N854AE

Part: FAN — INOPERATIVE (E/E BAY) · airframe 33,976 hrs · 30,938 cycles

SMOKE IN COCKPIT ON DEPARTURE ELECTRIC SMELL IN C/P / CABIN. EMERGENCY DECLARED CHG EQ. FLT CONT. " TRANSFERRED TO NRWC 854-DFW-03157"WHILE PERFORMING GVI FOR SMOKE/ABNORMAL SMELL IN THE CABIN/COCKPIT FOUND LFWD ELECTRONIC COMPARTMENT FAN INOP.-C/A-RAR LFWD ELECTRONIC COMPARTMENT FAN IAW EMB 140 AMM 21-26-02. OPC CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,531 hrs · 30,475 cycles

UPON PS-1 CHECK FOUND PASSENGER COMPARTMENT REAR FLOOR LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED REAR FLOOR LIGHT STRIP IAW AMM 33-50-12. OPS CHECK FAILED, FOUND BAD CONNECTION AT CRIMP, BROKEN CRIMP. T/S THE REAR EMERGENCY LIGHT FLOOR STRIP, FOUND CONNECTORS MISSING. FOUND SPLICES SP9212 AND SP9213 TO BE MISSING. INSTALLED SPLICES SP9212 AND SP9213 IAW SRM 20-21-00. NO FIX. REMOVED AND REPLACED THE NR 8 FLOOR PROXIMITY STRIP LIGHT IAW 33-50-12-000-801-A AND 33-50-12-400-801-A. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,126 hrs · 30,113 cycles

FLOOR PROX LIGHTS 6,7,AND 8 INOP. T/S PER WM 33-50-50, R & R #6 INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPC GOOD END

Part: PRESSURE SWITCH — INOPERATIVE (BRAKE SYSTEM) · airframe 33,014 hrs · 29,990 cycles

PARKING BRAKE DIDN T HOLD AFTER GRD CREW PULLED THE TUG. C/A-PERFORMED OPERATIONAL CHCK OF PARKING BRAKE PRESSURE PRESSURE SWITCH INOP PER LG PAGE 440451 ITEM 1 MEL AND IAW AMM 32-44-07.

Part: CONNECTOR — BROKEN (CABIN) · airframe 32,558 hrs · 29,582 cycles

SUPPLEMENTAL FLOOR PROXIMITY STRIP ON LAST ROW HAS A BROKEN WIRE AND DOES NOT ILLUMINATE. C/A-ITEM DEFERED PER MEL 33-30, AUTH 020987-C. NO M PROCEDURES. REMOVED ROW 16,17 FLOOR STRIP IAW AMM 33-50-12-000-801-A. REPAIRED BROKEN CONNECTOR IAW WM 33-50-50 REINSTALLED STRIP IAW AMM 33-50-12-400-801-A. OPC GOOD MEL RESTORED.

Part: DOOR SEAL — LACK OF LUBE (CABIN DOOR) · airframe 32,369 hrs · 29,430 cycles

EXTREMELY LOUD NOISE (SCREECHING) COMING FROM MAIN CABIN DOOR ON CLIMB OUT. FA CALLED US AT 060. NOISE SUBSIDED AS WE LEVELED OFF AT LL 120. PERFORMED CABIN PRESSURIZATION UP TO 4.0 PSI IAW AMM 21-31-00. PERFORMED LUBRICATION OF PAX DOOR SEALS IAW MAINTENANCE PRACTICES. FOUND NO LOUD NOISE OR SCREECHING NOISE COMING FROM MAIN PAX DOOR. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,022 hrs · 29,046 cycles

FOUND EMERGENCY FLOOR PROXIMITY STRIP AT 14A INOP-C/A-RAR FLOOR PROIMITY STRIP LIGHT AT 14A IAW EMB 140 AMM 33-50-12. OPC GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,936 hrs · 28,978 cycles

DURING OPC OF EMERGENCY LIGHTING SYS. FLOOR STRIPS FROM 3A TO 6A WERE INOP-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT DC/AC INVERTER, OPC GOOD, IAW AMM 33-50-11

