N667GB

Part: NONE — NONE · airframe 40,482 hrs · 36,740 cycles

ON DEPARTURE, UPON RETRACTING THE LANDING GEAR CREW RECEIVED LG/LEVER DISAGREE MESSAGE. COMPLIED WITH QRH RECEIVED WARNING AGAIN.UNABLE TO GET GEAR TO RETRACT AND UNABLE TO MAKE DFW ON FUEL LOAD. FLIGHT DIVERTED TO GGG. PLAN TO FERRY DFW-GGG TO RESCUE 50 PAX.-C/A-FOUND RH MLG UPLOCK UPPER SWITCH CONNECTOR LOOSE. REMOVED FOUND RH MLG UPLOCK UPPER SWITCH CONNECTOR LOOSE. REMOVED AND RECONNECTED THE CONNECTOR. PERFORMED LG EXTENSION AND RETRACTION OPERATIONAL CHECK IAW EMB145 AMM 32-30-00. OPERARTIONAL CHECK GOOD NO MESSAGE ON THE AICAS. AML # 4771680 ITEM 1 FOR DETAIL.

Part: SENSOR — MALFUNCTIONED (BRAKE TEMP) · airframe 39,300 hrs · 35,366 cycles

"BRAKE OVERHEAT" ON EICAS IN FLIGHT ON LEFT HAND, INBOARD-C/A-RAR LH INBOARD TEMPERATURE SENSOR IAW EMB 145 AMM 32-47-01. OPERATIONAL CHECK GOOD.

Part: LENS — DESTROYED (EXTERNAL LIGHT) · airframe 39,119 hrs · 35,181 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT LENS SHATTERED. C/A-MAIN DOOR EXTERNAL EMERGENCY LIGHT LENS R & R IAW EMB145 AMM 33-50-10.

Part: ENGINE — VIBRATION (NR 2) · airframe 38,582 hrs · 34,611 cycles

NR 2 ENGINE RUMBLE WHEN MOVEMENT BETWEEN MIDRANGE AND IDLE ON THE THROTTLE QUADRANT VIBRATIONS FELT IN RUDDER PEDALS ON THE GROUND AND IN THE AIR ON DESCENT AND APPROACH TO LANDING NO IMPACT TO FLIGHT CONTROLS OR EICAS INDICATION. BLEEDS WERE CONFIGURED NORMAL, NO ENGINE EICAS OR INSTRUMENT ABNORMALITIES. THE RUMBLE ONLY CAME ON THE RETARDING OF THE THROTTLE. C/A: REF NRWC 667-ORD-03902 FOR CORRECTIVE ACTION. R & R OF NR 2 ENGINE, IAW EMB 145 W/C 71-000-00. OPERATIONS AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 38,537 hrs · 34,569 cycles

MAIN CABIN DOOR NOT CLOSING ALL THE WAY. C/A LUBRICATED OUTSIDE HANDLE, OPENED AND CLOSED. OPERATIONAL CHECK GOOD, IAW EMB145 AMM 52-10-01.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 38,315 hrs · 34,347 cycles

FLT EXPERIENCED TWO HIGHSPEED WARNINGS DESCENDING 11000.1ST <10 SECOND 250-280. 2ND, 8 SECONDS 250-270.FLAPS AND GEAR WERE UP. PERFORMED PHASE 1 INSPECTION FOR OVERSPEED IAW AMM 05-50-04. NO DEFECTS NOTED AT THIS TIME.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 38,244 hrs · 34,295 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE ALL INDICATIONS NORMAL. LUBRICATED EXTERNAL HANDLE. CLEANED AND SERVICED MAIN DOOR ROLLERS. OPS CHECK GOOD IAW AMM 52-18-00 & AMM 53-21-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 38,095 hrs · 34,169 cycles

MOST AFT FLOOR PROXIMITY EMERGENCY LIGHTING STRIP HAS ONE BROKEN ELECTRICAL CONNECTOR-C/A-REPAIRED CONNECTOR FOR EMERGENCY LIGHTING STRIP IAW SWPM 20-21-00. OPC IS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 38,095 hrs · 34,169 cycles

FOUND BROKE WIRE NEAR EMERGENCY FLOOR LIGHT ASSEMBLY P/N 6636-7-C/A-REMOVED AND REPLACED EMERGENCY FLOOR LIGHT ASSEMBLY P/N 6636-7 IAW EMB-145 AMM 33-50-08 OPERATIONAL CHECK GOOD

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,012 hrs · 34,076 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #2 EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK IAW AMM 33-50-04. PERFORMED WIRING REPAIR ON WIRE W192-8627-20 AT SERVICE DOOR HINGE WIRING BUNDLE IAW SWPM 20-21-00 AND WM 33-50-50. OPS CHECK GOOD. CHARGER ASSY BATTERY P/N BA5-0933-901 S/N C01129

