N724AE

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,378 hrs · 24,653 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN FORWARD EMERGENCY FLASHLIGHT WAS NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN FWD EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB 135 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,038 hrs · 24,311 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT SEAT 7 AND 8 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP AT SEAT 7 AND 8 IAW EMB 135 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,823 hrs · 24,075 cycles

DURING B INSPECTION FOUND THE COURTESY LIGHTS REMAIN ILLUMINATED REGARDLESS OF SWITCH POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY ASSEMBLY IAW EMB 135 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,646 hrs · 23,867 cycles

ON FLIGHT 2980 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB 135 AMM 33-50-16 AND 33-51-01. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 26,573 hrs · 23,778 cycles

DURING B INSPECTION, FOUND FLASHLIGHT CHARGING BRACKET BEHIND CAPTAIN'S, SEAT DOES NOT HOLD FLASHLIGHT SECURELY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT CHARGING BRACKET IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,413 hrs · 23,602 cycles

DURING MAINTENANCE INSPECTION, FOUND THE NR 4 EMERGENCY POWER SUPPLY FUSE BURNED INTERNALLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-50-04 . OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 26,409 hrs · 23,598 cycles

DURING B INSPECTION, FOUND THE LEFT AFT EXTERIOR EMERGENCY LIGHT HAS A BROKEN NUTPLATE FOR THE LENS COVER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE WING EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHT) · airframe 26,413 hrs · 23,602 cycles

DURING MAINTENANCE INSPECTION, FOUND THE CONNECTOR, AIRCRAFT SIDE, FOR LEFT AFT EXTERNAL EMERGENCY EXIT LIGHT IS INTERMITTENTLY SHORTING OUT. OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,074 hrs · 23,220 cycles

DURING B INSPECTION, FOUND THE LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,896 hrs · 23,036 cycles

DURING B-INSPECTION FOUND THE CEILING EMERGENCY "EXIT" LIGHT (AT GALLEY) INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY "EXIT" LIGHT (GALLEY) IAW EMB 135 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,896 hrs · 23,036 cycles

DURING MAINTENANCE INSPECTION FOUND THE LAST EMERGENCY LIGHT PROXIMITY STRIP ON PANEL 251HF INOPERABLE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — NOT SEATED (EXTERIOR) · airframe 25,859 hrs · 22,995 cycles

DURING B-INSPECTION FOUND THE LEFT EXTERIOR AFT UPPER EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED THE LEFT EXTERIOR AFT EMERGENCY LIGHT LAMP RESEATED IAW EMB 135 AMM 33-50-10. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD IAW EMB 135 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,927 hrs · 22,087 cycles

DURING MAINTENANCE BASE INSPECTION FOUND FRAME 70 TO HAVE A TOOLING MARK AT 4 O'CLOCK POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 70 IN ACCORDANCE WITH EO EM-53MR-1891. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — MALFUNCTIONED (NR 3) · airframe 24,029 hrs · 2,164 cycles

ON FLIGHT 2944 AFTER TAKEOFF AND GEAR RETRACTION THE CREW REPORTED, RECEIVED NR 1 HYDRAULIC SYSTEM FAIL MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MAF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BRAKE ASSEMBLY IAW MTX W/C 32-600-14. THE OPERATIONAL BRAKE TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELAY — FAILED (COCKPIT) · airframe 23,755 hrs · 21,027 cycles

ON FLIGHT 4500 DURING CRUISE THE CREW REPORTED, ENCOUNTERED SEVERE ICING. THE AUTO-ANTI ICE DID NOT ACTIVATE. THE CREW HAD TO ACTIVATE MANUALLY. THE CAPTAIN ELECTED TO RETURN TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED DETAILED VISUAL INSPECTION OF CAPTAIN’S AND FIRST OFFICER’S PITOT/STATIC SYSTEM. FOUND WATER IN FIRST OFFICER’S DRAIN. DRAINED LINE ON FIRST OFFICER’S SYSTEM AS PER 34-13-00. THE OPERATIONAL AND LEAK TEST WERE GOOD AS PER AMM 34-13-00. PERFORMED OPERATIONAL TEST OF THE ANTI-ICE SYSTEM AS PER AMM 30-00-00. FOUND FIRST OFFICER’S PITOT STATIC HEATING INTERMITTENT. REMOVED AND REPLACED RELAY K0055 AS PER 20-13-02. THE OPEATIONAL TEST WAS GOOD AS PER 30-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — FAILED (CABIN) · airframe 23,287 hrs · 20,633 cycles

ON FLIGHT 4479 THE CREW REPORTED A STRONG ELECTRICAL ODOR IN GALLEY (IT WAS NOT DOCUMENTED WHEN THE CREW NOTICED THE ODOR). THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD BALLAST ABOVE SEAT 1BC IAW EMB 33-21-05, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,596 hrs · 18,270 cycles

