N917FX

Part: SKIN — DENTED (ZONE 200) · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200105 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: R/H EXTERNAL FUSELAGE BETWEEN FRAMES 19-20 AT STRINGER 11R HAS A DENT. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00240251_01...23669 ISSUE A, DATED 6/28/2024.

Part: PAN — DENTED (ZONE 200) · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 800003 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H AFT CARGO DOOR LOWER AFT CORNER OF PAN HAS A DENT. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 521100-300-812-A01.

Part: STIFFENER — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200093 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: FWD PRESSURE BULKHEAD FWD SURFACE MIDDLE STIFFENER HAS LEVEL 2 CORROSION AT UPPER END. CORRECTIVE ACTION: REPLACED STIFFENER PER ATR42 SRM 51-25-01 AND 51-25-04.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200081 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: INTERNAL FUSELAGE HAS LEVEL 2 CORROSION AT STRINGER 10AL BETWEEN FRAMES 20-21 UNDER INSULATION STANDOFF. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-803-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200083 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H OUTBOARD SEAT TRACK HAS LEVEL 2 CORROSION BETWEEN FRAMES 34-35. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-856-A01.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 100014 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: FWD CARGO DOOR THRESHOLD VERTICLE WEB HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER ATR SRM 533780-300-803-A01.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 100014 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: FRAME 14 FLOORBEAM HAS LEVEL 2 CORROSION ON THE AFT SIDE L/H OUTBOARD END. CORRECTIVE ACTION: REPAIRED PER SRAS ES-00241796_01...23805 ISSUE A, DATED 7/5/2024.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200071 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: INTERNAL FUSELAGE ABOVE STRINGER 6R BETWEEN FRAMES 20-21 HAS LEVEL 2 CORROSION UNDER INSULATION STANDOFF. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 530000-300-803-A01.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200066 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: L/H FRAME 19-20 WINDOW FRAME HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FRAME PER ATR42 SRM 51-25-04 AND 51-21-27.

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,461 hrs · 35,525 cycles

WO 254917 NR 200068 HEAVY DUTY COE/MAJOR REPAIR: DISCREPANCY: INTERNAL FUSELAGE STRINGER 6R HAS LEVEL 2 CORROSION FROM FRAMES 14-23. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-826- A01.

Part: GCU — FAULTED (UNKNOWN) · airframe 27,292 hrs · 35,283 cycles

FLT 7826, ENROUTE FCA-GTF AIR TURNBACK/DISCREPANCY: ON CLIMB OUT, THE #1 DC GENERATOR FAULTED. THE AIRCRAFT WAS RETURNED TO FCA. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE TROUBLESHOT AND REPLACED THE #1 DC GENERATOR CONTROL UNIT.

Part: STRINGER — CRACKED (ZONE 200) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 200070 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 1L IS CRACKED AT FRAME 34. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 53-00-00-300-826-A01.

Part: PANEL — CORRODED · corrosion level 2 · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 200059 HEAVY CHECK COE/MAJOR REPAIR: INNER SKIN HAS SPOTS OF INSULATIONS STANDOFF LEVEL 2 CORROSION FRAMES 28-29 STRINGER 1L-2L. CORRECTION ACTION: REPAIR PER ATR42 SRM 530000-300-864-A01.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 200063 HEAVY CHECK COE/MAJOR REPAIR: INNER SKIN HAS SPOTS OF INSULATIONS STANDOFF LEVEL 2 CORROSION FRAMES 28-29 STRINGER 2R-3R. CORRECTIVE ACTION: REPAIR PER SRAS ES_0161784_01...19268 ISSUE A, DATED 8/5/2022.

Part: PANEL — CORRODED (ZONE 600) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 600016 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4R AND 5R PANEL 622CT FLANE AND FOIL HAVE FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS- 4504/08...4888 ISSUE F, DATED 8/3/2022.

Part: PANEL — CORRODED (ZONE 500) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 500016 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4L AND 5L PANEL 522CT FLANGE AND FOIL HAVE FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-4504/08...4888 ISSUE F, DATED 8/3/2022.

Part: PANEL — CORRODED (ZONE 500) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 500015 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 1L AND 2L PANEL 521DT FLANGE AND FOIL HAVE FRETTING DAMAGE. CORRECTION ACTION: REPAIR PER SRAS DO/TS...4504/08...4888 ISSUE F.

Part: ATTACH BRACKET — BENT (ZONE 100) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100032 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 24 L/H LONGITUDINAL FLOORBEAM ATTACHMENT BRACKET IS BENT AND BOWED. CORRECTIVE ACTION: REMOVED AND REPLACED ATTACH BRACKET IAW EMPIRE AIRLINES E.O. 5315-01.

Part: ATTACH BRACKET — BENT (ZONE 100) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100032 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 24 L/H LONGITUDINAL FLOORBEAM ATTACHMENT BRACKET IS BENT AND BOWING. CORRECTIVE ACTION: REMOVED AND REPLACED ATTACH BRACKET IAW EMPIRE AIRLINES E.O. 5315-01.

