N618AE

Part: NONE — NONE · airframe 49,515 hrs · 45,085 cycles

FA AFT EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AUTH 110346M-C REF 25-32 MOC 630997

Part: NONE — NONE · airframe 49,475 hrs · 45,039 cycles

RH EXTERIOR OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH EXTERIOR OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10, NO FIX. RAR #4 EMERGENCY BATTERY PACK AND CHARGER IAW EMB 145 AMM 33-50-10. NO FIX. REMOVED RH EXTERIOR OVERWING EMERGENCY LIGHT ASSY IAW EMB 145 AMM 33-50-10, FOUND CANNON PLUG TO BE DISCONNECTED, REATTACHED CANNON PLUG AND REINSTALLED RH EXTERIOR OVERWING EMERGENCY LIGHT ASSY IAW EMB 145 AMM 33-50-10. OPC GOOD

Part: NONE — NONE · airframe 49,248 hrs · 44,782 cycles

MEL 2532 - AUTH# 100085M-C FA FWD FLASHLIGHT INOP LOGPAGE: 4715664-C/A-RAR FA FWD FLASHLIGHT ASSY IAW EMB145 AMM 33-50-16. OPC GOOD. MEL 25-32 AUTH# 100085M-C RESTORED.

Part: LIGHT — INOPERATIVE (SEAT 12A) · airframe 49,084 hrs · 44,593 cycles

SEAT 12A OVERWING EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-07. OPS CHECK GOOD.

Part: CONTACTOR — BURNED (RECIRC FAN) · airframe 48,490 hrs · 43,949 cycles

STRONG ELEC FUME SMELL WHILE DECENDING THROUGH FL240 CAME AND WENT FOR THE REMAINDEROF FLIGHT.-C/A- FOUND LH RECIRCULATION FAN CONTACTOR BURNED . RAR RECIRCULATION FAN CONTACTOR K0189 AND FUSE IAW AMM 21-24-03 . PERFORMED CHECK OF THE AIRCONDITIONING DISTRIBUTION SYSTEM IAW AMM 21-20-00-700-801-A/500. OPC GOOD .NO DEFECTS NOTED.

Part: STRINGER — CORRODED (FRAMES 19A-20) · airframe 47,720 hrs · 43,235 cycles

CORROSION ON STR 17R BETWEEN FR 19A AND FR 20. C/A: REMOVED AND REPLACED DAMAGED PORTION OF STRINGER 17R BETWEEN FR 16-24, IAW EMB 145 SRM 53-00-03 ITEM 7.

Part: VALVE — CORRODED (TOILET) · airframe 47,718 hrs · 43,234 cycles

SSI 53-20-29 TOILET WASTE VALVE BUCKET IS CORRODED. C/A: REMOVED AND REPLACED WASTE VALVE CUP (BUCKET), IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03.

Part: PROFILE — CORRODED (ESCAPE HATCH) · airframe 47,718 hrs · 43,234 cycles

SSI 52-21-06 CORROSION ON LT PASSENGER ESCAPE HATCH LOWER L PROFILE. C/A: REMOVED AND REPLACED LT PASSENGER ESCAPE HATCH LOWER L PROFILE, IAW EMB145 SRM 51-20-03, EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-01.

Part: DOOR SILL — CRACKED (FRAME 66) · airframe 47,718 hrs · 43,234 cycles

FRAME 66 CRACKED AT CARGO DOOR SILL ON T BRACKET. C/A: REMOVED AND REPLACED FR 66 LOWER SECTION, IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 64-68) · airframe 47,718 hrs · 43,234 cycles

SSI 53-30-48: AIRCRAFT STRUCTURE CARGO DOOR LOWER CUTOUT CORRODED, MARKED. C/A: REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT (SILL), IAW EMB 145 SRM 51-40-02.

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 47,718 hrs · 43,234 cycles

CORROSION ON CARGO DOOR LOWER LT PROFILE. C/A: R & R CARGO DOOR LOWER LT PROFILE, IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02.

Part: SKIN — DAMAGED (FRAMES 73-74) · airframe 47,718 hrs · 43,234 cycles

EXTERNAL FUSELAGE SKIN HAS A CREASE BETWEEN FR 73-74 AND STGR 12L-13L. C/A: PERFORMED A TYPE A SKIN DOUBLER REPAIR AT CEASE BETWEEN FR 73-74 STGR 12L-13L, IAW EMB 145 SRM 53-31-01RE ITEM 2 FIGURE 201 SHEET 1.

Part: PROFILE — CORRODED (ESCAPE HATCH) · airframe 47,718 hrs · 43,234 cycles

CORROSION ON RT PASSENGER ESCAPE HATCH LOWER LT PROFILE. C/A: R & R RT PASSENGER ESCAPE HATCH LOWER LT PROFILE, IAW EMB 145 SRM 51-20-03, 51-40-02, AND 51-20-01.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 47,718 hrs · 43,234 cycles

CARGO DOOR INNER WEBBING (SKIN) HAS 3 GOUGES AT PREVIOUS REPAIR. C/A: RE-ACCOMPLISHED 2 EACH REPAIRS ON THE CARGO DOOR INNER LOWER SKIN, IAW EMB 145 SRM 52-30-01 AND ETN-EM-52-043.

Part: DOOR FRAME — CORRODED (LT OVERWING) · airframe 47,718 hrs · 43,234 cycles

RT OVER WING HATCH LOWER FRAME IS CORRODED AROUND 2 FASTENER HOLES ON AFT END. C/A: R & R RT PASSENGER ESCAPE HATCH LOWER LT PROFILE BEAM, IAW EMB 145 SRM 51-20-03, 51-40-02 AND 51-20-01.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 47,718 hrs · 43,234 cycles

CARGO DOOR CUTOUT FR 65 SHEAR CLIP CORRODED. C/A: R & R CARGO DOOR CUTOUT FR 65 SHEAR CLIP, IAW EMB 145 SRM 53-31-04.

Part: BRACKET — CORRODED (FRAME 65) · airframe 47,718 hrs · 43,234 cycles

FR 65 T BRACKET CORRODED. C/A: R & R FR 65 T BRACKET, IAW EMB 145 SRM 51-40-02.

Part: YOKE — CRACKED (RT ENGINE) · airframe 47,718 hrs · 43,234 cycles

RT ENGINE FWD YOKE STRUCTURE, FWD OUTBOARD LOWER SIDE IS CRACKED. C/A: R & R RT ENGINE FWD LOWER YOKE FITTING, IAW ERS-EM-54MR-698.

Part: RIB — CRACKED (LT WING) · airframe 47,718 hrs · 43,234 cycles

LT WING RIB 21 IS CRACKED INSIDE THE PCA PANEL. C/A: PERFORMED REPAIR AT LT WING RIB 21 INSIDE THE PCA PANEL, IAW EMB 145 SRM 57-50-07 ITEM 4 FIGURE 203.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,718 hrs · 43,234 cycles

EMERGENCY LIGHT ON RIGHT WING OVERHEAD PANEL INOPERABLE. C/A COMPLETE: R & R EMERGENCY LIGHT BULB ON RIGHT WING OVERHEAD PANEL, IAW EMB 145 AMM 33-50-10. OPERATIONAL CHECK OK.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 47,718 hrs · 43,234 cycles

NR 1 EMERGENCY LIGHT STRIP CONNECTOR ON A/C SIDE IS BROKEN. C/A COMPLETE: R & R NR 1 EMERGENCY LIGHT STRIP CONNECTOR ON A/C SIDE, IAW EMB 145 SWPM 20-21-00. INSTALLED NR 1 EMERGENCY LIGHT STRIP, IAW EMB 145 AMM 30-50-12. OPERATIONS CHECK GOOD, IAW EMB 145 AMM 30-50-00.

