N315US, cancelled Jan 24, 2018

Service difficulty reports · 105

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 = 'N315US' AND deregistration_id = 'N315US-2018-01-24'
  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 DALA2017031302068Lens · missingFLOOR EMERGENCY LIGHT AT SEAT 11C RED LENS MISSING, REPLACED THE BULB AND LENS.Mar 12, 2017 · N315US · Airbus A320211 · Emergency LightingSDR DALA2017031001941Wire · brokenROW 9 EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE.Mar 9, 2017 · N315US · Airbus A320211 · Light System WiringSDR DALA2017020801180Bulb · inoperativeR2 DOOR EMERGENCY LIGHT SIGN ABOVE DOOR, ONE BULB INOPERATIVE, REPLACED THE BULB.Feb 8, 2017 · N315US · Airbus A320211 · Emergency LightingSDR DALA2016122210072Compressor · seizedHAD AN ACRID ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE WATER SYSTEM AIR COMPRESSOR. FOUND SEIZED. AIRCRAFT RETURNED TO SERVICE.Dec 20, 2016 · N315US · Airbus A320211 · Air Supply (Water Pressure System)SDR DALA2016102807847Wire · brokenBROKEN EMERGENCY LIGHT WIRE, REPAIRED THE WIRE.Oct 28, 2016 · N315US · Airbus A320211 · Light System WiringSDR DALA2015111206952Skin · corrodedCORROSION ON INSIDE SURFACE OF SKIN OTBD OF STR 42L BETWEEN FRAMES 56-57. PRI 541258-14AD, REV O,1,2. C/W PRI 541258-14AD, REV 2, STEP 9.Nov 11, 2015 · N315US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015111206951Skin · corrodedCORROSION ON SKIN UNDER STR 43L BETWEEN FRAME 56 & 57, PRI 541258-14AD, REV 0, 1, 2 AND ER/A 541258-14AD. BLENDED OUT CORROSION UNDER SKIN IAW 51-74-00, MININUM REMAINING THICKNESS .148.Nov 11, 2015 · N315US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015111206950Stringer · corrodedCORROSION ON STR 42L BETWEEN 56-57. EXISTING REPAIR BETWEEN FRAMES 57-58 AND A SPLICE UNDER FRAME 53. FABRICATED STR 42L BETWEEN FRAMES 55 & 58 AND COUPLER IAW SRM 53-00-13, FIG 201. TREATED AND PRIMED AND PAINTED IAW SRM 51-75-12, INSTALLED STR 42L IAW SRMNov 11, 2015 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015111206949Stringer · corrodedCORROSION ON STR 43L BETWEEN FRAMES 56-57. EXISTING SPLICE BETWEEN FRAMES 56-57 AND A SPLICE UNDER FRAME 54. FABRCATED STR 43L BETWEEN FRAMES 55 & 58 AND COUPLERS IAW SRM 53-00-13, FIG 201. TREATED PRIMED AND PAINTED STR IAW 51-75-12 INSTALLED STRINGER 43LNov 11, 2015 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13017723215Skin · corrodedDURING INSPECTION, FOUND CORROSION ON SKIN, AFT CARGO BAY S38R+1.5 AND FR 64+20. PERFORMED PERMANENT REPAIR ON SKIN IAW ERA 513499-14, REV ORIGINAL AND PR I N. 513499-14 REV 0.Apr 15, 2013 · N315US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13017703215Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY S38L BETWEEN FR 56 AND FR 57 LOWER SURFACE. PERFORMED REPAIR ON WEB IAW ERA 513503-14, REV ORIGINAL PRI FROM REVISION N.0 TO REVISION N.2.Apr 15, 2013 · N315US · Airbus A320211 · Fuselage Floor PanelSDR DALA13017373215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 41R LOCATED BETWEEN FR 28 TO FR 29 IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=0.250" W=0.100" D= 0.002" PERFORMED PERMANENT REPAIR ON STRINGER 41R LOCATED BETWEEN FRAME 28 TO FRAME 29 IN FWD CARGO COMPARTMENApr 15, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13017793215Stringer · corrodedDURING INSPECTION, FOUND CORROSION STRINGER 43L, AFT CARGO BETWEEN FR 58 AND FR 59. PERFORMED PERMANENT REPAIR IAW SRM 53-00-13, PARA 4.A FIG 201, PAGES 202 TO 208.Apr 14, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016873215Trunnion · wornDURING INSPECTION, FOUND SEVERE WEAR ON LOWER SURFACE OF LT INBD FLAP DRIVE TRUNNION, MEASURE THE OUTSIDE DIAMETER OF THE TRUNNION SHAFT IS:2.864". REPLACED LT INBD FLAP DRIVE TRUNNION IAW ER/A 512773-14AD REV ORIGINAL AND PRI NR 512773-14AD FROM REV NR 0 ANApr 13, 2013 · N315US · Airbus A320211 · Trailing Edge FlapsSDR DALA13016853215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 35R AFT CARGO COMP FR 64+20". REPLACED STRINGER 35R IAW SRM 51-72-11.Apr 13, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016843215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 44 BETWEEN FR 31 TO FR 32 AND Y 0 FWD CARGO COMPARTMENT. PERFORMED REPAIR ON STRINGER 44 IAW ER/A NR 512769-14. REV ORIGINAL AND PRI 512769-14, REV.Apr 13, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016833215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 41R BETWEEN FR 32 TO FR 33 