# Service difficulty reports: N689EC

A list on [N689EC](https://openairdocs.org/aircraft/N689EC.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 · 171 reports

- [SDR HNAA2026071300594](https://openairdocs.org/sdr/HNAA2026071300594.md): Hydraulic System · low · Jul 11, 2026 · N689EC · Emb EMB145LR · Hydraulic System, Main
  > HYD 1 LOW DISPLAYED IN FLIGHT. SERVICED NR 1 HYD SYSTEM IAW AMM 12-13-01. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE
- [SDR HNAA2026052600434](https://openairdocs.org/sdr/HNAA2026052600434.md): Bleed Valve · failed · May 23, 2026 · N689EC · Emb EMB145LR · Compressor Bleed Valve
  > E1 HSV FAIL ON EICAS FACT 23MAY26 17:19 GSO. R & R NR 1 HSV IAW AMM 36-11-02. OPS AND LEAK CHECK GOOD.
- [SDR HNAA2026050400366](https://openairdocs.org/sdr/HNAA2026050400366.md): Windshield · no discrepancy · May 2, 2026 · N689EC · Emb EMB145LR · Flight Compartment Windows
  > BIRD STRIKE DURING TAKEOFF. PERFORMED BIRDSTRIKE INSPECTION IAW 05-50-08. CLEANED BIRD REMAINS OFF WINDSHIELD. NO DAMAGE/DEFECTS NOTED. AIRCRAFT OK FOR SERVICE AT THIS TIME
- [SDR HNAA2026020100107](https://openairdocs.org/sdr/HNAA2026020100107.md): Adc · failed · Feb 1, 2026 · N689EC · Emb EMB145LR · Air Data Computer
  > ADC 1 FAILED IN FLIGHT FACT 01FEB26 17:47 ALB R&R'D ADC1 AT POS 100 IAW EMB145 AMM 34-15-01. PERFORMED LEAK CHECK IAW AMM 34-13-00. OPS CHECK DONE IAW AMM 34-15-00, SYSTEM TESTED SERVICEABLE, OK FOR SERVICE.
- [SDR HNAA2025090100583](https://openairdocs.org/sdr/HNAA2025090100583.md): Acm · smoke · Aug 30, 2025 · N689EC · Emb EMB145LR · Cabin Cooling System
  > SMOKE IN CABIN DURING CRUISE AT FL250. INSPECTED PACK SYSTEM, FOUND #200 ACM SIEZED W/ MELTED DUCTS ON #200 DUAL TEMP CONTROL VALVE. R/R'D DUCTS ON #200 DUAL TEMP CONTROL VALVE IRW AMM 21-60-01. R/R'D #200 ACM IRT AMM 21-61-03. OPS AND LEAK CHECK GOOD WITH NO
- [SDR HNAA2025081200567](https://openairdocs.org/sdr/HNAA2025081200567.md): Fan · clogged · Aug 12, 2025 · N689EC · Emb EMB145LR · Air Distribution Fan
  > FA REPORTS RUBBER HOSE SMELL WITH HISSING NOISE IN A ISLE GASPER AREA BETWEEN ROWS 2 AND 8 WITH GASPER FAN RUNNING. FOUND SEAT 8B GASPER TO BE CLOGGED. R/R'D PSU GASPER AIR ASSY IAW MM 25-22-05, OPS CK GOOD.
- [SDR HNAA2025040800197](https://openairdocs.org/sdr/HNAA2025040800197.md): Engine · bird ingestion · Apr 9, 2025 · N689EC · Emb EMB145LR · Engine (Turbine/Turboprop)
  > BIRD STRIKE ON #2 ENGINE. #2 ENG CHANGE. SEE W/C 71-00-00 ON WORK PACKAGE.
