# Service difficulty reports: N318US, cancelled Sep 28, 2018

A list on [N318US, cancelled Sep 28, 2018](https://openairdocs.org/deregistered/N318US-2018-09-28.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 · 131 reports

- [SDR DALA2017051403878](https://openairdocs.org/sdr/DALA2017051403878.md): Cover · missing · May 13, 2017 · N318US · Airbus A320211 · Emergency Lighting
  > ROW 11 RIGHT EMERGENCY LIGHT COVER MISSING, REPLACED THE COVER.
- [SDR DALA2017010800181](https://openairdocs.org/sdr/DALA2017010800181.md): Box Beam · cracked · Jan 7, 2017 · N318US · Airbus A320211 · Fuselage Main, Structure
  > LEFT SIDE BOX BEAM UPPER FLANGE CRACKED. REPAIRED IAW AMDS 5310-01450-02.
- [SDR DALA2016102707849](https://openairdocs.org/sdr/DALA2016102707849.md): Light · damaged · Oct 26, 2016 · N318US · Airbus A320211 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHT SEAT 21C DAMAGED, EMERGENCY LIGHT REPAIRED.
- [SDR DALA2016111808969](https://openairdocs.org/sdr/DALA2016111808969.md): Stringer · corroded · Jan 19, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 44 BETWEEN FRAMES 56 AND 59, REMOVED CORROSION AND INSTALLED REPAIR IAW SRM.
- [SDR DALA2016012100723](https://openairdocs.org/sdr/DALA2016012100723.md): Stringer · corroded · Jan 19, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > FOUND EVEDENCE OF CORROSION IN MULTIPLE LOCATIONS ON S42R BETWEEN FRAMES 54 & 58, REMOVED AREAS OF CORROSION REPAIR ON S42R BETWEEN FRAMES 54 & 58 IAW SRM 53-00-13 F 202.
- [SDR DALA2016111808971](https://openairdocs.org/sdr/DALA2016111808971.md): Frame · corroded · Jan 16, 2016 · N318US · Airbus A320211 · Fuselage Main, Frame
  > CORROSION ON FRAME 43L AT FRAME 55. REPAIR THE FRAME.
- [SDR DALA2016011900504](https://openairdocs.org/sdr/DALA2016011900504.md): Stringer · corroded · Jan 16, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 42L BETWEEN FRAMES 56 AND 57. REMOVED STR 42L BETWEEN FRAMES 55 AND 58. FABRICATED AND INSTALLED STRINGER SECTION AND COUPLING/SPLICE IAW SRM 53-00-13.
- [SDR DALA2016011900483](https://openairdocs.org/sdr/DALA2016011900483.md): Stringer · corroded · Jan 16, 2016 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 56 AND 57. REMOVED STR 43L BETWEEN FRAME 55 TO 59. INSTALLED NEW STRINGER SECTION IAW SRM 53-00-13.
- [SDR DALA2015022701737](https://openairdocs.org/sdr/DALA2015022701737.md): Wire · broken · Feb 25, 2015 · N318US · Airbus A320211 · Light System Wiring
  > DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 9 IS INOPERATIVE. FOUND BROKEN GROUND WIRE AT SPLICE. REPLACED SPLICE AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA2015022601674](https://openairdocs.org/sdr/DALA2015022601674.md): Wire · pulled · Feb 25, 2015 · N318US · Airbus A320211 · Light System Wiring
  > DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 12 INOPERATIVE. FOUND POWER WIRE PULLED FROM SPLICE. REINSTALLED WIRE TO SPLICE AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA14011823218](https://openairdocs.org/sdr/DALA14011823218.md): Power Supply · inoperative · Feb 21, 2014 · N318US · Airbus A320211 · Emergency Lighting
  > DURING NON-ROUTINE CHECK, FOUND SEVERAL SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED EPSU AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA13065943218](https://openairdocs.org/sdr/DALA13065943218.md): Connector · unsecure · Dec 3, 2013 · N318US · Airbus A320211 · Light System Wiring
  > DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT SYSTEM TEST FAILED. MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEATS 9C, 16C, 17C, 21C, 22C, 23C, INOPERATIVE. SECURED CONNECTOR AT 9C AND REPLACED 11WL EPSU. FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA13054143218](https://openairdocs.org/sdr/DALA13054143218.md): Relay · malfunctioned · Oct 20, 2013 · N318US · Airbus A320211 · Lighting System
  > DOOR LIGHTS ON AFTER GEAR UP. CABIN LIGHT UNCONTROLLABLE FROM F/A PANEL. R & R RELAY 8WL IAW ASM 33-51. OPS TESTED GOOD, OK FOR CONTINUED SERVICE.
- [SDR DALA13032633218](https://openairdocs.org/sdr/DALA13032633218.md): Profile · cracked · Jun 28, 2013 · N318US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS CRACK. HFEC IAW NTM 51-10-08 PT6, CONFIRMED CRACK BY FASTENER HOLE. REPLACED PROFILE, PN D5227902620200, BATCH NR 0002155894 IAW SRM 51-42-11 & DWG NR D52279010.
