N911FX

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100073 HEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 33 EXFOLIATED ON AFT SIDE BETWEEN L/H SEAT TRACKS. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-839-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100065 HEAVY CHECK COE/MINOR REPAIR: FRAME 27A R/H SUPPORT INTERCOSTAL FOR PANEL 193DL/194DR HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100031 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM CRACKED FORWARD OF FRAME 27. CORRECTIVE ACTION: REPAIRED PER E.O. 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100029 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 28. CORRECTIVE ACTION: REPAIRED PER E.O. 5315-01.

Part: CUP — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100032 HEAVY CHECK COE/MINOR REPAIR: R/H LANDING GEAR EMERGENCY EXTENSION CABLE PASS THROUGH CUP, FRAMES 25-26 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100018 HEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 36 TOP SURFACE HAS LEVEL 2 CORROSION. AREA AROUND THE L/H INBOARD SEAT TRACK IS OUT OF LIMITS. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-852-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100019 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM HAS LEVEL 2 CORROSION BETWEEN FRAMES 36-39. CORRECTIVE ACTION: REPAIRED PER E.O. 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100038 HEAVY CHECK COE/MAJOR REPAIR: R/H LONGITUDINAL FLOORBEAM CRACKED FORWARD OF FRAME 20. CORRECTIVE ACTION: REPAIRED PER E.O. 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100039 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 24. CORRECTIVE ACTION: REPAIRED PER E.O. 5315-01.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 200008 HEAVY CHECK COE/MINOR REPAIR: FRAME 14 STRINGER CLIP 5R HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED CLIP WITH OEM PART.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 500030 HEAVY CHECK COE/MAJOR REPAIR: CENTER WING HOUSING FOR ACCESS PANEL 521DT HAS FRETTING LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0118638_01...16226 ISSUE A, DATED 5/5/2020.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100011 HEAVY CHECK COE/MINOR REPAIR: STRINGER 21L JOINT STRINGER AT FRAME 13 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100009 HEAVY CHECK COE/MAJOR REPAIR: FRAME 17 LATERAL FLOORBEAM UPPER SURACE HAS LEVEL 2 CORROSION BETWEEN L/H OUTBOARD AND R/H INBOARD SEAT TRACKS. CORRECTIVE ACTION:REPAIRED PER SRM 530000-300-855-A01.

Part: TEE FITTING — CORRODED (LT AILERON) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 500028 HEAVY CHECK COE/MINOR REPAIR: L/H AILERON TAB CLOSING TEE HAS LEVEL 2 CORROSION UPPER SIDE NEAR STATIC WICK. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 500029 HEAVY CHECK COE/MAJOR REPAIR: CENTER WING HOUSING FOR ACCESS PANEL 522CT HAS FRETTING LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0118638_01...16226 ISSUE A, DATED 5/5/2020.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 100012 HEAVY CHECK COE/MINOR REPAIR: STRINGER 20L JOINT STRINGER AFT OF FRAME 13 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: GUIDE — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 500012 HEAVY CHECK COE/MINOR REPAIR: L/H OUTBOARD FLAP INBOARD DEFLECTOR THIRD CAM GUIDE FROM INBOARD HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: DEFLECTOR — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,837 hrs · 46,519 cycles

WO 213191 NR 500013 HEAVY CHECK COE/MAJOR REPAIR: L/H OUTBOARD FLAP INBOARD DEFLECTOR HAS LEVEL 2 CORROSION AT OUTBOARD CAM GUIDE. CORRECTIVE ACTION: REPAIRED PER SRM 575320-300-801-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, LEVEL 2 CORROSION ON INTERIOR FUSELAGE FLOORBEAM 7 UPPER AND LOWER SURFACES AT LBL28. SPLICE REPAIR PER SRM 531140-300-804-A01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, AFT CARGO COMP UNDERFLOOR STRINGER 15R HAS LEVEL 2 CORROSION, JUST FORWARD OF FRAME 36. REPAIRED PER SRAS PCE-1867/18...12952 DATED 5/25/2018.

Part: SKIN — GOUGED (FRAME 33) · airframe 38,074 hrs · 45,663 cycles

INTERIOR SKIN GOUGED WITH A PROTRUDING DENT AFT OF FRAME 33 BELOW STRINGER 20R. REPAIRED IAW ES-1889-16-10259, ISSUE B.

Part: SKIN — GOUGED (FRAME 32) · airframe 38,074 hrs · 45,663 cycles

EXTERIOR SKIN WAS FOUND GOUGED, FORWARD OF FRAME 32 AND COMMON TO STRINGER 20R. REPAIRED IAW SRAS ES-1889-16-10259 ISSUE B.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MINOR REPAIR, LEVEL 2 CORROSION FOUND ON INTERCOSTAL BETWEEN FB 10-11, RBL 12. REPLACED WITH OEM PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, LEVEL 2 CORROSION ON FRAME 9 FLOORBEAM AFT LOWER ANGLE OUTBOARD OF LBL 15. REPAIRED PER SRAS ES-2280/18...12908 DATED 5/24/2018.