Part: BULKHEAD — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 200028 HEAVY CHECK COE/MAJOR REPAIR: FWD PRESSURE BULKHEAD HAS MULTIPLE AREAS OF FRETTING AT THE RADOME BONDING POINTS. LEVEL 2 CORROSION CORRECTIVE ACTION: REPAIR PER SRAS ES_0162057_01...19253 ISSUE A, DATED 8/5/2022.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100023 HEAVY CHECK COE/MAJOR REPAIR: R/H LONGITUDINAL FLOORBEAM 38-39 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.

Part: MOUNT — CHAFED (ZONE 400) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 400024 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE FWD MOUNT TUBE 1 HAS CHAFE DAMAGE AFT OF THE FWD FITTING. CORRECTIVE ACTION: CORRECTIVE ACTION: REPAIR PER SRAS ES_0161869-01...19177 ISSUE A, DATED 8/4/2022.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100027 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE FLOORBEAM 15 UPPER SURFACE BETWEEN IB SEAT TRACKS HAVE LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 530000-300-846-A001.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100033 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 21 R/H LONGITUDINAL FLOORBEAM CRACKED AT ATTACHMENT. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100024 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM 33-34 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.

Part: STRINGER — DENTED (ZONE 200) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 200047 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE STRINGER 2L HAS A DENT BETWEEN FRAMES 22-23. CORRECTIVE ACTION: FABRICATION OF STRINGER IAW SRM 530000-300-826-A01.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 100025 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM IS CRACKED FRAMES 26-27. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 27,027 hrs · 34,946 cycles

WO 238445 NR 200019 HEAVY CHECK COE/MAJOR REPAIR: FRAME 26 SHEAR TIE STRINGER 12R-13R IS CRACKED. CORRECTIVE ACTION: REPLACED SHEAR TIE WITH NEW PER ATR42 SRM 51-25-01.

Part: ADC — FAULTED (NR 1) · airframe 26,723 hrs · 34,541 cycles

FLIGHT 7771, BZN-GTF/AIR TURNBACK DISCREPANCY: CAPTAIN VMO FLAGGED ON TAKEOFF, 15KTS DIFFERENCE ON STANDBY ASI COMPARED TO PRIMARYS. TORQUE BUGS FELL TO 20%. TCAS FAIL ON CAPTAIN SIDE. AIRCRAFT WAS RETURNED TO BZN. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE #1 AIR DATA COMPUTER AND CCAS COMPUTER. OPS CHECKS GOOD. OCF PERFORMED. ADC PN# 7000700-959 SN# 92025170, CCAS PN# 35-0A2-3008-314 SN# 346

Part: FLOORBEAM — CORRODED (FRAME 10) · corrosion level 2 · airframe 26,522 hrs · 34,219 cycles

FLOORBEAM 10 FLOORBOARD SUPPORT HAS LEVEL 2 CORROSION ON UPPER SURFACE. REPLACED WITH OEM PART.

Part: STRINGER — CRACKED (FRAME 17) · airframe 26,522 hrs · 34,219 cycles

STRINGER 1L IS CRACKED AT FRAME 17 DRAIN HOLE. REPAIRED PER SRM 53000-300-826-A01.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,522 hrs · 34,219 cycles

HEAVY CHECK COE/MAJOR REPAIR: FWD PRESSURE BULKHEAD LT MOST OUTBOARD STIFFENER HAS LEVEL 2 CORROSION NEAR THE TOP END. CORRECTIVE ACTION: REPAIRED PER SRM 531110-300-807-A01.

Part: FITTING — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 26,522 hrs · 34,219 cycles

L/H ELEVATOR TIP FITTING HAD CORROSION. REPLACED FITTING WITH OEM PART.

Part: SKIN — CORRODED (HORIZONAL STAB) · corrosion level 2 · airframe 26,522 hrs · 34,219 cycles

HORIZONTAL STABILIZER L/H LEADING EDGE LOWER ATTACH FLANGE INNER SURFACE HAD CORROSION. REPAIRED PER SRAS CETS-1484/16...10549 ISSUE B, DATED 6/8/2020.

Part: SKIN PANEL — NICKED (FUSELAGE) · airframe 26,522 hrs · 34,219 cycles

HEAVY CHECK COE, MAJOR REPAIR. FORWARD FUSELAGE RT LOWER SKIN PANEL HAS MULTIPLE NICKS BETWEEN FRAMES 13-14 AND STRINGERS 14R-15R. CORRECTIVE ACTION REPAIRED PER SRM 530000-300-805-A01.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,522 hrs · 34,219 cycles

HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE RT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 16-17 AND STRINGERS 10AR-11R. REPAIRED PER SRM 530000-300-803-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,522 hrs · 34,219 cycles

HEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 17 HAS LEVEL 2 CORROSION AT THE LT OUTBOARD END. REPAIRED PER SRM 530000-300-852-A01.

