# Service difficulty reports: N825AE

A list on [N825AE](https://openairdocs.org/aircraft/N825AE.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 2 · 80 reports

- [SDR SIMA202006298003](https://openairdocs.org/sdr/SIMA202006298003.md): Pressure Switch · failed · Jun 28, 2020 · N825AE · Emb EMB135KL · Hydraulic System, Main
  > SUPPLEMENTAL EMERG BRK LO PRES-C/A-ACCUMULATOR LOW PRESSURE SWITCH DEFERRED PER MEL 32-5,''M'' PROCUDERS IN SECTION 4 C/W. PERFORMED FIM TASK 32-44-00-810-801-A,REMOVED AND REPLACED EMEGENCY BRAKE LOW PRESSURE SWITCH IAW EMB 140 AMM CH 32-44-05. FUNCTIONAL CH
- [SDR SIMA201912043001](https://openairdocs.org/sdr/SIMA201912043001.md): Control Valve · failed · Dec 3, 2019 · N825AE · Emb EMB135KL · Cabin Cooling System
  > AFTER TAKEOFF, THE NR 2 PACK VALVE CLOSED ON EICAS. RESET IAW QRH. CREW SMELLED SLIGHT BURNING SMELL. NO ODOR NOTED IAW ETN-EM-72-034. REMOVED AND REINSTALLED THE RT DUAL TEMPERATURE CONTROL VALVE, INSTALLED A NEW SLEEVE ON CONTROL VALVE IAW AMM 21-60-01,
- [SDR SIMA2019111109004](https://openairdocs.org/sdr/SIMA2019111109004.md): Warning Message · false activation · Nov 9, 2019 · N825AE · Emb EMB135KL · Door Warning System
  > AFTER TAKE OFF "BAGGAGE DOOR" LIGHT ILLUMINATED RETURNED TO DFW "BAGGAGE DOOR LIGHT" TURNED OFF AFTER LANDING-C/A-DEFFERED BAGGAGE DOOR INDICATION PER MEL 52-5. CLEANED BAGGAGE DOOR WARNING MICROSWITCHES AND PERFORMED OPS TEST IAW EMB 140 AMM 52-76-01. OPS TE
- [SDR SIMA201911087003](https://openairdocs.org/sdr/SIMA201911087003.md): Connector · damaged · Nov 7, 2019 · N825AE · Emb EMB135KL · Light System Wiring
  > DURING PS-1 CHECK INSPECTION FOUND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP-C/A-REPAIRED ELECTRICAL CONNECTOR AT AFT EMERGENCY FLOOR LIGHT STRIP PER SWPM 20-50-00 OPS CHECK GOOD
- [SDR SIMA20191031005](https://openairdocs.org/sdr/SIMA20191031005.md): Warning System · false activation · Oct 31, 2019 · N825AE · Emb EMB135KL · Cabin Cooling System
  > PACK 1 OVERHEAT IN CRUISE BURNING SMELL RIGHT BEFORE CATION MESSAGE-C/A-FOUND PACK 1 SWITCH IN MANUAL MODE AND IN FULL HOT POSITION. PERFORMED PACK DUCT INSP. IAW AMM 21-51-14. PERFORMED GVI ACM INLET IAW AMM 21-51-00 NO DEFECTS NOTED PERFORMED OPS CHECK IAW A
- [SDR SIMA201908013001](https://openairdocs.org/sdr/SIMA201908013001.md): Coupling · leaking · Jul 31, 2019 · N825AE · Emb EMB135KL · Pneumatic Distribution System
  > BLEED 2 LEAK IMMEDIATELY AFTER TAKEOFF ASSOCIATED EICAS MESSAGE AND RED LEAK ON BLEED 2 BUTTON-C/A-INSPECTED AND FOUND ENGINE START GROUND CONNECTION COUPLING TO BE LEAKING SEVERLY. RAR GROUND CONNECTION COUPLING PER AMM 36-10-02. LEAK CHECK GOOD. NO BLEED