- [SDR HNAA2025030300117](https://openairdocs.org/sdr/HNAA2025030300117.md): Bleed Valve · abnormal · Mar 2, 2025 · N689EC · Emb EMB145LR · Compressor Bleed Valve
  > REJECTED T/O WITH HSV 2 FAIL DISPLAYED MSG WENT AWAY AFTER THRUST LEVERS PULLED BACK (DEACTIVATED BLEED VLV 2). R&R'D #200 HSV IAW 36-11-02-04 OPS CHECK GOOD NO RELATED EICAS MSGS OR OTHER DEFECTS NOTED AT THIS TIME
- [SDR HNAA2024103001043](https://openairdocs.org/sdr/HNAA2024103001043.md): Floor Support · corroded · Sep 30, 2024 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E058889 CARGO DOOR LOWER CUTOUT FLOOR SILL CORRODED. RAR CARGO DOOR LOWER CUTOUT FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024103001048](https://openairdocs.org/sdr/HNAA2024103001048.md): Floor Support · corroded · Sep 28, 2024 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E058583 PAX DOOR LWR FWD FLOOR SUPPORT HAS CORROSION AROUND NUT-PLATES HOLES. RAR PAX DOOR LWR FWD FLOOR SUPPORT IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024103001047](https://openairdocs.org/sdr/HNAA2024103001047.md): Floorbeam · corroded · Sep 28, 2024 · N689EC · Emb EMB145LR · Fuselage Main, Floor Beam
  > E058611 GALLEY FLOOR CROSSBEAM AT FR-20 BETWEEN STGRS 21L/18L HAS CORROSION. BLENDED OUT CORROSION ON GALLEY FLOOR CROSSBEAM AT FR-20 BETWEEN STGRS 21L/18L IAW EMB145 SRM 51-10-03 AND FOUND REMAINIG THICKNESS TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-21
- [SDR HNAA2024103001046](https://openairdocs.org/sdr/HNAA2024103001046.md): Floor Support · corroded · Sep 28, 2024 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E058596 PAX DOOR LWR AFT FLOOR SUPPORT HAS CORROSION AROUND NUT-PLATES HOLES. RAR PAX DOOR LWR AFT FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024103001042](https://openairdocs.org/sdr/HNAA2024103001042.md): Door Sill · corroded · Sep 28, 2024 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E058598 SERVICE DOOR LWR CENTER SILL HAS CORROSION AROUND NUT-PLATES HOLES. PREPPED, FABRICATED, AND INSTALLED DOUBLERS ON SERVICE DOOR CENTER SILL IAW EMB 145 SRM 53-21-02RE FIGURE 201 AND EO1-53-24-0604
- [SDR HNAA2024103001045](https://openairdocs.org/sdr/HNAA2024103001045.md): Attach Fitting · gouged · Sep 27, 2024 · N689EC · Emb EMB145LR · Ailerons
  > E058125 RH AILERON DAMPENER ATTACHMENT FITTING IS GOUGED IN MULTIPLE AREAS (ON AILERON). REMOVED AND REPLACED RH AILERON DAMPENER FITTING IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024103001041](https://openairdocs.org/sdr/HNAA2024103001041.md): Housing · corroded · Sep 27, 2024 · N689EC · Emb EMB145LR · Horizontal Stabilizer Structure
  > E058328 RH HORIZONTAL STAB SPHERICAL BEARING HOUSING PITTED. RPAIRED IAW SRM 55-30-02
- [SDR HNAA2024103001040](https://openairdocs.org/sdr/HNAA2024103001040.md): Profile · corroded · Sep 27, 2024 · N689EC · Emb EMB145LR · Passenger/Crew Doors
  > E058190 PAX DOOR LWR AFT PROFILES HAS CORROSION AROUND NUTPLATES HOLES. REPAIRED IAW EMB 145 SRM 52-10-04 STEP 3 FIGURE 201 SHEET 3 AND PIEDMONT EO1-52-24-0623.
- [SDR HNAA2024103001044](https://openairdocs.org/sdr/HNAA2024103001044.md): Torque Box · damaged · Sep 23, 2024 · N689EC · Emb EMB145LR · Wing Main, Frame Structure
  > E056822 RH WING TORQUE BOX 1 LOWER FWD CENTER FASTENER HOLE IS OVERSIZED AND DAMAGED. PREPPED, FABRICATED, AND INSTALLED BUSHINGS AND HILOCK IN RH WING TORQUE BOX 1 LOWER FWD HOLE IAW ETS2024-145-025752 "REV A" AND EO1-57-24-0603
- [SDR SIMA20220103001](https://openairdocs.org/sdr/SIMA20220103001.md): None · none · Jan 3, 2022 · N689EC · Emb EMB145LR · Emergency Lighting
  > INCORRECT FLIGHT ATTENDANT FLASHLIGHT INSTALLED-C/A-RAR FA FLASHLIGHT WITH CORRECT LED FLASHLIGHT ASSY IAW EMB-145 AMM 33-50-16 AND ETN-EM-33-059. OPC GOOD.
