N671AE

Part: NONE — NONE · airframe 41,416 hrs · 36,920 cycles

PASSENGER SEAT 15A AND 16A EMERGENCY LIGHT FLOOR POWER STRIP WIRE BORKEN.-C/A-RAR EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12 OPC GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,776 hrs · 36,140 cycles

GALLEY EMERGENCY LIGHT INOP. R & R GALLEY EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,431 hrs · 35,792 cycles

EMERGENCY INTERIOR LIGHT ADJ TO RH EMERGENCY EXIT INOP-C/A-REF TURNOVER, COMPLETED RAR OF #5 EMERG LIGHTS INVERTER IAW AMM 33-50-11. OPC GOOD.

Part: FLASHLIGHT ASSY — BROKEN · airframe 39,897 hrs · 35,218 cycles

AFT CABIN EMERGENCY FLASHLIGHT HOLDER HAD BROKEN CLIP-C/A-R & R AFT CABIN EMERGENCY FLASHLIGHT HOLDER ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 39,739 hrs · 35,052 cycles

AFT RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R AFT RT OVERWING EMERGENCY LIGHT ASSEMBLY OPERATIONS CHECK GOOD, IAW AMM 33-50-10.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,609 hrs · 34,928 cycles

RT UPPER EMERGENCY EXIT LIGHT INOPERABLE. C/A: R & R RT UPPER EMERGENCY LIGHT BULB, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECK GOOD. NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,518 hrs · 34,849 cycles

RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT LAMP, IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPERATIONS CHECK GOOD.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 39,059 hrs · 34,393 cycles

FOUND RT WING EMERGENCY LIGHT INOPERATIVE DURING PS-1 CHECK. REMOVED AND INSTALLED A NEW RT WING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,673 hrs · 33,985 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD. END.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 38,644 hrs · 33,957 cycles

R/H WING EMERGENCY LIGHT INOP-C/A-RAR R/H WING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: TRANSDUCER — FAILED (NR 2 ENGINE) · airframe 38,586 hrs · 33,905 cycles

H.S. REJECTED T/O (80 KTS) DUE E2 A/I FAIL ON T.O. ROLL-C/A-RRMOVED AND REPLACED ENGINE #2 ANTI-ICING PRESSURE TRANDUCER IAW EMB145 AMM 30-21-06 LEAK/ OPS CHECK GOOD

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 38,466 hrs · 33,801 cycles

E1 A/ICE FAIL MESSAGE DURING CLIMB. RAN CHECHLIST, BUT MESSAGE REMAINED AND VALVE WOULD NOT OPEN WITH OVERRIDE NOB IN ALL. ALSO GOT AN ENG A/I OVERPRESS ADVISORY MESSAGE.-C/A-DEFFERED PER MEL 30-11 "M" PROCEDURES COMPLIED WITH. REMOVED AND REPLACED E1 ENG PRESSURE TRANSDUCER AND ENG1 A/ICE VLV IAW EMB 145 AMM 30-21-06 AND 30-21-01 OPS AND LEAK TEST GOOD MEL ITEM RESTORED. PRESSURE TRANSDUCER P/N APS-5-1500 S/N 8538-3-37

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,193 hrs · 33,523 cycles

DURING PS-1 CHECK, FOUND EMERGENCY LIGHT INOPERATIVE BETWEEN 12A AND 9A. REMOVED AND REPLACED THE NR 3 BATTERY POWER SUPPLY AND BATTERY IAW AMM 33-50-04, OPS-CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,186 hrs · 33,517 cycles

FLOOR PROXIMITY STRIP NR 1 AFT SECTION INOPERATIVE. REMOVED AND REPLACED FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,186 hrs · 33,517 cycles

LEFT FORWARD LOWER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 38,186 hrs · 33,517 cycles

FOUND EMERGENCY LIGHT BATTERY PACKS NR 2 AND 3 LOW, LIGHTS SHUT OFF AFTER APPOX 10 SECONDS. REMOVED AND REPLACED THE NR 2 BATTERY. OPS CHECKED GOOD IAW AMM 33-50-04. REMOVED AND REPLACED NR 3 BATTERY, OPS CHECKED GOOD IAW AMM 33-50-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,044 hrs · 33,408 cycles

DURING PS-1 CHECK FOUND MULTIPLE EMERGENCY LIGHTS OUT NEAR CENTER FUSELAGE.-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY IAW EMB 145 W/C 33-700-19. OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 12788

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 37,933 hrs · 33,305 cycles

ON TAXI OUT AFTER SWITCHING PACK 1 BACK ON, COCKPIT FILLED WITH SMOKE. AFTER SWITCHING PACK 1 BACK OFF SMOKE DISSIPATED-C/A-PERFORMED FIM TASK PROCEDURES EMB 145 FIM 21-20-00. RAN PACK 1 AND PACK 2 AND PERFORMED ALL VISUAL INSPECTIONS. NO DISCREPANCIES NOTED. PERFORMED ETN-EM-72-034 PROCEDURES RAN ENGINES WITH CREW. DOCUMENTED ALL VALUES. NO SMOKE DETECTED IN COCKPIT OR CABIN. AIRCRAFT OKAY FOR SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,912 hrs · 33,281 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,761 hrs · 33,146 cycles

