# Service difficulty reports: N702AE, cancelled May 9, 2022

A list on [N702AE, cancelled May 9, 2022](https://openairdocs.org/deregistered/N702AE-2022-05-09.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SIMA200809302](https://openairdocs.org/sdr/SIMA200809302.md): Battery · inoperative · Mar 31, 2008 · N702AE · Emb EMB135LR · Emergency Lighting
  > ON FLIGHT 4620, CREW REPORTED OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE, OVERHEAD EMERGENCY EXIT SIGN AT ROW-9 INOPERATIVE AND LAST TWO ROWS (9-13) EMERGENCY EXIT LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY POWER SUPPLY N
- [SDR SIMA200709617](https://openairdocs.org/sdr/SIMA200709617.md): Bushing · worn · Apr 5, 2007 · N702AE · Emb EMB135LR · Control Column Section
  > CAPTAIN YOKE HAS APPROXIMATELY QUARTER INCH OF DEAD SPACE WHEN MOVING ELEVATOR. REMOVED AND REPLACED BUSHING ON ELEVATOR BELL CRANK IAW EMB AMM. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200703203](https://openairdocs.org/sdr/SIMA200703203.md): Floorbeam · corroded · Jan 28, 2007 · N702AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > FOUND OMEGA BEAM CORRODED AT FRAME 32. PERFORMED CUTOUT OF DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200703005](https://openairdocs.org/sdr/SIMA200703005.md): Floorbeam · corroded · Jan 24, 2007 · N702AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > FOUND LEFT OMEGA BEAM CORRODED AT FRAME 44. PERFORMED CUTOUT OF DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE COATING, RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200703004](https://openairdocs.org/sdr/SIMA200703004.md): Floorbeam · corroded · Jan 24, 2007 · N702AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > FOUND OMEGA BEAM CORRODED AT FRAME 38. PERFORMED CUTOUT OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE COATING, RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200633104](https://openairdocs.org/sdr/SIMA200633104.md): Unknown · odor · Nov 26, 2006 · N702AE · Emb EMB135LR · Air Distribution System
  > BURNED RUBBER SMELL IN COCKPIT. INSPECTED LEFT AND RIGHT COCKPIT PANELS, OPERATED APU AND AIR CONDITIONING PACKS WITH NO ODORS NOTED. ODOR DUPLICATED WHEN RECONNECTED GROUND HEATER. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200632602](https://openairdocs.org/sdr/SIMA200632602.md): Manifold · failed · Nov 20, 2006 · N702AE · Emb EMB135LR · Landing Gear Steering System
  > ABORTED TAKEOFF FOR TEMPORARY LOSS OF NOSEWHEEL STEERING, AIRCRAFT VEERED LEFT WITH FULL RIGHT RUDDER APPLIED. LOUD NOISE FROM NOSE AREA ENCOUNTERED DURING EVENT. REMOVED AND REPLACED STEERING MANIFOLD IAW EMB AMM 32-50-04. OPERATIONAL CHECKED GOOD. AIRCRA
- [SDR SIMA200606601](https://openairdocs.org/sdr/SIMA200606601.md): Unknown · unknown · Mar 6, 2006 · N702AE · Emb EMB135LR · Emergency Lighting
  > DURING TAXI TO ROLL AFTER APU SHUTDOWN GOT AN ELECTRIC EMERGENCY ABNORMAL/ EMERGENCY LIGHTS NOT ARMED. CREW DID AN ABORTED TAKEOFF, HOWEVER, IT DOES NOT REFLECT IT IN THE LOG BOOK WRITE-UP. PERFORMED ALL CHECKS IAW THE FIM AND COULD NOT DUPLICATE PROBLEM. A
- [SDR SIMA200509102](https://openairdocs.org/sdr/SIMA200509102.md): Floor Support · corroded · Mar 25, 2005 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200504814) (K)
- [SDR SIMA200509101](https://openairdocs.org/sdr/SIMA200509101.md): Floor Support · corroded · Mar 25, 2005 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24-25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200504814) (K)
- [SDR SIMA200420101](https://openairdocs.org/sdr/SIMA200420101.md): Pitot System · contaminated · Jul 16, 2004 · N702AE · Emb EMB135LR · Pitot/Static System
  > DUIRNG CRUISE FLIGHT, NR 1 ENGINE LOST POWER, REGAINED POWER TWO TIMES, THEN RAN NORMALLY. AFTER LANDING NR 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FAULT ISOLATION MANUAL AND FOUND WATER IN BOTH PITOT SYSTEMS. DRAINED PIT
- [SDR SIMA200308402](https://openairdocs.org/sdr/SIMA200308402.md): Window Frame · corroded · Mar 18, 2003 · N702AE · Emb EMB135LR · Fuselage Main, Structure
  > DURING AN IMBV INSPECTION, THE RIGHT WINDSHIELD LOWER BEAM OUTBOARD 8 SCREW HOLES WERE FOUND TO BE CORRODED. HOLES WERE REAMED TO REMOVED CORROSION. FIVE HOLES REQUIRED FURTHER REAMING AND REQUIRED BUSHINGS TO BE FABRICATED AND INSTALLED. ALL WORK WAS DONE
- [SDR SIMA200308401](https://openairdocs.org/sdr/SIMA200308401.md): Window Frame · corroded · Mar 18, 2003 · N702AE · Emb EMB135LR · Fuselage Main, Structure
  > ABI - DURING AN IMBV INSPECTION, THE LEFT WINDSHIELD LOWER OUTBOARD 14 SCREW HOLES WERE FOUND TO BE CORRODED. THE SCREW HOLES WERE REAMED TO REMOVE CORROSION. THREE HOLES REQUIRED REAMING A SECOND TIME. THREE BUSHINGS WERE FABRICATED AND INSTALLED. REPAIRE
