Boeing 737-281

Service difficulty reports · 120

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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 = '737281'
  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 P2EA97084Spar Chord · corrosionSJO - FOUND LEVEL 2 CORROSION RIGHT WING RSS 150, UPPER CHORD. DEFECT SIZE 1 INCH. ACCOMPLISHED REPAIR BETWEEN RSS 145 AND RSS 155 PER BOEING FAX NR C00-SJO-97-0294RR, DATED NOV 13, 1997. (M)Nov 27, 1997 · N219US · Boeing 737281 · Wing SparSDR P2EA97083Bulkhead Chord · crackedSJO - FOUND OUTBOARD CHORD CRACK FUSELAGE BULKHEAD, BS 1156, LEFT OUTBOARD CHORD WL 74. DEFECT SIZE 2 INCHES. REPAIRED FUSELAGE LEFT OUTBOARD CHORD IAW SB 737-53-1086. (M)Nov 26, 1997 · N219US · Boeing 737281 · Fuselage Main, BulkheadSDR P2EA97082Skin · corrosionSJO - FUSELAGE SKIN BULGED IN SEVERAL PLACES, LEVEL 2 CORROSION BETWEEN STRINGER 23 LEFT AND 25 LEFT, BS 927 TO BS 947. DEFECT SIZE 20 INCHES BY 20 INCHES. REPLACED FUSELAGE SKIN PER SRM 51-10-01 AND 51-30-02. (M)Nov 26, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97081Stringer · corrosionSJO - OBSERVED DURING FUSELAGE SKIN REPLACEMENT, LEVEL 2 CORROSION, STRINGER 24 LEFT, BS 1010. DEFECT SIZE 1.5 INCHES. ACCOMPLISHED STRINGER REPAIR IAW 53-10-03 FIG 1. (M)Nov 25, 1997 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA97080Stringer · corrodedSJO - OBSERVED DURING FUSELAGE SKIN REPLACEMENT, LEVEL 2 CORROSION, STRINGER 21 LEFT, BS 1010. DEFECT SIZE 2 INCHES. ACCOMPLISHED STRINGER REPAIR IAW 53-10-03 FIG 1. (M)Nov 25, 1997 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA97085Skin · damagedSJO - FOUND SKIN DAMAGED AT WINDSHIELD CENTER POST. DEFECT SIZE 4.5 INCHES BY .625 INCHES. REWORKED LEFT FUSELAGE WINDSHIELD CENTER POST SKIN IAW COOPESA EO-C00-3-53-530-97 DATED NOV 15, 1997. (M)Nov 24, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97079Stringer · corrodedSJO - DISCREPANCY FOUND DURING SCHEDULED MAINTENANCE C-CHECK, LOWER FUSELAGE, E/E COMPARTMENT STRINGER 23L CORRODED BETWEEN STATION 330-335. REPAIRED PER SRM 53-10-3. (M)Nov 24, 1997 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA97078Bulkhead · corrodedSJO - DISCREPANCY FOUND DURING SCHEDULED MAINTENANCE C-CHECK, NO DOCUMENTATION ON FILE FOR REPAIR AT NOSE WHEELWELL FWD BULKHEAD WEB, BS 294.5 BETWEEN RBL 5 INCH AND RBL 12 INCH, WL 169 TO WL 190. REPAIRED PER BOEING FAX NR C00-SJO-97-0297TRR DATED 11/14/97, Nov 24, 1997 · N219US · Boeing 737281 · Fuselage Main, BulkheadSDR P2EA97092Frame · crackedSJO - FRAME CRACK BETWEEN STRINGER 21 RIGHT AND STRINGER 22 RIGHT AT BS 500B LENGTH .375. ACCOMPLISHED TYPICAL FRAME REPAIR PER SRM 51-40-3 FIG 1. (M)Nov 18, 1997 · N219US · Boeing 737281 · Fuselage Main, FrameSDR P2EA97090Skin · dentedSJO - FOUND EXTERNAL SKIN DENT BETWEEN BS 798 AND BS 807, STRINGER 23 LEFT AND STRINGER 25 LEFT. DEFECT SIZE .80 INCH BY .50 INCH AND .036 DEEP. ACCOMPLISHED SKIN FLUSH REPAIR PER SRM 53-30-3 FIG 7. (M)Nov 18, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97089Skin · dentedSJO - FOUND EXTERNAL