N923FX

Part: CONTACTOR — BURNED (ANTI-ICE SYS) · airframe 32,924 hrs · 41,168 cycles

WO 207043 NR 1 FLIGHT 8737/ DISCREPANCY: DURING ENGINE START, SPARKS AND ELECTRICAL SMELLING SMOKE IN COCKPIT WERE DETECTED. ENGINE WAS SHUTDOWN. CORRECTIVE ACTION: MAINTENANCE TROUBLESHOT AND FOUND PROP ANTI-ICE CONTACTOR AND ASSOCIATED POWER WIRES BURNT. REPLACED THE 1DH PROP DEICE CONTACTOR AND REPLACED WIRES. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — FOD (RT ENGINE FUEL) · airframe 32,886 hrs · 41,110 cycles

TWO INCH POWER LEVER SPLIT, RT POWER LEVER FORWARD. MAINTENANCE REPLACED THE RT FUEL PUMP AND FUEL CONTROL UNIT. ON FURTHER INVESTIGATION, DISCOVERED FOD IN THE FUEL INLET PORT, CHAFING ON INTERNAL TUBE. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100028 HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM IS CRACKED FWD OF FRAME 30. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100009 HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 33-34. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100013 HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 22. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100007 HEAVY CHECK COE/MAJOR REPAIR: RT LONGITUDINAL FLOORBEAM FWD OF FRAME 33 IS CRACKED. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100011 HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 20. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100014 HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM IS CRACKED FWD OF FRAME 26. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,884 hrs · 41,106 cycles

WO 196790 NR 100012 HEAVY CHECK COE/MAJOR REPAIR: RT LONGITUDINAL FLOORBEAM IS CRACKED FORWARD OF FRAME 20. CORRECTIVE ACTION: REPAIR PER EO 5315-01.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 32,808 hrs · 41,027 cycles

DISCREPANCY: FIRST OFFICERS LEFT BRAKE INOP. CORRECTIVE ACTION: BLED ALL LOW PRESSURE BRAKE LINES. OPS NORMAL ON ALL BRAKE PEDALS DURING TAXI.

Part: MOUNT — GOUGED (RT ENGINE) · airframe 32,300 hrs · 40,503 cycles

RIGHT ENGINE AFT MOUNT TUBE NR 6 IS GOUGED. REPAIRED IAW PCE-1287/17.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MAJOR REPAIR: CARGO DOOR, 5TH FAME AFT, OUTER FLANGE IS CRACKED AT LEVEL OF THE DOOR HINGE. REPAIR PER SRM 523100-300-805-A01.

Part: PAN — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FORWARD CARGO DOOR UPPER PAN HAS LEVEL 2 CORROSION AT THE AFT EXTERNAL CORNER. REPAIRED IAW PCE-1014/17.

Part: INTERCOSTAL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FORWARD CARGO DOOR UPPER DOOR FRAME INTERCOSTAL HAS CORROSION ON THE LOWER SURFACE AFT OF FRAME 14. REPAIRED IAW ES-2654/17.

Part: CREASE BEAM — CORRODED (FRAMES 29-30) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

LEFT CREASE BEAM INNER ANGLE HAS CORROSION FRAMES 29-30. REPAIRED IAW SRAS ES-2637/17.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT WING REAR SPAR UPPER STRIP SLAT HAS LEVEL 2 CORROSION BETWEEN RIBS 13-21 LT. REPAIRED PER SRAS ES-2621/17. 11614 DATED 7/6/2017.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MAJOR REPAIR: STRINGER 21R HAS LEVEL 2 CORROSION BETWEEN FRAMES 31-32. REPAIRED PER SRAS PCE-933/17. 11542 DATED 6/22/2017.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MINOR REPAIR: SHEAR TIE AT STRINGER 21 LT AND FRAME 11 HAS LEVEL 2 CORROSION. REPLACED SHEAR TIE(FLANGE DOUBLER) WITH OEM.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

SKIN SURROUNDING AFT CARGO DOOR HAS CORROSION FROM CONTACT WITH AFT SHOOT BOLT. REPAIRED IAW EO 42R25100-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,300 hrs · 40,503 cycles

SKIN SURROUNDING AFT CARGO DOOR HAS DENT FROM CONTACT WITH SECOND FROM BOTTOM FORWARD SHOOT BOLT. REPAIR IAW EO 42R25100-02.

