N319NB

Service difficulty reports · 283

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 = 'N319NB' 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 DALA2019110706457Pressure Panel · crackedERA 582759-14AD SECTION I ISSUED FOR CRACK INDICATIONS FOUND DURING WORKCARD 5311-01171-04 INSPECTION OF FR35-36 PRESSURE PANEL. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION PRIOR TO THE EARLIER OF 57000 FLIGHT CYCLES OR 114000 FLIGHT HOURS FROMNov 6, 2019 · N319NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019102306107Door · missingPDA PART DEPARTING AIRCRAFT. A/C 3119 CLOSED LOG 5949432 FLT/CHK 2942. CDL 52-00-21 ADD DATE: 23SEP19 STA: LAX. BLUE HYDRAULIC ACCESS DOOR MISSING ON ARRIVAL INTO LAX. INSTALLED BLUE HYD ACCESS DOOR PER A319 AMM 52-41. DOOR ASSY P/N D5347508401200, STK # 09-52Sep 23, 2019 · N319NB · Airbus A319114 · Service DoorsSDR DALA2019022761271Doubler · detachedON ARRIVAL FOUND NR 1 ENGINE PYLON THUMBNAIL FAIRING DETACHED. CORR BY FANTA 00608873 SEA 19FEB19 ATA 5433. INSTALLED THUMBNAIL PANEL PER A319 AMM 54-22 AND COMPLETED PHASE 1 INSPECTION PER A319 AMM 05-51. NO DAMAGE NOTED.Feb 19, 2019 · N319NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2018102806347Power Supply · inoperativeFOUND RT EMERGENCY LIGHT POWER SUPPLY UNIT INOP. REPLACED RT EMERGENCY LIGHT POWER SUPPLY UNIT.Oct 27, 2018 · N319NB · Airbus A319114 · Emergency LightingSDR DALA2018080704895Trunnion · damagedFOUND THE LEFT INBD FLAP TRUNNION DAMAGED, REPLACED THE TRUNNION FITTING IAW AMDS 2750-6010-LT AND CMM 57-52-21.Aug 6, 2018 · N319NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2018031401703Wire · shortedEMERGENCY LIGHTS INOPERATIVE AT ROWS 1 AND 2, ON THE SEATS, REPAIRED A SHORTED WIRE IAW SWPM 20-10.Mar 13, 2018 · N319NB · Airbus A319114 · Light System WiringSDR DALA2017121408671Skin · crackedCRACKED EXTERNAL SKIN OF THE AFT LOWER CORNER OF THE LT AFT PASSENGER DOOR, PERFORMED A REPAIR IAW SRM 52-10-00-300-003.Dec 13, 2017 · N319NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2017121408670Skin · crackedCRACKED EXTERNAL SKIN LOCATED AFT LOWER CORNER FWD PASSENGER DOOR RT SIDE. REPAIRED THE SKIN IAW SRM 52-10-00-300-003.Dec 13, 2017 · N319NB · Airbus A319114 · Service DoorsSDR DALA2017121308669Shear Tie · corrodedCORROSION ON THE SHEAR TIE AT FR 55 BETWEEN STRINGERS 42L TO 43L IN THE AFT CARGO COMPARTMENT, REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DRAWING D53476342.Dec 12, 2017 · N319NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2017120508449Floor Support · corrodedCORROSION FLOOR BEAM +Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM +Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM A319 51-72-11 AND DWG #D53112812Dec 4, 2017 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017120508448Floor Support · corrodedCORROSION FLOOR BEAM +Y1292 LOC FROM FR64 TO FR66 AT AFT GALLEY AREA. REPLACED FLOOR BEAM +Y1292 LOC. FROM FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG#D53472000Dec 4, 2017 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017120508447Floor Support · corrodedCORROSION FLOOR BEAM -Y765 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y765 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWGS #D53112812Dec 4, 2017 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017120308446Floor Support · corrodedCORROSION FLOOR BEAM -Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG# D53112812Dec 2, 2017 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017120208445Dummy Rail · corrodedCORROSION