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 37,962 hrs · 34,014 cycles

FWD CABIN EMER FLASHLIGHT CRADLE DAMAGED-C/A-RAI NEW FWD CABIN FLASHLIGHT CRADLE IAW EMB 145 AMM33-50-16. LED IS ON GREEN WITH BUTTON PRESSED.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 37,852 hrs · 33,895 cycles

CABIN AISLE FWD CEILING EMERGENCY LIGHT IS INOP-C/A- FOUND #1 EMERG BATTERY SUPPLY CONNECTOR DISCONNECTED. RECONNECTED IAW EMB-145 AMM 33-50-04. OPC GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,852 hrs · 33,895 cycles

FWD LH EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR LH FWD EXTERNAL EMERGENCY LIGHT LAMP IAW EMB-145 AMM 33-50-10. OPC GOOD

Part: SKIN — CANNING (VERTICAL STAB) · airframe 37,653 hrs · 33,734 cycles

LEFT HAND VERTICAL STABILIZER SKIN JUST FORWARD OF TAIL ACCESS PANEL 324EL HAS OIL CANNING.-C/A-C/W REPAIR OF VERTICAL STABILIZER SKIN LOCATED JUST FWD OF TAIL ACCESS PANEL 324EL IAW ERS-EM-55MR-813.

Part: FITTING — CHAFED (AILERON DAMPER) · airframe 37,653 hrs · 33,734 cycles

RIGHT HAND AILERON DAMPER FITTING CHAFFED.-C/A-REMOVED AND REPLACED DAMPER FITTING ASSY IAW EO-EM-27MR-112.

Part: FITTING — CHAFED (AILERON DAMPER) · airframe 37,653 hrs · 33,734 cycles

LEFT HAND AILERON DAMPER FITTING CHAFFED. LEFT HAND AILERON PCA FITTING OUTBD HAT BUSHING IS MIGRATED OUT. -C/A-INSTALLED NEW AILERON DAMPER FITTING ASSY IAW EO-EM-27MR-112, STEP 3. REMOVED AND REPLACED LH AILERON PCA FITTING IAW EO-EM-27MR-112. FITTING P/N 145-69382-609

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,653 hrs · 33,734 cycles

FRAME 65 SHEAR CLIP CORRODED AT CARGO SILL LEVEL.-C/A-COMPLETED REPAIR OF FRAME 65 SHEAR CLIP IAW SRM 53-31-04.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · airframe 37,653 hrs · 33,734 cycles

SERVICE DOOR SILL HAS CORROSION. (CENTER)-C/A-REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRAME 10) · airframe 37,653 hrs · 33,734 cycles

RIGHT SIDE OF FRAME 10 HAS A 1/2" CRACK JUST BELOW F/O'S DV WINDOW SILL.-C/A-REPLACED RH FRAME 10 IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 37,653 hrs · 33,734 cycles

STRINGER CLIP AT FRAME 80 AND STR 9R HAS A 3/8 CRACK. (EVALUATED AND FOUND SHEAR CLIP AT FRAME 80 STRINGER 9R NOT TO BE CRACKED. CRACKED SHEAR CLIP IS LOCATED AT FRAME 80 STRINGER 7R.) -C/A-REMOVED AND REPLACED SHEAR CLIP AT FRAME 7R IAW SRM 51-40-02.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 37,653 hrs · 33,734 cycles

CARGO DOOR TORSION BAR BRACKET ON FRAME 61 HAS A 1/16" CRACK. -C/A-RAR'D CARGO DOOR TORSION BAR BRACKET ON FRAME 61 IAW SRM-51-40-02. REF NRTC E764850 FOR LIFTING AND LOWERING ADJUSTMENT/TEST.

Part: SKIN — CRACKED (FRAME 78) · airframe 37,653 hrs · 33,734 cycles

L/H REAR FUSELAGE II SKIN IS CRACKED AROUND A RIVET AT FR 78. (CRACK APROX 1/4 INCH LONG) -C/A-REPAIRED IAW SRM 53-32-01.

Part: ANGLE — CRACKED (FR 76) · airframe 37,653 hrs · 33,734 cycles

L/H VERT TO FUSELAGE ANGLE IS CRACKED AT FR 76.(CRACK APROX 1 INCH LONG) -C/A-INSTALLED NEW ANGLE IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (FRAME 68) · airframe 37,653 hrs · 33,734 cycles

STIFFENER ON THE AFT SIDE OF FRAME 68 FOR CARGO DOOR HOLD OPEN STRUT RECEPTACLE HAS TWO 1/2" CRACKS.C/A-RAR STIFFENERR IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 79) · airframe 37,653 hrs · 33,734 cycles

L/H REAR FUSELAGE II SKIN IS CRACKED AROUND A RIVET AT FR 79. (CRACK APROX 1/4 INCH LONG) -C/A-REPAIRED IAW SRM 53-32-01.

