N888PV

Part: STRUT — CORRODED (ZONE 500) · corrosion level 2 · airframe 39,870 hrs · 85,930 cycles

LT WING STRUT BOTTOM FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED, LT WING STRUT IAW DH6-300 MM CHAPTER 57-00.

Part: LONGERON — CRACKED (RT NACELLE) · airframe 30,798 hrs · 48,010 cycles

RT NACELLE OTBD LONGERON CRACKED. REMOVED AND REPLACED RT NACELLE OTBD LONGERON WITH FACTORY NEW PART.

Part: SKIN — CRACKED (RT WING) · corrosion level 2 · airframe 39,579 hrs · 84,609 cycles

AFTER REMOVING OTBD PLANK DOUBLERS AT WS 118 TO 138 OF THE RT WING, FOUND TWO CRACKS IN THE UPPER WING SKIN. ONE .7500 CRACK AT WS 123.5 AND 47 INCHES AFT OF NOSE SPAR AND ONE .5 INCH CRACK AT WS 123.5 AND 43 INCHES AFT OF THE NOSE SPAR. ACCOMPLISHED REPAIRS IAW SRM 57-30-00 FIG 6 PAGES 6 AND 7. ALL SURFACES CLEANED TREATED AND PRIMED IAW 1 GEN-5 CHAPTER 5. PLANK DOUBLERS REINSTALLED IAW RD6-57-618.

Part: SPAR — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 39,579 hrs · 84,609 cycles

FORWARD SEA FIN MOUNT CORRODED ON LEFT STABILIZATION. REMOVED AND REPLACED LEFT OUTBOARD STABILIZER FORWARD SPAR WITH FACTORY NEW PART.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 39,579 hrs

RT WING, RT ENGINE MOUNT BRACKET CORRODED. REMOVED AND REPLACED RT ENGINE MOUNT ADAPTOR IAW RD6-54-006. (K)

Part: DOUBLER — CORRODED (RT WING) · airframe 39,579 hrs · 84,609 cycles

RIGHT WING EXHAUST TRAIL DOUBLERS CORRODED. REMOVED AND REPLACED EXHAUST TRAIL DOUBLERS IAW RD6-57-618. ALL SURFACES CLEANED, TREATED, AND PRIMED IAW 1-GEN-5 CHAPTER 5.

Part: LONGERON — CRACKED (RT NACELLE) · airframe 39,028 hrs · 82,971 cycles

RT HAND NACELLE INBOARD LONGERON CRACKED 10 1/2 INCHES AFT OF THE FWD END. REMOVED AND REPLACED RT HAND INBD LONGERON IAW AC 4313-1B CH 4, RD 6-54-036 AND VERIFIED MOD 6/1655 IS INSTALLED PER AD 80-13-12 R1. (A)

Part: CHANNEL — CORRODED (AILERON WEIGHT) · corrosion level 2 · airframe 38,688 hrs · 81,986 cycles

DURING CAMP INSPECTION, FOUND LT AILERON OB WEIGHT BALANCE CHANNEL CORRODED. REMOVED AND REPLACED WEIGHT AND BALANCE CHANNEL, AND STATIC BALANCED AILERON IAW SRM 57-50-21 PAGE 3 AND SRM RD6-57-085.

Part: CONTROL ROD — CORRODED (TE FLAPS) · corrosion level 2 · airframe 38,491 hrs · 81,043 cycles

125 HR INSPECTION, EMERGENCY MEASURES EXECUTED, NO, AC GROUNDED. NO CORROSION FOUND ON RT FLAP INTERCONNECT ROD UNDER FLEXIBLE BOOT. ON IB END. REMOVED AND REPLACED CONTROL ROD.

Part: ATTACH BRACKET — CRACKED · airframe 38,287 hrs · 80,792 cycles

LT AND RT FORWARD STRUT FITTING CRACKED. REMOVED AND REPLACED LOWER STRUT TO FLOAT FITTINGS.

Part: FLOAT — TORN (MLG) · airframe 38,206 hrs · 80,555 cycles

HOLE IN LT FLOAT ABOVE WATER LINE. THE HOLE WAS LOCATED BETWEEN BAYS 4 AND 5 LT FLOAT OB. AIRCRAFT WAS FERRIED FROM SPB TO SSB. REMOVED AND REPLACED FLOAT ASSY IAW SBA WC 32.01

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 38,083 hrs · 80,188 cycles

"OPEN" LT WING IB PLANK DOUBLER (STATION 30) CORRODED AT LEADING EDGE.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 38,083 hrs · 80,188 cycles

"OPEN" RT WING BOTTOM SKIN CORRODED OB OF NACELLE AT STATION 147.

