# Service difficulty reports: N802AE, cancelled Feb 24, 2021

A list on [N802AE, cancelled Feb 24, 2021](https://openairdocs.org/deregistered/N802AE-2021-02-24.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 · 63 reports

- [SDR SIMA20150105002](https://openairdocs.org/sdr/SIMA20150105002.md): Target · out of adjust · Jan 5, 2015 · N802AE · Emb EMB135KL · Landing Gear Position and Warning
  > LEADING EDGE AIR & GND FAIL MSG ON EICAS. REF ITEM 2 THIS LOG PAGE FOR ACTION TAKEN. ADJUSTED NLG PROXIMITY SWITCH TARGET IAW AMM 32-63-05. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141018004](https://openairdocs.org/sdr/SIMA20141018004.md): Valve · defective · Oct 18, 2014 · N802AE · Emb EMB135KL · Air Distribution System
  > AUTO & MANUAL PRESSURIZATION INOPERATIVE. MAX DELTA P ACHIEVED DURING FLIGHT.4 PSI ALL AOM 1 PROCEDURES ACCOMPLISHED. R & R GND CONNECTION VLV IAW AMM 21-22-04. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140902002](https://openairdocs.org/sdr/SIMA20140902002.md): Light · inoperative · Sep 2, 2014 · N802AE · Emb EMB135KL · Landing Gear Brake System
  > BRAKE ON LIGHT WILL NOT ILLUMINATE. REPLACED PARK BRAKE LIGHT IAW AMM 20-13-04 & RESET EMER BRAKE CB. OPERATIONS CHECKED GOOD IAW AMM 32-44-11. BULBS USED FROM ACFT KIT.
- [SDR SIMA20140530001](https://openairdocs.org/sdr/SIMA20140530001.md): Light · inoperative · May 30, 2014 · N802AE · Emb EMB135KL · Emergency Lighting
  > RIGHT WING TO FUSELAGE FAIRING FWD EMER LIGHT INOPERATIVE. R & R RT WING TO FUSELAGE FAIRING FWD EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140326012](https://openairdocs.org/sdr/SIMA20140326012.md): Lamp · out of position · Mar 26, 2014 · N802AE · Emb EMB135KL · Emergency Lighting
  > LEFT SIDE EMERGENCY LIGHTS AFT LIGHT IS OUT. REPOSITIONED LAMP IAW AMM 33-50-10, LIGHT ILLUMINATES, OPS CHECKED GOOD.
- [SDR SIMA20140317003](https://openairdocs.org/sdr/SIMA20140317003.md): Audio Panel · failed · Mar 17, 2014 · N802AE · Emb EMB135KL · Audio Integrating System
  > DURING DESCENT INTO ABI FIRST OFFICER`S ACP APPEARED TO SHORT OUT WITH STATIC NOISE IN FIRST OFFICER`S SPEAKER & HEADSET. ALSO STRONG SMELL OF BURNING ELEC CIRCUITS. R & R FIRST OFFICER'S DAP IAW AMM 23-51-01, 23-51-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140205002](https://openairdocs.org/sdr/SIMA20140205002.md): Flashlight · inoperative · Feb 5, 2014 · N802AE · Emb EMB135KL · Emergency Lighting
  > FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 25-60-11, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131227006](https://openairdocs.org/sdr/SIMA20131227006.md): Sealant · loose · Dec 27, 2013 · N802AE · Emb EMB135KL · Emergency Lighting
  > CA SIDE OVERWING EMERGENCY LIGHT SEALANT COMING OFF. RE-SEALED EMERGENCY LIGHT SLEEVE IAW 140 MM 51-00-00 SRM.
- [SDR SIMA20130924005](https://openairdocs.org/sdr/SIMA20130924005.md): Cradle · broken · Sep 24, 2013 · N802AE · Emb EMB135KL · Emergency Equipment
  > F/A REAR FLASHLIGHT HOLDER BROKEN. REPLACED AND OPS CHECK AFT F/A FLASH LIGHT BRACKET IAW AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA20130703004](https://openairdocs.org/sdr/SIMA20130703004.md): Wheel · abnormal · Jul 3, 2013 · N802AE · Emb EMB135KL · Wheel/Ski/Float
  > THE CREW ABORTED TAKEOFF DUE TO EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL OVER 80 KTS. ACFT REMOVED FROM SERVICE. COMPLIED WITH HIGH SPEED TAXI. NO EXCESSIVE NOSE WHEEL SHIMMEY. ACFT IS OK FOR SERVICE.