Part: DOOR SILL — CORRODED (CARGO DOOR) · airframe 37,653 hrs · 33,734 cycles

CARGO DOOR SILL IS CORRODED.-C/A-COMPLETED INSTALLATION OF NEW CARGO DOOR SILL IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FRAME80) · airframe 37,653 hrs · 33,734 cycles

STRINGER CLIP AT FRAME 80 AND STR 7L HAS A 3/8" CRACK. -C/A-REMOVED AND REPLACED STRINGER CLIP AT FRAME 80 AND STR. 7L IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 37,653 hrs · 33,734 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER AFT ATTACH ANGLE HAS 1/4" CRACK ON THE AFT END. -C/A-REPAIRED RIGHT UPPER WING TO FUSELAGE FAIRING AFT LOWER ATTACH ANGLE IAW ETN-EM-53-412.

Part: ATTACH ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 37,653 hrs · 33,734 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER 2ND FROM THE AFT ATTACH ANGLE HAS 1/4" CRACK ON FWD END. -C/A-REPAIRED RIGHT UPPER WING TO FUSELAGE FAIRING LOWER 2ND FROM AFT ATTACH ANGLE IAW ETN-EM-53-142.

Part: CARBON SEAL — FAILED (RT ENGINE) · airframe 37,498 hrs · 33,585 cycles

STRONG BURNING SMELL EACH TIME ANTI-ICEING CAME ON-C/A-REMOVED AND REPLACED RH ENGINE #0 CARBON SEAL IAW RRMM TASK 72-25-25-000-801 & 72-25-25-400-801 AND OPC IAW ETN-EM-72-034 OPC GOOD AT THIS TIME PIREP RESTORED.

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 37,063 hrs · 33,142 cycles

SUPPLEMENTAL ENG(2) ANTI ICE FAIL. C/A-ENG 2 A/ICE VLV FAIL MSG ON CMC, FOLLOWED FIM TASK 30-21-00-810-804-A. FAIL RT ENGINE A/ICE VALVE. DEFERRED PER MEL 30-11. AUTH# 090264DM-C C/W "M" PROCEDURES. REMOVED AND REPLACED ENG 2 A/ICE VALVE, OPC GOOD, IAW AMM 30-21-01. MEL RESTORED

Part: O-RING — BLOWN (NR 2 BLEED DUCT) · airframe 36,944 hrs · 33,026 cycles

DURING CLIMB WHILE PERFORMING THE ICE PROTECTION TEST PNEUMATIC RECEIVED AN EICAS BLEED NR 2 WARNING MESSAGE. COMPLIED WITH CHECKLIST PROCEDURES AND DECLARED AND EMERGENCEY. PERFORMED PACK 2 OPERATIONAL CHECK REF AMM 21-00-00. FOUND BLEED 2 DUCT COUPLING AFT WHEEL WELL AREA BLOWN. INSTALLED NEW O RINGS AND RE INSTALLED COUPLING IAW AMM 36-11-10. PERFORMED AIR BLEED SYS OPS CHECK REF AMM 36-00-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: FLASHLIGHT — FAILED (COCKPIT) · airframe 36,943 hrs · 33,024 cycles

SMELL OF ELECT SMOKE IN COCKPIT.NO VISIBLE SMOKE.WINDSHIELD HEAT WENT OUT IN DECENT.NO EICAS MSG , NO POPPED CB'S , NO SWITCH ANOMOLY. UPON ARRIVAL TO COCKPIT DIDNT SMELL ANY ELEC SMOKE OR EICAS MSG.PERFORMED ETN-EM-72-034 ENG ODOR EVENT T/S SUP . NO ELECTRICAL SMELL NOTED IN COCKPIT. PERFORMED INSPECTION OF WINDSHIELD HEATING SENSORS 1 & 2 LEADS AND ATTACHING HARDWARE PARTIALLY AMM 30-42-04. PERFORMED INSPECTION OF LEADS ON W/S TEMP CONTROLLER 1 & 2 IAW ETN-EM-30-015 AND PARTIALLY TASK EMB145 AMM 30-42-01, OPS CHECK GOOD OF W/S HEATING SYSTEM IAW AMM 30-42-00. WHILE T/S IAW FIM 21-20-00-810-801-A, FOUND FLASHLIGHT ABOVE FA SEAT SLIGHT ELEC BURNING SMELL. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY ABOVE FA SEAT IAW EMB145 AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,398 hrs · 31,590 cycles

AFT CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 34,853 hrs · 31,039 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE-C/A-OPENED AND CLOSED DOOR SEVERAL TIMES. DID NOT FEEL ANY DIFFICULTY CLOSING DOOR. DID REMOVE SOME INSULATION THAT WAS EXPOSED. LUBRICATED ROLLERS IAW AMM 53-21-02. OPS CHECK GOOD. CONFIRMED DOOR CLOSES CORRECTLY IAW AMM 52-00-00.

