N606AE

Part: NONE — NONE · airframe 51,446 hrs · 43,658 cycles

OVERWING EMERGENCY EXIT LOCATOR MARKER AFT FACING INOP.-C/A-T/S PER WM 33-50-50. FOUND SP9125 DISCONNECTED.RAR SP9125 IAW SWPM 20-21-00. OPC GOOD IAW AMM 33-50-00.

Part: NONE — NONE · airframe 51,409 hrs · 43,618 cycles

ALL AFT INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP-C/A-T/S PER FIM TASK 33-50-00-810-804-A. FOUND #4 EMERGENCY LIGHT POWER SUPPLY TO BE INNOPERATIVE. RAR #4 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY IAW ENVOY WORK CARD 33-700-19. OPERATIONAL CHECK GOOD.

Part: NONE — NONE · airframe 51,264 hrs · 43,440 cycles

HYDRAULIC #2 FAIL IN FLIGHTL. EMERGENCY DECLARED-C/A-FOUND #2 HYDRAULIC SYSTEM PRESSURE TRANSMITTER TO BE LEAKING. RAR TRANSMITTER O-RING PER AMM 29-30-02. OPERATIONAL CHECK OF #2 HYDRAULIC SYSTEM GOOD PER AMM 29-10-00. LEAK CHECK GOOD

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 50,999 hrs · 43,139 cycles

MAIN DOOR HARD TO OPEN GETS STUCK WHEN TRYING TO OPEN IT.-C/A-PERFORMED LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02 OPS CK GOOD

Part: APU — FAILED · airframe 50,835 hrs · 42,945 cycles

APU FAIL WHEN IT FAIL DISTINCT SMELL SMOKE SMELL IN CABIN-C/A-DEFERRED APU SYSTEM M PROCEURES C/W AUTH 060253DM-CREF 49-01

Part: BATTERY — FAULTED (FLASHLIGHT) · airframe 50,713 hrs · 42,804 cycles

FA EMERGENCY FLASHLIGHT FLICKERING ON AND OFF-C/A-RAR FA EMERGENCY FLASHLIGHT BATTERY IAW E145 AMM 33-50-16. OPS CKED GOOD. IAW E145 AMM 33-51-01

Part: CRADLE — DETACHED (FLASHLIGHT) · airframe 50,657 hrs · 42,739 cycles

FA EMEREGNCY FLASHLIGHT HOLDER BROKEN REF AML PAGE 4734410/1 MEL 25-32, AUTH# 05-196M-C.-C/A-R&R FA EMERGENCY FLASHLIGHT HOLDER & PERFORMED OPS CHECK IAW AMM 33-50-16, OPS CHECK GOOD, MEL ITEM RESTORED.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 50,448 hrs · 42,502 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. C/A-LUBRICATED MAIN CABIN DOOR GUIDE ROLLERS, OPS CHECK GOOD AS PER AMM 52-10-00.

Part: QUICK DISCONNECT — BROKEN (EMERGENCY LIGHT) · airframe 49,550 hrs · 41,584 cycles

EMERGENCY FLOOR STRIP LIGHTING QUICK DISCONNECT BROKEN AT FLOOR BOARD PANEL 241BF. PERFORMED QUICK DISCONNECT REPLACEMENT AT EMERGENCY FLOOR STRIP LIGHTING IAW EMB-145 SWPM 20-21-00. OPT IS GOOD.

Part: ECU — MALFUNCTIONED (TE FLAPS) · airframe 49,431 hrs · 41,475 cycles

FLAP LOW SPEED MESSAGE DURING DESCENT. PERFORMED FIM 27-51-00-810-A, FOUND FECU BIT CODE 1110 CHANNEL 1 FAILURE. R & R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02, AND ACCOMPLISHED OPERATIONAL TEST IAW AMM 27-53-00, OPS TEST GOOD. NO MSG ON EICAS AND CMC. "REF NRWC 606-MIA-03282 FOR WORK PERFORMED"

Part: WIRE — BROKEN (CABIN) · airframe 49,193 hrs · 41,252 cycles

ROW 3 THRU 7 FLOOR PROXIMITY EMERGENCY LIGHTS ARE INOP.-C/A-REMOVED AND REPLACED #2 EMERGENCY BATTERY AND POWER SUPPLY IAW EMB 145 AMM 33-50-04, OP CHECK BAD. FOUND THE DC RETURN WIRE TO INVERTER BROKEN AT GROUNDING BLOCK. REPAIRED WIRE W192-8689-22N IAW EMB 145 SWPM 20-21-00. OP CHECK GOOD

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

SSI 53-20-10 LOWER SERVICE DOOR SILL CORRODED AROUND MULTIPLE NUTPLATE HOLES-C/A-REMOVED AND REPLACED LOWER SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02 AND SRM 51-20-01. REPAIR P/N: 145-22178-605

Part: GUIDE — CORRODED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

SSI 53-20-10 AFT SERVICE DOOR CUTOUT CORRODED UNDER AFT LOWER TEFLON GUIDE-C/A-REMOVED AND RE[LACED AFT SERVICE DOOR CUTOUT UNDER AFT TEFLON GUIDE (FR 22 BTW STGR 14R-15R) IAW ERS-EM-53MR-4096. REPLACEMENT PART PN 145-22191-015

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

INTERNAL FUSELAGE SKIN CORROSION AT FR 11-12 BETWEEN STGR 20R-21R ON PREVIOUS BLEND.-C/A-ACCOMPLISHED PERMANENT REPAIR ON INTERNAL FUSELAGE SKIN CORROSION BETWEEN FR 11-12 AND STGR 20R-21R IAW ERS-EM-53MR-4083. REPAIR MATERIALS: DOUBLER: AL CLAD 2024-T3, 0.050? THICK. FILLER: AL CLAD 2024-T3, 0.032? THICK. REPAIR FASTENERS: MS14218-AD5. ORIGINAL FASTENERS: SAME TYPE AS ORIGINAL.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

DURING MBV INSPECTION, QA FOUND THE LH UPPER SEAT TRACK SUPPORT CORRODED AT FR 46 AROUND LOWER RIVETS-C/A-REMOVED AND REPLACED LH UPPER SEAT TRACK SUPPORT AT FR 46 IAW EMB 145 SRM 51-40-02. REPAIR PN 145-30637-003

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

CORROSION FOUND ON CARGO DOOR SILL BETWEEN FR 65 AND FR 68-C/A-REMOVED AND REPLACED CARGO DOOR SILL BETWEEN FR 65 AND FR 68 IAW EMB 145 SRM 51-40-02. REPAIR PN 145-25480-603SD

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

DURING MBV INSPECTION, QA FOUND THE LH UPPER SEAT TRACK SUPPORT CORRODED AT FR 50 AROUND LOWER RIVETS-C/A-REMOVED AND REPLACED LH UPPER SEAT TRACK SUPPORT AT FR 50 IAW EMB 145 SRM 51-40-02. REPAIR PN 145-30637-005

Part: DOOR SEAL — CRACKED (CARGO DOOR) · airframe 49,192 hrs · 41,251 cycles

DURING MBV INSPECTION, QA FOUND THE CARGO DOOR FWD LOWER SEAL FLANGE CRACKED-C/A-REMOVED AND REPLACED CARGO DOOR FWD LOWER SEAL FLANGE IAW EMB 145 SRM 51-20-03 AND 51-40-02. REPAIR PN 145-29610-003

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 49,192 hrs · 41,251 cycles

LH OVERWING EXIT DOOR SMALL "EXIT" LIGHT IS INOP-C/A-COMPLETE:CONNECTED LH OVERWING EXIT DOOR SMALL EMERGENCY LIGHT CANNON PLUG/CONNECTOR IAW EMB 145 SWPM 20-50-00 AND AMM 33-50-00. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,192 hrs · 41,251 cycles

RH FLOOR SUPPORT AT FR 68 IS CRACKED-C/A-COMPLETE:REMOVED AND REPLACED RH FLOOR SUPPORT AT FR 68 IAW EMB 145 SRM 51-40-02.

