N308AE

Part: OIL SYSTEM — FLUCTUATES (NR 2 ENGINE) · airframe 18,608 hrs · 21,715 cycles

NR 2 ENGINE OIL PRESSURE LIGHT STARTED TO FLUCTUATE ALONG WITH LOW OIL PRESSURE IN THE CAP. THE OIL PRESSURE NEEDLE STARTED TO FLUCTUATE WITHIN THE YELLOW ARC AND SOON AFTER BOTH ENGINE OIL LIGHT AND CAP LIGHT ALONG WITH MASTER WARNING AND CRC. SHUT NR 2 ENGINE DOWN AS PER COMPANY PROCEDURES. FOLLOW PWC MM 05-50-22 STEP 5S FOR PROCEDURES FOR OIL LOSS OR LOW OIL PRESSURE. INSPECTED RGB AND TURBO ENG CHIP DETECTOR FOR DEBRIS AND CHECK OK IAW ATR JIC 79-22-62. REMOVED AND REPLACED SCAVENGE FILTER AND CARRY OUT PATCH CHECK AND FOUND OK IAW ATR 72 JIC 79-22-61 AND 72-01-50. REMOVED AND REPLACED PRESSURE OIL FILTER AND PATCH CHECK AND FOUND OK IAW ATR 72 JIC 79-22-62 AND 72-01-50. SERVICED ENG OIL . PERFORMED ENGINE RUN UP AT 80 PERCENT TQ FOR 10 MINUTES. CHECK FOR LEAKS AND FOUND SATISFACTORY, NO DEFECTS NOTED AT THIS TIME.

Part: HMU — FAILED (LT ENGINE) · airframe 29,514 hrs · 33,057 cycles

INITIALLY NR 1 FAILED COMPLETELY. REMOVED AND REPLACED LT ENGINE HMU/MFCU AS PER JIC NR 73-21-61-RAI-10000. OPS CHECK GOOD AS PER JIC NR 73-21-61-OPT-10000 AND AE MNTC NR 055007-CS-20000-001. FCF PASSED.

Part: ENGINE — POWER LOSS (LEFT) · airframe 29,514 hrs · 33,057 cycles

DURING APPROACH LT ENGINE TQ DROP 20 PERCENT. ENGINE WAS SHUTDOWN AND LANDED WITH NO FURTHER PROBLEMS. AWAITING AML PAGE FOR DETAILS.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 29,276 hrs · 32,778 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW JIC NR 33-50-00-RAI-10000-001.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 29,276 hrs · 32,778 cycles

MAIN PAX DOOR STAIR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW JIC NR 33-5-00-RAI-10000-001. OPERATION CHECK GOOD IAW JIC NR 33-50-00-OPT-10000-001.

Part: LAMP — LOOSE (EMERGENCY LIGHTS) · airframe 29,060 hrs · 32,531 cycles

MAIN PAX ENTRY DOOR EMERGENCY LIGHT IS INOPERATIVE. REPOSITIONED PAX ENTRANCE DOOR GROUND FLOOD EMERGENCY LIGHT AS PER JIC NR 33-51-00.

Part: WARNING LIGHT — FALSE INDICATION (FIRE WARNING) · airframe 27,699 hrs · 31,181 cycles

WHEN MOVING CONDITION LEVERS FWD, FIRE INDICATION ON CAP AND FIRE HANDLE. AFTER CONDITION LEVERS WERE MOVED TO FUEL S/O, FIRE INDICATION ON CAP AND FIRE HANDLE EXTINGUISH. PERFORMED SEVERAL OPERATIONAL CHECK ON BOTH ENGINE FIRE DETECTION SYSTEM WITH ENGINES RUNNING AS PER MM NR 26-12-00. ALSO, RESET MFC SYSTEM AS PER MM NR 31-48-00. AFTER INVESTIGATION, CONCLUDE THIS WAS A FALSE INDICATION.

