N408EA, cancelled Dec 4, 2000

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 = 'N408EA' AND deregistration_id = 'N408EA-2000-12-04'
  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.

SDR TWAA9810801Strainer · cloggedTYS - FLT 599 - THE RIGHT ENGINE OIL STRAINER CLOGGING LIGHT CAME ON. REDUCED POWER TO IDLE AND LIGHT WENT OUT. DECLARED AN EMERGENCY AND MADE UNSCHEDULED LANDING. FOUND SMALL AMOUNT OF METAL AND CARBON IN MAIN OIL SCREEN. INSTALLED NEW FILTER, DRAINED ANDJul 7, 1998 · N408EA · Doug DC951 · Turbine Engine Oil SystemSDR TWAA9712901Wire · shortedSTL - FLT 675 - DURING CRUISE, THE FORWARD LAVATORY SHOCKED A PASSENGER WHEN THE LAVATORY DOOR WAS LOCKED. REPLACED AND RE-ROUTED SHORTED WIRE. OPERATIONAL CHECK NORMAL. (M)Oct 29, 1997 · N408EA · Doug DC951 · Equipment/Furnishings WiringSDR TWAA9711102Turbine · damagedSTL - FLT 266 - DURING CLIMB, NR 1 ENGINE STALLED AND EPR DROPPED FROM 2.17 TO 1.8. FOREIGN OBJECT DAMAGE WAS FOUND AND ENGINE WAS REPLACED. ENGINE TEAR DOWN REVEALED COMPRESSOR DAMAGE WAS MINOR COMPARED TO TURBINE DAMAGE. A SECOND STAGE TURBINE VANE FRETTESep 10, 1997 · N408EA · Doug DC951 · Turbine SectionSDR TWAA9791001Bulkhead 'T' Cap · crackedSTL - PRESSURE BULKHEAD 'T' CAP CRACKED 2.5 INCHES AT STATION 1167 L-14. REPLACED 'T' CAP PER SRM 53-03. (M)Aug 10, 1997 · N408EA · Doug DC951 · Fuselage Main, BulkheadSDR TWAA9719003Battery Pack · dischargedSTL - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED DEPLETED BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL. (M)Feb 8, 1997 · N408EA · Doug DC951 · Emergency LightingSDR TWAA9614102Skin · corrodedSTL - DURING OP-15, FOUND PULLED RIVET HEAD AND SKIN PILLOWED, LONGERONS 29L, 30, AND 29R, STA 670. REPLACED SKIN AND INNER DOUBLER PER SRM 53-04, FIGURE 43, SHEET 4; SRM 51-00, AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. Nov 10, 1996 · N408EA · Doug DC951 · Fuselage Main, Plate/SkinSDR TWAA9614101Longeron · crackedSTL - DURING OP-15, FOUND A ONE INCH CRACK IN RIGHT LAV, UPPER FLANGE OF LONGERON 17R, STA 1151. REPLACED LONGERON PER MDC DRAWING C03607 AND SRM'S 51-30-2, 51-30-5, AND 51-10-3. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)Nov 7, 1996 · N408EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR TWAA9613508Skin · tornSTL - DURING OP-15, FOUND SKIN TORN AT FORWARD LOWER CORNER OF SERVICE DOOR OPENING. REPAIRED PER ARA 10588 AND SRO 9530172. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)Nov 2, 1996 · N408EA · Doug DC951 · Fuselage Main, Plate/SkinSDR TWAA9613606Floor Beam · wornSTL - DURING OP-15, FOUND WORN SPOT ON FLOOR BEAM APPROXIMATELY FOUR INCHES LEFT OF CENTERLINE, STATION 370. REPAIRED FLOOR BEAM PER SRM 53-05, PAGE 31, FIGURE 20A. (M)Nov 1, 1996 · N408EA · Doug DC951 · Fuselage Main, Floor BeamSDR TWAA9613507Bulkhead · crackedSTL - DURING OP-15, FOUND A FOUR INCH CRACK AT BOTTOM OUTBOARD CORNER OF FORWARD BULKHEAD OF RIGHT LAV, STA 1136. REPAIRED PER SRM 53-03, FIGURE 21, SHEETS 1 AND 2. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)Nov 1, 1996 · N408EA · Doug DC951 · Fuselage Main, BulkheadSDR TWAA9613506Floor Beam · wornSTL - DURING OP-15, FOUND WORN SPOT ON FLOOR BEAM APPROXIMATELY FOUR INCHES LEFT OF CENTERLINE, STA 370. REPAIRED FLOOR BEAM PER SRM 53-05, PAGE 31, FIGURE 20A. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)Nov 1, 1996 · N408EA · Doug DC951 · Fuselage Main, Floor BeamSDR TWAA9613505Seat Track · corrodedSTL - DURING OP-15, FOUND CORROSION ON INBOARD RT SEAT TRACK, FORWARD OF AFT END. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES.Oct 31, 1996 · N408EA · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9613504Skin · crackedSTL - DURING OP-15, FOUND NOSE SKIN CRACKED ABOVE STRAKE, RIGHT SIDE. REPAIRED PER SRM 53-04, FIGURE 38, AND ARA 10575. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)Oct 23, 1996 · N408EA · Doug DC951 · Fuselage Main, Plate/SkinSDR TWAA9613503Skin · crackedSTL - DURING OP-15, FOUND FUSELAGE NOSE SKIN CRACKED ABOVE STRAKES, LEFT SIDE. INSTALLED REPAIR DOUBLER PER ARA 10574. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)Oct 20, 1996 · N408EA · Doug DC951 · Fuselage Main, Plate/SkinSDR 96ZZZM55Shrader Vlv · failedJFK - FLT NR 227 - AFTER TAKEOFF, THE NOSE LANDING GEAR UNSAFE LIGHT CAME ON. RETURNED TO JFK. NOSE STRUT FLAT. CHANGED SHRADER VALVE, TWA 32-5315 MFG MS28778-7. SERVICED NOSE STRUT WITH HYDRAULIC FLUID AND DRY NITROGEN. LEAK CHECK OK.Dec 26, 1995 · N408EA · Doug DC951 · Nose/Tail Landing Gear Strut/AxleSDR 95ZZZX6290Eel Battery Pack · dischargedSTL - FLT 290 - DURING PRE-FLIGHT, ESCAPE PATH LIGHTING STRIP FROM SEAT ROW 6 TO ROW 23, REMAINED ILLUMINATED WITH LIGHT SWITCH IN THE ARMED POSITION. REPLACED BATTERY PACK, MFG PN 5822-2. ESCAPE PATH LIGHTING SYSTEM THEN CHECKED NORMAL. CHECK C-7-8-95 - STOct 11, 1995 · N408EA · Doug DC951 · Emergency Lighting
Back to N408EA, cancelled Dec 4, 2000