# Service difficulty reports: N810AE

A list on [N810AE](https://openairdocs.org/aircraft/N810AE.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 · 98 reports

- [SDR SIMA2020021231005](https://openairdocs.org/sdr/SIMA2020021231005.md): Light · unknown · Jan 31, 2020 · N810AE · Emb EMB135KL · Emergency Lighting
  > INSIDE MAIN CABIN THE #1 AND #2 EMERGENCY LIGHTING FLOOR PROXIMITY STRIPS DO NOT ILLUMINATE-C/A-PERFORMED OPC OF EMERGENCY LIGHTING SYSTEM IAW EMB 140 AMM 33-50-00, OPC GOOD.
- [SDR SIMA202001164002](https://openairdocs.org/sdr/SIMA202001164002.md): Smoke Warning · false activation · Jan 14, 2020 · N810AE · Emb EMB135KL · Smoke Detection
  > BAGG SMOKE WARNING ON GROUND EICAS MSG ANG BAGG EXTG BUTTON ILLUMINATED-C/A-PERFORMED FIRE DETECTION TEST IAW EMB 140 AMM 26-10-00. ALL MESSAGES CLEARED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE
- [SDR SIMA201910287002](https://openairdocs.org/sdr/SIMA201910287002.md): Fan · failed · Oct 27, 2019 · N810AE · Emb EMB135KL · Air Distribution Fan
  > ELECTRICAL SMELL IN FLIGHT DECK "TRANSFERRED TO NRWC 810-DFW-02773"-C/A-REMOVED AND REPLACED # 2 FWD ELECK COMPT COOLING FAN IAW AMM 21-26-02. OPCK GOOD. PERFORMED FIM TASK 21-20-00-810-801-A, TO COMPLETION. NO SMELL AT THIS TIME.
- [SDR SIMA2019100193003](https://openairdocs.org/sdr/SIMA2019100193003.md): Precooler · failed · Sep 30, 2019 · N810AE · Emb EMB135KL · Pneumatic Distribution System
  > BLEED 2 LEAK LEAK AFTER TAKEOFF AT TAKEOFF POWER @ 500' AGL. PERFORMED BLLED AIR SYSTEM LEAK CHECK IAW WORK CARD 36-700-06, AND REPLACED ORING AT RH BLEED JOINTS 6, 16, 20, 22 IAW AMM 36-11-10, REPLACED SEAL FOR RH FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06
- [SDR SIMA2019100193002](https://openairdocs.org/sdr/SIMA2019100193002.md): O-Ring · leaking · Sep 30, 2019 · N810AE · Emb EMB135KL · Pneumatic Distribution System
  > BLD 2 LEAK IMMEDIATLY AFTER TAKE OFF. REMOVED AND REPLACED THE O-RINGS AT JOINT 4 AND JOIMT 20 IAW AMM 36-11-00. PERFORMED A LEAK CHECK AND FOUND SATISFACTORY IAW AMM 36-10-00.
- [SDR SIMA20190929002](https://openairdocs.org/sdr/SIMA20190929002.md): O-Ring · damaged · Sep 29, 2019 · N810AE · Emb EMB135KL · Pneumatic Distribution System
  > BLD 2 LEAK IMMEDIATELY AFTER TAKEOFF. WAS NOT AN OVERWEIGHT LANDING.-C/A- REMOVED AND REPLACED O-RING AT JOINT NUMBER 26 AND 4 IAW AMM 36-11-10. PERFORMED LEAK CHECK AND FOUND SATISFACTORY IAW AMM 36-10-00. PERFORMED OPERATIONAL CHECK ON # 2 BLEED SYS. IAW AMM
- [SDR SIMA20190707001](https://openairdocs.org/sdr/SIMA20190707001.md): O-Ring · damaged · Jul 7, 2019 · N810AE · Emb EMB135KL · Pneumatic Distribution System
  > SUPPLEMENTAL BLEED 2 LEAK WARNING. C/A-FOUND LEAKING CONNECTION AT BLEED LINE #18 JOINT. REMOVED AND REPLACED #2 SYSTEM BLEED LINE O-RINGS AT #18 CONNECTION IAW AMM 36-11-10 OPS CECK GOOD NO LEAKS NOTED.