Part: STRINGER — CRACKED (FRAMES 20-21) · airframe 26,522 hrs · 34,219 cycles

WO 213629 NR 200018 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 1AR IS CRACKED BETWEEN FRAMES 20-21. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-826-A01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR: LEVEL 2 CORROSION ON STRINGER 16R BETWEEN FRAMES 34-35. REPAIRED PER SRM 530000-300-828-A01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 23. REPAIRED PER EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM IS CRACKED FWD OF FRAME 19. REPAIRED PER EO 5315-01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR: LEVEL 2 CORROSION ON STRINGER 18R BETWEEN FRAMES 14-20. REPAIRED PER SRM 530000-300-826-A01.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 622CT. LEVEL 2 REPAIRED PER DO/TS-4504/08...4888 ISSUE D, DATED 7/2/2018.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR, LT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 521DT. LEVEL 2 REPAIRED PER SRAS DO/TS-4504/08.4888 ISSUE D, DATED 7/2/2018.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR, LT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 522CT. LEVEL 2 REPAIRED PER SRAS DO/TS-4504/08...4888 ISSUE D, DATED 7/2/2018.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR, RT OUTBOARD SEAT TRACK GOUGED BETWEEN FRAMES 32-33. REPAIRED PER SRM 530000-300-856-A01.

Part: FITTING — NICKED (LT MLG) · airframe 25,854 hrs · 33,386 cycles

HEAVY CHECK COE/MAJOR REPAIR, LT MLG ACTUATOR FITTING HAS NICKS AND ALL 4 HOLES HAVE SLIGHT WEAR. REPAIRED PER SRAS ES-3162/18...13189 DATED 7/13/2018.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,510 hrs · 32,959 cycles

CREW REPORTED A SLIGHT ELECTRICAL BURNING ODOR IN THE COCKPIT. COMING THROUGH AT 11,000FT. SEEMED TO GO AWAY BELOW 7000FT. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE WAS UNABLE TO REPRODUCE THE ISSUE ON THE GROUND AND COULD NOT FIND ANY SIGNS OF ELECTRICAL OVERHEATING.

Part: ADC — FAULTED (NR 1) · airframe 25,437 hrs · 32,850 cycles

NR 1 AIR DATA COMPUTER FAULTED. THE CREW ELECTED TO RETURN TO DEPARTURE, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR DATA COMPUTER. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (RT AILERON) · airframe 23,335 hrs · 32,685 cycles

RT AILERON ASSY. CHANNEL CLOSING TEE REMOVED FROM 917FX, DUE TO AREAS OF LEVEL 2 CORROSION. REPAIRED IAW ES-3995/16.

Part: ADC — FAILED (NR 2) · airframe 25,352 hrs · 32,718 cycles

FLT 200: REPO FLIGHT GEG TO SBA, AIR TURNBACK. AIR DATA COMPUTER NR 2 FAILED AFTER TAKEOFF. CREW ELECTED TO RETURN TO GEG, NO EMERGENCY DECLARED. MAINTENANCE REPLACED THE NR 2 AIR DATA COMPUTER.

Part: ATTACH FITTING — CRACKED (RT MLG) · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT MLG ACTUATOR ATTACH FITTING IS CRACKED AT ATTACH HOLE. REPAIRED IAW SRAS S535R0342.10576.

Part: LUG — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

DURING HEAVY CHECK, RT OUTBOARD FLAP, INBOARD FLAP SUPPORT BEAM, LOWER INBOARD LUG HAS CORROSION. REPAIRED IAW SRAS CETS-3311/16.

Part: BRACE — CORRODED (RT WING) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

RIGHT WING RIB 8 FLAP SUPPORT BEAM SIDE BRACE HAD CORROSION. REPLACED SIDE BRACE.

Part: SKIN — CORRODED (FRAMES 36-37) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

EXTERIOR SKIN AFT CARGO DOOR AROUND RIVNUT FWD LOWER PLATE HAS LEVEL 2 CORROSION BETWEEN FRAMES 36-37. REPAIRED IAW CETS-3197/16

Part: STIFFENER — CORRODED (FWD BULKHEAD) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

FWD PRESSURE BULKHEAD RT STIFFENER HAS CORROSION. REPLACED THE STIFFENER.

Part: ATTACH ANGLE — CORRODED (RT WING) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

RIGHT WING LOWER CHORD DROP DOWN PANEL ATTACH ANGLE HAS LEVEL 2 CORROSION OUTBOARD OF RIB 6. REPLACED THE ATTACH ANGLE.

Part: ATTACH ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

LEFT WING LOWER DROP DOWN PANEL ATTACH ANGLE HAS CORROSION, RIB 9 TO OUTBOARD RIB 11. REPLACED THE ATTACH ANGLE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

SKIN UNDER THE FWD CARGO DOOR PROTECTION PLATES HAVE CORROSION AROUND THE BOTTOM OF THE DOOR OPENING. REPAIR PER CETS-3197/16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MINOR REPAIR. EXTERIOR SKIN UPPER TCAS ANTENNA DOUBLER HAS LEVEL 2 CORROSION. REPLACED DOUBLER.

Part: SPAR — CORRODED (ZONE 600) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

RIGHT WING LOWER SPAR STRIP SLAT INBOARD OF LEADING EDGE 611 HAS FRETTING CORRODED. REPAIR IAW CETS-3309/16.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

LEFT WING UPPER SPAR STRIP, TOP SURFACE HAS CORROSION DAMAGE BETWEEN RIBS 4-5 FROM CONTACT WITH PANEL 291CL. REPAIR PER CETS-3295/16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MINOR REPAIR, EXTERIOR SKIN LOWER TCAS ANTENNA DOUBLER HAS LEVEL 2 CORROSION. REPLACED DOUBLER.