- [SDR SIMA201812276001](https://openairdocs.org/sdr/SIMA201812276001.md): Pitot Tube · contaminated · Dec 26, 2018 · N825AE · Emb EMB135KL · Pitot/Static System
  > EMERGENCY DIVERT DUE TO UNRELIABLE AIRSPEED ON ALL 3 AIRSPEED INDICATORS AT FL 300. THE ISSUE DID NOT CLEAR UP UNTIL DESCENDING THROUGH FL 190 APPROXIMATLY. DECLARED EMERGENCY FLIGHT CANCELED.-C/A-INSPECTED PITOT DRAIN PROT AND EMPTIED MOISTURE IAW E145 AMM 3
- [SDR SIMA20181031001](https://openairdocs.org/sdr/SIMA20181031001.md): Flashlight · broken · Oct 31, 2018 · N825AE · Emb EMB135KL · Emergency Equipment
  > FA FLASHLIGHT BROKEN. REMOVED AND REPLACED FA FWD FLASHLIGHT IAW AMM 33-50-16 AND PERFORMED OPS CHECK IAW AMM 33-51-01. OPS CHK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR SIMA201808064001](https://openairdocs.org/sdr/SIMA201808064001.md): Light · inoperative · Aug 4, 2018 · N825AE · Emb EMB135KL · Emergency Lighting
  > FLOOR EMERGENCY LIGHT STRIPS NEAR THE LAVATORY WAS INOPERATIVE. REMOVED AND REPLACED FLOOR THE EMERGENCY LIGHTS IAW AMM 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA201808064002](https://openairdocs.org/sdr/SIMA201808064002.md): Light · inoperative · Aug 4, 2018 · N825AE · Emb EMB135KL · Emergency Lighting
  > FLOOR EMERGENCY LIGHT STRIPS BY THE SERVICE DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BY SERVICE DOOR IAW AMM 33-50-12. OPS CHECKED GOOD. NO FURTHER DEFECT NOTED.
- [SDR SIMA201807050001](https://openairdocs.org/sdr/SIMA201807050001.md): Relay · failed · Jul 4, 2018 · N825AE · Emb EMB135KL · Air Distribution System
  > SMELL OF BURNING ELECTRICAL STRONGEST ON CA SIDE DURING CRUSE. REMOVED AND REPLACED RELAY K0550 IAW AMM 20-13-02. OP CHECKING GOOD IAW AMM 27-25-00 SUBTASK 710-002-A UP TO STEP J(11). PERFORMED FIM TASKS 21-20-00-810-801 (UP TO PG 3, BLOCK 33), 34-22-00-810-83
- [SDR SIMA201807020003](https://openairdocs.org/sdr/SIMA201807020003.md): Battery · failed · Jul 1, 2018 · N825AE · Emb EMB135KL · Emergency Equipment
  > WEAK SMELL OF "WARM/OVERHEATED" ELECTRONICS MOSTLY AT CRUISE FL220 AND AQT CA SIDE. REMOVED AND REPLACED BOTH COCKPIT EMER FLASHLIGHT BATTERIES IAW CMM 25-60-11. (OLD BATTERIES HAD A VERY WEAK ELECTRICAL SMELL TO THEM NO FUTHER DEFECT NOTED)
- [SDR SIMA201806065004](https://openairdocs.org/sdr/SIMA201806065004.md): Smoke Detector · no test · Jun 5, 2018 · N825AE · Emb EMB135KL · Smoke Detection
  > CARGO SMOKE DETECTOR DID NOT TEST PROPERLY. LIGHT WILL NOT ILLUMINATE DURING THE TEST BUT AFTER TEST IT WILL. REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM 26-14-01. OPS CHECKED GOOD IAW AMM 26-15-00.