- [SDR SIMA201906254003](https://openairdocs.org/sdr/SIMA201906254003.md): O-Ring · leaking · Jun 24, 2019 · N810AE · Emb EMB135KL · Pneumatic Distribution System
  > BLEED 2 LEAK DURING CLIMBOUT. AFTER INSPECTION OF DUCT LINES, FOUND 12 AND 22 TO BE DAMAGED AND LEAKING IAW AMM 36-11-09. R & R THE DUCTS 12 AND 22 O-RINGS IAW AMM 36-11-09. PERFORMED AN OPS CHECK OF BLEED AIR SYSTEM IAW AMM 36-00-00-700-803-A/500. OPS CHECK
- [SDR SIMA2019062016002](https://openairdocs.org/sdr/SIMA2019062016002.md): Gps · malfunctioned · Jun 16, 2019 · N810AE · Emb EMB135KL · Global Positioning System
  > UNRELIABLE NAV INFORMATION IN FLIGHT BETWEEN FO X CA MFD FMS AND GPS. RESET AND PERFORMED OPC CHECK OF FMS/GPS IAW AMM 34-62-00. OPC CHECK GOOD. NO FAULTS NOTED AT THIS TIME. FOUND TO BE TRANSITORY CONDITION. A/C OK FOR SERVICE.
- [SDR SIMA201906176001](https://openairdocs.org/sdr/SIMA201906176001.md): Fms · malfunctioned · Jun 16, 2019 · N810AE · Emb EMB135KL · Omega Navigation System
  > UNRELIABLE NAV INFORMATION IN FLIGHT BETWEEN FO X CA MFD FMS AND GPS-C/A-RESET AND PERFORMED OPC CHECK OF FMS/GPS IAW AMM 34-62-00. OPC CHECK GOOD. NO FAULTS NOTED AT THIS TIME. FOUND TO BE TRANSITORY CONDITION. A/C OK FOR SERVICE.
- [SDR SIMA201906132006](https://openairdocs.org/sdr/SIMA201906132006.md): Light · inoperative · Jun 12, 2019 · N810AE · Emb EMB135KL · Emergency Lighting
  > EMERGENCY LIGHT STRIP INOPERATIVE AT ROWS 7-8. REMOVED AND REPLACED PROXIMITY LIGHT STRIP ON ROW 7-8 IAW AMM 33-50-122. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR SIMA201906132005](https://openairdocs.org/sdr/SIMA201906132005.md): Fan · failed · Jun 12, 2019 · N810AE · Emb EMB135KL · Air Distribution Fan
  > ELECTRICAL ODOR AND VISABLE HAZE IN CABIN REPORTED BY FA AND PAX. DIMINISHED ONCE RECIRC AND PACKS OFF.-C/A-PERFORMED OPERATIONAL CHECK OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW AMM 21-20-00. FOUND ODOR TO BE COMING FROM RH CABIN RECIRC FAN. REMOVED AND
- [SDR SIMA20190514001](https://openairdocs.org/sdr/SIMA20190514001.md): Flashlight · inoperative · May 14, 2019 · N810AE · Emb EMB135KL · Emergency Equipment
  > AFT CABIN CREW FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT CABIN CREW FLASHLIGHT IAW AMM 33-50-16 STEPS 2.I.(1) AND 3.H.(4). OPC GOOD.
- [SDR SIMA20190314001](https://openairdocs.org/sdr/SIMA20190314001.md): Amplifier · damaged · Mar 14, 2019 · N810AE · Emb EMB135KL · Interphone/Passenger Announcement (PA) System
  > CABIN AND CABIN EMERG BUTTON LIT UP IN CRUISE FLIGHT WAS NOT ABLE TO MAKE PA'S NO CHIMES/SOUNDS WITH NO SMOKING AND SEAT BELT SIGN SWITCH BEING TOGGLED. C/A-REMOVED AND CLEANED CONNECTORS ON BOTH FWRD AND AFT F/A HANDSET IAW AMM 23-31-03. OPS CHECK FAILED. FOU
- [SDR SIMA20190205005](https://openairdocs.org/sdr/SIMA20190205005.md): Proximity Sensor · failed · Feb 5, 2019 · N810AE · Emb EMB135KL · Drag Control System
  > DECLARED EMERGENCY AFTER SPOILER FAIL MESSAGE IN FLIGHT AT FL360 WENT AWAY AND BACK 5 TIMES UNTIL EMERGENCY XLIST COMPLETE AND CBS PULLED. OPEN INSCRIPTION ON EICAS AS WELL WITH EICAS MESSAGE NO ADVERSE EFFECT ON AIRCRAFT SPEED OR HANDLING NOTED. FOUND CORRODE
- [SDR SIMA20181023001](https://openairdocs.org/sdr/SIMA20181023001.md): Light · inoperative · Oct 23, 2018 · N810AE · Emb EMB135KL · Emergency Lighting
  > RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT AFT OVERWING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-07. OPS CHECK GOOD.