Part: DOOR SEAL — DIRTY (DOOR) · airframe 34,424 hrs · 30,660 cycles

MAIN DOOR DIFFICULT TO CLOSE-C/A-CLEANED AND LUBRICATED DOOR SEALS. PERFORMED OPS CHECK OF DOOR IAW AMM 52-11-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,230 hrs · 30,470 cycles

DURING PS-2 CHECK, OVERWING EMERGENCY EXIT FLOOR LIGHTING STRIP FOUND TO BE INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT FLOOR LIGHTING STRIP IAW AMM TASK 33-50-12. OP CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,703 hrs · 29,994 cycles

FA DETECTED A STRONG ODOR IN THE CABIN GOT WORSE WITH HEAT. COMPLIED WITH ETN-EM-72-034. COMPLETED RUNS AND INSPECTION, NO DETECTABLE ODOR NOTED

Part: SKIN — CRACKED (FRAME 75) · airframe 32,655 hrs · 28,997 cycles

RIGHT AFT FUSELAGE FRAME 75, SKIN CRACKED AT FASTENER BELOW STRINGER 2. REPAIRED IAW SRM 53-31-01, ITEM 11, FIGURE 219, SHEET 1, 51-20-03, AND 51-40-02.

Part: YOKE — CRACKED (RT ENGINE) · airframe 32,655 hrs · 28,997 cycles

RIGHT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND INSTALLED A NEW YOKE IAW EO EM-54MR-386.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,655 hrs · 28,997 cycles

LEFT AFT FUSELAGE FRAME 75 SKIN CRACKED AT FASTENER BELOW STRINGER 2. REPAIRED IAW SRM 53-31-01, ITEM 11, FIGURE 219, SHEET 1, 51-20-03, AND 51-40-02.

Part: YOKE — CRACKED (LT ENGINE) · airframe 32,655 hrs · 28,997 cycles

LT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND INSTALLED THE ENGINE YOKE IAW EO EM-54MR-386.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 32,655 hrs · 28,997 cycles

GOUGE FOUND ON CARGO DOOR APPROXIMATELY 10 INCHES AFT OF FORWARD END AND 24 INCHES UP FROM BOTTOM END. INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 52-30-01,ITEM 2, AND 51-40-02.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 32,655 hrs · 28,997 cycles

GOUGE FOUND ON CARGO DOOR APPROXIMATELY 24UP FROM THE BOTTOM AND 10 INCHES FORWARD OF AFT END. INSTALLED A DOUBLER, AND FILLER IAW SRM 52-30-01, ITEM 2, AND 51-40-02.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 29,308 hrs · 25,445 cycles

THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FCU — INOPERATIVE (FUEL INDICATION) · airframe 28,627 hrs · 24,768 cycles

ACFT DIVERTED FUEL 1 LO LEVEL INDICATION AND PACK 2 OVERHEAT INDICATION IN-FLIGHT. MAINTENANCE R & R FUEL CONDITIONING UNIT IAW AMM 28-41-01 AND IPC REF 28-41-00, FIG 16, ITEM 1A, OPS CHECK GOOD. MAINTENANCE R & R NR 2 ACM IAW AMM 21-51-03 AND IPC 21-51-00, FIG 26, PAGE 3, ITEM 30B, OPS CHECK GOOD. ACFT GOOD FOR SERVICE. FUEL CONDITIONING UNIT, PN ON: 367-934-002, SN ON: 630, PN OFF: 367-934-002, SN OFF: 294. NR 2 ACM, PN ON: 815240-3, SN ON: 960812 PN OFF 815240-3, SN OFF: 9805010. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 20,545 hrs · 14,934 cycles

DURING CREW INSPECTION THE EMERGENCY LIGHT SIGN AT OVERWING EXIT AND BACK HALF OF FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,180 hrs · 24,335 cycles

DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS FROM ROW 12 TO THE BACK WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,179 hrs · 24,334 cycles

REAR FUSELAGE 1 LOWER SKIN DENT & CREASE. FABRICATED & INSTALLED FILLER & DOUBLER IAW ERS-53MR-1123.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,175 hrs · 24,330 cycles

CEILING LIGHT AT SEAT 3A INOPERATIVE. R & R 3A CEILING PANEL EMER LIGHT LAMP IAW AMM 33-50-09.

Part: WIRE — BROKEN (CABIN) · airframe 28,175 hrs · 24,330 cycles

SERVICE DOOR LIGHT INOPERATIVE. REPAIRED BROKEN WIRE W716-0007-20 BETWEEN SPLICE SP 7376 & PIN C OF P 7198 IAW SWPM 20-21-00.

Part: SKIN — NICKED (FUSELAGE) · airframe 28,175 hrs · 24,330 cycles

EXTERNAL FUSELAGE SKIN NICKED BETWEEN FRAME 15 - 16, STRINGER 19L - 20L. REPAIRED DAMAGE IAW ERS -EM-53MR-1100.

