N701MH

Part: ENGINE — ODOR (NR 1) · airframe 16,286 hrs · 14,874 cycles

EXCESSIVE STINK COMING FROM PACKS DURING DESCENT. REMOVED AND REPLACED NUMBER 1 ENGINE IAW EMB 72-00-00. OPERATIONAL AND LEAKS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: CARBON SEAL — WORN (NR 1 ENGINE) · airframe 17,245 hrs · 17,152 cycles

OIL ODOR IN FLIGHT DECK. FOUND NR 1 ZERO CARBON SEAL WORN BEYOND LIMITS. REMOVED AND REPLACED NR 1 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: ELECTRONIC UNIT — FAILED (MLG) · airframe 15,914 hrs · 14,586 cycles

AFTER GEAR EXTENSION HEARD BANGING NOISE FROM NOSE GEAR AREA. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB AMM 32-32-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SWITCH — FAILED (NR 2 PACK) · airframe 15,802 hrs · 14,493 cycles

TURNED ON NR 2 PACK AND CABIN FILLED WITH SMOKE. REMOVED AND REPLACED NR 2 PACK OVERTEMP SWITCH IAW EMB AMM 21-51-09. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE

Part: LIGHT — INCORRECT (CABIN)

EMERGENCY EXIT FLOOR LIGHT PROXIMITY STRIP IS WRONG COLOR. REPLACED EMERGENCY EXIT PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (AVIONICS BAY)

DURING GEAR EXTENTION OBSERVED MOMENTARY EICAS MESSAGE MAIN PITCH TRIM FAIL AND BACKUP PITCH TRIM FAIL. WARNING WENT OUT AFTER GEAR EXTENDED. TROUBLESHOT SYSTEM REPLACED HORIZONTAL STABILIZER UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT CROSSBEAM FRAME 29. MAINTENANCE REMOVED AND REPLACED LEFT OMEGA BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND RIGHT OMEGA BEAM AT CROSS BEAM ATTACHMENT FRAME 29 CORRODED. REMOVED AND INSTALLED NEW OMEGA BEAM IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB)

SAW - DURING ALTERATION OF GUST LOCK SERVICE BULLETIN 145-55-0086, MISALIGNED HOLES ON RIGHT SIDE OF CARBON BOX OF HORIZONTAL STABILIZER. REPAIRED HOLES IAW ENGINEERING ORDER EB-55MR-094. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT CROSS BEAM CORRODED AT CROSS BEAM FRAME 25. MAINTENANCE REMOVED AND REPLACED LEFT OMEGA BEAM IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED IN FORWARD CABIN AT FRAME 25. REPLACED RIGHT OMEGA BEAM IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND CENTER AISLE RIGHT RAMP SUPPORT AT FRAME 20 IS CORRODED. INSTALLED NEW RAMP IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUSSET — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND GUSSET IN CENTER HAT TRACK UNDERFLOOR IS CORRODED BETWEEN FRAME 18-23. MAINTENANCE REPLACED GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND DOUBLER AT FRAME 18 UNDERFLOOR IS CORRODED. REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND DOUBLER AT FRAME 20 CORRODED. INSTALLED NEW DOUBLER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND LEFT FORWARD SEAT TRACK CORRODED AROUND ALL SCREWS. MAINTENANCE REPLACED SEAT TRACK IAW EMB 135 AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PLATE — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR FORWARD SILL CORRODED. REPLACED SERVICE DOOR FORWARD SILL PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PROFILE — CORRODED (FUSELAGE)

SAW - DURING CPCPC INSPECTION, FOUND PROFILE Z-RIGHT SIDE AT FRAME 22 IS CORRODED. MAINTENANCE REPLACED PROFILE Z IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND CENTER HAT SECTION REPAIR DOUBLER AT FRAME 20 IS CORRODED. MAINTENANCE REPLACED HAT BEAM SECTION IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND DIGITAL FORWARD AT FRAME 16 CORRODED. REPAIRED DIGITAL IAW EMB SRM 53-21-10 FIGURE 203. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 CORRODED. MAINTENANCE REPLACED LEFT OMEGA BEAM AT FRAME 20 IAW SRM 53-21-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND CENTER AISLE RAMP SUPPORT FRAME 20 CORRODED. MAINTENANCE REPLACED CENTER AISLE RAMP SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ODOR — DETECTED (COCKPIT)

