# Service difficulty reports: N207AN

A list on [N207AN](https://openairdocs.org/aircraft/N207AN.md).

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

- [SDR SIMA20260306001](https://openairdocs.org/sdr/SIMA20260306001.md): Seat Track · gouged · Mar 6, 2026 · N207AN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > NRWC#F106711- RH OTBD SEAT TRACK BETWEEN FRAME 23 AND 24 'IS CHAFED / GOUGED' FOUND TO BE OUT OF LIMITS. (MAJOR REPAIR) C/W REPAIR OF RH OTBD SEAT TRACK IAW ERS-EJ-53MR-5379.
- [SDR SIMA20260303001](https://openairdocs.org/sdr/SIMA20260303001.md): Seat Track · corroded · Mar 3, 2026 · N207AN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING PASSENGER SEAT REMOVAL FOR HEAVY CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK TO BE CORRODED BETWEEN FRAMES 19-20. (MAJOR REPAIR) (LEVEL 2 CORROSION). REPAIRED SEAT TRACK IAW ERS EJ-53MR-5374.
- [SDR SIMA20260207003](https://openairdocs.org/sdr/SIMA20260207003.md): Light · inoperative · Feb 7, 2026 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > RH#1 EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT INOP FAILED INSPECTION. COMPLETE:INSTALLED NEW RH#1 EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT IAW AMM 33-50-21 OPS CHECK GOOD
- [SDR SIMA20260207004](https://openairdocs.org/sdr/SIMA20260207004.md): Elec Connector · disconnected · Feb 7, 2026 · N207AN · Emb ERJ170200LR · Light System Wiring
  > COCKPIT EMERGENCY LIGHT INOP. REMOVED LIGHT AND FOUND TO NOT BE PLUGGED IN. REINSTALLED LIGHT IAW AMM 33-50-03, OPTS CHECK GOOD
- [SDR SIMA20251201001](https://openairdocs.org/sdr/SIMA20251201001.md): Battery · inoperative · Dec 1, 2025 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHTS ON FWD PASSENGER DOOR WILL NOT ILLUMINATE. FOUND EMERGENCY LIGHT POWER UNIT #2 TO BE INOP. RAR EMERGENY LIGHT POWER UNIT IAW AMM 33-50-01. OPC GOOD.
- [SDR SIMA20250927001](https://openairdocs.org/sdr/SIMA20250927001.md): Light · missing · Sep 27, 2025 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > CCI- FOUND A PIECE OF PHOTOLUMINESCENT STRIP IN MAIN CABIN MISSING AT SEAT 4DF. OPEN.
- [SDR SIMA20240119001](https://openairdocs.org/sdr/SIMA20240119001.md): Battery · inoperative · Jan 19, 2024 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT OVER ROW 12 IS OUT-C/A-RAR CABIN EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-13 AND EMERGENCY LIGHT POWER UNIT #4 IAW AMM 33-50-01 OPERATIONAL CHECK GOOD
- [SDR SIMA2024010231001](https://openairdocs.org/sdr/SIMA2024010231001.md): Light · inoperative · Dec 31, 2023 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > PORTIONS OF EMERGENCY LIGHTING FLOOR STRIP INOP-C/A-RAR PHOTOLUMINESCENT STRIP AT SEAT 3DF AND 4DF OPS CHECK GOOD
