N633AE

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 47,246 hrs · 44,871 cycles

ON TAKEOFF CLIMB AMBER BAG DOOR OPEN CAUTION MESSAGE CREW HEARD WHISTLING NOISE. BAG DOOR WARNING SYSTEM. SUPPLEMENTAL INFORMATION WILL FOLLOW, CURRENTLY ON THE MEL

Part: WEB — CHAFED (CARGO DOOR) · airframe 46,245 hrs · 43,726 cycles

BAGGAGE DOOR LOWER INNER WEB CHAFED BTW VB1-2 AT HB3. COMPLETE: REPAIRED BAGGAGE DOOR LOWER INNER WEB CHAFED BTW VB1-2 AT HB3 IAW PIEDMONT EO1-52-- 20-0067. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED · airframe 46,245 hrs · 43,726 cycles

LAVATORY RH OMEGA BEAM HAS CORROSION COMPLETE: REPAIRED LAVATORY RH OMEGA BEAM CORROSION IAW PIEDMONT EO1-53-20-- 0080. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 46,245 hrs · 43,726 cycles

SHEAR CLIP AT FR 65 STR 15L-18L CORRODED. COMPLETED INSTALL OF THE NEW SHEAR CLIP AT FR 65 STR 15L-18L IAW EMB 145 SRM 53-31-04

Part: FRAME — CORRODED (FRM 22) · airframe 46,245 hrs · 43,726 cycles

SSI 53-20-43 CORROSION ON FRAME 22 BETWEEN STRINGERS 15R -16R PREVIOUS REPAIR AT BLUE PAINT COMPLETE: REPAIRED CORROSION ON FRAME 22 BETWEEN STRINGERS 15R -16R IAW PIEDMONT EO1-53-20-0081. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: FRAME — CRACKED (FRM 66) · airframe 46,245 hrs · 43,726 cycles

FR 66 CRACKED BTW STR 16R-17R. COMPLETE: REMOVED AND REPLACED FR 66 (LOWER FRAME) IAW EMB145 SRM 51-40-02 AND SRM 51-20-- 01. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: FLOOR SUPPORT — CRACKED (FRAME 25) · airframe 46,245 hrs · 43,726 cycles

AFTER REMOVAL OF RH OTBD FLOOR SILL #1 FOUND FR 25 CRACKED AT ATTACHMENT POINT COMPLETE: REPAIRED FR 25 CRACK AT ATTACHMENT POINT IAW PIEDMONT EO1-53-20-0070. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: WEB — CHAFED (CARGO DOOR) · airframe 46,245 hrs · 43,726 cycles

BAGGAGE DOOR LOWER INNER WEB CHAFED BTW FWD LATERAL FRAME AND VB1 AT HB4. COMPLETE: REPAIRED BAGGAGE DOOR LOWER INNER WEB CHAFED BTW FWD LATERAL FRAME AND VB1 AT HB4 IAW PIEDMONT EO1-52-20-0066. SEE TASK AND WIP ENTRIES FOR DETAILS.

Part: SKIN — DENTED (FRAMES 8-9) · airframe 46,245 hrs · 43,726 cycles

DMT 40 - ACCOMPLISH PERMANENT REPAIR OF DENT IN LH FORWARD FUSELAGE NEAR ACCESS DOOR 123BL BETWEEN FR 8 AND 9,SL18L-19L COMPLETE: ACCOMPLISHED PERMANENT REPAIR OF DENT IN LH FORWARD FUSELAGE NEAR ACCESS DOOR 123BL BETWEEN FR 8 AND 9, SL18L-19L IAW PIEDMONT EO1-53-20-0065. SEE TASK AND WIP ENTRIES FOR DETAILS. DMT 40 CLOSED.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 45,972 hrs · 43,419 cycles

E1 REV DISAGREE DURING TAKE-OFF (C/W TAKE 78-31-01-980-801).....FIX: MELD IAW 78-2

Part: RELAY — FAILED (THRUST REVERSER) · airframe 45,957 hrs · 43,401 cycles

ON TAKEOOF, E1 REV DISAGREE MESSAGE ON EICAS....FIX:FOLLOWED FIM TASK 78-34-00-816-003-A. R&RD RLAY K0381 IN REF TO AMM 20-13-02-000/400-801-A.OPS CHECK T/R IN REF TO AMM 78-31-01-700-801-A. NO FUALTS FOUND.OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSERS) · airframe 36,683 hrs · 32,742 cycles

PDIS 633 78-33 1968501 27OCT19 PHL CLOSE E2 REV DIS MSG DISPLAYED ON T/O TODDS HISTORY: NONE FOR E2 (E1 15,24OCT) MEL 27OCT19 08:55 PHL C30007 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES FACT 27OCT19 14:51 PHL RE-ACTIVATED #2 THRUST REVERSER IAW AMM 78-31-01. CL EAR MEL 78-2.. TR OPS CHECK GOOD NO EICAS MSGS PRESENT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,660 hrs · 43,047 cycles

EMERGENCY LIGHT OUT FROM ROW 8 TO 12. FIX: REPLACED EMERGENCY BATTERY #3 IAW FIM TASK 33-50-00-810-804-A AND IAW AMM 33-50-50, AMM 33-50-04. OPS CHK IAW W/C 33-70-17. OK FOR SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (BRAKE SYSTEM) · airframe 45,582 hrs · 42,955 cycles

PDIS 633 31-50 1884491 08SEP19 PHL CLOSE TAKEOFF BRAKES WARNING. MSG COMES UP INTERMITTENTLY WITH THE EMERGENCY BRAKE RELEASED. FACT 08SEP19 13:24 PHL R&R PRES SW (EMRG/PRK BRK) IAW AMM 32-44-07 NO LEAKS NOTED. OPS CK TO CFG GOOD NO ERRONEOUS MSG. OPS CK GOOD OK FOR SERVICE.

Part: UPLOCK SENSOR — MALFUNCTIONED (RT MLG) · airframe 45,391 hrs · 42,750 cycles

RH MLG FLUCTUATING BETWEEN AMBER CROSSHATCHES AND UP ACCOMPANIED BY THUMPING NOISE,OCCURED WHEN GEAR SELECTED UP. R & R THE RH UPPER UPLOCK PROX SENSOR IAW AMM 32-63-01, PERFORMED LANDING GEAR RETRACTION AND EXTENSION, OPS CHECK GOOD OK FOR SERVICE.