Part: WIRE — BROKEN (CABIN) · airframe 49,192 hrs · 41,251 cycles

1EA PROX LIGHT WITH ARROWS HAS BROKEN WIRES-C/A-COMPLETE:REMOVED AND REPLACED 1EA PROX LIGHT WITH ARROWS IAW EMB 145 AMM 33-50-12 SEE NRTC BOW340840 FOR FINAL INSTALL AND OPS CHECKS

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 49,192 hrs · 41,251 cycles

R/H OVERWING EMERGENCY LIGHT IS INOP.-C/A-COMPLETE:RE-SEATED CANNON PLUG TO R/H OVERWING EXTERIOR EMERGENCY LIGHT IAW EMB 145 SWPM 20-50-00 AND AMM 33-50-00. OPS CHECK GOOD.

Part: CABLE — LACK OF LUBE (EMER BRAKE HANDL) · airframe 49,019 hrs · 41,076 cycles

EMERGENCY PARKING BRAKE DIFFICULT TO SET.-C/A-CLEANED AND LUBED PARKING BRAKE HANDLE / CABLE REF STD MTX PRACTICES.

Part: GCU — FAILED (APU) · airframe 48,796 hrs · 40,856 cycles

ELECTRICAL SMOKE SMELL NOTICED IN COCKPIT-C/A-C/W FIM TASK 21-20-00-810-801-A. FOUND SMELL TO BE APU GCU CAUSE. REMOVED AND REPLACED APU GCU IAW EMB 145 MM 24-34-02. OPS CHECK GOOD. NO DEFECTS NOTED

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 48,741 hrs · 40,803 cycles

CLIMBING THROUGH FL280 CABIN PRESSURE JUMPED RAPIDLY INTO THE AMBER ON THE EICAS BY THE TIME WE ESTABLISHED A DESCENT IT WAS IN THE RED AND RISING. FOUND KNOB ON MANUAL CONTROLLER STICKING. REMOVED AND REPLACED MANUAL CONTROLLER IAW AMM 21-31-02. OPS CHECKED GOOD. REMOVED AND REPLACED DIGITAL CONTROLLER FOR PRECAUTIONARY PURPOSES.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 48,488 hrs · 40,552 cycles

RTF CREW REPORTS AUTO PRESSURIZATION INOP, DECLRED EMERGENCY FLIGHT CONTINUED-C/A-ITEM DEFERRED PER MEL 21-17 AUTH# 110350DM-C "M" PROCUDERS C/W. REMOVED AND REPLACED DIGITAL CONTROLLER, OPC GOOD, IAW 21-31-01. M PROCEDURES COMPLIED WITH MEL RESTORED

Part: MAGNETIC SEAL — LEAKING (ENGINE) · airframe 48,447 hrs · 40,521 cycles

PARKED AT THE GATE, SHUTTING DOWN ENGINE #2 PRODUCED WHITE SMOKE AND A VERY STRONG ODER IN THE COCKPIT DURING TAXI. T/S PER ETN-EM-79-015. FOUND LTP SHAFT SEAL AND ACG MAGNETIC SEAL LEAKING. REMOVED AND REPLACED AGB MAGNETIC CARBON BREATHER SEAL IAW RRMM 72-63-10 AND R & R LPT SHAFT PLUG AND ASSOCIATED ORING IAW RR MM 72-59-15. C/W ETN-EM-72-034. NO ODOR EVENTS PRESENT. C/W ETN-EM-72-034. NO ODOR EVENTS PRESENT.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 48,356 hrs · 40,429 cycles

CARGO SMOKE INDICATION IN FLIGHT, NO SIGNS OF ACTUAL SMOKE, CARGO FIRE BOTTLE DISCHARGED. REPLACED BAGGAGE FIRE BOTTLES IAW AMM26-23-01. PERFORMED OPS CHECK OF APU IAW AMM 49-10-00 OPS CHECK GOOD NO DEFECTS FOUND. MEL RESTORED. REPLACED CARGO SMOKE DTECTORS, TIGHTEND BAGGAGE FAN RELAY, REPAIRED CONNECTOR PLUG AT MAINTENANCE PANEL. OPS CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 48,309 hrs · 40,385 cycles

BAG SMOKE INDICATION ON EICAS. C/A-FLIGHT CREW PACARDED BAG SMOKE IND. REOPENED MEL 26-3 MEL AUTH# 090489D-C REF# 26-3 MOC# 628765. C/W WORK SCOPE PER REAPEATS. NO FAULTS FOUND.REMOVED AND REPLACED RELAY K0625, K0629 AND K0630. IAW AMM 20-13-02. REMOVED AND REPLACED BOTH FWD AND AFT SMOKE DETECTORS IAW AMM 26-14-01. REMOVED AND REPLACED DAU 2 IAW AMM 31-41-01. OPS CHECK GOOD IAW AMM 26-23-00. CARGO AREA SMOKE DETECTOR P/N 473597-13 S/N 2519 FWD; UNIT DATA ACQUISTION P/N 7013348-949 S/N 01064364 AFT.

Part: CONTROL PANEL — FAILED (CARGO BAY) · airframe 48,303 hrs · 40,381 cycles

BAGG SMOKE WARNING MSG PRESENTED SHORT FINAL APPROACH. CREW REPORTS FIRE BOTTLES USED IN BAGGAGE COMPARTMENT. C/A-DEFERRED BAG SMOKE DETECTION SYSTEM MEL AUTH# 090488D-C REF# 26-3. DEFERRED BAGGAGE COMPARTMENT FIRE EXT SYSTEM. MEL AUTH# 090489D-C REF# 26-9. COMPLIED WITH WORK SCOPE. NO DISCREPENCIES NOTED. REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR IAW AMM 26-15-01. AND RAR BAGGAGE/ APU FIRE PANEL IAW AMM 26-00-01. OPS CHECK GOOD. MEL RESTORED. REMOVED AND REPLACED BAGGAGE COMPARTMENT FIRE BOTTLES IAW AMM 26-23-01. OPS CHECK OK . MEL RESTORED. CARGO AREA SMOKE DETECTOR P/N 473597-13 S/N 1043; FIREX BOTTLE-630 S/N 34600073-1 S/N 18563F1 LWR; FIREX BOTTLE-224 CU.IN. P/N 33700027-1 S/N 36345D1 UPR.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 48,300 hrs · 40,380 cycles

