N651TW
Service difficulty reports not matched to an aircraft · 30
They name N651TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N651TW' AND registry_match IS NULL 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 = 'N651TW' AND registry_match IS NULL 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 TWAA0019007Skin · dentedDURING CHECK-C MAINT ON LT WING A DENT TO NUMBER 2 SLAT WAS FILLED WITH BONDO. INSTALLED DOUBLER PER SRM 57-43-02 AND SRM 51-70-10. PRIMED AND PAINTED AS REQUIRED.SDR TWAA0019006Doubler · delaminatedDURING CHECK-C MAINT THE RT WING OTBD FLAP LOWER SURFACE REPAIR STILL HAD DELAMINATION ON INBD SIDE, 25 IN BY 12 IN REPAIR ON LOWER INBD CORNER. INSTALLED A 6 1/2 IN DIAMETER HOT BOND REPAIR PER SRM 51-70-07.SDR TWAA0019005Doubler · delaminatedDURING CHECK-C MAINT THE RIGHT WING OTBD FLAP LOWER SURFACE REPAIR STILL HAD DELAMINATION OF THE FIRST 14 IN BY 10 IN REPAIR ON OTBD SIDE. INSTALLED 250 DEGREE HOT BOND PER SRM 57-53-01, PAGE 20 FIG 201.SDR TWAA0019004Doubler · delaminatedDURING CHECK-C MAINT THE RT WING FLAP LOWER SURFACE, SECOND REPAIR INBD OF OTBD FLAP FLAIRING DELAMINATED. REMOVED 2 IN BY 4 IN SKIN AND 3 IN BY 6 IN OF DELAMINATED SKIN. DRESSED AREA AND INSTALLED A 3 IN BY 6 IN AND 5 IN BY 8 IN OVERLAY 250 DEGREE HOT BOND RSDR TWAA0019003Skin · delaminatedDURING CHECK-C MAINT THE RT WING OTBD FLAP LOWER SURFACE WAS DELAMINATED OTBD OF OTBD FAIRING. INSTALLED 6 IN BY 14 IN AND 5 IN DIAMETER OVERLAY HOT BOND REPAIR 250 DEGREE PER SRM 51-70-07.SDR TWAA0019002Doubler · damagedDURING CHECK-C MAINT THE INBD ELEVATOR PREVIOUS REPAIR HAD 2 AREAS OF DISTRESS. INSTALLED 200 DEGREE WET LAY 1 1/2 IN BY 6 IN PER SRM 55-20-01, PAGE 202 FIG 201.SDR TWAA0019001Skin · dentedDURING CHECK-C MAINT THE LOWER SURFACE OF THE RT HORIZONTAL STAB HAD DENT APPROX. 1.5 IN BY 1.5 IN BY 0.080 DEEP, SIX FEET OTBD FROM FUSELAGE. INSTALLED 5 IN DIA METAL TO METAL BOND DOUBLER PER SRM 51-70-10, PAGE 1 AND PAGE 30, FIG 3. PRIMED AND PAINTED.SDR TWAA0018907Skin · delaminatedDURING CHECK-C MAINT ON THE LT WING THE INBD FLAP TOP INBD AND 1 FOOT FROM INBD END, HAD 3/4 INCH DELAMINATION 6 IN FROM T.E. INSTALLED A 6 IN DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10.SDR TWAA0018908Skin · dentedDURING CHECK-C MAINT TOP OF RT WING INBD T/E FLAP SURFACE STRUCTURE HAD A DENT OF APPROX 1.75 IN LONG AND 1 INCH WIDE BY 1/16 IN DEEP. REPAIRED WITH METAL TO METAL HOT BOND PER SRM.SDR TWAA0017602Lamp · shortedTHE EGRESS LIGHTS WERE INOPERATIVE ON THE LT SIDE OF FIRST CLASS. A LAMP HAD SHORTED AND CAUSED THE POWER SUPPLY TO DISCHARGE. REPLACED THE LAMP AND POWER SUPPLY, (P/N 5822-43). CHECK-C 8-22-00.SDR TWAA0016002Power Supply · wornTHE EGRESS LIGHTS IN FIRST CLASS ON LT SIDE OF CABIN WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-22-00 LAX.SDR TWAA0015604Power Supply · inoperativeTHE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-22-00 LAX.SDR TWAA0013003Skin · delaminatedDURING CHECK-C MAINT ON THE RT WING LEADING EDGE THE NUMBER 10 SLAT HAD DELAMINATION ON TOP SIDE OF THE TRAILING EDGE WEDGE, SEVENTEEN INCHES FROM THE O/B END OF THE SLAT. INSTALLED METAL TO METAL HOT BOND 12 INCHES BY 27 INCHES, ON OUTER SKIN AND 6 INCHES BYSDR TWAA0007709Skin · delaminatedDURING CHECK-C MAINT, NUMBER 1 SLAT WAS DELAMINATED. REMOVED DELAMINATION, SKIN AND MOISTURE. INSTALLED FILLER AND 7 INCH BY 14 INCH DOUBLER METAL TO METAL HOT BOND PER SRM 51-70-10 AND SEALED EDGE.SDR TWAA0002415Skin · delaminatedDURING CHECK-C MAINT THE RT WING O/B FLAP, 5 FEET I/B OF O/B CANOE AND 6 INCHES FWD OF TE FLAP, AREA 3 IN BY 3 IN DELAMINATED. APPLIED