Part: LANDING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MINOR REPAIR, RT ENGINE INBD LATERAL PANEL AFT LANDING HAS LEVEL 2 CORROSION. REPLACED LATERAL REBATE WITH OEM PART.

Part: LANDING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MINOR REPAIR. RT ENGINE OTBD LATERAL PANEL AFT LANDING HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MINOR REPAIR, RT HORIZONTAL STABILIZER L/E 341 HAS AREAS OF LEVEL 2 CORROSION ON INNER SKIN. REPLACED WITH SERVICEABLE L/E.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 25,335 hrs · 32,685 cycles

DURING HEAVY CHECK, FWD CARGO DOOR, THIRD FRAME AFT, HAS A CRACK IN RADIUS OF WEB TO OUTER FLANGE AT LEVEL OF HINGE. REPLACED.

Part: CHANNEL — CORRODED (RT AILERON) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

RIGHT AILERON TRAILING EDGE HAS CORROSION COMMON TO STATIC DISCHARGERS. REPLACED THE AILERON ASSY WITH NEW.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM CRACKED JUST AFT OF FRAME 30. SPLICE REPAIR IAW EO 5315-01, REV F.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MAJOR REPAIR: RIGHT FUSELAGE INTERIOR SKIN HAS DRILL STARTS, DENTS UNDER CREASE BEAM CHORD FROM FRAMES 40-41. REPAIR IAW SRAS CETS-3304/16.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MINOR REPAIR: AFT CARGO DOOR THRESHOLD HAS LEVEL 2 CORROSION ON TOP SURFACE BETWEEN FRAMES 36 AND 39. REPLACED WITH OEM PART.

Part: FLOOR SUPPORT — CRACKED (FRAME 34) · airframe 25,335 hrs · 32,685 cycles

RIGHT LONGITUDINAL FLOOR SUPPORT CRACKED JUST AFT OF FRAME 34. REPAIRED IAW EO 5315-01 REV. F.

Part: FLOOR SUPPORT — CRACKED (FRAME 25) · airframe 25,335 hrs · 32,685 cycles

RIGHT LONGITUDINAL FLOOR SUPPORT IS CRACKED AFT OF FRAME 25. PERFORMED SPLICE REPAIR IAW EO 5315-01 REV. F.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT FUSELAGE INTERIOR SKIN HAS DRILL STARTS/DENTS UNDER CREASE CHORD FROM FRAMES 40-41. REPAIR IAW SRAS S536R0273.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT LONGITUDINAL FLOORBEAM IS CRACKED FWD OF FRAME 23. REPAIRED IAW EO 5315-01, REV G.

Part: FLOOR SUPPORT — CRACKED (FRAME 32) · airframe 25,335 hrs · 32,685 cycles

LEFT LONGITUDINAL FLOOR SUPPORT CRACKED JUST AFT OF FRAME 32. SPLICE REPAIRED IAW EO 5315-01 REV. F.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT OTBD WING LOWER SKIN PANEL BOTTOM SURFACE HAS AREAS OF LEVEL 2 CORROSION AT RIB 14-15. REPAIR IAW SRAS CETS-3308/16, 10498, DATED 8/4/2016.

Part: SPOILER — CORRODED (RT WING) · corrosion level 2 · airframe 25,335 hrs · 32,685 cycles

HEAVY CHECK, MINOR REPAIR: RT SPOILER OTBD T/E HAS LARGE AREA OF LEVEL 2 CORROSION, UNDERSIDE. REPLACED SPOILER WITH OEM PART.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,658 hrs · 31,820 cycles

RIGHT LONGITUDINAL FLOORBEAM IS CRACKED BETWEEN FRAMES 27 - 28. CUT OUT REPLACEMENT & REINFORCEMENT IAW EO 5315-01.

Part: FLOORBOARD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,658 hrs · 31,820 cycles

FLOORBOARD FLANGE ON THE AFT CARGO THRESHOLD FRAMES 36 - 38 HAS LEVEL 2 CORROSION. REPLACED WITH NEW PART.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,658 hrs · 31,820 cycles

CABIN CTR LONGITUDINAL FLOORBEAM HAS CRACK BETWEEN FRAMES 15 - 16. CUT OUT REPLACEMENT & REINFORCEMENT IAW EO5315-01.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 24,658 hrs · 31,820 cycles

RIGHT WING REAR SPAR LOWER CHORD HAS LEVEL 2 CORROSION RIB 25. REPAIR IAW SRAS S572R0166 2852 DATED 6/12/2014.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 24,658 hrs · 31,820 cycles

LEFT WING REAR SPAR LOWER CHORD HAS LEVEL 2 CORROSION RIB 25 - 26. REPAIR IAW SRAS S572R0167 2851 DATED 6/12/2014.

Part: SKIN — CORRODED (LT WING) · airframe 24,658 hrs · 31,820 cycles

LEFT WING PANEL LANDING 521DT HAS LEVEL 1 FRETTING CORROSION. REPAIR IAW SRAS SO & TS-4504 08 4888 6/17/2014.

Part: SKIN — CORRODED (RT WING) · airframe 24,658 hrs · 31,820 cycles

RIGHT WING LANDING PANEL 622CT HAS LEVEL 1 FRETTING CORROSION. REPAIR IAW SRAS SO & TS-4504 08 888 6/17/2014.

