N316NB
Service difficulty reports · 177
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 = 'N316NB' 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 = 'N316NB' 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 DALA2016111808904Frame · crackedFRAME 43 LEFT SIDE 2 AFT HOLES CRACKED IN FLANGE. REPAIR WAS ACCOMPLISHED PER 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.SDR DALA14004233116Wire · brokenFOUND WIRE BROKEN AT ROW 16 SEAT EMERGENCY LIGHT. REPAIRED BROKEN WIRE IAW SWPM 20-60. OPS CHECKED GOOD,OK FOR SERVICE.SDR DALA13072843116Connector · looseEMERGENCY LIGHTS OUT AT 1B, 2B AND 4B. SECURED LOOSE CONNECTORS AND REPLACED LAMPS IAW AMM 33-50. OPEN TESTED GOOD.SDR DALA13016993116Wire · exposedEXPOSED WIRES UNDERSEATS BY SEAT ATTACHMENT RAILS, ROWS 13 14 ABC/ INTERIOR. SECURED WIRES IN RACEWAY. OP CHECKED EMERGENCY LIGHTS. FOUND NORMAL. OK FOR SERVICE.SDR DALA13035503116Skin · dentedDENT IN FWD FUSELAGE AT APPROX BS 3850 FR2, STRINGER 22 . REMOVED DAMAGE IN SKIN. FABRICATED REPAIR PART IAW SRM 53-11-11, FIG 210. REPAIRED IAW SRM 53-11-11, PG 291.SDR DALA12009503116Slat · damagedON WALK AROUND NR 3 SLAT T/E EXTRUSION DAMAGED ON LT WING. INSPECTED DAMAGE IAW SRM 57-40-00. FOUND TO BE OUT OF LIMITS. REMOVED NR 3 SLAT IAW AMM 27-84. INSPECTED SLAT ATTACH POINTS. INSTALLED SLAT PER AMM 27-84-65 THRU SUBTASK 420-052-4 STEP(3). COMPLETESDR DALA12008243116Epsu · failedLINE CHECK FOUND "EPSU UNIT AFT L" ON CIDS PANEL. BITE TEST ON UNIT 13WL HAS UNIT FAIL FAULT LIGHT. R & R EPSU 13WL IAW AMM 33-51-38. OPS CHECKED GOOD. OK FOR SERVICE.SDR DALA13015733116Slat · dentedDENTED ON RT NR 2 SLAT DEPTH IS .3750" X 4" WIDE X 4.5" LONG. LOCATION IS 6.5 FEET FRIM INBD EDGE OF SLAT. FILLED DENT IAW SRM 57-40-00.SDR DALA1153163116Skin · damagedLT WING OTBD OF SLAT TRACK NR 6, LOWER SKIN HAS 3EA ELONGATED HOLES. UPON FURTHER INVESTIGATION IT WAS FOUND 4 ADDITIONAL ELONGATED HOLES. REAMED THE 7 ELONGATED HOLES IAW WITH PRELIM 01 OF ER/A 495623-14, PERFORMED A ROTO-PROBE INSPECTION TO REWORKED HOLES SDR DALA1151953116Fitting · brokenFITTING ON FR65 IS BROKEN. REMOVED AND REPLACED FITTING ON FR65 PN 5347119820900 IAW A319 SRM 51-42-11. APPLIED PRIMER TO FASTENERS IAW A319 SRM 51-21-11.SDR DALA1151573116Skin · damagedLT WING FUEL TANK ACCESS HOLE 540KB HAS 2EA SCREW HOLES DAMAGED. REAMED 1(EA) HOLE IAW A319 SRM 51-44-11 WITHIN LIMITS IAW A319 SRM 57-27-11 FIG 102. REAMED 1(EA) HOLE TO START REAM 0.360 IAW A319 SRM 57-21-11. FINAL REAMED HOLE TO 0.391 IAW A319 SRM 57-21-SDR DALA1151563116Trunnion · damagedLEFT INBD FLAP TRUNNION REWORK DEPTH IS 0.241" MAXIMUM ALLOWED DEPTH IS 0.236" PER AMDS CARD 5751-01025-01C. REPLACED (TRUNNION) TORSION SUPPORT ASSY ON LT INBD FLAP IAW A319 CMM SUBTASK 57-52-21-440-005-B01. REMOVED LT I/B FLAP PER TASK CARD 2750-1010-LT, LSDR DALA1151553116Skin · dentedLT WING 2 SLAT UPPER L/E SURFACE HAS DENT MEASURED L=3" W=1.5" D=.062" OUT OF LIMITS PER SRM 57-40-00 FIG 105. REMOVED DAMAGED AREA IAW A319 SRM 57-40-00 FIG 205. HFEC CUTOUT IAW NTM A319 51-10-08 P6. FABED REPAIR PARTS ON STAM TRAVELER T11/894803 IAW A319SDR