Part: PANEL — CHAFED (ZONE 300) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR: PANEL 321AL, UPPER TRAILING EDGE CHAFFED. LEVEL 2, REPAIRED PER SRAS PCE-1693/18...12901 DATED 5/24/2018.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MINOR REPAIR, LEVEL 2 CORROSION ON RT STEP UP INTERCOSTAL BETWEEN FB 9-10 RBL 12. REPLACED WITH OEM PART.

Part: SUPPORT — CORRODED (COCKPIT) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

CAPTAIN`S CONTROL COLUMN SUPPORT HAD CORROSION ON THE TOP SURFACE. REPLACED.

Part: INTERCOSTAL — CORRODED (FRAMES 10-11) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

CORROSION FOUND ON THE LBL 12 INTERCOSTAL, FRAMES 10 - 11. REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MINOR REPAIR, LEVEL 2 CORROSION ON FLOORBEAM 10 STEP UP INTERCOSTAL LBL13-RBL13. REPLACED WITH OEM PART.

Part: FLOORBEAM — CORRODED (FRAME 9) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

CORROSION FOUND ON FRAME 9, FLOORBEAM, LBL 15, AFT UPPER ANGLE. REPAIRED IAW SRAS ES-2280/18-12908.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MINOR REPAIR, LEVEL 2 CORROSION ON LBL 15 INTERCOSTAL, FB 10-11. REPLACED WITH OEM PART.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, STRINGER 3L HAS LEVEL 2 CORROSION BETWEEN FRAMES 16-17. REPAIRED PER SRM 530000-300-826-A01.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MINOR REPAIR, FWD CARGO STRINGER CLIP HAS LEVEL 2 CORROSION FRAME 16, STRINGER 13R. REPLACED CLIP WITH NEW FABRICATED PART.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, STRINGER 1L HAS LEVEL 2 CORROSION AND DAMAGE FRAMES 13-14. STRINGER SPLICE PER SRM 530000-300-826-A01.

Part: STRINGER SPLICE — CORRODED (FRAMES 14-15) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

STRINGER SPLICE 2AL HAD CORROSION BETWEEN FRAMES 14 - 15. STRINGER SPLICE IAW SRM 53-00-00-300-826-A01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, LEVEL 2 CORROSION AT FUSELAGE STRINGER 19R BETWEEN FRAMES 31-32. REPAIRED PER SRAS PCE-1719/18...12879 DATED 5/11/2018.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, RT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED FORWARD OF FRAME 28. REPAIR OF FLOORBEAM PER EA EO 5315-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, LT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED AFT OF FRAME 33. FLOORBEAM REPAIRED PER EA EO 5315-01.

Part: FRAME — CORRODED (FRM 30) · corrosion level 2 · airframe 38,074 hrs · 45,665 cycles

FRAME 30 FLANGE FORWARD SURFACE HAD CORROSION, STRINGERS 21L-21R. REPAIRED IAW SRAS ES-2178/18.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, MIDDLE LONGITUDINAL FLOORBEAM IS CRACKED AFT OF FRAME 34. FLOORBEAM REPAIR PER EA EO 5315-01.

Part: STRINGER — CORRODED (FRAMES 27-28) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

CORROSION FOUND ON STRINGER 21R BETWEEN FRAMES 27 - 28. REPLACED THE STRINGER.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR, LEVEL 2 CORROSION ON STRINGER 20R BETWEEN FRAMES 31-34. REPAIRED PER SRAS ES-1889/16...10259 ISSUE C, DATED 5/29/2018.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,074 hrs · 45,663 cycles

HEAVY CHECK COE/MAJOR REPAIR: LEVEL 2 CORROSION ON FUSELAGE STRINGER 21R BETWEEN FRAMES 31-32. REPAIRED PER SRAS ES-1889/16...10259 ISSUE C, DATED 5/29/2018.

Part: FRAME — CORRODED (FRM 30) · corrosion level 2 · airframe 38,074 hrs · 45,665 cycles

FRAME 30 FLANGE CORRODED ON THE FORWARD SURFACE, STRINGERS 18R-19R. REPAIRED SRAS ES-2178/18.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: FRAME 4 LT LOWER SEGMENT IS CRACKED ON THE INBD FLANGE. REPLACED FRAME WITH OEM PART.

Part: BRACKET — CORRODED (CONTROL COLUMN) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON PILOTS SIDE CONTROL COLUMN STOP BRACKET ASSEMBLY. REPLACED WITH OEM PART.

Part: MOUNT — NICKED (LT ENGINE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT ENGINE FRONT MOUNT TUBE NR 6 ON OTBD SIDE OF ENGINE HAS NICKS IN TUBE AT FWD END. REPAIRED IAW SRAS CETS-2205/16, 10322, DATED 6/3/2016.

