# Service difficulty reports: N811AE, cancelled Nov 20, 2019

A list on [N811AE, cancelled Nov 20, 2019](https://openairdocs.org/deregistered/N811AE-2019-11-20.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 · 70 reports

- [SDR SIMA20140613004](https://openairdocs.org/sdr/SIMA20140613004.md): Indication Sys · malfunctioned · Jun 13, 2014 · N811AE · Emb EMB135KL · Fuel Indicating System
  > AFTER TAKEOFF JET FUEL IMBALANCE MSG APPEARED ON EICAS. NR 2 FUEL QTY INDICATOR 900 LBS HIGHER THAN LT SIDE BUT PREVIOUSLY DEFERRED BY MX. LT FUEL INDICATION CO0NSUMING RAPIDLY. PERFORMED ENG RUNS FOR ABOUT 30 MINUTES. LT FUEL TANK QTY INDICATION SEEMED TO
- [SDR SIMA20140610003](https://openairdocs.org/sdr/SIMA20140610003.md): Metering Unit · leaking · Jun 10, 2014 · N811AE · Emb EMB135KL · Fuel Controlling System
  > FUEL LEAK FROM E1 AGAIN FROM DRAIN. R & R E1 FPMU IAW RRMM CHAPTER 73-21-10. PERFORMED ENG RUNS. OPERATIONS CHECKED GOOD, NO LEAKS FOUND.
- [SDR SIMA20140108001](https://openairdocs.org/sdr/SIMA20140108001.md): Control Lever · failed · Jan 8, 2014 · N811AE · Emb EMB135KL · Landing Gear Selector
  > ON APPROACH LG GEAR HANDLE WOULD NOT MOVE FROM UP POSITION. CONDUCTED EMERGENCY GEAR EXTENSION IAW AOM 1, LANDED WITHOUT INCIDENT. LG HANDLE DISAGREE WARNING ON EICAS & 3 DOWN RED INDICATION ON GEAR. R & R LG CONTROL LEVER IAW AMM 32-32-02. PERFORMED OPERA
- [SDR SIMA20131222004](https://openairdocs.org/sdr/SIMA20131222004.md): Battery · discharged · Dec 22, 2013 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION ON FLIGHT 3512 FOUND NR 3 FWD WING TO FUSELAGE EMERGENCY LIGHT INOPERABLE. R & R THE NR 1 POWER SUPPLY & BATTERY IAW AMM 33-50-04 OPERATIONS CHECKED GOOD RESTORE MEL.
- [SDR SIMA20131030010](https://openairdocs.org/sdr/SIMA20131030010.md): Door · lack of lube · Oct 30, 2013 · N811AE · Emb EMB135KL · Passenger/Crew Doors
  > F/A ADVISED THAT THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. LUBRICATED MAIN CABIN DOOR IAW AMM 52-18-00. OPS CHECKED GOOD.
