# Service difficulty reports: N201FR

A list on [N201FR](https://openairdocs.org/aircraft/N201FR.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR F3LA2021080400057](https://openairdocs.org/sdr/F3LA2021080400057.md): Intake · contaminated · Jul 30, 2021 · N201FR · Airbus A320214 · APU Core Engine
  > DISCREPANCY: STRONG BURNING RUBBER SMELL MID-FLIGHT ROWS 13-14 DURING DESCENT. / PERFORMED TSM 05-50-00-810-831-A DECISION TABLE MOST PROBABLE CAUSE APU. PERFORMED AMM 49-00-00-200-812-A. FOUND OIL ON INTAKE FLAP CLEANED AREA, OPENED APU AND INSPECTED, NO OTHE
- [SDR F3LA2019013100009](https://openairdocs.org/sdr/F3LA2019013100009.md): Slide · failed · Jan 28, 2019 · N201FR · Airbus A320214 · Escape Slide
  > DISCREPANCY: REFERENCE LOG PAGE LP1148549 ITEM 3, EPSU TEST FAILURE WITH MULTIPLE MX MESSAGES. AFTER FURTHER TROUBLE SHOOTING L1 DOOR SLIDE FOUND TO BE CAUSE. L1 DOOR SLIDE REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE REFERENCE
- [SDR F3LA2018101800457](https://openairdocs.org/sdr/F3LA2018101800457.md): Not Reported · malfunctioned · Oct 14, 2018 · N201FR · Airbus A320214 · Rudder Control System
  > ABORTED TAKE-OFF FOR RUDDER JAM/DIFFICULT DIRECTIONAL CONTROL. THE AIRCRAFT WAS GROUNDED DUE TO THE EVENT. MX PERFORMED YAW DAMP SYS TEST AMM 22-63-00-710-001-A, ADIRS SYS TEST AMM 34-14-00-740-004-A, AFS TEST AMM 22-91-00-710-001-A, AUTO CHANGEOVER FUNCTION A
- [SDR F3LA2018092500444](https://openairdocs.org/sdr/F3LA2018092500444.md): Door Frame · cracked · Sep 5, 2018 · N201FR · Airbus A320214 · Emergency Exits
  > LT FWD EMERG EXIT DOOR FWD I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT FWD EMERGENCY EXIT DOOR FWD I/B FRAME IAW EA A2-52R-34380.
- [SDR F3LA2018092500443](https://openairdocs.org/sdr/F3LA2018092500443.md): Door Frame · cracked · Sep 5, 2018 · N201FR · Airbus A320214 · Emergency Exits
  > LT AFT EMERG EXIT DOOR FWD I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT AFT EMERGENCY EXIT DOOR FWD I/B FRAME IAW EA A2-52R-34380.
- [SDR F3LA2018092500442](https://openairdocs.org/sdr/F3LA2018092500442.md): Door Frame · cracked · Sep 5, 2018 · N201FR · Airbus A320214 · Emergency Exits
  > RT FWD EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED RT FWD EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
- [SDR F3LA2018092400441](https://openairdocs.org/sdr/F3LA2018092400441.md): Door Frame · cracked · Sep 5, 2018 · N201FR · Airbus A320214 · Emergency Exits
  > RT AFT EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED RT AFT EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
- [SDR F3LA2018092400440](https://openairdocs.org/sdr/F3LA2018092400440.md): Door Frame · cracked · Sep 5, 2018 · N201FR · Airbus A320214 · Emergency Exits
  > LT FWD EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT FWD EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
- [SDR F3LA2018092100439](https://openairdocs.org/sdr/F3LA2018092100439.md): Door Frame · cracked · Sep 5, 2018 · N201FR · Airbus A320214 · Emergency Exits
  > LT AFT EMERGENCY EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT AFT EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.
- [SDR F3LA2018091700433](https://openairdocs.org/sdr/F3LA2018091700433.md): Dummy Rail · corroded · Sep 4, 2018 · N201FR · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LONGITUDINAL FLOORBEAM TOP CAP CORRODED, Y+503.2, FR16. REMOVED AND EVALUATED CORROSION ON MAIN CABIN LONGITUDINAL FLOORBEAM AT Y+503.2 FR16. MAT REMOVED.082", MAX ALLOWED.047" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004 FIG 006 SHEET 1, RE
- [SDR F3LA2018091700437](https://openairdocs.org/sdr/F3LA2018091700437.md): Door Sill · corroded · Sep 4, 2018 · N201FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL CORRODED AT THE FWD AND AFT BLANKING PLATE FASTENER HOLES. REMOVED AND REPLACED THE L2 DOOR SILL IAW SRM 53-41-14-300-001, 51-72-11-911-001, 51-42-11 AND AMM 38-30-00.
