# Service difficulty reports: N203FR, cancelled Dec 17, 2018

A list on [N203FR, cancelled Dec 17, 2018](https://openairdocs.org/deregistered/N203FR-2018-12-17.md).

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

- [SDR F3LA2018050100336](https://openairdocs.org/sdr/F3LA2018050100336.md): Doubler · gouged · Apr 23, 2018 · N203FR · Airbus A320214 · Cargo/Baggage Doors
  > AFT CARGO DOOR LOWER AFT INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE AFT CARGO DOOR LOWER INNER SKIN DOUBLER REPAIR IAW AMM 52-32-00-300-016, EA A2-52R-33760, 52-32-14-PB400-COMP-00, NTM 51-10-08M, 52-32-21-000-003-A, SRM 51-21-11, AND SRM 51
- [SDR F3LA2018050100335](https://openairdocs.org/sdr/F3LA2018050100335.md): Doubler · gouged · Apr 23, 2018 · N203FR · Airbus A320214 · Cargo/Baggage Doors
  > FWD CARGO DOOR LOWER AFT INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE FWD CARGO DOOR LOWER AFT INNER SKIN DOUBLER IAW SRM 52-41-11, 52-31-13, PB 401, CONF 00, EA A2-52R-34068, SRM 51-21-11, NTM 57-10-08, AND 51-10-01.
- [SDR F3LA2018050100334](https://openairdocs.org/sdr/F3LA2018050100334.md): Doubler · gouged · Apr 23, 2018 · N203FR · Airbus A320214 · Cargo/Baggage Doors
  > FWD CARGO DOOR LOWER FWD INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE DOUBLER AT FWD DOOR INNER SKIN IAW SRM 51-42-11, NTM 51-10-08, AMM 52-31-21-000-003-A, EA A2-52R-34068, AND SRM 51-21-11.
- [SDR F3LA2017070500184](https://openairdocs.org/sdr/F3LA2017070500184.md): Windshield · failed · Jul 2, 2017 · N203FR · Airbus A320214 · Flight Compartment Windows
  > FOUND THE CAPTAIN'S WINDSHIELD SHATTERED. REPLACED THE WINDSHIELD IAW AMM 56-11-11 PB 401. OPS CHECKED GOOD.
- [SDR F3LA2017051600138](https://openairdocs.org/sdr/F3LA2017051600138.md): Floor Support · corroded · May 10, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y1292 FROM FRAMES 64 - 66 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.
- [SDR F3LA2017051600139](https://openairdocs.org/sdr/F3LA2017051600139.md): Floor Support · corroded · May 9, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT -Y254 BETWEEN FRAMES 68 - 70 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051700141](https://openairdocs.org/sdr/F3LA2017051700141.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y1292 AT FR 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED, NEW FLOORBEAM -Y1292 AT FR66 IAW SRM A320-51-42-11 AND 51-72-911-01.
- [SDR F3LA2017051700140](https://openairdocs.org/sdr/F3LA2017051700140.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM Y765 AT FR66 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION ON FLOORBEAM Y765 AT FR66 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y765 AT FR66 REPLACE WITH NEW FLOORBEAM Y765 IAW SRM A320-51-72-11.
- [SDR F3LA2017051600132](https://openairdocs.org/sdr/F3LA2017051600132.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM Y1292 AT FR68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500137](https://openairdocs.org/sdr/F3LA2017051500137.md): Floor Support · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y765 BETWEEN FRAMES 67 AND 68 HAS CORROSION ON UPPER SERVICE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.
- [SDR F3LA2017051500136](https://openairdocs.org/sdr/F3LA2017051500136.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM Y254 BETWEEN FR66-FR67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED NEW FLOORBEAM Y254 BETWEEN FR66-FR67 IAW SRM 51-72-11, 51-42-11 AND 53-41-14.
- [SDR F3LA2017051500135](https://openairdocs.org/sdr/F3LA2017051500135.md): Floor Support · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT -Y765, FRAMES 67 - 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500134](https://openairdocs.org/sdr/F3LA2017051500134.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y765 AT FRAME 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500133](https://openairdocs.org/sdr/F3LA2017051500133.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.
