N629AE

Part: BLEED VALVE — FAULTED (NR 2) · airframe 49,545 hrs · 47,498 cycles

BLEED 2 VALVE FAILURE ON T/O POWER ( C/W RMM 36-11-05) T/S FIM 36-11-00-810-806-A STEPS 1 2 3 20 21 AND 22 R/R #2 HIGH STAGE PRESSURE SWITCH IAW AMM 36-11-07. OPS CHECK GOOD. NO OTHER DEFECTS NOTEDAT THIS TIME. CLEAR MEL 36-1-3.OK FOR SERVICE.

Part: NONE — NONE · airframe 49,018 hrs · 46,899 cycles

PDIS 629 36-21 2116541 12JUN22 RIC CLOSE BLEED 1 LEAK IN FLT 29363 00 RS FACT 13JUN22 06:07 RIC FOUND THERMAL SWITCH WIRE NOT SOLDERED IN AFT AVIONIS BAY BY THE CROSS BLEED VALVE. SOLDERED WIRE IRT AMM 36-20-02-400-801-A. THEN FOUND O-RINGS BROKEN ON AFT APU BLEED AIR CHECK VLV DUCT LINE, R&R'D O-RINGS IRT AMM 36-11-10-000/400-801-A. OPS CHECK GOOD LEAK CHECK GOOD OK FOR SERVICE SEEHA-300 SEQ 16 PACKAGE 6-13-22

Part: NONE — NONE · airframe 48,409 hrs · 46,220 cycles

PDIS 629 21-01 2706202 17FEB22 CAK CLOSE ELETRICAL BURNING SMELL DURING DESCENT LASTED FOR 30 SEC. SMELL WAS NOTICED FWD CABIN/FLT DECK AREA. 27933 00 RS FACT 17FEB22 00:26 CAK PERFORMED GVI OF RELAY,CONTACTORS, COMP., AND FWD AVIONICS BAY NO ELE SMELL NOTED OR SIGNS OF BURNING/ARCHING. POWER UP A/C INSPECTED DISPLAY UNITS, W/S HEAT TERMINALS AND SURROUNDING ELETRONICS STILL NO SMELL NOTED R AN APU BLEEDS & PACKS FOR SEVERAL MINS WITHNO ABNORMAL SMELL A/C OK FOR SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 48,357 hrs · 46,154 cycles

PDIS 629 36-11 2706101 07FEB22 ISP CLOSE HS 1 VLV FAIL MSG DURING TAKE OFF ROLL. REJECTED TAKE OFF AT 65 KTS FULL THROTTLE FACT 07FEB22 11:24 ISP PERFORMED OPS TEST OF AIR BLEED SYS WITH CREW IAW AMM 36-00-00-700-803. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE

Part: VALVE — FAULTED (NR 2 A/C PACK) · airframe 47,843 hrs · 45,555 cycles

ON TAKE OFF PACK 2 VALVE CLOSED MSG WOULD NOT CLEAR UNTIL LANDING. DURING INSPECTION OF AIR CON/PNUMATIC PANEL FOUND AND REPAIRED BROKEN WIRE IAW SWPM 20-5000 (SHORT SIGN)CHANGED RELAYS K0320, K0263, K0262, K0184 IAW AMM 20-13-02. REMOVED AND REPLACED PACK 2 PUSH BUTTON IAW AMM 20-13-04. NO FIX PACK 2 INOP SEE PG 213988 SEQ 2. (REMOVED AND REPLACED #2 PACK VALVE IAW AMM 21-51-01 OPS CHECK GOOD. LEAK CHECK GOOD. OKAY FOR SERVICE AT THIS TIME.)

Part: PIPE — LEAKING (BLEED VALVE) · airframe 47,668 hrs · 45,353 cycles

BLEED 1 LEAK MSG DURING CLIMB. T/S IN REF W/FIM TASK 36-20-00-810-801-A. FOUND Y-PIPE AFTER #100 ENG BLD VLV TO BE DAMAGED. R&R'D Y-PIPE AFTER #100 ENG BLD VLV IN REF W/AMM 36-11-09. OPS CHECKED IN REF W/AMM 36-00-00. OPS CK GOOD. RE-ACTIVATED #100 ENGINE BLD VLV PER MEL. CLEAR MEL 36-1-1. OK FOR SERVICE.

Part: UPLOCK — FAULTED (RT MLG) · airframe 47,596 hrs · 45,252 cycles

AFTER GEAR RETRACTION, RIGHT MAIN INDICATION ALTERNATED BETWEEN UP AND LOCKED AND IN TRANSIT. R&R'D R/H MLG UP LOCK BOX IAW AMM 32-33-10-04. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: UPLOCK — MALFUNCTIONED (RT MLG) · airframe 47,596 hrs · 45,252 cycles

AFTER GEAR RETRACTION CONTINUOUS THUMPING NOISE HEARD FROM NOSE BAY AREA. AFTER R/H MLG UP LOCK BOX WAS R&R'D REF LOG PAGE 260829-2. NO NOISE HEARD IN NOSE BAY AREA. NO DEFECT NOTED.

