EXPRESSJET AIRLINES LLC

Operated by ExpressJet Airlines (per NTSB report)

The tractor driver's failure to give way to the taxiing airplane.

Operated by EXPRESSJET AIRLINES INC (per NTSB report)

the failure of flight 908's captain to ensure adequate clearance between the wingtip of his airplane and flight 4226's empennage when he attempted to pass behind the other airplane.

Operated by EXPRESSJET AIRLINES INC (per NTSB report)

The uncommanded left deflection of the airplane's nose wheel due to a malfunction of the electrohydraulic servo valve (EHSV) within the nose wheel steering manifold assembly. The reason for the malfunction could not be determined; however, a foreign substance was found between the armature and coil of the EHSV that once removed improved the performance of the unit. It is unknown how the foreign substance was introduced to this location.

Operated by EXPRESSJET AIRLINES INC (per NTSB report)

The uncommanded left deflection of the airplane's nose wheel likely due to seal deterioration and subsequent contamination within the Electrohydraulic Servo Valve (EHSV). Contributing to the incident was the undersized condition of the filter plugs within the EHSV which likely caused the C2 orifice filter seal to extrude and deteriorate.

Operated by EXPRESSJET AIRLINES INC (per NTSB report)

the Gulfport control tower local controller cleared two aircraft for takeoff from runways with intersecting departure flight paths without ensuring the first aircraft had passed the flight path intersection prior to clearing the second aircraft for takeoff.

Operated by EXPRESSJET AIRLINES INC (per NTSB report)

The pilots' lack of consideration for developing and known weather conditions en route to and at the destination airport, resulting in a runway excursion and subsequent incursion.

Operated by EXPRESSJET AIRLINES INC (per NTSB report)

An in-flight encounter with lightning. Contributing to the incident was the damaged and displaced tailcone bulkhead frame that inhibited the full travel of the elevator during approach.

Operated by ExpressJet Airlines Inc. (per NTSB report)

The captain's failure to attain a proper touchdown on runway, and his subsequent failure to perform a go-around, both of which resulted in a runway overrun. Factors were the company's inadequate dispatch procedures with their failure to provide all NOTAMS for the airport to the flight crew, and the snow covered runway.