Part: UPLOCK SENSOR — OBSTRUCTED (RT MLG) · airframe 45,391 hrs · 42,750 cycles

AFTER TAKEOFF UPON SELECTING GEAR UP,RH MLG, POSITION INDICATION FLUCTUATED BETWEEN AMBER AND GREEN FOLLOWED BY THUMPING NOISE. TAPE REMOVED FROM BOTH RIGHT LANDING GEAR UPLOCK SENSORS

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 44,853 hrs · 42,135 cycles

633 52-30 1942571 23APR19 AGS ASSGN BAG DOOR 'OPEN' EICAS MESS.INDICATION ON TAKEOFF FRO M CLT. LARRYS HISTORY: . MEL 23APR19 15:49 AGS C11320 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING

Part: SWITCH — MALFUNCTIONED (WINDOW HEAT) · airframe 44,580 hrs · 41,818 cycles

PDIS 633 30-41 1292532 02MAR19 PHL CLOSE W/S HEAT 1 FAIL MESSQAGE IN FLIGHT INTERMITTANTLY. 21968 00 DEW FACT 02MAR19 14:25 PHL R/R W/S HEAT 1 SWITCH IAW AMM 20-13-04. OPS CHECK IAW AMM 30-42-00. OPS CHECK GOOD ABOUT 30 TIMES. AIRCRAFT OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 44,463 hrs · 41,686 cycles

WINDSHIELD HEAT 1 FAIL. R&R WINDSHIELD TEMP CONTROLLER NR 1 WINDSHIELD HEATING. OPS CHECK GOOD IAW MM 30-42-00. TASK 30-42-00-700-801-A.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 43,899 hrs · 41,013 cycles

DURING T/O ROLL RUD SYS 2 INOP DISPLAYED ON EICAS AT APPROX 95 KTS. R&R NR 2 RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 43,843 hrs · 40,946 cycles

PDIS 633 21-01 1664333 21SEP18 ERI CLOSE STRONG ELECTRICAL ODER IN CRUISE FLIGHT FOR TEN MINUETS. IN COCKPIT AND FWD CABIN. ODER THEN DISSIPATED. 29917 00 JBU FACT 21SEP18 23:35 ERI INSPECTED COCKPIT AND FWD CABIN AREA FOR POSSIBLE SOURCES OF ODER, NONE FOUND. ACCOMPLISHED FIM TASK 21- 20-00-810-801-A NO DEFECTS NOTED AIRCRAFT OK FOR SERVICE.

Part: SCREW — LOOSE (BLEED VALVE) · airframe 43,197 hrs · 40,206 cycles

NR 1 BLEED VALVE FAILED ON TAKEOFF ROLL. ABORTED TAKE OFF. INSPECTED THE NR 1 ENGINE BLEED VALVE AND FOUND THE LOCK SCREW TO BE LOOSE. TIGHTENED THE LOCK SCREW. PERFORMED AN ENGINE BLEED VALVE FUNCTIONAL, OPS CHECKED IAW AMM 36-11-05. FUNCTIONAL/OPS CHECKED GOOD. OK FOR SERVICE.

Part: LOCK SCREW — LOOSE (BLEED VALVE) · airframe 43,197 hrs · 40,206 cycles

NR 1 BLEED VALVE FAILED ON TAKEOFF ROLL. ABORTED THE TAKEOFF. INSPECTED THE NR 1 ENGINE BLEED VALVE AND FOUND THE LOCK SCREW TO BE LOOSE. TIGHTENED THE LOCK SCREW. PERFORMED AN ENGINE BLEED VALVE FUNCTIONAL OPS CHECK IAW AMM 36-11-05. CHECKED GOOD. OK FOR SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 43,172 hrs · 40,175 cycles

MAIN DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. PERFORMED AN EMERGENCY LIGHTS OPS CHECK IAW ERJ145 33-50-00. CHECKED FOR VOLTAGE AT CONNECTORS, VOLTAGE CHECKED GOOD. CLEANED AND RESEATED THE CONNECTORS. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED VALVE) · airframe 43,103 hrs · 40,097 cycles

DURING TAKEOFF ROLL, NR 1 BLEED VALVE FAIL CAUTION AND NR 1 BLEED LEAK WARNING MESSAGES DISPLAYED ON EICAS. PERFORMED AN OPS CHECK OF THE ENGINE BLEED VALVE IAW AMM 36-11-05-700-802-A, OPS CHECKED GOOD, NO DEFECTS NOTED. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,486 hrs · 39,437 cycles

PDIS 633 05-50 1094931 09DEC17 PHL CLOSE DURING CLIMB OUT, ELECTRICAL ODOR IN BOTH FLT DECK A ND CABIN, ENG BLEEDS WERE ON AND APU WAS OFF. WHILE RETURNING TO FIELD SMELL DISIPATED FACT 09DEC17 02:19 PHL PERFORMED OPS CHECK OF ENGINE BLEEDS, NO ODOR FOUND OPS CHECK GOOD. NO EVIDENCE OF ELETRICAL ODOR FOUND MORE IN CABIN OR FLIGHT DECK WITH BLEEDS AND PACKS ON.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 42,189 hrs · 39,137 cycles

ON GROUND, DURING TEST OF THE WING AND STAB ANTI ICE, A FAILED MESSAGE. DISPLAYED CREW CONFIRMED TEST WAS PERFORMED FOR APROXIMATELY 20 SECONDS AND FAILED ON SECOND ATTEMPT. PERFORMED AN OPS CHECK IAW AMM 36-11-05-700-802-A, AND 30-00-00-700-802-A. OPS CHECKED GOOD. NO MESSAGES NOTED. OK FOR SERVICE.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 42,016 hrs · 38,951 cycles

CARGO DOOR ACTUATING HANDLE CUTOUT AFT END CRACKED. PERFORMED A PERMANENT REPAIR IAW ERS-EM-52MR-795.

Part: TRUNNION — CRACKED (RT MLG) · airframe 42,016 hrs · 38,951 cycles

RIGHT AFT UPPER MLG TRUNNION CRACKED. REMOVED AND REPLACED THE TRUNNION IAW ERS-EM-57MR-838

Part: WIRE — BROKEN (CABIN) · airframe 42,016 hrs · 38,951 cycles

NR 3 FLOOR PROXIMITY LIGHT WIRES BROKEN. REPLACED NR 3 FLOOR PROXIMITY LIGHT IAW AMM 33-50-12.