1EA BROKEN WIRE ON EMERGENCY LIGHT STRIP AT FLOOR PANEL 251BF-C/A-REPAIRED 1EA WIRES AT FLOOR PANEL 251BF IAW SWPM 20-21-00. OPS CHK GOOD

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 37,761 hrs · 33,146 cycles

3EA WIRES BROKEN ON EMERGENCY LIGHT STRIP FLOOR CONNECTIONS-C/A-REPAIRED 3EA WIRES AT FLOOR PAELS 261BF AND 251FF IAW SWPM 20-21-00. OPS CHK GOOD

Part: SHUNT — GOUGED (FRAME 80) · airframe 37,761 hrs · 33,146 cycles

FRAME 80 AFT SIDE AT APU SHUNT CONNECTION IS GOUGED (FRAME REINFORCEMENT)-C/A-REMOVED AND REPLACED REINFORCEMENT IAW SRM 53-32-04, GPM17-13 AND SRM 51-40-02.

Part: STOP FITTING — DAMAGED (CARGO DOOR) · airframe 37,761 hrs · 33,146 cycles

CARGO DOOR FWD CONTINUOS STOP IS BENT AND CRACKED AT LOWER END-C/A-REMOVED AND INSTALLED NEW CARGO DOOR FWD CONTINUOS STOP IAW EMB 145 SRM 51-40-02

Part: STRINGER — CRACKED (FRAME 13) · airframe 37,761 hrs · 33,146 cycles

STGR 6R CRACKED AT FR 13-C/A-REMOVED AND INSTALLED NEW STRINGER 6R AT FRAME 13 IAW EMB 145 SRM 51-40-02.

Part: RIB — CRACKED (LT WING) · airframe 37,761 hrs · 33,146 cycles

LH WING RIB 21 IS CRACKED INSIDE PANEL 551CB.-C/A-REPAIRED LH WING RIB 21 INSIDE PANEL 551CB IAW EMB 145 SRM 57-20-07, ITEM #4.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,761 hrs · 33,146 cycles

CARGO DOOR LOWER SILL IS CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB-145 SRM 51-40-02.

Part: RIB — CRACKED (RT WING) · airframe 37,761 hrs · 33,146 cycles

RH WING RIB 21 IS CRACKED INSIDE PANEL 651CB. REPAIRED RH WING RIB 21 INSIDE PANEL 651CB IAW EMB 145 SRM 57-20-07, ITEM #4

Part: RIB — CRACKED (LT ELEVATOR) · airframe 37,761 hrs · 33,146 cycles

LEFT ELEVATOR INBOARD HINGE CUTOUT INBOARD NOSE RIB IS CRACKED -C/A-REMOVED AND INSTALLED NEW INBD NOSE RIB ON THE LEFT ELEVATOR INBOARD HINGE CUTOUT IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 37,761 hrs · 33,146 cycles

SSI 53-20-11 LH OMEGA BEAM SIDEWALL CORRODED AT FR 29. REPAIRED LH OMEGA BEAM SIDEWALL AT FR 29 IAW ENVOY ERS-EM-53MR-3903

Part: FLOOR SUPPORT — CRACKED (FR 47) · airframe 37,761 hrs · 33,146 cycles

LH OMEGA BEAM OUTBD SUPPORT IS CRACKED AT PREVIOUS REPAIR AT FR 47-C/A-REMOVED AND REPLACED L/H OMEGA OUTBD SUPPORT AT FR 47 IAW EMB 145 SRM 53-23-02 AND SRM 51-40-02

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,761 hrs · 33,146 cycles

SSI 53-30-48 FR 65 SHEAR CLIP IS CORRODED AT CARGO DOOR SILL AND ABOVE GUIDE PLATE-C/A-REMOVED AND INSTELLED SERVICEABLE SECTION OF FRAME 65 SHEAR IAW EMB 145 SRM 53-31-04.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 37,761 hrs · 33,146 cycles

CARGO DOOR LOWER FRAME IS CORRODED AROUND 2 SCREW HOLES AT FWD END.-C/A-REMOVED AND INSTALLED NEW CARGO DOOR LOWER FRAME IAW EMB 145 SRM 51-20-03, 51-40-06 AND 51-40-02.

Part: FRAME — GOUGED (FR 68) · airframe 37,761 hrs · 33,146 cycles

FR 68 Z FRAME IS GOUGED AROUND 4 SCREW HOLES RH SIDE LOWER END-C/A-REMOVED AND REPLACED GOUGED FR 68 Z FRAME IAW EMB 145 SRM 51-40-02.

