# Service difficulty reports: N708AE, cancelled Sep 9, 2019

A list on [N708AE, cancelled Sep 9, 2019](https://openairdocs.org/deregistered/N708AE-2019-09-09.md).

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

- [SDR SIMA200827304](https://openairdocs.org/sdr/SIMA200827304.md): Unknown · odor · Sep 27, 2008 · N708AE · Emb EMB135LR · Air Distribution System
  > ON FLIGHT 4574 DURING CRUISE CREW ADVISES NOTICEABLE BURNING SMELL IN COCKPIT. ACFT REMOVED FROM SERVICE. C/A PERFORMED VISUAL INSPECTION OF CABIN BALLASTS, CABIN LIGHTS, CONTROL MODULE. NO DEFECTS NOTED. NO BURNING SMELL NOTED AT THIS TIME. ACFT RETURNED
- [SDR SMIA200806501](https://openairdocs.org/sdr/SMIA200806501.md): Contactor · inoperative · Mar 2, 2008 · N708AE · Emb EMB135LR · Light System Wiring
  > ON FLIGHT 4778, CREW REPORTED ON CLIMB-OUT A OIL ODOR IN FORWARD PART OF THE CABIN. CREW DIVERTED TO BWI, NO OTHER PROBLEMS NOTED. AIRCRAFT REMOVED FROM SERVICE. DURING TROUBLE SHOOTING FOUND LEFT LANDING LIGHT CONTACTOR INOPERATIVE. REMOVED AND REPLACED C
- [SDR SIMA200733909](https://openairdocs.org/sdr/SIMA200733909.md): Battery · inoperative · Dec 3, 2007 · N708AE · Emb EMB135LR · Emergency Lighting
  > FORWARD SECTION OF EMERGENCY STRIP LIGHTS INOP. REMOVED AND REPLACED NUMBER 1 AND 2 BATTERY’S AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200709913](https://openairdocs.org/sdr/SIMA200709913.md): Floorbeam · corroded · Apr 6, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > CENTER OMEGA BEAM CORRODED AT FRAME 33. PERFORMED CUTOUT OF CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 203. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200709910](https://openairdocs.org/sdr/SIMA200709910.md): Floorbeam · corroded · Apr 3, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > LEFT OMEGA BEAM CORRODED AT FRAME 33. PERFORMED CUTOUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 202. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200709402](https://openairdocs.org/sdr/SIMA200709402.md): Sill · corroded · Mar 31, 2007 · N708AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200709403](https://openairdocs.org/sdr/SIMA200709403.md): Floorbeam · corroded · Mar 28, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED CORROSION BY CUTOUT, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200709203](https://openairdocs.org/sdr/SIMA200709203.md): Floorbeam · corroded · Mar 27, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > RIGHT FLOORBEAM SUPPORT FOUND CORRODED IN GALLEY AREA. REMOVED AND REPLACED SUPPORT IAW EMB SRM 51-40-02. OPERATIONAL CHECK GOOD.
- [SDR SIMA200709202](https://openairdocs.org/sdr/SIMA200709202.md): Bearing Cap · corroded · Mar 27, 2007 · N708AE · Emb EMB135LR · Nose/Tail Landing Gear
  > NOSE LANDING GEAR LEFT BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20-01. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200633108](https://openairdocs.org/sdr/SIMA200633108.md): Control Unit · faulty · Nov 26, 2006 · N708AE · Emb EMB135LR · Stabilizer Control System
  > PITCH TRIM INOP MESSAGE, RETURNED TO BOS. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTOL UNIT IAW EMB AMM 27-40-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200605801](https://openairdocs.org/sdr/SIMA200605801.md): Windshield · cracked · Feb 23, 2006 · N708AE · Emb EMB135LR · Flight Compartment Windows
  > NR 2 WINDSHIELD SHATTERED DURING DESCENT. REPLACED NR 2 WINDSHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR SIMA200311805](https://openairdocs.org/sdr/SIMA200311805.md): Floorbeam · corroded · Apr 23, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > DURING AN IMBV INSPECTION, THE LT FLOORBEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION ON THE LEFT FLOORBEAM. CLEANED, AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW E
