N607AE

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

SMALL CRACK IN SHEET METAL WHERE LH NLG FORWARD HINGE ASSEMBLY PASSES THROUGH TO ATTACHMENT POINT.-C/A-REPAIRED LH NLG DOOR FORWARD HINGE ASSY PASS THROUGH POINT IAW ERS-EM-53MR-4100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

FR 59 LH IS CHAFFED AT THE OVER HEAD BIN ATTACHMENT ARM NEAR STR. 5 LH.-C/A-REPAIRED SRM 53-00-04. CHAFE DAMAGE ASSIGNED DT-EM-53-1299.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

CABIN LH OMEGA BEAM HAS CORROSION ON PREVIOUS REPAIRED AREA AT FRAME 20.-C/A-DISASSEMBLED PREVIOUS REPAIR OF CABIN LH OMEGA BEAM AT FR 20. REMOVED CORROSION FROM SHIMS AND FOUND SHIMS STILL SERVICEABLE. CLEANED AND REAPPLIED PRTOECTIVE FINISH TO ALL REPAIR PARTS IAW CPM 5121-06 AND ETN-EM-51-091. REINTALLED REPAIR IAW SRM 51-40-02. REFERENCE NRWC E783615 FOR INSTALLATION OF THE CROSS-MEMBER AT FR 20.

Part: RIB — BENT (RUDDER) · airframe 49,060 hrs · 40,999 cycles

RUDDER 1 SKIN SUPPORT FLANGE (RIB) AT THE LOWER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.

Part: RIB — DAMAGED (RUDDER) · airframe 49,060 hrs · 40,999 cycles

RUDDER 1 LEADING EDGE RIB ABOVE CENTER HINGE FITTINGS (ZV=2312.0) HAS DAMAGED FLANGE ON INTERIOR SIDE.-C/A- REMOVED AND REPLACED RIB AT ZV=2312.0 IAW EMB SRM 51-40-02.

Part: RIB — BENT (RUDDER) · airframe 49,060 hrs · 40,999 cycles

RUDDER 1 SUPPORT FLANGE SKIN AT THE UPPER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.

Part: RIB — DENTED (RUDDER) · airframe 49,060 hrs · 40,999 cycles

RUDDER 1 LEADING EDGE RIB BELOW CENTER HINGE FITTINGS (ZV=1897.0) IS DENTED.-C/A-REMOVED AND REPLACED RIB AT ZV=1897.0 FOR RUDDER LEADING EDGE BELOW CENTER HINGE FITTING IAW SRM 51-40-02.

Part: CHANNEL — CRACKED (NLG WW) · airframe 49,060 hrs · 40,999 cycles

WEB SUPPORT IN THE AFT END OF THE NLG BAY AT FRAME 7 IS CRACKED.-C/A-RAI WEB SUPPORT (CHANNEL) IN THE AFT END OF THE NLG BAY AT FR 7 IAW SRM 51-10-02.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 49,060 hrs · 40,999 cycles

BAGGAGE DOOR SKIN HAS A CRACK JUST UNDER THE OPEN/CLOSE HANDLE. (CRACK APPROX 1 " LONG)-C/A-C/W ERS-EM-52MR-1073 BAGGAGE DOOR CARGO DOOR HANGLE CUTOUT CRACK PERMANENT REPAIR.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

CARGO DOOR ASSIST TORSION BAR MOUNT BRACKET IS CRACKED AT FR 60 RH. -C/A-REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

CARGO BAY DOOR HOLD OPEN ROD SUPPORT BRACKET IS CRACKED. -C/A-INSTALLED NEW BRACKET IAW EMB--145 SRM CH. 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

CARGO BAY DOOR FUSELAGE SILL IS CORRODED. -C/A-REMOVED AND REPLACED CARGO BAY DOOR FUSELAGE SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

SHEAR CLIP CRACKED AT FRAME 16 BETWEEN STRINGERS 1 R -2 R.-C/A-RAR SHEAR CLIP AT FR 16 IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

LH WING-TO-FUSELAGE UPPER SUPPORT ANGLE HAS EVIDENCE OF A CRACK BY THE RIVET. APPROX 1" LONG AT FRAME 48.-C/A-REPAIRED IAW SRM 53-23-12 ITEM #3.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 49,060 hrs · 40,999 cycles

RH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #2 IS CRACKED ON THE FWD END. UP TO THE 1ST RIVET, AND IS APPROX 3/8" LONG. -C/A-C/W REPLACEMENT OF #2 RH WING TO FUSELAGE LOWER SUPPORT ANGLE IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 49,060 hrs · 40,999 cycles

LH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #2 IS CRACKED ON THE FWD END. UP TO THE 1ST RIVET, AND IS APPROX 3/8" LONG.-C/A-REMOVED AND REPLACED LH WING TO FUSELAGE LOWER SUPPORT ANGLE #2 IAW SRM 51-40-02, AND ETN-EM-53-142.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 49,060 hrs · 40,999 cycles

LH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #3 IS CRACKED ON THE FWD END. AND IS APPROX 1 1/2" LONG. -C/A-R EMOVED AND REPLACED LH WING TO FUSELAGE LOWER SUPPORT ANGLE #3 IAW SRM 51-40-02, AND ETN-EM-53-142.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 49,060 hrs · 40,999 cycles

LH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #4 IS CRACKED ON THE FWD END. AND IS APPROX 1 1/2" LONG. -C/A-REPAIRED LH WING TO FUSELAGE LOWER SUPPORT ANGLE #4 IAW ETN-EM-53-142.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

CARGO BAY UNDER FLOOR FRAME IS CRACKED AT FR 72 LH AND STR.16 LH. -C/A-REPAIRED FRAME 72 IAW ERS-EM-53MR-4094.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,060 hrs · 40,999 cycles

RT EXTRUSION NR 7 DAMAGED. REMOVED AND REPLACED RT EXTRUSION NR 7, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,060 hrs · 40,999 cycles

RT EXTRUSION NR 4 DAMAGED. REMOVED AND REPLACED RT EXTRUSION NR 4, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,060 hrs · 40,999 cycles

RT EXTRUSION NR 6 DAMAGED. REMOVED AND REPLACED RT EXTRUSION NR 6, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,060 hrs · 40,999 cycles

EMERGENCY LIGHT NR 5 EXTRUSION DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT NR 5 EXTRUSION, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,060 hrs · 40,999 cycles

EMERGENCY LIGHT NR 1 EXTRUSION DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT NR 1 EXTRUSION, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION. C/W REPAIR IAW ERS-EM-53MR-3758 PART B. TDMI RESTORED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 49,060 hrs · 40,999 cycles

TDMI 607T5323 ORIGNAL LG PG 4475656/3 TRANSFERRED FROM NRTC E710113, COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION ERS-EM-53MR-3758 PTB TRANSFERRED TO NRTC E782419 C BRODA 460360. UPGRADED TO A MAJOR REPAIR REFERENCE ERS-EM-53MR-3758. C/A-C/W REPAIR IAW ERS-EM-53MR-3758 PART B. TRANSFERRED TO NON-ROUTINE E782419. TDMI RESTORED.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,060 hrs · 40,999 cycles

EMERGENCY LIGHT NR 8 EXTRUSION DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT NR 8 EXTRUSION, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.

