N603KC

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHT) · airframe 50,240 hrs · 43,536 cycles

FWD LEFT EMERGENCY LIGHT WAS INOPERATIVE, EXTERIOR. R & R THE EMERGENCY BATTERY AND POWER SUPPLY IAW AMM 33-50-04-000/400-801A, OPS CHECKED GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 49,641 hrs · 42,859 cycles

STRONG ELECTRICAL/BURNING SMELL COMING FROM FRONT OF A/C (VERY PROMINANT FROM FWD FA VENT). FOUND BURNT OUT LH SIDE WALL BALLEST. REMOVED AND REPLACED BURNT BALLAST IAW 33-21-03. OPS CHECK GOOD OK FOR SERVICE. INSPECTED LIGHT SOCKETS, NO DEFECTS FOUND IN SUROUNDING AREA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,816 hrs · 41,921 cycles

NR 5 EMERGENCY LIGHT STRIP INOPERATIVE. R & R THE PROXIMITY LIGHT STRIP IAW AMM 33-50-12-400-801-A

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,573 hrs · 41,634 cycles

AIRCRAFT 603 ABORT T/O IN PHL DUE TO MOMENTARY HSV FAIL MESSAGE ON T/O. NO HISTORY. FIX: CREW RECONFIGURED AC AND PERO CHK. ALL SYSTEMS OPS NORM THROUGH STANDARD CREW PROCEDURES.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,414 hrs · 41,448 cycles

PDIS 603 05-50 1851062 30MAY19 CLT CLOSE CREW REPORTS BURNING RUBBER SMELL FROM 80 KTS TO 6000 FEET FACT GROUND RAN AIRCRAFT WITH BLEEDS ON. NO RUBBER SMELL NOTED. SUSPECT ODOR WAS FROM SURROUNDIND AIRCRAFT. OOK FOR SERVICE. 30MAY19 12:20 CLT

Part: TERMINAL BLOCK — BURNED (WINDOW HEAT) · airframe 48,028 hrs · 41,011 cycles

NDIS 603 30-41 0020580 09FEB19 CLT CLOSE PLEASE FOLLOW UP WITH WIND SCREEN HEAT OPS CHECK FOR #2 W/S DUE TO OCCASIONAL OCCURANCES OF FAIL INDICATIONS THEN INSTANTLY CLEARING ITSELF AND OPERATING NORMALLY. DFRL 09FEB19 10:53 CLT PLEASE PERFORM OPS AND FUNCTION CHECK IN AMM 30-42-00-05. DFRL 12FEB19 09:11 SBY PERFORMED OPS CHECK AS REQUIRED. FOUND ZERO VOLTAGE AT PIN B ON WINDSHIELD HEAT CONTROLLER. FOUND BURN MARKS ON TERMINAL BLOCK ON CONTROLLER. REPAIRED PIN B TERMINAL RING REFERENCING SWPM 20-21-00. R&R' D WINDSHIELD HEAT CONTROLLER REFERENCING AMM 30-42-01. COMPLIED WITH HIDDEN DAMAGE INSPECTION P/N ON CONTROLLER 1300126, S/N ON 6019 P/N OFF CONTROLLER 1300126, S/N OFF 711

Part: RELAY — MALFUNCTIONED · airframe 47,966 hrs · 40,942 cycles

PDIS 603 31-50 1983712 01FEB19 PHL CLOSE NO TAKE OFF CONFIG WARNING DURING TAKE OFF. FACT 01FEB19 15:23 PHL T/S IAW EMB FIM 31-51-00-810-804A BLOCK 1. R/R RELAY K0212 IAW EMB AMM 20-13-02/400. OPERATIONAL CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: SOLENOID — FAILED (THRUST REVERSER) · airframe 47,266 hrs · 40,113 cycles

ENG 1 IDLE STOP FAIL AFTER ENGINE START. IDLE STOP SOLENOID.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 47,262 hrs · 40,107 cycles

E1 IDLE STOP FAIL. TROUBLESHOT IN REF TO FIM 76-13-810-801-A PG 210 BLOCK 32. FAILURE OF RELAY K0257. R&R RELAY K0257 IN REF TO AMM 20-13-02-04. OPS CHECK GOOD AT THIS TIME OK FOR SERVICE.

Part: NONE — NONE (FLAPS) · airframe 47,232 hrs · 40,074 cycles

NDIS 603 31-33 0015960 22AUG18 SBY CLOSE MAINTENANCE FOLLOW UP: PREVIOUSLY RECORDED FDR DATA VALIDATED ON 8/23/18 INDICATES THAT A/C EXCEDED THE AIRSPEED/FLAP POSITION OPERAIONAL LIMIT FACT 22AUG18 08:00 SBY PERFORMED EDDY CURRENT INSP. IAW EMB 145. MM 05-50-07. NO DEFECTS NOTED. AND C/W W/C 05-20-06. EXCEEDING FLAP/ DOWN SPEED CONDITION- INSP

Part: STEERING SYS — OUT OF ADJUST (NLG) · airframe 47,094 hrs · 39,899 cycles

DURING TRAXI AND TAKEOFF ROLL AIRCRAFT PULLS TO THE LEFT. PERFORMED NWS SYSTEM QUICK ADJUSTMENT IAW AMM 32-50-00 OPS CHECK GOOD OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,072 hrs · 39,878 cycles

DAU NR 2 SYS MISCMP EICAS MSG ON TAKEOFF. PERFORMED T/S IAW FIM 31-41-00-817-006A BLOCKS 1, 2, 14. FOUND TO BE CONDITION ON IC 1, DAU NR 1 AND NR 2. OPS CHECK GOOD OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,844 hrs · 39,597 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,844 hrs · 39,597 cycles

SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE BULB.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,492 hrs · 39,193 cycles

RIGHT FWD EMERGENCY LIGHT INOPERATIVE. MULTIPLE INTERIOR OVERHEAD AND EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY AND POWER SUPPLY ASSY IAW AMM 33-58-04-400-801-A.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 45,826 hrs · 38,512 cycles

WINDSHIELD HEAT NR 1 FAIL MESSAGE DISPLAYED IN FLT. NOT IN ICING CONDITIONS. R & R THE NR 1 WINDSHIELD HEAT CONTROLLER IAW AMM 30-42-01. OPS CHECKED IAW AMM 30-42-00. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: SPRING — OUT OF ADJUST (WINDSHIELD WIPER) · airframe 45,483 hrs · 38,165 cycles

CAPT'S WINDSHIELD WIPER WILL NOT PARK AND BOUNCES OFF OF WINDSHIELD AT SPEEDS ABOVE 160 KNOTS. ADJUSTED WIPER ARM SPRING TENSION IAW AMM 30-41-03 OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,288 hrs · 37,965 cycles

FLOOR PROXIMITY EMERGENCY LIGHTS AND EXIT DOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE

Part: SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 44,733 hrs · 37,390 cycles

WING ANTI ICE FAIL MESSAGE, ICE CONDITION ANTI ICE WARNING, AND BLEED 1 LEAK EICAS MESSAGES DISPLAYED. RETURNED TO THE FIELD. FOUND BROKEN WIRES TO THE THERMAL SWITCH ON THE NR 1 ANTI ICE VALVE. R & R THE THERMAL SWITCH IAW AMM 36-20-02-400-801-A. PERFORMED AN OPS CHECK IAW AMM 30-00-00-700-803-A, AND 30-00-00-700-802-A. OPS CHECKED GOOD AT THIS TIME. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 44,729 hrs · 37,385 cycles

DURING FLIGHT IN ICING CONDITIONS, AN EICAS MESSAGE FOR THE STAB ANTI-ICE FAILED, FOLLOWED BY A WARNING MESSAGE. GROUND RAN THE ACFT AND PERFORMED AN ANTI ICE VALVE TEST IAW AMMM 30-21-00-700-804-A/500, NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: LINE — CRACKED (ANTI ICE SYSTEM) · airframe 44,726 hrs · 37,378 cycles

EICAS MESSAGE. ANTI-ICE FAILED. DOWNLOAD SHOWED WING ANTI-ICE FAILED MESSAGE.FOUND LEFT WING REFERENCE LINE CRACKED. R & R THE LINE, OPS CHECKED GOOD, OK FOR SERVICE.

Part: ENGINE — UNKNOWN (NR 2) · airframe 44,700 hrs · 37,344 cycles

NR 2 ENGINE FAILED TO START. FIRST START, ENGINE DID NOT REACH 30 N2. SECOND START, ENGINE DID GET TO 30 N2, BUT THEN SHUTDOWN. NO WARNING OR CAUTION MESSAGE. STARTED AIRCRAFT ENGINES SEVERAL TIMES IAW RUN UP CHECKLIST. ENGINES STARTED WITH NO DEFECTS. OK FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (COFFEEMAKER) · airframe 44,528 hrs · 37,139 cycles

DURING CLIMB OUT, FLIGHT ATTENDANT NOTICED FUMES/STEAM FROM GALLEY HOT JUG AND SOCKET. NO DEFECTS NOTED. INSPECTED WIRING FOUND COFFEE RESIDUAL AT CONNECTION. CLEANED CONNECTION. REMOVED AND AND REPLACED 2 O-RING TERMINALS. OPS CHECKED HOT JUG. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: FRAME — CORRODED (FRM 65) · airframe 44,015 hrs · 36,608 cycles

FRAME 65 IS CORRODED ABOVE CARGO DOOR GUIDE PLATE. REPAIRED THE FRAME IAW SRM 53-31-04, FIGURE 212.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,015 hrs · 36,608 cycles

GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK ASSEMBLY IAW AMM 33-50-04.

Part: DOOR SILL — CORRODED (FRAME 65-68) · airframe 44,015 hrs · 36,608 cycles

CARGO LOWER DOOR SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · airframe 44,015 hrs · 36,608 cycles

LEFT CENTER AISLE FLOOR SUPPORT CORRODED BETWEEN FRAMES 58-59. R & R THE FLOOR SUPPORT IAW SRM 51-20-03, AND 51-40-02/06.

Part: BRACKET — CORRODED (FRAME 66) · airframe 44,015 hrs · 36,608 cycles

TEE BRACKET AT FRAME 66 UNDER CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL TEE BRACKET IAW SRM 51-40-02, 51-20-03

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 44,015 hrs · 36,608 cycles

FRAME 65 SHEAR TIE CORRODED. REPAIRED THE SHEAR TIE IAW SRM 53-31-04, FIGURE 213.

Part: BRACKET — CORRODED (FRAME 68) · airframe 44,015 hrs · 36,608 cycles

CARGO DOOR LOWER SILL TEE BRACKET AT FRAME 68 IS CORRODED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, AND 51-20-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,014 hrs · 36,607 cycles

EMERGENCY LIGHT AT 253CLC BEHIND THE EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,014 hrs · 36,607 cycles

EMERGENCY LIGHTS IN GALLEY AREA INOPERATIVE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 43,881 hrs · 36,474 cycles

FORWARD F/A FLASHLIGHT NOT CHARGING. R & R FOWARD F/A FLASHLIGHT IAW AMM 33-50-16.

