# Service difficulty reports: N608LM

A list on [N608LM](https://openairdocs.org/aircraft/N608LM.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 3 · 126 reports

- [SDR HNAA2021083100437](https://openairdocs.org/sdr/HNAA2021083100437.md): Warning Message · false activation · Aug 31, 2021 · N608LM · Emb EMB145LR · Engine Anti-Icing System
  > DURING CLIMBOUT, BLEED 1 LOW TEMP MSG IN ICING CONDITIONS. PERFORMED OPERATION CHECK OF THE AIR BLEED SYSTEM IAW AMM 36-00-00-700-806. NO DEFECTS NOTED COULD NOT DUPLICATE OPS CHECK GOOD OK FOR SERVICE.
- [SDR HNAA2021070600315](https://openairdocs.org/sdr/HNAA2021070600315.md): Sign · inoperative · Jul 5, 2021 · N608LM · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT STRIP ON SIDEWALL PANEL AFT OF LH EMERGENCY EXIT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY SIGN ASSEMBLY PANEL ON LH AFT UPPER SIDEWALL PANEL IAW EMB 145 AMM 33-50-14-000/400-801-A. OK FOR SERVICE.
- [SDR HNAA2021052000221](https://openairdocs.org/sdr/HNAA2021052000221.md): Inverter · faulted · May 19, 2021 · N608LM · Emb EMB145LR · Emergency Lighting
  > L/H SIDEWALL EMERGENCY EXIT SIDEWALL SIGN LIGHT INOP, JUST AFT OF EXIT OPENING. FOUND TO BE NUMBER 5 INVERTER IN CEILING TO BE FAULTY, REMOVED AND REPLACED NUMBER 5 INVERTER IAW AMM 33-50-11-000-801-A, 33-50-11-400-801-A.
- [SDR HNAA2021022700063](https://openairdocs.org/sdr/HNAA2021022700063.md): Switch · malfunctioned · Feb 24, 2021 · N608LM · Emb EMB145LR · Engine Thrust Reverser
  > ENGINE NR 2 T/R DEPLOYED AT 85 TO 90 KNOTS ON TAKE OFF ROLL. ABORTED TAKEOFF. MAINTENANCE PERFORMED: MEL 24FEB21 09:04 ROA C05503 78-1 THRUST REVERSES C/W MAINT AND FLT CREW PROCEDURES. FDR SHOWS #2 ENGINE TR WAS IN TRANSIT. ELECTRICALLY TESTED BOTH THE UPPE
- [SDR HNAA2021022500061](https://openairdocs.org/sdr/HNAA2021022500061.md): Bleed Valve · failed · Feb 23, 2021 · N608LM · Emb EMB145LR · Compressor Bleed Valve
  > PDIS 608 36-11 2329701 23FEB21 ROA CLOSE ENG 1 BLEED VALVE FAIL WHEN AT FULL POWER. EICAS MESSAGE CLEARS WHEN POWER AT IDLE. FACT 23FEB21 23:11 ROA. R & R'D HIGH STAGE PRESSURE SWITCH IAW 36-11-00. OPS CHECK GOOD.
- [SDR HNAA2020102200288](https://openairdocs.org/sdr/HNAA2020102200288.md): Inverter · inoperative · Oct 20, 2020 · N608LM · Emb EMB145LR · Emergency Lighting
  > AISLE FLOOR SECTIONS 4-5 EMERGENCY LIGHTS INOPERABLE. MAINTENANCE: R & R NR 5 EMERGENCY LIGHT INVERTER, IAW AMM 33-50-11-000-801-A. OPERATIONS CHECK GOOD, OK FOR SERVICE.
- [SDR HNAA2020030900091](https://openairdocs.org/sdr/HNAA2020030900091.md): Fcu · malfunctioned · Mar 7, 2020 · N608LM · Emb EMB145LR · Fuel Indicating System
  > REJECTED TAKEOFF DUE TO FUEL 2 LO LEVEL WARNING MSG ON EICAS. WING TANK FUEL QTY INDICATIONS ON EICAS AND MFD NORMAL. MOC ISSUED MEL 28-12 WITH CREW. MAINTENANCE: R/R'D FCU REF AMM 28-41-01. OPS CHECK GOOD, OK FOR SERVCIE.
