# Service difficulty reports: N207FR

A list on [N207FR](https://openairdocs.org/aircraft/N207FR.md).

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

- [SDR ANCF202512221840](https://openairdocs.org/sdr/ANCF202512221840.md): Bearing · excess play · Dec 18, 2025 · N207FR · Airbus A320214 · Rudder Control System
  > HIGH AIR FRAME VIBRATION AT: ALT 17000, ALT 27000, SPD 330 KTS, SPP 310KTS. IAW AMM 27-34-00-200-001-A FUNCTIONAL CHK OF ELEV SERVO CONTROL BEARINGS FOR EXCESSIVE PLAY & CONDITION. IAW AMM 27-24-00-210-001-A VISUAL INSP OF RUDDER SERVO CONTROLS FOR HYD LEAKS
- [SDR ANCF20240502011](https://openairdocs.org/sdr/ANCF20240502011.md): Control Unit · unserviceable · Apr 28, 2024 · N207FR · Airbus A320214 · Engine Controls
  > ENG 1 THR LEVER DISAGREE DURING APPROACH ENG 1 WENT AT IDLE WHEN SLATS WERE EXTENDED LDGW 64.300 KG. IN ACCORDANCE WITH ASM 73-25-12 THE WIRING BETWEEN THE CTL-UNIT THROTTLE ENG1 8KS1 CONNECTOR D AND ECU 4000KS J4; AND BETWEEN CTL-UNIT THROTTLE ENG1 8KS1 CO
- [SDR ANCF20240430010](https://openairdocs.org/sdr/ANCF20240430010.md): Warning Message · illuminated · Apr 28, 2024 · N207FR · Airbus A320214 · Engine Indicating System
  > DURING ONE ENG START "ENG 1 ONE TLA FAULT". DURING TAKE OFF ONCES THE TAKE OFF POWER WAS SELECTED "ENG 1 THR LEVER DISAGREE ON ECAM, AND ENG 1 THR WENT TO IDLE. WE ABORTED THE TAKE AFF AT 30 KTS APPROXIMATELY. IN ACCORDANCE WITH TSM TASK 76-11-00-810-813-A R
- [SDR ANCF20231411034](https://openairdocs.org/sdr/ANCF20231411034.md): Control Unit · faulted · Nov 14, 2023 · N207FR · Airbus A320214 · Landing Gear System
  > BRAKES ALTN L RELEASED. INOP SYS ALTN L BRK. IAW TSM TASK 32-43-00-810-824-A REV.66 / DATE 01-NOV-2023, RESET OF BSCU WAS PERFROMED SATISFACTORILY. APTL
- [SDR F3LA2022010030011](https://openairdocs.org/sdr/F3LA2022010030011.md): Support Frame · corroded · Sep 23, 2022 · N207FR · Airbus A320214 · Fuselage Main, Structure
  > SUPPORT FRAME BETWEEN F65 AND FR70 AT STR 23R HAS HEAVY CORROSION. REMOVED AND REPLACED SUPPORT FROM AT FR69 TO FR70 STR 23R IAW SRM 51-74-11 AND SRM 51-42-11
- [SDR F3LA2022111000146](https://openairdocs.org/sdr/F3LA2022111000146.md): Stringer · corroded · Sep 22, 2022 · N207FR · Airbus A320214 · Fuselage Main, Longeron/Stringer
  > BULK CARGO S-39F, FR64 TO F67 HAS DEEP CORROSION AT SEVERAL FASTENER LOCATIONS. REMOVED AND REPLACED STRINGER P/N D5348012521401 BATCH 4009142 AT BULK CARGO FR64 TO FR67 S-39R IAW SRM 51-72-11-911-002 AND SRM 51-42-11.
