N474DA, cancelled Aug 21, 2003
Service difficulty reports · 29
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 = 'N474DA' AND deregistration_id = 'N474DA-2003-08-21' 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 = 'N474DA' AND deregistration_id = 'N474DA-2003-08-21' 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 DL72K972733Battery · dischargedFWD LT WING OUTSIDE EMERG LIGHT INOP. REPLACED BATTERY, CKS OK.SDR DL72K972143Hyd Line · leakingAFTER TAKEOFF 'B' SYSTEM HYDRAULIC PRESSURE AND QTY WENT TO ZERO. HYDRAULIC SYSTEM LEAK OR LOSS AND B SYSTEM LEAK OR LOSS FOLLOW UP PROCEDURES ACCOMPLISHED. MAINTENANCE FOUND OUTBOARD B SYSTEM PUMP CASE DRAIN AND PRESSURE LINES CHAFFED AND LEAKING. REPLACEDSDR DL72K971956Skin · corrosionTHE SKIN JUST FWD OF THE BUTT SPLICE AT STA 80 WAS FOUND TO BE CORRODED AND WAS CUT OUT. THE RESULTING CUT OUT MEASURES 4.25 X 3. THIS CUT OUT IS 3 AWAY FROM AN EXISTING EXTERNAL REPAIR AT S-28R WHICH REPAIRS A 5 X 1 CUT OUT. BOTH REPAIRS WILL BE INCLUDED ISDR DL72K971895Skin · crackedA 2 INCH CRACK NR 7 SLAT COVE SKIN ATTACH ANGLE AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72K971894Skin · dentedFOUND DURING B-2 LETTER CHECK, LT ELEV HAS DENT AT L/E FWD OF O/B END OF TAB. INSTALLED DOUBLER PER SRM 55-20-3 FIG 5.SDR DL72K971893Skin · crackedFOUND DURING B-2 LETTER CHECK, SKIN CRACKED AT S-DUCT INLET 12 O'CLOCK POSITION 3.5 IN AFT OF LIP. INSTALLED REPAIR PER M/M 54-30-0 PG 802.SDR DL72K971733Battery Pack · dischargedLT FWD OVRWING EMERG LIGHT INOP. REPLACED BATT AND RACK\M654, OPS CHKS GOOD.SDR DL72K971051Battery · dischargedRIGHT OVERWING EMERGEMCY EXIT SIGNS INOP. REPLACED BATTERY PACK, CHECKS NORMAL.SDR DL72K971050Battery · dischargedR1 EMERGENCY OVHD EXIT LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.SDR DL72K970570Battery Pack · dischargedOVERWING EMERGENCY HATCH LIGHT INOP. REPLACED BATT PACK.SDR DL72K961909Fuel Pump · failedNR 3 ENGINE LOST THRUST SHORTLY AFTER GEAR RETRACTION. THERE WERE NO ACCOMPANYING SOUNDS HEARD IN COCKPIT. ENGINE INSTRUMENTS INDICATED ENGINE FAILURE. NORMAL DESCENT, APPROACH AND LANDING. REPLACED FUEL PUMP, OPS CHECK NORMAL.SDR DL72K961854Battery Pack · dischargedLT OVERWING EMERGENCY EXIT LIGHT SIGNS INOP. REPLACED BATTERY PACK, CKS NORMAL.SDR DL72K961761Window Post · crackedFOUND A CRACK IN THE LT SIDE F-N COCKPIT WINDOW POST. REPAIRED PER S/B 737-53-0086, REV 11 IN ACCORDANCE WITH A.D. 93-05-17 AND 90-06-09.SDR DL72K961728Light · inoperative1L EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY.SDR DL72K961733Angle · crackedA .