# Service difficulty reports: N683AE

A list on [N683AE](https://openairdocs.org/aircraft/N683AE.md).

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

Page 1 of 4 · 166 reports

- [SDR HNAA2026041200283](https://openairdocs.org/sdr/HNAA2026041200283.md): Switch · failed · Apr 12, 2026 · N683AE · Emb EMB145LR · Elevator Control System
  > MAIN PITCH TRIM INOP MESSAGE DURING CLIMB USING CAPT YOKE SWITCH. R&R PITCH TRIM SWITCH IAW EMBR AMM 27-40-03. PERFORMED HORIZONTAL STAB ADJUSTMENT TEST EMBR 145 AMM 27-40-00 TROUBLESHOOTED USING EMBR 145 FIM 27-43-00-810-801-A. NO DEFECTS NOTED, A/C GOOD FO
- [SDR HNAA2026032700249](https://openairdocs.org/sdr/HNAA2026032700249.md): Switch · intermittent · Mar 26, 2026 · N683AE · Emb EMB145LR · Stabilizer Position Indicating
  > DURING CLIMB PITCH TRIM MAIN AND BACKUP FAILED ON BOTH SIDES WITH NO EICAS MESSAGES, NO CMC MESSAGES. WAS STUCK UP 2 DEGREES. NO CMC MESSAGES. FACT 26MAR26 08:00 PIT FOLLOWED FIM 27-43-00-810-820-A BLOCKS 1, 2, 3, 8. PERFORMED OPS CHECK IAW AMM 27-40-0
- [SDR HNAA2025100300661](https://openairdocs.org/sdr/HNAA2025100300661.md): Floor Support · corroded · Sep 26, 2025 · N683AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > F068535 CORROSION ON LH OTBD #2 FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON LH OTBD #2 FLOOR SILL IAW EMB145 SRM 51-40-02.
- [SDR HNAA2025100300670](https://openairdocs.org/sdr/HNAA2025100300670.md): Skin · buckled · Sep 9, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > F069494 RH WHEEL WELL INTERNAL SKIN IS BUCKLED AT FR3. REPAIRED BUCKLED RH WHEEL WELL INTERNAL SKIN AT FR 3 IAW PIEDMONT EO1-53-25-0329 AND ETD2025-145-928107.
- [SDR HNAA2025100300669](https://openairdocs.org/sdr/HNAA2025100300669.md): Crossbeam · damaged · Sep 5, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Structure
  > CROSSMEMBER AT FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED CROSSMEMBER AT FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0326 AND ETD2025-145-927858.
- [SDR HNAA2025100300668](https://openairdocs.org/sdr/HNAA2025100300668.md): Frame · damaged · Sep 5, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0330 AND ETD2025-145-927849.
- [SDR HNAA2025100300675](https://openairdocs.org/sdr/HNAA2025100300675.md): Shear Tie · damaged · Sep 4, 2025 · N683AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > FRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300667](https://openairdocs.org/sdr/HNAA2025100300667.md): Frame · damaged · Sep 4, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW PIEDMONT EO1-53-25-0327 AND ETD2025-145-927854.
- [SDR HNAA202510030075](https://openairdocs.org/sdr/HNAA202510030075.md): Frame · damaged · Sep 4, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300674](https://openairdocs.org/sdr/HNAA2025100300674.md): Stringer · damaged · Sep 4, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 14R HAS AN OVERSIZED HOLE AT FR2. RAR STRINGER 14R BTW FR 1A-6 IAW EMB 145 SRM 51-40-02. DURING REPLACEMENT FOUND 13 HOLES BETWEEN FR 2-3 TO ONLY HAVE 1.5D EDGE DISTANCE. 13 HOLES ARE ACCEPTED AS A PERMANENT REPAIR IAW ETD2025-145-928801 AND EO1-53-2
- [SDR HNAA2025100300676](https://openairdocs.org/sdr/HNAA2025100300676.md): Frame · damaged · Sep 4, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW EO1-53-25-0327 AND ETD2025-145--927854.