WHEN RELEASING THE PARKING BRAKE BAGG SMOKE MASTER CAUTION ILL. "TRANSFERRED TO NRWC # 606-MIA-02757" . -C/A-FOUND BAGGAGE FIRE BOTTLES DISCHARGED. REMOVED AND REPLACED BAGGAGE FIRE BOTTLES IAW AMM 26-23-01 AND REMOVED AND REPLACED FWD AND AFT SMOKE DETECTORS IAW 26-15-01. OPS CHECK GOOD IAW 26-15-00. REMOVED AND REPLACED #2 AFT SMOKE DETECTOR IAW 26-15-01. NO HELP. CONTINUE T/S. REMOVED AND REPLACED BAG COMPT FIRE BOTTLES IAW AMM 26-23-01. REMOVED AND REPLACED FWD AND AFT BAGGAGE SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECK SATISFACTORY IAW AMM 26-15-00. CARGO AREA SMOKE DETECTOR P/N 473597-13 S/N 0094 FWD, S/N 2179A AFT; FIREX BOTTLE-224 CU.IN. P/N 33700027-1 S/N 33700027-1 UPR; FIREX BOTTLE-630 CU.IN. P/N 34600073-1 S/N 17295F1 LWR; CARTRIDGE P/N M30903870.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 48,162 hrs · 40,280 cycles

HYD SYS 2 FAIL INFLIGHT. R & R HYD PUMP ASSY ON THE # 2 ENGINE IAW EMB145 AMM 29-10-03 OPS CHECK AND LEAK CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,942 hrs · 40,093 cycles

RT OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07 OPS CHECK GOOD.

Part: CONNECTOR — BROKEN (CABIN) · airframe 47,913 hrs · 40,059 cycles

NUMBER # 1 EMERGENCY LIGHT STRIP HAS BROKEN TERMINAL ON AIRCRAFT SIDE. C/A-REPAIRED #1 EMERGENCY LIGHT STRIP CONNECTOR IAW SWPM 20-21-00. OPERATIONAL TEST GOOD.

Part: TUBE — DEFECTIVE (BLEED AIR SYS) · airframe 47,195 hrs · 39,382 cycles

BLD 1 LEAK INFLIGHT. "TRANSFERRED TO NRWC 606-ORD-02422" MM 841029. C/A- REMOVE AND REPLACED LT TUBE ASSY FWD OF PACK NR 1 VALVE PER AMM 36-11-09. PERFORMED OPC OF AIR BLEED SYS PER AMM 36-00-00. OPS CHECK AND LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,048 hrs · 39,237 cycles

TRANSFERRED FROM TSA LOG PAGE 363038 ITEM #1 FWD FLOOR EMERGENCY LITES INOP-C/A-COMPLETE:REMOVED AND INSTALLED #1 FWD FLOOR EMERGENCY LITE /WITH EXTRUSION IAW EMB 145 AMM 33-50-12 SEE TURNOVER FOR DETAILS

Part: LIGHT — DAMAGED (CABIN) · airframe 47,048 hrs · 39,237 cycles

LH #6 EMERGENCY LIGHT STRIP SIDEWALL IS DAMAGED.-C/A-COMPLETE:RAR LH #6 EMERGENCY LIGHT STRIP EXTRUSION IAW EMB 145 AMM 33-50-12.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 47,048 hrs · 39,237 cycles

LH #5 EMERGENCY LITE STRIP ACFT SIDE HAS DAMAGED WIRE-C/A-COMPLETE:REPLACED LH #5 EMERGENCY LITE STRIP ACFT SIDE DAMAGED WIRE IAW EMB145 SWPM 20-21-00. SEE NRTC E692589 FOR OPS CHECK DUE

Part: EXTINGUISHER — LEAKING (PORTABLE) · airframe 45,928 hrs · 38,283 cycles

AFT PORTABLE FIRE EXTINGUISHER LEAKING. R & R THE PORTABLE FIRE EXTINGUISHER.

Part: SEAL — LEAKING (NR 2 BLEED) · airframe 45,928 hrs · 38,283 cycles

NR 2 BLEED LEAK DURING FLIGHT. R & R THE BLEED SEALS AT 4, 16, 20, AND 22. NO OTHER LEAKS FOUND THIS TIME. OPS CHECKED GOOD.

Part: RIB — CRACKED (WING) · airframe 44,321 hrs · 36,858 cycles

RIGHT SPAR 1 WING RIB NR 9 HAS CRACK AT SCREW HOLE. REPAIRED THE RIB.

Part: YOKE — CRACKED (LT ENGINE MOUNT) · airframe 44,321 hrs · 36,858 cycles

LEFT ENGINE FORWARD LOWER YOKE CRACKED. ACOMPLISHED REPAIR OF LT LOWER ENGINE YOKE.

Part: MUFFLER — DISCONNECTED (LT A/C PACK) · airframe 42,462 hrs · 35,332 cycles

LOUD BANG HEARD DURING APPROACH TO RDU. SMOKE SEEN FROM BELOW 10A. TURNING OFF BLEED AND PAC STOPPED SMOKE. FOUND LT PACK MUFFLER DISCONNECTED. SECURED MUFFLER. OPS CHECK GOOD

Part: BULB — INOPERATIVE (EXTERIOR) · airframe 42,395 hrs · 35,281 cycles

EXTERIOR EMERGENCY EXIT LIGHT IN FRONT OF RT WING, LIGHT NR 4, IS INOPERATIVE. R & R BULB IN EXTERIOR EMERGENCY EXIT LIGHT IN FRONT OF RT WING, LIGHT NR 4. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,395 hrs · 35,281 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 7, LIGHT NR 16B, IS INOPERATIVE. R & R BULB IN CEILING EMERGENCY EXIT LIGHT AT ROW 7, LIGHT NR 16B. OPS CHECKED GOOD.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 42,060 hrs · 35,008 cycles

F/O FLASHLIGHT NOT INDICATING THAT IT IS CHARGING. PERFORMED TEST OF F/O'S FLASHLIGHT. OPS CHECK GOOD.

Part: O-RING — LEAKING (PNEUMATIC SYS) · airframe 41,882 hrs · 34,860 cycles

BLEED 2 LEAK EICAS WARNING MESSAGE IN FLIGHT IN ICING CONDITION WITH NO LEAK LIGHT ON OVERHEAD PANEL. R & R 2 O-RINGS AT POSITION 14. OPS AND LEAK CHECK GOOD.

Part: SEAL — WORN (BLEED) · airframe 41,781 hrs · 34,779 cycles

BLEED 2 LEAK EICAS MSG DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE REPLACED BLEED SEALS AT POSITION 14 ON NR 2 BLEED IN FWD CARGO BULKHEAD, OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED SYS) · airframe 41,773 hrs · 34,774 cycles

BLEED 2 LEAK IN FLIGHT. CHECKED ALL JOINTS AND CLAMPS ON BLEED 2 SYS, NO LEAKS FOUND. UNABLE TO DUPLICATE. OK FOR SERVICE.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 40,548 hrs · 33,787 cycles

LEFT ELEVATOR UPPER SKIN HAS LARGE AREA OF OIL CANNING, SKIN AFT OF FRONT SPAR & BETWEEN YH-1898.0 & YH-2223.0. COMPLETED REPAIR WITH ERS-EM-55MR-263.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

FUSELAGE SKIN CORRODED UNDER COCKPIT FLOOR BETWEEN FRAMES 13 & 14 BETWEEN STRINGERS 20R & 19R. REPAIRED IAW ERS-EM-53MR-1160 & ERS-EM-53MR-1163.

