# Service difficulty reports: N313US, cancelled Sep 27, 2018

A list on [N313US, cancelled Sep 27, 2018](https://openairdocs.org/deregistered/N313US-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 · 115 reports

- [SDR DALA2018060403785](https://openairdocs.org/sdr/DALA2018060403785.md): Structure · cracked · Jan 24, 2018 · N313US · Airbus A320211 · Cargo/Baggage Doors
  > OVERSIZED 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.
- [SDR DALA2017080906065](https://openairdocs.org/sdr/DALA2017080906065.md): Connector · malfunctioned · Aug 8, 2017 · N313US · Airbus A320211 · Emergency Lighting
  > WHILE 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.
- [SDR DALA2017070205105](https://openairdocs.org/sdr/DALA2017070205105.md): Lamp · inoperative · Jun 30, 2017 · N313US · Airbus A320211 · Emergency Lighting
  > EMERGENCY LIGHT SEAT 5 LT INOPERATIVE, REPLACED THE LAMPS.
- [SDR DALA2017020601038](https://openairdocs.org/sdr/DALA2017020601038.md): Battery Pack · no test · Feb 5, 2017 · N313US · Airbus A320211 · Emergency Lighting
  > SERVICE CHECK FOUND EMERGENCY LIGHTS TEST FAILED, REPLACED THE BATTERY.
- [SDR DALA2016120709694](https://openairdocs.org/sdr/DALA2016120709694.md): Frame · cracked · Dec 6, 2016 · N313US · Airbus A320211 · Fuselage Main, Frame
  > FRAME 16 WAS FOUND CRACKED, PERFORMED TEMPORARY REPAIR IAW ER/A 551555-14AD REVISION ORIGINAL.
- [SDR DALA2016120509631](https://openairdocs.org/sdr/DALA2016120509631.md): Stringer · corroded · Dec 4, 2016 · N313US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION 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.
- [SDR DALA2016120409627](https://openairdocs.org/sdr/DALA2016120409627.md): Stringer · corroded · Dec 3, 2016 · N313US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION 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.
- [SDR DALA2016112909407](https://openairdocs.org/sdr/DALA2016112909407.md): Frame · cracked · Nov 28, 2016 · N313US · Airbus A320211 · Fuselage Main, Structure
  > CRACK 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 D52279010
- [SDR DALA2015092905867](https://openairdocs.org/sdr/DALA2015092905867.md): Light · damaged · Sep 28, 2015 · N313US · Airbus A320211 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED LIGHT ASSY.
- [SDR DALA2014090404911](https://openairdocs.org/sdr/DALA2014090404911.md): Light · missing · Sep 1, 2014 · N313US · Airbus A320211 · Emergency Lighting
  > DURING NON-ROUTINE CHECK, FOUND SEAT 20A MISSING AISLE EMERGENCY LIGHT. MAINTENANCE REPLACED EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA2014070703901](https://openairdocs.org/sdr/DALA2014070703901.md): Wire · pulled · Jul 4, 2014 · N313US · Airbus A320211 · Light System Wiring
  > DURING 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.
- [SDR DALA13035083213](https://openairdocs.org/sdr/DALA13035083213.md): Battery Pack · failed · Jul 12, 2013 · N313US · Airbus A320211 · Emergency Lighting
  > DURING 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.
- [SDR DALA13034043213](https://openairdocs.org/sdr/DALA13034043213.md): Epsu · failed · Jul 8, 2013 · N313US · Airbus A320211 · Emergency Lighting
  > DURING NON ROUTINE CHECK, FOUND EPSU INTERNAL LOAD EMERGENCY LIGHT FAILED. MX REPLACED EPSU 10WL AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA13007133213](https://openairdocs.org/sdr/DALA13007133213.md): Shear Tie · corroded · Feb 11, 2013 · N313US · Airbus A320211 · Fuselage Internal Mounting Structure
  > DURING 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
- [SDR DALA13006653213](https://openairdocs.org/sdr/DALA13006653213.md): Floor Panel · corroded · Feb 7, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING 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.
- [SDR DALA13006643213](https://openairdocs.org/sdr/DALA13006643213.md): Web · corroded · Feb 7, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING 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 T13/97964
- [SDR DALA13006633213](https://openairdocs.org/sdr/DALA13006633213.md): Structure · cracked · Feb 7, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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 51-4
- [SDR DALA13006623213](https://openairdocs.org/sdr/DALA13006623213.md): Structure · cracked · Feb 7, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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 51-4
- [SDR DALA13006353213](https://openairdocs.org/sdr/DALA13006353213.md): Structure · corroded · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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
- [SDR DALA13006483213](https://openairdocs.org/sdr/DALA13006483213.md): Profile · cracked · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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 D5227904
- [SDR DALA13006433213](https://openairdocs.org/sdr/DALA13006433213.md): Structure · cracked · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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.
- [SDR DALA13006423213](https://openairdocs.org/sdr/DALA13006423213.md): Structure · cracked · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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
- [SDR DALA13006413213](https://openairdocs.org/sdr/DALA13006413213.md): Structure · corroded · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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.
- [SDR DALA13006403213](https://openairdocs.org/sdr/DALA13006403213.md): Structure · corroded · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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.
- [SDR DALA13006393213](https://openairdocs.org/sdr/DALA13006393213.md): Structure · corroded · Feb 6, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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.