Part: SKIN — CORRODED (LT WING) · airframe 24,658 hrs · 31,820 cycles

LEFT WING PANEL LANDING FOR 522CT HAS LEVEL 1 FRETTING CORROSION. IAW SRAS DO TS-4504 08 4888 6/17/2014.

Part: FLOORBEAM — BENT (FUSELAGE) · airframe 24,644 hrs · 31,813 cycles

NR 1 DAMAGE TO FLOOR BEAM 17, OTBD END HAS BEND. COMMON TO AFT LOWER AREA OF FWD CARGO DOOR. PROBABLE CONTACT FROM GND EQUIPMENT.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 24,132 hrs · 31,292 cycles

DURING TROUBLESHOOTING FOR UNRELATED DISCREPANCY, MAINTENANCE CREW FOUND A LONGITUDINAL FLOORBEAM BROKEN AT FRAME 28, LEFT SIDE OF AIRCRAFT. THIS FLOORBEAM WAS ADDED DURING THE PASSENGER TO FREIGHT MOD, UNDER STC ST01189WI. AIRCRAFT WAS RELOCATED TO GEG FOR MAINTENANCE UNDER A FERRY PERMIT. THE PLANNED REPAIR WILL BE A SPLICE OF THE BROKEN JOINT, REF EA ENGINEERING ORDER 5315-01.

Part: MOUNT — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CK / LEVEL 2 CORROSION: LEFT ELEVATOR HORN LEADING EDGE MOUNT ASSEMBLY INCLUDING BALANCE WEIGHT MOUNT HAS CORROSION (LENGTH 2.2", WIDTH .750", DEPTH .020"). REMOVED CORROSION AND REMOVED AND REPLACED LEFT ELEVATOR HORN LEADING EDGE MOUNT(LEFT ELEVATOR TIP RIB NOSE) WITH OEM PART.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: STR 1L - 1R FS 256.19, BL 0.00 SKIN DOUBLER REAR CUTOUT OF DAMAGE AT ZONE 1 WHICH INTERFERS WITH THE HARDPOINT INSTALLATION. FABRICATE AND INSTALL REPAIR DOUBLER OF SKIN CUTOUT AT HP1 FS 256.19, BL 0.00 IAW M7 DRW.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: STR 1L FROM FR 13-16 FOUND DAMAGED. FABRICATED AND INSTALL NEW STRINGER SPLICE STR 1L SPLICE AT FR 13-16, HP1 FS 256.19, BL 0.00 PER SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB 2ND FROM BOTTOM RUDDER ATTACH FITTING IS CORRODED ON THE UPPER SURFACE (LENGTH 2", WIDTH 4", DEPTH .095"). REPLACE UPPER MACH WEB WITH OEM PART PER ATR42 SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: RIGHT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED (.25") FWD OF FRAME 25. FABRICATE AND REPLACE FLOORBEAM SECTION - RIGHT OUTBOARD FLOORBEAM FWD OF FRAME 25, STA 11400 WATERLINE 2327.5 AND BUTT LINE 645R.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: RIGHT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED (.25") FWD OF FRAME 40 STA 18400 WATERLINE 2327.5. FABRICATE AND REPLACE FLOORBEAM.

Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: RIGHT MLG WHEEL WELL PRESSURE DECK, 5TH STIFFENER AFT OF FRAME 25 (11.33 INCHES FORWARD OF FRAME 26) HAS AREAS OF CORROSION. FABRICATE AND INSTALL NEW FORMED STIFFENER PER ATR SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: LEFT OUTBOARD LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 29 (CRACK APPROXIMATELY .25 INCHES IN LENGTH). FABRICATED FLOORBEAM SPLICE IN ACCORDANCE WITH EA EO-5315-01.

Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: RIGHT MLG WHEEL WELL PRESSURE DECK, 6TH STIFFENER AFT OF FRAME 25 (6 INCHES FORWARD OF FRAME 26) HAS AREAS OF CORROSION. FABRICATE AND INSTALL NEW FORMED STIFFENER.

Part: ANGLE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: HORIZONTAL STABILIZER LEFT LOWER MOUNT FLANGE FOR PANEL 325CR IS CORRODED. WILL REPAIR OR REPLACE PER MANUFACTURER'S INSTRUCTIONS.

Part: ANGLE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: HORIZONTAL STABILIZER RIGHT LOWER MOUNT FLANGE FOR PANEL 325CR CORRODED. WILL REPAIR OR REPLACE PER MANUFACTURER'S INSTRUCTION.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: RIGHT MLG WHEEL WELL PRESSURE DECK, 2ND STIFFENER 7.25 INCHES AFT OF FRAME 25 HAS AREAS OF LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: AFT AVIONICS DOOR SKIN CUTOUT ON BOTH FWD AND AFT EDGES HAS CORROSION (LENGTH 15", WIDTH 1.5", DEPTH .071"). REMOVED AND REPLACED DOOR REINFORCE WITH OEM PART PER ATR42 SRM.

Part: SKIN — CHAFED (LT WING) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: LEFT WING OUTBOARD FLAP MIDDLE HINGE FAIRING IS CHAFING TO UNDERSIDE OF WING. BLENDED OUT REPAIR. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.