- [SDR DALA13032693218](https://openairdocs.org/sdr/DALA13032693218.md): Profile · cracked · Jun 28, 2013 · N318US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS SEVERAL CRACKS AROUND FASTENER HOLES. HFEC IAW NTM 51-10-08, PT6, CONFIRMED CRACK AROUND FASTENERS. REPLACED PROFILE IAW SRM 51-42-11 & DWG D52279010.
- [SDR DALA13032683218](https://openairdocs.org/sdr/DALA13032683218.md): Attach Fitting · corroded · Jun 28, 2013 · N318US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LWR AFT LATCH HOOK ATTACH FITTING HAS CORROSION. REMOVED OLD FITTING IAW SRM 51-42-11. LOCATED AND DRILLED NEW LATCH HOOK FITTING, IAW SRM 51-44-11. INSTALLED NEW FITTING IAW SRM 51-42-11 AND DWG D5227904
- [SDR DALA13032673218](https://openairdocs.org/sdr/DALA13032673218.md): Plate · chafed · Jun 28, 2013 · N318US · Airbus A320211 · Leading Edge Devices
  > DURING INSPECTION, FOUND LT NR 3 SLAT TRACK COVER PLATE CHAFING W/ SLAT T/E LWR SKIN. ACCOMPLISHED REPAIR IAW ER/A 494603-14MA, SECTION 1, PERMANENT REPAIR IDENTIFIED REPAIR AS PERMANENT & ENGINEERING APPROVED IAW PS 900-5-1, NR 4.
- [SDR DALA13032653218](https://openairdocs.org/sdr/DALA13032653218.md): Floor Support · cracked · Jun 27, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND COCKPIT FLOOR SUPPORT RT SIDE FWD FR8 Y-1292, AROUND NUTPLATE SHEETMETAL CRACKED. ACCOMPLISHED REPAIR IAW ER/A 515379-14, REV ORIGINAL SECTION I PERMANENT REPAIR. IDENTIFIED REPAIR AS ENGINEERING APPROVED & PERMANENT IAW PS 900-5-1,
- [SDR DALA13031533218](https://openairdocs.org/sdr/DALA13031533218.md): Floor Support · corroded · Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND AFT CARGO BETWEEN FR 58-59, STR 44, FLOOR SUPPORT HAS SURFACE CORROSION. BLENDED CORROSION. BLENDED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS IAW SRM 53-41-14, REPLACED FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR DALA13031523218](https://openairdocs.org/sdr/DALA13031523218.md): Floor Panel · damaged · Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > MID CABIN, FLOOR PANEL 241AF FOUND ONE ELONGATED HOLE AND CRACKED. FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007-A.
- [SDR DALA13031513218](https://openairdocs.org/sdr/DALA13031513218.md): Floor Panel · delaminated · Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162CF DELAMINATED 21" X 15". AFT CARGO COMPARTMENT SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
- [SDR DALA13031503218](https://openairdocs.org/sdr/DALA13031503218.md): Floorbeam · corroded · Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Main, Floor Beam
  > DURING INSPECTION, FOUND AFT CARGO FLOORBEAM AT FR58, LT SIDE, FWD FACE HAS 2EA AREAS OF CORROSION. REMOVED FLOORBEAM AT FR 58 IAW SRM 51-42-11. NO ALLOWABLE LIMITS IN SRM. INSTALLED NEW FLOORBEAM IAW SRM 51-42-11.
- [SDR DALA13033173218](https://openairdocs.org/sdr/DALA13033173218.md): Skin · damaged · Jun 23, 2013 · N318US · Airbus A320211 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND AFT LT PASSENGER DOOR EXTERNAL FROM LOWER EDGE TO ABOVE 16 INCHES SKIN HAS DENT. FOUND OUT OF LIMITS IAW SRM 52-10-00, DIAGRAM 103. CUTOUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-42-11 & SRM 52-10-00, FIG 2
- [SDR DALA13030913218](https://openairdocs.org/sdr/DALA13030913218.md): Stringer · corroded · Jun 22, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, FOUND AFT CARGO COMPARTMENT BETWEEN FR56-FR57, STR 43L CORRODED. CLEANED AREA IAW AMM 12-21-12. CORROSION FOUND. NO LIMITS ESTABLISHED IAW SRM 53-41-13, FIG 101. REPAIRED DAMAGE STRINGER IAW SRM 53-00-13, FIG 201, STRINGER FABRICATED ON
- [SDR DALA13032663218](https://openairdocs.org/sdr/DALA13032663218.md): Stringer · damaged · Jun 21, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, FOUND AFT CARGO AT FR 65, STR 43L HAS CORROSION. REMOVED CORROSION IAW SRM A320 51-74-00. NO ALLOWABLE DAMAGE FOUND ON SRM. PERFORMED STRINGER REPAIR IAW SRM 53-00-13, FIG 201, SHEET 2.