Part: ECU — FAILED (TE FLAP) · airframe 37,478 hrs · 32,967 cycles

AFTER TAKE OFF UPON RETRACTING THE FLAPS, WE GOT FLAPS FAIL MESSAGE ON THE EICAS. FLAPS DID NOT RETRACT AND STAYED AT 9*. WE COMPLIED WITH CHECKLIST AND LANDED IN MIA. C/A-REMOVE AND REPLACE FECU IAW AMM 27-53-02. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 35,588 hrs · 31,191 cycles

EMEREGENCY EXIT LIGHTED SIGN ON BACKSIDE OF AFT CALLEY (FACING THE SEATS) INOP. REMOVED AND REPLACED NR 2 DC/AC INVERTER IAW AMM 33-50-11 AND EMERGENCY LIGHTS OPS CHECK GOO IAW AMM 33-50-00-700-801.

Part: GENERATOR — MALFUNCTIONED (NR 3) · airframe 35,445 hrs · 31,041 cycles

NR 3 GENERATOR OFF BUSS DURING TAKEOFF ROLL. REMOVED AND REPLACED THE NR 3 GENERATOR IAW WC 24-800-00, OP CHECKED GOOD AND LEAK CHECKED GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 35,406 hrs · 31,005 cycles

FLAP FAIL AFTER TAKE OFF STUCK AT 9. CMC HAD MULTIPLE OCURRENCES OF DRIVE SENSOR FAIL. HAD ONE OCURRENCE OF FLAP RT TRANSMISSION FAIL. TROUBLESHOT IAW FIM 27-51-00-810-817-A, AND FIM 27-51-00-810-801-A. REMOVED AND REPLACED THE FECU IAW AMM 27-53-02. OPS CHECKED GOOD. ALL CMC MESSAGES CLEARED. DID NOT REAPPERED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,284 hrs · 30,908 cycles

EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 34,229 hrs · 29,976 cycles

BOTH AFT OVERWING EMERGENCY LIGHTS FAILED TO ILLUMINATE. COMPLIED WITH FIM 33-50-00. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER IAW 33-50-04. OPS CHECKED GOOD IAW AMM 33-50-04.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,197 hrs · 29,944 cycles

BOTH AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: CONTACTOR — DIRTY (EMERGENCY LIGHT) · airframe 34,189 hrs · 29,932 cycles

AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND CLEANED THE CONTACTORS IAW GENERAL MAINTENANCE, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,189 hrs · 29,932 cycles

SEVERAL EMERGENCY LIGHTS FOUND INOPERATIVE, LT AND RT EXTERNAL OVERWING. REMOVED AND REPLACED THE NR 4 BATTERY, PERFOMED AN OPS CHECK IAW 33-700-17. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 34,101 hrs · 29,862 cycles

LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. TROUBLESHOT IAW WM 33-50-50, AND R 7 R THE NR 4 EPSU IAW AMM 30-50-04. OPS CHECKED GOOD. BATTERY CHARGER ASSY.

Part: WIRE HARNESS — FAILED (NLG) · airframe 34,101 hrs · 29,861 cycles

RECEIVED A LANDING GEAR AIR/GND FAIL CAUTION MESSAGE DURING CLIMBOUT. COULD NOT BRING GEAR UP. MESSAGE EXTINGUISHED 2 MINUTES LATER. BROUGHT GEAR UP. LANDED BACK AT DEPARTURE, GEAR DOWN. REMOVED AND REPLACED NLG AIR /GROUND WOW PROXIMITY SENSOR NR 2 IAW AMM 32-63-02 OPS CHECKED GOOD IAW AMM 32-63-00.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 33,957 hrs · 29,721 cycles

BOTH AFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT CHARGER AND BATTERY ASSY, OPS CHECKED BAD IAW AMM 33-50-04.

Part: FUSE — FAILED (POWER SUPPLY) · airframe 33,815 hrs · 29,615 cycles

LH AND RH AFT OVERWING EMERGENCY LIGHTS INOP.-C/A-T/S PER FIM 33-50-00-810-804A. FOUND #4 EMERGENCY BATTERY POWER SUPPLY FUSE F1 INOP. REMOVED AND REPLACED #4 EMERGENCY BATTERY POWER SUPPLY FUSE F1 IAW CMM 25-60-03. OPS CHECK GOOD AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,591 hrs · 29,424 cycles

BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-50-04. OPS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,544 hrs · 29,384 cycles

LT AND RT OVERWING EMERGENCY LIGHT INOP. REPLACED NR 4 EMERGENCY BATTERY AND BATTERY POWER SUPPLY IAW AMM 33-50-04 OPS GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 19591.

Part: CHARGER — FAILED (CABIN) · airframe 33,339 hrs · 29,190 cycles

FOUND O/W RT AND O/W LT EXTERIOR EMERGENCY LAMPS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-50-04 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 73813.

