N111NG

Service difficulty reports · 60

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 = 'N111NG' 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.

SDR DALA2022051003267Waste Box · corrodedAFT WASTE BOX, INTERIOR, FORWARD OUTBOARD CORNER IS CORRODED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 034-0001:5327-01014-01/002 00188 REPAIRED PER ER/A 599003-14AD PRI REV. 0, REV. 1, REV. 2, REV. 3, AND COMPLIED May 10, 2022 · N111NG · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022051003266Waste Box · corrodedAFT WASTE BOX, EXTERIOR, FORWARD OUTBOARD CORNER IS CORRODED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 034-0001:5327-01014-01/001 00187 REPAIRED PER ER/A 599003-14AD PRI REV. 0, REV. 1, REV. 2, REV. 3, AND COMPLIED May 10, 2022 · N111NG · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022051203305Nut Plate · crackedLH HORIZONTAL STABILIZER: #3 ELEVATOR HINGE CRACKED AT LOWER NUTPLATE ROW AND CHUNK MISSING. -M. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0257:2090-2039-LH/ 004 00023 SUMMARY - 532877 - LARSON, THOMAS J. - 05/07/2022 15: 44 COMPLETE: COMPLIED WITH ER/A 59May 8, 2022 · N111NG · Airbus BD5001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022051203306Hinge · crackedLH HORIZONTAL STABILIZER: # 2 ELEVATOR HINGE CRACKED AT LOWER NUT PLATE ROW. -M. COMPLIED WITH PRI 598945-14 REV O, PRI 598945-14 REV 1, PRI 598945 REV 2 AND FINAL ER/A 598945 REV ORIGINAL. SEE NR 17. ASSOCIATED ER/A 14-598945 ADDED FOR AC 8111. (LP#2227042)May 7, 2022 · N111NG · Airbus BD5001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022051203304None · noneERA 599003-14AD SECTION I ACCOMPLISHED DURING CCK IN MSP. FOLLOW ON ACTION IS REQUIRED. ERA 599003-14AD SECTION I REPAIR IS LIMITED TO 8500 FH. FURTHER ANALYSIS AND ERA REVISION IS REQUIRED FOR AIRCRAFT TO FLY BEYOND THIS LIMIT., ASSOCIATED AA 5327-01014 ADDEDMay 6, 2022 · N111NG · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022051003269None · noneERA 599003-14ADSECTION I ACCOMPLISHED DURING CCK I NMSP. FOLLOW ON ACTION IS REQUIRED. ERA 599003-14AD SECTION III EVERY 1700 FH AFTER SECITON I UNTIL SECITON IV. ASSOCIATED AA 5327-01014 ADDED FOR AC 8111. (LP# 2225854)May 6, 2022 · N111NG · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022051003268None · noneERA 599003-14AD SECTION I ACCOMPLISHED IN MSP DURING CCK. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 599003-14 SECTION II EVERY 850 FH AFTER SECTION I UNTIL SECTION IV ASSOCIATED AA 5327-01014 ADDED FOR AC 8111 ASSOCIATED ER/A 00-599003 ADDED FOR AC 8111. (LMay 6, 2022 · N111NG · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022011600295None · noneER/A 590172-14 HAS BEEN UPDATED TO REV. A TO INCORPORATE REVISED REO APPROVAL. THE NEW APPROVAL INTRODUCES ADDTIONAL TIMECONTROL AND INSPECTION REQUIREMENTS. FOLLOW ON ACTION IS REQUIRED. ER/A 590172-14 REV. A SECTION III IS TO BE ACCOMPLISHED WITHIN 3 0000FC Jan 11, 2022 · N111NG · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2020072762645Flex Coupling · kinkedON TAKEOFF AROUND 300 AGL RECEIVED EQIP BAY SMOKE FAIL CAUTION MESSAGES. COMPLETED CHECKLIST, RETURNED TO DEPARTURE. FOUND FAULT CODE 2613F0002, EE BAY LOW AIR FLOW SMOKE DET 1&2 ( A238 & A239) DETECT LOW AIR FLOW CH A & CH B. PERFORMED EFIM SOLUTION 2-41919,Jul 24, 2020 · N111NG · Airbus BD5001A10 · Fire Protection System WiringSDR DALA2019070504122Slide · faultedDURING TAXI IN HAD WING SLIDE CAUTION MSG AND INFO MSG 52 WING SLIDE - R OWE SLIDE INOP. MSG CLEARED AFTER 5 MINUTES. REMOVED AND REPLACED RT OVERWING SIDE PER CARD 2563-4005 C/W REQUIRED RII INSPECTION ON RT OVER WING SLIDE PER CARD 2563 -4005 VERIFIED SAFTY Jul 3, 2019 · N111NG · Airbus BD5001A10 · Escape Slide
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