N176CA

Part: SLEEVE — PERFORATED (THRUST REVERSER) · airframe 73,337 hrs · 22,272 cycles

NR 1 ENGINE, OUTBOARD THRUST REVERSER INNER SLEEVE PANEL PERFORATED AT THE 7:00 POSITION. REPAIRED IAW EA 17131, REVISION IR.

Part: BULKHEAD WEB — CHAFED (APU BAY)

APU COMPARTMENT FORWARD BULKHEAD CHAFED AT BS 1885 AND RBL 6, APPROXIMATELY 8 INCHES FROM LOWER EDGE OF BULKHEAD. REPAIRED THE FIREWALL IAW SRM 53-80-08, REPAIR 2.

Part: STRAP — CRACKED (BS 365) · airframe 72,604 hrs · 22,071 cycles

FLOORBEAM BS 365, BL 0, ABOVE NOSE GEAR BOX HAS A BROKEN STRAP. REMOVED AND REPLACED THE STRAP IAW SRM 53-00-51, SRM 53-00-51, SRM 53-00-51, SRM 51-40-02, AND SRM 53-00-51-2R-12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,503 hrs · 22,043 cycles

EXTERIOR EMERGENCY LIGHT AT R3 DOOR IS INOPERATIVE. REPLACED LAMP AT EXTERNAL EMERGENCY LIGHT AT R3 DOOR PER MM 33-51-06.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,313 hrs · 21,985 cycles

R3 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,240 hrs · 21,964 cycles

L1 EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. SYSTEM OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,103 hrs · 21,925 cycles

L1 DOOR EMERGENCY LIGHTS INOPERATIVE REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,086 hrs · 21,917 cycles

LEFT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER FAILED DURING TEST. REMOVED AND REPLACED LEFT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IN ACCORDANCE WITH AMM 33-51-07. OPERATIONAL CHECK FOUND SATISFACTORY.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,086 hrs · 21,917 cycles

RIGHT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER FAILED DURING TEST. REMOVED AND REPLACED RIGHT AFT CABIN EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IN ACCORDANCE WITH AMM 33-51-07. OPERATIONAL CHECK FOUND SATISFACTORY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,797 hrs · 21,841 cycles

DURING INSPECTION, FOUND RT AFT EMERGENCY EXTERIOR LIGHT LAMP NOT ILLUMINATED. R & R LIGHT BULB AND PERFORMED OPS CHECK IAW AMM 33-51-07.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,780 hrs · 21,833 cycles

DURING FLIGHT WALK AROUND INSPECTION, R1 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED THE FWD DOOR POWER SUPPLY IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,780 hrs · 21,833 cycles

DURING FLIGHT WALK AROUND INSPECTION, L1 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: LAMP — DEFECTIVE (INDICATOR) · airframe 71,484 hrs · 21,759 cycles

SLIDE LIGHT AT DOOR R2 WILL NOT ILLUMINATE. REPLACED THE LAMP IAW AMM 33-16-02, CHECKED OK. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 71,116 hrs · 21,661 cycles

DURING OPS CHECK OF EMERGENCY EXIT LIGHT, DOOR 2 LT AND 2 RT AND SEAT ROWS 2 THROUGH 6 OVERHEAD EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. R & R EMERGENCY EXIT LIGHT BATTERY PACKS IAW AMM CHAPTER 33-51-07, ALL EMERGENCY EXIT LIGHTS OPERATIONALLY CHECK GOOD.

Part: FRAME — CRACKED (ZONE 500) · airframe 70,509 hrs · 21,503 cycles

LEFT WING AT WS 70. L/E ACCESS PANEL FRAME CRACKED, CRACK LENGTH 1.5". CRACK REPAIRED IAW FAS EA 15777.

Part: TEE FITTING — CORRODED (BS 1220) · corrosion level 2 · airframe 70,509 hrs · 21,503 cycles

RIGHT AT BS 1220, WING TO BODY FAIRING, T-CHORD HAS CORROSION AT BOTTOM END. REPLACED WING TO BODY FAIRING T-CHORD.

Part: SUPPORT FRAME — CORRODED (BS 1280) · corrosion level 2 · airframe 70,509 hrs · 21,503 cycles

LOWER FUSELAGE RT SIDE AT WING TO BODY FAIRING PANEL 196DR. CORROSION ON SUPPORT FRAME. SUPPORT FRAME REPLACED WITH NEW SUPPORT FRAME.

Part: RESERVOIR — LOW PRESSURE (DOOR ASSIST) · airframe 70,509 hrs · 21,503 cycles

LEFT NR 4 ENTRY DOOR POWER ASSIST RESERVOIR HAS LOW PRESSURE. SERVICED RESERVOIR IAW AMM 12-15-10.