Part: CONNECTOR — MISSING (EMERGENCY LIGHTS) · airframe 47,718 hrs · 43,234 cycles

NR 1 AND NR 2 EMERGENCY FLOOR LIGHT STRIPS ARE MISSING CONNECTORS ON A/C SIDE. C/A COMPLETE: INSTALLED NEW AND SERVICEABLE CONNECTORS AT NR 1 AND NR 2 EMERGENCY FLOOR LIGHT STRIPS ON A/C SIDE, IAW EMB 145 SWPM 20-21-00. SEE BOW347724 TASK NR 1 FOR OPERATIONAL CHECK. CRIMPER EASI NR 102.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,712 hrs · 43,225 cycles

DURING PS-1 CHECK, FOUND LT ABOVE WING EXTERIOR EMERGENCY LIGHT INOP. C/A: R & R EXTERIOR EMERGENCY LIGHT ASSEMBLY, IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,654 hrs · 43,161 cycles

DURING PS-1 CHECK FOUND R/H O/W EMERGENCY LIGHT INOP-C/A-RAR R/H O/W EMERGENCY LIGHT BULB IAW EMB-145 AMM 33-50-10

Part: CONNECTOR — DETACHED (EMERGENCY LIGHTS) · airframe 47,568 hrs · 43,065 cycles

LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R LT EXTERIROR OVERWING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-10. OPS CHECK FAILED. REMOVED ACESS PANEL 195AL AND FOUND THE CONNECTOR PLUG DETACHED FROM LT EXTERIOR OVERHEAD LIGHT ASSY. CONNECTED THE CONNECTOR PLUG TO LIGHT ASSY AND REINSTALLED PANEL 195AL. OPS CHECKED GOOD.

Part: FLAPPER VALVE — FAULTY (CABIN PRESSURE) · airframe 47,457 hrs · 42,938 cycles

SUPPLEMENTAL LOST PRESSURIZATION AT APPROX 13,500 COULD CABIN ALT (2000) FEET WAS THE BEST. DEFER AUTO PRES M PROCEDURES C/W MANUAL PRESS OPS CHECK GOOD IAW AMM 21-31-00 MEL 21-17 AUTH 060107DM-C MOC 607038. REMOVED AND REPLACED FLAPPER VALVE IAW AMM 21-22-04. OPS CHECK GOOD. REFER AML 4538336/1. MEL RESTORED "M" PROCEDURES REVERSED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,430 hrs · 42,910 cycles

LEFT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY INVERTER IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. NO FIX, REMOVED AND REPLACED NR 3 EMERGENCY BATTERY IAW AMM 33-50-04-000-801-A, 33-50-04-400-801-A, 33-50-04-000-802-A AND 33-50-04-400-802-A. OPERATION CHECK GOOD. EMERGENCY LIGHTING BATTERY PN 2013-1ASMI SN 69127.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,430 hrs · 42,910 cycles

LEFT AFT OVERWING EMERGENCY LIGHT. REMOVED AND REPLACED LT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A, NO FIX.. REMOVED AND REPLACED LT AFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW 33-50-07-000-802-A AND 33-50-07-400-802-A. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,430 hrs · 42,910 cycles

RIGHT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY INVERTER IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801-A, NO FIX. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY IAW AMM 33-50-04-000-801-A, 33-50-04-400-801-A, 33-50-04-000-802-A AND 33-50-04-400-802-A. OPERATIONS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,392 hrs · 42,873 cycles

INTERIOR RH EXIT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #2 BATTERY CHARGER ASSEMBLY, IAW AMM 33-50-04, OPERATIONS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 13247

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 47,360 hrs · 42,844 cycles

RIGHT HAND OVERWING EXIT LIGHT INOP-C/A-REMOVED AND REPLACED LAMP FOR THE RH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-07. OPS CHECK GOOD

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,242 hrs · 42,753 cycles

LH AND RH OVER WING EMERGENCY LIGHTS WILL NOT ILLUMINATE-C/A-RE-LAMPED RH OVER WING EMERGENCY LIGHT NO FIX. RAR BATTERY AND CHARGER #4 IAW WC 33-700-19 OPC CHECK GOOD

Part: BRAKE — LACK OF LUBE (PARKING) · airframe 47,004 hrs · 42,508 cycles

PARKING BRAKE HARD TO SET.-C/A-CLEANED AND LUBRICATED PARKING BRAKE IAW EMB 145MM 32-44-10. OPS CK GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (AFT CARGO BAY) · airframe 46,965 hrs · 42,468 cycles

CARGO SMOKE INDICATION AT PARKING BRAKE SET CFR RESPONDED. NO EVIDENCE OF SMOKE DETECTED. R & R THE SMOKE DETECTORS NR 1 AND 2 IAW AMM 26-15-01. OPS CHECKED GOOD IAW AMM 26-15-00.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 46,962 hrs · 42,467 cycles

REAR FLASHLIGHT HOLDER IN CABIN BROKEN. REMOVED AND REPLACED AFT FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 46,712 hrs · 42,260 cycles

HYD SYS 1 LO QTY RETURNED TO BASE TRANSFER TO NRWC# 618-MIA-03437-C/A-REPAIRED HYD RETURNED LINE ITEM#1 FIG 17 ON IPC 29-11-00 LEAK CHECK GOOD NO DISCREPANCIES NOTED IAW STANDARD PRACTICE 20-10-03

Part: INVERTER — INOPERATIVE (CABIN) · airframe 46,117 hrs · 41,737 cycles

RT UPPER EMERGENCY EXIT LIGHT AT ROW 12C INOP. C/A-REMOVED AND R EPLACED EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11 OPC GOOD.

Part: CONTROL MODULE — ODOR (CABIN LIGHTS) · airframe 45,511 hrs · 41,137 cycles

FA REPORTS PANGENT SMELL COMING FROM SERVICE DOOR BACK TO ROW 6-C/A-FOUND CABIN LIGHT CONTROL MODULE TO BE THE SOCRCE REMOVED AND REPLACED CONTROL MODULE ASSEMBLY IAW 145 AMM 33-21-01 OPS-CHECK GOOD NO FURTHER SMELL DETECTED

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 45,075 hrs · 40,760 cycles

DURING INSTALLATION OF FLOOR PANEL 261BF FOUND FLOOR PROXIMITY STRIP LIGHT WIRE CONNECTOR BROKEN.-C/A-INSTALLED MISSING SPLICE MALE CONNECTOR IN FLOOR PROXIMITY STRIP LIGHT #8 IAW EMB 145 AMM 20-00-03. OPS CHECK GOOD IAW EMB145 AMM 33-50-12

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,867 hrs · 40,554 cycles

LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND AMM 33-50-10-400-801-A. OPS CHECK GOOD. NO MORE DEFECTS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,451 hrs · 40,200 cycles

LH EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (FLAP SYSTEM) · airframe 44,306 hrs · 40,092 cycles