- [SDR SIMA20130715008](https://openairdocs.org/sdr/SIMA20130715008.md): Handle · out of adjust · Jul 15, 2013 · N811AE · Emb EMB135KL · Passenger/Crew Doors
  > DURING B INSPECTION, FOUND MAIN PASSENGER DOOR GETTING JAMMED AND IT WOULD NOT OPEN. ACFT REMOVED FROM SERVICE. REPOSITIONED INSIDE MAIN DOOR HANDLE IAW AE MX WC 52-600-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
- [SDR SIMA20130715001](https://openairdocs.org/sdr/SIMA20130715001.md): Flashlight · inoperative · Jul 15, 2013 · N811AE · Emb EMB135KL · Emergency Equipment
  > DURING MX INSPECTION, FOUND THE F/O EMERGENCY FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. OPS CHECKED GOOD. NO DEFECTS NOTED. THE ACFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130714001](https://openairdocs.org/sdr/SIMA20130714001.md): Roller · lack of lube · Jul 14, 2013 · N811AE · Emb EMB135KL · Passenger/Crew Doors
  > F/A REPORTED MAIN DOOR WAS HARD TO OPERATE. ACFT REMOVED FROM SERVICE. CLEANED AND LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. PERFORMED A TEST OF THE MAIN DOOR INTERNAL ACTUATING HANDLE IAW AMM 52-18-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
- [SDR SIMA20130710008](https://openairdocs.org/sdr/SIMA20130710008.md): Unknown · vibration · Jul 10, 2013 · N811AE · Emb EMB135KL · Fuselage Structure (General)
  > DURING CRUISE AT 24000 FT, NOTICED A LOUD NOISE ACCOMPANIED BY A CONTINOUS VIBRATION. DECELLERATED FROM 300 KTS TO 200KTS (APPROX). NOISE DECREASED BUT DID NOT GO AWAY. SUSPECT NOSE GEAR DOORS DEPLOYED PREMATURELY AS NOISE WAS MORE PRONOUNCED IN NOSE OF ACFT
- [SDR SIMA20130529001](https://openairdocs.org/sdr/SIMA20130529001.md): Adc · failed · May 29, 2013 · N811AE · Emb EMB135KL · Air Data Computer
  > AT 36000 FT, SPS ADVANCED CAUTION ON EICAS, CA`S AIRSPEED INDICATOR STARTED SLOWING DOWN AND DIFFERENT FROM F/O BY 30 KTS AND WENT DOWN FROM THERE, ALTITUDE INDICATIOR OFF BY 200 FT, RECEIVED LOWER ALL PROBLEMS RETURNED NORMAL. F/O SMELLED AN ELECTRICAL BU
- [SDR SIMA20130427001](https://openairdocs.org/sdr/SIMA20130427001.md): Mechanism · lack of lube · Apr 29, 2013 · N811AE · Emb EMB135KL · Passenger/Crew Doors
  > ON FLIGHT 3341 FOUND MAIN DOOR DIFFICULT TO CLOSE SOMETIMES LEVES GAP AT TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W PERFORMED LUBRICATION OF THE STANDARD MAIN-DOOR ACTUATING AND LOCKING MECHANISM IAW EMB AMM 52-11-00. OPS CHECK GOOD. THE AIRCRAFT WAS
- [SDR SIMA20121117016](https://openairdocs.org/sdr/SIMA20121117016.md): Seat Track · corroded · Nov 17, 2012 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK, FOUND RT OTBD SEAT TRACK CORRODED AT FR-50. REPAIRED RT OTBD SEAT TRACK IAW EO-53MR-2042.
- [SDR SIMA20121117010](https://openairdocs.org/sdr/SIMA20121117010.md): Gusset · corroded · Nov 17, 2012 · N811AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING B INSPECTION FOUND THE RIGHT LAV FLOORBEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT LAV FLOORBEAM GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121117009](https://openairdocs.org/sdr/SIMA20121117009.md): Gusset · corroded · Nov 17, 2012 · N811AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING B INSPECTION FOUND THE LAV CENTER FLOORBEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAV CENTER FLOORBEAM GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121117008](https://openairdocs.org/sdr/SIMA20121117008.md): Connector · missing · Nov 17, 2012 · N811AE · Emb EMB135KL · Light System Wiring
  > DURING B INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIP NR 5 IS MISSING ONE CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FLOOR EMERGENCY LIGHT STRIP NR 5 SPLICE (SP9115) CONNECTOR IAW EMB 140 SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVI
- [SDR SIMA20121117007](https://openairdocs.org/sdr/SIMA20121117007.md): Light · damaged · Nov 17, 2012 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING B INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIPS NR 1, 6 AND 7 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIPS NR 1, 6 AND 7 IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121117006](https://openairdocs.org/sdr/SIMA20121117006.md): Crossbeam · corroded · Nov 17, 2012 · N811AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING B INSPECTION FOUND THE GALLEY CROSSBEAM AT FRAME 20 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE CROSSBEAM AT FRAME 20 IAW AEA ETN EM-53-139R2. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20120917004](https://openairdocs.org/sdr/SIMA20120917004.md): Light · inoperative · Sep 17, 2012 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXTERIOR EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK
- [SDR SIMA20120809009](https://openairdocs.org/sdr/SIMA20120809009.md): Fan · failed · Aug 13, 2012 · N811AE · Emb EMB135KL · Air Distribution System
  > FLIGHT 9806, CREW REPORTED BLEED 1 OVERTEMP WARNING ALTERNATING WITH BLD 2 LOW TEMP CAUTION MESSAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW AMM 36-11-03. OPS CHECK GOOD IAW AMM 36-00-00. THE AIRCRAFT RETURN TO SE
- [SDR SIMA20120809003](https://openairdocs.org/sdr/SIMA20120809003.md): Valve · failed · Aug 9, 2012 · N811AE · Emb EMB135KL · Pneumatic Distribution System
  > FLIGHT 9806, CREW REPORTED THAT WHILE ON APPROACH, RECEIVED AN INTERMITTENT BLEED 2 OVERTEMP WARNING MESSAGE ON EICAS. FOLLOWED AOM VOL 1 PROCEDURES. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 FAN
- [SDR SIMA20120709003](https://openairdocs.org/sdr/SIMA20120709003.md): Ballast · burned · Jul 9, 2012 · N811AE · Emb EMB135KL · Passenger Compartment Lighting
  > FLIGHT 3355, CREW REPORTED THEY NOTICED AN ODOR NEAR THE COCKPIT AND GALLEY. THE FLIGHT ATTENDANT TURNED OFF LIGHTS AND COFFEEMAKER AND THE ODOR DISAPPEARED. AIRCRAFT REMOVED FROM SERVICE. FOUND SIDEWALL BALLAST ON ROW 18BC SMELLING BURNED. REMOVED AND R
- [SDR SIMA20120403002](https://openairdocs.org/sdr/SIMA20120403002.md): Lamp · inoperative · Apr 3, 2012 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY EXIT CEILING LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY EXIT CEILING IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA20120318008](https://openairdocs.org/sdr/SIMA20120318008.md): Light · inoperative · Mar 18, 2012 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERHEAD EMERGENCY LIGHT IAW AMM TASK 33-50-07-000-01-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS
- [SDR SIMA201132103](https://openairdocs.org/sdr/SIMA201132103.md): Velocity Sensor · inoperative · Nov 16, 2011 · N811AE · Emb EMB135KL · Trailing Flap Position Indicating System
  > ON FLIGHT 4098 ON DESCENT THE CREW REPORTED THEY RECEIVED AN EICAS MESSAGE FLAP FAIL WHEN FLAPS SELECTED TO 9 DEGREES. NO FLAP MOVEMENT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED
- [SDR SIMA201132201](https://openairdocs.org/sdr/SIMA201132201.md): Warning System · malfunctioned · Nov 15, 2011 · N811AE · Emb EMB135KL · Trailing Edge Flap Control System
  > ON FLIGHT 4049 THE CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE DISPLAY DURING DESCENT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AIRCRAFT WAS REMOVED FROM SERIVCE. RESET FLAP SYSTEM IAW FIM 27-51-00-810-804-A. NO PARTS REMOVED OR REPLACED.