DALA1151543116Skin · damagedLT WING ACCESS PNL 540JB CUTOUT HAS 9 EA HOLES HAVE DAMAGE AS MARKED. REAMED 9EA FASTENER HOLES PER A319 SRM 51-44-11. HFEC AND ROTO PROBE HOLES PER NTM 51-10-08 PT.6 & 51-10-01 FIG.6, NO CRACK INDICATION NOTED, COLD WORKED HOLES PER A319SRM 51-21-11 FIG 20SDR DALA1151943116Support Fitting · damagedPER ER/A 494421-14AD, FOLLOW-UP ACTIONS ARE REQ PER SECT II AND SECTION III, TO INSP AND MODIFY THE 80VU AVIONICS RACK SUPPORT FITTINGS. SECTION I HAS BEEN ACCOMPLISHED AT CURRENT M-CK AUG 2011. ACCOMP SECT II INSP EVERY 750 FC AFTER 31AUG11, UNTIL SECT IIISDR DALA1150713116Floor Panel · damagedAFT PIT PANEL 151ZG IS DAMAGED. N/R 150/25. AFT CARGO FLOOR PANEL 151ZG FABRICATED NEW ON STAM TRAVELER T11/893925 IAW A319 DWG 3D25-40640. DAMAGE DIM L=2.50" W=2.50".SDR DALA1150703116Floor Panel · damagedAFT PIT FLOOR PNL 151VG IS DAMAGED. N/R 150/52. AFT CARGO FLOOR PANEL 151VG FABRICATED ON STAM TRAVELER T11/893917 IAWA319 DWG 3D25-40640. DAMAGE DIM L=2.75" W=2.00".SDR DALA1150693116Floor Panel · damagedAFT PIT FLOOR PANEL 151PE IS DAMAGED. N/R 150/51. AFT CARGO FLOOR PANEL 151PE FABRICATED NEW ON STAM TRAVELER T11/893924IAW A319 DWG 3D25-40640. DAMAGE DIM L=1.75" W=1.75".SDR DALA1150683116Floor Panel · damagedAFT PIT PANEL 151FE IS DAMAGED. N/R 150/24. AFT CARGO FLOOR PANEL 151FE FABRICATED NEW ON STAM TRAVELER T11/893905 IAW A319 DWG 3D25-40640. DAMAGE DIM L=2.25" W=1.25".SDR DALA1150673116Floor Panel · damagedAFT PIT FLOOR PNL 152UG IS DAMAGED. N/R 150/49. AFT CARGO FLOOR PANEL 152UG FABRICATED NEW ON STAM TRAVELER T11/893979IAW A319 DWG 3D25-40640. DAMAGE DIM L=2.5" W=2.5".SDR DALA1150663116Floor Panel · damagedAFT PIT PANEL 151DE IS DAMAGED. N/R 150/23. AFT CARGO FLOOR PANEL 151DE FABRICATED NEW ON STAM TRAVELER T11/893904 IAW A319 DWG 3D25-40640. DAMAGE DIM L=4.25" W=4.25".SDR DALA1150653116Floor Panel · damagedAFT PIT FLOOR 151TG IS DAMAGED. N/R 150/53. AFT CARGO FLOOR PANEL 151TG FABRICATED NEW ON STAM TRAVELER T11/893921 IAW A319 DWG 3D25-40640. DAMAGE DIM L=3.50" W=3.50".SDR DALA1150633116Floor Panel · damagedAFT PIT FLOOR PANEL IS DAMAGED (151VG) N/R 150/54. AFT CARGO FLOOR PANEL FABRICATED NEW ON STAM TRAVELER T11/893923 IAW A319 DWG 3D25-40640. DAMAGE DIM L=4.5" W=4.5".SDR DALA1150623116Floor Panel · damagedAFT PIT FLOOR PNL 151AE IS DAMAGED. N/R 150/55. AFT CARGO FLOOR PANEL 151AE FABRICATED NEW ON STAM TRAVELER T11/893918IAW A319 DWG 3D25-40640. DAMAGE DIM L=4.25" W=3.75".SDR DALA1150613116Floor Panel · damagedAFT PIT PANEL 151CE IS DAMAGED. N/R 150/22. AFT CARGO FLOOR PANEL 151CE FABRICATED NEW ON STAM TRAVELER T11/893903 IAW A319 DWG 3D25-40640. DAMAGE DIM. L=5.5" W=4.5.SDR DALA1150603116Floor Panel · delaminatedAFT PIT PANEL 161PF IS DELAMINATED. N/R 150/19. AFT CARGO FLOOR PANEL 161PF FABRICATED NEW ON STAM TRAVELER T11/893926 IAW A319 DWG 3D25-40640. DAMAGE DIM L=2.5" W=2.5,".SDR DALA1150593116Floor Panel · delaminatedAFT PIT PANEL 161CF IS DELAMINATED. N/R 150/18. AFT CARGO FLOOR PANEL 161CF FABRICATED NEW ON STAM TRAVELER T11/893907 IAW A319 DWG 3D25-40640. DAMAGE DIM. L=3.0" W=2.0".SDR DALA1150583116Floor