Part: ACTUATOR — FAULTED (HORIZONTAL STAB) · airframe 47,523 hrs · 45,180 cycles

PITCH TRIM BACK UP INOP. R&R HORIZONTAL STABILIZE ACTUATOR IAW EMB 145 AMM 27-40-02-000/A00-801A REQUIRES ZERO RIG CHECK AMM TASK 27-40-02-700-801-A/500. PERFORMED ELECTRICAL ZERO POSITION OF HORIZONTAL STABILIZER IAW AMM 27-40-02-801-A/500 OPS CHECK GOOD P/N ON 362200-501 S/N 1251 P/N OFF 362200-50-15 S/N 1164

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 47,444 hrs · 45,095 cycles

PDIS 629 27-41 2580431 21MAY21 CLT CLOSE PITCH TRIM MAIN INOP MESSAGE AT 6000 FT AFTER TAKE OFF FACT 21MAY21 15:06 CLT R/R HORIZONTAL STAB CONTROL UNIT IAW AMM 27-40-01.OPS CHECK GOOD OK FOR SERVICE.

Part: CONTROL MODULE — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 45,101 hrs · 42,503 cycles

EMERGENCY LIGHT NOT ARMED, EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED CONTROL MODULE ASSY IAW AMM 33-21-01 SUBTASK 33-25-00-700-801-A AND 33-50-00-700-801-A. OPS CHECK GOOD,OK FOR SERVICE

Part: BLEED VALVE — FAILED (NR 2) · airframe 44,413 hrs · 41,683 cycles

PDIS 629 36-10 2048721 20APR19 PHL CLOSE BLD 2 VLV FAIL WHEN ENTERING ICING CONDITIONSFACT 20APR19 15:10 PHL R&R'D ENG BLEED VALVE 2 IAW EMB 145 AMM 36-11-05 OPS CHECK GOOD AT THIS TIME

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 44,405 hrs · 41,671 cycles

629 33-51 0014160 16APR19 RIC CLOSE EMERGENCY LIGHT OVER SERVICE DOOR DOORWAY WILL NOT ILLUMINATE 27751 00 NGR FACT 16APR19 09:57 RIC DISCONNECTED EMERGENCY LIGHT INVERTER + RESEATED CONNECTOR AS REQ.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 43,756 hrs · 40,907 cycles

DURING TAXI IN TO GATE. FO'S PFD WENT BLANK ALONG WITH ELECTRICAL ODOR. SELECTED AVIONICS BUSS 2 OFF. SWAPED FO'S PFD AND MFD PER AMM 34-22-01 AND DEACTIVATED MFD PER MEL.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 43,422 hrs · 40,518 cycles

DISCREPANCY: THE EMERGENCY LIGHTS CONNECTED TO THE #2 POWER SUPPLY DID NOT COME ON DURING OPS CHECK. CORRECTIVE ACTION: REMOVED CIELING PANEL IN FRONT OF GALLEY TO GAIN ACCESS TO #2 POWER SUPPLY. FOUND CHAFFED WIRES NEAR #2 POWER SUPPLY, REPLACED WIRES AND REINSTALLED CIELING PANEL IN FRONT OF GALLEY.

Part: MODULE — MALFUNCTIONED (CABIN PRESSURE) · airframe 43,102 hrs · 40,149 cycles

ABSENCE OF PRESSURIZATION INDICATIONS ON EICAS PANEL. DASH LINES IN BOXES. R&R CPAM, C/W OP AND ALT CK'S REF 21-32-01, C/W NR 3 STATIC SYSTEM LK CK. OK IAW TASK 34-13-00-790-804.

Part: PITCH CONTROL — MALFUNCTIONED · airframe 42,616 hrs · 39,580 cycles

MAIN PITCH TRIM IS INOPERATIVE. INSPECTED & OPERATED THE MAIN & B/U PITCH TRIM SWITCHES WITH NO FAULTS, COMPLIED WITH FIM 27-43-00-810-801-A, AND 27-43-810-802-A, NO FAULTS FOUND. R & R THE HSCU IAW AMM 27-40-01. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (ICE PROTECTION) · airframe 42,189 hrs · 39,112 cycles

ICE CONDITION ADV MESSAGE DISPLAYED. ACFT WAS NOT IN ICING CONDITIONS. MESSAGE WENT OUT AT 13000 FEET AND CREW SMELLED SOMETHING BURNING. PERFORMED ICE DETECTION SYSTEM OPS CHECK IAW AMM 30-80-00. ALL OPS CHECKED GOOD. ICE PROTECTION ELECTRICAL TEST ACCOMPLISHED AND PNEUMATIC ICE PROTECTION ON GROUND TEST ACCOMPLISHED. OPS CHECKED GOOD. OK FOR SERVICE.

Part: DUCT — UNSECURE (CABIN PRESSURE) · airframe 42,171 hrs · 39,096 cycles

RAPID DEPRESSURIZATION WHILE HOLDING SHORT IN AUTOMATIC MODE. MANUAL MODE OVER PRESSURIZED. INSPECTED THE NR 1 PACK AREA AND FOUND A DUCT LOOSE. SECURED THE DUCT. PRESSURIZED IAW AMM 21-31-00. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,016 hrs · 38,923 cycles

DURING POST INSPECTION WALK AROUND, FOUND A DENT AND SCRAPE UNDER CARGO DOOR. REPAIRED IAW ERS-EM-53MR-3025.

Part: CONTROL ROD — CORRODED (MLG DOORS) · airframe 42,016 hrs · 38,923 cycles

LEFT AND RIGHT, FORWARD AND AFT, FOUR MAIN LANDING GEAR DOOR CONTROL RODS ARE CORRODED. REMOVED AND REPLACED THE CONTROL RODS IAW AMM 32-10-06, STEPS 1, 5, & 9, AND ETN-EM-32-256.