- [SDR SIMA20230428001](https://openairdocs.org/sdr/SIMA20230428001.md): Light · damaged · Apr 28, 2023 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > ALL RH AND LH EMERGENCY PHOTOLUMINESCENT FLOOR PATH STRIPS REQUIRE REPLACEMENT DUE TO FADING STRIPS AND/OR DAMAGED COVER.-C/A-COMPLETE:REPLACED ALL UNSERVICABLE LH EMERGENCY PHOTOLUMINESCENT FLOOR PATH STRIPS IAW AMM 33-50-21. REFERENCE NRWC E975733 FOR INSTAL
- [SDR SIMA20220110003](https://openairdocs.org/sdr/SIMA20220110003.md): None · none · Jan 10, 2022 · N207AN · Emb ERJ170200LR · Flight Compartment Windows
  > O WINDSHIELD CRACKED AS WE CLIMB THROUGH 6000 FEET, RTF, NO OVERWEIGHT LANDING./ DECLARDED EMERGDENCY EQP SWAP FLT CONT. "TRANSFERRED TO NRWC 007-MIA-00911" RS 222659-C/A-REMOVED FO WINDSHEILD IAW AMM 56-11-00 STEPS 2A THRU G (10-C/A-REMOVED AND REPLACED RIGHT
- [SDR SIMA20210828002](https://openairdocs.org/sdr/SIMA20210828002.md): Power Supply · inoperative · Aug 28, 2021 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHTS ON AFT LH PASSENGER DOOR INOP-C/A-RAR EMERGENCY- LIGHT POWER UNIT #3 IAW 33-50-01. OPC GOOD. NO DEFECTS NOTED
- [SDR SIMA20201209001](https://openairdocs.org/sdr/SIMA20201209001.md): Engine · vibration · Dec 9, 2020 · N207AN · Emb ERJ170200LR · Engine (Turbine/Turboprop)
  > ENGINE 2 LP VIBRATION 4.0 IN FLIGHT. C/A: PERFORMED RT ENGINE FAN BLADES AND PINS-N1 VIB TROUBLESHOOTING, IAW WORK CARD EA72-00-00-012. OPERATIONAL CHECK GOOD.
- [SDR SIMA20201206001](https://openairdocs.org/sdr/SIMA20201206001.md): Battery Pack · discharged · Dec 6, 2020 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > AFT EMERGENCY LIGHTS OVERHEAD, LT OVERDOOR, AND LT LOWER INOPERABLE. C/A: ACCOMPLISHED CHARGE OF EMERGENCY LIGHT POWER SUPPLIES AND OPERATIONS CHECK GOOD, IAW AMM 33-50-01.
- [SDR SIMA20200918002](https://openairdocs.org/sdr/SIMA20200918002.md): Door · vibration · Sep 18, 2020 · N207AN · Emb ERJ170200LR · Passenger/Crew Doors
  > FA 1 REPORTED L1 DOOR VIBRATION INFLIGHT, VIBRATION FELT AROUND DOOR AND FLOOR. STATUS PAGE SHOWED DOOR INDICATION GREEN. C/A MAIN DOOR (L1) DEFLECTOR DEFERRED, M PROC, C/W.
- [SDR SIMA202008076001](https://openairdocs.org/sdr/SIMA202008076001.md): Pressure Switch · failed · Aug 6, 2020 · N207AN · Emb ERJ170200LR · Landing Gear Brake System
  > INBOUND FLIGHT DECLARED AN EMERGENCY FOR MECH PARKING BRAKE NOT RELEASE MESSAGE EICAS. CFR FOLLOWED FLT TO GATE, PARKING BRAKE NOT RELEASED EICAS MESSAGE ILLUMINATED. FOLLOWED FIM 32-41-00, R & R EMERGENCY BRAKE PRESSURE SWITCH SYSTEM NR 2 IAW AMM 32-44-09.
- [SDR SIMA202007109002](https://openairdocs.org/sdr/SIMA202007109002.md): Door · lack of lube · Jul 9, 2020 · N207AN · Emb ERJ170200LR · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO OPEN. INSPECTED AND LUBE MAIN DOOR, IAW AMM 52-11-02, OPS. CHECK GOOD.
- [SDR SIMA2020062401003](https://openairdocs.org/sdr/SIMA2020062401003.md): Frame · cracked · Jun 1, 2020 · N207AN · Emb ERJ170200LR · Emergency Lighting
  > FWD SERVICE DOOR LWR FWD EMERGENCY LIGHT FRAME CRACKED. REMOVED AND REPLACED THE FWD SERVICE DOOR LWR FWD EMERGENCY LIGHT FRAME IAW AMM 33-50-15-04.