Sanction: $72,000 · case closed 2019-06-12

Sanction: $67,500 · case closed 2016-09-26

Sanction: $48,750 · case closed 2015-07-16

Sanction: $105,000 · case closed 2016-11-14

Sanction: $5,000 · case closed 2015-04-06

Sanction not stated · case closed 2013-02-26

Sanction: $11,000 · case closed 2013-05-07

Sanction: $25,000 · case closed 2013-02-26

Sanction: $22,000 · case closed 2013-08-07

Sanction: $10,000 · case closed 2011-12-07

Sanction: $10,000 · case closed 2011-12-07

Sanction: $20,000 · case closed 2011-12-07

Sanction: 3500 · case closed 2012-02-06

Sanction: $8,750 · case closed 2011-10-27

Sanction: $8,750 · case closed 2011-10-27

Sanction: $8,750 · case closed 2011-10-27

Sanction: $5,000 · case closed 2011-08-16

Sanction: $10,374 · case closed 2011-06-01

Sanction: $38,000 · case closed 2010-12-01

Sanction: $16,000 · case closed 2010-09-14

Sanction: $2,000 · case closed 2008-10-23

Sanction: $1,850 · case closed 2009-03-11

Sanction: $70,000 · case closed 2010-05-27

Sanction: $1,000 · case closed 2009-03-11

Sanction: $2,500 · case closed 2009-03-11

Sanction: $3,600 · case closed 2008-01-08

Sanction: $7,000 · case closed 2008-01-24

Sanction: $11,000 · case closed 2007-01-31

Sanction: $6,000 · case closed 2007-04-17

Sanction: $675 · case closed 2006-03-20

Sanction: $8,000 · case closed 2006-04-19

Sanction: $3,500 · case closed 2006-04-19

Sanction: $15,000 · case closed 2005-06-02

Sanction: $2,500 · case closed 2005-07-20

Sanction: $5,000 · case closed 2005-02-24

Sanction: $8,250

Sanction: $8,500 · case closed 2005-06-03

Sanction: $1,000 · case closed 2005-07-20

Sanction: $11,000

Sanction: $20,000 · case closed 2005-06-23

Sanction: $6,000 · case closed 2004-07-30

Sanction: $10,000 · case closed 2004-07-30

Sanction: $20,000 · case closed 2004-07-16

Sanction: $95,000 · case closed 2004-07-08

Sanction: $3,000 · case closed 2003-09-09

Sanction: $650 · case closed 2003-09-09

Sanction: $5,000 · case closed 2003-09-09

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 30,230 hrs · 28,049 cycles

DEFECT - ROW 9 AND 20 SIDEWALL LIGHT INOPERATIVE. LH FWD EMERGENCY LIGHT INOPERATIVE. COURTESY LIGHTS IN GALLEY INOPERATIVE. RESOLUTION - REMOVED AND REPLACED SIDEWALL LIGHTS IN ACCORDANCE WITH EMB145 AMM 33-21-06. REMOVED AND REPLACED EMERGENCY LIGHT IN ACCORDANCE WITH EMB 145 AMM 33-50-10. REMOVED AND REPLACED COURTESY LIGHTS FOR SERVICE DOOR IN ACCORDANCE WITH EMB145 AMM 33-26-05.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 36,411 hrs · 33,371 cycles

DEFECT - RH OVER WING EMERGENCY LIGHT INOPERATIVE. CORRECTIVE ACTION - REPLACED LAMP PER EMB-145 AMM 33-50-10 OPS CHECK GOOD.

Part: BRAKE — ABNORMAL · airframe 36,383 hrs · 33,346 cycles

DISCREPANCY - ON LANDING APPLIED FULL BRAKE PRESSURE AND DIDN'T FEEL ANY BRAKING. BRAKE TEMPS OUTBOARD LEFT - HOT, INBOARD LEFT - COLD, INBOARD RIGHT - COLD, OUTBOARD RIGHT - HOT. CORRECTIVE ACTION - INSPECTED BRAKES AND BLED MAIN LANDING GEAR BRAKES IN ACCORDANCE WITH EMB 145 AMM 32-40-00-800-801-A, OPERATION AND LEAK CHECK GOOD. PERFORMED HIGH ENERGY BRAKING WITH EXPRESSJET FLIGHT OPS. NO DEFECTS NOTED. NO FURTHER MAINTENANCE ACTION REQUIRED. AIRCRAFT OKAY FOR RETURN TO SERVICE.

Part: BRAKE SYS — WEAK (ZONE 700) · airframe 36,379 hrs · 33,344 cycles

DISCREPANCY - ANTI-SKID CATCHES ON APPLICATION OF BRAKES, FULL BREAKING NOT FELT. LEFT CALIPER ON BOTH MAINS GOT REALLY HOT ( RE BREAK TEMPERATURE INDICATORS) BUT RIGHT CALIPER TEMPERATURES HARDLY ROSE UNDER FULL BREAKING ACTION. CORRECTIVE ACTION - TROUBLESHOT BRAKE SYSTEM WITH FIELD ANALYZER REFERENCE EMB 145 FIM 32-41-00-810-824-A, REPLACED OB BRAKE CONTROL VALVE REFERENCE EMB 145 AMM 32-41-06-000/401-801-A. BLED BRAKE SYSTEM REFERENCE EMB 145 AMM 32-40-00-800-801. OPERATIONAL CHECK BRAKE SYSTEM REFERENCE EMB 145AMM 32-41-00-700-801. OPERATIONAL CHECK GOOD.

Part: LIGHT — NO TEST (ROW 18A) · airframe 44,871 hrs · 27,938 cycles

EMERGENCY EXIT LIGHT AT ROW 18A, LT OVER WING EMERGENCY EXIT FAILED OPERATIONAL CHECK.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,371 hrs · 29,027 cycles

AIRCRAFT RIGHT HAND SERVICE DOOR, BELOW THRESHOLD, CORROSION ALONG DOOR FRAME.

