# Service difficulty reports: N712AE

A list on [N712AE](https://openairdocs.org/aircraft/N712AE.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 · 51 reports

- [SDR SIMA20130227004](https://openairdocs.org/sdr/SIMA20130227004.md): Holder · broken · Feb 27, 2013 · N712AE · Emb EMB135LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT HOLDER IAW EMB-135 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS
- [SDR SIMA20130119004](https://openairdocs.org/sdr/SIMA20130119004.md): Connector · defective · Jan 19, 2013 · N712AE · Emb EMB135LR · Light System Wiring
  > DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON THE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE WIRE CONNECTOR ON WIRE W799-8001-20 IAW EMB 135 SWPM 20-21-00. THE OPERATIONAL CHECK OF THE EMERGENCY LIG
- [SDR SIMA20130114003](https://openairdocs.org/sdr/SIMA20130114003.md): Light · inoperative · Jan 14, 2013 · N712AE · Emb EMB135LR · Emergency Lighting
  > DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130105001](https://openairdocs.org/sdr/SIMA20130105001.md): Flashlight · unserviceable · Jan 5, 2013 · N712AE · Emb EMB135LR · Emergency Equipment
  > ON FLIGHT 3248 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WOULD NOT STAY IN FLASHLIGHT HOLDER/CHARGER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB 135 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. T
- [SDR SIMA20121115002](https://openairdocs.org/sdr/SIMA20121115002.md): Wire · broken · Nov 15, 2012 · N712AE · Emb EMB135LR · Light System Wiring
  > DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE AT SERVICE DOOR EMERGENCY LIGHT CONNECTOR IAW EMB135 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD IAW EMB135 AMM 33-50-00. T
- [SDR SIMA20121026004](https://openairdocs.org/sdr/SIMA20121026004.md): Acm · malfunctioned · Oct 26, 2012 · N712AE · Emb EMB135LR · Cabin Cooling System
  > FOR FLIGHT 2802 THE CREW REPORTED THAT WHILE PARKED AT THE GATE RUNNING APU FOR ABOUT 20 MINUTES CLOSED THE MAIN DOOR AND ABOUT 30 SECONDS LATER HAD SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RIGHT SIDE AIR CYCLE MACHINE LOC
- [SDR SIMA20121019002](https://openairdocs.org/sdr/SIMA20121019002.md): Light · inoperative · Oct 19, 2012 · N712AE · Emb EMB135LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE 4TH EMERGENCY LIGHTING STRIP FROM REAR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING STRIP IAW EMB 135 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS R
- [SDR SIMA20121019001](https://openairdocs.org/sdr/SIMA20121019001.md): Fan · malfunctioned · Oct 19, 2012 · N712AE · Emb EMB135LR · Air Distribution Fan
  > ON FLIGHT 2802 THE CREW REPORTED THAT AFTER LANDING THE SMELL OF ELECTRICAL SMOKE WAS DETECTED AND THEN DISSIPATED SHORTLY THEREAFTER. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE COCKPIT RECIRULATION FAN SMELLED BURNT. REMOVED AND REPLACED WITH SERVICEABLE C
- [SDR SIMA20120718001](https://openairdocs.org/sdr/SIMA20120718001.md): Unknown · odor · Jul 18, 2012 · N712AE · Emb EMB135LR · Air Distribution System
  > FLIGHT 3337, RAMP CREW REPORTED THEY NOTICED A SMOKE ODOR IN CARGO BAY. AIRCRAFT REMOVED FROM SERVICE. INSPECTED CARGO BAY FOR OBVIOUS DEFECTS, NONE NOTED. GROUND RAN BOTH ENGINES IAW 71-00-01, NO ODOR NOTED WITH BOTH BLEEDS AND PACKS ON. AIRCRAFT OK FOR
- [SDR SIMA20120710005](https://openairdocs.org/sdr/SIMA20120710005.md): Light · inoperative · Jul 10, 2012 · N712AE · Emb EMB135LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND THE OVERHEAD AISLE EMERGENCY EXIT LIGHT OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERHEAD AISLE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA201136315](https://openairdocs.org/sdr/SIMA201136315.md): Light · inoperative · Dec 28, 2011 · N712AE · Emb EMB135LR · Emergency Lighting
  > MEL 3330. EMERGENCY FLOOR PROXIMITY LIGHT INOP ON FLOOR SEATS 5 AND 6. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT SEATS 5 AND 6 IAW EMB 135 AMM 33-50-12 OPS CHECK GOOD MEL 3330 RESTORED.
