N830AE

Part: CONTROL PANEL — FAILED (PITCH TRIM) · airframe 36,309 hrs · 33,565 cycles

PTCH TRIM BACK UP INOP DURING CRUSING. PITCH TRIM FAIL MSG. DECLARED EMERG. LANDED SAFELY-C/A-RAR PITCH TRIM CONTROL PANEL IAW EMB 140 AMM 20-13-10. OPC GOOD IAW EMB 140 AMM 27-40-00. NO DEFECTS NOTED.

Part: BRAKE — UNKNOWN (PARKING) · airframe 36,113 hrs · 33,393 cycles

PARKING BRAKE IS NOT WORKING PROPERLY. DIFFICULTY SETTING IT-C/A-PERFORMED OPC OF PARKING EMERGENCY BRAKE IAW EMB 140 AMM 32-44-00. OPC GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: NONE — NONE · airframe 36,091 hrs · 33,376 cycles

BIRD STRIKE ON T/O ROLL ON NOSE CONE AN 2 RH WING LEADING EDGE HIGH SPEED ABORT LESS THAN 110 KT-C/A-C/W BIRD STRIKE INSPECTION WORK CARD 05-200-07 NO DAMAGE NOTED OK FOR SERVICE

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,803 hrs · 33,114 cycles

AFT FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT FLASHLIGHT BATTERY IAW CMM 25-60-11 OPC GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 35,794 hrs · 33,106 cycles

AT 19000 FT DURING ICE PROT PNEUMATIC TEST, BLD 2 LEAK / FA REPORTS LOUD BANG. QRH CLEARED MSG. C/A-REMOVED AND REPLACED RT BLEED JOINT NR 2 O-RING AND REASSEMBLED IAW AMM 36-11-10.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 35,715 hrs · 33,033 cycles

FLAP FAIL ON EICAS CAUTION MESSAGE AFTER SELECTING FLAPS 9 FLAPS STAYED UP. RESET FLAPS SYSTEM IAW FIM TASK 27-51-00-810-801-A, RECEIVED FLAPS AT 9 DEGREES FOR FERRY FLIGHT PERFORMED GVI OF FLAPS NO DEFECTS NOTED. PERFORMED CMC DOWNLOAD IAW AMM 45-45-00, C/W RESISTANCE CHECK AT P11041 IAW FIM 27-51-00 810 805 A. REMOVED AND REPLACED WITH SERVISABLE FECU IAW AMM 27-53-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 35,713 hrs · 33,031 cycles

FLAP FAIL MSF WHEN SELECTING FLAPS 22. RESET SYSTEM C/W OPERATIONAL CHECK IAW E140 AMM 27-51-00-700-801-A. NO FAULTS FOUND. A/C OK FOR SERVICE

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 35,154 hrs · 32,483 cycles

AFT CABIN CREW FLASHLIGHT BASE BROKEN. C/A-REMOVED AND REPLACED CABIN CREW FLASHLIGHT BASE IAW AMM 33-50-16. OPC GOOD.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 33,614 hrs · 31,029 cycles

ADVISORY MESSAGE BLD 2 VLV CLOSED. REMOVED AND REPLACED ENGINE BLEED 2 VALVE IAW AMM 36-11-05. REMOVED AND REPLACED BLEED AIR NR 2 PUSHBUTTON IAW AMM 20-13-04. PERFORMED OPERATIONAL CHECK OF ENGINE NR 2 BLEED VALVE IAW AMM 36-11-05. ALL OPS NML AT THIS TIME.