CREW NOTED BURNING ODOR IN COCKPIT DURING TAXI. PERFORMED GVI OF FORWARD AVIONICS AND UNDER FLOOR COMPARTMENTS. PERFORMED OPERATIONAL CHECKS OF WINDSHIELD HEAT, ANTI-ICE, AIR CONDITIONING AND ENGINES WITH NO DESCREPANCIES NOTED. AC RETURNED TO SERVICE. (SW21200404961)

Part: SILL — CORRODED (CARGO DOOR)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SILL, INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142 REV 20, CHAPTERS 51-40-02, 51-20-03, 51-40-06. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION, TWO DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 (SRM 145/1142, REV 20) 53-21-10 PARA 4, AND STANDARD SRM PRACTICES. (M)

Part: GUSSET — CORRODED (GALLEY)

FOUND DUIRNG A IMBV INSPECTION, DIAMOND GUSSET ON RIGHT BEAM AT FRAME 22 CORRODED. REMOVED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 145/135 SRM 51-40-02. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - FOUND DUIRNG AN IMBV INSPECTION, EXTENSION AT CENTER BEAM BETWEEN FRAME 22 AND 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE EXTENSION IAW EMB 135 SRM 51-40-02. (M)

Part: RAMP — CORRODED (GALLEY)

ABI - THIS IS LEVEL 2 FINDING ON CRIC NR 29272, FOUND DURING AN IMBV INSPECTION, GALLEY CENTER BEAM RAMP CORRODED. REMOVED AND INSTALLED SERVICEABLE BEAM RAMP IAW EMB 135 SRM 51-40-02 AND 51-40-03. (M)

Part: SILL — CORRODED (GALLEY)

THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION CORROSION ON LEFT SILL AFT OF PASSENGER DOOR BETWEEN FRAME 18L AND 22L AT STRINGER 15L. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

FOUND DURING AN IMBV INSPECTION, CORROSION ON GUSSET AT CENTER BEAM SECTION BETWEEN FRAME 18 AND 22 ABOVE STRINGER 21L. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 135 SRM 51-40-02. (M)

Part: ACTUATOR — OUT OF ADJ (THRUST REVERSER)

DFW - FLT 3423 - NR 2 THRUST REVERSER DISAGREE DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED NR 2 THRUST REVERSER ACTUATOR ROD ENDS IAW AMM 78-32-01-420-001-A00. OPS CHECK GOOD. (M)

Part: SKIN — CORRODED

ABI - DURING MBV MAINTENANCE, FOUND CORROSION IN THE OMEGA BEAM. MAINTENANCE REPAIRED OMEGA BEAM IAW EMB SRM 53-21-10. (M)

Part: SKIN — CORRODED

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD GALLEY DIGITAL CORRODED. MAINTENANCE REPAIRED THE GALLEY DIGITAL IAW EMB REPAIR STATEMENT GST-1630/01. (M)

Part: SKIN — CORRODED

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE AFT GALLEY DIGITAL TO BE CORRODED. MAINTENANCE REPAIRED AFT GALLEY DIGITAL IAW EMB GST 1630/01. (M)

Part: SKIN — CORRODED

DURING MBV INSPECTION, MAINTENANCE FOUND THE OMEGA BEAM AT FRAME 20 CORRODED. MAINTENANCE REMOVED CORROSION AND INSTALLED DOUBLER REPAIR IAW EMB GST 1630/01. (M)

Part: TRIM SWITCH — DIRTY (COCKPIT)

DAY - FLT 4196 - DURING CLIMB-OUT FROM DAY, FIRST OFFICERS PITCH TRIM SWITCH WOULD NOT WORK. ALL OTHER TRIM SWITCHES FUNCTIONED NORMALLY IN NORMAL AND STANDBY POSITIONS. MAINTENANCE FOUND FIRST OFFICERS TRIM SWITCH TO BE STICKING DUE TO DIRT/GRIME CONTAMINATION. CLEANED SWITCH AND PERFORMED SYSTEM OPERATIONS TEST PER AMM 27-40-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 1,803 hrs · 1,690 cycles

ORD - FLT 4084 - FLOOR EMERGENCY LIGHTING NEAR SEAT 12/13A FAILS TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY AND CHARGER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN)

ORD - FLT 4084 - FLOOR EMERGENCY LIGHTING NEAR SEAT 12/13A FAILS TO ILUMINATE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY AND CHARGER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA2131. (M)