FLAP LOW SPEED ADVISORYIN CRUISE AT FL 370 NO FLAPS SELECTED LEVER NOT MOVED MECH FLAP WARNING AT ALTITUDE AND POSS AIRSPEED UNRELIABLE EMERGENCY DECLARED.-C/A-CHECKED CMC MESSAGES. FOUND 1 OCCURANCE OF MESSAGE "FLAP FEEDBACK POS FAIL" T/SHOT PER FIM TASK 27-51-00-810-807-A. NO DEFECTS FOUND PER INITIAL EVALUATION PER FIM TASK CYCLED FLAP 1 & FLAP 2 CIRCUIT BREAKERS PER FIM TASK AND FAULT CLEARED. PERFORMED OPERATIONAL CHECK OF FLAPS IAW AMM 27-51-00-700-801-A. OPERATIONAL CHECK GOOD. FOUND TO BE TRANSITORY CONDITION. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXIT ROW) · airframe 44,302 hrs · 40,087 cycles

NO ORANGE EMERGENCY LIGHT SECTION BESIDE WINDOW EXIT ROWS PER FA-C/A-REMOVED AND REPLACED EMER. EXIT ROW FLOOR FLIGHTING STRIP AND OPC GOOD IAW EMB145 AMM 33-50-12 AND 33-50-00.

Part: INDICATION SYS — INTERMITTENT (FUEL SYSTEM) · airframe 43,815 hrs · 39,647 cycles

TANK 1 FUEL INDICATION READING ERRONEOUS FUEL LOAD INTERMITTENT. FUEL INDICATION DEFERRED ON DMI 2840001. WILL SEND MORE INFORMATION WHEN AVAIABLE

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,389 hrs · 39,270 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT NR 6 IS INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 42,758 hrs · 38,740 cycles

CARGO DOOR SKIN CRACKED AT UPPER AFT CORNER OF DOOR HANDLE CUTOUT. INSTALLED A FILLER AND DOUBLER.

Part: SKIN — DAMAGED (FRAMES 72-73) · airframe 42,758 hrs · 38,740 cycles

REAR FUSELAGE EXTERNAL SKIN DENTED AND SCRATCH BETWEEN FRAMES 72 - 73, STRINGERS 10R-13R. FABRICATED AND INSTALLED A STRAP AND REPAIR PARTS.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 40,451 hrs · 36,751 cycles

NR 2 HYDRAULIC SYS FLUID LOW. SERVICED THE NR 2 HYDRAULIC SYS AND R & R THE NR 2 ENGINE HYD PUMP. OPS LEAK CHECKED GOOD.

Part: COUPLING — WORN (BLEED VALVE) · airframe 39,541 hrs · 36,371 cycles

BLEED 2 LEAK EICAS MESSAGE IN FLIGHT. FOUND NR 2 ENGINE BLEED VALVE OUTLET COUPLING BAD, R & R BLEED COUPLING. OPS CHECK GOOD. INSPECTED BLEED DUCTS NO LEAKS NOTED.

Part: PRESSURE SWITCH — INOPERATIVE (BLEED SYS) · airframe 39,426 hrs · 35,941 cycles

BLEED 2 CLOSED EICAS MSG. R & R NR 1 HIGH STAGE PRESSURE SWITCH. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,803 hrs · 35,414 cycles

GALLEY FLOOR SUPPORT FWD DIGITAL CRACKED. REPAIRED FWD DIGITAL CRACK IAW ERS-EM-53MR-1584.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,803 hrs · 35,414 cycles

RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 2R & 3R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75, BETWEEN STRINGERS 2R & 3R IAW ERS-EM-53MR-1588.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,803 hrs · 35,414 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1L & 3L IAW ERS-EM-53MR-1587.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 38,803 hrs · 35,414 cycles

STRINGER 18L AT FRAME 71 GOUGED. PERFORMED PERMANENT REPAIR OF STRINGER 18L AT FRAME 71 IAW SRM 53-00-03-RE.

Part: WIRE — BROKEN (CABIN) · airframe 38,803 hrs · 35,414 cycles

EMERGENCY LIGHT STRIP HARNESS, BROKEN WIRE UNDER FLOOR PANEL 231GF. REPAIRED LIGHT STRIP FLOOR PROXIMITY LIGHT WIRES UNDER PANEL 231GF IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: WIRE — BROKEN (CABIN) · airframe 38,803 hrs · 35,414 cycles

FOUND NR 2 FLOOR PROXIMITY LIGHT AT 241DF WIRES BROKEN. REPAIRED NR 2 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 38,803 hrs · 35,414 cycles

CARGO DOOR FWD PROFILE LOWER NUTPLATE HOLE CORRODED & CRACKED. REPAIRED IAW ERS-EM-52MR-414.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,803 hrs · 35,414 cycles

FRAME 65 CORRODED AROUND LOWER STRIKER PLATE. REPAIRED FRAME 65 BETWEEN STRINGERS 16L & 17L IAW ERS-EM-53MR-1577.

Part: YOKE — CRACKED (LT NACELLE) · airframe 38,803 hrs · 35,414 cycles

LEFT ENG FWD, LOWER YOKE CRACKED BEHIND ENG MOUNT. R & R LT ENG LOWER FWD YOKE IAW EO EM-54MR-386.

Part: WIRE — BROKEN (CABIN) · airframe 38,803 hrs · 35,414 cycles

EMERGENCY LIGHT STRIP WIRES AT 251 DF ARE BROKEN. INSTALLED CONNECTOR ON BROKEN EMER LIGHT STRIP WIRES AT 251 DF IAW SWPM 20-00-03 & 20-21-00. TOOL SN6277, SEE NRTC BOW 199115 FOR THE OPERATIONAL TEST OF THE EMER LIGHT STRIP AT 251 DF.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,803 hrs · 35,414 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK IS APPROX. 3/8" LONG. REPAIRED LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABOVE STRINGER 2L IAW ERS-EM-53MR-1587.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 38,803 hrs · 35,414 cycles

CARGO DOOR FWD FRAME IS CRACKED UNDERNEATH LOWER GUIDE. REPAIRED CARGO DOOR FWD FRAME CRACKED UNDERNEATH LOWER GUIDE IAW ERS-EM-52MR-414. SEE NRTC TURNOVERS FOR DETAILS.

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 38,803 hrs · 35,414 cycles

CARGO DOOR FWD PROFILE LOWER NUTPLATE HOLE CORRODED. REPAIRED CORRODED NUTPLATE HOLE ON CARGO DOOR FWD PROFILE LOWER IAW ERS-EM-52MR-414.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 38,279 hrs · 34,916 cycles

RIGHT EMER EXIT, AFT EXIT MARKER LIGHT FAILED TO ILLUMINATE. R & R NR 5 EMER LIGHT INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 38,264 hrs · 34,905 cycles

CAPTAINS SIDE FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 38,187 hrs · 34,844 cycles

REAR CABIN FLASHLIGHT CLIP BROKEN. R & R REAR CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,987 hrs · 34,667 cycles

CENTER AISLE OVERHEAD EMER LIGHT AT ROW 7 INOPERATIVE. R & R CTR AISLE OVERHEAD EMER LAMP AT ROW 7 IAW TASK 33-50-08-000-801-A & TASK 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: PIN — MALFUNCTIONED (COCKPIT WINDOW) · airframe 37,851 hrs · 34,557 cycles