- [SDR HNAA2025100300664](https://openairdocs.org/sdr/HNAA2025100300664.md): Floor Support · corroded · Aug 27, 2025 · N683AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > F068625 GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND STGR-16 HAS CORROSION. RAR GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND R/H STGR 16 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300673](https://openairdocs.org/sdr/HNAA2025100300673.md): Shear Tie · cracked · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > F068552 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 16R-17R IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300672](https://openairdocs.org/sdr/HNAA2025100300672.md): Skin · damaged · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > F068464 FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT REQUIRES REPLACEMENT DUE TO MULTIPLE TOOL MARKS. REMOVED MULTIPLE TOOLING MARKED FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT, PREPPED AND INSTALLED SERVICEABLE SKIN
- [SDR HNAA2025100300666](https://openairdocs.org/sdr/HNAA2025100300666.md): Floor Support · corroded · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > F068510 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-35/38 HAVE CORROSION. REMOVED AND REPLACED CABIN L/H OMEGA BEAM GUSSET #4 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300665](https://openairdocs.org/sdr/HNAA2025100300665.md): Floorbeam · corroded · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > F068508 CORROSION ON LH #3 FLOOR BEAM GUSSET. REMOVED AND REPLACED LH #3 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300663](https://openairdocs.org/sdr/HNAA2025100300663.md): Floorbeam · corroded · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > F068549 CORROSION ON RH CROSS FLOORBOARD SUPPORT AT FRAME 28. R & R RH CROSS FLOORBOARD SUPPORT AT FRAME 28 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300662](https://openairdocs.org/sdr/HNAA2025100300662.md): Floor Support · corroded · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > F068545 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-51/53 HAVE CORROSION. REMOVED AND REPLACED L/H OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300660](https://openairdocs.org/sdr/HNAA2025100300660.md): Floor Support · cracked · Aug 26, 2025 · N683AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > F068523 CABIN CENTER OMEGA BEAM GUSSET BETWEEN FR-39/42 HAVE CORROSION. REMOVED AND REPLACED CABIN CENTER OMEGA BEAM GUSSET BTW FR 39-42 (NO.4) IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300671](https://openairdocs.org/sdr/HNAA2025100300671.md): Skin · cracked · Aug 20, 2025 · N683AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > F066756 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR 6R / 7R. ACCOMPLISHED BUSHING REPAIR ON REAR FUSELAGE EXTERNAL SKIN AT FR 77 BETWEEN STGR 6R /7R IAW EO1-53-25-0351 AND EMB-145 SRM 53-32-01 RE, ITEM 9, FIGURE 213, SHEETS 1-3.
- [SDR HNAA2023120400454](https://openairdocs.org/sdr/HNAA2023120400454.md): Unknown · unknown · Dec 3, 2023 · N683AE · Emb EMB145LR · Autopilot System
  > AUTO FAIL WITH AUTO TRIM FAIL. OPS CHECK AUTOPILOT AND AUTO PILOT TRIM IAW 22-11-00. OPS CHECK GOOD CLEAR MEL 22-1-1.