Part: TAB — DAMAGED (RT COWLING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT LOWER COWL INBD FORWARD MOUNT TAB HAS FRETTING DAMAGE. REPAIR IAW SRAS CETS-2185/16, 10320 DATED 6/3/2016.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION FOUND ON FLOORBEAM 5, UPPER FLANGE AT MOUNTING POINT FOR LT SIDE RUDDER PEDAL BOX. REPLACED FLOORBEAM WITH FABRICATED PART.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

NR 8 HEAVY CHECK, COE/MAJOR REPAIR: GOUGE DAMAGE WITH OIL CANNING ON REAR FUSELAGE LOWER SKIN PANEL AFT OF FRAME 33 AT STR 21R. REPAIRED IAW SRAS ES-1889/16, 10259 DATED 5/25/2016.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK, COE/MAJOR REPAIR: FLOORBEAM 5 HAS LEVEL 2 CORROSION AROUND NUTPLATES ON THE TOP FLANGE UPPER SURFACE. REPAIRED FLOORBEAM BY FABRICATION.

Part: STRINGER — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. STRINGER 21R BETWEEN FRAMES 32 - 33 HAS TOOLING DAMAGE. REPAIR IAW SRM 530000-300-828-A01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. ANGLE ATTACHED TO INBD SIDE OF STRINGER 21R HAS LEVEL 2 CORROSION BETWEEN FRAMES 32 - 33. REPLACED WITH OEM PART.

Part: MOUNT — CRACKED (RT SPOILER) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT SPOILER BLOCK VALVE INBD MOUNT CRACKED. REPAIR IAW CE-1885/16 DATED 6/3/2016.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE RT LOWER SKIN PANEL HAS TOOLING DAMAGE UNDER FRAME 26 SHEAR TIE, STR 12-13. REPAIR IAW SRAS CE-1815/16, 10272, DATED 6/3/2016.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 450,770 cycles

HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON FRAME 25A RT INBD INTERCOSTAL ATTACH ANGLE. REPLACED WITH OEM PART.

Part: TAB — WORN (LT ENGINE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK: FORWARD LT ENGINE MOUNT TABS WORN. REPAIRED IAW SRAS CE-1800/16.10318 DATED 6/3/2016.

Part: TAB — WORN (RT ENGINE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK: FORWARD RT ENGINE MOUNTS TABS WORN. REPAIR IAW SRAS CE-1800/16.10319 DATED 6/6/2016.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK: LEVEL 2 CORROSION FOUND ON UPPER SURFACE OF FLOORBEAM 9 AT GROUNDING POINTS UNDER CENTER PEDESTAL. REPAIRED IAW SRAS S531R0336.10310 DATED 6/8/2016.

Part: TORQUE TUBE — CORRODED (RUDDER) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

WO 156831 NR 300007 HEAVY CHECK COE & MINOR REPAIR. RUDDER UPPER TORQUE TUBE HAS LEVEL 2 PITTING CORROSION ON THE UPPER & LOWER BEARING SURFACES. REPLACED TORQUE TUBE ASSEMBLY.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK: LEFT MLG ACTUATOR TO FUSELAGE FITTING HAS LEVEL 2 CORROSION AND 1 ELONGATED HOLE. REPAIR IAW SRAS AIR AMS/ATR30212/97, 1031 ISSUE B DATED 6/10/2016.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK. LOWER KEELBEAM AT FRAME 27 HAS LEVEL 2 CORROSION. REPLACED LOWER WEB WITH OEM PART.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. NOSE FUSELAGE LT AFT LOWER SKIN PANEL HAS LEVEL 2 CORROSION FRAME 8 - 9, STRINGER 21L - 21R AT DME 2 ANTENNA LOCATION. DOUBLER REPAIR IAW SRM 531129-300-802-B01.

Part: STRIP — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT ELEVATOR TIP UPPER PANEL ASSEMBLY STRIP HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE-1605/16, 10303, DATED 6/8/2016.

Part: FLOOR PANEL — CORRODED (COCKPIT) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: COCKPIT FLOOR PANEL 211FF HAS AREAS OF LEVEL 2 CORROSION ON TOP SURFACE. REPLACED PANEL WITH OEM PART.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: FWD CENTER FUSELAGE INTERNAL BONDED DOUBLER AT ANTENNA LOCATION, FRAMES 20-21 HAVE LEVEL 2 CORROSION. REPAIR IAW SRAS CE-1825/16, 10215, DATED 5/19/2016.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD FWD SURFACE, LOWER RT INBD BONDING POINT HAS FRETTING. LEVEL 2 CORROSION CORRECTIVE ACTION. DOUBLER REPAIR SRM 531110-300-808-A01.

Part: BULKHEAD — CHAFED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: FWD PRESSURE BULKHEAD UPPER LT FORWARD SURFACE HAS LEVEL 2 CORROSION. REPAIRED IAW SRAS CE-1460/16, 10247 DATED 5/23/2016.

Part: BULKHEAD — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD WEB FWD HAS FRETTING. UPPER LT INBD BONDING POINT LEVEL 2 DOUBLER REPAIR AT FRAME 1 IAW SRM 531110-300-803-A01.

Part: BULKHEAD — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD WEB, FWD SURFACE HAS FRETTING, UPPER RT INBD BONDING POINT LEVEL 2. DOUBLER REPAIR AT FRAME 1 IAW SRM 531110-300-803-A01.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD, LOWER LT INBD BONDING POINT HAS FRETTING AT LOWER LT CORNER. LEVEL 2 CORROSION CORRECTIVE ACTION. DOUBLER REPAIR SRM 531110-300-808-A01.