Panel · delaminatedAFT PIT PANEL 162BF IS DELAMINATED. N/R 150/13. AFT CARGO FLOOR PANEL 162BF FABRICATED NEW ON STAM TRAVELER T11/893927IAW A319 DWG 3D25-40640. DAMAGE DIM. L=2.0" W=2.0"SDR DALA1150183116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 FR68-FR69 HAS CORROSION. REMOVED CORROSION PER A319 SRM 51-74-00.DIM. L=1.0" W=.500" D=.058" OUT OF LIMITS PER A319 TRM 53-41-15. REMOVED AND INSTALLED NEW FLOORBEAM SUPPORT 4EA SPLICES 4EA HARD POINT FITTINGS AND 2EA BRACSDR DALA1150173116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 HAS CORROSION AT FR66. REMOVED CORROSION PER A319 SRM 51-74-00 DIMENSIONS L=1.0" W=1.0" D=.040" OUT OF LIMITS PER A319 TRM 53-41-15. REMOVED AND INSTALLED NEW FLOOR SUPPORT, 4EA SPLICES, AND 3EA BRACKETS PER A319 SRM 51-42SDR DALA1150163116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM +Y1292 FR66-FR68 HAS CORROSION.REMOVED CORROSION IAW A319 SRM 51-74-00 DIMENSIONS L=.500" W=.600" D=.041" FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15 ORIG MAT .087". REMOVED AND REPLACED FLOOR SUPPORT BEAM +Y1292 W/ NEW IAW ASDR DALA1150153116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 HAS CORROSION AT FR66-FR68 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00.DIM. L=.500" W=.600" D=0.042" FOUND OUT OF LIMITS PER A319 TRM 53-41-15. REMOVED INSTALLED NEW SUPPORT BEAM PER A319 SRM 51-42-11 PER A319 SDR DALA1150313116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 HAS TWO EA SPLICER CORRODED AT FR 68, I/B FLANGE. REMOVED 2 EA SPLICES ON N/R 260/17. INSTALLED 2EA SPLICES IAW A319 SRM 51-42-11. CORROSION DIMENSION: L=1" W=0.5" D=0.045". OUT OF LIMITS IAW TRM 53-41-15.SDR DALA1150303116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM +Y765 FR66-FR70 HAS CORROSION AT 5 PLACES. REMOVED CORROSION IAW A319 SRM 51-74-00. DIMENSIONS L=.400" W=.250" D=.059" FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. ORIGINAL MAT .157" MAT REMAINING .098" RECEIVED NEW FLOOR SUPSDR DALA1150283116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM +Y765 FR64-FR66 FWD & AFT HOLES CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00. DIMENSIONS: L=.700, W=.300, D=.040. FOUND OUT OF LIMITS IAW A319 TRM 53-41-15. ORIGINAL MATERIAL THICKNESS =.087. REMAINING MATERIAL=.047. RESDR DALA1150273116Sill · corrodedAFT CABIN LT DOOR SILL, AND SHAPE SILL HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. DIMENSIONS: L=1.700, W=.550, D=.045, FOUND OUT OF LIMITS IAW A319 SRM 53-41-14 FIG 101. REMOVED AND REPLACED MID SHAPE SILL P/N: D5348004800003 IAW A319 SRM 51-4SDR DALA1150333116Pin · wornNR 2 PYLON RIB 4, 2 EACH OUTER PINS HAVE WEAR MARKS ON HEAD SIDE. ON INSPECTION FOUND DEEP SCRATCHES ON HEADSIDE. FOUND TO BE OUT OF LIMITS IAW A319 AMM 54-51-17-200-002. RECEIVED 2 EA OUTER PINS. TO BE INSTALLED ON W/C 5450-30205-02.SDR DALA1150323116Pin · wornNR 2 PYLON RIB 10 3 EACH OUTER PINS HAVE WEAR MARKS ON HEAD SIDE. ON INSPECTION FOUND DEEP SCRATCHES ON HEAD SIDE, FOUND TO BE OUT OF LIMITS IAW A319 AMM 54-51-17-200-002. RECEIVED 3 EACH NEW OUTER PINS, TO BE INSTALLED ON W/C 