N34838, cancelled Mar 16, 2005

Service difficulty reports · 31

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 = 'N34838' AND deregistration_id = 'N34838-2005-03-16'
  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 CALA0100219Cylinder · defectiveTHE NLG DID NOT EXTEND ON APPROACH TO IAH. THE NOSE LIGHT INDICATED UNSAFE AND THE NLG INDICATION PIN WAS RETRACTED. RAN UNSAFE GEAR, GEAR HANDLE DOWN CHECKLIST DURING A GO AROUND AND THE GEAR EXTENDED WITH SAFE INDICATION. THE AIRCRAFT LANDED WITHOUT INCIDMar 9, 2001 · N34838 · Doug DC982 · Landing Gear Retraction/Extension SystemSDR CALA9901646Spar · bentINSPECTION FOUND RT HORIZONTAL STABILIZER REAR SPAR U-CHANNEL BENT BETWEEN HINGE NR 4 AND NR 5. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-02 AND 51-30-08.Dec 17, 1999 · N34838 · Doug DC982 · Horizontal Stabilizer, Spar/RibSDR CALA9901645Pan · crackedINSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR INNER PAN AROUND AFT LOCKING CAM. THE CRACKED AREA WAS BLENDED OUT, TREATED, AND PRIMED IAW SRM 52-01, FIGURE 1, 51-10-3, AND 51-01, FIGURE 1.Dec 17, 1999 · N34838 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9901580Skin · dentedINSPECTION FOUND THE FORWARD ENTRY DOOR EXTERNAL SKIN DENTED AT LOWER EDGE. THE DENTED AREA WAS REMOVED SRM 52-05, FIGURE 37. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 37, 51-10-04, 51-10-03, AND 51-30-02.Dec 9, 1999 · N34838 · Doug DC982 · Passenger/Crew DoorsSDR CALA9901576Threshold · tornINSPECTION FOUND OUTBOARD LIP OF MID PIT DOOR THRESHOLD PANEL TORN AT FS 636-693. THE AREA WAS ROUTED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-03952, SRM 53-01, FIGURE 2, AND 51-30-2.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901575Floorboard · corrodedINSPECTION FOUND COCKPIT FLOORBOARD BETWEEN TWO LOWER FIRST OFFICER'S SEAT TRACKS CORRODED. THE FLOORBOARD WAS REMOVED AND A NEW FLOORBOARD WAS INSTALLED IAW SRM 53-05, FIGURE 1.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Floor PanelSDR CALA9901574Door Pan · crackedINSPECTION FOUND RT MAIN GEAR DOOR OUTBOARD AFT PAN CRACKED ON CORNER. THE DOOR PAN WAS REMOVED AND REPLACED IAW SRM 51-10-3.Dec 7, 1999 · N34838 · Doug DC982 · Landing Gear DoorsSDR CALA9901573Skin · crackedINSPECTION FOUND LT SIDE OF AFT AIRSTAIRS LOWER SEGMENT SKIN CRACKED AT ROLLER BEARINGS. THE CRACK WAS ROUTED OUT AND STOP DRILLED IAW SRM 53-01, FIGURE 1. A REPAIR PATCH WAS INSTALLED IAW SRM 52-60-0, FIGURE 3, 51-10-4, 51-30-1, AND 51-30-5.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9901572Web · puncturedINSPECTION FOUND CUSP WEB PUNCTURED AT FS 190, LBL 6. THE PUNCTURED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, AND 51-30-2.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901571Web · crackedINSPECTION FOUND A 6 INCH CRACK IN CUSP WEB AT FS 1180, LBL 44. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901570Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1136-1117, LBL 56. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9901569Threshold · dentedINSPECTION FOUND AFT CARGO DOOR THRESHOLD DENTED AND GOUGED. A STRAP REPAIR WAS INSTALLED IAW ECRA 5310-03954.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901567Angle · crackedINSPECTION FOUND A 6 INCH CRACK IN MID CARGO COMPARTMENT FORWARD FALSE BULKHEAD FRAME LOWER PANEL SUPPORT ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.Dec 7, 1999 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901562Skin · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB LOWER SECTION OF SKIN CORRODED FROM STA 370-427. THE DOOR JAMB PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 53-05, FIGURE 44, 51-10-01, 51-10-02, AND 51-10-04.Dec 6, 1999 · N34838 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9801204Fitting · looseTHE RT HYDRAULIC PUMP PRESSURE DROPPED TO ZERO FOLLOWED BY THE RT HYDRAULIC SYSTEM QUANTITY DROPPING TO ZERO WHILE EN ROUTE FROM EWR TO MCO. EMERGENCY GEAR EXTENSION WAS USED ON APPROAH TO MCO AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAJul 3, 1998 · N34838 · Doug DC982 · Hydraulic System, MainSDR CALA9800573Strut · flatTHE NOSE GEAR INDICATED UNSAFE WITH GEAR HANDLE UP AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE NOSE STRUT WAS SERVICED WITH FLUID AND NITROGEN. IN ADDITION, THE NOSE STRUT SEAMar 