Part: WIRE — DAMAGED (CABIN) · airframe 28,175 hrs · 24,330 cycles

SERVICE DOOR TRIM EMER EXIT SIGN WIRES HAVE DAMAGED INSULATION. REPAIRED SERVICE DOOR TRIM EMER EXIT SIGN WIRES IAW SWPM 20-21-00. SEE BOW 181673 FOR OPERATIONS CHECK FOUND DURING CLOSE UP.

Part: ELT — FAILED · airframe 28,175 hrs · 24,330 cycles

EMERGENCY LOCATOR TRANSMITTER SYS FAILED OPERATIONAL CHECK, 3 FLASHES AFTER BUILT IN TEST. R & R ELT IAW AMM 25-61-01 & ETN-EM-25-435. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — SEPARATED (CABIN) · airframe 28,175 hrs · 24,330 cycles

EMERGENCY LIGHT STRIP WIRE CONNECTOR SEPARATED FROM WIRE AT AFT END OF 251DF. REPAIRED EMER LIGHT STRIP WIRE CONNECTOR AT AFT END OF 251DF IAW SWPM 20--21-00. SEE BOW 181673 FOR OPERATIONS CHECK OF EMER LIGHT STRIPS. FOUND ON CLOSE UP.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 28,175 hrs · 24,330 cycles

CARGO DOOR LOWER NUTPLATE HOLES HAVE SURFACE CORROSION. PERFORMED PERMANENT REPAIR TO CARGO DOOR LOWER NUTPLATE HOLES IAW ERS-EM-52MR-291.

Part: FIREWALL — CHAFED (APU BAY) · airframe 28,175 hrs · 24,330 cycles

APU FIREWALL IS CHAFED AT UPPER LT AREA. PERFORMED REPAIR OF CHAFED AREA ON APU FIREWALL AT UPPER LT AREA IAW ERS-EM-53MR-1090.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,175 hrs · 24,330 cycles

EXTERNAL FUSELAGE LIGHTNING STRIKE DAMAGE BETWEEN FRAME 13 - 14 STRINGERS 21L - 21R. PERFORMED PERMANENT REPAIR TO SKIN AT FRAME 13 - 14 & STRINGER 21L - 21R IAW ERS-EM-53MR-1085.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 28,175 hrs · 24,330 cycles

SERVICE DOOR LOWER NUTPLATE HOLES HAVE CORROSION. REMOVED CORROSION FROM SERVICE DOOR LOWER NUTPLATE HOLES IAW ERS-EM-52MR-289.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 28,175 hrs · 24,330 cycles

SERVICE DOOR UPPER NUTPLATE HOLES HAVE CORROSION. PERFORMED REPAIR TO SERVICE DOOR UPPER NUTPLATE HOLES IAW ERS-EM-52MR-289.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 28,175 hrs · 24,330 cycles

INTERIOR FUSELAGE STRINGER 2L CHAFED AFT OF FRAME 20. PERFORMED PERMANENT REPAIR TO STRINGER 2L AFT OF FRAME 20 IAW ERS-53MR-1086.

Part: SHROUD — CORRODED (LT AILERON) · airframe 28,175 hrs · 24,330 cycles

LEFT WING UPPER AILERON SHROUD MOUNTING FLANGE HAS 10 CORRODED SCREW HOLES. REPAIRED LT WING UPPER AILERON SHROUD FLANGE IAW ERS-EM-57MR-384.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 28,175 hrs · 24,330 cycles

CARGO DOOR FWD NUTPLATE HOLES HAVE SURFACE CORROSION. REPAIRED CARGO DOOR FWD NUTPLATE HOLES IAW ERS-EM-52 MR-295.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 28,175 hrs · 24,330 cycles

CARGO DOOR UPPER NUTPLATE HOLES HAVE SURFACE CORROSION. CARGO DOOR UPPER NUTPLATE HOLES FOUND TO BE WITHIN LIMITS IAW ERS-EM-52MR-290.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,175 hrs · 24,330 cycles

EXTERIOR FUSELAGE LIGHTNING STRIKE DAMAGE JUST AFT OF FRAME 23, STRINGER 3R - 4R. REPAIRED EXTERIOR FUSELAGE LIGHTNING STRIKE DAMAGE IAW ERS-EM-53 MR-1083.

Part: FITTING — CRACKED (CABIN) · airframe 28,175 hrs · 24,330 cycles

RIGHT FWD CARPET EXTRUSION CRACKED. R & R RT FWD CARPET EXTRUSION IAW AMM 33-50-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,175 hrs · 24,330 cycles

RIGHT BEAM INBD SUPPORT IS CRACKED BETWEEN FRAME 47 & 48. REMOVED CRACKED RT BEAM INBD SUPPORT BETWEEN FRAME 47-48 & INSTALLED BEAM SUPPORTS IAW SRM 53-23-02 & SRM 51-40-02.