- [SDR SIMA200307916](https://openairdocs.org/sdr/SIMA200307916.md): Sill · corroded · Mar 14, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVIVCE DOOR SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB145/1142 REV 20, CHAPTERS 51-40-02, 51-20-03, AND 51-40-06. (M)
- [SDR SIMA200309012](https://openairdocs.org/sdr/SIMA200309012.md): Floor Support · corroded · Mar 12, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - THIS IS A LEVEL TWO FINDING FOUND DUIRNG AN IMBV INSPECTION, FORWARD PASSENGER DOOR FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW EMB135 SRM 51-40-02 ND ETN EB 53-032R1. (M)
- [SDR SIMA200309011](https://openairdocs.org/sdr/SIMA200309011.md): Floor Support · corroded · Mar 11, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, RIGHT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-20-03, 51-40-02, 51-40-06. (M)
- [SDR SIMA200307908](https://openairdocs.org/sdr/SIMA200307908.md): Floorbeam · corroded · Mar 11, 2003 · N702AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING AN IMBV INSPECTION, CORROSION ON THE CENTER OMEGA BEAM AT FRAME 20. REMOVED CORRODED AREA BY CUTOUT. FABRICATED AN EXTERNAL U-SHAPE DOUBLER. REPAIRE DONE IAW EMB 145 SRM (145/1142, REV 20) 53-21-10 PARA 5, FIG 204 SHEET 2 AND STANDARD SRM PRACT
- [SDR SIMA200309008](https://openairdocs.org/sdr/SIMA200309008.md): Bracket · corroded · Mar 8, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION PASSENGER DOOR FORWARD FLOOR SUPPORT BRACKET CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW EMB 135/145 SRM 51-40-02. (M)
- [SDR SIMA200309009](https://openairdocs.org/sdr/SIMA200309009.md): Sill · corroded · Mar 8, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION PASSENGER DOOR AFT FLOOR SUPPORT BRACKET CORRODED. REMOVED AND INSTALLED NEW SUPPORT IAW EMB135 SRM 51-40-02 AND 51-20-03. (M)
- [SDR SIMA200309007](https://openairdocs.org/sdr/SIMA200309007.md): Support · corroded · Mar 7, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION FLOOR BOARD RAMPS SUPPORT CORRODED. REMOVED AND INSTALLED NEW RAMP SUPPORTS IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-04. (M)
- [SDR SIMA200309004](https://openairdocs.org/sdr/SIMA200309004.md): Gusset · corroded · Mar 7, 2003 · N702AE · Emb EMB135LR · Fuselage Main, Structure
  > ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 135 51-40-02. (M)
- [SDR SIMA200389005](https://openairdocs.org/sdr/SIMA200389005.md): Crossbeam · corroded · Mar 7, 2003 · N702AE · Emb EMB135LR · Fuselage Main, Structure
  > THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION CROSSBEAM CORRODED AT FRAME 22. REMOVED AND INSTALLED NEW CROSSBEAM SUPPORT IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M)
- [SDR SIMA200309013](https://openairdocs.org/sdr/SIMA200309013.md): Sill · corroded · Mar 7, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION AFT SILL PLATE CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DOOR SILL IAW EMB 135 51-40-02. (M)
- [SDR SIMA200309006](https://openairdocs.org/sdr/SIMA200309006.md): Gusset · corroded · Mar 7, 2003 · N702AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 135 SRM 51-40-02. (M)
- [SDR SIMA200119701](https://openairdocs.org/sdr/SIMA200119701.md): Floorbeam · corroded · Jul 5, 2001 · N702AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING MBV INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. BEAM WAS REPAIRED IAW EMB SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR SIMA3561](https://openairdocs.org/sdr/SIMA3561.md): Connector · loose · Dec 21, 2000 · N702AE · Emb EMB135LR · Engine Thrust Reverser
  > BOS - FLT 4980 - ON TAKEOFF ROLL, TR1 DISAGREE CAME ON THE EICAS, ABORTED TAKEOFF AND RETURNED TO GATE FOR MAINTENANCE. MEL''D TR1 SYSTEM. MAINTENANCE TIGHTENED CANNON PLUG ON T/R STOW SWITCH. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR SIMA2732](https://openairdocs.org/sdr/SIMA2732.md): Switch · stuck · Sep 29, 2000 · N702AE · Emb EMB135LR · Engine Thrust Reverser
  > RIC - FLT 4940 - DURING TAKEOFF, CREW NOTED E2 THRUST REVERSER DISAGREE MESSAGE ON EICAS. TAKEOFF ABORTED, AIRCRAFT RETURNED TO GATE. PUT ON MEL AT THIS TIME. MAINTENANCE FOUND RIGHT ENGINE THRUST REVERSER LOWER STOW SWITCH STUCK. REMOVED SWITCH, LUBED, AN
- [SDR SIMA200006901](https://openairdocs.org/sdr/SIMA200006901.md): Duct · defective · Mar 9, 2000 · N702AE · Emb EMB135LR · Pneumatic Distribution System
  > FLT 4035 - ORD - CREW REPORTED UNUSUAL ODOR IN AIRCRAFT ACCOMPANIED BY EYE IRRITATION AND THROAT IRRITATION AFTER DEPARTURE. MAINTENANCE INSPECTED AIRCRAFT AND ALL FLUID SYSTEMS AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR FCF. FCF WAS SATISFACTORY AND A

## 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 = 'N702AE' AND deregistration_id = 'N702AE-2022-05-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N702AE-2022-05-09/reports

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