Part: ATTACH FITTING — WORN (RT WING) · airframe 42,016 hrs · 38,923 cycles

INBOARD SPOILER FITTING ON REAR SPAR 3 HAS A WORN HAT BUSH BORE. REMOVED AND REPLACED INBD SPOILER ATTACH BRACKET (INCLUDED NEW HAT BUSHINGS) IAW AMM 57-51-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 42,016 hrs · 38,923 cycles

LEFT WING EIGHTH AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 42,016 hrs · 38,923 cycles

LEFT WING FIFTH AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142 IAW NRTC E605570.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 42,016 hrs · 38,923 cycles

RIGHT WING THIRD AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN ER ETN-EM-53-142.

Part: SUPPORT BRACKET — CRACKED (FRAME 61) · airframe 42,016 hrs · 38,923 cycles

AFT CARGO DOOR FORWARD TORSION BAR SUPPORT BRACKET AT FRAME 61 CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 10) · airframe 42,016 hrs · 38,923 cycles

COCKPIT FRAME 10 IS CRACKED, BELOW WINDOW. REMOVED AND REPLACED THE FRAME IAW 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,016 hrs · 38,923 cycles

COCKPIT LT FRAME 10 IS CRACKED, BELOW DV WINDOW. REMOVED AND REPLACED COCKPIT LT FRAME 10 SECTION BELOW DV WINDOW IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 42,016 hrs · 38,923 cycles

LEFT WING SECOND AFT LOWER ATTACH ANGLE IS CRACKED IN SEVERAL PLACES. -INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FRAME 10) · airframe 42,016 hrs · 38,923 cycles

COCKPIT LT FRAME 10 ATTACH ANGLE AT TOP OF FRAME IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FRAME 10) · airframe 42,016 hrs · 38,923 cycles

COCKPIT FRAME 10 ATTACH ANGLE AT TOP OF FRAME IS CRACKED. REMOVED AND REPLCED THE ATTACH ANGLE IAW SRM 51-40-02.

Part: CLEAT — CRACKED (FRAME 10) · airframe 42,016 hrs · 38,923 cycles

COCKPIT LT FRAME 10 CLEAT IS CRACKED. -INSTALLED A NEW CLEAT IAW SRM 51-40-02.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 42,016 hrs · 38,923 cycles

CENTER FUSELAGE UPPER SKIN PANEL BETWEEN FR 35-36 STRG 1R-3R GOUGES, PERMANENT REPAIR. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2836.

Part: A/C PACK — MALFUNCTIONED (NR 2) · airframe 41,874 hrs · 38,780 cycles

NR 2 PACK OVERLOAD IN FLIGHT AT FL 250 WITH THE NR 1 PACK. REMOVED AND REPLACED THE RT PACK VALVE IAW AMM 21-51-01. OPS CHECK FAILED. OPEN

Part: LAMP — CRACKED (LANDING LIGHT) · airframe 41,660 hrs · 38,562 cycles

NR 1 LANDING LIGHT CRACKED. R & R THE LANDING LIGHT LAMP IAW AMM 33-41-02. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,554 hrs · 38,437 cycles

LEFT OVERWING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING PANEL EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 30,412 hrs · 26,064 cycles

THE CREW REPORTED THAT THE FRONT DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE WHEN IN EMERGENCY LIGHT MODE. MAINTENANCE INSPECTED THE ACFT AND FOUND THAT THE SIGN WAS DISCONNECTED. MAINTENANCE RECONNECTED THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACCESS DOOR — CRACKED (E&E BAY) · airframe 37,798 hrs · 34,630 cycles

REAR ELECTRONICS ACCESS HATCH 272DR IS CRACKED UNDER EYELET BRACKET. REPAIRED IAW ERS-EM-52MR-334.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,798 hrs · 34,630 cycles

FUSELAGE SKIN CRACKED ON FRAME 75 AT THIRD FASTENER BELOW STRINGER 2R, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORMED PERMANENT REPAIR OF FUSELAGE SKIN CRACK ON FRAME 75 AT THIRD FASTENER IAW ERS-EM-53MR-1308.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,798 hrs · 34,630 cycles

FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-1309.

Part: SKIN — CHAFED (FUSELAGE) · airframe 37,798 hrs · 34,630 cycles

AIRLINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB. PERFORMED PERMANENT REPAIR OF AIR LINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB IAW ERS-EM-53MR-1307.

Part: CONNECTOR — MISSING (CABIN) · airframe 37,798 hrs · 34,630 cycles

POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 4 IS MISSING A CONNECTOR. INSTALLED CONNECTOR & PIN ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 4 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. SEE NRTC E450553 FOR OPERATIONS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 37,798 hrs · 34,630 cycles

EMERGENCY LIGHT STRIP NR 3 HAS BROKEN WIRE ON LIGHT STRIP SIDE. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 37,798 hrs · 34,629 cycles

EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRE ON LIGHT STRIP SIDE. EMER LIGHT STRIP NR 2 IS INOPERATIVE. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 37,798 hrs · 34,630 cycles

POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 HAS A DAMAGED CONNECTOR. INSTALLED CONNECTOR & PIN ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. SEE NRTC E450553 FOR OPERATIONS CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,798 hrs · 34,630 cycles