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UPSTOP PAD IN COVE SKIN ATTACH ANGLE. INSTALLED DOUBLER PER M/M 57-54-0 PG 816.SDR DL72K961717Stiffener · crackedFOUND 1 CRACK IN WING L/E SPAR STIFFENERS OF NR 2 O/B TRACK. REPAIRED PER M/M 57-20-21 PG 813.SDR DL72K961716Bracket · crackedFOUND NR 7 SLAT ACTUATOR CRACKED I/B BRACKET UPPER LOBE. REPAIRED PER ERA 303841-14.SDR DL72K961715Stiffener · crackedFOUND 1.25 INCH CRACKS AT WING L/E SPAR STIFFENERS AFT OF NR 3 SLAT I/B TRACK TWO EACH. REPAIRED BY REPLACING STIFFENERS PER M/M 57-20-21 PG 813.SDR DL72K961714Cove Skin Angle · crackedFOUND .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UP STOP PAD, IN COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0 PG 816.SDR DL72K960962Light · defectiveAFT 3 SECTIONS OF EMERGENCY PATH LIGHTS REMAIN ON WITH SWITCH IN OFF POSITION. FOUND EMERGENCY LIGHT ASSY L622 OVER AFT STAIRS DEFECTIVE. REPLACED-OPS NML.SDR DL72K961608Transverse Beam · crackedCRACKS ON THE LOWER TORQUE BOX AT FS 1263. THE CRACKS ARE ON THE FORWARD RT SIDE TRANSVERSE BEAM AND THE RT VERTICAL WEB. THE RT VERTICAL WEB HAS A 1 INCH CRACK AT THE FUEL LINE CUTOUT. NORMALLY, THE FUEL LINE IS REMOVED AND THE REPAIR DOUBLER (65-17517-31,SDR DL72K954265Skin · corrodedAT LETTER CHECK IN TPA, CORROSION WAS DISCOVERED ON THE UPPER SKIN AT THE S-24R LAP JOINT THAT WARRANTED A 12.5 INCH BY 3 INCH CUT OUT, BETWEEN STA 294.5 AND STA 312 BY MTC. THIS ER/A WILL REPAIR THE DAMAGED AREA PER SRM 53-30-3 FIG 14 DETAIL 4 WITH THE VARIASDR DL72K954264Side Wall · crackedDURING LETTER CHECK AT TPA, TWO .25 CRACKS WERE DISCOVERED IN THE .040 2024-T3 CLAD RIGHT SIDE WALL OF THE NOSE LANDING GEAR WHEEL WELL APPROX STA 277.0. THIS ER/A PROVIDES REPAIR OF CRACK DAMAGE AND INSTALLATION OF A MOD STRAP AT DAMAGE LOCATION, AD 90-06-09SDR DL72K954219Skin · crackedFOUND ON A2 LETTER CK, 1 INCH CRACK AT FASTENER NUMBER 2 ENGINE INLET OUTER SKIN LT SIDE FWD OF SADDLE PANEL. REPAIRED PER MM 54-30-0.SDR DL72K954218Web · crackedFOUND ON A2 LETTER CK, 1 INCH CRACK IN TORQUE BOX WEB LT SIDE FWD END ALONG UPPER ROW OF RIVETS. REPAIRED PER MM 53-11-0.SDR DL72K954217Angle · crackedFOUND ON A2 LETTER CK, .25 INCH CRACK NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0.SDR DL72K954150Battery Pack · dischargedLEFT LOWER AFT BODY FAIRING E-PATH LIGHT INOP. REPLACED BATTERY PACK AT APPROX ROW 23ABC. E-PATH LIGHT CKS NORMAL.SDR DL72K953019Skin · crackedA CRACK IN NR 3 L/E FLAP I/B EDGE, 1 INCH FROM LIP. FOUND DURING A-2 LTR CK TPAMM. REPAIRED PER MM 57-53-0 PG 804.SDR DL72K952948Blkhd Web · crackedSEVERAL CRACKS WERE FOUND IN FS 1183 BULKHEAD WEB AND STIFFENERS AFTER AIRCRAFT FAILED TO PRESSURIZE IN BOS. A 4 INCH LONG L-SHAPED CRACK WAS FOUND IN FS 1183 BLKHD WEB AT LBL 46.9 AND WL 213.67. THE LBL 46.93 VERTICAL STIFFENER HAD MULTIPLE CRACKS WITH MAXI
Back to N474DA, cancelled Aug 21, 2003