N33202, cancelled Jan 21, 1998

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 = 'N33202' AND deregistration_id = 'N33202-1998-01-21'
  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 CALA9700912Wire Harness · damagedTHE APU FIRE LIGHT ILLUMINATED ON SHORT FINAL INTO CLE DURING APU START. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE APU HAD TORCHED ON START RESULTING IN BURN THROUGH OF HARNESS FOR TAILPIPE FIRE DETECTOR. THE APU COMBUSTOR AND TJun 17, 1997 · N33202 · Boeing 737130 · APU System WiringSDR CALA9700066Prox Sensor · inoperativeTHE LEFT MLG RED UNSAFE LIGHT ILLUMINATED AFTER GEAR WAS EXTENDED ON APPROACH. EMERGENCY PROCEDURES WERE COMPLIED WITH PER AIRCRAFT FLIGHT MANUAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOWNLOCK PROXIMITY SENSOR AT FAULT. THE Jan 16, 1997 · N33202 · Boeing 737130 · Landing Gear Position and WarningSDR CALA9601521Skin · crackedINSPECTION FOUND CRACKS IN SECTION 41 RT FUSELAGE EXTERNAL SKIN FROM BS 188 TO 251.6, WL 207 TO 234. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE SKIN WAS REPAIRED IAW EA 5310-01188.Oct 23, 1996 · N33202 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9601519Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FRAME FITTING AT BS 685, WL 208, LBL 62. THE FASTENER HOLE WAS COLD WORKED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-03346.Oct 23, 1996 · N33202 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CALA9601517Frame · crackedINSPECTION FOUND A 2 INCH CRACK EXTENDING AFT OF SECOND FASTENER HOLE IN LT BS 727 FRAME CHORD. THE LOWER CHORD SEGMENT WAS REMOVED AND REPLACED IAW CAL WORK CARD JA5310-0163802001.Oct 23, 1996 · N33202 · Boeing 737130 · Fuselage Main, FrameSDR CALA9601518Floorbeam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 675, BBL 0. THE LOWER T-CHORD WAS REMOVED, A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 51-20-2, 51-30-2 AND BOEING DRAWING NR 65-45410.Oct 22, 1996 · N33202 · Boeing 737130 · Fuselage Main, Floor BeamSDR CALA9601520Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT FUSELAGE SKIN AT BS 747 AND AT BS 727A. BOTH CRACKED AREAS WERE CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED OVER EACH CRACK FROM STA 725 TO 790 IAW SRM 53-30-3.Oct 21, 1996 · N33202 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9601516Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD BEHIND STIFFENER ON RT SIDE AT STA 178, WL 218. ALSO, A 1 INCH CRACK WAS FOUND AT WL 230.5, RT SIDE. THE CRACKED AREA AT WL 218 WAS REMOVED AND THE CRACK AT WL 230.5 WAS STOP DRILLED IAW SRM 53-10-11. REPAIR DOUBLOct 21, 1996 · N33202 · Boeing 737130 · Fuselage Main, BulkheadSDR CALA9601423Wire · burnedSMOKE DEVELOPED FROM BEHIND COCKPIT OVERHEAD PANEL AFTER TURNING ON ENGINE ANTI-ICE WHILE CRUISING AT FL 240 EN ROUTE FROM EWR TO CAE. THE SMOKE CEASED WHEN ANTI-ICE WAS TURNED OFF. THE FLIGHT WAS CONTINUED TO CAE WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAIOct 7, 1996 · N33202 · Boeing 737130 · Engine Bleed Air System WiringSDR CALA9601017Tire · failedA LOUD BANG WAS HEARD AFTER TAKEOFF, WHILE CLIMBING THROUGH 3,000 FEET. THE FLIGHT CONTINUED TO BOS WHERE IT LANDED SAFELY. MAINTENANCE FOUND THAT THE NR 3 TIRE HAD BLOWN RESULTING IN DAMAGE TO RT OUTBOARD SIDE OF WHEEL WELL. THE RT I/B FLAP TRACK FAIRING AJul 13, 1996 · N33202 · Boeing 737130 · TireSDR CAL960190Lamp · inoperativeFLT NR 591 - MSP - THE RIGHT MLG GREEN LIGHT DID NOT ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH TO MSP, AND IT WOULD NOT TEST. CHANGING BULBS DID NOT HELP. THE GEAR WAS VISUALLY INSPECTED AND CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WIFeb 25, 1996 · N33202 · Boeing 737130 · Landing Gear Position and WarningSDR CAL951130Stringer · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN RT WING STR 13 AT WBL 92.5 AND A 1.5 INCH CRACK IN SAME STRINGER AT WBL 114. THE STRINGER WAS REPAIRED IAW BOEING DWG 65C34533. (X)Nov 22, 1995 · N33202 · Boeing 737130 · Wing, Longeron/StringerSDR CAL951131Chord · crackedGSO - INSPECTION FOUND STA 727 RT CHORD CRACKED AT STR 18A. THE CRACK WAS LOCATED AT BOTH FORWARD AND AFT FASTENERS AND TOTALED 1 INCH IN LENGTH. THE CRACKED CHORD SEGMENT WAS REMOVED AND REPLACED IAW EA 5310-01638 AND BOEING DWG 65C33722. (X)Nov 17, 1995 · N33202 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL951129Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 440. THE FRAME WAS REMOVED AND REPLACED IAW SRM 53-10-04 AND SRM 51-30-0. (X)Nov 10, 1995 · N33202 · Boeing 737130 · Fuselage Main, FrameSDR CAL950984Pcu · leakingFLT NR 1790 - THE B-HYDRAULIC SYSTEM HAD A PARTIAL DROP IN QUANTITY WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE B-SYSTEM AILERON PCU LEAKING. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71 AND OPERATIOOct 30, 1995 · N33202 · Boeing 737130 · Aileron Control SystemSDR CAL950294Hyd Line · leakingEWR - FLT 1477 - THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON DESCENT INTO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE IN LEFT WING ABOVE LEFT GEAR LEAKING. THE LINE WAS REPLACED USApr 18, 1995 · N33202 · Boeing 737130 · Hydraulic System, Main
Back to N33202, cancelled Jan 21, 1998