Part: CONTROL CABLE — FRAYED (RUDDER) · airframe 31,370 hrs · 29,027 cycles

FOUND RIGHT HAND RUDDER CONTROL CABLE FRAYED AND PULLY DAMAGED.

Part: SKIN — DISTORTED (FRM19-20 S11-12L) · airframe 29,924 hrs · 27,714 cycles

DISCREPANCY - LEFT HAND SIDE FUSELAGE JUST AFT OF ENTRY DOOR AND FORWARD OF REPAIR HAS "OIL CANNING" AND DISTORTION THAT IS APPROXIMATELY 2 INCH'S SQUARE. CORRECTIVE ACTION - REPAIRED LEFT HAND SIDE FUSELAGE JUST AFT OF ENTRY DOOR IN ACCORDANCE WITH EMB 145 SRM 51-75-00. THE DAMAGE REPAIR WAS CLASSIFIED AS A MAJOR REPAIR AND IS LOCATED ON THE CENTER FUSELAGE I, LEFT HAND FUSELAGE SKIN BETWEEN FRAMES FR19L & FR20L AND STRINGERS STR11L & STR12L.

Part: CONTROL MODULE — SMOKE (CABIN LIGHTS) · airframe 36,650 hrs · 22,805 cycles

IAH FLIGHT 3907. THE CREW REPORTED AN ELECTRICAL SMOKE ODOR IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (SEATS 19A-21A) · airframe 44,202 hrs · 27,402 cycles

MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY FOR SEATS 19A-21A. OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 44,202 hrs · 27,402 cycles

BHM-FLIGHT 4369, THE CREW REPORTED SMELL OF SMOKE AND VISIBLE SMOKE ON SIDEWALL LIGHT PANEL 20A WITH A VISIBLE BURN MARK. THE AIRCRAFT LANDED IN BHM WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. DEACTIVATED LIGHT ASSEMBLY AT SEAT 20A AND PLACE IN MEL 33-20-00-2 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR FILED OPEN PENDING FINAL CORRECTIVE ACTION.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,796 hrs · 21,934 cycles

IAH-FLIGHT 3916 THE EMERGENCY EXIT SIGN NEAR SEAT 1A WAS REPORTED AS COMING OFF AND WOULD NOT LIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER, REINSTALLED THE EXIT SIGN, AND OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,371 hrs · 24,239 cycles

FLIGHT 4087, DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS AT THE FA SEAT AND EMERGENCY EXIT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,371 hrs · 24,239 cycles

FLIGHT 4087, DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS AT THE FA SEAT AND EMERGENCY EXIT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,722 hrs · 21,892 cycles

CREW REPORTED MID CABIN OVERHEAD EMERGENCY LIGHT BURNED OUT. MAINTENANCE REPLACED MID CABIN OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 39,363 hrs · 31,216 cycles

FLIGHT 3914, DURING MAINTENANCE INSPECTION THE #2 EMERGENCY LIGHT BATTERY PACK PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — SEPARATED (RT MLG) · airframe 43,785 hrs · 34,243 cycles

FLIGHT 3990, DURING CLIMB THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE. AIRCRAFT RETURNED DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RT MLG SIDE STRUT LOWER STRUT ASSEMBLY TO BE SEPARATED FORM THE LOWER ATTACH POINT. MAINTENANCE REMOVED & REPLACED THE AFFECTED RT MLG SIDE STRUT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. INSPECTED THE MLG ATTACH POINTS AND STRUCTURE WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — INOPERATIVE (NR PRIMARY) · airframe 44,763 hrs · 26,728 cycles

IAH - FLIGHT 3980, THE CREW REPORTED PFD#1 FAIL "SMOKED SMELL". THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PFD#1, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,098 hrs · 30,995 cycles

DURING MX INSPECTION THE #3 EMERGENCY LIGHT BATTERY PACK WILL NOT ILLUMINATE LIGHTS. MX R&R #3 EMERGENCY LIGHT BATTERY WITH OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,098 hrs · 30,995 cycles

DURING MX INSPECTION THE #1 EMERGENCY LIGHT BATTERY PACK WILL NOT ILLUMINATE LIGHTS. MX R&R #1 EMERGENCY LIGHT BATTERY WITH OPERATIONAL CHECK GOOD.