Part: CONTROL UNIT — MALFUNCTIONED (RT ENGINE) · airframe 27,470 hrs · 30,979 cycles

NR 2 ENGINE TQ WENT DOWN TO 0 PERCENT, NP TO 0 PERCENT AND THE ENGINE SHUT DOWN BY ITSELF. REMOVED AND REPLACED MULTI-FUCTION COMPUTER (MFC) IAW JIC NR 31-48-81. REMOVED AND REPLACED TORQUE SIGNAL CONTROL UNIT(AFU) IAW JIC NR 77-13-62. PERFORMED GROUND POWER RUN-UP IAW W/C 055007-CS-20000-001.

Part: CONTROL UNIT — MALFUNCTIONED (RT ENGINE) · airframe 27,470 hrs · 30,979 cycles

NR 2 ENGINE TQ WENT DOWN TO 0 PERCENT, NP TO 0 PERCENT AND THE ENGINE SHUT DOWN BY ITSELF. REMOVED AND REPLACED MULTI-FUNCTION COMPUTER (MFC) IAW JIC NR 31-48-81. REMOVED AND REPLACED TORQUE SIGNAL CONTROL UNIT(AFU) IAW JIC NR 77-13-62. PERFORMED GROUND POWER RUN-UP IAW W/C 055007-CS-20000-001.

Part: WINDSHIELD — BROKEN (COCKPIT) · airframe 27,468 hrs · 30,976 cycles

F/O WINDSHIELD CRACKED AT 17,000 FT, CRUISING ALTITUDE, NO WINDSHIELD HEATER FAULT INDICATION. REMOVED AND REPLACED WINDSHIELD IAW JIC 56-11-00. PERFORMED OPT AND FUSELAGE PRESSURIZATION LEAK TEST IAW JIC 05-53-00.

Part: FIRE WARNING — FALSE INDICATION · airframe 27,146 hrs · 30,684 cycles

APPROXIMATELY 3 TO 5 MINS AFTER STARTING ENG NR 1, AN ENG NR 1 FIRE INDICATION ON CAP, CONDITION LEVER NR 1 AND FIRE HANDLE NR 1 ENGINE FIRE EMERGENCY PROCEDURES WERE PERFORMED. SPECIAL DVI AFTER ENGINE FIRE WAS PERFORMED IAW JIC NR 70-00-00 SDI 10000. RE-CHECKED WIRES AND TESTED LT ENGINE LP VALVE SEVERAL TIMES WITH NR 1 FIRE HANDLE IAW JIC NR 28-24-00 AND FOUND WORKING PROPERLY. GROUND RUN-UP PERFORMED IAW JIC NR 72-00-00 AND FOUND SATISFACTORY. ANALYZED AS A FALSE FIRE INDICATION. POSSIBLE HEAVY TAIL WIND WHILE TAXIING.

Part: WHEEL — DAMAGED (NR 3) · airframe 27,135 hrs · 30,675 cycles

POST FLIGHT INSPECTION REVEALED NR 3 WHEEL TIRE AT ODD ANGLE AND BRAKE DISC OUT OF POSITION. REMOVED AND REPLACED RT MLG AS PER JIC 32-11-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,975 hrs · 30,515 cycles

PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REPOSITIONED LAMP AND PERFORMED OP CK IAW JIC NR 33-50-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

LT "Z" FLOOR UPPER AND LOWER SURFACE BETWEEN FRAME 39 AND 40 CORRODED. LEFT "Z" FLOOR SUPPORT BETWEEN FRAME 39-40 REPLACED AS PER SRM 51-25-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

RT THRESHOLD SUPPORT AND LOWER SURFACE BETWEEN FRME 36 TO 39 CORRODED. RT THRESHOLD BETWEEN FRAME 36 TO 39 REPLACED AS PER SRM 51-25-01.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

LT GUTTER CORRODED BETWEEN FRAME 36 AND 39. NEW LT GUTTER BETWEEN FRAME 36 AND 39, INSTALLED IAW SRM 51-25-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

