N317NB

Service difficulty reports · 178

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 = 'N317NB' 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 DALA2021060103005Oxygen Mask · no testSHIP 3117 - WORKING WORK CARD 2527, MASK DROP SEAT 2C DID NOT DROP PER STEP 1. CORRECTIVE ACTION: AFTER INSPECTION AND REPACK PER STEP 4-13, OPS CHECK GOOD IAW WC 2527. (7330242)May 29, 2021 · N317NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2021010500048Anti-Ice Valve · faultedDE DECLARED AN EMERGENCY ON APPROACH DUE TO A WING ANTI-ICE SYSTEM FAULT WITH THE AIRCRAFT IN ICING CONDITIONS. CORRECTIVE ACTION: REPLACED THE LT WING ANTI-ICE VALVE.Jan 1, 2021 · N317NB · Airbus A319114 · Airfoil Anti/De-ice SystemSDR DALA2020092103139Power Supply · inoperativeON CHECK FOUND EPSU EMER L INOP. CORRECTIVE ACTION: R & R EPSU & BATT, IAW A319 AMM 33-51-38-0401. OPS TEST OK. OK FOR SERVICE.Sep 20, 2020 · N317NB · Airbus A319114 · Emergency LightingSDR DALA2019111706735Arming Lever · malfunctionedFA REPORTED DOOR 1L ARM LEVER POPPED UP INFLIGHT ILLUMINATED CABIN PRESS LIGHT, TWICE. PERFORMED OPS CHECK OF DOOR 1L OPENED CLOSED DOOR SEVERAL TIMES, ARM, DISARMED DOOR SEVERAL TIMES NO DEFECT NOTED DURING LEVER OPERATION ON BOTH SYSTEMS. PERFORMED OPS CHECKNov 16, 2019 · N317NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2019102906227Sensor · out of alignmentA/C 3117 CLOSED LOG 3995730 FLT/CHK 2089. ASHORTLY AFTER T/O, RCVD "DOOR R EMER EXIT" MSG ON ECAM. COMPLIED W/ ECAM /QRH PROC, NO ABNORMAL V/S INDICATION ON PRESS PAGE. CABIN PRESS NORMAL. FOUND SENSOR ON R EMERGENCY OVERWING DOOR TOP PANEL OUT OF ALIGNMENT. ROct 29, 2019 · N317NB · Airbus A319114 · Door Warning SystemSDR DALA2019102906226Proximity Switch · out of adjustA/C 3117 CLOSED LOG 3995728 FLT/CHK 2089. SHORTLY AFTER TAKE OFF RCVD DOOR L EMER EXIT MSG ON ECAM. COMPLIED WITH ECAM/QRH PROCEDURES. NO ABNORMAL VERTICAL SPEED INDICATION ON PRES PAGE. CABIN PRESSURE NORMAL. *** CONTRACT MAINTENANCE EVENT - OCM: 220350 *** AOct 28, 2019 · N317NB · Airbus A319114 · Door Warning SystemSDR DALA2019102806224Pressure Panel · crackedA CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. LIAISON ENGINEERING CORRECTIVE ACTION IS REQUIRED PRIOR TO FURTHER FLIGHT. HOLE #B17. AA 5311-01171 SB A320-53-1263 AD- 2018-06-04. REPAIRED PER PRIOct 27, 2019 · N317NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019102806223Pressure Panel · crackedA/C 3117 CLOSED LOG 1334310 FLT/CHK 3117. A CRACK THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. MODIFY IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT. HOLE # 8.AA 5311-01171Oct 27, 2019 · N317NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019102806222Pressure Panel · crackedFOUND HOLE A CRACKED DURING INSPECTION 5311-01171-02A OF PRESSURE PANEL HOLES FR35/36, CRACK RUNS FWD AND AFT OF HOLE A. REPAIR IAW AMDS 5311-01171-04A. REF. AA 5311-01171,SB A320-53- 1264 AND AD-2018-06-04. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 040-0001:5Oct 27, 2019 · N317NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019102806220Pressure Plate · crackedA CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. LIAISON ENGINEERING CORRECTIVE ACTION IS REQUIRED PRIOR TO FURTHER FLIGHT. HOLE # 20. AA 5311-01171 SB A320-53-1263 AD- 2018-06-04. REPAIRED PER PRIOct 27, 2019 · N317NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019102876221Clamp · broken#1 ENG. - OVER PRESSURE VALVE CLAMP BROKE THRU AND CRACKED LH T/R COWL WEB AT 11:30 POS. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0233:7100-3010-LT/ 002 00127 CLOCKED CLAMP ON OVER PRESSURE VALVE, REF. NR 209. INSTALLED OVERHAULED THRUST REVERSER COWL (P/Oct 26, 2019 · N317NB · Airbus A319114 · Engine Thrust ReverserSDR DALA2019061093466Line · damagedHYD B RSVR LOW LEVEL IN CRUISE FLIGHT, BLUE ELEC PUMP PLACED OFF BEFORE QUANTITY REACHED ZERO. T/S FOUND BLUE HYDRALIC PUMP RETURN LINE DAMAGED CHAFED BY ADJACENT BRAIDED HYD HOSE. INSPECTED BRAIDED LINE, NO DAMAGE. REPOSITIONED HOSE FOR PROPER CLEARANCE. REMOJun 9, 2019 · N317NB · Airbus A319114 · Hydraulic System, MainSDR DALA2018060803913Sign · malfunctionedEMERGENCY EXIT FWD FACING MID CABIN EXIT SIGN INOP, CYCLED 1L EMERGENCY LIGHT SW. EXIT SIGN NOW