N371NW

Service difficulty reports · 185

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 = 'N371NW' 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 DALA12009813271Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261FF DAMAGED. REPLACED FLOOR PANEL IAW SRM 5172-11.Oct 9, 2012 · N371NW · Airbus A320212 · Fuselage Floor PanelSDR DALA12009803271Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CABIN UTILITY FLOOR PANEL 232DF IS DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.Oct 9, 2012 · N371NW · Airbus A320212 · Fuselage Floor PanelSDR DALA12009793271Floor Panel · damagedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221DF HAS DAMAGED INSERT. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.Oct 9, 2012 · N371NW · Airbus A320212 · Fuselage Floor PanelSDR DALA12009783271Floor Panel · damagedDURING INSPECTION, FOUND CTR CABIN FLOOR PANEL 242FF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.Oct 9, 2012 · N371NW · Airbus A320212 · Fuselage Floor PanelSDR DALA12009773271Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261BG HAS DAMAGED EDGE. FABRICATED FLOOR PANEL IAW DWG 3D25-37498. DAMAGE DIM. L=2.0" W=1.0".Oct 9, 2012 · N371NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12009743271Floor Support · corrodedDURING INSPECTION, FOUND AFT B UTILITY LT DOOR SILL HAS CORROSION ON FLOOR SUPPORT SECTION AT FR66. LT AFT DOOR SILL REPAIR AT FR66 HAS BEEN ACCOMPLISHED IAW ER/A 506755-14, REV ORIG SECTION I PERMANENT REPAIR & SRM 53-41-14 FIG 201 REPAIR PRINCIPLE 6. THIS Oct 8, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009593271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY -Y1292 FLOOR SUPPORT BETWEEN FR 66 AND 68 HAS CORROSION AROUND FASTENERS AND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT .087" DAMAGE " W=0.3" =.037" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, FIG 1. ROct 7, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009583271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY -Y1292 FLOOR SUPPORT BETWEEN FR 64 AND 66 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMIT. REPLACED FLOOR SUPPORT IAW TO SRM 51-42-11.Oct 7, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009573271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY -Y1292 FLOOR SUPPORT BETWEEN FR 69 AND 69 IS CORRODED AROUND FASTENERS. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT .157" DAMAGE DIM L=1.9" W=0.7" D=.051" FOUND TO BE OUT OF LIMITS IAW TRM53-41-15, FIG 1. REPLACED FLOOR Oct 7, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009473271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY Y1292 FLOOR SUPPORT HAS EXFOLIATION AROUND HARD POINT MOUNT HOLE BETWEEN FR 64 AND FR 66. REPLACED FLOOR SUPPORT AT FR 64- FR 66 Y1292 IAW SRM 51-42-11. ORG MAT. .087" MAT LOSS L=4.0" W=1.5" D=.087" FOUND TO BE OUT OF LIMIOct 6, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009463271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY Y1292 FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AND UPPER SURFACE BETWEEN FRAME 66 AND 68. REPLACED FLOOR SUPPORT AT FR 66 - FR 68 Y1292 IAW SRM 51-42-11, ORG MAT .087" MAT. LOSS L=1.0" W=1.0" D=.036". FOUND TO BEOct 6, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009453271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY Y1292 FLOOR SUPPORT HAS CORROSION AROUND FASTENERS AND FASTENER HOLES BETWEEN FR 68 AND 70. SSI 534147.NR 260-83. REPLACED FLOOR SUPPORT AT FR 68 AND 70 Y1292 SRM 51-42-11, ORG MAT .157" MAT.LOSS L=1.0 W=1.0 .064 FOUND TO Oct 6, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009433271Web · corrodedDURING INSPECTION, FOUND AFT UTILITY RT SIDE WEB BETWEEN FR 68 AND FR 69 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. L=0.5", W=0.5", D=0.020". NO ALLOWABLE LIMITS FOUND IN SRM. REPLACED SHEAR TRAY IAW SRM 51-42-11.Oct 6, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009563271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY -Y465 FLOOR SUPPORT HAS 4 AREAS WITH HEAVY CORROSION BETWEEN FR 64 AND 67. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS AFTER REWORK. ORIG MAT. .149" DAMAGE DIM. L=1.1" W=1.0" D=.040" IAW SRM 53-00-14, Oct 4, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009293271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY -Y765 FLOOR SUPPORT HAS 4 LARGE AREAS OF EXFOLIATION BETWEEN FR66 AND 70. BLENDED AREA IAW SRM 51-74-00, DIM OF BLENDOUT AREA, ORIGINAL MAT. 0.157" L=1.25" W=1.1" D=0.065 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15, FIG 1Oct 3, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009283271Sill · corrodedDURING INSPECTION, FOUND R2 DOOR CUT OUT CENTER SHAPE SILL CORRODED. REMOVED CORROSION IAW SRM 51-74-00. DIMENSION OF REWORKED AREA ORIGINAL MAT. 0.100 L=1.65" W=0.600" D=0.030" NO ALLOWABLE DAMAGE FOUND IN THE SRM. REPLACED SHAPE SILL IAW SRM 51-42-11.Oct 3, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009303271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FR 20 FLOOR SUPPORT -Y765 HAS CORROSION. BLENDED CORROSION IAW SRM 51-74-00.L=2.0 W=1.060 D=0.079. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Oct 2, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009203271Shear Plate · corrodedDURING INSPECTION, FOUND AFT UTILITY RT SHEAR PLATE SUPPORT BETWEEN FR69 AND FR70 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00, DIM OF BLENDED OUT ARE: L= 1.5" W=1.0" D=0.020" NO ALLOWABLE LIMITS FOUND IN SRM. REMOVED DAMAGED SHEAR PLATE SUPPORT IAW SRM 51-Oct 2, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009193271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FR20 FLOOR SUPPORT WEB -Y1732 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLEND SIZE:L=3.0" W=1.5" D=.035".NO LIMIT ON SRM. REPLACED FLOOR SUPPORT (WEB) PN D5311278520301 IAW SRM 51-42-11, SRM 51-Oct 2, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009183271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA BTW FR16 - FR21 FLOOR SUPPORT -Y254 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00(6PLS) BLEND SIZE 2"W X 6 "L X .025"D, 2.5"L X 2"W X .028"D, 3"L X 1.4"W X .012"D, 2.8"L X 1.2"W X .013"D, 1.3" X .8"X .0Oct 2, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009153271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FR16 -FR20 FLOOR SUPPORT Y1292 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED & DRILLED NEW FLOOR SUPPORT IAW SROct 2, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009073271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FR16 FLOOR SUPPORT Y940 HAS CORROSION. BLENDED FLOOR SUPPORT IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 106, REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-42-11.Oct 1, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009063271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FR 20 FLOOR SUPPORT Y765 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. R & R FLOOR SUPPORT IAW SRM 51-42-11.Sep 30, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009053271Floorbeam · corrodedDURING INSPECTIONS, FOUND AFT UTILITY Y765 HAS CORROSION AROUND HARD POINT MOUNT HOLE ABOVE FR66. REMOVED CORROSION IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REPLACED FLOORBEAM IAW SRM 51-42-11.Sep 30, 2012 · N371NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA12009043271Floor Support · corrodedDURING INSPECTIONS, FOUND MAIN CABIN FWD UTILITY AREA, FR 16-21 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 106. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Sep 30, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009033271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA BETWEEN FR 16-21 FLOOR SUPPORT HAS SEVERAL CORROSION. BLENDED DAMAGED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 102, REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11, INSTALLED NSep 30, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009143271Floor Support · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FLOOR SUPPORT CORRODED. BLENDED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 51-11-14 FIG 103. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Sep 29, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12009133271Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT HAS CORROSION. BLENDED AREAS IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.Sep 28, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA12008913271Floor Support · corrodedDURING INSPECTIONS, FOUND MAIN CABIN UTILITY AREA BTW FR 20-21 FLOOR SUPPORT -Y189 HAS CORROSION. BLENDED AREA L=2.0"W=1.0"& 0.150" FOUND OUT OF LIMITS IAW SRM 53-11-14. R & R FLOOR SUPPORT IAW SRM 51-42-11.Sep 28, 2012 · N371NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA1170603271Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT SEAT 8 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Dec 19, 2011 · N371NW · Airbus A320212 · Light System WiringSDR DALA1119923271Connector · unsecureDURING EMERGENCY LIGHT TEST FOUND SEAT 7C PATH LIGHT INOP. SECURED CONNECTOR AND TESTS OK.Mar 16, 2011 · N371NW · Airbus A320212 · Light System WiringSDR DALA105363271Wire Harness · damagedDURING TEST FOUND EMERGENCY AISLE LIGHT 23C INOP, WIRING HARNESS WAS REPLACED AND CHECKED OK.Mar 9, 2010 · N371NW · Airbus A320212 · Light System WiringSDR DALA103693271Wire · brokenDURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROW 1 & 2 INOPERATIVE. MX REPAIRED BROKEN WIRE AND OPS CHECK WAS NORMAL.Feb 13, 2010 · N371NW · Airbus A320212 · Light System WiringSDR DALA100783271Wire · looseDURING A NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT ROW 23 INOPERATIVE. MX RECONNECTED LOOSE WIRE AT LIGHT ASSY. OPS CHECK WAS GOOD.Jan 17, 2010 · N371NW · Airbus A320212 · Light System WiringSDR NWAA071173271Battery Pack · inoperativeDURING EMERGENCY LIGHT CHECK, FOUND RIGHT EMERGENCY EPSU BATTERY INOP. REPLACED RIGHT EMERGENCY EPSU BATTERY, OPERATES GOOD.Mar 26, 2007 · N371NW · Airbus A320212 · Emergency Lighting
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