LT THRESHOLD CORRODED BETWEEN FRAME 36 AND 39. NEW LT THRESHOLD BETWEEN FRAME 36 AND 39 INSTALLED IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

FLOORBEAM 36 CORRODED ON UPPER AND LOWER SURFACE. NEW FLOORBEAM 36 INSTALLED IAW SRM 51-25-01.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

LT AFT PASSENGER DOOR THREAD SUPPORT 5 IS CORRODED. NEW THREAD SUPPORT 5 INSTALLED IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

FLOORBEAM 39 UPPER AND LOWER SURFACE CORRODED. FLOORBEAM 39 REPLACED AS PER SRM 51-25-01.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,120 hrs · 29,680 cycles

LT AFT PASSENGER DOOR THREAD SUPPORT 1(BOTTOM) IS CORRODED. NEW THREAD SUPPORT 1 (BOTTOM), INSTALLED IAW SRM 51-25-01.

Part: WIRE — DAMAGED (CABIN)

WHILE PERFORMING POST FLIGHT, CREW NOTICED MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE AT MAIN CABIN EMERGENCY EXIT LIGHT ASSY IAW 33-22-17. (K)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJU-PUJ - FLT 5102 - WHILE IN TAXI, EMERGENCY LIGHTS ON AT ALL TIME IN FORWARD CABIN. AIRCRAFT RETURNED TO GATE FOR CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW JIC 33-51-21. OP CHECK SATISFACTORY. (M)

Part: POWER SUPPLY — MALFUNCTIONED (CABIN)

WHILE TAXIING, FA REPORTED EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH OR RESET TO OFF. REPLACED EMERGENCY LIGHTS POWER PACK. (K)

Part: FIRE WARNING — FALSE ACTIVATION (LT ENGINE)

LT ENGINE FIRE WARNING INDICATION CAME ON. CREW DEPLOYED THE FIRE BOTTLE AS A PRECAUTIONARY METHOD. NO EVIDENCE OF FIRE FOUND. LOOKS LIKE A TAIL WIND PROMOTE THE FALSE. ENGINE FIRE WARNING INDICATION.

Part: LIGHT — INOPERATIVE (PAX DOOR)

MIA - FLT 5053 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON SEAT TRACKS, LEFT AFT OUTBOARD AND RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINES ENGINEERING ORDER E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP2 INSPECTION, FOUND CORROSION ON FLOORBEAM 40. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ATR72 SRM 51-25-02. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP2 INSPECTION, FOUND CORROSION ON SEAT TRACKS, LEFT AFT OUTBOARD AND RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AMERICAN EAGLE AIRLINES ENGINEERING ORDER E2-53MR-115. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DFW - FLT 3633 - EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT STRIP AT ROW 15-17 IAW AMM 33-50-00. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3857 - CREW REPORTED NUMEROUS EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY BATTERY PACK AT POSITION 73WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — INOPERATIVE (MAIN DOOR)

DFW - DURING SCHEDULED PS-2 CHECK, FOUND THE MAIN DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED BULB FOR MAIN DOOR EMERGENCY LIGHT, OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5236 - LIGHT ON FLOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. ISSUED MEL 33-30 UNTIL ITEM CAN BE REPAIRED. MAINTENANCE REPLACED LIGHT ASSEMBLY AT SEAT 6A IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — DAMAGED (GALLEY)

MIA - FLT 5350 - FLIGHT ATTENDANT REPORTED THE FIRST FLOOR PROXIMITY EMERGENCY LIGHT IN THE GALLEY AREA TO BE IN NEED OF REPAIR. MAINTENANCE REPLACED THE LIGHT ASSEMBLY IN THE GALLEY AREA. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — INOPERATIVE (CABIN)

MIA - FLT 5236 - MAIN CABIN DOOR EMERGENCY ENTRY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED ENTRY EMERGENCY LIGHT BULB. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SOCKET — FAILED (GALLEY)

MCO - FLOOR EMERGENCY LIGHTING IN GALLEY INOPERATIVE. REMOVED AND REPLACED LAMP HOLDER IAW AMM. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