Part: SENSOR — FAILED (RT WING TE FLAPS) · airframe 33,172 hrs · 29,040 cycles

DURING CLIMB, RETRACTED FLAPS TO 0 DEGREES ON THE SELECTOR. RECIEVED FLAP FAIL ON EICAS. FLAPS INDICATED 9 DEGREES. RETURNED FOR LANDING AND LANDED. REMOVED AND REPLACED THE RT VELOCITY SENSOR IAW AMM 27-51-12. REMOVED AND REPLACED FLAP CONTROL UNIT IAW AMM 27-53-02. OPS CHECKED GOOD IAW AMM AMM 27-51-00.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 32,796 hrs · 28,713 cycles

CLIMBING TRHROUGHT 15000 FT, THE CABIN RATE BEGAN TO FLUCTUATE, BETWEEN 2000 AND -2000 FPM, CABIN ALTITUDE DISPLAY, FOUR ORANGE DASHES. SELETED MANUAL MODE IAW AOM, VOL 1 PROCEDURES, COULD NOT CONTROL PRESSURIZATION IN MANUAL MODE BOTH IN AIR AND ON GROUND. REMOVED AND REPLACED PRESSURIZATION DIGITAL CONTROL IAW AMM 21-31-01. PERFORMED PRESSURIZATION OPS CHECK IN AUTO AND MANUAL MODE IAW AMM 21-30-00. OPS CHECKED GOOD. PRESSURIZATION MANUAL MODE OPS CHECK IAW AMM 21-31-00-700-801-A.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 32,763 hrs · 28,673 cycles

ALL EMERGENCY LIGHTS THAT ARE POWER BY EMERGENCY BATTERY NR 1 DO NOT TURN ON. REMOVED AND REPLACED EMERGENCY BATTERY AND CHARGER IAW WC 33-700-19

Part: STRINGER — CHAFED (FRAMES 20-21) · airframe 32,763 hrs · 28,673 cycles

STRINGER 2L IS CHAFED BETWEEN FRAMES 20 - 21. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FR 65) · airframe 32,763 hrs · 28,673 cycles

FR 65 CHANNEL IS CORRODED AROUND SCREW HOLE AT STRINGER 14L. REPAIRED THE CHANNEL IAW ERS-EM-53MR-2761.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · airframe 32,763 hrs · 28,673 cycles

LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58 AND 59. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2773.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,763 hrs · 28,673 cycles

LEFT EMERGENCY LIGHT NR 4 WIRES ARE BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12

Part: FRAME — CRACKED (FRM 73) · airframe 32,763 hrs · 28,673 cycles

FRAME 73 CRACKED AT STRINGER 17R-C/A-REMOVED AND REPLACED FR 73 AT STRINGER 17R IAW EMB 145 SRM 51-40-02

Part: SKIN — CRACKED (FRAME 75) · airframe 32,763 hrs · 28,673 cycles

LEFT AFT FUSELAGE FRAME 75 HAS A SKIN CRACK ABOVE STRINGER 2L. PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 32,763 hrs · 28,673 cycles

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

Part: STRUCTURE — CORRODED (LAVATORY VALVE) · airframe 32,763 hrs · 28,673 cycles

LAVATORY BUCKET IS CORRODED AROUND TOILET WASTE VALVE. REMOVED AND REPLACED TOILET WASTE VALVE SUPPORT BUCKET IAW SRM 51-40-02

Part: MANIFOLD — NO TEST (NLG STEERING) · airframe 32,684 hrs · 28,573 cycles

NOSE WHEEL STEERING MANIFOLD FAILED TO TEST IAW AMM 32-50-04 STEP J1E. SERVO VALVE CURRENT MUST BE 0 +- O.5 MILLIAMPS. CURRENT READS OVER 2 MILLIAMPS. REPLACE MANIFOLD. REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD IAW AMM 32-50-04. INSTALLED NEW ZERO INDICATION MARKING PLATE IAW AMM 32-50-10. PERFORMED NOSE WHEEL STEERING SYSTEM ADJUSTMENT AND TEST IAW AMM 32-50-00, OPS CHECKED GOOD. FCF FOUND SATISFACTORY. REMOVED AND REPLACED NOSE STEERING MANIFOLD RH SIDE HYDRAULIC LINE IAW AMM 32-50-04. LEAK CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,371 hrs · 28,336 cycles

FLOOR EMERGENCY LIGHT NR 8, HAS A BROKEN WIRE SPLICE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: REFLECTOR — CORRODED (FLASHLIGHT) · airframe 32,371 hrs · 28,336 cycles

PILOT`S FLASHLIGHT LIGHT REFLECTOR CORRODED. REMOVED AND REPLACED THE FLASHLIGHT ASSY IAW AMM 33-50-16.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,182 hrs · 24,083 cycles

EMERGENCY LIGHTS INOPERATIVE IN GALLEY, ROW 7 OVERHEAD & 3 FWD AISLE STRIPS. R & R BATTERY POWER SUPPLY NR 2, BATTERY AND CHARGER, IAW AMM 33-50-04. OPERATIONAL TEST GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,180 hrs · 24,080 cycles

LEFT & RT OVERWING PANEL EXIT LIGHTS DO NOT COME ON. R & R NR 4 BATTERY POWER SUPPLY, CHARGER & NR 4 BATTERY ASSEMBLY IAW AMM 33-50-04. EMER LIGHTING OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,180 hrs · 24,080 cycles

EMERGENCY LAMP ON CEILING PANEL 263ALC WILL NOT COME ON. R & R EMER LAMP ON CEILING PANEL 263ALC IAW AMM 33-50-08. OPERATIONAL CHECK PERFORMED & FOUND SATISFACTORY.

