N391CM

Service difficulty reports · 59

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 = 'N391CM' 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 MK1Y20220429009None · noneTAILCONE ASSY, STA 1943.50 TO STA 1952.00: DURING MAINTENANCE INSPECTION MULTIPLE LIGHTING STRIKES WERE FOUND ON TAILCONE ASSY 148T8301-1 (148T8301-1 7 -2 SKINS). THE DAMAGES WERE BLENDED OUT AS REQUIRED, AND NDT HAS PERFORMED REMAINING MATERIAL THICKNESS AND Apr 29, 2022 · N391CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220429008None · noneL/H WING, OUTBD TRAILING EDGE FLAP (P/N: 113T3100-95G, S/N: 000251): DURING MAINTENANCE INSPECTION AT IAI, AN UNDOCUMENTED REPAIR WITH LIGHT CORROSION WAS FOUND ON THE LOWER SKIN PANEL OF THE FLAP AT APPROXIMATELY OTEF 300.88. AFTER THE REPAIR WAS DIMANTLED, AApr 29, 2022 · N391CM · Boeing 767323 · Wing StructureSDR MK1Y20220429007None · noneFUSELAGE FRAME, STA 1461, STR-4R – STR-5R: DURING MAINTENANCE INSPECTION AT IAI, CRACKS WERE FOUND AT DATUM LOCATION. SEE RFTA 02815-0223. THE DAMAGE WAS REMOVED PER J/C MF02815R0223-01 INSTRUCTIONS. THE CUTOUT IS ABOVE 1.99X0.73 INCH.Apr 29, 2022 · N391CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220429006None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, RBL 28.33, STR-U10: DURING MAINTENANCE INSPECTION, CORROSION DAMAGE WAS FOUND AT DATUM LOCATION AS MENTIONED ABOVE. THE CORROSION WAS REMOVED AND REMAINING MATERIAL THICKNESS MEASUREMENT WAS PERFORMED.SEE RFTAApr 29, 2022 · N391CM · Boeing 767323 · Empennage StructureSDR MK1Y20220429005None · noneENGINE # 1 LH CORE COWL HAT FRAME NAC STA 303.75, MID LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, A 1.2 INCH CRACK WAS FOUND ON THE ENG # 1 L/H CORE COWL AFT HAT FRAME P/N 224-2318. THE AFT HAT FRAME FALLS UNDER ZONE CC2 AS PER TABLE 101 B767-300 SRMApr 29, 2022 · N391CM · Boeing 767323 · Engine Cowling SystemSDR MK1Y20220429004None · noneEXTERNAL FUSELAGE SKIN, SECTION 41, STA 168, BELOW STR-21R; 141T3211: DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLENApr 29, 2022 · N391CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220429003None · noneSTA 132.5 – STA 172.5, ABOVE STR-21L: DURING MAINTENANCE INSPECTION AT IAI, MULTIPLE EXISTING UNDOCUMENTED BLEND OUTS WERE FOUND ON THE EXTERNAL FUSELAGE SKIN. ALSO, A GOUGE WAS FOUND ON THE EDGE OF THE DATUM SKIN, STA 132.5.Apr 29, 2022 · N391CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220429002None · noneEXTERNAL FUSELAGE SKIN, SECTION 46, STA 1485, STR-37R; 146T3240: DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND ON THE EXTERNAL FUSELAGE SKINS AT STA 1485, STR-37R. THE AFFECTED FASTENER IN THE BLEND OUT AREA WAS REMOVED. AFTER INSPECTIApr 29, 2022 · N391CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220429001None · noneEXTERNAL FUSELAGE SKIN - STA 1261.5, STR 28R-STR 29R:DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND , COMMON TO THE FASTENER, THAT IS NOT ALLOWED PER B767-300 SRM 53-00-01, AD1.Apr 29, 2022 · N391CM · Boeing 767323 · Fuselage Structure (General)
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