- [SDR SIMA201136309](https://openairdocs.org/sdr/SIMA201136309.md): Light · inoperative · Dec 23, 2011 · N712AE · Emb EMB135LR · Emergency Lighting
  > EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOP SEAT 5 & 6. DEFERRED PER MEL 33-30, M PROCEDURE C/W.
- [SDR SIMA201136303](https://openairdocs.org/sdr/SIMA201136303.md): Light · inoperative · Dec 22, 2011 · N712AE · Emb EMB135LR · Emergency Lighting
  > FOUND 2ND LIGHT STRIP EMERGENCY AISLE INOP. REMOVED AND REPLACED AISLE LIGHT STRIP EMERGENCY IAW EMB-135 AMM 33-50-08. OPS CHECK GOOD.
- [SDR SIMA201111601](https://openairdocs.org/sdr/SIMA201111601.md): Antenna · damaged · Apr 23, 2011 · N712AE · Emb EMB135LR · VHF Communications System
  > ON FLIGHT 2895 CREW REPORTED ACFT EXPOSED TO SEVERE AND EXTREME TURBULENCE, LIGHTNING STRIKES & STRONG VIBRATIONS THROUGH COCKPIT FLOOR & CABIN ROW 2. CREW LOST ACARS & RADIOS. RETURNED BUT COULD NOT LAND DUE TO WINDSHEAR, MICRO BURSTS & DIVERTED TO DAL. AC
- [SDR SIMA201107604](https://openairdocs.org/sdr/SIMA201107604.md): Support Bracket · cracked · Mar 17, 2011 · N712AE · Emb EMB135LR · Passenger/Crew Doors
  > DURING MAINTENANCE VISIT FOUND THE PASSENGER DOOR INTERNAL HANDLE SUPPORT BOX BRACKET CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED PASSENGER DOOR INTERNAL HANDLE SUPPORT BOX BRACKET IAW AE ETN-EM-52-037R1 AND EO EM-52MR-250. THE AIRCRAFT WAS RET
- [SDR SIMA201106905](https://openairdocs.org/sdr/SIMA201106905.md): Light · inoperative · Mar 6, 2011 · N712AE · Emb EMB135LR · Emergency Lighting
  > FOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE FIRST CEILING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST CEILING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD
- [SDR SIMA201034304](https://openairdocs.org/sdr/SIMA201034304.md): Warning System · malfunctioned · Dec 5, 2010 · N712AE · Emb EMB135LR · Trailing Flap Position Indicating System
  > ON FLIGHT 4470 THE CREW REPORTED A FLAP FAIL MESSAGE ON EICAS WHEN SELECTED TO 9 DEGREES FLAPS STAYED AT 0 DEGREES. THE CAPTAIN DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED FIM TASK 27
- [SDR SIMA201030503](https://openairdocs.org/sdr/SIMA201030503.md): Cradle · broken · Oct 29, 2010 · N712AE · Emb EMB135LR · Emergency Lighting
  > FOR FLIGHT 4547 DURING TAXI THE REAR CABIN FLASHLIGHT WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT AND CRADLE ASSEMBLY IAW E135 AMM 33-10-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SE
- [SDR SIMA201023801](https://openairdocs.org/sdr/SIMA201023801.md): Ballast · defective · Aug 25, 2010 · N712AE · Emb EMB135LR · Passenger Compartment Lighting
  > ON FLIGHT 4524 THE CREW REPORTED A STRONG SMOKE ODOR COMING FROM A PASSENGER SERVICE UNIT AT SEAT 8A IN THE CABIN. THE CAPTAIN DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT BOS. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BURNING ODOR
- [SDR SIMA200934303](https://openairdocs.org/sdr/SIMA200934303.md): Flap System · malfunctioned · Dec 5, 2009 · N712AE · Emb EMB135LR · Trailing Edge Flap Control System
  > DURING FLIGHT 4546 WHILE ON APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE. THE MESSAGE INDICATED THAT THE FLAPS WERE ON 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP RESET. PE
- [SDR SIMA200933803](https://openairdocs.org/sdr/SIMA200933803.md): Brake · failed · Dec 3, 2009 · N712AE · Emb EMB135LR · Trailing Edge Flap Control System
  > DURING FLIGHT 4485 ON APPROACH THE CREW REPORTED A FLAP FAIL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW LEFT FLAP TRANSMISSION BRAKE IAW EMB AMM 27-51-01. OPERATIONAL CHECK WAS GOOD.