Part: FITTING — CRACKED (CABIN) · airframe 28,175 hrs · 24,330 cycles

LEFT FLOOR LIGHT EXTRUSIONS 2, 3, 4 & 6 ARE CRACKED. R & R LT FLOOR LIGHT EXTRUSIONS 2, 3, 4 & 6 IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 28,175 hrs · 24,330 cycles

PASSENGER CABIN EMER LIGHT STRIPS NR 3 & 6 HAVE BROKEN WIRES. R & R PAX CABIN EMER LIGHT STRIPS NR 3 & 6 IAW AMM 33-50-12.

Part: FITTING — CRACKED (CABIN) · airframe 28,175 hrs · 24,330 cycles

RIGHT FLOOR EXTRUSIONS 5 & 8 ARE CRACKED. R & R RT FLOOR EXTRUSIONS 5 & 8 IAW AMM 33-50-12.

Part: LIFE VEST — TORN (COCKPIT) · airframe 28,175 hrs · 24,330 cycles

COCKPIT LIFE VEST TORN. R & R COCKPIT LIFE VEST IAW EEL-08-12.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 28,175 hrs · 24,330 cycles

RESTORE INFANT LIFE VEST. INSTALLED SERVICEABLE INFANT LIFE VEST.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 28,029 hrs · 24,207 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 27,509 hrs · 23,804 cycles

FLASHLIGHT CRADLE BEHIND CAPTAIN`S SEAT DOES NOT HOLD THE FLASHLIGHT. R & R FLASHLIGHT CRADLE BEHIND CAPTAIN`S SEAT. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,363 hrs · 23,688 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REPLACED CAPTAIN`S FLASHLIGHT IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,310 hrs · 23,643 cycles

SERVICE DOOR HINGE EMER LIGHT INOPERATIVE. R & R LAMP IN SERVICE DOOR HINGE LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,062 hrs · 23,446 cycles

FIRST OFFICER`S FLASHLIGHT IS DEAD. R & R FIRST OFFICER`S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: DME — FAILED (NR 2) · airframe 26,989 hrs · 23,386 cycles

DURING THE CLIMB OUT THE CREW WAS ALERTED TO A NAV 2 FAIL. THEY FOLLOWED THE GUIDANCE OF THE AOM-1 & MEL BOOK. THEY NOTIFIED SOC & MOC OF THE FAILURE & SENT AN M20 MSG. WHEN THEY ARRIVED THEY WERE ABOUT 300LBS UNDER PLANNED ARRIVAL FUEL, THEY DECIDED TO FLY A GPS APPROACH TO 27R VS THE LOC 27 BECAUSE OF THE FPA. DURING THE APPROACH ATC TOLD THEM TO GO AROUND. SINCE THE ALT WX AS THE SAME AS ORD 1100 OVER, THE CAPTAIN DECIDED NOT TO DIVERT. DECLARED AN EMER WITH ATC SO THAT HE COULD SHOOT AN ILS 27R APPROACH, BECAUSE OF SINGLE NAV SOURCE & FUEL RSVS & WX A 1100FT CEILING WITH AN MDA OF 1200FT ON THE LOC & GPS. THE CAPTAIN MADE A PA TO THE PAX & INFORMED THE FA. ONCE SAFELY ON THE GND THE CREW TAXIED TO THE GATE & MADE THE APPROPRIATE AML ENTRY. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 2 NAV UNIT IAW MM 34-52-01. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. RVSM & CAT II COMPLIANT & CERTIFIED.

Part: WIRE — OVERHEATED (COCKPIT) · airframe 26,143 hrs · 22,530 cycles

INTENSE ELECTRICAL ODOR INFLIGHT AT 22,000. INFRARED CAMERAS REVEALED WIRE HARNESS FWD OF CAPTAIN`S RT RUDDER PEDAL WAS HOT. PERFORMED DVI OF RUDDER PEDAL HARNESS AREA, COCKPIT PANELS, WINDSHIELD TEMP CONTROL UNITS, CABIN AIR DIST, SYSTEM, ELECTRICAL BAY COMPONENTS, BOTH LT AND RT RELAY PANELS,. NO DEFECTS NOTED.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,143 hrs · 22,530 cycles

EMERGENCY LIGHTING FLOORBOARD STRIP DAMAGED, NR 4. R & R FLOORBOARD STRIP IAW AMM 33-50-12, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 23,991 hrs · 23,991 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT STRIP CONNECTOR AT SEAT POSITION 9A MISSING CONNECTOR. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT STRIP CONNECTOR AT SEAT POSITION 9A IAW SWPM 20-21-00, STEP 5 AND REINSTALLED EMERGENCY LIGHT STRIP LT NR 5 AT SEAT POSITION 9A IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 23,991 hrs · 20,748 cycles