24, 1998 · N34838 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA9701789Cable · wornTHE LT TAILCONE RELEASE CABLE WAS FOUND WORN AND FRAYED WHERE IT PASSES OVER UPPER MOST PULLEY. THE CABLE WAS REPLACED AND THE TAILCONE WAS RIGGED IAW MM 53-53-00.Dec 22, 1997 · N34838 · Doug DC982 · Aerodynamic FairingsSDR CALA9700204Lock Link · failedTHE NLG COLLAPSED AT END OF RUNWAY AT APPROXIMATELY 15 KNOTS AFTER LANDING. THE PASSENGERS WERE EVACUATED VIA STAIRS. THERE WAS NO EMERGENCY AND NO PASSENGERS WERE INJURED. THE AIRCRAFT WAS TOWED TO THE HANGAR. INVESTIGATION FOUND THAT THE NLG UPPER LOCK LIFeb 17, 1997 · N34838 · Doug DC982 · Nose/Tail Landing GearSDR CALA9700128Circuit Breaker · inoperativeTHE CENTER FUEL TANK WAS NOT FEEDING ENGINES WHILE EN ROUTE. THE CENTER FUEL BOOST PUMP CIRCUIT BREAKERS WERE POPPING AND WOULD NOT RESET. APPROPRIATE CHECKLISTS WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTFeb 2, 1997 · N34838 · Doug DC982 · Fuel Boost PumpSDR CALA9600682Battery · dischargedINSPECTION FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERY AND A BAD TERMINAL END WERE REPLACED AND OPERATION OF THE LIGHTS WERE RESTORED.Jun 1, 1996 · N34838 · Doug DC982 · Emergency LightingSDR CAL960119Skin · gougedMIA - INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AND GOUGED AT FS 350 BETWEEN LONGERON 28R AND 29R. THE GOUGE WAS BURNISHED. THE SMALL DENT WAS DRILLED OUT, AND FLUSH FASTENERS WERE INSTALLED IAW SRM 53-01, FIGURE 38, SHEET 1. (M)Jan 21, 1996 · N34838 · Doug DC982 · Fuselage Main, Plate/SkinSDR CAL960114Support · corrodedMIA - INSPECTION FOUND FLOORBOARD SUPPORT AT FORWARD SERVICE DOOR, STATION 200 CORRODED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. (M)Jan 21, 1996 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960112Angle · corrodedMIA - INSPECTION FOUND ANGLE UNDER LEFT FLOOR TRACK IN AFT PIT CORRODED AT STATION 1287. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-05-4 AND 51-30-02. (M)Jan 21, 1996 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960164Chord · crackedMIA - INSPECTION FOUND A 1 INCH CRACK IN INBOARD LOWER CHORD OF INBOARD LEFT HORIZONTAL STABILIZER LEADING EDGE FLANGE. THE CRACK WAS LOCATED AT ROLLER FITTING. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-30-2. (M)Jan 20, 1996 · N34838 · Doug DC982 · Horizontal Stabilizer StructureSDR CAL960163Skin · crackedMIA - INSPECTION FOUND A .5 INCH CRACK IN SKIN AT AFT HINGE CUTOUT FOR RIGHT NLG STRUT DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 62. (M)Jan 20, 1996 · N34838 · Doug DC982 · Fuselage Main, Plate/SkinSDR CAL960118Longeron · corrodedMIA - INSPECTION FOUND LONGERON 28L CORRODED AT STATION 1287 IN AFT CARGO COMPARTMENT. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 1. (M)Jan 20, 1996 · N34838 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CAL960117Skin · delaminatedMAI - THE SECOND FROM INBOARD SECTION OF RIGHT WING TRAILING EDGE FLAP WAS FOUND DELAMINATED. A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-70-2. (M)Jan 20, 1996 · N34838 · Doug DC982 · Trailing Edge FlapsSDR CAL960113Support · corrodedMIA - INSPECTION FOUND CORROSION ON WEB AND FLOOR SUPPORT STRUCTURE UNDER BRACKET AT AFT SERVICE DOOR AREA, FS 1142. THE CORRODED AREAS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3 AND 4. (M)Jan 16, 1996 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960115Angle · corrodedMIA - INSPECTION FOUND FORWARD ANGLE UNDER PANEL AT AFT SERVICE DOOR ENTRY, STATION 1150 CORRODED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2A AND 51-30-2. (M)Jan 11, 1996 · N34838 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL950622Nr 3 Bearing · failedFLT NR 0204 - STL - THE NR 1 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED DURING CLIMB-OUT. THE CHECK LIST WAS COMPLIED WITH, BUT THE LIGHT REMAINED ILLUMINATED. ALL OTHER PARAMETERS WERE NORMAL. THE AIRCRAFT WAS DIVERTED TO STL WHERE IT LANDED WITHOUT INCIDEJul 27, 1995 · N34838 · Doug DC982 · Turbine Engine Compressor SectionSDR CAL950218Eel Batteries · dischargedIAH - FLT 0403 - INSPECTION FOUND SEVERAL ROWS OF EMERGENCY LIGHTING INOP. (ROWS 6-10 AND 17-23). BATTERY PACKS REPLACED, OPS CHKS GOOD. (X)Mar 20, 1995 · N34838 · Doug DC982 · Emergency Lighting
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