Part: INTERCOSTAL — CORRODED (FRAMES 27A-28A) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

CORROSION ON INTERCOSTAL STRINGER 20R FRAME 27A-28A. REPLACED THE INTERCOSTAL.

Part: SKIN — CORRODED (FRAMES 14-17) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

CORROSION FOUND ON THE FWD CENTER FUSELAGE LT LOWER SKIN PANEL AROUND THE FWD CARGO DOOR. REPAIRED IAW PCETS-859/17.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON FORWARD PRESSURE BULKHEAD LOWER STIFFENER CLIP, RBL 187 INBOARD. REPLACED CLIP WITH OEM PART.

Part: LANDING — CORRODED (LT WING) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MAJOR REPAIR: FUEL PANEL 522CT LANDING HAS FRETTING DAMAGE, LEVEL 2. REPAIRED PER SRAS DO/TS-3988/07...4261 DATED 7/4/2017.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD HAS CORROSION BELOW TRIM ACTUATOR. REPAIRED IAW SRAS ES-2577/17.

Part: SPAR — DAMAGED (RT WING) · airframe 32,300 hrs · 40,503 cycles

RIGHT WING FRONT SPAR UPPER FLANGE HAS TWO WORN HOLES AT RIB 10. REPAIRED THE SPAR IAW ES-2663/17.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

PANEL LANDING 521DT CORRODED. REPAIRED IAW SRAS DO/TS-3988/07.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON FORWARD PRESSURE BULKHEAD LOWER CLIP, RBL 187 OUTBOARD. REPLACED WITH OEM PART.

Part: STRAP — CORRODED (FRAME 16) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

SKIN STRAP AT FRAME 16 HAS CORROSION FORWARD OF THE FRAME, BELOW STRINGER 10R. REPAIRED IAW SRAS PCETS-852/17.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

RIGHT REAR RIB 23 HAS AREAS OF CORROSION. REPAIRED IAW ES-2409/17.

Part: STRAP — CORRODED (FRAME 16) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

SKIN STRAP AT FRAME 16 CORRODED FORWARD OF THE FRAME, BELOW STRINGER 9R. REPAIRED IAW PCETS-852/17.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

LEFT WING REAR SPAR UPPER STRIP SLAT HAS CORROSION AT THE INBOARD END OF THE SPOILER. REPAIRED IAW ES-2621/17.

Part: FITTING — CHAFED (LT WING TE FLAP) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

LEFT OTBD FLAP FITTING AT FLAP RIB 10, WING RIB 13 HAS CHAFING DAMAGE FROM FLAP INTERCONNECT ROD. REPAIRED IAW SRAS ES-2568/17.

Part: STIFFENER — CORRODED (FRAMES 29-30) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

DURING HEAVY CHECK, CORROSION WAS FOUND ON THE RT CREASE BEAM LOWER STIFFENER, FRAMES 29-30. REPLACED WITH OEM PART.

Part: CREASE BEAM — CORRODED (FRAMES 27-28) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAMES 27-28 RT INNER CREASE BEAM ANGLE CORRODED. REPLACED .

Part: STRINGER CLIP — CORRODED (FRAME 32) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

CORROSION FOUND ON FRAME 32 STRINGER CLIP 20R. REPLACED WITH OEM PART.

Part: STRINGER CLIP — CORRODED (FRAME33) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME 33, STRINGER 20R CLIP CORRODED. REPLACED THE STRINGER CLIP.

Part: WEB — CORRODED (FRAMES 27-28) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAMES 27-28 CREASE BEAM WEB CORRODED AROUND FLOOR PANEL HOLES. REPLACED.