FORWARD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 41R IAW ER/A NR 512764-14, REV ORIGINAL AND PRI 512764-14 REV NR 0 AND REV NR 1.Apr 13, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016813215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L, AFT CARGO BAY BETWEEN FR 64 AND STR 65. PERFORMED PERMANENT REPAIR ON STRINGER 43L IAW SRM A320 53-00-13, FIG 201 (SHEET 2) PAGES 211 TO 212.Apr 12, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016803215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 35R, AFT CARGO BAY FR 64+15". REPLACED STRINGER 35R, IAW SRM 51-72-11.Apr 12, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016793215Skin · corrodedDURING INSPECTION, FOUND SEVERE CORROSION ON INTERNAL SURFACE SKIN LOCATED BETWEEN FR 33 TO FR 34 AND STRINGERS 39R TO 41L IN FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON INTERNAL SURFACE SKIN IAW ER/A 512771-14, REV ORIGINAL AND PRI 512771-14, REV Apr 12, 2013 · N315US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13016783215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 41R LOCATED BETWEEN FR 31 TO FR 32 IN FORWARD CARGO COMPARTMENT. PEFORMED REPAIR ON STRINGER 41R IAW ER/A NR 512772-14, REV ORIGINAL AND PRI 512772-14 REV O;Apr 12, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13016773215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BTW FR 24 TO FR 24A IN FORWARD CARGO COMPARTMENT. PERFORMED REPAIR ON STRINGER 44 IAW ER/A 512766-14 REV.Apr 12, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13015943215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43R LOCATED BTW FR 32 TO FR 33 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. POINT 1 L=0.100" W=0.098" D=0.001"; POINT 2 L=0.105" W=0.097" D=0.001", POINT 3 L=0.095 W=0.088" D=0.001"; REPAIRED STRINGER 43R LOCATEApr 10, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13015933215Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FR 51 TO FR 52 STR 38R IN AFT CARGO COMPARTMENT (AFTER REMOVED PROFILE LOC BETWEEN FR 48 AND FR 52A STR 38R AFT CC PERFORMED VISUAL INSPECTION) REPLACED WEB LOCATED BETWEEN FR 51 TO FR 52 STR 38R IN AApr 10, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13016193215Cargo Track · corrodedDURING INSP, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.300" D=0.003" REPLACED CLEAT AT FR 32 AND BTW STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 9, 2013 · N315US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13016183215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 42R TO STR 43R IN FWD CARGO COMPARTMENT. MEASURES APROX. L=2.00" W=0.300" D=0.003" REPLACED CLEAT AT FR 34 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM A320 51-72-11 Apr 9, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13016173215Cover · corrodedDURING INSPECTION, FOUND CORROSION ON COVER SHEET, AFT CARGO COMP. DOOR (L=1.900"; W=0.155" AND DEPT=0.001") REPLACED COVER SHEET, AFT CARGO COMPT. DOOR IAW SRM 51-72-11 AND DWG D53475500.Apr 9, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13015893215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 40R LOCATED AT LEVEL FR 34 IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.175" W=0.120"D=0.001" PERFORMED PERMANENT REPAIR ON STRINGER 40R LOCATED AT LEVEL FR34 IN FORWARD CARGO COMPARTMENT IAW SRM A320Apr 9, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13015833215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=0.800" W=0.300" D=0.002". REPLACED CLEAT AT FR 33 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 9, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13015823215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=3.00" W=0.350" D=0.002". REPLACED CLEAT AT FR 30 BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 9, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13015903215Stringer · wornDURING INSPECTION, FOUND WEAR ON STRINGER 42L, AFT COMP BETWEEN FR 57 AND FR 58. PERFORMED PERMANENT REPAIR ON STRINGER 42L BETWEEN FR 57 TO FR58 AFT CARGO COMP. SRM 53-00-13, PARA 4A, FIGURE 201 (SHEET 3) PAGE 213/214.Apr 8, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13015073215Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE, AFT CARGO BAY STR 38R, FR 51 (L=0.026", W=0.017" AND D=0.003") WC 5320-5010. REPLACED STRINGER SPLICE LOC STR 38R AT LEVEL OF FR 51 AFT CARGO COMP IAW SRM 51-72-11.Apr 7, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13015063215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 