DURING CLIMB, CREW HEARD A SQUEAL & NOTED THE PIN ON THE DV WINDOW MOVE FROM FLUSH TO THE PROTRUDING POSITION. RETURNED WITHOUT INCIDENT. OPS TESTED THE DV WINDOW IAW AMM 56-11-01. TESTED SATISFACTORILY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,626 hrs · 34,351 cycles

NUMBER 1 BLEED LEAK ILLUMINATED ON CLIMB OUT ON EICAS & NR 1 ENG BLEED SWITCH. SECURED NR 1 ENG BLEED SWITCH & ANNUNCIATION EXTINGUISHED, HAPPENED DURING CLIMB OUT JUST AFTER ANTI-ICE SYS TURNED OFF. INSPECTED DUCTS & JOINTS IN THE NR 1 BLEED SYS IAW ETN-EM-36-048, NO LEAKS FOUND. PERFORMED THE OPERATIONS TEST OF THE AIR BLEED SYS IAW AMM 36-00-00. OPERATIONS CHECKED GOOD. NO BLEED LEAK MSG.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 37,538 hrs · 34,250 cycles

STRONG ELEC BURNING SMELL IN COCKPIT. PERFORMED GVI OF COCKPIT & ELEC PANELS & FWD E BAY, NO DEFECTS NOTED. NO EVIDENCE OF ELEC FAULTS.

Part: UPLOCK — FAILED (RT MLG) · airframe 37,341 hrs · 34,060 cycles

AFTER TAKEOFF WITH GEAR UP, FELT A THUMPING UNDER THE ACFT. DECLARED AN EMERGENCY & RETURNED TO DEPARTURE. THE THUMPING CONTINUED UNTIL GEAR WAS DOWN. REPLACED RT MLG UPLOCK BOX IAW MM 32-33-10. OPS & LEAK CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,309 hrs · 34,022 cycles

BOTH AFT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT POWER SUPPLY & BATTERY IAW WC 33-700-19. OPERATIONAL CHECK GOOD. EMER LIGHTING BATTERY PN 2013-1A SN 67262.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,280 hrs · 33,994 cycles

EXTERIOR OVERWING EMER LIGHTS INOPERATIVE. R & R OVERWING EMER LIGHT BATTERY & CHARGER ASSEMBLY NR 4 IAW AMM 33-05-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 15847.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 37,098 hrs · 33,811 cycles

STRONG ELEC SMELL IN COCKPIT AFTER LANDING & TOWARDS FRONT OF CABIN. FOUND CAPTAIN`S FLASHLIGHT TO HAVE BURNT SMELL. R & R FLASHLIGHT & FLASHLIGHT HOLDER IAW AMM 33-50-16.

Part: SUPPORT — BROKEN (AILERON) · airframe 37,065 hrs · 33,785 cycles

EXCESSIVE RESISTANCE ON YOLK WHEN PULLED AFT, LAST 1/3. TRANSFERRED TO NRWC 618-DFW-02203. IAW TO NRWC 618-DFW-02205 FOUND AILERON SUPPORT BROKEN & SUPPORT SEMI GROMMET DAMAGED AT STATION 5418.0 & 5833.0 IAW NRWC 618-DFW-02206. PERFORMED ELEVATOR CONTROL CABLE TENSION CHECK. SYS OPERATIONS CHECKED GOOD.

Part: STRUCTURE — LEAKING (RT WING) · airframe 36,601 hrs · 33,427 cycles

FLUID LEAKING & STREAMING OVER RT FLAPS INFLIGHT. TRANSFER TO NRWC 618-SGF-02120, ITEM 1. FOUND LEAK ON RT WING SEAM BETWEEN ACCESS PANEL 641AB-631DB. RESEALED SEAMS AS REQUIRED. LEAK CHECKED GOOD IAW AMM 28-11-01.

Part: DUCT — LEAKING (BLEED SYS) · airframe 36,356 hrs · 33,224 cycles

CLIMBING THROUGH 6000 FT, NR 1 BLEED LEAK EICAS MESSAGE PRESENTED. COMPLETED EPC & AOM 1 PROCEDURES. MESSAGE TOOK ABOUT 2 1/2 MINUTES TO CLEAR, BUT CLEARED. DIVERTED & RETURNED. REMOVED AND REPLACED LT PACK VALVE AND Y-DUCT IAW AMM 21-51-01 AND FLEX DUCTS ON LT PACK TEMP CONTROL VALVE IAW 21-60-01. LEAK CHECKED GOOD IAW AMM 36-00-00, NRWC'S 618-DFW-02033, 02034, 02043 AND 02052. PERFORMED LT FUSELAGE AIR BLEED DUCT LEAK TEST IAW 36-00-00. FOUND BLEED JOINTS 17 AND 25 TO BE LEAKING AIR AND REPLACED O-RINGS. PERFORMED LT FUSELAGE AIR BLEED DUCT LEAKAGE TEST AFTER REPLACEMENT OF O-RINGS IAW 36-00-00. LEAK CHECKED GOOD.

Part: HEATER — UNKNOWN (WINDSHIELD) · airframe 36,353 hrs · 33,218 cycles

NR 1 WINDSHIELD HEAT FAILED IN FLIGHT. REMAINED AFTER AOM VOL 1 PROCEDURE COMPLETED. PERFORMED OPS CHECK OF WINDSHIELD HEATING SYS IAW AMM 30-42-00. OPS CHECKED GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 36,354 hrs · 33,219 cycles

BLD 1 LEAK INDICATION ON EICAS DURING EN ROUTE CLIMB THRU 10000 MSC RAN A011 CHECK LIST BLD LEAK INDICATION EXTINGUISHED AFTER APPROX 3 MINUTES. R & R ORING IAW ETN EM 36-048 ON BLD DUCT LOCATION 28, 17, 15, 9 & 7 IAW AMM 36-11-09. GND RAN OPERATIONS CHECK NO BLD 1 INDICATION NOTED.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 36,046 hrs · 32,990 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED MAIN DOOR FRAME ROLLER & CHECKED OK IAW MM 53-21-02.

Part: LIGHT — MISSING (CABIN) · airframe 35,901 hrs · 32,873 cycles

EMERGENCY FLOOR PROXIMITY LIGHTING STRIP AT ROWS 17 & 18 DISCOVERED TO BE NOT ON ACFT. LOCATION UNKNOWN. DISCOVERED LOCATION OF ROW 17 & 18 EMERGENCY FLOOR PROXIMITY LIGHTING STRIP. INSTALLED EMERGENCY LIGHTING STRIP IAW AMM 33-50-12. OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,868 hrs · 32,845 cycles

EMERGENCY LIGHT STRIP & RT & LT OVERWING LIGHTS INOPERATIVE. R & R NR 4 BATTERY CHARGER & THE BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 35,426 hrs · 32,520 cycles

UPON LG RETRACTION DEPARTING DFW HAD LG AIR & GND FAIL MSG ON EICAS. R & R LT MLG WOW 1 & WOW 2 PROX SWITCHES & RT MLG WOW 1 PROX SWITCH IAW AMM 32-63-01. FUNCTION CHECK GOOD IAW AMM 32-63-05.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 35,335 hrs · 32,437 cycles

LG AIR, GND FAIL MESSAGE ON EICAS AFTER GEAR RETRACTION. R & R RT MLG WOW NR 1 SWITCH & LT MLG WOW NR 1 SWITCH IAW AMM 32-63-01. ADJUSTED THE TARGET ON LT MLG WOW NR 2 SWITCH IAW AMM 32-63-05. OPERATIONS CHECKED GOOD IAW AMM 32-63-00.