Part: MOUNT FITTING — SCRATCHED (FUSELAGE) · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MAJOR REPAIR: SCRATCHES ON FRAME 27 RT BULKHEAD ON THE FLOORBOARD MOUNT SURFACE BETWEEN THE RT SEAT TRACKS. REPAIRED PER SRAS PCETS-834/17 11537 DATED 6/23/2017.

Part: STRINGER — GOUGED (FRAME 16) · airframe 32,300 hrs · 40,503 cycles

GOUGE AT STRINGER 3A, FRAME 16. REPAIRED IAW SRM 530000-300-826-A01.

Part: STRINGER CLIP — CORRODED (FRAME 32) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME 32, STRINGER CLIP AT 18R CORRODED. REPLACED THE STRINGER CLIP.

Part: FRAME — CORRODED (FRAME 37) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME 37 AFT FLANGE BETWEEN STRINGERS 13 - 14R CORRODED. REPLACED THE FRAME SEGMENT.

Part: FRAME — CORRODED (FRM 28) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME 28 FLANGE BETWEEN STRINGERS 16L - 17L HAS CORROSION ON THE AFT SURFACE. REPAIRED IAW PCETS-2355/17.

Part: STRINGER — GOUGED (FRAMES 15-16) · airframe 32,300 hrs · 40,503 cycles

GOUGE ON STRINGER 4R, FRAMES 15-16. THE STRINGER WAS REPAIR IAW SRM 530000-300-826-A01.

Part: STRINGER CLIP — CORRODED (FRAME 33) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME 33, STRINGER CLIP 18R CORRODED. REPLACED THE STRINGER CLIP.

Part: WEB — CORRODED (FRAMES 18-19) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

CORROSION FOUND ON THE LT CREASE BEAM WEB, FRAMES 18 - 19. REPLACED.

Part: FRAME — CORRODED (FRM 31) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME 31 LOWER FLANGE BETWEEN STRINGERS 18 - 19R HAD CORROSION. REPAIR IAW SRAS PCETS-864/17.

Part: STIFFENER — CORRODED (FRAMES 41-42) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAMES 41-42, LT CREASE BEAM STIFFENER HAS CORROSION. REPLACED THE STIFFENER.

Part: FRAME — CORRODED (FRM 28) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

FRAME FLANGE 28 BETWEEN STRINGERS 20L - 21L HAS CORROSION ON THE AFT SURFACE. REPAIRED IAW PCETS-2355/17.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 32,300 hrs · 40,503 cycles

CARGO DOOR, 4TH FRAME AFT, OUTER FLANGE AT THE LEVEL OF THE HINGE IS CRACKED. REPAIRED IAW SRM 523100-300-805-A01.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 32,300 hrs · 40,503 cycles

CARGO DOOR, 8TH FRAME AFT, OUTER FLANGE IS CRACKED AT THE LEVEL OF THE DOOR HINGE. REPAIRED IAW PCE-1014/17.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 32,300 hrs · 40,503 cycles

HEAVY CHECK COE/MAJOR REPAIR: CARGO DOOR, 7TH FRAME AFT, OUTER FLANGE IS CRACKED AT LEVEL OF DOOR HINGE. REPAIR PER SRM 523100-300-805-A01.

Part: RIB — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 32,300 hrs · 40,503 cycles

RIGHT HORIZONTAL STABILIZER OUTBOARD RIB HAS CORROSION ON THE EXTERIOR SURFACE. REPAIRED IAW PCE-1044/17.