Part: SKIN — SCRATCHED (RUDDER) · airframe 42,016 hrs · 38,951 cycles

RUDDER SCRATCHED ON BOTTOM LT SIDE. ACCOMPLISHED A PERMANENT REPAIR OF THE RUDDER SKIN IAW ERS-EM-55MR-556

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 42,016 hrs · 38,951 cycles

SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 53-21-02, AND 51-20-03

Part: TRUNNION — CRACKED (RT MLG) · airframe 42,016 hrs · 38,951 cycles

RIGHT WING AFT MAIN LANDING GEAR TRUNNION FITTING FOUND CRACKED. COMPLIED WITH ERS EM-57MR-838 RT MLG AFT TRUNNION FITTING REPLACEMENT.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 42,016 hrs · 38,951 cycles

FWD CABIN EMERGENCY FLASHLIGHT INTERMITTENT. REMOVED AND REPLACED FWD CABIN EMERGENCY FLASHLIGHT IAW AMM 33-50-16. LIGHT CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,315 hrs · 36,154 cycles

THE CREW REPORTED THAT THE MAION CABIN DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT SIGN, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (COCKPIT) · airframe 39,288 hrs · 36,100 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE F/A JUMPSEAT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED THE ACFT PERFORMED AN OPS TEST OF THE EMEREGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — MISINSTALLED (SERVICE DOOR) · airframe 38,670 hrs · 35,477 cycles

DURING CRUISE THE SERVICE DOOR SEAL WAS FOUND TO HAVE GAPS WHERE LIGHT WAS VISIBLE AND WAS MAKING A LOUD SQUEALING SOUND. THE AIRCREW DIVERTED AND LANDED SAFELY WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. UPON INSPECTION, MAINTENANCE FOUND THE SEAL TO BE INSTALLED INCORRECTLY. THEY REMOVED AND REINSTALLED THE SERVICE DOOR SEAL IAW AMM 52-43-04. PRESSURIZATION CHECK WAS GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 37,874 hrs · 34,684 cycles

AT FRAME 33 BROKEN WIRE FOR EMER LIGHT STRIP. BROKEN WIRE REPAIRED ON EMER LIGHT STRIP IAW SPWM 20-21-00. SEE NRTC BOW 194910 TASK 1 FOR OPERATIONS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,874 hrs · 34,684 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW ERS-EM-53MR-1413.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,874 hrs · 34,684 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R IAW ERS-EM-53MR-1413.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,874 hrs · 34,684 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK IS APPROX 3/4" IN LENGTH. EASI 8071 USED. FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABOVE STRINGER 2L IAW ERS-EM-53MR-1412. SEE TURNOVER FOR DETAILS.

Part: CONNECTOR — MISSING (CABIN) · airframe 37,872 hrs · 34,683 cycles

LEFT EMER LIGHT STRIP NR 1 WIRE IS MISSING CONNECTOR WHERE IT COMES THROUGH THE FLOORBOARD. INSTALLED SERVICEABLE CONNECTOR ON LT EMER LIGHT STRIP NR 1 WIRE IAW SWPM 20-50-01.

Part: BRACKET — CRACKED (LT PYLON) · airframe 37,872 hrs · 34,683 cycles

LEFT PYLON FWD LOWER YOKE FWD BRACKET IS CRACKED. REMOVED & INSTALLED SERVICEABLE LT PYLON FWD LOWER YOKE IAW EO EM-54MR-386.

Part: WIRE — BROKEN (CABIN) · airframe 37,872 hrs · 34,683 cycles

NUMBER 7 EMER LIGHT STRIP HAS A BROKEN WIRE. REPAIRED WIRE W192-8710-22 ON EMER LIGHT STRIP NR 7 IAW AWPM 20-21-00.

Part: SKIN — GOUGED (PAX DOOR) · airframe 37,874 hrs · 34,684 cycles

REF AML 3806014 TDMI 633T5222 MAIN PAX DOOR GOUGE. PERMANENT REPAIR ERS-EM-52DF-349 REPAIRED PAX DOOR IAW ERS-EM-52MR-373. SEE NRTC E453271 FOR WORK ACCOMPLISHED.

Part: SEALANT — MISSING (FUEL TANK) · airframe 37,872 hrs · 34,683 cycles

EVIDENCE OF FUEL LEAK FWD OF WING BOX, IN CABIN, LT SIDE. APPLIED SEALANT & ANT BIOLOGICAL COATING TO TWO LOCK FASTENERS. MISSING SEALANT IN LT CTR BAY TANK TOP SIDE FWD CTR FIRST TWO FASTENERS. REMOVED OLD SEALANT & APPLIED NEW SEALANT & ANT BIOLOGICAL COATING ON CTR FWD BAY WALL BOLT NUT FASTENER IAW AMM 28-11-00, SRM 51-20-01 & ETN-EM-51-091R5. LEAK CHECKED GOOD.

Part: BRACKET — CRACKED (LT PYLON) · airframe 37,871 hrs · 34,682 cycles

LEFT PYLON FWD LOWER YOKE FWD BRACKET IS CRACKED. REMOVED & INSTALLED SERVICEABLE LT PYLON FWD LOWER YOKE IAW EO EM-54MR-386.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,871 hrs · 34,682 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK IS APPROX 3/4" IN LENGTH. EASI 8071 USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABOVE STRINGER 2L IAW ERS-EM-53MR-1412. SEE TURN OVER FOR DETAILS.

Part: WIRE — BROKEN (CABIN) · airframe 37,871 hrs · 34,682 cycles

EMERGENCY LIGHT STRIP NR 7 ON LT SIDE OF FLOORBOARD 251HF HAS BROKEN WIRE. REPAIRED WIRE W192-8710-22 ON EMER LIGHT STRIP NR 7 IAW SWPM 20-21-00. SEE BOW 192974 FOR OPERATIONS CHECK. CALIBRATED EQUIPMENT USED, CRIMPER SN 611497.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,871 hrs · 34,682 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. EASI 8071 USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R IAW ERS-EM-53MR-1413. SEE TURN OVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,871 hrs · 34,682 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. EASI 8071 USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R IAW ERS-EM-53MR-1413.

Part: WIRE — BROKEN (CABIN) · airframe 37,871 hrs · 34,682 cycles

LEFT NR 1 EMER LIGHT STRIP HAS BROKEN WIRES. R & R LT NR 1 EMER LIGHT STRIP IAW AMM 33-50-12. SEE BOW 192974 FOR FINAL INSTALLATION & OPERATIONAL TEST.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,647 hrs · 34,469 cycles

AFT GALLEY EMER SIGN INOPERATIVE. R & R AFT GALLEY EMER SIGN INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: POST — DEFECTIVE (FUSELAGE) · airframe 37,524 hrs · 34,345 cycles

WHILE COMPLYING WITH EM-53AD-2237, DEFECT FOUND AT LT WINDSHIELD POST TOP AFT RIVET. COMPLIED WITH REPAIR OF LT WINDSHIELD POST IAW EO EM-5300-2232R2.

