# Service difficulty reports: N731BE, cancelled Jan 27, 2014

A list on [N731BE, cancelled Jan 27, 2014](https://openairdocs.org/deregistered/N731BE-2014-01-27.md).

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

- [SDR SIMA200726301](https://openairdocs.org/sdr/SIMA200726301.md): Acm · seized · Sep 19, 2007 · N731BE · Emb EMB135LR · Cabin Cooling System
  > ON SHUT DOWN, SMOKE AND BURNING ODOR ENTERED COCKPIT, SLIGHTLY VISIBLE SMOKE. CEASED WHEN PACK WAS SELECTED OFF. FOUND NR 2 AIRCYCLE MACHINE SEIZED UP. REMOVED AND REPLACED NR 2 AIRCYCLE MACHINE IAW AMM 21-51-03-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SE
- [SDR SIMA200719704](https://openairdocs.org/sdr/SIMA200719704.md): Wire Harness · burned · Jul 16, 2007 · N731BE · Emb EMB135LR · Light System Wiring
  > BURNING ODOR IN AFT CABIN. REMOVED AND REPLACED RIGHT AFT WALL LIGHT HARNESS ASSEMBLY IAW EMB AMM 33-21-05. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200717506](https://openairdocs.org/sdr/SIMA200717506.md): Structure · damaged · Jun 20, 2007 · N731BE · Emb EMB135LR · Fuselage Main, Structure
  > AIRCRAFT STRUCK RUNWAY WITH ALL THREE LANDING GEAR IN THE UP AND STOWED POSITION, GO AROUND PROCEDURE WAS EXECUTED. RECEIVED FLAP FAIL MESSAGE DURING SECOND APPROACH. EMERGENCY DECLARED. EMERGENCY GEAR EXTENSION PROCEDURES WAS PERFORMED WITH THREE GREEN DOW
- [SDR SIMA200715901](https://openairdocs.org/sdr/SIMA200715901.md): Power Supply · failed · Jun 4, 2007 · N731BE · Emb EMB135LR · Emergency Lighting
  > FOUND EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED NUMBER TWO EPSU IAW EMB IAW AMERICAN EAGLE WORK CARD 33-700-19 AND SECURED LOOSE GROUND STUD GS8506DC IAW EMB AMM 20-13-21. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200706404](https://openairdocs.org/sdr/SIMA200706404.md): Actuator · worn · Mar 1, 2007 · N731BE · Emb EMB135LR · Pneumatic Distribution System
  > VIBRATION FELT IN BOTH IN CABIN AROUND ROW 6 AND FLIGHT DECK, NO VIBRATION IN FELT IN CONTROLS. REMOVED AND REPLACED NR 1 RAM AIR VALVE ACTUATOR ASSEMBLY, LEFT EMERGENCY VENT VALVE ASSEMBLY AND RIGHT EMERGENCY VENT VALVE ASSEMBLY IAW EMB AMM. OPERATIONAL CHE
- [SDR SIMA200620501](https://openairdocs.org/sdr/SIMA200620501.md): Relay · failed · Jul 21, 2006 · N731BE · Emb EMB135LR · Emergency Lighting
  > CLE - FLT 4888 - ELECTRICAL EMERGENCY ABNORMAL INDICATION AFTER V1 SPEED DURING TAKEOFF. EMERGENCY LIGHT ILLUMINATED WITH EMERGENCY LIGHTS NOT ARMED INDICATION. FOLLOWED AOM AND LANDED SAFELY AND ALL OTHER INDICATIONS NORMAL. RAI BAD ESS TIMER RELAY, OPS C
- [SDR SIMA200612101](https://openairdocs.org/sdr/SIMA200612101.md): Unknown · odor · Apr 27, 2006 · N731BE · Emb EMB135LR · Air Distribution System
  > AFTER TAKEOFF, SMELLED FUMES IN COCKPIT. AT 8000 FT, SMELLED FUMES AGAIN BUT MUCH STRONGER THIS TIME. F/A CONFIRMED BURNING SMELL. UPON REDUCING THRUST FOR THE DESCENT AND LANDING THE SMELL SUBSIDED AND DID NOT RETURN. THE AC WAS UNDER THE MAX LANDING WEIG
- [SDR SIMA200425309](https://openairdocs.org/sdr/SIMA200425309.md): Floor Support · corroded · Sep 4, 2004 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL BETWEEN FRAMES 14 AND 16 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 16.25 INCH SECTION OF THE FORWARD DIGITAL. FABRICATED A 16.25 INCH REPAIR PLATE. FABRICATED A RIGHT DOUBLER AND LEFT DOUBLER SHIMS. REPA