Part: LEAD — DAMAGED (PROP HEATER) · airframe 32,264 hrs · 40,444 cycles

CREW RECEIVED A NR 1 PROP ANTI ICE FAULT. ELECTED TO RETURN TO DEPARTURE DUE TO ICING CONDITIONS EXPECTED. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 PROP HEATER LEAD. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LEVER — LOCKED (MLG) · airframe 32,204 hrs · 40,352 cycles

AFTER DEPARTURE, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT WAS RETURNED TO DEPARTURE, NO EMERGENCY DECLARED. AFTER TROUBLESHOOTING, MAINTENANCE REPLACED THE GEAR LEVER 4GA AND RELAY 29GB. NUMEROUS GEAR SWINGS WERE PERFORMED WITH NO MALFUNCTIONS. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — CORRODED (MLG) · airframe 32,201 hrs · 40,350 cycles

LANDING GEAR WOULD NOT RETRACT AFTER MULTIPLE ATTEMPTS. THE CREW ELECTED TO RETURN TO DEPARTURE, NO EMERGENCY WAS DECLARED. MAINTENANCE JACKED UP THE AIRCRAFT, FOUND CORROSION ON PINS AND SOCKETS OF CONNECTOR 5002VP. CLEANED PINS AND SOCKETS. ALL LANDING GEAR INDICATIONS OPERATED NORMALLY, PERFORMED NUMEROUS GEAR SWINGS WITH NO DISCREPANCIES. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 32,200 hrs · 40,347 cycles

FLIGHT 7358 IDA TO SLC, AIR TURNBACK DISCREPANCY: AFTER TAKEOFF ON CLIMBOUT, THE LANDING GEAR WOULD NOT RETRACT NORMALLY. CYCLING THE GEAR HANDLE HAD NO EFFECT. SIMULTANEOUSLY, THE CREW RECEIVED A "DON'T SINK" WARNING (ALTHOUGH THE AIRCRAFT WAS WELL ABOVE ANY TERRAIN) AND INTERMITTENT STICK SHAKER. CREW ELECTED TO RETURN TO IDA, NO EMERGENCY WAS DECLARED. AFTER EXTENSIVE TROUBLESHOOTING MAINTENANCE REPLACED THE LG CONTROL LEVER AND RADIO ALTIMETER TRANSCEIVER. OPS CHECKS GOOD AND OCF WAS SATISFACTORY. PN LG CONTROL LEVER, F96GA0102 SN 124: TRANSCEIVER, 9599-607-14562 SN 4575.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. CTR FUSELAGE CROWN PANEL, BETWEEN FRAMES 23 - 24, INTERNAL SKIN HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 5362 15 9696 DATED 10 23 15.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT UPPER INTERIOR FUSELAGE SKIN HAS LEVEL 2 CORROSION & SCRATCH DAMAGE, EXCEEDING SRM LIMITATIONS. REPAIR IAW SRM 42 530000-300-834-A01-001-01 REV 106.

Part: SKIN — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. VERTICAL STABILIZER LE 323AL HAS AREAS OF LEVEL 2 CORROSION UNDER THE DE-ICE BOOT. REPAIR IAW SRAS ES-5185 15 9718 DATED 11 6 15.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. STRINGER 12L IS DAMAGED AT FRAME 21. SPLICE REPAIR IAW SRM 530000-300-826-A01.

Part: STRIP — DAMAGED (RT WING) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT WING FWD SPAR LOWER STRIP SLAT HAS LEVEL 2 FRETTING DAMAGE, INBD OF RIB 5. REPAIRED IAW SRAS DT S-5890 13 8054 DATED 10 15 15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. UPPER FLOORBEAM 41 HAS LEVEL 1 CORROSION NEAR THE RT OTBD FWD EDGE ON THE UPPER FLANGE. REPAIRED IAW SRAS CE-5309 15 9701 ISSUE A DATED 11 2 15.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. CTR FUSELAGE, LT UPPER SKIN PANEL HAS NUMEROUS AREAS OF INTERNAL LEVEL 2 CORROSION, FRAMES 23 - 25, STRINGER 6A - 10A. REPAIRED IAW SRAS ES-5457 15 9750.

