N14062, cancelled Jun 11, 2003
Service difficulty reports · 53
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 = 'N14062' AND deregistration_id = 'N14062-2003-06-11' 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.
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 = 'N14062' AND deregistration_id = 'N14062-2003-06-11' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA0100244Support · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. THE PIVOT SUPPORT WAS REPLACED IAW EA 5310-03417 AND ECRA 5310-04118.SDR CALA0100238Skin · corrodedINSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT STA 1364. THE CORRODED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 20.SDR CALA0100237Bolt · shearedINSPECTION FOUND BOLT SHEARED IN RT WING FORWARD SPAR TO FUSELAGE ATTACH ANGLE. THE BOLT WAS REPLACED IAW SRM 51-38-01.SDR CALA0100236Beam · corrodedINSPECTION FOUND GALLEY G1A-G5 RT SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-35-00.SDR CALA0100235Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 1139, LONGERON 51L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW SECTION WAS INSTALLED.SDR CALA0100217Floorbeam · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 1298, RT, APPROXIMATELY TEN INCHES FROM EXTERNAL SKIN JOINT. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 7.SDR CALA0100210Floor Support · corrodedINSPECTION FOUND GALLEY G6 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48R. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844.SDR CALA0100209Floor Support · corrodedINSPECTION FOUND GALLEY G7 I/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1887-2007, X = 24L. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844.SDR CALA0100208Floor Support · corrodedINSPECTION FOUND GALLEY G7 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48L. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844.SDR CALA0000083Skin · corrodedINSPECTION FOUND LOWER FUSELAGE SKIN CORRODED WITH A PULLED RIVET AT STA 1761 BETWEEN STRINGER 45R AND 47R. REPAIRED IAW SRM 51-71-00.SDR CALA0000079Door Sill · corrodedINSPECTION FOUND FORWARD CARGO DOOR JAMB LOWER AFT CORNER DOOR SILL CORRODED. THE DOOR SILL WAS REPAIRED IAW SRM 53-70-00.SDR CALA9900120Support · corrodedINSPECTION FOUND THE RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. REPAIRED IAW ECRA 5743-01013.SDR CALA9800218Actuator · leakingTHE NLG WAS VERY SLOW TO EXTEND AND INDICATE DOWN WHEN GEAR WAS LOWERED DURING TEST FLIGHT WHILE AIRCRAFT WAS IN D-CHECK AT MAN. MAINTENANCE FOUND THE NLG DOWNLOCK ACTUATOR LEAKING INTERNALLY. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-35-00.SDR CALA9800193Frame · corrodedINSPECTION FOUND CORROSION IN FRAME AND INTERCOSTALS IN AVIONICS BAY AT STA 450 BETWEEN STRINGER 44 AND 64L. THE AREA WAS REPAIRED IAW SRM 53-30-00.SDR CALA9800192Stiffener · corrodedINSPECTION FOUND CORROSION AT LOWER LT CORNER OF DOOR IN AVIONICS COMPT AT REAR PRESSURE BULKHEAD STA 475, LT HORIZONTAL AND VERTICAL BEHIND GUSSET PLATE. THE AREA WAS REPAIRED IAW SRM 53-12-01.SDR CALA9800184Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36R. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-10-00.SDR CALA9800176Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36L. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-00-00.SDR CALA9800131Bulkhead · frettedINSPECTION FOUND, FRETTING ON CLG AFT PRESSURE BULKHEAD AT STA 1521. A REPAIR WAS ACCOMPLISHED IAW DOUGLAS DRAWING 90-53-1022.SDR CALA9800107Angle · crackedINSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3.SDR CALA9701708Frame · crackedTHE A/C LOST NR 3 HYDRAULIC SYSTEM AND GEAR UNSAFE LIGHT ILLUMINATED WHILE INBOUND TO EWR. THE A/C WAS TAKEN OUT OF SERVICE FOR T/S. INITIAL FINDINGS REVEALED THE LT MLG RETRACT ACTUATOR SUPPORT FRAME ASSEMBLY WAS CRACKED. THE SUPPORT FRAME WAS REMOVED AND SDR CALA9701278Blade · failedNR 3 ENG MADE A LOUD BANG WITH EGT RISING TO 800 DEGREES AND N1 DROPPING TO 80 PERCENT WHILE EN ROUTE. THE ENGINE POWER WAS REDUCED TO IDLE AND OIL QUANTITY BEGAN TO DROP. THE ENG WAS SHUTDOWN AND THE ACFT WAS DIVERTED TO BSB WHERE IT LANDED WITHOUT INCIDENTSDR CALA9700731Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO SKIN AT STA 1901 TO 1921, STRINGER 7R AND SHEAR TIE HAD A 1.5 AND 1 INCH CRACK AT STA 1921 BETWEEN STRINGER 7R AND 8R. THE SKIN AND SHEAR TIE WERE REPAIRED IAW SRM 53-20-00, FIGURE 6.SDR CALA9700730Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1900 TO 1921 BETWEEN STRINGERS 7L AND 8L. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIGURE 6.SDR CALA9700743Tee Section · corrodedINSPECTION FOUND T-SECTION CORRODED AT STA 1986, LONGERONS 50R AND 51R. THE T-SECTION WAS REPLACED IAW SRM 53-10-00.SDR CALA9700742Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 1975, LONGERON 47R AND 48R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-10-00.SDR CALA9700752Beam · corrodedINSPECTION FOUND SUPPORT BEAM CORRODED AT STA 1834 TO 1879, LAV F, X= -33. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.SDR CALA9700751Beam · corrodedINSPECTION FOUND LATERAL SUPPORT BEAMS CORRODED AT STA 1879, X= +38 TO +53 AND X= -38 TO -53. THE SUPPORT BEAMS WERE REPLACED IAW SRM 53-22-00.SDR CALA9700750Beam · corrodedINSPECTION FOUND SUPPORT BEAM CORRODED AT STA 1834 TO 1879, LAV E. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.SDR CALA9700749Beam · corrodedINSPECTION FOUND INBOARD SUPPORT BEAM AND LATERAL SUPPORT BEAM CORRODED AT STA 1841 TO 1887, LAV F. THE SUPPORT BEAMS WERE REMOVED AND REPLACED IAW SRM 53-22-00.SDR CALA9700748Beam · corrodedINSPECTION FOUND SUPPORT BEAMS CORRODED AT STA 1879, X = 4 TO 33 AND X = -4 TO -33. THE SUPPORT BEAMS WERE REPLACED IAW SRM 53-22-00.SDR CALA9700747Beam · corrodedINSPECTION FOUND FLOORBOARD SUPPORT BEAM CORRODED AT STA 1899, X = 0 TO +20. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.SDR CALA9700745Beam · corrodedINSPECTION FOUND LT GALLEY SUPPORT BEAM CORRODED AT STA 1879 TO 2007, X = 24. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.SDR CALA9700746Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT L-1 DOOR, STA 395 TO 433. THE FLOORBEAM WAS REPLACED IAW SRM 53-27-00.SDR CALA9700744Beam · corrodedINSPECTION FOUND LONGITUDINAL SUPPORT BEAM CORRODED AT LAV G, STA 1913 TO 2007. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-0.SDR CALA9700297Prox Switch · inoperativeWHEN GEAR WAS EXTENDED FOR LANDING, THERE WERE NO GREEN LIGHTS INDICATED ON FORWARD PANEL OR SECOND OFFICER'S PANEL. THE GEAR WAS CYCLED AND INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY CONTROSDR CALA9700287Hyd Line · chafedTHE NR 1 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE DROPPED TO ZERO WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE TO LT ENGINE DRIVEN HYDRAULIC PUMP CHAFED THROUGH. THE HYDRAULIC LISDR CALA9601793Hyd Line · rupturedTHE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM FLUID AFTER FLAP RETRACTION DEPARTING MAD. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO MAD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LT ENGINE DRIVEN PUMP PRESSURE LINE TO MANIFOLD RUPTURSDR CALA9601489Wat Sep Bags · dirtyTHE FLIGHT ATTENDANTS REPORTED AN ODOR OF ELECTRICAL SMOKE WHILE ON APPROACH. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FOR AN ELECTRICAL FAILURE AND FOUND NO FAULTS. ALL THREE WATER SEPARATOR BAGS WERE FOUND EXTREMELY SDR CAL960407Skin · damagedKUL - INSPECTION FOUND IMPACT DAMAGE AT LOWER AFT SECTION OF FORWARD CARGO DOOR CUT-OUT. THE AREA WAS REPAIRED IAW ECRA 5330-02370. (X)SDR CAL960405Angle · crackedKUL - INSPECTION FOUND TWO 1 INCH CRACKS IN ANGLE AT STA XCW 14 LT AND XCW 14 RT, BS 2123. A REPAIR WAS CARRIED OUT PER SRM 53-00-01, PAGE 7. (X)SDR CAL960404Skin · crackedKUL - INSPECTION FOUND A DENT AND 1.25 INCH CRACK IN THE TOP SKIN OF THE LT HORIZONTAL STABILIZER INBOARD PANEL. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-71-00 AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 57-71-00, PAGE 65. (X)SDR CAL960406Frame · damagedKUL - INSPECTION FOUND A .50 INCH DIAMETER HOLE IN FRAME, STA 1841, ABOVE CENTER CARGO FLOOR AREA ON LT SIDE. THE FRAME WAS REPAIRED IAW ECRA 5310-03243. (X)SDR CAL960408Spar Cap · crackedKUL - INSPECTION FOUND A 6 INCH CRACK JUST ABOVE RADIUS ON FORWARD SIDE OF RT WING AFT LOWER SPAR CAP AT STA 1043. THE SPAR CAP WAS REPAIRED IAW ECRA 5710-01720. (X)SDR CAL960158Valve · leakingFLT NR 10 - EWR - THE NR 1 HYDRAULIC SYSTEM BEGAN TO LOSE FLUID WHILE EN ROUTE FROM IAH TO ORY. THE QUANTITY DROPPED STEADILY. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LOWER PRIMARY TRIM CONTROL VALVE LEAKING.SDR CAL951068Hyd Pump · case crackedFLT NR 0005 - IAH - THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED AND THE NR 3 HYDRAULIC QUANTITY AND PRESSURE DECREASED TO ZERO IN FLIGHT. THE EMERGENCY CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3SDR CAL950941Eel Pin · looseLAX - FLT NR 0063 - ROWS 19-33, INCLUDING OVERWING EMERGENCY LIGHTS COME ON WHEN POWER IS SHUTOFF. FOUND PIN 'V' DISARMED, PUSHED PIN BACK IN AT CONNECTOR. (M)SDR CAL950919Trailing Edge · missingFLT NR 0011 - ORY - A WALK AROUND INSPECTION, FOUND RIGHT INBOARD ELEVATOR TRAILING EDGE STRIP MISSING (APPROXIMATELY 24 INCHES). A PERMANENT REPAIR WAS PERFORMED PER SRM 55-30-00, FIGURE 2. (M)SDR CAL950600Eel Battery · dischargedFLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BASDR CAL950599Eel Battery · dischargedFLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BASDR CAL950598Eel Batt Charger · inoperativeFLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BA
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