N377AT

Part: STRUCTURE — CORRODED (LT WING) · airframe 33,635 hrs · 33,670 cycles

LT WING FUEL PUMP CUT OUT AREA CORRODED. COMPLIED WITH EO E2-5700-476.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,538 hrs · 33,541 cycles

1 AISLE PATH EVACUATION LIGHT IS INOPERATIVE BY ROW 8. R & R EMERGENCY LIGHT IAW MM 33-51-21. OPS TESTED SATISFACTORY IAW JIC 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,544 hrs · 33,551 cycles

1 AISLE PATH EVACUATION LIGHT INOPERATIVE BY ROW 8. R & R ROW 8 EMERGENCY LIGHT FLOOR ESCAPE PATH IAW MM 33-51-21. OPS TESTED SATISFACTORY IAW JIC 33-50-00 OPT 10000.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 32,284 hrs · 32,194 cycles

DISCREP: EMERGENCY LIGHTS ON FLOOR BY 1-B ARE INOP. C/A: DEFERRED MEL 33-29 AUTHOR 301690D-C ENTERED ON MIC SHEET. ON 03/24/2011: RELAMPED BULB ON FLOOR BY SEAT 1B .OPS CHECK GOOD IAW JIC 33-50-00. MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN)

FRONT HALF OF EMERGENCY LIGHTS IN-OP. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: LAMP — BURNED OUT (AFT MAIN CABIN) · airframe 30,499 hrs · 30,121 cycles

ACFT AIR INTERRUPT. AFT SMOKE WENT OFF MOMENTARILY. INSPECTED CABIN, LAVATORY, BOTH AFT CARGO COMPTS. AND AT THIS TIME NO EVIDENCE OF SMOKE OR SMOKE SMELL WERE NOTED ONLY FOUND 2 CEILING LAMPS BURNED OUT AT 15 & 16 AB PERFORMED AN OPS CK OF THE SMOKE DETECTION SYS IAW AMM 26-15-00-OPT-10000-004 AND R & R CEILING LAMPS AT 15 & 16 AB IAW AMM 33-21-23-RAI-10000-010.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 30,474 hrs · 30,096 cycles

AREA OF CORROSION WAS FOUND AT RT WING LOWER SKIN AROUND JACK POINT AT RIB 10. CORROSION WAS BLENDED OUT IAW SRM 51-21-42 AND NDT ASSURING THERE IS NOT MORE CORROSION. CORROSION DOES NOT REACH ANY FASTENER SEATING, FASTENERS WERE NOT REMOVED. REF SRI NR DO/TS-1340/10-12988, SRAS NR ANA/E/3454/2005, 3275 ISSUE D, ACCOMPLISHED EO E2-57MR-371.

Part: PRESSURE BLKHD — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,474 hrs · 30,096 cycles

CORROSION WAS FOUND ON THE FWD PRESSURE BULKHEAD IN ONE AERA OF THE WEB. REMOVED CORROSION IAW ATR SRI DO/TS-1189/10-13104, REF NDT REPORT AMS 100226-19 FOR HFEC AND UT RESULTS, COMPLIED WITH ATR SARAS DO/TS-1189-10...5623, C/W EO E2-53MR-236. NO SUPPLIEMENTARY INSP NEEDED.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 30,474 hrs · 30,096 cycles

CORROSION AROUND LT WING LWR SURFACE BOOST PUMP BETWEEN RIBS 4-5. CORROSION REPAIRED IAW ATR SRI DO/TS-1229/10-13115, REF NDT REPORT AMS 100226-20 FOR HEFC AND UT RESULTS, COMPLIED WITH ANA/E/3684/2004/E-002 3038 ISSUE B. ACCOMPLISHED EO E2-57MR-370, SUPPLEMENTARY INSP EVERY 2 YEARS.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 30,474 hrs · 30,096 cycles

CORROSION WAS FOUND DURING INSP AT C-CHECK AROUND THE SECTION OF THE RT WING, LOWER SKIN SURROUNDING THE RT BOOST PUMP AREA BETWEEN RIBS 4-5. CORROSION WAS REPAIRED IAW SRI INSTRUCTIONS AND EO. REF SRI NR DO/TS-1341/10-13139, SRAS NR DO/TS-3929/09, 5349 ISSUE B AND EO E2-57MR-372.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 30,474 hrs · 30,096 cycles

AN AERA OF CORROSION WAS FOUND AT RT WING LOWER SKIN T/E BETWEEN RIBS 6-7. C/A: CORROSION WAS BLENDED OUT IAW SRM AND ATR SRI, MINIMUM REMAINING THICKNESS IS 0.287 IN FOR A NOMINAL THICKNESS OF 0.318 IN. REF SRI NR DO/TS-1345/10-13152, SRAS NR DO/TS-3929/09, 5348 ISSUE B AND EO E2-57MR-373.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 30,474 hrs · 30,096 cycles