- [SDR F3LA2017051500131](https://openairdocs.org/sdr/F3LA2017051500131.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500130](https://openairdocs.org/sdr/F3LA2017051500130.md): Floorbeam · corroded · May 8, 2017 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM -Y1292 AT FRAME 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2016081700001](https://openairdocs.org/sdr/F3LA2016081700001.md): Coffeemaker · odor · May 19, 2016 · N203FR · Airbus A320214 · Buffet/Galleys
  > F/A SMELLED ODOR COMING FROM AFT CABIN DESCRIBED AS POSSIBLY POPCORN, BURNING RUBBER, OF BURNED COFFEE. POSSIBLY COMING FROM HIGHER IN THE CABIN PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831A. IDENTIFIED THE MOST PROBABLE CAUSE OF THE ODOR TO BE COMING
- [SDR F3LA2016052000048](https://openairdocs.org/sdr/F3LA2016052000048.md): Coffeemaker · dirty · May 19, 2016 · N203FR · Airbus A320214 · Buffet/Galleys
  > REFERENCE LOG PAGE 989574, DURING CRUISE THE CREW NOTED AN ODOR COMING FROM THE AFT CABIN & THE ACFT DIVERTED. MX IDENTIFIED THE CAUSE OF THE ODOR TO BE THE AFT GALLEY COFFEE MAKER & FOUND BURNT DRIED COFFEE RESIDUE ON AFT GALLEY COFFEE MAKER. MX CLEANED & I
- [SDR F3LA2015112001153](https://openairdocs.org/sdr/F3LA2015112001153.md): Safety Valve · inoperative · Nov 15, 2015 · N203FR · Airbus A320214 · Landing Gear Door Retract Section
  > DISCREPANCY ITEM 1, SPOILERS 1 & 2 FAULT INFLIGHT. DISCREPANCY ITEM NR 2 NOSE WHEEL STEERING FAULT INFLIGHT. RESET SEC 1 & 2. OPERATIONS CHECKED OK IAW AMM 27-94-00-710-001 & -002. NR 2 R & R NLG ELECTRONIC BOX 5GC IAW AMM 32-51-12-000-001 & 32-51-12-400-0
- [SDR F3LA2015111201152](https://openairdocs.org/sdr/F3LA2015111201152.md): Line · chafed · Nov 8, 2015 · N203FR · Airbus A320214 · Hydraulic System, Main
  > HYD RESERVOIR LOW LEVLE, DURING CRUISE FLIGHT. DECLARED AN EMERGENCY. MX FOUND A HOLE IN THE RETURN LINE FOR THE NR 2 ENG THRUST REVERSER HYDRAULIC LINE. THE LINE WAS REPLACED IAW AMM 78-31-49 & HYD SYS SERVICED IAW AMM 29-13-00-710003-A.
- [SDR F3LA2015101401150](https://openairdocs.org/sdr/F3LA2015101401150.md): Slide · defective · Oct 10, 2015 · N203FR · Airbus A320214 · Escape Slide
  > EMERGENCY SLIDE LIGHT AT DOOR 1 RT INOPERATIVE. PLACED ON MEL CONTROL NR 1116039. REPLACED L1 DOOR SLIDE AMM 25-62-44-000-002-A & 25-62-44-400-006-A. OPERATIONAL CHECKED GOOD, LIGHTS OPERATE NORMAL & PLACARD REMOVED.
- [SDR F3LA2015030901117](https://openairdocs.org/sdr/F3LA2015030901117.md): Wire · damaged · Mar 7, 2015 · N203FR · Airbus A320214 · Light System Wiring
  > DISCREPANCY, EMER EXIT LIGHTS INOPERATIVE AT L1, L2, R1 & R2. RETERMINATED WIRING AT ALL 4 EPSUS AS REQUIRED, COMPLIED WITH EA A2-33R-33040. EMER LIGHTS OPERATIONS CHECKED GOOD. PN INVOLVED, 10WL 3351-5408, 11WL 3351-1917, 12WL 3351-1779 & 13WL 3351-1927.
