N856AE

Part: UPLOCK — FAULTED (MLG) · airframe 33,936 hrs · 31,110 cycles

LOUD THUMPING NOISE COMING FROM NOSE SECTION OF AIRCRAFT UNDERNIETH MAYBE IN THE NOSE CONE RADOM. GEAR WAS UP IN THE GEAR WELL."TRANSFERRED TO NRWC 856-LGA-03250"-C/A-SUSPECTED LH AND RH MLG UPLOCK BOXES TO BE FAULTY REMOVED AND REPLACED LH AND RH MLG UPLOCK BOXES IAW AMM 32-33-10. PERFORMED OPERATIONAL CHECK EXTENISON AND RETRACTION AS PER AMM 32-30-00 & FUNCTIONAL CHECK OF LDG EMERGENCY EXTENSION PER AMM 32-34-00. OPS CHECK GOOD. NO DEFECTS NOTED/NO LEAKS. UPLOCK BOX ASSY P/N 2309-2900-401 S/N 1315 RH

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 33,624 hrs · 30,824 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. -C/A-CLEANED & LUBRICATED MAIN DOOR ROLLER & CHECK OK IAW MM 52-18-00.

Part: LIGHT — INOPERATIVE (MAIN DOOR) · airframe 33,592 hrs · 30,786 cycles

FOUND MAIN-DOOR EMERGENCY LIGHT TO BE INOP DURING PS-1 CHECK-C/A-REMOVED AND REPLACED MAIN-DOOR EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-06. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,343 hrs · 30,508 cycles

GREEN LIGHT FLOOR EMERGENCY PROXIMITY STRIP FAILS TO ILLUMINATE NEXT TO SEAT 2A AND 3A.-C/A-EMERGENCY FLOOR PROX STRIP AT 2A AND 3A DEFERRED PER MEL 33-30.

Part: CRADLE — CRACKED (HANDSET) · airframe 33,191 hrs · 30,358 cycles

FA FORWARD HANDSET CRACKED. R&R AFT F/A CRADLE IAW AMM 23-31-03, OPS CHECK GOOD.

Part: HANDSET — CRACKED (CABIN) · airframe 33,188 hrs · 30,356 cycles

FA FORWARD HANDSET CRACKED. SWAPPED FORWARD WITH AFT, AFT FA HANDSET ON MEL. M PROCEDURES C/W.

Part: STRUT — LOW (LT MLG) · airframe 32,477 hrs · 29,704 cycles

RTF LDG GEAR DISAGREE. AFTER ROTATION DURING GEAR RETRACTION, LG/LVR DISAGREE MESSAGE ON EICAS FOLLOWED SHORTLY BY ENG 1-2 REV DISAGREE. GEAR SHOWED 3 WHITE UP INDICATIONS AND SEEMED TO OPERATE NORMALLY. MESSAGES EXTINGUISHED ONCE THE GEAR WAS EXTENDED. SERVICED LT MAIN LANDING GEAR STRUT IAW AMM 32-10-02

Part: ENGINE — ODOR (BOTH) · airframe 31,881 hrs · 29,028 cycles

MUSTY ODOR AFTER TL TO THRUST SET POSITION ON TAKEOFF ROLL. AT 500 FT HAD A LAVATORY SMOKE WARNING MESSAGE. FA REPORTED SMOKE IN CABIN, RETURNED FOR LANDING. FA REPORTED THE SMOKE ODOR DISAPATED BY THE TIME OF FINAL APPROACH. REMOVED AND REPLACED BOTH ENGINES.

Part: ACM — FAILED (AC BAY) · airframe 31,881 hrs · 29,027 cycles

RECEIVED "LAV SMOKE" INDICATION AT APPROXIMATELY 800 AFL IN CLIMB THERE WAS A SMOKE SMELL IN CABIN NORMAL LANDING NOT OVERWEIGHT. "TRANSFERRED TO NRWC 856-DFW-02713" REMOVED AND REPLACED RT ACM IAW AMM 21-51-03. OPS CHECK GOOD. 30 MINUTE OF PACK 2 ON APU LEAVES NO SMELL IN CABIN OR LAV.