EYW - FLT 5226 - EMERGENCY LIGHT ON AIRSTAIR INOPERATIVE, INSPECTED AND FOUND A BROKEN WIRE ON THE AIRSTAIR BUNDLE, REPAIRED WIRE OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (GALLEY)

EYW - FLT 5226 - TWO EMERGENCY FLOOR PROX LIGHT INOPERATIVE, INSPECTED AND FOUND A BULBS INOPERATIVE IN GALLEY. REPLACED BULB IN FORWARD POSITION AND ENTERED THE AFT IN MEL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FAN — MALFUNCTIONED (CABIN)

NAS - FLT 5365 - DURING PREFLIGHT INSPECTION, THE FLIGHT ATTENDANT REPORTED A BURNING ELECTRICAL SMELL ON THE AIRCRAFT. THE CAPTAIN WENT TO THE COCKPIT AND NOTICED THE ODOR WAS VERY STRONG AND ALSO NOTICED A HAZE IN THE AIR. THE CAPTAIN TURNED ALL POWER OFF AND DISCONNECTED THE GROUND POWER UNIT. NO OTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED BOTH RECIRCULATIONS FANS IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.(M)

Part: MOUNT — DAMAGED (CABIN)

MIA - FLT 5270 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 6 INOPERATIVE. MEL 33-30. REMOVED AND REPLACED HOLDER, SOCKET, LENS, AND LAMP IAW ATR AMM. OPS CHECK GOOD. (M) REF SIMA3324.

Part: LAMP — INOPERATIVE (CABIN)

MIA - FLT 5270 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 6 INOPERATIVE. MEL 33-30. REMOVED AND REPLACED HOLDER, SOCKET, LENS, AND LAMP IAW ATR AMM. OPS CHECK GOOD. (M) REF SIMA3324.

Part: LENS — BROKEN (CABIN)

MIA - FLT 5270 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 6 INOPERATIVE. MEL 33-30. REMOVED AND REPLACED HOLDER, SOCKET, LENS, AND LAMP IAW ATR AMM. OPS CHECK GOOD. (M)

Part: SOCKET — INOPERATIVE (CABIN)

MIA - FLT 5270 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 6 INOPERATIVE. MEL 33-30. REMOVED AND REPLACED HOLDER, SOCKET, LENS, AND LAMP IAW ATR AMM. OPS CHECK GOOD. (M) REF SIMA3324.

Part: SKIN — DAMAGED (FWD CARGO DOOR)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE FORWARD CARGO DOOR OUTER SKIN DAMAGED. MAINTENANCE REPAIRED THE DOOR IAW SRM 52-31-10, 52-31-00 AND EO E2-52MR-043. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD LOWER SKIN PANEL BETWEEN FRAME 4 AND 7 IAW SRM 51-25-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FOR MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 5 AND 6, 7 AND 8, 8 AND 9, AND 9 AND 10 IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3064. (M)

Part: INTERCOSTAL — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FOR MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 5 AND 6, 7 AND 8, 8 AND 9, AND 9 AND 10 IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3064. (M)

Part: INTERCOSTAL — DENTED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FOR MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 5 AND 6, 7 AND 8, 8 AND 9, AND 9 AND 10 IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — DENTED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTUAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT CORD BETWEEN FRAME 5 AND 7, AND 7 AND 13 IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD LOWER SKIN PANEL BETWEEN FRAME 7 AND 13 IAW SRM 51-25-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — DENTED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REPAIRED FRAME 5 BETWEEN STRINGERS 11 AND 14, FRAME 8 BETWEEN STRINGERS 11 AND 14, FRAME 9 BETWEEN STRINGERS 11 AND 17 AND FRAME 12 BETWEEN STRINGERS 16 AND 21 IAW SRM 53-11 40. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FOR MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 5 AND 6, 7 AND 8, 8 AND 9, AND 9 AND 10 IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3064. (M)