- [SDR HNAA2019120200373](https://openairdocs.org/sdr/HNAA2019120200373.md): Wire · broken · Nov 27, 2019 · N608LM · Emb EMB145LR · Light System Wiring
  > MDIS 608 33-50 2106261 27NOV19 LEX CLOSE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 INOP DUE TO BROKEN WIRE AND DAMAGED FIXTURE AT CONNECTOR. 42300 00 DEW OVERHEAD EMERGENCY EXIT LIGHT AT
- [SDR HNAA2019112700371](https://openairdocs.org/sdr/HNAA2019112700371.md): Spoiler Sys · malfunctioned · Nov 22, 2019 · N608LM · Emb EMB145LR · Drag Control System
  > SPOILER FAIL MESSAGE ON DESCENT WITH STRONG LEFT ROLLING TENDENCY....FIX: INSPECTED AND CLEANED PROX SWITCH FOR SPOILER SYSTEM, NO DEFECTS NOTED.PERFORMED SPOILER OPS CK IAW AMM 27-63-01.TRANSITORY CONDITION OF SCU. T/S IAW FIM 27-63-00-810-802-A
- [SDR HNAA2019110400341](https://openairdocs.org/sdr/HNAA2019110400341.md): Actuator · faulty · Nov 3, 2019 · N608LM · Emb EMB145LR · Elevator Control System
  > PDIS 608 27-31 2128242 03NOV19 CLT CLOSE CONTROL COLUMN FEELS LIKE IT CATCHING ON SOMETHING WITH INCREASED FRICTION WHEN PULLED BACK ACCOMPANIED BY FAINT CLICKING NOISES FACT 03NOV19 06:54 ROA FOUND STICK PUSHER ACTUATOR
- [SDR HNAA2019050200133](https://openairdocs.org/sdr/HNAA2019050200133.md): Light · inoperative · Apr 30, 2019 · N608LM · Emb EMB145LR · Emergency Lighting
  > NDIS 608 33-51 0021800 30APR19 RIC CLOSE EMERGENCY EXIT AISLE ILLUMINATION LIGHT AT RT WING EXIT DOOR INOP. 36218 00 NGR FACT 30APR19 09:57 RIC R/R LAMP FOR PSU EMERGENCY LIGHT AT SEAT 12B AND 12C IN REF TO AMM 33-50-08-000/400-801-A. OPS CHECK GOOD.
- [SDR HNAA2019050200132](https://openairdocs.org/sdr/HNAA2019050200132.md): Connector · not seated · Apr 30, 2019 · N608LM · Emb EMB145LR · Light System Wiring
  > NDIS 608 33-51 0021790 30APR19 RIC CLOSE AISLE 12 EMERGENCY EXIT SIGN AFT PORTION NOT ILLUMINATED 36218 00 NGR FACT 30APR19 09:55 RIC RESEATED CONNECTORS FOR AFT EXIT LOCATING SIGN AT ROW 12 IN REF TOAMM 33-50-15-000/400-801-A. OPS CHECK GOOD OK F
- [SDR HNAA2019043000130](https://openairdocs.org/sdr/HNAA2019043000130.md): Warning Light · illuminated · Apr 29, 2019 · N608LM · Emb EMB145LR · Cargo/Baggage Doors
  > PDIS 608 52-30 1869733 29APR19 PHL ASSGN ON CLIMBOUT, RECEIVED BAG DOOR OPEN INDICATION. RETURN TO FIELD. LARRYS HISTORY: NONE MEL 29APR19 22:27 PHL C11918 52-3-2
- [SDR HNAA2019041300099](https://openairdocs.org/sdr/HNAA2019041300099.md): Skin · corroded · Apr 5, 2019 · N608LM · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING HVY CHK MAINTENANCE FOUND CORROSION ON FUSELAGE INTERNAL SKIN UNDER FR 61 TEAR STRAP BETWEEN STGR 17L-18L. REPAIRED IAW SRM 53-31-01
- [SDR HNAA2019041100098](https://openairdocs.org/sdr/HNAA2019041100098.md): Rod End · damaged · Apr 2, 2019 · N608LM · Emb EMB145LR · Ailerons
  > R/H AILERON ACTUATOR ROD END FITTING O/B HAT BUSHING HOLE OVERSIZED FOUND IN HVY CHK. INSTALLED BUSHING PER SRM 51-20-09
- [SDR HNAA2019040700091](https://openairdocs.org/sdr/HNAA2019040700091.md): Door Sill · corroded · Apr 1, 2019 · N608LM · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING HVY CHK MAINTENANCE FOUND CORROSION AROUND SERVICE DOOR FWD SILL NUT PLATE HOLES. R&R.