Part: INVERTER — FAILED (CABIN) · airframe 49,028 hrs · 40,966 cycles

FLOOR EMERGENCY LIGHT STRIP INOP #1-C/A-REMOVED AND REPLACED INVERTER OVER SERVICE DOOR IAW 33-50-11 OPS CHECK GOOD

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 48,690 hrs · 40,717 cycles

FWD ATTENDANT EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-REMOVED AND REPLACED FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: FAN — FAILED (RECIRCULATION) · airframe 48,204 hrs · 40,267 cycles

CLIMBING THROUGH 15000' WE HEARD AND FELT A THUD FOWLLED BY A ELEC/OZONE BURNING SMELL FOR 30 SEC IN THE COCKPIT AND GALLY THE SAME SMELL OCCURED FOR 10 SEC IN FLIGHT COMMING BACK TO CHICAGO AND THEN ON THE GROUND FOR 5 SEC TAXING IN, BOTH ENGINE ON NO SMOKE OR HAZE OBSERVED. NO UNUSALL ENGINE OR INSTRUMENTS INDICATION OBSERVED ON THE EICAS, PFD, ALL THE MFD PAGES NORMAL. SPEED 270 KTS CLIMBING, IMC, ICE PROTECTION GOING ON AND OFF AS NORMAL PACK 1+2 WERE ON, ENG BLEEDS ON, APU BLEED CLOSED/ PASSENGER HEARD THUD ON RIGHT SIDE OF AIRCRAFT BY LANDING GEAR. FLIGHT ATTENDANT REPORTS ELECTRICAL/OZONE SMELL WAS IN THE GALLEY FORWARD TO THE COCKPIT DOOR. PASSENGER SAID IT SOUNDED LIKE THE LANDING GEAR WAS RETRACTING OE EXTENDING 15 MIN AFTER DEPATRURE WHEN THE THUD-C/A-INSPECTED AND RETORQUED CAPT WINDSHEILD CONTROLER IAW EMB 145 AMM 30-42-01 NO ODOR NOTED. INSPECTED COCKPIT WINDSHEILDS HEATING SENSORS FOR SMOKE OR ELECTRICAL BURNING SMELL PER EMB 145 FIM 21-20-00-810-801-A NONE NOTED. C/W INSPECTION FOR SMOKE OR ELECTRICAL BURNING SMELL AT THE DISPLAY UNITS PER EMB 145 FIM 21-20-00-810-801-A. PERFORMED ETN-EM-72-034 AND T/S IAW EMB 145 FIM 21-20-00-810-801-A. REF 607--ORD-02771 AND REF NRWC 607-ORD-02772 FOR ALL WORK ACCOMPLISHED NO ODOR OR SMOKE NOTED. RE ATTACHED AFT END OF #2 RERICULATION FAN EXHAUST MUFFLER IAW EMB 145AMM 21-24-02. REMOVED AND REPLACED #2 RECIRCULATION FAN IAW EMB145 AMM 21-24-01. PERFORMED GVI OF RH PACK AREA, NO BLOW OR DAMAGED DUCT

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 47,971 hrs · 40,045 cycles

#3 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW AMM 33-50-=04.OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 19422

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 47,971 hrs · 40,045 cycles

#2 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW AMMK 33-50-04.OPS CHECK GOOD. BATTEERY CHARGER ASSY P/N 11-0049 S/N 14731

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 47,971 hrs · 40,045 cycles

#4 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW AMM 33-50-04.OPS CHECK GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 47,971 hrs · 40,045 cycles

#1 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY #1 IAW AMM 33-50-04 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 67260

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 47,832 hrs · 39,906 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT FOUND DAMAGED. C/A-REMOVED AND REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 47,693 hrs · 39,768 cycles

FA FWD FLASHLIGHT NOT WORKING. REMOVED AND REPLACED FLASHLIGHT BATTERY AS REQUIRED OPC GOOD.

Part: MODULE — FAILED (CABIN LIGHTS) · airframe 47,664 hrs · 39,746 cycles

CABIN LIGHTS WILL NOT TURN OFF. BURNING SMELL FROM LIGHT BULB NEAR FA CONTROL PANEL AND FORWARD WINDOW. REMOVED AND REPLACED CABIN LIGHTS MODULE CONTROL ASSY IAW AMM 33-21-01 OPTS CHECK GOOD .

Part: FAN — INOPERATIVE (NR 2 RECIRC) · airframe 47,632 hrs · 39,724 cycles

OIL SMELL IN THE COCKPIT, INSPECTED NR 1 & 2 PACK RECIRCULATION SYSTEMS AND FOUND NR 2 RECIRCULATING FAN INOPERATIVE, REMOVED AND REPLACED THE NR 2 RECIRCULATION FAN IAW AMM 21-24-01, OPS CHECKED GOOD, NO SMELL. INSPECTED NR 1 & 2 PACKS FOR LEAKS AND SYSTEM OPERATION AND FOUND WORKING PROPERLY IAW AMM 21-20-00, INSPECTED NR 1 & 2 PACK RECIRCULATION DUCTS AND FOUND NR 1 RECIRCULATION FAN MUFFLER BROKEN, REPLACED THE MUFFLER DUCT IAW AMM 21-24-02 AND SECURED THE NR 2 RECIRCULATION FAN MUFFLER DUCT IAW AMM 21-21-02.

Part: WIRE — BROKEN (CABIN) · airframe 47,552 hrs · 39,658 cycles

FOUND EMERGENCY LIGHT STRIP WIRE BROKEN IN ROW 16A. C/A-REMOVED AND REPLACED EMERGENCY FLOOR STRIP LIGHT IAW AMM 33-50-12 OPS CHECK GOOD.

Part: DOOR SEAL — TORN (PAX DOOR) · airframe 47,394 hrs · 39,503 cycles

PASSENGER DOOR SEAL ON DOOR SIDE IS TORN (MAIN DOOR DIFFICULT TO OPEN/CLOSE). -C/A-REMOVED AND REPLACED PAX DOOR SEAL IAW AMM 52-18-04, REFER TO 607-MQT-02445 FOR CABIN LEAK CHECK.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 47,393 hrs · 39,502 cycles

SUPPLEMENTAL MAIN DOOR DIFFICULT TO OPEN/CLOSE "TRANSFERRED TO NRWC 607-ORD-02433". C/A-REF NRWC # 607-ORD-02433 REF AML # 4532148 ITEM #1 AND #3 FOR CORRECTIVE ACTION AND FERRY TO MQT. END. PAX DOOR SEAL AND FRAME SEAL FOUND TORN AND PAX DOOR FOUND OUT OF ADJUSTMENT. REMOVED AND REPLACED PAX DOOR SEAL IAW AMM 52-18-04; REMOVED AND REPLACED PAX FRAME SEAL IAW AMM 53-21-01. ADJUSTED PAX DOOR STEP IAW AMM 52-18-00, STEP AND STOP GAPS CHECK GOOD. INSTALLED PAX DOOR IAW AMM 52-18-00, FOLLOW ON TASK COMPLIED WITH, INNER HANDLE CHECKS GOOD AT 40 LBS. C/W CABIN LEAKAGE FUNCTIONAL CHECK IAW AMM 21-31-00, LEAK CHECK GOOD.