AREA OF CORROSION WAS FOUND AT RT WING LOWER SKIN AROUND JACK POINT AT RIB 10. CORROSION WAS BLENDED OUT IAW SRM 51-21-42 AND NDT ASSURING THERE IS NOT MORE CORROSION. CORROSION DOES NOT REACH ANY FASTENER SEATING, FASTENERS WERE NOT REMOVED. REF SRI NR DO/TS-1340/10-12988, SRAS NR ANA/E/3454/2005, 3275 ISSUE D, ACCOMPLISHED EO E2-57MR-371.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 29,251 hrs · 28,700 cycles

DURING TAXI HALF PART OF EMERGENCY LIGHTS STAY ON AT ALL TIMES. REMOVED AND REPLACED LIGHT POWER SUPPLY AS PER JIC NR 33-51-21. OPS CHECK WORKING PROPERLY. ALSO, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AS PER JIC NR 33-51-21.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 28,474 hrs · 27,837 cycles

EXTERIOR EMERGENCY LIGHT BELOW SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FIN NR 73WL AND PERFORMED OPS CHECK IAW JIC NR 33-51-21.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,268 hrs · 26,605 cycles

FOUND SEAT TRACK LT I/B FRAME 29 TO FRAME 35 CORRODED. FOUND SEAT TRACK LT I/B FRAME 29 TO FRAME 35. REPLACED IAW SRM 51-25-04.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,268 hrs · 26,605 cycles

FOUND LT O/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35 CORRODED. LEFT O/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35. REPLACED IAW SRM 51-25-04.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,268 hrs · 26,605 cycles

RT I/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35 CORRODED. RT I/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35. REPLACED IAW SRM 51-40-22.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,268 hrs · 26,605 cycles

RT INBOARD SEAT TRACK FRAME 23- FRAME 29 CORRODED. RT INBOARD SEAT TRACK FRAME 23 TO FRAME 29. REPAIRED AS PER SRM 53-00-00.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 27,097 hrs · 26,450 cycles

MULTIPLE EMERGENCY LIGHTS ON ERRONEOUSLY. REPLACED EMERGENCY LIGHTS POWER SUPPLY 61WL AS PER 33-51-21 AND FOUND WORKING PROPERLY.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 27,097 hrs · 26,450 cycles

MULTIPLE EMERGENCY LIGHTS ON ERRONEOUSLY. REPLACED EMERGENCY LIGHTS POWER SUPPLY 61WL AS PER 33-51-21 AND FOUND WORKING PROPERLY.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 26,625 hrs · 26,026 cycles

FWD CABIN EMERGENCY LIGHTS (UPPER AND LOWER) INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK 43WL IAW JIC NR 33-51-21.

Part: PROXIMITY SWITCH — DEFECTIVE (RT MLG)

WHILE IN TAKEOFF, LANDING GEAR HANDLE WILL NOT COME UP. REPLACED RT MLG PROXIMITY SWITCH, 54GB, IAW MM. (K)

Part: FDAU — BURNED (E/E BAY)

UPON LANDING, SMELL OF SMOKE FELT FOLLOWED BY EXHAUST MODE FAULT INDICATION. MAINTENANCE PERSONNEL FOUND FLIGHT DATA ACQUISITION UNIT (FDAU) WITH BURNING SMELL. FDAU REPLACED IAW MM. (K)

Part: WIRE HARNESS — INTERMITTENT (LT MLG)

(REF NR: SDR2005066) AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT AND THE IDLE GATE DID NOT MOVE INTO THE FLIGHT POSITION. AIRCRAFT RETURNED TO AIRPORT. REPLACED MAIN LANDING GEAR HARNESS. (K)

Part: BOLT — BROKEN (STRUT ASSY) · airframe 22,772 hrs

REF: (SDR2005049) WHILE PERFORMING A WALK-AROUND INSPECTION, FOUND THE LT MAIN CYLINDER OUT OF PLACE. REPLACED LT MAIN GEAR SHOCK ABSORBER BOLT. (K)

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE)

DURING GROUND OPERATION, THE RIGHT ENGINE HAD A NACELLE OVERHEAT LIGHT ON, FOLLOWED BY A FIRE WARNING ON AND AN INCREASE IN ITT. TAIL WIND OF 10 TO 14 KNOTS WERE PRESENT. PERFORMED A VISUAL CHECK THE RIGHT ENGINE AND FOUND NO EVIDENCE OF FIRE NOR DAMAGE. (M)