EMERGENCY LIGHT STRIP NR 1 IS INOPERATIVE. R & R NR 2 BATTERY POWER SUPPLY & BATTERY PACK IAW AMM 33-50-04 & AMM 20-10-01. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 37,798 hrs · 34,629 cycles

POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 HAS A DAMAGED CONNECTOR. INSTALLED NEW CONNECTOR ON WIRE NR W192-8831-22 AT SPLICE SP9211 ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. SEE NRTC E450553 FOR THE OPERATIONAL CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,798 hrs · 34,629 cycles

LEFT FWD CARGO FLOOR SILL HAS CORROSION AT ALL NUTPLATE HOLES. REPAIRED LT FWD CARGO FLOOR SILL CORROSION AT NUTPLATE HOLES IAW SRM 51-10-03, CPM 51-14-02, SRM53-31-10 & ERS-EM-53MR-1288. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,798 hrs · 34,629 cycles

FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. CRACK IS APPROX 3/8" IN LENGTH EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. REPAIRED FUSELAGE SKIN CRACKS JUST AFT OF FRAME 75 BETWEEN STRINGERS 2R - 3R IAW ERS-EM-53MR-1308.

Part: YOKE — CRACKED (RT ENGINE) · airframe 37,798 hrs · 34,629 cycles

RIGHT ENG FWD LOWER ENG YOKE HAS CRACK, ENG SIDE OF YOKE. REMOVED & INSTALLED SERVICEABLE RT ENG FWD LOWER ENG SIDE OF YOKE IAW EO-EM-54MR-386.

Part: WIRE — BROKEN (CABIN) · airframe 37,798 hrs · 34,629 cycles

EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRE ON LIGHT STRIP SIDE. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 37,798 hrs · 34,629 cycles

POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 4 IS MISSING A CONNECTOR. INSTALLED NEW CONNECTOR ON WIRE NR W192-8703-22 AT SPLICE SP9103 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. SEE NRTC E450553 FOR OPERATIONAL CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 37,798 hrs · 34,629 cycles

EMERGENCY LIGHT STRIP NR 3 HAD BROKEN WIRE ON LIGHT STRIP SIDE. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: YOKE — CRACKED (LT ENGINE) · airframe 37,798 hrs · 34,629 cycles

LEFT ENG FWD LOWER ENG YOKE HAS CRACK ENG SIDE OF YOKE. REMOVED & INSTALLED SERVICEABLE LT ENG FWD LOWER ENG SIDE OF YOKE IAW EO-EM-54MR-386.

Part: SKIN — CRACKED (FRAME 75) · airframe 37,798 hrs · 34,629 cycles

FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH. REPAIRED SKIN CRACK AT FRAME 75 & STRINGER 2L IAW ERS-EM-53MR-1309.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,798 hrs · 34,629 cycles

EMERGENCY LIGHT STRIP NR 2 IS INOPERATIVE. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: DETECTION SYS — MALFUNCTIONED (CARGO BAY) · airframe 37,627 hrs · 34,489 cycles

BAGGAGE EXT STAYS ILLUMINATED AFTER FIRE TEST IS PERFORMED. PERFORMED ELEC RESET IAW AMM 24-40-00. BAGGAGE SMOKE DETECTION SYS TEST IAW AMM 26-15-00.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 37,627 hrs · 34,489 cycles

PTRIM MAIN INOPERATIVE. DURING CLIMB AT FL 2900 WARNING MSG ON EICAS. TRANSFERRED TO NRWC 629-DFW-02203. R & R HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD. NO DEFECTS NOTED.

Part: CONTROLLER — FAILED (CABNI PRESSURE) · airframe 37,324 hrs · 34,180 cycles

AUTO PRESSURIZATION DID NOT WORK IN FLIGHT SEE PREVIOUS LOG PAGE 3732954. PREVIOUS WRITE UP MANUAL PRESS CONTROL FUNCTIONS OK. R & R PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,980 hrs · 32,847 cycles

FLOOR PROXIMITY LIGHT STRIP INOPERATIVE AT EMER OVERWING EXIT. R & R FLOOR STRIP LIGHTS AT OVERWING EXIT ROW IAW MM CH 33-50-12.

Part: GENERATOR — FAILED (NR 4) · airframe 35,672 hrs · 32,564 cycles

MEL 24-4 AUTH 050987DM-B ORG LPG 3521386, GEN 4 OFF BUS EICAS MSG ON ENG 1 SHUT DOWN. R & R NR 4 GEN IAW MM 24-31-01. OPERATIONS & LEAK CHECKED GOOD MEL RESTORED.

Part: TIRE — DAMAGED (NLG) · airframe 35,395 hrs · 32,294 cycles

LOUD NOISE FROM NOSE WHEEL CONTINUED FOR ABOUT 7 MIN AFTER TAKEOFF & THEN WAS OUT & CAME BACK AGAIN, IT SEEMS LIKE WAS A GRINDING NOISE. DURING CLIMB NO EICAS INDICATION. INSPECTED ACFT NOSE AREA INCLUDING NLG & FOUND NOSE TIRES WITH FLAT SPOTS. R & R NLG TIRES IAW AMM 32-49-05 & WORK CARD 32-700-17.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 35,396 hrs · 32,295 cycles

UPON GEAR RETRACTION AFTER TAKEOFF, NOSE GEAR DOORS REMAINED OPEN WITH GEAR UP, RETURNED TO MIA, NO OTHER GEAR ISSUES. REPLACED NLG DOOR SEQUENCE PROX SWITCH IAW AMM 32-63-03. REFERENCE ITEM NR 2 OF THIS LOG PAGE FOR OPERATIONS CHECK.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 34,890 hrs · 31,908 cycles

FLASHLIGHT HOLDER AT AFT CABIN & FIRST OFFICER`S POSITION BROKEN. R & R FLASHLIGHT HOLDERS IAW AMM 33-50-16. NO FURTHER DEFECT NOTED, OPERATIONS CHECKED GOOD.