- [SDR SIMA20211217001](https://openairdocs.org/sdr/SIMA20211217001.md): None · none · Dec 17, 2021 · N689EC · Emb EMB145LR · Engine (Turbine/Turboprop)
  > E2 SHUTOFF AT FL240/ SPD 290KTS/ OIL QUANTITY WENT TO RED AT 3 QTS. FLT DECLRD EMERG. LANDED SAFELY-C/A-REMOVED AND REPLACED #2 ENGINE IAW ENGINE REMOVAL AND INSTALLATION EMB 145 WORK CARD 71-000-00 OPERATION AND LEAK CHECK ARE GOOD.
- [SDR SIMA20211212001](https://openairdocs.org/sdr/SIMA20211212001.md): None · none · Dec 12, 2021 · N689EC · Emb EMB145LR · Emergency Lighting
  > FWD FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY BROKEN-C/A-FLIGHT CREW PLACARDED FWD FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY M PROCEDURES C/W REF: MEL 25-32 AUTH: 120159M-C MOC: 056020
- [SDR SIMA20210920003](https://openairdocs.org/sdr/SIMA20210920003.md): None · none · Sep 20, 2021 · N689EC · Emb EMB145LR · Speed-Attitude Correction System
  > CA DECLARED EMERGENCY DUE TO UNRELIABLE AIRSPEED. AMBER IAS ON AIRSPEED INDICATOR FOLLOWED BY SPS ADVANCED EICAS MSG. QRH PROCEDURE C/W. AIRSPEED RETURNED TO NORMAL AND MSG CLEARED IN DESCENT.CAPT DECLARED EMERGENCY DUE TO UNRELIABLE AIRSPEED. -C/A-INTERROGAT
- [SDR SIMA20210614001](https://openairdocs.org/sdr/SIMA20210614001.md): Light · inoperative · Jun 14, 2021 · N689EC · Emb EMB145LR · Emergency Lighting
  > FLOOR EMERGENCY LIGHTS, 2 AND 3 INOP. R & R 2 AND 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIPS IAW EMB145 AMM 33-50-12. OPS CHECK GOOD
- [SDR SIMA20210516003](https://openairdocs.org/sdr/SIMA20210516003.md): Inverter · inoperative · May 16, 2021 · N689EC · Emb EMB145LR · Emergency Lighting
  > ROW 12 OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR #6 EMERGENCY DC/AC INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD
- [SDR SIMA20210301002](https://openairdocs.org/sdr/SIMA20210301002.md): Wire · damaged · Mar 1, 2021 · N689EC · Emb EMB145LR · Light System Wiring
  > SEVENTH EMERGENCY LIGHT STRIP ON LH SIDE FLOOR WIRES DAMAGED, LIGHT INOP-C/A-RAR FLOOR STRIP EMERGENCY LIGHT IAW EMB145 AMM 33-50-12. OPS CHECK GOOD.
- [SDR SIMA202009098005](https://openairdocs.org/sdr/SIMA202009098005.md): Warning Message · illuminated · Sep 8, 2020 · N689EC · Emb EMB145LR · Elevator Control System
  > SPS 2 INOP WARNING AND SPS ADVANCED CAUTION ON EICAS DURING APPROACH TO LANDING. C/A PERFORMED FIM TASKS 27-36-00. SPS ADVANCED MESSAGE REMAINS, SEE AML 4558647 ITEM 2 FOR CONTINUED DISCREPANCY.