Part: WINDOW FRAME — DAMAGED (CABIN) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. FRETTING DAMAGE ON LOWER INBD SURFACE OF WINDOW FRAME, FRAME 32 - 33, LEVEL 2. REPAIRED IAW SRAS CE 1526 16 10124 DATED 4 8 2016.

Part: RIB — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR, LEFT ELEVATOR CENTER RIB UNDER PANEL 334FT HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT FRAME 26, SHEAR TIE ANGLE IS CRACKED BETWEEN STR`S 12R AND 13R. REPLACED ANGLE BY FABRICATION.

Part: PLUG — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. LT CARGO COMPARTMENT WINDOW PLUG HAS LEVEL 2 FRETTING CORROSION. REPLACED WINDOW PLUG WITH OEM PART.

Part: ANGLE — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

WO 156831 NR 300013 HEAVY CHECK COE & MINOR REPAIR. LT ELEVATOR CTR RIB INBD ANGLE UNDER PANEL 334FT HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. LT CARGO COMPARTMENT WINDOW FRAME, BETWEEN FRAMES 23 & 24 HAS LEVEL 2 CORROSION. REPLACED WINDOW FRAME WITH OEM PART.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: RT FRAME 5 IS CRACKED BELOW NODE 6. REPLACED WITH OEM PART.

Part: DOUBLER — CORRODED (LT NACELLE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. LT NACELLE INBD SHEET METAL PANEL LANDING REAR SECTION HAS LEVEL 2 FRETTING. REPLACED WITH OEM PART.

Part: WEB — CORRODED (RT NACELLE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. RT NACELLE INBD SHEET METAL PANEL LANDING REAR SECTION HAS LEVEL 2 FRETTING. REPLACED WITH OEM PART.

Part: DOUBLER — CORRODED (RT NACELLE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. RT NACELLE OTBD SHEET METAL PANEL LANDING REAR SECTION HAS LEVEL 2 FRETTING. REPLACED WITH OEM PART.

Part: WEB — CORRODED (LT NACELLE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. LT NACELLE OTBD SHEET METAL PANEL LANDING REAR SECTION HAS LEVEL 2 FRETTING. REPLACED WITH OEM PART.

Part: STRAP — DAMAGED (CARGO DOOR) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: FWD CARGO DOOR INTERIOR SUPPORT STRAP FWD AND AFT OF CENTER HOOK BENT AND GOUGED. REPAIRED IAW SRAS CE-1557/16, 10271, DATED 6/3/2016.

Part: HINGE — CORRODED (RT AILERON TAB) · corrosion level 2 · airframe 37,507 hrs · 45,071 cycles

HEAVY CHECK COE/MINOR REPAIR: RT AILERON TAB OTBD HINGE HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.

Part: TAB — CORRODED (RT AILERON) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: RT AILERON TAB INBD UPPER CORNER HAS LEVEL 2 CORROSION. REPLACED CHANNEL WITH OEM PART.

Part: SUPPORT — CORRODED (LT AILERON) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: LT AILERON TRIM BEAR CLAW, BELLCRANK, HAS LEVEL 2 CORROSION AND PLAY AT TRIM ACTUATOR ATTACH POINT. REPLACED SUPPORT WITH OEM PART.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON INTERCOSTAL IN RT WHEEL WELL ON FRAME 25A. REPLACED INTERCOSTAL WITH OEM PART.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON INTERCOSTAL IN RT WHEEL WELL IN FRAME 25A. REPLACED INTERCOSTAL WITH OEM PART.

Part: FITTING — CRACKED (RT MLG) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: RT MLG ACTUATOR FITTING ON THE FUSELAGE IS CRACKED AT THE BOTTOM FORWARD BOLT. REPLACED FITTING WITH OEM PART.

Part: STRUCTURE — CORRODED (NLG WW) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: NOSE WHEEL WELL RT UPPER CHORD HAS LEVEL 2 CORROSION UNDER FITTING AT FRAME 5. REPAIR IAW SRAS CE-1501/16, 10214, DATED 5/10/2016.

Part: DOUBLER — CORRODED (NLG WW) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON NOSE WW PANEL 116AZ DOUBLER. REPLACED DOUBLER WITH OEM PART.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT LONGITUDINAL FLOORBEAM CRACKED AT FRAME 29. REPAIRED IAW EO 5315-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: LEFT FRAME 26 IS CRACKED AT STR 13L. REPLACED FRAME WITH OEM PART.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: INTERIOR FUSELAGE UNDER FLOOR BETWEEN FRAMES 25 & 26, CABLE PASS THROUGH CUP HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE RT UPPER SKIN PANEL HAS LEVEL 2 CORROSION AFT OF FRAME 17, BETWEEN STRINGER 7A RT & 8R. DOUBLER REPAIR IAW SRM 53-00-00-300-803.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: STR 3R, SPLICE FWD OF FRAME 23 HAS LEVEL 2 CORROSION. REPLACED SPLICE WITH OEM PART.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MAJOR REPAIR: LT UPPER WING OTBD REMOVABLE PANEL HAS LEVEL 2 CORROSION AT RIB 21 NEXT TO VORTEX GENERATOR. REPAIRED IAW SRAS CE-1347/15, 10273, DATED 5/30/2016.