Part: SENSOR — FAILED (NR 1 ENGINE) · airframe 37,426 hrs · 34,259 cycles

AT ABOUT 10,000 FT DURING CLIMB OUT WE NOTICED NR 1 ENG OIL TEMP WAS APPROX 126? IN THE RED. IT CLIMBED TO 132? & WE REDUCED THRUST. OIL TEMP RETURNED TO THE GREEN RANGE UPON POWER REDUCTION IN THE DESCENT BACK. TROUBLE SHOT IAW FIM TASK 79-37-00. R & R NR 1 ENG OIL TEMP & PRESS SENSOR IAW MM. PERFORMED OPERATIONS TEST OF ENG IAW MM 72-00-00. OPERATIONS TESTED GOOD.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 37,144 hrs · 33,974 cycles

WING ANTI-ICE FAIL & STAB ANTI-ICE FAIL DURING SINGLE BLEED OPERATION IN ICING CONDITION, FOLLOWED BY ICE CONDITION ANTI-ICE INOPERATIVE WARNING. PERFORMED OPERATIONAL TEST IAW MM 30-00-00. OPERATIONS CHECK GOOD. BLEED 1 OVER TEMP WARNING DURING CLIMB, TROUBLE SHOT. R & R FAN AIR VLV IAW AMM 36-11-03. GND OPERATIONS CHECKED GOOD.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 37,121 hrs · 33,936 cycles

AFTER TAKEOFF, AFTER GEAR RETRACTION, LG AIR & GND FAIL, ENG 1 2 REV FAIL AFTER GEAR EXTENSION, ALL MSG EXTINGUISHED BUT ENG POWER DID NOT GO TO TAKEOFF. 1 THRUST SETTING WITH GEAR EXTENSION BLOW 15,000 FT AFTER GEAR EXTENSION, ALL GEAR SYS FUNCTIONED NORMALLY. INSPECTED WIRING & NLG PROXIMITY SWITCH, NO DEFECTS NOTED. COMPLIED WITH ETN EM-32-245. SERVICED NLG STRUT WITH NITROGEN IAW AMM 32-20-01. COMPLIED WITH ELEC CONTROL SYS ADJUSTMENT & TESTED IAW AMM 76-12-00. ALL CHECKS WERE NORMAL. ACFT OK FOR FCF PURPOSES ONLY. SEE ITEM 2 THIS LOG PAGE IAW NRWC 633-ORD-02079. R & R NLG HARNESS W019 & NOSE WOW PROXIMITY SWITCH IAW MM 32-00-03 & MM 32-63-02. ACFT RELEASED FOR FCF PURPOSES ONLY. REF ITEM 4 THIS LOG PAGE FOR FCF INFO.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,969 hrs · 33,800 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW EEL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,678 hrs · 33,579 cycles

FLASHLIGHT ON LAVATORY WALL INOPERATIVE. R & R FLASHLIGHT ASSEMBLY ON LAVATORY WALL IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 35,835 hrs · 32,809 cycles

CAPTAINS FLASHLIGHT EMITTING STRONG BURNT ELEC SMELL. REMOVED CAPTAINS FLASHLIGHT FROM ACFT & DEFERRED IAW MEL 25-53. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL 25-53 RESTORED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,835 hrs · 32,809 cycles

ON APPROACH AT ABOUT 6000 FT COCKPIT CREW & JUMP SEAT NOTICED A STRONG ELEC BURNING SMELL. LAST ABOUT 1 MIN WINDOWS HAD FOGGED UP WITH CONDENSATION INSIDE. PERFORMED INSPECTION & VERIFIED OPERATIONS OF WINDSHIELD, FWD COOLING FANS, RECIRC FANS, PACKS & COCKPIT FLASHLIGHTS. ALL SYS CHECKED NORMAL IAW AML 3579708 ITEM 2.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 35,796 hrs · 32,763 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: HOSE — FAILED (MLG ACTUATOR) · airframe 34,801 hrs · 31,947 cycles

ON FLIGHT 9805, FOUND AFTER TAKEOFF WHEN GEAR SELECTED UP HYD SYS 1 FAIL AIL SYS 1 INOPERATIVE. E1 HYD PUMP FAIL HYD 1 LO QTY LG LEVER DISAGREE, HYD SYS 1 SHOWED QTY ZERO, 100 PSI GEAR RED AMBER RED. ACFT WAS REMOVED FROM SERVICE. R & R NR 2 MLG ACTUATOR HYD HOSES IAW AMM PT 32-33-08. OPERATIONS CHECK LEAK, CHECKED GOOD RII DUE TO GEAR SWING RII LOW 173773.

Part: HYDRAULIC LINE — DEFECTIVE (HYDRAULIC SYS) · airframe 34,801 hrs · 31,946 cycles

AFTER ROTATION CREW WERE UNABLE TO RETRACT GEAR & RECEIVED EICAS HYD 1 FAIL MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY & RETURNED TO SYR WITHOUT INCIDENT. NO STEERING NO OUTBOARD BRAKES NO E1 REV TOWED OFF RUNWAY TO GATE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 HYD EDP PRESSURE LINE IAW EMB 29-10-03 OPS CHECK GOOD REFERENCE ACTION TACKEN ON ITEM 1 LP 3484171.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,582 hrs · 31,784 cycles

AFTER TAKEOFF, CABIN ALTITUDE BEGAN CLIMBING AT +2500 - +3000 FPM. ATTEMPTED MANUAL MODE, INOPERATIVE. PERFORMED A FUNCTIONAL CHECK OF AUTO & MANUAL IAW 21-31-00-700-801A & 21-31-00-700-802A. OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,575 hrs · 31,776 cycles

NO EICAS MESSAGES AUTO PRESSURIZATION FAILED TO KEEP THE CABIN WITHIN LIMITS. MAIN PRESSURIZATION DID NOT FUNCTION. KNOB INEFFECTIVE CABIN STABILIZED AT 9200 FT.

