N313US, cancelled Sep 27, 2018

Service difficulty reports · 115

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 = 'N313US' AND deregistration_id = 'N313US-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 DALA2018060403785Structure · crackedOVERSIZED HOLES AND CRACKS WERE FOUND DURING SHOP ACCOMPLISHMENT OF EM 5230-01163 (AD 2017-22-07) TO FWD CARGO DOOR, P/N D52371000012 S/N UH-1153, REPAIRED PER ER/A 567106-14AD SECTION I.Jan 24, 2018 · N313US · Airbus A320211 · Cargo/Baggage DoorsSDR DALA2017080906065Connector · malfunctionedWHILE PERFORMING EMERGENCY LIGHT TEST DURING SERVICE CHECK, HAD MULTIPLE MESSAGES INTERNAL LIGHT FAULT. DISCONNECTED & RECONNECTED R MIN CABIN EPSU CONNECTOR. TEST OK. OK ON EPSU AND FAP.Aug 8, 2017 · N313US · Airbus A320211 · Emergency LightingSDR DALA2017070205105Lamp · inoperativeEMERGENCY LIGHT SEAT 5 LT INOPERATIVE, REPLACED THE LAMPS.Jun 30, 2017 · N313US · Airbus A320211 · Emergency LightingSDR DALA2017020601038Battery Pack · no testSERVICE CHECK FOUND EMERGENCY LIGHTS TEST FAILED, REPLACED THE BATTERY.Feb 5, 2017 · N313US · Airbus A320211 · Emergency LightingSDR DALA2016120709694Frame · crackedFRAME 16 WAS FOUND CRACKED, PERFORMED TEMPORARY REPAIR IAW ER/A 551555-14AD REVISION ORIGINAL.Dec 6, 2016 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016120509631Stringer · corrodedCORROSION ON STRINGER 31R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 31R IN AFT CARGO COMPARTMENT FROM FRAME 64 TO FRAME 67 AS PER SRM 51-72-11 AND DWG D53480020.Dec 4, 2016 · N313US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016120409627Stringer · corrodedCORROSION ON STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FR 64 TO FR 67 AS PER SRM 51-72-11 AND DRAWING D53480020.Dec 3, 2016 · N313US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016112909407Frame · crackedCRACK ON LATERAL FWD SEGMENT FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN, REPLACED LATERAL FWD SEGMENT FRAME IAW SRM 51-72-11 AND DRAWING D52279010Nov 28, 2016 · N313US · Airbus A320211 · Fuselage Main, StructureSDR DALA2015092905867Light · damagedEMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED LIGHT ASSY.Sep 28, 2015 · N313US · Airbus A320211 · Emergency LightingSDR DALA2014090404911Light · missingDURING NON-ROUTINE CHECK, FOUND SEAT 20A MISSING AISLE EMERGENCY LIGHT. MAINTENANCE REPLACED EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.Sep 1, 2014 · N313US · Airbus A320211 · Emergency LightingSDR DALA2014070703901Wire · pulledDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT SEATS 08C-23C INOPERATIVE. MAINTENANCE FOUND WIRE PULLED FROM SPLICE AT EACH LOCATION. SPLICED WIRES BACK TOGETHER AND FUNCTIONAL CHECK WAS NORMAL.Jul 4, 2014 · N313US · Airbus A320211 · Light System WiringSDR DALA13035083213Battery Pack · failedDURING CRUISE EMERGENCY EXIT LIGHTS AND THE EMERGENCY AISLE LIGHTING WERE FLASHING ERRATICALLY ON AND OFF WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. MX REPLACED FWD LT EPSU AND BATTERY. FUNCTIONAL CHECKED NORMAL.Jul 12, 2013 · N313US · Airbus A320211 · Emergency LightingSDR DALA13034043213Epsu · failedDURING NON ROUTINE CHECK, FOUND EPSU INTERNAL LOAD EMERGENCY LIGHT FAILED. MX REPLACED EPSU 10WL AND FUNCTIONAL CHECKED NORMAL.Jul 8, 2013 · N313US · Airbus A320211 · Emergency LightingSDR DALA13007133213Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO AT FR 31 BET CENTERLINE AND STR 43R, SHEAR TIE HAS CORROSION. CHECKED LIMITS L=1.00" W=1.00" D=0.010". NO ALLOWABLE DAMAGE IAW SRM 53-21-12. REMOVED AND INSTALLED FABRICATED SHEAR TIE ON STAM TRAVELER T13/982826 MAT 2024-0 Feb 11, 2013 · N313US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13006653213Floor Panel · corrodedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF IS CORRODED. REMOVED CORROSION IAW SRM 51-74-00, L=1.0" W=0.70" D=0.050 NO ESTABLISHED SRM LIMITS.Feb 7, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13006643213Web · corrodedDURING INSPECTION, FOUND AFT CARGO BAY FRAME 55-56, STR 39-40R WEB PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW ER/A 484892-14MA DIMENSION L=1.80" W=2.00" D=0.047". FABRICATED COVER SHEET IAW STAM TRAVELER T13/97964Feb 7, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006633213Structure · crackedDURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLES (5EA) HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" LENGTH OF CRACK, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-4Feb 7, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006623213Structure · crackedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FOUR FASTENER HOLES HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" LENGTH OF CRACK, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-4Feb 7, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006353213Structure · corrodedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLES IAW SRM 51-42-11 LOCATED AND DRILLED NEW "T" SECTION IAW SRM 5 1-44-11.INSTALLED NEW "T" SECTION IAW SRM Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006483213Profile · crackedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE (4EA) FASTENER HOLES HAS CRACK. CRACK INDICATION NOTED .025" LENGTH OF DAMAGE, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG D5227904Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006433213Structure · crackedDURING INSP, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOAD TRANSMITTING PROFILE (9EA) FASTENER HOLE HAS CRACKED. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006423213Structure · crackedDURING INSPECTION, RT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLE HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .027" LENGTH OF DAMAGE, NO DAMAGE ALLOWED IAW SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006413213Structure · corrodedDURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=.90" W=.80" D=.010" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006403213Structure · corrodedDURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.0" W=.70" D=.012" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006393213Structure · corrodedDURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2.0" W=1.5" D=.040" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006383213Floor Support · corrodedDURING INSPECTION, FOUND AFT CARGO BAY FRAME 59 STR 44 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION NO LIMITS IN SRM 53-41-14 L=.5" W=.5" D=.020". REMOVED CORRODED PROFILE. LOCATED AND DRILLED NEW PROFILE. TREATED AND PRIMED HOLES IAW SRM 51-21-, INSTALLEFeb 6, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006673213Floor Support · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 58-59, STR 44, FLOOR SUPPORT CORRODED. REMOVED AFT CARGO FLOOR SUPPORT IAW A320 SRM 51-42-11 FR 58-59 STR 44. REMOVED CORROSION IAW SRM 51-74-00 OUT OF LIMITS IAW SRM 53-00-14. NO ESTABLISHED LIMITS L=1.5"W=1.0"D=0.03Feb 5, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006363213Door · corrodedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLE S IAW SRM 51-42-11 LOCATED AND DRILLED NEW "T" SECTION IAW SRM 51-44-11. INSTALLED NEW "T" SECTION IAW SRMFeb 4, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006323213Structure · gougedDURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE AFT GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW A320 TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.284" W=0.062" D=0.063"; AREA 2 L=0.299" W=0.049" D=0.053". FOUND TO BE OUT OF LIMITS IAW TRM 54-51-18 FIG 2. ACFeb 4, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Main FrameSDR DALA13006313213Structure · gougedDURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE MID GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.446" W=0.022" D=0.046"; AREA 2 L=0.338" W=0.047" D=0.080"; AREA 3 L=0.360" W=0.071" D=0.156". FOUND TO BE OUT OF LIMFeb 4, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Main FrameSDR DALA13006303213Frame · gougedDURING INSPECTION, FOUND FWD CARGO COMPT FR28 FRAME SPLICE AFT FACE IS GOUGED STR 35L. BLENDED FISH PLATE IAW SRM 51-73-00, MEASUREMENTS ARE L=1.5" W=.5" D=. 014, NO LIMITS FOUND IN SRM R & R IAW SRM 51-42-11.Feb 4, 2013 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA13006293213Frame Splice · gougedDURING INSPECTION, FOUND FWD CARGO COMPT FR26 FRAME SPLICE AFT FACE IS GOUGED STR 35L. REPLACED FISH PLATE IAW SRM 51-42-11 DWG NR C2.D53230405. BLENDED FISH PLATE IAW SRM 51-73-00, L=2.0" W=1.5" D=1.5" NO ESTABLISHED LIMITS IN SRM.Feb 4, 2013 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA13006663213Frame · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 55-58, STR 43L HAS CORROSION. REMOVED CORROSION IAW 51-74-00 FROM STRINGER 43L BET FRAME 55-58 AND FOUND NO ESTABLISHED DAMAGE LIMITS. DAMAGE DIMENSIONS L=2.5 "W=1.0" D=0.015". REPAIRED STRINGER IAW SRM 53-00-13, FIG Feb 3, 2013 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA13006283213Stop Fitting · chafedDURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE FRAME 68 ROLLER STOP FITTING ON MID OUTER SURFACE HAS CHAFED. REPLACED