Part: VORTEX GEN — CORRODED (RT WING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE/MINOR REPAIR: RT UPPER OTBD WING HAS 2 EA VORTEX GENERATORS WITH LEVEL 2 CORROSION. REPLACED VORTEX GENERATORS WITH OEM PARTS.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK, COE/MAJOR REPAIR. RIGHT UPPER WING SKIN HAS AREAS OF LEVEL 2 CORROSION AROUND AND UNDER THE VORTEX GENERATORS BETWEEN RIBS 23 AND 29. REPAIR IAW SRAS S572R0357.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT UPPER WING OTBD PANEL HAS AREAS OF LEVEL 2 CORROSION OTBD OF RIBS 23 - 29 UNDER VORTEX GENERATORS. REPAIRED IAW SRAS S572R0357 10305 DATED 6 3 2016.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT UPPER WING OTBD PANEL HAS AREAS OF LEVEL 2 CORROSION ALONG FWD EDGE OF SKIN, BETWEEN RIBS 23 - 26. REPAIRED IAW SRAS S572R0357 10305 DATED 6 3 2016.

Part: VORTEX GEN — CORRODED (LT WING) · corrosion level 2 · airframe 37,507 hrs · 45,070 cycles

HEAVY CHECK COE & MINOR REPAIR. LT UPPER OTBD WING HAS 3 GENERATORS WITH LEVEL 2 CORROSION. REPLACED VORTEX GENERATORS.

Part: WINDOW FRAME — CRACKED (WINDSHIELD) · airframe 36,508 hrs · 44,265 cycles

DURING HEAVY CHECK. A CRACK INDICATION ON LT WINDSHIELD FRAME AT NODE FIVE. REPAIRED IAW SRAS IAW SO ET560 1925 00 1210 ISSUE B.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,508 hrs · 44,265 cycles

HEAVY CHECK COE MINOR REPAIR. LOWER TCAS ANTENNA DOUBLER LE HAS LEVEL 2 CORROSION. REPLACED DOUBLER WITH NEW.

Part: SKIN PANEL — DEBONDED (LT NACELLE) · airframe 36,508 hrs · 44,265 cycles

WORK ORDER 132789 NR 400004 HEAVY CHECK COE MAJOR REPAIR. PANEL 476AR INNER SKIN SEPARATED FROM CORE. LT NACELLE INBD LATERAL PANEL. REPAIR IAW SRAS DT S-1417/14 8311 DATED 3/21/2014.

Part: BELLCRANK — CORRODED (RT AILERON TAB) · corrosion level 2 · airframe 36,508 hrs · 44,265 cycles

HEAVY CHECK COE MINOR REPAIR. RT AILERON TAB BELLCRANK HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 36,508 hrs · 44,265 cycles

HEAVY CHECK COE MINOR REPAIR. RT WING TE SUPPORT, LOWER ATTACH BRACKET AT RIB 15 ON LOWER SPAR IS CRACKED. REPLACED WITH NEW PART.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,508 hrs · 44,265 cycles

HEAVY CHECK COE MAJOR REPAIR. LEVEL 2 CORROSION DAMAGE TO LT LOWER SIDE BOX WEB AT FRAME 25-26. REPAIR IAW SRAS DT S-1206 14 8299 DATED 3/21/2014.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,508 hrs · 44,265 cycles

LEFT OTBD LONGITUDINAL FLOOR BEAM AT FRAME 21 IS CRACKED. REPAIR IAW EO 5314-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,508 hrs · 44,265 cycles

RT OTBD LONGITUDINAL FLOORBEAM FWD OF FRAME 31 IS CRACKED. REPAIR PER EO 5315-01 REV D.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,508 hrs · 44,265 cycles

WORK ORDER 132789 NR 100010 HEAVY CHECK COE MAJOR REPAIR. INTERIOR FUSELAGE, RT LOWER SIDE BOX WEB BETWEEN FRAMES 25 & 26 HAS LEVEL 2 CORROSION. REPAIR IAW SRAS DO TS-1513 10 5654 DATED 3/19/2014.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,508 hrs · 44,265 cycles

HEAVY CHECK COE MAJOR REPAIR. LEVEL 2 CORROSION DAMAGE TO RT LOWER SIDE BOX STRAP AT FRAME 26. REPAIR IAW SRAS DO TS 1513-10 5654.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,508 hrs · 44,265 cycles

STRINGER 19R HAS LEVEL 2 CORROSION BETWEEN FRAMES 32 & 33. REPAIR IAW SRM 53-00-00 FIG 424.

Part: SPAR — ERODED (RT WING) · airframe 35,730 hrs · 43,448 cycles

HEAVY CHECK / MAJOR REPAIR: RT WING FRONT SPAR LOWER CHORD BETWEEN RIBS 4 & 5 (BL 1210R TO 1625R) HAS FRETTING INBOARD OF HINGED LEADING EDGE. SUBMITTED TO ATR, REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.