Part: FITTING — WORN (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. NLG, LT AFT DOOR, AFT FUSELAGE FITTING HAS PLAY. REPLACED PART BY FABRICATION.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT LONGITUDINAL FLOORBEAM CRACKED, BETWEEN FRAMES 24 - 25. REPAIRED IAW EO 5315-01 REV F.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS AREAS OF LEVEL 2 CORROSION, 11.2" FWD OF FRAME 22 AT STRINGER 11-11A. REPAIR IAW SRAS CE-5345 15 9684 DATED 10 23 15.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS AREA OF LEVEL 2 CORROSION, 2.5" FWD OF FRAME 22, .78" ABOVE STRINGER 10A. BLEND REPAIR IAW SRAS CE-5345 15 9684 DATED 10 23 15.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD FUSELAGE LT UPPER SKIN PANEL HAS NUMEROUS AREAS OF LEVEL 2 CORROSION, FRAME 20 - 23, STRINGER 4 - 12A. REPAIR IAW SRAS ES-5456 15 9754 DATED 9754.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS AREA OF LEVEL 2 CORROSION, 2" AFT OF FRAME 23, 1.1" ABOVE STRINGER 10A. BLEND REPAIR IAW SRAS CE-5345 15 9684 DATED 10 23 15.

Part: LANDING — DAMAGED (RT NACELLE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT NACELLE INBD LATERAL PANEL LANDING HAS LEVEL 2 FRETTING DAMAGE WITH A GOUGE AT THE BOTTOM OF THE LANDING. REPAIR IAW SRAS CE 5326 15 9686 DATED 10 20 15.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT LONGITUDINAL FLOORBEAM CRACKED, BETWEEN FRAMES 28 - 29. REPAIRED IAW EO 5315-01 REV F.

Part: SKIN — CORRODED (RT WING) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT WING INBD UPPER REMOVABLE PANEL CUT OUT FOR ACCESS DOOR 622CT HAS LEVEL 1 CORROSION. THE CUT OUT WAS BLENDED SMOOTH IAW SRM 511412-300-80. REPAIRED IAW SRAS DO TS-3988 07 4261 ISSUE DATED 10 22 15.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MINOR REPAIR. LT PRESS DECK FREE FALL CABLE PASS THROUGH, HAS LEVEL 2 CORROSION BEYOND SRM LIMITATIONS. REPLACED WITH OEM PART.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT LONGITUDINAL FLOORBEAM CRACKED, BETWEEN FRAMES 36 - 40. REPAIRED IAW EO 5315-01 REV F.

Part: LANDING — DAMAGED (LT NACELLE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT NACELLE OTBD LATERAL PANEL, LANDING HAS LEVEL 2 FRETTING DAMAGE WITH A GOUGE AT THE BOTTOM OF THE LANDING. REPAIR IAW SRAS CE-5323 15 9685 DATE 10 20 15.

Part: DOUBLER — DAMAGED (RT NACELLE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MINOR REPAIR. RT NACELLE OTBD LATERAL PANEL LANDING HAS LEVEL 2 FRETTING & GOUGING. REPLACED WITH OEM PART.

Part: LANDING — DAMAGED (LT NACELLE) · corrosion level 2 · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MINOR REPAIR. LT NACELLE INBD LATERAL PANEL AFT LANDING, HAS LEVEL 2 FRETTING & GOUGING. REPLACED WITH OEM.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 31,794 hrs · 39,842 cycles

HEAVY CHECK COE & MAJOR REPAIR. AFT ENTRY DOOR SECOND SHOOT BOLT FITTING FROM TOP, AT FRAME 39, HAS IMPACT DAMAGE. REPAIRED IAW SRAS CE 5256 15 9699 DATED 11 05 15.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 31,695 hrs · 39,762 cycles