- [SDR SIMA200931301](https://openairdocs.org/sdr/SIMA200931301.md): Flap · malfunctioned · Nov 5, 2009 · N712AE · Emb EMB135LR · Trailing Edge Flap Control System
  > ON FLIGHT 4552 DURING DESCENT WHILE SELECTING FLAPS 9 FROM ZERO THE CREW RECEIVED AN EICAS FLAP FAIL MESSAGE. THE MESSAGE INDICATED ZERO DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING INSP
- [SDR SIMA200929906](https://openairdocs.org/sdr/SIMA200929906.md): Velocity Sensor · defective · Oct 25, 2009 · N712AE · Emb EMB135LR · Trailing Flap Position Indicating System
  > ON FLIGHT 4472 DURING THE DESCENT THE CREW REPORTED A FLAP FAILURE MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT SYSTEM IAW FIM 27-51-00-810-816-A AND FOUND THE LEFT VELOCITY
- [SDR SIMA200912001](https://openairdocs.org/sdr/SIMA200912001.md): Unknown · odor · Apr 29, 2009 · N712AE · Emb EMB135LR · Air Distribution System
  > ON FLIGHT 3226 CREW REPORTED, RETURNED TO GATE DUE TO AN ELECTRICAL BURNING ODOR IN THE COCKPIT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION, NO DEFECT NOTED. ALSO PERFORMED VISUAL INSPECTION OF THE DUCTS, DUCTS IN ACM, NO DEFECT NOTED. AIRC
- [SDR SIMA200910406](https://openairdocs.org/sdr/SIMA200910406.md): Floor Support · corroded · Apr 9, 2009 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING A MBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 38 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A DOUBLER, FILLER, AND TWO SHIMS. DRILLED, CLEANED AND TREATED PARTS AND INSTALLED. REPAIR DONE IAW SRM 53-0
- [SDR SIMA200909805](https://openairdocs.org/sdr/SIMA200909805.md): Floor Support · corroded · Apr 7, 2009 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING A MBV INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. PERFORMED A CUTOUT TO REMOVE THE CORROSION. TRIMMED EPNEM5354701 AND 54703 FOR USE ON DOUBLER AND FILLER. FABRICATED TWO SHIMS FOR REPAIR. DRILLED, CLEANED, ALODINED AND PRIME
- [SDR SIMA200909806](https://openairdocs.org/sdr/SIMA200909806.md): Floor Support · corroded · Apr 6, 2009 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING MBV, THE CENTER OMEGA BEAM WAS FOUND CORRODED. REMOVED CORROSION AND PERFORMED NDR INSPECTION. CLEANED, ALODINED, PRIMED AND FILLED BLEND AREA. FABRICATED DOUBLER. CLEANED, ALODINED, PRIMED AND INSTALLED DOUBLER IAW SRM 53-21-10. AIRCRAFT RETURNED
- [SDR SIMA200721801](https://openairdocs.org/sdr/SIMA200721801.md): Relay · failed · Aug 2, 2007 · N712AE · Emb EMB135LR · Emergency Lighting
  > EMERGENCY LIGHTS NOT ARM AND ELECTRICAL EMERGENCY ABNORMAL MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED BATTERY RELAY BOX IAW EMB AMM 24-33-02. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200716202](https://openairdocs.org/sdr/SIMA200716202.md): Unknown · odor · Jun 7, 2007 · N712AE · Emb EMB135LR · Air Distribution System
  > SMOKE APPEARED AFTER SELECTING CRUISE THRUST, EMERGENCY DECLARED. DIVERTED TO JFK. PERFORMED TROUBLESHOOTING IAW ROLLS ROYCE FAULT ISOLATION MANUAL 72-00-00 AND EMB AMM 21-20-00 WITH NO DEFECTS NOTED. PERFORMED 75 PERCENT N2 RUNS WITH AND WITHOUT PACKS WITH
- [SDR SIMA200708202](https://openairdocs.org/sdr/SIMA200708202.md): Unknown · smoke · Mar 21, 2007 · N712AE · Emb EMB135LR · Air Distribution System
  > SMOKE REPORTED IN CABIN AFTER NR 1 ENGINE START. PERFORMED VISUAL INSPECTION OF NR 1 ENGINE, APU AND BOTH PACKS WITH NO DEFECTS NOTED. PERFORMED ENGINE START OF NR 1 ENGINE. ALL PARAMETERS NORMAL WITH NO EICAS MESSAGES OR EVIDENCE OF SMOKE, RETURNED AIRCRAF
- [SDR SIMA200705707](https://openairdocs.org/sdr/SIMA200705707.md): Floorbeam · corroded · Feb 16, 2007 · N712AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200705706](https://openairdocs.org/sdr/SIMA200705706.md): Skin · dented · Feb 13, 2007 · N712AE · Emb EMB135LR · Fuselage Main, Plate/Skin
  > FOUND RIGHT NOSE SKIN DENTED BETWEEN STRINGER 13 RIGHT AND 16 RIGHT AND FRAMES 7 AND 8. PERFORMED RECONTOUR OF DENT, PERFORMED NDT. FABRICATED AND INSTALLED REPAIR DOUBLER. RESTORED PROTECTIVE FINISH IAW EMB IC2007-145/01083.
