N311US, cancelled Sep 27, 2018

Service difficulty reports · 130

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 = 'N311US' AND deregistration_id = 'N311US-2018-09-27'
  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 DALA14028663211Battery Pack · inoperativeRT EMERGENCY LIGHT PACK BATTERY FAULTED. R & R BATTERY PACK IAW AMM 33-51. CHECKED NORMAL.May 5, 2014 · N311US · Airbus A320211 · Emergency LightingSDR DALA14021943211Light · damagedDURING NON-ROUTINE CHECK, FOUND 16 ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT AND LAMP HOLDER AT SEAT 16 ABC AND FUNCTIONAL CHECKED NORMAL.Apr 9, 2014 · N311US · Airbus A320211 · Emergency LightingSDR DALA13023993211Door · out of adjustAFT RT EMERGENCY OVERWING EXIT AMBER CAUTION LIGHT CAME ON, ON UPPER ECAM DURING FCF. AFT RT EMERGENCY OVERWING EXIT COVER FLAP ADJUSTED IAW AMM 52-21-11-700-050-B. OPS TEST GOOD.May 16, 2013 · N311US · Airbus A320211 · Emergency ExitsSDR DALA13022533211Epsu · failedDURING NON ROUTINE CHECK, FOUND POWER SUPPLY 13WL FAILED TEST. REMOVED EPSU 13WL IAW AMM 33-51-38-000-001-A. MX INSTALLED SERVICEABLE EPSU AT 13WL AND FUNCTIONAL CHECK WAS NORMAL.May 14, 2013 · N311US · Airbus A320211 · Emergency LightingSDR DALA13023973211Strut · wornLEFT FLAP INTERCONNECT STRUT HAS EXCESSIVE SIDE PLAY AND ACTUATING ROD WORN. REPLACED WITH NEW INTERCONNECTING STRUT ON LT FLAP IAW AMM 27-51-44, PB 401. ADJUSTMENT GOOD IAW AMM 27-51-44-820-001-A. TEST GOOD IAW AMM 27-51-44-710-056-A AND ACCOMPLISHED OPS TESMay 10, 2013 · N311US · Airbus A320211 · Trailing Edge FlapsSDR DALA13021713211Skin · damagedDURING INSPECTION, MX REPLACED FWD CENTER TITANIUM & RT FUSELAGE LATERAL SKIN PANEL BETWEEN FR1-FR 12 IAW ER/A 512316-14. REPLACED FWD CENTER TITANIUM SKIN IAW REPAIR DWG R5311269007 & RT FUSELAGE LATERAL SKIN PANEL FR 1-12 IAW REPAIR DWG R53112168000.May 9, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13021703211Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131GF HAS MULTIPLE DENTS AND SCRATCHES. FABRICATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.May 8, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13021693211Skin · damagedDURING INSPECTION, FOUND LT WING NR 3 SLAT TOP SKIN AT RIB OTBD OF TRACK NR 7 DENT IS OUT OF NEARNESS TO RIB & SPAR. NO ALLOWABLE LIMIT ON THIS AREA IAW SRM 57-40-00, FIG 102. CUT OUT DAMAGE IAW SRM 57-40-00, FIG 102. FABRICATED SKIN INSERT, BACKING PLATES.May 7, 2013 · N311US · Airbus A320211 · Leading Edge DevicesSDR DALA13021473211Web · gougedDURING INSPECTION, FOUND FWD CARGO THRESHOLD WEB HAS DEEP GOUGE 7" AFT OF FR26. REPLACED DAMAGED THRESHOLD WEB IAW DWG 53230315 & SRM 51-42-11.May 7, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13021463211Structure · corrodedDURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LOWER CURVE EDGE FWD TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM 52-20-00.May 7, 2013 · N311US · Airbus A320211 · Emergency ExitsSDR DALA13021453211Structure · corrodedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM 52-20-00.May 7, 2013 · N311US · Airbus A320211 · Emergency ExitsSDR DALA13021443211Structure · corrodedDURING INSPECTION, FOUND LEFT FWD EMERGENCY EXIT DOOR LOWER CURVE EDGE AFT TEE SECTION CORRODED. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM A32 0 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM A320 52-20-00.May 7, 2013 · N311US · Airbus A320211 · Emergency ExitsSDR DALA13021433211Structure · corrodedDURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM 51-20-00. ORIG MAT IS .078".May 7, 2013 · N311US · Airbus A320211 · Emergency ExitsSDR DALA13021683211Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131HF HAS MULTIPLE DENTS & SCRATCHES. FABRICTATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.May 6, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13020903211Hinge Fitting · damagedDURING INSPECTION, FOUND LT MLG DOOR FWD HINGE AFT LUG, INBD SIDE IS CHAFED. NO ESTABLISHED LIMITS IAW SRM 53-36-11, PAGE 101. REPLACED FITTING IAW DWG