RAIL DUMMY Y503.2 LOC. FR12 TO FR16 AT FWD GALLEY AREA, REPLACED RAIL DUMMY Y503.2 LOC. FR12 TO FR16 AT FWD GALLEY AREA AS PER SRM 51-42-11 AND DRAWING D53112826Dec 1, 2017 · N319NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017120208444Floor Support · corrodedCORROSION FLOOR BEAM +Y765 FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM +Y765 FROM FR22 TO FR24 AT FWD GALLEY AREA AS PER SRM A319 51-72-11Dec 1, 2017 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2015122507768Power Supply · inoperativeEMERGENCY EXIT SIGNS ABOVE RT OVERWING DOOR AND CEILING WILL NOT ILLUMINATE. REPLACED EPSU W/O BATTERY AT RT OVERWING EXIT.Dec 24, 2015 · N319NB · Airbus A319114 · Emergency LightingSDR DALA2015122207698Power Supply · inoperativeINOPERATIVE, 12WL, EPSU IN PASSENGER CABIN, REPLACED EPSU.Dec 17, 2015 · N319NB · Airbus A319114 · Emergency LightingSDR DALA1704473119Floor Panel · delaminatedDELAMINATED FLOOR PANEL 261BG AT AFT GALLEY AREA.Dec 16, 2015 · N319NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13068353119Wire Harness · damagedROW 4 + 6 EMERGENCY IN-SEAT LIGHTS ARE INOPERATIVE. REPLACED DAMAGED HARNESS IN ROWS 4 AND 6. OPS CHECKED GOOD IAW AMM 33-51.Dec 10, 2013 · N319NB · Airbus A319114 · Light System WiringSDR DALA13046513119Battery Pack · inoperativeDURING EMERGENCY LIGHT TEST. EPSU EMERGENCY RT FAULT. R & R THE EPSU BATTERY. OPS CHECKED GOOD. EMERGENCY LIGHT TEST PASSED. ALL MX COMPLETED IAW AMM 33-51-38. ACFT OK FOR SERVICE.Sep 21, 2013 · N319NB · Airbus A319114 · Emergency LightingSDR DALA13025863119Charger · inoperativeEMERGENCY LIGHTS TEST FAIL EPSU UNIT AFT L MESSAGE. REPLACED CHARGER, CHECKED GOOD REF AMM 33-51 EPSU, WITH OUT BATTERY .May 25, 2013 · N319NB · Airbus A319114 · Emergency LightingSDR DALA13024343119Wire Harness · inoperativeEMERGENCY LIGHT AT SEAT C4 INOPERATIVE. REPAIRED SEAT HARNESS AT SEAT C4. OP'S CHECKED GOOD. OK FOR SERVICE.May 21, 2013 · N319NB · Airbus A319114 · Light System WiringSDR DALA13023913119Lanyard · damagedDOOR 1 LT SLIDE DISARM PIN LANYARD DAMAGED.May 15, 2013 · N319NB · Airbus A319114 · Escape SlideSDR DALA13012293119Wire Harness · inoperativeSEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 15. R & R EMERGENCY LIGHT PIGTAIL HARNESS. OPS CHECKED GOOD. OK FOR SERVICE.Mar 18, 2013 · N319NB · Airbus A319114 · Light System WiringSDR DALA13004643119Wire Harness · brokenEMERGENCY EXIT LIGHT (RED) AT 9C INOPERATIVE. FOUND WIRE HARNESS UNDER SEAT BROKEN. REPAIRED BROKEN WIRE BY INSTALLING BUTT SPICE. PERFORMED OPS CHECK. CHECKS GOOD.Jan 26, 2013 · N319NB · Airbus A319114 · Light System WiringSDR DALA12010593119Wire · unsecureSEAT 19A LOOSE CABLES/WIRES. STOWED AND SECURED SEAT 19A EMERGENCY LIGHT WIRING AS REQUIRED. ACFT OK FOR SERVICE.Oct 18, 2012 · N319NB · Airbus A319114 · Light System WiringSDR DALA1219263119Sill · bentFOUND FORWARD CARGO COMPT DOOR SILL WEB AND INTERCOSTAL BENT BETWEEN FR26 - FR27 APPROX STR 41R. REMOVED WEB IAW A319 SRM 51-42-11. RECEIVED NEW WEB IAW A319 SRM 53-21-13. LOCATED AND DRILLED NEW WEB IAW A319 SRM 51-44-11. TREATED AND PRIMED NEW WEB IAW A3Mar 27, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219233119Epsu · faultyAIRCRAFT 3119. OVERWING EMERGENCY EXIT SIGNS FLASH WHEN TURNED ON. REMOVED AND REPLACED EPSU PER AMM. OPERATIONAL CHECK WAS GOOD.Mar 26, 2012 · N319NB · Airbus A319114 · Emergency LightingSDR DALA1219213119Floor Support · corrodedAFT CARGO COMPT BETWEEN FR64 TO FR65 STGR 44 VERTICAL FLOOR SUPPORT CORRODED. SSI 534107. BLENDED FLOOR SUPPORT DAMAGE DIM L=1.5" X