- [SDR SIMA2020061530001](https://openairdocs.org/sdr/SIMA2020061530001.md): Slide · unknown · Apr 30, 2020 · N207AN · Emb ERJ170200LR · Escape Slide
  > RECORDS REVIEW STATES EMERGENCY EVACUATION SLIDE, FWD FS DOOR P/N 4A4030-7 S/N ED1922 REQUIRES RESTORATION. TRANSFERED TO DWMS NRTC E794894. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE, FWD FS DOOR P/N 4A4030-7 S/N ED1922 IAW WC 25-65-01-001-A. SEE NRTC E7
- [SDR C77A202002170006](https://openairdocs.org/sdr/C77A202002170006.md): Skin · gouged · Feb 18, 2020 · N207AN · Emb ERJ170200LR · Wing, Plate/Skin
  > DURING BASIC CHECK AT EAMS, GOUGE DAMAGE WAS DISCOVERED ON THE LH WING FIXED LEADING EDGE SKIN (P/N 170-31031-021) OF AIRCRAFT 207AN BETWEEN RIB 1 AND RIB 4. REFERENCE ETD2020-170-004771-A FIGURES 1 AND 2 FOR THE DAMAGE LOCATION AND DIMENSIONS. THE DAMAGE E
- [SDR C77A202002170005](https://openairdocs.org/sdr/C77A202002170005.md): Skin · dented · Feb 17, 2020 · N207AN · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING BASIC CHECK AT EAMS, DENT DAMAGE WAS DISCOVERED ON THE P/N 170-61701-013 REAR FUSELAGE LOWER SKIN AT THREE LOCATIONS IN TWO BAYS BETWEEN FR94/FR95 AND S-21L/S-23L. REFERENCE ETD2020-170-005177-A FIGURE 1 FOR DAMAGE DETAILS. THE DAMAGE IS NOT ALLOWABLE P
- [SDR C77A202002170004](https://openairdocs.org/sdr/C77A202002170004.md): Skin · gouged · Feb 17, 2020 · N207AN · Emb ERJ170200LR · Wing, Plate/Skin
  > DURING BASIC CHECK AT EAMS, GOUGE DAMAGE WAS DISCOVERED ON THE RH WING FIXED LEADING EDGE SKIN (P/N 170-31031-022) OF AIRCRAFT 207AN BETWEEN RIB 1 AND RIB 2. REFERENCE ETD2020-170-004755 FIGURES 1 AND 2 FOR THE DAMAGE LOCATION AND DIMENSIONS. THE DAMAGE EXCEED
- [SDR C77A202002170003](https://openairdocs.org/sdr/C77A202002170003.md): Firewall · cracked · Feb 17, 2020 · N207AN · Emb ERJ170200LR · APU Cowling/Containment
  > DURING THE B1 BASIC CHECK IN BNA, CRACK DAMAGE WAS FOUND IN TWO LOCATIONS AT THE UPPER AND LOWER CORNERS OF THE RH APU FIREWALL REMOVABLE PANEL 351BZ (P/N 170-50263-401) ON AIRCRAFT N207AN. THE DAMAGE WAS REPAIRED PER SRM PART II 53-31-21/REPAIR 02 USING THE T
- [SDR C77A202002170002](https://openairdocs.org/sdr/C77A202002170002.md): Fitting · chafed · Feb 17, 2020 · N207AN · Emb ERJ170200LR · Engine Thrust Reverser
  > GE LMM 78-30-00, REPAIR 017 GIVES INSTRUCTIONS TO ACCOMPLISH A REPAIR OF THE UPPER RIGHT ACTUATOR FITTING LOCATED ON THE FRONT FRAME OF THE RIGHT-HAND THRUST REVERSER HALF. THIS EO PROVIDES INSTRUCTIONS TO ACCOMPLISH SUBTASK 78-30-00-350-029, WHICH INSTALLS A
- [SDR C77A202002170001](https://openairdocs.org/sdr/C77A202002170001.md): Skin · cracked · Feb 17, 2020 · N207AN · Emb ERJ170200LR · Wing, Plate/Skin
  > THIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART II, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT RH WING TIP SPAR 1 (P/N 171-16231-002 OR 171-16231-004) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-171-22480-40
- [SDR C77A2020021530035](https://openairdocs.org/sdr/C77A2020021530035.md): Seat Track · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE RH INBOARD SEAT TRACK AFT OF FR17 (P/N 170-03263-001). REFERENCE ETD2020-170-003756, FIGURE 1 FOR DETAILS, FOR THE DAMAGE LOCATION AND DIMENSION. EAMS REQUESTED & RECEIVED PERMANENT
- [SDR C77A2020021630034](https://openairdocs.org/sdr/C77A2020021630034.md): Door Sill · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020021630033](https://openairdocs.org/sdr/C77A2020021630033.md): Seat Track · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE FORWARD FUSELAGE RH IB SEAT TRACK (P/N 170-03263-001) BETWEEN FR13 AND FR14 IN THE FORWARD CABIN FLOOR STRUCTURE.