- [SDR F3LA2013111800934](https://openairdocs.org/sdr/F3LA2013111800934.md): Seat Track · corroded · Oct 30, 2013 · N203FR · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C8/S2 CHECK. SEAT TRACK Y1292 HAS CORROSION AT FRAME 16. SEAT TRACK CORROSION EVALUATED AND FOUND OUT OF LIMITS. REMOVED DAMAGED TRACK AND INSTALLED NEW SEAT TRACK, IAW SRM 51-42-11, SECT 5.A THRU C.6 AND SECT 7.B3 A-D.
- [SDR F3LA2013111800933](https://openairdocs.org/sdr/F3LA2013111800933.md): Skin · damaged · Oct 23, 2013 · N203FR · Airbus A320214 · Elevator, Plate/Skin
  > DURING C8/S2 CHECK. THERMOGRAPHIC INSPECTION OF LT ELEVATOR REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00, PB201, PARA 2.A.-B, PARA. 2.B, 2.B(1)(A)2, SRM 55-21-11, PB201, C1 PARA.5.E.(2)(A)(B), FIGURE 20
- [SDR F3LA2013111800932](https://openairdocs.org/sdr/F3LA2013111800932.md): Sill · corroded · Oct 22, 2013 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING C8/S2 CHECK. FORWARD CARGO LOWER SILL UPPER SURFACE HAS CORROSION BETWEEN FRAMES 26 AND 27. REPAIRED IAW SRM 51-74-00 PARA 6.A - 6.B(2}(5), SRM 51-75-12, SRM 51-21-11 AND SRM 51-23-11.
- [SDR F3LA2013111800931](https://openairdocs.org/sdr/F3LA2013111800931.md): Sill · corroded · Oct 22, 2013 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING C8/S2 CHECK. FORWARD CARGO DOOR SILL LOWER SKIN HAS SURFACE CORROSION ON UPPER SURFACE AT FRAMES 24 TO 25. REPAIRED IAW SRM 5L-74-00 PARA 6.A-6.B.
- [SDR F3LA2013111800930](https://openairdocs.org/sdr/F3LA2013111800930.md): Shear Tie · corroded · Oct 20, 2013 · N203FR · Airbus A320214 · Fuselage Internal Mounting Structure
  > DURING C8/S2 CHECK, LT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. REMOVED AND REPLACED IAW SRM 51-42-11, PARAGRAPH 6.B., 1 THROUGH 8.
- [SDR F3LA2013111800929](https://openairdocs.org/sdr/F3LA2013111800929.md): Shear Tie · corroded · Oct 20, 2013 · N203FR · Airbus A320214 · Fuselage Internal Mounting Structure
  > DURING C8/S2 CHECK. RT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. R & R IAW SRM 51-42-11, PARA 6.B., 1 THROUGH 8.
- [SDR F3LA2012050400750](https://openairdocs.org/sdr/F3LA2012050400750.md): Lamp · burned out · May 1, 2012 · N203FR · Airbus A320214 · Emergency Lighting
  > SEAT ROW 25 EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-18-400-002A. OPS CHECKED OK.
- [SDR F3LA2012050400749](https://openairdocs.org/sdr/F3LA2012050400749.md): Lamp · burned out · May 1, 2012 · N203FR · Airbus A320214 · Emergency Lighting
  > SEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. R & R BULBS, IAW AMM 33-41-11-400-002A, 33--41-11-000-002A. OPS CHECKED OK.
- [SDR F3LA2012011300699](https://openairdocs.org/sdr/F3LA2012011300699.md): Electrical Box · failed · Jan 12, 2012 · N203FR · Airbus A320214 · Entertainment System
  > ODOR OF ELETRICITY BETWEEN ROW 3 AND 4. NO VISIBLE SMOKE. TURNED OFF LIVE TV AND ODOR CLEARED. PERFORMED ELETRICAL ODOR SYS INTEGRITY CHECK IAW LTV AMM 44-25-00. NO DISCREPANCIES NOTED. CHANGED SEB IAW LTV AMM 44-25-00. OPS CHECKED GOOD.