Part: VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 43,831 hrs · 36,420 cycles

IN FLIGHT, ACFT PRESSURIZATION WOULD NOT STOP CLIMBING. CABIN WHENT AS HIGH AS 10,000 FT. AUTO MODE WAS CLIMMING AT 1,000 FT + MIN AND WOULD NOT STOP. AUTO MODE AND MANUAL MODES VIRTUALLY UNRESPONSIVE. R & R GROUND CONNECTION VALVE AND SEAL IAW AMM 21-22-04. OPS CHECKED GOOD

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,781 hrs · 35,519 cycles

LEFT EXTERIOR FWD OVERWING EMER LIGHT INOPERATIVE. R & R LT EXTERIOR FWD OVERWING EMER LIGHT BULB IAW AMM 33-50-10, NO FIX. R & R ASSEMBLY IAW AMM 33-50-10, NO FIX. R & R NR 1 EMER BATTERY 33-50-04-000-802-A & 33-50-04-400-802-A, BATTERY CHARGER IAW AMM 33-50-04-000-801-A & 33-50-04-400-801-A. PERFORMED OPERATIONS CHECK IAW 33-50-00-700-801-A. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 13559.

Part: ACTUATOR — FAILED (LT SPOILER) · airframe 42,748 hrs · 35,486 cycles

LEFT SPOILER NOT STOWING PROPERLY, IT LAGS BY = 5 SEC, SPOILER LEVER DISAGREE MSG. ACFT YAWED DRASTICALLY TO LT AS WE RECEIVED SPOILER LEVER DISAGREE MSG. R & R LT SPEED BRAKE ACTUATOR IAW AMM 27-62-02. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 42,700 hrs · 35,446 cycles

RIGHT UPPER WING SKIN CRACKED AT GND SPOILER, CTR HINGE CUT OUT, 1.17 INCHES LONG. TRANSFERRED TO NRWC 603 MQT 02576. REPAIRED AREA IAW ERS-EM-57MR-569.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,700 hrs · 35,446 cycles

LEFT FWD FAIRING, NR 1 CEILING & MAIN DOOR EMER LIGHTS INOPERATIVE. R & R NR 1 BATTERY & POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A, SN 104542.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,646 hrs · 35,390 cycles

TWO STRIPS, CAPTAINS SIDE, EMER LIGHT INOPERATIVE ABOUT MIDWAY IN CABIN. OPERATIONS CHECK OF EMER LIGHTS IAW AMM 33-50-12, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,115 hrs · 34,894 cycles

MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,115 hrs · 34,894 cycles

LEFT FWD WING EXTERIOR EMER LIGHT INOPERATIVE. R & R LT FWD WING EXTERIOR EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 41,965 hrs · 34,770 cycles

RIGHT WING EMER LIGHT INOPERATIVE. R & R RT WING EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 41,848 hrs · 34,689 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. REPLACED RT OVERWING EMER LIGHT LAMP IAW AMM TASKS 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,657 hrs · 34,510 cycles

LEFT EXTERIOR FORWARD EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB FOR LEFT EXTERIOR FORWARD EMERGENCY LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,896 hrs · 33,831 cycles

OVERWING LT AFT EMER LIGHT INOPERATIVE. R & R LT EXTERNAL EMER LIGHT LAMP ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD LT & RT EXTERNAL EMER LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,896 hrs · 33,831 cycles

AFT OVERWING EMER LIGHT INOPERATIVE AT LOWER HAND. R & R BATTERY PACK & POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECK FAILED, SEE NRWC 603-DFW-02208. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 & SN C01494.

Part: EPSU — INOPERATIVE (CABIN) · airframe 40,843 hrs · 33,794 cycles

AFT OVERWING EMER LIGHTS OVER BOTH WINGS INOPERATIVE. R & R NR 4 EPSU. OPERATIONS CHECKED GOOD IAW WC 33-700-19. BATTERY CHARGER ASSEMBLY PN 11-0049, SN 12711.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,767 hrs · 33,732 cycles

OPERATIONS REPORTED TO MOC, ELEC BURNING SMELL IN THE GALLEY. NOTE, ACFT ONLY ON GND POWER. ACFT CONFIGURED THE SAME AS WHEN OPERATIONS NOTICED SMELL & ODOR. INVESTIGATED GALLEY & SURROUNDING AREA FOR ODOR, NO EVIDENCE OF COMPONENTS EMANATING BURNING SMELL. NO DEFECTS OR ODOR PRESENT DURING GVI.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,698 hrs · 33,666 cycles

LEFT & RIGHT OVERWING EXTERIOR EMER LIGHTS INOPERATIVE. R & R NR 4 EMER BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 SN C00952.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,528 hrs · 33,529 cycles

LEFT EXT OVERWING EMER LIGHT INOPERATIVE. R & R LT EXT OVERWING EMER LIGHT LAMPS IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, NO FIX. TROUBLE SHOT & FOUND NR 4 BATTERY POWER SUPPLY TO BE BAD. R & R IAW WC 33-700-19. OPERATIONS CHECK & FUNCTIONAL CHECK GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 19174.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,500 hrs · 33,510 cycles

BOTH AFT OUTSIDE EMER LIGHTS INOPERATIVE. R & R BATTERY POWER SUPPLY 4 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A SN 104600.

