N638AE

Service difficulty reports · 156

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 = 'N638AE' AND registry_match = 'registration'
  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 SIMA20130423006Cradle · brokenDURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTIAN’S EMERGENCY FLASHLIGHT CRADLE IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WApr 23, 2013 · N638AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20130125002Switch · looseFOR FLIGHT 4110 THE CREW REPORTED THE EMERGENCY LIGHT ARMING SWITCH WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED JAM NUT ON EMERGENCY LIGHT ARM SWITCH IAW STANDARD MTX PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 25, 2013 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20130121001Connector · looseDURING B INSPECTION FOUND THE FORWARD FACING CENTER AISLE EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED LOOSE CONNECTION ROW 12 FORWARD CEILING EXIT MARKING SIGN IAW EMB AMM 33-50-15-000-801/33-50-15-400-801. COMPLIED WITH EJan 21, 2013 · N638AE · Emb EMB145LR · Light System WiringSDR SIMA20121206008Flashlight · inoperativeON FLIGHT 3536 THE CREW REPORTED THE CRADLE AND FLASHLIGHT BEHIND THE CAPTAIN’S SEAT WAS INOPERABLE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 6, 2012 · N638AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20121206005Flashlight · inoperativeON FLIGHT 3536 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FIRST OFFICER’S FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW AMM 25-60-00. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 6, 2012 · N638AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20121206002Battery · dischargedON FLIGHT 9513 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BATTERY AS PER EMB 145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS Dec 6, 2012 · N638AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20120831002Battery Pack · unserviceableFOR FLIGHT 3546 THE CREW REPORTED THAT WHEN THEY ARRIVED AT THE AIRCRAFT THE EMERGENCY LIGHTS WERE ON. THE AIRCRAFT HAD BEEN UNOCCUPIED FOR AT LEAST 25 MINUTES AND COULD NOT DETERMINE STATUS OF THE EMERGENCY LIGHT BATTERIES. THE AIRCRAFT WAS REMOVED FROM SERAug 31, 2012 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20120814001Seal · dirtyFLIGHT 4361, FLIGHT ATTENDANT UNABLE TO CLOSE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED CABIN DOOR SEAL IAW EMB 145 AMM 52-18-00. OPS CHECKED GOOD. THE AIRCRAFT RETURNED TO SERVICE.Aug 14, 2012 · N638AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20120713002Lamp · inoperativeDURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB ON THE LEFT OVERWING IAW AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. OPS CHECKED GOOD. AIRCRAFTJul 13, 2012 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20120528002Battery Pack · inoperativeDURING B INSPECTION, FOUND THE AISLE EMERGENCY EXIT SIGN FORWARD SIDE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.May 28, 2012 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20120526004Bulb · inoperativeDURING B INSPECTIONS, FOUND THE NUMBER 4 AISLE EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 AISLE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.May 26, 2012 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20120517004Light · not seatedDURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT IN AISLE CEILING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED BULB IN AFT EMERGENCY EXIT AISLE CEILING AS REQUIRED. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOODMay 17, 2012 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20120423010Mount Fitting · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT LOWER YOKE 1 FORWARD ENGINE MOUNT FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO-EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.May 4, 2012 · N638AE · Emb EMB145LR · Engine Mount SectionSDR SIMA20120423011Charger · brokenDURING B INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT CHARGER HAS BROKEN HOLDING BRACKET/BASE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT CHARGER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS Apr 23, 2012 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA20120402002Connector · failedON FLIGHT 2736 THE CREW REPORTED ON TAKEOFF REQUIRED A SIGNIFICANT AMOUNT OF RIGHT RUDDER AND THEN HEARD A CLANKING NOISE AT ROTATION, ON LANDING RUDDER CONTROL FELT NORMAL. THE CREW DECLARED AN EMERGENCY AND CALLED CRASH, FIRE AND RESCUE FOR LANDING. THE AIApr 2, 2012 · N638AE · Emb EMB145LR · Landing Gear System WiringSDR SIMA201205402Tire · damagedON FLIGHT 2716 THE CREW REPORTED THAT AT ROTATION HEARD A LOUD GRINDING NOISE SOUND FROM NOSE WHEEL AND FELT AND SOUNDED LIKE THE TIRE WAS COMING APART. THE FLIGHT ATTENDANT ALSO CONFIRMED THE NOISE AS WELL. THE CREW ELECTED TO RETURN FOR LANDING. AFTER GFeb 22, 2012 · N638AE · Emb EMB145LR · TireSDR SIMA201134205Power Supply · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE RIGHT EXTERIOR FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 8, 2011 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA2011327005Mechanism · lack of lubeON FLIGHT 3475 THR CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO LOCK AND UNLOCK. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED EXTERNAL MECHANISM OF MAIN CABIN DOOR IAW EMB 145 AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNEDNov 23, 2011 · N638AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA201124103Warning System · false activationON FLIGHT 3988 DURING THE CLIMBOUT THE CREW REPORTED, RECEIVED A BRAKE OVERHEAT MESSAGE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED MAIN BRAKE TEMPERATAug 26, 2011 · N638AE · Emb EMB145LR · Landing Gear Brake SystemSDR SIMA201123002Roller · obstructedON FLIGHT 4330 THE CREW REPORTED THE MAIN CABIN DOOR IS EXTREMELY HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEBRIS FROM MAIN PASSENGER DOOR SEAL AND LUBED ROLLERS IAW EMB145 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVEDAug 17, 2011 · N638AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA201122705Seal · dirtyMAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. CLEANED DEBRIS FROM MAIN CABIN DOOR SEAL AND LUBED WITH REFERENCE TO EMB-145 AMM 52-18-00. OPS CHECKS GOOD.Aug 12, 2011 · N638AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA201117809Door · malfunctionedON FLIGHT 3975 THE CREW REPORTED THE CABIN DOOR HARD TO CLOSE. THE RED LINES ON THE LEFT SIDE OF CABIN DOOR DO NOT MATCH UP. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF MAIN CABIN DOOR IN A EMB AMM 52-18-00. THE OPERATIONAL TEST WAJun 26, 2011 · N638AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA201113608Sleeve · defectiveON FLIGHT 2765 THE CREW REPORTED, RECEIVED A PACK 1 OVERLOAD CAUTION MESSAGE. THE CAPTAIN ELECTED TO DIVERT TO SGF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SLEEVE AND CLAMP ON THE DUAL HEAT EXCHMay 14, 2011 · N638AE · Emb EMB145LR · Cabin Cooling SystemSDR SIMA201109409Smoke Detector · faultyON FLIGHT 2793 UPON LANDING THE CREW REPORTED, RECEIVED A BAGGAGE SMOKE WARNING MESSSAGE. THE BAGGAGE EXTINGUISHER BUTTON WAS PRESSED. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AND AFT CARGO Apr 1, 2011 · N638AE · Emb EMB145LR · Smoke DetectionSDR SIMA201020202Unknown · odorON FLIGHT 3332 THE CREW REPORTED A BURNING OIL ODOR IN THE COCKPIT DURING THE TAKEOFF ROLL & CLIMBOUT. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS REMOVED FROM SERVICE. PERFORMED BLACKLIGHT AND BRIGHT LIGHT INSPECTION. CW ETN EM-72-034 R4 ENGINE ODOR EVENTJul 20, 2010 · N638AE · Emb EMB145LR · Air Distribution SystemSDR SIMA201017501Pressure Switch · inoperativeON FLIGHT 3310 THE CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW, RECEIVED A RUDDER SYSTEM 1 AND 2 FAIL AND AUTOPILOT FAIL MESSAGE. THE CAPTAIN ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ANJun 22, 2010 · N638AE · Emb EMB145LR · Rudder Control SystemSDR SIMA201016901Rivet · misinstalledDURING MAINTENANCE BASE INSPECTION FOUND THE PREVIOUS REPAIR BETWEEN FRAMES 27-28 AT STRINGER 21 RIGHT HAD IMPROPERLY INSTALLED RIVETS THAT ARE AGAINST STRINGER 21 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1574 FOR THE INSTALLATIOJun 17, 2010 · N638AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA201016804Wire · brokenDURING MAINTENANCE BASE VISIT FOUND THE LEFT NR 3 EMERGENCY LIGHT STRIP HAS A BROKEN A WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 17, 2010 · N638AE · Emb EMB145LR · Light System WiringSDR SIMA201016902Angle · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE GALLEY RAMP ON THE LEFT BEAM CORRODED FORWARD OF FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED GALLEY RAMP ON THE LEFT BEAM FORWARD OF FRAME 20 AND INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51Jun 15, 2010 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200921103Engine · power lossON FLIGHT 3996 CREW REPORTED IN CRUISE ENGINE 2 ROLL BACK OCCURRED. AIRCRAFT RETURNED TO CHA. AIRCRAFT LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. ISSUED MEL 78-1, PER FLIGHT DATA RECORDER, DATA READOUT TESTED ENGINE 2 THRUST REVERSER FADEC INTERFACE WIRJul 28, 2009 · N638AE · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200920801Connector · damagedON FLIGHT 4136 - CREW REPORTS SHORTLY AFTER TAKEOFF RECEIVED A SMOKE IN LAV INDICATION ON EICAS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CONNECTOR ON ENGINE 1 FIRE BOTTLE. AIRCRAFT RETURNED TO SERVICE.Jul 25, 2009 · N638AE · Emb EMB145LR · Fire Protection System WiringSDR SIMA200826803Solenoid Valve · malfunctionedON FLIGHT 3942 CREW REPORTED AT 22,000 FT .77 MACH GEAR UNSAFE MSG ON EICAS. GEAR DOOR OPEN. CREW DECLARED EMERGENCY INTO ORD AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A REPLACED NLG DOOR SOLENOID VALVE. IAW EMB 145 AMM 32-33-02. OPS CHECKSep 22, 2008 · N638AE · Emb EMB145LR · Landing Gear Door Retract SectionSDR SIMA200822203Engine · malfunctionedON FLIGHT 3457 - CREW REPORTED TWO TIMES DURING FLIGHT E2 N1 DROPPED TO IDLE (N1-60 PRECENT AND N1-72-73 PERCENT) WITH NO INDICATION ON EICAS. (S)Aug 8, 2008 · N638AE · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200812110Controller · malfunctionedON FLIGHT 4306, CREW REPORTED WHILE CLIMBING THRU 19000 THEY RECEIVED CABIN ALT WARNING AND AURAL WARN. CREW REQUESTED EMERGENCY DESCENT TO 10000 AND RETURNED TO CVG. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW Apr 28, 2008 · N638AE · Emb EMB145LR · Cabin Pressure ControllerSDR SIMA200811902Control Valve · malfunctionedON FLIGHT 4331, CREW REPORTED SMOKE IN CABIN BEFORE BOARDING WITH APU RUNNING. AIRCRAFT REMOVED FROM SERVICE. FOUND MAIN DISTRIBUTION DUCT OVERHEATED. REMOVED AND REPLACED MAIN DISTRIBUTION DUCT, DUAL TEMP CONTROL VALVE, PACK OVER TEMP SWITCH IAW AMM 21-51-Apr 24, 2008 · N638AE · Emb EMB145LR · Cabin Temperature Control SystemSDR SIMA200435818Sill · corrodedDURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED DOOR SILL TO REMOVE CORROSION. FABRICATED AN INTERNAL DOUBLER. REPAIR DONE IAW AEA. (SW21200501984) (K)Dec 21, 2004 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200435817Floor Support · corrodedDURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR FROME THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DOEN IAW SRM. (SW21200501984) (K)Dec 21, 2004 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200435816Floorbeam · corrodedDURING AN MBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED DIGITAL TO REMOVED CORROSION. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200501984) (K)Dec 20, 2004 · N638AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200419405Power Supply · inoperativeORD - FLT 4065 - FOUND EMERGENCY EXIT LIGHTS ON BOTH WALLS NEAR OVERWING EMERGENCY EXITS ARE INOPERATIVE. REPLACED EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jul 9, 2004 · N638AE · Emb EMB145LR · Emergency LightingSDR SIMA200304808Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED EXISTING SHIM AND DOUBLERS. REMOVED SECTION OF THE FORWARD DIGITAL. FABRICATED TWO DOUBLERS AND SHIMS. PREPARED NEW SECTION STRAP.Feb 7, 2003 · N638AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200304102Floorbeam · corrodedDURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGE AREA TO COMPLETELY REMOVE THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REPAIR AREA. FABRICATED A U-SHAPED DOUBLER. REPAIR DOFeb 1, 2003 · N638AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200304809Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGE AREA TO COMPLETELY REMOVE THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REPAIR AREA. FABRICATED A U-SHAPED DOUBLER. REPFeb 1, 2003 · N638AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200305014Gusset · corrodedDURING AN IMBV INSPECTION A LEVEL 2 FINDING FOUND LAVATORY CENTER BEAM GUSSET CORRODED. REMOVED AND REPLACED LAVATORY CENTER GUSSET IAW EMB 145 SRM 51-40-02. (M)Jan 30, 2003 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200305010Seat Track · corrodedABI - DURING IMBV INSPECTION A LEVEL 2 FINDING FOUND, LEFT LOWER FORWARD NR 1 SEAT TRACK CORRODED AROUND HARDWARE. REMOVED AND INSTALLED LEFT LOWER NR 1 SEAT TRACK IAW EMB 145 SRM 53-01-06. (M)Jan 30, 2003 · N638AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200304807Sill · corrodedABI - DURING AN IMBV INSPECTION, THE CARGO OPENING LOWER CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CARGO LOWER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-20-03, 51-40-02, 51-40-Jan 27, 2003 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200305013Sill · corrodedABI - DURING AN IMBV INSPECTION A LEVEL 2 FINDING WAS FOUND. CORROSION ON SERVICE DOOR AFT SILL. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M)Jan 25, 2003 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200305015Sill · corrodedABI - DURING AN IMBV INSPECTION A LEVEL 2 FINDING WAS FOUND. CORROSION ON LEFT SILL BETWEEN FRAME 19 AND 23. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-02, 51-40-06. (M)Jan 25, 2003 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200305012Doubler · corrodedDURING IMBV INSPECTION, A LEVEL 2 FINDING WAS FOUND. CORROSION ON DIAMOND DOUBLER ON RIGHT HAT BEAM AT FRAME 22. INSTALLED SERVICEABLE DIAMOND DOUBLER IAW EMB 145 SRM 51-20-01, 51-20-03 AND 51-40-02, 51-40-04, 51-40-06. (M)Jan 25, 2003 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200305011Doubler · corrodedABI - DURING IMBV INSPECTION A LEVEL 2 FINDING FOUND. DIAMOND DOUBLER ON RIGHT HAT BEAM AT FRAME 20 CORRODED. INSTALLED NEW DIAMOND DOUBLER IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-40-06. (M)Jan 25, 2003 · N638AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20011403Skin · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD DIGITAL CORRODED. CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW EMB GST-1595/01. (M)May 18, 2001 · N638AE · Emb EMB145LR · Fuselage Structure (General)
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