- [SDR DALA13030903218](https://openairdocs.org/sdr/DALA13030903218.md): Shear Tie · corroded · Jun 21, 2013 · N318US · Airbus A320211 · Fuselage Internal Mounting Structure
  > DURING INSPECTION, FOUND FWD CARGO COMPT BILGE AREA AT FR 28 STGR 41R -42R CLIP HAS CORROSION. REMOVED SHEAR CLIP IAW SRM 51-42-11. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. FABRICATED, LOCATED & DRILLED, TREATED AND PRIMED, APPLIED TOPCOAT, AND INSTALLED NE
- [SDR DALA13030153218](https://openairdocs.org/sdr/DALA13030153218.md): Stringer · corroded · Jun 19, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, FOUND FWD CARGO BAY, FR 33-34, S41L CORRODED. BLENDED CORROSION IAW SRM 51-74-00 CHECKED LIMITS, WITH NO ALLOWABLE DAMAGE FOUND ON SRM. CUT OUT DAMAGED STRINGER IAW SRM 53-00-13, FIG 201. LOCATED AND DRILLED NEW STRINGER IAW SRM 51-44-11.
- [SDR DALA13030143218](https://openairdocs.org/sdr/DALA13030143218.md): Stringer · corroded · Jun 19, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, FOUND AFT CARGO BAY FR58 - 59 S42L CORRODED. CLEANED AREA IAW AMM 12-21-12. NO LIMITS ON CORROSION ESTABLISHED IAW SRM 53-41-13, FIG 101. REMOVED DAMAGED STRINGER IAW SRM 53-00-13, FIG 201, SHT. 2. REPAIRED STRINGER IAW SRM 53-00-13, FIG
- [SDR DALA13032643218](https://openairdocs.org/sdr/DALA13032643218.md): Angle · cracked · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Main, Structure
  > DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS SEVERAL CRACKS AROUND FASTENER. HFEC IAW NTM 51-10-08, PT6 CONFIRMED CRACKS AROUND FASTENER HOLES. REMOVED CRACKED ANGLE IAW SRM 51-42-11. LOCATED AND DRILLED IAW SRM 51-44
- [SDR DALA13029903218](https://openairdocs.org/sdr/DALA13029903218.md): Floor Panel · delaminated · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152EF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029893218](https://openairdocs.org/sdr/DALA13029893218.md): Floor Panel · damaged · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF HAS SEVERAL BROKEN EDGES & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029873218](https://openairdocs.org/sdr/DALA13029873218.md): Floor Panel · delaminated · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151LF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37705.
- [SDR DALA13029863218](https://openairdocs.org/sdr/DALA13029863218.md): Floor Panel · delaminated · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151AF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.
- [SDR DALA13029853218](https://openairdocs.org/sdr/DALA13029853218.md): Floor Panel · delaminated · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152BF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37705.
- [SDR DALA13029843218](https://openairdocs.org/sdr/DALA13029843218.md): Floor Panel · delaminated · Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151QF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029823218](https://openairdocs.org/sdr/DALA13029823218.md): Floor Panel · punctured · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151NF HAS SEVERAL PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029813218](https://openairdocs.org/sdr/DALA13029813218.md): Floor Panel · punctured · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151HF HAS SEVERAL PUNCTURES & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029803218](https://openairdocs.org/sdr/DALA13029803218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151JF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029643218](https://openairdocs.org/sdr/DALA13029643218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029633218](https://openairdocs.org/sdr/DALA13029633218.md): Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152MF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029623218](https://openairdocs.org/sdr/DALA13029623218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152RF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029613218](https://openairdocs.org/sdr/DALA13029613218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161BF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029603218](https://openairdocs.org/sdr/DALA13029603218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151EF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029593218](https://openairdocs.org/sdr/DALA13029593218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161FF DELAMINATED. FABRICATED FLOOR PANEL IAW BFM 53-02-00, FIG 209.
- [SDR DALA13029583218](https://openairdocs.org/sdr/DALA13029583218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161EF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029573218](https://openairdocs.org/sdr/DALA13029573218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029563218](https://openairdocs.org/sdr/DALA13029563218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151FF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029553218](https://openairdocs.org/sdr/DALA13029553218.md): Floor Panel · punctured · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 162FF HAS PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029543218](https://openairdocs.org/sdr/DALA13029543218.md): Floor Panel · damaged · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF HAS SEVERAL BROKEN INSERTS & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029533218](https://openairdocs.org/sdr/DALA13029533218.md): Floor Panel · delaminated · Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Next page: https://openairdocs.org/deregistered/N318US-2018-09-28/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 = 'N318US' AND deregistration_id = 'N318US-2018-09-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N318US-2018-09-28/reports

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