N708AE, cancelled Sep 9, 2019

Service difficulty reports · 33

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SIMA200827304Unknown · odorON 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 RETURNEDSep 27, 2008 · N708AE · Emb EMB135LR · Air Distribution SystemSDR SMIA200806501Contactor · inoperativeON 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 CMar 2, 2008 · N708AE · Emb EMB135LR · Light System WiringSDR SIMA200733909Battery · inoperativeFORWARD SECTION OF EMERGENCY STRIP LIGHTS INOP. REMOVED AND REPLACED NUMBER 1 AND 2 BATTERY’S AIRCRAFT RETURNED TO SERVICE.Dec 3, 2007 · N708AE · Emb EMB135LR · Emergency LightingSDR SIMA200709913Floorbeam · corrodedCENTER 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.Apr 6, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200709910Floorbeam · corrodedLEFT 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.Apr 3, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200709402Sill · corrodedSERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.Mar 31, 2007 · N708AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200709403Floorbeam · corrodedLEFT 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.Mar 28, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200709203Floorbeam · corrodedRIGHT FLOORBEAM SUPPORT FOUND CORRODED IN GALLEY AREA. REMOVED AND REPLACED SUPPORT IAW EMB SRM 51-40-02. OPERATIONAL CHECK GOOD.Mar 27, 2007 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200709202Bearing Cap · corrodedNOSE LANDING GEAR LEFT BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20-01. RETURNED AIRCRAFT TO SERVICE.Mar 27, 2007 · N708AE · Emb EMB135LR · Nose/Tail Landing GearSDR SIMA200633108Control Unit · faultyPITCH 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.Nov 26, 2006 · N708AE · Emb EMB135LR · Stabilizer Control SystemSDR SIMA200605801Windshield · crackedNR 2 WINDSHIELD SHATTERED DURING DESCENT. REPLACED NR 2 WINDSHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)Feb 23, 2006 · N708AE · Emb EMB135LR · Flight Compartment WindowsSDR SIMA200311805Floorbeam · corrodedDURING 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 EApr 23, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200311315Frame · damagedDURING 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.Apr 22, 2003 · N708AE · Emb EMB135LR · Fuselage Main, FrameSDR SIMA200311804Frame · damagedDURING 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)Apr 22, 2003 · N708AE · Emb EMB135LR · Fuselage Main, FrameSDR SIMA200311803Stringer · chafedABI - 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 STAApr 21, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR SIMA200311311Floorbeam · corrodedDURING 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, Apr 19, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200311314Beam · corrodedDURING 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 14Apr 18, 2003 · N708AE · Emb EMB135LR · Fuselage Main, StructureSDR SIMA200311313Sill · corrodedDURING 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)Apr 17, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200311312Floorbeam · corrodedABI - 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 CHAApr 17, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200312709Support · corrodedTHIS 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)Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200312708Support · corrodedPASSENGER DOOR OPENING FORWARD THRESHOLD SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M)Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200312707Gusset · corrodedABI - 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)Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Main, StructureSDR SIMA200312705Beam · corrodedTHIS 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)Apr 16, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200312710Gusset · corrodedTHIS 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)Apr 15, 2003 · N708AE · Emb EMB135LR · Fuselage Main, StructureSDR SIMA200312706Structure · corrodedTHIS 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)Apr 15, 2003 · N708AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200123428Floorbeam · corrodedABI - 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)Aug 22, 2001 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200123420Floorbeam · corrodedABI - 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)Aug 20, 2001 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200116003Control Unit · failedYQB - 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 EMBJun 9, 2001 · N708AE · Emb EMB135LR · Trailing Edge Flap Control SystemSDR SIMA20011426RadomeORD - 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 GOODMay 22, 2001 · N708AE · Emb EMB135LR · Inertial Guidance SystemSDR SIMA3493Sensor · malfunctionedLGA - 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 REPORDec 14, 2000 · N708AE · Emb EMB135ER · Overheat DetectionSDR SIMA1633Windshield · crackedCLE - 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 56-10-01-40Jun 11, 2000 · N708AE · Emb EMB135ER · Flight Compartment WindowsSDR SIMA1412Warning System · false indicationORF - 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 TMay 20, 2000 · N708AE · Emb EMB135ER · Emergency ExitsSDR SIMA200004902Hydraulic Line · leakingORD - 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)Feb 18, 2000 · N708AE · Emb EMB135ER · Hydraulic System, Main
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