N322NB
Service difficulty reports · 179
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 = 'N322NB' 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 = 'N322NB' 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 DALA12001373122Panel · damagedAFT CARGO SLOPE PANEL 152WG DAMAGED. SLOPING WALL PANEL 152WG WAS FABRICATED IAW DRAWING 3D25-40532. DAMAGED DIM: L=7.0 INCH W=1.5 INCH D=0.09 INCH. RETAIN FOR RECORDS. STRINGER 645112 BFM.SDR DALA12001363122Panel · damagedAFT CARGO SLOPE PANEL 161CF DAMAGED. SLOPING WALL PANEL 161CF WAS FABRICATED IAW DRAWING 3D25-40532. DAMAGED DIM: L=4.9 INCH W=3.0 INCH D=0.10 INCH. RETAIN FOR RECORDS. STRINGER 645112 BFM.SDR DALA12001353122Floor Panel · damagedAFT CARGO FLOOR PANEL 151ZG DAMAGED. FLOOR PANEL 151ZG WAS FABRICATED IAW DRAWING 3D25-40532. DAMAGED DIM: L=1.0' W=2.0" D=0.33". RETAIN FOR RECORDS. STRINGER 645112 BFM.SDR DALA12001343122Floor Panel · damagedAFT CARGO FLOOR PANEL 161NF DAMAGED. FLOOR PANEL 161NF WAS FABRICATED IAW DRAWING 3D25-40532. DAMAGED DIM: L=6.0 INCH W=4.0 INCH D=0.25 INCH. RETAIN FOR RECORDS, STRINGER 645112 BFM.SDR DALA12001333122Floor Support · damagedAFT CARGO FLOOR PANEL 151VG EDGE DAMAGE. FLOOR PANEL 151VG WAS FABRICATED IAW DRAWING 3D25-40532. DAMAGED DIM: L=4.0 INCH W=3.0 INCH D=0.1 INCH. RETAIN FOR RECORDS. STRINGER 645112 BFM.SDR DALA12001303122Blanking Plate · corrodedL1 DOOR AFT BLANKING PLATE CORRODED. RECEIVED NEW BLANKING PLATE. PART TO BE INSTALLED ON WORK CARD 2500-6601. DAMAGED DIM. L=1 INCH W=.5 INCH.SDR DALA12001293122Floor Panel · corrodedFLOOR PANEL 222FF IS CORRODED. RECEIVED NEW FLOOR PANEL 222FF FLOOR PANEL 222FF TO BE INSTALLED ON WORK CARD 2500-6617.SDR DALA12004963122Skin · dentedLEFT SIDE OF FORWARD FUSELAGE FRAMES 23 - 24, STR 21-22L, SKIN DENTED. MEASURED DENT IAW SRM FIG 105 T=.047 INCH D=.080 INCH A=2.5 INCH B=0.125 INCH. FOUND OUT OF LIMITS IAW SRM 53-11-11 DIA 103. CUT OUT DAMAGE L=3.4 INCH W=1.5 INCH IAW SRM 53-11-11 FIG 2SDR DALA12001183122Floor Panel · delaminatedAFT CABIN FLOOR PANEL 262HG IS DELAMINATED, FABRICATED NEW IAW FLOOR PANEL DWG 3D25-40640. DAMAGE DIM. L=2.50 INCH W=2.50 INCH.SDR DALA12001193122Floor Support · corrodedFLOOR SUPPORT BETWEEN FR 64 TO FR 68 Y1292 UPPER FLANGE AND HOLES CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. ORIG MAT. .087 DAMAGE DIM. L=1.0 INCH W=.496 INCH D=.058 INCH. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM SDR DALA12001143122Floor Support · corrodedFLOOR SUPPORT BTW FR64 TO FR66 Y1292 UPPER FLANGE AND HOLES CORRODED. BLENDED AREA IAW SRM 51-74-00 L=2.0 INCH W=1.0 INCH D=.075 INCH. ORIG. .087 INCH OUT OF LIMIT IAW SRM 53-41-15. REMOVED AND INSTALLED NEW FLOOR SUPPORT BEAM IAW SRM 51-42-11.SDR DALA12001133122Blanking Plate · corrodedL2 DOOR AFT BLANKING PLATE CORRODED. RECEIVED NEW BLANKING PLATE. PANEL INSTALLED ON WORKCARD 2500-6602. PANEL EXCEEDS ALLOWABLE OR REPAIRABLE DAMAGE. PANEL CRACKED/BROKEN AT EDGE.SDR DALA12001043122Floor Support · corrodedFLOOR SUPPORT BETWEEN FR 68 TO FR 69 LT Y1291 UPPER FLANGE AND HARD POINTS HOLES CORRODED. BLENDED FLOOR SUPPORT. FOUND OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.SDR DALA12000963122Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BEAM AT FR21 -Y189 HAS CORROSION. BLENDED AREA. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT BEAM.SDR DALA12000953122Sill · corrodedRIGHT AFT FUSELAGE PASSENGER/CREW ENTRANCE LOWER CENTER CORNER UNDER SCUFF PLATE FWD FITTING CORRODED. REMOVED EXFOLIATED CORROSION CENTER SHAPE SILL. LOCATED AND DRILLED NEW SHAPE SILL. TREATED AND PRIMED FASTENERS HOLE ON NEW SHAPE SILL. INSTALLED NEW SHSDR DALA12000943122Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT WEB BEHIND FR12 BETWEEN -Y81 TO -Y1290 HAS CORROSION. REMOVED CORROSION. NO ESTABLISHED LIMITS AVAILABLE. REMOVED AND REPLACED FLOOR SUPPORT.SDR DALA12001013122Shear Plate · crackedAFT UTILITY AREA LT SHEAR PLATE BETWEEN FR 68 - 69 Y1732 CRACKED. REPLACED LT SHEAR PLATE AT Y1732 FR 68 - 69.SDR DALA12000923122Floor Support · corrodedFLOOR SUPPORT AT FR68 -Y765 UPPER FLANGE HAS SURFACE CORROSION. BLENDED AREA. FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT. RECEIVED NEW FLOOR SUPPORT INSTALLED NEW .SDR DALA12000913122Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR64 TO FR66 -Y765 2 HARD POINT HOLES CORRODED. BLENDED AREA. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM IAW A319 SRM 51-42-11. RECEIVED NEW FLOORBEAM. INSTALLED NEW FLOORBEAM.SDR DALA12000813122Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR66 TO FR68 -Y1292 UPPER FLANGES AND HOLES CORRODED. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED (4) SPLICE ON FR66 AND REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED AND DRILLED NEW FLOORSDR DALA12000803122Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR68 TO FR69 -Y1292 UPPER FLANGES AND HOLES CORRODED. BLENDED AREA. FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED AND DRILLED NEW FLOOR SUPPORT. TREATED AND PRIMED HOLES ON NEW FLOOR SUPPSDR DALA12000263122Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT +Y503.2 FR16 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. ORIG MAT. 0.149 DAMAGE DIM. L=1 INCH W=.453 INCH D=.049 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 103. REMOVED FLOOR SUPPORT +Y503.2 IAW SRM 51-42-11, RECEIVESDR DALA12000933122Blanking Plate · corrodedR1 DOOR BLANKING PLATE CORRODED FORWARD. REPLACED BLANKING PANEL PLATE. PANEL INSTALLED. NO ESTABLISHED LIMITS.SDR DALA12001313122Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BEAM AT FR 16 -Y1292 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00 WAS FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 102 DIM: L=1 INCH W=.595 INCH D=.027 INCH. REMOVED AND INSTALLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51SDR DALA12000743122Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT +Y254 FROM FR 12-FR 24 HAS EXFOLIATION CORROSION. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT +Y254 IAW A319 SRM 51-42-11,LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-44-11. TRANSFERRED 1 BRACKET TO NEW SDR DALA12000733122Floorbeam · corrodedFORWARD CABIN FLOORBEAM +Y1292 AT FR 16 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMIT. REMOVED FLOORBEAM IAW SRM 51-42-11. INSTALLED NEW FLOORBEAM.SDR DALA104273122Bleed Air Sys · malfunctionedON CLIMB OUT RECEIVED MESSAGE "AIR ENG 1 BLEED FAULTX" "AIR ENG 2 BLEED FAULTX" AND "CAB PR LO DIFF PRXX" "AIR PACK 1X2 FAULTX" WITH SUBSEQUENT LOSS OF PRESSURIZATION. CREW DECLARED EMERGENCY AND DIVERTED FLIGHT, WHERE LANDING WAS UNEVENTFUL. NR 1 ENGINE FANSDR NWAA082933132Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK AT LT OVERWING EXIT INOP. REPLACED BATTERY POWER SUPPLY UNIT, CHECKS GOOD. (A)SDR 0700473122Battery Pack · no testEPSU FAULT ON EXIT LIGHT SYSTEM TEST. CORRECTED BY REPLACING BOTH LEFT EPSU BATTERIES. CHECKS OK.
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