- [SDR SIMA200425311](https://openairdocs.org/sdr/SIMA200425311.md): Sill · corroded · Sep 3, 2004 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BEYOND LIMITS. REMOVED DAMGAED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-40-02. (M)
- [SDR SIMA200426902](https://openairdocs.org/sdr/SIMA200426902.md): Dampener · damaged · Sep 2, 2004 · N731BE · Emb EMB135LR · Elevator Control System
  > DURING AN IMBV INSPECTION, THE LEFT AILERON DAMPENER FITTING WAS FOUND DAMAGED. REMOVED THE DAMGAED FITTING AND INSTALLED NEW FITTING IAW EMB SERVICE BULLETIN 145-27-0061. (M)
- [SDR SIMA200425303](https://openairdocs.org/sdr/SIMA200425303.md): Stringer · chafed · Sep 2, 2004 · N731BE · Emb EMB135LR · Fuselage Main, Longeron/Stringer
  > ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R AT FRAME 52 AND 53 WAS FOUND TO BE CHAFED BEYOND SRM LIMITS. BLENDED CHAFED AREA SMOOTH. PERFORMED A DOUBLER ANGLE, TWO FILLERS, REPAIR DONE IAW EMB STATEMENT IC2004-145/3093A. (M) SIMA
- [SDR SIMA200426903](https://openairdocs.org/sdr/SIMA200426903.md): Floor Support · corroded · Sep 1, 2004 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMGAED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4061B DATED AUGUST 31, 2004. (M
- [SDR SIMA200425310](https://openairdocs.org/sdr/SIMA200425310.md): Floor Support · corroded · Sep 1, 2004 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FS 25 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 27, 53-22-10. (M)
- [SDR SIMA200425308](https://openairdocs.org/sdr/SIMA200425308.md): Floor Support · corroded · Sep 1, 2004 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - DURNG AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4061B DATED AUGUST 31, 2004
- [SDR SIMA200425307](https://openairdocs.org/sdr/SIMA200425307.md): Floor Support · corroded · Aug 31, 2004 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER, SHIM AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 27, 53-21-10. (M)
- [SDR SIMA200421901](https://openairdocs.org/sdr/SIMA200421901.md): Fcu · inoperative · Aug 5, 2004 · N731BE · Emb EMB135LR · Trailing Edge Flap Control System
  > FOUND FLAP FAIL MESSAGE. FLAPS STUCK IN FULL UP POSITION. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPERATIONAL CHECK OF FLAP CONTROL SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR SIMA200406806](https://openairdocs.org/sdr/SIMA200406806.md): Control Unit · inoperative · Mar 6, 2004 · N731BE · Emb EMB135LR · Elevator Control System
  > PITCH NR 1 AND NR 2 INOPERATIVE. COMPLIED WITH ETN EB 27-0022R1 AND REPLACED HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (SW21200404960)
- [SDR SIMA200405902](https://openairdocs.org/sdr/SIMA200405902.md): Control Unit · inoperative · Feb 25, 2004 · N731BE · Emb EMB135LR · Elevator Control System
  > AFTER LANDING, DURING TAXI, CREW REPORTED THE PITCH TRIM 1 AND 2 INOPERATIVE ILLIMINATED. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED
- [SDR SIMA200333802](https://openairdocs.org/sdr/SIMA200333802.md): Connector · loose · Dec 4, 2003 · N731BE · Emb EMB135LR · Flight Control System Wiring