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,721 hrs · 28,750 cycles

LT AFT OVERWING EMERGENCY EXIT LIGHT INOP. -C/A-REMOVED AND REPLACED LT AFT OVERWING EMERGENCY EXIT LIGHT IAW 33-50-07, OP CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 76040

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,505 hrs · 28,547 cycles

LEF CABIN FLOOR EMERGENCY LIGHT STRIP NR 3 HAD WIRES BROKEN. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 31,505 hrs · 28,547 cycles

SERVICE DOOR CENTER SILL HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE SERVICE DOOR SILL IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 75) · airframe 31,505 hrs · 28,547 cycles

LEFT UPPER AFT FUSELAGE SKIN WAS CRACKED AT FRAME 75, ABOVE STRINGER 2L. REPAIRED THE SKIN IAW SRM 53-31-01 ITEM 11 FIG 219

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,505 hrs · 28,547 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-COMPLETE:REMOVED LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-10-020-005-A AND FOUND CONNECTOR P8563 TO BE DISCONNECTED. CONNECTED CONNECTOR P8563 AND REINSTALLED LH OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-10-420-005-A. OPERATIONAL CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 31,505 hrs · 28,547 cycles

EMERGENCY FLOOR LIGHT EXTRUSION CRACKED LH #1-#2-#3-#4-#5-#6-#7-C/A-COMPLETE:RAR EMERGENCY FLOOR LIGHT EXTRUSION LH #1-#2-#3-#4-#5-#6-#7 IAW EMB 140 MM 33-50-12

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 31,505 hrs · 28,547 cycles

EMERGENCY LIGHT STRIP CONNECTOR AT PANEL 251DF IS BROKEN.-C/A-COMPLETE:RAR EMERGENCY LIGHT STRIP CONNECTOR AT PANEL 251DF IAW EMB 140 SWPM 20-21-00. EASI# 102. FOR OPERATIONAL CHECK OF EMERGENCY LIGHT SEE BOW 300222.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 31,505 hrs · 28,547 cycles

EMERGENCY EXIT LIGHT LENS CRACKED ON CEILING PANEL 253CLC-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS ON CEILING PANEL 253 CLC IAW CD CMM 25-28-24.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,716 hrs · 27,840 cycles

EMERGENCY FLOOR LIGHTS AT 3A TO 6A INOP-C/A-ADJUSTED EMERG FLOOR LIGHT STRIPS IAW AMM 33-50-12. NO DEFECTS FOUND AT THIS TIME.

Part: LIGHT — UNKNOWN (CABIN) · airframe 29,888 hrs · 26,927 cycles

RIGHT FWD WING EMERGENCY LIGHT IS INOPERATIVE. COMPLIED WITH EMERGENCY LIGHT OPS CHECK IAW AMM TASK 33-50-00-700-801-A. FOUND SYSTEM OK.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 29,745 hrs · 26,776 cycles

STRONG ODOR OF BURNING ELECIRICAL IN COCKPIT, PASENGERS SMELLED THE ODOR FROM 11B. DECLARED EMERGENCY AND LANDED. FA SMELLED BURNING ODOR AS WELL. NO SMOKE WAS SEEN. INSPECTED PACK SYSTEM AND PERFORMED ODOR EVENT WORK CARD IAW ETN-EM-72-034R9, NO ODOR NOTED.

Part: HANDLE — DETACHED (PAX DOOR) · airframe 29,622 hrs · 26,658 cycles

WHILE TRING TO OPEN THE MAIN CABIN DOOR. DOOR HANDLE CAME OFF. REMOVED AND REPLACED MAIN CABIN DOOR HANDLE IAW AMM 52-18-05. OPS CHECKED GOOD.

Part: HANDLE — LOOSE (PAX DOOR) · airframe 29,537 hrs · 26,574 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. INSPECTED AND FOUND INTERNAL DOOR HANDLE TO BE LOOSE. REINSTALLED THE HANDLE IAW AMM TASK 52-18-05. OPS CHECKED GOOD

Part: TERMINAL — DAMAGED (PAX DOOR) · airframe 29,472 hrs · 26,490 cycles

MAIN DOOR WILL NOT OPEN. REMOVED AND REPLACED TERMINAL END ON THE SIDE HINGED MAIN DOOR FOLDING FLAP ACTUATING CAM IAW AMM 52-18-02. OPS CHECKED GOOD. NO DEFECTS FOUND.