- [SDR F3LA2022101100133](https://openairdocs.org/sdr/F3LA2022101100133.md): Frame · mechanic error · Sep 15, 2022 · N207FR · Airbus A320214 · Standard Practices/Structures
  > FRAME 69, S23L HAS DOUBLE DRILLED HOLES. REMOVED AND REPLACED FRAME 69 BETWEEN STRINGER 15 TO STRINGER 29 IAW SRM 51-42-11
- [SDR F3LA2022111000145](https://openairdocs.org/sdr/F3LA2022111000145.md): Stringer · corroded · Sep 13, 2022 · N207FR · Airbus A320214 · Fuselage Main, Structure
  > DISCREPANCY: REFERENCE NRB000859 AT CARGO COMPARTMENT. RH SIDE BETWEEN FR64 TO FR65 S-37 TO S-39 RIVETS WERE FOUND WITH CORROSION CORRECTIVE ACTION REMOVED AND REPLACED CORRODED STRINGER FR64-FR65 S-39R P/N D5348003022000 S/N 81130763/003/2022#A IAW EA A2-53R
- [SDR F3LA2022100300124](https://openairdocs.org/sdr/F3LA2022100300124.md): Plate · corroded · Sep 8, 2022 · N207FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > RH AFT PAX CABIN WET PLATE THAT ATTACH THE FLOOR BETWEEN FR68-69 HAS CORROSION AT HOLES. MANUFACTURED AND REPLACED WET PLATE IAW DWG D534800192 AND SRM 51-42-11
- [SDR F3LA2022101000129](https://openairdocs.org/sdr/F3LA2022101000129.md): Seat Track · corroded · Aug 21, 2022 · N207FR · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > PASSANGER RH SEAT TRACK Y-1292 BETWEEN FR20 TO FR21 HAS CORROSION AROUND AND IN THE CROWN AREA OF THE SEAT TRACK. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN RH Y-1292 BETWEEN FR20 AND FR21 IAW SRM 51-42-11 AND DRW# D53112782 REV 01.
- [SDR F3LA2022101900134](https://openairdocs.org/sdr/F3LA2022101900134.md): Support · corroded · Aug 19, 2022 · N207FR · Airbus A320214 · Fuselage Main, Structure
  > DISCREPANCY: REFERENCE NR B000525 AFT MAIN CABIN AT FR66 FLOOR SUPPORT STRUCTURE NEXT TO RH AFT PAX DOOR HAS CORROSION CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SUPPORT FR66 TO FR69 IAW SRM 51-42-11/END//
- [SDR F3LA2022100300120](https://openairdocs.org/sdr/F3LA2022100300120.md): Floor Support · corroded · Aug 19, 2022 · N207FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > AT MAIN CABIN AT FR66 LH SIDE ABOUT 13INCHES FROM DOOR CUT OUT, FLOOR SUPPORTS STRUCTURE HAS CORROSION. CORROSION FOUND OUT OF LIMITS IAW SRM 53-11-14-283-004. REMOVED AND REPLACED AFT CABIN FLOOR SUPPORT FR66 LH SIDE IAW SRM 51-42-11 AND SRM 51-44-11
- [SDR F3LA2022100300117](https://openairdocs.org/sdr/F3LA2022100300117.md): Floor Support · corroded · Aug 19, 2022 · N207FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN AT FR69 RBL31 FLOOR SUPPORT STRUCTURE HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE AT MAIN CABIN FR 68 TO FR70 RBL31. IAW DWG D53472201 REV B AND SRM 51-42-00 AND SRM 51-72-11-911-001
- [SDR F3LA2022101100132](https://openairdocs.org/sdr/F3LA2022101100132.md): Support Frame · corroded · Aug 18, 2022 · N207FR · Airbus A320214 · Fuselage Main, Structure
  > DISCREPANCY: REFERENCE NR B000466 SUPPORT FRAME BETWEEN FR69 TO FR70 S-23L HAS HEAVY CORROSION ON LOWER SURFACE. CORRECTIVE ACTION REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-42-11//END//
- [SDR F3LA2022100400122](https://openairdocs.org/sdr/F3LA2022100400122.md): Structure · corroded · Aug 14, 2022 · N207FR · Airbus A320214 · Fuselage Main, Structure
  > AFT LH PAX DOOR LOWER CUT OUT AFT CORNER STRUCTURE HAS CORROSION. BLENDED AREA AT AFT LH PAX DOOR LOWER CUT OUT IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-300-001. INSTALLED REPAIR STRAP AND FILLER IAW SRM 53-41-16-300-001
- [SDR F3LA2022100300123](https://openairdocs.org/sdr/F3LA2022100300123.md): Door Sill · corroded · Aug 14, 2022 · N207FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DISCREPANCY: AFT RH PAX DOOR CUT OUT LOWER STRUCTURE HAS CORROSION ON SEVERAL PLACES. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-29-283-001 CORRECTIVE ACTION: REMOVED AND REPLACED DOOR SILL AND SHAPE IAW 51-42-11