Part: SEAL — DAMAGED (EMERGENCY EXIT) · airframe 47,320 hrs · 39,423 cycles

LOUD NOISE COMMING FROM PAX DOOR OR CA DV WINDOW AT ABOUT 4.8 PSI ^P-C/A-REPAIRED CA SIDE COCKPIT EMERGENCY-EXIT RUBBER TRIM SEAL IAW AMM 56-11-02 LEAK CHECK GOOD REPAIRED CAPTIANS SIDE COCKPIT EMERGENCY-EXIT RUBBER TRIM SEAL IAW AMM 56-11-02 LEAK CHECK GOOD REF WORK ITEM TURN OVER THIS NRWC FOR WORK ACCOMPLISHED. ALSO INSPECTED PAX DOOR IAW ETN-EM-52-052 NO DEFECTS NOTED. INSPECTED PAX DOOR IAW ETN-EM-52-052 AND PERFORMED OPS TEST IAW EMB 145 AMM 52-18-00 REF NRWC 607-ORD-02401 FOR WORK ACCOMPLISHED OPS CHECK GOODPRESSURE CHECK GOOD IAW EMB 145 AMM 21-31-00

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,320 hrs · 39,423 cycles

DURING PS-1 CHECK FOUND SERVICE DOOR EXIT FLOOR PROX LIGHT INOP-C/A-REMOVED AND REPLACED SERVICE DOOR EXIT FLOOR PROX LIGHT IAW AMM 33-50-12. OPS CHECK GOOD

Part: DOOR — LEAKING · airframe 47,306 hrs · 39,411 cycles

AT 15,000 FEET WE HEARD A VERY LOUD WHISTLING SOUND COMING FROM THE CABIN. WE NOTICED THE CABIN ALTITEDE INCREASING MORE RAPIDLY . WE DECLARED AN EMERGENCY AND PERFORM A NORMAL LANDING IN MIA "TRANSFERRED TO NRWC 607-MIA-02391" FOUND SEVERAL LEAKS AND REPAIRED PER AMM. PERFORM REPAIRS TO BOTH DOORS IAW AMM 52-00-04 OPS AND LEAK CHECK GOOD. PERFORM PRESSURE LEAK DOWN TEST IAW AMM 21-31-00-700-808-A OPS CHECK GOOD, NO NOISE OR WHISTLING NOTED

Part: LIGHT — INOPERATIVE · airframe 47,188 hrs · 39,316 cycles

LT EMERGENCY LIGHT ABOVE WING IS INOP. C/A-RAR LT ABOVE WING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,078 hrs · 39,195 cycles

COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION. C/A-PERFORMED TEMPORARY REPAIR OF COCKPIT UNDERFLOOR FUSEALGE SKIN BETWEEN FR 13-14 AND STR 20R-18L IAW ERS-EM-53MR-3758 PART A.

Part: WIRE — BROKEN (CABIN) · airframe 47,078 hrs · 39,195 cycles

NR 7 FLOOR LIGHT STRIP WIRIES BROKEN OFF. C/A-REMOVED AND REPLACED NR 7 FLOOR LIGHT STRIP IAW AMM 33-50-12.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 47,078 hrs · 39,195 cycles

VERTICAL STABILIZER LH LOWER DRAG ANGLE CRACKED AT FR 76. REMOVED AND REPLACED VERTICAL STABILIZER LH LOWER DRAG ANGLE AT FR 76 IAW EMB145 SRM 51-40-02

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,184 hrs · 38,431 cycles

RAM AIR VALVE FAIL. RESET AND OPS CHECK OF RAM AIR VALVES GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,768 hrs · 38,059 cycles

SERVICE DOOR EXTERIOR EMERGENCY FLOOD LIGHT NR 2 INOPERATIVE. R & R THE BULBS, OPS CHECKED GOOD.

Part: HINGE FITTING — DAMAGED (LT ELEVATOR) · airframe 44,151 hrs · 36,622 cycles

LEFT ELEVATOR HAS DAMAGE AT THE TOP OF THE CENTER HINGE. REPAIRED THE ELEVATOR CENTER HINGE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 49-50) · corrosion level 2 · airframe 44,151 hrs · 36,622 cycles

CENTER OMEGA BEAM IS CORRODED ABOVE CROSSBEAM BETWEEN FRAMES 49 - 50. REPAIRED IAW ETD2017-145-053515.

Part: YOKE — CRACKED (RT PYLON) · airframe 44,151 hrs · 36,622 cycles

RIGHT PYLON FWD YOKE CRACKED. REMOVED AND REPLACED THE RT PYLON FWD YOKE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,151 hrs · 36,622 cycles

CRACK IN FUSELAGE EXTERNAL SKIN AT FRAME 61 AND STRINGER 17L APPROX ¾” IN LENGTH END MARKED. FOUND BY HFEC. PERFORMED REPAIR ON FUSELAGE EXTERNAL SKIN AT FRAME 61 AND STRINGER 17L.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,151 hrs · 36,622 cycles

AFT FUSELAGE FR 75 SKIN CRACK AT FASTENER HOLE BELOW STR 2. CUT OUT DAMAGE AND APPLIED FILLER AND DOUBLER TO FR 75 STR 2R CRACK.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 44,151 hrs · 36,622 cycles

TOILET WASTE VALVE SUPPORT BUCKET HAS ARES OF CORROSION. R & R THE TOILET WASTE VALVE SUPPORT.

Part: STRUCTURE — BROKEN (EMERGENCY EXIT) · airframe 43,531 hrs · 36,090 cycles

LEFT EMERGENCY EXIT SURROUND TOP TRIM IS BROKEN. REPAIRED THE EMERGENCY EXIT SURROUND TOP TRIM, OPS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (RAM AIR) · airframe 43,143 hrs · 35,789 cycles

RAM AIR VALVE FAILED. RESET RAM AIR VALVE CIRCUIT BREAKERS AND PERFORMED OPS CHECK, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 42,587 hrs · 35,336 cycles

LANDING GEAR FAILED TO RETRACT ON TAKEOFF, TROUBLESHOOTING ISSUE.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 42,586 hrs · 35,335 cycles

HYD SYSTEM 1 QTY WENT TO ZERO ON CLIMBOUT, ROUGHLY 10K FT, NO OVERWEIGHT LANDING. PERFORMED GVI OF ACFT FOUND HYD LEAK AT PANEL 651CB, SERVICE HYD SYS 1 IAW AMM 12-13-01. REMOVED PANELS 651CB AND 651FT IAW AMM 27-12-01, PERFORMED OPS CHECK OF HYD SYS 1 IAW AMM 29-10-00, OPS CHECK FAIL, LOSS OF HYD FLUID FROM BROKEN HYD HOSE ABOVE RT PCA, R & R HYD HOSE 230, REF IPC 27-12-00, PRESSURIZED HYD SYS AND ACTUATED AILERONS IAW AMM 27-12-00, NO LEAKS NOTED.