Part: HYDRAULIC LINE — FAILED (MLG) · airframe 33,234 hrs · 30,674 cycles

HYDRAULIC SYSTEM 1 LOW QUANTITY FOLLOWED BY A RAPID LOSS OF HYDRAULIC FLUID. TRANSFERRED HYDRAULIC FLUID FROM SYS 2 TO SYS 1 IAW ETN-EM-29-023R2. FOUND LT AND RT MLG RETRACT ACTUATOR RETRACT HOSES LEAKING. APPLIED TORQUE TO BOTH HOSES IAW AMM 32-33-08-400-801A STEP 3I(10), NUTS DID NOT MOVE. REMOVED AND REPLACED LT MLG RETRACT ACTUATOR GEAR UP HYDRAULIC HOSE IAW AMM 32-33-08 SUBTASK 020-002-A STEP (1) AND SUBTASK 420-002A STEP (10). LEAK CHK GOOD AT THIS TIME IAW. ERS-EM-2900-014. REMOVED AND REPLACED RT MLG RETRACT ACTUATOR GEAR UP HYDRAULIC HOSE IAW AMM 32-33-08 SUBTASK 020-002-A STEP (1) AND SUBTASK 420-002A STEP (10). LEAK CHK GOOD AT THIS TIME IAW ERS-EM-2900-014.

Part: SELECTOR — FAILED (TE FLAPS) · airframe 33,101 hrs · 30,539 cycles

FLAP INDICATION WHEN SET IN ANY POSITION. COMPLETED A FLAP FAIL CHECKLIST AND PERFORMED NO FLAP LANING. AFTER LANDING FLAPS INDICATED 0 IN FLAPS 22 POSITION. FLAPS UP OUTSIDE AIRCRAFT. REMOVED AND REPLACED THE FLAPS SELECTOR LEVER IAW AMM 27-53-03. COMPLIED WITH AN OPS CHECK, SATISFACTORY AT THIS TIME.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,493 hrs · 29,883 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 6 FASTENERS ON FR 78 RT SIDE BELOW VERTICAL STAB. REPAIRED FUSELAGE SKIN CRACKS ON 6 FASTENERS ON FR78 IAW ERS-EM-53MR-3087.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 32,493 hrs · 29,883 cycles

EMERGENCY LIGHT CONNECTOR HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-00-03, AND 20-21-00.

Part: FRAME — DENTED (FUSELAGE) · airframe 32,493 hrs · 29,883 cycles

DENT ON RT FWD FUSELAGE STRINGER 14R AFT OF RADOME. REPAIRED DENT ON RT FWD FUSELAGE STRINGER 14R AFT OF RADOME IAW ERS-EM-53MR-3107.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,493 hrs · 29,883 cycles

LT OMEGA BEAM OUTBOARD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REPAIRED LEFT OMEGA BEAM OUTBOARD SUPPORT BETWEEN FRAMES 47-48 IAW SRM 53-23-10.

Part: SKIN — CRACKED (FRAMES 77 & 78) · airframe 32,493 hrs · 29,883 cycles

FUSELAGE SKIN CRACKED, FRAME 77 AND 78. REPAIRED THE SKIN IAW ERS-EM-53MR-3709.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 32,493 hrs · 29,883 cycles

LEFT OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW EO-EM-53MR-1518, REV 3.

Part: STOP FITTING — CRACKED (SERVICE DOOR) · airframe 32,493 hrs · 29,883 cycles

SERVICE DOOR FORWARD LOWER STOP BRACKET IS CRACKED. REMOVED AND REPLACED THE SERVICE DOOR FORWARD LOWER STOP BRACKET IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 32,493 hrs · 29,883 cycles

CENTER OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW EO-EM-53MR-1518, REV 3.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,493 hrs · 29,883 cycles

FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R. REPAIRED THE SKIN IAW SRM 53-31-01

Part: DOOR SILL — CORRODED (FRAME 16) · airframe 32,493 hrs · 29,883 cycles

CARGO DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02

Part: RIB — CRACKED (LT ELEVATOR) · airframe 32,493 hrs · 29,883 cycles

LEFT ELEVATOR NOSE RIB ON INBOARD HINGE CUTOUT INBOARD SIDE CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02

Part: STRINGER — DAMAGED (FRAMES 48-50) · airframe 32,493 hrs · 29,883 cycles

STRINGER 13L DAMAGED BETWEEN FRAMES 48 AND 50. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02, AND 51-20-01

Part: CROSSMEMBER — CORRODED (FRAMES 33-34) · airframe 32,493 hrs · 29,883 cycles

CENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 33-34. REMOVED AND REPLACED THE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241.