- [SDR F3LA2018091700436](https://openairdocs.org/sdr/F3LA2018091700436.md): Floor Support · corroded · Sep 4, 2018 · N201FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN LONGITUDINAL FLOORBEAM TOP CAP CORRODED, FR16-FR18 BL 8.5+Y. REMOVED AND EVALUATED CORROSION OF FLOORBEAM AT Y8.5 FR16-18. MAX ALLOWED REMOVAL IS.031" MAT. REMOVED.038 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004. REMOVED AND REPLACED FLOORB
- [SDR F3LA2018091700435](https://openairdocs.org/sdr/F3LA2018091700435.md): Floorbeam · corroded · Sep 4, 2018 · N201FR · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM TOP CAP, CORRODED 1292, FR16. REMOVED CORROSION AND EVALUATED FLOORBEAM 1292 FR16. REMOVED.0185 MATERIAL, FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, 52-11-15 AND 51-44-11.
- [SDR F3LA2018091700434](https://openairdocs.org/sdr/F3LA2018091700434.md): Door Sill · corroded · Sep 3, 2018 · N201FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION AROUND FASTENER HOLE AT FWD SECTION. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001, 53-41-14-283-002, 51-42-11 AMM 38-30-00.
- [SDR F3LA2018091300430](https://openairdocs.org/sdr/F3LA2018091300430.md): Floorbeam · corroded · Sep 3, 2018 · N201FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y765 CORRODED FR 68. REMOVED AND REPLACED FLOORBEAM -Y765 FROM FS 67 TO FS 70 IAW SRM 51-72-11, 51-42-11 AND 53-00-14.
- [SDR F3LA2018091300429](https://openairdocs.org/sdr/F3LA2018091300429.md): Floorbeam · corroded · Sep 3, 2018 · N201FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y765 CORRODED FR66. REMOVED AND REPLACED FLOORBEAM -Y765 FROM FS 64 TO FS 66 IAW SRM 51-72-11, 51-42-11 AND 53-00-14.
- [SDR F3LA2017021500081](https://openairdocs.org/sdr/F3LA2017021500081.md): Skin · corroded · Jan 27, 2017 · N201FR · Airbus A320214 · Fuselage Main, Plate/Skin
  > AFT RIGHT FUSELAGE LAVATORY BACKING SYSTEM EXHAUST VENT SKIN CUT-OUT SEPERATING AND CORRODED JUST FORWARD OF FRAME 70. REPAIRED THE SKIN.
- [SDR F3LA2014122901095](https://openairdocs.org/sdr/F3LA2014122901095.md): Hydraulic Line · failed · Dec 24, 2014 · N201FR · Airbus A320214 · Hydraulic System, Main
  > GREEN SYS HYD LINE FAILED, FLUID LOSS, RETURNED TO THE FIELD. R & R THE LINE ASSEMBLY IAW AMM 32-31-39-400-001-A. OPERATIONS IAW AMM 32-31-00-710-002-A01 & LEAK CHECKED NORMAL. LOG PAGE 911844 2.
- [SDR F3LA2013082600903](https://openairdocs.org/sdr/F3LA2013082600903.md): Skin · dented · Aug 16, 2013 · N201FR · Airbus A320214 · Leading Edge Devices
  > ACFT OUT OF SERVICE DURING C4/S1 CHECK. LT WING L/E NR 1 SLAT DAMAGED OTBD END. REPAIRED IAW SRM 57-40-00, PB201.
- [SDR F3LA2013082600902](https://openairdocs.org/sdr/F3LA2013082600902.md): Plate · corroded · Aug 10, 2013 · N201FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK. CABIN RT AFT SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6.B.(1)-(8). ACFT OUT OF SERVICE.
- [SDR F3LA2010082400486](https://openairdocs.org/sdr/F3LA2010082400486.md): Wire Harness · failed · Aug 22, 2010 · N201FR · Airbus A320214 · Equipment/Furnishings Wiring
  > SMOKE REPORTED IN AFT GALLEY. POWER WAS SHUTOFF AND BREAKERS PULLED, PERFORMED VISUAL INSP BEHIND AFT GALLEY UNIT, POWER CONTROL PANEL FOR COFFEE MAKERS, OVEN, INSPECTED WIRING HARNESS NO BURN MARKS, NO BURN MARKS ON PLUMBING LINES, FOUND AFT OVEN VENT FILTERS
- [SDR F3LA2009052600087](https://openairdocs.org/sdr/F3LA2009052600087.md): Attach Fitting · broken · May 24, 2009 · N201FR · Airbus A320214 · Wing, Control Surface Attach Fittings
  > DURING DAILY CHECK, DEN MAINTENANCE NOTED THE LEFT INBOARD ELEVATOR SERVO CONTROL ATTACH POINT ANTI-ROTATION LUG WAS BROKEN. MAINTENANCE PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTALLING A REPAIR LUG TO THE LEFT HAND ELEVATOR INBOARD SERVO CONTROL FITTIN

## 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 = 'N201FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N201FR/reports

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