# Service difficulty reports: N700LE, cancelled Nov 30, 2017 A list on [N700LE, cancelled Nov 30, 2017](https://openairdocs.org/deregistered/N700LE-2017-11-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SIMA200700308](https://openairdocs.org/sdr/SIMA200700308.md): Switch · failed · Dec 20, 2006 · N700LE · Emb EMB135LR · Elevator Tab Control System > FIRST OFFICER'S PITCH TRIM MAIN INOP MESSAGE ILLUMINATED ON CLIMB-OUT. AIRCRAFT DECLARED EMERGENCY. REMOVED AND REPLACED FIRST OFFICERS YOKE TRIM SWITCH IAW EMB AMM 27-40-03. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICED. - [SDR SIMA200633805](https://openairdocs.org/sdr/SIMA200633805.md): Wire Harness · damaged · Nov 29, 2006 · N700LE · Emb EMB135LR · Light System Wiring > BURNING SMELL NOTED COMING FROM MIDDLE ROW SEATS. REMOVED AND REPLACED HARNESS ASSEMBLY AT ROW 7A IAW EMB AMM 33-21-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. - [SDR SIMA200617302](https://openairdocs.org/sdr/SIMA200617302.md): Warning Message · false activation · Jun 21, 2006 · N700LE · Emb EMB135LR · Landing Gear Brake System > ON INITIAL POWER UP FOR TAKEOFF RECEIVED BRAKE DEGRADE EICAS MESSAGE. UPON ABORT OF TAKEOFF MESSAGE WENT AWAY UNTIL RESET FOR TAKEOFF. ONCE POWER WAS ADDED ABOVE IDLE POSITION, MESSAGE CAME BACK. PERFORMED INSPECTION OF ALL BRAKES, NO DEFECTS NOTED. NO BRA - [SDR SIMA200525225](https://openairdocs.org/sdr/SIMA200525225.md): Battery · discharged · Sep 8, 2005 · N700LE · Emb EMB135LR · Emergency Lighting > CLT - FLT 4892 - DURING PREFLIGHT, EMERGENCY LIGHT FROM ROW 7 FORWARD FAILED TO ILLUMINATE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR SIMA200507514](https://openairdocs.org/sdr/SIMA200507514.md): Sill · corroded · Mar 11, 2005 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED AFT SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 28, CHAPTERS 51-20-03 AND 51-40-02. (M) - [SDR SIMA200507513](https://openairdocs.org/sdr/SIMA200507513.md): Sill · corroded · Mar 11, 2005 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED FORWARD SILL. INSTALLED SERVICEABLE SILL IAW EMB 145 (SRM-145/1142 REV 28, CHAPTERS 51-20-03, 51-40-06 AND 51-40-02. (M) - [SDR SIMA200507512](https://openairdocs.org/sdr/SIMA200507512.md): Sill · corroded · Mar 10, 2005 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMIOVED - [SDR SIMA200508701](https://openairdocs.org/sdr/SIMA200508701.md): Floor Support · corroded · Mar 9, 2005 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORRODED SECTION. FABRICATED A FILLER, EXTERNAL ANGLE, SHIM AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10. (M) - [SDR SIMA200300811](https://openairdocs.org/sdr/SIMA200300811.md): Floorbeam · corroded · Dec 28, 2002 · N700LE · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY AREA CENTER BEAM HAS CORROSION AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 53-21-40. (M) - [SDR SIMA200300813](https://openairdocs.org/sdr/SIMA200300813.md): Support · corroded · Dec 28, 2002 · N700LE · Emb EMB135LR · Fuselage Main, Structure > ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION GALLEY AREA RAMP SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M) - [SDR SIMA200300604](https://openairdocs.org/sdr/SIMA200300604.md): Sill · corroded · Dec 28, 2002 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTER 51-40-02, 51-20-03, AND EMB 145 CPM 51-21-04 THROUG - [SDR SIMA200300605](https://openairdocs.org/sdr/SIMA200300605.md): Floorbeam · corroded · Dec 27, 2002 · N700LE · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - DURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 15.5 INCHES BY 21.25 INCH SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPAIR DOUBLER FOR FLANGE TO BE INSTALLED - [SDR SIMA200300603](https://openairdocs.org/sdr/SIMA200300603.md): Fitting · gouged · Dec 26, 2002 · N700LE · Emb EMB135LR · Vertical Stabilizer, Attach Fittings > ABI - DURING AN IMBV INSPECTION, VERTICAL STABILIZER FITTINGS THAT ATTACH TO THE HORIZONTAL STABILIZER WERE FOUND TO BE GOUGED. REMOVED GOUGES BY REAMING LEFT AND RIGHT FITTINGS TO 2.2834 INCH. REPAIR DONE IAW EMB GST-3689/02. (M) - [SDR SIMA200236302](https://openairdocs.org/sdr/SIMA200236302.md): Beam · corroded · Dec 20, 2002 · N700LE · Emb EMB135LR · Fuselage Main, Structure > ABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. PERFORMED TWO CUT OT OF DAMAGED AREAS. BOTH CUTOUT AREAS FALL WITHIN THE TOTAL LENGTH OF CUTOUT ALLOWED. FABRICATED A U-SHAPE EXTERNAL DOUBLER. REPAIR DONE - [SDR SIMA200300812](https://openairdocs.org/sdr/SIMA200300812.md): Floorbeam · corroded · Dec 18, 2002 · N700LE · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - THIS IS A LEVEL 2 FINDING DURING AN IMBV INSPECTION, GALLEY AREA AFT DIGITAL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE DIGITAL IAW EMB 145 SRM 51-40-02. (M) - [SDR SIMA200300814](https://openairdocs.org/sdr/SIMA200300814.md): Sill · corroded · Dec 18, 2002 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION GALLEY AREA LEFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M) - [SDR SIMA200300815](https://openairdocs.org/sdr/SIMA200300815.md): Sill · corroded · Dec 18, 2002 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION SERVICE DOOR AFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M) - [SDR SIMA200300816](https://openairdocs.org/sdr/SIMA200300816.md): Beam · corroded · Dec 18, 2002 · N700LE · Emb EMB135LR · Fuselage Main, Structure > ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT OMEGA BEAM DOUBLER BETWEEN FRAME 65 AND 68 CORRODED. REMOVED AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-40-02. (M) - [SDR SIMA200300817](https://openairdocs.org/sdr/SIMA200300817.md): Sill · corroded · Dec 18, 2002 · N700LE · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - THIS IS LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION SERVICE DOOR FORWARD SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-14-02. (M) - [SDR SIMA200206201](https://openairdocs.org/sdr/SIMA200206201.md): Proximity Switch · failed · Mar 2, 2002 · N700LE · Emb EMB135LR · Landing Gear Position and Warning > RDU - FLT 4879 - RIGHT MAIN GEAR UNSAFE INDICATION ON APPROACH INTO RDU. CREW PERFORMED CHECKLIST. GEAR STILL SHOWING UNSAFE. LANDED WITHOUT INCIDENT HAD GEARS PINNED BEFORE EXITING RUNWAY. RAI CHANNEL A PROX SWITCHES ON RIGHT AND LEFT MLG IAW AMM 32-61-02 - [SDR SIMA200115803](https://openairdocs.org/sdr/SIMA200115803.md): Switch · failed · Jun 7, 2001 · N700LE · Emb EMB135LR · Engine Noise Suppressor > DFW - FLT 3423 - NR 1 THRUST REVERSER DISAGREE DURING TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LOWER