N315NB

Service difficulty reports · 172

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 = 'N315NB' 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 DALA2017042803457Doubler · corrodedCORROSION DOUBLER ON INTERNAL STRUCTURE AT LEVEL FR 26 BTW STR 38R AND STR 41R IN FWD CARGO COMPARTMENT. REPLACED FISHPLATE LOC ON INTERNAL STRUCTURE AT LEVEL FR 26 BTW STR 38R AND STR 41R IN FWD CC AS PER SRM 51-72-11 AND DRAWING D53233414.Apr 25, 2017 · N315NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2017041703158Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT -Y254, FRAME 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11. AND DRAWING D53111462.Apr 14, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017041503155Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT -Y765, FRAMES 12 - 24, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53112812.Apr 14, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017041403016Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y189, FRAMES 20 TO 24 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT.Apr 13, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017041303015Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT +Y254, FRAMES 12 TO 24 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT.Apr 13, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017041002953Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y765 BETWEEN FRAMES 66 - 70. REPLACED THE FLOOR SUPPORT.Apr 8, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017040902952Seat Track · corrodedSEAT TRACK Y765, FOUND CORRODED BEYOND LIMITS FRAME 47+4 - 54+1 UPPER SURFACE. REPLACED THE SEAT TRACK.Apr 8, 2017 · N315NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017040902951Dummy Rail · corrodedCORROSION ON DUMMY RAIL Y503.2 LOCATED FRAMES 12 - 16. REPLACED THE DUMMY RAIL.Apr 8, 2017 · N315NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017040902950Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66-68. REPLACED THE FLOOR SUPPORT.Apr 8, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017040902949Floor Support · corrodedCORROSION ON FLOORB SUPPORT -Y1162 BETWEEN FRAMES 68 & 69 IN AFT GALLEY. REPLACED FLOOR SUPPORT.Apr 8, 2017 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018052403543Skin · damagedWHILE ACCOMPLISHING THE 2KU MODIFICATION IN DTW THE FWD ATG4 ANTENNA DOUBLER, SPOT FACE ONE LOCATION AND 36 OVERSIZE HOLES REPAIR PER ER/A 557344-14.Apr 5, 2017 · N315NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2016120209542Battery Pack · no testLEFT AFT EMERGENCY BATTERY FAULTED DURING EMERGENCY LIGHT TEST, REPLACED LEFT AFT EMERGENCY LIGHT BATTERYNov 30, 2016 · N315NB · Airbus A319114 · Emergency LightingSDR DALA2017050803737Skin · dentedER/A 552994-14 ISSUED FOR DENT DAMAGE NOTED AROUND THE STABILIZATION JACK POINT BETWEEN FR73 AND FR74, BETWEEN S32L AND S-32R. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FR 73 RO FR 74 AND STR 31L TO STR 31R LOWER AFT FUSELAGE AS PER E/RA 552994-1Nov 21, 2016 · N315NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13072163115Wire · brokenAFT EMERGENCY LIGHT AT ROW 3AB INOPERATIVE, REPAIRED BROKEN WIRE.Dec 24, 2013 · N315NB · Airbus A319114 · Light System WiringSDR DALA13058023115Connector · inoperativeSEAT 18C EMERGENCY LIGHT INOPERATIVE. REPLACED CONNECTOR IAW SPWM CH 20. CHECKED GOOD.Nov 1, 2013 · N315NB · Airbus A319114 · Light System WiringSDR DALA1159713115Epsu · inoperativeEMERGENCY LIGHTS TEST FAULTED. MAINTENANCE REMOVED AND REPLACED BOTH EPSU AND BATTERY AT ROW 9. TEST OK. AIRCRAFT OK FOR SERVICE.Oct 24, 2011 · N315NB · Airbus A319114 · Emergency LightingSDR DALA1150143115Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM +Y1292 FR68-FR69 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 