Part: O-RING — LEAKING (BLEED SYS) · airframe 42,543 hrs · 35,302 cycles

BLEED 1 LEAK. R & R O-RINGS AND SECURED DUCT FOR PAC EXHAUST. OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,830 hrs · 33,913 cycles

RIGHT OVERWING EXTERIOR EMERGENCY FLOOD LIGHT NR 6 INOPERATIVE. MAINTENANCE REPLACED NR 4 BATTERY POWER SUPPLY, OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,830 hrs · 33,913 cycles

LEFT OVERWING EXTERIOR EMERGENCY FLOOD LIGHT NR 5 INOPERATIVE. MAINTENANCE REPLACED NR 4 POWER SUPPLY BATTERY, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,616 hrs · 33,744 cycles

LEFT OVERWING AFT EMER LIGHT INOPERATIVE. R & R LT AFT OVERWING EMER LIGHT LAMP & RESEATED LIGHT ASSEMBLY CONNECTOR IAW AMM 33-50-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,616 hrs · 33,744 cycles

LEFT OVERWING AFT EMER LIGHT INOPERATIVE. R & RT LT AFT OVERWING EMER LIGHT LAMP & RESEATED LIGHT ASSEMBLY CONNECTOR IAW AMM 33-50-10. OPERATIONALLY CHECKED EMER LIGHTING SYS. CHECKED GOOD.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

THREE EACH ELONGATED HOLES ON STRINGER 17L BETWEEN FRAMES 68 & 69. REPAIRED IAW ERS-EM-53MR-1267.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

RIGHT OMEGA BEAM IS CRACKED AT THE NUTPLATE HOLE JUST AFT OF FRAME 59. REPAIRED RT OMEGA BEAM JUST AFT OF FRAME 59 IAW ERS-EM-53MR-1241.

Part: FASTENER — MISSING (LT WING) · airframe 40,612 hrs · 33,741 cycles

LEFT WING REAR SPAR UPPER FLANGE, PREVIOUS REPAIR HAS 2 HOLES WITHOUT FASTENERS LOCATED JUST INBD OF GND SPOILER CTR HINGE POINT. LT WING REAR SPAR UPPER FLANGE REPAIRED IAW ERS-EM-57MR-430.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

RIGHT OMEGA BEAM IS CRACKED AT THE NUTPLATE HOLE JUST AFT OF FRAME 59. REPAIRED IAW ERS-EM-53MR-1241.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · airframe 40,612 hrs · 33,741 cycles

INBD SPRING TAB HINGE FITTING & OTBD SERVO TAB HINGE FITTING ON RT ELEVATOR ARE CORRODED. R & R INBD SPRING TAB & OTBD SERVO TAB HINGE FITTINGS IAW AMM 55-22--01, REF NRTC E446214 FOR TAB INSTALLATION. HINGE SUPPORT 145-27288-401.

Part: HINGE FITTING — CORRODED (ELEVATOR TAB) · airframe 40,612 hrs · 33,741 cycles

TRANSFERRED FROM NRTC E446215, LT ELEVATOR INBD & OTBD SERVO TAB HINGE FITTINGS ARE CORRODED. R & R LT ELEVATOR INBD & OTBD SERVO TAB HINGE FITTINGS IAW AMM 55-22--01. REF NRTC E446215 FOR SERVO TAB INSTALLATION. FITTING PN 145-27288-402.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L & 7L HAS A 2 INCH CRACK. R & R SHEAR CLIP IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

LEFT LOWER AFT FAIRING SUPPORT IS CRACKED. REPAIRED AFT BELLY PANEL, LT LOWER ATTACHMENT SUPPORT IAW ERS-EM-5300-122.

Part: ANGLE — CRACKED (LT WING) · airframe 40,612 hrs · 33,741 cycles

LEFT WING UPPER SURFACE L ANGLE SUPPORT FOR PANEL 195EL IS CRACKED. R & R THE LT WING UPPER SURFACE L ANGLE SUPPORT FOR PANEL 195EL IAW SRM 51-40-02.

Part: RIB — CRACKED (RT WING) · airframe 40,612 hrs · 33,741 cycles

RIGHT WING RIB 5 HAS A 1 INCH CRACK LOCATED 1ST LARGE CUT OUT FROM AFT EDGE, 7:OO POSITION, OTBD SIDE. COMPLIED WITH REPLACEMENT OF RT WING RIB 5 IAW EO EM-57MR-595.

Part: FIREWALL — CRACKED (APU BAY) · airframe 40,612 hrs · 33,741 cycles

APU FIREWALL CRACKED ON THE AFT RT SIDE. COMPLETED REPAIR OF APU FIREWALL IAW ETN-EM-53-244 & EO-EM-53AD-1883.

Part: BRACKET — CRACKED · airframe 40,612 hrs · 33,741 cycles

RIGHT FWD PRE-COOLER BRACKET CRACKED. REPLACED RT FWD PRE-COOLER BRACKET IAW SRM 51-40-02 & ETN EM-54-056.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

RIGHT OMEGA BEAM SUPPORT ANGLE IS CRACKED. INBD ANGLE BETWEEN FRAMES 47 - 48. R & R RT OMEGA BEAM SUPPORT ANGLES IAW SRM 53-23-02 & SRM 51-40-02.

Part: BRACKET — CRACKED · airframe 40,612 hrs · 33,741 cycles

LEFT FWD PRE-COOLER BRACKET CRACKED. REPLACED LT FWD PRE-COOLER BRACKET IAW SRM 51-40-02 & ETN EM-54-056.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

LEFT OMEGA BEAM SUPPORT ANGLE IS CRACKED. OTBD ANGLE BETWEEN FRAMES 47 - 48. R & R LT OMEGA BEAM SUPPORT ANGLE IAW SRM 53-23-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 40,612 hrs · 33,741 cycles

LEFT BLEED DUCT SUPPORT BRACKET JUST AFT OF FRAME 68 & BELOW THE FLOOR LEVEL IS CRACKED, APPROX 1 1/2 INCH. COMPLETED FABRICATION & INSTALLATION OF NEW BRACKET IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (CABIN) · airframe 40,612 hrs · 33,741 cycles

LEFT EMER LIGHT FLOOR EXTRUSION NR 1 IS CRACKED. R & R LT EMER LIGHT FLOOR EXTRUSION NR 1 IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 40,612 hrs · 33,741 cycles

NUMBER 3 FLOOR PROXIMITY EMER LIGHT HAS A BROKEN WIRE. R & R NR 3 FLOOR PROXIMITY EMER LIGHT IAW AMM 33-50-12.

