N33714

Service difficulty reports · 88

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 = 'N33714' AND registry_match = 'registration'
  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 CALA2012120500847Frame · crackedCRACK INDICATION NOTED ON FRAME BS 440 BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. FRAME BS 440 HAS BEEN REPAIRED IAW EA 5310-04716, REV D OP1 FIG 3.Dec 5, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120500846Cargo Track · crackedAFT CARGO TRACK CRACKED AT BS 727B-767 LOWER ATTACH LEG RADIUS. REPLACED CARGO TRACK IAW SRM 53-00-53.Dec 5, 2012 · N33714 · Boeing 737724 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2012120400845Frame · crackedA CRACK INDICATION NOTED AT FRAME BS 520 BETWEEN STR 8 AND 9R DURING MFEC INSPECTION. FRAME REPAIRED IAW EA 5310-04716 REV D OP 1.Dec 4, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400844Frame · crackedA CRACK INDICATION NOTED AT FRAME BS 400 BETWEEN STR 8 AND 9R. DURING MFEC INSPECTION. FRAME REPAIRED IAW EA 5310-04716, REV D OP 1.Dec 4, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400843Frame · crackedA CRACK INICATION NOTED AT FRAME BS 380 BETWEEN S8-9R. DURING MFEC INSPECTION. REPAIRED IAW EA5310-04716 OP1 REV C.Dec 3, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400842Frame · crackedA CRACK INDICATION NOTED AT FRAME BS 500A RT BETWEEN S8 - 9R DURING MFEC INSPECTION. REPAIRED IAW EA 5310-04716, REV D OP 1.Dec 3, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400841Frame · crackedA CRACK INICATION NOTED AT FRAME BS 400 BETWEEN S8 AND 9L DURING MFEC INSPECTION. INSTALLED REPAIR IAW EA 5310-04716.Dec 3, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400840Frame · crackedA CRACK INDICATION NOTED AT FRAME BS 480 BETWEEN S8 AND 9R DURING MFEC INSPECTION. REMOVED DAMAGE. FABRICATED AND INSTALLED FRAME REPAIR IAW EA 5310-04716, REV D, OP 1.Dec 2, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400839Frame · crackedCRACK INDICATION NOTED AT FRAME STA 867 BETWEEN S8 AND 9R DURING MFEC INSPECTION. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLES REF 5310-04716, REV D OP 1.Dec 2, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400835Frame · crackedAD 2009-01-02 CRACK INDICATION NOTED AT FRAME STA 727B BETWEEN STRINGER 8-9L DURING MFEC INSPECTION. REMOVED DAMAGE IAW EA. FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D.Dec 2, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400838Frame · crackedCRACK INDICATION NOTED AT FRAME BS 500C BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5 310-04716, REV D, OP1.Dec 2, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400837Frame · crackedCRACK INDICATION NOTED AT FRAME BS 727D RT BETWEEN S8-9R DURING MFEC INSPECTION. