N144DA, cancelled Jan 24, 2020
Service difficulty reports · 54
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 = 'N144DA' AND deregistration_id = 'N144DA-2020-01-24' 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.
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 = 'N144DA' AND deregistration_id = 'N144DA-2020-01-24' 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 DALA2017021001128Connector · detachedEMERGENCY LIGHTS AT 5FE ARE INOPERATIVE. MAINTENANCE RECONNECTED THE ELECTRICAL CONNECTOR. SYSTEM OPERATION IS NORMAL.SDR DALA2016122810105Skin · delaminatedDURING WALK AROUND INSPECTION, FOUND AREA OF DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL LOCATED AT FSS 220 AND BL 1750. DELAMINATION IS OUT OF SRM LIMITS. REPAIRED IAW SRM 51-70-10, REP 4SDR DALA2016112309132Seat Track · brokenSEAT TRACK BROKEN. CUT OUT DAMAGED SECTION OF SEAT TRACK & FABRICATED A REPAIR IAW SRM 53-00-52 REPAIR 1 FIG.201 AND INSTALLED THE REPAIR IAW SRM 53-00-52, REPAIR 1, FIG 201.SDR DALA2015091205677Structure · crackedLEFT HORIZONTAL INNER CHORD CRACKED OUT OF FASTENER, BS 1809, REPAIRED IAW SRM 53-80-08.SDR DALA13056451404Wire · disconnectedEMERGENCY LIGHTS AT SEAT 5FE ARE INOPERATIVE. MX FOUND A WIRE DISCONNECTED. CONNECTED WIRE SYS OPS NORMAL.SDR DALA13049581404Skin · crackedNR 2 PYLON FWD UPPER PYLON DRAIN HOLE CRACKED. REPAIRED IAW ERA 519157-14.SDR DALA13021221404Squib · inoperativeDURING CHANGE OF LT WING SLIDE BOTTLE, FOUND RT WING SPOILER BLOW DOWN SQUIB BAD. REPLACED RT WING SPOILER OVERRIDE ACTUATOR SQUIB.SDR DALA1230061404Frame · crackedFS 903 LT BETWEEN STR 20L AND STR 21L FRAME CHORD CRACKED. CHORD CRACK REPAIR ACCOMPLISHED AS PER ERA 501545-14AD REV ORG SECTION 1.SDR DALA1230051404Frame · crackedFS 903 RT BETWEEN STR 20R AND STR 21L INNER CHORD CRACKED. TRIMMED OUT AND REPAIRED AS PER ERA 501546-14AD REV ORG SECTION 1.SDR DALA1230041404Spar · crackedNR 1 PYLON FWD UPPER SPAR WEB LT DRAIN HOLE FOUND CRACKED. REPAIRED AS PER ERA 502699-14AD, REV ORG NRC 52915.SDR DALA1229051404Failsafe · corrodedLT STA 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE CORRODED. REPAIRED AS PER ERA 501535-14AD, REV ORG.SDR DALA1229041404Tee Fitting · corrodedRIGHT BS 955 REAR SPAR BULKHEAD FITTING FOUND CORRODED AT TEE FITTING. REPLACED TEE FITTING AS PER ERA 501536-14AD, REV ORG.SDR DALA1229031404Tee Fitting · crackedLEFT BS 955 REAR SPAR BULKHEAD FITTING CRACKED AT TEE FITTING. TEE FITTING REPLACED AS PER ERA 501535-14AD, ORG.SDR DALA1229021404Failsafe · crackedRIGHT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP CRACKED, AREA TRIMMED OUT AND REPAIRED AS PER ERA 501536-14AD REV. ORGSDR DALA1224811404Fairing · delaminatedRT I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED IN 3 PLACES. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-05 PAR 5A(1) FIG 5.SDR DALA1223701404Tee Fitting · crackedFS 955 LT REAR SPAR BLKHD "T" FITTING AT FAILSAFE IS CRACKED AT A HOLE, WORKING FROM A PRI.SDR DALA1223681404Tee Fitting · corrodedFS 955 RT REAR SPAR BLKHD "T" FITTING HAS A FASTENER HOLE CORRODED, WORKING ON PRI.SDR DALA1223591404Frame · crackedFS 903 LT BETWEEN STR 20L-21L FRAME INNER CHORD IS CRACKED, WORKING FROM PRI.SDR DALA1223581404Frame · crackedFS 903 BETWEEN STR 20R-21R FRAME INNER CHORD IS CRACKED, WORKING FROM PRI.SDR