- [SDR SIMA20130621006](https://openairdocs.org/sdr/SIMA20130621006.md): Door · binding · Jun 21, 2013 · N802AE · Emb EMB135KL · Passenger/Crew Doors
  > DURING MX INSPECTION, FOUND MAIN PASSENGER DOOR HARD TO OPEN. ACFT REMOVED FROM SERVICE. ADJUSTED AFT UPPER STOP AND LUBED DOOR IAW 52-18-00. OPS CHECKED AND OPENING PRESSURE ON DOOR HANDLE WAS WITHIN ALLOWABLE LIMITS. ACFT RETURNED TO SERVICE.
- [SDR SIMA20130525006](https://openairdocs.org/sdr/SIMA20130525006.md): Battery · discharged · May 25, 2013 · N802AE · Emb EMB135KL · Emergency Lighting
  > DURING B INSPECTION FOUND THE NR 4 AND NR 5 FLOOR EMERGENGY LIGHT STRIPS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY BATTERY AND CHARGER ASSY IAW W/C 33-700-19. THE OPS CHECK WAS GOOD IAW AE WC 33-700-17. THE ACFT WAS RETURNED TO
- [SDR SIMA20130415002](https://openairdocs.org/sdr/SIMA20130415002.md): Roller · dirty · Apr 15, 2013 · N802AE · Emb EMB135KL · Passenger/Crew Doors
  > ON FLIGHT 4263 THE CREW REPORTED THE CABIN MAIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED DOOR ROLLER IAW EMB 140 AMM STANDARD PRATICES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVI
- [SDR SIMA20130313003](https://openairdocs.org/sdr/SIMA20130313003.md): Roller · lack of lube · Mar 14, 2013 · N802AE · Emb EMB135KL · Passenger/Crew Doors
  > ON FLIGHT 3987 FOUND MAIN CABIN DOOR HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVE FROM SERVICE. LUBRICATED MAIN CABIN DOOR GUIDE ROLLERS AND PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW EMB AMM 52-18-00. OPS CHECK GOOD FOUND TO BE WITHIN LIMITS
- [SDR SIMA20130117013](https://openairdocs.org/sdr/SIMA20130117013.md): Skin · cracked · Jan 17, 2013 · N802AE · Emb EMB135KL · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE INSPECTION FOUND LEFT REAR FUSELAGE I SKIN ABOVE FRAME 75 CRACKED BEYOND THE LIMITS OF THE SRM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2064. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130117012](https://openairdocs.org/sdr/SIMA20130117012.md): Drag Angle · cracked · Jan 17, 2013 · N802AE · Emb EMB135KL · Fuselage, Stabilizer Attach Fittings
  > DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD FUSELAGE TO VERTICAL DRAG ANGLE HAS 2 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1281 PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121231019](https://openairdocs.org/sdr/SIMA20121231019.md): Frame · cracked · Dec 31, 2012 · N802AE · Emb EMB135KL · Fuselage Main, Frame
  > FRAME 23, CRACKED BETWEEN STR 15R AND 16R. REPAIRED FRAME 23 BETWEEN STR 15R AND 16R IAW AEA EO EM-53MR-1808.
- [SDR SIMA20121231018](https://openairdocs.org/sdr/SIMA20121231018.md): Shear Tie · corroded · Dec 31, 2012 · N802AE · Emb EMB135KL · Cargo/Baggage Doors
  > CARGO DOOR SHEAR TIE AT FRAME 65 CORRODED. REPAIRED SHEAR TIE IAW AEA EO-EM53-MR-1129.