Part: ROLLER — DAMAGED (PAX DOOR) · airframe 34,346 hrs · 31,480 cycles

PASSENGER ENTRY DOOR CANNOT BE OPENED FROM INSIDE. RESEATED UNDER THE ROLLER ARM INTERNAL ACTUATING HANDLE IAW AMM-52-18-05. OPS CHECKED GOOD IAW 52-18-00.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 34,217 hrs · 31,378 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. ON/OFF BUTTON IS MISSING. R & R WITH SERVICEABLE FLASHLIGHT. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,130 hrs · 31,295 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,945 hrs · 31,147 cycles

INNER FUSELAGE SKIN IS CORRODED BETWEEN S21L AND 21R AT FR 67. REPAIRED SKIN IAW EO EM-53MR-2189.

Part: SPAR — CRACKED (LEFT WING) · airframe 33,945 hrs · 31,147 cycles

FOUND A CRACK 2.4 INCH LONG ON LT WING SPAR NR 3. REPAIRED IAW EO EM-57MR-700 AND ETA EM5700-807. ACFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,945 hrs · 31,147 cycles

DURING HMBV FOUND UPPER HALF OF FRAME 81 CRACKED AT RIVET HOLES AT STRINGERS 3L AND 3R. R & R UPPER HALF OF FRAME 81 IAW SRM 51-40-02.

Part: FRAME — CHAFED (FRAME 81) · airframe 33,945 hrs · 31,147 cycles

DURING HMBV INSPECTION, FOUND AFT SIDE OF FRAME 81 CHAFED AT THE 6:00 POSITION. R & R FRAME 81 LOWER SECTION IAW SRM 51-40-02.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 33,945 hrs · 31,147 cycles

DURING HMBV INSPECTION, FOUND CARGO DOOR SILL CORRODED BETWEEN FRAMES 65-68. R & R CARGO DOOR SILL IAW SRM 51-40-02.

Part: SKIN — CANNING (RUDDER) · airframe 33,945 hrs · 31,147 cycles

DURING HMBV INSPECTION FOUND RT SIDE RUDDER NR 1 HAS OIL CANNING SKIN JUST BELOW UPPER HINGE POINT. REPAIRED DAMAGE IAW EO EM-55MR-436.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 33,945 hrs · 31,147 cycles

EMERGENCY LIGHT WIRING SEEMS TO BE IMPROPERLY CLAMPED AT FRAME 51. ROUTED WIRING IAW SWPM 20-21-00.

Part: PLATE — CORRODED (FUSELAGE) · airframe 33,945 hrs · 31,147 cycles

PLATE IN BELLY OF ACFT FWD OF FRAME 67 BETWEEN STR'S 21L AND 20L IS CORRODED AROUND THE RIVETS. PLATE IN BELLY OF ACFT FWD OF FRAME 67 BETWEEN STR'S 21L AND 20L REMOVED REFER TO EO EM-53MR-2189, STEP 12 AND ETA EM-5300-3088.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,945 hrs · 31,147 cycles

INNER FUSELAGE SKIN IS CORRODED BETWEEN STRINGERS 21L AND 21R AT FRAME 67. REPAIRED FUSELAGE SKIN IAW EO EM-53MR-2189.

Part: SPAR — CRACKED (LT WING) · airframe 33,944 hrs · 31,146 cycles

CRACK ON LT WING SPAR, STARTING ON MLG WIRE HARNESS ACCESS HOLE GOING UPWARDS TO 1 O'CLOCK, CRACK APROX 2.4". ACCOMPLISHED EDDY CURRENT INSP IAW ETN-EM-51-113. FOUNDED LINEAR INDICATION ON DISPLAY UNIT.

Part: LENS — CRACKED (FLASHLIGHT) · airframe 33,044 hrs · 30,412 cycles

ON FLIGHT 3941 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT LENS RING WAS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,036 hrs · 30,407 cycles

DURING B INSPECTION FOUND THE 4TH AFT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 4TH AFT CEILING EMERGENCY LIGHT IAW EMB 145 TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 32,368 hrs · 29,891 cycles

ON FLIGHT 2842 THE CREW REPORTED THE CAPTAIN’S MFD FAILED IN FLIGHT (WENT COMPLETELY BLANK SUDDENLY) DURING APPROACH MFD CAME BACK UP, BUT WITH AN ACRID ODOR. PULLED MFD 1 CB, ODOR CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S MFD. THE OPERATIONAL CHECK WAS GOOD IAW AMM 34-22-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP. REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT.