DIMENSIONS L=.900" W= 1" D=.059" FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15 ORIG MAT.157". REMOVED AND REPLACED FLOOR SUPPORT BEAM +Y1292 FR68 TO FR69 W/ NEAug 28, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148773115Floor Panel · damaged0372062 FWD CARGO COMPT FLOOR PANEL 131AF HAS MULTIPLE PUNCTURES & 1EA CRACK APPROX 4 INCHES IN LENGTH. REMOVED FLOOR PNL 131AF IAW AMM 53-22-14. FABRICATED FLOOR PNL 131AF IAW DWG 3D25-40532 FROM MATERIAL A402AB-60X144 BN 2066145 INSTALLED FLOOR PNL 131AF IAug 19, 2011 · N315NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1148633115Frame · damagedAFT CARGO AT FR 53 STR 35R SEALING PROFILE HOLE ELONGATED THRU FRAME. CUT OUT DAMAGED FRAME SECTION IAW A319 SRM 53-00-12 FIG 204, FABED NEW FRAME SECTION FABED 2EA SPLICES LOCATED AND DRILLED FRAME SECTION AND 2 EA SPLICES IAW A319 SRM 53-00-12 FIG 204 AND 5Aug 17, 2011 · N315NB · Airbus A319114 · Fuselage Main, FrameSDR DALA1148333115Plate · damagedRT WING NR 2 SLAT TRACK CLOSING PLATE CHAFING W/SLAT. BLENDED AREA PER A319 SRM 51-73-00 L=3.25 W=.25 D=.032 ORIG .080. ACCOMP DVI INSP PER NTM 51-90-00 NO DISCREPANCIES NOTED. ACCOMP HFEC PER NTM 51-10-08 NO DISCREPANCIES NOTED ACCOMP WORK PER ATTACHED REPAug 16, 2011 · N315NB · Airbus A319114 · Leading Edge DevicesSDR DALA1148313115Skin · damagedRT WING NR 1 SLAT TRACK CLOSING PLATE CHAFING W/SLAT INNER SKIN. BLENDED OUT DAMAGE PER A319 SRM 51-73-00. ACCOMP DVI PER NTM 51-90-00 NO DISCREPANCIES NOTED. ACCOMP HFEC PER NTM 51-10-08 NO DISCREPANCIES NOTED. ACCOMP WORK PER ATTACHED REPAIR DWG R574-602Aug 16, 2011 · N315NB · Airbus A319114 · Leading Edge DevicesSDR DALA1148253115Plate · crackedFWD CARGO COMPT SEALING PLATE AT FR30 ABOVE STR 38R CRACKED. REMOVED IAW A319 SRM 51-42-11, LOCATED & DRILLED NEW PLATE IAW A319 SRM 51-44-11, TREATED AND PRIMED NEW SEALING PLATE IAW A319 SRM 51-21-11, INST NEW SEALING PLATE IAW A319 SRM 51-42-11, INST 3EA Aug 15, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148243115Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT AT FR28 CRACKED AND DEFORMED. FLOOR SUPPORT AT FR28 FOUND TO BE CRACKED L=1/2" W=1/2" FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-00-14. REMOVED FLOOR SUPPORT IAW A319 SRM 51-42-11. FABBED FLOOR SUPPORT PER ER/A 494429-14 REVAug 15, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148233115Plate · crackedFWD CARGO COMPT SEALING PLATE BET FR 28 AND FR29 LT SIDE CRACKED SEALING PLATE CRACKED AT FR28 L=1/2 W=1/2 AND AT FR29 L=1/2 W=1/2 FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-00-14. FABED NEW SEALING PLATE ON STAM TRAVELER T11/891979 MAT 2024 T2 .040 BATCH 0001Aug 15, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148223115Sill · corrodedAFT CARGO DOOR SILL UNDER TIE DOWN FITTING AT S 38R HAS CORROSION. REMOVED & REPLACED SHEET SEALING ASSY IAW A319 SRM 51-42-11.Aug 15, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148053115Sill · corrodedR1 DOOR SILL AREA UNDER FWD GIRT BAR FITTINGS AROUND FASTENER HOLES CORRODED. SSI 531189 DAMAGE DIMENSIONS: L=2.500" W=2.000" MAX DEPTH=0.037". NO LIMITS OR REPAIRS ARE ESTABLISHED ON SRM. REMOVED DAMAGED DOOR SILL IAW A319 SRM 51-42-11. INSTALLED NEW DOOR Aug 14, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148043115Sill · corrodedAFT CARGO DOOR SILL WEB HAS 4 AREAS WITH CORROSION AT FR56. SSI 534107 BLENDED OUT CORROSION AREA IAW A319 SRM 51-74-00AREA 1 W=2" L=5.7 5" MAX D=.049, AREA 2 L=9.40" W=1.90" MAX D=.055 AREA 3 L=3" W=3" MAX D=.055 AREA 4 L=4" W=3.60" MAX D=.060" NO LIMITS OF RAug 13, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148063115Sill · corrodedL1 DOOR SILL AREA UNDER AFT GIRT BAR FITTING HAS CORROSION AROUND FASTENERS. ACCOMPLISHED ER/A 494420-14 REV ORG. PERMANENT