R53370500C & SRM 51-42-11.May 4, 2013 · N311US · Airbus A320211 · Fuselage, Door HingeSDR DALA13020913211Hinge Fitting · damagedDURING INSPECTION, FOUND LT MLG DOOR FWD HINGE, FWD LUG, FWD FACE HAS CHAFE DAMAGE, FITTING R & R IAW REPAIR DWG R53370500C & SRM 51-42-11.May 3, 2013 · N311US · Airbus A320211 · Fuselage, Door HingeSDR DALA13020893211Fitting · out of adjustDURING INSPECTION, FOUND RT SIDE OF FWD FUSELAGE BETWEEN FR3 - FR4 STATIC PORT FITTING REQUIRES REPLACEMENT. REMOVED STATIC FITTING IAW SRM 51-42-11. LOCATED AND DRILLED REPLACEMENT FITTING IAW DWG R53112169, SH 2, REV A INSTALLED FITTING IAW SRM 51-42-11 ANMay 3, 2013 · N311US · Airbus A320211 · Pitot/Static SystemSDR DALA13020613211Plate · corrodedDURING INSPECTION, FOUND AFT CARGO BAY CENTER SEALING PLATE CRACKED AROUND SCREW HOLE AND FITTING ATTACHMENT CORRODED. REMOVED SEALING PLATE AND TIE DOWN FITTING IAW SRM 51-42-11. FABRICATED NEW SEALING PLATE IAW DWG D53974839. INSTALLED NEW SEALING PLATE AMay 1, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13020253211Floor Panel · corrodedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132DF CORRODED AND GOUGED. REPLACED FLOOR PANEL IAW SRM 51-72-11.Apr 29, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13019423211Floor Support · bentDURING INSPECTION, FOUND AFT CARGO BAY FR 58-59 FLOOR SUPPORT BENT AT FWD CORNER & CORRODED AROUND SCREW HOLE. REMOVED CORROSION IAW 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REPLACED FLOOR SUPPORT IAW SRM 51-44-11 AND SRM 51-42-11, APPLIED TOP Apr 27, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13019413211Floor Panel · corrodedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 231AF HAS CORROSION ON HINGE AND PANEL. REPLACED FLOOR PANEL.Apr 27, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13019323211Skin · damagedDURING INSPECTION, FOUND LOWER FWD FUSELAGE EXTERNAL SKIN BETWEEN FR 26-27 S40R HAS TWO LIGHTNING STRIKES. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSPECTION OF ONE OPEN FASTENER HOLE IAW NTM 51-10-01 PT6 WITH NO INDICATIONApr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13019433211Web · damagedDURING INSPECTION, FOUND FWD FUSELAGE RT UPPER SPLICE SUPPORT WEB APPROX STR 4R BETWEEN FR 1 & FR 3 HAS SEVERAL TOOL MARKS. REPLACED RT UPPER SPLICE SUPPORT WEB IAW SRM 51-42-11. TOP COATED AREA IAW SRM 51-75-12.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13019403211Skin · damagedLOWER FWD FUSELAGE EXTERNAL SKIN BETWEEN FR26-27 STRGR 40R HAS 2EA LIGHTNING STRIKE. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSPECTION OF ONE OPEN FASTENER HOLE IAW NTM 51-10-01 WITH NO INDICATIONS NOTED. COLD WORKED FASTENEApr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13019393211Floor Panel · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF HAS CORROSION. REPLACED FLOOR PANEL IAW SRM 51-72-11.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13019383211Skin · damagedDURING INSPECTION, FOUND LOWER FORWARD FUSELAGE RT SIDE AT FR 30, STGR 39R EXTERNAL SKIN HAS LIGHTNING STRIKE. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSP OF 1EA OPEN FASTENER HOLE IAW NTM 51-10-01 WITH NO INDICATIONS NOTED.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13019373211Skin · damagedDURING INSPECTION, FOUND LOWER FWD FUSELAGE RT SIDE AT FR 30, S39R EXTERNAL SKIN HAS LIGHTNING STRIKE AS MARKED. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSPECTION OF ONE OPEN FASTENER HOLE IAW NTM 51-10-01 WITH NO INDICATIONApr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13019363211Floor Panel · damagedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 232DF HAS TWO BAD INSERTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13019353211Floor Panel · puncturedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AF HAS PUNCTURED 1" X 1". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13019343211Floor Panel · corrodedDURING INSPECTION, FOUND FLOOR PANEL 261FF HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-74-00, REPLACED FLOOR PANEL, IAW SRM 51-72-11.