Part: STRUCTURE — CRACKED (CABIN) · airframe 40,612 hrs · 33,741 cycles

RIGHT EMER LIGHT FLOOR EXTRUSION NR 7 IS CRACKED. R & R RT EMER LIGHT FLOOR EXTRUSION IAW AMM 33-50-12.

Part: STRUCTURE — CRACKED (CABIN) · airframe 40,612 hrs · 33,741 cycles

LEFT EMER LIGHT FLOOR EXTRUSION NR 2 IS CRACKED. R & R LT EMER LIGHT FLOOR EXTRUSION NR 2 IAW AMM 33-50-12.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 40,302 hrs · 33,442 cycles

AFT GALLEY WALL EMER EXIT SIGN INOPERATIVE. R & R NR 3 EMER LIGHT INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: SPLICE — DAMAGED (CABIN) · airframe 40,269 hrs · 33,409 cycles

EXIT LOCATOR AT AFT GALLEY WALL WILL NOT ILLUMINATE. REPAIRED SPLICE SP 9223 IAW WM 20-21-00. EMER LIGHTING SYS OPERATION IS GOOD IAW AMM 33-50-00.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 40,269 hrs · 33,409 cycles

AFT FLIGHT ATTENDANT`S FLASHLIGHT SWITCH IS INTERMITTENT. R & R AFT PAX COMPARTMENT FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 40,046 hrs · 33,221 cycles

BULB BURNED OUT IN THE CAPTAIN'S FLASHLIGHT. R & R IAW AMM 25-60-05. OPERATIONS CHECKED GOOD.

Part: FMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 39,442 hrs · 32,660 cycles

DURING STARTING NR 2 ENG, RAMP AGENT NOTICED ALOT OF SMOKE COMING OUT OF NR 2 WITH FUEL SMELL IN CABIN & COCKPIT. ABORTED START NR 2 AROUND 32%, FOLLOW CHECKLIST FOR ABORTED START, NR 2 DID NOT GET ABOVE 32%. INSPECTED & NR 2 ENG FPMU SEEPING FROM BODY HALVES. R & R FPMU ASSEMBLY IAW MM 73-21-10. PERFORMED ENG RUNS & NO LEAKS OR STARTING PROBLEMS NOTED. PERFORMED ETN-EM-72-034 & NO SMELL OF FUEL WITHIN COCKPIT OR CABIN NOTED.

Part: STRUCTURE — CRACKED (SPOILER) · airframe 39,155 hrs · 32,412 cycles

SECOND FROM FUSELAGE SPOILER HINGE POCKET ON RT WING IS CRACKED. TRANSFERRED TO NRWC 607-MQT-02022. IAW NRWC 607-MQT-02022, COMPLIED WITH REPAIR IAW ERS-EM-57MR-218.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 38,949 hrs · 32,244 cycles

HYD 2 LOW QTY ADVISORY IN FLIGHT, ABOUT 20 - 30 MINUTES LATER HYD 2 PUMP FAIL MSG. POST FLIGHT SHOWS HYD FLUID COATING INSIDE NR 2 WW. R & R NR 2 ENG DRIVEN PUMP IAW AMM 29-10-03. RAN ENGS LEAK & OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 38,390 hrs · 31,795 cycles

FLASHLIGHT IN COCKPIT BROKEN. R & R FLASHLIGHT IN COCKPIT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,776 hrs · 31,316 cycles

FORWARD BULKHEAD EMERGENCY LIGHT STRIP INOPERATIVE. R & R FWD BULKHEAD EMERGENCY LIGHT STRIP, OPERATIONS CHECKED GOOD IAW EMB 33-50-13.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,646 hrs · 31,207 cycles

REMOVED PANEL 251BF TO FOM & FOUND EMERGENCY LIGHT STRIP TO BE DAMAGED. R & R EMERGENCY LIGHT STRIP IAW AMM 33-50-12, OPERATIONS CHECKED GOOD.

Part: FAN — MALFUNCTIONED (NR 1) · airframe 37,646 hrs · 31,207 cycles

TRANSFERRED FROM AML PAGE 3508764 ITEM 2 IAW ITEM NR 1 STRONG ELECTRIC ODOR IN COCKPIT. TROUBLE SHOOTING FOUND NR 1 RECIRCULATING FAN SQUEALING. R & R NR 1 RECIRCULATING FAN IAW AMM 21-24-01. OPERATIONS CHECKED GOOD AT THIS TIME. RAN PACKS & ELEC SMELL FOUND IN COCKPIT OR CABIN. .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,334 hrs · 30,974 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 2948 FOUND MAIN DOOR HINGE EMERGENCY LAMP INOPERABLE. R & R THE MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,267 hrs · 30,918 cycles

LAST THREE EMERGENCY FLOOR STRIPS LIGHTS INOPERATIVE. R & R NR 6 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11. OPERATIONS CHECKED GOOD IAW AE WC 33-700-17.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 36,984 hrs · 30,689 cycles

CREW REPORT CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33=50-16.

Part: BATTERY PACK — UNKNOWN (EMERGENCY LIGHT) · airframe 36,581 hrs · 30,335 cycles

REF ITEM 2 , REPLACE EMERGENCY BATTERY ASSY 4 ,WC 33-700-19. R & R NR 4 EMERGENCY BATTERY ASSY IAW WC 33-700-19.

Part: WIRE — BROKEN (CABIN) · airframe 35,912 hrs · 29,793 cycles

DURING MX INSP, FOUND THE EMERGENCY PROXIMITY LIGHT STRIP TO HAVE A WIRE BROKEN UNDER FLOORBOARD 251BF. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED NEW CONNECTOR SPLICE IAW SWPM 20-50-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND THE LT WING, RIB 5 CRACKED. THE ACFT WAS REMOVED FROM SERVICE. LT WING RIB 5 HAS BEEN REPLACED IAW EO EM-57MR-594. THE ACFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK FOUND STRINGER 18 RIGHT, IS CORRODED BETWEEN FRAMES 13 AND 14. THE ACFT WAS REMOVED FROM SERVICE. R & R STRINGER PROFILE BETWEEN FRAMES 13 AND 14 AT STRINGER 18 RT IAW SRM 51-40-02. THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND LT ELEVATOR SKIN TO BE DAMAGED UNDERNEATH UPPER SPRING TAB FAIRING BRACKET. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED LT ELEVATOR SKIN IAW EO EM-55MR-424.

