N259US, cancelled Nov 2, 2001

Service difficulty reports · 16

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 = 'N259US' AND deregistration_id = 'N259US-2001-11-02'
  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 98ZZZM687Acm · failedUNABLE TO MAINTAIN CABIN PRESSURE. AIRCRAFT DIVERTED TO CSO. FOUND RT ACM DEFECTIVE.Aug 29, 1998 · N259US · Boeing 727251 · Cabin Cooling SystemSDR 98ZZZX2403Panel · misinstalledF/A REPORTED FUEL LEAKAGE FROM RT WING. AIRCRAFT RETURNED TO CUN. FOUND LOWER ACCESS PANEL ON RT WING LEAKING. RESECURED AND TORQUED HARDWARE IAW MM 28-11-21.Jun 14, 1998 · N259US · Boeing 727251 · Wing, Plate/SkinSDR 98ZZZX2404Battery · dischargedDURING B-CHECK INSPECTION, FOUND 2 EACH OVERHEAD EMERGENCY LIGHTS NOT WORKING. REPLACED BATTERIES. OPS CHECKED OK.Jun 10, 1998 · N259US · Boeing 727251 · Emergency LightingSDR 97ZZZX3350Bulkhead · crackedTHE CRACK WAS FOUND IN THE AFT BULKHEAD VERTICAL BEAM LBL 26.83 WL 257.0. THE CRACK IS ATTRIBUTED TO PRESSURIZATION CYCLES. RECOMMENDATION: THE SB 53-0182 RECOMMENDED TO INSTALL THE PREVENTIVE MODIFICATION AT OR BEFORE 60,000 CYCLES. SUBMITTER RECOMMENDED Jul 3, 1997 · N259US · Boeing 727251 · Fuselage Main, BulkheadSDR 97ZZZX3349Bulkhead · beam crackedTHE CRACK WAS FOUND IN THE AFT BULKHEAD VERTICAL BEAM LBL 36.83 (LT/RT). THE SUSPECT CAUSE WAS THE RESULT OF FATIGUE THAT WAS CAUSED BY PRESSURIZED FLIGHTS. SUBMITTER RECOMMENDATION: THERE SHOULD BE A LIMITED TIME TO INSTALL THE PREVENTIVE MODIFICATION PER Jul 3, 1997 · N259US · Boeing 727251 · Fuselage Main, BulkheadSDR 97ZZZX3348Bulkhead · beam crackedTHE CRACK WAS FOUND IN THE AFT BULKHEAD VERTICAL BEAM LBL 36.83 (LT/RT). THE SUSPECT CAUSE WAS THE RESULT OF FATIGUE THAT WAS CAUSED BY PRESSURIZED FLIGHTS. SUBMITTER RECOMMENDATION: THERE SHOULD BE A LIMITED TIME TO INSTALL THE PREVENTIVE MODIFICATION PER Jul 3, 1997 · N259US · Boeing 727251 · Fuselage Main, BulkheadSDR USVA49701Tube · crackedENGINE NR 3 SHUT DOWN DUE TO FIRE WARNING. FOUND NR 3 ENGINE BLEED AIR MANIFOLD TUBE SEPARATED AT FLANGE WHERE ATTACHED TO FUEL HEAT VALVE. REPAIRED FLANGE TO PIPE IAW PWA ENGINE MANUAL 72-09-71. OPS CHECKED FUEL HEAT VALVE. NO LEAK NOTED. (M)Apr 9, 1997 · N259US · Boeing 727251 · Engine Fuel DistributionSDR 97ZZZX1428Lap Seam · corrodedDURING VISUAL INSPECTION OF SB 727-53-0072 R5, LAP SEAM 520L AT STA 1170 WAS FOUND BULGING WITH POPPED RIVET HEADS IN THE LAP. LEVEL 2 CORROSION WAS NOTED BEHIND THE LAP SEAM WHEN OPENED UP FOR REPAIR.Oct 9, 1996 · N259US · Boeing 727251 · Fuselage Miscellaneous StructureSDR IXKA9600077Controller · inoperativeFLT 9 - EWR-MCO - AT CRUISE, EXPERIENCED RAPID DECOMPRESSION AT 31,000 FEET, DECLARED EMERGENCY AND FOLLOWED RAPID DECOMPRESSION AND EMERGENCY DESCENT PROCEDURES. MADE NORMAL APPROACH AND LANDING AT MCO. VISUALLY INSPECTED EXTERIOR DOOR SEALS AND OUTFLOW VALSep 5, 1996 · N259US · Boeing 727251 · Cabin Pressure ControllerSDR IXKA9600053Battery Pack · dirtyFORWARD EMERGENCY CEILING LIGHT OUT. REMOVED BATTERY AND CLEANED CONTACTS INSTALLED BATTERY PACK, OPS CHECK OK AS PER MM 33-50-01. (M)Jun 23, 1996 · N259US · Boeing 727251 · Emergency LightingSDR IXKA9600052Flow Contl Valve · intermittentAFTER TAKEOFF AT ATL, FLT 73, ATL TO MCO, AIR TURN BACK DUE TO UNABLE TO PRESSURIZE ON DEPARTURE IN AUTO OR MANUAL. TROUBLESHOT PRESSURIZATION TO INTERMITTENT FLOW CONTROL VALVE. REMOVED AND REPLACED FLOW CONTROL VALVE PER MM 36-12-11. PRESSURIZED A/C PER MJun 20, 1996 · N259US · Boeing 727251 · Cabin Pressure Control SystemSDR IXKA960016Power Pack · inoperativeEWR - FLT 81 - POST-FLIGHT, AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND RPELACED POWER PACK. (X)Apr 17, 1996 · N259US · Boeing 727251 · Emergency LightingSDR IXKA960011Battery Pack · dischargedEWR - POST-FLIGHT - OVERHEAD EMERGENCY EXIT LIGHT ROW 11, INOPERATIVE. REMOVED AND REPLACED BATTERIES.Apr 13, 1996 · N259US · Boeing 727251 · Emergency LightingSDR IXKA960001Torque Tube · looseATL/MDW - FLT 59 - INBOARD FLAPS WOULD NOT RETRACT ABOVE 15 DEGREES. AIR TURN BACK TO ATL. ON SYSTEM OPS AND INSPECTION, FOUND FLAPS IN BYPASS MODE. RESET ASSYMETRY. FOUND LOOSE TORQUE TUBE COUPLING AT OUTBOARD FLAP POWER CONTROL UNIT. SECURED LOOSE TORQUJan 2, 1996 · N259US · Boeing 727251 · Trailing Edge FlapsSDR 95ZZZX2871Stringer · corrodedDURING BOEING C.P.C.P. INSPECTION, FOUND SKIN BULGE AT STR 26R, STA 359. CUT OUT DAMAGED STRINGER SECTION. SKIN NOT DAMAGED. FABRICATED REPAIR FILLER AND DOUBLER FROM 7075-T6. TREATED PARTS AND PRIMED, AND INSTALLED IAW SRM 51-40-4, SRM 51-20-2, SRM 51-20-Feb 17, 1995 · N259US · Boeing 727251 · Fuselage Main, Longeron/StringerSDR 95ZZZX2870Stringer · corrodedDURING INSPECTION OF AD 91-06-06, FOUND STR 19L AT BS 675 EXFOLIATED ON INBOARD LOWER FLANGE. REMOVED DAMAGED AREA OF STRINGER. FABRICATED STRINGER SPLICE FROM BAC 1498-125, 7075-T6 STRINGER MATERIAL AND NEW STRINGER TIE FROM .040 INCH, 7075-T6. TREATED MATFeb 17, 1995 · N259US · Boeing 727251 · Fuselage Main, Longeron/Stringer
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