Part: FITTING — CRACKED (RT AILERON) · airframe 40,548 hrs · 33,787 cycles

RIGHT AILERON OTBD LUG FITTING CRACKED & BENT. REQUIRES NEW FITTING & HAT BUSHING. REPLACED PCA FITTING IAW EO EM-27MR-112.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

STRINGER 18R PROFILE AT FRAME 13 IS CORRODED BEYOND LIMITS. R & R STRINGER 18R AT FRAME 13 IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 40,548 hrs · 33,787 cycles

LEFT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. CRACK IS APPROX 1 INCH LONG. REPAIRED DAMAGED ANGLE IAW ETN-EM-53-142.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

CARGO DOOR SILL CORRODED. REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 40,548 hrs · 33,787 cycles

RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. CRACK APPROX 1 INCH LONG. R & R ATTACH ANGLE IAW SRM 51-40-02 & ETN EM-53-142.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

RIGHT FWD CARGO DOOR TORSION BAR SUPPORT IS CRACKED AT FRAME 61. REPLACED RT FWD CARGO DOOR TORSION BAR SUPPORT IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 40,548 hrs · 33,787 cycles

LEFT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 47. CRACK APPROX 1 INCH LONG. REPAIRED DAMAGED ANGLE IAW ETN-EM-53-142.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED APPROX 4 INCHES BETWEEN FRAMES 47 & 48. REPAIRED IAW SRM 53-23-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 40,548 hrs · 33,787 cycles

LEFT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 48. CRACK APPROX 1 INCH LONG. REPAIRED DAMAGED ANGLE IAW ETN-EM-53-142.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

FUSELAGE SKIN CRACKED AT FRAME 75 BETWEEN STRINGER 1RT & 3RT APPROX 3/4". REPAIR HAS BEEN COMPLETED IAW ERS-EM-53MR-1184.

Part: FLOOR SUPPORT — CHAFED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

CENTER OMEGA BEAM IS CHAFED IN 2 AREAS. 1ST CHAFE IS AFT OF FRAME 55 & THE 2ND CHAFE IS AFT OF FRAME 54. REPAIRED OMEGA BEAM IAW ERS-EM-53MR-1162.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

FUSELAGE SKIN CRACKED AT FRAME 75 BETWEEN STRINGER 1 LT & 3 LT, APPROX 1/2". REPAIR HAS BEEN COMPLETED IAW ERS-EM-53MR-1185.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,548 hrs · 33,787 cycles

SHEAR CLIP AT FRAME 79, STRINGER 3R IS CRACKED .500 INCH. R & R SHEAR CLIP AT FRAME 79 STRINGER 3RH IAW SRM 51-40-02.

Part: SPAR — CRACKED (LT WING) · airframe 40,548 hrs · 33,787 cycles

LEFT WING SPAR 3 IS CRACKED NEAR RIB 3 AT THE WIRING HARNESS HOLE. COMPLIED WITH REPAIR LT SPAR 3 PERM REPAIR IAW ERS-EM-57MR-403.

Part: BRAKE — CONTAMINATED (MLG) · airframe 40,498 hrs · 33,731 cycles

DURING LANDING NOTICED DECREASED BRAKING EFFECTIVENESS. ON POST FLIGHT RT MAIN NOTED SMOKING. TEMPS HIGHER THAN LT SIDE BUT NOT ABNORMAL. DETERMINED BRAKES COVERED IN DEICE FLUID. PERFORMED TAXI CHECK WITH CREW. OPERATIONS CHECKED BRAKE IAW AMM 32-41-00. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LENS — BROKEN (EXTERIOR LIGHT) · airframe 40,367 hrs · 33,580 cycles

SERVICE DOOR EXTERNAL EMER LIGHT LENS BROKEN. REPLACED IAW AMM 33-50-10-420-002-A00.

Part: LIGHT — WRONG PART (CABIN) · airframe 40,117 hrs · 33,393 cycles

EMERGENCY LIGHTS FLOOR STRIP LT SIDE WRONG SIDE MARKING EMER EXIT. R & R FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: CABLE — MISINSTALLED (COCKPIT) · airframe 40,101 hrs · 33,375 cycles

ON DESCENT RADAR ALT STUCK AT 20 FT CONTINUOUS GPWS AUDIOS. RAD ALT TEST SHOWED RAD ALT 2 FAIL BELOW 10,000 WENT BACK TO NORMAL. ITEM DEFERRED IAW MEL 34-10. DMA MTX ACTION COMPLIED WITH IAW MEL 34-10. SEE ITEM NR 1 LOG PAGE 3731388 FOR ACTION TAKEN. RECONNECTED CO AX CABLE CORRECTLY. THIS RESTORES MEL 34-51. ACFT IS COMPLIANT FOR CAT II OPERATIONS. REF ITEM 1 ABOVE THIS LOG PAGE ACTION TAKEN PERFORMED OPERATIONS CHECK TCAS SYS IAW AMM 34-43-00. OPERATIONS CHECKED GOOD AT THIS TIME. MEL 34-33 RESTORED.

Part: WIRE HARNESS — DEFECTIVE (RADIO ALTIMETER) · airframe 40,100 hrs · 33,373 cycles

RAD ALT STUCK AT 25' DURING CLIMB OUT. NO EICAS MSGS. RECEIVED BANK ANGLE ALERTS ABOVE 3000' AGL. RAD ALT BEGAN WORKING AGAIN ON RETURN AT 2500' AGL. TRANSFERRED TO NRWC 606-DFW-02150. XFER FROM NRWC 606-DFW-02150. R & R RAD ALT HARNESS IAW AMM 34-31-01, AMM 34-31-02 & WM 34-31-50. OPERATIONS CHECKED GOOD IAW AMM 34-31-00. ACFT IS COMPLIANT FOR CAT II OPERATIONS.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 40,021 hrs · 33,312 cycles

CABIN AFT EMER FLASHLIGHT CRADLE IS BROKEN. R & R CABIN AFT EMER FLASHLIGHT CRADLE IAW AMM 33-50-16.

Part: LIGHT — UNSECURE (FLASHLIGHT) · airframe 40,021 hrs · 33,312 cycles

CAPTAIN'S EMER FLASHLIGHT IS INOPERATIVE. SECURED CAPTAIN'S EMER FLASHLIGHT LAMP IAW CMM 25-60-11. OPERATIONAL CHECKED GOOD.

Part: STRIP — WRONG PART (CABIN) · airframe 39,831 hrs · 33,160 cycles

EMERGENCY STRIP 18A ORANGE READING EMER EXIT, SHOULD BE ORANGE ARROWS POINTING FWD TO EMER EXIT. R & R REAR STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,596 hrs · 32,967 cycles

EMERGENCY FLOOR LIGHTING STRIP AT ROW 12 - 13 INOPERATIVE. R & R EMER FLOOR LIGHTING STRIP AT ROW 12 - 13 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — LEAKING (WING) · airframe 39,594 hrs · 32,966 cycles

FUEL SMELL IN COCKPIT TAXIING IN, REPEAT WRITE UP. APU OFF NO REPORT OF SMELL IN CABIN. PERFORMED GVI OF WINGS & OF ALL PREVIOUS REPAIRS, NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY WHILE PERFORMING TAXI CHECK. REFERENCE WORK ORDER 1142R1695, FOUND FUEL SEEP BETWEEN 4TH & 5TH STRINGERS FWD OF AFT SPAR AT RIB 1 UP TO RIB 2 Y-960.00 - Y-1300.00. CLEANED & RESEALED WITH PR1826 B1/2. FUELED TO 4800 LBS, LEAK CHECKED GOOD IAW SRM 51-20-01 & AMM 28-11-00.

