N14079, cancelled Jun 14, 2012
Service difficulty reports · 31
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 = 'N14079' AND deregistration_id = 'N14079-2012-06-14' 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 = 'N14079' AND deregistration_id = 'N14079-2012-06-14' 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 CALA0001683Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN RT HORIZONTAL STABILIZER UPPER AFT O/B SKIN. THE RT UPPER AFT O/B SKIN PANEL WAS REPAIRED IAW ECRA 5511-01035.SDR CALA0001681Fitting · corrodedINSPECTION FOUND LAV E O/B SUPPORT BEAM CORRODED AT AFT ATTACHMENT FITTING, STA Y = 1831-1887, X = 31L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001657Floor Support · corrodedINSPECTION FOUND LAV F I/B SUPPORT BEAM CORRODED. A NEW BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001656Floor Support · corrodedINSPECTION FOUND LAV E I/B SUPPORT BEAM CORRODED AT STA. Y = 1831-1887, X = 5L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001655Floor Support · corrodedINSPECTION FOUND GALLEY G-2 SUPPORT BEAM CORRODED AROUND FORWARD ATTACHMENT BOLT HOLE AT STA Y = 392-412, X = 8R. A REPAIR WAS INSTALLED IAW GMM 10-900-01 AND 53-11-01.SDR CALA0001654Floor Support · corrodedINSPECTION FOUND GALLEY G-2 FLOOR SUPPORT CHANNEL SECTION CORRODED AT STA Y = 392-459, X = 40R. A NEW FLOOR SUPPORT CHANNEL SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.SDR CALA0001653Floor Support · corrodedINSPECTION FOUND LONGITUDINAL SUPPORT BEAM AFT OF GALLEY G-1 CORRODED AT STA Y = 412-487, X = 24L. A NEW SECTION OF SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.SDR CALA0001652Floor Support · corrodedINSPECTION FOUND GALLEY G-6 O/B SUPPORT BEAM CORRODED AT FORWARD END. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001651Floor Support · corrodedINSPECTION FOUND GALLEY G-1 SUPPORT BEAM CORRODED AT STA Y = 392-422, X = 20L. A REPAIR WAS PERFORMED IAW GMM 10-900-01 AND SRM 53-11-1.SDR CALA0001650Floor Support · corrodedINSPECTION FOUND LAV F O/B SUPPORT BEAM CORRODED AT Y = 1831-1887, X = 31R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-16-01.SDR CALA0001641Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM J SECTION AT BASE OF FLIGHT DECK STEP CORRODED AT STA Y = 392, X = 20L-20R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.SDR CALA0001640Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP FORWARD OF GALLEY 6 AND 7 CORRODED AT STA Y = 1914, X = 17L-17R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001639Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM FWD OF LAV H CORRODED AT STA Y = 1914, X = 44L-66L. A NEW SUPPORT SECTION WAS INSTALLED IAW SRM 53-16-01 AND GMM 10-900-01.SDR CALA0001628Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP AFT OF LAVS E AND F AT STA Y = 1887, X = 5R-24R CORRODED. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001627Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIPS AFT OF LAVS E & F AT STA Y = 1887, X = 28L-32L AND X = 38L-58L CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001626Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM CAPPING SECTIONS AFT OF LAVS E & F AT STA Y = 1887, X = 5L-24L AND X = 27R-53R CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001625Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM J SECTION CORRODED AT STA Y = 421, X = 24L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.SDR CALA0001624Floorbeam · corrodedINSPECTION FOUND GALLEY G3 LATERAL FLOORBEAM J SECTION CORRODED AT STA Y = 459, X = 18L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.SDR CALA0001623Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT LAVS E & F, STA Y = 1887, X = 38R-58R. A REPAIR WAS ACCOMPLISHED BY INSTALLING A NEW J SECTION IAW GMM 10-900-01 AND SRM 53-16-01.SDR CALA0001622Floorbeam · corrodedINSPECTION FOUND LATERAL FLOORBEAM CORRODED AT STA Y = 459, X = 38R-41R. A SPLICE REPAIR WAS PERFORMED IAW SRM 53-30-00.SDR CALA0000146Fuse · failedTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM HNL. THE A/C WAS RETURNED TO HNL WHERE IT LANDED W/O INCIDENT. MX FOUND THE MLG INTERLOCK CYLINDER RETRACTED. RESET TRIM CYLINDER FUSE. INTERLOCK CYLINDER NOW IN PROPER POSITION IAW MM 32-31-06, PAGE 201SDR CALA9901499Safety Wire · out of positionCREW RECEIVED RED GEAR WARNING LIGHTS WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND GEAR WAS EXTENDED MANUALLY. ALL GEAR LIGHTS WERE GREEN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR CONTROL HANDLE WAS NOT MAKING COSDR CALA9901480Angle · crackedINSPECTION FOUND NR 1 ENGINE INTAKE EXTERNAL SIDE AFT SUPPORT ANGLES(2) CRACKED. THE CRACKS WERE 1 LONG. THE SUPPORT ANGLES WERE REPLACED IAW SRM 51-30-00.SDR CALA9901479Angle · crackedINSPECTION FOUND A 3 CRACK IN RT WING FIXED L/E SUPPORT ANGLE AT STA XOS 414.125. A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01.SDR CALA9901478Skin · crackedINSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CRACKED AT STA XORS 455 AND STA XORS 506. BOTH CRACKS WERE 1 LONG. REPAIRS WERE INSTALLED IAW DRAWING ARB2933-46, DRAWING ARB2933-10, SRM 57-10-00, FIGURE 49 AND 51-31-01.SDR CALA9901444Strip · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT O/B STRIP. PERFORMED REPAIR IAW SRM 57-10-00.SDR CALA9901434Skin · crackedINSPECTION FOUND A 0.9 INCH CRACK IN RT WING LEADING EDGE SKIN AT XORS 783. A REPAIR WAS INSTALLED IAW SRM 57-10-00, FIGURE 68.SDR CALA9900509Rod · disconnectedUNABLE TO ARM L3 DOOR AT DEPARTURE. FOUND ROD AT LOCKING MECHANISM OUT OF PLACE. REINSTALLED ROD AND TIGHTENED HARDWARE.SDR 98ZZZX4012Fan Frame · crackedTHE NR 1 ENGINE REVERSER SEAL SUPPORT RING, LEFT, WAS FOUND CRACKED AT ALL FIVE FORWARD ATTACH POINTS. THE FLANGE SECTIONS HAD BROKEN COMPLETELY AWAY FROM THE TWO BOLT ATTACHMENTS IN AN ARC THE CRACK PASSING THROUGH THE TOP ROW OF TWO ATTACHMENT RIVETS OF A SSDR CALA9801671Hyd Line · puncturedTHE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN HYDRAULIC PRESSURE LINE TO LEFT HYDRAULIC PUMP AND THE RIGHT PUMP WAS LEAKING HYDRAULIC FLUID OUT DRAIN MAST. THE SDR CALA9801456Smoke Detector · inoperativeTHE AFT CARGO FIRE WARNING LIGHT AND SMOKE DETECTOR LIGHT ILLUMINATED WHILE ENROUTE. EMERGENCY PROCEDURES WERE COMPLIED WITH AND THE LIGHTS EXTINGUISHED. BOTH CARGO FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO SJU WHERE IT LANDED WITHOUT INC
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