INBOARD UPPER OUTBOARD STOW SWITCH IAW EMB AMM 78-34-01-000. OPS CHECK GOOD. (M) - [SDR SIMA200115703](https://openairdocs.org/sdr/SIMA200115703.md): Warning System · malfunctioned · Jun 6, 2001 · N700LE · Emb EMB135LR · Engine Thrust Reverser > SAV - FLT 3478 - ABORTED TAKEOFF. THRUST REVERSE DISAGREE ICAS MESSAGE. PERFORMED OPS CHECKS AND HIGH SPEED RUNS IAW AMM. OPS CHECK GOOD. COULD NOT DUPLICATE. (M) - [SDR SIMA200115621](https://openairdocs.org/sdr/SIMA200115621.md): Warning System · false indication · Jun 5, 2001 · N700LE · Emb EMB135LR · Engine Thrust Reverser > MKE - FLT 3276 - THRUST REVERSER DISAGREE ON TAKEOFF ROLL ALONG WITH NO TAKEOFF CONFIG ON EICAS. COMPLETED HIGH SPEED TAXI AND THRUST REVERSER OPS CHECK IAW AMM 78-31-01. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR SIMA20011171](https://openairdocs.org/sdr/SIMA20011171.md): Floorbeam · corroded · Apr 21, 2001 · N700LE · Emb EMB135ER · Fuselage Main, Floor Beam > ABI - MAINTENANCE REPORTED THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 23 AND 25. MAINTENANCE REPAIRED DAMAGE IAW EMB SRM AND REPAIR STATEMENT GST 1298/01. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA20011172](https://openairdocs.org/sdr/SIMA20011172.md): Floorbeam · corroded · Apr 21, 2001 · N700LE · Emb EMB135ER · Fuselage Main, Floor Beam > ABI - MAINTENANCE FOUND THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. MAINTENANCE REPAIRED FRAME IAW EMB SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA0091](https://openairdocs.org/sdr/SIMA0091.md): Smoke Detector · malfunctioned · Jan 9, 2001 · N700LE · Emb EMB135ER · Smoke Detection > ORD - FLT 4433 - CREW REPORTED THAT AFTER TAKEOFF LAV SMOKE WARNING CAME ON EICAS. CREW FOLLOWED AOM PROCEDURE AND RETURNED TO ORD. LAV SMOKE WARNING LIGHT WENT OUT DURING APPROACH, BUT NOTED NO BURNING SMELL IN LAV AREA. REMOVED AND REPLACED LAV SMOKE DETE - [SDR SIMA0093](https://openairdocs.org/sdr/SIMA0093.md): Smoke Detector · malfunctioned · Jan 9, 2001 · N700LE · Emb EMB135ER · Smoke Detection > ORD - FLT 4127 - LAVATORY SMOKE INDICATION CAME ON DURING CLIMB-OUT. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) - [SDR SIMA2321](https://openairdocs.org/sdr/SIMA2321.md): Unknown · odor · Aug 19, 2000 · N700LE · Emb EMB135ER · Air Distribution System > CMH - FLT 5169 - CREW DETECTED AN OIL ODOR IN THE COCKPIT. OIL PRESSURE SENSOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. (X) - [SDR SIMA1744](https://openairdocs.org/sdr/SIMA1744.md): Unknown · odor · Jun 22, 2000 · N700LE · Emb EMB135ER · Air Distribution System > MSN - FLT 4116 - UPON LANDING, CREW NOTED FOG/SMOKE IN CABIN AREA WITH OILY SMELL AND LAV SMOKE INDICATION. CREW TAXIED TO GATE, NO FIRE BOTTLES WERE USED. NO FURTHER INCIDENTS WERE REPORTED. APU PUT ON MEL AT THIS TIME. (M) - [SDR SIMA0923](https://openairdocs.org/sdr/SIMA0923.md): Light · inoperative · Apr 1, 2000 · N700LE · Emb EMB135ER · Emergency Lighting > CMH - FLT 4980 - EMERGENCY FLOOR LIGHTING INOPERATIVE ON CENTER SECTION. REMOVED AND REPLACE DLIGHT STRIP. OPS CHECK GOOD. (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 = 'N700LE' AND deregistration_id = 'N700LE-2017-11-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N700LE-2017-11-30/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.