Part: FRAME — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REPAIRED FRAME 5 BETWEEN STRINGERS 11 AND 14, FRAME 8 BETWEEN STRINGERS 11 AND 14, FRAME 9 BETWEEN STRINGERS 11 AND 17 AND FRAME 12 BETWEEN STRINGERS 16 AND 21 IAW SRM 53-11 40. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3063. (M)

Part: FRAME — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REPAIRED FRAME 5 BETWEEN STRINGERS 11 AND 14, FRAME 8 BETWEEN STRINGERS 11 AND 14, FRAME 9 BETWEEN STRINGERS 11 AND 17 AND FRAME 12 BETWEEN STRINGERS 16 AND 21 IAW SRM 53-11 40. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3063. (M)

Part: FRAME — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTURAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REPAIRED FRAME 5 BETWEEN STRINGERS 11 AND 14, FRAME 8 BETWEEN STRINGERS 11 AND 14, FRAME 9 BETWEEN STRINGERS 11 AND 17 AND FRAME 12 BETWEEN STRINGERS 16 AND 21 IAW SRM 53-11 40. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3063. (M)

Part: INTERCOSTAL — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM MIA FOR STRUCTUAL DAMAGE TO THE LEFT FORWARD SIDE OF FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT CORD BETWEEN FRAME 5 AND 7, AND 7 AND 13 IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3065. (M)

Part: LAMP — MALFUNCTIONED (CABIN) · airframe 17,142 hrs · 19,273 cycles

MIA - FLT 5352 - EXTERIOR EMERGENCY LIGHT IN PASSENGER DOOR IS VERY DIM. MAINTENANCE REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 5427 - EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — DAMAGED (FUSELAGE)

SAW - AIRCRAFT WAS DAMAGED IN MIA AND FERRIED TO SAW FOR REPAIR. DAMAGE WAS TO THE RIGHT OF THE FUSELAGE BETWEEN FRAMES 43 AND 44 AND STRINGERS 10 AND 13. MAINTENANCE REPAIRED THE LOWER SECTION OF FRAME 43, P/N S53871702200IAW SRM 53-00-00 FIGURE 437, AND REPLACED THE UPPER SECTION OF FRAME, 43, P/N S53871701203. MAINTENANCE REPAIRED THE FUSELAGE SKIN P/N S53872501201, IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — INOPERATIVE (CABIN)

MIA - ROW 15 FLOOR PROXIMITY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 5216 - 4 AFT EMERGENCY LIGHTS WILL NOT GO OUT. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY BATTERY PACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,411 hrs · 18,383 cycles

MIA - FLT 5217 - THREE EMERGENCY EXIT LIGHTS INOPERABLE AT SEATS, 8, 9, 10, AND 11AB. FOUND CONNECTOR LOOSE AT FLOOR PANEL, RECONNECTED SAME. OPS CHECK IAW JIC 33-55-00. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURNIG CPCP-4 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT MIDDLE INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT AFT FLIGHT ATTENDANT, RIGHT AFT CARGO, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND OUTBOARD, RIGHT FORWARD INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ZEE MEMBER — CORRODED (FUSELAGE)

SAW - DURING CPCP-4 INSPECTION, FOUND THE RIGHT AFT ZEE MEMBER CORRODED BETWEEN FRAMES 39 AND 42. REMOVED AND REPLACED THE ZEE MEMBER AND FLOOR CHANNEL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ZEE MEMBER — CORRODED (FUSELAGE)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT ZEE MEMBER AND FLOOR CHANNEL CORRODED BETWEEN FRAMES 39 AND 40. REMOVED AND REPLACED THE ZEE MEMBER AND FLOOR CHANNEL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAM 36.38 AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — FAILED (CABIN)

ORD - FLT 4131 - FORWARD CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED WITH SWITCH IN ALL POSITIONS. REPLACED EMERGENCY BATTERY PACK IAW ATR 72 JIC 33-51-21. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ORD - FLT 4388 - EMERGENCY FLOOR LIGHTING STAYS ON WHEN SWITCH IS OFF. REPLACED POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)