Part: PRESSURE SWITCH — DEFECTIVE (RUDDER) · airframe 35,296 hrs · 32,408 cycles

RUDDER SYS 2 INOPERATIVE, CAUTION AFTER LIFTOFF. R & R RT PRESS SWITCH PO 378, OPERATIONS CHECKED GOOD IAW MM 27-23-00. NO DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 35,014 hrs · 32,167 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. AFT FLIGHT ATTENDANT`S FLASHLIGHT USED IN ITS PLACE. CREW PLACARDED IAW MEL 2553 AUTH 010724-C MOC 686519.

Part: FRAME — CHAFED (FUSELAGE) · airframe 34,558 hrs · 31,816 cycles

FRAME 15 CHAFED AT STRINGER 2R. REPAIRED FRAME IAW EO-EM-53MR-2225.

Part: SPAR — CRACKED (LT WING) · airframe 34,558 hrs · 31,816 cycles

CRACK ON LT SPAR 3 AROUND HARNESS CUT OUT HOLE. PERFORMED REPAIR IAW EO EM-57MR-727.

Part: STRAP — CHAFED (FRAME 54) · airframe 34,558 hrs · 31,816 cycles

CHAFED REINFORCEMENT STRAP OF FR 54 BETWEEN STR 9R AND 11R. PERFORMED CUTOUT OF DAMAGES AND FABRICATED FILERS, STRAP AND PREP IAW EO EM-53MR-2226.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,558 hrs · 31,816 cycles

EMERGENCY LIGHT AT ROW 9 HAS A BROKEN WIRE. INSTALLED SERVICEABLE SPLICE AND PIN ON EMERGENCY LIGHT STRIP WIRE AT ROW 9 IAW SWPM 20-21-00 AND 20-50-01.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 3,499 hrs · 31,735 cycles

AFT FLASHLIGHT MISSING. INSTALLED FLASHLIGHT IAW AMM 33-50-16. OPS GOOD.

Part: RMU — INOPERATIVE · airframe 34,298 hrs · 31,594 cycles

CREW REPORTED AFTER TAKEOFF, RMU 1 DISPLAYED ALL DASHES EXCEPT COMM 1 WINDOW. RMU 2 DISPLAYED ALL DASHES. 115 VAC BUSS OFF ILLUMINATED FOR APPROX 30 SECONDS AND THEN EXTINGUISHED. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R RMU 1, OPERATES OK IAW AMM 23-81-01. R & R RMU NR 2 OPERATES OK IAW AMM 23-81-01. REPLACED SWITCH FOR THE ACFT POWER ELECTRICAL SYS IAW AMM 20-13-04. OPS CHECKED GOOD IAW 24-20-00. ACFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,844 hrs · 31,239 cycles

DURING B INSPECTION, FOUND AFT CEILING PANEL EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 33,651 hrs · 31,070 cycles

DURING CRUISE RECEIVED A "HYD 1 LOW QTY" EICAS MESSAGE, FOLLOWED A FEW MINUTES LATER BY A "HYD E1 PUMP FAIL" EICAS MESSAGE. HYD SYS 1 PRESSURE AT 2900 PSI INDICATED THAT E1 ENGINE DRIVEN PUMP HAD FAILED. A FEW MINUTES LATER HYD PRESSURE DROPPED BELOW 2900 PSI ACCOMPANIED BY NOISE REPORTED BY THE F/A INDICATING THE ELECTRICAL PUMP WAS CAVITATING. ELECTRICAL HYD PUMP WAS TURNED OFF TO PREVENT FURTHER DAMAGE. FOLLOWED AOM 1 PROCEDURES AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE #1 ELECTRIC MOTOR-DRIVEN PUMP IAW AMM 29-10-04.THE OPERATIONAL AND LEAK CHECK WAS GOOD THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,582 hrs · 31,006 cycles

DURING MX INSPECTION, FOUND THE SECOND FROM AFT FLOOR PROXIMITY STRIP LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE SECOND FROM AFT FLOOR PROXIMITY STRIP LIGHT IAW AMM-33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 33,574 hrs · 30,999 cycles

DURING MX INSP, FOUND THE SECOND TO LAST EMERGENCY LIGHT PROXIMITY STRIP WIRE BROKEN. THE ACFT WAS REMOVED FROM SERVICE. CRIMPED ON NEW CONNECTOR IAW SWPM 20-50-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTACTOR — INOPERATIVE (NR 1) · airframe 33,469 hrs · 30,912 cycles

THE CREW REPORTED THAT DURING THE CLIMB OUT, RECEIVED MW FUEL 2 LOW LEVEL. NOTICED A LOUD BANGING UNDER COCKPIT FLOOR. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE EBC NR 1 K0079 CONTACTOR. EBC NR 1 K0079 CONTACTOR. THE ACFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 33,199 hrs · 30,686 cycles

ON FLIGHT 3554 THE CREW REPORTED THAT DURING CLIMBOUT AT 13000 FT - EXTG BAGG LIGHT ILLUMINATED. FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL FROM THE LAV EXT FIRE BOTTLE WAS ACTIVATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED FOR SIGNS OF ELECTRICAL SMOKE. PERFORMED ENGINES GROUND RUN UPS FOR ABOUT 20 MIN. DID NOT FIND ANY SIGNS OF ELECTRICAL SMOKE OR OTHER ABNORMALITIES. REMOVED AND REPLACED CARGO COMPT AFT SMOKE DETECTOR IAW EMB AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 33,164 hrs · 30,661 cycles

FOR FLIGHT 4093 THE CREW REPORTED FUMES IN COCKPIT AFTER ENGINE 1 START COMPLIED WITH AOM PROCEDURES. THE AIRCRAFT RETURNED TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE ODOR EVENT TROUBLESHOOTING IAW ETN: ETN-EM-72-034. COULD NOT DUPLICATE AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,715 hrs · 30,329 cycles

DURING MAINTENANCE INSPECTION FOUND THE SECOND AND THIRD FLOOR EMERGENCY LIGHT STRIP ASSEMBLIES ON THE FORWARD SECTION INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND NR 3 DC TO AC INVERTER TO BE INOP. REMOVED AND REPLACED THE NR 3 DC TO AC INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 32,539 hrs · 30,197 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 3 EMERGENCY LIGHT INVERTER WOULD NOT POWER EMERGENCY FLOOR STRIP SECTIONS 2 AND 3. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR P8528 NOT FULLY SECURE. TIGHTENED CONNECTOR AND PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW EMB 145 AMM 33-50-00. ALL CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,539 hrs · 30,197 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 5 EMERGENCY LIGHT INVERTER WOULD NOT ILLUMINATE RIGHT EMERGENCY EXIT SHROUD "EXIT" SIGN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AC/DC POWER INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,104 hrs · 29,841 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW EMB AMM TASK 33-26-04-000-801-A AND 33-26-04-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,836 hrs · 29,639 cycles

DURING MAINTENANCE INSPECTION FOUND THE CENTER AISLE EMERGENCY FLOOR LIGHT, THIRD FROM THE FRONT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT WING) · airframe 31,819 hrs · 29,621 cycles