Part: PROXIMITY SWITCH — DIRTY (LANDING GEAR) · airframe 31,765 hrs · 29,435 cycles

ON FLIGHT 3546 THE CREW REPORTED THAT WHILE ON DESCENT INTO MIA RECEIVED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. THE CREW FOLLOWED EMERGENCY PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT IN MIA. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORM OPERATIONAL CHECK OF (5) WEIGHT ON WHEELS SWITCHES WITH GSE 212 AND THE OPERATIONAL CHECK WAS GOOD. CLEANED AND INSPECT ALL WOW PROXIMITY SWITCHES AND THE OPERATIONAL CHECK WAS GOOD IAW AMM 32-63. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,568 hrs · 29,308 cycles

ON FLIGHT 3536 THE CREW REPORTED THAT A PASSENGER REPORTED A LIGHT BLUB BURNED OUT AT SEAT 5A WITH A BURNING SMELL AND AREA AROUND LIGHT SOCKET WAS OVERHEATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 5A READING LIGHT BLUB IAW EMB 145 AMM 33-25-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,539 hrs · 29,287 cycles

DURING B INSPECTION FOUND THE RIGHT FRONT EXTERNAL EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FRONT EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 31,369 hrs · 29,163 cycles

ON FLIGHT 4204 THE CREW REPORTED THAT UPON LANDING AND CLEARING RUNWAY WENT TO RAISE THE FLAPS AND GOT A FLAP FAIL AND SPS ADVANCED EICAS MSG. FLAPS WERE STUCK AT 22 DEGREES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 31,259 hrs · 29,074 cycles

FLIGHT 2885, CREW REPORTED DURING CLIMB THROUGH 10,000 FT, RECEIVED AN EICAS WARNING MESSAGE AND CABIN ALTITUDE ABOVE 10,000FT. PERFORMED AOM PROCEDURE BUT ACFT WOULDN'T PRESSURIZE IN MANUAL MODE. DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEPARTURE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED GROUND CONNECTION VALVE IAW AMM 21-22-04. PERFORMED PRESSURIZATION IN MANUAL AND AUTO, OPS CHECKED GOOD IAW AMM 21-31-00.

Part: UNKNOWN — ODOR (AFT CABIN) · airframe 31,037 hrs · 28,886 cycles

FLIGHT 2739, THE FLIGHT ATTENDANT REPORTED AN OILY ODOR IN THE BACK OF THE AIRCRAFT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ENGINE RUNS AS PER ETN NR EM-72-034R4. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 30,806 hrs · 28,685 cycles

ON FLIGHT 3209 THE CREW REPORTED THAT AFTER COMPLETING THE AFTER TAKEOFF CHECK LIST RECEIVED A NR 2 BLEED LEAK WARNING MESSAGE ON CLIMBOUT THRU 4000 FEET. THE CREW PERFORMED AN EPC/AOM CHECKLIST - LEAK INDICATION EXTINGUISHED AFTER APPROX 60 SECONDS OF SHUTTING BLEED NR 2 OFF. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED CLAMP ON NR 2 ENGINE BLEED VALVE IN RIGHT PYLON REF AMM 36-11-05 AND REPLACED CLAMPS AT RIGHT TUBE FROM DUAL TEMP VALVE TO HEAT EXCHANGER REF 21-60-01. PERFORMED OPERATIONAL CHECKS OF THE BLEED AIR AND PACKS IAW AMM 36-00-00 AND 21-51-00 NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 30,289 hrs · 28,278 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT SEATS 10 AND 11A IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRE IAW EMB WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,214 hrs · 28,230 cycles

DURING B-INSPECTION, FOUND THE CEILING AISLE EMERGENCY LIGHT NEAR EXIT ROW INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CEILING AISLE EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-08-000-801-A AND TASK 33-50-08-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,905 hrs · 27,982 cycles

ON FLIGHT 4107 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 29,798 hrs · 27,899 cycles

ON FLIGHT 4347 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED PASSENGER DOOR IAW AMM 52-18-00 DOOR OPENS AND CLOSE GOOD AND WITHIN LIMITS IAW AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DAMAGED (CABIN DOOR) · airframe 29,771 hrs · 27,875 cycles

ON FLIGHT 4290 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOWER AFT MAIN DOOR FRAME ROLLER DAMAGED. REMOVED AND REPLACED THE LOWER AFT MAIN DOOR FRAME ROLLER IAW EMB 145 AMM 53-21-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,758 hrs · 27,863 cycles

ON FLIGHT 3508 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR IAW EMB SP 20-30-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — OUT OF ADJUST (CABIN DOOR) · airframe 29,553 hrs · 27,707 cycles

ON FLIGHT 3235 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR HARD WAS TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERIVCE. ADJUSTED MAIN CABIN DOOR INTERNAL HANDLE IN REFERENCE TO EMB 145 AMM 52-18-05. NO PARTS REMOVED FOR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 29,509 hrs · 27,672 cycles

FOR FLIGHT 2963 THE CREW REPORTED THE MAIN DOOR WON'T CLOSE (LARGE GAP AT THE TOP). THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR FRAME ROLLERS. THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 29,449 hrs · 27,634 cycles

ON FLIGHT 2742 THE CREW REPORTED THE PASSENGER DOOR RED HANDLE WAS DIFFICULT TO PULL. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED FRAME ROLLERS. THE OPERATIONAL CHECK WAS GOOD 52-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,349 hrs · 27,558 cycles

DURING MAINTENANCE BASE VISIT FOUND FORWARD FUSELAGE II SKIN CRACKED AT LEFT WINDSHIELD SIDE POST UPPER END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1890. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FCU — INOPERATIVE (FUEL SYSTEM) · airframe 29,325 hrs · 27,539 cycles