Part: FRAME — CHAFED (FUSELAGE) · airframe 28,180 hrs · 24,080 cycles

FUSELAGE FRAME 60 CHAFED AT STRINGER 05L.L PERFORMED ERS-EM-53MR-1098 FOUND TO BE ACCEPTED AS IS.

Part: RIB — GOUGED (LT WING) · airframe 28,180 hrs · 24,080 cycles

LEFT WING INBD RIB GOUGED AFT OF THE MLG UPLOCK BOX. PERFORMED ERS-EM-57MR-388 FOUND TO BE ACCEPTED AS IS.

Part: FRAME — CHAFED (FUSELAGE) · airframe 28,180 hrs · 24,080 cycles

GALLEY AREA FRAME 19 CHAFED AT STRINGER 03R. PERFORMED ERS-EM-53MR-1099 FOUND TO BE ACCEPTED AS IS.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 28,180 hrs · 24,080 cycles

SERVICE DOOR LOWER FWD & AFT SCREW HOLES ARE CORRODED WHERE LINER ATTACHES. PERFORMED ERS-EM-52MR-294 FOUND TO BE ACCEPTED AS IS.

Part: WIRE — NICKED (CABIN) · airframe 28,180 hrs · 24,080 cycles

CABIN MOST AFT FLOOR PROXIMITY LIGHT WIRE INSULATION NICKED AT LT OMEGA BEAM. REPAIRED THE CABIN MOST AFT FLOOR PROXIMITY LIGHT WIRE INSULATION AT LT OMEGA BEAM IAW SWPM 20-21-00.

Part: WIRE — NICKED (CABIN) · airframe 28,180 hrs · 24,080 cycles

FLOOR PROX LIGHT WIRE INSULATION NICKED AT FRAME 49. REPAIRED THE FLOOR PROX LIGHT WIRE INSULATION AT FRAME 49 IAW SWPM 20-21-00.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 28,180 hrs · 24,080 cycles

FUSELAGE SKIN SCRATCHED FRAME 16 - 17, STRINGER 12R. PERFORMED ERS-EM-53MR-1087 FOUND TO BE ACCEPTED AS IS.

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 28,180 hrs · 24,080 cycles

SERVICE DOOR FWD INNER SKIN GOUGED AT LOWER CORNER. PERFORMED ERS-EM-52MR-292 FOUND TO BE ACCEPTED AS IS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,180 hrs · 24,080 cycles

RIGHT OMEGA BEAM INBD SUPPORT CRACKED BETWEEN FRAME 47 - 48. REMOVED & INSTALLED SERVICEABLE SUPPORTS FOR RT OMEGA BEAM INBD SIDE BETWEEN FRAME 46 - 50 OVER THE WING BOX IAW SRM 51-40-02 & SRM 53-23-02.

Part: LIGHT — BROKEN (CABIN) · airframe 28,180 hrs · 24,080 cycles

EMERGENCY LIGHT STRIP ON LT FLOOR EXTRUSION NR 1 WIRES BROKEN. R & R EMER LIGHT STRIP ON LT FLOOR EXTRUSION 1 IAW AMM-33-50-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,180 hrs · 24,080 cycles

RIGHT OMEGA BEAM OTBD SUPPORT CRACKED BETWEEN FRAME 47 - 48. REMOVED & INSTALLED SERVICEABLE LONGER SUPPORT FOR RT OMEGA BEAM OTBD SIDE BETWEEN FRAME 46 - 50 OVER THE WING BOX IAW SRM 51-40-02 & SRM 53-23-02.

Part: LIGHT — SHORTED (CABIN) · airframe 28,032 hrs · 23,943 cycles

DURING PS1 INSPECTION FOUND BOTH OVERWING AFT EMER LIGHT INOPERATIVE. FURTHER TROUBLESHOOTING FOUND CONNECTOR P8503, PIN 9 PUSHED OUT & WILL NOT RESEAT. R & R CONNECTOR P8503 IAW ESPM 20-50-01, DID NOT FIX PROBLEM. R & R EPSU INVERTER 6 IAW AMM 33-50-11, DID NOT FIX. BATTERY CHARGER PN 11-0049 SN 13541, EMER LIGHTING BATTERY PN 2013-1A SN 71822. RT OVERWING EMER LIGHT WAS SHORTED. R & R EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,747 hrs · 23,669 cycles

MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,600 hrs · 23,523 cycles

OVERWING EMER LIGHT INOPERATIVE. R & R NR 4 BATTERY PACK & CHARGER ASSEMBLY IAW AMM-33-50-04. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,543 hrs · 23,478 cycles

RIGHT AFT OVERWING EMER EXIT LIGHT INOPERATIVE. REPLACED RT SIDE CTR FAIRING EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-10 2 L 2 4 K 13. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — FAILED · airframe 27,365 hrs · 23,326 cycles

TAKEOFF ABORTED AT 70 - 80 KNOTS DUE TO MASTER WARNING & MASTER CAUTION & SPS ADVANCED GPWS INOPERATIVE SPS 1 & 2. STALL PROTECTION SYS OPERATIONS GOOD IAW AMM 145 27-36-00. SEE THIS LOG PAGE ITEMS 2 & 3. EGPWS WIND SHEAR WARNING & FLIGHT GUIDANCE SYS, WIND SHEAR MODE INOPERATIVE. CANNOT DUPLICATE. TEST INDICATES NO CURRENT FAULTS. OPS CHECKED GOOD IAW AMM 34-41-00.