- [SDR SIMA2018091008001](https://openairdocs.org/sdr/SIMA2018091008001.md): Charger · failed · Sep 8, 2018 · N810AE · Emb EMB135KL · Emergency Lighting
  > CABIN FLOOR EMER LIGHT 1,2 & 3 INOP. R&R NR 2 BATT PACK AND CHARGER IAW AMM 33-50-04. OP CK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 84695.
- [SDR SIMA201809043002](https://openairdocs.org/sdr/SIMA201809043002.md): Light · inoperative · Sep 3, 2018 · N810AE · Emb EMB135KL · Emergency Lighting
  > LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD.
- [SDR SIMA2018082019005](https://openairdocs.org/sdr/SIMA2018082019005.md): Light · inoperative · Aug 19, 2018 · N810AE · Emb EMB135KL · Emergency Lighting
  > SECOND EMERGENCY PROXIMITY STRIP FROM MAIN ENTRANCE TO SEAT 3A INOPERATIVE. REMOVED AND REPLACED EMERGERCY LIGHT IAW AMM 33-57-12. OPS CHECKED GOOD.
- [SDR SIMA2018080131001](https://openairdocs.org/sdr/SIMA2018080131001.md): Antenna · failed · Jul 31, 2018 · N810AE · Emb EMB135KL · VHF Communications System
  > LIGHTNING STRIKE AT 16,000 FEET IN CRUISE CLEAN CONFIGURATION ARCED ACROSS NOSE OF AIRPLANE LOST COMMS 1+2 OR THE REGAINED COMM 1. COMM 2 IS RECEIVE ONLY OR WONT TRANSMIT. ALSO ONLY ONE CRACKLES WHEN PTT IS PRESSED. NR 1 VHF COMM OPC GOOD IAW AMM 23-12-00. R&R
- [SDR SIMA201807132003](https://openairdocs.org/sdr/SIMA201807132003.md): Unknown · malfunctioned · Jul 12, 2018 · N810AE · Emb EMB135KL · Fuel Indicating System
  > FUEL QUANTITY INDICATION ON BOTH ENGINES AND TOTAL FUEL INDICATED INCREASED AND DECREASED UP TO 900 POUNDS. THE FUEL IMBALANCE MESSAGE APPEARED AND DISAPPEARED MULTIPLE TIMES DURING FLIGHT. PERFORMED FUEL BALANCE (WING TRANSFER) IAW AMM 28-10-00. NO FURTHER IM
- [SDR SIMA201806186001](https://openairdocs.org/sdr/SIMA201806186001.md): Switch · out of adjust · Jun 16, 2018 · N810AE · Emb EMB135KL · Door Warning System
  > ABORTED TAKEOFF BELOW V1, DUE TO A CARGO DOOR OPEN EICAS MESSAGE. ADJUSTED THE CARGO DOOR WARNING SWITCHES IAW AMM 52-76-01. OPS CHECKED GOOD.
- [SDR SIMA20180301002](https://openairdocs.org/sdr/SIMA20180301002.md): Wire · broken · Mar 1, 2018 · N810AE · Emb EMB135KL · Light System Wiring
  > FLOOR EMERGENCY LIGHT STRIP ASSEMBLY AT 261BF HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180227003](https://openairdocs.org/sdr/SIMA20180227003.md): Skin · damaged · Feb 27, 2018 · N810AE · Emb EMB135KL · Passenger/Crew Doors
  > DOOR EXTERNAL SKIN HAS 1 DENT APPROX. 2 INCHES, FRONT FWD EDGE AND 6 INCHES FROM UPPER EDGE. SKIN IS BENT AND KNIFE EDGED APPROXIMATELY 8 INCHES FROM UPPER EDGE. REPAIRED THE DOOR SKIN IAW ERS-EM-52MR-857.
- [SDR SIMA20180219004](https://openairdocs.org/sdr/SIMA20180219004.md): Door Sill · corroded · Feb 19, 2018 · N810AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20180219003](https://openairdocs.org/sdr/SIMA20180219003.md): Door Sill · corroded · Feb 19, 2018 · N810AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20180218005](https://openairdocs.org/sdr/SIMA20180218005.md): Wire · broken · Feb 18, 2018 · N810AE · Emb EMB135KL · Light System Wiring
  > LEFT NR 3 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180218006](https://openairdocs.org/sdr/SIMA20180218006.md): Frame · cracked · Feb 18, 2018 · N810AE · Emb EMB135KL · Fuselage Main, Frame
  > RIGHT FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20180218007](https://openairdocs.org/sdr/SIMA20180218007.md): Frame · cracked · Feb 18, 2018 · N810AE · Emb EMB135KL · Fuselage Main, Frame
  > LEFT FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAMEIAW SRM 51-40-02.