ON FLIGHT 4154 THE CREW REPORTED THAT WHILE REACHING CRUISE ALT SELECTED CRZ TRUST RATING APPROX 20 SEC LATER EICAS WARNING FUEL 1 LO LEVEL CAUTION FUEL IMBALANCE. EICAS INDICATED NR 1 ENG 0 PPH 0 LBS FUEL. MFD FUEL PG INDICATED TANK 1 0LBS. FMS FUEL PAGE INDICATED TANK 1 0LBS. FMS FUEL PAGE INDICATED ONLY AVAILABLE FUEL WAS WHAT WAS IN THE NR 2 FUEL TANK. ALL COCKPIT INDICATIONS WERE ONLY FUEL ON BOARD WAS WHAT THE NR 2 TANK HAD AVAILABLE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO FWA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FUEL CONDITIONING UNIT IAW EMB 145 AMM 28-41-01. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,205 hrs · 26,736 cycles

FOR FLIGHT 2769 DURING THE PREFLIGHT INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT CHARGER HOUSING BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,166 hrs · 26,708 cycles

FOR FLIGHT 2969 DURING THE PREFLIGHT INSPECTION FOUND THE LEFT FUSELAGE AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FUSELAGE AFT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (FECU) · airframe 26,509 hrs · 25,565 cycles

ON FLIGHT 2915 DURING CRUISE THE CREW REPORTED FLAP INDICATOR INDICATED SEVERAL DIFFERENT DEGREE POSITION FROM 1 DEGREE TO 43 INTERMITTENTLY. EN ROUTE FLAPS DID NOT MOVE. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR J1 ON THE FLAP ELECTRONIC CONTROL UNIT WAS LOOSE. RE-SECURED AND PERFORMED OPERATIONAL CHECK OF FLAPS PER AMM 27-52-00-700-802-A. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,825 hrs · 25,021 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,227 hrs · 24,575 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR) · airframe 25,207 hrs · 24,556 cycles

FOR FLIGHT 3243 PRIOR TO FLIGHT MAINTENANCE DISCOVERED THE SERVICE DOOR (CABIN) NEEDS TO BE LUBRICATED DUE TO IT WAS HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SERVICE DOOR LINING PANEL PERFORMED SERVICE DOOR ACTUATING AND LOCKING MECHANISM LUBRICATION AS PER EMB 145 AMM 52- 43-00 AND RE-INSTALLED SERVICE DOOR LINING PANEL AS PER EMB 145 25-23-05. PERFORMED OPENING AND CLOSING OF SERVICE DOOR AND FOUND SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,129 hrs · 24,495 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD EXIT EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY & CHARGER IAW EMB145 AMM TASK 33-50-04-000-801-A & 37--50-04-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 25,129 hrs · 24,495 cycles

DURING MAINTENANCE BASE VISIT FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT OVERHEAD EMERGENCY LIGHT LAMP IAW AMM EMB 145 TASK33-50-08000-801A & 33-50-08-400-801A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 24,513 hrs · 23,988 cycles

DURING MAINTENANCE INSPECTION FOUND TWO GOUGES IN THE LOWER FORWARD FUSELAGE SKIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE TWO GOUGES IN THE LOWER FORWARD FUSELAGE SKIN IAW EO EM-53MR-1150 R2 PT C. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,513 hrs · 23,988 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER CROSS BEAM CORRODED UNDER CROSS BEAM BETWEEN FRAME 24 AND FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CROSS BEAM IAW EMB 145 SRM 53-00-10 FIGURE 203, SHEET 2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,516 hrs · 23,988 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THAT THE LEFT NR 1 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH CONNECTORS IAW EMB 145 SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 24,513 hrs · 23,988 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SKIN ABOVE CENTER MOUNT ON LEFT ELEVATOR CRACKED / BENT. THE CRACK LENGTH IS APPROXIMATELY .9 / .7 INCHES. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGE, INSTALLED DOUBLER IAW EMB SRM 55-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 22,381 hrs · 22,146 cycles

ON FLIGHT 4209 CREW REPORTED ELECTRICAL BURNING ODOR IN THE FWD CABIN GALLEY AREA. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED CEILING AND SIDE WALL BALLAST IAW AMM 33-21-03, IAW AMM 33-21-05 OPS CHECKED GOOD NO MORE BURNING SMELLS DETECTED. ACFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

ON FLIGHT 3411 DURING PREFLIGHT THE CREW FOUND THE EMERGENCY EXIT IDENTIFIER OVER GALLEY AND THE OVERHEAD CENTER AISLE AT EMERGENCY EXIT ROW DOES NO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. WHEN MAINTENANCE ARRIVED ALL THE EMERGENCY LIGHTS WERE OPERATING AS INDICATED. NO MAINTENANCE PERFORMED AND NO PARTS INSTALLED. AIRCRAFT RETURNED TO SERVICE. (A)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,284 hrs · 20,128 cycles

ON FLIGHT 4036, CREW REPORTED EMERGENCY EXIT LIGHT IS INOPERATIVE OVER GALLEY SERVICE DOOR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER 2 (PS 8501-234) IAW EMB 145 33-50-11. OPERATIONAL CHECKED GOOD OF EMERGENCY LIGHT SYSTEM IAW EMB 145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 19,976 hrs · 19,845 cycles

DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND REPLACED WITH NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,976 hrs · 19,845 cycles

DURING MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 23 WAS FOUND CORRODED. REWORKED AREA IAW SRM 53-21-10, FIG 206. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,976 hrs · 19,845 cycles

DURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,976 hrs · 19,845 cycles

DURING MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 53-00-10, 53-20-03, 51-21-04 AND 51-21-05. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — BURNED (RECIRC FAN) · airframe 17,961 hrs · 17,972 cycles

STRONG ELECTRICAL ODOR FOR ONE MINUTE AND THEN DISSIPATED. REMOVED AND REPLACED NR 1, NR 2 RECIRCULAR FANS AND NR 1 RECIRCULAR FAN INVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: ECU — FAILED (T/E FLAP)

FLAP FAIL MESSAGE FLAP STUCK BETWEEN 0-8 DEGREES. REPLACED FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, CORROSION WAS FOUND ON SERVICE DOOR CENTER SILL THAT WAS BEYOND SRM LIMITS. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE BLENDED AREAS. NO DEFECTS NOTED. FABRICATED THREE REPAIR DOUBLERS. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A IMBV INSPECTION LEFT HAND BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAGED BEAM. FABRICATED A FILLER, TWO SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER FLOORBEAM INSTALLED NEW BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, THE DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS, SHIMS. REPAIR DONE IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LEFT HAND OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS, PLATE. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 29. REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS. REPAIR DONE IAW SRM.

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED. BLENDED CHAFE. PERFORMED AND NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGED AREA TO COMPLETELY REMOVED THE CORROSION. FABRICATED A U SHAPED DOUBLER. REPAIR DONE IAW SRM.

Part: SILL — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION OF AIRCRAFT, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED SERVICEABLE SILL IAW SRM.

Part: FRAME — CHAFED (FUSELAGE)

DURING A IMBV INSPECTION FOUND LOWER FRAME 81 CHAFED BEYOND SRM LIMITS. REMOVED EXISTING LOWER FRAME 81. INSTALLED NEW FRAME IAW SRM.

Part: SILL — CORRODED (FUSELAGE)

RIGHT SILL CORRODED BETWEEN FRAME 24 AND 29. PERFORMED EDDY CURRENT AND THICKNESS INSPECTION WITH NO DEFECTS FOUND. REPLACED SILL IAW GST.

Part: SILL — CORRODED (FUSELAGE)

RIGHT HAND SILL IS CORRODED BETWEEN FRAME 29 AND 35. PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. REPAIRED RIGHT HAND SILL BETWEEN FR 29-35 IAW GST.

Part: FRAME — CORRODED (FUSELAGE)

STRINGER 19L HAS CORROSION BETWEEN FRAMES 23 AND 24 UNDER FLOOR. PERFORMED EDDY CURRENT AND THICKNESS, NO DEFECTS. REPAIR DONE IAW GST.

Part: FLOORBEAM — CORRODED (FUSELAGE)

LEFT HAND FLOOR BEAM GUSSET IS CORRODED BETWEEN FRAME 65-68. INSTALLED SERVICEABLE GUSSET IAW SRM.

Part: SILL — CORRODED (FUSELAGE)

CARGO DOOR SILL IS CORRODED. REMOVED AND INSTALLED NEW CARGO DOOR SILL IAW CPM.

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION MAINTENANCE FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFED AREA. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB-145 SRM 145/1142, CHAPTER 53, REV 19, 53-24-02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PREVIOUS REPAIR AT FRAME 20 ON LEFT FLOORBEAM IS CORRODED. REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER BEAM RAMP IS CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM GUSSET IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PASSENGER DOOR FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE)

PROFILE AT FRAME 23 IS CORRODED. REMOVED AND REPAIRED PROFILE AND DOUBLER. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

RIGHT FLOORBEAM CORRODED AT FRAME 23. REPAIRED IAW SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE)

CROSSMEMBER AT FRAME 23 IS CORRODED. REMOVED CROSSMEMBER AND REPAIRED IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK CORRODED BETWEEN FRAMES 18 AND 23 ON LEFT FLOORBEAM. REMOVED AND REPLACED SEAT TRACK IAW AMM.

Part: ENGINE — FLAMED OUT (NR 2)

DISC - NR 2 ENGINE FLAME OUT DURING CRUISE. WOULD NOT RESTART. C/A REPLACED NR 2 ENGINE.

Part: DRAIN LINE — ODOR (TAIL) · airframe 2,328 hrs · 2,531 cycles

HSV - FLT 4403 - FLIGHT CREW DETECTED A STRONG SMELL OF JET FUEL/EXHAUST SMELL WHEN THE APU WAS ON. THE PACKS WERE ON AT THE TIME. APU PUT ON MEL. MAINTENANCE REMOVED AND REPLACED DRAIN HOSE FROM THE COLLECTOR TUBE TO THE APU DRAIN SYSTEM OUTLET IAW EMBRAER MM. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (ROW 12)

DFW - FLT 3700 - FOUND EMERGENCY LIGHTS INOPERATIVE AT ROW 12. REMOVED AND REPLACED EMERGENCY LIGHTS AT ROW 12. OPS CHECK GOOD. (M)

Part: UNKNOWN — ODOR (CABIN)

ORD - FLT 4162 - STRONG FUEL ODOR IN CABIN NEAR PASSENGER SEAT ROWS 14 AND 15. INSPECTED AIRCRAFT EXTERNAL DRAINS AND PANELS. OPENED CABIN FLOOR PANELS AND PERFORMED ENGINE GROUND RUNS, BUT NO EVIDENCE OF LEAKS OR VAPORS WAS DETECTED OF ANY KIND. AIRCRAFT RETURNED TO SERVICE. (X)