- [SDR SIMA2018083027010](https://openairdocs.org/sdr/SIMA2018083027010.md): Shear Tie · cracked · May 27, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACK IN SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 6L AND 7L-C/A-INSTALLED EWIS PROTECTION IAW EMB SWPM 20-21-00. REMOVED LH PRECOOLER FLEXIBLE DUCT TO FOM IAW EMB 140 AMM 36-11-04. REMOVED SHEAR CLIP IAW EMB 140 SRM 51-40-02. LOCATED DRILLED AND ALODINED NEW C
- [SDR SIMA20180527004](https://openairdocs.org/sdr/SIMA20180527004.md): Fitting · damaged · May 27, 2018 · N825AE · Emb EMB135KL · Ailerons
  > LEFT AILERON PCA FITTING WAS NICKED AND GOUGED. REMOVED DAMAGE, AND FOUND TO BE OUT OF LIMITS IAW SRM 57-60-02. REMOVED AND REPLACED THE PCA FITTING IAW SRM 51-40-02, AMM 20-10-07, SRM 51-20-03,CPM 51-21-04, CPM 51-21-05, 51-21-06, AND ETN EM-51-091.
- [SDR SIMA201805297003](https://openairdocs.org/sdr/SIMA201805297003.md): Fitting · damaged · May 27, 2018 · N825AE · Emb EMB135KL · Wing, Attach Fittings
  > RIGHT AILERON PCA FITTING WAS NICKED AND GOUGED. REMOVED DAMAGE, AND DETERMINED TO BE OUT OF LIMITS IAW SRM 57-60-02. REMOVED THE PCA FITTING IAW SRM 51-40-02. LOCATED DRILLED AND ALODINED NEW FITTING IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED THE NEW F
- [SDR SIMA201805296001](https://openairdocs.org/sdr/SIMA201805296001.md): Sign · inoperative · May 26, 2018 · N825AE · Emb EMB135KL · Emergency Lighting
  > LEFT OVERWING EXIT UPPER EMERGENCY EXIT SIGN WAS INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-14. OPS CHECKED GOOD IAW 33-50-00.
- [SDR SIMA201805296003](https://openairdocs.org/sdr/SIMA201805296003.md): Wire · broken · May 26, 2018 · N825AE · Emb EMB135KL · Light System Wiring
  > LEFT EMERGENCY LIGHT, NR 6 LIGHT ASSY HAD A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD
- [SDR SIMA201805296002](https://openairdocs.org/sdr/SIMA201805296002.md): Power Supply · inoperative · May 26, 2018 · N825AE · Emb EMB135KL · Emergency Lighting
  > NUMBER 1 AISLE EMERGENCY LIGHT AND COCKPIT ENTRANCE LIGHT DID NOT OPERATE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY CHARGER IAW AMM 33-50-04, AND OPS CHECKED GOOD IAW AMM 33-50-00-700-801.
- [SDR SIMA2018052120004](https://openairdocs.org/sdr/SIMA2018052120004.md): Shear Tie · corroded · May 20, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CORROSION IN THE LATERAL L SHAPE AT FRAME 65, AT THE LOWER DOOR STOP. REMOVED THE DAMAGED SEGMENT OF LATERAL L SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 15L AND 16L IAW SRM 53-31-04, FIG 212. PERFORMED HFEC ALONG CUT OUT, NO DEFECTS NOTED IAW NDTM 51-00-00-9
- [SDR SIMA2018052120003](https://openairdocs.org/sdr/SIMA2018052120003.md): Support · cracked · May 20, 2018 · N825AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CRACKED LT OMEGA BEAM OTBD SUPPORT BETWEEN FRAMES 47 AND 48. CUT THE LT OMEGA OTBD SUPPORT IAW SRM 53-23-02. PERFORMED HFEC INSPECTION ALONG THE CUT LINE IAW NDTM 51-00-00-916-803 A, NO DEFECTS NOTED. LOCATED, DRILLED, AND ALODINED A REPAIR IAW SRM 51-20-0
- [SDR SIMA2018052120002](https://openairdocs.org/sdr/SIMA2018052120002.md): Floor Support · corroded · May 20, 2018 · N825AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE LT OMEGA BEAM, FRAMES 23 TO 32. BLENDED CORROSION ON THE OMEGA BEAM IAW SRM 53-22-10 AND 51-10-03, FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, AND ALODINED A NEW OMEGA BEAM IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED THE NEW OMEGA B
- [SDR SIMA2018052120001](https://openairdocs.org/sdr/SIMA2018052120001.md): Beam · corroded · May 20, 2018 · N825AE · Emb EMB135KL · Fuselage Main, Structure
  > COROSSION IN CARGO DOOR CUTOUT LOWER THRESHOLD BEAM BETWEEN FRAMES 65 AND 68. REMOVED THE THRESHOLD BEAM IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-21-04.
