED SLIDE AND TAIL CONE ASSEMBLY PER MM 25-63-01 AND 53-53-00.May 12, 1998 · N18835 · Doug DC982 · Escape SlideSDR CALA9800399Bolt · looseTHE GROUND SHIFT SWITCH FAILED TO MOVE TO THE FLIGHT MODE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT RAISE. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOLT BACKED OUT OF NOSE GEAR OLEO SWITCH. REPLACED HARDWARE IAW IMar 8, 1998 · N18835 · Doug DC982 · Landing Gear Position and WarningSDR CALA9700491Control Valve · leakingTHE RIGHT HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ON APPROACH TO EWR, THE LANDING GEAR WAS EXTENDED MANUALLY. THE AIRCRAFT LANDED AT EWR WITH DAMAGE TO THE RT MLG DOOR AND SKID PLATE. MAINTENANCE FOUND THE LANDING GEAR CONTROL VALVE LEAKING. NEW PACKING WAApr 6, 1997 · N18835 · Doug DC982 · Landing Gear Retraction/Extension SystemSDR CALA9601139Circuit Breaker · trippedWHILE OPERATING THE APU ON TAKEOFF WITH THE LT GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR WAS LOST AND HAD NO CROSSTIE. THE APU GENERATOR COULD NOT BE RESET AND THE AIRCRAFT WAS RETURNED TO LAS. MAINTENANCE FOUND THE APU CONTROL CIRCUIT BREAKER POPPEAug 8, 1996 · N18835 · Doug DC982 · AC Generation SystemSDR CALA9600955Latches · out of adjustTHE PULL REQUIRED TO RELEASE TAILCONE USING THE EXTERIOR HANDLE WAS LOW. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-10.Jun 29, 1996 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CALA9600954Clips · out of adjustEXCESSIVE PULL WAS REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.Jun 29, 1996 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CALA9600958Floor Support · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT INBOARD OF FORWARD ENTRY DOOR AT STA 180 TO 195. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Jun 19, 1996 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9600957Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT AT AFT SERVICE DOOR CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5 AND 51-10-3.Jun 19, 1996 · N18835 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL950637Postion Sensor · out of adjustIAH - FLT 0664 - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. MAINTENANCE FOUND THE NOSE GEAR UP/DOWN POSITION SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED PER MM 32-60-05 AND OPERATION CHECKED GOOD. Aug 3, 1995 · N18835 · Doug DC982 · Landing Gear Position and WarningSDR CAL950603Switch · inoperativeFLT NR 0117 - LAX - ALL THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WHILE IN FLIGHT. THE GEAR WAS CYCLED, BUT THE LIGHTS DID NOT EXTINGUISH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE S1-319 LEFT THROTTLE SWITCH IN THE PEDESTAL AT FAULT. THE Jul 18, 1995 · N18835 · Doug DC982 · Landing Gear Position and WarningSDR CAL950214Hyd Line · rupturedIAH - FLT 0459 - LT HYDRAULIC SYSTEM PRESSURE AND QUANTITY BEGAN TO DECREASE IN-FLIGHT. THE LT ENGINE HYDRAULIC PUMP WAS TURNED OFF AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE FROM LT PYLON FITTING TO ENGINE CASE DRAMar 18, 1995 · N18835 · Doug DC982 · Hydraulic System, MainSDR CAL950048Clip · brokenHOU - THE FORCE REQUIRED TO PULL HANDLE FROM CLIPS WAS TOO LOW DURING TAIL CONE DROP TEST. REMOVED AND REPLACED BROKEN CLIP. (W)Jan 11, 1995 · N18835 · Doug DC982 · Aerodynamic FairingsSDR CAL950047Cables · out of adjustHOU - THE TAILCONE RELEASE PULL TEST FAILED AT ALL THREE POSITIONS. THE TAILCONE RELEASE CABLES WERE RIGGED PER MM 53-53-00, PARAGRAPH 3A, PAGE 502, CONFIGURATION 1. (Z)Jan 11, 1995 · N18835 · Doug DC982 · Aerodynamic Fairings
Back to N18835, cancelled Jun 23, 2005