Part: WIRE — BROKEN (CABIN) · airframe 39,588 hrs · 32,958 cycles

NUMBER 3 FLOOR PROXIMITY STRIP LIGHT DOES NOT ILLUMINATE HAS BROKEN WIRE. R & R NR 3 FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12 OPERATIONS CHECKED GOOD.

Part: FUEL TANK — LEAKING (FUEL SYSTEM) · airframe 39,588 hrs · 32,958 cycles

COCKPIT SMELL LIKE JET FUEL FROM UNKNOWN SOURCE, TRANSFERRED TO NRWC 606-ORD-01996. PERFORMED FIM TASK 21-20-00-810-803-A THROUGH ALL STEPS. NO FUEL ODOR DETECTED AT THIS TIME. ODOR DETERMINED TO BE COMING FROM APU BLEED APU AND APU FUEL VALVE DEFFERRED PER MEL 49-1 AND 28-5 REF AML 3663526 ITEMS 3 AND 4 FOR DEFERRAL. FOUND FUEL LEAK FORWARD RT SIDE CENTER BOX AT STRINGER 19R BODY STATION X 13601.0 ON BOLT THAT GOES THRU STRINGER 19R INTO RT CENTER BOX. REMOVED AND REINSTALLED BOLT IAW SRM 51-40-02 AND SRM 57-00-01 FOR SEALING BOLT IN TANK. COMPLIED WITH LEAK CHECK IAW ETN EM 28-045. NO LEAKS NOTED. APU SOV OPS CHECK GOOD IAW EMB AMM 28-22-01. MEL ITEM RESTORED. APUL MEL 49-1 RESTORED DUE TO MEL 28-5 RESTORATION. OPS CHECK GOOD IAW EMB AMM 49-10-00. MEL ITEM RESTORED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 39,563 hrs · 32,929 cycles

COCKPIT SMELLS LIKE FUEL ODOR FROM UNKNOWN ORIGIN. PERFORMED FIM TASK 21-20-00-810-803-A THROUGH ALL STEPS. NO FUEL ODOR DETECTED AT THIS TIME.

Part: UNKNOWN — ODOR · airframe 39,431 hrs · 32,784 cycles

STRONG JET FUEL ODOR WITH PACKS RUNNING. TRANSFERRED TO NRWC 606-ORD-01973. REF NRWC 606-ORD-01973 PERFORMED PACK 1 & 2 OPERATIONAL CHECK FOR 1 HOUR IAW AMM 21-51-00. OPERATIONS CHECKED GOOD, NO SMELL REF ITEM 2 THIS LOG PAGE.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 39,420 hrs · 32,770 cycles

FUEL ODOR SMELL IN COCKPIT WHILE RUNNING PACKS NR 1 & 2 ON APU BLEED AIR. TRANSFERRED TO NRWC 606-ORD-01972. TROUBLE SHOT IAW FIM 21-20-00-810-803A. ABNORMAL SMELL IN COCKPIT & CABIN, UNKNOWN SOURCE. FOUND APU OIL OVER SERVICED. DRAINED OIL DOWN TO FULL LIMIT. GND RAN TO CLEAN OIL CONTAMINATION FROM DUCTS IAW AMM 21-20-00-100-805A. NO DEFECTS NOTED.

Part: UPLOCK — FAILED (RT MLG) · airframe 39,402 hrs · 32,753 cycles

ON CLIMB OUT LG LEVER DISAGREE WHEN PUTTING GEAR UP. RT MAIN GEAR INDICATED UNSAFE. INSPECTED & FOUND RT MLG UPLOCK BOX TO BE LEAKING. R & R RT MLG UPLOCK BOX IAW AMM 32-33-10. OPERATIONS CHECKED GOOD.

Part: VALVE — FAULTY (AC BAY) · airframe 39,055 hrs · 32,460 cycles

AFTER & IN THE CLIMB OUT WE HAD THE RAPID CAIN DEPRESSURIZATION WARNING. DID ALL THE EMERGENCY CHECKLIST & STOPPED THE CLIMB AT 12000 CABIN ALT, ON THE THE MANUAL & CONTROL BUT COULD NOT CONTROL THE DESCEND UNTIL WE GOT TO 10,000'. RETURNED BACK & LANDED WITH AN OVERWEIGHT OF 45558 POUNDS. HAD A SMOOTH LANDING WITHOUT EXCEEDING 300 FEET PER MINUTE. OVERWEIGHT LANDING WITHIN LIMITS IAW AMM 5-50-25. DEFERRED PRESSURIZATION IAW MEL 21-21. INSTALLED NEW GND CONNECTION VLV IAW AMM 21-22-04, OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.

Part: VALVE — FAILED (NR 2 A/C PACK) · airframe 38,946 hrs · 32,364 cycles

NR 2 A/C PACK OVERHEAT MESSAGE ON EICAS THAT WOULD NOT GO OUT, WITH A HOT OR BURNING ODOR. R & R DUAL TEMP CONTROL VALVE IAW AMM 21-60-01. OS CHECKED GOOD. LEAK CHECKED GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,689 hrs · 32,140 cycles

SHEAR CLIP AT FRAME 14 RT SIDE BETWEEN STRINGER 6R - 8R CRACKED. REPAIRED SHEAR CLIP AT FRAME 14 RT SIDE BETWEEN STRINGER 6R - 8R IAW ERS-EM-53MR-424 PART A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE SKIN. R & R LT CTR FUSELAGE SKIN IAW SRM 51-40-02 & ETN-EM-53-262.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT, REPLACE RT CTR FUSELAGE SKIN. R & R RT CTR FUSELAGE SKIN IAW SRM 51-40-02 & ETN-EM-53-262.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE LT ELEVATOR INBD MID SKIN. R & R LT ELEVATOR INBD MID SKIN IAW SRM 51-40-02, AEA ETN-EM-55-073 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE LT STABILIZER SKIN. R & R LT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE LT FWD FUSELAGE I SKIN. R & R LT FWD FUSELAGE I SKIN IAW SRM 51-40-02 & AEA ETN-EM-53-235.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT STABILIZER SKIN. R & R RT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT ELEVATOR MID SKIN. R & R RT ELEVATOR MID SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT, REPLACE CTR FUSELAGE II TOP SKIN. R & R CTR FUSELAGE II TOP SKIN IAW SRM 51-40-02 & AEA ETN-EM-53-263.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER INBD SKIN. R & R RT ELEVATOR UPPER INBD SKIN IAW SRM 51-40-02, AEA ETN-EM-55-076 & ETN-EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE RT ELEVATOR SKIN TIP. R & R RT ELEVATOR SKIN TIP IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,689 hrs · 32,140 cycles

MULTIPLE HAIL DAMAGE EVENT REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & AEA ETN-EM-55-073.

