# Service difficulty reports: N202FR

A list on [N202FR](https://openairdocs.org/aircraft/N202FR.md).

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

- [SDR F3LA2021082000061](https://openairdocs.org/sdr/F3LA2021082000061.md): Latch · out of adjust · Aug 19, 2021 · N202FR · Airbus A320214 · Fluid Service Doors
  > DISCREPANCY: LP1199237 ITEM 1: AT APPROXIMATELY 80-90 KNOTS ON TAKEOFF, REFUEL PANEL CAME OPEN. T/O WAS ABORTED. HIGHEST BRAKE TEMP WAS 738. CORRECTIVE ACTION: ADJUSTED REFUELING PANEL DOOR LATCHES. OPS CHECKED GOOD. REF AMM 28-25-58-400-001-A.
- [SDR F3LA2021072100056](https://openairdocs.org/sdr/F3LA2021072100056.md): Slide · leaking · Jul 10, 2021 · N202FR · Airbus A320214 · Escape Slide
  > R1 SLIDE RESERVOIR PRESSURE IS FOUND OUT OF LIMITS. PER EO # A0-25EO-35106, AD 2020-25-03. REMOVED R1 DOOR SLIDE ASSY IAW AMM 25-62 44-012-A. INSTALLED R1 DOOR SLIDE ASSY PER AMM 23-62-44-400-805-A. TEST OK.
- [SDR F3LA2021050300034](https://openairdocs.org/sdr/F3LA2021050300034.md): Line · failed · Apr 29, 2021 · N202FR · Airbus A320214 · Hydraulic System, Main
  > LP133846 ITEM 1 DISCREPENCY -- HYD Y RSVR LO LVL CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENG YELLOW HCU PIPE REF AMM 29-13-49-000-048-A AND AMM 29-1349-400-099-A OPS CHECK/LEAK CHECK GOOD. T/W F9T10230C DUE 6/21. SERVICED YELLOW HYD SYST. REF AMM 12-12-29-6
- [SDR F3LA201909030101](https://openairdocs.org/sdr/F3LA201909030101.md): Unknown · odor · Sep 2, 2019 · N202FR · Airbus A320214 · Air Distribution System
  > SMELLED BURNING ELECTRIC FOR ABOUT 30 SEC ONLY IN COCKPIT NO SMOKE ASSOCIATED W/SMELL. CONDUCTED VISUAL INSPECTION OF AVIONICS COMPARTMENT AND NO DEFECTS FOUND AT THIS TIME. PERFORMED 10 MINUTE GROUND RUN. NO DEFECTS OF SMELLS ACCURD. OPS CHECK GOOD. OK FOR SE
- [SDR F3LA2019051700038](https://openairdocs.org/sdr/F3LA2019051700038.md): Apu · leaking · May 15, 2019 · N202FR · Airbus A320214 · APU Core Engine
  > DISCREPANCY: REFERENCE LP1170958 ITEM#1 - ON DECENT F/A'S NOTICED STRONG ACRID ODOR WAS ALSO NOTICED IN THE COCKPIT. CORRECTIVE ACTION - REF TDI CNTRL# 1150146 FOR PRIOR FUME EVENT. PER ES# AO21T - 34386 C/W TROUBLESHOOTING IAW TSM 05-50-00-810-831-A. CAPTAIN
- [SDR F3LA2019051400037](https://openairdocs.org/sdr/F3LA2019051400037.md): Apu · leaking · May 11, 2019 · N202FR · Airbus A320214 · APU Core Engine