Part: FRAME — CRACKED (R2 DOOR) · airframe 70,509 hrs · 21,503 cycles

RIGHT NR 2 DOOR FORWARD SIDE UPPER HINGE ROD CUTOUT CRACKED. CRACK LENGTH 1.5". REPAIRED RT NR 2 DOOR FORWARD SIDE UPPER HINGE CUTOUT IAW SRM 52-10-02, REPAIR 1.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 70,509 hrs · 21,503 cycles

LEFT INBD FLAP OTBD AREA LOWER SIDE HAS 3 EACH DENTS BETWEEN WRS 320-340. REPAIRED LEFT INBD FLAP LOWERSKIN IAW SRM 57-53-01-2R-1, REPAIR 1, AND SRM 51-70-10, REPAIR 2.

Part: RECEPTACLE — DIRTY (EMERGENCY LIGHT) · airframe 70,509 hrs · 21,503 cycles

RIGHT NR 4 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LIGHT IS INOPERATIVE. CLEANED RT NR 4 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LAMP RECEPTACLE, INSTALLED LAMP. PERFORMED SATISFACTORY TEST IAW AMM 33-51-07.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 70,509 hrs · 21,503 cycles

LEFT NR 2 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LIGHT IS INOPERATIVE. REPLACED LT NR 2 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LAMP IAW AMM 33-51-06, OPERATIONALLY TESTS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 70,509 hrs · 21,503 cycles

LEFT NR 4 ENTRY/EXIT DOOR ESCAPE SLIDE LIGHT INOPERATIVE. RELAMPED LT NR 4 ENTRY/EXIT DOOR EMERGENCY ESCAPE SLIDE LIGHT IAW AMM 33-51-06, OPERATIONALLY TESTS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,509 hrs · 21,503 cycles

RIGHT NR 3 EMERGENCY EXIT DOOR ESCAPE SLIDE LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY ASSEMBLY AND ESCAPE SLIDE LAMP. PERFORMED SATISFACTORY OPS TEST IAW AMM 33-51-07.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 70,509 hrs · 21,503 cycles

ALL EMERGENCY EXIT SIGNS IN THE AFT GALLEY AT BS 1664 ARE INOPERATIVE. FOUND CONNECTOR D78 NOT PROPERLY SEATED. SECURED CONNECTOR D78. PERFOMED SATISFACTORY OPS TEST OF EMERGENCY EXIT SIGNS AT AFT GALLEY IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,988 hrs · 21,389 cycles

DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND RT EMERGENCY EXIT DOOR (R-3) EXTERIOR LIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,988 hrs · 21,389 cycles

DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND EMERGENCY LIGHT ASSY AT FLOOR LEVEL OF THE LT NR 2 DOOR WITH SOME OF THE BULBS INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,988 hrs · 21,389 cycles

DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND EMERGENCY LIGHT OVERHEAD OF SEAT 16D INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,263 hrs · 21,189 cycles

WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND EMER EXIT LIGHT AT SEAT ROW 25 LT INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-01. TESTED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

EMERGENCY AISLE LIGHT AT SEAT ROW 20 RT BELOW OVERHEAD BIN INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

LEFT PAX DOOR 1 SIDEWALL EXIT LIGHT HAS 1 EACH BULB BURNT OUT. LAMPED L1 DOOR SIDEWALL EXIT LIGHT IAW AMM 33-51-01. TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND RT PAX DOOR 1 EMER EXIT LIGHT INOPERATIVE. R & R LAMPS IAW AMM 33-51-01. TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

LEFT PAX DOOR 2 SIDEWALL EXIT LIGHT HAS TWO EACH BULBS BURNT OUT. LAMPED L2 DOOR SIDEWALL EXIT LIGHT IAW AMM 33-51-01. TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND LT PAX DOOR 1 EMER EXIT LIGHT INOPERATIVE. R & R LAMPS IAW AMM 33-51-01. TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

EMERGENCY AISLE LIGHT AT SEAT ROW 21 LT BELOW OVERHEAD BIN IS INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

WHILE ACCOMPLISHING TASK CARD 33-001-00-01 FOUND RT EMER EXIT DOOR LIGHT INOPERATIVE. R & R BURNT LAMPS IAW AMM 33-51-01. TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,263 hrs · 21,189 cycles

EMERGENCY AISLE LIGHT AT SEAT ROW 18 LT BELOW OVERHEAD BIN INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,940 hrs · 21,118 cycles

WHILE PERFORMING TASK CARD 33-001-00-01 FOUND EMER BATTERY PACK AT L1 DOOR INOPERATIVE. REPLACED BATTERY PACK.