DALA1223571404Fitting · crackedFS 927 AT STR 20R-21R FRAME TO WING CENTER SECTION FITTING IS CRACKED AND BEING REPLACED PER B767-300 SRM 51-10-02 PG 8 PARA 9 AND DWG 100T1410.SDR DALA1223201404Fairing · gougedLT HORIZONTAL STAB L/E FAIRING 332DL IS GOUGED AND REPAIRED PER B767-300 SRM 55-10-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201 SHT 2.SDR DALA1223191404Wedge · delaminatedNR 4 SLAT T/E WEDGE IS DELAMINATED IN 2 PLACES AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202 SHT 1.SDR DALA1223181404Fairing · delaminatedLT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING IS DELAMINATED IN 2 PLACES AND HAS BEEN REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND SRM 51-70-05 PAR 5A(1) FIG 5.SDR DALA1221451404Failsafe · crackedRIGHT FUSELAGE STATION 955 REAR SPAR BULKHEAD FAILSAFE STRAP FASTENER HOLE CRACKED.SDR DALA1221431404Failsafe · crackedLEFT FUSELAGE STATION 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE FOUND CORROSION AND CRACKED.SDR DALA1013110144Wire · brokenFOUND ON PDC/DRC CHECK, EMERGENCY LIGHT IS INOPERATIVE AT THE BASE OF LAVATORY 215. MX REPAIRED A BROKEN WIRE FOUND AT BASE. SYS OPS IS NORMAL. (DL76P101504)SDR DL76P100749Connector · disconnectedEMERGENCY PATH LIGHT AT 3AB IS INOPERATIVE. MX FOUND CONNECTORS DISCONNECTED AND RECONNECTED THEM. SYS OPS IS NORMAL.SDR DL76P100623Control Panel · odorACRID ODOR IN COCKPIT DURING CRUISE AND IN DESCENT LASTING FOR APPROX. 10 SECONDS EACH TIME. FOUND GALLEY CONTROL PANEL AT 1R WITH ACRID ODOR. SUSPECT 5 AMP FREEZER C/B AS SOURCE. (NOT TRIPPED) REPLACED C/B AND OPERATED FOR SEVERAL HOURS WITH NO DISCREPANCIESDR DL76P092019Turbine Blades · damagedNR 2 ENGINE FAILED, OP 5067 BOROSCOPE 2ND STAGE. PERFORMED NR 2 OP 5067 ENG BOROSCOPE. FOUND ONE 2ND STG HPT BLADE DAMAGE. ALSO AP-9 DAMAGE EMP 221084. SEE ITEM 009 FOR ENGINE REPLACEMENT.SDR DL76P091971Indicator · malfunctionedRTB DUE TO INOPERATIVE SPEED FLAG ON ADIS RESET TMC C/BS. FLAGS CLEARED - NO ADC FAULTS. TMC TESTS GOOD. A/T SERVO TESTS GOOD.SDR DL76P090752Starter · inoperativeAPU START 15-20 PSI RT ENG BEGAN TO START W/N2 AT LEAST 8 THEN ROLLED BACK. START VALVE LITE NORMAL. TRIED AIR FROM LT ENG NR N2 OR OIL PRESS. REMOVED AND REPLACED NR 2 ENG STARTER. OPS CKS NML. INSTALLED STARTER BORROWED FROM AIR CANADA AIRLINES MFG P/N 7SDR DL76P090381Generator · faultedAFTER PUSHBACK LT GEN DID NOT AUTOMATICALLY PICK UP THE LOAD. MANUAL RESET BROUGHT GEN ONLINE. DUE TO MULTIPLE EICAS MSGS RE EECS ACFT RETURNED TO GATE. BIT BPCU NO LAST FAULTS NOTED. RAN LT ENG AT GATE WITH NO DISCREPANCIES NOTED. OK FOR SVC.SDR DL76P090292Idg · inoperativeON NR 2 ENG START NR 1 GEN FELL OFF LINE. L ENG EEC C1 STATUS MSG BIT BPCU LEFT ENG FAULT LOW FREQ TRIP. BIT PIMU ON LT ENG HAD NUMEROUS FAULTS DUE TO POWER DROPPING OFF RESET PIMU. PERFORMED TWO ENG RUNS NO MSGS ON EPCS PG OR PIMU. DISC LT IDG DUE TO HISTSDR DL76P090261Gcu · failedLT ENG GENERATOR FAILED ON TAXI OUT DURING X BLEED START. REPLACED LEFT GCU RAN ENG OPS CK OK.SDR DL76P090192Probe · unknownRIGHT ENGINE CONTROL EICAS MESSAGE AFTER ENGINE START. REPLACED P2/T2 PROBE, OPS NORMAL.SDR DL76P091576Transmitter · failedRTB - FLAPS WILL NOT LOWER AND FLAP DISAGREE EICAS MSG. T/S PER FIM 27-51-00 FIG 105. DIRECTED TO FIM 27-51-00 FIG 11, CHECKS OK UP TO STEP 5-SHEET 3 FIG 