Part: TIRE — BLOWN (LT MLG) · airframe 29,199 hrs · 26,177 cycles

LEFT MAIN INBD TIRE BLOWN. R & R NR 2 MLG TIRE IAW WORK CARD 32-700-11.

Part: CONNECTOR — LOOSE (CABIN) · airframe 29,109 hrs · 26,095 cycles

FLOOR EMERGENCY LIGHT 2-3 INOPERATIVE. FOUND LOOSE CONNECTION ON FLOOR STRIP, RECONNECTED. OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,069 hrs · 26,055 cycles

THE SECOND AND THIRD FLOOR EMERGENCY LIGHT STRIPS INOPERATIVE. RESET CIRCUIT BREAKER AND PERFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: BATTERY — SEPARATED (CABIN) · airframe 28,536 hrs · 25,526 cycles

WHILE PERFORMING PS-2 INSPECTION FOUND NR 1 & 2 FLOOR PROXIMITY EMER LIGHT STRIPS INOPERATIVE & GALLEY SERVICE DOOR EMER LIGHTING INOPERATIVE. TROUBLESHOOTING REVEALED THAT THE NR 2 EMER BATTERY HAD BECOME SEPARATED FROM ITS CHARGER & HOLDER ABOVE THE GALLEY SERVICE DOOR. INSPECTED & SECURED BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,439 hrs · 25,435 cycles

FRAME 23 CRACKED BETWEEN STRINGERS 15R - 16R. REPAIRED FRAME 23 IAW EM-53MR-1808.

Part: CONNECTOR — MISSING (CABIN) · airframe 28,439 hrs · 25,435 cycles

FLOOR EMER LIGHT STRIP WIRE AT FRAME 57 IS MISSING CONNECTOR. REPLACED MISSING CONNECTOR AT FLOOR EMER LIGHT STRIP WIRE AT FRAME 57 IAW SWPM 20-00-03 & 20-21-00.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 28,439 hrs · 25,435 cycles

FRAME 68 SHEAR CLIP PREVIOUS REPAIR CORRODED AT LOWER CARGO DOOR CUT OUT. REPAIRED FRAME 68 SHEAR CLIP AT PREVIOUS REPAIR IAW SRM 53-31-04.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 28,439 hrs · 25,435 cycles

FRAME 65 SHEAR CLIP PREVIOUS REPAIR CORRODED AT LOWER CARGO DOOR CUT OUT. REPAIRED FRAME 65 SHEAR CLIP AT PREVIOUS REPAIR IAW SRM 53-31-04.

Part: CONTACTOR — DEFECTIVE (FLASHLIGHT) · airframe 28,409 hrs · 25,410 cycles

FLASHLIGHT AT THE LAVATORY IS NOT SHOWING IT IS CHARGING, THE LED DOES NOT COME ON. R & R CONTACTORS TO WIRES W775-0005-24RD SP3557 & W775-0006-24BK SP3558 FOR FLASHLIGHT AT THE LAVATORY IAW SWPM 20-50-01 & 20-00-03. SYS CHECKED GOOD IAW AMM 33-50-16 STEP 3 I 2.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,409 hrs · 25,410 cycles

RIGHT OMEGA BEAM INBD & OTBD SUPPORTS ARE CRACKED AT FRAME 47. REMOVED CRACKED RT OMEGA BEAM INBD & OTBD SUPPORTS AT FRAME 45 - 52 & INSTALLED SERVICEABLE RT OMEGA BEAM INBD & OTBD SUPPORTS IAW SRM 51-40-02 & 53-23-02.