- [SDR HNAA2019041300100](https://openairdocs.org/sdr/HNAA2019041300100.md): Skin · dented · Mar 29, 2019 · N608LM · Emb EMB145LR · Cargo/Baggage Doors
  > DISCREPANCY: DURING HVY CHK MAINTENANCE FOUND CARGO DOOR EXTERNAL SKIN HAS A DENT WITH A GOUGE ON THE FWD LOWER CORNER. CORRECTIVE ACTION: REPAIRED IAW ETD2019-145-044683
- [SDR HNAA2019041100097](https://openairdocs.org/sdr/HNAA2019041100097.md): Housing · cracked · Mar 29, 2019 · N608LM · Emb EMB145LR · Cargo/Baggage Doors
  > DURING HVY CHECK CARGO DOOR EXTERNAL HANDLE CUTOUT IS CRACKED AT THE END. REPAIRED IAW SRM 52-30-01RE.
- [SDR HNAA2018082400205](https://openairdocs.org/sdr/HNAA2018082400205.md): Uplock · failed · Aug 23, 2018 · N608LM · Emb EMB145LR · Landing Gear Retraction/Extension System
  > PDIS 608 32-30 1576422 23AUG18 PHL CLOSE ON GEAR UP SELECTION LANDING GEAR DISAGREE MESSAGE D ISPLAYED ON EICAS AND LEFT GEAR DID NOT RETRACT CREW PERFORMED QRH AND GEAR STAYED IN DOWN POSITION. NO EMERGENCY WAS DECLARED.
- [SDR HNAA2017081600275](https://openairdocs.org/sdr/HNAA2017081600275.md): Anti-Ice Valve · failed · Aug 14, 2017 · N608LM · Emb EMB145 · Airfoil Anti/De-ice System
  > IN ICING CONDITIONS, WING ANTI-ICE FAILED MESSAGE. CMC SHOWS WING 2 ANTI-ICE LEAK. PUSHED BUTTON OPEN INSCRIPTION SHOWED VALVE CLOSED DURING ICING IN AUTO MODE. R & R THE ANTI-ICE VALVE IAW 30-11-01. GROUND RUN, OPS CHECKED IAW AMM 30-00-00-700-802A/500, O
- [SDR HNAA2017062100210](https://openairdocs.org/sdr/HNAA2017062100210.md): Engine · failed · Jun 16, 2017 · N608LM · Emb EMB145 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FAILURE DURING LANDING ROLLOUT. EICAS MESSAGES FOR NR 1 ENGINE EXCEEDANCE, HS VALVE NR 1 FAILED. CREW STATED A STRONG ELECTRICAL ODOR IN COCKPIT AND FORWARD CABIN THAT GOT WORSE WHEN APU TURNED ON. CMC MESSAGES FOUND WHERE HS VALVE NR 1 FAILED.