Part: SUPPORT — CRACKED (FRAMES 47-48) · airframe 32,493 hrs · 29,883 cycles

RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47 - 48. REMOVED AND REPLACED THE SUPPORT IAW SRM 53-23-02.

Part: CROSSMEMBER — CORRODED (FRAMES 24-25) · airframe 32,493 hrs · 29,883 cycles

CENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 24-25. REMOVED AND REPLACED THE CENTER AISLE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,229 hrs · 29,589 cycles

F/O'S FLASHLIGHT HOLDER BROKEN. REMOVED AND INSTALLED F/O'S FLASHLIGHT CRADLE IAW AMM 33-50-16.

Part: LEVER — DEFECTIVE (CARGO DOOR) · airframe 32,174 hrs · 29,529 cycles

BAGGAGE DOOR WARNING SYS MFD/EICAS, BAGGAGE DOOR WARNING ILLUMINATED AFTER TAKEOFF AND EXTINGUISHED AFTER LANDING. RESTORATION OF MEL ITEMS REVIEW THE MEL AND ENSURE APPROPRIATE MAINTENANCE ACTIONS ARE TAKEN TO RESTORE THE ITEM, SYSTEM CONDITIONS AND LIMITATIONS THAT WERE REQUIRED BY THE MEL. DURING DEFERRAL, COMPLY WITH PROCEDURES IN MEL MANUAL 1-06 INCLUDING NOTIFICATION. ENTER FACT INFORMATION INTO FMR RECORD IAW GPM 04-00 AND 16-00. TROUBLESHOT IAW AMM 52-76-01 AND AMM 52-31-00. AFT MICROSWITCH BELLCRANK LEVER AND AFT UPPER LOCK LEVER ON DOOR NEED REPLACEMENT AND RIGGED. R & R AFT BAGGAGE DOOR MICRO SWITCH ACTUATING LEVER. OPC GOOD WITH AND WITHOUT ACFT PRESSURIZED, MEL 52-05.

Part: LEVER — DEFECTIVE (CARGO DOOR) · airframe 31,742 hrs · 29,039 cycles

ON ROLL OUT AT 80KTS, RECEIVED ADVISORY CARGO DOOR OPEN. TAKEOFF ABORTED. RETURNED TO GATE. GND PERSONNEL REVISED DOOR. DOOR INDICATION ON MFD FLICKERING GREEN TO RED & EICAS MSG KEPT DISPLAYING. VERIFIED BAG DOOR CLOSES & LATCHES FLUSH AS REQUIRED IAW MEL 52-05. BAG DOOR INDICATION INTERMITTENT. R & R DAMAGED LEVER ON AFT BAGGAGE DOOR MICROSWITCH & ADJUSTED MICROSWITCH. COMPLIED WITH BAGGAGE DOOR OPERATIONS CHECK IAW AMM 52-76-00 MEL ITEM RESTORED.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 31,498 hrs · 28,732 cycles

BAGGAGE COMPARTMENT SMOKE DETECTOR FAILS FIRE TEST. R & R BAGGAGE COMPARTMENT FWD SMOKE DETECTOR IAW AMM 26-15-01. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 31,372 hrs · 28,605 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-07. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (SPOILER) · airframe 30,544 hrs · 27,699 cycles