- [SDR SIMA202009065002](https://openairdocs.org/sdr/SIMA202009065002.md): Clamp · loose · Sep 5, 2020 · N689EC · Emb EMB145LR · Pneumatic Distribution System
  > BLEED 1 LEAK IN FLIGHT (DIVERTED BACK TO DFW) NO EMERGENCY DECLARED. -C/A-OPENED PACK 1 TO VERIFY BLEED LEAK TIGHTENED HOSE CLAMPS WAITED FOR EICAS MESSAGE. OPC GOOD IAW AMM 36-00-00/ETN-EM-21-956/21-51-02.
- [SDR SIMA202009064001](https://openairdocs.org/sdr/SIMA202009064001.md): Computer · malfunctioned · Sep 4, 2020 · N689EC · Emb EMB145LR · Stall Warning System
  > ON DESCENT SPS 2 INOPERABLE WARNING WENT AWAY, BUT CAME RIGHT BACK AS WE RAN THE QRH SPS 1 INOPERABLE AS WELL WE ALSO RECEIVED STICK PUSHER FAIL AND SPS ADVANCED MECH, SPS FAIL. EMERGENCY DECLARED C/A-REF FIM TASK 27-36-00-810-A. PERFORMED RESET OF STALL PROT
- [SDR SIMA20200827001](https://openairdocs.org/sdr/SIMA20200827001.md): Door Sill · corroded · Aug 27, 2020 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SSI 53-30-48; CARGO DOOR SILL IS CORRODED. -C/A-EVALUATED CORROSION ON CARGO DOOR CENTER SILL AND FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-31-15AD. REMOVED AND REPLACED CARGO DOOR CENTER SILL IAW EMB 145 SRM 51-40-02 MATERIALS USED PN: 145-25480-603SD CARG
- [SDR SIMA202008276002](https://openairdocs.org/sdr/SIMA202008276002.md): Structure · corroded · Aug 26, 2020 · N689EC · Emb EMB145LR · Fuselage Main, Structure
  > SSI 53-30-03; FRAME 68 CARGO DOOR LATERAL L-SHAPE IS CORRODED. -C/A-ACCOMPLISHED PERMANENT REPAIR ON FRAME 68 CARGO DOOR LATERAL L-SHAPE SHEAR CLIP IAW EMB 145 SRM 53-31-04RE ITEM 4D
- [SDR SIMA202008276001](https://openairdocs.org/sdr/SIMA202008276001.md): Rib · cracked · Aug 26, 2020 · N689EC · Emb EMB145LR · Wing, Rib/Bulkhead
  > LH WING RIB 21 IS CRACKED INSIDE PANEL 551CB (AS MARKED).-C/A-REMOVED, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND SHIM AT LH WING RIB 21 IAW EMB 145 SRM 57-20-07. MATERIAL LIST: FILLER: AL CLAD 2024 T3 OR AL CLAD 2024 T42 OR AL 7475 T7451 OR AL 7475
- [SDR SIMA202008242004](https://openairdocs.org/sdr/SIMA202008242004.md): Web · gouged · Aug 22, 2020 · N689EC · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL WEB STRUCTURE GOUGED. REPAIRED CARGO DOOR INNER WEB IAW SRM 52-30-01.
- [SDR SIMA202008242002](https://openairdocs.org/sdr/SIMA202008242002.md): Skin · cracked · Aug 22, 2020 · N689EC · Emb EMB145LR · Fuselage Main, Frame
  > LH UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX. 3/8? LONG ENDS ARE MARKED.-C/A-FABRICATED AND INSTALLED A REPAIR DOUBLER, FILLER, REPAIR ANGLE AND SHIM IAW EMB 145 SRM 53-31-01. MATERIALS USED: REPAIR DOUBLER ? A
- [SDR SIMA202008251003](https://openairdocs.org/sdr/SIMA202008251003.md): Doubler · gouged · Aug 21, 2020 · N689EC · Emb EMB145LR · Cargo/Baggage Doors
  > 2 PREVIOUSLY INSTALLED DOUBLERS ON CARGO DOOR LOWER WEB SECTION GOUGED. -C/A-REMOVED, FABRICATED AND INSTALLED DOUBLERS FOR CARGO DOOR INNER LOWER WEB IAW EMB 145 SRM 52-30-01 ITEM 12. MATERIAL FOR DOUBLERS: AL 7475-T761 (.040).