Part: ODOR — DETECTED (COCKPIT)

ELECTRICAL HEAT AND SMELL COMING FROM THE CIRCUIT BREAKER PANEL BEHIND F/O SEAT. VISUALLY INSPECTED CIRCUIT BREAKER PANELS, WIRING AND CONTACTORS AND OFUND NO EVIDENCE OF ELECTRICAL DAMAGE. (M)

Part: ANGLE — CORRODED (FUSELAGE)

SAW - DURNG CPCP INSPECTION, FOUND RIGHT AND LEFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED ZEE MEMBERS IAW SRM 51-25-03. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURNG CPCP INSPECTION FOUND RIGHT AND LEFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED BEYOND LIMITS. REMOVE AND REPLACED ZEE MEMBERS IAW SRM 51-25-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT FLOOR SUPPORT BETWEEN FRAMES 38 TO 39 AND 39 TO 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SUPPORTS IAW SRM 51-25-02. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND FOUR SEAT TRACKS CORRODED, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT MID INBOARD, AND RIGHT AFT INBOARD. REMOVED AND REPLACED FOUR SEAT TRACKS IAW EO E9-5300-013. (M)

Part: CLIP — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND CLIP ON LEFT STRINGER 17 AT FRAME 36 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CLIP IAW SRM 51-25-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND FOUR SEAT TRACKS CORRODED, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT MID INBOARD, AND RIGHT AFT INBOARD. REMOVED AND REPLACED FOUR SEAT TRACKS IAW EO E9-5300-013. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND 3 FLOORBEAMS 35, 36, AND 39 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAMS IAW SRM. REF SIMA36113. (M)

Part: STRINGER — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND STRINGER 17 BETWEEN FRAMES 36 AND 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER IAW SRM 51-25-01. (M)

Part: WEB — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND FLOORBEAM WEB CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM WEB IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT UNDER FLOOR WEB BETWEEN FRAMES 39 AND 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEB IAW SRM 51-25-03. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND 3 FLOORBEAMS 35, 36, AND 39 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAMS IAW SRM. REF SIMA36113. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND FLOORBEAM 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-25-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND LEFT FLOOR SUPPORT BETWEEN FRAMES 38 TO 39 AND 39 TO 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SUPPORTS IAW SRM 51-25-02. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND FLOORBEAM WEB CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEB IAW SRM 51-03-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND 3 FLOORBEAMS 35, 36, AND 39 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAMS IAW SRM. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP INSPECTION, FOUND FOUR SEAT TRACKS CORRODED, LEFT AFT OUTBOARD, LEFT AFT INBOARD, LEFT MID INBOARD, AND RIGHT AFT INBOARD. REMOVED AND REPLACED FOUR SEAT TRACKS IAW EO E9-5300-013. REF SIMA36114. (M)

Part: SKIN — BIRD STRIKE (FUSELAGE)

SAW - DURING MBV-1 INSPECTION, MAINTENANCE CLEARED TMDI AUTHORIZATION 377MQ530294, BIRD STRIKE TO RIGHT SIDE OF FUSELAGE JUST FORWARD AND BELOW STATIC PORT. MAINTENANCE REMOVED AND REPLACED THE FORWARD UPPER SKIN IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE OUTBOARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLAED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR AND SERVICE DOOR SILL PLATES CORRODED LOCATED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE SILL PLATES IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (SERVICE DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR AND SERVICE DOOR SILL PLATES CORRODED LOCATED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE SILL PLATES IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0036. (M)

Part: LIGHT — CORRODED (CABIN)

MIA - FLT 5379 - EMERGENCY LIGHT ON PAX ENTRY DOOR DOES NOT WORK. REPLACED LIGHT ASSEMBLY AND REPAIRED BROKEN WIRE AT CANNON PLUG 253VC. OPS CHECK GOOD. (M)

Part: BULB — INOPERATIVE (CABIN)

JAX - FLT 5247 - MAIN CABIN DOOR GROUND EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: UPLOCK SWITCH — FAILED (NLG)

MIA - FLT 5265 - NOSE GEAR UNLOCK DURING CRUISE FLIGHT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK SWITCH. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (FUSELAGE)