Part: POTENTIOMETER — FAILED (NLG STEERING) · airframe 40,429 hrs · 33,450 cycles

ON LANDING ACFT PULLED HARD TO RIGHT, DID NOT TOUCH TILLER, APPLIED 3/4 FULL LEFT RUDDER PEDAL & BRAKE, ACFT WENT STRAIGHT AT THAT POINT. THEN CAME FULL LEFT RUDDER PEDAL AT APPROX 60KTS TAKING HIGH SPEED. ACFT RESPONDED FINE BUT SEEMED SLUGGISH. TAXI WITH TILLER RESPONDED NORMAL AT LOW TAXI SPEED. WHILE SITTING ON TAXI WAY WAITING ON GATE STEERING INOPERATIVE, APPEARED ON EICAS CAUTION. R & R FEEDBACK POTENTIOMETER IAW AMM 32-50-07. STEERING OPERATIONS CHECKED GOOD IAW AMM 32-50-00.

Part: RADIO ALTIMETER — DEFECTIVE · airframe 40,293 hrs · 33,311 cycles

DURING DESCENT OUT OF 14,000 FT AURAL WARNING FOR LG. CONTINUED EVERY TIME THRUST REDUCED FOR DESCENT. R & R RADAR ALTIMETER IAW AMM 34-31-00. REF ITEM NR 2 BELOW FOR OPERATIONS CHECK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,265 hrs · 33,274 cycles

RIGHT AFT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R RT AFT EXTERNAL OVERWING EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-000-801-A. OPERATIONS CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

DURING MBV INSPECTION, QA FOUND THE FUSELAGE SKIN GOUGED INSIDE LT PYLON BETWEEN PANELS 414CB & 414DB. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON THE FUSELAGE SKIN GOUGE INSIDE LT PYLON BETWEEN PANELS 414CB & 414DB IAW ERS-EM-53MR-926. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIR MATERIALS, DOUBLER 2024T3 .063, ANGLE 2024T3 .063, FILLER 2024T3 .063, SHIM 2024T3 .063, BUSHING PN EPNEM53EP1489-01.

Part: SPAR — CRACKED (RT WING) · airframe 40,173 hrs · 33,191 cycles

DURING MBV INSPECTION, QC FOUND RT SPAR III CRACKED AT THE HARNESS CUT OUT. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON RT SPAR III IAW ERS-EM-57MR-330. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIR DOUBLER PART NR EPNEM57EP702.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

DURING MBV INSPECTION, QA FOUND FRAME 68 UPPER SECTION CORRODED AROUND NUTPLATE HOLES. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON FRAME 68 UPPER SECTION DAMAGE AT NUTPLATE HOLES IAW EO-EM-53MR-887R1. REPAIR MATERIAL 2024T3 .040. FRAME PN 145-64141-001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

DURING MBV INSPECTION, QA FOUND RT UPPER FUSELAGE SKIN WITH 3 CRACKS AT FRAME 75 BETWEEN STRINGERS 1R & 3R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN AT FRAME 75 BETWEEN STRINGERS 1R & 3R IAW ERS-EM-53MR-923. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIR MATERIALS, FILLER 2024T3 .063, REPAIR DOUBLER, 2024T3 .080, REPAIR ANGLE 2024T3 .063, ANGLE FILLER 2024T3 .032.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

DURING MBV INSPECTION, QA FOUND LT UPPER FUSELAGE SKIN WITH 2 CRACKS AT FRAME 75 BETWEEN STRINGERS 1L & 3L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN AT FRAME 75 BETWEEN STRINGERS 1L & 3L IAW ERS-EM-53MR-924. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. (REPAIR MATERIALS, FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .063, ANGLE FILLER 2024T3 .032.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

FUSELAGE SKIN CRACKED AT FRAME 75 FASTENER JUST BELOW STRINGER 2R. CRACK IS APPROX 1/4 INCH IN LENGTH. CRACK END IS MARKED. EASI 8071 USED, 400 KHZ, LPF 100, V-GAIN=76, H-GAIN=64, 50-500 KHZ PROBE. DO NOT STRIP FOR NDT. PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN CRACK AT FRAME 75 FASTENER JUST BELOW STRINGER 2R IAW ERS-EM-53MR-923. SEE TURNOVER FOR DETAILS.

Part: CONNECTOR — BROKEN (CABIN) · airframe 40,173 hrs · 33,191 cycles

EMERGENCY LIGHT STRIP NR 7 HAS A BROKEN CONNECTOR, CABIN SIDE. REPAIRED CONNECTOR FOR EMER LIGHT STRIP NR 7, CABIN SIDE, IAW SWPM 20-00-03.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 40,173 hrs · 33,191 cycles

CARGO DOOR SKIN DENT APPROX 11 INCHES AFT OF LE & 13 INCHES BELOW TOP EDGE FOUND TO HAVE CRACK, CRACK IS APPROX 1/8 INCHES IN LENGTH. REPAIRED CARGO DOOR SKIN DENT & CRACK IAW ERS-EM-5200-250.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

LEFT EXTERNAL FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 78. REPAIRED LT EXTERNAL FUSELAGE SKIN AROUND 2 RIVETS AT FRAME 78 IAW ERS-EM-5300-878. SEE TURNOVER FOR DETAILS.

Part: MOUNT — BROKEN (FLASHLIGHT) · airframe 40,173 hrs · 33,191 cycles

GALLEY FLIGHT ATTENDANT FLASHLIGHT MOUNT IS BROKEN. R & R GALLEY FLIGHT ATTENDANT FLASHLIGHT BASE IAW AMM 33-50-16. OPERATIONAL CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 40,173 hrs · 33,191 cycles

EMERGENCY PROX LIGHT STRIPS 2, 3, 7 & 8 HAVE BROKEN WIRES. R & R EMER LIGHT STRIPS 2, 3, 7 & 8 IAW AMM 33-50-12. SEE NRTC BOW 170665 FOR FINAL INSTALL & OPERATIONS CHECKS.