Part: UNKNOWN — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 27,152 hrs · 23,114 cycles

AD 2 AIRSPEED & ALT WAS OFF DUE TO WATER OR ICE ON THE STATIC PORTS. CLEARED ON DESCENT. INSPECTED PITOT DRAIN HOSE FOR WATER IAW AMM 34-13-00 & PERFORMED OPERATIONS CHECK OF ADC 2. ADC 2 CHECKS NORMAL IAW AMM 34-15-00.

Part: ICU — FAILED (VHF COMM) · airframe 26,547 hrs · 22,512 cycles

DURING FLIGHT 3273 CREW REPORTED COMM 1 & COMM 2 RADIO FAILURE AFTER TAKEOFF. EMER WAS DECLARED THE ACFT WAS REMOVED FROM SERVICE. TROUBLESHOOT IAW FIM TASK 23-12-00-810-802-A. FOUND COMM 2 TO BE WORKING NORMALLY. R & R VHF 1 ICU IAW AMM 23-00-01-000-801-A & 23-00-01-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME. ACFT REMAINS RVSM ELIGIBLE. THE ACFT RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 26,408 hrs · 22,362 cycles

FIRST OFFICER`S FLASHLIGHT CRADLE DAMAGED. R & R FIRST OFFICER`S FLASHLIGHT CRADLE IAW AMM TASK 33-50-16-000-801-A & 33-50-16-400-801-A.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,385 hrs · 22,338 cycles

SERVICE DOOR FAIRING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT LAMP IN SERVICE DOOR FAIRING IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (PRECOOLER) · airframe 26,242 hrs · 22,202 cycles

CLIMBING THROUGH 7000 FT, RECEIVED A NR 2 BLEED OVERTEMP IN ICING CONDITIONS. REMOVED AND REPLACED PRECOOLER TEMP SENSOR IAW MM 36-20-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,017 hrs · 21,993 cycles

LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT CHARGER & BATTERY IAW WC 33-700-17, OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,951 hrs · 21,935 cycles

RIGHT & LT EXTERIOR OVERWING EMERGENCY LAMPS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW AMM 33-50-04-000-801-A & 33-50-04-400-801-A. NO FIX, TROUBLESHOT EXTERNAL OVERWING EMERGENCY LAMPS USING WM 33-50-50. LAMPS TESTED GOOD WITH 6VDC APPLIED TO PIN 9 ON PLUG P8503. TRIED 2 MORE BATTERIES & 3 MORE CHARGERS, NO POWER COMING FROM CHARGER TO PIN 9. TRANSFERRED TO AML PAGE 3476335 ITEM 1.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 25,892 hrs · 21,881 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,080 hrs · 21,291 cycles

F/O'S RECHARGEABLE FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16.

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 25,080 hrs · 21,291 cycles

FOUND F/A'S FLASHLIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,929 hrs · 20,348 cycles

DURING B-INPSECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE MAIN DOOR EMERGENCY LIGHT IAW AMM TASK 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: BATTERY — DISCHARGED (CABIN) · airframe 23,911 hrs · 20,335 cycles

THE CREW REPORTED THE LT WING TO FUSELAGE EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. LT LIGHT EMERGENCY PN: 30-2510-3. BATTERY, EMERGENCY LIGHTING PN: 2013-1A. SN: 113275. BATTERY CHARGER ASSY PN: 11-0049. SN: 15185. ALLOWED BATTERIES TO CHARGE. THE OPS CHECK WAS GOOD IAW AMM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (ANTI ICE SYS) · airframe 23,909 hrs · 20,334 cycles

SHORTLY AFTER TAKEOFF IN ICING CONDITIONS, RECEIVED A NR 2 BLEED OVERTEMP EICAS MESSAGE. RAN AOM VOL 1 CHECKLIST. RECEIVED A WING ANTI ICE FAIL EICAS CAUTION MESSAGE FOLLOWED BY AN ICE COND - A/I INOPERATIVE EICAS WARNING MESSAGE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED ANTI-ICING SYSTEM OPS TEST, OPS TEST GOOD IAW MM 30-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,858 hrs · 20,298 cycles

DURING MX INSPECTION FOUND THE LT NR 2 & LT NR 5 EMERGENCY LIGHT STRIPS HAVE BROKEN WIRES. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT NR 2 & LT NR 5 EMERGENCY LIGHT STRIPS IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: TERMINAL — MISSING (CABIN) · airframe 23,858 hrs · 20,298 cycles

DURING MX INSP, FOUND THE TERMINAL FOR EMERGENCY LIGHT STRIP AT FLOOR PANEL 241DF MISSING. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED THE TERMINAL FOR EMERGENCY LIGHT STRIP AT FLOOR PANEL 241DF IAW MM 20-21-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,858 hrs · 20,298 cycles