FLIGHT 8291, DISCREPANCY, DURING CLIMB OUT, THE LG INDICATING LIGHTS CYCLED LOCKED TO UNLOCKED SEVERAL TIMES. THE CREW COULD HEAR THE LG BANGING AS IT WAS TRYING TO LOCK IN PLACE. THE CREW TRIED SEVERAL MORE TIMES & FINALLY IT LOCKED IN PLACE. ACFT RETURNED, NO EMER WAS DECLARED & LANDING WITHOUT FURTHER INCIDENT. REPLACED THE LG SELECTOR VLV. RETRACTION NORMAL, OPERATIONS CHECKED GOOD, NO LEAKS FOUND. ACFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (TORQUE INDICATOR) · airframe 31,126 hrs · 39,184 cycles

DURING CLIMB OUT, NR 1 TORQUE INDICATOR JUMPED TO 120%. DECLARED AN EMERGENCY & PERFORMED AN ENGINE SHUTDOWN. RETURNED TO DEPARTURE & LANDED SAFELY. AFTER TROUBLESHOOTING, DETERMINED THE CAUSE TO BE AN EXPOSED OR BROKEN WIRE ON CONNECTOR 417VC WIRE D. REMOVED EXPOSED SECTION OF WIRE, PINED & INSTALLED. ALSO REPLACED CONNECTOR 417VC. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FRAME SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, FRAME 8 SPLICE AT BL 0 HAD CORROSION. REPLACED WITH OEM PART.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, CORROSION FOUND ON STRINGER CLIP AT FRAME 10 AND STRINGER 20R. REPLACED STRINGER CLIP BY FABRICATION.

Part: SUPPORT FITTING — CORRODED (RUDDER PEDAL) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

HEAVY CHECK COE/MINOR REPAIR: FLOOR MOUNT FITTING FOR THE RT RUDDER PEDALS HAS LEVEL 2 CORROSION ON THE UPPER SURFACE AT FLOORBEAM 5. REPLACED WITH OEM PART.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, RT FLOORBEAM FLANGE AT FRAME 9 CORRODED ON THE UPPER SURFACE. REPAIR IAW SRAS DT/S-5911/13.

Part: FRAME SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, FRAME 10 DOUBLER AT STRINGER CUTOUT TO THE RT OF BL 0 HAD CORROSION. REPLACED FRAME SPLICE WITH OEM PART.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, FLOORBEAM 7 UPPER SURFACE CORRODED ON BOTH SIDES OF THE PEDESTAL. REPAIR IAW SRAS DT/S-5716/13.

Part: STIFFENER — CORRODED (ZONE 300) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, CORROSION FOUND ON TEE STIFFENER. REPLACED WITH NEW OEM PART.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, FLOOR FITTING FOR THE LT CONTROL COLUMN IS CORRODED JUST FORWARD OF FLOORBEAM 7. REPLACED WITH OEM PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

FLOOR BEAM 11 UPPER SURFACE HAS LEVEL 2 CORROSION & SEVERE TOOLING DAMAGE. ALL DAMAGED AREAS HAVE BEEN BLENDED & IN LIMITS EXCEPT THE TOOLING DAMAGED AREA. REPAIR IAW SRAS DT S 5864 13 8080 11/21/2013.

Part: STRUCTURE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

HEAVY CHECK, MAJOR REPAIR. AFT DORSAL FIN HAS NUMEROUS AREAS OF LEVEL 2 CORROSION AROUND THE NUT PLATES. REPLACED PART BY FABRICATION IAW ATR42 SRM 55-35-30 REV 100 FIGURE 101.

Part: PAN — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, AFT RT SERVICE DOOR FWD PAN CORRODED. REPAIRED IAW SRAS DT/S-5781/13.

Part: SPAR — CHAFED (RT WING) · airframe 30,905 hrs · 38,940 cycles

RIGHT WING FWD SPAR LOWER STRIP SLAT HAS CHAFFING DAMAGE AT INBD END OF LE PANEL 611. BLEND REPAIR IAW SRAS DT S 4818/13 7978 DATED 11/6/2013.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

HEAVY CHECK, MINOR REPAIR. LEFT WING INBD TE PANEL INBD ATTACH STRUT BRACKET HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, LEFT WING OTBD FLAP INNER SURFACES & DEFLECTOR HAVE CORROSION. FLAP REPLACED WITH NEW IAW AMM 57-53-00.