Part: CASE — CHAFED (EMERGENCY LIGHT) · airframe 28,409 hrs · 25,410 cycles

RIGHT OVERWING PANEL EMER LIGHT ASSEMBLY INTERIOR CASE IS CHAFED. R & R RT OVERWING PANEL EMER LIGHT ASSEMBLY INTERIOR CASE IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 28,409 hrs · 25,410 cycles

NUMBER 2 LT FLOOR EMER LIGHT STRIP WIRE BROKEN. R & R NR 2 LT FLOOR EMER LIGHT STRIP IAW AMM 33-50-12. SEE BOW 216337 FOR INSTALLATION OF PROXIMITY LIGHTS.

Part: STRIP — CRACKED (CABIN) · airframe 28,409 hrs · 25,410 cycles

NUMBER 8 LT FLOOR SIDEWALL STRIP CRACKED. R & R NR 8 LT FLOOR SIDEWALL STRIP IAW AMM 33-50-12. SEE BOW 216337 FOR INSTALLATION OF PROXIMITY LIGHTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,409 hrs · 25,410 cycles

AFT FUSELAGE RT SIDE FRAME 75 HAS POSSIBLE CRACK AT ONE FASTENER. COMPLIED WITH ERS-EM-53MR-2059 RT RFI SKIN CRACKED AT FRAME 75, BETWEEN STRINGER 2R - 3R REPAIR.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,409 hrs · 25,410 cycles

RIGHT OVERWING PANEL EMER LIGHT INOPERATIVE. R & R NR 4 EMER SYS POWER SUPPLY IAW WC 33-700-19. FUNCTIONAL CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,409 hrs · 25,410 cycles

LEFT OMEGA BEAM OTBD SUPPORT IS CRACKED AT FRAME 47. REMOVED CRACKED LT OMEGA BEAM OTBD SUPPORT, BETWEEN FRAME 45 - 50 & INSTALLED LT OMEGA BEAM OTBD SUPPORT IAW SRM 51-40-02.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 28,293 hrs · 25,281 cycles

CONNECTOR FOR EMER LIGHT STRIP ATTACHED TO FLOOR PANEL261 BF IS PULLED OFF WIRE. REPAIRED CONNECTOR FOR EMER LIGHT STRIP ATTACHED TO FLOOR PANEL261 BF IAW SWPM 20-21-00. SEE NRWC 854-ABI-01856 FOR OPERATIONS CHECK. FOUND DURING CLOSE UP.

Part: DOOR SEAL — DEFECTIVE (SERVICE DOOR) · airframe 27,271 hrs · 24,386 cycles

SERVICE DOOR SQUEAL IN FLIGHT WITH VISIBLE GAP. TRANSFERRED TO NRWC 854-DFW-01564. REF ITEM NR 1, NR 2 & NR 3 NRWC 854-DFW-01564. R & R FRAME SEAL IAW 52-43-04. LEAK CHECKED GOOD.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 26,872 hrs · 24,084 cycles

AFTER TAKEOFF IN CLIMB PTRIM MAIN INOPERATIVE, RETURNED TO AIRPORT. CMC POSTED HORIZONTAL STAB CONTROL UNIT FAILURE. REPLACED HSCU IAW AMM 27-40-01. OPERATIONAL TEST CHECKED GOOD. ACFT IS COMPLIANT FOR CONTINUED CAT11 OPERATION.

Part: ACM — FAILED (AC BAY) · airframe 26,636 hrs · 23,845 cycles

DURING CLIMB OUT AT FL 200 VISIBLE SMOKE & A BURNING SMELL WERE PRESENT IN THE CABIN & COCKPIT. FOLLOWED EPC & AOM1 PROCEDURES CONDUCTED EMER LANDING. R & R NR 1 AIR CYCLE MACHINE IAW AMM 21-51-03. OPERATIONS CHECKED GOOD. PERFORMED ETN-EM-72-034 R9. NO DEFECTS NOTED. NO VISIBLE SMOKE OR BURNING SMELL IN CABIN OR COCKPIT NOTED.

Part: DOOR SEAL — DAMAGED (SERVICE DOOR) · airframe 26,077 hrs · 23,279 cycles

FLIGHT ATTENDANT NOTIFIED OF STRONG WHISTLING NOISE FROM THE SERVICE DOOR STARTING AT 11000'. REPAIR SERVICE DOOR SEAL IAW ETN EM-52-024R2. OPERATIONS CHECKED IAW MM-21-31-00 & NO LEAKS NOTED.