REPAIR SECTION I STEPS 1-14. BLENDED AREA IAW A319 SRM 51-74-00 L=5.5" W=4.5" D=0.022" NO ESTABLISHED LIMITS IN A319 SRM. SECTION IIAug 12, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1148033115Sill · corrodedAFT CARGO BILGE AREA FROM FR56 TO FR58 STR 38L SILL PLATE CORRODED. BLENDED AREA IAW A319 SRM 51-74-00 SILL PLATE OUT OF LIMITS DIM: L=6" W=2" D=.025" REMAINING MAT.014 IAW SRM 53-00-14. REMOVED SILL PLATE FROM FR56 TO FR58 STR 38L IAW SRM 51-42-11 RECEIVEDAug 12, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1147413115Cargo Fitting · corrodedAFT CARGO FITTING BETWEEN FR58 AND FR59 ABOVE S38L HAS CORROSION. REMOVED AND REPLACED FITTING IAW A319 SRM 51-42-11, P/N D5367227420000 BATCH 0002082646.Aug 9, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1147403115Profile · corrodedAFT CARGO FLOOR SEALING PROFILE AT FR56 HAS CORROSION AT 10 AREAS BETWEEN S41R AND S38L. BLENDED CORRODED AREAS IAW A319SRM 51-74-00 OUT OF LIMITS IAW A319 TRM 53-00-14 L=2.5" W=2.0" D=.025" REMAINING MAT.= .014", REMOVED SEALING PROFILE IAW A319 SRM 51-42-11Aug 9, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1146833115Sill · corrodedL1 DOOR CENTER SHAPE SILL HAS CORROSION AROUND FASTENER HOLES. REMOVED L1 AFT GIRT BAR FITTING IAW A319 SRM 51-42-11. REMOVED 02 EA SPLICES FROM FR16 AND FR20 IAW A319 SRM 51-42-11. REMOVED CENTER DOOR SILL. LOCATED AND DRILLED NEW CENTER DOOR SILL IAW A31Aug 7, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1146863115Spar · buckledLT PYLON, INBD SIDE, LWR SPAR BUCKLED LOCATED ABOVE ELECTRICAL JUNCTION BOX. REMOVED LWR SPAR IAW A319 SRM 51-42-11. REFORMED LWR SPAR ANGLE IAW A319 SRM 51-26-11. FPIAREA IAW NTM A319 51-80-00, NO CRACKS NOTED. INSTALLED LWR SPAR ANGLE IAW A319 51-42Aug 5, 2011 · N315NB · Airbus A319114 · Nacelle/Pylon, Frame/Spar/RibSDR DALA1146853115Floor Support · corrodedFWD CABIN FLOOR SUPPORT BEAM -Y254 BET FR16 TO FR21 SEVERAL AREAS AROUND FASTENER HOLES CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 L=1.100" W=.200" D=.055" NO DAMAGE ALLOWED IAW A319 SRM 53-11-14 FIG 103. REMOVED FWD CABIN FLOORBEAM -Y254 IAW A319 SRMAug 5, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1146843115Floor Support · corrodedFWD CABIN FLOOR SUPPORT BEAM +Y254 BET FR16 TO FR20 SEVERAL AERAS CORRODED. BLENDED DAMAGED AREA PER A319 SRM 51-74-00. ORIG MAT: .079" L=2.0" W=1.0" D=.050" FOUND TO BE OUT OF LIMITS PER A319 SRM 53-11-14 FIG 105, PG 112. REMOVED AND REPLACED FLOOR SUPPORTAug 5, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1146063115Sill · corrodedAFT LT DOOR SILL FWD & AFT AREA HAS CORROSION. BLENDED AFT LT DOOR SILL, ORIGINAL MATERIAL .098" D=.040" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-14. REMOVED & REPLACED AFT LT DOOR SILL IAW SRM 51-42-11 A319.Aug 3, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1146053115Floor Support · corrodedAFT LT CABIN FLOOR SUPPORT BEAM +Y765 FR 66 - FR 70 HAS CORROSION ON SEVERAL PLACES. REMOVED FLOOR PANEL 251 FOR ACCESS IAW A319 SRM 51-42-11. REMOVED AND INSTALLED NEW FLOOR SUPPORT BEAM +Y765 PND5347219220000 IAW A319 SRM 51-42-11. FLOOR PANEL INSTALLED OAug 1, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145853115Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM Y1292 FR68-FR69 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 DIMENSIONS ORIG THICKNESS .125" MAT LOSS .025" REMAINING MAT .100" OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT BEAM Y1292 FR68-FR69 IAW AQAug 1, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145813115Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM +Y765 FROM FR64-FR66 CORRODED FWD AND AFT AREA. BLENDED CORROSION IAW A319 SRM 51-74-00 L=1.5 W=1.2 D=.021. OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM +765 P/N #D5347209000200 IAW A319 SRM 5Aug 1, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145803115Seat Track · corrodedSEAT TRACK LT SIDE AFT CABIN Y1732 BETWEEN FR65 AND FR66 CORRODED AT TWO LOCATIONS AS MARKED. BLENDED AREA IAW A319 SRM 51-74-00, DIM OF BLEND 1) L=1.5" W=1. 