- [SDR HNAA2023051600160](https://openairdocs.org/sdr/HNAA2023051600160.md): Unknown · unknown · May 15, 2023 · N683AE · Emb EMB145LR · Cabin Cooling System
  > PACK 2 OVERHEAT DISPLAYED ON EICAS DURING TAKE OFF, AIR COND PACK N650 AND ABOVE AMENDED. R & R PACK 2 OVERTEMP SWITCH, TEMP SENSOR, AND CONDENSOR MIXER. RAN ENGINES AT POWER WITH BLEEDS AND PACKS ON. NO PACK 2 OVHT MESSAGE DISPLAYED AT THIS TIME. R/R #2 PA
- [SDR HNAA2023031100079](https://openairdocs.org/sdr/HNAA2023031100079.md): Unknown · unknown · Mar 5, 2023 · N683AE · Emb EMB145LR · Vertical Stabilizer
  > VERTICAL STABILIZER LH AND RH SPHERICAL BEARING HOUSINGS ARE OUT OF DIMENSIONAL TOLERANCE. REPAIRED IAW EO1-55-23-0044
- [SDR HNAA2023031000074](https://openairdocs.org/sdr/HNAA2023031000074.md): Unknown · unknown · Feb 27, 2023 · N683AE · Emb EMB145LR · Fuselage Main, Structure
  > COCKPIT LH LATERAL BRACKET, LH OF OVERHEAD PANEL, BETWEEN FR 12 AND 13 CRACKED. REPAIRED IAW 145 SRM51-40-02
- [SDR HNAA2023031000075](https://openairdocs.org/sdr/HNAA2023031000075.md): None · none · Feb 26, 2023 · N683AE · Emb EMB145LR · Fuselage Main, Structure
  > PILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. REPAIRED IAW EO1-53-23-0046
- [SDR HNAA2023031100082](https://openairdocs.org/sdr/HNAA2023031100082.md): Unknown · unknown · Feb 23, 2023 · N683AE · Emb EMB145LR · Wing Structure
  > LH WING TIP UPPER ATTACHMENT FLANGE IS SCRATCHED. REPAIRED IAW EMB145 SRM 51-10-03 AND 57-20-07AD
- [SDR HNAA2023031100080](https://openairdocs.org/sdr/HNAA2023031100080.md): Unknown · unknown · Feb 23, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > FRAME 65 IS CHAFED BETWEEN STRINGERS 2L-3L. REPAIRED IAW ETD 2023-145-004197
- [SDR HNAA2023031000076](https://openairdocs.org/sdr/HNAA2023031000076.md): Unknown · unknown · Feb 23, 2023 · N683AE · Emb EMB145LR · Fuselage Main, Structure
  > RH FWD VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK AT MARKED LOCATIONS. REPAIRED IAW EMB145 SRM 51-40-02
- [SDR HNAA2023031000073](https://openairdocs.org/sdr/HNAA2023031000073.md): Unknown · unknown · Feb 23, 2023 · N683AE · Emb EMB145LR · Passenger/Crew Doors
  > AFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042
- [SDR HNAA2023031000072](https://openairdocs.org/sdr/HNAA2023031000072.md): Unknown · unknown · Feb 23, 2023 · N683AE · Emb EMB145LR · Fuselage Main, Structure
  > AFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042
- [SDR HNAA2023030800064](https://openairdocs.org/sdr/HNAA2023030800064.md): Unknown · unknown · Feb 22, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSION ON CARGO DOOR SILL. REPAIRED IAW SRM 51-40-02, 51-20-03, AND 51-40-06
- [SDR HNAA2023030800086](https://openairdocs.org/sdr/HNAA2023030800086.md): Unknown · unknown · Feb 19, 2023 · N683AE · Emb EMB145LR · Aircraft Structures
  > LEVEL 2 CORROSION IN LAV FLOOR GUSSET BETWEEN FRAMES 59-61. REPAIRED IAW EMB145 SRM 51-10-03, 51-40-02, 51-20-03, AND 53-24-10AD
- [SDR HNAA2023031100077](https://openairdocs.org/sdr/HNAA2023031100077.md): Unknown · unknown · Feb 19, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSION IN GALLEY FLOOR LH CROSSBEAM AT FRAME 18. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-01, AND 51-21-06.
- [SDR HNAA2023030800068](https://openairdocs.org/sdr/HNAA2023030800068.md): Unknown · unknown · Feb 19, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSION ON CROSS BEAM BRACKET BETWEEN LH FLOOR GUSSET AND LH FLOOR SIL IN LAV AREA BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03 AND 51-40-02.
- [SDR HNAA2023030800067](https://openairdocs.org/sdr/HNAA2023030800067.md): Unknown · unknown · Feb 19, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSION ON SPLICE BRACKET ON LH FLOOR SILL IN LAV BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03, AND 51-40-02.