ON FLIGHT 3945 THE CREW RECEIVED A WING ANTI ICE FAIL MESSAGE ON EICAS IN ICING CONDITIONS. THE CREW FOLLOWED AOM 1 PROCEDURE AND THE MESSAGE REMAINED. THE CREW DECLARED AN EMERGENCY AND CONTINUED THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING ANTI ICE VALVE IAW M/M 30-11-01 AND PERFORMED OPERATIONAL CHECK AND LEAK CHECK IAW M/M 30-00-00. NO FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,752 hrs · 29,558 cycles

DURING B INSPECTION FOUND THE MAIN DOOR CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR CEILING EMERGENCY LIGHT LAMP IAW EMB AMM TASKS 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 31,533 hrs · 29,379 cycles

ON FLIGHT 2952, THE CREW REPORTED A POSSIBLE FUEL LEAK ON RIGHT WING TRAILING EDGE FROM INBOARD PORTION OF AILERON. AT 6000 FEET, THE FLIGHT ATTENDANT NOTIFIED THE CREW OF FUEL LEAKING FROM THE RIGHT SIDE WING. THE CAPTAIN DECLARED AN EMERGENCY, COMPLETED AOM VOL 1 CHECKLIST AND RETURNED TO DEPARTURE. AIRCRAFT REMOVED FROM SERVICE. FOUND FLAPPER VALVE AT RIGHT WING RIB NR 19 BROKEN. REPLACED FLAPPER VALVE AS PER AMM 28-11-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — INOPERATIVE (ENGINE) · airframe 31,490 hrs · 29,347 cycles

FLIGHT N2765, CREW REPORTED THAT DURING CLIMB ON GEAR RETRACTION, NOTICED ITT’S BETWEEN E1 AND E2 WERE RATHER LARGE. AFTER TAKEOFF NR E1 ITT 840 . E 2 ITT 670. AFTER CLIMB CHECKLIST, E1 ITT 740- E2 ITT 650 ITT SPLIT RANGED BETWEEN 110 TO 140. AFTER CLIMBING THRU 21000 NR 1 ITT CLB PAST 800 AND CLIMBED SLOWLY. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 ENGINE B ITT HARNESS IAW MM 77-21-20. PERFORMED OPS CHECKS IAW MM 72-00-00, OPS CHECKED GOOD. ENGINE PERAMETERS NORMAL AT THIS TIME. REMOVED AND REPLACED NR 2 ENGINE B THERMOCOUPLE HARNESS IAW MM 77-21-20. RETORQUED CLAMPS ON NR 1 ENGINE Y DUCT IAW AMM 36-11-09. LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,768 hrs · 28,763 cycles

DURING B INSPECTION, FOUND COCKPIT EMERGENCY CEILING LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED COCKPIT EMERGENCY CEILING LAMP IAW AMM TASKS 33-50-05-000-801-A AND 33-50-05-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,313 hrs · 28,400 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY CEILING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW EMB MM 33-50-08 IAW EMB MM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 30,202 hrs · 28,315 cycles

ON FLIGHT 2839 THE FLIGHT ATTENDANT NOTED THE IN-FLOOR CABIN EMERGENCY LIGHTING STRIP AT OVERWING EXIT WAS NON STANDARD CONFIGURATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP AT OVER THE WING EXIT IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (E/E DOOR) · airframe 30,056 hrs · 28,197 cycles

DURING MAINTENANCE BASE VISIT, FOUND REAR ELECTRONIC COMPARTMENT HATCH SKIN CRACKED WHERE THE SAFTEY LATCH RECEIVER ON DOOR IS ATTACHED UP UNDER INNER LIP OF THE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED REAR ELECTRONIC DOOR IAW EO EM-52MR-303. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 30,120 hrs · 28,247 cycles

DURING B-INSPECTION FOUND APU FIREWALL CRACKED UPPER RIGHT QUADRANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACEMENT OF APU FIREWALL IAW PT D OF EO EM-5300-1931. THE AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,982 hrs · 28,144 cycles

DURING MAINTENANCE BASE INSPECTION FOUND BOTH REAR OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH REAR OVERWING EMERGENCY LIGHT BULBS IAW EMB 145 AMM 33-50-07 DID NOT FIX. TROUBLESHOT IAW EMB 145 WIRING MANUAL 33-50-50. FOUND NR 4 BATTERY POWER SUPPLY TO BE BAD. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,978 hrs · 28,139 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVER THE WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVER THE WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,304 hrs · 28,082 cycles

GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY LAMP IAW EMB 145 AMM TASKS 33-50-09-000-801-A & 33-50-09-400-801-A, OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (COCKPIT) · airframe 29,767 hrs · 27,987 cycles

DURING PS-2 CHECK FOUND MAIN DOOR EXIT MARKER AND COCKPIT STEP EXIT IDENTIFIER INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 27,863 hrs · 26,477 cycles

FOR FLIGHT 3902 THE CREW REPORTED THAT AFTER THE NUMBER 1 ENGINE STARTED WITH THE AUXILIARY POWER UNIT ON, AND BOTH PACKS SELECTED A SMOKE ODOR WAS DETECTED IN THE COCKPIT. THE CREW ALSO NOTICED A SMOKE HAZE. THE CREW IMMEDIATELY TURNED ALL BLEEDS, PACKS, AND RECIRCULATION FANS OFF. THE SMOKE/HAZE CLEARED OUT BY THE TIME THE CREW RETURNED TO THE GATE. THE AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AIR CYCLE MACHINE IAW ERJ 145 AMM 21-51-03 (LEFT). THE OPERATIONAL AND LEAK CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,693 hrs · 26,355 cycles

FOR FLIGHT 3655 DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT FLOOR LIGHTS WERE FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP LIGHT SECOND TO LAST IAW EMB-145-MM-33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 27,552 hrs · 26,257 cycles

DURING MAINTENANCE BASE VISIT FOUND THE PASSENGER DOOR INNER HANDLE SUPPORT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE PASSENGER DOOR INNER HANDLE SUPPORT IAW EO EM 52MR-250. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 26,559 hrs · 25,489 cycles

ON FLIGHT 3332 THE CREW REPORTED THAT DURING TAKEOFF AND CLIMBOUT DETECTED A BURNING OIL ODOR IN THE COCKPIT. THE CREW ELECTED TO CONTINUE TO DESTINATION AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW W/C 71-000-00. ALL OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. THE FINDINGS FROM THE TEAR DOWN REPORT REVEALS THAT THE NR 4 CARBON SEAL FAILED.