Part: SPAR — ERODED (LT WING) · airframe 35,730 hrs · 43,448 cycles

HEAVY CK / MAJOR REPAIR: LT WING FRONT SPAR LOWER CHORD BETWEEN RIBS 4 & 5 (BL 1210L TO BL 1625L) HAS FRETTING INBOARD OF HINGED LEADING EDGE. SUBMIT TO ATR AND REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,730 hrs · 43,448 cycles

HEAVY CK / MAJOR REPAIR: DENT ON FUSELAGE SKIN AFT CARGO DOOR CUTOUT AFT SIDE OF DOOR FROM 2ND FROM BOTTOM SHOOT BOLT FITTING. SUBMITTED DATA TO ATR, REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS.

Part: SUPPORT FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 35,730 hrs · 43,448 cycles

HEAVY CHECK / MAJOR REPAIR / LEVEL 2 CORROSION: RT MAIN GEAR TRUNNION SUPPORT FITTING UPPER EDGE HAS CORROSION AROUND SOME FASTENERS. SUBMIT DATA TO ATR AND REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,730 hrs · 43,448 cycles

HEAVY CK / MAJOR REPAIR: DENT ON FUSELAGE EXTERIOR SKIN AFT CARGO DOOR CUTOUT, AT TOP FWD SHOOT BOLT FITTING. SUBMITTED REPAIR REQUIREMENTS TO ATR. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,730 hrs · 43,448 cycles

HEAVY CK / MAJOR REPAIR: DENT ON FWD EDGE OF AFT CARGO DOOR CUTOUT, EXTERIOR SKIN COMMON TO 2ND FROM BOTTOM SHOOT BOLT FITTING. SUBMIT DATA TO ATR AND REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,730 hrs · 43,448 cycles

HEAVY CK / MAJOR REPAIR / LEVEL 2 CORROSION: MULTIPLE AREAS OF SURFACE CORROSION ON FUSELAGE SKIN AT FWD LOWER CORNER OF CARGO DOOR CUTOUT. SUBMIT TO ATR AND REPAIR PER ATR STRUCTURAL REPAIR INSTRUCTIONS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,730 hrs · 43,444 cycles

HEAVY CK / MAJOR REPAIR: LEFT O/B LONGITUDINAL FLOORBEAM IS CRACKED AFT OF FRAME 19. REMOVED LEFT O/B FLOORBEAM BETWEEN FRAME 19 AND 20, FABRICATED AND INSTALLED NEW LEFT O/B LONGITUDINAL FLOORBEAM REF EO 5315-01 REV D.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 35,709 hrs · 43,426 cycles

AIR TURNBACK TO SEA: AFTER TAKEOFF ON FLT 7076 AIRCRAFT GEAR LEVER WOULD NOT UNLOCK AND ALLOW THE GEAR TO RETRACT. CREW RETURN TO SEA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR LEVER. AIRCRAFT RETURNED TO SERVICE.

Part: RECEIVER — MALFUNCTIONED (NR 2 NAV) · airframe 35,338 hrs · 43,003 cycles

ON FLIGHT 8216 WHILE EN ROUTE FROM SIT TO KTN THE NR 2 NAV BECAME INOP. IT WAS DECIDED TO OVERFLY KTN AND CONTINUE TO SEA WHERE THERE WAS MORE SUITABLE MAINTENANCE AND PARTS AVAILABLE. MAINTENANCE REMOVED AND REPLACED THE NR 2 NAV RECEIVER. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — FAULTY (DE-ICE SYSTEM) · airframe 35,294 hrs · 42,964 cycles

DURING CLIMB OUT FROM KTN FLIGHT 7202 TO SIT CREW RECEIVED FAULTS ON THE NR 1 ENGINE DEICE, NR 1 PROP DEICE AND AIRFRAME DEICE. DUE TO ICING CONDITIONS IN SIT CREW ELECTED TO CONTINUE TO JNU FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED DEICE CONTROLLER. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (OIL SYSTEM) · airframe 35,206 hrs · 42,886 cycles

ATB JNU FLIGHT 8216: SHORTLY AFTER ROTATION THE NR 2 ENGINE OIL PRESSURE GAUGE ILLUMINATED FALLING OIL PRESSURE, CRC ACTIVATED FOR 5 SECONDS THEN RETURNED TO NORMAL. CREW ELECTED TO RETURN TO JNU. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED OIL PRESSURE REGUATOR INTERNALS AND REMOVED AND REPLACED OIL PRESSURE TRANSMITTER AND LOW OIL PRESSURE SWITCH. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — FAULTY (NR 2) · airframe 35,036 hrs · 42,723 cycles

ENROUTE FROM SIT TO KTN FLIGHT 8216: WHILE ENROUTE THE NR 2 DC GENERATOR CONTROL UNIT WENT OFF LINE. CREW ATTEMPTED TO RESET THE GENERATOR WITHOUT SUCCESS. CREW ELECTED TO DIVERT TO SEA WHERE MAINTENANCE WAS AVAILABLE. SEA MAINTENANCE REMOVED AND REPLACED THE DC GENERATOR. AIRCRAFT RETURNED TO SERVICE.