DURING MAINTENANCE INSPECTION THE NUMBER 1 FLOOR LIGHT STRIP WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 FLOOR LIGHT STRIP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE BASE INSPECTION FOUND STIFFENER BETWEEN LEFT BEAM AND PASSENGER DOOR AT FRAME 17-18 TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STIFFENER BETWEEN LEFT BEAM AND PASSENGER DOOR IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 81 CLIP AT THE 9 O’CLOCK POSITION CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FRAME 81 CLIP IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BULKHEAD — WORN (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE PILOTS BULKHEAD OUTBOARD GUIDE PIN HOLE WORN/ELONGATED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PILOTS BULKHEAD OUTBOARD GUIDE IAW ETN-EM-53-153R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR ROD CLIP HOLDER BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR ROD CLIP HOLDER BRACKET IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLATE — WORN (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE PILOTS BULKHEAD INBOARD GUIDE PIN HOLE WORN/ELONGATED. AIRCRAFT REMOVED FROM SERVICE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE BASE VISIT FRAME 67 ON THE CARGO ENTRY FLOOR RAMP PANEL BRACKET WAS FOUND TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW FRAME 67 CARGO ENTRY FLOOR RAMP BRACKET IAW EMB SRM 51-20-01, 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE BASE VISIT FRAME 66 ON THE CARGO ENTRY FLOOR RAMP PANEL BRACKET WAS FOUND TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW FRAME 66 CARGO ENTRY FLOOR RAMP BRACKET IAW EMB SRM 51-20-03, 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT DIGITAL TO BE DENTED/CRACKED AND CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NEW SERVICEABLE AFT DIGITAL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE STIFFENER BETWEEN THE LEFT BEAM AND PASSENGER DOOR FRAME 17-18 TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STIFFENER BETWEEN LT BEAM AND THE PASSENGER DOOR AT FRAME 17-18 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT BEAM RAMP ANGLE BETWEEN FRAMES 18-20 TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT BEAM RAMP ANGLE BETWEEN FRAMES 18-20. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR FLOOR SUPPORT CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED WITH A NEW PASSENGER DOOR FLOOR SUPPORT IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT BEAM GUSSET AT FRAME 22 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT GUSSET BEAM AT FRAME 22 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT BEAM GUSSET AT FRAME 20 TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE RIGHT HAND GUSSET AT FRAME 20 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE GALLEY CENTER BEAM RAMP TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CENTER BEAM RAMP IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND CROSS MEMBER IS CORRODED AT FRAME 22 ON THE RIGHT SIDE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CROSSMEMBER AT FRAME 22 RT IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 20,499 hrs · 18,183 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR INTERNAL SUPPORT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE PASSENGER DOOR INTERNAL SUPPORT BRACKET IAW EO EM-52-037. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — FAILED (LEFT DC)

ON FLIGHT 4772 AFTER TAKEOFF CREW REPORTED LT DC GEN LIGHT ON CWP. CREW ELECTED TO RETURN TO FIELD. EMERGENCY WAS DECLARED, ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT DC GEN IAW MTX W/C 24-47-33. ACFT RETURNED TO SERVICE. (S)

Part: CONTROL CABLE — OUT OF ADJUST (AILERONS) · airframe 15,904 hrs · 14,367 cycles

CREW NOTIFIED IN FLIGHT THAT FLIGHT CONTROLS STIFF AND AIRCRAFT FLY’S TAIL HEAVY DURING FLIGHT CONTROL CHECKS FOR BEFORE TAKEOFF FOUND PITCH AND ROLL TO BE STIFFENER THAN NORMAL. WITH PITCH TRIM PROPERLY SET FOR TAKEOFF (17 PAX AND 348 CARGO) AIRCRAFT WANTED TO ROTATE PRIOR TO REACHING VI/VR. UPON ROTATION FORWARD YOKE BIAS AND PITCH DOWN TRIM REQUIRED. IN LEVEL FLIGHT, PITCH WAS ZERO GENERALLY 1 OR 2 IN A 135 A/C ADDITIONALLY IN-FLT FLIGHT CONTROLS FELT SLUGGISH AND HEAVY. ADJUSTED AILERON CABLE TENSION. AIRCRAFT PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICED.

Part: SIGN — FAILED (EMEGENCY LIGHTS) · airframe 15,695 hrs · 14,180 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

LEFT INBOARD SEAT TRACK NUMBER 2 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

LEFT INBOARD SEAT TRACK NUMBER 1 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

RIGHT OUTBOARD SEAT TRACK NUMBER 3 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

RIGHT OUTBOARD SEAT TRACK NUMBER 4 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

RIGHT OUTBOARD SEAT TRACK NUMBER 2 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

SEAT TRACK NUMBER 5 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

LEFT OUTBOARD SEAT TRACK NUMBER 2 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,687 hrs · 14,171 cycles