Part: UNKNOWN — SMOKE (CABIN) · airframe 28,961 hrs · 24,989 cycles

ON FLIGHT 3961 THE CREW REPORTED THAT DURING CLIMBOUT A "LAV SMOKE" WARNING MESSAGE ILLUMINATED IN EICAS. THE CREW CHECKED WITH THE FLIGHT ATTENDANT AND CONFIRMED THE PRESENTS OF SMOKE. THE CREW ELECTED TO DIVERT TO ROC. THE SMOKE DISSIPATED PRIOR TO ARRIVAL. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED LAVATORY, LIGHTING AND VENTILATION, EMERGENCY LIGHTS AND INSPECTED ENGINES FOR LEAKS OR ANY OBVIOUS DEFECTS. NO DEFECTS NOTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT PURPOSES. THE FUNCTIONAL CHECK FLIGHT WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,340 hrs · 24,518 cycles

FOR FLIGHT 3881 DURING INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IAW EMB 145AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,280 hrs · 24,475 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FORWARD GALLEY EMERGENCY EXIT SIGN TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY EXIT SIGN. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 25,210 hrs · 24,411 cycles

DURING MAINTENANCE BASE VISIT FOUND THAT STRINGER 19R IS CHAFED BETWEEN FRAMES 52-53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER 19R BETWEEN FRAMES 52-53 IAW SRM 53-24-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPLICE PLATE — CHAFED (FUSELAGE) · airframe 25,210 hrs · 24,411 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 65 ON THE RIGHT BETWEEN STRINGER 12 RIGHT AND 13 RIGHT HAS DAMAGED SPLICE PLATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW ENGINEERING ORDER EM-53MR-1483. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 25,210 hrs · 24,411 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE BAGGAGE DOOR CUTOUT FORWARD LOWER L SHAPE CORNER TO HAVE A SMALL AREA OF CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGE IAW EO EM-53MR-1129. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 25,210 hrs · 24,411 cycles

DURING THE MAINTENANCE BASE VISIT THE LEFT AILERON ACTUATOR FITTINGS WERE FOUND TO BE LOOSE IN BORES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,210 hrs · 24,411 cycles

DURING THE MAINTENANCE BASE VISIT FRAME 65 WAS FOUND TO BE CORRODED NEAR THE BAGGAGE DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 65 IAW EO EM-53MR-1482. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 25,210 hrs · 24,411 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIRS TO ANGLES IAW ENGINEERING ORDER EM-53MR-1281. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,210 hrs · 24,411 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD FUSELAGE HAS BIRD STRIKE DAMAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW EO EM-53MR-1360. THE AIRCRAFT WAS RETURNED TOSERVICE.

Part: SHUTTLE VALVE — FAULTY (BRAKE SYS) · airframe 24,964 hrs · 24,210 cycles

ON FLIGHT 3664 AFTER TAKEOFF THE DFW TOWER INFORMED THE FLIGHT CREW AS WELL AS MAINTENANCE OPERATIONS CONTROL THAT A LARGE AMOUNT OF FLUID OR SMOKE WAS COMING FROM THE RIGHT WING. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. DETERMINED THE FLUID OR SMOKE ISSUE WAS CAUSED BY VENTING HYDRAULIC FLUID. NR 2 SIDE-BALANCED HYDRAULIC NR 1 AND NR 2 IAW ETN-EM-29-017. REMOVED AND INSTALLED NR 1 AND NR 4 BRAKE SHUTTLE VALVES IAW 32-49-03. NO LEAKS NOTED. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — ODOR (NR 1) · airframe 20,058 hrs · 19,828 cycles

ON FLIGHT 4501 - CLIMBING THRU 700 FEET, AFL MODERATE INTENSITY HAZE FILLED COCKPIT VERIFIED IN CABIN AS WELL, FOLLOWING EMERGENCY PROCEDURES CHECK LIST HAZE BEGAN TO DISSIPATE WHEN RECIRC FAN SELECTED OFF. RETURNED TO ORD EMERGENCY VEHICLES MET AIRCRAFT. INSPECTED A/C UPON RETURN AND THEY FOUND NO EXTERNAL OR INTERNAL ABNORMALITIES. APU WAS SELECTED OFF FOR THIS ENTIRE EVENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE IAW 71-00-00. PERFORMED OPERATIONAL CHECK OPERATION CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT AND FOUND SATISFACTORY. NO ODOR OR HAZE NOTED AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN)

FOUND ELECTRICAL ODOR IN CABIN AROUND ROWS 2-7 AND PROGRESSING TO AFT OF CABIN. (M)

Part: SEAL — LOOSE (T/E FLAP)

MDT - FLT 4293 - DURING CLIMB, THROUGH APPROXIMATELY FL300, CREW BEGAN TO HEAR A HUM AND FEEL A HIGH FREQUENCY VIBRATION. THE F/A AT THE SAME WAS ALSO FEELING A VIBRATION, WHICH WAS MORE NOTICEABLE IN THE REAR OF THE CABIN THAN IN THE FRONT. THE VIBRATION WAS NOT FELT IN THE CONTROL YOKE, BUT WAS FELT SLIGHTLY IN THE RUDDER PEDALS. RAI RT INBOARD LOWER FLAP SHROUD SEAL, RA RT OVERWING FAIRING NUT PLATES, RAI RIVETS IN RT INBOARD FLAP SHROUD, IAW EMB SRM 51-40-02 AND PERFORMED FLAP RIG, IAW EMB AMM 27-51-00, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SEAL — DAMAGED (RT TE FLAP)

FLIGHT CREW HEARD A HUM AND FELT A HIGH FREQ VIBRATION WAS FELT SLIGHTLY IN THE RUDDER PEDALS. REPLACED RIGHT INBOARD LOWER FLAP SHROUD SEAL. REPLACED RIGHT OVERWING FAIRING NUT PLATES. REPLACED RIVETS IN RIGHT INBOARD FLAP SHROUD, AND C/W FLAP RIGGING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: MOUNT — UNKNOWN (LEFT ENGINE)

VIBRATION FELT IN THE REAR OF AIRCRAFT AND IN RUDDER PEDALS. REPLACED ALL ENGINE MOUNTS ON LEFT ENGINE P/N AFT LOWER LM223-SA7, AFT UPPER LM2235K7, FORWARD LOWER LM223SA51, FWD UPPER LM223SA51. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BUSHING — MIGRATED (HORIZ STAB)

DURING HMBV INSPECTION FOUND HORIZONTAL STABILIZER NR 1 BUSHING TO BE MIGRATING. INSTALLED NEW BUSHING IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: HINGE — WORN (RUDDER)

DURING COMPLIANCE WITH EO THE RUDDER II CENTER UPPER HINGE FLANGED BUSHING WAS FOUND LOOSE AND FITTING (LOWER HALF) WORN. MAINTENANCE REPLACED THE RUDDER II IAW AMM. PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. (K)

Part: VALVE — BROKEN (RT WING FLAPPER)

FUEL STREAMING FROM RIGHT WING. REPLACED RIGHT FUEL TANK OUTBOARD FLAPPER VALVE IAW 28-11-04. PERFORMED A FUNCTIONAL CHECK FLIGHT WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: VALVE — LEAKING (RT WING)

DFW - FLT 3807 - FUEL STREAMING FROM THE RIGHT WING. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED RIGHT FUEL VENT VALVE AND OUTBOARD FUEL FLOAT VALVE PER AMM 05-50-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. FLOAT VALVE P/N 2930015101. (M)

Part: SKIN — CORRODED (LT ELEVATOR)

ABI - DURING AN MBV INSPECTION, TORN SKIN WAS DISCOVERED ON THE LEFT ELEVATOR AT THE SERVO TAB ROD CUTOUT. PERFORMED A CUTOUT OF THE DAMAGED MATERIAL AND TREATED THE EDGES. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 55-20-01. (M)

Part: SILL — CORRODED (SERVICE DOOR)

DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED CORRODED AREA AND PERFORMED NDT INSPECTION. FILLED BLENDED AREA WITH EPOXY RESIN EA 934NA AND SANDED SMOOTH. FABRICATED THREE DOUBLERS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-02. (M)