Part: CROSSBEAM — CRACKED (NLG) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK FOUND NLG AFT CROSSBEAM IS CHAFED AND CRACKED. THE ACFT WAS REMOVED FROM SERVICE. R & R NLG CROSSBEAM IAW SRM 51-40-02. THE ACFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND CORROSION ON FRAME 68 SHEAR CLIP AT CARGO DOOR CUTOUT. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1129. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND LT OMEGA BEAM IS CORRODED AT FRAME 57- 59 UNDERNEATH THE CROSSBEAM. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED LT OMEGA BEAM IAW AMERICAN EAGLE EO EM-53MR-1518, PART A. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND CORROSION ON FRAME 65 SHEAR CLIP AT CARGO DOOR CUTOUT. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1129. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND FUSELAGE SKIN CRACKED AT FRAME 75 STR 2L. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED FUSELAGE SKIN IAW EO EM-53MR-2132. THE ACFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND THE CARGO SILL CORRODED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CARGO DOOR SILL IAW SRM 51-40-02. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND SERVICE DOOR SURROUND STRUCTURE AT FRAME 22 BEHIND LOWER AFT DOOR GUIDE FRAME CORRODED. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED FRAME IAW SRM 53-00-04 AND 51-40-02. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND LT OMEGA BEAM CORRODED AT FRAME 29, UNDERNEATH THE CROSSBEAM. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED LT OMEGA BEAM IAW EO EM-53MR-1530, PART A. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK FOUND THE CENTER OMEGA BEAM IS CORRODED AT FRAME 57, 59 UNDERNEATH THE CROSSBEAM. REPAIRED OMEGA BEAM IAW AMERICAN EAGLE EO EM-53MR-1518 PART B. LEVEL OF CORROSION NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (LT AILERON) · airframe 35,882 hrs · 29,767 cycles

DURING HEAVY CHECK, FOUND LT AILERON PCA FITTING, 2ND FROM OUTBD HAT BUSHING BORE IS WORN. THE ACFT WAS REMOVED FROM SERVICE. R & R LT AILERON PCA FITTING IAW EO EM-27MR-112. THE ACFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,875 hrs · 29,760 cycles

CORROSION ON FRAME 68, SHEAR TIE AT CARGO DOOR CUTOUT. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.

Part: WIRE — BROKEN (CABIN) · airframe 35,912 hrs · 29,793 cycles

DURING MX INSP, FOUND THE 6TH EMERGENCY PROXIMITY LIGHT STRIP ON THE LT SIDE CRACKED AND FOUND THE 5TH EMERGENCY PROXIMITY LIGHT STRIP TO HAVE A BROKEN WIRE ON THE LT SIDE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE 6TH EMERGENCY PROXIMITY LIGHT STRIP IAW AMM 33-50-12. REPAIRED BROKEN WIRE ON THE 5TH EMERGENCY PROXIMITY LIGHT STRIP. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,874 hrs · 29,760 cycles

DURING MX INSPECTION, FOUND THE NR 1 & NR 2 BATTERY INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 1 BATTERY AND THE NR 2 BATTERY AND NR 2 BATTERY CHARGER. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,912 hrs · 29,793 cycles

DURING MX INSP, FOUND THE LIGHT STRIP ASSY FOR THE LT FWD PROXIMITY STRIP PANEL CRACKED AND HAD A BROKEN WIRE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LIGHT STRIP ASSY IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: TERMINAL — LOOSE (BUSS TIE RELAY) · airframe 35,527 hrs · 29,481 cycles

ON FLIGHT 2970 THE CREW REPORTED AN UNKNOWN ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND TERMINAL END ON BUS TIE RELAY LOOSE. REPLACED BOLT AND WASHERS AND NUT IAW MM 24-60-01 AND COMPLIED WITH OPERATIONAL CHECKS IAW 24-60-00. OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 35,389 hrs · 29,380 cycles

FLIGHT 4329. CREW REPORTED AFT CABIN FLASHLIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: CONNECTOR — CORRODED (SPOILER SENSOR) · airframe 35,026 hrs · 29,091 cycles

RT SPOILER PROXIMITY SENSOR HAS CORRODED CONNECTOR. INSTALLED CONNECTOR IAW EO EM-57MR-663.

Part: SPAR — CRACKED (RT WING)

RIGHT WING SPAR III CRACKED AT STA 1690.00 (MLG HARNESS FEED THRU) TOWARD UPPER FLANGE OF SPAR AND TERMINATING AT UPPER SKIN TO SPAR FASTENER 3.5 INCHES LONG.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 34,673 hrs · 28,816 cycles

ON FLIGHT 4089 THE CREW REPORTED THAT WHILE EXCITING FINAL STAGES OF ARRIVAL DESCENT AFTER HAVING FLOWN THROUGH A 2 MIN EXPOSURE TO MOD RIME ICE AT FLAP 9 SELECTION FLAPS REMAINED AT ZERO. SYSTEM WAS RESET AFTER CHECKLIST, COMPLIANCE AND FLAP SYSTEM OPERATIONS WERE NORMAL AFTER BEING RETRACTED THEN RESET TO 9. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. UPON ARRIVAL MOC AND SOC WERE ADVISE AND CONSULTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION OF FLAPS NO DEFECTS NOTED. PERFORMED FIM 27-51-60-810-803-A, FOUND TO BE TRANSITORY CONDITION, SYSTEM OPERATIONS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — OVERTEMP (NR 2) · airframe 34,299 hrs · 28,528 cycles

ON FLIGHT 2829 THE CREW REPORTED THAT ON CLIMBOUT HAD A NR 2 ENGINE OVERTEMP INDICATION. THE CREW REDUCED THRUST AND LEVELED OFF AT 10,000 FEET. THE CREW CONTACTED ATC, DECLARED AN EMERGENCY AND COMPLETED THE AOM VOL 1 CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RIGHT ENGINE LOWER COWLING REMOVED TO FOM- INSTALLED RIGHT ENGINE LOWER COWLING IAW EMB 145AMM 71-12-01. RIGHT ENGINE UPPER COWLING REMOVED TO FOM. INSTALLED RIGHT ENGINE UPPER COWLING IAW EMB 145 AMM 71-11-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTACTOR — DEFECTIVE (RECIRC FAN) · airframe 34,210 hrs · 28,454 cycles

ON FLIGHT 3265 THE CREW REPORTED, THEY SMELLED A BURNING RUBBER TYPE ODOR AND MADE THE DECISION TO RETURN FOR AN OVERWEIGHT LANDING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RECIRCULATION FAN NR 1 TO BE INOPERATIVE. REMOVED AND REPLACED LEFT RECIRCULATION FAN CONTACTOR K0189 REF EMB 145 AMM 21-24-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 33,937 hrs · 28,232 cycles

FLIGHT 2865, THE CREW REPORTED THE FLIGHT ATTENDANT REAR FLASHLIGHT WAS MISSING. INSTALLED NEW FLASHLIGHT, OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,830 hrs · 28,154 cycles

DURING B INSPECTION, FOUND THE EMERGENCY EXIT LIGHT AT MAIN PASSENGER DOOR INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT NR 1 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 33,762 hrs · 28,098 cycles

ON FLIGHT 3329 THE FLIGHT ATTENDANT NOTIFIED THE CREW OF AN ELECTRICAL ODOR IN THE GALLEY. THE CREW RAN THE CABIN/COCKPIT SMOKE/FIRE CHECKLIST IN AOM VOL 1. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SAT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED GALLEY WORK LIGHT BALLAST IAW 145 AMM 33-29-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 33,712 hrs · 28,062 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD CEILING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR NOT SEATED PROPLEY RESEATED CONNECTOR AND THE OPERATIONAL CHECK WAS GOOD IAW EMB MM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 33,634 hrs · 27,994 cycles