- [SDR SIMA20121231012](https://openairdocs.org/sdr/SIMA20121231012.md): Light · inoperative · Dec 31, 2012 · N802AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 A
- [SDR SIMA20121231011](https://openairdocs.org/sdr/SIMA20121231011.md): Inverter · inoperative · Dec 31, 2012 · N802AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE LAST 3 CENTER AISLE EMERGENCY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 DC/AC INVERTER IAW EMB 140 AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121231010](https://openairdocs.org/sdr/SIMA20121231010.md): Seal · cut · Dec 31, 2012 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING B INSPECTION FOUND THE PASSENGER DOOR FRAME SEAL CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR FRAME SEAL IAW EMB 140 AMM 53-21-01. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20121231009](https://openairdocs.org/sdr/SIMA20121231009.md): Connector · broken · Dec 31, 2012 · N802AE · Emb EMB135KL · Light System Wiring
  > DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP 3 CONNECTOR BETWEEN FRAME 34 AND FRAME 35 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE EMERGENCY LIGHT STRIP 3 CONNECTOR BETWEEN FRAME 34 AND FRAME 35 IAW EMB 140 SWPM 20-00-03, 20-21-00 AND
- [SDR SIMA20120728002](https://openairdocs.org/sdr/SIMA20120728002.md): Bulb · inoperative · Jul 28, 2012 · N802AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND THE EXTERIOR RIGHT AFT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERIOR RIGHT AFT EMERGENCY LIGHT IAW 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA20120702004](https://openairdocs.org/sdr/SIMA20120702004.md): Gasper Fan · malfunctioned · Jul 2, 2012 · N802AE · Emb EMB135KL · Air Distribution Fan
  > ON FLIGHT 2897 THE FLIGHT ATTENDANT REPORTED A LIGHT ODOR OF SMOKE IN MID CABIN FOR A SHORT TIME. THE ODOR WAS ALSO PRESENT IN THE COCKPIT. THE ODOR WAS NOT ELECTIRCAL AND LASTED 30 SECONDS. THE ODOR REPEATED ON FINAL INTO DFW. THE FLIGHT ATTENDANT DESCRIB
- [SDR SIMA20120531003](https://openairdocs.org/sdr/SIMA20120531003.md): Panel · damaged · May 31, 2012 · N802AE · Emb EMB135KL · Passenger/Crew Doors
  > DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT COVER PANEL HAS DIME SIZE HOLE NEXT TO LIGHT ASSEMBLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT COVER PANEL PER EMB 140 AMM 25-23-04. EMERGENCY LIGHTS OPE
- [SDR SIMA20120411001](https://openairdocs.org/sdr/SIMA20120411001.md): Uplock · inoperative · Apr 7, 2012 · N802AE · Emb EMB135KL · Landing Gear Position and Warning
  > ON FLIGHT 3366 THE CREW REPORTED THAT AFTER TAKEOFF WHEN GEAR WAS SELECT DUP, GOT A LANDING/DISAGREE MESSAGE RIGHT GEAR SHOWED UNSAFE. COMPLIED WITH AOM PROCEDURES AND DECLARED EMERGENCY AND RETURNED TO CAE NO OTHER PROBLEMS NOTED. THE AIRCRAFT LANDED WITHOU
- [SDR SIMA20120331003](https://openairdocs.org/sdr/SIMA20120331003.md): Door Seal · torn · Mar 31, 2012 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > FOR FLIGHT 3421 THE GATE AGENT REPORTED THE CABIN DOOR SEAL (FRAME SIDE) HAS A TEAR ON UPPER SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON MAIN DOOR FRAME RUBBER SEAL (UPPER TRAILING EDGE) IAW AMM 53-21-01. THE OPERATIONAL CHECK WAS GOOD
- [SDR SIMA201132910](https://openairdocs.org/sdr/SIMA201132910.md): Unknown · malfunctioned · Nov 24, 2011 · N802AE · Emb EMB135KL · APU Start/Ignition System
  > TRIED TO START THE APU WITH THE GPU. THE APU DID NOT START & THEN A BURNING SMELL WAS PRESENT IN THE COCKPIT. RESET GPU. STARTED APU IAW EMB GHC. NO DEFECTS NOTED.