Part: CONNECTOR — BROKEN (CABIN) · airframe 38,689 hrs · 32,140 cycles

SERVICE DOOR FRAME FWD LOWER TRIM PANEL EMERGENCY LIGHT CONNECTOR BROKEN. REPAIRED CONNECTOR ON SERVICE DOOR FRAME FWD LOWER TRIM PANEL EMERGENCY LIGHT IAW SWPM 20-21-00 STEP 5. LIGHT OPERATIONS CHECK GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 38,654 hrs · 32,118 cycles

DURING CLIMB FROM DFW, RECEIVED PTRIM MAIN INOPERATIVE EICAS WARNING AFTER PASSING ACCELERATION ALTITUDE. BOTH CAPTAIN & FIRST OFFICER SWITCHES INOPERATIVE, BACKUP SWITCH NORMAL. CONTINUED TO SDF FOR CONTRACT MX. RESET IAW FIM 27-43-00 & OPERATIONS CHECK IAW AMM 27-43-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,658 hrs · 32,121 cycles

FOUND LT WING TO FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE & COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD, NO FURTHER FAULTS FOUND.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,614 hrs · 32,085 cycles

EMERGENCY LIGHT FWD OF WING INOPERATIVE. R & R FWD EMERGENCY LIGHT IAW AMM 33-50-10, LIGHT OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 37,843 hrs · 31,487 cycles

ON FLIGHT 3226 THE CREW REPORTED CAPTAIN`S FLASHLIGHT HOLDER BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R 7 R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16 & OPERATIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 37,130 hrs · 30,884 cycles

F/A FLASHLIGHT WILL NOT CHARGE. R & R FLASHLIGHT ASSY IAW EAMM 33-50-16, OPS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 37,038 hrs · 30,813 cycles

FWD F/A EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-55-16. OPS CHECKED GOOD.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 36,758 hrs · 30,572 cycles

NR 1 HYD QTY LOW, "EMPTY". HYD SYS 1-FAIL AND GEAR ELECTRICAL OVERIDE DID NOT ACTUATE. FREE FALL LEVER WAS USED TO LOWER GEAR IAW AOM-1. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R NR 1 HYD ENGINE DRIVEN PUMP IAW AMM 29-10-03. OPS AND LEAK CHECKED GOOD. R & R HYD SYS NR 1 EMDP IAW AMM 29-10-04. OPS CHECKED GOOD. R & R HYD FILTERS FOR SYS NR 1 IAW AMM 29-10-08. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 36,340 hrs · 30,237 cycles

THE CREW REPORTED THAT DURING CRUISE FLIGHT, NR 2 ENGINE (N1) SMOOTHLY ROLLED BACK ABOUT 25-30 PERCENT AND THEN SMOOTHLY CAME BACK UP, IT DID THIS 3 TIMES IN ABOUT 15 MINUTES AND THEN RETURNED TO NORMAL. ON LANDING, GOT E1 EXCEEDANCE ON EICAS. THE ACFT WAS REMOVED FROM SERVICE. DOWNLOADED CMC, FOUND 2B INPUT FAIL MESSAGES. R & R THE 2B FADEC IAW AMM 73-25-10. GROUND RAN CHECK AND IT WAS GOOD. NO DISP E1, E2 NOTED. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,317 hrs · 30,222 cycles

DURING B INSPECTION, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, STEPS 2M(1)(A-F) AND 3IL(1)(A-G). OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,166 hrs · 30,109 cycles

DURING B INSPECTION FOUND THE MAIN PASSENGER DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR EXTERNAL EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,007 hrs · 29,974 cycles

DURING B INSPECTION FOUND THE MID CABIN OVER HEAD FORWARD FACING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 AC/DC INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,715 hrs · 29,735 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD FUSELAGE I UPPER SKIN DENTED DUE TO BIRD STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED DOUBLER IAW AEA EO EM-53MR-1887. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,734 hrs · 29,756 cycles

DURING B INSPECTION FOUND THE NR 1 AND 8 EMERGENCY LIGHT STRIPS NEED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AND 8 EMERGENCY LIGHT STRIPS AND FLOOR SIDEWALL BASE ASSEMBLIES IAW EMB 145 AMM 33-50-12.

Part: WIRE — CUT (CABIN) · airframe 35,734 hrs · 29,756 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 8 CONNECTOR WIRES ON AIRCRAFT SIDE CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP NR 8 WIRES IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 35,733 hrs

DURING MAINTENANCE INSPECTION FOUND THE NR 3 AND 6 EMERGENCY LIGHT STRIP CONNECTORS ON THE FLOOR BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE NR 3 AND 6 EMERGENCY LIGHT STRIP CONNECTORS IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — CHAFED (CABIN) · airframe 35,734 hrs · 29,756 cycles

DURING MAINTENANCE INSPECTION FOUND THE WIRE HARNESS (AIRCRAFT SIDE) FOR THE EMERGENCY LIGHT STRIP NR 1 CHAFED ON BOTH WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE WIRE HARNESS (AIRCRAFT SIDE) FOR THE EMERGENCY LIGHT STRIP NR 1 IAW EMB 145 AMM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — TORN (MAIN DOOR) · airframe 35,733 hrs · 29,755 cycles

DURING B INSPECTION FOUND THE MAIN DOOR SEAL TORN ALONG THE UPPER SURFACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR SEAL IAW EMB145 AMM 52-18-04. THE FUNCTIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DETACHED (CABIN) · airframe 35,734 hrs · 29,756 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP 3 WIRE HARNESS DETACHED FROM THE LIGHT STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP #3 IAW EMB145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUIDE — OBSTRUCTED (CABIN DOOR) · airframe 35,706 hrs · 29,722 cycles

ON FLIGHT 2759 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED EXCESSIVE MOLYKOTE FROM MAIN DOOR GUIDES IAW EMB 145 AMM 20-30-04. PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW EMB 145 AMM 52-18-00-820-001-A00. FOUND EFFORT AT 44 IBS WITHIN LIMITS. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — CONTAMINATED (RUDDER) · airframe 35,706 hrs · 29,722 cycles

FOR FLIGHT 2759 THE CREW REPORTED THAT DURING THE HYDRAULIC FLIGHT CONTROL CHECK NR 2 HYD RIGHT RUDDER DIFFICULT TO PUSH FORWARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLED RUDDER SYSTEM NR 1 AND SYSTEM NR 2 IAW EMB 145 AMM 27-22-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 35,620 hrs · 29,644 cycles

ON FLIGHT 4092 THE CREW REPORTED THE MAIN PASSENGER CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED THE PASSENGER DOOR. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (NOSE) · airframe 35,446 hrs · 29,516 cycles

NOSE SKIN DENTED. C/W PART B OF EO EM-53MR-1887, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: WIRE — LOOSE (EXIT SIGN) · airframe 35,279 hrs · 29,383 cycles

DURING B INSPECTION FOUND THE EMERGENCY SIGN ON CEILING (FORWARD FACING) INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED EMERGENCY SIGN IN CEILING (FORWARD FACING) FOUND LOOSE WIRE AND REPAIRED AS NEEDED IAW EMB 145 AMM TASK 33-50-15-000-801-A AND 33-50-15-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RETAINING RING — MISSING (CABIN DOOR) · airframe 35,249 hrs · 29,352 cycles

ON FLIGHT 4092 THE FLIGHT ATTENDANT REPORTED THE CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MISSING RETAINING RING ON FOLDING FLAP ACTUATING ROD. INSTALLED NEW RETAINING RING PER STANDARD MAINTENANCE PRACTICES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUEL SYS — LEAKING (LT WING) · airframe 35,231 hrs · 29,340 cycles