- [SDR C77A2020021530032](https://openairdocs.org/sdr/C77A2020021530032.md): Splice · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020021530031](https://openairdocs.org/sdr/C77A2020021530031.md): Gusset · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020021530030](https://openairdocs.org/sdr/C77A2020021530030.md): Gusset · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020021530029](https://openairdocs.org/sdr/C77A2020021530029.md): Floor Support · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A202002153028](https://openairdocs.org/sdr/C77A202002153028.md): Shear Panel · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020021503027](https://openairdocs.org/sdr/C77A2020021503027.md): Shear Panel · corroded · Feb 15, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830026](https://openairdocs.org/sdr/C77A2020020830026.md): Splice · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830025](https://openairdocs.org/sdr/C77A2020020830025.md): Gusset · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830024](https://openairdocs.org/sdr/C77A2020020830024.md): Gusset · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830023](https://openairdocs.org/sdr/C77A2020020830023.md): Floor Support · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830022](https://openairdocs.org/sdr/C77A2020020830022.md): Shear Panel · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020300021](https://openairdocs.org/sdr/C77A2020020300021.md): Shear Panel · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830020](https://openairdocs.org/sdr/C77A2020020830020.md): Floor Support · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170
- [SDR C77A2020020830019](https://openairdocs.org/sdr/C77A2020020830019.md): Seat Track · corroded · Feb 8, 2020 · N207AN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE RH INBOARD SEAT TRACK AFT OF FR17 (P/N 170-03263-001). REFERENCE ETD2020-170-003756, FIGURE 1 FOR DETAILS, FOR THE DAMAGE LOCATION AND DIMENSION. EAMS REQUESTED & RECEIVED PERMANENT
- [SDR C77A2020020700041](https://openairdocs.org/sdr/C77A2020020700041.md): Seat Track · corroded · Feb 7, 2020 · N207AN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE FORWARD FUSELAGE RH IB SEAT TRACK (P/N 170-03263-001) BETWEEN FR13 AND FR14 IN THE FORWARD CABIN FLOOR STRUCTURE.
- [SDR C77A2019071000001](https://openairdocs.org/sdr/C77A2019071000001.md): Strut · lack of lube · Jul 9, 2019 · N207AN · Emb ERJ170200LR · Nose/Tail Landing Gear Strut/Axle
  > LG WOW SYS FAIL. PERFORMED NLG SHOCK STRUT SERVICING IAW AMM 12-12-09. DURING RELEASE OF NITROGEN AND HYDRAULIC FLUID, FOUND NO FLUID IN NLG SHOCK STRUT. WO REMAINS OPEN. GEAR SWING REQUIRED. PERFORMED FUNCTIONAL TEST OF THE LG EXTENSION AND RETRACTION SYSTEM
- [SDR C77A20170124002](https://openairdocs.org/sdr/C77A20170124002.md): Unknown · smoke · Jan 22, 2017 · N207AN · Emb ERJ170200LR · Air Distribution System
  > FLIGHT RETURNED TO DEPARTURE DUE TO REPORTED SMOKE AND BURNING ODOR IN THE CABIN AFTER TAKE OFF BELOW 1000 FEET.. REPORTS INDICATE THAT THE SUSPECTED SMOKE DISSIPATED AND HAS NOT CAUSED ANY ISSUES. AN EMERGENCY WAS DECLARED. LANDED SAFELY WITHOUT INCIDENT. P

## 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 = 'N207AN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N207AN/reports

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