N314AM

Part: SWITCH — INOPERATIVE (RT MAIN GEAR)

MCO - FLT 5410 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. CREW FOUND LDG BREAKER OUT. LANDING GEAR PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG PROXIMITY SWITCH IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (LT ENGINE) · airframe 17,464 hrs · 19,682 cycles

MIA - FLT 5356 - DURING LANDING, THE CREW REPORTED HEARING A BANG FROM THE NR 1 ENGINE, FOLLOWED BY MILD SMOKE IN THE COCKPIT AND A LOW OIL PRESSURE LIGHT. CREW SHUT DOWN THE NR 1 ENGINE AND REQUESTED CFR. CFR MET THE AIRCRAFT AT THE END OF THE LANDING ROLL. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE IAW ATRMM. OPS AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LINK — UNSERVICEABLE (LT WING)

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD LOWER WING TO FUSELAGE JUNTION ROD (DOG BONE) HAD AN EXCESSIVELY TIGHT BEARING AND PITTED BUSHING. MAINTENANCE REMOVED AND REPLACED THE JUNCTION ROD IAW JIC 57-15-21-RAI-10000-006. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FITTING — DEFECTIVE (LT WING)

SAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4 FORWARD INBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. MAINTENANCE REPAIRED THE HOLES IAW EO E1-57MR-081. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FITTING — DEFECTIVE (RT WING)

SAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4 FORWARD INBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. MAINTENANCE REPAIRED THE HOLES IAW EO E1-57MR-081. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SPAR — DEFECTIVE (RT WING)

SAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4 FORWARD INBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. MAINTENANCE REPAIRED THE HOLES IAW EO E1-57MR-081. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FITTING — DEFECTIVE (LT WING)

SAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4 FORWARD INBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. MAINTENANCE REPAIRED THE HOLES IAW EO E1-57MR-081. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FITTING — DEFECTIVE (RT WING)

SAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4 FORWARD INBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. MAINTENANCE REPAIRED THE HOLES IAW EO E1-57MR-081. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FITTING

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE LEFT AFT LOWER WING TO FUSELAGE FITTING AT FRAME 27 RIB 4 BEARING FROZE. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW JIC 535740-RAI-10000-001. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ANGLE — BENT (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT LOWER SHEAR WEB ANGLE BETWEEN FRAME 25 AND 27 BENT. MAINTENANCE REMOVED AND REPLACED THE SHEAR WEB ANGLE IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MOUNT — GOUGED (LT NACELLE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE LEFT ENGINE W MOUNT FORWARD TUBE GOUGED. MAINTENANCE REMOVED AND REPLACED THE W MOUNT IAW JIC 54-11-61-RAI-10000-004. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — MISDRILLED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED A MISDRILLED HOLE IN THE FUSELAGE SKIN AT FRAME 40 BETWEEN STRINGER 21L AND 21R. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 407. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM 38 AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3072. (M)

Part: STRINGER — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED STRINGER 15 RIGHT BETWEEN FRAMES 36 AND 40 CORRODED, AND STRINGER 16 RIGHT BETWEEN FRAMES 36 AND 37 CORRODED. MAINTENANCE REPAIRED THE STRINGERS IAW SRM 53-00-00 FIGURE 428. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED STRINGER 15 RIGHT BETWEEN FRAMES 36 AND 40 CORRODED, AND STRINGER 16 RIGHT BETWEEN FRAMES 36 AND 37 CORRODED. MAINTENANCE REPAIRED THE STRINGERS IAW SRM 53-00-00 FIGURE 428. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PLATE — CORRODED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED FRAME 27A CORRODED. MAINTENANCE REMOVED AND REPLACED FRAME 27A IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM 38 AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3072. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAME 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PLATE — CORRODED (WHEEL WELL)

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE KEEL BEAM LOWER PLATE IN THE MAIN LANDING GEAR WELL CORRODED. MAINTENANCE REMOVED AND REPLACED THE PLATE IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM 38 AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED FRAME 26 RIGHT, CRACKED AT THE UPPER RADIUS ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE UPPER SECTION OF FRAME 26 RIGH IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE UPPER SECTION OF FRAME 26 CRACKED AT CENTER WING BOX ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE FRAME IAW SRM 51-25-04. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT INTERCOSTAL AFT OF FRAME 27 AT STRINGER 4 CRACKED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — BENT (FUSELAGE)

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE LEFT STRINGER 4 INTERCOSTAL BETWEEN FRAME 25 AND 27 BENT. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-25-04. (M)

Part: WEB — CRACKED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE LEFT UPPER WEB AT THE TOP OF FRAME 26 CRACKED. MAINTENANCE REMOVED AND REPLACED THE WEB IAW SRM 51-25-04. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT INTERCOSTAL BETWEEN FRAME 25 AND 27 AT STRINGER 4 CRACKED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (PAX STAIRS)