SPOILER FAIL MSG PRESENTED. SPOILERS SHOWED OPEN INTERMITTENTLY. RAN INADVERTENT SPOILER OPEN IN FLIGHT CHECKLIST. FLIGHT ATTENDANT DID NOT OBSERVE OPEN SPOILERS. NO CHANGES IN FLIGHT CHARACTERISTICS NOTED. R & R LT INBD SPOILER PROX SWITCH IAW AMM 27-63-04, OPERATIONS CHECKED GOOD. R & R CONNECTOR P1167 IAW SWPM 20-50-01, SPOILERS SYS CHECKED GOOD IAW AMM 27-63-01. AT GATE SHORTLY AFTER POWER UP, SPOILERS RAPIDLY SWITCHED FROM OPEN TO CLOSED INDICATION. REF LOG PAGE 3879476. R & R RT INBD GND SPOILER PROX SENSOR & HARNESS CONNECTOR IAW AMM 27-63-04 & SWPM 20-50-00. OPERATIONS CHECKED GOOD. NO CMC MSG NOTED. PROXIMITY SENSOR PN 8-527-01, SN A8992 POSITION SPL 5.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,371 hrs · 27,526 cycles

HYDRAULIC SYS 1 LO LEVEL IN FLIGHT. LEVEL 3/4 FULL ON GND & AT CRUSE. DECREASED INTO AMBER. HYD LO LEVEL ON EICAS, SUSPECT LEAK. TRANSFERRED HYD FLUID IAW ETN EM-29-023. PERFORMED WALK AROUND INSPECTION NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,058 hrs · 27,211 cycles

IAW PS1 CHECK, RT EXTERNAL EMER LIGHT IS INOPERATIVE. REMOVED & INSTALLED RT EXTERNAL EMER LIGHT IAW AMM 33-50-10.

Part: WIRE — PULLED (CABIN) · airframe 29,966 hrs · 27,128 cycles

LAST EMER LIGHT PROXIMITY STRIP AFT WIRES PULLED FROM SPLICES. R & R SPLICES SP 9502 & SP 9503 IAW SWPM 20-21-00. EMER LIGHT STRIP OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 28,694 hrs · 26,005 cycles

FLIGHT ATTENDANT REPORTS CABIN ENTRY DOOR IS HARDER TO OPERATE WHEN OPENING. CLEAN & LUBED MAIN CABIN DOOR. OPERATIONS CHECKED GOOD IAW SP.

Part: CONTROL MODULE — FAULTY (FIRE DETECTION) · airframe 28,522 hrs · 25,866 cycles

ON TAXI GOT APU FIRE EICAS WHILE APU WAS OFF. PRESSED APU EXT BUTTON IAW CHECK LIST. MSG EXTINGUISHED THEN REAPPEARED & EXTINGUISHED AGAIN. R & R APU FIRE DETECT CONTROL MODULE & TROUBLE SHOT SYS IAW AMM 26-12-02 & FIM 26-12-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

DURING IMBV INSPECTION, QA FOUND LT AFT FUSELAGE FASTENER HOLE CRACKED AT FRAME 75 STRINGER 2 AREA. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON LT AFT FUSELAGE FASTENER HOLE CRACK AT FRAME 72 STRINGER 2 AREA IAW ERS-EM-53MR-600. REPAIR MATERIALS DOUBLER 2024T3 .080, FILLER 2024T3 .063, ANGLE 2024T3 .063, ANGLE FILLER 2024T3 .032.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

DURING IMBV INSPECTION, QA FOUND FRAME 23 CRACKED BETWEEN STRINGER 15R - 16R. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON FRAME 23 BETWEEN STRINGER 15R - 16R IAW EO-EM-53MR-1808. FABRICATED REPLACEMENT SECTION FRAME AL7475-T761 032, L SHAPED SPLICE AL7475-T761 040.

Part: WIRE — BROKEN (CABIN) · airframe 28,520 hrs · 25,865 cycles

ONE PROX LIGHT WITH ARROWS & ONE PROX LIGHT WITHOUT ARROWS HAVE BROKEN WIRES AT PROX LIGHT. R & R IAW AMM 33-50-12. SEE NRTC BOW 159263 FOR FINAL INSTALL & OPERATIONS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

AFT UPPER LT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 77. REPAIRED DAMAGE BY INSTALL BUSHING & FILET SEALED IAW ERS-EM-5300-562. SEE TURNOVER FOR DETAILS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

RIGHT AFT FUSELAGE FRAME 75 FASTENER HOLE CRACKED STRINGER 3 AREA MARKED. REPAIRED DAMAGE AT RT AFT FUSELAGE BY INSTALLING BUSHING IAW ERS-EM-5300-575. SEE TURNOVER FOR DETAILS.