DURING MX INSEPCTION, FOUND THE NR 1 EMERGENCY LIGHT STRIP HAD A BROKEN CONNECTION. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 23,991 hrs · 20,748 cycles

DURING B INSP FOUND THE F/O EMERGENCY FLASHLIGHT WOULD NOT STAY ON. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O EMERGENCY FLASHLIGHT IAW AMM 33-50-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,932 hrs · 19,886 cycles

ON FLIGHT 4130 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — LOOSE (COCKPIT) · airframe 22,673 hrs · 19,664 cycles

ON FLIGHT 3254 THE CREW REPORTED THE CAPTAIN’S SIDE FLASHLIGHT HOLDER WAS LOOSE CAUSING INTERMITTENT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER IAW EMB 145 33-50-16 AMM. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,523 hrs · 19,541 cycles

DURING B INSPECTION FOUND THE RIGHT FORWARD WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD EMERGENCY LIGHT LAMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM TASK 33-50-07-000-801 AND EMB AMM TASK 33-50-07-400-801. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,481 hrs · 19,502 cycles

DURING B INSPECTION FOUND THE RIGHT EMERGENCY LIGHT AT WING/FUSELAGE FAIRING FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EMERGENCY LAMP AT WING/FUSELAGE FAIRING FRONT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,299 hrs · 19,361 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP PER EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801. NO FIX. FOUND AND REPAIRED BROKED WIRE PER EMB WIRING STANDARD PRACTICES MANUAL 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — UNSERVICEABLE (MAIN DOOR) · airframe 22,090 hrs · 19,176 cycles

ON FLIGHT 3332 THE CREW REPORTED THE MAIN DOOR HANDLE CAME OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR INTERIOR HANDLE BOLT AMM 52-18-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 21,907 hrs · 19,013 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND BROKEN WIRE AT SERVICE DOOR HINGE AREA. SPLICED BROKEN WIRE IAW WM 20-21-00. OPS CHECKED NORMAL. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 21,805 hrs · 18,933 cycles

FLIGHT 3552, THE MAIN DOOR WAS HARD TO OPEN AND CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR IAW AMM 52-19-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,640 hrs · 18,788 cycles

DURING PS-2 CHECK, FOUND THE OVERHEAD PASSENGER DOOR EMERGENCY LIGHT TO BE BURNED OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IAW AMM 33-50-06. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,341 hrs · 18,568 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT OUT AT ROW 14A TO ROW 18A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW BATTERY AND BATTERY CHARGER, PER WORKCARD NR 1 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,280 hrs · 17,727 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FUSELAGE FORWARD EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS RMOVED FROM SERVICE. RELAMPED RIGHT FUSELAGE FORWARD EXTERIOR EMERGENCY LIGHT PER EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — FAILED (FWD CABIN) · airframe 20,094 hrs · 17,604 cycles

FLIGHT 2560, CREW REPORTED THE FORWARD CABIN FLASHLIGHT HAD AN ELECTRICAL BURNED PLASTIC TYPE ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT ASSEMBLY IAW AMM 25-60-00. THE OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — LOOSE (PAX DOOR) · airframe 20,085 hrs · 17,598 cycles

ON FLIGHT 2949 THE CREW REPORTED THE MAIN DOOR CABIN DOOR HARD TO OPEN/CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED BOLT ON DOOR HANDLE SUPPORT BRACKET, LUBE HINGES DOORS, THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 52-18-00 AMM. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 52-18-00 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,902 hrs · 17,450 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IN THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 19,822 hrs · 17,383 cycles

FOR FLIGHT 4196 THE CREW REPORTED AT THE GATE THE CAPTAIN’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER ASSEMBLY IAW EMB 145 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 19,326 hrs · 16,999 cycles

DURING MAINTENANCE BASE VISIT FOUND A MIS-DRILLED HOLE AT END OF FRAME 66, UPPER FLANGE WHERE IT ATTACHES TO CARGO DOOR LOWER SILL AND FLOOR SUPPORT ANGLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,326 hrs · 16,999 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 44. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: ATTACH FITTING — DAMAGED (AILERON) · airframe 19,326 hrs · 16,999 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT AILERON INBOARD ATTACH FITTING HAS DAMAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,326 hrs · 16,999 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 29. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: FLAPPER VALVE — FAULTY (RT WING) · airframe 18,998 hrs · 16,752 cycles

ON FLIGHT 2737 THE CREW REPORTED THAT DURING THE CLIMB THE FLIGHT ATTENDANT NOTICED THE RIGHT WING WAS STREAMING. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT HAD AN OVERWEIGHT LANDING BUT UNDER 300 FEET MINIMUM DESCENT RATE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAPPER VALVE ON RIB 19 RIGHT WING IAW EMB 145 AMM 28-11-04. REFERENCE NRWC 667-DFW-00414 FOR PANEL INSTALL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 18,764 hrs · 16,555 cycles