SKIN DENT BETWEEN BS 919 AND BS 927, STRINGER 18 LEFT AND STRINGER 19 LEFT. DEFECT SIZE 2 INCHES BY 1 INCH AND .048 DEEP. ACCOMPLISHED FUSELAGE FLUSH REPAIR BETWEEN STRIGNER PER SRM 53-30-3 FIG 2. (M)Nov 18, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97088Skin · dentedSJO - FOUND EXTERNAL SKIN DENT BS 744 TO BS 758, STRINGER 22 LEFT AND STRINGER 24 LEFT. DEFECT SIZE 1.6 INCHES BY 1 INCH AND .043 INCH DEEP. ACCOMPLISHED FUSELAGE SKIN EXTERNAL REPAIR AT STRINGER PER SRM 53-30-3 FIG 6. (M)Nov 18, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97087Skin · crackedSJO - FOUND SKIN CRACK BETWEEN BS 902 AND BS 908, STRINGER 5 RT AND 7 RT. DEFECT SIZE .25 INCHES. ACCOMPLISHED SKIN BUTT JOINT EXTERNAL REPAIR. (M)Nov 18, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97086Skin · corrodedSJO - FOUND SKIN BULGED, BS 434 TO BS 442, STRINGER 21 LEFT AND 22 LEFT. DEFECT SIZE LENGTH 3 INCHES BY 3 INCHES. ACCOMPLISHED FUSELAGE FLUSH SKIN REPAIR. (M)Nov 18, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97091Skin · dentedSJO - FOUND EXTERNAL SKIN DENT, BETWEEN BS 270 AND BS 274, STRINGER 3 LEFT AND STRINGER 4 LEFT. DEFECT SIZE .80 INCHES BY .65 INCHES AND .048 DEEP. ACCOMPLISHED SMALL SKIN FLUSH REPAIR PER SRM 53-30-3 FIG 5. (M)Nov 13, 1997 · N219US · Boeing 737281 · Fuselage Main, Plate/SkinSDR P2EA97030Connector · looseFLT 125 - MCI - RADAR PAINTS ON BOTH SIDES BUT NOT IN THE MIDDLE. FOUND FORWARD BULKHEAD CANNON PLUG BACKSHELL LOOSE AND CANNON PLUG DIRTY. RESECURED BACKSHELL CLEANED CONNECTOR. PERFORMED OPS CHECK PER MM 34-41-0A. OPS CHECK GOOD. (M)Apr 21, 1997 · N219US · Boeing 737281 · Weather Radar SystemSDR P2EA97002Bleed Duct · damagedFLT 612 - DEN - AFTER DEPARTING DEN, FLIGHT ATTENDENT INFORMED ME OF A SMELL COMING FROM THE CABIN, HAD ELECTRICAL ODOR. RETURNED TO DEN FOR INSPECTION. FOUND BLEED DUCT WITH HOLE, FORWARD CARGO PIT, RT AFT CEILING. DUCT REPLACED, RAN PACK, NO SMOKE IN CABIJan 24, 1997 · N219US · Boeing 737281 · Pneumatic Distribution SystemSDR P2EA96013Stringer · crackedDURING C-CHECK, PERFORMED INSPECTION IAW AD95-12-17, FINDINGS RESULTED IN THE FOLLOWNG REPAIR; PERFORMED MAJOR REPAIR IAW SB737-53-1066R1, PERTINENT DETAILS UNDER WO NR 0003-02-F055 AND 0003-02-F056. INSPECTION AND REPAIRS COMPLETED DURING C-CHECK BY SABRE TENov 13, 1996 · N219US · Boeing 737281 · Fuselage Main, Longeron/StringerSDR P2EA96007Airspeed Ind · failedFLT 130 - MCI - ABORTED T/O, NO AIRSPEED F/O SIDE. REJECTED T/O AT 100 KTS. NR 2 AIRSPEED IND REMAINED AT 0 WITH NO MOVEMENT. CHECKED QUICK DISCONNECT SECURITY AT IND'S, CHECKED PITOT DRAIN CAPS FOR SECURITY, CHECKED PITOT HEAD FOR OBSTRUCTIONS. PERFORMED Sep 13, 1996 · N219US · Boeing 737281 · Airspeed/Mach IndicatorSDR P2EA95004Garloc Seal · failedFLT NR 114A - MCI - NR 2 ENGINE LOST OIL QUANTITY THEN OIL PRESSURE. ENGINE WAS SHUT DOWN INFLIGHT. MAINTENANCE REMOVED AND REPLACED GEARBOX GARLOC SEAL. (W)May 1, 1995 · N219US · Boeing 737281 · Turbine Engine Accessory Drive
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