Part: FLANGE — CORRODED (RT WING) · airframe 28,520 hrs · 25,865 cycles

RIGHT LE NR 2 OTBD MACHINED FLANGE IS CORRODED. REPAIRED IAW ERS-EM-5700-182. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

AFT UPPER RT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 78. REPAIRED DAMAGE BY INSTALLING BUSHING IAW ERS-EM-5300-563. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

AFT UPPER RT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 79 MARKED. REAMED FASTENER HOLE ON AFT UPPER RT EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGER 3R - 4R AS REQUIRED TO REMOVE DAMAGE. FABRICATED & INSTALLED BUSHING IAW ERS-EM-5300-588. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE REINFORCEMENT CRACKED AT LT FLOORBEAM. R & R SPLICE PLATE IAW SRM 51-30-01, 51-40-02 & GPM 17-13. SEE WIPS & TASKS FOR ADDITIONAL INFORMATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,520 hrs · 25,865 cycles

NUMBER 1 AISLE EMER LIGHT STRIP NOT WORKING. R & R NR 1 AISLE EMER FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE BOW 159263 TASK NR 1 FOR OPERATIONAL CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 28,520 hrs · 25,865 cycles

FORWARD PROXIMITY LIGHT STRIP WIRE BROKEN AT SPLICE CONNECTOR. REPAIRED FWD PROXIMITY LIGHT STRIP WIRE AT SPLICE CONNECTOR IAW SWPM 20-21-00 STEP 6.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,520 hrs · 25,865 cycles

CABIN RT FLOORBEAM OTBD SUPPORT CRACKED AT WING BOX BETWEEN FRAME 47 & 48. REMOVED RT CABIN OMEGA BEAM TO WING BOX OTBD SUPPORT ANGLE & DRILLED FASTENER HOLES IN NEW TWO PIECE REPAIR ANGLE IAW SRM 53-23-02 & 51-20-03.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 28,105 hrs · 25,477 cycles

EMERGENCY LIGHTS INOPERATIVE IN CABIN. R & R EMERGENCY LIGHT CHARGERS & BATTERIES AT POSITION 1, 3 & 4 IAW WC 33-700-19.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 27,831 hrs · 25,238 cycles

LOST ALL HYD FLUID IN NR 2 SYS.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 27,130 hrs · 24,555 cycles

HYD 1 LOW IN FLIGHT. TRANSFER HYD FLUID IAW EM-29-023. DIVERTED. NO LEAKS NOTED, OK FOR RETURN TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 26,180 hrs · 23,625 cycles

THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS MISSING. THE ACFT WAS REMOVED FROM SERVICE. FOUND FLASHLIGHT BEHIND THE CAPTAINS’S SEAT, PLACED BACK IN FLASHLIGHT HOLDER AS REQUIRED. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ANTI-ICE VALVE — FAILED · airframe 26,049 hrs · 23,489 cycles

DURING CLIMB, AN ENGINE AIR INLET ANTI-ICE VALVE CAME OPEN WITH PB SELECTED OFF. TAT INFLIGHT WITH VALVE OPEN EXCEEDED + 20 F. RECEIVED AN ASSOCIATED EICAS MESSAGE OF NO ICE ANTI-ICE. REPAIRED IAW AMM 30-21-06.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,906 hrs · 23,327 cycles

DURING B INSPECTION FOUND NUMEROUS EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — ACTIVATED (CABIN) · airframe 25,706 hrs · 23,166 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY POWER SUPPLY BATTERY WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 25,430 hrs · 22,906 cycles