Part: WINDOW — CRACKED (COCKPIT) · airframe 68,444 hrs · 21,003 cycles

CRACK FOUND AT FIRST OFFICER`S WINDOW R 1.

Part: SLIDE RAFT — UNSERVICEABLE (R1 DOOR) · airframe 68,419 hrs · 22,990 cycles

RIGHT DOOR NR 1, SLIDE RAFT FOUND UNSERVICEABLE DUE TO THE RT SIDE BULGING OUT & BENDING RELEASE PINS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,419 hrs · 20,990 cycles

DURING ACCOMPLISHMENT OF TASK CARD 33-004-01-01, THE L2 DOOR EMER LIGHT FAILED THE EMER LIGHT TEST. FOUND BATTERY PACK DEPLETED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,419 hrs · 20,990 cycles

DURING ACCOMPLISHMENT OF ERO 5330ERO1712, INSPECTION NOTED A CRACKED STRINGER. STRINGER 16 LEFT BODY STATION 613. CRACK LENGHT .5".

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,419 hrs · 20,990 cycles

RIGHT WING TO BODY FAIRING, ATTACH FRAME, HAS CORROSION AT SEVERAL AREAS BS 870, AREAS WERE BLENDED IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS OF 0.063 INCHES, LOSS OF MATERIAL .002 INCHES & REMAINING MATERIAL THICKNESS OF .061 INCHES. ALODINED PRIMED & TOP COATED IAW SRM 51-20-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,348 hrs · 20,953 cycles

EMERGENCY EXIT AISLE LIGHTS INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,348 hrs · 20,953 cycles

EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. FOUND BATTERY PACK DISCHARGED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 68,348 hrs · 20,953 cycles

EMERGENCY EXIT LIGHT AT RT NR 2 DOOR INOPERATIVE. FOUND BATTERY PACK DISCHARGED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,292 hrs · 20,934 cycles

DURING SERVICE CHECK RIGHT NR 4 DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. FOUND BATTERY PACK DISCHARGED. R & R BATTERY PACK IAW AMM33-51-07. CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,227 hrs · 20,881 cycles

EMERGENCY EXIT LIGHT ABOVE L1 DOOR INOPERATIVE.

Part: ACCESS DOOR — MISSING (ZONE 100)

ON ARRIVAL, FOUND GROUND AIR SUPPLY ACCESS DOOR MISSING FROM ACFT. NO OTHER DAMAGE NOTED TO ACFT.

Part: SIGNAL COND UNIT — FAILED (NR 2 ENGINE) · airframe 67,624 hrs · 20,510 cycles

NR 2 ENGINE HIGH VIBRATION INDICATION IN FLIGHT, PRECAUTIONARY ENGINE SHUTDOWN OF THE NR 2 ENGINE ACCOMPLISHED OIL PRESSURE NORMAL. ENGINE WINDMILLED APPROXIMATELY 20 MINUTES. SIGNAL COND. UNIT REPLACED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT OVER SEAT 34ABC INOPERATIVE. REPLACED LAMP IAW AMM 33-21-10. OPS CHECKED GOOD.

Part: LEVER — LACK OF LUBE (L1 DOOR) · airframe 67,114 hrs · 20,205 cycles

L1 DOOR DISARMING LEVER HARD TO MOVE BETWEEN ARM AND DISARM. CLEANED AND LUBED DOOR LINKAGE FOR ARMING LEVER IAW MM 12-21-18. OPS CHECKED GOOD AT THIS TIME.

Part: LEVER — LACK OF LUBE (L1 DOOR) · airframe 67,114 hrs · 20,205 cycles

L1 DOOR DISARMING LEVER HARD TO MOVE BETWEEN ARM AND DISARM. CLEANED AND LUBED DOOR LINKAGE FOR ARMING LEVER IAW MM 12-21-18. OPS CHECK GOOD AT THIS TIME.

Part: WEDGE — DELAMINATED (NR 1 SLAT) · airframe 67,065 hrs · 20,179 cycles

DURING INSPECTION, FOUND NR 1 SLAT T/E WEDGE, FOUND DEBONDED. AREA OF DISBOND 4.5" DIAMETER.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

DURING INSPECTION, FOUND CORROSION AT RT NR 4 PASSENGER DOOR LOWER MAIN SILL. REPAIR PERFORMED IAW SR 2-2346032878.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 67,065 hrs · 20,179 cycles

STIFFNER AT LT STRUT ACCESS PANEL 433CL CUTOUT PP STA 153.9, FOUND CRACKED. CRACK LENGTH .7" STIFFNER.

