# Service difficulty reports: N311US, cancelled Sep 27, 2018 A list on [N311US, cancelled Sep 27, 2018](https://openairdocs.org/deregistered/N311US-2018-09-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 130 reports - [SDR DALA14028663211](https://openairdocs.org/sdr/DALA14028663211.md): Battery Pack · inoperative · May 5, 2014 · N311US · Airbus A320211 · Emergency Lighting > RT EMERGENCY LIGHT PACK BATTERY FAULTED. R & R BATTERY PACK IAW AMM 33-51. CHECKED NORMAL. - [SDR DALA14021943211](https://openairdocs.org/sdr/DALA14021943211.md): Light · damaged · Apr 9, 2014 · N311US · Airbus A320211 · Emergency Lighting > DURING 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. - [SDR DALA13023993211](https://openairdocs.org/sdr/DALA13023993211.md): Door · out of adjust · May 16, 2013 · N311US · Airbus A320211 · Emergency Exits > AFT 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. - [SDR DALA13022533211](https://openairdocs.org/sdr/DALA13022533211.md): Epsu · failed · May 14, 2013 · N311US · Airbus A320211 · Emergency Lighting > DURING 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. - [SDR DALA13023973211](https://openairdocs.org/sdr/DALA13023973211.md): Strut · worn · May 10, 2013 · N311US · Airbus A320211 · Trailing Edge Flaps > LEFT 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 TES - [SDR DALA13021713211](https://openairdocs.org/sdr/DALA13021713211.md): Skin · damaged · May 9, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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. - [SDR DALA13021703211](https://openairdocs.org/sdr/DALA13021703211.md): Floor Panel · damaged · May 8, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING 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. - [SDR DALA13021693211](https://openairdocs.org/sdr/DALA13021693211.md): Skin · damaged · May 7, 2013 · N311US · Airbus A320211 · Leading Edge Devices > DURING 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. - [SDR DALA13021473211](https://openairdocs.org/sdr/DALA13021473211.md): Web · gouged · May 7, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING INSPECTION, FOUND FWD CARGO THRESHOLD WEB HAS DEEP GOUGE 7" AFT OF FR26. REPLACED DAMAGED THRESHOLD WEB IAW DWG 53230315 & SRM 51-42-11. - [SDR DALA13021463211](https://openairdocs.org/sdr/DALA13021463211.md): Structure · corroded · May 7, 2013 · N311US · Airbus A320211 · Emergency Exits > DURING 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. - [SDR DALA13021453211](https://openairdocs.org/sdr/DALA13021453211.md): Structure · corroded · May 7, 2013 · N311US · Airbus A320211 · Emergency Exits > DURING 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. - [SDR DALA13021443211](https://openairdocs.org/sdr/DALA13021443211.md): Structure · corroded · May 7, 2013 · N311US · Airbus A320211 · Emergency Exits > DURING 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. - [SDR DALA13021433211](https://openairdocs.org/sdr/DALA13021433211.md): Structure · corroded · May 7, 2013 · N311US · Airbus A320211 · Emergency Exits > DURING 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". - [SDR DALA13021683211](https://openairdocs.org/sdr/DALA13021683211.md): Floor Panel · damaged · May 6, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131HF HAS MULTIPLE DENTS & SCRATCHES. FABRICTATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705. - [SDR DALA13020903211](https://openairdocs.org/sdr/DALA13020903211.md): Hinge Fitting · damaged · May 4, 2013 · N311US · Airbus A320211 · Fuselage, Door Hinge > DURING 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. - [SDR DALA13020913211](https://openairdocs.org/sdr/DALA13020913211.md): Hinge Fitting · damaged · May 3, 2013 · N311US · Airbus A320211 · Fuselage, Door Hinge > DURING 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. - [SDR DALA13020893211](https://openairdocs.org/sdr/DALA13020893211.md): Fitting · out of adjust · May 3, 2013 · N311US · Airbus A320211 · Pitot/Static System > DURING 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 AN - [SDR DALA13020613211](https://openairdocs.org/sdr/DALA13020613211.md): Plate · corroded · May 1, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING 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 A - [SDR DALA13020253211](https://openairdocs.org/sdr/DALA13020253211.md): Floor Panel · corroded · Apr 29, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132DF CORRODED AND GOUGED. REPLACED FLOOR PANEL IAW SRM 51-72-11. - [SDR DALA13019423211](https://openairdocs.org/sdr/DALA13019423211.md): Floor Support · bent · Apr 27, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING 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 - [SDR DALA13019413211](https://openairdocs.org/sdr/DALA13019413211.md): Floor Panel · corroded · Apr 27, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 231AF HAS CORROSION ON HINGE AND PANEL. REPLACED FLOOR PANEL. - [SDR DALA13019323211](https://openairdocs.org/sdr/DALA13019323211.md): Skin · damaged · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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 INDICATION - [SDR DALA13019433211](https://openairdocs.org/sdr/DALA13019433211.md): Web · damaged · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Miscellaneous Structure > DURING 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. - [SDR DALA13019403211](https://openairdocs.org/sdr/DALA13019403211.md): Skin · damaged · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > LOWER 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 FASTENE - [SDR DALA13019393211](https://openairdocs.org/sdr/DALA13019393211.md): Floor Panel · corroded · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF HAS CORROSION. REPLACED FLOOR PANEL IAW SRM 51-72-11. - [SDR DALA13019383211](https://openairdocs.org/sdr/DALA13019383211.md): Skin · damaged · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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. - [SDR DALA13019373211](https://openairdocs.org/sdr/DALA13019373211.md): Skin · damaged · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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 INDICATION - [SDR DALA13019363211](https://openairdocs.org/sdr/DALA13019363211.md): Floor Panel · damaged · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 232DF HAS TWO BAD INSERTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. - [SDR DALA13019353211](https://openairdocs.org/sdr/DALA13019353211.md): Floor Panel · punctured · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AF HAS PUNCTURED 1" X 1". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. - [SDR DALA13019343211](https://openairdocs.org/sdr/DALA13019343211.md): Floor Panel · corroded · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FLOOR PANEL 261FF HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-74-00, REPLACED FLOOR PANEL, IAW SRM 51-72-11. - [SDR DALA13019333211](https://openairdocs.org/sdr/DALA13019333211.md): Floor Panel · corroded · Apr 25, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING 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. - [SDR DALA13018973211](https://openairdocs.org/sdr/DALA13018973211.md): Skin · gouged · Apr 24, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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 DOUBL - [SDR DALA13017803211](https://openairdocs.org/sdr/DALA13017803211.md): Skin · cracked · Apr 18, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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, - [SDR DALA13017763211](https://openairdocs.org/sdr/DALA13017763211.md): Skin · cracked · Apr 17, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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, FIG - [SDR DALA13017753211](https://openairdocs.org/sdr/DALA13017753211.md): Skin · dented · Apr 16, 2013 · N311US · Airbus A320211 · Fuselage Main, Plate/Skin > DURING 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, F - [SDR DALA13017743211](https://openairdocs.org/sdr/DALA13017743211.md): Floor Panel · delaminated · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498. - [SDR DALA13017733211](https://openairdocs.org/sdr/DALA13017733211.md): Floor Panel · damaged · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FLOOR PANEL 261PF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498. - [SDR DALA13017713211](https://openairdocs.org/sdr/DALA13017713211.md): Floor Panel · punctured · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FLOOR PANEL 262AB HAS NUMEROUS PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498. - [SDR DALA13017693211](https://openairdocs.org/sdr/DALA13017693211.md): Floor Panel · delaminated · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FLOOR PANEL 261DF IS DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498. - [SDR DALA13017683211](https://openairdocs.org/sdr/DALA13017683211.md): Floor Panel · corroded · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FLOOR PANEL 262EF HAS CORROSION. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498. - [SDR DALA13017673211](https://openairdocs.org/sdr/DALA13017673211.md): Floor Panel · punctured · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 232FF HAS PUNCTURE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498. - [SDR DALA13017663211](https://openairdocs.org/sdr/DALA13017663211.md): Floor Panel · cracked · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING 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. - [SDR DALA13017653211](https://openairdocs.org/sdr/DALA13017653211.md): Floor Panel · corroded · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FLOOR PANEL 261EF CORRODED IN SEVERAL PLACES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498. - [SDR DALA13017643211](https://openairdocs.org/sdr/DALA13017643211.md): Floor Panel · punctured · Apr 15, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AB HAS TWO PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498. - [SDR DALA13017203211](https://openairdocs.org/sdr/DALA13017203211.md): Seat Track · corroded · Apr 14, 2013 · N311US · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings > DURING 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. - [SDR DALA13017783211](https://openairdocs.org/sdr/DALA13017783211.md): Floor Panel · damaged · Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131CF PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705. - [SDR DALA13017543211](https://openairdocs.org/sdr/DALA13017543211.md): Floor Panel · damaged · Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131BF CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705. - [SDR DALA13017533211](https://openairdocs.org/sdr/DALA13017533211.md): Floor Panel · damaged · Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131KF HAS MULTIPLE DENTED & CRACKED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705. - [SDR DALA13017523211](https://openairdocs.org/sdr/DALA13017523211.md): Floor Panel · damaged · Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF HAS MULTIPLE DENTS & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705. - [SDR DALA13017513211](https://openairdocs.org/sdr/DALA13017513211.md): Floor Panel · damaged · Apr 13, 2013 · N311US · Airbus A320211 · Fuselage Floor Panel > DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162BF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705. Next page: https://openairdocs.org/deregistered/N311US-2018-09-27/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N311US-2018-09-27/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.