ON FLIGHT 4479 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE AND HOT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BULB IAW AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,363 hrs · 22,844 cycles

DURING B INSPECTION FOUND THE EMERGENCY CEILING LIGHT INOPERABLE AT ROW 3. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,056 hrs · 22,580 cycles

FWD CABIN FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FWD CABIN FLASHLIGHT AND CRADLE ASSY IAW EMB 140 AMM CHAPTER 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 24,235 hrs · 21,808 cycles

DURING B INSPECTION, FOUND THE FLOOR EMERGENCY PROXIMITY LIGHT AT SEAT 1A AND 2A NR 3 ON THE CEILING ABOVE THE SERVICE DOOR INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 INVERTER ABOVE THE SERVICE DOOR. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,016 hrs · 21,632 cycles

DURING B INSPECTION, FOUND THE NR 4 PROXIMITY LIGHT HAS A BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DISCONNECTED (FLSHLIGHT CRADLE) · airframe 24,016 hrs · 21,632 cycles

DURING B INSPECTION, FOUND THE FLASHLIGHT ON AFT STOWAGE UNIT NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. DISCONNECTED AND RECONNECTED SP3557 AND SP3558 TO CORRECT WIRES IAW SWPM 20-21-00 AND EMB 140 WM 33-51-50. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,016 hrs · 21,632 cycles

DURING MAINTENANCE INSPECTION, FOUND A BROKEN WIRE ON THE NR 5 EMERGENCY LIGHT ASSEMBLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 23,859 hrs · 21,510 cycles

ON FLIGHT 2782 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 23,799 hrs · 21,450 cycles

DURING PS-2 INSPECTION, FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE BULB IN SOCKET. RESECURED BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 23,442 hrs · 21,120 cycles

FLT 4370 CREW REPORTED AFTER TAKEOFF ENGINE 1 STARTED TO SURGE. SMELLED AN ELECTRICAL ODOR. MOVED THRUST LVL 1 TO IDLE - NO SURGING OR ODOR. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SHUT ENGINE 1 DOWN AFTER LANDING NO SMOKE COMING FROM ENG 1 HAD LOSS OF ENG 1 ITT THROUGHOUT INCIDENT. INITIAL T/S REVEALED AN ITT SPLIT OF ABOUT 100 DEGREES. (NR 1 ENGINE APPROX 550 NR 2 ENGINE 450) SUSPECTED POSSIBLE INTERNAL BLEED LEAK. REMOVED AND REPLACED ENGINE NR 1 IAW W/C 71-000-00. THE OPERATIONAL LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (TE FLAP) · airframe 22,716 hrs · 20,492 cycles

ON TAKEOFF FROM YOW WHEN LOWERING FLAPS GOT FLAP LOW SPEED. ON DESCENT INTO ORD WHEN LOWERING FLAPS TO 9 GOT A FLAP FAIL. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. RESET AND PERFORMED OPERATIONAL CHECK OF FLAP DRIVE SENSOR IAW EMB FIM 27-51-00-810-805 FOUND TO BE A TRANSITORY CONDITION OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,540 hrs · 20,337 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FORWARD EXIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD EXIT BULB IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHROUD — LOOSE (TE FLAP) · airframe 22,299 hrs · 20,124 cycles

ON FLIGHT 4099 THE CREW REPORTED THAT ON APPROACH, SELECTED FLAPS 9 DEGREES. FLAPS STOPPED AT 1 DEGREE WITH FLAP FAIL MESSAGE ON EICAS. THE CREW DECLARED AN EMERGECNY. THE CREW DID ZERO FLAP LANDING AS PER AOM VOL 1. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RIGHT INBOARD FLAP, ROLLER TRACK GIMBAL SHROUD BINDING & LOOSE. RE-SECURED & TIGHTENED THE SHROUD PER EMB140 AMM 27-50-00. THE OPERRATIONAL CHECK WAS GOOD FOR FLAP SYSTEM PER EMB 140 AMM 27-53-00. PERFORMED GENERAL VISUAL INSPECTION OF FTB'S, DRIVE UNITS & FLEX SHAFTS. NO DEFECTS NOTED. NO MESSAGES NOTED ON EICAS AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (FIRE DETECTOR) · airframe 21,805 hrs · 19,731 cycles