ON FLIGHT 4284 THE CREW REPORTED VISUAL FUEL LEAK STREAMING FROM LEFT WING NEAR ROOT FROM HINGES OF THE SPOILER (UPPER SIDE OF WING) AND FROM INBOARD AND OUTBOARD FLAPS. VISUAL CONFIRMATION OF 1800 LBS IMBALANCE IN FLIGHT. REPORTS OF FUEL STREAMING HEAVIER DURING CLIMB AND LESS DURING DESCENT. THE CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO ROC. FUEL LEAK EMERGENCY CHECKLIST WAS PERFROMED AND AN OVERWEIGHT LANDING CHECK LIST WAS PERFORMED BEFORE ARRIVAL INTO ROC. THE AIRCRAFT LANDED WITHOUT INCIDENT. LANDING EMERGENCY AT 44100 LBS AT A RATE OF 200 FPM AT TOUCHDOWN AND FELT SMOOTH. SMELL OF FUEL CONFIRMED EVEN AFTER PARKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED LEFT WING FUEL TANK FLAPPER AT RIB 19 IAW EMB 145 AMM 28-11-04. NO DEFECTS NOTED (SEE ITEM NR 4 BELOW) FUELED AIRCRAFT TO 11000+LBS AND TAXIED. NO FUEL LEAKS NOTED. VISUALLY INSPECTED ALL FUEL TANK PANELS AND FUEL CAP NO LEAKS NOTED. ONLY FLUID NOTED ON REAR OF LEFT WING WAS FOUND TO BE WATER CONDENSATION AND DE-ICE FLUID.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 35,205 hrs · 29,317 cycles

ON FLIGHT 4103 THE CREW REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS IAW EMB-145 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 35,030 hrs · 29,174 cycles

DURING B INSPECTION FOUND SEAT 12A FORWARD EMERGENCY SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER PER EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,977 hrs · 29,134 cycles

DURING B INSPECTION FOUND THE CENTER AISLE EMERGENCY LIGHT NR 4 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT NR 4 IAW AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 34,829 hrs · 29,023 cycles

ON FLIGHT 2724 - THE CREW REPORTED THE MAIN PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. CREW REPORTED IT FELT ABNORMAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED THE MAIN DOOR HINGE AND ROLLERS. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,479 hrs · 28,726 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT INOPERATIVE AT 12C. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT AT 12C IAW AMM TASK: 33-50-08-000-801-A, AND 33-50-08-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 34,168 hrs · 28,502 cycles

ON FLIGHT 3248 THE FLIGHT ATTENDANT REPORTED THE FLASHLIGHT CATCH IS NOT HOLDING LIGHT IN THE HOLDER & KEEPS FALLING OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN EMERGENCY FLASHLIGHT AND CRADLE IN ACCORDANCE WITH EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,875 hrs · 28,261 cycles

DURING B INSPECTION, FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 12 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERHEAD AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,860 hrs · 28,246 cycles

FOR FLIGHT 2952 THE CREW REPORTED AN AMBER EICAS MESSAGE "PACK 1 OVLD" PRECEEDED BY A ODOR LIKE COOKING FOOD. TRIPPED OFF ON APU AND ENGINE BLEEDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PACK COOLING SYSTEM NR 1 WAS VERIFIED AND OPERATED NORMAL. BLEED TEMP IN NORMAL AND TEMP CONTROL FUNCTION NORMAL. SYSTEM OPERATED FOR 25 MINUTES NO FAULT FOUND IAW EMB-145 AMM 21-00-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HINGE — LACK OF LUBE (MAIN DOOR) · airframe 33,682 hrs · 28,099 cycles

ON FLIGHT 2845 THE CREW REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN, THE ROLLER PIN CATCHES ON LATCH AND METAL IS WORN SHARP. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR HINGES IAW AMM 52-18-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,529 hrs · 27,980 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT OVER WING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVER WING EMERGENCY LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,503 hrs · 27,966 cycles

DURING B-INSPECTION, FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 12. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 12 CEILING EMERGENCY LIGHT LAMP IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,479 hrs · 27,944 cycles

DURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT HAND OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,407 hrs · 27,889 cycles

DURING B-INSPECTION FOUND THE CEILING EMERGENCY LIGHT AT 12A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT AT 12A IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 33,210 hrs · 27,737 cycles

ON FLIGHT 2786 FLIGHT ATTENDANT REPORTED FLASHLIGHT MISSING ABOVE FLIGHT ATTENDANT JUMPSEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMPSEAT AS PER EMB MM 25-60-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COUPLING — INOPERATIVE (NR 1 A/C PACK) · airframe 33,154 hrs · 27,688 cycles

ON FLIGHT 2040 THE CREW REPORTED A BLEED LEAK NR 1. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FWA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH BLEED LEAK OPERATIONAL CHECK IAW AMM 36-00-00. BLEED NR 1 LEAK STAYS EXTINGUISHED. REMOVED AND REPLACED LOWER COUPLING ON NR 1 PAC IAW AMM 21-20-04. THE OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,825 hrs · 27,443 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT INOPERABLE AT SEATS 14-16 A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PROXIMITY LIGHT AT SEATS 14-16 A IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — OUT OF ADJUST (CABIN DOOR) · airframe 32,585 hrs · 27,288 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN. ADJUSTED AND SET MAIN CABIN DOOR HANDLE IAW EMB AMM 52-18-00.

Part: SHUTOFF VALVE — LEAKING (LT WING) · airframe 32,293 hrs · 27,074 cycles

ON FLIGHT 3314 THE CREW REPORTED A FUEL SEAP ON THE LEFT WING INFLIGHT. THE CREW ELECTED TO DIVERT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT SHUTOFF VALVE IAW EMB AMM 28-23-02. THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 30,991 hrs · 26,098 cycles

ON FLIGHT 2702 THE CREW REPORTED THAT AT 37,000 FLIGHT LEVEL IN CRUISE THE AUTO CABIN PRESSURIZATION FAILED CABIN. THE PRESSURIZATION WAS AT 11,000. NO MASK DROP. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED INTO MTY. THE CREW DID NOT USE MANUAL MODE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. EMOVED AND REPLACED THE DIGITAL CONTROLLER, CLEANED NR 3 PITOT STATIC SYSTEM, AND THE LEAK CHECK WAS GOOD. CHECKED NR 1 AND 2 PITOT STATIC FOR MOISTURE. THE FUNCTIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 30,976 hrs · 26,086 cycles

ON FLIGHT 3565 THE CREW REPORTED THAT CLIMBING THROUGH FLIGHT LEVEL 270-280 THEY LOST CONTROL OF AUTO PRESSURIZATION. THE CAPTAIN DECLARED AN EMERGENCY DESCENT AND WENT TO MANUAL MODE. THE PANEL WENT TO DASHES IN MANUAL MODE. THE AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03 . REMOVED AND REPLACED THE CHECK VALVE AND THE OUTFLOW O-RINGS VALVES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,870 hrs · 26,000 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED AT FRAME 25 WHERE CARBON BEAM ATTACHES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,870 hrs · 26,000 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND CENTER OMEGA BEAM CORRODED AT FRAME 25 WHERE CARBON BEAM ATTACHES. THE AIRCRAFT WAS REMOVED FROM SERCVICE. REPAIRED CENTER OMEGA BEAM AT FRAME 25 WITH DOUBLER REPAIR IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,870 hrs · 26,000 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSS MEMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW SRM 53-00-10 FIGURE 201. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 30,661 hrs · 25,845 cycles

ON FLIGHT 2848 THE CREW REPORTED THAT DURING CRUISE AT 36,000 FEET THE CABIN PRESSURE DROPPED. THE CREW INITIATED DESCENT IMMEDIATELY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO XNA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND PNEUMATIC OUTLFOW VALVE TAKING LONGER THAN NORMAL TO OPEN DURING FUNCTIONAL, REMOVED AND REPLACED VALVE IAW EMB-145 AMM 21-31-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — DAMAGED (ANTI-ICE SYS) · airframe 27,543 hrs · 23,398 cycles