- [SDR HNAA2017050700154](https://openairdocs.org/sdr/HNAA2017050700154.md): Switch · dirty · May 7, 2017 · N608LM · Emb EMB145LR · Door Warning System
  > DURING TAKE OFF, RECEIVED A MASTER CAUTION EICAS MESSAGE FOR THE CARGO DOOR OPEN. ABORTED TAKE OFF AND RETURNED TO GATE. CLEANED AND LUBED FWD AND AFT CARGO DOOR SWITCHES.
- [SDR HNAA2017032000089](https://openairdocs.org/sdr/HNAA2017032000089.md): Warning Message · false activation · Mar 18, 2017 · N608LM · Emb EMB145LR · Ice/Rain Protection System
  > ANTI ICE FAIL MESSAGE ILLUMINATED ON EICAS AT 65 KTS DURING TAKEOFF. THE TAKEOFF WAS ABORTED. GROUND RAN AIRCRAFT AND PERFORMED OPS CHECK IAW AMM 30-00-00. NO DEFECTS FOUND AT THIS TIME. EICAS MESSAGE CLEARED. OKAY FOR SERVICE.
- [SDR HNAA2017021500051](https://openairdocs.org/sdr/HNAA2017021500051.md): Pressure Switch · failed · Feb 10, 2017 · N608LM · Emb EMB145LR · Airfoil Anti/De-ice System
  > DURING CLIMBOUT, WING ANTI ICE FAIL EICAS CAUTION FOLLOWED BY ANTI ICE WARNING EICAS, COMPLIED WITH QRH AND MESSAGE DISAPPEARED SHORTLY BEFORE REAPPEARING. R & R RIGHT WING ANTI-ICE VALVE IAW MM 30-11-01 AND RT WING ANTI ICE LOW PRESSURE SWITCH IAW 30-11-02.
- [SDR HNAA2017020800045](https://openairdocs.org/sdr/HNAA2017020800045.md): Anti-Ice System · malfunctioned · Feb 5, 2017 · N608LM · Emb EMB145LR · Ice/Rain Protection System
  > DURING DESCENT AT 66% POWER, WING ANTI ICE FAIL CAUTION LIGHT ILLUMINATED WITH NO ICE CONDITION. MESSAGE CHANGED TO ANTI ICE FAIL ICE CONDITION ON ENTERING ICE CONDITIONS. ALL MESSAGE CLEARED AFTER EXITING ICE COND,LEVELING OFF AND PUSHING POWER LEVERS FWD.
- [SDR HNAA2017020300038](https://openairdocs.org/sdr/HNAA2017020300038.md): Pressure Switch · malfunctioned · Feb 3, 2017 · N608LM · Emb EMB145 · Pneumatic Distribution System
  > DURING CLIMB, NR 2 BLEED LEAK EICAS MESSAGE ILLUMINATED ALONG WITH PB LEAK ILLUMINATED. CLEARED MESSAGE. REMOVED AND REPLACED NR 2 LOW PRESSURE, OPS CHECKED OK AT THIS TIME. SWITCH REPLACED IAW MM 30-11-00-810-811-A.
- [SDR HNAA2017020300034](https://openairdocs.org/sdr/HNAA2017020300034.md): Warning Message · false activation · Feb 3, 2017 · N608LM · Emb EMB145 · Central Warning
  > AURAL TAKEOFF TRIM DURING TAKEOFF. TRIM WAS IN GREEN. COMPLIED WITH TASK 27-40-00-700-805-A. OPS CHECKED GOOD. OKAY FOR SERVICE.
- [SDR HNAA2016121200383](https://openairdocs.org/sdr/HNAA2016121200383.md): Anti-Ice System · no test · Dec 11, 2016 · N608LM · Emb EMB145LR · Airfoil Anti/De-ice System
  > DURING AN ANTI-ICE TEST IN FLIGHT, EICAS MESSAGE STAB ANTI ICE FAILED DISPLAYED. ATTEMPTED TEST 3 TIMES.