MIA - FLT 5227 - EMERGENCY EXIT LIGHT ON STAIRS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — MISSING (CABIN)

MIA - FLT 5356 - FORWARD TOP EMERGENCY EXIT LIGHT INOPERATIVE. FUOND BATTERY PACK MISSING. INSTALLED EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M)

Part: LIGHT — FAILED (CABIN)

SAW - DURING PS-2 INSPECTION, FOUND THE PASSENGER DOOR EMERGENCY LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN JUST FORWARD OF THE WINDSHIELD CENTER LINE BETWEEN FRAME 2 AND 3, MEASURING 2 INCHES BY 1 INCH BY .032 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 408 AND SRAS ASI/E/35391/99. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — PUNCTURED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, CLEARED TDMI NR 14AMQ53002A, RIGHT FORWARD UPPER LATERAL SKIN TEMPORARY REPAIR. REMOVED AND REPLACED RIGHT FORWARD UPPER LATERAL SKIN BETWEEN FRAME 1 AND 13 IAW 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FRAME 43)

SAW - DURING MBV-1 INSPECTION, FOUND A DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN AT FRAME 43 BETWEEN STRINGER 8 AND 9, MEASURING 24MM BY 3MM BY .044 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACKS — CORRODED (FUSELAGE)

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

Part: SEAT TRACKS — CORRODED (FUSELAGE)

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

Part: SEAT TRACKS — CORRODED (FUSELAGE)

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

Part: SEAT TRACKS — CORRODED (FUSELAGE)

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

Part: SEAT TRACKS — CORRODED (FUSELAGE)

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

Part: SEAT TRACKS — CORRODED (FUSELAGE)

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

Part: DRAIN TRACK — CORRODED (SERVICE DOORWAY)

SAW - DURING CPCP-2 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE DRAIN TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — DENTED (FRAME 12-13)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 WITH AN OVERSIZED HI-LOCK HOLE. SPLICED IN NEW SECTION OF FLOORBEAM 2 INCH BY 7 INCH BY .067 DEEP DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 12 AND 13 AND STRINGERS 9 AND 13. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403 AND 407. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FRAME 12-13)

SAW - DURING MBV-1 INSPECTION, FOUND A 2 INCH BY 7 INCH BY .067 DEEP DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 12 AND 13 AND STRINGERS 9 AND 13. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403 AND 407. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CHORD — CORRODED (FRAME 36-38)

SAW - DURING MBV-1 INSPECTION, FOUND THE RIGHT OUTER CHORD BETWEEN FRAMES 36 AND 38 AT STRINGER 17 CORRODED. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 53-16-14. AIRCRAFT RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CORRODED (FRAME 36-38)

SAW - DURNIG MBV-1 INSPECTION, FOUND THE RIGHT INTERCOSTAL BETWEEN FRAMES 36 AND 38 AT STRINGER 17 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FRAME 1-2)

SAW - DURING MBV-1 INSPECTION, FOUND A 2 INCH BY 1 INCH BY .066 DEEP DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 1 AND 2 AND STRINGERS 10 AND 11. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (FRAME 13-14)

ABI - AIRCRAFT ARRIVED FOR REPAIR OF DAMAGE ON LEFT FUSELAGE SKIN PANEL BETWEEN FRAMES 13 AND 14 DAMAGED JOINT STRIGNERS 10 AND 11. REMOVED DAMAGED JOINT STRINGERS 10 AND 11. RECONTOURED SKIN PANEL BETWEEN FRAMES 13 AND 14 AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACKS FOUND. FABRICATED AN EXTERNAL DOUBLER .063. TREATED DOUBLER AND JOINT STRINGERS WITH ALODINE AND ONE COAT OF PRIMER. INSTALLED DOUBLER AND STRINGERS. APPLIED POLYURETHANE TOP COAT TO EXTERNAL AND INTERNAL SURFACES FO REPAIR AREA. APPLIED WATER REPELLENT PROTECTIVE COATING TO INNER REPAIR AREA. WORK DONE IAW ATR SRM 53-00-00 PAGE 418-421, FIG 405. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — PUNCTURED (FRAME 2-3)

FOUND 8 INCH SKIN PUNCTURE ON RIGHT SIDE OF NOSE SECTION BETWEEN FRAMES 2 AND 3. REPAIRED SKIN. AIRCRAFT RETURNED TO SERVICE. (M)

Part: GEAR HANDLE — SHORTED (FLT DECK)

FLT 4519 - CLE - CREW REPORT LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. CREW USED EMERGENCY EXTENSION SYSTEM. REPLACED LANDING GEAR SELECTOR HANDLE.