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13019333211Floor Panel · corrodedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF CORROSION ON LOWER SIDE. DAMAGE DIA L=6" X W=18" NO ALLOWABLE LIMIT ON SRM, REPLACED AFT CARGO FLOOR PANEL IAW SRM 51-72-11.Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13018973211Skin · gougedDURING INSPECTION, FOUND LOWER FUSELAGE 3IN FWD OF FR51 AND ONE INCH BELOW STRG 41L HAS SKIN GOUGE. BLENDED AREA IAW 51-73-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11, FIG 101, MATERIAL LOSS IS MORE THAN 25 PERCENT OF THICKNESS. PERFORMED EXTERNAL DOUBLApr 24, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13017803211Skin · crackedDURING INSPECTION, FOUND LWR AFT FUSELAGE LAV VENT, FUSELAGE SKIN BETWEEN STGR 29R AND STG R 30R, BETWEEN FR69 AND FR70 HAS CRACK ON SKIN NEXT TO VENT. CUT OUT DAMAGE SKIN, FABRICATED 1EA REPAIR DOUBLER FROM 2024-73 .071"C & 2 EA FILLERS FROM 2024-73 .063"C, Apr 18, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13017763211Skin · crackedDURING INSPECTION, FOUND LWR AFT FUSELAGE LAV BENT, FUSELAGE SKIN BETWEEN STGR 29R AND STGR 30R, BETWEEN FR69 AND FR70 HAS CRACK ON SKIN NEXT TO BENT. CUT OUT DAMAGE SKIN, FABRICATED REPAIR DOUBLER & TWO FILLERS, LOCATED & DRILLED PARTS IAW SRM 53-41-11, FIGApr 17, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13017753211Skin · dentedDURING INSPECTION, FOUND LT SIDE OF FWD FUSELAGE AT FR15 WHERE DOOR STOP TOUCHES ACFT SKIN DENT IS OUT OF NEARNESS TO FRAME. DENT FOUND FWD OF FRAME 15 BETWEEN STR 19 & 20 NO ALLOWABLE DAMAGE IAW SRM 53-11-11, FIG 201. CUT-OUT DAMAGE AREA IAW SRM 53-11-11, FApr 16, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13017743211Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017733211Floor Panel · damagedDURING INSPECTION, FOUND FLOOR PANEL 261PF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017713211Floor Panel · puncturedDURING INSPECTION, FOUND FLOOR PANEL 262AB HAS NUMEROUS PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017693211Floor Panel · delaminatedDURING INSPECTION, FOUND FLOOR PANEL 261DF IS DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017683211Floor Panel · corrodedDURING INSPECTION, FOUND FLOOR PANEL 262EF HAS CORROSION. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017673211Floor Panel · puncturedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 232FF HAS PUNCTURE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017663211Floor Panel · crackedDURING INSPECTION, FOUND FWD UTILITY AREA FLOOR PANEL 232MF IS CRACKED 12 INCHES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017653211Floor Panel · corrodedDURING INSPECTION, FOUND FLOOR PANEL 261EF CORRODED IN SEVERAL PLACES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017643211Floor Panel · puncturedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AB HAS TWO PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498 .Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017203211Seat Track · corrodedDURING INSPECTION, FOUND FORWARD CABIN SEAT TRACK BETWEEN FR 20-24, Y-1292. SEAT TRACK CROWN AND UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. REPLACED SEAT TRACK IAW SRM 51-42-11.Apr 14, 2013 · N311US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13017783211Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131CF PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017543211Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131BF CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017533211Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131KF HAS MULTIPLE DENTED & CRACKED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017523211Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF HAS MULTIPLE DENTS & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017513211Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162BF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel
Back to N311US, cancelled Sep 27, 2018