29 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT; MEASURES APROX L=1.700" W=0.300" D=0.002". REPLACED CLEAT LOCATED AT FR 29 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT IAW SRM 51Apr 7, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13015053215Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY ARE FLOOR SUPPORT BETWEEN FR 64-66,Y765 UPPER SURFACE FLANGE HAS CORROSION. BLENDED AREA L=1.8",W=1.8"D=.034", MAX ALLOWABLE D=.027" AND FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 AND SRM 51-74-00. REPLACED FLOOR SUApr 6, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13015043215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=0.750",W=0.250", D=0.002". REPLACE CLEAT AT FR 33 AND BETWEEN, STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 5, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13015033215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FORWARD CARGO COMPARTMENT L=0.800", W=0.250", D=0.002" MEASURES APPROX SSI 532180. REPLACED CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FWD CARGO COMPARTMENT IAW SRM 51Apr 5, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13015023215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=2.00", W=0.310", D=0.002". REPLACED CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 5, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014993215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.375" D=0.002". REPLACED CLEAT AT FR 33 AND BTW STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT IAW SRM 51-7Apr 4, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014703215Fitting · corrodedCORROSION ON CORNER FITTING LOCATED FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE. L=4" W=1.25" D=0.003" APPROX. REPLACED CORNER FITTING LOCATED FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE IAW SRM 51-72-11.Apr 4, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014693215Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BTW FR 66 AND FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE L=2" W=1.5" D=0.003" APPROX. SSI 534147. REPLACED LOWER SILL AND FASTENERS LOCATED BETWEEN FR 66 AND FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE IAW SRApr 4, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014683215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=1.300" W=0.350" D=0.003". REPLACED CEAT AND FASTENERS LOCATED FR 31 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COApr 4, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014713215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" =0.800" D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 31 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT IAWApr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014673215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=2.100" W=0.300" D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 34 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMApr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014663215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=3.00" W=0.375" D=0.003". REPLACED CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014653215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=0.750" W=0.210" D=0.002". REPLACED CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014643215Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 25R, BULK CARGO COMP BETWEEN FR 64 AND FR 65. REPLACED STRINGER 25R LOCATED BULK CARGO COMPARTMENT BETWEEN FR 64 TO FR 67 IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13014633215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APPROX. L=0.800" W=0.300" D=0.002". REPLACED CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM A320 51-72-11.Apr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014623215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" W=0.300" D=0.002". REPLACED CLEAT ON FWD CARGO COMP FR 30 BETWEEN STR 41R AND STR 42R IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014613215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.00" W=0.310" D=0.002". REPLACED CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-1Apr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13014603215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.750" W=0.210 " D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGOApr 3, 2013 · N315US · Airbus A320211 · Fuselage Main, Attach Fittings
Back to N315US, cancelled Jan 24, 2018