N14233, cancelled Jun 24, 1999

Service difficulty reports · 52

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 = 'N14233' AND deregistration_id = 'N14233-1999-06-24'
  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 CALA9801858Line · leakingTHE NR 1 ENGINE THROTTLE WAS TWO KNOBS AHEAD OF NR 2 WITH CLIMB POWER SET OUT OF MSP. THE SPLIT INCREASED TO ABOUT 3 KNOBS DIFFERENCE AS CLIMB PROGRESSED. FUEL FLOW WAS ABOUT 2000 LBS HIGHER ON NR 1 FOR SAME ENGINE PARAMETERS AT ABOUT 31,000 FT. THE NR 1 ENSep 25, 1998 · N14233 · Boeing 737217 · Fuel Controlling SystemSDR CALA9800039Control Cable · out of adjTHE LANDING GEAR HANDLE COULD NOT BE MOVED BEYOND THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG TELEFLEX CABLE OUT OF ADJUSTMENT. THJan 14, 1998 · N14233 · Boeing 737217 · Landing Gear Retraction/Extension SystemSDR CALA9800017Solenoid · inoperativeTHE LANDING GEAR HANDLE WOULD NOT GO PAST THE OFF DETENT AFTER TAKEOFF. THE OVERRIDE DID NOT WORK EITHER. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE M241 LEVER LATCH SOLENOID AT FAULT. THE SOLENOID WAS REPLACEDJan 12, 1998 · N14233 · Boeing 737217 · Landing Gear Retraction/Extension SystemSDR CALA9701377Hyd Line · chafedTHE A-HYDRAULIC SYSTEM BEGAN TO LEAK SLOWLY WHILE EN ROUTE. THE HYDRAULIC PUMPS WERE TURNED OFF BEFORE LOW PRESSURE LIGHTS ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM HYDRAULIC PRESSURE LINE IN Sep 20, 1997 · N14233 · Boeing 737217 · Hydraulic System, MainSDR CALA9700160Skin · crackedINSPECTION FOUND A 4.5 INCH CRACK IN RT WING LEADING EDGE SKIN AT WS 190. THE CRACKED AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-2, FIGURE 2.Feb 6, 1997 · N14233 · Boeing 737217 · Wing, Plate/SkinSDR CALA9700176Angle · crackedINSPECTION FOUND A 2.5 INCH CRACK IN RIB LOWER CHORD ANGLE AT S3 IN FUEL ACCESS PANEL 7202 AT LT WING FUEL TANK, WBL 135.5. THE CRACKED AREA WAS REMOVED, A REPAIR TEE WAS INSTALLED IAW BOEING SERVICE BULLETIN 737-57-1186 AND REPAIR ENGINEERING ORDER NUMBER 02Feb 5, 1997 · N14233 · Boeing 737217 · Wing Miscellaneous StructureSDR CALA9700175Angle · crackedINSPECTION FOUND STA 540 WING TO BODY FRAME CRACKED LOWER AREA LBL 31, T-ANGLE WAS CRACKED INTO TWO PIECES. THE CRACKED SECTION WAS REMOVED, ANGLES AND T-CHORD WERE FABRICATED AND INSTALLED IAW SRM 51-30-2.Feb 5, 1997 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9700172Web · crackedINSPECTION FOUND THREE EACH CRACKS AT RIVETS OF WEB UNDER NR 3 SEAT TRACK AT BS 715. THE CRACKS WERE APPROXIMATELY 2 INCHES LONG. THE CRACKED AREAS WERE REMOVED, REPAIR SHIMS AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.Feb 5, 1997 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9700171Bulkhead Web · puncturedINSPECTION FOUND A .25 INCH DIAMETER PUNCTURE IN AFT PRESSURE BULKHEAD WEB AT 8:30 POSITION, TWO FEET FROM CENTER. THE DAMAGED AREA WAS REMOVED, A DOUBLER AND FASTENERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-30-0.Feb 5, 1997 · N14233 · Boeing 737217 · Fuselage Main, BulkheadSDR CALA9700170Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN SKIN PANEL AT LEADING EDGE STA 213 OF LT WING LOWER SURFACE. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-0 AND 51-30-2.Feb 5, 1997 · N14233 · Boeing 737217 · Wing, Plate/SkinSDR CALA9700169Stringer · crackedINSPECTION FOUND A 2 INCH CRACK IN STRINGER AT STA 907. THE CRACKED SECTION OF STRINGER WAS REMOVED IAW SRM 53-10-3, STRINGER SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-3 AND 51-30-2.Feb 5, 1997 · N14233 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CALA9700168Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN RADIUS OF STRINGER 6L AT STA 787. THE CRACKED SECTION OF STRINGER WAS REMOVED, A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-2, AND 51-20-4.Feb 5, 1997 · N14233 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CALA9700167Fitting · crackedINSPECTION FOUND A 1 INCH CRACK AT BOTTOM AFT FACE OF VERTICAL STABILIZER LT AFT OUTBOARD FITTING TO LUG. THE CRACKED FITTING WAS REMOVED, A NEW FITTING WAS DRILLED AND INSTALLED IAW SRM 51-10-7 AND 51-30-2.Feb 5, 1997 · N14233 · Boeing 737217 · Vertical StabilizerSDR CALA9700166Support · brokenINSPECTION FOUND FORWARD CARGO PIT FLOOR SUPPORT BROKEN AT STA 490 ABOVE STRINGER 28L. THE BROKEN SECTION WAS REMOVED IAW SRM 53-10-1 AND 51-30-2, A NEW SECTION OF SUPPORT WAS TRIMMED, FITTED AND SPLICED IAW SRM 53-10-5. THE NEW SECTION AND SPLICES WERE INSTFeb 5, 1997 