  > DISCREPANCY: REFERENCE LP1110900 ITEM 1. FIRST FLT OF THE DAY TURNED APU ON AND A STRONG DIRTY MUSTY SOCK ODOR FILLED THE CABIN. TURNED PACKS OFF AND ODOR RESCINDED. CORRECTIVE ACTION: TROUBLE SHOOTING PER TSM 05-50-00-810-831-A AND EA#A0-211-34386 FOUND OIL L
- [SDR F3LA2018110800478](https://openairdocs.org/sdr/F3LA2018110800478.md): Panel · defective · Nov 6, 2018 · N202FR · Airbus A320214 · Communications System
  > DISCREPANCY: REFERENCE LOG PAGE LP1112557 ITEM 1, RMP 1 MALFUNCTION VERY STRONG ELECTRICAL ODOR. CORRECTIVE ACTION: REMOVED AND REPLACED 1RG1 RMP REF AMM 23-13-13-400-001-A. OPS TEST OK, A/C OK TO CONTINUE./END/
- [SDR F3LA2018103100475](https://openairdocs.org/sdr/F3LA2018103100475.md): Control Cable · corroded · Oct 24, 2018 · N202FR · Airbus A320214 · Rudder Control System
  > DISCREPANCY: REFERENCE N/R 2168N511 RUDDER LT OUTBOARD CABLE RUSTED LOCATED UNDER DUMMY BEAM Y503.2. CORRECTIVE ACTION: CABLE FWD CONNECTION REMOVED AND REPLACED WITH NEW CABLE IAW AMM 27-21-61 PB401 AND AMM 27-21-820-002-A./END/
- [SDR F3LA2018102200459](https://openairdocs.org/sdr/F3LA2018102200459.md): Floorbeam · corroded · Oct 16, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R 2168N412, P/R (721615) FLOORBEAM Y765 CORRODED AT FR66-70. CORRECTIVE ACTION: EVALUATED FLOORBEAM Y765 AT FR66-70. REMOVED.030 MAT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11./END/
- [SDR F3LA2018102900469](https://openairdocs.org/sdr/F3LA2018102900469.md): Beam · cracked · Oct 15, 2018 · N202FR · Airbus A320214 · Engine Thrust Reverser
  > DISCREPANCY: REFERENCE N/R 2168N342 CRACK ON ENG 2 I/B THRUST REVERSER PIVOT FITTING BEAM. CORRECTIVE ACTION: REMOVED AND REPLACED NR 2 ENG I/B THRUST REVERSER KEEL BEAM UPPER FAIRING WEB IAW GOODRICH CMM 78-32-36 REPAIR 61./END/
- [SDR F3LA2018102500466](https://openairdocs.org/sdr/F3LA2018102500466.md): Floorbeam · corroded · Oct 12, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y254 CORRODED AT FR16. REMOVED AND REPLACED FLOORBEAM -Y254 AT FR16 IAW SRM 51-72-11 AND SRM 51-74-00 TASK 5-A AND 53-11-14-283-004.
- [SDR F3LA2018102500465](https://openairdocs.org/sdr/F3LA2018102500465.md): Floorbeam · corroded · Oct 12, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y1292 CORRODED AT FR16. REMOVED AND REPLACED FLOORBEAM -Y1292 AT FR 16 IAW SRM 51-72-11, SRM 51-74-00, TASK 5-A AND SRM 53-11-14-283-004.