ROLLER STOP FITTING AT LT AFT PAX ENTRANCE ON FRAME 68 IAW SRM 51-49-00 (TR14925 TORQUE WRENCH USED) DUE TO NO ESTABLISHED LIMIT FOUND IAFeb 3, 2013 · N313US · Airbus A320211 · Fuselage Main, StructureSDR DALA13005903213Skin · gougedDURING INSPECTION, FOUND RT NR 4 SLAT LWR T/E SKIN HAS GOUGE 10" INBD OF SLAT TRACK NR 10. ACCOMPLISHED REPAIR IAW ER/A 509275-14 REV ORIGINAL AS PERMANENT REPAIR SECTION I. DAMAGE DIMENSIONS L=0.70", W=0.30", D=0.125". FOUND TO BE OUT OF LIMITS IAW SRM 57-4Feb 2, 2013 · N313US · Airbus A320211 · Leading Edge DevicesSDR DALA13005893213Stringer · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 56-57, STR 41L HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DAMAGE DIMENSION S L=5.0" W=1.0"D=0.012". NO ESTABLISHED LIMITS IN SRM. REPLACED STRINGER IAW SRM 51-42-11 AND DWG D53470345.Feb 2, 2013 · N313US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13006373213Floorboard · crackedDURING INSPECTION, FOUND MID CABIN FLOORBOARD 232MF CORNER EDGE IS CRACKED. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209.Jan 31, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005583213Floorboard · delaminatedDURING INSPECTION, FOUND MID CABIN BETWEEN FR35 TO 36 MOST CENTER FLOORBOARD 241AF HAS DELAMINATION. REPLACED FLOORBOARDIAW AMM 53-12-12-400-001-A. FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.Jan 30, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005383213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161 BF IS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-5019 AND DWG 3D25-37705. MISSING INSERTS & EDGE DELAMINATED.Jan 29, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005373213Floor Panel · damagedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF INSERTS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-6602.Jan 28, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005053213Floor Support · damagedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 16-20 Y-254 UPPER FLANGE HOLES HAS CORROSION. REMOVED DAMAGE IAW SRM 51-74-00. DAMAGE MEASURES: AREA NR 1 L=1.8 W=1.2 D=.010, AREA NR 2 L=1.1 W=1.0 D=.015 NO LIMITS FOUND IN SRM. REPAIJan 28, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005063213Skin · gougedDURING INSPECTION, FOUND LOWER FUSELAGE JUST AFT OF FR 65 BETWEEN STR 28L - 29L SKIN APPEARS TO BE GOUGED UNDER PAINT. N/R 100/4. CUTOUT DAMAGED SKIN IAW SRM 53-41-11. DIM. L=1.78" W=1.75". FABRICATED DOUBLER FROM 2024T30.071 IAW SRM 53-41-11, FIG 214. INSJan 23, 2013 · N313US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13004233213Sill · corrodedDURING INSPECTION, FOUND RT AFT PASSENGER ENTRANCE LOWER DOOR SILL AT FWD FR68 GIRT BAR & INBD HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLENDED AREA MEASURES L=1.5" W= 1.0" D=.110" AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. REMOVJan 23, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13004203213Fitting · corrodedDURING INSPECTION, FOUND NR 1 ENGINE SPIGOT RECEPTACLE FITTING BORE AT UPPER SPAR HAS FITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-00 FINAL DIAMETER FOUND TO BE OUT OF LIMITS OF 4.345 ALLOWABLE DIA 4.335 IAW SRM 54-51- 12, FIG 101. REMOVED FITTING IAW Jan 23, 2013 · N313US · Airbus A320211 · Nacelle/Pylon Miscellaneous StructureSDR DALA13003753213Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION 4" X 6". REPLACED FLOOR PANEL IAW SRM 51-72-00.Jan 22, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13003743213Floor Panel · gougedDURING INSPECTION, FOUND MAIN CABIN FWD AREA FLOOR PANEL 231CF HAS GOUGE 3" X 2". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 22, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13003733213Floorboard · damagedDURING INSPECTION, FOUND MAIN CABIN, FWD AREA FLOORBOARD 232DF HAS A HOLE .300" X .500". FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209.Jan 22, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13003623213Web · corrodedDURING INSPECTION, FOUND FORWARD CABIN RT SIDE STRINGER 23 BETWEEN FR 20 TO 21 UPPER SURFACE WEB CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REPLACED WEB IAW SRM 51-42-11.Jan 21, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13003563213Floor Panel · puncturedDURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241LF HAS PUNCTURE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13003553213Floor Panel · dentedDURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241DF HAS INDENTION ON BOTTOM. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
Back to N313US, cancelled Sep 27, 2018