Part: BALLAST — FAILED (LAVATORY LIGHTS) · airframe 31,781 hrs · 28,897 cycles

CLIMBING THROUGHT 8000 FT, AFTER TAKE OFF, RECEIVED A LAVATORY SMOKE EICAS WARNING. F/A DID NOT SEE SMOKE BUT SMELLED UNUSUAL FUMES. RETURNED TO DEPARTURE. SMELLED FUMES IN COCKPIT ON FINAL. REMOVED AND REPLACED THE LT LAVATORY BALLAST IAW AMM 33-28-02. OPS CHECKED GOOD.

Part: BEAM — DAMAGED (FRAMES 60-62) · airframe 31,632 hrs · 28,688 cycles

PREVIOUS REPAIR FWD OF FR 61 ON LAVATORY CENTER BEAM ELONGATED HOLE DAMAGED. PERFORMED A REPAIR IAW ERS-EM-53MR-2868.

Part: FRAME — CRACKED (FR 23) · airframe 31,632 hrs · 28,688 cycles

FRAME 23 CRACKED AT RIVET HOLE BETWEEN STRINGERS 15 - 16R. REPAIRED THE FRAME IAW SRM 53-00-04, ITEM 3, FIG 201.

Part: LIGHT — DAMAGED (CABIN) · airframe 31,632 hrs · 28,688 cycles

NR 2 LT EMERGENCY LIGHT STRIP DAMAGED AT THE WIRE HOLE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 31,632 hrs · 28,688 cycles

NR 6 EMERGENCY LIGHT STRIP DAMAGED ON THE END. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 31,632 hrs · 28,688 cycles

NR 5 LT EMERGENCY LIGHT STRIP DAMAGED AT THE WIRE HOLE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: STRUCTURE — GOUGED (PAX DOOR) · airframe 31,632 hrs · 28,688 cycles

AFT EDGE OF PAX DOOR LOWER AREA IS GOUGED. REPAIRED IAW ERS-EM-52MR-797.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 31,528 hrs · 28,592 cycles

FA REPORTED THE MAIN DOOR DIFFICULT TO OPEN, FEELS LIKE THE HANDLE IS CATCHING OR HAS MORE RESISTANCE TO OPEN THAN USUAL. CLEANED AND LUBED MAIN CABIN DOOR IAW AMM 52-10-00. OPS CHECKED GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 31,490 hrs · 28,552 cycles

AUTOPILOT FAILED DURING GO AROUND, WITH UP & DOWN DRAFT OVERSPEED INDICATION FOR ABOUT 3 MINUTES. PERFORMED A PHASE I INSPECTION IAW AMM 05-50-04, SUB TASK 212-002-A. NO DEFECTS NOTED

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 31,166 hrs · 28,230 cycles

AFT CABIN FLASHLIGHT CRADLE IS BROKEN. REMOVED AND REPLACED THE CRADLE IAW AMM 33-50-16.

Part: PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,960 hrs · 28,054 cycles

PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT PANEL ASSY, IAW AMM 25-23-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,083 hrs · 27,212 cycles

MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R LAMP IN MAIN DOOR EMER LIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 29,236 hrs · 26,244 cycles

CAPTAINS FLASHLIGHT WILL NOT CHARGE. TRIED 2 DIFFERENT HOLDERS. FOUND FLASHLIGHT BULB ASSEMBLY DAMAGED. R & R LAMP ASSEMBLY IAW CMM 25-60-02. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT ASSY — BROKEN (COCKPIT) · airframe 29,236 hrs · 26,244 cycles

WHILE TROUBLESHOOTING FLASHLIGHT PIREP, FOUND CAPTAIN'S FLASHLIGHT CRADLE BROKEN. R & R HOLDER IAW AMM 33-50-16.