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLES IAW EC/R A 5310-04716, REV D, OP1.Dec 2, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400836Frame · crackedCRACK INDICATION NOTED AT FRAME BS 480 BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. FRAME REPAIRED IAW EA 5310-04716, REV D, OP1 FIG 3.Dec 2, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400834Frame · crackedA CRACK INDICATION NOTED AT FRAME BS 787 BETWEEN STRINGER 8-9L DURING MFEC INSPECTION. REMOVED DAMAGE IAW EA. FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D.Dec 1, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400833Frame · crackedA CRACK INDICATION NOTED AT FRAME BS 380 BETWEEN STRINGER 8-9L DURING MFEC. REMOVED DAMAGE IAW EA FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D.Dec 1, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400832Frame · crackedFRAME AT BS 500A SHOWS CRACK INDICATION DURING MFEC INSPECTION, FRAME REPAIRED IAW EA 5310-04716, REV D, OP1 FIG 3.Dec 1, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2012120400831Frame · crackedFRAME BS 727D SHOWS CRACK INDICATION BETWEEN STR 8 AND 9L. DURING MFEC INSPECTION. FRAME REPAIRED IAW EA 5310-04716 REV D OP 1 FIG 3.Dec 1, 2012 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA2011101800666Seal · wornON TAKEOFF AN AIRCRAFT ON GROUND BEHIND US REPORTED WHAT THEY THOUGHT WAS FUEL LEAKING FROM LEFT WING. TEMP AND DEWPOINT WAS 26/08 VERY DRY AIR CONTINUED TO NEXT LOG PAGE 8912999 LOG NOTED SEE L/P 8912999 FOR CORRECTIVE ACTION AND SIGN OFF - CHECKED VOLUMETROct 18, 2011 · N33714 · Boeing 737724 · Fuel StorageSDR CALA2011083000566Fseu · inoperativeFLAPS WOULD NOT EXTEND PAST 10 DEGREES ON LANDING PERFORMED ALT FLAP LANDING AT FLAPS 15 DEGREES. FSEU SHOWS FAULT 27-53279-L 28VAC EXC INV. FAULT CLEARS. CK`S VOLTAGES IAW FIM 27-51-00-810-822. VOLTS CHECK GOOD. R&R FSEU PRECAUTIONARY. PERF ALL TEST IAWAug 30, 2011 · N33714 · Boeing 737724 · Trailing Edge Flap Control SystemSDR CALA2011011700026Battery · dischargedON PREFLIGHT - F/A FOUND AFT FLASHLIGHT NOT FLASHING. R&R'ED BATTERY AFT OUTBOARD FLASHLIGHT. IND TEST OK - TO CONTINUE.Jan 17, 2011 · N33714 · Boeing 737724 · Emergency EquipmentSDR CALA2010122200629Battery Pack · dischargedMULT-33-3-0001; LT EXTERIOR OVERWING HATCH EMERGENCY EXIT LIGHT IS INOP. REMOVED & REPLACED BATTERY PACK M1668, PERFORMED OPS CHECK GOOD IAW B737-700AMM 33-51-06.Dec 22, 2010 · N33714 · Boeing 737724 · Emergency LightingSDR CALA2010122200628Wire · brokenMULT-33-3-0001; SEAT ROW 22 RT OVERHEAD STOWAGE BIN EMERGENCY EXIT AISLE LIGHT IS INOP. REPAIRED WIRE AT BULB, WIRE W4142 AT STA 680 WITH AN ENVINOMENTAL SPLICE IAW BSWPM 20-10-13 & AMM 33-55-11, EMERGENCY LIGHT CHECKS GOOD IAW J/C 29-0550-8-0002.Dec 22, 2010 · N33714 · Boeing 737724 · Light System WiringSDR CALA2010122200627Wire · brokenMULT-33-3-0001, SEAT ROWS 1 & 2 LT EMERGENCY EXIT FLOOR PROXIMITY LIGHTS ARE INOP. REPAIRED BROKEN WIRE WITH ENVIROMENTAL SPLICE IAW BSWPM 20-10-13, WIRE W3142 AT STA 399. OPS CHECKED GOOD IAW B737-700 AMM 33-55-11.Dec 22, 2010 · N33714 · Boeing 737724 · Light System WiringSDR CALA2010111700582Skin · damagedSUPPORT TASK: LOWER FUSELAGE AT STA 807 FROM STRINGER 27L TO 27R APPEARS TO BE CREASED. INSTALLED REPAIR DOUBLER REF ECRA 5330-04087. INITIATED DIP 53-DIP CTL NUMBER 007952 TO ACCOMPLISH PERMANENT REPAIR PRIOR TO 50,000 TOT