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.

SDR DALA1149853116Floor Panel · damagedAFT PIT FLOOR PANEL 152TG IS DAMAGED AFT CARGO FLOOR PANEL 152TG. FABRICATED NEW ON STAM TRAVELER T11/893922 IAW A319 DWG 3D25-40640.Aug 25, 2011 · N316NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1149843116Floor Panel · damagedAFT PIT FLOOR PANEL 152XG IS DAMAGED AFT CARGO FLOOR PANEL 152XG. FABRICATED NEW ON STAM TRAVELER T11/893920 IAW A319 DWG 3D25-40640.Aug 25, 2011 · N316NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1149833116Floor Panel · damagedAFT MAIN DECK FLOOR PANEL 261HG IS BROKEN ON EDGE AND MISSING INSERT. FABRICATED NEW FLOOR PANEL 261HG ON STAM TRAVELER T11/893910 IAW NWD 3D25-40640. DAMAGE DIM. W=4.0" D=3.0" STAM CRS# MZAR013L.Aug 25, 2011 · N316NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1149873116Panel · damagedAFT PIT PANEL 151GE IS DAMAGED N/R 150/20. AFT PIT PANEL 151GE FABRICATED NEW ON STAM TRAVELER T11/893902 IAW DWG 3D25-40640. DAMAGE DIM. L=4" W=4".Aug 24, 2011 · N316NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1149863116Seat Track · corrodedFWD UTILITY AREA SEAT TRACK RT SIDE -Y1292 EXFOLIATED AT SEVERAL LOCATIONS BETWEEN FR16 & FR20. REMOVED CORROSION IAW A319 SRM 51-74-00, DIMENSION REWORKED L=3" W=2" D=.030" THICKNESS ORIG .079" REMAINING MAT 049" OUT OF LIMITS IAW A319 SRM 53-11-14. REMOVEAug 24, 2011 · N316NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1149823116Floor Panel · delaminatedCOCKPIT FLOOR PANEL 211FF HAS DELAM AND PEELING UPPER SKIN N/R 210/12. COCKPIT FLOOR PANEL 211FF FABRICATED NEW ON STAM TRAVELER T11/893915 IAW DWG 3D25-40640. DAMAGE DIM. L=2.5" W=2.5".Aug 24, 2011 · N316NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1149813116Sill · corrodedAFT CABIN LT AFT DOOR SILL, AFT SHAPE SILL HAS CORROSION. BLENDED OUT CORRODED AREA IAW A319 SRM 51-74-00, L=1.0" W=0.500" MAX DEPTH=0.080", ORIG MAT THICK. =0.080". NO LIMITS OR REPAIRS ARE ESTABLISHED ON SRM. REMOVED DAMAGED SHAPE SILL IAW A319 SRM 51-42-Aug 24, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149903116Attach Angle · wornNR 2 PYLON AFT ATTACHMENT FITTING LUG BEARING ASSY WORN. REPLACED NR 2 PYLON AFT ATTACHMENT BEARING ASSY IAW A319 AMM 57-26-12 PB 401. ORIG MAT 2.265" DAMAGE DIM L=.328" W=.109" D=.018.Aug 23, 2011 · N316NB · Airbus A319114 · Nacelle/Pylon, Attach FittingsSDR DALA1149893116Shackle · damagedNR 1 PYLON RIB 10 ONE EACH SHACKLE HAS TOOL MARKS AT TWO LOCATIONS N/R 470/41. RECEIVED 1EA RIB 10 SHACKLE TO BE INSTALLED ON CARD 5450-6010-LT DAMAGE FOUND TO BE OUT OF SERVICEABLE LIMITS PER A319 AMM 54-51-17-200-004. ORIG MAT .633" DAMAGE DIM. L=.328" W=.Aug 23, 2011 · N316NB · Airbus A319114 · Nacelle/Pylon Miscellaneous StructureSDR DALA1149803116Floor Panel · brokenAFT GIRT BAR LATCH FLOOR PANEL AT R-2 DOOR HAS BROKEN EDGE N/R 250/8. AFT GIRT BAR LATCH FLOOR PANEL AT R2 DOOR . REPLACED IAW A319 SRM 51-76-00, PN D5348015900700. DAMAGE DIM. L=.5"W=.5"Aug 23, 2011 · N316NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1149763116Dummy Rail · corrodedFWD UTILITY AREA DUMMY RAIL RT SIDE -Y189 BETWEEN FR 20 & FR24 EXFOLIATED BETWEEN FR 20 & FR 21. REMOVED CORROSION IAW A319 SRM 51-74-00. ORIG MAT .060" DAMAGE DIM. L=2" W=2" D=.060- REMOVED AND REPLACED DUMMY RAIL IAW A319 SRM 51-42-11.Aug 23, 2011 · N316NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1149573116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y765 FWD & AFT OF FR66 HAS CORROSION.SSI 534147 REMOVED CORROSION IAW A319 SRM 51-74-00. CHECK LIMITS L=1" W=.600 D=0.040" ORIG MAT THICKNESS .087 AFTER BLEND MAT REMAINING .047 FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. Aug 23, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149563116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y465 FWD & AFT OF FR66 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00.DIM: L=1.3" W=1.0" D=.025" ORIGINAL MAT THICKNESS .152 FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. LOCATED AND DRILLED NEW SUPPORT BEAAug 23, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149543116Seat Track · corrodedFWD UTILITY AREA SEAT TRACK RT SIDE -Y765 CORRODED AT FR 20.SSI 531189. BLENDED AREA IAW A319 SRM 51-74-00 L=3.0" W=.700" D=.050" OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 