Part: FITTING — GOUGED (LT AILERON) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV, FOUND LT AILERON FITTING GOUGED AND CORRODED ON THE INNER SIDES OF THE ATTACH FITTING. LT AILERON DAMPER FITTING REPLACED IAW EO EM-27MR-112. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (COCKPIT EXTERIOR) · airframe 34,077 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND FUSELAGE SKIN BETWEEN FRAMES 13 TO 14 STRINGERS 18 TO 21R CORRODED. REPAIRED SKIN IAW EO-EM-53MR-2207. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 34,077 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN OIL CANNING. REPAIRED IAW EO EM-55MR-440. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER SPLICE — CORRODED (18 RIGHT) · airframe 34,077 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND STRINGER SPLICE 18R CORRODED, JUST AFT OF FRAME 13. INSTALLED NEW STRINGER SPLICE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND RT SIDE UPPER SHEAR TIE ON FRAME 80 IS CRACKED. INSTALLED SHEAR TIE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (LT OVERWING) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND LT OVERWING PANEL LOWER NUT PLATE FLANGE ANGLE IS CRACKED AT FRAME 47, 0.5 INCH LONG. REMOVED AND REPLACED ANGLE IAW ETN-EM-53-142. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,077 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND AT FRAME 10, SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND LT SIDE UPPER SHEAR TIE ON FRAME 80 CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (RT WING) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND RT WING PANEL LOWER NUT PLATE FLANGE ANGLE FWD OF FRAME 48 IS CRACKED .5 INCH LONG. REMOVED AND REPLACED IAW ETN-EM-53-142. AIRCRAFT RETURNED TO SERVICE.

Part: SPAR — CRACKED (LT WING) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND LT WING SPAR 3 CRACKED AT HARNESS HOLE BETWEEN RIBS 3 AND 4. REPAIRED IAW EO EM-57MR-719 REVISION 1. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND LT UPPER FRAME 10 CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (RT OVERWING) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND RT OVERWING LOWER NUT PLATE FLANGE ANGLE FWD OF FRAME 47 IS CRACKED 0.75 INCH LONG. REMOVED AND REPLACED ANGLE IAW ETN-EM-53-142. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (LT OVERWING) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND LT OVER WING PANEL LOWER NUT PLATE FLANGE ANGLE IS CRACKED AT FRAME 45, 0.6 INCH LONG. REMOVED AND REPLACED ANGLE IAW ETN-EM-53-142 AND SRM 51-20-01. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,077 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND RT OVERWING PANEL LOWER NUT PLATE FLANGE ANGLE BETWEEN FRAMES 44 AND 41 IS CRACKED IN FIVE SPOTS .75 INCH LONG. REPAIRED IAW ETN-EM-53-142, SRM 51-20-01. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION, FOUND CARGO DOOR TORSION SUPPORT CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV FOUND RT OMEGA BEAM OTBD SUPPORT ANGLE CACKED BETWEEN FRAME 47 AND 48. REMOVED AND REPLACED OMEGA BEAM IAW SRM 53-23-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION FOUND LT OMEGA BEAM OTBD SUPPORT ANGLE CRACKED BETWEEN FRAMES 47 AND 48. REMOVED AND REPLACED OMEGA BEAM IAW SRM 53-23-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,078 hrs · 31,363 cycles

DURING HMBV INSPECTION FOUND RT OMEGA BEAM INBD SUPPORT ANGLE CRACKED BETWEEN FRAMES 47 AND 48. REMOVED AND REPLACED THE RIGHT OMEGA BEAM IAW SRM 51-40-02 AND SRM 53-23-02. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 34,077 hrs · 31,363 cycles

LEFT ELEVATOR LOWER SKIN HAS LARGE AREA OF OIL CANNING SKIN BETWEEN STATIONS YH-1898.00 AND YH-2223.00, AFT OF ELEVATOR FRONT SPAR. PERFORMED PERMANENT REPAIR IAW EO EM-55MR-440.

Part: STRUCTURE — DENTED (MAIN PAX DOOR) · airframe 34,078 hrs · 31,363 cycles

MAIN PAX DOOR DENTED. PERFORMED PERMANENT REPAIR IAW EO EM-5200-329.

Part: STRUCTURE — DENTED (MAIN PAX DOOR) · airframe 34,078 hrs · 31,363 cycles

MAIN PAX DOOR DENTED 10 INCHES FROM AFT EDGE 15 INCHES FROM BOTTOM. PERFORMED PERMANENT REPAIR IAW EO EM-5200-329.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,078 hrs · 31,363 cycles

EMERGENCY LIGHT HAS A BROKEN WIRE. R & R FLOOR EMERGENCY LIGHT IAW AMM 33-50-12.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 34,078 hrs · 31,363 cycles

AFT EMERGENCY LIGHT UNDERFLOOR WIRING IS MISSING A CONNECTOR. REPLACED BOTH EMERGENCY LIGHT CONNECTORS IAW SWPM 20-50-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,078 hrs · 31,363 cycles

NR 5 EMERGENCY LIGHT HAS A BROKEN WIRE. NEW EMERGENCY LIGHT INSTALLED IAW AMM 33-50-12.

Part: LIGHT — CRACKED (CABIN) · airframe 34,078 hrs · 31,363 cycles

NR 1 EMERGENCY LIGHT CRACKED. R & R FLOOR EMERGENCY LIGHT IAW AMM 33-50-12.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 33,651 hrs · 31,015 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE WITH RED CHARGE LIGHT ON WHEN IN CHARGER. R & R AFT EMERGENCY FLASHLIGHT ASSY AMM 33-50-16. OP CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,600 hrs · 30,975 cycles

EXIT MARKING SIGN ON FWD RT GALLET INOPERATIVE. R & R EXIT MARKING SIGN ON RT GALLERY IAW AMM 33-50-14. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,324 hrs · 30,746 cycles

DURING B INSPECTION, FOUND THE LT EMERGENCY LIGHT INOPERABLE ABOVE L/E ( EXTERIOR FWD BULB). R & R NR 1 EMERGENCY BATTERY AND POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD. MEL RESTORED. PLACARDS REMOVED. LAMP, PN: 1317. LIGHT EMERGENCY LT, PN: 30-2510-3. NR 1 BATTERY - EMERGENCY LIGHTING, PN 2013-1A. SN: 69701. NR 1 BATTERY CHARGER ASSY, PN: 11-0049. SN: 19174. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,097 hrs · 30,565 cycles

ON FLIGHT 2793 THE CREW REPORTED THAT ON CLIMBOUT THEY FLEW THROUGH A FLOCK OF BIRDS. SUSPECT ENGINE 1 & 2 INGESTION. FOUL ODOR THRU PACKS SHORTLY THERE AFTER. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED BIRD STRIKE INSPECTION IAW WORKCARD 05-200-07. NO DAMAGE NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,014 hrs · 30,500 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EMERGENGY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY AND BATTERY POWER SUPPLY IAW EMB-145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