- [SDR SIMA200705101](https://openairdocs.org/sdr/SIMA200705101.md): Sill · corroded · Feb 13, 2007 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > BAGGAGE DOOR FRAME LOWER SILL FOUND CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINISH. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200704501](https://openairdocs.org/sdr/SIMA200704501.md): Sill · corroded · Feb 13, 2007 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED REPAIR AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINISH. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200630204](https://openairdocs.org/sdr/SIMA200630204.md): Flap System · malfunctioned · Oct 24, 2006 · N712AE · Emb EMB135LR · Trailing Edge Flap Control System
  > ON APPROACH SELECTED FLAPS 9, FLAPS STAYED AT 0 WITH ASSOCIATED EICAS MESSAGE "FLAP FAIL". NO CIRCUIT BREAKERS POPPED. COMPLIED WITH AIRCRAFT OPERATING MANUAL VOLUME 1, FLAP FAIL PROCEDURE. INFLIGHT EMERGENCY WAS DECLARED. (M)
- [SDR SIMA200519315](https://openairdocs.org/sdr/SIMA200519315.md): Floorbeam · corroded · Jul 7, 2005 · N712AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > THE GALLEY AREA FORWARD DIGITAL PREVIOUS REPAIR WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR, BLENDED THE DAMAGE AREA OF THE FORWARD DIGITAL TO REMOVE THE CORROSION FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200519314](https://openairdocs.org/sdr/SIMA200519314.md): Floor Support · corroded · Jul 7, 2005 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVE CORROSION FABRICATED A FILLER DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200317608](https://openairdocs.org/sdr/SIMA200317608.md): Floorbeam · corroded · Jun 23, 2003 · N712AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM LOEW FLANGE AND WEB WERE FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 20 AND 22. BLENDED THE DAMGE AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFEC
- [SDR SIMA200317604](https://openairdocs.org/sdr/SIMA200317604.md): Floorbeam · corroded · Jun 21, 2003 · N712AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING AN IMBV INSPECTION, FOUND CORROSOIN ON THE EXISTING REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED EXISTING REPAIR. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND INSTALLED. REPAIR DONE IAW EMB 145, SRM 145/1142 REV 22, 53-21-10 PARA 2
- [SDR SIMA200317401](https://openairdocs.org/sdr/SIMA200317401.md): Sill · corroded · Jun 18, 2003 · N712AE · 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 CENTER SILL, INSTALLED NEW CENTER SILL IAW EMB REPAIR STATEMENT IC2003-145/0818 AND STANDARD SRM, SRM 145/1142 REV 22 PRACTICES. (M)
- [SDR SIMA200307001](https://openairdocs.org/sdr/SIMA200307001.md): Odor · detected · Mar 10, 2003 · N712AE · Emb EMB135LR · Air Distribution System
  > CMH - FLT 4576 - AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED STRONG BURNING RUBBER ODOR. PERFORMED PNEUMATIC BLEED CHECK WITH BOTH ENGINES AND APU OPERATING AND RUN UP AT POWER SETTINGS. NO UNUSUAL ODOR WAS NOTED IN THE CABIN OR COCKPIT. AIRCRAFT WAS THEN
- [SDR SIMA200232907](https://openairdocs.org/sdr/SIMA200232907.md): Engine · malfunctioned · Nov 23, 2002 · N712AE · Emb EMB135LR · Engine (Turbine/Turboprop)
