N687FE
Service difficulty reports · 126
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 = 'N687FE' AND registry_match = 'registration' 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 = 'N687FE' AND registry_match = 'registration' 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 FDEA201510143195Floor Panel · crackedMAIN DECK FLOOR PANEL 251PH CRACKED. FLOOR PANEL 251PH FABRICATED ON T15 1165777 IAW SRZ 25-005 REV L. CLASSIFIED AS A MAJOR CAT A REPAIR.SDR FDEA201510143194Floor Panel · crackedMAIN DECK FLOOR PANEL 252WH CRACKED, FLOOR PANEL 252WH FABRICATED ON T15 1165619 IAW SRZ 25-005 REV L. CLASSIFIED AS A MAJOR CAT A REPAIR.SDR FDEA201510143191Floor Panel · crackedMAIN DECK FLOOR PANEL 251YG CRACKED. FLOOR PANEL 251YG FABRICATED ON T15 1165772 IAW SRZ 25-005 REV L. CLASSIFIED AS A MAJOR CAT A REPAIR.SDR FDEA201510143190Floor Panel · crackedMAIN DECK FLOOR PANEL 251VF CRACKED. FLOOR PANEL 251VF FABRICATED ON T15 1165779 IAW SRZ 25-005 REV L. CLASSIFIED AS A MAJOR CAT A REPAIR.SDR FDEA201510133181Floor Support · bentTWO BENT FLOOR SUPPORTS AT FRAME 48 & 49, BETWEEN SEAT TRACK Y0 & -Y450. FABRICATED 2 EACH CROSS BEAMS ON T15 1166549 IAW SRM 53-15-15. R & R 2 EACH CROSS BEAMS IAW SRM 51-40-21 & 51-40-44.SDR FDEA201510093152Seat Track · gougedMAIN DECK SEAT TRACK Y 1456, BETWEEN FRAME 59 & 67 HAS NUMEROUS GOUGES. R & R SEAT TRACK Y 1456, FRAME 59 TO 67 IAW SRM 53-10-16 FIG 201. REPAIR CLASSIFIED AS A CATEGORY -A- MAJOR REPAIR.SDR FDEA201510083125Seat Track · gougedMAIN DECK SEAT TRACK Y 1456, BETWEEN FRAME 57 & 57.1, HAS 2 EACH GOUGES. R & R DAMAGED SEAT TRACK IAW SRM 53-10-16-201.SDR FDEA201510083124Dummy Rail · wornMAIN CABIN AFT NR 5 LT DUMMY TRACK EXCEEDS GAP VALUE OF .0157. REMOVED NR 5 LT DUMMY SEAT TRACK IAW SRM 51-40-21, FABRICATED INSERT ON T15 1165653 IAW SRM 53-15-16. INSTALLED NEW INSERT IAW SRM 53-15-16. INSTALLED DUMMY SEAT TRACK IAW SRM 51-40-21.SDR FDEA201510083123Dummy Rail · wornMAIN CABIN AFT NR 5 LT DUMMY TRACK EXCEEDS GAP VALUE OF .0157. REMOVED NR 5 LT DUMMY SEAT TRACK IAW SRM 51-40-21. FABRICATED INSERT ON T15 1165653 IAW SRM 53-15-16. INSTALLED NEW INSERT IAW SRM 53-15-16. INSTALLED DUMMY SEAT TRACK IAW SRM 51-40-21.SDR FDEA201510073113Mount · corrodedNUMBER 1 PYLON FWD MOUNT, OTBD AFT BOLT HOLE IS CORRODED. FINAL REAMED HOLE TO DIAMETER 0.0997" IAW SRM 54-51-81 FIG 202 FOR BUSING REPAIR, NO CORROSION NOTED. HFEC HOLE IAW NTM 51-60-00, NO CRACK INDICATION OR CORROSION NOTED. CAD PLATED FWD MOUNT, OTBD AFSDR FDEA201510073112Shear Plate · crackedMAIN CABIN DECK HAS A 1.5 INCH CRACK IN SHEAR TIE AFT FRAME 79, STRINGER 26L. REMOVED SHEAR PLATE IAW SRM 51-40-21. LOCATED & DRILLED HOLES IN NEW SHEAR PLATE IAW SRM 51-40-44, PN A5398111320051. INSTALLED NEW SHEAR PLATE IAW SRM 51-40-21. APPLIED TOP COATSDR FDEA201510073111Shear Web · crackedMAIN CABIN DECK HAS 1.4 INCH CRACK IN SHEAR WEB AFT OF FRAME 79, STRINGER 26R. REWORKED & REPLACED SHEAR PLATE PN A5398111320151, BATCH 2855490 IAW SRM 51-40-21 & SRM 51-40-44.SDR FDEA201510073110Shear Web · crackedMAIN CARGO DECK HAS 1.4 INCH CRACK IN SHEAR WEB AFT OF FRAME 79, STRINGER 26R. REWORKED & REPLACED SHEAR PLATE IAW SRM 51-40-21 & SRM 51-40-44.SDR FDEA201506171839Rib · corrodedRIGHT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0318222 WINGS BASIC WING STRUCTURE CORROSION REPAIR OF RIB 5 FWD LUG RT.SDR FDEA201506171838Rib · corrodedLEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0318219 WINGS BASIC WING STRUCTURE. CORROSION REPAIR OF RIB 5 FWD LUG LT.SDR FDEA201310152507Skin · dentedDENT IN LT INNER FLAP BOTTOM SKIN . REPAIRED IAW SRM 57-50-00 PB 201, FIG 205, REV 79. REPAIRED AREA REPROTECTED AND TOP COAT APPLIED IAW SRM 51-75-10. REPAIR CAT A , MAJOR. SHT 1 , ITEMS 1-4 FOR DETAIL.SDR FDEA201310102469Skin · damagedSCORE IN LEFT INNER FLAP BOTTOM SKIN. REPAIRED IAW EA6-57-50-T0303127 PT1.SDR FDEA201310102468Skin · gougedBULK CARGO DOOR SURROUND HAS A SMALL NICK AT UPPER AFT CORNER OF SKIN. REPAIRED IAW EA 6-5300-T0303107.SDR FDEA201310092458Frame · damagedFRAME 58 FOUND DAMAGED BETWEEN STRINGERS 14 AND 15 LEFT. REPAIRED IAW SRM 25-58- 22, CAT B.SDR FDEA201106172308Skin · dentedRT WING INBD FLAP LOWER SURFACE BETWEEN RIB 1C AND RIB 3 AT APPROX 25 INCHES FROM FORWARD EDGE FOUND WITH A SMOOTH DENT. TRIMMED OUT AS PER SRM 57-50-00 REV 20, FIG 205. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-50-00 REV 20, FIG 205. REPAIRSDR FDEA201106142230Skin · dentedRT WING INBD FLAP LOWER SURFACE BETWEEN RIB 10A AND RIB 11 AT APPROX 18 INCH FROM AFT EDGE FOUND WITH A SMOOTH DENT. LOWER SKIN RT WING INNER FLAP. TRIMMED OUT AS PER SRM 57-50-00 REV 20, FIG 205. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-50- SDR FDEA201106142229Skin · dentedRT WING INBD FLAP LOWER SURFACE BETWEEN RIB 4 AND RIB 5 AT APPROX 5 INCHES FROM AFT EDGE, FOUND WITH A SMOOTH DENT. LOWER SKIN RT WING INNER FLAP. TRIMMED OUT AS PER SRM 57-50-00 REV 20, FIG 205. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-50-0SDR FDEA201106142227Skin · dentedRT WING INBD FLAP LOWER SURFACE BETWEEN RIB 4 AND RIB 4A AT APPROX 5 INCH FROM AFT EDGE FOUND WITH A SMOOTH DENT, LOWER SKIN RT WING INNER FLAP. TRIMMED OUT AS PER SRM 57-50-00 REV 20, FIG 205. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-50-00 RSDR FDEA201106142226Skin · dentedRT WING INBD FLAP LOWER SURFACE BETWEEN RIB 1C AND RIB 3 AT APPROX 25 INCH FROM FORWARD EDGE, FOUND WITH A SMOOTH DENT.SDR FDEA200902280772Warning Light · illuminatedAFTER TAKEOFF 3000 FT RECEIVED FWD CARGO DOOR OPEN ECAM AND AFTER 5 MIN FWD CARGO SWITCH FAULT. RETURNED TO OMA. ACN RELEASED FOR SERVICE PER MEL/CDL. FWD LWR DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE INOP. FWD LWR OVERWEIGHT LANDING WEIGHT INSP SDR FDEA200812115123Skin · dentedLT WING INBD FLAP BOTTOM SURFACE IS DENTED AT 67 INCH FROM THE INBD EDGE AND 22 INCH FROM THE TRAILING EDGE. DENT WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, PG 120, FIG 105. REMOVED DAMAGE IAW SRM 57-55-00, PG 225, FIG 6. FABBED DOUBLER AND 1 FILLER IA
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