ON FLIGHT 2887 THE CREW REPORTED THE COCKPIT FLASHLIGHT BEHIND THE CAPTAIN’S SEAT WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE MISSING FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 33,486 hrs · 27,873 cycles

ON FLIGHT 3402, THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 33-51-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 33,211 hrs · 27,654 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT AT SERVICE DOOR EXIT MARKER INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 32,889 hrs · 27,409 cycles

DURING B-INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT BASE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — CRACKED (CABIN) · airframe 32,475 hrs · 27,102 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT IS LOOSELY SECURED IN CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LOWER ARM OF CRADLE WAS CRACKED. REMOVED AND REPLACED CRADLE IAW EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,006 hrs · 26,787 cycles

THE CREW REPORTED THE LEFT EMERGENCY LIGHTS BY THE EMERGENCY EXITS ARE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ARRANGED EMERGENCY PROXIMITY LIGHT STRIPES IN ACCORDANCE WITH EMB 145 AMM 33-50-12. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 31,844 hrs · 26,662 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTING STRIP 3RD FROM FRONT AT SEAT 6A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW CONNECTORS TO NR 3 EMERGENCY FLOOR STRIP IAW EMB WM 20-21-00 TASK F. 5. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 31,385 hrs · 26,308 cycles

LT OMEGA BEAM AT FR25 CORRODED AND CRACKED. REPAIRED LT OMEGA BEAM AT FR25 IAW AE EO EM--53MR-1842.

Part: BRAKE — FAILED (MLG)

OPERATOR EXPERIENCED AN ON-WING CARBON RUPTURE EVENT FOLLOWING LANDING. THE EVENT OCCURRED ON THE NR 3 POSITION BRAKE ( RT INBD) PN 21707, SN 2398, AND RESULTED IN A COMPLETE RUPTURE OF THE PRESSURE PLATE AND NR1 ROTOR. PASSENGERS WERE REQUIRED TO PERFORM AN EMERGENCY DEPARTURE FOLLOWING REPORTS THA THE BRAKES WERE SMOKING, BUT NO INJURIES WERE REPORTED. INITIAL FEEDBACK SUGGENSTS THAT THE BRAKE HAD SUSTAINED 3787 CYCLES PRIOR TO RUPTURE. THE CAUSE IS STILL UNKNOWN PENDING INVESTIGATION.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 31,037 hrs · 26,019 cycles

ON FLIGHT 4176 THE TOWER ADVISED THAT AFTER TOUCHDOWN SAW A PUFF OF WHITE SMOKE FROM AIRCRAFT. DURING TAXI THE CREW NOTICED THE LEFT BRAKE PEDAL SOFT. THEN LOST NR 2 SYSTEM QUANTITY & PRESSURE AS THE CREW STOPPED THE AIRCRAFT. ON INSPECTION FOUND PIECES OF BRAKE AND HYDRAULIC FLUID ON THE GROUND. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2, 3 AND 4 TIRE ASSEMBLY IAW AE MTX WC 32-700-11. REMOVED AND REPLACED THE NR 2 AND 3 BRAKE IAW AE MTX WC 32-600-14. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RMU — MALFUNCTIONED (COMM SYSTEM) · airframe 30,402 hrs · 25,535 cycles

THE CAPTAIN DECLARED AN EMERGENCY ON FLIGHT 2704 DURING THE CLIMB THE CREW REPORTED THE NR 1 AND NR 2 COMMUNICATION RADIO MANAGEMENT UNIT FAILED AS UNABLE TO CHANGE THE FREQUENCY. THE CAPTAIN ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AND NR 2 RADIO MANAGEMENT UNITS. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — FAILED (BLEED AIR SYS) · airframe 30,010 hrs · 25,262 cycles

ON FLIGHT 2710 THE CREW REPORTED RECEIVED A BLEED 2 LEAK. THE CREW COMPLIED WITH AOM MESSAGE AND CLEARED. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED SAFELY AT DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS ON NR 6 CONNECTOR IAW EMB 145 AMM 36-11-10 AND REMOVED AND REPLACED NR 8 CONNECTOR IAW EMB 145 AMM 36-11-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 29,105 hrs · 24,581 cycles

ON FLIGHT 3294 DURING TAXI THE FLIGHT ATTENDANT AND PASSENGERS NOTED AND SMELLED SMOKE. THE CAPTAIN WALKED BACK AND NOTED THE SAME ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AREA AT 10BC AND REPLACED BURNT FLUORESCENT LIGHT HARNESS ASSEMBLY AT 9BC AND 10BC AND REPLACED FLUORESCENT TUBES AT 9BC AND 10BC IAW AMM 33-21-06. NO FURTHER ODORS NOTICED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — FAILED (BLEED AIR SYS) · airframe 28,320 hrs · 23,943 cycles

ON FLIGHT 3906 DURING CLIMB THE CREW RECEIVED AN EICAS WARNING FOR NR 2 BLEED LEAK. THE CREW ELECTED TO RETURN TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AIR BLEED LINE O-RING AT JOINT NR 16 (UNDER CARGO FLOOR PANEL 272BF) IAW EMB 145 AMM 36-11-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 28,108 hrs · 28,108 cycles

ON FLIGHT 9808 AFTER TAKEOFF THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. THE CREW RECEIVED A LANDING AIR/GROUND FAIL MESSAGE ON EICAS. THE CREW ELECTED TO RETURN TO CMH AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SWITCH. THE OPERATIONAL CHECK WAS GOOD, REFERENCE EMB AMM 32-63-02. ALSO REMOVED AND REPLACED THE NOSE LANDING GEAR HARNESS, REFERENCE AMM 32-00-03. EXTENSION AND RETRACTION OF LOG SYSTEM REFERENCE EMB AMM 32-30-00. THE HARNESS PART AND SERIAL NUMBERS: P/N 14521495403, S/N NA. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 27,867 hrs · 23,557 cycles

DURING MAINTENANCE BASE VISIT FOUND THE REAR PRESSURE BULKHEAD DENTED/CREASED BEYOND LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED REAR PRESSURE BULKHEAD IAW EO EM-53MR-1438. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — MELTED (CABIN) · airframe 27,863 hrs · 23,550 cycles

DURING PS-1 CHECK FOUND THE CABIN CEILING PANEL 263ALC EMERGENCY LIGHT ASSEMBLY HAD MELTED TO BULB AND CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON CABIN CEILING PANEL 263ALC IAW EMB145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 27,436 hrs · 23,156 cycles

DURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE AFT PRESSURE BULKHEAD HAS A DENT, (AT 4 O’CLOCK POSITION VIEWED FROM INSIDE AFT AVIONICS COMPARTMENT LOOKING AFT). THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED DOUBLER REPAIR TO BULKHEAD IAW AEAI EO-53MR-1438. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DRIVE UNIT — MALFUNCTIONED (TE FLAP) · airframe 26,827 hrs · 22,656 cycles