ON FLIGHT 9807 THE CREW REPORTED THAT RIGHT BEFORE TOUCHDOWN RECEIVED A LOW OIL PRESSURE WARNING MESSAGE. OIL QUANTITY IN NR 2 ENGINE DROPPED TO 3 QTS, ENGINE 2 OIL PRESSURE DROPPED TO RED RANGE, RED EICAS ALERT. THE CAPTAIN SHUT DOWN ENGINE NR 2 DOWN IMMEDIATELY UPON SLOWING TO TAXI SPEED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GEAR BOX BREATHER CARBON SEAL IAW RRMM 72-63-10-000-802. THE LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,796 hrs · 15,831 cycles

DURING MAINTENANCE BASE VISIT FOUND THE COCKPIT BULKHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 EMERGENCY BATTERY PER AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (REQUEST TO MAKE SEPARATE SDR’S)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 17,796 hrs · 15,831 cycles

(REQUEST TO MAKE SEPARATE SDR’S) DURING MAINTENANCE BASE VISIT FOUND THE COCKPIT BULKHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER PER AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RUDDER CONTROL — MALFUNCTIONED

EMERGENCY DECLARED, RUDDER 1/2 INOP IN FLIGHT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,654 hrs · 8,876 cycles

EMERGENCY LIGHTS AT ROW 12-18 INOP, FOUND DURING MORNING PREFLIGHT. SFP TO DFW FOR EMERGENCY BATTERY PACK. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOOR) · airframe 9,629 hrs · 8,854 cycles

DURING IMBV INSPECTION, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REPLACED SILL WITH PN 145-25480-603 IAW SRM 51-40-02, 51-40-06, 51-40-06, 51-40-10. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (COMM DOOR) · airframe 9,629 hrs · 8,854 cycles

DURING MBV INSPECTION, A DENT BEYOND MANUAL LIMITS WAS FOUND UNDER THE COMM DOOR ON THE FORWARD FUSELAGE. REPAIRED DENT ON FORWARD FUSELAGE UNDER COMM DOOR PER EMB SRM -145/1142 REV 38 CHAPTER 53-11-01. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,629 hrs · 8,854 cycles

DURING MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS AT FRAME 20. REMOVED CORRODED AREA AND REPLACED PER. EMB SRM CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAILED (SPOILERS) · airframe 8,640 hrs · 7,930 cycles

SPOILER FAIL MESSAGE, ABORTED TAKEOFF AT 50 KNOTS. REMOVED AND REPLACED RELAYS K0059, K0112, K4363 AND K4363 IAW EMB AMM 20-13-02 AND OPERATIONAL CHECKED IAW AMM 37-63-01 WITH NO DEFECTS. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (ZONE 100) · airframe 8,641 hrs · 7,932 cycles

RECEIVED SPOILER FAIL MESSAGE AT 50 KNOTS, ABORTED TAKEOFF. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB AMM 27-63-02. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SWITCH — FAILED (ZONE 700) · airframe 8,614 hrs · 7,932 cycles

SPOILER FAIL MESSAGE, ABORTED TAKEOFF AT 50 KNOTS. REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEEL SWITCH IAW EMB AMM 32-63-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 8,631 hrs · 7,918 cycles

RECEIVED SPOILER FAIL MESSAGE AFTER FLAPS RETRACTED ON CLIMB-OUT, FAIL MESSAGE WENT AWAY AFTER FLAPS 22 SELECTED ON APPROACH. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB AMM 27-63-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,576 hrs · 6,937 cycles

NUMBER 2 EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED NUMBER 2 EMERGENCY LIGHTING POWER SUPPLY IAW AMERICAN EAGLE WORK CARD 33-700-19. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: WIRE — BURNED (COCKPIT)

IN FLIGHT HAD SMOKE COMING FROM FLIGHT OFFICERS YOKE CHARTHOLDER AREA, SMOKE LASTED ONLY A FEW SECONDS. FOUND WIRES ON UNDERSIDE OF CHARTHOLDER BURNED. REPAIRED DAMAGED WIRES. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. (M)

Part: RHEOSTAT — BURNED (COCKPIT)

SMOKE REPORTED IN THE COCKPIT COMING FROM BEHIND THE FIRST OFFICERS GLARESHIELD. SMOKE WAS VISIBLE ELECTRICAL SMOKE. REMOVED AND REPLACED FIRST OFFICERS CHART HOLDER RHEOSTAT IAW EMB AMM 20-13-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ORD - FLT 4048 - MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 1, NR 2, NR 3 AND NR 4 EMERGENCY LIGHT BATTERIES, IAW EMB AMM 33-50-04 AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREAS TO REMOVE THE DAMAGE. APPLIED ALODINE, EPOXY PRIMER AND POLYURETHANE TOP COAT TO THE REWORKED AREAS. FABRICATED 3 REPAIR DOUBLERS. REPAIR DONE IAW SRM. (K)