114C. SUSPECT BYPASS VLV - 318717- FOUND NR 4 FLAP POS XMITTER OUT OF RANGE. ETOPS CATEGORY 'F': ANY SDR DL76P081154Starter · failedNR 1 ENG NO START NO ROTATION, FOUND STARTED AT FAULT. REPLACED STARTER.SDR DL76P080378Hydraulic Line · leakingON LANDING ROLLOUT, AFTER ACTUATING THRUST REVERSERS LOST RT HYDRAULIC QTY. FOUND REVERSER HYDRAULIC LINE WITH HOLE IN IT. PERFORMED TEMP REPAIR PER MM 20-10-09-358-151. CYCLED REVERSER AND ALL HYDRAULIC SYSTEMS SEVERAL TIMES. OPS NORMAL. OLD BAD HYDRAULISDR DL76P071602Indicator · odorCAPTAINS VSI WENT BLANK. DETECTED FAINT ELECTRICAL ODOR. PULLED VSI CIRCUIT BREAKER. ODOR DISSIPATED. REPLACED CAPTS VSI, OPS TESTS GOOD.SDR DL76P071007Loop · unknownPASSING 28000 FT T/O PLUS 15 MIN CLIMB PWR RT DUCT BLEED LIGHT AND EICAS MSG. COMPLETED WITH QRH PROCEDURE RT DUCT BLEED LEAK EXTINGUISHED PASSING 32500 FEET. VISUALLY INSPECTED PNEU DUCTING AND CLAMPS ALONG WITH CHECKING FOR LEAKS FROM RT ENG PYLON TO RT ECSDR DL76P071029Control Module · malfunctionedSPOILERS CAUTION LIGHT ON TAXI OUT. RESET PCA3 FAULT ON 2L SPOILER CONTROL MODULE. OPERATED SPOILERS ALL MODES WITH DIFFERENT POWER SOURCES.SDR DL76P070953Circuit Card · defectiveRIGHT DUCT LEAK LIGHT INFLIGHT CLIMBING THRU FL210. CHECKED ALL DUCTS FROM RT ENGINE TO THE RT ISOL VALVE. REPLACED WHEEL WELL OVHT ECS DUCT LEAK DETECTION SYS CONTROL CARD. RAN ENGINES AT IDLE FOR 30 MINUTES, T/O POWER FOR 10 MINUTES AND 15 MINUTES AT CLIMSDR DL76P060811Fan · odorEQUIPMENT COOLING OVHT LIGHT ON OVERHEAD PANEL ACCOMPANIED BY BURNING SMELL IN COCKPIT. FOUND EICAS MSG FWD EQUIP SUPPLY FAN 1 PULLED AND COLLARD C/B H-18 FWD TO MCO AND PLAC 21-58-03B FWD SUPPLY FAN MOTOR BURNED UP NEEDS NEW FAN ASSY. REMOVED AND REPLACED FWSDR DL76P040974Turbine · damagedON T/O ROLL APPROX 130 KTS CREW EXPERIENCED LOUD BANG AND FLASH FOLLOWED BY YAW TO THE RIGHT. EGT REPORTED OFF SCALE ON RT ENG. PASSENGERS REPORTED SMOKE FROM ENG. BOTH FIRE BOTTLES AND RTO PERFORMED. MTC FOUND METAL IN THE TAILPIPE AND EGT RECORDED AT 729SDR DL76P040882Smoke Detector · malfunctionedMID CABIN SMOKE ALARM WENT OFF ON T/O. F/A NOTIFIED CREW SHORTLY AFTER T/O. THOROUGHLY INSPECTED AIRCRAFT, RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE.SDR DL76P040694Bulb · inoperativeON LAYOVER FOUND EMERGENCY LIGHTS INOPERATIVE AT FWD F/A OVERHEAD AND AFT OVERHEAD AT SEAT 47 C AN E. RELAMPED OPERATION OK.SDR DL76P040250Power Supply · inoperativeEMERGENCY PATH LIGHTS INOP IN FIRST CLASS. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK.SDR DL76P021416Odor · detectedAFTER TAKE OFF, FLT ATTENDANT REPORTED STRANGE FUMES & ODOR IN MIDSECTION GALLEY AREA. LT ENGINE BLEED AND PACK TURNED OFF AND ODOR SUBSIDED & DISSIPATED. BLEED AND PACK LT OFF. REMAINDER OF FLT UNEVENTFUL. INSPECTED INLET EXHAUST - NO VISIBLE OIL - PERF PNSDR DL76P020666Skin · dentedFUSELAGE / SKIN / FS 374 / STRG. 17L / SKIN LAP JOINT : DENT REPAIR THE FUSELAGE SKIN AT FS 374 AT THE STRINGER 17L LAP JOINT WAS DENTED. THE DENT WAS REMOVED WITH A 4.5" X 3.9" CUTOUT IN THE UPPER AND LOWSDR DL76P020536Bolt · shearedON TAXI OUT, GOT L/E ASYMMETRY T/S AND FOUND PROX SENSOR TARGET AT S286 LEFT SLAT NR 5 EXTEND PLATE MISSING AND ATTACH SCREW SHEARED. INSTALLED NEW TARGET AND ATTACHING SCREW. SYSTEM OPS NORMAL.
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