Part: SUPPORT — CRACKED (NLG WW) · airframe 40,173 hrs · 33,191 cycles

NLG BAY HYD HOSE SUPPORT STIFFENER CRACKED. ACCOMPLISHED TEMP REPAIR ON NLG BAY HYD HOSE SUPPORT IAW ERS-EM-53DF-922 PART A. SEE NRTC E418232 FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

RIGHT EXTERNAL FUSELAGE SKIN CRACKED AROUND 4 RIVETS FRAME 79. REPAIRED RT EXTERNAL FUSELAGE SKIN CRACKED AROUND 4 RIVETS FRAME 79 IAW ERS-EM-5300-877. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

LEFT EXTERNAL FUSELAGE SKIN CRACKED AROUND 3 RIVETS FRAME 79. REPAIRED LT EXTERNAL FUSELAGE SKIN AROUND 3 RIVETS AT FRAME 79 IAW ERS-EM-5300-878. SEE TURNOVER FOR DETAILS.

Part: PANEL — CRACKED (CABIN) · airframe 40,173 hrs · 33,191 cycles

EMERGENCY PROX LIGHT STRIP PANEL NR 6 IS CRACKED. R & R EMER PROX LIGHT STRIP PANEL 6 IAW AMM 33-50-12. SEE NRTC BOW 170665 FOR FINAL INSTALL.

Part: PANEL — CRACKED (CABIN) · airframe 40,173 hrs · 33,191 cycles

EMERGENCY PROX LIGHT STRIP PANELS 1, 2 & 5 ARE CRACKED. R & R EMER PROX LIGHT STRIP PANELS 1, 2 & 5 IAW AMM 33-50-12. SEE NRTC BOW 170665 FOR FINAL INSTALL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,173 hrs · 33,191 cycles

FUSELAGE SKIN CRACKED AT FRAME 75 FASTENER JUST BELOW STRINGER 2L. CRACK IS APPROX 1/4 INCHES IN LENGTH. CRACK END IS MARKED. EASI 8071 USED, 400 KHZ, LPF 100, V-GAIN=76, H-GAIN=64, 50-500 KHZ PROBE. DO NOT STRIP FOR NDT. SEE NRWC E417618 FOR REPAIR OF AREA. PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L IAW ERS-EM-53MR-924. SEE TURNOVER FOR DETAILS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,813 hrs · 32,928 cycles

RIGHT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SUPPORT BRACKET — CRACKED (LT ENGINE) · airframe 39,684 hrs · 32,825 cycles

DURING GVI OF PYLON AREA FOR LT ENG CHANGE, FOUND DAMPENER SUPPORT CRACKED. R & R LT ENG HYD DAMPENER SUPPORT BRACKET WITH SERVICEABLE UNIT IAW MM CH 29-10-20.

Part: TEE FITTING — CRACKED (BLEED AIR SYS) · airframe 39,668 hrs · 32,807 cycles

BLEED 1 LEAK INFLIGHT. TRANSFERRED TO NRWC 603-DFW-01980. SEE NRWC 603-DFW-01980 FOR WORK PERFORMED. REPLACED TEE DUCT ASSEMBLY IN CARGO, NO LEAKS NOTED. INSPECTED & FOUND TEE FITTING IN CARGO ON LT UPPER BLEED DUCTS CRACKED. REMOVED TEE FITTING IAW AMM 36-11-09.

Part: VALVE — FAULTY (RIGHT) · airframe 39,565 hrs · 32,729 cycles

ABNORMAL VIBRATION & NOISE FROM NOSE WHEEL. POOR CLIMB PERFORMANCE. TRANSFERRED TO NRWC 603-DFW-01952. COMPLIED WITH DETAIL VISUAL INSPECTION FOR VIBRATION IAW WC 12-200-01. SEE NRWC 603-DFW-01946 & 603-DFW-01945 FOR FINDINGS. INSTALLED NEW PANEL 327BL & 327CL IAW AMM 52-40-04. R & R RT RAM AIR VLV IAW AMM 21-25-01. OPERATIONS CHECKED GOOD AT THIS TIME. ACFT WILL BE RELEASED FOR FUNCTIONAL CHECK FLIGHT IAW NRWC 603-DFW-01952. COMPLETED WC 12-200-01. FUNCTIONAL CHECK FLIGHT FOUND SATISFACTORY.

Part: SENSOR — FAULTY (BRAKE SYSTEM) · airframe 39,522 hrs · 32,693 cycles

ON GEAR RETRACTION BRAKE OVERHEAT MSG ON EICAS. LT OTBD SHOW TOP OF YELLOW. USING DIGITAL THERMOMETER FOUND TEMP OK. R & R NR 1 BRAKE TEMP SENSOR. OPERATIONS CHECKED GOOD IAW AMM 32-47-01.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 39,226 hrs · 32,448 cycles

FLASHLIGHT HOLDER ON CAPTAINS SIDE IS BROKEN. R & R CAPTAINS SIDE FLASHLIGHT ASSEMBLY IAW EMB 33-50-16. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 38,747 hrs · 32,084 cycles

IAS MSG ON BOTH CAPTAIN & FIRST OFFICER AIRSPEED, PERFORMED A CHECKLIST & CAPTAIN`S WAS CORRECT. FOUND WATER IN PITOT LINES & DRAINED IAW AMM 34-13-00. PERFORMED OPERATIONAL CHECK OF PITOT STATIC SYS IAW AMM 34-13-00.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 38,321 hrs · 31,696 cycles