Part: WINDOW — MALFUNCTIONED (COCKPIT)

ORD - FLT 4233 - CREW REPORTED SMOKE SMELL IN COCKPIT WHEN USING CAPTAIN WINDOW HEAT. REPLACED CAPTAIN WINDOW IAW AMM 56-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RADOME — BIRD STRIKE (FUSELAGE)

DURING TAKEOFF FROM BUF, CREW REPORTED A BIRD STRIKE TO THE NOSE AREA. MAINTENANCE REMOVED AND REPLACED FRAMES 3, 4, 5 AND 6, STRINGER 4R, RIGHT FORWARD NOSE TOP SKIN PANEL, RIGHT AFT NOSE TOP SKIN PANEL IAW EMB SRM 51-42-01 AND REPAIRED SKIN FORWARD OF RIGHT WINDSHIELD AFT OF FRAME 6 BETWEEN STRINGERS 4R AND 6R IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: FRAME — DAMAGED (FUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND FRAME 72 DENTED AND BENT AT SPLICE JOINT ABOVE FLOOR ON LEFT SIDE OF CARGO. REMVOED FRAME 72 SPLICE CHANNEL. RECONTOURED DENT. PERFORMED NDT AND FOUND NO DEFECTS. FABRICATED TWO DOUBLER ANGLE, REPAIR DONE IAW EMB GST-2022/02-A, ITEM 7, GST-2075/02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - MAINTENANCE FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAIR DONE IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FRAME — DENTED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION FOUND DENT ON FRAME 67 BETWEEN STRINGER 14R AND 15R. RECONTOURED DENT PERFORMED NDT AND FOUND NO DEFECTS. FABRICATED TWO DOUBLERS ANGLES, REPAIR DONE IAW EMB GST-2022/02-A ITEM 5, AND STANDARD SRM PRACTICES. (M)

Part: WINDOW FRAME — CORRODED (FUSELAGE)

ABI - MAINTENANCE FOUND RIGHT WINDSHIELD CUT OUT STRUCTURE HAS 25 CORRODED HOLES. REMOVED CORROSION BY REAMING BOLT HOLES. FABRICATED FREEZE PLUGS. REPAIR DONE IAW EMB GST 2022/02, ITEM 9 AND STANDARD SRM PRACTICES. (M)

Part: WINDOW FRAME — CORRODED (FUSELAGE)

ABI - MAINTENANCE FOUND LEFT WINDSHIELD CUT OUT STRUCTURE HAS 15 CORRODED HOLES. REMOVED CORROSION BY REAMING/BOLT HOLES. FABRICATED FREEZE PLUGS. REPAIR DONE IAW EMB GST-2022/02, ITEM 9 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - MAINTENANCE FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED SERVICEABLE BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18 51-40-02, AEA ETN EM-53-028 R1, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO PREVIOUS REPAIR. FABRICATED DOUBLER, PLATE, AND SHIMS. REPAIR DONE IAW EMB 145 SRM 145/1142 CHAPTER 53, REV 18 53-21-01, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - MAINTENANCE FOUND CARGO DOOR LOWER SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 145/1142, CHAPTER 51 REV 18 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M)

Part: CLIP — CRACKED (FUSELAGE)

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND SHEAR CLIP CRACKED ON FRAME 81 AT THE 2 O'CLOCK POSITION. REMOVED DAMAGE SHEAR CLIP. INSTALLED SERVICEABLE CLIP IAW EMB GST-2022/02A, AND STANDARD SRM PRACTICES. (M)

Part: GUSSET — CORRODED (FUSELAGE)

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

Part: STRUCTURE — GOUGED (FUSELAGE)

ABI - FOUND NUMEROUS SMALL GOUGES JUST INBOARD OF WASTE SERVICE ACCESS PANEL AT FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. GOUGES BLENDED, PERFORMED NDT, NO DEFECTS, ACCEPTED AS IS IAW EMB GST-1999/02. SURFACE PROTECTION RESTORED. (M)

Part: SKIN — GOUGED (FUSELAGE)

ABI - FOUND GOUGE BETWEEN FRAMES 28/29 AND STRINGERS 17R/18R. BLENDED GOUGES, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW EMB GST-1999/02, SURFACE PROTECTION RESTORED. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - FOUND ONE DENT MARKED NR 3 AFT OF PAX DOOR LOWER CORNER AT FRAMES 19 AND 20 AND STRINGER 15L AND 16L. ALSO FOUND CRACK. REMOVED DAMAGE BY CUT OUT, FABRICATED A REPAIR DOUBLER AND FILLER, REPAIR DONE IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-21-01, AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT CENTER SILL HAS CORROSION. REMOVED CORROSION BY BLENDING, FILLED WITH EPOXY RESIN AND SANDED. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW ETN-53-036, FIG 5, AND STANDARD SRM PRACTICES. M)

Part: SKIN — GOUGED (FUSELAGE)

ABI - FOUND GOUGE WITH DENT AT FRAME 66 AND 67 BELOW CARGO DOOR AREA AND STRINGERS 18L AND 20L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW EMB GST-1997/02, SURFACE PROTECTION RESTORED. (M)

Part: SKIN — GOUGED (FUSELAGE)

ABI - FOUND GOUGE AT FRAME 63/64 AND STRINGERS 19L AND 20L JUST BELOW AND FORWARD OF CARGO DOOR CUTOUT. BLENDED GOUGES, PERFORMED NDT, NO DEFECTS, ACCEPTED AS IS IAW EMB GST-1997/02, SURFACE PROTECTION RESTORED. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING. PASSENGER DOOR ENTRY FLOORBOARD SUPPORT HAS CORROSION. PERFORMED NDT, NO DEFECTS. FLOOR SUPPORTS FOUND TO BE WITHIN EMB 145-21-10 LIMITS. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - FOUND ONE DENT AFT OF PASSENGER DOOR ON EMB PLACARD AT FRAME 19 AND 20 AND STRINGER 14L AND 15L. PERFORMED NDT, NO DEFECTS, DENT ACCEPTED AS IS IAW EMB GST-1999/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM IN GALLEY HAS CORROSION. REPAIRED HAT BEAM IAW ETN 53-036. (M)

Part: STRUCTURE — GOUGED (PAX DOOR)

ABI - FOUND PASSENGER DOOR IS GOUGED IN TWO PLACES. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. REPAIR DONE IAW EMB GST-2005/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. AFT DIGITAL HAS CORROSION. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. DIGITAL FOUND TO BE WITHIN EMB 145 SRM 53-21-10 LIMITS. (M)

Part: GEARBOX — MAKING METAL (ENGINE)

METAL DEBRIS FOUND ON CHIP COLLECTOR DRAIN VALVE (GEARBOX, OIL TANK).

Part: LIGHT — INOPERATIVE (CABIN)

LBB - FLT 3892 - REAR FLOOR STRIP OF EMERGENCY LIGHTING SYSTEM INOPERATIVE, NOTIFIED CONTRACT MAINTENANCE ISSUED A FERRY PERMIT TO DFW FOR MAINTENANCE. FLOOR EMERGENCY LIGHT STRIP WAS REMOVED AND REPLACED. OPERATIONAL WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — FAILED (EXTERIOR)

ORD - FLT 4389 - RIGHT FORWARD EXTERIOR EMERENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKED GOOD. (X)