N10236, cancelled Jun 15, 1999

Service difficulty reports · 36

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 = 'N10236' AND deregistration_id = 'N10236-1999-06-15'
  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 CALA9801537Solenoid · inoperativeTHE LANDING GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION TO UP UNLESS OVERRIDE TRIGGER WAS PULLED AFTER TAKEOFF. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER LOCK SOLENOID AT FAULT. THE LEVER LOCK SOLENOID WAS REMOVED AND REPLACED IAW MM 32-31-31. IN ADAug 26, 1998 · N10236 · Boeing 737222 · Landing Gear SelectorSDR CALA9800690Line · leakingTHE B SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.8 GALLONS IN FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF THE B SYSTEM LOW QUANTITY LIGHT. THE ABNORMAL CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING EDApr 23, 1998 · N10236 · Boeing 737222 · Hydraulic System, MainSDR CALA9800390Sign · shortedTHE CREW REPORTED SMOKE APPEARED MOMENTARILY IN CABIN AT PUSH TIME. MAINTENANCE FOUND THE NO SMOKING FASTEN SEAT BELT SYSTEM INOPERATIVE WITH THE ROW 6 ABC OVERHEAD PSU BASE ASSEMBLY SHORTED OUT. THE WIRES FOR PSU AT ROW 6 ABC WERE CUT AND STOWED AND THE SYSMar 5, 1998 · N10236 · Boeing 737222 · Passenger Compartment LightingSDR CALA9701651Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 1.5 AND LBL 9. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03623.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor BeamSDR CALA9701650Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 312, RT OUTBOARD END. THE CORRODED SECTION WAS REMOVED IAW SRM 51-30-2, REPAIR FILLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2, AND 51-30-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor BeamSDR CALA9701649Web · corrodedINSPECTION FOUND WEB CORRODED AT BS 330 TO 340, RT CUSP. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous StructureSDR CALA9701648Angle · corrodedINSPECTION FOUND CORROSION IN ANGLE AT BS 797, S26L. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-3, FIGURE NR 1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-2, AND 51-30-0.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous StructureSDR CALA9701647Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 344 FROM LBL 24 TO RBL 24. THE CORRODED FLOORBEAM CAP WAS REMOVED, A REPLACEMENT CAP AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 53-30-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor BeamSDR CALA9701646Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 TO 344, LBL 10. THE FLOOR SUPPORT WAS REMOVED IAW SRM 53-10-2. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous StructureSDR CALA9701645Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294.5 TO 312, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous StructureSDR CALA9701644Frame · corrodedINSPECTION FOUND CABIN FLOOR FRAME CORRODED AT STA 987 FROM BL 55L TO BL 55R. THE CORRODED UPPER CAP WAS REMOVED IAW SRM 51-30-2. A NEW UPPER CAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CALA9701643Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CAP AND WEB CORRODED INSIDE E AND E COMPARTMENT AT BS 328. THE CORRODED SECTION OF BEAM CAP WAS REMOVED AND A NEW SECTION AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2. THE CORRODED SECTION OF FLOORBEAM WEB Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor BeamSDR CALA9701642Support · corrodedINSPECTION FOUND FLOOR SUPPORT UPPER PLATE CORRODED AT STA 328 TO 344, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous StructureSDR CALA9701376Hyd Line · crackedTHE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE CRACKED. THE HYDRAULIC PRESSURE LINE WAS REMOVED Sep 17, 1997 · N10236 · Boeing 737222 · Hydraulic System, MainSDR CALA9601488Stringer · crackedRIGHT A/C BAY OUTBOARD SIDE APPROX 1.5 LONG CRACK EXTENDING UNDER STIFFENER AT FUSELAGE STATION. REMOVED STIFFENER, STOP DRILLED CRACK, AND INSTALLED PER SRM 51-10-1 AND 51-30-2.Oct 12, 1996 · N10236 · Boeing 737222 · Fuselage Main, Longeron/StringerSDR CALA9601487Skin · corrodedAFT FUSELAGE STATION 877 TO 857 AT STATION 24R LAP JOINT SWOLLEN BETWEEN FASTENER HEADS. REMOVED FASTENERS AT LAP JOINT AND CORROSION PER SRM 51-10-2 AND 51-10-6 AND INSTALLED FASTENERS PER SRM 51-30-2.Oct 12, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/SkinSDR CALA9601486Battery Pack · dischargedL2 DOOR MOUNTED ESCAPE SLIDE LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-63.Oct 12, 1996 · N10236 · Boeing 737222 · Emergency LightingSDR CALA9601485Skin · bulgedEXTERIOR SKIN ON LEFT SIDE NOSE WHEEL WELL EDGE HAS BULGES AND RIVETS PULLING THROUGH FROM STATION 235.8 TO 251.8. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED PER SRM 53-30-3, 51-30-2, AND 51-10-2.Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/SkinSDR CALA9601484Skin · oil canFUSELAGE SKIN OIL CAN AT BS 390L AND STR 17L. TRIMMED OUT DAMAGED AREA PER SRM 53-30-3, FABRICATED DOUBLER PER SRM 53-30-3 AND 51-10-2, INSTALLED DOUBLER PER SRM 53-30-3 AND 51-30-2.Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/SkinSDR CALA9601483Blkhd Web · crackedFORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON LEFT SIDE ABOVE WL 208 APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED PER SRM 53-10-11, 51-30-2, AND 51-10-2.Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, BulkheadSDR CALA9601482Bulkhead · crackedFORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON RIGHT SIDE ABOVE WL STA 208, APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS, INSTALLED PER SRM 53-10-11, 53-30-2, AND 51-10-2.Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, BulkheadSDR CALA9601481Skin · crackedFUSELAGE SKIN CRACKED IN 2 PLACES ON LEFT SIDE BETWEEN STA 727A AND 727B AT STRINGER 18 APPROX 3 EACH. CUT OUT DAMAGED AREA, FABRICATED FILLER AND EXTERNAL DOUBLER AND INSTALLED PER SRM 53-30-3, 53-30-2, AND 51-10-2.Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/SkinSDR CAL950970Battery Pack · dischargedGSO - EXIT LIGHT INOP. REPLACED RIGHT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M)Oct 24, 1995 · N10236 · Boeing 737222 · Emergency LightingSDR CAL950969Battery Pack · dischargedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND LEFT EXTERNAL EMERGENCY LIGHT INOP. REPLACED LEFT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M)Oct 24, 1995 · N10236 · Boeing 737222 · Emergency LightingSDR CAL950968Battery Pack · dischargedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND BATTERY PACK INOP. REPLACED BATTERY PACK FOR L-1 SLIDE. (M)Oct 24, 1995 · N10236 · Boeing 737222 · Emergency LightingSDR CAL950967Frame · crackedGSO - AIRCRAFT IN D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATLY .75 INCH AT BS 500A BETWEEN S20L, S21L, AND ABOVE S23L, REMOVED AND REPLACED. (M0Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950966Frame · crackedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK APPROXIMATELY .75 INCH IN FRAME SEGMENT AT BS 400 BETWEEN S21L AND S22L, REMOVED AND REPLACED. (M)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950965Frame · crackedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATELY .75 INCH AT BS 500A BETWEEN S20R AND S21R, REMOVED AND REPLACED. (M)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950964Frame · crackedGSO - AIRCRAFT IN ONE-HALF D-CHECK. DURING INSPECTION, FOUND CRACK APPROXIMATELY .75 INCH AT BS 420 BETWEEN S21L, S22L, S23L. STOP DRILLED CRACK AND INSTALLED DOUBLER. (X)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950963Frame · crackedGSO - AIRCRAFT IN ONE-HALF D-CHECK DURING INSPECTION, FOUND CRACK FRAME SEGMENT APPROXIMATELY .05 INCH AT BS 480 BETWEEN S20L AND S21L. REMOVED AND REPLACED. (X)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950962Frame · crackedGSO - AIRCRAFT IN 1/2 D-CHECK DURING INSPECTION, FOUND CRACK IN FRAME SEGMENT AT BS 460 APPROXIMATELY .75 INCH, BETWEEN S20L AND S21L. REMOVED AND REPAIRED. (X)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950960Frame · crackedGSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500B BETWEEN STR 19L AND STR 20L, AND BETWEEN STR 25L AND STR 27L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .33 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (XOct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950959Frame · crackedGSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500 BETWEEN STR 21L AND STR 22L AND STR 22L AND STR 23L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950958Frame · crackedGSO - INSPECTION FOUND A CRACK IN FRAME AT BS 420 BETWEEN S22R AND S21R AND BETWEEN S21R AND S20R. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X)Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, FrameSDR CAL950956Skin · crackedGSO - INSPECTION FOUND A .50 INCH CRACK AT FORWARD LOWER CORNER OF AFT CARGO DOOR CUT-OUT, EXTERNAL SKIN. THE CRACKED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW TIMCO ENGINEERING ORDER RFO-01655. (X)Oct 24, 1995 · N10236 · Boeing 737222 · Cargo/Baggage DoorsSDR CAL950527Hyd Line · wornFLT NR 1728 - CLE - THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IND. BOTH THE RED AND GREEN LIGHTS REMAINED ON. WHEN THE GEAR HANDLE WAS PLACED DOWN, THE RED LIGHT EXTINGUISHED. THE HYDRAULIC QUANTITY GAUGE DROPPED TO .8 GALS. THE AIRCRAFT WJun 28, 1995 · N10236 · Boeing 737222 · Hydraulic System, Main
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