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9700159Frame · corrodedINSPECTION FOUND STA 250 RT VERTICAL STIFFENER, STA 277 RT FRAME WEB, STA 270 RT SHEAR TIE ANGLE CHORD IN RT NOSE WHEEL WELL CORRODED. A VERTICAL BEAM, FRAME WEB REPAIR ANGLES, AND SHEAR TIE REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2Feb 4, 1997 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CALA9700158Frame · corrodedINSPECTION FOUND STA 270 LT FRAME, STA 277 LT CAP ANGLE, FRAME WEB, STIFFENER CHANNELS AT STA 270 AND 277, AND BEAR STRAP AT STA 277 LT CORRODED. FRAME ANGLES, WEB, REPAIR DOUBLER, STIFFENER CHANNELS, BEAR STRAP, FILLER AND DOUBLERS WERE FABRICATED AND INSTALFeb 4, 1997 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CALA9700157Bulkhead · crackedINSPECTION FOUND A 8.25 INCH CRACK AT RBL 7.5 AND A 5.25 INCH CRACK AT LBL 6.12 IN BULKHEAD, STA 294.5. THE CRACKED AREAS WERE CUT OUT, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03410.Feb 4, 1997 · N14233 · Boeing 737217 · Fuselage Main, BulkheadSDR CALA9700146Frame · crackedINSPECTION FOUND FRAME CRACKED AND BENT AT STA 987, BL ZERO - RBL 10. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CALA9700145Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACKS 2-13 AT STA 360. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9700144Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 744, RBL 15 TO LBL 15. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9700143Floorbeam · corrodedINSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 980. THE UPPER FLANGE WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9700142Support · crackedINSPECTION FOUND TWO 8 INCH CRACKS IN FORWARD CARGO PIT FLOOR SUPPORT AT STA 460, RBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-40-4.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9700141Floorbeam · corrodedINSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, RBL 24 TO RBL 50. THE UPPER CHORD OF BEAM WAS REMOVED. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9700138Skin · gougedINSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER SKIN GOUGED. THE GOUGED SKIN WAS CUT OUT, REPAIR FILLERS AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5330-02484.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CALA9700137Angle · corrodedINSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 947 TO 970, ON RT SIDE. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED, A REPAIR SECTION AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CALA9700136Floorbeam · crackedINSPECTION FOUND A 2 INCH CRACK ON UPPER FLANGE OF FLOORBEAM AT BS 667, BL 0. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5710-01779.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9700135Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 685, BL 0. A 1 INCH CRACK WAS FOUND IN TRANSVERSE BEAM AT STA 675, BL 0. THE FLOORBEAM WAS REPAIRED IAW BAC DRAWING 65C19643. THE TRANSVERSE BEAM WAS REPAIRED IAW BAC DRAWING 65C17103.Feb 3, 1997 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CALA9700134Bulkhead · crackedINSPECTION FOUND AN 8 INCH CRACK IN BULKHEAD AT STA 178, RBL 29 AND A 10 INCH CRACK WAS FOUND IN BULKHEAD AT STA 178, LBL 29. THE CRACKED AREAS WERE CUT OUT, FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-11.Jan 30, 1997 · N14233 · Boeing 737217 · Fuselage Main, BulkheadSDR CALA9700133Stringer · crackedINSPECTION FOUND A .25 INCH CRACK IN STRINGER AT RT WING FS 465 LEADING EDGE SLAT WELL. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-30-2.Jan 30, 1997 · N14233 · Boeing 737217 · Wing, Longeron/StringerSDR CAL960447Floorbeam · crackedGSO - INSPECTION FOUND A .50 INCH CRACK AND CORROSION ON COCKPIT AFT FLOORBEAM AT STA 459. THE CORRODED AREAS WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)Apr 5, 1996 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CAL960449Frame · crackedGSO - INSPECTION FOUND A 3 INCH CRACK IN LOWER FORWARD FRAME OF C-1 DOOR. THE FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Mar 30, 1996 · N14233 · Boeing 737217 · Cargo/Baggage DoorsSDR CAL960448Skin · corrodedGSO - INSPECTION FOUND THE NR 2 ENGINE FORWARD OUTBOARD COWL OUTER SKIN CORRODED AROUND ENGINE RADIUS WARNING PLACARD. THE CORRODED SECTION OF SKIN WAS CUT OUT. A DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-2. (X)Mar 28, 1996 · N14233 · Boeing 737217 · Nacelle/Pylon, Plate/SkinSDR CALA950524Line · chafedDFW - FLT 1648 - LOSS OF A-SYSTEM