- [SDR F3LA2011080400663](https://openairdocs.org/sdr/F3LA2011080400663.md): Feel Unit · binding · Jul 29, 2011 · N203FR · Airbus A320214 · Rudder Control System
  > REFERENCE PILOT REPORT LOG PAGE 615630 ITEM 1, UPON TOUCHDOWN PILOT NEEDED RIGHT RUDDER TO STRAIGHTEN NOSE BUT RUDDER FELT LOCKED IN CENTERED POSITION. AFTER APPLYING MORE PRESSURE PEDAL UNLOCKED AND APPEARED TO WORK NORMALLY. REMOVED AND REPLACED ARTIFICIAL F
- [SDR F3LA2010111400548](https://openairdocs.org/sdr/F3LA2010111400548.md): Module · loose · Nov 14, 2010 · N203FR · Airbus A320214 · Emergency Lighting
  > C-CHECK: NON ROUTINE N0694; EMERGENCY EXIT LIGHTS ON SEAT ROWS 16 AND 24 ARE INOP. RETERMINATED PINS ON EMERGENCY EXIT LIGHT CONNECTORS AT SEATS 16 LT AND 24 LT IAW AMM 33-51-19-020-051, STEP 4A1C AND AMM 33-51-19-420-051 STEP 4B1B. OPS CHECK GOOD IAW AMM 33-
- [SDR F3LA2010111400547](https://openairdocs.org/sdr/F3LA2010111400547.md): Floorbeam · corroded · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0566; MAIN CABIN FLOORBEAM RT SIDE NR4 BETWEEN FRAME 67-69, CORROSION ON BOTTOM SIDE OF FLOORBEAM AT FASTENER HOLE. R & R FLOORBEAM IAW SRM 51-72-11, PAGE 1 AND 2.
- [SDR F3LA2010111400546](https://openairdocs.org/sdr/F3LA2010111400546.md): Plate · corroded · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0561; AFT GALLEY UNDERFLOOR STRUCTURE RT LATERAL SHEAR PLATE BETWEEN FRAME 69 AND 70, HAS CORROSION AT 8 IN AFT OF FRAME 69 (ABOUT 2 SQUARE INCHES). R & R SHEARPLATE IAW SRM 51-42-11.
- [SDR F3LA2010111400545](https://openairdocs.org/sdr/F3LA2010111400545.md): Sill · corroded · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0558; MAIN CABIN FLOOR AT FRAME 68L FLOOR SUPPORT HAS CORROSION APPROX 25 SQ IN AT THE FASTENER HOLES. CORROSION ON FLOOR SILL. REMOVED CORROSION ON L-2 DOOR SILL AT FRAME 68 IAW SRM 51-74-00 BLEND OUT FOUND TO BE OUT OF LIMITS, REPAIRED
- [SDR F3LA2010111400544](https://openairdocs.org/sdr/F3LA2010111400544.md): Floorbeam · corroded · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0557; MAIN CABIN FLOORBEAM, NR 4 LT BETWEEN FRAME 67-68 HAS APPROX 2 SQ IN OF CORROSION AT THE FASTENER HOLES. R & R FLOORBEAM IAW SRM 51-44-11, SRM 51-42-11.
- [SDR F3LA2010111400543](https://openairdocs.org/sdr/F3LA2010111400543.md): Floor Panel · delaminated · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0401; FLOORBOARD UNDER LAV E IS DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.
- [SDR F3LA2010111400542](https://openairdocs.org/sdr/F3LA2010111400542.md): Transition Panel · debonded · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0291; FWD CARGO TRANSITION PANEL 132FF UPPER SURFACE DEBONDED 6 SQ IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.
- [SDR F3LA2010111400541](https://openairdocs.org/sdr/F3LA2010111400541.md): Transition Panel · delaminated · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0289; FWD CARGO TRANSITION PANEL 132GF UPPER SURFACE IS DELAMINATED IN 2 PLACES, 2 SQUARE IN, 4 SQUARE IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.
- [SDR F3LA2010111400540](https://openairdocs.org/sdr/F3LA2010111400540.md): Floor Panel · corroded · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Floor Panel
  > C-CHECK: FWD CARGO PIT TRANSITION FLOOR PANEL 131BF UPPER SURFACE AFT END DISBOUNDED 8 SQUARE INCHES. FABRICATED TRANSITION PANEL IAW MCW IRM 9701 REV G.