Part: SPAR — CHAFED (RT WING) · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, RT WING FWD SPAR LOWER STRIP-SLAT HAS CHAFING DAMAGE AT INBD END OF PANEL 611. BLEND REPAIR IAW SRAS DT/S-4818/13.

Part: STRIP — DAMAGED (LT WING) · airframe 30,905 hrs · 38,940 cycles

HEAVY CHECK, MAJOR REPAIR. LEFT WING FWD SPAR LOWER STRIP SLAT HAS FRETTING DAMAGE RIB 13 - RIB 15. REPAIR IAW SRAS S572R0320 8066.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

HEAVY CHECK, MINOR REPAIR. LEVEL 2 CORROSION FOUND ON FRAME 24A WEB, FLANGE & SUPPORT BRACKET. REPAIR IAW SRM 53-91-43 2B, MINOR REPAIR DUE TO SECONDARY STRUCTURE.

Part: STRINGER CLIP — CORRODED (FRAME 24) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, STRINGER CLIP AT FRAME 24 HAS CORROSION. REPLACED WITH NEW OEM PART.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 30,905 hrs · 38,940 cycles

DURING HEAVY CHECK, LT UPPER WING CUT-OUT FOR PANEL 522CT HAS FRETTING ON TOP SURFACE. REPAIR IAW SRAS DO/TS-3988/07, 4261, REV D.

Part: STRUCTURE — CORRODED (CENTER WING) · airframe 29,018 hrs · 36,386 cycles

DURING INSPECTION, FRETTING CORROSION WAS FOUND ON THE CENTER WING CUTOUT OF THE FUEL PANEL HOUSING AT 522CT. REFERENCE ATR42 SRM 57-14-12 PAGE 302 FIG 301 SHEET 1. AFTER DAMAGE REMOVAL THE REMAINING THICKNESS IS 0.425 AROUND THE ENTIRE CIRCUMFERENCE OF THE DOOR HOUSING. THE REPAIR IS IAW ATR 42 STRUCTURAL REPAIR INSTRUCTION DO/TS-3988/079267 REF: ANA/E/4237/2007/E-001. APPLICABILITY: ATR 42 MSN 135 DATED 09/21/2007.

Part: TEE FITTING — CORRODED (AILERON) · airframe 29,018 hrs · 36,386 cycles

DURING INSPECTION, LEVEL 3 CORROSION WAS FOUND ON 4 T-FITTINGS INSIDE THE LEFT WING AILERON. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM FITTINGS ATTACHED TO A COMPOSITE SPAR). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 19. REFERENCE ATR SRM 57-61-10 PAGES 115 AND 116. THE TYPE OF CORROSION WAS EXFOLIATION. THE FITTING P/N ARE: S57610025200, S57610025204, AND S57610025202.

Part: FITTING — CORRODED (RT AILERON) · airframe 29,018 hrs · 36,386 cycles

DURING INSPECTION, LEVEL 3 CORROSION WAS FOUND ON 4 T FITTINGS INSIDE THE RIGHT WING AILERON. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM FITTINGS ATTACHED TO A COMPOSITE SPAR). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 19. REFERENCE ATR 42 SRM 57-61-10 PAGE 115/116. THE TYPE OF CORROSION FOUND WAS EXFOLIATION. THE FITTING PART NUMBERS ARE: S57610025202, S57610025204, AND S57610025200.

Part: FITTING — CRACKED (AILERON) · airframe 29,018 hrs · 36,386 cycles

DURING INSPECTION, LEVEL 2 INTERGRANULAR CORROSION AND CRACKS WERE FOUND ON THE CENTER HINGE BEARING FITTING. THE PART NUMBERS REPLACED ARE: 576106-02 & 576106-01. REFERENCE ATR 42 CMM 5761-11 AND SRM 57-61-00.