  > BOS - FLT 4592 - FLAP FAIL/SPS ADVANCED FLAPS REMAINED AT ZERO REGARDLESS OF FLAP SELECTOR POSITION. RESECURED CONNECTOR ON FLAP VELOCITY SENSOR PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR SIMA200317404](https://openairdocs.org/sdr/SIMA200317404.md): Relay · inoperative · Jun 19, 2003 · N731BE · Emb EMB135LR · DC Power Distribution System
  > DURING CLIMB CREW REPORTED AN ELECTRICAL EMERGENCY ABNORMAL EICAS MESSAGE ABOUT 1 SECOND AFTER TURNING APU OFF AS PER CLIMB-OUT PROCEDURE. AIRCRAFT WAS RETURNED TO FIELD. THE CREW RESTARTED THE APU AND REESTABLISHED ELECTRICAL POWER TO THE AIRCRAFT. MAINTEN
- [SDR SIMA200302005](https://openairdocs.org/sdr/SIMA200302005.md): Light · inoperative · Jan 18, 2003 · N731BE · Emb EMB135LR · Emergency Lighting
  > EWR - FLT 4503 - DURING PREFLIGHT, CREW REPORTED ALL THE EMERGENCY LIGHTS TO BE INOPERATIVE. AIRCRAFT WAS INSPECTED AND FERRIED TO BOS FOR REPAIR. MAINTENANCE COLD NOT DUPLICATE DISCREPANCY AFTER AIRCRAFT LANDED IN BOS. SUSPECT BATTERIES CHARGED DURING FLIG
- [SDR SIMA200216406](https://openairdocs.org/sdr/SIMA200216406.md): Structure · chafed · Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > FORWARD FLOOR EXTENSION IS CHAFED AT FRAME 22. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS. BLENDED OUT CHAFE, WITHIN MFG SRM LIMITS.
- [SDR SIMA200216404](https://openairdocs.org/sdr/SIMA200216404.md): Longeron · dented · Jun 11, 2002 · N731BE · Emb EMB135LR · Engine Cowling System
  > RIGHT UPPER COWLING LOWER INBOARD LONGERON DENTED. C/A FABRICATED AND INSTALLED. A DOUBLER, REPAIR DONE IAW SRM.
- [SDR SIMA200216408](https://openairdocs.org/sdr/SIMA200216408.md): Longeron · dented · Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)
  > LEFT UPPER COWLING LOWER INBOARD LONGERON DENTED. RECONTOURED LONGERON, PERFORMED EDDY CURRENT, NO DEFECTS. ACCEPTED AS IS IAW. TREATED FOR CORROSION.
- [SDR SIMA200216407](https://openairdocs.org/sdr/SIMA200216407.md): Gusset · gouged · Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)
  > CENTER GUSSET GOUGED FROM FRAMES 20 T0 22. C/A REMOVED GOUGED BY BLENDING, WITHIN SRM LIMITS. RESTORED SURFACE PROTECTION.
- [SDR SIMA200216405](https://openairdocs.org/sdr/SIMA200216405.md): Extinguisher · chafed · Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)
  > AFT FLOOR EXTENTION IS CHAFED FROM FRAMES 22-23. C/A PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS. BLENDED CHAFE IAW SRM LIMITS.
- [SDR SIMA200216409](https://openairdocs.org/sdr/SIMA200216409.md): Bracket · gouged · Jun 10, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)
  > APU FIREWALL GOUGED BY APU BLEED AIR VALUE BRACKET. PERFORMED EDDY CURRENT, NO DEFECTS. REPAIR DONE ON GOUGE IAW SRM.
- [SDR SIMA200205401](https://openairdocs.org/sdr/SIMA200205401.md): Apu · failed · Feb 23, 2002 · N731BE · Emb EMB135LR · Airborne Auxiliary Power Unit (APU) System
  > EWR - FLT 4587 - DURING TAXI OUT, CREW NOTED SMOKE IN CABIN AFTER APU FAIL AND SHUT DOWN. CREW RETURNED TO GATE AND PASENGERS WERE DEPLANED NORMALLY. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE WAS SENT FROM LGA. AIRCRAFT WAS INSPECTED AND APU WAS DEFE

## 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 = 'N731BE' AND deregistration_id = 'N731BE-2014-01-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N731BE-2014-01-27/reports

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