FORWARD PART OF FLASHLIGHT MOUNT ON FIRST OFFICER SIDE BROKEN OFF. ACFT WAS REMOVED FROM SERVICE. R & R FIRST OFFICER'S FLASHLIGHT HOLDER IAW AMM 33-50-16, OPERATIONS CHECKED GOOD & MEL ITEM RESTORED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,292 hrs · 31,670 cycles

PERFORMED PERMANENT REPAIR OF CTR FUSELAGE 1 SKIN REPAIR IAW PT C OF EO EM 53MR-2094.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 38,253 hrs · 31,643 cycles

EMERGENCY LIGHT OF PAX DOOR IS INOPERATIVE. R & R EMERGENCY LIGHT BULB FOR PAX DOOR IAW MM 33-50-06, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 37,274 hrs · 30,844 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,025 hrs · 30,611 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,508 hrs · 30,122 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 36,347 hrs · 29,992 cycles

ON FLIGHT 4046 CREW REPORTED WHILE CRUISING AT FLIGHT LEVEL 330 60 MILES WEST OF BUFFALO THEY RECEIVED AN EICAS BAGGAGE SMOKE MESSAGE AND MASTER WARNING LIGHT. THE CREW COMPLIED WITH MEMORY ITEMS, EPC AND AOM VOL 1 CHECKLIST AND DECLARED AN EMERGENCY. DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. CRASH, FIRE AND RESCUE INSPECTED THE AIRCRAFT AND FOUND NO VISIBLE OR THERMAL EVIDENCE OF A FIRE. AIRCRAFT WAS REMOVED FROM SERVICE. R&R THE HIGH RATE BOTTLE AND METERING BOTTLE FOR BAGGAGE COMPARTMENT IAW AMM 26-23-04. FIRE X BOTTLE-630 CU. INCH PART NUMBER 346000731. SN 34267F1. FIRE X BOTTLE-224 CU. INCH PART NUMBER 337000271. SN 44332D1. THE OPERATIONAL CHECK WAS GOOD FOR THE BAGGAGE SMOKE DETECTION SYSTEM. THE OPERATIONAL CHECK WAS GOOD IAW AMM 26-15-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (OVERWING EXIT) · airframe 36,206 hrs · 29,867 cycles

DURING PS1 CHECK FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BULB LOOSE IN SOCKET. RESECURED BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,161 hrs · 29,821 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,161 hrs · 29,821 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 145 AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,161 hrs · 29,821 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT IAW EMB 145 AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — DAMAGED (CABIN AIR) · airframe 36,121 hrs · 29,788 cycles

FLIGHT 3577, NR 1 ENGINE BLEED LEAK WHILE CLIMBING THRU 1000 FT. DECLARED AN EMERGENCY AND FOLLOWED AOM EMERGENCY PROCEDURES. INDICATION EXTINGUISHED 2.5 MINTUES AFTER BLEED VALVE WAS CLOSED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HORIZITAL DUCT ASSEMBLY ON LT AFT CARGO WALL IAW MM 36-11-09. PERFORMED OPS IAW MM 36-00-00 700-803-A . OPS CHECKED GOOD. NO LEAKS FOUND ON BLEED SYSTEM. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (ANTI-ICE SYS) · airframe 36,068 hrs · 29,745 cycles

ON FLIGHT 3947 THE CREW REPORTED THAT DURING THE CLIMB AT AROUND FL 180 ANTIICE CAME ON. SHORTLY AFTER WING A-ICE FAIL MESSAGE CAME ON. THE CREW FOLLOWED AOM VOL 1 PROCEDURES. THE MESSAGE EXTINGUISHED BUT CAME BACK. BLEED ONE LOW TEMP MESSAGE ALSO CAME ON WITH CLIMB POWER SELECTED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT PICCOLO PRESSURE DROP SWITCH IAW AMM 30-11-04. LEAK CHECKED GOOD. THE OPERATIONAL CHECK WAS GOOD IAW 30-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 35,916 hrs · 29,615 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,884 hrs · 29,590 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 65 GOUGED BETWEEN STR 12R AND 13R. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR IAW AEAEO EM-53MR-2084. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,884 hrs · 29,590 cycles

DURING MAINTENANCE INSPECTION FOUND EVIDENCE OF CORROSION ON THE CARGO RAMP PANEL SUPPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EM-53MR-2085. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,884 hrs · 29,590 cycles

DURING MAINTENANCE INSPECTION FOUND WIDESPREAD CORROSION ON CENTER FUSELAGE INNER AND OUTER SKIN FROM SKIN SPLICE BETWEEN FR 14-14, STR19L-18R TO FR 19 BETWEEN STR 21R - 21L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED FORWARD SECTION OF CENTER FUSELAGE SKIN. FABRICATED, PREPPED AND INSTALLED SKIN IAW EO EM-53MR-2094 PTA. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 35,885 hrs · 29,590 cycles

RT RIB 5 CRACKED. R & R WITH NEW SERVICABLE RIB IAW AEM EO EM-57MR-595.