CONDUCTIVE COATING AND PRIMED PER SRM 51-24-02. PAINTED PER SRM 51-24-00. APPLIED 7 IN BY 5 IN PATCH PER SRM 51-70-05. RESDR TWAA0002506Skin · delaminatedDURING CHECK-C MAINT, THE RT WING O/B FLAP, 3 FEET I/B OF O/B CANOE AND 5 INCHES FROM T/E HAD A 5 INCH DIAMETER AREA DELAMINATED. INSTALLED A 9 INCH BY 4.5 INCH HOT BOND REPAIR PER SRM 51-70-07. PRIMED AND PAINTED PER SRM 51-10-00.SDR TWAA0002505Skin · delaminatedDURING CHECK-C MAINT, THE RT WING O/B FLAP, 12 FT I/B OF O/B CANOE, 6 INCHES FWD OF THE T/E HAD DELAMINATION IN TWO AREAS THAT WERE ONE INCH IN DIAMETER. INSTALLED A 9 INCH BY 9 INCH HOT BOND REPAIR PER SRM 51-70-07. APPLIED PRIMER AND PAINT PER SRM 51-10-00SDR TWAA0002504Skin · delaminatedDURING CHECK-C MAINT, THE RT WING O/B FLAP, 10 INCHES FROM O/B END AND 2 INCHES FROM TE BOTTOM OF FLAP, THE FLAP HAD DELAMINATION APPROXIMATELY 3 IN BY 2 INCHES IN DIAMETER. INSTALLED 8 INCH BY 9 INCH 200 DEGREE WET LAYUP REPAIR PER SRM 51-70-17.SDR TWAA0002503Skin · delaminatedDURING CHECK-C MAINT, THE RT WING O/B FLAP HAD DELAMINATION BOTTOM SIDE 3 INCHES I/B OF O/B CANOE AND 6 INCHES FWD OF THE TE A 3 INCH BY 3 INCH AREA. INSTALLED A 9.5 IN BY 3.5 IN HOT BOND REPAIR PER SRM 51-70-07. PRIMED AND PAINTED PER SRM 51-10-00.SDR TWAA0002502Skin · delaminatedDURING CHECK-C MAINT, THE LEFT WING NUMBER 1 LE SLAT ROUND PATCH TOP OF SLAT AT CENTER, 5 INCH DIAMETER WAS DELAMINATING. INSTALLED HOT BOND REPAIR WITH FILLER SKIN 2 INCHES IN DIAMETER AND OVERLAY METAL DOUBLER TO 5 INCH DIAMETER PER SRM 51-70-10.SDR TWAA0001901Charger · failedTHE RT SIDE AND LT SIDE NUMBER 4 CABIN DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE CHARGER/POWER SUPPLY. CHECK-C 10-23-99 MCI.SDR TWAA9908702Battery Pack · dischargedTHE EGRESS LIGHT AT ROWS 11 TO 16 ON RT SIDE STAYED ON. REPLACED THE BATTERY PACK AND CLEANED MOISTURE FROM THE LIGHT STRIP. CHECK-C 4-7-99 LAX.SDR TWAA9908704Light · malfunctionedTHE CABIN EGRESS LIGHTS AT ROWS 11 TO16 ON RT SIDE STAYED ON ALL THE TIME. SYSTEM OPERATION CHECKED NORMAL. UNABLE TO DUPLICATE THE PROBLEM. CHECK-C 4-7-99 LAX.SDR TWAA9908502Battery Pack · dischargedTHE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 10 TO 15. REPLACED THE BATTERY PACK. CHECK-C 4-7-99 LAX.SDR TWAA9816201Connector · looseFOUND EGRESS LIGHT STRIP INOPERATIVE ON RT SIDE BY CABIN SEATS 19-8 TO 22-8. SECURED LOOSE LIGHT STRIP CONN AT SEAT 22-8. CHECK-C 9-23-98 LAX.SDR TWAA9805402Battery Pack · dischargedJFK - DURING MAINTENANCE CHECK OF THE AIRCRAFT, THE EGRESS LIGHTS WERE FOUND FLASHING FROM ROW 30 TO ROW 35 AFT RT SIDE OF CABIN. REPLACED BATTERY PACK. CHECK-C 3-27-98 LAX. (X)SDR TWAA9703003Pressure Switch · failedLGW - DURING CRUISE, BOTH FORWARD AND AFT FUEL PUMP LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED BOTH FORWARD AND AFT FUEL PRESSURE SWITCHES, MFG P/N 7G110-3. OPERATIONAL CHECK NORMAL. (M)SDR 96ZZZM1040Oven · dirtyJFK - DURING CRUISE E6 OVEN EMITTED SMOKE. TURNED OFF OVEN. FOUND DEBRIS IN OVEN. REPLACED OVEN, MFG P/N 8201-11-0000. OVEN OPERATION THEN CHECKED NORMAL.SDR 96ZZZM660Power Supply · inoperativeLAX - FLT NR 15 - DURING CRUISE LEFT AISLE EGRESS LIGHT AT SEAT ROWS 30 TO 35 AND L3 DOOR, ILLUMINATED. CYCLED SWITCH AND BACK TO ARMED. FOUND POWER SUPPLY, MFG P/N 5822-43, FAULTY. REPLACED POWER SUPPLY AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. (MSDR 96ZZZX640Floor Beam · corrodedMCI - DURING OP-16, FOUND CORROSION ON FLOOR BEAM CAP, STA 1518, RBL 18. REMOVED CORROSION AND REPAIRED PER SRM 53-00-51. AIRCRAFT TOTAL TIME: 38,181 HOURS; 13,720 CYCLES.
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