MIA - FLT 5340 - EMERGENCY EXIT LIGHT ILLUMINATE WHEN SWITCH IS PLACED IN THE ARM POSITION. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 5311 - FORWARD EMERGENCY LIGHT STAYS ON. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK 3WL. OPS CHECKS GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 5356 - EMERGENCY EXIT LIGHT ON DURING FLIGHT. REMOVED AND REPLACED BATTERY IN SUPPLY UNIT. OPS CHECK GOOD. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATTENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATTENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WEB — CORRODED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT WEB FORWARD OF THE PASSENGER DOOR BETWEEN FRAMES 35 AND 36 ARE CORRODED. REMOVED AND REPLACED THE WEB IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATTENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATTENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATTENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATTENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND CORROSION ON FLOORBEAM 36 AROUND NUTCLIPS. REMOVED AND REPLACED FLOORBEAM 36 IAW EO E2-53-00-029. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, FOUND THREE DENTS IN THE LOWER SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 41 AND 43 AND STRINGERS 20 AND 21, MEASURING 2.17 BY 1.34 BY .080, AND 1.50 BY .058, AND 1.50 BY .052 INCHES. REPAIRED THE DENTS IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, FOUND TWO DENTS IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 39 AND 42 AND STRINGERS 11 AND 12, MEASURING 1.27 BY .060 AND 1.37 BY .78 BY .056 INCHES. REPAIRED THE DENTS IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981201, 98ZZZX1964, AND 98ZZZX1966.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981201, 98ZZZX1964, AND 98ZZZX1965.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1964, 98ZZZX1965, AND 98ZZZX1966. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981201, 98ZZZX1965, AND 98ZZZX1966.

Part: ZEE — CORRODED (FUSELAGE)

SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT ZEE MEMBER LOCATED BETWEEN FRAMES 39 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT ZEE MEMBER IAW SRM 51-21-28. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1967. (X)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL SIMA981193

Part: BATTERY — DISCHARGED (CABIN)

ORD - FLT 4234 - AFT EMERGENCY LIGHTS AND AFT EXT SIGN OUT. RAI BATTERY PACK 62WL AS REQUIRED. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SAW - DURING PS-2 CHECK MAINTENANCE DISCOVERED THE NR 1, 3, 5, 7 AND 9 FLOOR PROXIMITY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT LOCATION 43WL. AN OPERATIONAL CHECK WAS PERFORMED IAW JIC 33-50-00-OPT AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS IN CABIN DON'T COME ON CORRECTLY. RAI'D BATTERY PACK 43WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - FLT 3620 - APPROXIMATELY HALF OF THE EMERGENCY EXIT LIGHTS IN THE CABIN WILL NOT EXTINGUISH UNLESS THEY ARE SELECTED OFF AND THE EMERGENCY EXIT LT CB IS PULLED. REPLACED EMERGENCY LIGHTING POWER SUPPLY AT 6WL. OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: SWITCH — FAILED (NLG)

DFW - FLT NR 3651 - NOSE LANDING GEAR UPPER PANEL INDICATES UNLOCK INFLIGHT AND THE GEAR IS MAKING A CLICKING SOUND. MX REPLACED THE NOSE GEAR UPLOCK MICROSWITCH. CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3819 - CENTER AIRCRAFT EMERGENCY LIGHTS STAYED ON ALL THE TIME. MAINTENANCE REPLACED THE NR 2 BATTERY PACK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: UPLOCK BOX — FAILED (RT MLG)

YHZ - FLT 4398 - RT MLG SHOWED UNLK ON BOTH INDICATION PANELS, RETURNED TO YHZ. MAINTENANCE PINNED GEAR THEN ISSUED MEL. DEAD HEADED AIRCRAFT TO ALB. MAINTENANCE REMOVED AND INSPECTED UPLOCK BOX SYSTEM. OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TQ PROBE — DEFECTIVE (NR 1 ENGINE)

AFTER TAKEOFF FROM DFW, AIRCRAFT EXPERIENCED A NR 1 ENGINE TORQUE FLUX WITH YAW. CREW SHUT DOWN ENGINE AS A PRECAUTIONARY. REPLACED NH PROBE ON NR 1 ENGINE, PERFORMED GROUND MAINTENANCE RUNS AND PERFORMED SATISFACOTRY TEST FLIGHT. AIRCRAFT RELEASED FOR SERVICE. (W)

Part: RECIRC FAN — FAILED (RIGHT)

ACT - FLT 3833 - DURING CRUISE FLIGHT, CREW SMELLED ODOR OF SMOKE. AIRCRAFT DIVERTED TO ACT AND CFR DECLARED. AIRCRAFT LANDING MADE WITHOUT INCIDENT. EMERGENCY EVACUATION WAS CONDUCTED. MTX INSPECTED, FOUND SMELL TO COME FROM NR 2 RECIRC FAN. MEL'D FAN AND CONTINUED FLIGHT TO DFW. DFW MTX REPLACED FAN. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2578. (X)