CKS GOOD.Jun 7, 2018 · N317NB · Airbus A319114 · Emergency LightingSDR DALA2017111608207Angle · damagedELONGATED HOLE BRACKET ANGLE LOCATED ON FR 66 STR 9L IN PASSENGER CABIN, REPLACED BRACKET ANGLE LOC. ON FR66 STR 9L IN PASSENGER CABIN AS PER .SRM 51-72-11 AND DRAWING D53480062Nov 14, 2017 · N317NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017111108155Stringer · damagedELONGATED HOLES ON STRINGER 9L, FRAME 66. REPLACED THE STRINGER IAW SRM 51-72-11, DWG D534805050, AND D53474160Nov 11, 2017 · N317NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2017111008154Seat Track · corrodedCORRODED SEAT TRACK Y1292, FRAME 46+6 INCHES. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWG D53371112, AND DGW D53370500.Nov 9, 2017 · N317NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017110908153Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1225 BETWEEN FRAMES 66+5 AND 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND DRAWING D53472815.Nov 8, 2017 · N317NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017110908152Floor Support · corrodedCORRODED FLOOR SUPPORT -Y254, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND DRAWING #53111462Nov 8, 2017 · N317NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017110607991Frame Splice · crackedFRAME 68 CRACKED ON THE SPLICE CONNECTION AT STRINGER 24L, REPLACED THE FRAME SPLICE IAW SRM 51-42-11 AND DRAWING D53474250.Nov 5, 2017 · N317NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2017110508151Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1162.5, BETWEEN FRAMES 67+17" TO 69+4", REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472815.Nov 4, 2017 · N317NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017110507990Floor Support · corrodedCORRODED FLOOR SUPPORT -Y1162, FRAMES 67-69, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Nov 4, 2017 · N317NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017110607993Floorbeam · corrodedCORRODED FLOORBEAM -Y1225. REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND DRAWING D53472780.Nov 3, 2017 · N317NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2017110607992Floorbeam · corrodedCORRODED FLOORBEAM -Y1292, FR65 + 22 INCHES IN THE AFT GALLEY AREA, REPLACED THE FLOORBEAM IAW 51-42-11Nov 3, 2017 · N317NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2017110207917Seat Track · corrodedCORRODED SEAT TRACK -Y765 AT FRAME 20. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG D53110920.Nov 2, 2017 · N317NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017103107875Seat Track · corrodedCORROSION SEAT TRACK -Y1292 AT LEVEL OF FR20 AT FWD GALLEY AREA. REPLACED SEAT TRACK -Y1292 AND FASTENERS BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112812.Oct 30, 2017 · N317NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017110107916Dummy Rail · corrodedCORROSION ON THE DUMMY RAIL -Y189 AT FRAME 23. REPLACED THE DUMMY RAIL IAW SRM 51-72-11, AND DRAWING D53111406Oct 29, 2017 · N317NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017110107915Dummy Rail · corrodedCORROSION ON THE DUMMY RAIL Y503.2 AT FWD GALLEY AREA, REPLACED THE DUMMY RAIL IAW SRM 51-72-11, DRAWING D53110984 AND D53112825.Oct 29, 2017 · N317NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017103107876Floorbeam · corrodedCORROSION FLOORBEAM +Y254 AT FWD GALLEY AREA, REPLACED FLOORBEAM LOC +Y254 BTW FR12 TO FR24 FLOOR STRUCTURE FWD GALLEY AREA IAW SRM 51-72-11 AND DWG NR D53112816.Oct 29, 2017 · N317NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2017053104405Doubler · dentedDENT FOUND LEFT SIDE OF REAR ATG-4 DOUBLER PLATE. FABRICATED AFT ATG 4 REPAIR DOUBLER, FILLER COMPLIED WITH ER/A 559096-14.May 31, 2017 · N317NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2018052403544Structure · damagedWHILE ACCOMPLISHING FWD ATG4 DE-MOD PER GOGO DRAWING P19110-21402 REV B, THIRTY TWO (32) HOLES WERE FOUND TO BE OVERSIZED. ONE HOLE WAS REPORTED TO BE ON THE CHEM-MILL. REPAIR PER ER/A 559100-14.May 27, 2017 · N317NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017051303859Slide · faultedPSU EXT LOAD AFT L FAULT. REPLACED AFT RT EVAC SLIDE.May 12, 2017 · N317NB · Airbus A319114 · Escape SlideSDR DALA2017051103818Pressure Panel · crackedSIDE BOX BEAM FLANGE AT FRAME 43 HAD A CRACK INDICATION ON LT SIDE PRESSURE PANEL. REPLACED THE PRESSURE PLATE IAW AMDS CARD 5310-01450-02May 10, 2017 · N317NB · Airbus A319114 · Fuselage Main, BulkheadSDR DALA2017051103817Box Beam · crackedSIDE BOX BEAM FLANGE AT FRAME 43, HAS A CRACK INDICATION ON AFT FASTENER .250 HOLE. REPAIRED IAW AMDS 5310-01450-02.May 10, 2017 · N317NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2014080404300Battery Pack · faultedEPSU BATTERY FWD LT FAULT, TROUBLESHOT IAW TSM 33-51-00-810-802-A. REPLACED EPSU BATTERY IAW AMM 33-51-38. FAULT CLEARED, OK FOR SERVICE.Aug 4, 2014 · N317NB · Airbus A319114 · Emergency LightingSDR DALA14028653117Battery Pack · inoperativeLEFT AFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51. OPS CHECKED NORMAL.May 6, 2014 · N317NB · Airbus A319114 · Emergency LightingSDR DALA13054163117Battery Pack · malfunctionedEPSU BATTERY AFT LT FAILED DURING EMERGENCY LIGHT TEST. RESET EPSU BATTERY. TESTED OK.Oct 20, 2013 · N317NB · Airbus A319114 · Emergency LightingSDR DALA13030823117Connector · looseEMERGENCY ESCAPE LIGHT AT SEAT 5B INOPERATIVE. FOUND A LOOSE CONNECTION UNDER SEAT. OPS CHECKED GOOD.Jun 20, 2013 · N317NB · Airbus A319114 · Light System WiringSDR DALA13000853117Battery · faultedEMERGENCY LIGHTS CHECK FWD LT BATTERY FAULT. BITE CHECK EPSU FAULTS BATTERY. R & R BATTERY. CHECKED GOOD IAW AMM.Jan 11, 2013 · N317NB · Airbus A319114 · Emergency LightingSDR DALA1213343117Intercostal · crackedDURING NON ROUTINE CHECK, MAINTENANCE FOUND L2 DOOR MID FWD INTERCOSTAL HAS CRACKED APPROXIMATELY .5 INCHES. REMOVED L2 DOOR MID FWD INTERCOSTAL AND INSTALLED NEW PER SRM 51-42-11.Mar 3, 2012 · N317NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA1211383117Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 152WG PUNCTURED DAMAGED AREA MEASURES L=1.5" X W=1.0". N/R 150/34. FABRICATED FLOOR PANEL 152WG PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211343117Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 131CG DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 130/23. FABRICATED FLOOR PANEL 131CG PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211323117Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 161BF DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 150/21. FABRICATED FLOOR PANEL 161BF PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211313117Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152TG DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 150/20. FABRICATED FLOOR PANEL 152TG PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211303117Floor Panel · damagedFWD CARGO COMP FLOOR PANEL 131BF DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 130/19. FABRICATED FLOOR PANEL 131BF PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211293117Floor Panel · damagedAFT CARGO COMP FLOOR PANEL 151TG DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 150/18. FABRICATED FLOOR PANEL 151TG PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211283117Floor Panel · damagedAFT CARGO COMP FLOOR PANEL 161NF DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 150/17. FABRICATED FLOOR PANEL 161NF PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211213117Floor Panel · damagedAFT CARGO COMP FLOOR PANEL 151ZG DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 150/16. FABRICATED FLOOR PANEL 151ZG PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1211203117Floor Panel · damagedAFT CARGO COMP FLOOR PANEL 151VG DAMAGE BEYOND LIMITS IAW SRM 53-02-00. N/R 150/15. FABRICATED FLOOR PANEL 151VG PER DWG 3D25-40532. RETAIN FOR RECORDS.Feb 22, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1210153117Floor Panel · corrodedAFT CABIN ENTRY WAY FLOOR PANEL 262FF HAS CORROSION ON UNDER SIDE OF PANEL. FLOOR PANEL INSTALLED PER CARD NR 250/37.Feb 19, 2012 · N317NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1210143117Floor Support · corrodedAFT CABIN BETWEEN FR 66 & 68 FLOOR SUPPORT -Y1292 CORRODED. BLENDED AREA IAW SRM 51-74-00. CHECKED LIMITS L=5" W=3" D=.040". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Feb 18, 2012 · N317NB · Airbus A319114 · Fuselage Miscellaneous Structure
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