- [SDR SIMA20200821002](https://openairdocs.org/sdr/SIMA20200821002.md): Door Frame · corroded · Aug 21, 2020 · N689EC · Emb EMB145LR · Fuselage Main, Structure
  > CARGO DOOR LOWER FRAME CORRODED AT SCREW HOLE. REMOVED AND REPLACED THE CARGO DOOR LOWER FRAME IAW SRM 51-40-02.
- [SDR SIMA202008210002](https://openairdocs.org/sdr/SIMA202008210002.md): Floor Support · corroded · Aug 20, 2020 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM AT FR 24-25 IS CORRODED. -C/A-BLENDED OUT CORROSION ON CENTER OMEGA BEAM AT FR 24-25 IAW SRM 51-10-03 AND CPM 51-14-02. REMAINING THICKNESS FOUND TO BE BEYOND LIMITS IAW SRM 53-22-10. FABRICATED AND INSTALLED A DOUBLER FOR REPAIR OF CENTER OM
- [SDR SIMA2020082519006](https://openairdocs.org/sdr/SIMA2020082519006.md): Frame · corroded · Aug 19, 2020 · N689EC · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 65 IS CORRODED ABOVE CARGO DOOR SILL.-C/A-REMOVED AND REPLACED FR 65 SECTION AT CARGO DOOR CUTOUT IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 145-64106-001 FR 65 SECTION, PN: 145-03301-003 STR 16L SUPPORT (SHEAR CL
- [SDR SIMA2020082419005](https://openairdocs.org/sdr/SIMA2020082419005.md): Shear Tie · corroded · Aug 19, 2020 · N689EC · Emb EMB145LR · Fuselage Internal Mounting Structure
  > FRAME 65 CARGO DOOR SHEAR TIE WAS CORRODED. REMOVED AND REPLACED FR 65 CARGO DOOR SHEAR TIE IAW SRM 51-40-02.
- [SDR SIMA20200817001](https://openairdocs.org/sdr/SIMA20200817001.md): Frame · cracked · Aug 17, 2020 · N689EC · Emb EMB145LR · Fuselage Main, Frame
  > DURING HMBV INSPECTION, FR 73 CRACKED BETWEEN STR 15R-16R-C/A-RAR FR 73 LOWER SECTION TO REPAIR CRACK BETWEEN STR 15R-16R IAW EMB 145 SRM 51-40-02
- [SDR SIMA202008174004](https://openairdocs.org/sdr/SIMA202008174004.md): Fitting · damaged · Aug 14, 2020 · N689EC · Emb EMB145LR · Wing, Attach Fittings
  > RH AILERON PCA FITTING HAS ELONGATED BUSHING HOLES-C/A-RAR RH AILERON PCA FITTING IAW EO-EM-27MR-112
- [SDR SIMA202008174003](https://openairdocs.org/sdr/SIMA202008174003.md): Service Panel · corroded · Aug 14, 2020 · N689EC · Emb EMB145LR · Fuselage Main, Structure
  > LAV BUCKET CORRODED AROUND SERVICING NIPPLE AND DRAIN HANDLE-C/A-RAR LAV BUCKET IAW EMB 145 SRM 51-40-02 AND 51-20-03
- [SDR SIMA20200813002](https://openairdocs.org/sdr/SIMA20200813002.md): Floor Support · corroded · Aug 13, 2020 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM AT FR 24-25 CORRODED-C/A-ACCOMPLISHED PERMANENT REPAIR ON LH OMEGA BEAM AT FR 24-25 IAW ERS-EM-53MR-4163. REPAIR MATERIAL; DOUBLER- 2024T3-.063?
- [SDR SIMA20200726008](https://openairdocs.org/sdr/SIMA20200726008.md): Bulb · inoperative · Jul 26, 2020 · N689EC · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT ON CEILING PANEL AT 7A INOP. C/A COMPLETE: REMOVED AND REPLACED BULB ON CEILING PANEL 7A, IAW EMB 145 AMM 33-50-08. CHECKS GOOD.