Part: WIRE — BROKEN (CABIN) · airframe 35,946 hrs · 29,638 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT SEAT 14 HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE EMERGENCY LIGHT STRIP AT SEAT 14. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 35,946 hrs · 29,638 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT SEAT 7 HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE EMERGENCY LIGHT STRIP AT SEAT 7. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 35,946 hrs · 29,638 cycles

DURING B INSPECTION FOUND THE LEFT NR 5 PROXIMITY LIGHT STRIP HAS A BROKEN WIRE AT THE BASE OF LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — DAMAGED (EMERGENCY EXIT) · airframe 35,945 hrs · 29,637 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT SEAL DAMAGED ALONG IT’S LOWER EDGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT SEAL ALONG LOWER EDGE IAW EMB 145 AMM 52-00-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,885 hrs · 29,590 cycles

STRINGER 18R CORRODED BETWEEN FR 13-FR 14. REMOVED STRINGER, REPAIRED IAW EO EM-53MR-2094, PART A.

Part: PIN — CORRODED (EMERGENCY EXIT) · airframe 35,946 hrs · 29,638 cycles

DURING B INSPECTION FOUND THE RIGHT EMERGENCY EXIT DOOR, AFTER COMPLYING WITH NRTC E280705, (CORROSION ON GUIDE PIN), EXCESSIVE PITTING WAS FOUND ON FORWARD PIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GUIDE PIN ON THE RIGHT EMERGENCY EXIT DOOR IAW EMB 145 AMM 52-21-00 STEP 3.I.(3) TO (6) AND (13). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 35,946 hrs · 29,638 cycles

DURING B INSPECTION FOUND THE LEFT PROXIMITY FLOOR LIGHT PROXIMITY FLOOR LIGHT SIDEWALL ASSEMBLIES CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1, 4 AND 6 PROXIMITY FLOOR LIGHT SIDEWALL ASSEMBLIES IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER SPLICE — CORRODED (18 RT) · airframe 35,885 hrs · 29,590 cycles

STRINGER SPLICE 18R CORRODED BETWEEN FRAMES 13-14. REMOVED STRINGER SPLICE, FABRICATED, PREPPED AND INSTALLED SERVICEABLE SPLICE AND SHIM IAW EO EM-53MR-2094 PART A AND SRM 51-40-02.

Part: RIB — CRACKED (LT WING) · airframe 35,885 hrs · 29,590 cycles

THE LT WING RIB 5 IS CRACKED. R & R WITH NEW SERVICABLE RIB IAW AEM EO EM-57MR-594.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,529 hrs · 29,325 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT LIGHT BULB INOPERABLE ON THE PASSENGER ENTRY COURTESY LIGHT UNIT. THE OPERATIONAL CHECK COURTESY LIGHT IAW AMM 33-26-00 CHECK WAS GOOD. THE EMERGENCY LIGHT ON THE COURTESY LIGHT ASSEMBLY WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW AMM 33-26-04. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-26-00 AND 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — UNSERVICEABLE (AFT CEILING) · airframe 34,673 hrs · 28,654 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,230 hrs · 34,230 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ON SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 34,166 hrs · 28,275 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT BATTERY BAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BATTERY USING GENERAL KNOWLEDGE. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,015 hrs · 28,150 cycles

DURING B INSPECTION, FOUND THE RIGHT FORWARD WING EXTERIOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD WING EXTERIOR EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,514 hrs · 27,778 cycles

DURING PS-2 FOUND THE RIGHT FORWARD EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD EMERGENCY BULB IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,010 hrs · 27,357 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FURTHERMOST AFT CABIN CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IN AFT CABIN CEILING EMERGENCY LT IAW EMB 145 AMM 33-50-08-000-801-A/33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,792 hrs · 27,192 cycles

NR 4 EMERGENCY LIGHT STRIP INOP. DURING ROUTINE INSPECTION CHECK. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT STRIP. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,318 hrs · 26,859 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED LEFT WING EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,137 hrs · 26,420 cycles

ON FLIGHT 4165 THE CREW REPORTED THE LEFT AFT EXTERNAL OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT EXTERNAL OVERWING LIGHT BULB IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUIDE — DEFECTIVE (CABIN DOOR) · airframe 31,778 hrs · 26,461 cycles

ON FLIGHT 3374 THE FLIGHT ATTENDANT REPORTED THAT SHE COULD NOT SHUT THE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE UPPER AFT MAIN DOOR TEFLON GUIDE IAW EMB 145 AMM 53-21-06. PERFORMED OPERATIONAL CHECK IAW EMB 145 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CONTAMINATED (CABIN)

HOT ELECTRICAL ODOR IN CABIN. MTX HELD BOARDING. FOUND COFFEE SPLASHED ON LIGHTING AT SEAT 3A THAT HAD COOKED ON AND WAS RELEASING ODOR.

Part: CONTACTOR — BURNED (LANDING LIGHT) · airframe 31,320 hrs · 26,090 cycles

ON FLIGHT 4076 THE CREW REPORTED AN ELECTRICAL ODOR IN THE COCKPIT ON LANDING. THE CREW DID NOT DECLARE AN EMERGENCY. THE AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ODOR COMING FROM THE LEFT ELECTRICAL POWER CONTROL/DISTRIBUTION BOX. REMOVED AND REPLACED THE LANDING LIGHT 1 CONTACTOR IAW EMB145 AMM 33-41-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OUTBOARD SEAT TRACK SUPPORT BETWEEN FRAMES 42-48 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK SUPPORT BETWEEN FRAMES 42 AND 48 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OUTBOARD SEAT TRACK SUPPORT BETWEEN FRAMES 48-52 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK SUPPORT IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT CARGO FRAME 64 TO BE GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO FRAME 64 IAW EO EM-53MR-1818. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CHAFED (LT WING) · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT INTERNAL WING RIB 21 JUST OUTBOARD OF PCA CHAFED FROM PCA HOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WING RIB 21 IAW EO EM-57MR-546. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,228 hrs · 26,013 cycles