DURING MAINTENANCE INSPECTION FOUND OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVE FROM SERVICE. C/W: REMOVED AND REPLACED RAR EPSU BATTERY AND CHARGER IAW WC 33-70019 SYSTEM CHECKS GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 32,751 hrs · 30,304 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHTS AT COCKPIT CEILING, FORWARD CEILING IN CABIN AND EXIT FORWARD LEFT WING LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,412 hrs · 30,033 cycles

DURING MAINTENANCE INSPECTION FOUND MULTIPLE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT CHARGER AND BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW WORK CARDS 33-700-17 AND 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,328 hrs · 29,965 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FWD FAIRING, AISLE NR 1, AND COCKPIT EMERGENCY LIGHTS WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FWD EXTERNAL BULB IAW EMB 145 AMM33-50-10. PART # 1317. REMOVED AND REPLACED NR 1 BATTERY AND CHARGER IAW WC 33-700-19 AND 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 32,294 hrs · 29,937 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD WING EMERGENCY LIGHT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FUSE AT NR 1 BATTERY CHARGER IAW. CMM 25-60-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHT) · airframe 32,187 hrs · 29,849 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE WIRE CONNECTOR FOR SERVICE DOOR LIGHT IAW EMB 145 STANDARD WIRING PRACTICES MANUAL 20-21-00. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM)

BRAKES DEGRADED MESSAGE ON EICAS, O/B BRAKE NR 1 AT BOTTOM OF GREEN, I/B BRAKE NR 2 TOP OF GREEN, BRAKES ON THE OTHER SIDE BOTH MID RANGE. MESSAGE CAME ON WHEN WE EXTENDED THE GEAR AND WENT AWAY WHEN WE RETRACTED, CAME BACK WHEN WE EXTENDED THE GEAR A 2ND TIME. T/S BRAKE DEGRADED MESSAGE PER EMB FIM 32-41-00-810-804-A. PERFORMED BRAKE FUNCTION CHECK IAW EMB AMM 32-41-00. NO DISCREPANCIES NOTED. CONSIDERED TO BE A TRANSITORY CONDITION OF THE BRAKE CONTROL UNIT PER FIM. A/C OK FOR SERVICE AT THIS TIME.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,926 hrs · 29,661 cycles

ON FLIGHT 4314 THE CREW REPORTED THEY FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW EMB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 31,721 hrs · 29,513 cycles

DURING B INSPECTION FOUND THE COCKPIT EMERGENCY FLOOD LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTING BATTERY AND CHARGER ASSEMBLY IAW AE WC 33-700. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,461 hrs · 29,294 cycles

ON FLIGHT 2877 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WOULD NOT HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 30,755 hrs · 28,719 cycles

ON FLIGHT 3261, THE CREW REPORTED EN ROUTE AT FL370 CAPTAIN AND THE FIRST OFFICER HEARD AND FELT A LOUD `POP` FROM FORWARD AND UNDERNEATH THEIR FEET. CREW ASSUMED NOSE GEAR DOOR(S) HAD OPENED. AC SPEED AT THE TIME WAS 240 KTS AND DECREASED TO 230 KTS. 1 TO 2 MINS LATER CREW HEARD AND FELT A SIMILAR `POP`. FIVE OR SIX MINUTES LATER CREW HEARD AND FELT A THIRD `POP`. NO INDICATIONS WERE SEEN AS TO WHAT WAS CAUSING THE FEELING AND SOUND OF THE NOISE. THE CREW DECLARED AN EMERGENCY AND DIVERTED. AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION SHOWED NOTHING AMISS. REMOVED AND REPLACED LANDING GEAR DOOR SOLENOID VALVE IAW 32-33-02, OP CHECKED GOOD IAW 32-30-00 EMB AMM. REMOVED AND REPLACED BOTH NOSE LANDING GEAR UPLOCK BOX PROXIMITY SWITCHES IAW AMM 32-61-01. OP CHECKED GOOD. REMOVED AND NR 1 UPLOCK BOX PROXIMITY SWITCH HARNESS IAW AMM 32-60-00. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 29,822 hrs · 27,932 cycles

DURING MAINTENANCE INSPECTION THE CARGO SMOKE DETECTORS WOULD NOT TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CARGO SMOKE DETECTOR IAW EMB AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,767 hrs · 27,892 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,754 hrs · 27,882 cycles

DURING B- INSPECTION FOUND THE RIGHT OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERHEAD EMERGENCY LIGHT BULB IAW AMM TASK 30-50-08-000-801-A AND 30-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 29,572 hrs · 27,741 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-57MR-59R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (LAVATORY SERVICE) · corrosion level 2 · airframe 29,572 hrs · 27,741 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LAVATORY SERVICE HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-53MR-1926. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MODULE — INOPERATIVE (ELECTRICAL SYS) · airframe 29,458 hrs · 27,665 cycles

ON FLIGHT 2827 THE CREW REPORTED THAT ON CLIMBING THROUGH 14000 FEET A LOUND CLUNK WAS HEARD BEHIND THE FIRST OFFICERS SEAT. RECEIVED AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE AND EMERGENCY LIGHT NOT ARMED MESSAGES ON EICAS. BOTH MESSAGES DISAPPEARED AFTER A COUPLE OF MINUTES. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ELECTRICAL MODULE ASSEMBLY IAW EMB 145 AMM CHAP 20-13-10 . THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · airframe 28,742 hrs · 27,145 cycles

ON FLIGHT 4004 THE CREW REPORTED THAT AFTER LANDING, INITIAL APPLICATION OF BRAKES GAVE NO BRAKING ACTION ALONG WITH A BRAKE DEGRADE CAUTION ON EICAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BRAKE CONTROL UNIT IAW AMM# 32-41-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 28,715 hrs · 27,126 cycles

ON FLIGHT 2882 THE CREW REPORTED THAT DURING CLIMBOUT THROUGH 4500 FEET RECEIVED AN EICAS MESSAGE OF LAV SMOKE. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO XNA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE E2 ZERO CARBON SEAL. REPLACEMENT COMPLETED IAW RR AMM 72-25-25-400-801. VIBRATION AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,363 hrs · 26,875 cycles

FOUND RT OVERWING EXTERNAL EMERGENCY LIGHT INOP. REPLACED BULB.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,805 hrs · 26,492 cycles

FOR FLIGHT 2975 DURING THE PREFLIGHT INSPECTION FOUND THE RIGHT OVERWING EXIT UPPER EXIT SIGN LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTS NR 5 INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — BLOWN (NR 3) · airframe 25,864 hrs · 25,029 cycles