- [SDR SIMA2011299019](https://openairdocs.org/sdr/SIMA2011299019.md): Seal · missing · Oct 24, 2011 · N811AE · Emb EMB135KL · Fire Bottle, Portable
  > DURING MAINTENANCE INSPECTION FOUND THE AFT FIRE EXTINGUISHER SEAL IS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED AFT FIRE EXTINGUISHER SEAL AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201125106](https://openairdocs.org/sdr/SIMA201125106.md): Uplock · inoperative · Sep 2, 2011 · N811AE · Emb EMB135KL · Landing Gear Retraction/Extension System
  > ON FLIGHT 3363 DURING CLIMBOUT THE CREW REPORTED, HAD A LANDING GEAR LEVER DISAGREE MESSAGE. THE NOSE GEAR INDICATION WAS RED. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM
- [SDR SIMA201122007](https://openairdocs.org/sdr/SIMA201122007.md): Duct · failed · Aug 6, 2011 · N811AE · Emb EMB135KL · Cabin Cooling System
  > CREW REPORTED PACK 1 VLV FAIL DIVERTED TO LIT FOR A FUEL STOP ISSUED MEL 2129. FOUND DUCT BLOWN OFF THAT CONNECTS TO HEAT EXCHANGER. REMOVED AND REPLACED DUCT AND CLAMPS IAW EMB140AMM 21-51-02. OPS CHECK GOOD IAW EMB140 AMM 21-51-00.
- [SDR SIMA201111903](https://openairdocs.org/sdr/SIMA201111903.md): Sign · inoperative · Apr 27, 2011 · N811AE · Emb EMB135KL · Emergency Lighting
  > ON FLIGHT 2712 DURING THE PRE FLIGHT INSPECTION FOUND THE AFT EMERGENCY EXIT SIGN ON THE CENTER CEILING PANEL FOR THE OVERWING DOORS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 DC/AC INVERTER AND SIGN ASSEMBLY EMERGENCY L
- [SDR SIMA201103106A](https://openairdocs.org/sdr/SIMA201103106A.md): Charger · inoperative · Jan 31, 2011 · N811AE · Emb EMB135KL · Emergency Lighting
  > (REQUEST TO MAKE SEPARATE SDR’S) DURING MAINTENANCE BASE CHECK FOUND THE LEFT WING (EXTERNAL) EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201103106](https://openairdocs.org/sdr/SIMA201103106.md): Battery · discharged · Jan 31, 2011 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE BASE CHECK FOUND THE LEFT WING (EXTERNAL) EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 EMERGENCY SYSTEM POWER SUPPLY BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE. (REQUEST TO MAKE SEPA
- [SDR SIMA201100301](https://openairdocs.org/sdr/SIMA201100301.md): Receptacle · leaking · Dec 30, 2010 · N811AE · Emb EMB135KL · Fuel Storage
  > ON FLIGHT 2750 THE CREW REPORTED THAT AFTER THE ENGINE START/SHUT DOWN OF APU, FUEL ODOR WAS DETECTED IN THE COCKPIT. THE ODOR THEN DISAPATED. EN ROUTE A HINT OF FUEL ODOR RETURNED. THE FLIGHT ATTENDANT REPORTED NO ODOR IN CABIN. THE AIRCRAFT WAS REMOVED F
- [SDR SIMA201030802](https://openairdocs.org/sdr/SIMA201030802.md): Sign · inoperative · Nov 4, 2010 · N811AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY ROW CEILING AFT LIGHT EXIT LOCATING SIGN TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY ROW CEILING LIGHT EXIT LOCATION SIGN. THE AIRCRAFT WAS RETURNED TO SERVICE
- [SDR SIMA201004611](https://openairdocs.org/sdr/SIMA201004611.md): Wire Harness · failed · Feb 11, 2010 · N811AE · Emb EMB135KL · Landing Gear System Wiring
  > ON FLIGHT 3069 DURING THE TAKEOFF ROLL AT 70 KNOTS THE CREW REPORTED THAT THE AIRCRAFT PULLED HARD TO THE RIGHT. THE CREW ELECTED TO ABORT THE TAKEOFF. THE CONFIGURATION WARNING CAME ON THEN WENT OFF. AFTER CLEARING THE RUNWAY THE RUDDER SYSTEM 1 FAIL MESSA
- [SDR SIMA200922604](https://openairdocs.org/sdr/SIMA200922604.md): Engine · malfunctioned · Aug 12, 2009 · N811AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > ON FLIGHT 4373 THE CREW NOTICED A STRONG BURNING SMELL AFTER TAKEOFF. THE ODOR WAS NOTICEABLE THROUGHOUT THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO THE FIELD AS AN UNSCHEDULED LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE 1 IAW E
- [SDR SIMA200915401](https://openairdocs.org/sdr/SIMA200915401.md): Switch · out of rig · Jun 2, 2009 · N811AE · Emb EMB135KL · Landing Gear Retraction/Extension System
  > ON FLIGHT 4823, CREW REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTURE. AIRCRAFT REMOVED FROM SERVICE. RIGGED GEAR ELECTRICAL OVERRIDE SWITCH. PERFORMED MULTIPLE GEAR EXTENSION AND RETRACTIONS IAW EMB AMM 32-32-00. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED.