Part: UNKNOWN — SMOKE (CABIN) · airframe 29,091 hrs · 26,081 cycles

AFTER TAKEOFF SMOKE IN THE CABIN, FOLLOWED BY LAVATORY SMOKE EICAS WARNING. COMPLIED WITH ETN EM 72-034 & FIRST STEPS OF ENG GROUP WORK SCOPE. ALTHOUGH INITIAL TESTS PRODUCED A ODOR SUBSEQUENT RUNS IAW ETN EM 72-034 & FIM TASKS PRODUCED NO ODOR. ALL FIM TASKS HAD NO DEFECTS NOTED. COMPLIED WITH EMB FIM TASK 34-22-00-810-835-A. NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,351 hrs · 25,335 cycles

DURING PS 2 CHECK, FOUND MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW MM 33-50-10. OPS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,301 hrs · 25,279 cycles

FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 27,852 hrs · 24,851 cycles

IMMEDIATELY AFTER ROTATION RECEIVED A LG AIR & GND FAIL CAUTION MSG & COULD NOT RAISE THE LG, MSG EXTINGUISHED UPON TOUCHDOWN. R & R NOSE GEAR WEIGHT ON WHEELS SWITCH. OPERATIONS CHECKED GOOD IAW AMM CH 32-63-02 & 32-63-05, PN DIFFERENCE CC JY, 192395.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 27,765 hrs · 24,772 cycles

COCKPIT OVERHEAD EMER LIGHT INOPERATIVE. R & R COCKPIT OVERHEAD EMER LIGHT LAMP IAW AMM 33-50-05-000-801-A & 33-50-05-400-801-A. OPERATIONS CHECKED GOOD.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 27,753 hrs · 24,761 cycles

FUEL PIPE SUPPORT BRACKET AT RT WING RIB 3 BENEATH 631AB IS CRACKED. REMOVED & INSTALLED NEW FUEL PIPE SUPPORT BRACKET IAW AMM 20-10-01.

Part: WEB — CRACKED (LT MLG WW) · airframe 27,753 hrs · 24,761 cycles

LEFT MLG AFT GEAR WELL WEB HAS A 1 INCH LONG CRACK. R & R LT MLG AFT GEAR WELL WEB IAW SRM 51-40-02.

Part: ATTACH BRACKET — CRACKED (LT PYLON) · airframe 27,753 hrs · 24,761 cycles

LEFT ENG PYLON FWD PRE-COOLER ATTACHMENT BRACKET IS CRACKED. R & R LT ENG FWD PRE-COOLER ATTACH BRACKET ETN EM-54-056.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

CLIP ON THE AFT EDGE OF THE SERVICE DOOR SILL OTBD FLOOR SUPPORT HAS 1/8 INCH CRACK. INSTALLED NEW CLIP ON THE AFT EDGE OF THE SERVICE DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 27,753 hrs · 24,761 cycles

FUEL PIPE SUPPORT BRACKET AT RT WING BENEATH 631AB IS CRACKED. REMOVED & INSTALLED NEW FUEL PIPE SUPPORT BRACKET IAW AMM 20-10-01.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 27,753 hrs · 24,761 cycles

FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH 531AB IS CRACKED. R & R FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH PANEL 531AB IAW AMM 20-10-01.

Part: FIREWALL — CRACKED (APU BAY) · airframe 27,753 hrs · 24,761 cycles

APU FIRE WALL IS CRACKED AT THE LOWER LT MOUNT AREA, THE UPPER LT MOUNT & THE LOWER RT MOUNT AREA. 3 CRACKS TOTAL APPROX 4.5 INCHES IN LENGTH. COMPLIED WITH PART B & C OF EO EM-53AD--1883 R4.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 27,753 hrs · 24,761 cycles

FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH 531AB IS CRACKED. R & R FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH 531AB IAW AMM 20-10-01.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 27,753 hrs · 24,761 cycles

RIGHT ENG TR LOWER DOOR SKIN HAS A CRACK AROUND A RIVET AT THE OTBD CORNER. REPAIRED IAW SRM 54-30-01 FIGURE 207.

Part: ATTACH BRACKET — CRACKED (RT PYLON) · airframe 27,753 hrs · 24,761 cycles

RIGHT ENG PYLON FWD PRE-COOLER ATTACHMENT BRACKET IS CRACKED. REPLACED PRE-COOLER ATTACH BRACKET IAW SRM 51-40-02.