105. REMOVED SEAT TRACK IAW A319 SRM 51-42-11. LOCATED AND DRILLED NEW SEAT TRACK IAAug 23, 2011 · N316NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1149533116Plate · corrodedAFT CABIN RT SUPPORT PLATE AFT OF FR 68 HAS SURFACE CORROSION SSI 534147. BLENDED CORRODED AREA IAW A319 SRM 51-74-00 DIM: L=3.1" W=2.55" D=0.039". NO ESTABLISHED LIMITS. REMOVED SUPPORT PLATE IAW A319 SRM 51-42-11. FABED NEW SUPPORT IN MATERIAL P/N: 20Aug 22, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149193116Floor Support · corrodedFWD UTILITY AREA RT SIDE -Y1732 FLOOR SUPPORT BETWEEN FR20 &FR 24 CORRODED AT FR20. REMOVED CORROSION FROM FLOOR SUPPORT-Y1732 IAW A319 SRM 51-74-0 0, L=3.5 W=3.0 D=0.050 FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 101. REMOVED FLOOR SUPPORT -Y1732 IAug 21, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149183116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y765 FR66-FR70 CORRODED AT 4 PLACES. REMOVED CORROSION IAW A319 SRM 51-74-00 L=4.00" W=1.00" D=0.056" OUT OF LIMITS IAW A319 TRM 53-41-15 ORIG MATERIAL 0.157 REMAINING MATERIAL 0.101". REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 5Aug 21, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149163116Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y254 FR68-FR70 HAS CORROSION JUST FWD OF FR70. REMOVED CORROSION IAW A319 SRM 51-74-00. DAMAGE DIMENSIONS L=2.5- W=.800" D=.025" ORIG MAT .153 FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR Aug 21, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149143116Sill · corrodedAFT CABIN RT DOOR SILL AFT SHAPE SILL CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 & 51-21-11. DIMENSION OF DAMAGE ARE AS FOLLOWS L=0.175", W=0.750" MAX. D=0.030".ORIGINAL MTL. THICKNESS IS 0.080 NO ALLOWABLE DATA FOUND ON SRM. REMOVED RT AFT SHAPE SIAug 21, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1149153116Dummy Rail · corrodedFWD UTILITY AREA DUMMY RAIL, LT SIDE, +Y503 BETWEEN FR 12 & FR 16 CORRODED AT TWO LOCATIONS AT FR 16. REMOVED CORR IAW A319 SRM 51-74-00. DIMENSIONS REWORKED 2EA (1) L=2.5" W=1.5"D=.050" THICKNESS ORIG MAT.150 REMAINING .100 OUT OF LIMITS (2) L=3.0 W=2.0 D=.Aug 20, 2011 · N316NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1152523116Skin · dentedRT FWD FUSELAGE EXTERNAL SKIN DENTED AT FR 13 APPROX STR 23R MEASURED DENT PER A319 SRM 53-11-11 FIG 105. OUT OF NEARNESS/FORM PER A319 SRM 53-11-11 DIA 103. CUT OUT DAMAGED SKIN IAW A319 SRM 53-11-11 FIG 210 L=5.5 W=3.5. FABED REPAIR DOUBLER IAW A319 SRM 53Aug 19, 2011 · N316NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA1153183116Sill · corrodedAFT CABIN RT DOOR SILL UNDER FWD GIRT BAR HAS CORROSION AND AT AFT DOOR SILL FR 68. BLENDED OUT FWD CORRODED AREA (FR66) IAW A319/320 TRM 53-41-14, IN LIMITS IAW TRM 53-41-14. BLENDED OUT AFT CORRODED AREA (FR68) IAW TRM 53-41-14, OUT OF LIMITS IAW A31/320 TAug 16, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1153173116Sill · corrodedAFT CABIN LT AFT DOOR SILL AT FR 66 & FR 68 HAS CORROSION BLENDED OUT FWD CORRODED AREA (FR66) IAW A319/320 TRM 53-41-14, IN LIMITS IAW TRM 53-41-14. BLENDED OUT AFT CORRODED AREA (FR68) IAW TRM 53-41-14, OUT OF LIMITS IAW A31/320 TRM 53-41-14 IAW ER/A 494437Aug 16, 2011 · N316NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1129313116Wire · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY EXIT PATH LIGHT AT 6ABC INOPERATIVE. MX REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Apr 26, 2011 · N316NB · Airbus A319114 · Light System WiringSDR DALA1018333116Wire · disconnectedDURING EMERGENCY LIGHT TEST, FOUND ROW 1 ISLE EXIT LIGHT WIRES PULLED OUT OF CONNECTOR, REPAIRED CONNECTOR WIRING AND TESTS OK.Aug 4, 2010 · N316NB · Airbus A319114 · Light System WiringSDR NWAA093913116Battery Pack · dischargedEMERGENCY LIGHT SYSTEM FAILS TEST. REPLACED EPSU BATTERY PACK, TESTS OK.Nov 14, 2009 · N316NB · Airbus A319114 · Emergency LightingSDR 0501883116Power Supply · dischargedEMERGENCY LIGHT TEST FAILED, FAULT SHOWS EPSU INT LOAD EMER R. RELAMPED CABIN EMERGENCY LIGHTS RIGHT CABIN AND REPLACED EPSU 12WL PER 33-51-39-000-001. OPS CHECKED GOOD.Dec 28, 2005 · N316NB · Airbus A319114 · Emergency Lighting
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