- [SDR SIMA200915404](https://openairdocs.org/sdr/SIMA200915404.md): Manifold · failed · Jun 1, 2009 · N811AE · Emb EMB135KL · Hydraulic System, Main
  > ON FLIGHT 4596, CREW REPORTED HYDRAULIC SYSTEM 1 FAIL ON CLIMB. CREW DECLARED A EMERGENCY AND RETURNED TO BLOCK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 MANIFOLD ASSEMBLY PER EMB 140 AMM 27-12-02 LEAK AND OPERATIONAL CHECK
- [SDR SIMA200908201](https://openairdocs.org/sdr/SIMA200908201.md): Sign · failed · Mar 18, 2009 · N811AE · Emb EMB135KL · Emergency Lighting
  > ON FLIGHT 4609, CREW REPORTED ROW 11 EMERGENCY EXIT LIGHT AFT SIDE DID NOT COME ON DURING EMERGENCY LIGHT TEST. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EXIT EMERGENCY LOCATION SIGN IAW EMB 140 AMM 33-50-15. OPERATIONAL CHECKED GOOD. AIRCRAFT RE
- [SDR SIMA200727408](https://openairdocs.org/sdr/SIMA200727408.md): Electronic Unit · malfunctioned · Sep 29, 2007 · N811AE · Emb EMB135KL · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, CREW TRIED TO RETRACT THE GEAR AND NOTHING HAPPENED. NO SINK RATE WAS BELOW 200 FT/MIN. INSPECTED LANDING GEAR AND FOUND NLG DOWN LOCK PROX SWITCHES OUT OF ADJUSTMENT. ADJUSTED NLG DOWN LOCK SWITCHES IAW EMB MM 32-63-05-700-804-A. ALSO REMOVE
- [SDR SIMA200720427](https://openairdocs.org/sdr/SIMA200720427.md): Sill · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > FORWARD SERVICE DOOR SILL CORRODED BETWEEN FRAMES 18 AND 20. REMOVED AND REPLACED DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200720426](https://openairdocs.org/sdr/SIMA200720426.md): Floor Support · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM CORRODED BETWEEN FRAMES 57 AND 59. REPAIRED DAMAGED AREA IAW IC2007-145/03984. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200720425](https://openairdocs.org/sdr/SIMA200720425.md): Doubler · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage Main, Structure
  > DOUBLER PLATE AT FRAME 20 CORRODED. REMOVED AND REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200719412](https://openairdocs.org/sdr/SIMA200719412.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719410](https://openairdocs.org/sdr/SIMA200719410.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719409](https://openairdocs.org/sdr/SIMA200719409.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719407](https://openairdocs.org/sdr/SIMA200719407.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719406](https://openairdocs.org/sdr/SIMA200719406.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 19 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719405](https://openairdocs.org/sdr/SIMA200719405.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBORAD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719411](https://openairdocs.org/sdr/SIMA200719411.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200719408](https://openairdocs.org/sdr/SIMA200719408.md): Seat Track · corroded · Jun 21, 2007 · N811AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBORAD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Next page: https://openairdocs.org/deregistered/N811AE-2019-11-20/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 = 'N811AE' AND deregistration_id = 'N811AE-2019-11-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N811AE-2019-11-20/reports

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