N416EA, cancelled Apr 30, 2013
Service difficulty reports · 16
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 = 'N416EA' AND deregistration_id = 'N416EA-2013-04-30' 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 = 'N416EA' AND deregistration_id = 'N416EA-2013-04-30' 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 TWAA9903207Beam · crackedDURING OP-9, FOUND .5 INCH CRACK IN THE TOP BEAM AFT CORNER OF THE FWD RT SERVICE DOOR. REPAIRED PER THE SRM 52-51.D.SDR TWAA9903206Pressure Panel · crackedDURING CHECK-C, FOUND THE HORIZONTAL PRESSURE PANEL AT STATION 83.5 ON THE RT SIDE TUNNEL AREA HAD A .5 INCH CRACK. STOP DRILLED THE CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER PER THE SRM 53-10-10.5.SDR TWAA9815901Light · shortedFWD SECTION OF FIRST CLASS FLOOR EGRESS LIGHTING INOPERATIVE. REPLACED SHORTED LIGHT STRIP. CHECK-C 12-17-97 STL.SDR TWAA9808001Power Supply · inoperativeSTL - FLT 625 - DURING PREFLIGHT INSPECTION, FOND AFT EGRESS AND AFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK MFG P/N 5822-2, FLEX CABLES MFG P/NS 5853-1 AND 5854-3. (M)SDR TSAA9808001Power Supply · inoperativeSTL - FLT 625 - DURING PRE-FLIGHT INSPECTION, FOUND AFT EGRESS AND AFT OVERWING EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY PACK MFG P/N 5822-2, FLEX CABLES MFG P/N 5853-1 AND P/N 5854-3. OP-15 12-17-97 STL CLOSED. (X)SDR TWAA9803302Power Supply · inoperativeSTL - FLT 651 - EGRESS LIGHTS WERE FOUND INOPERATIVE IN THE AFT SECTION OF FIRST CLASS AND THE FORWARD SECTION OF COACH. REPLACED EMERGENCY LIGHT POWER SUPPLY FOR EGRESS LIGHTS AT ROW 6. (M)SDR TWAA9713102Pump · wornBDL - FLT 290 - DURING CLIMB, THE NR 1 ENGINE, S/N 1705, HYDRAULIC PUMP FAILED DUE TO WEAR. REMOVED AND REPLACED THE HYDRAULIC PUMP MANUFACTURED BY VICKERS. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9712404Connector · dirtySTL - FLT 433 - FIRST SECTION OF COACH EMERGENCY LIGHTS WERE INOPERABLE. CLEANED CONNECTOR AND RECHARGED BATTERIES. CK-C 2-4-97 STL - (X)SDR TWAA9790001Bungee Cyl · brokenSTL - FLT 539 - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT DUE TO A BROKEN BUNGEE CYLINDER. REMOVED AND REPLACED RETRACT BUNGEE CYLINDER, MFG P/N 3914016-6505, MANUFACTURED BY DOUGLAS AIRCRAFT COMPANY. OPERATIONAL CHECK NORMAL. (M)SDR 96ZZZM1460Power Supply · inoperativeSTL - DURING CRUISE, EGRESS LIGHTS ILLUMINATED. CYCLED SWITCH. FOUND BATTERY POWER SUPPLY WEAK, MFG P/N 5822-2. REPLACED BATTERY POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.SDR 96ZZZM1466Lights · moisture contamSTL - DURING CRUISE, EGRESS LIGHTS ILLUMINATED IN AFT END OF CABIN. CYCLED SWITCH TO OFF AND BACK TO ARMED. FOUND MOISTURE IN LIGHT TRACK. CLEANED AND DRIED TRACK. LIGHT OPERATION CHECKED NORMAL.SDR 96ZZZM658Batteries · dischargedSTL - DURING ROUTINE MAINTENACNE CHECK, EXTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE. FOUND BATTERIES, MFG P/N 41B030CF00101, WEAK. REPLACED BATTERIES AND EXTERIOR LIGHT OPERATION CHECKED NORMAL. (M)SDR 96ZZZM51Control Vlv · lack of lubeOKC - FLT NR 265 - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON. CHECKED AND LUBRICATED LANDING GEAR VALVE. OPERATIONAL CHECK NORMAL.SDR 96ZZZM674Contl Valve · lack of lubeFLT NR 430 - OKC - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON. CHECKED AND LUBRICATED LANDING GEAR CONTROL VALVE. OPERATIONAL CHECK NORMAL. (M)SDR 96ZZZX229Angle · crackedSTL - DURING CHECK C, FOUND A .3750 INCH CRACK IN RIGHT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, STA 1292. REPAIRED BY INSTALLLING DOUBLER PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES.SDR 96ZZZX228Angle · crackedSTL - DURING CHECK C, FOUND A 2.50 INCH CRACK AT LEFT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, FS 1292. REPAIRED PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES.
Back to N416EA, cancelled Apr 30, 2013