Part: STRUT — ICED (NLG) · airframe 25,533 hrs · 22,704 cycles

AFTER TAKEOFF EICAS LANDING AIR & GND FAIL, LT GEAR DOWN & RETURNED TO FIELD. NLG WOW PROXIMITY SWITCH DISAGREE & STRUT COATED WITH 1/4 INCHES ICE, DE-ICED ACFT & ALL WOW SWITCHES FCK CHECKED OK IAW AMM 32-63-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,910 hrs · 22,173 cycles

FLIGHT CREW REPORTS THAT FLOOR LIGHTS, EMERGENCY, IN MIDDLE CABIN, COME ON NORMALLY AND THEN FADE TO DIM QUICKLY. R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04, OPS CK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,388 hrs · 20,961 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 23 CRACKED BETWEEN STRINGERS 15R - 16-R. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGED SECTION, SPLICED IN NEW SECTION PER EO-EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (FLASHLIGHT) · airframe 23,437 hrs · 20,998 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN AFT FLASHLIGHT CHARGER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT CHARGER IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 23,195 hrs · 20,789 cycles

FLIGHT 4435, CREW REPORTED A BURNING ODOR IN THE COCKPIT TWICE DURING FLIGHT. THE CREW SMELLED IT IN THE COCKPIT AND CABIN AND THE ODOR LASTED APPROX ONE MINUTE EACH TIME THEN DISSIPATED. SMELLED ELECTRICAL. COM 1 WAS REPLACED IN RDU. AIRCRAFT REMOVED FROM SERVICE. PERFORMED FIM TASK 21-20-00-810-801-A. NO SOURCE FOUND. FUNCTIONAL CHECK FLIGHT FOUND TO BE SATISFACTORY. COMPLIED WITH AIRWORTHINESS RELEASE SIGN-OFF. NO SOURCE FOUND OF ODOR FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — UNKNOWN (CABIN) · airframe 23,102 hrs · 20,702 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY LIGHTING CHARGER ASSEMBLY AND BATTERY NEEDS REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHTING CHARGER ASSEMBLY AND BATTERY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,320 hrs · 20,052 cycles

ON FLIGHT 3279 THE CREW REPORTED A POSSIBLE BIRD IN NR 1 ENGINE. REPORTED THEY COULD NOT SEE ANYTHING ON ENGINE BUT NOTICED AN ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH BIRD STRIKE INSPECTION WORK CARD # 05-200-07 NO EVIDENCE OF E1 INGESTION, OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — CORRODED (LT COWLING) · airframe 22,243 hrs · 19,990 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE LOWER COWL AFT HINGE BOLT SEVERELY CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW BOLT IN LEFT ENGINE LOWER COWLING IAW EMB 140 AMM 71-12-0. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,897 hrs · 19,628 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT SIDE FORWARD LOWER FAIRING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RELAMPED THE LEFT SIDE FORWARD LOWER FAIRING EMERGENCY LIGHT IAW 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,429 hrs · 17,991 cycles

DURING MAINTENANCE BASE VISIT FOUND THE NR 2 EMERGENCY BATTERY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY AND CHARGER IAW EMB-140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,407 hrs · 17,970 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BULB AT SEAT 11B IAW EMB 140 MM 33-50.13. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — BURNED (LEFT) · airframe 19,573 hrs · 17,073 cycles

ON FLIGHT 3822 THE CREW REPORTED THAT DURING CRUISE DETECTED A STRONG ODOR OF SMOKE IN THE COCKPIT AND FRONT OF THE AIRCRAFT CABIN. CONFIRMED ODOR OF SMOKE WITH DEAD HEADING CREW MEMBERS SEATED IN THE MIDDLE AND AFT CABIN. THE CREW PERFORMED SMOKE AND COCKPIT/CABIN PROCEDURES. THE CREW DECLARED AN EMERGENCY AND LANDED IMMEDIATELY DIVERTING TO HDN. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON LANDING, CRASH, FIRE AND RESCUE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF FIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND INOPERATIVE LEFT RECIRCULATION FAN. REMOVED AND REPLACED THE LEFT RECIRCULATION FAN IAW EMB 140 AMM 21-24-01. THE OPERATIONAL CHECK WAS GOOD. NO ODOR FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 17,148 hrs · 14,375 cycles