Part: PANEL — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR / LEVEL 2 CORROSION: LEFT LEADING EDGE HORIZONTAL STABILIZER PANEL 331AB HAS CORROSION. SUBMIT TO ATR FOR REPAIR INSTRUCTIONS TO LEFT LEADING EDGE HORIZONTAL STABILIZER PANEL 331AB. REPAIR PER SRAS FROM ATR.

Part: STIFFENER — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB FWD SPAR WEB HAS CORROSION ON THE 2ND AND 3RD STIFFENERS FROM THE TOP (LENGTH .5", WIDTH 6", DEPTH .53"). REMOVED AND REPLACED STIFFENER WITH OEM PART PER ATR42 SRM.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: LEFT UPPER WING CUTOUT FOR PANEL 522CT HAS FRETTING AND LEVEL 2 CORROSION (LENGTH .5", WIDTH 6", DEPTH .44") SUBMIT TO ATR FOR REPAIR INSTRUCTIONS TO TOP OF LEFT WING SKIN CUTOUT WHERE PANEL 522CT SITS BETWEEN BL 1210L - 1625L. REPAIR PER SRAS FROM ATR.

Part: ANGLE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: HORIZONTAL STAB LOWER MOUNT FLANGE FOR PANEL 325CL IS CORRODED (LENGTH 2", WIDTH 1", DEPTH .014"). REMOVED AND REPLACED ANGLE WITH OEM PART PER ATR42 SRM.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: TOP OF LEFT WING SKIN CUTOUT WHERE PANEL 622CT SITS BETWEEN BL 1210R - 1625R HAS FRETTING AND LEVEL 2 CORROSION (LENGTH .5", WIDTH 6", DEPTH .53"). SUBMIT TO ATR FOR REPAIR INSTRUCTIONS TO TOP OF LEFT WING SKIN CUTOUT WHERE PANEL 622CT SITS BETWEEN BL 1210R - 1625R. REPAIR PER ATR SRAS.

Part: STRAP — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB REAR SPAR WEB STRAP ABOVE PANEL 324AZ IS CORRODED (LENGTH 1", WIDTH 2", DEPTH .005"). REMOVED AND REPLACED WEB REAR SPAR STRAP WITH OEM PART PER ATR42 SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / MAJOR REPAIR: LEFT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED (.25") AFT OF FRAME 34. REMOVED, FABRICATED AND INSTALLED FLOORBEAM SECTION LEFT OUTBOARD JUST AFT OF FRAME 34 STA 1700 WATERLINE 2327.5 AND BUTTLINE 645L REF EA EO 5315-01.

Part: STIFFENER — CORRODED (VERTICAL STAB) · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB FWD SPAR WEB STIFFENER APPROXIMATELY 5 INCHES ABOVE THE VOR ANTENNA HAS CORROSION (LENGTH .5", WIDTH 6", DEPTH .53"). REMOVED AND REPLACED STIFFENER WITH OEM PART PER ATR42 SRM.

Part: STIFFENER — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 23,866 hrs · 30,949 cycles

HEAVY CHECK / LEVEL 2 CORROSION: RIGHT HORIZONTAL STAB REAR SPAR STIFFENER ON THE OUTBOARD SIDE OF THE INBOARD ELEVATOR ATTACH FITTING IS CORRODED (LENGTH 3", WIDTH .5", DEPTH .004"). REMOVED AND REPLACED STIFFENER WITH OEM PART PER ATR42 SRM.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: LT HORIZONTAL FWD SPAR WEB CRACKED AT LIGHTNING HOLE AT STA Y1764, ZONE 300 WL 8050. WAITING FOR REPAIR INSTRUCTIONS FROM ATR.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: CARGO COMPARTMENT CEILING PRESSURE DECK ANGLE JUST AFT OF FR27 AT STR 4L IS CRACKED (.800'). WAITING FOR REPAIR INSTRUCTIONS FROM ATR.

Part: STOP FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: LEVEL 2 CORROSION: AT PANEL 632CB FOUND CORROSION ON OUTBOARD STOP FITTING AT REAR SPAR. REMOVED CORROSION DAMAGE THAT WAS BEYOND LIMITS, LENGTH 1.6 INCH, WIDTH .9 INCH PER SRM. AWAITING INSTRUCTIONS FROM ATR.

Part: ANGLE — CORRODED (NLG WW) · corrosion level 2 · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: LEVEL 2 CORROSION: AT NOSE GEAR WELL FORWARD UPPER ANGLE CHORD HAS LEVEL 2 CORROSION. CORROSION DAMAGE 9.25 INCHES IN LENGTH, 1.25 INCH IN WIDTH AND .009' IN DEPTH WAS BLENDED IAW SRM. AWAITING REPAIR INSTRUCTIONS FROM ATR (SRI / SRAS).

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: TOP OF FUSELAGE PRESSURE DECK JUST AFT OF FRAME 27 AT STRINGER 4R FOUND CRACK APPROXIMATELY 5 INCHES LONG ON FORMED PART. AWAITING REPAIR INSTRUCTIONS FROM ATR.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: LEVEL 2 CORROSION: WHILE CLOSING PANEL 631AB FOUND FLAP HINGE ON WING SIDE RIB 8 WITH LEVEL 2 CORROSION (RT WING). REMOVED AND REPLACED BEAM ASSEMBLY IAW SRM.