Part: SKIN — CORRODED (FRAME 4) · airframe 44,895 hrs · 28,040 cycles

TYS A/C IS HERE FOR A REPAIR OF A DOUBLER AT FRAME 4 AND STRINGERS 9L TO 11L DUE TO MORE DAMAGE FOUND. MAINTENANCE CUT OUT THE DAMAGE AREAS, FABRICATED FILLERS AND A NEW DOUBLER, INSTALLED REPAIR PARTS IAW ETD 2020-145-019642. ALLODINED,PRIMED AND PAINTED IAW EMB 145-CPM-51-21--04/05/06. ALL WORK ACCOMPLISHED AND WILL BE RELEASED BACK TO SERVICE. 5

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,561 hrs · 21,728 cycles

IAH - FLIGHT 4249, DURING MAINTENANCE INSPECTION THE EXIT ROW EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION STRINGER 19R EXTERNAL REINFORCEMENT TEE WEB WAS FOUND TO HAVE CHAFE DAMAGE BETWEEN 52 AND FRAME 53 BY WING TO FUSELAGE FAIRING. MAINTENANCE REPAIRED STRINGER 19R I/A/W SRM 53-24-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION CENTER FLOOR BEAM SUPPORT CORRODED AROUND FASTENERS AND IN CORNER RADIUS.FRAME 46-50. MAINTENANCE REPAIRED WITH FILLER AND DOUBLER I/A/W ETD2020-145-01566.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND CHAFE DAMAGE TO STRINGER 19L EXTERNAL REINFORCEMENT TEE WEB BETWEEN FRAME 52 AND 53. CHAFE CAUSED BY WING TO FUSELAGE FAIRING. MAINTENANCE REPAIRED STRINGER 19L (ONE ANGLE REPAIR) I/A/W SRM 53-24-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,418 hrs · 32,296 cycles

IAH- FLIGHT 4289 DURING MAINTENANCE INSPECTION THE R/H EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT POWERSUPPLY BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRAY — DEFECTIVE (CABIN) · airframe 41,003 hrs · 32,030 cycles

DURING MX INSPECTION THE LH AND RH OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX REMOVED AND REPLACED #4 EMERGENCY BATTERY TRAY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE 4/20/20.

Part: ACM — FROZEN (AC BAY) · airframe 44,325 hrs · 26,799 cycles

IAH - DURING FLIGHT THE CREW REPORTED THAT THEY SMELLED BURNING / SMOKE. RAN QRH TURNED OFF THE RECIRC FAN AND THE SMELL DISSIPATED. THE AIRCRTAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS OR SMOKE SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 41,003 hrs · 32,030 cycles

DURING MX INSPECTION THE EXIT AISLE PATH LIGHTING FROM ROW 8 TO 11 WAS FOUND INOPERATIVE. ALSO EXIT ROW 18 UPPER AND LOWER SIDEWALL SIGNS INOP AND ROW 18 AFT CEILING EXIT SIGN INOP. MX PERFORMED OPS CHECK OF EMERGENCY LIGHTS WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE 4/20/20.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND FRAME TO SKIN SPLICE PLATE @ FRAME 81 BETWEEN STRINGER 2L-2R CRACKED. MAINTENANCE REPLACED THE CRACKED SKIN SPLICE PLATE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND CRACK OUT OF RIVET HEAD ON FRAME 81 BETWEEN STRINGER 2L-3L. MAINTENANCE REPAIRED I/A/W ETD2020-145-015556

Part: INVERTER — INOPERATIVE (CABIN) · airframe 41,674 hrs · 36,860 cycles

DURING ROUTINE MAINTENANCE LEFT AND RIGHT OVERWING FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE #4 EMERGENCY LIGHT BATTERY INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FLAP — DELAMINATED (ZONE 500)

L/H I/B FLAP HAS AREAS OF DELAMINATION ON TRAILING EDGE. REPAIRED DELAMINATION IAW EA12-2020-055. FLAP WAS RETURNED TO STOCK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,982 hrs · 35,769 cycles