DURING MX INSPECTION FOUND THE EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4 EMERGENCY BATTERY & BATTERY CHARGER IAW WC 33-700-19. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 23,858 hrs · 20,298 cycles

DURING MX INSPECTION, FOUND THE GALLEY CENTER BEAM GUSSET CORRODED BETWEEN FRAMES 20 AND 23. THE ACFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW GALLEY CENTER BEAM GUSSET IAW SRM 51-40-02. THE LEVEL OF CORROSION WAS NOT SPECIFIED. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 23,858 hrs · 20,298 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT STRIP AT SEAT 10A LIFTING OFF OF THE FLOOR. THE ACFT WAS REMOVED FROM SERVICE. REATTACHED THE EMERGENCY LIGHT STRIP AT SEAT 10A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE · airframe 23,848 hrs · 20,289 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,702 hrs · 20,181 cycles

ON FLIGHT 4394 THE CREW REPORTED THE LAST ROW FLOOR EMERGENCY LIGHTING WAS INOPERABLE. FLOOR PROXIMITY STRIP LAST ROW DEFER PER MEL 33-30 AUTH #040689-C MAINT PROCEDURE COMPLIED WITH. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,489 hrs · 20,014 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT OVER THE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT BULB IAW EMB 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 — DISCHARGED (CABIN) · airframe 23,148 hrs · 19,747 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. PART NUMBER 1317. NO FIX. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY & CHARGER IAW W/C 33-700-19 AND W/C 33-700-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — ODOR (FLASHLIGHT) · airframe 23,099 hrs · 19,708 cycles

ON FLIGHT 3264 THE CREW REPORTED THE FLIGHT DECK FLASHLIGHT ON THE FIRST OFFICER’S SIDE HAD AN ELECTRICAL ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BATTERY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,099 hrs · 19,708 cycles

ON FLIGHT 3264 THE CREW REPORTED THE FLIGHT DECK FLASHLIGHT ON THE BULKHEAD WALL WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,090 hrs · 18,159 cycles

DURING MAINTENANCE INSPECTION FOUND THE EXIT IDENTIFIERS AT COCKPIT STEP AND GALLEY AISLE CEILING PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER IAW EMB-145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — FAULTY (GALLEY) · airframe 20,513 hrs · 17,682 cycles

ON FLIGHT 4197 THE CREW REPORTED THE GALLEY SMOKE DETECTOR WAS INOPERABLE FOR LAV DETECTION. LAV SMOKE DET SYSTEM DEFERED PER MEL 26-02. REMOVED AND REPLACED CONNECTOR P8100 IAW EMB 145 SWPM 20-50-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 20,136 hrs · 17,416 cycles

ON FLIGHT 2816 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT RETAINING CLAMP WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND CAPTAINS FLASHLIGHT BRACKET ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 20,069 hrs · 17,373 cycles

DURING INSPECTION FOPUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 20,089 hrs · 17,386 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-05. THE OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,888 hrs · 16,493 cycles

FOR FLIGHT 3371 DURING MAINTENANCE CHECK FOUND THE LEFT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — LEAKING (RT WING) · airframe 16,943 hrs · 15,093 cycles

ON FLIGHT 2813 THE CREW REPORTED VIA LOG PAGE THAT AFTER TAKEOFF ANOTHER AIRCRAFT REPORTED A WHITE TRAIL COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP VALVE ON RIB 19 ON THE RIGHT WING IAW EMB 145 AMM 28-11-04. NO LEAKS NOTED. REFERENCE 2494037, 2494035. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,638 hrs · 14,839 cycles

FOR FLIGHT 4007 DURING INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,197 hrs · 14,534 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE FORWARD EMERGENCY FLOOR LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AEAI WORK CARDS 33-700-19 AND 33-700-17 AND REPLACED BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — INOPERATIVE (CABIN) · airframe 15,791 hrs · 14,220 cycles

DURING COURTESY CHECK FOR FLIGHT 4393 MAINTENANCE FOUND THE LEFT FORWARD WING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EMERGENCY SUPPLY BATTERY HOLDER. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 13,802 hrs · 12,598 cycles

ON FLIGHT 4120, WHILE CLIMBING THROUGH 32,000 FT, THE CABIN BEGAN LOOSING PRESSURIZATION RAPIDLY. ACCOMPANYING THE LOSS OF PRESSURIZATION WAS A SIGNIFICANT VIBRATION IN THE FLT CONTROLS AND ACFT ITSELF. RAPID DECOMPRESSION EVENT CHECKLIST COMPLETED & EMERGENCY DECLARED. ACFT LANDED WITH NO INCIDENT. ACFT REMOVED FROM SERVICE. COMPLIED WITH AE WORK CARD 12-200-01, VIBRATION-DETAILED VISUAL INSPECTION. NO DISCREPANCIES NOTED. VIBRATION NOTED IN NR 1 ABOVE ATTRIBUTED TO THE OUTFLOW VALVES EXHAUSTING DIRECTLY ON FLT CONTROLS IN THE TAILCONE. R & R MANUAL CONTROLLER IAW AMM 21-31-02 AND REMOVED AND REPLACED PNEUMATIC OUTFLOW VALVE IAW AMM 21-31-04. AIRCRAFT RETURNED TO SERVICE.