- [SDR F3LA2022101100131](https://openairdocs.org/sdr/F3LA2022101100131.md): Bracket · corroded · Aug 12, 2022 · N207FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE NR B000311 MAIN DCK AFT CABIN FLOOR STRUCTURE PLATE/BRACKET, LH, BETWEEN FR69 AND FR70 HAS CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PLATE/BRACKET IAW SRM 51-42-11//END//
- [SDR F3LA2022031400008](https://openairdocs.org/sdr/F3LA2022031400008.md): None · none · Mar 11, 2022 · N207FR · Airbus A320214 · Pneumatic Distribution System
  > DISCREPANCY: REFERENCE LP 191667 ITEM 1-SLIGHT DIRTY SOCK SMELL IN STEEP DESCENT WENT AWAY BEFORE LANDING. THIS SMELL WAS NOTICED IN FLIGHT DECK AND CABIN FOR SHORT PEROID -
- [SDR F3LA2021112300085](https://openairdocs.org/sdr/F3LA2021112300085.md): Unknown · odor · Nov 18, 2021 · N207FR · Airbus A320214 · Engine Bleed Air System
  > DURING DESCENT FA IN FRONT AND BACK OF CABIN SMELLED A VERY STRONG DIRTY SOCK ODOR. REF LP202944 ODOR EVENT WAS ISOLATED TO ENGINE 2 BLEED SYSTEM. DEFERRED ENGINE 2 BLEED AIR SUPPLY PER MEL 36-11-01A. FOUND NO OIL CONTAMINATION REF TSM 05-50-00-810-831
- [SDR F3LA2021111400083](https://openairdocs.org/sdr/F3LA2021111400083.md): Unknown · odor · Nov 11, 2021 · N207FR · Airbus A320214 · Air Distribution System
  > DURING DESCENT FA(B) CALLED AND SAID HE SMELLED A STRONG "DIRTY SOCK" ODOR. ALL FA'S AGREED. SMELL STRONGEST IN AFT CABIN. SMELL SEEMED TO DISSAPATE DURING APPROACH AND LANDING. PERFORMED TSM 71-0000-810-802-A NO SMOKE OR ODOR NOTED AT THIS TIME T/W P843059
- [SDR F3LA202003020013](https://openairdocs.org/sdr/F3LA202003020013.md): Unknown · smoke · Mar 1, 2020 · N207FR · Airbus A320214 · Air Distribution System
  > 03/02/2020 - PRELIMINARY SUBMISSION: LP1140723 ITEM 1 -- 5-10 MINUTES AFTER APU + PACK START UP CABIN FILLED WITH SMOKE/ FUME / SMELL. BURNING SMELL AND REDUCED VISIBILITY IN CABIN OBSERVED BY ALL 6 CREW MEMBERS. TURNED OFF APU BLEED +APU.
- [SDR F3LA2020021200008](https://openairdocs.org/sdr/F3LA2020021200008.md): Acm · seized · Feb 10, 2020 · N207FR · Airbus A320214 · Cabin Cooling System
  > LP 1175072 ITEM 2: STRONG ODER IN A/C. STRONGER IN REAR OF CABIN. ENG DEPT CREATING WORK SCOPE TO HELP WITH ID OF CAUSE AND T/S FOR PERMANENT FIX. R&R ACM PER A320 AMM 21-52-21-000-001-A, 21-52-21-400-001-A.
- [SDR F3LA2020020760006](https://openairdocs.org/sdr/F3LA2020020760006.md): Oil Cooler · leaking · Feb 6, 2020 · N207FR · Airbus A320214 · APU Oil System
  > TS DIRTY SOCK SMELL AS REQUIRED. DOWN TO APU REF TSM 05-50-00-869-051-A. INSPECTED APU FOR OIL LEAKS, FOUND AIR OIL COOLER AND FAN ASSEMBLY OIL COOLER LEAKING. APU WILL BE PLACED ON MEL ON LP1175030 ITEM 3.
- [SDR F3LA20200120002](https://openairdocs.org/sdr/F3LA20200120002.md): Oil System · leaking · Jan 19, 2020 · N207FR · Airbus A320214 · APU Oil System
  > 02/08/2020 - SUPPLEMENT ON LP 1175060 - REF TO MDDR# 1160287, FOUND APU LEAKING OIL, R&R APU IN REF TO TASK CARD MP49111-02, OPS/LEAK CHECK IS SATISFACTORY AT THIS TIME. T/W F9TAB4789C DUE 08/2020. T/W F9TAB4788C DUE 08/2020. T/WF9TAB4688C DUE 07/2020.HOIST, A
- [SDR F3LA202001030001](https://openairdocs.org/sdr/F3LA202001030001.md): Unknown · fumes · Jan 1, 2020 · N207FR · Airbus A320214 · Air Distribution System
  > THIS IS A SUPPLEMENT TO SDR F3LA202001030001 ORIGINAL SUBMITTED ON 01/03/2020. SUPPLEMENT: 01/07/2019 - PERFORMED FUME EVENT INSPECTION, NO DEFECTS FOUND PER TSM-05-50-00-810-831A, CLEARED MEL 49-10-01A AND RETURNED APU TO SERVICE. DISCREPENCY: LP1257733 ITEM
- [SDR F3LA201912110150](https://openairdocs.org/sdr/F3LA201912110150.md): Acm · damaged · Dec 9, 2019 · N207FR · Airbus A320214 · Cabin Cooling System
  > FUME EVENT ONCE APU TURNED ON. INSPECTED AND FOUND HEAT DAMAGE TO THE NR 1 PACK. INSTALLED NR 1 ACM IAW AMM 21-52-21-PB401, OPS CHECKED GOOD.