- [SDR HNAA2023030800066](https://openairdocs.org/sdr/HNAA2023030800066.md): None · none · Feb 19, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSOIN IN LAV FLOOR GUSSET BETWEEN FRAMES59-61. REPAIRED IAW EMB145 SRM 51-10-03, 53-24-10AD, 51-40-02, AND 51-20-03.
- [SDR HNAA2023030800065](https://openairdocs.org/sdr/HNAA2023030800065.md): Unknown · unknown · Feb 16, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSION ON LH #3 FLOOR SILL. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-03, AND 51-40-09
- [SDR HNAA2023030800062](https://openairdocs.org/sdr/HNAA2023030800062.md): Unknown · unknown · Feb 12, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSOIN ON INTERNAL FUSELAGE REINFORCEMENT SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068 FIG 7 DETAIL A2
- [SDR HNAA2023030800063](https://openairdocs.org/sdr/HNAA2023030800063.md): Unknown · unknown · Feb 11, 2023 · N683AE · Emb EMB145LR · Standard Practices/Structures
  > LEVEL 2 CORROSION ON INTERNAL FUSELAGE SKIN PLATE BETWEEN FRAMES 62-63 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068
- [SDR HNAA2023010500018](https://openairdocs.org/sdr/HNAA2023010500018.md): Clamp · loose · Jan 4, 2023 · N683AE · Emb EMB145LR · Air Distribution System
  > ON DESENT, ACFT THROUGH RAIN & TURBULENCE. A SUDDEN ELECTRICAL ODOR IN FLT DECK & GALLEY FOR APPROX 5 MINS. ODOR DISSIPATED ON ITS OWN WITHOUT CREW INPUT. AT GATE UNDER APU POWER NO ODOR NOTED. PERFORMED GVI UNDER INSTRUMENT PANEL IN COCKPIT, INSP CIRCUI
- [SDR HNAA2022111400302](https://openairdocs.org/sdr/HNAA2022111400302.md): Localizer · faulted · Nov 12, 2022 · N683AE · Emb EMB145LR · Localizer/VOR System
  > BOTH LOCALIZER SIGNALS UNRELIABLE ON APPROACH TO FWA. DIVERTED TO DAY. PERFORMED VOR/ILS SYSTEM OPERATIONAL TEST IAW AMM 34-32-00-700-801-A. VOR/ILS SYSTEMS #1 AND #2 OPERATIONAL TESTS PASSED. AIRCRAFT OK FOR SERVICE
- [SDR HNAA2022062300226](https://openairdocs.org/sdr/HNAA2022062300226.md): None · none · Jun 22, 2022 · N683AE · Emb EMB145LR · Fuel Indicating System
  > PDIS 683 28-41 2646932 22JUN22 CLT CLOSE AFTER TAKE OFF #1 FUEL QTY READ 0 AND TOTAL FUEL QTY READ 0 FACT 22JUN22 18:39 CLT UPON ARRIVAL TO A/C FOUND FUEL QTY TO BE OPERATING NORMALLY. AS POSITIVE MX R&R FUEL CONDITIONING UNIT
- [SDR HNAA2021102600523](https://openairdocs.org/sdr/HNAA2021102600523.md): Control Unit · faulted · Oct 23, 2021 · N683AE · Emb EMB145LR · Trailing Edge Flap Control System
  > FLAP FAILURE ON APPROACH, FLAP FAIL STUCK ON 14 DEGREES. R+R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02-000/400-801-A. OPS CHECK GOOD OK FOR SERVICE.