Part: RECEPTACLE — INOPERATIVE (COFFEEMAKER) · airframe 14,187 hrs · 12,946 cycles

ON FLIGHT 3849, DURING THE LANDING ROLL, THE FLIGHT ATTENDANT REPORTED THE SMELL OF ELECTRICAL SMOKE IN THE GALLEY. NO VISIBLE SMOKE DETECTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 HOT JUG RECEPTACLE PLUG/AFT GALLEY ASSEMBLY IAW EBB 145 MM STANDARD MAINTENANCE 20-13-07. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS NOTED. THE AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 13,802 hrs · 12,598 cycles

ON FLIGHT 4120 WHILE CLIMBING THROUGH 32,000 FEET THE CABIN BEGAN LOSING PRESSURIZATION RAPIDLY. ACCOMPANYING THE LOSS OF PRESSURIZATION WAS A SIGNIFICANT VIBRATION IN FLIGHT CONTROLS AND THE AIRCRAFT ITSELF. RAPID DECOMPRESSION EVENT CHECKLIST COMPLETED AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH WORK CARD 12-200-01 "VIBRATION-DETAILED VISUAL INSPECTION". NO DISCREPANCIES NOTED. VIBRATION NOTED IN NR 1 ABOVE ATTRIBUTED TO OUTFLOW VALVES EXHAUSTING DIRECTLY ON FLIGHT CONTROL CABLES IN TAIL CONE. REMOVED AND REPLACED MANUAL CONTROLLER IAW EMB AMM 21-31.02, REMOVED AND REPLACED PNEUMATIC OUTFLOW VALVE IAW EMB AMMM 21-31-04. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOOR) · airframe 9,733 hrs · 8,888 cycles

DURING IMBV INSPECTION THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REPLACED CARGO DOOR SILL IN ACCORDANCE WITH EMBRAER SRM (SRM-145/1142 REV. 38) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,733 hrs · 8,888 cycles

AIRCRAFT WAS REMOVED FROM SERVICE. DURING IMBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 9,233 hrs · 8,445 cycles

FLAP EXTENDED ABOVE AIRSPEED LIMITATION ON APPROACH AND IMMEDIATELY SELECTED FLAPS 22. COMPLIED WITH AE MTX WORK CARD 05-200-06 FLAP EXCEEDANCE CONDITION INSPECTION. AIRCRAFT RETURN TO SERVICE.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 8,088 hrs · 7,366 cycles

AT TAKEOFF POWER RIGHT ENGINE HIGH ITT, RIGHT ENGINE PARAMETERS HIGH, RETURNED TO ORD.

Part: BATTERY — DISCHARGED (CABIN)

DFW - FLT 3377 - EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR POWER SUPPLY BATTERIES (S/N`S 70964, 68422, 687110, 73063) IAW AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. (M)

Part: TRIM PANEL — INOPERATIVE

ORD - FLT 4259 - DURING CLIMB THROUGH 280 KNOTS, 11,000 FT, LOST MAIN PITCH TRIM, STANDBY WAS WORKING. EICAS MESSAGE `PTRIM MAIN INOP` PERFORMED EMERGENCY CHECKLIST. MAIN PITCH TRIM INOPERATIVE. BACK TRIM FAIL TO TRIM UP. NO EICAS MESSAGE. CONTINUE CHECKLIST WITH DUAL PITCH TRIM FAILURE. RESET CIRCUIT BREAKER E-11, C-24, REGAINED MAIN PITCH TRIM. REMOVED AND REPLACED STANDBY PITCH TRIM PANEL AND HSCU P/N 362100101013, S/N 4613. OPERATIONAL CHECK GOOD. AIRCRAFT PASSED FUNCTIONAL CHECK FLIGHT. RETURNED AIRCRAFT TO SERVICE. (M)

Part: UNKNOWN — UNKNOWN (UNKNOWN)

DAY - FLT 4193 - ON DESCENT, WITH AUTO PILOT ENGAGED RECEIVED BACKUP PITCH TRIM INOPERATIVE MSG FOLLOWED BY ANOTHER RED MSG THE CREW COULDN’T READ. CAPT FELT A SMALL VIBRATION IN THE YOKE, VIBRATION ASSOCIATED WITH AUTO PILOT. ISSUED MEL 22-01, COMPLIED WITH EO EM-53MR-696. OPS CHECK GOOD. RETURN AIRCRAFT TO SERVICE. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

DAY - FLT 4193 - ON DESCENT WITH AUTO PILOT ENGAGED RECEIVED, BACKUP PITCH TRIM INOP MESSAGE FOLLOWED BY ANOTHER RED MESSAGE THAT CREW COULD NOT READ. CAPT FELT A SMALL VIBRATION IN THE YOKE. (M)

Part: LIGHT — FAILED (CABIN)

DISC - EMERGENCY EXIT SIGN LIGHT AT THE COCKPIT DOOR STEP INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT. OPERATIONAL CHECK GOOD. RETURNED TO SERVICE. (K)