Part: BRACKET — CRACKED (ZONE 100) · airframe 67,065 hrs · 20,179 cycles

FOUND BRACKET, CRACKED AT BS 1540.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO DOOR LOWER SILL SCUFF PLATE, FWD EDGE OTBD CORNER HAS CRACK, CRACK LENGTH 2".

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

MAIN CABIN BS 1600-1620, STRINGER 17R, STRINGER HAS CORROSION, CORROSION LENGTH 1.6", WIDTH .8" DEPTH .016", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL .047". STRINGER REPAIRED IAW INSTRUCTIONS.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 67,065 hrs · 20,179 cycles

EMERGENCY LIGHT BATTERY PACK CAN NOT BE DEEP CHARGED.

Part: RETAINER — CRACKED (THRUST REVERSER) · airframe 67,065 hrs · 20,179 cycles

NR 2 ENGINE THRUST REVERSER "C" DUCT T/E UPPER FORWARD RETAINER HAS TWO CRACKS. CRACK ONE LENGTH .25" CRACK TWO LENGTH .5". REPAIRED IAW DWG 5430D1519.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 67,065 hrs · 20,179 cycles

LEFT HORIZONTAL STABILIZER L/E INBD FAIRING 332AL UPPER SURFACE AFT AREA FOUND CRACK.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1640, STRINGER 29L TO 29R FRAME WEB HAS HEAVY CORROSION. REPLACED FROM STRINGER 24L TO S24R IAW DWG 146N1032. REF NRC HFL6086. GENERATED FROM TASK CARD 53-222-00-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO BS 640-660, LBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5" WIDTH 1", DEPTH .029" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .034". FLOOR SUPPORT REPLACED IAW DWG 143N5370.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO BS 640-660 RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .018", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .045". FLOOR SUPPORT REPLACED IAW DWG 143N5370.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO BS 640-660, LBL 7.55", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .017", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .046", FLOOR SUPPORT REPLACED IAW DWG 143N5370.

Part: FAIRING — SCRATCHED (ZONE 300) · airframe 67,065 hrs · 20,179 cycles

LEFT HORIZONTAL STABILIZER L/E MID FAIRING 332CL 2 EA AREAS SCRATCHED, (AREA 1 LENGTH 1.2" WIDTH .9", DEPTH .017", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .046"). (AREA 2 LENGTH 1.2", WIDTH .9", DEPTH .013" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .050').

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO BS 640-660 LBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1",DEPTH .023" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .040". FLOOR SUPPORT REPLACED IAW DWG 143N5370.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO BS 640-660, RBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .037" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .026". FLOOR SUPPORT REPLACED IAW DWG 143N5370.

Part: DOUBLER — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

NR 2 PYLON ACCESS PANEL 443LL CUT OUT SKIN DOUBLER HAS CORROSION LENGTH 2.5", WIDTH 1.1", DEPTH .065", ORIGINAL MATERIAL THICKNESS .090", REMAINING MATERIAL THICKNESS .065".

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1390-1410, RBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .014" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .049". SUPPORT REPLACED IAW DWG 146N5417. REF NRC HFL5880.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1360-1380, LBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5, WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERILA THICKNESS .025". REPLACED FLOOR SUPPORT IAW DWG 146N5417.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1460-1480, LBL 10.45" FLOOR SUPPORT HAS CORROSION ON AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH .5", DEPTH .038" ORIGINAL THICKNESS .063", REMAINING THICKNESS .025". SUPPORT, REPLACED IAW DWG 146N5447. REF NRC HFL5781.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1360-1380 RBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT AREAS, LENGTH 1.5", WIDTH 1", DEPTH .035", ORIGINAL MATERIAL THICKNESS .063", REMAINING THICKNESS .028". SUPPORT REPLACED FROM STATION 1340-1445 IAW DWG 146N5417.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1350-1380, RBL 16.1", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5",WIDTH 1", DEPTH .021", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .042". FLOOR SUPPORT REPLACED5 IAW DWG 146N5417.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1460-1500, RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT AREAS, LENGTH 1.5, WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". SUPPORT REPLACED FROM STATION 1450-1500 IAW DWG 146N5447.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1450-1490, RBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1" DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". REPAIRED IAW SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1460-1490, LBL 70. 55, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5",WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". FLOOR SUPPORT REPAIRED IAW SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1450-1500 RBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1" DEPTH .038" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". FLOOR SUPPORT, REPLACED IAW DWG 146N5447.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1380-1400, RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", MATERIAL THICKNESS REMAINING .025". REPLACED SUPPORT FROM STATION 1340-1445 IAW DWG 146N5417.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

AFT CARGO BS 1450-1500 RBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .038" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". SUPPORT REPLACED IAW DWG 146N5447.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

FORWARD CARGO DOOR CUT OUT BS 560-620 LOWER SILL HAS CORROSION IN NUT PLATE AREA. LENGTH 3.2", WIDTH 1", DEPTH .042". ORIGINAL MATERIAL THICKNESS .300", REMAINING MATERIAL THICKNESS .258".