- [SDR F3LA2019012900008](https://openairdocs.org/sdr/F3LA2019012900008.md): Line · leaking · Jan 26, 2019 · N207FR · Airbus A320214 · Hydraulic System, Main
  > GREEN HYDRAULIC FLIUD LEVEL LOW. LEAK APPEARS TO BE ENG 1 PYLON. AC GROUNDED DUE TO LOSS OF HYD SYSTEM. REMOVED AND REPLACED ENGINE # 1 GREEN SYS PRESSURE PIPE. T/W USED F9TAB3947C, T/W USED F9T063, AMM 29-11-49-000-008-A. AC RETURNED TO SERVICE ALL OPS /
- [SDR F3LA2018122100482](https://openairdocs.org/sdr/F3LA2018122100482.md): Valve · faulty · Dec 17, 2018 · N207FR · Airbus A320214 · Waste Disposal System
  > DISCREPANCY: LP11766619-1 DURING #1 ENGINE START WITH APU BLEED AIR AN UNKNOWN ODOR ENTERED THE AIRCRAFT AND WAS IMMEDIATELY REPORTED BY THE FA'S. QRH PROCEDURES C/W, BTB. CORRECTIVE ACTION: AIRCRAFT WAS GROUNDED DUE TO EVENT, AND THEN A MAINTENANCE FERRY
- [SDR F3LA2017082800199](https://openairdocs.org/sdr/F3LA2017082800199.md): Battery · no test · Aug 27, 2017 · N207FR · Airbus A320214 · Emergency Lighting
  > EMERGENCY LIGHT FAULTED AFTER BATTERY CAPACITY TEST. REMOVED AND REPLACED THE EPSU BATTERY 11WL IAW AMM 33-51-38-000-002-A, AND 33-51-38-400-002-A. OPS CHECKED GOOD.
- [SDR F3LA2016031400010](https://openairdocs.org/sdr/F3LA2016031400010.md): Floor Panel · corroded · Mar 11, 2016 · N207FR · Airbus A320214 · Fuselage Main, Plate/Skin
  > DURING C CHECK INSPECTION NOTED AFT WET AREA FLOOR STRUCTURE AFT RT CORNER, BETWEEN FRAME 69 & 70, SHEAR PLATE CORRODED. R & R AFT WET AREA FLOOR STRUCTURE LT CORNER, FRAME 69 & 70, SHEAR PLATE IAW SRM 51-42-11.
- [SDR F3LA2016031400009](https://openairdocs.org/sdr/F3LA2016031400009.md): Shear Plate · corroded · Mar 11, 2016 · N207FR · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION NOTED AFT WET AREA FLOOR STRUCTURE AFT RT CORNER, BETWEEN FRAME 69 & 70, SHEAR PLATE CORRODED. R & R AFT WET AREA FLOOR STRUCTURE RT CORNER, FRAME 69 & 70, SHEAR PLATE IAW SRM 51-42-11.
- [SDR F3LA2011121100691](https://openairdocs.org/sdr/F3LA2011121100691.md): Actuator · tripped · Dec 8, 2011 · N207FR · Airbus A320214 · Leading Edge Slat Actuator
  > "F/CTL SLATS FAULT" (EMERGENCY DECLARED). TROUBLESHOT IAW TSM 27-81-00-810-810. FOUND ROTARY ACTUATOR 6029CM TRIPPED. R & R TYPE B ACTUATOR IAW AMM 27-84-49, PB401. NO FAULTS NOTED.
- [SDR F3LA2010061600443](https://openairdocs.org/sdr/F3LA2010061600443.md): Electrical Box · odor · Jun 16, 2010 · N207FR · Airbus A320214 · Entertainment System
  > REF: PILOT WRITE UP LOG PAGE 530969, ITEM 1, 06/16/2010. HOT SMELL NOTED ROW 24D. TV SYS SHUT OFF, SMELL WENT AWAY. AIR TURN BACK. DEFER REF IAW MEL 44-20-01AA CONTROL NR 1075944. NO ODOR NOTICED ON GROUND. REF LOG PAGE 530975, ITEM 2, 06/17/2010. R & R

## 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 = 'N207FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N207FR/reports

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