Part: BUSHING — LOOSE (LT AILERON) · airframe 27,753 hrs · 24,761 cycles

LEFT AILERON OTBD ACTUATOR ATTACHMENT LUG HAS BOTH HAT BUSHINGS LOOSE OR MIGRATING. LT AILERON OTBD HAT BUSHING ON THE DAMPER FITTING IS LOOSE IN THE FITTING BORE. R & R LT AILERON PCA FITTING & THE DAMPER FITTING IAW EO EM-27MR-112. FITTING PN 145-69382-609.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

LEFT UPPER ATTACHMENT ANGLE IS CRACKED 1/2 INCH BY A RIVET BETWEEN FRAMES 48 - 49. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R LT UPPER ATTACHMENT ANGLE BETWEEN FRAMES 48 - 49 IAW SRM 53-23-12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

FRAME 23 IS CRACKED AT STRINGER 15R. COMPLETED REPAIR IAW E0-EM-53MR-1808.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

LEFT LOWER ATTACHMENT ANGLE NR 1 IS CRACKED ON THE LE APPROX 2 INCHES LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. REPLACED DAMAGED LT LOWER ATTACHMENT ANGLE NR 1 ON LE IAW ETN EM-53-142.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

RIGHT VERTICAL STAB TO FUSELAGE SUPPORT ANGLE IS CRACKED IN 2 AREAS NEAR FRAME 76 RT. REPLACED RT VERTICAL STAB TO FUSELAGE FWD SUPPORT ANGLE IAW EO EM-53MR-1281.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

RIGHT LOWER ATTACHMENT ANGLE NR 2 IS CRACKED ON THE LE APPROX 3/8 INCHES LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R RT LOWER ATTACHMENT ANGLE NR 2 IAW ETN EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

LEFT LOWER ATTACHMENT ANGLE NR 2 IS CRACKED ON THE LE APPROX 1 INCH LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R LT LOWER ATTACHMENT ANGLE NR 2 FOR THE LATERAL WING TO FUSELAGE FAIRING IAW SRM 51-40-02 & ETN EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,753 hrs · 24,761 cycles

RIGHT LOWER ATTACHMENT ANGLE NR 3 IS CRACKED ON THE LE APPROX 1/2 INCH LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R RT LOWER ATTACHMENT ANGLE NR 3 IAW ETN EM-53-142.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 27,535 hrs · 24,594 cycles

REF ITEM NR 1 LOG PAGE 3653889 IAW REPEAT DESK NR 2 FAN AIR VLV NEEDS TO BE REPLACED. BLEED 2 OVER TEMP EICAS MSG & BLEED 2 POINTER IN RED RANGE. R & R NR 2 FAN AIR VLV IAW AMM 36-11-03, DID NOT FIX. SEE PIREP NR 1 LOG PAGE 3653889.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,206 hrs · 24,316 cycles

MAIN DOOR EXTERNAL EMER LAMP INOPERATIVE. R & R EMER LAMP ON MAIN DOOR HINGE IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,064 hrs · 24,197 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,773 hrs · 23,963 cycles

AFT EMER FLOOR PROX LIGHT INOPERATIVE. R & R AFT FLOOR PROX LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,747 hrs · 23,942 cycles

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

Part: ENGINE — LEAKING (NR 1) · airframe 26,685 hrs · 23,887 cycles

SMOKE IN CABIN & LAVATORY, OIL SMELL. LAVATORY SMOKE INDICATOR ON EICAS. PERFORMED ETN-EM-72-034 ENG ODOR EVENT. TROUBLESHOOTING SUPPLEMENT. FOUND SMOKE SMELL ASSOCIATED WITH NR 1 ENG. PERFORMED BORESCOPE OF NR 1 ENG FLOW PATH EXTENSION IAW ETN-EM-79-014. FOUND OIL WETTING OF BOLT HEADS. ENG REQUIRES REPLACEMENT IAW ITEM NR 3 BELOW.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 26,685 hrs · 23,887 cycles

DUCT FROM PYLON TO START CONTROL VLV CRACKED. R & R DUCT IAW ENG CHANGE WC 71-000-00. LEAK CHECKED GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 26,515 hrs · 23,744 cycles