- [SDR SIMA200311315](https://openairdocs.org/sdr/SIMA200311315.md): Frame · damaged · Apr 22, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Frame
  > DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND FRAME 18 DAMAGED ON LOWER EDGE. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW EMB 135 SRM 145/1142 CHAPTER 51, REV 21, 51-40-02, 51-20-03, 51-20-01.
- [SDR SIMA200311804](https://openairdocs.org/sdr/SIMA200311804.md): Frame · damaged · Apr 22, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Frame
  > DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND FRAME 81 DAMAGED ON LOWER EDGE. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW EMB 135, SRM 145/1142 CHAPTER 51, REV 21, 51-40-02, 51-20-03, 51-20-01 AND STANDARD SRM PRACTICES. (M)
- [SDR SIMA200311803](https://openairdocs.org/sdr/SIMA200311803.md): Stringer · chafed · Apr 21, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Longeron/Stringer
  > ABI - DURING A IMBV INSPECTION STRINGER 19L WAS FOUND TO HAVE A 2.3 INCHES LONG CHAF BELOW SRM LIMITS. BLENDED THE CHAFE AREA AND PERFORMED AN NDT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A REPAIR DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STA
- [SDR SIMA200311311](https://openairdocs.org/sdr/SIMA200311311.md): Floorbeam · corroded · Apr 19, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > DURING AN IMBV INSPECTION A PREVIOUS REPAIR ON THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142 REV 21,
- [SDR SIMA200311314](https://openairdocs.org/sdr/SIMA200311314.md): Beam · corroded · Apr 18, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Structure
  > DURING AN IMBV INSPECTION, THE GALLEY CENTER HAT BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED AREA OF THE HAT BEAM, CLEANED AND TRETED THE AREA. FABRICATED A REPAIR DOUBLER AND ATTACHED. REPAIR DONE IAW EMB 145 SRM, SRM EMB 14
- [SDR SIMA200311313](https://openairdocs.org/sdr/SIMA200311313.md): Sill · corroded · Apr 17, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING AN IMBV INSPECTION, THE CARGO DOOR OPENING LOWER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SILL AND CLEANED AREA. INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 21 CHAPTERS 51-40-02 AND 51-20-03. (M)
- [SDR SIMA200311312](https://openairdocs.org/sdr/SIMA200311312.md): Floorbeam · corroded · Apr 17, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING AN IMBV INSPECTION, THE GALLEY FORWARD FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION OF THE FORWARD FLOORBEAM. FABRICATED A REPAIR STRAP, SHIM AND TWO DOUBLERS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21 CHA
- [SDR SIMA200312709](https://openairdocs.org/sdr/SIMA200312709.md): Support · corroded · Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, PASSENGER DOOR OPENING AFT THRESHOLD SUPPORT HAS CORROSION. REMOVED CORRODED DOOR OPENING AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M)
- [SDR SIMA200312708](https://openairdocs.org/sdr/SIMA200312708.md): Support · corroded · Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > PASSENGER DOOR OPENING FORWARD THRESHOLD SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M)
- [SDR SIMA200312707](https://openairdocs.org/sdr/SIMA200312707.md): Gusset · corroded · Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Structure
  > ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, THE DIAMOND GUSSET AND RIGHT HAT BEAM AT FRAME 20 HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET ON RIGHT HAT BEAM IAW EMB 135 SRM 51-20-03, 51-40-02/06. (M)
- [SDR SIMA200312705](https://openairdocs.org/sdr/SIMA200312705.md): Beam · corroded · Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION GALLEY CENTER BEAM RAMP CORRODED. REMOVED AND REPLACED CENTER GALLEY BEAM IAW EMB 135 SRM 51-40-2/04, 51-20-03. (M)