- [SDR SIMA20200726007](https://openairdocs.org/sdr/SIMA20200726007.md): Floor Support · corroded · Jul 26, 2020 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS CORROSION AT FR 31, AS MARKED. C/A COMPLETE: FOUND CORROSION ON RT FLOOR SILL AT FR 31 TO BE OUT OF LIMITS, IAW EMB 145SRM 53-22-10. R & R CABIN RT NR 2 FLOOR SILL, IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20200726006](https://openairdocs.org/sdr/SIMA20200726006.md): Cradle · broken · Jul 26, 2020 · N689EC · Emb EMB145LR · Emergency Equipment
  > EMERGENCY FLASHLIGHT CRADLE ON LAV WALL IS BROKEN. C/A COMPLETE: R & R EMERGENCY FLASHLIGHT CRADLE ON LAV WALL, IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA20200726009](https://openairdocs.org/sdr/SIMA20200726009.md): Power Supply · not reported · Jul 26, 2020 · N689EC · Emb EMB145LR · Emergency Lighting
  > STD REQ A110 OPS A. REPLACE EPSU CRJ WC 33-002 OR EMB WC 33-700-19 PN: 11-0049 SN: 18369 POS: 2. C/A COMPLETE: PCW BY RECORDS REVIEW AND DVI OF EQUIPMENT INSTALLED ON AIRCRAFT, REF CITRIX (MTX OPS) NRWC 689-DFW-04797 DATED: 07/19/20. FOR R&R OF POS NR 2 EME
- [SDR SIMA20200726005](https://openairdocs.org/sdr/SIMA20200726005.md): Floor Support · corroded · Jul 26, 2020 · N689EC · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LT FLOOR SILL HAS CORROSION AT FR32, AS MARKED. C/A COMPLETE: BLENDED AND FOUND AREAS AT LT FLOOR SILL AT FR 32 TO BE OUT OF LIMITS, IAW EMB 145 SRM 51-10-03 AND 53-22-10. R&R LT OUTBOARD SILL NR 3, IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20200726004](https://openairdocs.org/sdr/SIMA20200726004.md): Connector · broken · Jul 26, 2020 · N689EC · Emb EMB145LR · Light System Wiring
  > EMERGENCY LIGHT STRIP NR 6 HAS BROKEN CONNECTOR. C/A COMPLETE: REMOVED AND REPLACED EMERGENCY LIGHT STRIP NR 6 BROKEN CONNECTOR, IAW EMB 145 SWPM 20-21-00.
- [SDR SIMA202007189003](https://openairdocs.org/sdr/SIMA202007189003.md): Charger · inoperative · Jul 9, 2020 · N689EC · Emb EMB145LR · Emergency Lighting
  > DURING PS-1 INSP FOUND EMERGENCY LIGHTS AT SERVICE DOOR AND RH WING TO FUSELAGE FAIRING INOP.-C/A-RAR #2 EMERGENCY BATTERY AND CHARGER ASSY IAW E145 AMM 33-50-04. OPERATIONAL CHECK GOOD
- [SDR SIMA2020040130001](https://openairdocs.org/sdr/SIMA2020040130001.md): Battery · discharged · Mar 30, 2020 · N689EC · Emb EMB145LR · Emergency Lighting
  > SUPPLEMENTAL MAIN DOOR (ENTRANCE CEILING) EMERG LIGHT INOP. CONTINUITY TO GROUND WHEN CONNECTOR P8500 (BATTERY CRADLE) DISCONNECTED AND POSITIVE WIRE AT BULB (W766-8052-20) BOTH WIRES AT BULB DISCONNECTED. NEW CRADLE NEEDED. (WHEN A NEW CRADLE INSTALLED BULB L
- [SDR SIMA2020040130003](https://openairdocs.org/sdr/SIMA2020040130003.md): Battery · broken · Mar 30, 2020 · N689EC · Emb EMB145LR · Emergency Lighting
  > #4 EMERGENCY LIGHT BATTERY HAS A BROKEN CAM LOCK.-C/A-REPLACED #4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS GOOD

Next page: https://openairdocs.org/aircraft/N689EC/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 = 'N689EC' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N689EC/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.