N450ML, cancelled May 14, 2013
Service difficulty reports · 20
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 = 'N450ML' AND deregistration_id = 'N450ML-2013-05-14' 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 = 'N450ML' AND deregistration_id = 'N450ML-2013-05-14' 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 22AA200900031Elt · malfunctionedON PRE-FLIGHT FOUND ELT LIGHT BLINKING. ENTERED ON DMI NR 23233 IAW MEL 25-40-2 CAT "A" C/B COLLARED VERIFIED NO AUDIO TRANSMIT ON VHF FREQ, PLACARD INSTALLED DMI NR 23233.SDR 22AA200900022Slat System · malfunctionedON SHORT FINAL, SLAT DISAGREE LIGHT ILLUMINATED CAUSING STICK SHAKER. PROMPT APPLICATION OF FIREWALL POWER AND INCREASE IN SPEED PUT SLATS BACK IN "LAND" LANDING UNEVENTFUL. APP GW OF 305.000 LBS. 35/EXT REF OF 133+5 KTS. (K)SDR 22AA2009000022Slat System · malfunctionedON SHORT FINAL, SLAT DISAGREE LIGHT ILLUMINATED CAUSING STICK SHAKER PROMPT APPLICATION OF FIREWALL POWER AND INCREASE IN SPEED, PUT SLATS BACK IN LAND; LANDING UNEVENTFUL. APP GW OF 35.000 LBS, 35/EXT. REF. OF 133 + 5 KTS. INSPECTED SLAT SYS CABLES, PULLEYS,SDR 22AA20081006Slat · damagedON SERVICE CHECK, RT WING SLAT NR 8 LEADING EDGE DAMAGE. FOUND BIRD STRIKE ON RT WING SLAT NR 8 LEADING EDGE; INSPECTED RT WING SLAT NR 8 LEADING EDGE IN ACCORDANCE WITH DC10 M/M 05-62-00. PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATISDR 22AA20081001Hydraulic Line · damagedAFTER CLOSING CARGO DOOR FOR DEPARTURE, HARD ODOR OF HYDRAULIC FLUID IN FLIGHT DECK. REMOVED AND REPLACED MAIN CARGO DOOR CLOSE LINE AS REQUIRED; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 52-34-01, NO LEAKS FOUND.SDR 22AA20080903Slide Raft · deployedL-1 DOOR SLIDE RAFT DEPLOYED. REMOVED L-1 DOOR SLIDE RAFT IN ACCORDANCE WITH DC-10 M/M 25-61-07; PERFORMED DOOR CHECK FOUND NORMAL IN ACCORDANCE WITH DC-10 M/M 52-11-07. TRANSFERRED TO DMI 22064 AS PER MEL 52-10-2, CAT "C". REMOVED & REPLACED L-1 DOOR RAFT SDR ARWA20080903Slide · unwanted deployL-1 DOOR SLIDE RAFT DEPLOYED. REMOVED L-1 DOOR SLIDE RAFT IAW MM 26-61-07, PERFORMED DOOR CHECK FOUND NORMAL IAW MM 52-11-07. TRANSFERRED TO DMI NR 22064 IAW MEL 52-10-2,, CAT (C). (K)SDR ARWA20080706Hydraulic System · lowNR 1 HYDRAULICS NEED SERVICING. SERVICED NR 1 HYDRAULIC SYSTEM AS REQUIRED IN ACCORDANCE WITH DC10 M/M 12-13-02; CHECKED FOR LEAKS IN ACCORDANCE WITH DC10 M/M 29-00-00, NO LEAKS NOTED. (A)SDR ARWA20080505Shutoff Valve · faultyNR 1 REVERSER PRESSURE LIGHT CAME ON DURING CRUISE, WENT OUT WHEN THROTTLES RETARDED FOR DESCENT. AS PER TAFI M/M 78-30-00 FOUND OVERPRESSURE INLET SHUTOFF VALVE BAD. REMOVED AND REPLACED VALVE IN ACCORDANCE WITH M/M 78-31-09, CHECK SYSTEMS NORMAL.SDR ARWA20080405Warning Light · false activationDURING TAKEOFF ROLL ENGINE NR 3 REVERSER OPEN (REV OIL) LIGHT ON. ABORTED TAKEOFF, RETURNED TO THE RAMP 78-34-4-3. INSPECTED ENGINE