FLIGHT CYCLES. PLANNING TO CONTANov 17, 2010 · N33714 · Boeing 737724 · Fuselage Main, Plate/SkinSDR CALA2010101500481A/C Pack · malfunctionedAN ELECTRICAL SMELL WAS OBSERVED ON RIGHT SIDE OF FIRST OFFICER SEAT, BELOW THE R3 WINDOW. NO SMOKE OBSERVED, SMELL CONFIRMED BY 2 CREW MEMBERS ISOLATED ODOR TO LEFT PACK "OILY" ODOR, PLACED LEFT PACK ON MEL 21-01-1L AND COMPLIED WITH DISPATCH DEVIATION PROCEOct 15, 2010 · N33714 · Boeing 737724 · Cabin Cooling SystemSDR CALA2009020500085Battery Pack · dischargedLEFT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECKS GOOD.Feb 4, 2009 · N33714 · Boeing 737724 · Emergency LightingSDR CALA060141Floorbeam · corrodedAFT CABIN FLOORBEAM AT STA 986.5 AND LBL 30 IS CORRODED. REPAIRED BEAM PER SRM 53-00-51, FIG 203, PG 208.Apr 26, 2006 · N33714 · Boeing 737724 · Fuselage Main, Floor BeamSDR CALA0600144Floorbeam · corrodedFWD ENTRY FLOORBEAM CORRODED STA 328. REPAIRED PER SRM 53-00-51, FIG 203.Apr 26, 2006 · N33714 · Boeing 737724 · Fuselage Main, Floor BeamSDR CALA0600143Beam · corrodedAFT ENTRY CORRODED AT STA 986.5 AND RBL 18. REPAIRED PER SRM 53-00-51, FIG 203, PG 208.Apr 26, 2006 · N33714 · Boeing 737724 · Fuselage Main, StructureSDR CALA0600142Floorbeam · corrodedAFT ENTRY FLOORBEAM UPPER CHORD CORRODED AT STA 986.5 AND LBL 4 AND RBL 34. REPAIRED BEAM PER SRM 53-00-51 FIG 203, PG 208.Apr 26, 2006 · N33714 · Boeing 737724 · Fuselage Main, Floor BeamSDR CALA0600140Angle · corrodedR2 DOOR Z-ANGLE CORRODED. REPLACED Z-ANGLE PER SRM 51-40-02.Apr 26, 2006 · N33714 · Boeing 737724 · Passenger/Crew DoorsSDR CALA0600139Floor Support · corrodedAFT ENTRY FLOOR SUPPORT BETWEEN STA 947.5 AND 967 AT RBL 50 CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02.Apr 26, 2006 · N33714 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA0400334Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696.Apr 7, 2004 · N33714 · Boeing 737724 · Horizontal Stabilizer StructureSDR CALA0400333Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696.Apr 7, 2004 · N33714 · Boeing 737724 · Horizontal Stabilizer StructureSDR CALA0400332Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696.Apr 7, 2004 · N33714 · Boeing 737724 · Horizontal Stabilizer StructureSDR CALA0300516Frame · gougedINSPECTION FOUND FRAME GOUGED UNDER Z-CHANNEL IN AFT CARGO COMPARTMENT AT STA 947.5, S25R. REPAIRED DAMAGED FRAME SECTION IAW ECRA 5311-01165.Sep 8, 2003 · N33714 · Boeing 737724 · Fuselage Main, FrameSDR CALA0100366Hinge · wornINSPECTION FOUND LEFT ELEVATOR TAB I/B NR 1 HINGE POINT WORN. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-31-00.Apr 15, 2001 · N33714 · Boeing 737724 · Elevator, Tab StructureSDR CALA0000314Fire Detector · malfunctionedNR 2 ENG FIRE DET FAULT LIGHT ILLUM ON CLIMBOUT AND LEVEL OFF AT CRUISE. WHEN LOOPS A & B WERE TESTED NR 2 FIRE HANDLE WOULD NOT ILLUM. SYSTEM CHK OK ON DESCENT. MX FOUND NO EVIDENCE OF FIRE. FIRE DET UNIT WAS REMOVED AND REPLACED, OPS CHK GOOD IAW MM 26-Mar 19, 2000 · N33714 · Boeing 737724 · Fire Detection
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