Part: INLET GUIDE VANE — CRACKED (ENGINE) · airframe 38,073 hrs · 80,152 cycles

DURING 400 HOUR BORESCOPE INSPECTION, FOUND CRACKS ON CT STATOR THAT ARE BEYOND SERVICEABLE LIMITS. PERFORMED HOT SECTION INSPECTION. REPLACED IE DUCT ASSEMBLY.

Part: ARM — CORRODED (FLAP HINGE) · airframe 37,776 hrs · 79,253 cycles

LEFT HAND I/B FORE FLAP O/B HINGE ARM CORRODED. REMOVED AND REPLACED FORE FLAP

Part: FAN — ODOR (CABIN) · airframe 37,767 hrs · 79,226 cycles

ODOR OF BURNING WIRES IN AIRCRAFT. SHUTDOWN AIR CONDITIONING AND CABIN FANS. ODOR SUBSIDED. REMOVED AND REPLACED LT AND RT CABIN BLOWER FANS. (SZ57-003-2A)

Part: ATTACH BRACKET — CRACKED (ZONE 300) · corrosion level 2 · airframe 19,351 hrs · 42,064 cycles

RIGHT HAND FLOAT FORWARD SPREADER BAR ATTACH FITTING HAS A LONGITUDINAL CRACK (WITH THE GRAIN) ACROSS THE TOP OF THE SPREADER BAR ATTACHMENT LUG.

Part: ATTACH FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 374,908 hrs · 78,409 cycles

RT WING AFT ATTACH FITTING CORRODED. REMOVED AND REPLACED WING ATTACH FITTING IAW SB 6/295 REV D.

Part: SPAR CAP — CORRODED (RT WING) · corrosion level 2 · airframe 37,490 hrs · 78,409 cycles

FOUND CORROSION ON RT WING LOWER MAIN WING SPAR CAP BETWEEN STATION 35.2 AND STATION 74. REPAIRED IAW RD-57-24 AND INSTALLED SKIN PATCH IAW SRM 57-30-00 FROM STA 47 TO STATION 60.

Part: FRAME — CORRODED (LT NACELLE) · airframe 36,815 hrs · 76,354 cycles

CORROSION FOUND ON LT NACELLE HOOP FRAME (ANGLE FIREWALL) REMOVED AND REPLACE HOOP FRAME IAW AC 43.13-1B PARA 4.23 AND 4-6.

Part: MOUNT — CORRODED (ZONE 400) · airframe 36,815 hrs · 76,354 cycles

RIGHT ENGINE UPPER ENGINE MOUNT PLATE HAS CORROSION. REMOVED AND REPLACED UPPER ENGINE MOUNT PLATE IAW RD-54-006.

Part: MOUNT — CORRODED (ZONE 400) · airframe 36,815 hrs · 76,354 cycles

RIGHT ENGINE RIGHT ENGINE MOUNT PLATE HAS CORROSION. REMOVED AND REPLACED RIGHT ENGINE MOUNT PLATE IAW RD-54-006.

Part: ANGLE — CORRODED (FIREWALL) · airframe 36,815 hrs · 76,354 cycles

RIGHT HAD ENGINE NACELLE HOOP (ANGLE FIREWALL) FRAME HAS CORROSION. REMOVED AND REPLACED HOOP FRAME.

Part: FRAME — CORRODED (BS 218) · airframe 36,815 hrs · 76,354 cycles

DURING WING STRUT BOLT INSPECTION, FOUND CORROSION ON STS 218.11 (MAIN FRAME). REMOVED AND REPLACED MAIN FRAME IAW SERVICE BULLETIN 6/354.

Part: RING — CRACKED (RT ENGINE VANE) · airframe 36,729 hrs · 76,084 cycles

REF NR (S9BA-002) DURING HSI FOUND CRACK ON THE PT VANE RING. LOOKING FROM AFT TO FWD AT 3 OCLOCK POSITION CRACK EXTENDS ACROSS INNER HOUSING THROUGH THE FILLET RADIUS AND AIRFOIL. REMOVED AND REPLACED PT VANE RING. (K)

Part: SKIN — CORRODED (LT WING)

CORRODED SKIN ALONG THE FIRST ROW OF RIVETS ON UPPER LEFT WING IB OF THE NACELLE BETWEEN STATIONS 60 AND 72.5. CORRODED SKIN WAS TRIMMED OUT AND AN EXTERNAL PATCH RIVETED IN PLACE IAW RD6-57-077. (K)

Part: STRUCTURE — CORRODED (TAIL) · airframe 36,153 hrs · 74,217 cycles

(REF NR: 888-07)LT LWR FINLET REQUIRES CHANGE DUE TO CORROSION. REMOVED AND REPLACED LT LWR FINLET ASSY IAW MM.(K)