- [SDR F3LA2018102200461](https://openairdocs.org/sdr/F3LA2018102200461.md): Floorbeam · corroded · Oct 12, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R 2168N291, FLOORBEAM Y1292 CORRODED AT FR16. CORRECTIVE ACTION: EVALUATED FLOORBEAM Y1292 AT FR16 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004. REPLACED FLOORBEAM IAW SRM 51-72-11-911-001./END/
- [SDR F3LA2018102900473](https://openairdocs.org/sdr/F3LA2018102900473.md): Floorbeam · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R 2168N246, FLOORBEAM CORRODED BETWEEN FR16 TO FR20. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM IAW 51-72-11-911 AND 53-11-15-283-003./END/
- [SDR F3LA2018102900470](https://openairdocs.org/sdr/F3LA2018102900470.md): Door Sill · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R 2168N238, L2 DOOR SILL CORRODED AT FR66 FWD SPLICE. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR SILL (L2 DOOR) IAW SRM 53-41-14-283-002, SRM 51-72-11-911-001, AMM 38-30-00-010-002, AMM 38-30-00-410-002A, AMM 52-13-31-000-003-A AND A
- [SDR F3LA2018102600467](https://openairdocs.org/sdr/F3LA2018102600467.md): Door Sill · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R 2168N247, R2 DOOR SILL CORRODED AT FWD SPLICE FR66. CORRECTIVE ACTION: REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11 AND SRM 53-41-14./END/
- [SDR F3LA2018102300464](https://openairdocs.org/sdr/F3LA2018102300464.md): Floorbeam · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R 2168N233 FWD DUMMY BEAM Y503.2 CORRODED BETWEEN FR12 TO FR16. CORRECTIVE ACTION: DUMMY FLOORBEAM REMOVED AND REPLACED IAW SRM 51-72-11-911 (FR12 TO FR16)./END/
- [SDR F3LA2018102300463](https://openairdocs.org/sdr/F3LA2018102300463.md): Floorbeam · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R 2168N242, FLOORBEAM -Y765 CORRODED AT FR66-FR70. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM -Y765 FR66 TO FR70 IAW SRM 51-72-11, 51-44-11, 53-00-14-283-002./END/
- [SDR F3LA2018102300462](https://openairdocs.org/sdr/F3LA2018102300462.md): Floorbeam · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R 2168N241, FLOORBEAM Y254 CORRODED 2 INCHES FWD OF FR66. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM Y254 FR66 IAW SRM 51-72-11-911-001, 51-74-00, 51-44-11, 53-00-14-283-003./END/
- [SDR F3LA2018102200460](https://openairdocs.org/sdr/F3LA2018102200460.md): Shear Web · corroded · Oct 11, 2018 · N202FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R 2168N230, LT FR70 LATERAL SHEAR WEB PLATE AT CABIN FLOOR CORROSION. CORRECTIVE ACTION: EVALUATED LT FR70 SHEAR WEB FOUND TO BE OUT OF LIMITS IAW SRM 51-11-11. REPLACED SHEAR WEB IAW SRM 51-72-11./END/
- [SDR F3LA2018072600375](https://openairdocs.org/sdr/F3LA2018072600375.md): Unknown · odor · Jul 25, 2018 · N202FR · Airbus A320214 · Air Distribution System
  > FLIGHT ATTENDANTS COMPLANIED OF ODOR FUMES DURING TAXI. UPON DEBRIEF THEY SAID THEY COULD SMELL IN DESCENT. DID TRY TO ISOLATE BETWEEN PACK 1 AND 2 DURING SHORT TAXI, NO HELP. PER AMM 05-50-00-810-831-1A. INSPECTED ENGINE. APU AND PACKS FOR POTENTIAL OIL AND H
- [SDR F3LA2018060400350](https://openairdocs.org/sdr/F3LA2018060400350.md): Unknown · odor · May 31, 2018 · N202FR · Airbus A320214 · Air Distribution System
  > AT FL350 F/AS CALLED AND SMELLED AN ODOR LIKE MUSTY DIRTY SOCKS, ELECTRICAL, NAIL POLISH SWEET ODOR FROM ROW 14 AFT. RAN ELIMINATION OF ODOR IN CABIN /COCKPIT CHECKLIST IAW VOL 2. DECLARED EMERGENCY, LANDED SAFELY. MAINTENANCE PERFORMED TSM 05-50-00-810-8
- [SDR F3LA2016091500055](https://openairdocs.org/sdr/F3LA2016091500055.md): Proximity Sensor · out of adjust · Sep 14, 2016 · N202FR · Airbus A320214 · Landing Gear Position and Warning
  > LANDING GEAR NOT UPLOCKED. LANDING SYSTEM DISAGREE, AIR TURNBACK. POST FLIGHT REPORT SHOWED 25GA NLG EXTENTION PROXIMITY SWITCH IAW TSM 32-31-00-810-842-A AND 32-31-00-810-868-A. REMOVED AND REPLACED PROXIMITY SWITCH 25GA AND ADJUSTED DIMENSIONAL CHECKS FOR
- [SDR F3LA2013091600909](https://openairdocs.org/sdr/F3LA2013091600909.md): Plate · corroded · Sep 3, 2013 · N202FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > ACFT IS OUT OF SERVICE FOR C4/S1 CHECK. AFT CABIN LATERAL PLATE HAS CORROSION AT FR 69-70, S23R. R & R SHEAR PLATE IAW SRM 51-42-11, PAR 6, PAR 7, AND PAR 13.