- [SDR SIMA2018052119005](https://openairdocs.org/sdr/SIMA2018052119005.md): Shear Tie · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACKED SHEAR AT FRAME 65, BETWEEN STRINGER 7L AND 9L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, 53-31-04, FIGURE 202, CPM 51-21-04, CPM 51-21-06, AND CPM 51-61-00.
- [SDR SIMA2018052119001](https://openairdocs.org/sdr/SIMA2018052119001.md): Shear Tie · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACKED SHEAR TIE, FRAME 68, BETWEEN STRINGERS 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND SRM 53-31-04, FIG 205.
- [SDR SIMA2018052119002](https://openairdocs.org/sdr/SIMA2018052119002.md): Shear Tie · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACKED SHEAR TIE AT FRAME 61, BETWEEN STRINGER 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-06 AND ETN EM -51-091.
- [SDR SIMA2018052219003](https://openairdocs.org/sdr/SIMA2018052219003.md): Shear Tie · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACK IN THE SHEAR TIE AT FRAME 67, BETWEEN STRINGER 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, 53-31-04, FIGURE 204, CPM 51-21-04, SRM 53-31-04 CPM 51-21-06, AND CPM 51-61-00.
- [SDR SIMA2018052119004](https://openairdocs.org/sdr/SIMA2018052119004.md): Shear Tie · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACKED SHEAR TIE AT FRAME 46, STRINGER 16L. REMOVED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED, ALODINED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-20-03, CPM 51-21-04, SRM 51-40-02, CPM 51-21-06, AND ETN EM-51-091.
- [SDR SIMA2018052119006](https://openairdocs.org/sdr/SIMA2018052119006.md): Stringer · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT FRAME 20, REMOVED THE STRINGER IAW SRM 51-40-02. LOCATED, DRILLED, ALODINED AND INSTALLED THE NEW STRINGER IAW SRM 51-20-03, CPM 51-21-04, CPM 51-21-05, 51-21-06, ETN EM-51-091, AND AMM 20-10-01.
- [SDR SIMA2018052119007](https://openairdocs.org/sdr/SIMA2018052119007.md): Shear Tie · cracked · May 19, 2018 · N825AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > CRACKED SHEAR TIE AT FRAME 24, BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-06 AND ETN EM-51-091.
- [SDR SIMA20150702003](https://openairdocs.org/sdr/SIMA20150702003.md): Flashlight · damaged · Jul 2, 2015 · N825AE · Emb EMB135KL · Emergency Equipment
  > FORWARD CABIN EMER FLASHLIGHT HAS DAMAGED CONNECTOR. R & R FWD CABIN EMER FLASHLIGHT IAW WC 33-700-20. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20150414005](https://openairdocs.org/sdr/SIMA20150414005.md): Light · inoperative · Apr 14, 2015 · N825AE · Emb EMB135KL · Emergency Lighting
  > 4TH FROM FWD EMER PROXIMITY LIGHTED STRIP IS INOPERATIVE. R & R 4TH FWD EMER PROXIMITY LIGHTED STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141014003](https://openairdocs.org/sdr/SIMA20141014003.md): Indicator · malfunctioned · Oct 14, 2014 · N825AE · Emb EMB135KL · Integrated Flight System
  > STAND BY ATT CAGED BETWEEN 80 & 90 KTS ON TAKEOFF ROLL. PERFORMED FIM TASK 34-01-00-816-001-A. ATT FUNCTION SET TO TRUE VALUE IN STABILIZED CONDITION. CONSIDERED TO BE TRANSITORY CONDITION IAW FIM 34-01-00.