Part: STOP FITTING — CORRODED (NLG WW) · corrosion level 2 · airframe 34,776 hrs · 37,214 cycles

HEAVY CHECK COE; LEVEL 2 CORROSION MINOR REPAIR: NOSE GEAR WELL FWD LEFT GEAR DOOR, AFT SPRING STOP TRIANGULAR SHAPED STRUCTURE CORRODED. REMOVED AND REPLACED LT NLG DOOR STOP ASSEMBLY WITH SERVICEABLE UNIT PER SRM.

Part: PRESSURE PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,776 hrs · 42,463 cycles

HEAVY CHECK COE; LEVEL 2 CORROSION MAJOR REPAIR: CARGO COMPARTMENT, RT CREASE BEAM PRESSURE DECK WEB FWD OF FRAME 27 HAS AN AREA OF SURFACE CORROSION & CORRODED ATTACH ANGLE. REMOVED ATTACH ANGLE AND CORROSION IAW SRM. REQUESTED SRAS FROM ATR TO LEAVE BLEND OUT AS IS.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,776 hrs · 42,463 cycles

HEAVY CHECK COE; MAJOR REPAIR: STRINGER 7L AT FRAME 31 IS CRACKED AT FASTENER HOLE. STRINGER SPLICED IAW SRM.

Part: SELECTOR SWITCH — BROKEN (POWER MANAGEMENT) · airframe 34,287 hrs · 41,992 cycles

DURING CLIMB, POWER MANAGEMENT SWITCH FAILED. CREW UNABLE TO SELECT DESIRED MODE. CREW ELECTED TO BYPASS SIT AND LAND WHERE MX WAS AVAILABLE. MX REMOVED SELECTOR SWITCH AND REPLACED LOCKING TAB. SELECTOR SWITCH WAS REINSTALLED. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE)

FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: LEVEL 2 CORROSION: SRAS: FOUND CORROSION ON EXTERNAL SURFACE OF FUSELAGE SKIN UNDER THE CARGO DOOR THRESHOLD PROTECTION PLATE. PROTECTION PLATE INSTALLED BY M7 AEROSPACE STC ST01189WI. BLENDED-OUT AREAS OF CORROSION ON EXTERNAL FUSELAGE SKIN PER SRAS DO/TS-2668...4699, DO/TS-2668-08-10359, JUSTIFICATION DOCUMENTS REF: NOTE DO/TS-2717/08. SKIN THICKNESS LEFT AS-IS AFTER BLENDING. (S)

Part: SPAR — CORRODED (VERTICAL STAB)

FOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION AROUND THE RIVET FILLED TOOLING HOLE ON THE AFT SURFACE OF VERTICAL STAB REAR SPAR. LOCATED IN THE CENTERLINE OF THE SHEAR WEB BETWEEN STIFFENERS (P/N`S S55371300230 AND S55371300225). REPAIRED PER SRAS DO/TS-2656/08-4694, NOTE DO/TS-2665/08-10353. CORROSION REMOVED FROM THE RIVET HOLE AREA PER THE SRM. A REPAIR DOUBLER WAS MADE & INSTALLED ON THE STABILIZER SPAR. (S)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: RT LONGITUDINAL FLOOR SUPPORT AT FRAME 36R IS CRACKED ABOVE STRINGER 18R. REPAIRED PER EMPIRE AIRLINES EO 5315-01 REV B. REMOVED & REPLACED RT LONGITUDINAL FLOOR BEAM FROM FRAME 36R TO 40R. (S)

Part: CREASE BEAM — CORRODED (FUSELAGE)

FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: LEVEL 2 CORROSION: THE RT CREASE BEAM BETWEEN FRAMES 35R & 36R HAS AREAS OF MISSING PAINT & SURFACE CORROSION. FOUND CORROSION BETWEEN WEB DOUBLER PLATE AND CREASE BEAM WEB. REMOVED CORROSION FROM WEB AND REMOVED & REPLACED WEB DOUBLER ON CREASE BEAM WEB BETWEEN FRAMES 35R & 36R. (S)

Part: SPAR — CORRODED (VERTICAL STAB)

FOUND DURING HEAVY CHECK AT COE. AFT SURFACE OF VERTICAL STAB REAR SPAR HAS AREAS OF SURFACE CORROSION BETWEEN LOWER & UPPER RUDDER ATTACH FITTINGS. REPAIRED PER SRAS DO/TS-2656/08-4694, NOTE DO/TS-2665/08-10353. CORROSION REMOVED FROM THE RIVET HOLE AREA PER THE SRM. A REPAIR DOUBLER WAS MADE & INSTALLED ON THE STABILIZER SPAR. (S)

Part: ANGLE — CORRODED (FUSELAGE)

FOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION ON FLOORBEAM 12 REINFORCEMENT ANGLE FOR ENGINE CABLE QUADRANT ABOVE STRINGER 20R HAS EXFOLIATION. REMOVED CORRODED ANGLE, MADE AND INSTALLED REPLACEMENT ANGLE. (S)