- [SDR SIMA20180218004](https://openairdocs.org/sdr/SIMA20180218004.md): Wire · broken · Feb 18, 2018 · N810AE · Emb EMB135KL · Light System Wiring
  > LEFT NR 7 EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180217015](https://openairdocs.org/sdr/SIMA20180217015.md): Web · chafed · Feb 17, 2018 · N810AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > LEFT OVERWING EMERGENCY EXIT INTERNAL WEB CHAFED ABOVE WINDOW CUTOUT. REPAIRED IAW ERS-EM-52MR-854
- [SDR SIMA20180214004](https://openairdocs.org/sdr/SIMA20180214004.md): Frame · cracked · Feb 14, 2018 · N810AE · Emb EMB135KL · Fuselage Main, Frame
  > FRAME 23 IS CRACKED BETWEEN STRINGERS 16R - 15R. REPAIRED THE FRAME IAW EM-53MR-1808.
- [SDR SIMA20180124006](https://openairdocs.org/sdr/SIMA20180124006.md): Door Frame · corroded · Jan 24, 2018 · N810AE · Emb EMB135KL · Fuselage Main, Structure
  > PASSENGER DOOR LOWER FRAME CORRODED AT 2 NUTPLATE HOLES. REPAIRED DOOR FRAME IAW ERS-EM-52MR-858.
- [SDR SIMA20180124005](https://openairdocs.org/sdr/SIMA20180124005.md): Floor Support · corroded · Jan 24, 2018 · N810AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > LEFT CENTER OMEGA BEAM CORRODED UNDER THE CARBON CROSS MEMBER AT FRAME 44. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3147.
- [SDR SIMA20140612002](https://openairdocs.org/sdr/SIMA20140612002.md): Flashlight · dim · Jun 12, 2014 · N810AE · Emb EMB135KL · Emergency Equipment
  > CAPTAIN`S SIDE FLASHLIGHT VERY DIM. R & R FLASHLIGHT IAW ETN-EM-33-034, OPS CHECKED GOOD.
- [SDR SIMA20140423003](https://openairdocs.org/sdr/SIMA20140423003.md): Wire Harness · damaged · Apr 23, 2014 · N810AE · Emb EMB135KL · Light System Wiring
  > FLIGHT ATTENDANT REPORTS STRONG ODOR OF BURNING SMELL WHEN SHE TURNED LIGHTS ON AFTER LANDING. SMELL IS IN FWD PART OF CABIN. TRANSFERRED TO NRWC 810-ORD-01663. FOUND FWD SOCKET ON CEILING LIGHT HARNESS ABOVE SEAT 1A TO BE BURNT. R & R ELEC HARNESS IAW A
- [SDR SIMA20140331002](https://openairdocs.org/sdr/SIMA20140331002.md): Wire · failed · Mar 31, 2014 · N810AE · Emb EMB135KL · Equipment/Furnishings Wiring
  > FLIGHT ATTENDANT REPORTED THAT AFTER LANDING GEAR EXTENSION, A MEDIUM STRENGTH ODOR OF BURNING RUBBER LASTING 1 TO 3 MINUTES IN THE FWD GALLEY AREA & FWD ENTRY AREA. FOUND & REPAIRED DAMAGED WIRING AT LT HOT JUG RECEPTACLE. IAW NRWC 810-DFW-1600 TESTED & FOU
- [SDR SIMA20140222002](https://openairdocs.org/sdr/SIMA20140222002.md): Charger · failed · Feb 22, 2014 · N810AE · Emb EMB135KL · Emergency Lighting
  > PASSENGER DOOR & OVERHEAD ENTRY EMERGENCY LIGHT BULBS INOPERATIVE, 0 VOLTS. R & R NR 1 EMERGENCY BATTERY CHARGER & OPERATIONS CHECKED GOOD IAW AMM 33-50-04.
- [SDR SIMA20140120003](https://openairdocs.org/sdr/SIMA20140120003.md): Display · failed · Jan 20, 2014 · N810AE · Emb EMB135KL · Central Display
  > AT INITIAL POWER UP CAPTAIN'S MFD DID NOT COME ON ASSOCIATED WITH A STRONG ODOR. MFD 1 CB FOUND POPPED. R & R NR 1 MFD IAW AMM 31-41-02, OPERATIONS CHECKED GOOD.