- [SDR SIMA2011312007](https://openairdocs.org/sdr/SIMA2011312007.md): Light · not seated · Nov 7, 2011 · N802AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT EMERGENCY LIGHT ABOVE WING INOPERABLE. FOUND THE LIGHT IN FRONT OF THE LEFT WING EMERGENCY LIGHT INOPERABLE. FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEAT
- [SDR SIMA201124403](https://openairdocs.org/sdr/SIMA201124403.md): Light · inoperative · Sep 1, 2011 · N802AE · Emb EMB135KL · Emergency Lighting
  > FOR FLIGHT 4167 DURING INSPECTION FOUND THE FRONT EMERGENCY FLOOR PROXIMITY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRONT EMERGENCY FLOOR PROXIMITY LIGHT IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AI
- [SDR SIMA201109604](https://openairdocs.org/sdr/SIMA201109604.md): Light · inoperative · Apr 2, 2011 · N802AE · Emb EMB135KL · Emergency Lighting
  > FOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201105602](https://openairdocs.org/sdr/SIMA201105602.md): Structure · dented · Feb 24, 2011 · N802AE · Emb EMB135KL · Fuselage Main, Structure
  > WHILE ON THE RAMP THE AIRCRAFT WAS STRUCK BY A DEICE TRUCK NEAR THE SERVICE DOOR. SKIN HAS SEVERAL DENTS ON FRAME 22 BETWEEN STRINGERS 20 AND 18. THE SHEAR CLIP FROM 18 TO 19 CRACKED. SHEAR CLIP FROM 19 TO 20 WAS DENTED. THE AIRCRAFT WAS REMOVED FROM SERVI
- [SDR SIMA201103406](https://openairdocs.org/sdr/SIMA201103406.md): Sill · corroded · Jan 29, 2011 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE BASE VISIT INSPECTION FOUND CENTER SERVICE DOOR SILL TO HAVE CORROSION AROUND THE NUT PLATES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CENTER SERVICE DOOR SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE
- [SDR SIMA201103407](https://openairdocs.org/sdr/SIMA201103407.md): Floor Support · corroded · Jan 28, 2011 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED (FORWARD AND AFTWARD OF FRAME 20 ON A PREVIOUS REPAIR). THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED DOUBLER ON THE LEFT OMEGA BEAM AT FRAME 20 IAW EMBRAER SRM 53-00-10. THE AIRCRAFT
- [SDR SIMA201103405](https://openairdocs.org/sdr/SIMA201103405.md): Floor Support · corroded · Jan 28, 2011 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM BETWEEN FRAMES 59-60 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO THE LEFT OMEGA BEAM BETWEEN FRAMES 59-60 IAW EO EM-53MR-1518 PART A. THE AIRCRAFT WAS RETURNED
- [SDR SIMA201103404](https://openairdocs.org/sdr/SIMA201103404.md): Floor Support · corroded · Jan 26, 2011 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM AT FRAME 27 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 27 IAW EMBRAER SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201103403](https://openairdocs.org/sdr/SIMA201103403.md): Floor Support · corroded · Jan 26, 2011 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM FORWARD OF FRAME 25 AT THE CARBON CROSSMEMBER TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED REPAIR DOUBLER IAW EMBRAER SRM 53-00-10 AND 51-40-02. THE AIRCRAFT WAS RETURNED T
- [SDR SIMA201103401](https://openairdocs.org/sdr/SIMA201103401.md): Frame · cracked · Jan 26, 2011 · N802AE · Emb EMB135KL · Fuselage Main, Frame
  > DURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT FRAME 23 CRACKED AT THE FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACKED FRAME IAW EO EM-53MR-1759. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201034101](https://openairdocs.org/sdr/SIMA201034101.md): Unknown · malfunctioned · Dec 6, 2010 · N802AE · Emb EMB135KL · VHF Communications System
  > FOR FLIGHT 2855 SOC REPORTED THE CREW LOST COMMUNICATION RADIOS 1 & 2, WOULD NOT TRANSMIT. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. AFTER TROUBLESHOOTING CANNOT DUPLICATE PROBLEM. BOTH