DURING NORMAL APU START AT THE GATE RECEIVED APU FIRE WARNING FOR APROX 6 SECONDS AT 59 PERCENT ROTOR SPEED. APU AUTOMATICALLY SHUT DOWN THEN APU FIRE FAIL EXTINGUISHED SUBSEQUENT RECEIVED APU FUEL LO PRESS AND APU FAIL MESSAGES DID NOT PUSH APU FIRE EXTG BUTTON DUE TO APU FIRE EXTINGUISHED. CLEANED APU FIRE DETECTOR ELECTRICAL CONNECTOR PERFORMED FIRE DETECTION SYSTEM ADJUSTMENT TEST IAW EMB 140 AMM 26-10-00 NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,704 hrs · 18,814 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD FLOOR EMERGENCY PROXIMITY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLOOR EMERGENCY PROXIMITY LIGHT IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,624 hrs · 18,756 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD WING EMERGENCY EXIT LOCATING SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EXIT LOCATING SIGN AND EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 19,969 hrs · 18,233 cycles

FOR FLIGHT 3274 DURING PREFLIGHT CHECK THE CREW FOUND THE FLOOR EMERGENCY LIGHTING STRIP AT ROW 16A TO BE INOPERABLE (A POSSIBLE BROKEN WIRE). ACFT REMOVED FROM SERVICE. REPAIRED WIRE CONNECTOR FOR EMERGENCY FLOOR LIGHT AT SEAT 16A IAW MM 20-221-00. OPS CHECKED GOOD IAW MM 33-50-12. ACFT RETURNED TO SERVICE.

Part: CARBON SEAL — FAULTY (NR 4) · airframe 19,616 hrs · 17,980 cycles

ON FLIGHT 3355 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON THE TAKEOFF ROLL. THE CAPTAIN ELECTED TO ABORT. SMOKE BEGAN TO DISSAPATE AFTER POWER TO IDLE AND TAXI TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY IAW WORK CARD 71--000-00. THE AIRCRAFT WAS RETURNED TO SERVICE. MANUFACTURER DETERMINED THE NR 4 CARBON SEAL WAS FAULTY.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 19,444 hrs · 17,852 cycles

FOR FLIGHT 2766 DURING THE INSPECTION FOUND THE NR 1 FLOOR PROXIMITY STRIP LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTORS DISCONNECTED. RECONNECTED THE CONNECTORS IAW EMB 140 AMM 33-50-12. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,411 hrs · 17,826 cycles

ON FLIGHT 4027 DURING INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (BS 3293) · airframe 18,994 hrs · 17,479 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT HAND FRAME 10 CRACKED UNDER DV WINDOW. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: REMOVED AND REPLACED FRAME 10 WITH NEW FRAME 10 IAW EMB SRM 51-40-02 AND SRM 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 18,994 hrs · 17,479 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SHEAR CLIP AT FRAME 65 CORRODED AT CARGO DOOR CUTOUT LOWER CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SHEAR CLIP AT CARGO DOOR CUTOUT LOWER CORNER AT FRAME 65 IAW EO EM-53MR-1129. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,994 hrs · 17,479 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR CUTOUT LOWER CENTER SILL TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR CUT OUT LOWER CENTER SILL IAW EMB 140 SRM 51-40-02, 51-40-06, 51-20-03, 51-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,717 hrs · 15,576 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT EXTERNAL EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TESTING. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE LEFT AFT EXTERNAL EMERGENCY LIGHT ASSEMBLY. THE AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 15,705 hrs · 13,260 cycles