ON FLIGHT 3648 DURING LANDING THE AIRCRAFT HAD A BLOWN TIRE AND DAMAGE TO THE FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 TIRE, PART NUMBER 31641, SERIAL NUMBER 11920643P. ALSO REMOVED AND REPLACED THE RIGHT HAND INBOARD FLAP ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,456 hrs · 24,701 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE EXIT CEILING LIGHT. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — ACTIVATED (HYDRAULIC SYS) · airframe 25,105 hrs · 24,435 cycles

ON FLIGHT 3321 CREW REPORTED, RECEIVED A HYDRAULIC 2 LOW QUANTITY MESSAGE WITH A FLUID LEVEL THAT APPEARED TO BE DROPPING. THE CREW ELECTED TO DIVERT TO GDL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE E2 HYDRAULIC PUMP IAW AMM 29-10-03. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — BROKEN (CABIN) · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT NR 1 EMERGENCY LIGHT STRIP TO BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT FOUND THAT THE FUSELAGE HAS A DENT BETWEEN FRAMES 19 AND 19A AND STRINGERS 11R AND 12R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAMES 19 AND 19A AND STRINGERS 11R AND 12R IAW EMB SRM 53-21-01 FIG 204. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT STRIP FEMALE CONNECTOR AT SEAT 1A TO BE MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP CONNECTOR AT SEAT 1A FUSELAGE SIDE IAW EMB 145 WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (E&E DOOR) · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT FOUND THE REAR ELECTRONIC COMPARTMENT DOOR (272DR) TO BE CRACKED UNDER UPPER HINGE POINT SUPPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLER IAW EO EM-52MR-234. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT REAR FUSELAGE I SKIN AT FRAMES 65 - 66, AND STRINGER 20L - 51L TO BE DENTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT REAR FUSELAGE I SKIN AT FRAMES 65 - 66, AND STRINGER 20L - 51L IAW EO EM-53MR-1479. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT FOUND THE HORIZONTAL STABILIZER ANTI-ROTATION TAB TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED A SERVICEABLE HORIZONTAL STABILIZER FITTING IAW EO EM-55MR-324. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,584 hrs · 24,045 cycles

DURING THE MAINTENANCE BASE VISIT THE LEFT OMEGA BEAM THAT HAD PREVIOUS REPAIRS AT FRAME 20 WAS FOUND TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB SRM 53-00-10 FIG 201 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,584 hrs · 24,045 cycles

DURING THE MAINTENANCE BASE VISIT THE RIGHT OUTBOARD SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED AT FRAME 50. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT OUTBOARD SEAT TRACK SUPPORT AT FRAME 50 IAW EO EM-53MR-1476. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE VISIT THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FORWARD OF FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM FORWARD OF FRAME 25 IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,513 hrs · 23,988 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT NR 1 CABIN FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,584 hrs · 24,045 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT NR 1 FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1 FLOOR SILL IAW EMB SRM 51-40-02 AND 51-40-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 22,723 hrs · 22,323 cycles

ON FLIGHT 4078, CREW REPORTED AFTER TAKEOFF RECEIVED LAV SMOKE WARNING. F/A REPORTS NO VISUAL SMOKE OR ODOR. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND 0 CARBON SEAL LEAKING REMOVED AND REPLACED "0" CARBON SEAL OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT)

ON FLIGHT 3968 - CREW REPORTED AFTER TAKEOFF THEY RECEIVED LANDING GEAR AIR/GROUND FAIL AND FEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT MAIN LANDING GEAR WOW PROX SW NR 2. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. REMOVED AND REPLACED CARDAN JOINT ON RT MAIN LANDING GEAR. FCF PASSED. AIRCRAFT RETURNED AT SERVICE. (A)

Part: ELECTRONIC UNIT — MALFUNCTIONED (MLG)

ON FLIGHT 4113, CREW REPORTED WHEN AIRCRAFT BECAME AIRBORNE, "LG AIR/GND FAIL" MESSAGE APPEARED ON EICAS AND GEAR HANDLE WOULD NOT MOVE SO GEAR WOULD NOT RETRACT. RETURNED FOR LANDING WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB AMM 32-32-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 19,993 hrs · 19,813 cycles

DURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REPAIRED SERVICE DOOR SILL IAW EMB SRM 53-21-02 FIG 201 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE

Part: SENSOR — BROKEN (AOA) · airframe 19,350 hrs · 19,295 cycles

ABORTED TAKEOFF AT 80 KTS FOR WARNING SPS 1 INOP MESSAGE. ON POST FLIGHT INSPECTION, FOUND AOA 1 VANE BROKEN. REMOVED AND REPLACED NR 1 AOA SENSOR IAW EMB145 AMM 27-36-00 BECAUSE VANE ON AOA SENSOR DAMAGED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL ROD — EXCESS PLAY (RUDDER) · airframe 17,809 hrs · 17,937 cycles

PERFORMING AN A CHECK FOUND UPPER RUDDER CONTROL ROD HAD PLAY BETWEEN THE ROD END AND ROD TUBE. REMOVED AND REPLACED UPPER RUDDER CONTROL FOR PLAY AND LOWER CONTROL ROD AS PRECAUTIONARY, FDR DOWNLOADED. COMPONENTS AND FDR DATA RELEASED TO OEM FOR ANALYSIS. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — VIBRATES (NR 2) · airframe 16,915 hrs · 17,202 cycles

POWER WAS REDUCED BELOW 75 PERCENT ENGINE 2 HAD A NOTICEABLE VIBRIATION. REMOVED AND REPLACED NR 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 16,766 hrs · 17,054 cycles

FORWARD FACING EMERGENCY EXIT LIGHT INOP IN CABIN. RESECURED FORWARD EMERGENCY CENTER AISLE EXIT LIGHT IAW EMB AMM 33-55-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (RUDDER)

DURING LANDING FLARE EICAS MESSAGE RUDDER SYSTEM ONE AND 2 INOPERATIVE. NO RUDDER CONTROL DURING REMAINDER OF LANDING OR DURING TAXI. PERFORMED OPERATIONAL CHECK OF THE RUDDER SYSTEM WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (K)

Part: SKIN — GOUGED (PAX DOOR)

SAW - DURING PHASE 5A INSPECTION, FOUND GOUGE ON EXTERNAL SKIN ON PASSENGER DOOR AFT LOWER EDGE. REPAIRED PAX DOOR BY INSTALLING EXTERNAL DOUBLER IAW SRM 52-10-01 FIGURE 204 AND IC 2005-145/4892. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE RT HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 23. BLENDED THE RT HAT BEAM TO REMOVE CORROSION. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER. REPAIR DONE IAW SRM.