DURING MANTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 34 AND 35. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM AT FRAMES 34-35 IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 29 CARBON CROSSBEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 29 IAW EO EM-53MR-1812. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB-51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,228 hrs · 26,013 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 44 CARBON CROSSBEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH REPAIR OF THE LEFT OMEGA BEAM IAW EO-EM-53MR-1816. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PITOT SYSTEM — CONTAMINATED · airframe 31,166 hrs · 25,957 cycles

ON FLIGHT 2817 THE CREW REPORTED DURING CRUISE IN HEAVY RAIN, AIRSPEEDS VARIED BY 10-20 KTS ALONG WITH A 'SPS ADVANCED 'CAUTION MESSAGE. DURING DESCENT THROUGH 33000 THE CAPTAIN AND FIRST OFFICER’S AIRSPEED BEGAN RAPIDLY SLOWING THROUGH 160 KNOTS, AS STANDBY SHOWED 270 KNOTS. THE CAPTAIN AND FIRST OFFICER’S ALTIMETERS SHOWED DIVERGING INDICATIONS AND RECEIVED ' I/C WOW ' CAUTION AND AUTOPILOT DISCONNECTED EVERYTHING APPEARED TO STABILIZE AROUND 15000. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO SPS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. DRAINED WATER FROM PITOT SYSTEM DRAIN AND PERFORMED PITOT SYSTEM TEST AND LEAK CHECK WITH NO DEFECTS NOTED IAW AMM CH 34-13-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GENERATOR — INOPERATIVE (NR 3) · airframe 31,151 hrs · 25,950 cycles

ON FLIGHT 2765 THE CREW REPORTED THE TAKEOFF WAS PERFORMED WITH THE AUXILIARY POWER UNIT ON. AFTER TAKEOFF THE AUXILIARY POWER UNIT WAS SHUT DOWN AND GEN 3 WENT OFF BUS GEN 3 RESET THEN WENT OFF BUSS AGAIN. THE CREW ELECTED TO RETURN TO DFW. THE NR 3 MAIN TIRE WAS MISSING ABOUT HALF OF TREAD DAMAGE MAY HAVE OCCURED ON LANDING AT DFW. THE NR 3 RIGHT INBOARD FLAP WAS DAMAGED FROM TREAD SEPERATION FROM NR 3 TIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 GEN IAW EMB 145 AMM 24-31-01 AND WC 24-800-00. REMOVED AND REPLACED THE RIGHT INBOARD FLAP IAW AE WC 27-400-01 THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. REMOVED AND REPLACED THE NR 3 TIRE IAW EMB 145 W/C 32-700-1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 31,034 hrs · 25,869 cycles

ON FLIGHT 3364 THE FLIGHT ATTENDANT REPORTED AN ELECTRIC ODOR NEAR THE HOT JUG MOUNT, NO HOT JUGS INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECT BOTH COFFEE POT RECEPTACLE PLUG, COFFEE POT CONTROL MODULE, ELECTRICAL CONNECTION ABOVE GALLEY, VISUAL CHECK ARE GOOD, NO ELECTRICAL BURNING MARK AT ALL. NO PARTS REMOVE OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,161 hrs · 24,459 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLATE — LACK OF LUBE (CABIN DOOR) · airframe 28,483 hrs · 23,917 cycles

FOR FLIGHT 3427 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN CABIN DOOR STRIKE PLATES IAW 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 26,739 hrs · 22,323 cycles

ON A HMBV INSPECTION FOUND DOUBLER ON LEFT FWD FUSELAGE BETWEEN FRAME 7 AND 8 AND STRINGER 14L AND 15L CORRODED. REMOVED AND REPLACED OLD DOUBLER ON LEFT FWD FUSELAGE BETWEEN FRAME 7 AND 8 AND STRINGER 14L AND 15L. FABRICATED A 6.75 X 8.5 INCHES DOUBLER USING AL2024T3 0.040 INCH AND A 2.5 X 4 INCHES FILLER USING AL2024T3 0.032. CLEANED, PREPPED, ALODINED, PRIMED AND INSTALLED REPAIR IAW EMB SRM 53-10-01 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: WEB — DAMAGED (FUSELAGE) · airframe 26,740 hrs · 22,323 cycles

DISC - DURING IMBV THE SERVICE DOOR CUTOUT LOWER WEB WAS FOUND TO HAVE ELONGATED HOLES. AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGED WEB. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED NEW WEB. (P/N 145-22101-003) IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: WEB — DAMAGED (DOOR FRAME)

DURING AN IMBV THE SERVICE DOOR CUT OUT LWR WEB WAS FOUND TO HAVE ELONGATED HOLES. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE EXACT CAUSE OF DAMAGE. (K)

Part: DOOR FRAME — CORRODED (FUSELAGE)

DURING AN IMBV THE SERVICE DOOR CUT OUT AFT FRAME WAS FOUND TO BE CORRODED. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE EXACT CAUSE OF DAMAGE. (K)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,740 hrs · 22,323 cycles

DURING IMBV THE SERVICE DOOR FRAME WAS FOUND TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED THE CORRODED FRAME. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED NEW FRAME P/N 145-22191-015 IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-40-06 AND EO EM-53MR-1325. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM @ FRAME 20 WAS FOUND CORRODED. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE EXACE CAUSE OF DAMAGE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,739 hrs · 22,323 cycles

DISC - DURING IMBV INSP FOUND CORROSION ON A PREVIOUS REPAIR OF THE LT OMEGA BEAM AT FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW EMB SRM 53-00-10 FIGURE 201. AIRCRAFT RETURNED TO SERVICE.