0" D=.010" 2) L=2.0" W=1.0" D=.015. REMOVED FLOORBEAM IAW A319 SRM 51-42-11. LOCATED AND DRILLED NAug 1, 2011 · N315NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1145793115Floor Support · corrodedAFT CABIN LT FLOOR SUPPORT BEAM Y1292 FWD & AFT OF FR67 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 DIMENSIONS ORIG THICKNESS .125" MAT LOSS .035" REMAINING MAT. .090" OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT BEAM Y1292 FR66-FAug 1, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145783115Floor Support · corrodedAFT CABIN LT FLOOR SUPPORT BEAM +Y1292 FR64-FR66 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. DIMENSION: THICKNESS ORIGINAL 0.125, MAT LOSS 0.030, REMAINING MAT 0.095, FOUND TO BE L=1.5 W=1.5 D=.030 IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPAug 1, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145773115Floor Panel · delaminatedFWD CABIN FLOOR PANEL 232FF IS DELAMINATED 4.0" X 4.0". FWD CABIN FLOOR PANEL 232FF FABRICATED NEW ON STAM TRAVELER T11/890812IAW DWG 3D25-40640.Aug 1, 2011 · N315NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1145663115Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 BET FR66 & FR68 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00 L=2" W=1.40" D=0.0425 OUT OF LIMITS IAW A319 TRM 53-41-15, REMOVED DAMAGED FLOORBEAM IAW A319 SRM 51-42-11, REMOVED 4 EA SPLICES IAW A319 SRM 51-42-11, INSTJul 31, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145653115Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 FR66 - FR66 CORRODED. BLENDED AREA IAW A319 SRM 51-74-00 L=3.10" W=1.80" D=0.065 FOUND TO BE OUT OF LIMITS IAW A319TRM 53-41-15 RECEIVED NEW FLOORBEAM P/N 5347218920200. INSTALLED NEW FLOORBEAM IAW A319 SRM 51-42-11.Jul 31, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145643115Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM -Y1292 FR64 TO FR66 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00 L=3.50" W=1.20" D=0.069 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. RECEIVED NEW FLOORBEAM P/N 5347219021100 INSTALLED NEW FLOOR SUPPORT BEAM IAW A319 SRJul 31, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145563115Floor Support · corrodedFWD CABIN FLOOR SUPPORT BEAM +Y1292 AT FR16 CORRODED. REMOVED CORR IAW A319 SRM 51-74-00. REMOVED FLOOR SUPPORT BEAM AT +Y1292 IAW A319 SRM 51-42-11. LOCATED & DRILLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51-44-11. TRANSFERRED 12 EA BRACKETS FROM OLD SUPPOJul 31, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1146043115Floorboard · delaminatedFWD CABIN FLOORBOARD 231FF IS DELAMINATED. FWD CABIN FLOOR PANEL 231FF FABRICATED NEW ON STAM TRAVELER T11/890811 IAW DWG 3D25-40640. ORIG MAT: 0.400" DAMAGE DIM: L=2.5" W=1.9" D=0.25.Jul 30, 2011 · N315NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1145633115Profile · corrodedAFT CARGO SEALING PROFILE AT FR58 HAS CORROSION FROM S41R TOS38L. BLENDED CORRODED AREA SEALING PROFILE AT FR58 IAW 319 SRM 51-74-00 L=6.0, W=2.5, D=.026 ORIG MAT .039 OUT OF LIMITS IAW A319 SRM 53-00-14, REMOVED IAW A319 SRM 51-42-11 RECEIVED NEW PART D53974Jul 30, 2011 · N315NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1145623115Floor Panel · delaminatedAFT PIT FLOOR PANEL 151ZG IS DELAMINATED, 2 AREAS OF 3" X 3". AFT CARGO PIT FLOOR PANEL 151ZG FABRICATED NEW ON STAM TRAVELER T11/890400 IAW DWG 3D25-40532.Jul 30, 2011 · N315NB · Airbus A319114 · Fuselage Floor Panel
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