Part: HINGE — CORRODED (RT AILERON)

FOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION ON RT AILERON O/B HINGE FITTING ON THE AILERON HAS EXFOLIATING CORROSION. REMOVED AND REPLACED RT AILERON ASSY. (S)

Part: FITTING — CORRODED (RT AILERON)

FOUND DURING HEAVY CHECK AT COE. RT AILERON CENTER TEE PICKUP FITTING I/B SIDE HAS EXFOLIATING CORROSION. REMOVED AND REPLACED RT AILERON ASSY. (S)

Part: SKIN — MISREPAIRED (FUSELAGE)

FOUND DURING HEAVY CHECK AT COE. PREVIOUSLY INSTALLED REPAIR DOUBLER ON THE EXTERNAL SKIN BETWEEN FRAMES 5 & 6 JUST ABOVE RT AFT NLG DOOR IS INSTALLED WITH CHERRY MAX RIVETS. REMOVED CHERRY MAX RIVETS AND INSTALLED SOLID RIVETS. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: LEVEL 2 CORROSION: FLOORBEAM 13, BL 0 HAS 5 EACH FLOORBOARD SCREW HOLES EXFOLIATING ON TOP AND BOTTOM OF FLOORBEAM UPPER FLANGES. FLOORBEAM 13 REPLACED WITH AN ADDED SPLICE TO THE BEAM AT BL 0. (S)

Part: RIB — CORRODED (TE FLAP)

FOUND DURING HEAVY CHECK AT COE. LEVEL 2 CORROSION ON RT WING OUTBOARD FLAP, FLAP RIB 18 FWD PICK UP IS EXFOLIATING INSIDE OF FLAP. REPLACED OUTBOARD FLAP ASSEMBLY. (S)

Part: WIRE HARNESS — WORN (NLG UP RT)

AIR TURN BACK. FLT NR 8804. AFTER TAKE OFF THE LANDING GEAR WOULD NOT RETRACT. CREW ATTEMPTED SEVERAL CYCLES BEFORE ELECTING TO RETURN. GEAR LIGHTS RED AND GREEN, WOULD CYCLE BETWEEN GEAR DOWN AND LOCKED AND UNLOCKED. NO EMERGENCY WAS DECLARED AND THE PLANE LANDED NORMALLY AND SAFETY. REPLACED NOSE LANDING GEAR WIRE HARNESS. (K)

Part: AHRS — FAILED (E&E BAY)

FLT NR 8202 JUN TO SIT, FLT NR 7203 SEA TO KTN AIR TURN BACKS: NR 2 AHRS (ALTITUDE AND HEADING REF SYSTEM) WITH EFIS COMP ( ELECTRONIC FLIGHT INSTRUMENTS SYS FAULTED). FLT NR 8203 AHRS CONNECTIONS CLEANED AND RESECURED, SYSTEM OPERATED NORMALLY FOR 3 STOPS. FLT NR 7203 AHRU REPLACED (ALTITUDE AND HEADING REF UNIT). REF NR 45982, 86. (K)

Part: CONNECTOR — DIRTY (NR 2 AHRS)

FLT 7202 - ABORTED APPROACH, OVERFLYING KTN AND SIT, WHILE ON APPROACH INTO KTN FROM SEA, NR 2 AHRS WITH EFIS COMP ALERTED ON THE CREW ALERT PANEL. APPROACH WAS TERMINATED AND THE AIRCRAFT CONTINUED ON TO JNU, OVERFLYING KTN AND SIT. AHRS CONNECTIONS CLEANED AND RESECURED. (M)

Part: WIRE HARNESS — SHORT (NR GEN)

FLT 100 - WHILE ENROUTE, NR 1 ACW GENERATOR FAULT AFTER TAKEOFF. RETURNED GEG. REPAIRED (3) CHAFED WIRES ON 411VC HARNESS NR 2422-2525, 2526, AND 2527. (M)

Part: CONTROL UNIT — SHORTED (NR 1 ENGINE)

WHILE ENROUTE, NR 1 ACW GENERATOR FAULT WOULD NOT RESET. SMELLED ELECTRICAL SMOKE FOR 30 SECONDS THEN WENT AWAY. REMOVED AND REPLACED NR 1 ACW GENERATOR AND ACW GENERATOR CONTROL UNIT. (M)

Part: WIRE — SHORTED (CONTROL UNIT)

WHILE EN ROUTE FROM KTN-SIT, THE NR 2 HEADING BUG AND INDICATOR FAILED. CREW ELECTED TO OVERFLY SIT AND CONTINUE ON TO JUN FOR MAINTENANCE. SECURED LOOSE WIRING, CLEANED AND RE-CLAMPED CONNECTOR ON THE COURSE AND HEADING CONTROL UNIT. (M)

Part: VALVE — INOPERATIVE (NR 2 ENGINE)

NR 2 ENGINE ANTI-ICE FAULT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. PILOT ELECTED TO TURN BACK. AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 2 DUEL DISTRIBUTOR DEICE VALVE WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. (K)