- [SDR HNAA2021052500224](https://openairdocs.org/sdr/HNAA2021052500224.md): Indicator · faulted · May 21, 2021 · N683AE · Emb EMB145LR · Fuel Quantity Indicator
  > PDIS 683 28-41 2407312 21MAY21 GSP CLOSE ON DECENT FUEL 1 QTY DISPLAYED 0LBS. 10 MINUTES LATER FUEL QTY 2 DISPLAYED 0LBS. BOTH INDICATIONS CAME BACK AFTER 1 MINUTE. FACT 21MAY21 23:09 GSP PERF ELEC FUEL QTY IND OPS CHECK IN REF
- [SDR HNAA2021030800094](https://openairdocs.org/sdr/HNAA2021030800094.md): Unknown · odor · Mar 7, 2021 · N683AE · Emb EMB145LR · Cabin Cooling System
  > PDIS 683 21-01 2532571 08MAR21 FLO ASSGN PACK 2 OVERHEAT WITH BURNING SMELL IN COCKPIT AND TR OUBLE COOLING A/C. BURNING SMELL ALSO NOTICED WITH O NLY PACK 1 RUNNING (NOTE: CREW STATED IT TAKES RUN NING 3 MINS BEFORE SME
- [SDR HNAA2021021100048](https://openairdocs.org/sdr/HNAA2021021100048.md): Unknown · odor · Feb 10, 2021 · N683AE · Emb EMB145LR · Air Distribution System
  > PDIS 683 21-01 2343301 10FEB21 SDF CLOSE ON TAKEOFF AT APPROX 115KTS BURNING SMELL NOTICED IN FLIGHT DECK, FOLLOWED BY ICE COND A/ICE INOP MSG ON EICAS. FACT 10FEB21 20:17 SDF RAN AIRCRAFT WITH CREW, NO DEFECTS OR BURNING SMELL
- [SDR HNAA2021010500004](https://openairdocs.org/sdr/HNAA2021010500004.md): Switch · malfunctioned · Dec 31, 2020 · N683AE · Emb EMB145LR · Air Conditioning System
  > AFTER T/O SMOKE SMELL IN COCKPIT. SHORTLY AFTER PACK 1 OVERHEAT MESSAGE ON EICAS. PACK 1 SHUTDOWN AUTOMATICALLY AND SMELL DISAPPATED W/I 3-4 SECONDS. CW FIM TASK 21 51 00 810 803 A BLOCKS 1 AND 2. RAN WITH APU AND ENGINE NO EICAS MESSAGE/TRANSITORY COND.
- [SDR HNAA2020120700336](https://openairdocs.org/sdr/HNAA2020120700336.md): Pressure Switch · malfunctioned · Dec 5, 2020 · N683AE · Emb EMB145LR · Rudder Control System
  > PDIS 683 27-21 2302681 05DEC20 ALB CLOSE. ON CLIMB OUT RUD 1-2 FAIL EICAS MESSAGE PRESENTED. PERFORMED QRH RUD SYSTEM 1 CAME BACK ONLINE. FACT 05DEC20 12:34 ALB. FOLLOWED EMB 145 FIM 27-22-00-810-804 A TO BLOCK 19 FOUND TO BE TRANSITORY CONDITION OF THE RU
- [SDR HNAA2020051800149](https://openairdocs.org/sdr/HNAA2020051800149.md): Sensor · failed · May 9, 2020 · N683AE · Emb EMB145LR · Trailing Flap Position Indicating System
  > FLAP FAIL EICAS MESSAGE ON ARRIVAL TO HTS WHEN FLAPS SELECTED TO 9 DEGREES WITH NO FLAP MOVEMENT. R&R'D L/H FLAP VELOCITY SENSOR IAW AMM 27-51-12. RAN FLAPS UP AND DOWN A COUPLE TIMES OPS CHECK GOOD AT THIS TIME.
- [SDR HNAA2020050500148](https://openairdocs.org/sdr/HNAA2020050500148.md): Warning System · false activation · May 4, 2020 · N683AE · Emb EMB145LR · Trailing Flap Position Indicating System
  > FLAP FAIL ON EICAS WHEN FLAPS SELECTED DOWN. TROUBLESHOT IAW FIM TASK 27-51-00-810-816-A, STEPS 1,2,3, OPS CHECK IAW 27-51-00-700-801-A. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N683AE/reports.md?page=2

## 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 = 'N683AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N683AE/reports

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