- [SDR SIMA200312710](https://openairdocs.org/sdr/SIMA200312710.md): Gusset · corroded · Apr 15, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Structure
  > THIS IS A LEVEL 2 FINDING FOUND DURNG AN IMBV INSPECTION, CENTER FLOORBEAM GUSSET CORRODED IN GALLEY. REMOVED AND INSTALLED SERVICEABLE CENTER FLOOR GUSSET IN GALLEY IAW EMB 135 SRM 51-40-02/06, 51-20-03. (M)
- [SDR SIMA200312706](https://openairdocs.org/sdr/SIMA200312706.md): Structure · corroded · Apr 15, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION CABIN EXTENSION PROFILER RIGHT CORRODED. REMOVED AND INSTALLED SERVICEABLE CABIN EXTENSION PROFILE IAW EMB 135 SRM 51-40-02. (M)
- [SDR SIMA200123428](https://openairdocs.org/sdr/SIMA200123428.md): Floorbeam · corroded · Aug 22, 2001 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE RIGHT OMEGA BEAM LOWER FLANGE FORWARD OF FRAME 25 TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST 2830/01 AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
- [SDR SIMA200123420](https://openairdocs.org/sdr/SIMA200123420.md): Floorbeam · corroded · Aug 20, 2001 · N708AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT OMEGA BEAM AT FRAME 20 TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
- [SDR SIMA200116003](https://openairdocs.org/sdr/SIMA200116003.md): Control Unit · failed · Jun 9, 2001 · N708AE · Emb EMB135LR · Trailing Edge Flap Control System
  > YQB - FLT 4771 - DURING DESCENT, CREW SELECTED FLAPS TO 9 DEGREES. RECEIVED TOTAL FLAP FAILURE. FLAP FAILED AND SPS ADVANCED ON EICAS. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB
- [SDR SIMA20011426](https://openairdocs.org/sdr/SIMA20011426.md): Radome · May 22, 2001 · N708AE · Emb EMB135LR · Inertial Guidance System
  > ORD - FLT 4237 - CREW REPORTED THAT AFTER FLYING THROUGH PRECIPITATION, WEATHER RADAR DISPLAYED ARC OF PRECIPITATION THAT WS NOT THERE. CREW RETURNED AIRCRAFT TO ORD FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RADOME IAW EMB MM. OPS CHECK WAS GOOD
- [SDR SIMA3493](https://openairdocs.org/sdr/SIMA3493.md): Sensor · malfunctioned · Dec 14, 2000 · N708AE · Emb EMB135ER · Overheat Detection
  > LGA - FLT 4555 - DURING CLIMB-OUT, CREW NOTED NR 2 BRAKE OVERHEAT INDICATION WAS FLUCTUATING AND AT ONE POINT POINTER ON INDICATOR DISAPPEARED. CREW RETURNED TO LGA. AN EMERGENCY LANDING WAS DECLARED. AIRCRAFT LANDED SAFELY. NO FURTHER INCIDENTS WERE REPOR
- [SDR SIMA1633](https://openairdocs.org/sdr/SIMA1633.md): Windshield · cracked · Jun 11, 2000 · N708AE · Emb EMB135ER · Flight Compartment Windows
  > CLE - FLT 5169 - AIRCREW REPORTS DURING CRUISE FLIGHT, THE F/O OUTER WINDSHIELD CRAZED AND VISIBILITY DROPPED TO ZERO ON F/O SIDE. EMERGENCY DIVERT TO CLE. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSCREEN IAW EMBRAER MM 56-10-01-000-801A AND 56-10-01-40
- [SDR SIMA1412](https://openairdocs.org/sdr/SIMA1412.md): Warning System · false indication · May 20, 2000 · N708AE · Emb EMB135ER · Emergency Exits
  > ORF - FLT 4968 - ON CLIMB-OUT, HAD COCKPIT ACCESS LATCH WARNING, AND THE IND DID NOT GO OUT WHEN CABIN WAS PRESSURIZED. AIRCRAFT RETURNED BACK TO ORF TO INSPECTION LATCH WAS IN THE SECURED POSITION, SO IT WAS MEL''''D UNDER 52-05 DOOR WARNING. ADJUSTED AND T
- [SDR SIMA200004902](https://openairdocs.org/sdr/SIMA200004902.md): Hydraulic Line · leaking · Feb 18, 2000 · N708AE · Emb EMB135ER · Hydraulic System, Main
  > ORD - FLT 4109 - CREW REPORTED HYD 2 QUANTITY WARNING FOLLOWED BY HYD 2 PUMP FAILURE WARNING. MAINTENANCE FOUND A HYDRAULIC LINE LEAKING. LINE WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

## 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 = 'N708AE' AND deregistration_id = 'N708AE-2019-09-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N708AE-2019-09-09/reports

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