- [SDR SIMA20161119003](https://openairdocs.org/sdr/SIMA20161119003.md): Frame · bent · Nov 19, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 72 IS BENT AT STRINGER 16R INSIDE CARGO. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-40-02.
- [SDR SIMA20161114005](https://openairdocs.org/sdr/SIMA20161114005.md): Rib · chafed · Nov 14, 2016 · N608LM · Emb EMB145LR · Wing, Rib/Bulkhead
  > LEFT WING RIB LOCATED BETWEEN 551CB AND 551DB, CHAFED UNDER THE PCA HOSES. REPAIRED THE RIB IAW ERS-EM-57MR-723.
- [SDR SIMA20161114004](https://openairdocs.org/sdr/SIMA20161114004.md): Frame · cracked · Nov 14, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Frame
  > OUTBOARD RIVET HOLE CRACKED ON LOWER END OF FRAME 66. REPAIRED THE FRAME IAW ERS-EM-53MR-2405.
- [SDR SIMA20161114003](https://openairdocs.org/sdr/SIMA20161114003.md): Shear Tie · corroded · Nov 14, 2016 · N608LM · Emb EMB145LR · Fuselage Internal Mounting Structure
  > FRAME 68 SHEAR TIE IS CORRODED AT CARGO DOOR CUT LOWER CORNER. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.
- [SDR SIMA20161114002](https://openairdocs.org/sdr/SIMA20161114002.md): Shear Tie · corroded · Nov 14, 2016 · N608LM · Emb EMB145LR · Fuselage Internal Mounting Structure
  > FRAME 65 SHEAR TIE CORRODED BELOW CARGO LOWER GUIDE AND AT CARGO DOOR SILL. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.
- [SDR SIMA20161112004](https://openairdocs.org/sdr/SIMA20161112004.md): Skin · cracked · Nov 12, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Plate/Skin
  > LEFT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1 AND 2L. REPAIRED THE SKIN IAW SRM 53-31-01.
- [SDR SIMA20161111004](https://openairdocs.org/sdr/SIMA20161111004.md): Door Sill · corroded · Nov 11, 2016 · N608LM · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER SILL CORRODED REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 53-40-02.
- [SDR SIMA20161111003](https://openairdocs.org/sdr/SIMA20161111003.md): Stringer · cracked · Nov 11, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 6R CRACKED AT FRAME 13. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02.
- [SDR SIMA20161111002](https://openairdocs.org/sdr/SIMA20161111002.md): Frame · cracked · Nov 11, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT FRAME 68 FRAME CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20161111001](https://openairdocs.org/sdr/SIMA20161111001.md): Door Frame · corroded · Nov 11, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Structure
  > LEFT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED AT AFT GUIDE BLOCK AND FWD GROUNDING CLIP. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-40-02
- [SDR SIMA20161110003](https://openairdocs.org/sdr/SIMA20161110003.md): Door Sill · corroded · Nov 10, 2016 · N608LM · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW EMB145 53-21-02, AND 51-20-03
- [SDR SIMA20161110004](https://openairdocs.org/sdr/SIMA20161110004.md): Skin · corroded · Nov 10, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION JUST AFT OF 123BL ACCESS PANEL BENEATH TCAS II ANTENNA, BETWEEN FRAMES 10 AND 11. REPAIRED THE SKIN IAW SRM 53-00-23.
- [SDR SIMA20161110002](https://openairdocs.org/sdr/SIMA20161110002.md): Skin · corroded · Nov 10, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION BENEATH TDR MODE-S ANTENNA, BETWEEN FRAMES 20 AND 21. REPAIRED THE SKIN IAW SRM 53-00-23.
- [SDR SIMA20161109003](https://openairdocs.org/sdr/SIMA20161109003.md): Contact · missing · Nov 9, 2016 · N608LM · Emb EMB145LR · Light System Wiring
  > LEFT NR 1 EMERGENCY LIGHT CONTACT MISSING. INSTALLED CONTACT IAW SWPM 20-00-03.