- [SDR SIMA20130710003](https://openairdocs.org/sdr/SIMA20130710003.md): Inverter · inoperative · Jul 10, 2013 · N810AE · Emb EMB135KL · Emergency Lighting
  > DURING B INSPECTION, FOUND FORWARD LEFT EMERGENCY LIGHTING AND SERVICE DOOR LOWER EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R NR 2 EMERGENCY LIGHT BALLAST INVERTER IAW AMM 33-50-11. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130710002](https://openairdocs.org/sdr/SIMA20130710002.md): Flashlight · inoperative · Jul 10, 2013 · N810AE · Emb EMB135KL · Emergency Equipment
  > DURING B INSPECTION, FOUND THE FWD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FORWARD CABIN EMERGENCY FLASHLIGHT IAW WC 33-700-20. THE ACFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130505004](https://openairdocs.org/sdr/SIMA20130505004.md): Wire · broken · May 5, 2013 · N810AE · Emb EMB135KL · Light System Wiring
  > DURING B INSPECTION FOUND THE AFT LEFT EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING STRIP IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERV
- [SDR SIMA20130220004](https://openairdocs.org/sdr/SIMA20130220004.md): Light · inoperative · Feb 20, 2013 · N810AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT W
- [SDR SIMA20130211005](https://openairdocs.org/sdr/SIMA20130211005.md): Connector · unserviceable · Feb 11, 2013 · N810AE · Emb EMB135KL · Landing Gear System Wiring
  > ON FLIGHT 3866 THE CREW REPORTED THAT DURING CRUISE FLIGHT LEVEL 360 A BRAKE LIGHT CAME ON AND REMAINED ON TO THE GATE. THE CREW DECLARED AN EMERGENCY. THE FLIGHT AND LANDING WERE NORMAL. NO MALFUNCTION NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVE
- [SDR SIMA20130127002](https://openairdocs.org/sdr/SIMA20130127002.md): Unknown · fumes · Jan 27, 2013 · N810AE · Emb EMB135KL · Air Distribution System
  > DURING MAINTENANCE INSPECTION WHEN APU WAS STARTED FUEL FUMES WERE NOTICED IN THE COCKPIT WITH THE ENGINE RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. RAN BOTH ENGINES IAW ERJ GHC AND OPS CHECKED THE APU IAW AMM 49-02-00. OPS CHECK GOOD. NO FUEL SMELL N
- [SDR SIMA20121129003](https://openairdocs.org/sdr/SIMA20121129003.md): Angle · cracked · Nov 29, 2012 · N810AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE INSPECTION FOUND THE RIGHT VERTICAL STABILIZER TO FUSELAGE ANGLE AT FRAME 76 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1281, PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121129002](https://openairdocs.org/sdr/SIMA20121129002.md): Fitting · damaged · Nov 29, 2012 · N810AE · Emb EMB135KL · Ailerons
  > DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING OUTBOARD LUG SCORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121128012](https://openairdocs.org/sdr/SIMA20121128012.md): Floor Support · dented · Nov 28, 2012 · N810AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK INSPECTION FOUND THE RIGHT OMEGA BEAM BETWEEN FRAME 71 AND 72 HAS A LARGE DENT ON UPPER SURFACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO RIGHT OMEGA BEAM BETWEEN FRAME 71-72. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121205001](https://openairdocs.org/sdr/SIMA20121205001.md): Skin · cracked · Nov 28, 2012 · N810AE · Emb EMB135KL · Electrical/Electronic Compartment Doors
  > DURING HEAVY CHECK INSPECTION FOUND REAR ELECTRONICS COMPARTMENT DOOR 272DR HAS 2 EACH CRACKS UNDER THE ATTACHMENT HOOK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AFT AVIONICS DOOR IAW EO EM-52MR-334. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121128009](https://openairdocs.org/sdr/SIMA20121128009.md): Skin · cracked · Nov 28, 2012 · N810AE · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE INSPECTION FOUND THE RIGHT FUSELAGE SKIN HAS A CRACK 3/8" LONG AT FRAME 75 AND STRINGER 2R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT FUSELAGE SKIN IAW EO EM-53MR-2039. THE AIRCRAFT WAS RETURNED TO SERVICE.

Next page: https://openairdocs.org/aircraft/N810AE/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 = 'N810AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N810AE/reports

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