HYD QUANTITY. REQUIRED BRAKE REPLACEMENT TO REMOVE FROM RUNWAY DUE TO OVERTEMP ON LANDING. FOUND LINE ON NR 2 ENGINE DRIVEN PUMP CHAFED. REPLACED LINE, FLUSHED, OPERATION AND LEAK CHECKED SYSTEM. REMOVED AND REPLACED NR 1,Jun 25, 1995 · N14233 · Boeing 737217 · Hydraulic System, MainSDR CAL950484Cargo Door · crackedCLE - FLT 1639 - MAINTENANCE FOUND TWO CRACKS IN THE FORWARD CARGO DOOR AT THE SEAL RETAINER WHILE UNDERGOING A DECAY CHECK FOR PRESSURIZATION PROBLEMS. THE CRACKS WERE 8 INCHES AND 4.5 INCHES LONG. THE FORWARD CARGO DOOR WAS REMOVED AND REPLACED IAW MM 52-3Jun 13, 1995 · N14233 · Boeing 737217 · Cargo/Baggage DoorsSDR CAL950339Fan Blade · bentFLT NR 1464 - IAH - ON MAINTENANCE WALKAROUND, FOUND NR 2 ENGINE FAN BLADE BENT OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE ENGINE C1 DISK FAN ASSY. CHANGE COMPLETED, OPS CHECK GOOD. (W)Apr 28, 1995 · N14233 · Boeing 737217 · Turbine Engine Compressor SectionSDR CAL950273Hyd Module · failedGSO - FLT 1735 - THE A-HYDRAULIC SYSTEM PRESSURE DROPPED TO ZERO DURING CLIMB OUT OF GSO. CHECK LIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CHECK VALVE FAILURE OF THE A-HYDRAULApr 15, 1995 · N14233 · Boeing 737217 · Hydraulic System, MainSDR CAL950111Skin · crackedGSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES ON RT SIDE OF FUSELAGE BETWEEN BS 188 AND BS 251.6. ALL CRACKS WERE APPROXIMATELY 1 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CAL950110Skin · crackedGSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES BETWEEN BS 188 AND BS 251.6 ON THE LT SIDE OF FUSELAGE. ALL CRACKS WERE APPROXIMTELY .25 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CAL950109Skin · corrodedGSO - INSPECTION FOUND CORROSION ON RT EXTERNAL SKIN AND DOUBLER AT STA 727 BETWEEN STR 17R AND STR 18R. THE CORROSION WAS REMOVED AND A DOUBLER IN INSTALLED IAW EC 5330-02227. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Plate/SkinSDR CAL950108Skin · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN THE LT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN AT STA 66. THE CRACK WAS STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 55-10-3 AND SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Horizontal Stabilizer, Plate/SkinSDR CAL950107Intercostal · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BEHIND AFT FORMER IN E AND E BAY. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CAL950106Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500 BETWEEN STR 21L AND STR 20L. THE CRACKED BELT FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950100Frame · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN BELT FRAME AT BS 480 BETWEEN STR 21L AND STR 20L. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-30-0. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950099Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500A BETWEEN STR 21L AND STR 20L. THE CRACKED FRAME WAS CUT OUT IAW BOEING DRAWING 65C225113 AND A REPAIR WAS INSTALLED IAW SRM 51-30-0. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950098Belt Frame · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN BELT FRAME AT BS 420, STR 22L. THE CRACK WAS REPAIRED IAW BOEING DRAWING 65C25113. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950097Frame · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN STA 578 MAIN CABIN FRAME AT STR 16 - STR 17L. THE FRAME WAS REPAIRED IAW SRM 51-40-3 AND SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950096Stringer · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN STR 5R AT STA 685. THE CRACK WAS STOP DRILLED AND A REPAIR CHANNEL WAS INSTALLED IAW SRM 53-10-3. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CAL950095Chord · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN RT STA 727 OUTBOARD CHORD AT STR 18A. THE CRACKED CHORD WAS REMOVED AND A NEW CHORD WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 65C33722. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CAL950094Floor Panel · corrodedGSO - INSPECTION FOUND THE NR 6 FLOOR PANEL SUPPORT CORRODED AT STA 312. THE PANEL SUPPORT WAS REPAIRED IAW SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Floor PanelSDR CAL950093Floorbeam · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN STA 639 LT SIDE FLOORBEAM WEB CABLE CUTOUT. THE FLOORBEAM WEB WAS REPAIRED IAW BOEING DRAWING 65C25211. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Floor Beam
Back to N14233, cancelled Jun 24, 1999