OILY SMELL IN COCKPIT & CABIN DURING HIGH POWER SETTING. PERFORMED ENG RUNS IAW ETN-EM-72-034 R9. NO DETECTABLE SMELL NOTED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,906 hrs · 23,167 cycles

FIRST OFFICER`S FLASHLIGHT HOLDER BROKEN. R & R FIRST OFFICER`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 25,770 hrs · 23,039 cycles

EMERGENCY LIGHT ON THE FLOOR COMING LOOSE AT SEAT ROW 8A. R & R EMERGENCY LIGHTNING FLOOR SIDE WALL ASSEMBLY AT ROW 8A IAW AMM 33-50-12. EMERGENCY LIGHT OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — BROKEN (CABIN) · airframe 25,770 hrs · 23,039 cycles

EMERGENCY LIGHTNING STRIP AT SEAT ROW 6A EMERGENCY LIGHT COMING APART. R & R EMERGENCY LIGHTNING FLOOR SIDE WALL ASSEMBLY IAW AMM 33-50-12. EMERGENCY LIGHT OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: RELAY — FAILED · airframe 25,595 hrs · 22,874 cycles

BOTH ENGINES STARTED FOR TAXI OUT, SHUT DOWN NR 2 ENG TO SAVE FUEL. WHEN NR 2 ENG SHUT DOWN WE IMMEDIATELY GOT, RUD HDOV PROT FAIL & E2 SHORT DISP ON EICAS RTG. R & R RT RELAYS KO774, K0112 & K0384 IAW EMB AMM 20-13-02 ENGINE RUN REQUIRED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,881 hrs · 22,207 cycles

F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 24,273 hrs · 21,624 cycles

CREW REPORTED CAPTAIN’S FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW MM SP 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 23,662 hrs · 21,095 cycles

ON FLIGHT 4076 THE CREW REPORTED THE FLASHLIGHT HOLDER AT FIRST OFFICER’S RIGHT LEG DOES NOT HOLD FLASHLIGHT IN CRADLE SECURELY. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED AT THIS TIME, MEL RESTORED END. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 23,522 hrs · 20,955 cycles

FLIGHT 4531, CREW REPORTED AFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW MM 33-50-16. OPS CHECKED WAS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,302 hrs · 20,727 cycles

DURING B INSPECTION FOUND THE UPPER ARM OF EMERGENCY FLASHLIGHT HOLDER BEHIND CAPTAINS SEAT HAS COMPLETELY BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT HOLDER BEHIND CAPTAINS SEAT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,233 hrs · 20,663 cycles

FOR FLIGHT 4514 MAINTENANCE CHECKED FOR SUSPECTED BIRD INGESTION. BIRD ODOR WAS NOTED IN THE CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH BIRD STRIKE INSPECTION WORK CARD 05-200-07. NO SIGN OF INGESTION AND NO DAMAGES NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,088 hrs · 20,524 cycles

ON FLIGHT 4467 THE CREW REPORTED THE ECS SYSTEM SMELLED OF OIL. INSPECTED AND VERIFIED THE SMELL IS FROM NR 1 THE AIR CYCLE MACHINE NOT FROM ENGINE OR APU BLEED SOURCES. PERFORMED ENGINE RUNS PER EMB MM 72-00-00. NR 1 AIR CYCLE MACHINE DEFERRED PER (EMB) AEA MEL. INSPECTED NR 1 AIR CYCLE MACHINE AND RAN UP ENGINES TO TROUBLESHOOT SMELL IAW FIM TASK 21-20-00-810-801-A AND 72-00-00-810-808A. FOUND NO ODOR SMELL DURING RUN-UP. THE OPERATIONAL CHECK OF NR 1 AIR CYCLE MACHINE WAS GOOD IAW EMB AMM 21-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,871 hrs · 20,322 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED AT STRINGER 15 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (CABIN) · airframe 22,872 hrs · 20,323 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT NR 2 EMERGENCY LIGHT EXTRUSION CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE LEFT NR 2 EMERGENCY LIGHT EXTRUSION IAW AMM 33-50-12. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 22,872 hrs · 20,323 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHTING SYSTEM POWER SUPPLY NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE NR 1 EMERGENCY LIGHTING SYSTEM POWER SUPPLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,872 hrs · 20,323 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT STRIP NR 5 HAS A BROKEN WIRE AT BASE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE LEFT EMERGENCY LIGHT STRIP NR 5 IAW AMM 33-50-12. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — WEAK (CABIN) · airframe 22,871 hrs · 20,322 cycles