- [SDR F3LA2013091600908](https://openairdocs.org/sdr/F3LA2013091600908.md): Skin · gouged · Aug 27, 2013 · N202FR · Airbus A320214 · Fuselage Main, Plate/Skin
  > ACFT IS OUT OF SERVICE FOR C4/S1 CHECK. LOWER FUSELAGE AT FR 53, STRINGER 37L, DENTED WITH A GOUGE IN THE CENTER. REPAIRED IAW SRM 53-41-11, PB201.
- [SDR F3LA2013091600907](https://openairdocs.org/sdr/F3LA2013091600907.md): Skin · dented · Aug 27, 2013 · N202FR · Airbus A320214 · Fuselage Main, Plate/Skin
  > ACFT IS OUT OF SERVICE FOR C4/S1 CHECK. RT FWD FUSELAGE FR 10, STRINGER 23R DENTED. REPAIRED IAW SRM 53-11-11 PB201, PARA 5.J.
- [SDR F3LA2013091600906](https://openairdocs.org/sdr/F3LA2013091600906.md): Skin · dented · Aug 19, 2013 · N202FR · Airbus A320214 · Fuselage Main, Plate/Skin
  > ACFT OUT OF SERVICE FOR C4/S1 CHECK. DENT FWD OF THE L2 DOOR APPROXIMATELY.054" DEEP, 3.5" LONG, 3.375" WIDE. REPAIRED IAW SRM 53-00-11, PB201, PARA 4.A.
- [SDR F3LA2012102800807](https://openairdocs.org/sdr/F3LA2012102800807.md): Line · chafed · Oct 29, 2012 · N202FR · Airbus A320214 · Hydraulic System, Main
  > YELLOW SYS LOW LEVEL HYDRAULICS. R & R NR 2 ENGINE HYD LOW PRESSURE SWITCH TUBE. REF AMM 29-13-49-000-005A AND 29-13-49-400-005A. OPS AND LEAK CHECK GOOD.
- [SDR F3LA2012003140721](https://openairdocs.org/sdr/F3LA2012003140721.md): Proximity Switch · failed · Mar 10, 2012 · N202FR · Airbus A320214 · Door Warning System
  > MAIN CABIN DOOR DOES NOT SHOW CLOSED ON ECAM WHEN IT IS CLOSED. R & R LT 1 DOOR PROXIMITY SWITCH, OPS CHECK GOOD AMMS2-71-11-401.
- [SDR F3LA2012022300711](https://openairdocs.org/sdr/F3LA2012022300711.md): Girt Bar · out of adjust · Feb 17, 2012 · N202FR · Airbus A320214 · Emergency Equipment
  > R2 DOOR ARMED INDICATION INTERMITTENT. FOUND R2 DOOR GIRT BAR FITTING OUT OF ADJUSTMENT. ADJUSTED R2 DOOR GIRT BAR FITTING AMM 52-13-00-820-057 A.
- [SDR F3LA2012021400708](https://openairdocs.org/sdr/F3LA2012021400708.md): Proximity Switch · failed · Feb 11, 2012 · N202FR · Airbus A320214 · Door Warning System
  > L1 DOOR INDICATES OPEN WHEN IT IS CLOSED. R & R L1 DOOR PROXIMITY SWITCH AMM52-71-11, PB 401.

## 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 = 'N202FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N202FR/reports

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