  > LGA - FLT 4401 - AFTER TAKEOFF, CREW REPORTED LAVATORY SMOKE MESSAGE ON EICAS AND SMOKE IN CABIN. APU ALREADY ON MEL. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SER
- [SDR SIMA200232906](https://openairdocs.org/sdr/SIMA200232906.md): Solenoid · malfunctioned · Nov 22, 2002 · N712AE · Emb EMB135LR · APU Engine Fuel and Control
  > CMH - FLT 4564 - AFTER TAKEOFF, CREW REPORTED SMELLING FUMES IN COCKPIT AND FLIGHT ATTENDANT REPORTED A HAZE IN THE CABIN LIKE A BURNING PLASTIC SMELL. MAINTENANCE FOUND THE APU HAD DUMPED ITS OIL INTERNALLY INTO THE AIR CONDITIONING SYSTEM. APU WAS PUT ON M
- [SDR SIMA200131805](https://openairdocs.org/sdr/SIMA200131805.md): Support · corroded · Nov 13, 2001 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED RAMP SUPPORT AND INSTALLED NEW RAMP IAW EMB 135/145 SRM 51-40-02. (M)
- [SDR SIMA200131806](https://openairdocs.org/sdr/SIMA200131806.md): Floor Support · corroded · Nov 13, 2001 · N712AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM GUSSET CORRODED. RAI SERVICEABLE GALLEY CENTER BEAM IAW EMB 135 SRM 51-40-02. (M)
- [SDR SIMA200130304](https://openairdocs.org/sdr/SIMA200130304.md): Floorbeam · corroded · Oct 25, 2001 · N712AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > DURING MBV INSPECTION, FOUND CORROSION ON THE GALLEY LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED FILLER AND DOUBLER. REPAIR DONE IAW EMB 145 (SRM 145/1142 CHAPTER 53 REV 15). 53-21-10, PAGE 204, FIG 201 AND STANDARD SRM PRACTICES. (
- [SDR SIMA200130303](https://openairdocs.org/sdr/SIMA200130303.md): Floorbeam · corroded · Oct 25, 2001 · N712AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > ABI - DURING MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE FORWARD DIGITAL IN GALLEY AREA. REMOVED CORROSION BY BLENDING IT OUT. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED REPAIR DOUBLER IAW EMB135 GST-3493/01 AN
- [SDR SIMA07817](https://openairdocs.org/sdr/SIMA07817.md): Rod · out of adj · Mar 19, 2001 · N712AE · Emb EMB145LR · Engine Thrust Reverser
  > ORD - FLT 4230 - DURING TAKEOFF ROLL, CREW NOTED T/REV DISAGREE MSG ON EICAS. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. NO FURTHER INCIDENTS WERE REPORTED. SYSTEM WAS LATER MEL''D. MAINTENANCE ADJUSTED NR 2 UPPER SHELL ACTUATOR ROD IAW ENGINEERING
- [SDR SIMA0737](https://openairdocs.org/sdr/SIMA0737.md): Relay · failed · Mar 14, 2001 · N712AE · Emb EMB145LR · Engine Thrust Reverser
  > ORD - FLT 4123 - DURING TAKEOFF ROLL, AFTER 80 KNOTS BUT PRIOR TO Y1 CREW RECEIVED THE NR 2 REVERSER DISAGREE MESSAGE. TAKEOFF WAS ABORTED. MESSAGE CLEARED DURING THE ABORT. MAINTENANCE REPLACED RELAY K0640. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETU
- [SDR SIMA2093](https://openairdocs.org/sdr/SIMA2093.md): Switch · malfunctioned · Jul 27, 2000 · N712AE · Emb EMB145LR · Engine Exhaust System
  > BOS - FLT 5172 - DURING TAKEOFF ROLL, CREW NOTED NR 2 THRUST REVERSER DISAGREE MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE. NO FURTHER INCIDENTS REPORTED. THRUST REVERSERS PUT ON MEL. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE STOW TRANSIT MICROSWITCHE

Next page: https://openairdocs.org/aircraft/N712AE/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 = 'N712AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N712AE/reports

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