ON FLIGHT 4553, AFTER 80 KTS ON TAKEOFF ROLL COCKPIT BECAME HAZY WITH SMOKE ACCOMPANIED BY ODOR. ABORTED TAKEOFF. SMOKE DISSIPATED FAIRLY RAPIDLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BURNED (COCKPIT) · airframe 12,229 hrs · 10,593 cycles

CAPTAIN CHART HOLDER SMOKES WITH A VISIBLE GLOW. REMOVED AND REPLACED CHART HOLDER IAW EMB 25-15-11. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 12,195 hrs · 10,566 cycles

BAGGAGE SMOKE INDICATION LIGHT ILLUMINATED INFLIGHT WITH NO AURAL WARNING, RETURNED TO LAW. POST INSPECTION REVEALED NO EVIDENCE OF SMOKE. PERFORMED OPERATIONAL CHECK OF SYSTEM IAW EMB AMM WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE.

Part: BRACKET — CORRODED (FLOOR SUPPORT)

DURING AN MBV INSPECTION, THE FLOOR SUPPORT BRACKET AT FRAME 20 WAS FOUND CORRODED THROUGH THE AFT END. MAINTENANCE REPLACED FLOOR SUPPORT BRACKET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE OMEGA BEAM WAS FOUND CORRODED THROUGH AT FRAME 20 WHERE CROSSBEAM CONNECTS. REPAIRED OMEGA BEAM AT FRAME 20 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE LT FORWARD IB SEAT TRACK WAS FOUND WITH NUMEROUS AREAS OF CORROSION AROUND SCREW HOLES. MAINTENANCE INSTALLED NEW SEAT TRACK IAW MM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159)

Part: SELECTOR — INOPERATIVE (COCKPIT)

DURING APPROACH TO SNA CREW REPORTED A FLAP FAIL MESSAGE ON EICAS AND THE FLAPS STAYED AT 9 DEGREES. AIRCRAFT DIVERTED TO LAX. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FCU — FAILED (AVIONIC BAY)

DURING FLIGHT CREW REPORTED A FLAPS FAIL MESSAGE ON EICAS AND FLAPS STUCK IN THE FIVE DEGREE POSITION. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — DIRTY (COCKPIT)

FIRST OFFICERS SEAT DIFFICULT TO LOCK IN PLACE. SEAT MOVED BACK IN FLIGHT. CLEANED DEBRIS FROM SEAT TRACK, OP CHECK GOOD. (M)

Part: LOCKPIN — LACK OF LUBE (COCKPIT SEAT)

DURING TAKEOFF, CRWE REPORTED THE CAPTAINS SEAT PINS FAILED TO ENGAGE AND PILOTS SEAT SLIDE TO THE AFT POSITION. MAINTENANCE CLEANED THE CAPTAINS SEAT TRACKS AND LUBRICATED THE SEAT PINS. OPS CHECK WAS GOOD IAW CMM 25-21. (M)

Part: SKIN — DAMAGED (FUSELAGE)

AIRCRAFT HAS LIGHTNING DAMAGE APPROX 1.5 INCH FORWARD OF FRAME 62A BETWEEN STRINGERS 21L AND 21R. REPAIRED DAMAGE IAW EMB SRM 53-31-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN)

CVG - CREW REPORTED WHEN POWER WAS REMOVED FROM AIRCRAFT THE EMERGENCY LIGHTS STAYED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY IAW EMB AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (T/E FLAP)

ORD - FLT 4165 - DURING APPROACH, CREW REPORTED THE FLAPS FAILED/STOPPED AT 3 DEGREES. AN EMERGENCY DECLARED AND NO FLAP LANDING WAS SAFELY COMPLIED WITH. WHILE TROUBLESHOOTING FLAP SYSTEM MAINTENANCE FOUND THE CANNON PLUG ON THE NR 1 FLAP DRIVE LOOSE. CANNON PLUG WAS RECONNECTED AND FLAPS WERE CYCLED MULTIPLE TIMES. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)