- [SDR SIMA20141002005](https://openairdocs.org/sdr/SIMA20141002005.md): Switch · broken · Oct 2, 2014 · N825AE · Emb EMB135KL · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT BUTTON ON & OFF BROKEN OFF. LOOSE FAS SEAT. REPAIRED WITH SERVICED FLASHLIGHT SWITCH. OPERATIONS CHECKED GOOD SMP.
- [SDR SIMA20140829004](https://openairdocs.org/sdr/SIMA20140829004.md): Brake Assy · leaking · Aug 29, 2014 · N825AE · Emb EMB135KL · Brake
  > EMER BRAKE LOW PRESS ON EICAS. PARKING BRAKE NOT HOLDING PRESS. FOUND NR 3 BRAKE LEAKING & NR 4 BRAKE SHUTTLE VLV SEE NRWC 825-MIA-01756 FOR COMPLIANCE OF WORK PERFORMED. R & R NR 3 MLG BRAKE ASSEMBLY IAW 32-600-14 & 32-700-11. R & R NR 4 BRAKE SHUTTLE VLV
- [SDR SIMA20140117002](https://openairdocs.org/sdr/SIMA20140117002.md): Light · inoperative · Jan 17, 2014 · N825AE · Emb EMB135KL · Emergency Lighting
  > EMERGENCY CEILING LIGHT AT LT EMERGENCY EXIT INOPERATIVE. R & R LAMP IAW AMM 33-50-09. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20130807008](https://openairdocs.org/sdr/SIMA20130807008.md): Hydraulic System · warning message · Aug 7, 2013 · N825AE · Emb EMB135KL · Hydraulic System, Main
  > DURING DESCENT AFTER GEAR RETRACTION, HYD SYS 1 QTY LOWERED TO THE BOTTOM OF THE GREEN RANGE, BUT WAS STILL IN THE GREEN RANGE. RECEIVED AN EICAS HYD 1 QTY LOW MESSAGE. THE QTY WAS AT THE TOP OF THE YELLOW RANGE AND STABLE. DECLARED AN EMEGENCY. LANDED WI
- [SDR SIMA20130623001](https://openairdocs.org/sdr/SIMA20130623001.md): Roller · damaged · Jun 23, 2013 · N825AE · Emb EMB135KL · Passenger/Crew Doors
  > DURING B-INSPECTION, FOUND THE MAIN CABIN DOOR UPPER AFT FRAME ROLLER OUT OF ROUND AND DIFFICULT TO ROTATE. THE DOOR WAS DIFFICULT TO OPERATE. ACFT REMOVED FROM SERVICE. R & R ROLLER IAW AMM 53-21-02 AND OPS GOOD. ACFT RETURNED TO SERVICE.