ON FLIGHT 3962 DURING CRUISE A FLAP FAIL MESSAGE APPEARED AND REMAINED ON EICAS. THE FLAPS FAILED AT 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. THE AIRCRAFT WAS INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN SAFE CONDITION FOR A FERRY FLIGHT. REMOVED AND REPLACED SERVABLE FLAP MOTOR DRIVE IAW EMB 145 AMM 27-53-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (THRUST REVERSER)

AMA - FLT 3861 - FLIGHT CREW REPORTED ENGINE NR 2 THRUST REVERSER HAD FAILED INDICATION ON EICAS DURING APPROACH. REPLACED LOWER OUTBOARD STOW SWITCHES AND BOTH UPPER STOW SWITCHES S/N'S 2374, 2370. (M)

Part: CHARGER — MELTED (FLASHLIGHT)

ORD - FLT 4178 BURNING OR HOT INSULATOR ODOR IN THE VICINITY OF THE FA SEAT NOTED DURING DESCENT INTO ORD. AIRCRAFT LANDED SAFELY NO FURTHER INCIDENTS NOTED. NO EMERGENCY REPORTED. NOTED F/A FLASHLIGHT HOLDER ASSEMBLY DEFORMED. RAI FLASHLIGHT HOLDER. OPS CHECK GOOD. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL BEYOND SRM LIMITS AFT BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER 4.3 INCH BY 2.1 INCH .040 INCH THICK. REPAIR DONE IAW EMB GST-0488/02, EMB145 SRM145/1142, REV 16 51-40-02, 51-40-04, 51-40-06, CPM 51-21-04, 51-21-05 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED BETWEEN FRAME 52 AND 53. FABRICATED AND INSTALLED A TEMPORARY DOUBLER AND TWO SHIMS IAW EMB GST-0154/02 PERMANENT REPAIR BY NEXT C-CHECK IAW GST-0289/02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING OUT. FABRICATED AND INSTALLED A 'U' CHANNEL DOUBLER IAW EMB GST-0130A/02 ITEM 6, GST-0276/02 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY FLOORBEAM 3 INCH AFT OF FRAME 22. REMOVED CORROSION BY BLENDING OUT. FABRICATED AND INSTALLED U-CHANNEL DOUBLER IAW EMB GST-0130A/02 ITEM 6, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND CORROSION BY CUT OUT. FABRICATED AND INSTALLED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS IAW EMB145 SRM 145/1142 CHAPTER 53 REV 16, 53-21-10 AND STANDARD SRM PRACTICES. (M)

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE)

ORD - FLT 4112 - NR 2 ENGINE OIL PRESSURE WENT TO 113 PSI ON TAKEOFF. REMOVED AND REPLACED OIL PRESSURE SWITCH IAW EMB AMM. OPS CHECK GOOD. (M)

Part: VALVE — FAILED (A/C PACK) · airframe 3,821 hrs · 4,174 cycles

ORD - FLT 4101 - PACK VALVES FAILED IN CRUISE. AIRCRAFT WOULD NOT PRESSURIZE. CREW RETURNED TO ORD FOR MTX. MTX RESET POWER AND NO DEFECTS NOTED. OPS CHECKED GOOD. (X)

Part: BULB — FAILED (CABIN)

TOL - FLT 4350 - FIRST AND LAST EMERGENCY OVERHEAD LIGHTS INOPERATIVE. FOUND CANNON PLUG P8635 DISCONNECTED. RECONNECTED SAME. REMVOED AND REPLACED 4 EACH BULBS. OPS CHECK GOOD IAW AMM 33-50-08. (M)

Part: REGULATOR — FAILED (ELEVATOR)

DFW - FLT 3619 - PILOT REPORTED VIBRATION IN CONTROL COLUMN WHEN PASSING THROUGH 24,000 FEET. INSPECTED AND FOUND ELEVATOR TENSION REGULATOR BAD CAUSING CONTROL CABLES TO SLACK AND BECOME FRAYED. REMOVED AND REPLACED ELEVATOR TENSION REGULATOR AND BOTH CONTROL CABLES. OPS CHECK AND FUNCTIONAL CHECK FLIGHT WERE SATISFACTORY AIRCRAFT RETURNED TO SERVICE. (M)

Part: REGULATOR — FAILED (ELEVATOR)

DFW - FLT 3619 - PILOT REPORTED VIBRATION IN CONTROL COLUMN WHEN PASSING THROUGH 24,000 FEET. INSPECTED AND FOUND ELEVATOR TENSION REGULATOR BAD CAUSING CONTROL CABLES TO SLACK AND BECOME FRAYED. REMOVED AND REPLACED ELEVATOR TENSION REGULATOR AND BOTH CONTROL CABLES. OPS CHECK AND FUNCTIONAL CHECK FLIGHT WERE SATISFACTORY AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL CABLE — FRAYED (ELEVATOR)

DFW - FLT 3619 - PILOT REPORTED VIBRATION IN CONTROL COLUMN WHEN PASSING THROUGH 24,000 FEET. INSPECTED AND FOUND ELEVATOR TENSION REGULATOR BAD CAUSING CONTROL CABLES TO SLACK AND BECOME FRAYED. REMOVED AND REPLACED ELEVATOR TENSION REGULATOR AND BOTH CONTROL CABLES. OPS CHECK AND FUNCTIONAL CHECK FLIGHT WERE SATISFACTORY AIRCRAFT RETURNED TO SERVICE. (M)

Part: SOCKET — SHORTED (LIGHT)

SAW - DURING PS-2 INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 1AB TO 9AB. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 3WL, 29WL, 18WL AND 10WL IAW JIC 335121-RAI-10000. OPS CHECK GOOD. (M)

Part: FUSE — BLOWN (CABIN)

DFW - FLT 3756 - FOUND ROW 7 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT SOCKET AND FUSE TO NUMBER 2 EMERGENCY BATTERY PACK. (M)

Part: SMOKE DETECTORS — MALFUNCTIONED (CARGO BAY)

DAY - FLT 4313 - BAGGAGE SMOKE WARNING CAME ON IN-FLIGHT. DEFERRED BAGGAGE SMOKE WARNING SYSTEM PER MEL 26-13. REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTOR SENSORS. OPERATIONAL CHECKED GOOD. MEL CLEARED. REF: OPERATOR CONTROL NR 99ZZZX___. (X)

Part: SMOKE DETECTORS — MALFUNCTIONED (CARGO BAY)

DAY - FLT 4313 - BAGGAGE SMOKE WARNING CAME ON IN-FLIGHT. DEFERRED BAGGAGE SMOKE WARNING SYSTEM PER MEL 26-13. REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTOR SENSORS. OPERATIONAL CHECKED GOOD. MEL CLEARED. REF: OPERATOR CONTROL NR SIMA982855.