ON FLIGHT 3071 DURING THE CLIMBOUT THE CREW REPORTED A STRONG OIL ODOR AT 11000 FEET. THE ODOR DECREASED ONCE THE NUMBER 1 PACK WAS TURNED OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 ENGINE IAW 71-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — DEFECTIVE (RT ENGINE) · airframe 17,148 hrs · 14,373 cycles

ON FLIGHT 3038 DURING CRUISE THE CREW REPORTED A VERY STRONG "OIL" ODOR PRESENT IN CABIN AND FLIGHT DECK WITH ENGINE BLEEDS ON IN FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ZERO CARBON SEAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 16,862 hrs · 14,067 cycles

FOR FLIGHT 4397 PRIOR TO FLIGHT THE FLIGHT ATTENDANT WAS HAVING A DIFFICULT TIME CLOSING THE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED THE MAIN DOOR IAW EMB 145 AMM 25-23-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — UNKNOWN (SEAT 3 B/C) · airframe 13,727 hrs · 11,229 cycles

ON FLIGHT 3023 CREW REPORTED EXIT SIGN FWD OF SEAT 3 B/C AND FLOOR PROX STRIPS FORWARD OF ROW 6 ARE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NUMBER 2 IAW EMB -140 AMM 33-50-04, OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT BEAM — CRACKED (FWD FUSELAGE) · airframe 10,767 hrs · 8,945 cycles

ON APPROACH, PASSING THROUGH 210 KTS A HEAVY VIBRATION STARTED THROUGH CONTROL COLUMN. WITH AUTO PILOT ENGAGED, AFTER SLOWING IT WAS NOT AS INTENSIVE. BUT STILL PREVALENT, MEL 2201 APPLIED. REPAIRED CRACKED SUPPORT BEAM FOR AHRS MOUNTS IAW EO EM-53MR-840. AUTOPILOT OPS CHECKS GOOD. FUNCTIONAL CHECK FLIGHT REVEALED NO DISCREPANCIES. MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 9,759 hrs · 8,272 cycles

RIGHT CENTER FUSELAGE II SKIN DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER. INSTALLED IAW EMB SRM 53-22-01, FIGURE 201, SHEET 1. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,759 hrs · 8,272 cycles

CARGO DOOR SILL FOUND CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB SRM 51-20-03 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE.

Part: STRINGER SPLICE — DAMAGED (ZONE 100) · airframe 9,759 hrs · 8,272 cycles

STRINGER 19L SPLICE SECTION BETWEEN FRAMES 23 AND 24 DAMAGED. REMOVED DAMAGE AND INSTALLED NEW SPLICE IAW EMB IC2007-145/0329A. AIRCARFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,758 hrs · 8,272 cycles

SHEAR CLIP AT FRAME 68 LOWER SECTION FOUND CORRODED. REMOVED AND REPLACED SHEAR CLIP IAW EMB IC2007-145/03294A. RETURNED AIRCRAFT TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,758 hrs · 8,272 cycles

SHEAR CLIP AT FRAME 65 LOWER SECTION CORRODED. REMOVED AND REPLACED SHEAR CLIP IAW EMB IC2207-145/03294A. RETURNED AIRCRAFT TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FRAME 25)

THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FRAME 25 LT)

THE LT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FRAME 20)

THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE COROSION BY MAKING A CUT OUT. FABRICATED A FILLER EXTERNAL ANGLE, PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

DFW - FLT 3582 - DUAL PITCH TRIM FAILURE ON LANDING WITH AUTO PILOT ON. DECLARED EMERGENCY AND LANDED WTHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

DFW - FLT 3486 - ON APPROACH INTO DFW GOT PITCH BACKUP WARNING AND PITCH MAIN WARNING. REPLACED HSCU IAW ETN EB-27-022. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)