RIGHT INBOARD SEAT TRACK NUMBER 1 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS COME ON FOR 2 SECONDS THEN GOES OUT WHEN TESTED. RAI BATTERY PACKS 1-4 PER AMM EMB 135 AMM 33-50-04. OPS CHECKED GOOD. BATTERY PACK 1 P/N 203-1A S/N 77461 BATTERY PACK 2 P/N 2013-1A S/N 60649, BATTERY PACK 3 P/N 203-1A S/N 82610 BATTERY PACK 4 P/N 2013-1A S/N 20131A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — BIRD STRIKE (FUSELAGE)

JFK - FLT 4613 - AIRCRAFT EXPERIENCED BIRDSTRIKE ON LEFT CORNER OF WINDSHIELD. COMPLETED BIRDSTRIKE INSPECTION AND FERRIED AIRCRAFT TO SAW FOR FUSELAGE STRUCTURAL REPAIR BETWEEN FRAME 1 AND FRAME 5, FORWARD OF CAPTAINS WINDSHIELD. MAINTENANCE INSTALLED NEW FUSELAGE SKIN P/N 12041320065, UPPER LEFT FRAME 2 P/N 12001897001, AND REPAIRED STRINGER P/N 12041320043 4L IAW EMB SRM 51-40-02, 53-00-00 FIG 201. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACM — ODOR (NR 1)

CREW GOT A SMOKE ODOR WITH A HINT OF VISIBLE SMOKE IN COCKPIT AFTER STARTING THE APU AND TURNING ON PACKS ON THE GROUND. INSPECTED/ TROUBLESHOT FOR DISCREPANCY IAW MM. ISOLATED TO NR 1 ACM. NR 1 PACK DEFERRED IAW MEL. (K)

Part: BEAM — CORRODED (FRAME 25)

THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKEING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SKIN — DENTED (MAIN DOOR)

A DENT WITH GOUGES WAS FOUND ON THE OUTER SKIN OF THE MAIN DOOR. REMOVED THE PAINT FROM AREA AND BLENDED OUT GOUGES. PERFORMED NDT INSP OF AREA WITH NO INDICATIONS NOTED. FABRICATED A DOUBLER, REPAIR DONE IAW REPAIR STATEMENT AND SRM. (K)

Part: BEAM — CORRODED (GALLEY)

THE LT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING CUTOUT. FABRICATED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FRAME 20)

A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALL NEW SILL IAW EMB STATMENT IC2003-145/0818 AND 3829. (M)

Part: PROFILE — CORRODED (FUSELAGE)

ABI - DURING A IMBV INSPECTION, THE RIGHT PROFILE AFT OF FRAME 18 WAS FOUND CORRODED BELOW LIMITS AROUND NUT PLATE. CUT OUT SECTION OF CORRODED PROFILE, PERFORMED NDT INSPECTION AND TREATED BARE METAL. FABRIATED A REPAIR ANGLE. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3289 DATED NOV 17, 2003. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL AS FOUND CORRODED BELOW SRM LIMITS. CUT OUT CORRODED SECTION OF THE FORWARD DIGITAL. MADE REPLACEMENT STRAP, FABRICATED SHIM, TWO DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 23, CHAPTER 53-21-10 FIGURE 203. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV INSPECTION STRINGER 19 WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52R AND 53R. BLENDED THE CHAFE ON STRINGER 19R AND PERFORMED AN NDT INSPECTION. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIRS DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED A REPAIR DOUBLER. REPAIRED IAW EMB GST-1254/02, ITEM 4 AND STANDARD SRM PRACTICES. (M)

Part: SKIN — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION OF AIRCRAFT, FOUND FOUR GROUPS OF GOUGES ON THE LEFT FORWARD FUSELAGE BETWEEN FRAMES 12 AND 13, ALONG STRINGER 16L. BLENDED GOUGES PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIRED IAW EMB GST-1265/02, AND STANDARD SRM PRACTICES. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON CENTER BEAM AT FRAME 20. REMOVED CORRODED BY CUT OUT. FABRICATED TWO DOUBLER ANGLES, A FILLER, AND A U-SHAPE DOUBLER CHANNEL. REPAIRED IAW EMB145 (SRM145/1142, CHAPTER 53, REV 17) 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSLEAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1141, CHAPTER 53, REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE AND FILLER. REPAIRED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: LIGHT — LOOSE (PAX DOOR)

ORD - FLT 4054 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE IN SOCKET AND A GROUND WIRE THAT WAS LOOSE. THE BULB WAS TIGHTENED IN SOCKET AND THE GROUND WIRE WAS ALSO TIGHTENED. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (HORIZ STAB)

ORD - FLT 4139 - CREW REPORTED PITCH TRIM ON CAPTAINS AND FIRST OFFICERS YOKE TO BE INOPERATIVE AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — INOPERATIVE (RIGHT ENGINE) · airframe 197 hrs · 193 cycles

FIC - FLT 4939 - DURING TAKEOFF, CREW NOTED E2 FUEL LOW PRESSURE WARNING. PUT ON MEL. MAINTENANCE REMOVED AND REPLACED LOW PRESSURE SWITCH IAW EMB MM. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)