Part: SPAR — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 22,989 hrs · 50,923 cycles

HEAVY CK COE: LEVEL 2 CORROSION: RT HORIZONTAL AFT SPAR WEB HAS AREAS OF LEVEL 2 CORROSION. AWAITING INSTRUCTION PER SRAS FROM ATR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: LEVEL 2 CORROSION: LT CREASE BEAM WEB BETWEEN FR13 -14 HAS LEVEL 2 CORROSION ON THE BOTTOM SIDE AROUND MULTIPLE FASTENERS. REMOVED CREASE BEAM WEB AND REPLACED WITH FABRICATED PART IAW SRM.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: WHILE WORKING LT CREASE BEAM WEB BETWEEN FR 12-18, FOUND PREVIOUS TOOLING DAMAGE ON CREASE BEAM OUTER CHORD. BLENDED OUT AND REQUEST TO "LEAVE AS IS". AWAITING SRAS FROM ATR.

Part: SPAR — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: LEVEL 2 CORROSION: LT HORIZONTAL AFT SPAR WEB HAS AREAS OF LEVEL 2 CORROSION. AWAITING INSTRUCTION PER SRAS FROM ATR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: FRAME 16 AT STRINGER 15L BY CARGO DOOR OPENING HAS RIVNUT AND SCREW IMPACTING BOTH FRAME AND CLIP FROM INSTALL OF LOWER SKIN PROTECTION PLATE. DAMAGE WAS CAUSED DURING STC MOD RIVNUT INSTALLATION. TRIM OUT DAMAGE. TRIM OUT CAN BE LEFT "AS IS" PER SRI DO\TS-2872/10-13554. AWAITING COMPLETED SRAS.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: WHILE WORKING LT CREASE BEAM AT FRAME 17 FOUND PREVIOUS TOOLING DAMAGE ON TOP SURFACE OF INNER FLANGE FR17 AT STRINGER 14 LT. BLEND OUT DAMAGE ON INNER FLANGE OF FRAME 17 AT LEVEL OF CARGO DOOR THRESHOLD PER SRM. TOOLING MARKS TO LEFT "AS IS" PER SRI DO\TS-2871/10-13552. AWAITING COMPLETE SRAS.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: LEVEL 2 CORROSION: LT CREASE BEAM WEB FR 17-18 HAS MANY AREAS OF LEVEL 2 CORROSION. REMOVED AND REPLACED CREASE BEAM WEB PER ATR42 SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: LT CREASE BEAM BETWEEN FR 13-14 FOUND DRILL STARTS ON INSIDE SURFACE OF EXTERNAL FUSELAGE SKIN BELOW STR 14LT. REMOVED DRILL STARTS IN AREA OF APPROXIMATE 1 X 3 INCH. FOUND BLENDED AREA OF SKIN TO BE OUT OF LIMITS. DOUBLER CUTOUT AND REPAIR IAW SRM 53-00-00 PG 410 FIG 403 1 INCH BELOW STRINGER 14L, 2 INCHES AFT OF FRAME 13L AND 4.2 INCHES FWD OF FRAME 14L.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: TOP OF FUSELAGE PRESSURE DECK AFT OF FRAME 27 AT STRINGER 4R FOUND LEVEL ONE CORROSION. LEVEL ONE CORROSION REMOVED AND FOUND 2.2 INCH CRACK ON SEAL RETAINER AT FRAME 27 COMMON TO WING BOX. PERFORMED CUTOUT AND SPLICE TO U-CHANNEL PER SRI DO\TS-2825/10-13542. AWAITING COMPLETED SRAS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

HEAVY CK COE: MAJOR REPAIR: CARGO COMPARTMENT CEILING PRESSURE DECK ANGLE JUST AFT OF FRAME 27 AT STRINGER 4R HAS 2.2 INCH CRACK. APPLIED SEALANT AND DID NOT DRILL CRACK HOLES TO AVOID THE RISK OF DAMAGING THE BACK STRUCTURE AS PER SRI DO/TS-2795/10-13538. POSSIBLE REDUCTION OF INSPECTION INTERVAL WILL BE CONFIRMED IN FINAL SRAS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

LEFT LONGITUDINAL CARGO MOD FLOORBEAM JUST FORWARD OF FRAME 26 IS CRACKED. CRACK 0.5 INCHES IN LENGTH. REPAIR PER ENGINEERING ORDER 5315-01 (M7 SERVICE BULLETIN ATR 42-53-023 (R2).

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

LEFT LONGITUDINAL CARGO MOD FLOORBEAM JUST FORWARD OF FRAME 17 IS CRACKED. CRACK 0.5 INCHES IN LENGTH. REPAIR PER ENGINEERING ORDER 5315-01 (M7 SERVICE BULLETIN ATR42-53-023 (R2).

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,989 hrs · 30,158 cycles

LEFT LONGITUDINAL CARGO MOD FLOORBEAM JUST FORWARD OF FRAME 21 IS CRACKED. CRACK IS 0.5 INCHES IN LENGTH. REPAIR PER ENGINEERING ORDER 5315-01 (M7 SERVICE BULLETIN ATR 42-53-023).