5450-30205-02.SDR DALA1150293116Seat Track · corrodedFWD UTILITY AREA SEAT TRACK LT SIDE +Y254 CORRODED AT 4 LOCATIONS BETWEEN FR16 & FR20 AND HAS DAMAGE AT 2 LOCATIONS BETWEEN FR21 & FR23. BLENDED OUT DIMENSIONS ARE L=3.00", W=1.500", D=0.063" FOUND OUT OF LIMITS PER A319 SRM 53-11-14 FIG 106. ACCOMPLISHED WISDR DALA1150263116Floor Panel · delaminated(PANEL RACK) FWD CABIN FLOOR PANEL 232FF IS DELAM/PEELING ON LOWER SURFACE FWD CABIN FLOOR PANEL 232FF FABRICATED NEW ON STAM TRAVELER T11/893912 IAW A319 DWG 3D25-40640. SPLICE PLATE INSTALLED ON WC 2500-6601. DAMAGE AREA IS 3"X3".SDR DALA1150253116Floor Panel · punctured(PANEL RACK) FWD CABIN FLOOR PANEL 232DF HAS SMALL PUNCTURE ON UPPER SURFACE AND A CORRODED INSERT CAUSING LOWER SURFACETO DELAM. FABRICATED NEW ON STAM TRAVELER T11/893914 PER DWG3D25-40640. SPLICE PLATE INSTALLED ON W/C 2500-6601. RETAIN FOR RECORDS.SDR DALA1150243116Floor Panel · delaminated(PANEL RACK) COCK PIT FLOOR PANEL 211EF HAS DELAM AND PEELING UP PER SKIN. COCKPIT FLOOR PANEL 211EF FABRICATED NEW STAM TRAVELER T11/8939 16 IAW A319 DWG 3D25-40640.SDR DALA1150233116Floor Panel · punctured(PANEL RACK) FWD CABIN FL PANEL 231KF HAS 7IN PUNCTURE ON UPPER SURFACE. FWD CABIN FLOOR PANEL 231KF FABRICATED NEW ON STAM TRAVELER T11/893913 IAW A319 DWG 3D25-40640.SDR DALA1150223116Floor Panel · torn(PANEL RACK) AFT CABIN FLOOR PANEL 261PF HAS TORN-OUT AND MISSING INSERT. FABRICATED NEW FLOOR PANEL 261PF ON STAM TRAVELER T11/893911 PER DWG 3D25-40640.SDR DALA1150213116Floor Panel · torn(PANEL RACK) MAIN DECK AFT CABIN FLOOR PANEL 262EF HAS TORN-OUT/MISSING INSERT MAIN DECK AFT CABIN FLOOR PANEL 262EF FABRICATED NEW ON STAM TRAVELER T11/893909 IAW A319 DWG 3D25-40640.SDR DALA1150203116Floor Panel · torn(PANEL RACK) CENTER AFT LAV FLOOR PANEL ON MAIN DECK 261CG HAS 2 EA TORN AREAS ON LOWER SKIN. FABRICATED NEW FLOOR PANEL 261CG ON STAM TRAVELER T11/893908 PER DWG 3D25-40640.SDR DALA1150193116Seat Track · corrodedFWD UTILITY AREA SEAT TRACK RT SIDE -Y254 CORRODED AT SEVERAL LOCATIONS BETWEEN FR18 AND FR20. REMOVED CORROSION IAW A319 SRM 51-74-00 L=4.0" W=1.5" D=.080" FOUND TO BE OUT OF LIMITS IAW A319 53-11-14 FIG 105. REMOVED AND INSTALLED HARDPOINT FITTINGS. TRANSSDR DALA1149923116Sill · damagedAFT CABIN LT AFT DOOR SILL AT FR66 & FR68 REQUIRES FOLLOW-ON INSPECTION PER SRI TASK IIR 53-41-14-2-001-00 PER A319 SRM 53-41-14, FIGURE 201. AFT CABIN LT AFT DOOR SILL WAS REPAIRED PER A319 SRM 53-41-14, FIGURE 201 DURING M-CHECK AT BFM ON N/R 260/2. THIS LSDR DALA1149913116Sill · damagedAFT CABIN RT DOOR SILL UNDER FWD GIRT BAR REQUIRES FOLLOW-ON INSPECTION PER SRI TASK IIR 53-41-14-2-001-00 PER A319 SRM 53-41-14, FIGURE 201. ENTR 280814 S. AFT CABIN RT DOOR SILL WAS REPAIRED PER A319 SRM 53-41-14, FIGURE 201 DURING M-CHECK AT BFM ON N/R 260SDR DALA1149883116Pin · damagedNR 1 PYLON 1 EACH PIN FOR RIB 4 COATING DAMAGED. FOUND COATING DAMAGED, FOUND TO BE OUT OF LIMITS IAW A319 AMM 54-51-17-200-002. RECEIVED 1 EACH PIN FOR RIB 4. TO BE INST ON W/C 5450-3020S-01. DAMAGE DIM. L=2.0" W=1.0"
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