- [SDR DALA13006383213](https://openairdocs.org/sdr/DALA13006383213.md): Floor Support · corroded · Feb 6, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING 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-, INSTALLE
- [SDR DALA13006673213](https://openairdocs.org/sdr/DALA13006673213.md): Floor Support · corroded · Feb 5, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING 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=0.03
- [SDR DALA13006363213](https://openairdocs.org/sdr/DALA13006363213.md): Door · corroded · Feb 4, 2013 · N313US · Airbus A320211 · Emergency Exits
  > DURING 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 SRM
- [SDR DALA13006323213](https://openairdocs.org/sdr/DALA13006323213.md): Structure · gouged · Feb 4, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Main Frame
  > DURING 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. AC
- [SDR DALA13006313213](https://openairdocs.org/sdr/DALA13006313213.md): Structure · gouged · Feb 4, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Main Frame
  > DURING 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 LIM
- [SDR DALA13006303213](https://openairdocs.org/sdr/DALA13006303213.md): Frame · gouged · Feb 4, 2013 · N313US · Airbus A320211 · Fuselage Main, Frame
  > DURING 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.
- [SDR DALA13006293213](https://openairdocs.org/sdr/DALA13006293213.md): Frame Splice · gouged · Feb 4, 2013 · N313US · Airbus A320211 · Fuselage Main, Frame
  > DURING 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.
- [SDR DALA13006663213](https://openairdocs.org/sdr/DALA13006663213.md): Frame · corroded · Feb 3, 2013 · N313US · Airbus A320211 · Fuselage Main, Frame
  > DURING 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
- [SDR DALA13006283213](https://openairdocs.org/sdr/DALA13006283213.md): Stop Fitting · chafed · Feb 3, 2013 · N313US · Airbus A320211 · Fuselage Main, Structure
  > DURING 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 IA
- [SDR DALA13005903213](https://openairdocs.org/sdr/DALA13005903213.md): Skin · gouged · Feb 2, 2013 · N313US · Airbus A320211 · Leading Edge Devices
  > DURING 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 57-4
- [SDR DALA13005893213](https://openairdocs.org/sdr/DALA13005893213.md): Stringer · corroded · Feb 2, 2013 · N313US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING 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.
- [SDR DALA13006373213](https://openairdocs.org/sdr/DALA13006373213.md): Floorboard · cracked · Jan 31, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND MID CABIN FLOORBOARD 232MF CORNER EDGE IS CRACKED. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209.
- [SDR DALA13005583213](https://openairdocs.org/sdr/DALA13005583213.md): Floorboard · delaminated · Jan 30, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING 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.
- [SDR DALA13005383213](https://openairdocs.org/sdr/DALA13005383213.md): Floor Panel · damaged · Jan 29, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING 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.
- [SDR DALA13005373213](https://openairdocs.org/sdr/DALA13005373213.md): Floor Panel · damaged · Jan 28, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF INSERTS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-6602.
- [SDR DALA13005053213](https://openairdocs.org/sdr/DALA13005053213.md): Floor Support · damaged · Jan 28, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING 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. REPAI
- [SDR DALA13005063213](https://openairdocs.org/sdr/DALA13005063213.md): Skin · gouged · Jan 23, 2013 · N313US · Airbus A320211 · Fuselage Main, Plate/Skin
  > DURING 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. INS
- [SDR DALA13004233213](https://openairdocs.org/sdr/DALA13004233213.md): Sill · corroded · Jan 23, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING 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. REMOV
- [SDR DALA13004203213](https://openairdocs.org/sdr/DALA13004203213.md): Fitting · corroded · Jan 23, 2013 · N313US · Airbus A320211 · Nacelle/Pylon Miscellaneous Structure
  > DURING 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
- [SDR DALA13003753213](https://openairdocs.org/sdr/DALA13003753213.md): Floor Panel · corroded · Jan 22, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION 4" X 6". REPLACED FLOOR PANEL IAW SRM 51-72-00.
- [SDR DALA13003743213](https://openairdocs.org/sdr/DALA13003743213.md): Floor Panel · gouged · Jan 22, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND MAIN CABIN FWD AREA FLOOR PANEL 231CF HAS GOUGE 3" X 2". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13003733213](https://openairdocs.org/sdr/DALA13003733213.md): Floorboard · damaged · Jan 22, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND MAIN CABIN, FWD AREA FLOORBOARD 232DF HAS A HOLE.300" X.500". FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209.
- [SDR DALA13003623213](https://openairdocs.org/sdr/DALA13003623213.md): Web · corroded · Jan 21, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR DALA13003563213](https://openairdocs.org/sdr/DALA13003563213.md): Floor Panel · punctured · Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241LF HAS PUNCTURE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13003553213](https://openairdocs.org/sdr/DALA13003553213.md): Floor Panel · dented · Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Floor Panel
  > DURING 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.

Next page: https://openairdocs.org/deregistered/N313US-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 = 'N313US' AND deregistration_id = 'N313US-2018-09-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N313US-2018-09-27/reports

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