IAH - FLIGHT 3985, DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8-9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIGHT STRIP ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 04/15/20 IAH MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INTERMITTENT (PAX DOOR) · airframe 43,368 hrs · 33,645 cycles

IAH - FLIGHT 4229, DURING MX INSPECTION THE MAIN PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 35,215 hrs · 21,835 cycles

DEN - FLIGHT 3938 THE EMERGENCY LIGHT STRIP AT SEAT 3A WOULD NOT GLOW. THE LIGHT STRIP WAS PLACED ON MEL 33-50-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 04/07 THE IAH MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — DEFECTIVE (AC BAY) · airframe 37,130 hrs · 24,009 cycles

XNA - FLIGHT 3951 THE CREW REPORTED AN ELECTRICAL SMELL IN THE COCKPIT ONLY WITH PACK ONE (1) ON, AND THAT THE SMELL DISSIPATED WHEN PACK ONE (1 WAS TURNED OFF. THE AIRCRAFT WAS INSPECTED AND PACK ONE (1) WAS PLACED ON MEL 21-51-00-3. ON 04/04/20 THE AIRCRAFT LANDED IN IAH WHERE MAINTENANCE REMOVED AND REPLACED THE #1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,461 hrs · 32,938 cycles

CARGO DOOR CUT-OUT SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUT-OUT SILL. AIRCRAFT STILL IN C CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,701 hrs · 33,320 cycles

IAH DURING MAINTENACE INSPECTION THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 42,461 hrs · 32,938 cycles

STRINGER 6R SPLICE IS CRACKED @ FWD END @ FRAME 19 (MARKED). REMOVED AND REPLACED CRACKED STIFFENER IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,461 hrs · 32,938 cycles

RH OMEGA BEAM CORRODED BETWEEN FRAMES 59-60 AT NUTPLATE. REPAIRED RH OMEGA BEAM BETWEEN FRAMES 56-60 AT NUTPLATE IAW EMB 145 SRM 53-24-10.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,701 hrs · 33,320 cycles

IAH DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLIES AND BATTERY PACKS #3 AND #4. EMERGENCY LIGHTS WERE OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,701 hrs · 33,320 cycles

IAH DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLIES AND BATTERY PACKS #3 AND #4. EMERGENCY LIGHTS WERE OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND FLOOR BEAM SUPPORT CRACKED FRAME 50 LEFT SIDE. MAINTENANCE REPAIRED FLOOR BEAM ANGLE/STUB BINDING IA/W ETD2020-145-015166

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND RT FLOORBEAM SUPPORT LOCATED BETWEEN FRAME 47-50 CRACKED IN AFT END BEND RADIUS. MAINTENANCE REMOVED AND REPLACED FLOORBEAM SUPPORT.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND FLOORBEAM SUPPORT CRACKED BETWEEN FRAME 47-50 IN AFT END BEND RADIUS. MAINTENANCE REPLACED FLOORBEAM SUPPORT.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,293 hrs · 22,462 cycles

RH FLOOR SILL CORRODED FROM FRAME 29-35. REMOVED AND REPLACED RH FLOOR SILL FRAME 29-35 IAW EMB SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,293 hrs · 22,462 cycles

CORROSION ON LH FLOOR SILL AT FRAME 24-35. REMOVED AND REPLACED FLOOR SILLS AT FRAME 24-29 AND 29-35 IAW EMB 145 SRM 51-40-02.

Part: CONNECTOR — DETACHED (EXTERIOR LIGHT) · airframe 45,198 hrs · 26,847 cycles

IAH - FLIGHT 4328, DURING MX INSPECTION THE LEFT HAND EXTERIOR FWD EMERGENCY LIGHT WAS FOUYND TO BE INOPERATIVE. MAINTENANCE REATTACHED CANNON PLUG P8561, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 42,577 hrs · 33,029 cycles

DURING C CHECK INSPECTION FOUND 2 CRACKS ON APU FIREWALL RIGHT SIDE AT STIFFENER END. . MAINTENANCE REPLACED APU FIREWALL .