N335NB

Service difficulty reports · 199

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 = 'N335NB' 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 DALA13018543135Floor Panel · puncturedCENTER CABIN FLOOR PANEL 251NF PUNCTURED & DELAMINATED L=10.0" X W=10.0". FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40640 AND SRM 53-02-00, FIG 209.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018533135Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 241GF DELAMINATED L=20.0" X 10.0". FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40640 AND SRM 53-02-00, FIG 209.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018523135Floor Panel · puncturedCENTER CABIN FLOOR PANEL 251GF PUNCTURED & DELAMINATED L=10.0" X W=12.0". FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40640 AND SRM 53-02-00, FIG 209.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018513135Floor Support · corrodedMAIN CABIN, RT AFT FLOOR SUPPORT FR66-FR68 HAS CORROSION AROUND FASTENER HOLES & SURFACES. -Y1292. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13018503135Floor Support · corrodedMAIN CABIN, RT AFT FLOOR SUPPORT FR64-FR66 -Y1292 FWD AND AFT AREAS HAS CORROSION AROUND FASTENER HOLES AND SURFACES. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13018493135Floor Support · corrodedMAIN CABIN LT AFT FLOOR SUPPORT BET FR66 & FR68 +Y1292 HAS CORROSION. BLENDED CORRODED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018483135Floor Support · corrodedMAIN CABIN FLOOR SUPPORT FR68 TO FR69 +Y1292 HAS CORROSION AROUND FASTENER HOLE. BLENDED CORRODED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018473135Floor Support · corrodedMAIN CABIN LT AFT FLOOR SUPPORT FROM FR64-FR66 HAS CORROSION AT AFT SURFACE, +Y1292. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-13. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 23, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13018463135Sill · corrodedLT AFT PASSENGER DOOR CUT OUT, DOOR SILL AFT CORNER FITTING HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. CHECKED LIMITS L=0.484 W=0.502" D=0.125". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-13. R & R AFT CORNER FITTING IAW SRM 51-42-11 AND DWG D53480505. REApr 22, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13018453135Floor Panel · damagedAFT UTILITY FLOOR PANEL 262EF DAMAGED 4" X 4". FABRICATED FLOOR PANEL IAW DWG 3D25-40640 AND SRM 53-02-00, FIG 209.Apr 22, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018443135Floor Panel · damagedAFT UTILITY FLOOR PANEL 261PF DAMAGED 2.5" X 2.5". FABRICATED FLOOR PANEL IAW DWG 3D25-40640 AND SRM 53-02-00, FIG 209.Apr 22, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018433135Floor Panel · damagedAFT UTILITY FLOOR PANEL 262HG DAMAGED 3" X 3". FABRICATED FLOOR PANEL IAW DWG 3D25-40640 AND SRM 53-02-00, FIG 209.Apr 22, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13018423135Blanking Plate · corrodedL2 DOOR AFT GIRT BAR FITTING BLANKING PLATE CORRODED & TEFLON JOINT MISSING. REMOVED CORROSION ON BLANKING PLATE IAW SRM 51-74-00. CHECKED LIMITS L=2.0" W=0.50" D=0.010" FOUND TO BE OUT OF LIMITS IAW SRM 53-12-00. RECEIVED NEW BLANKING PLATE PN:D534801590060Apr 22, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13018413135Sill · corrodedRT FWD PASSENGER DOOR CUT OUT, DOOR MID SHAPE SILL AFT AREA CORRODED. R & R SILL IAW SRM 51-42-11 AND DWG D53112198. REMOVED CORROSION IAW SRM 51-74-00. NO DAMAGE LIMITATION FOUND IN SRM.Apr 22, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13018403135Seat Track · corrodedMAIN CABIN RT, SEAT TRACK AT FR 20 -Y765 CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. R & R SEAT TRACK IAW SRM 53-21-01 AND DWG D53110900.Apr 22, 2013 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13021913135Skin · dentedDENT ON LT FUSELAGE BETWEEN S22-23L AFT OF L-1 DOOR LOWER AFT CUTOUT CORNER. PERFORMED DETAILED INSPECTION ON EXTERNAL SKIN OF DENTED AREA, NO CRACKS NOTED. HFEC INTERNAL AND EXTERNAL SKIN IAW NTM 51-10-08, NO DEFECTS NOTED. DENT FOUND TO BE WITHIN ALLOWABLEApr 19, 2013 · N335NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13018113135Seat Track · corrodedMAIN CABIN RT, SEAT TRACK FROM FR 16 TO FR 21 -Y1292 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14.Apr 19, 2013 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13019163135Skin · dentedTWO EXTERNAL SKIN DENTS FWD OF CAPTAIN`S WINDSHIELD. FOUND FWD DENT TO BE OUT OF LIMITS IAW SRM 53-11-11, PARG 4C, FIG 105. CUTOUT DAMAGED AREAS IAW SRM 53-11-11, FIG 210. HFEC CUTOUT AREA IAW NTM 51-10-08, NO CRACKS NOTED. FABRICATED REPAIR DOUBLER IAW SApr 18, 2013 · N335NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13018103135Floor Support · corrodedMAIN CABIN RT, FLOOR SUPPORT FR 16 TO FR 20 -Y254 HAS CORROSION. REMOVED DAMAGE AND CHECKED LIMITS L=2.0" W=1.5"D=.030". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 18, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017953135Web · corrodedMAIN CABIN RT,FLOOR WEB AT FR20 -Y1584 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=5.0" W= 1.5" D=0.022". NO ALLOWABLE LIMITS IN SRM. R & R FLOOR WEB IAW SRM 51-42-11 AND DWG NR D53114332. R & R ANGLE FITTING IAW SRM 51-42-11 FABRICAApr 18, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017943135Sill · corrodedLT FWD PASSENGER DOOR CUT-OUT, DOOR SILL MID SHAPE SILL AFT AREA HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. AFTER BLEND OUT, DIMENSION OF REWORK, L=1.15" W=1.0" D=0.030". NO ALLOWABLE LIMITS IAW SRM. R & R CENTER SHAPE SILL PN D5311219820006, IAW SRM Apr 18, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017933135Floor Support · corrodedLEFT MAIN CABIN FWD FLOOR SUPPORT FR16-FR20 +Y254 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. CHECKED LIMITS L=2.0" W=1.5" D=0.050". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. R & R FLOOR SUPPORT IAW TRM 53-21-01.Apr 17, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017923135Floor Support · corrodedMAIN CABIN LT AFT FLOOR SUPPORT FROM FR68 TO FR70 +Y254 HAS CORROSION AROUND FASTENER HOLES AT BOTH END. BLENDED AREA IAW SRM 51-74-00. DIM OF BLEND OUT ARE:L=2.0" W=1.0" D=0.027". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, REMOVED DAMAGED FLOOR SUPPORT IAWApr 17, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017913135Floor Support · corrodedMAIN CABIN, RT AFT FLOOR SUPPORT FROM FR67 TO FR70 HAS SURFACE CORROSION FR68, -Y464. BLENDED CORROSION IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102, L=1" W=1" D=.049". R & R FLOOR SUPPORT IAW SRM 51-42-11 IAW TRM 53-21-01, DWG D53472Apr 17, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017903135Web · crackedMAIN CABIN, RT AFT SUPPORT WEB BET FR 68 & FR 69 BEHIND DOOR SILL HAS CRACKED OF 5" LONG. R & R AFT SUPPORT WEB IAW SRM 51-42-11 AND DWG D534800192175.Apr 17, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017893135Structure · gougedLT PYLON PYRAMID AFT ALIGNMENT PINHOLE GOUGED. BLENDED DAMAGE AREA IAW SRM 51-73-00. CHECKED LIMITS DIMENSION; D1=0.030", D2=0.010", S1=0.0015" FOUND TO BE WITHIN LIMITS IAW SRM 54-51-18, FIG 105 (SHT-1). PERFORMED FPI IAW NTM 51-80-00 PT8 NO CRACK INDICATIApr 16, 2013 · N335NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA13017883135Structure · damagedLT PYLON PYRAMID CTR ALIGNMENT PIN HOLE GOUGED. BLENDED DAMAGE AREA IAW SRM 51-73-00. CHECKED LIMIT DIMENSIONS; D1=0.025", D2=0.015". S1=0.0018" FOUND TO BE WITHIN LIMITS IAW SRM 54-51-18, FIG 105 (SHEET 1). PERFORMED FPI IAW NTM 51-80-00 PT8 NO CRACK INDICApr 16, 2013 · N335NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA13017033135Floor Panel · damagedAFT UTILITY FLOOR PANEL 262FF DAMAGED 5" X 5". FLOOR PANEL REPLACED IAW SRM 51-72-11 AND SRM 51-72-11.Apr 16, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13017023135Floor Support · corrodedLEFT MAIN CABIN FWD FLOOR SUPPORT FR16 TO FR20 +Y1292 HAS SURFACE CORROSION. BLENDED AREA IAW SRM 51-74-00. CHECKED LIMITS L=2.0" W=1.0" D=0.05". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 16, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13017013135Floor Panel · damagedAFT UTILITY FLOOR PANEL 261FF DAMAGED 4" X 4". FLOOR PANEL REPLACED IAW SRM 51-72-00 AND SRM 51-72-11.Apr 16, 2013 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13016983135Floor Support · corrodedMAIN CABIN LT AFT FLOOR SUPPORT FROM FR64 TO FR68 +Y512 HAS CORROSION AT MID SURFACE. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53472815.Apr 15, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016743135Floor Support · corrodedLT MAIN CABIN FWD FLOOR SUPPORT FR16 +Y765 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Apr 13, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016733135Sill · corrodedLEFT AFT PASSENGER DOOR CUTOUT, DOOR SILL MID SHAPE SILL AFT AREA CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO LIMITS IAW SRM 53-41-79. R & R SHAPE SILL IAW SRM 51-42-11.Apr 13, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016723135Floor Support · corrodedMAIN CABIN, RT AFT FLOOR SUPPORT FROM FR 64-FR66 -Y765 HAS CORROSION AROUND FASTENER HOLES AT FWD AND AFT AREA. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11, TRM 53-21-01 AND DWG 17D5347200Apr 13, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016713135Floor Support · corrodedMAIN CABIN LT AFT FLOOR SUPPORT FR64 TO FR66 +Y765 HAS CORROSION AROUND FASTENER HOLES. BLENDED AREA IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53472815.Apr 13, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016703135Floor Support · corrodedMAIN CABIN LT AFT FLOOR SUPPORT FR66 TO FR70 +Y765 HAS CORROSION AT UPPER SURFACES. BLENDED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-1 AND DWG D53472815.Apr 13, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016693135Support · corrodedAFT CABIN BETWEEN FR 69-70, S23-24R UPPER AND LOWER SURFACE OF SHEAR PLATE SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-73-00. R & R SUPPORT IAW SRM 51-42-11.Apr 13, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016683135Blanking Plate · corrodedFWD CABIN PAX DOOR FR16 GIRT BAR FITTING BLANKING PLATE CORRODED. REMOVED DAMAGE IAW SRM 51-74-00. INSTALLED NEW BLANKING PLATE ON WC 2500-6601.Apr 12, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13016673135Seat Track · corrodedMAIN CABIN LT FLOOR SUPPORT DUMMY BEAM +Y503.2, FR 16 HAS CORROSION. BLENDED CORROSION IAW SRM 51-74-00, L=2.5", W=2.2", D=.083". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 106, ORIG MAT .149". R & R DUMMY RAIL IAW SRM 51-42-11.Apr 12, 2013 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13016663135Sill · corrodedMAIN CABIN, RT AFT DOOR SILL INBD END AT FR68 HAS CORROSION AROUND FASTENER HOLE. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101, CUT OUT DAMAGE IAW SRM 53-41-14, FIG 201, REP 5. FABRICATED REPAIR ANGLE AND TWO FILLERApr 11, 2013 · N335NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010353135Floor Panel · damagedAFT CARGO FLOOR PANELS HAVE SEVERAL SMALL HOLES. REPAIRED IAW SRM 53-02-00. OK FOR SERVICE.Oct 16, 2012 · N335NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000643135Floor Panel · damagedFORWARD CARGO FLOOR PANEL 131AF DAMAGED AND WORN. REPAIRED PER SRM 53-02-00/101.May 20, 2012 · N335NB · Airbus A319113 · Fuselage Floor PanelSDR DALA1214443135Wire · damagedAIRCRAFT 3135. SEAT 14C EMERGENCY SEAT LIGHT INOPERATIVE. REPAIRED WIRE PER A319 SWPM. OPERATIONAL CHECK WAS GOOD.Mar 9, 2012 · N335NB · Airbus A319114 · Light System WiringSDR DALA1022503135Connector · inoperativeDURING A NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT ROW 7C INOPERATIVE. MX INSTALLED NEW CONNECTOR AT SEAT HARNESS. FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Sep 12, 2010 · N335NB · Airbus A319113 · Light System WiringSDR DALA101683135Wire Harness · damagedEMERGENCY LIGHT SEAT 11C INOP, REPLACED DAMAGED WIRING HARNESS AND CHECKS OK.Jan 23, 2010 · N335NB · Airbus A319113 · Light System WiringSDR DALA13020853135Skin · damagedUPPER FUSELAGE BET FR12 TO FR15, STR 3R TO 2L FUSELAGE SKIN HAS LIGHTNING STRIKE ON SEVERAL AREAS. REPAIRED IAW ERA 490253-14 REV "O" SECTION II STEPS 1-3.Jul 6, 2009 · N335NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13020833135Skin · damagedUPPER FUSELAGE AT FR 12 APPROX AT STR 4L, 1EA RIVET HAS LIGHTNING STRIKE. REPAIRED IAW ERA 490253-14, REV "O" SECTION II STEPS 1-3.Jul 5, 2009 · N335NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13020823135Skin · damagedUPPER FUSELAGE 2.5" FWD OF FR 14 AT APPROX STR 4R FUSELAGE SKIN HAS LIGHTNING STRIKE. REPAIRED IAW ERA 490253-14 REV "O" SECTION III STEPS 1-3.Jul 1, 2009 · N335NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR 0600653135Power Supply · no testDURING A-CHECK, THE AFT EMERGENCY POWER SUPPLY UNIT TEST FAILED. REPLACED EPSU 31-3350-9-0001, S/N 04489 AND BATTERY PACK.Mar 31, 2006 · N335NB · Airbus A319114 · Emergency Lighting
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