- [SDR SIMA201013807](https://openairdocs.org/sdr/SIMA201013807.md): Light · inoperative · May 18, 2010 · N802AE · Emb EMB135KL · Emergency Lighting
  > DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-07-000-801A AND 33-00-07-400-801-A. THE AIRCRAFT
- [SDR SIMA201002603](https://openairdocs.org/sdr/SIMA201002603.md): Proximity Switch · inoperative · Jan 24, 2010 · N802AE · Emb EMB135KL · Landing Gear Position and Warning
  > ON FLIGHT 4602 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. COULD NOT SELECT GEAR UP. THE CREW ELECTED TO RETURN TO BOS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND
- [SDR SIMA201002604](https://openairdocs.org/sdr/SIMA201002604.md): Proximity Switch · inoperative · Jan 22, 2010 · N802AE · Emb EMB135KL · Landing Gear Position and Warning
  > ON FLIGHT 4455 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A WEIGHT ON WHEEL INOPERABLE MESSAGE ON EICAS. THE CREW ELECTED TO RETURN TO JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE
- [SDR SIMA201002605](https://openairdocs.org/sdr/SIMA201002605.md): Proximity Switch · inoperative · Jan 22, 2010 · N802AE · Emb EMB135KL · Landing Gear Position and Warning
  > ON FLIGHT 4694 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. THE LANDING GEAR WAS NOT RETRACTED. THE CREW ELECTED TO RETURN TO JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. R
- [SDR SIMA200925204SUP](https://openairdocs.org/sdr/SIMA200925204SUP.md): Windshield · failed · Oct 22, 2009 · N802AE · Emb EMB135KL · Flight Compartment Windows
  > ON FLIGHT 4913, DURING CLIMB OUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS COCKPIT WINDSHIELD IAW AMM 5610-01 MANUAL.
- [SDR SIMA200925204](https://openairdocs.org/sdr/SIMA200925204.md): Windshield · cracked · Sep 9, 2009 · N802AE · Emb EMB135KL · Flight Compartment Windows
  > ON FLIGHT 4913 DURING CLIMBOUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS COCKPIT WINDSHIELD IAW AMM 5610-01. COMPLIED UP TO S
- [SDR SIMA200909102](https://openairdocs.org/sdr/SIMA200909102.md): Floor Support · corroded · Mar 30, 2009 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING HMBV THE LEFT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. CUT OUT THE DAMAGED AREA. PREPARED A 1.6" X 12.25" FILLER FROM P/N EPNEM53EP54703 AND A 15.5" X 3.6" DOUBLER FROM P/N EPNEM53EP54701. CLEANED, TREATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53
- [SDR SIMA200909101](https://openairdocs.org/sdr/SIMA200909101.md): Sill · corroded · Mar 30, 2009 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING HMBV THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED SERVICE DOOR SILL IN TWO AREAS. ALODINE AND PRIMED BLENDED AREA. FILLED BLENDED AREA USING EPOXY RESIN HYSOL 9894. FABRICATED, ALODINED, PRIMED AND INSTALLED TWO DOUBLERS ONE 1.1" X 3.2"
- [SDR SIMA200720107](https://openairdocs.org/sdr/SIMA200720107.md): Skin · cracked · May 25, 2007 · N802AE · Emb EMB135KL · Fuselage Main, Plate/Skin
  > CRACK DEVELOPED DURING DAMAGE CONTOUR. CUT OUT DAMAGE AREA. FABRICATED DOUBLER AND FILLER. INSTALLED IAW EMB IC 2007-145/03554A, PARAGRAPH 1.
- [SDR SIMA200720106](https://openairdocs.org/sdr/SIMA200720106.md): Sill · corroded · May 24, 2007 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200720104](https://openairdocs.org/sdr/SIMA200720104.md): Floor Support · corroded · May 21, 2007 · N802AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > GALLEY CENTER HAT BEAM CORRODED. REMOVED AND REPLACED HAT BEAM IAW EMB SRM 51-40-02 AND 51-40-04. AIRCRAFT RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N802AE-2021-02-24/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 = 'N802AE' AND deregistration_id = 'N802AE-2021-02-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N802AE-2021-02-24/reports

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