ON FLIGHT 4187 THE CREW REPORTED DURING THE APPROACH RECEIVED A STABILIZER ANTI ICE FAIL MESSAGE WITH AN AUTOPILOT DISCONNECT. THE CREW DECLARED AN EMERGENCY. THE CREW FOLLOWED THE AOM CHECKLIST AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL LOW PRESSURE SWITCHES NR 1 AND NR 2 IAW EMB 145 AMM 30-12-02, EMB 145 AMM 30-00-00. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 26,937 hrs · 22,899 cycles

ON FLIGHT 3739 THE CREW REPORTED A BURNING SMELL IN THE GALLEY AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NEW RECIRCULATION GASPER FAN IAW EMB-145 AMM 21-24-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND RIGHT OUTBOARD STRINGER 19R CHAFED BETWEEN FRAMES 52R AND 53R. REMOVED CHAFED BY BLENDING. FABRICATED FOUR SHIMS AND TWO DOUBLER ANGLES. REPAIR DONE IAW EMB GST-3895/01, GST 3958/01, GST-3458/01, GST-3486/01, GST-3725/01, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY BLENDING OUT. FABRICATED A Z-PROFILE REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3862/01, ITEM 14 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM AT FRAMES 20 AND 23. REMOVED CORROSION BY BLENDING OUT AT FRAME 20 AND 23. FABRICATED TWO U-CHANNEL REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-3862-/01, ITEM 10 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV INSPECTION, FOUND LEFT OUTBOARD STRINGER 19L CHAFFED BETWEEN FRAMES 52L AND 53L. REMOVED CHAFED BY BLENDING. FABRICATED FOUR SHIMS AND TWO DOUBLER ANGLES. REPAIR DONE IAW EMB GST 3895/01, GST3458/01, GST-3486/01, GST 3725/01, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE RIGHT GALLEY FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING OUT. FABRICATED AN U-CHANNEL REPAIR DOUBLER. WORK DONE IAW EMB GST 3862/01, ITEM 12 AND STANDARD SRM PRACTICES. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

LEVEL 2 CORROSION ON BEAM BENEATH LOWER BAGGAGE DOOR CUT OUT PLATE. REPLACED LOWER BAGGAGE DOOR CUTOUT FRAME IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING, FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED NEW DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM CORRODED. INSTALLED REPAIR DOUBLERS ON GALLEY CENTER BEAM ON FRAME 20-23 IAW EMB GST-3862/01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING. RIGHT GALLEY FLOORBEAM CORRODED. INSTALLED REPAIR DOUBLER AT FRAME 20 IAW EMB 145 GST 3862/01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS LEVEL 2 FINDING. LEFT OMEGA AT FRAME 20 HAS CORROSION ON PREVIOUS REPAIR. REPAIRED IAW EMB145 SRM 53-21-10. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AFT DIGITAL CORRODED. REPAIRED IAW EMB GST-3862/01. (M)

Part: CAP — CORRODED (LT MLG) · corrosion level 2

THIS IS A LEVEL 2 FINDING. LEFT FORWARD MLG BEARING CAP CORRODED. REMOVED AND INSTALLED SERVICEABLE STRUT SWIVEL CAP IAW EMB 145 AMM 32-10-01-000-801-A, 32-10-01-400-801-A. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS LEVEL 2 FINDING. FORWARD DIGITAL CORRODED. REPAIRED IAW EMB GST-3862/01. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

THIS A LEVEL 2 FINDING. SERVICE DOOR SILL (FORWARD) CORRODED. INSTALLED REPAIR DOUBLER IAW EMB GST-3862/01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF A/C, FOUND CORROSION ON THE LEFT OMEGA BEAM AND PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR AND CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 9SRM145/1142 CHAPTER 53 REV 16) 53-21-01 AND STANDARD SRM PRACTICES. (M)

Part: FRAME — DAMAGED (FUSELAGE)

ABI - DURING AN IMBV, FOUND A HOLE IN FRAME 23 FLANGE AT STRINGER 17R. REAMED HOLE TO .193 INCH. PARTIALLY COUNTERSUNK AND DEBURRED. PERFORMED ET INSPECTION OF THE HOLE WITH NO REJECTABLE INDICATIONS. WORK DONE IAW EMB GST-3894/01 AND STANDARD SRM PRATICES. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ORD - FLT 4221 - DURING TAXI, AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND CANNON PLUG FOR AFT OVERHEAD EMERGENCY LIGHT TO BE DISCONNECTED. CANNON PLUG WAS RECONNECTED IAW EMB 145 AMM. LIGHT OPERATIONALLY CHECKED GOOD. (M)

Part: SHUTTLE VALVE — DEFECTIVE (BRAKE SYS)

ORD - FLT 3331 - DURING CRUISE, CREW NOTED HYDRAULIC SYSTEM ONE QUANTITY IN THE YELLOW. PRESSURE WAS WITHIN LIMITS. CREW DIVERTED TO ORD, EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE BRAKE SHUTTLE VALVE IAW EMB MM AND SERVICED THE NR 1 HYDRAULIC SYSTEM. OPS AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: NOZZLE — MALFUNCTIONED (FUEL SYSTEM)

XNA - FLT 3705 - DURING FLIGHT, CREW NOTED EXHAUST SMELL IN FLIGHT COMPARTMENT AND CABIN. NOTE ANIT-ICE SYSTEM WAS ON AT THE TIME. AIRCRAFT LANDED SAFELY IN XNA. NO FURTHER INCIDENTS WERE REPORTED. MAINTNANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL AND LEAK WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WARNING SYSTEM — FALSE ACTIVATION (ENGINE OIL)

CLE - FLT 4028 - HAD E1 HIGH OIL PRESSURE ON TAKEOFF ROLL, WAS WITHIN LIMITS BUT ABORTED TAKEOFF ANYWAY. PERFORMED OPS CHECK. NO DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER)

FLT 4084 - ORD - ON TAKEOFF ROLL, CREW HAD ENGINE .5 REVERSE DISAGREE ON EICAS, ABORTED TAKEOFF AND RETURNED TO GATE. (M)

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE)

ON TAKEOFF ROLL, CREW NOTED ENGINE 2 HAD OIL PRESS WARNING OF 91 PSI. ABORTED TAKEOFF AND RETURNED TO GATE. TROUBLESHOT SYSTEM AS PER AMM. OIL PRESSURE WAS WITHIN LIMITS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUSE — INOPERATIVE (BATTERY PACK)

ORD - FLT 4355 - TWO CONSECUTIVE EMERGENCY FLOOR LIGHT SECTIONS WILL NOT TEST. REMOVED AND REPLACED FUSE IN NR 2 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PUMP — FAILED (NR 1 HYD SYSTEM)

ORD - FLT 4329 - FLIGHT CREW DECLARED EMERGENCY ANNOUNCING NR 1 HYDRAULIC SYSTEM OVERHEATED INDICATION DURING FLIGHT. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP. OPS AND PRESSURE CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — LEAKING (HYDRAULIC SYSTEM)

CLE - FLT 4387 - NR 1 HYDRAULIC SYSTEM FAILED. LANDING GEAR HAD TO BE MANUALLY EXTENDED. REMOVED AND REPLACED LEAKING HYDRAULIC PRESSURE SWITCH. SERVICED SYSTEM AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER DEFECTS NOTED. (X)