Part: BEAM — CORRODED (GALLEY) · airframe 11,907 hrs · 12,610 cycles

DURING AN MBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER HAT BEAM. INSTALLED SERVICEABLE HAD BEAM IAW SRM. (SW21200501979) (K)

Part: SILL — CORRODED (SERVICE DOOR) · airframe 11,907 hrs · 12,610 cycles

DURING INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200501979) (K)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,695 hrs · 12,410 cycles

DAMAGE ON THE AFT LOWER FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 211. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,695 hrs · 12,410 cycles

DAMAGE ON AFT LOWER FUSELAGE AT FRAME 68 AND STRINGER 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.(K)

Part: CONTROL UNIT — INOPERATIVE (AVIONICS BAY)

FWA - FLT 3794 - AFTER TAKEOFF, CREW RECEIVED PITCH TRIM MAIN AND PITCH TRIM BACKUP INOPERATIVE MESSAGE. PERFORMED AOM PROCEDURES AND PITCH TRIM WAS NOT REESTABLISHED. CREW ELECTED TO RETURN TO FWA. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TIRE — SEPARATED (NR 2)

FLT 3518 - XNA - ON TAKEOFF, NR 2 TIRE THREW THE TREAD. PERFORMED PRECAUTIONARY EMERGENCY LANDING IN DFW WITH NO INCIDENT. REPLACED NR 2 WHEEL ASSEMBLY AND REPLACED DAMAGED ENGINE NR 1 DAMAGED CORE VANES. A/C RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SDF - FLT 4087 - DURING PREFLIGHT CREW NOTED EMERGENCY LIGHTS WILL NOT TURN ON AND ILLUMINATE. AIRCRAFT WAS INSPECTED AND FERRIED TO ORD FOR REPAIR. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHTS. ALL WERE OPERATING EXCEPT FOR THE THIRD FLOOR LIGHT STRP. THE LIGHT WAS DEFERRED AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LOCK PIN — LACK OF LUBE (CAPTAINS SEAT)

CAPTAIN SEAT WILL NOT STAY LOCKED CAUSING FORE/AFT MOVEMENT IN FLIGHT. CLEANED AND LUBRICATED SEAT LOCK PIN AND SEAT RAILS IAW AE WORK CARD 25-200-07. (M)

Part: LIGHT — INOPERATIVE (GALLEY)

CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE GALLEY AREA. MAINTENANCE REMOVED AND REPLACED THE FORWARD PASSENGER LIGHT ASSEMBLY ABOVE ROW 2A IAW RMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

ABI - REPAIR TO A DENT AND GOUGE IN THE LEFT REAR FUSELAGE SKIN SPANNING THE SIN PANEL SEAM BETWEEN STRINGERS 17L AND 18L, FRAMES 70 AND 71. RECONTOURED THE DENTED SKIN. PERFORMED AN EDDY CURRENT INSPECTION OF THE REWORKED AREA AND OFUND THE SKIN AND SPLICE STRAP HAD CRACKS. COMPLETELY REMOVED CRACKED SECTION OF FUSELAGE SKIN BY PERFORMING A CUTOUT. FABRICATED A SPLICE STRAP AND TWO FUSELAGE SKIN DOUBLERS. REPAIR DONE IAW EMB STATEMENT IC2003-145/2421, IC 2003-145/2445 AND EMB 145 SRM, SRM 145/1142 REV 22, 51-00-01. (M)

Part: SILL — CORRODED (SERVICE DOOR)

DURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB GST.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION CORROSION AS FOUND ON A PREVIOUS REPAIR TO THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTED THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 20) 53-21-10 PARA 2, FIG 201 SHEET 1, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (CARGO DOOR)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM (SRM EMB 145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-20-01, 51-40-04, 51-40-06 AND EMB 145 CPM 51-21-04, 51-21-05. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGE PREVIOUS REPAIR SECTION OF THE FORWARD DIGITAL. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAIR DONE IAW EMB-145 (SRN-145/1142, CHAPTER 53, REV 20) 53-21-10 PARA 4 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - STRINGER 19L WAS FOUND TO BE CHAFFED BEYOND SRM LIMITS AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 20) 53-24-02 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (GALLEY DOOR)

A LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE DOOR SILL IAW SRM.

Part: GUSSET — CORRODED (FUSELAGE)

LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. RT BEAM AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

A LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION REFERENCE. PASSENGER DOOR AREA FORWARD FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED A SERVICEABLE FORWARD FLOOR SUPPORT IAW SRM.

Part: PROFILE — CORRODED (GALLEY RAMP)

LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. GALLEY RAMP PROFILE AT FRAME 20 CORRODED. REMOVED AND INSTALLED SERVICEABLE PROFILE IAW SRM.

Part: SEAT TRACK — CORRODED (GALLEY)

A LEVEL 2 CORROSION FOUND DURING A IMBV INSPECTION. LT HAND FORWARD LOWER SEAT TRACK CORRODED BETWEEN FRAMES 19 AND 24. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

A LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. PASSENGER DOOR AREA AFT FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICABLE SUPPORT IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ABI - FLT 3502 - DURING TAXI OUT, THE FLOOR EMERGENCY LIGHTS ROW 8 THROUGH 12 CAME ON. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 2,320 hrs · 2,514 cycles

DFW - FLT 3272 - CREW REPORTED SMOKE IN CABIN. MAINTENANCE FOUND THE NR 1 ENGINE ZERO CARBON SEAL LEAKING OIL. CARBON SEAL REMOVED AND REPLACED BY ROLLS ROYCE MECHANIC IAW ALLISON MM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — INOPERATIVE (NR 2)

CVG - FLT 4095 - EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE ROWS 8A THRU 12A. REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT NR 1, 2 AND 3 POSITION. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (NR 3)

CVG - FLT 4095 - EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE ROWS 8A THRU 12A. REMOVED AND REPLACED EMEREGNCY BATTERY PACKS AT NR 1, 2 AND 3 POSITION. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (NR 1)

CVG - EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE ROWS 8A THRU 12A. REMOVED AND REPLACED EMEREGNCY BATTERY PACKS AT NR 1, 2 AND 3 POSITION. OPS CHECK GOOD. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

ORD - FLT 4226 - LAVATORY SMOKE INDICATION IN FLIGHT. TROUBLESHOT SYSTEM AND PERFORMED OPERATIONAL CHECK, COULD NOT DUPLICATE PROBLEM. (M)