Part: PCU — OUT OF RIG (NR 2) · airframe 22,479 hrs · 29,606 cycles

AIR TURN BACK: ON FLIGHT 8202, CREW OBSERVED NR2 NP DID NOT RESPOND TO POWER LEVER ADJUSTMENT AND DID NOT HOLD 100 PERCENT NP ON APPROACH WITH POWER LEVER ANGLE BELOW 60 DEGREES. CREW ELECTED TO RETURN TO DEPARTURE FOR MX PURPOSES. AFTER TROUBLESHOOTING, MX RE-RIGGED HMU AND PCU. OPS CHECK GOOD AND ACFT RETURNED TO SERVICE.

Part: RIB — CORRODED (LT AILERON)

FOUND AT COE LEVEL 2 CORROSION. CORROSION ON LT WING AILERON HORN ATTACHMENT RIB.

Part: PANEL — CORRODED (RT CENTER WING)

FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. CORROSION ON CENTER WING UPPER SKIN, ON THE CUTOUT FLANGE FOR PANEL 622CT.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

MAJOR REPAIR, LT FLOOR SUPPORT BEAM THAT RUNS FROM FR 20 TO 25 IS CRACKED. OPEN

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND AT COE MAJOR REPAIR FLOOR BEAM 10 IS CORRODED ON THE UPPER AND LOWER SURFACE OF THE INTERCOSTAL 10 INCHES LT AND RT OF BL 0.

Part: STIFFENER — CORRODED (BULKHEAD)

MAJOR REPAIR AND LEVEL 2 CORROSION. FWD BULKHEAD EXTRUDED STIFFENER HAS SURFACE CORROSION AROUND ATTACHMENT RIVETS. CORROSION BLEND-OUT WAS BEYOND ACCEPTABLE LIMITS. FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. FWD BULKHEAD EXTRUDED STIFFENER HAS SURFACE CORROSION AROUND ATTACHMENT RIVETS. CORROSION BLEND OUT WAS BEYOND ACCEPTABLE LIMITS. BLENDED OUT DAMAGED AREA ON THE VERTICAL STIFFENER AND LEFT AS IS. R&R FASTENERS IN AREA OF CORROSION AND INSPECTED HOLES FOR CRACKS.

Part: SKIN — DAMAGED (LT WING SLAT)

FOUND AT COE LT WING FWD UPPER LEADING EDGE SLAT HAS MECHANICAL DAMAGE. AWAITING DISPOSITION FROM ATR.

Part: SKIN — CORRODED (AILERON)

MAJOR REPAIR AND LEVEL 2 CORROSION. RT WING AILERON TRAILING EDGE HAS SURFACE CORROSION, JUST OB OF THE TRIM TAB. CORROSION BLEND-OUT WAS BEYOND ACCEPTABLE LIMITS. FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. RT WING AILERON TRAILING EDGE HAS SURFACE CORROSION, JUST OTBD OF THE TRIM TAB. CORROSION BLEND OUT WAS BEYOND ACCEPTABLE LIMITS. CUT OUT DAMAGED AREA ON CHANNEL. INSTALLED A SPLICE OVER THE CHANNEL WITH FILLER. (K)

Part: SPINNER — CRACKED (LT PROPELLER)

MAJOR REPAIR, LT ENGINE PROPELLER SPINNER IS CRACKED AT 3 BOLT HOLES AND OTHER HOLES SHOW SIGNS OF WEAR. FOUND AT COE MAJOR REPAIR LT ENGINE PROPELLER SPINNER IS CRACKED AT 3 BOLT HOLES AND OTHER HOLES SHOW SIGNS OF WEAR. CUT OUT 3 CRACKED CORNERS AND MADE REPLACEMENT CORNER PIECES. INSTALLED THE 3 CORNERS WITH REINFORCEMENT STRIPS DOUBLERS ON THE SPINNER. INSTALLED A 4TH REINFORCEMENT STRIP AS A COUNTER BALANCE ON THE SPINNER.

Part: COOLING FAN — FAILED (CABIN)

ODOR IN CREW COMPARTMENT, AFTER LANDING, WHILE TAXIING TO PARKING RAMP. THE CREW NOTICED A LIGHT BURNING SMELL IN COCKPIT, FOLLOWED BY NR1 PACK VALVE FAULT. SHORTLY AFTER ARRIVAL, PERFORMED A TEST ENGINE RUN WITH MECHANIC ON BOARD, TO DUPLICATE. WITH THE NR1 ENGINE PACK ON, AFTER 10 MINUTES, COCKPIT AND CABIN FILLED WITH WHITE SMOKE. CANCELLED FLIGHT DUE TO PROBLEM NOT BEING IDENTIFIED. TROUBLESHOOTING FOUND GROUND COOLING FAN INOPERATIVE AND AFT FLAP VANE DAMAGED. REPLACED GROUND COOLING FAN. (K)

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT)

EMERGENCY BATTERY CHARGE FAULT LIGHT CAME ON DURING CLIMB OUT. AC RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY. MAINTENANCE CONTROL STATES BATTERY WAS NOT HOT WHEN REMOVED. AIRCRAFT WAS RETURNED TO SERVICE. (K)