N328NB
Service difficulty reports · 175
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 = 'N328NB' 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 = 'N328NB' 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 DALA12002153128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT -Y254 HAS CORROSION ABOVE FR 68. REMOVED FLOOR SUPPORT AT -Y254 IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT AT -Y254 IAW SRM 51-42-11. DAMAGE DIM: L=1.4 W=1.1 D=.023.SDR DALA12002143128Panel · delaminatedFORWARD CARGO SLOPE PANEL 131EG DELAMINATED. FABRICATED SLOPE PANEL 131EG DWG 3D25-40532. DAMAGE DIM. L=3.0 INCH W=1.0 INCH.SDR DALA12002133128Floor Support · corrodedFWD MAIN CABIN FLOOR SUPPORT BETWEEN FR16 - FR21 +Y254 HAS CORROSION AT SEVERAL LOCATIONS. BLENDED AREAS IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 107. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED, DRILLED AND TRANSFERRED BRACKESDR DALA12002123128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT -Y465 HAS EXFOLIATION ABOVE FR68. BLENDED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102 L=1.0 INCH W=.5 INCH D=0.055 INCH. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED 4 BRACKETS ON NEWSDR DALA12002113128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT -Y465 HAS CORROSION AROUND HARD POINT MOUNT HOLES BETWEEN FR 65 AND FR 66. BLENDED CORROSION IAW A319 SRM 51-74-00, FOUND OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102 L=2.0 INCH W=1 INCH D=.025 INCH. REMOVED DAMAGED FLOOR SUPPORT IAWSDR DALA12002013128Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FR 16 AND FR 23 -Y1292 HAS CORROSION AT SEVERAL LOCATIONS. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMIT IAW SRM 53-11-14 FIG 105. REMOVED DAMAGE FLOORBEAM IAW SRM 51-42-11. TRANSFERRED 6 BRACKET, 1 HARD PSDR DALA12002003128Sill · corrodedAFT UTILITY R2 DOOR CENTER SEAL SHAPER CORRODED. REMOVED AND REPLACED CENTER SHAPE SILL. NO SRM LIMITS. DAMAGE DIM: L=1.0 INCH W=0.987 INCH D=0.032 INCH.SDR DALA12001903128Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FR 14 AND FR16 +Y1292 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 CHECKED LIMITS L=2.0 INCH W=1.0 INCH D=0.067 OUT OF LIMITS IAW SRM 53-11-14 FIG 105. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.SDR DALA12001863128Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT AT FR16 +Y503.2 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND SRM 51-44-11.SDR DALA12001993128Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT -Y189 AT FR 21 CORRODED. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.SDR DALA12002353128Skin · dentedLOWER FUSELAGE EXTERIOR SKIN BETWEEN FR 21 AND FR 23, STR 24L AND STR 25L HAS DENT. DENT EVALUATED IAW SRM 53-11-11 FIG 104. DENT FOUND TO BE WITHIN LIMITS IAW SRM 53-11-11 TABLE 101 PARA 4B, DIA 102 NOTE 5.SDR DALA12001823128Attach Fitting · corrodedAFT UTILITY L2 DOOR SILL AFT GIRT BAR FITTING ATTACH POINTS 2 FORWARD HOLES HAVE CORROSION. REMOVED CORROSION IAW SRM 51-74-00. DIMENSIONS OF REWORKED AREAS HOLE 1: L=0.8 INCH W=0.3 INCH D=0.040 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101.SDR DALA12001813128Sill · corrodedAFT UTILITY R2 DOOR SILL -Y1732 HAS CORROSION ABOVE FR 68, N/R 260/43. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECKED LIMITS: L= 1.0 INCH W=0.15 INCH D=0.025 INCH ORIG MAT 0.063 INCH. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-14 FIG 101. DOOR SILL TO SDR DALA12001803128Attach Fitting · corrodedAFT UTILITY R2 DOOR SILL AFT GIRT BAR ATTACHMENT AREA 6 HOLES HAVE CORROSION AROUND FASTENER HOLES N/R 260/42. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS: L=0.80 INCH W=0.60 INCH D=0.020 INCH ORIG MAT 0.098 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-SDR DALA12002103128Floor Panel · tornAFT CABIN FLOOR PANEL 251JG OUTER PLY TORN. REMOVED FLOOR PANEL IAW AMM 53-42-12. BONDED AND REPAIRED IAW SRM 53-02-00 PARA 8J FIG 212. INSTALLED FLOOR PANEL IAW AMM 53-42-12.SDR DALA12002093128Floor Panel · tornAFT CABIN FLOOR PANEL 251PF OUTER PLY TORN. REMOVED FLOOR PANEL IAW AMM 53-42-12. BONDED AND REPAIRED IAW SRM 53-02-00 PARA 8.J FIG 212. INSTALLED FLOOR PANEL IAW AMM 53-42-12.SDR DALA12002083128Floor Panel · tornAFT CABIN FLOOR PANEL 251FF OUTER PLY TORN. REMOVED AFT CABIN FLOOR PANEL IAW AMM 53-42-12. BONDED MOISTURE BARRIER FOIL AND CLEANED IAW SRM 53-02-00 PARA 8.J(3) SOLUTION B PG 247 FIG 212. INSTALLED FLOOR PANEL IAW AMM 53-42-12.SDR DALA12002073128Floor Panel · tornAFT CABIN FLOOR PANEL 252GF OUTER PLY TORN. REMOVED AFT CABIN FLOOR PANEL IAW AMM 53-42-12. BONDED MOISTURE BARR FOIL. CLEANED IAW SRM 53-02-00 PARA 8.J(3) SOLUTION B PG 247 FIG 212. INSTALLED FLOOR PANEL IAW AMM 53-42-12.SDR DALA12002063128Floor Panel · tornAFT CABIN FLOOR PANEL 251JF OUTER PLY TORN. REMOVED FLOOR PANEL 251JF IAW AMM 53-42-12. BONDED AND REPAIRED IAW SRM 53-02-00 PARA 8J, FIG 212. INSTALLED FLOOR PANEL 251J IAW AMM 53-42-12.SDR DALA12002053128Floor Panel · tornAFT CABIN FLOOR PANEL 251HF OUTER PLY TORN. REMOVED FLOOR PANEL 251HF IAW A319 AMM 53-42-12. BOND AND REPAIRED IAW SRM 53-02-00 PAR 8J FIG 212. INSTALLED FLOOR PANEL IAW AMM 53-42-12.SDR DALA12002033128Floor Panel · tornAFT CABIN FLOOR PANEL 251SF OUTER PLY TORN. REMOVED FLOOR PANEL 251SF IAW AMM 53-42-12. REPAIRED AFT CABIN FLOOR PANEL 251SF TORN OUTER PLY IAW SRM 53-02-00 FIG 212. INSTALLED FLOOR PANEL 251SF IAW AMM 53-42-12.SDR DALA12002023128Floor Panel · tornAFT CABIN FLOOR PANEL 251TF OUTER PLY TORN. REMOVED FLOOR PANEL 251TF IAW AMM 53-42-12. BONDED AND REPAIRED IAW SRM 53-02-00 PARA 8.J FIG 212. INSTALLED FLOOR PANEL 252TF IAW AMM 53-42-12.SDR DALA1169893128Power Supply · failedEMERGENCY LIGHT SUPPLY UNIT 11 WL FAILED BITE CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT 11 WL AND BATTERY PACK PER AMM. OPERATIONAL CHECK WAS NORMAL.SDR NWAA 091503128Battery Pack · malfunctionedEMERGENCY LIGHT SYSTEM MESSAGE "EPSU INT LOAD AFT L", REPLACED BATTERY AND TESTED GOOD.SDR 0201813128Outflow Valve · failedPRIOR TO FLIGHT, THE CABIN PRESSURE SYSTEM 2 WAS INOPERATIVE AND DEFERRED PER MEL 21-31-01. AT FL340, RECEIVED ECAM MESSAGE CABIN PR SYS 1 FAULT. CABIN PRESSURE BEGAN CLIMBING AT 4000-5000 FPM. BEGAN IMMEDIATE RAPID DESCENT AND SWITCHED TO MANUAL PRESSURIZA
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