- [SDR SIMA20161025001](https://openairdocs.org/sdr/SIMA20161025001.md): Yoke · cracked · Oct 25, 2016 · N608LM · Emb EMB145LR · Nacelle/Pylon, Main Frame
  > RT FWD LOWER YOKE CRACKED FWD UPPER EDGE. REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386
- [SDR SIMA20161019013](https://openairdocs.org/sdr/SIMA20161019013.md): Skin · cracked · Oct 19, 2016 · N608LM · Emb EMB145LR · Fuselage Main, Plate/Skin
  > UPPER LEFT FUSELAGE SKIN HAS TWO CRACKS, ONE CRACK IS JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, AND 3/8 INCH LONG, AND THE OTHER CRACK IS AT FRAME 75 TOP FASTENER JUST BELOW LT DRAG ANGLE, APPROX. 1/4 INCH LONG. PERFORMED REPAIR IAW SRM 53-31-01
- [SDR SIMA20161018004](https://openairdocs.org/sdr/SIMA20161018004.md): Charger · failed · Oct 18, 2016 · N608LM · Emb EMB145LR · Emergency Lighting
  > LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EPSU NR 4 IAW W/C 33-700-19 AND OPS CHECK GOOD IAW W/C 33-700-17. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 76324.
- [SDR SIMA20161014001](https://openairdocs.org/sdr/SIMA20161014001.md): Light · inoperative · Oct 14, 2016 · N608LM · Emb EMB145LR · Emergency Lighting
  > LEFT WING EMEGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT AW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20160708006](https://openairdocs.org/sdr/SIMA20160708006.md): Pump · failed · Jul 8, 2016 · N608LM · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main
  > HYD2 LO QTY FOLLOWED BY HYD SYS 2 FAILED. REMOVED AND REPLACED ENGINE NR 2 HYDRAULIC EDP IAW EMB 145 AMM 29-10-03 PERFORMED LEAK AND OPS CHECK IAW AMM 72-00-00 NO LEAKS DETECTED
- [SDR SIMA20160627001](https://openairdocs.org/sdr/SIMA20160627001.md): Brake · failed · Jun 27, 2016 · N608LM · Emb EMB145LR · Brake
  > LEFT MAIN BRAKES ON FIRE, REPORTED BY TOWER, PERFORMED GROUND EVACUATION. REF ITEMS NR 1 AND NR 2 LOG PAGE 4036786, ITEMS NR 1,2 AND 3. NR 2 BRAKE FAILURE. R & R NR 2 BRAKE ASSY IAW W/C 32-600-14. R & R NR 2 BRAKE LINES IAW CMM 32-10-01. NO LEAKS NOTED.
- [SDR SIMA20160520003](https://openairdocs.org/sdr/SIMA20160520003.md): Power Supply · inoperative · May 20, 2016 · N608LM · Emb EMB145LR · Emergency Lighting
  > LEFT & RIGHT OVERWING EMER LIGHTING INOPERATIVE. TROUBLE SHOT LT & RT OVERWING EMER LIGHTING & ISOLATED PROBLEM TO EMER BATTERY POWER SUPPLY. R & R EMER BATTERY POWER SUPPLY IAW AMM-33-50-04.
- [SDR SIMA20160130001](https://openairdocs.org/sdr/SIMA20160130001.md): Gcu · failed · Jan 30, 2016 · N608LM · Emb EMB145 · AC Regulator
  > ON FINAL WE TURNED THE APU ON IAW MEL 24-4, ONCE APU ON LINE, RECVD GEN 1 - 4 OFF BUS, SHORTLY AFTER WE LOST EICAS FOR 5 - 10 SECONDS, GEN 1 WAS SHOWING 7.4 VOLTS 0 A. SUSPECT NR 4 GCU. R & R GCU IAW AMM 24-31-02. PERFORMED OPERATIONS CHECK IAW AMM 24-31-00

Next page: https://openairdocs.org/aircraft/N608LM/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 = 'N608LM' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N608LM/reports

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