W=.8" X D=.015 OUT OF LIMITS. REMOVED AND REPLACED NEW PROFILE FORCE SUPPORT IAW A319 SRM 51-42-11.Mar 26, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217173119Floor Support · corrodedMAIN CABIN FR16 FLOOR SUPPORT WEB -Y1732 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00 MAT THICKNESS. .70" L=1.3" W=1.0" D=.033". NO ESTABLISHED LIMITS. REMOVED AND REPLACED FLOOR SUPPORT WEB -Y1732 IAW A319 SRM 51-42-11.Mar 18, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217063119Crossbeam · damagedMAIN DECK FWD UTILITY AREA AT Y1732 FRAME 23 CROSS BEAM UPPER FLANGE LWR SURFACE HAS START DRILLED DAMAGE SSI 531189. REMOVED DAMAGED CROSSBEAM IAW A319 SRM 53-00-14FIG 203. FABRICATED NEW PARTS (CROSSBEAM AND COUPLING), INSTALLED CROSSBEAM AND COUPLING IAW Mar 15, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215843119Support Fitting · gougedFWD CARGO DOOR SILL SUPPORT FITTING 2ND FROM FWD HAS GOUGE. BLENDED AREA IAW A319 SRM 51-73-00.L=.150" W=.120" D=.030". NO ESTABLISHED LIMITS PER A319 SRM 53-26-00. REMOVED, REPLACED AND INSTALLED NEW FITTING IAW A319 SRM 51-42-11. STRINGER 645112 BFM.Mar 13, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215813119Fitting · corrodedLEFT AFT DOOR LOWER AFT CORNER FITTING CORRODED. SSI 534147. BLENDED CORRODED AREA IAW A319 SRM 51-74-00 L=1.20" W=0.750" D=0.040". NO LIMIT ESTABLISHED FOR THE AREA. REMOVED AND REPLACED AFT CORNER FITTING IAW A319 SRM 51-42-11.Mar 12, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215803119Sill · corrodedRIGHT AFT DOOR THRESHOLD SILL FR 66 TO FR 68 UPPER SURFACE CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00, DIMENSION OF OVERSIZE HOLE AFT INBD W=.500 X L=.850. FWD INBD W=.550 X L=.800 FOUND OUT OF LIMITS IAW A319 TRM 53-41-13 FIG.1 SHT 3DETAIL II. REMOVEMar 12, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215783119Floor Support · corrodedMAIN CABIN FR20 FLOOR SUPPORT WEB Y1732 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00 DIMENSION L=1" W=1" D=.015". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14. RECEIVED NEW REPLACEMENT PART. REMOVED WEB IAW A319 SRM 51-42-11. LOCATED AND DRILLED Mar 12, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215303119Floor Support · corrodedAFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR64 TO FR66 -Y1292 UPPER BEAM SURFACE CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 L=3.0", W=1.0" D=0.035". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM Mar 11, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215113119Floor Support · corrodedAFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR 66 Y765 UPPER AND LOWER SURFACE HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00. L=2"W=1" D=.040". FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. REMOVED FLOOR SUPPORT Y765 FROM FR64 - FR66. REMOVED 4EA SPLMar 11, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215103119Hinge Fitting · corrodedR2 DOOR AFT CORNER FITTING FR 68 CORRODED. REMOVED AND REPLACED 1 EA AFT CORNER FITTING AT R2 DOOR FR68 IAW A319 SRM 51-42-11. DAMAGE DIM L=.350" W=.200" D=.030".Mar 10, 2012 · N319NB · Airbus A319114 · Fuselage, Door HingeSDR DALA1215093119Floor Support · corrodedAFT UTILITY AREA CABIN FLOOR SUPPORT AT FR66 TO FR70 Y765 UPPER FLANGED CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 OUT OF LIMITS IAW A319 SRM 51-41-15. REMOVED FLOOR SUPPORT Y765 FR66-FR70 IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT BEAM Y765 Mar 10, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215033119Floor Support · corrodedCABIN FLOOR SUPPORT AT FR 66 Y1292 UPPER FLANGE SURFACE HOLE CORRODED. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECK DIMENSION L=1.700",W=1.100",D=.055" FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. TR INSTRUMENT 17451. REMOVED FLOOR SUPPORMar 10, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215003119Floor Support · corrodedCABIN FLOOR SUPPORT AT FR 66 TO FR 68 Y1292 UPPER AND LOWER FLANGE CORRODED. SSI 534147. REMOVED CORROSION IAW A319 51-74-00. CHECK DIMENSIONS L=1.500" W=1.300"D=.043". FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15, TR INSTRUMENT 17451, Y1292 FR 66 TMar 10, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1214993119Floor Support · corrodedCABIN FLOOR SUPPORT AT FR 68 TO FR 69 Y1292 UPPER FLANGE SURFACE BEAM CORRODED. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECK DIMENSIONS L=1.300" W=1.300"D=.014". FOUND TO BE WITHIN LIMITS IAW A319 TRM 53-41-15. TREATED AND PRIMED ARMar 10, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1214983119Floor Support · corrodedAFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR66 TO FR68 -Y1292 UPPER AND LOWER HOLES SURFACE CORRODED. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00 L=1.05" W=1.0" D=0.040". FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACEMar 10, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1214973119Floor Support · corrodedAFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR68 TO FR 69 -Y1292 UPPER FLANGE BEAM CORRODED AND SEVERAL RIVETS BROKEN. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00 L=2.05",W=1.05 D=0.045-. FOUND TO BE OUT OF LIMITS IAW A319 SRM 5341-15. REMOVED ANMar 10, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1214433119Floor Support · corrodedMAIN CABIN BTW FR18 AND FR20 FLOOR SUPPORT -Y254 HAS CORROSION AS MARKED. REMOVED CORROSION IAW A319 SRM 51-74-00, NO ALLOWABLE LIMITS. INSTALLED NEW BEAM IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.Mar 8, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1214423119Floor Support · corrodedMAIN CABIN BTW FR20 AND FR21 SEAT TRACK -Y765 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. DIM. L=.50" W=.30" D=.14-0", ORIG THICK. .147". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 102. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11Mar 8, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1214403119Floor Panel · puncturedFWD CARGO COMPARTMENT SLOPE PANEL 132DG HAS MULTIPLE PUNCTURES. FABRICATED NEW SLOPE PANEL 132DG IAW DWG# 3D25-40532. DAMAGE DIA. L=2.0" X W=2.0".Mar 7, 2012 · N319NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1214383119Floor Panel · puncturedFWD CARGO COMPARTMENT SLOPE PANEL 132EG HAS PUNCTURES. FABRICATED NEW SLOPE PANEL 132EG IAW DWG# 3D25-40532. DAMAGE DIA. L=4.5" X W=3.5".Mar 7, 2012 · N319NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1214373119Floor Panel · puncturedFWD CARGO COMPARTMENT SLOPE PANEL 131DG HAS PUNCTURES. FABRICATED NEW SLOPE PANEL 131DG IAW DWG# 3D25-40532. DAMAGE DIA L=3.75" X W=4.0". RETAIN FOR RECORDS.Mar 7, 2012 · N319NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1214363119Floor Support · corrodedFLOOR SUPPORT AT FR65 TO FR67 -Y583 SEVERAL HOLES POINT CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO LIMITS FOR ALLOWABLE DAMAGE. REMOVED AND REPLACED NEW FLOOR SUPPORT IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.Mar 7, 2012 · N319NB · Airbus A319114 · Fuselage Miscellaneous Structure
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