DURING MAINTENANCE INSPECTION FOUND THE BATTERY WEAK/LIGHTS ON EMERGENCY LIGHT STRIPS BY ROWS 8-10 GO OUT AFTER SHORT TIME WITH EMERGENCY LIGHTS TURNED ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — WEAK (CABIN) · airframe 22,872 hrs · 20,323 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP IN CABIN BY SEAT ROW 8, 9 & 10 WOULD COME ON AND FADE OFF WHEN EMERGENCY LIGHTS WERE TURNED ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED EMERGENCY BATTERY NR 3 IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 22,579 hrs · 22,579 cycles

FOR FLIGHT 3007 ON THE ON PREFLIGHT THE CREW FOUND THE COCKPIT FLASHLIGHT ON/OFF SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB 140 AMM CHAPTER 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 22,228 hrs · 19,672 cycles

ON FLIGHT 2868, THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT CHARGER WAS DAMAGED AND DOES NOT HOLD THE FLASHLIGHT SECURELY IN PLACE FOR CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY AS PER EMB AMM 25 60 00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,104 hrs · 19,579 cycles

DURING MAINTENANCE INSPECTION, FOUND THE NR 3 EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT IAW 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 20,897 hrs · 18,351 cycles

FOR FLIGHT 3068 THE CREW REPORTED THAT AFTER PUSHBACK PRIOR TO ENGINE START RECEIVED A BAGGAGE EXTINGUISH RED LIGHT FOLLOWED BY AN EICAS "BAGG SMOKE" THE BAGGAGE EXTINGUISH BUTTON WAS PRESSED. AN EMERGENCY WAS DECLARED AND THE FIRE DEPARTMENT WAS CALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. NO FIRE PRESENT. REMOVED AND REPLACED SMOKE DETECTOR IAW ERJ-140 AMM 26-15-01 (CARGO). PART NUMBER: 473597-13. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 19,227 hrs · 16,498 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CENTER BEAM FORWARD OF FRAME 61 TO HAVE AN ELONGATED HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED CUT OUT OF DAMAGED AREA ON THE LAVATORY CENTER BEAM AND INSTALLED REPAIR PARTS ON LAVATORY CENTER BEAM IAW EO EM-53MR-1817. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,227 hrs · 16,498 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED AT STRINGER 15 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FR23 IAW EO EM-53MR-1813. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT BRACKET — CRACKED (DOOR) · airframe 19,227 hrs · 16,498 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EQUIPMENT BAY DOOR 272DR HAD CRACKS AROUND MOUNT PIN BRACKET RIVETS. FIVE CRACK LENGTHS: 2, .3, .25, .2, .1. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EQUIPMENT BAY DOOR 272DR IAW EO: EM-52MR-285. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: A/C PACK — ODOR (NR 1) · airframe 19,106 hrs · 16,364 cycles

FLIGHT 3067 WHILE AT GATE CREW REPORTED, DETECTED AN UNUSUAL ODOR WHICH WAS THOUGHT DUE TO CABIN CLEANING. DURING ENGINE SPOOL-UP FOR TAKEOFF ODOR BECAME STRONGER & COULD BE DETECTED THROUGHOUT CABIN. AT 90 KAIS EICAS PRESENTED "PACK 1 OVHT". TAKEOFF ABORTED. ODOR WAS NOT ELECTRICAL. ODOR SIMILAR TO DEAD ANIMAL. ACFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF CABIN LIGHTS, NO DISCREPANCIES NOTED. INSPECTED ALL VISIBLE AIR CON DUCTING, NO DISCREPANCIES NOTED. PERFORMED ENGINE RUNS PER ETN EM-72-034R4. FOUND PACK 1 TO HAVE AN ODOR. PACK 1 OVERHEAT ON EICAS DISPLAYED DURING RUNS. PERFORMED LT PACK (AIR CON) OPS CHECKED IAW AMM 21-20-00. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 18,869 hrs · 16,099 cycles