THRUST REVERSER, NO DAMAGE NOTED. DEACTIVATED REVERSER AND LOCKED IN ACCORDANCE WITH MM 78-00-01; ENTERED ON DMI NR 21655 IN SDR ARWA20080401Gcu · malfunctioned24-20-BD 1 BY 3 CHANNEL WILL NOT PARALLEL. RERACKED GCU 1 BY 3; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH MM 24-20-00.SDR ARWA20080303Battery · dischargedON PRE-FLIGHT, FOUND BATTERY VOLTS READS ZERO. REMOVED 02 BATTERY IN ACCORDANCE WITH A/M/M 24-34-01. CHARGED 02 BATTERY IN ACCORDANCE WITH DC-10-A/M/M 24-34-01; REINSTALLED 02 BATTERY IN ACCORDANCE WITH 24-34-01. TEST CHECK OK IN ACCORDANCE WITH A/M/M 24-34SDR ARWA20080101Mechanism · damagedSLAT DISAGREE LIGHT ILLUMINATED WHEN SLATS SELECTED IN POST FLIGHT; INSPECTION FOUND LT INBOARD SLAT DEPLOYED. REMOVED AND REPLACED ASSEMBLY RUN NR 53A, NR 54A, NR 55A, AND NR 56A; NR 55C AND TWO (2) PULLEYS ASSEMBLY ON LT NR 7 AND NR 2 SLAT IN ACCORDANCE WITSDR ARWA20071206O-Ring · leakingLOST HYDRAULIC QUANTITY BELOW 6 GALLONS SYSTEM 3; HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT "ON". REMOVED AND REPLACED "O" RING AT LOWER FITTING OF REVERSIBLE MOTOR PUMP SHUTOFF VALVE NR 1-3 IN ACCORDANCE WITH M/M 29-22-01; OPERATIONAL CHECK AND LEAK CHECKED IN ASDR ARWA20071204Wire · damagedDURING INITIAL TAKEOFF ROLL SPOOLING UP NR 1 ENGINE REVERSER PRESSURE LIGHT CAME ON. TRANSFERRED TO DMI NR 21307, MEL 78-1 CAT "C", INSTALLED PLACED AND DEACTIVATED FAN REVERSER IAW DDG. REPAIRED WIRES AT THRUST REVERSER LOCK SWITCH CAM ASSEMBLY THROTTLE MOSDR ARWA20070704Tire · failedNR 7 TIRE BLEW DURING LANDING AT SEGU. REMOVED AND REPLACED NR 7 MAIN WHEEL ASSEMBLY AND BRAKE ASSEMBLY AS PER M/M 32-41-03 AND 32-43-01; ALSO NR 8 TIRE INSPECTED AND FOUND SERVICEABLE TO BE DISPATCHED IN ACCORDANCE WITH ARROW AIR GMM 5-23-7, SECTION "C".SDR ARWA20070502Tire · failedPOST FLIGHT FOUND NR 5 TIRE SHREDDED AND DAMAGE TO AIRCRAFT AND NR 1 ENGINE. [SUP 06-01-07] REMOVED AND REPLACED NR 6 MAIN WHEEL ASSEMBLY IN ACCORDANCE WITH DC-10 M/M 32-41-01.SDR ARWA20070501Blades · damagedJUST PRIOR TO ROTATION, DURING TAKEOFF ROLL, A/C SUDDENDLY BEGAN TO VIBRATE, AND DURING INITIAL CLIMB VIBRATION WAS DETERMINED TO BE COMING FROM NR 1 ENGINE. ENGINE WAS SHUTDOWN. [SUP 06-01-07] PERFORMED FULL BOROSCOPE INSPECTION AND FOUND COMPRESSOR SECTIOSDR ARWA20061104B-Nut · looseLOSS OF HYDRAULIC FLUID IN SYSTEM NR 3 ACCOMPANIED BY "HYDRAULIC SYSTEM NR 3 ELEVATOR OFF LIGHT". FOUND HORIZONTAL STABILIZER UPPER PRIMARY TRIM CONTROL VALVE PRESSURE LINE B-NUT LOOSE; TIGHTENED PRIMARY TRIM CONTROL VALVE PRESSURE LINE "B" NUT IN ACCORDANCE SDR ARWA20061003Seal · missingLOG PAGE NR 125045. UNABLE TO CONTROL PRESSURE IN NORM, AUT, IN MAN CABIN START CLIMB WITH OUTFLOW VALVE FULLY CLOSED. FOUND SEAL MISSING ON OUT-FLOW BUTTERFLY VALVE; INSTALLED SEAL; ON OPERATIONAL CHECK FOUND NORMAL IAW MM 21-30-00.
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