- [SDR SIMA20130411017](https://openairdocs.org/sdr/SIMA20130411017.md): Terminal · missing · Apr 11, 2013 · N825AE · Emb EMB135KL · Light System Wiring
  > DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 5 WIRE TERMINALS MISSING ACFT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP NR 5 WIRE TERMINALS ON ACFT SIDE IAW EMB-140 SWPM 20-21-00. THE AIRCRAFT WAS RET
- [SDR SIMA20130411016](https://openairdocs.org/sdr/SIMA20130411016.md): Wire · damaged · Apr 11, 2013 · N825AE · Emb EMB135KL · Light System Wiring
  > DURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY LIGHT STRIP HAS DAMAGED WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 2 EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130411015](https://openairdocs.org/sdr/SIMA20130411015.md): Gusset · corroded · Apr 11, 2013 · N825AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING B INSPECTION FOUND THE LAVATORY CENTER BEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED LAVATORY CENTER BEAM GUSSET, DRILLED AND INSTALLED NEW LAV GUSSET IAW EMB SRM 51-40-02 51-20-03. LEVEL OF CORRSION NOT SPECIFIED. TH
- [SDR SIMA20130411014](https://openairdocs.org/sdr/SIMA20130411014.md): Light · damaged · Apr 11, 2013 · N825AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT EXTRUSIONS (1, 2, 3, 4, 6) DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT EXTRUSIONS (1, 2, 3, 4, 6) IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETUR
- [SDR SIMA20130401002](https://openairdocs.org/sdr/SIMA20130401002.md): Flashlight · intermittent · Apr 1, 2013 · N825AE · Emb EMB135KL · Emergency Equipment
  > DURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT ABOVE FLIGHT ATTENDANT’S SEAT WORKING INTERMITTANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT IAW EMB-140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GO
- [SDR SIMA20130225003](https://openairdocs.org/sdr/SIMA20130225003.md): Light · inoperative · Feb 25, 2013 · N825AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FUSELAGE EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RE
- [SDR SIMA20130114002](https://openairdocs.org/sdr/SIMA20130114002.md): Light · inoperative · Jan 14, 2013 · N825AE · Emb EMB135KL · Emergency Lighting
  > DURING B INSPECTION FOUND THE EMERGENCY LIGHT IN THE COCKPIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. THE OPERATIONAL CHECK WAS GOOD.
- [SDR SIMA20121216005](https://openairdocs.org/sdr/SIMA20121216005.md): Flashlight · inoperative · Dec 16, 2012 · N825AE · Emb EMB135KL · Emergency Equipment
  > ON FLIGHT 4463 THE CREW REPORTED THE COCKPIT FLASHLIGHT WAS INOPERATIVE AND SWAPPED WITH AFT CABIN FLASHLIGHT. THE FLIGHT CREW PLACARD PER MEL 25-53 AUTH # 120852-C MOC #498684. REPLACED AFT CABIN FLASHLIGHT ASSEMBLY IAW EMB MM 33-50-16. THE OPERATIONAL TES
- [SDR SIMA20121208001](https://openairdocs.org/sdr/SIMA20121208001.md): Flashlight · inoperative · Dec 8, 2012 · N825AE · Emb EMB135KL · Emergency Equipment
  > ON FLIGHT 4243 THE CREW REPORTED THE AFT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW EMB-140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20120627002](https://openairdocs.org/sdr/SIMA20120627002.md): Cradle · damaged · Jun 27, 2012 · N825AE · Emb EMB135KL · Emergency Equipment
  > DURING MAINTENANCE INSPECTION FOUND THE COCKPIT FLASHLIGHT CRADLE RETAINING TAB BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT FLASHLIGHT CRADLE IAW/EMB140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETU
- [SDR SIMA20120611008](https://openairdocs.org/sdr/SIMA20120611008.md): Display · failed · Jun 11, 2012 · N825AE · Emb EMB135KL · Central Display
  > FLIGHT 4450 - FIRST OFFICER’S PRIMARY FLIGHT DISPLAY UNIT FAILED, TOTAL DARK AT 65 KTS, RETURNED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S PRIMARY FLIGHT DISPLAY UNIT IAW AMM 34-22-01. OPS CHECKED GOOD. AIRCRAFT RET
- [SDR SIMA20120425010](https://openairdocs.org/sdr/SIMA20120425010.md): Light · inoperative · Apr 25, 2012 · N825AE · Emb EMB135KL · Emergency Lighting
  > DURING B-INSPECTION FOUND THE LEFT FORWARD WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING FORWARD EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURN

Next page: https://openairdocs.org/aircraft/N825AE/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 = 'N825AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N825AE/reports

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