ON FLIGHT 3118 THE CREW REPORTED THAT ON SELECTING TAKEOFF THRUST (ALT T/O-1) EXPERIENCED SMOKE AND FUMES IN COCKPIT OUT OF THE AIR CONDITIONING VENTS (SMELLED LIKE BURNT OIL). THE FLIGHT ATTENDANT REPORTED HAZE AND FUMES IN CABIN ALSO. THE SMOKE AND FUMES DISSIPATED IMMEDIATELY WHEN THRUST LEVERS RETURNED TO IDLE. ABORTED TAKEOFF AND RETURNED TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THIS AIRCRAFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLT & FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT. R & R NR 1 ENGINE IAW WORK CARD 71-000-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,125 hrs · 15,146 cycles

DURING MAINTENANCE INSPECTION FOUND MID CABIN CEILING FORWARD EMERGENCY EXIT LOCATOR SIGN TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT DC/AC INVERTER IAW ERJ 140 AMM 33-50-11. THE OPERTIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 18,493 hrs · 15,020 cycles

ON FLIGHT 4122 THE FLIGHT ATTENDANT REPORTED THAT THE MAIN CABIN DOOR HANDLE WAS DIFFICULT TO ROTATE IN BOTH DIRECTIONS. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR RUBBER TRIM AND FRAME RUBBER SEAL IAW EMB AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,667 hrs · 12,661 cycles

DURING MAINTENANCE INSPECTION, FOUND THE AFT NR 2 EMERGENCY LIGHT ON CEILING INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY POWER SUPPLY IAW AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

HALF OF CABIN EMERGENCY LIGHTS INOP DISC, AWAITING LOG PAGE FOR ACTUAL DISC.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,528 hrs · 8,610 cycles

AFT HALF OF CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB-140 AMM 33-50-04. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: APU — LEAKING · airframe 10,389 hrs · 8,506 cycles

OIL SMELL WITH BLEEDS ON. FOUND APU LEAKING OIL AND PLACED THE APU ON MEL. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED APU IAW AE WORKCARD 49-800-05 MEL RESTORED

Part: OIL SYSTEM — LEAKING (APU) · airframe 10,389 hrs · 8,506 cycles

OIL ODOR WITH BLEEDS ON. FOUND APU LEAKING OIL AND PLACED THE APU ON MEL.

Part: AIR DATA MODULE — FAILED (ZONE 100) · airframe 9,828 hrs · 8,055 cycles

RECEIVED AIR SPEED AND SPS ADVANCE WARNING MESSAGES WITH BURNT SMELL IN THE FLIGHT DECK, RETURNED TO DFW. REMOVED AND REPLACED NUMBER TWO AIR DATA COMPUTER AND ISIS IAW EMB AMM 34-01-01. OPERATIONAL CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: PRESSURE SWITCH — FAILED (ZONE 400) · airframe 9,491 hrs · 7,826 cycles

ENGINE ONE HYDRAULIC PUMP FAIL MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 HYDRAULIC ENGINE DRIVEN PUMP PRESSURE SWITCH IAW EMB 29-10-19. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE

Part: CHARGER — FAILED (CABIN) · airframe 9,438 hrs · 7,792 cycles

AFT EMERGENCY LIGHTS INOPERATIVE OVERWING. REMOVED AND REPLACED BATTERY PACK AND CHARGER IAW CRJ AMM 33-51-17. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (FR 11)

THE FUSELAGE SKIN JUST AFT OF FRAME 11 AND BETWEEN STRINGERS 20L AND 21L WAS FOUND TO BE DENTED. REMOVED THE DAMAGED SKIN BY MAKING A CUT OUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW EMB SRM, SRM 145 1142 REV 30, CHAPTERS 53-10-01. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE SERVICE DOOR TO REMOVE CORROSION. FABRICATED TWO DOUBLERS FOR REPAIR. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-21-02. (M)