- [SDR F3LA2010111400539](https://openairdocs.org/sdr/F3LA2010111400539.md): Floor Panel · punctured · Nov 14, 2010 · N203FR · Airbus A320214 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0286; FWD CARGO TRANSITION FLOOR PANEL 131BF HAS A 1 SQUARE IN PUNCTURE. FABRICATED REPLACEMENT PANEL IAW MCG 9701, REV G.
- [SDR F3LA2010111400538](https://openairdocs.org/sdr/F3LA2010111400538.md): Cover · gouged · Nov 14, 2010 · N203FR · Airbus A320214 · Cargo/Baggage Doors
  > C-CHECK: NON ROUTINE N0138; FWD CARGO DOOR INTERNAL SIDE HAS 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 26.5 INCHES FWD AFT DOOR SEAL IS GOUGED, THAT MEASURES 1/8 INCH WIDE BY 3/4 INCH LONG BY.008 INCH DEEP. REPAIRED IAW A320SRM 52-31-00 PARAGRAPH (O).
- [SDR F3LA2010111400537](https://openairdocs.org/sdr/F3LA2010111400537.md): Seal · gouged · Nov 14, 2010 · N203FR · Airbus A320214 · Cargo/Baggage Doors
  > C-CHECK: NON ROUTINE N0134; AFT CARGO DOOR INTERNAL SIDE HAS 2 IN ABOVE THE LOWER SEAL AND 25 INCHES OF FWD SEAL IS GOUGED THAT MEASURES.3750 IN WIDE X.7500 IN LONG X 0018 INCH DEEP. REPAIRED IAW SRM 52-31-00, PARAGRAPH (O)
- [SDR F3LA2010111400536](https://openairdocs.org/sdr/F3LA2010111400536.md): Panel · gouged · Nov 14, 2010 · N203FR · Airbus A320214 · Cargo/Baggage Doors
  > C-CHECK: NON ROUTINE N0132; AFT CARGO DOOR INTERNAL SIDE HAS A 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 27 INCHES FWD OF AFT SEAL IS A GOUGE THAT MEASURES.7500 IN WIDE BY 1 IN LONG BY.090 IN DEEP. REPAIRED IAW SRM 52-30-00, PARAGRAPH (O).
- [SDR F3LA2010071400466](https://openairdocs.org/sdr/F3LA2010071400466.md): Bleed Valve · faulted · Jul 13, 2010 · N203FR · Airbus A320214 · Compressor Bleed Valve
  > AIR TURNBACK DUE TO ENGINE NUMBER 1 CONTROL VALVE FAULT. REMOVED AND REPLACED TRANSIENT BLEED VALVE REFERENCE AMM 75-26-10-000-001 AND AMM 75-26-10-400-001. OPERATIONAL CHECK GOOD.
- [SDR F3LA2009120400241](https://openairdocs.org/sdr/F3LA2009120400241.md): Relay · inoperative · Dec 4, 2009 · N203FR · Airbus A320214 · Emergency Lighting
  > REF LOG PAGE 492624. FLIGHT CREW MAD A BLOCK TURN BACK DUE TO THE F/A CIDS PANEL EMERGENCY LIGHTS ON AND COULD NOT BE RESTORED AND TURNED OFF. MX REMOVED AND REPLACED RELAY 8WL IAW AMM 33-31-00-710-004.
- [SDR F3LA2009042700081](https://openairdocs.org/sdr/F3LA2009042700081.md): Oxygen Mask · no test · Apr 24, 2009 · N203FR · Airbus A320214 · Passenger Oxygen System
  > DURING AIRCRAFT INDUCTION CHECK, THE FORWARD LAVATORY OXYGEN MASK WOULD NOT DROP DURING THE MANUAL MASK DROP TEST. MAINTENANCE REPACKED THE OXYGEN MASK AND PERFORMED SATISFACTORY DROP TEST, REFERENCE AMM 35-23-00-550-053.

## 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 = 'N203FR' AND deregistration_id = 'N203FR-2018-12-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N203FR-2018-12-17/reports

---
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