N14239, cancelled May 2, 2000

Service difficulty reports · 33

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 = 'N14239' AND deregistration_id = 'N14239-2000-05-02'
  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 CALA9801831Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WAS LOST AFTER TAKEOFF. A MANUAL GEAR EXTENSION WAS ATTEMPTED. THE NOSE GEAR DID NOT EXTEND ON FIRST PULL OF HANDLE. THE HANDLE WAS PULLED AGAIN AND THE GEAR EXTENDED BUT NOSE EXTENSION CABLE WOULD NOT RETRACT FUSep 21, 1998 · N14239 · Boeing 737214 · Hydraulic System, MainSDR CALA9700350Hyd Line · leakingTHE COCKPIT AND CABIN FILLED WITH SMOKE AFTER TAKEOFF FROM EWR. THE AIR CONDITIONING SMOKE CHECKLIST WAS ACCOMPLISHED AND A RETURN TO EWR WAS BEGUN. THE CREW NOTED A HYDRAULIC SYSTEM LOSS ON FINAL APPROACH. THE A/C LANDED WITHOUT INCIDENT. MX FOUND THE NR Mar 17, 1997 · N14239 · Boeing 737214 · Hydraulic System, MainSDR CALA9601368Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN FLOORBEAM AT STA 724, BL 0. THE WEB AND STIFFENER WERE REMOVED IAW SRM 51-30-2. A WEB AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-4, 57-30-2, ECRA 5710-01755 AND REO 02209.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Floor BeamSDR CALA9601367Fitting · gougedINSPECTION FOUND THE RT HORIZONTAL STABILIZER UPPER AFT SPAR INBOARD ATTACH FITTING GOUGED. THE ATTACH FITTING WAS REPAIRED IAW ECRA 5510-01338.Sep 18, 1996 · N14239 · Boeing 737214 · Horizontal Stabilizer, Attach FittingsSDR CALA9601366Floorbeam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM AT STA 684, LBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Floor BeamSDR CALA9601365Skin · crackedINSPECTION FOUND FOUR .125 INCH CRACKS IN SECTION 41, LT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Plate/SkinSDR CALA9601364Skin · crackedINSPECTION FOUND THREE .125 INCH CRACKS IN SECTION 41R, RT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Plate/SkinSDR CALA9601363Keel Beam · galledINSPECTION FOUND LT KEEL BEAM FAYING FLANGE FROM BS 663 TO 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. EXISTING HOLES WERE OVERSIZED AND 3 EACH PRESS FIT BUSHINGS WERE INSTALLED. A REPAIR STRAP WAS FABRICATED AND INSTALLED. Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, KeelSDR CALA9601362Flange · galledINSPECTION FOUND RT KEEL BEAM FAYING FLANGE FROM BS 663 TO BS 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND ECRA 5310-03324.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, KeelSDR CALA9601361Frame · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FRAME AT STA 947, STRINGER 18R. THE FRAME WAS REPAIRED IAWS SRM 53-10-2, 53-10-4, 51-10-7, 51-10-2 AND 51-30-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, FrameSDR CALA9601360Floorbeam · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 684, RBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Floor BeamSDR CALA9601359Chord Angle · crackedINSPECTION FOUND A 3.25 INCH CRACK IN MAIN CABIN FLOORBEAM LOWER CHORD ANGLE AT STA 673, BL 0. THE AREA WAS REPAIRED IAW BOEING DRAWING 65-45410, CAL ENGINEERING ORDER 031-5710-01322, SRM 51-40-4 AND 51-30-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Miscellaneous StructureSDR CALA9601358Angle · crackedINSPECTION FOUND A .5 INCH CRACK THROUGH RADIUS OF RT WING ROOT FORWARD FILLET PANEL SUPPORT ANGLE. THE CRACK WAS LOCATED AT STA 540, 10 INCHES BELOW LOWER CAP OF FORWARD SPAR ADJACENT TO FORWARD END OF HINGED RAM AIR DUCT ACCESS PANEL. THE ANGLE WAS REPAIRESep 18, 1996 · N14239 · Boeing 737214 · Fuselage Miscellaneous StructureSDR CALA9601357Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN STIFFENER BETWEEN STRINGER 10L AND 11L AT FS 295. THE CRACKED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-10-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Miscellaneous StructureSDR CALA9601356Floorbeam · corrodedINSPECTION FOUND FLOORBEAM AND SUPPORT CORRODED AT AFT CABIN L-2 DOOR THRESHOLD, STA 986. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2 AND 51-30-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Floor BeamSDR CALA9601355Skin · corrodedINSPECTION FOUND SKIN BULGED/CORRODED WITH POPPED FASTENERS AT FORWARD INBOARD CORNER OF AFT LAV DUMP CHUTE DOOR CUTOUT. THE CORRODED AREA OF SKIN WAS REMOVED IAW SRM 53-30-3. SKIN FILLER, DOUBLER AND SHIMS WERE FABRICATED IAW SRM 53-30-2. STRINGER 26R WAS Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Plate/SkinSDR CALA9601354Stringer · crackedINSPECTION FOUND A 1.25 INCH CRACK IN WING SUPPORT STRINGER AT RIGHT WBL 70.85, WS 6. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 8 AND SRM 57-10-2.Sep 18, 1996 · N14239 · Boeing 737214 · Wing, Longeron/StringerSDR CALA9601353Skin · dentedINSPECTION FOUND A 3 BY 5 INCH AREA OF FUSELAGE SKIN DENTED AT BS 890, LT SIDE, TOP OF WINDOW BELT. THE DENTED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2 AND SRM 51-30-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Plate/SkinSDR CALA9601352Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACK ROW D AND CUSP LINE AT STA 360. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2 AND 51-30-3.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Floor BeamSDR CALA9601351Bulkhead · crackedINSPECTION FOUND A 3.25 CRACK IN R/H SIDE OF PRESSURE BULKHEAD AT STA 178. THE BULKHEAD WAS REPAIRED IAW SRM 53-10-11 AND 53-10-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, BulkheadSDR CALA9601350Beam · crackedINSPECTION FOUND A 3 INCH CRACK IN RADIUS OF TRANSVERSE BEAM AT STA 685. THE CRACK WAS STOP DRILLED, REPAIR ANGLES AND RADIUS FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND BAC DRAWING NR 65C17103.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Miscellaneous StructureSDR CALA9601349Stringer · crackedINSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 17R BELOW CABIN FLOOR AT FS 837. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-30-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Longeron/StringerSDR CALA9601348Stringer · crackedINSPECTION FOUND A .75 INCH CRACK AT RT OUTBOARD END OF CENTER WING BOX UPPER STRINGER NR 3. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 4 FIGURE 8 AND SRM 57-10-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Longeron/StringerSDR CALA9601347Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN STRINGER 12L AT STA 295. THE STRINGER WAS REPAIRED IAW SRM 53-10-2.Sep 18, 1996 · N14239 · Boeing 737214 · Fuselage Main, Longeron/StringerSDR CALA9601149Gcu · inoperativeTHE LEFT BUS OFF LIGHT COME ON SHORTLY AFTER TAKEOFF. THE LIGHT WAS ACCOMPANIED BY AN ELECTRICAL ODOR OR AIR CONDITIONING PACK SMELL AND A CLICKING SOUND, LIKE THAT OF A RELAY OPENING AND CLOSING, THE SOUND WAS HEARD COMING FROM BEHIND THE SECOND OFFICER'S SEAug 11, 1996 · N14239 · Boeing 737214 · AC Generation SystemSDR CALA9601042Hyd Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP SHORTLY AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK ACTUATOR UPPER LINE LEAKING. THE LINE WAS REMOVED AND REPLACED, LEAK CHECK WAS GJul 21, 1996 · N14239 · Boeing 737214 · Hydraulic System, MainSDR CAL951064Dnlock Actuator · brokenFLT NR 1249 - EWR - THE RIGHT MLG WOULD NOT RETRACT AFTER DEPARTING BDL FOR CLE. THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK ACTUATOR BROKEN. Nov 21, 1995 · N14239 · Boeing 737214 · Landing Gear Position and WarningSDR CAL950661Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 440L BETWEEN STRINGERS 19L-20L. THE CRACKED FRAME SECTION WAS CUT OUT. A NEW FRAME AND CHORD SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING NR 65C27113. (M)Aug 5, 1995 · N14239 · Boeing 737214 · Fuselage Main, FrameSDR CAL950659Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 639R, STRINGER 16. REMOVED CRACKED UPPER CHORD AND FRAME WEB AND INSTALLED REPAIR PARTS IAW BOEING DRAWING NR 65C31658 AND SRM 51-30-2. (M)Aug 5, 1995 · N14239 · Boeing 737214 · Fuselage Main, FrameSDR CAL950658Floor Beam · corrodedGSO - INSPECTION FOUND CORROSION ON FLOOR BEAM UNDER COCKPIT FLOOR PANEL AT STATION 250, BBL 0. A WEB AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-40-4. (M)Aug 5, 1995 · N14239 · Boeing 737214 · Fuselage Main, Floor BeamSDR CAL950657Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FORWARD GALLEY DOOR LOWER SIDE OF FRAME AT LOWER FORWARD STOP FITTING. THE CRACKED SEGMENT OF FRAME WAS REMOVED. A NEW SEGMENT WAS INSTALLED PER ECRA 5240-01089 AND BAC DRAWING 69-69680. (M)Aug 5, 1995 · N14239 · Boeing 737214 · Galley DoorsSDR CAL950656Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 420L BETWEEN STRINGERS 20L-21L. THE DAMAGE WAS CUT OUT AND A NEW FRAME, CHORD, AND SPLICES WERE INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING 65C25113. (M)Aug 5, 1995 · N14239 · Boeing 737214 · Fuselage Main, FrameSDR CAL950654Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STATION 460L AND STRINGERS 21L-22L. CUT OUT DAMAGE AND INSTALLED A NEW FRAME, CHORD AND SPLICES IAW SRM 51-30-2 AND BOEING DRAWING 65C25113. (M)Aug 5, 1995 · N14239 · Boeing 737214 · Fuselage Main, Frame
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