Part: NOSE COWL — CORRODED (ZONE 400) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

NR 1 ENGINE NOSE COWL 11 O'CLOCK POSITION AREA INNER SANDWICH PANEL FOUND CORROSION. REF NRC HFL0717, COWL REPLACED. GENERATED FROM TASK CARD 71-802-50-01.

Part: BLADES — DEBONDED (NR 1 ENGINE) · airframe 67,065 hrs · 20,179 cycles

NR 1 ENGINE, NR 14 FAN BLADE FOUND TAP DISPLAY MORE THAN 600 DB AT SEC "C" OUT OF LIMITS IAW SB RB211-72-9660. GENERATED FROM TASK CARD 72-136-01-01.

Part: FITTING — CHAFED (ZONE 400) · airframe 67,065 hrs · 20,179 cycles

NR 1 PYLON MID-BULKHEAD RT FITTING, CHAFING, LENGTH 3", WIDTH 1" DEPTH .095", ORIGINAL MATERIAL THICKNESS .388", REMAINING MATERIAL THICKNESS .293". MFG FOUND CONDITION ACCEPTABLE AS IS.

Part: NOSE COWL — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

NR 1 ENGINE NOSE COWL FOUR O'CLOCK ARE INNER SANDWICH PANEL FOUND CORRODED. NOSE COWL REPLACED.

Part: WEB — CRACKED (ZONE 200) · airframe 67,065 hrs · 20,179 cycles

MAIN DECK BS 1660-1680, RBL 3 FLOOR WEB CRACKED ON FORWARD UPPER CORNER. CRACK LENGTH 1.2". REPLACED WEB, IAW DWG 146N5190.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

MAIN DECK BS 365-440 RBL 40", SEAT TRACK CORRODED, LENGTH = 4.1", WIDTH = .7", DEPTH = .098", ORIGINAL THICKNESS .225" REMAINING THICKNESS = .127". SEAT TRACK, REPLACED FROM BS 365-440 IAW DWG 141N5131.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 67,065 hrs · 20,179 cycles

FORWARD LOWER BODY FAIRING SUPPORT FRAME STA 900. LBL 4 ATTACH CLIP CRACKED, REPLACED IAW DWG 149N7130.

Part: WEB — CRACKED (ZONE 200) · airframe 67,065 hrs · 20,179 cycles

MAIN DECK BS 400-420 RBL 45" FLOOR SUPPORT INTERCOSTAL WEB, TWO LOCATIONS, CRACKED. CRACK LENGTH .5 INCHES ON AFT UPPER CORNER OF WEB. REPLACED WEB IAW DWG 141N5150.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

MAIN DECK BS 1680-1720 DECK PLATE HAS FIVE LOCATIONS OF HEAVY CORROSION, LENGTH = 50", WIDTH = 4", DEPTH= .035" ORIGINAL THICKNESS = .071". DECK PLATE, REPLACED FROM BS 1680-1720 LBL 58" - RBL 58".

Part: DOUBLER — CORRODED (BS 1645) · corrosion level 2 · airframe 67,065 hrs · 20,179 cycles

BS 1645, STRINGER 29L-29R SKIN DOUBLER HAS CORROSION. CORROSION AREA LENGTH .3", WIDTH .2", DEPTH .035", ORIGINAL THICKNESS .061". SKIN DOUBLER, REPLACED IAW DWG 146N3600.

Part: AIR DUCT — CRACKED (ZONE 100) · airframe 67,005 hrs · 20,147 cycles

LOST PRESSURIZATION- REGAINED AT 10,000 FEET. FOUND AIR DUCT CRACKED.

Part: WEDGE — DELAMINATED (NR 2 SLAT) · airframe 66,660 hrs · 19,936 cycles

NR 2 SLAT T/E WEDGE DELAMINATED ON AFT EDGE 28" FROM INBD EDGE AREA 1.1250" X 5.5". REF AD 91-22-51, SB 757-57-0066.

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 66,660 hrs · 19,936 cycles

NR 4 SLAT T/E WEDGE AFT EDGE DELAMINATED 30.5 FROM INBD END AREA .75 X 2.8750. REF AD 91-22-51, SB 757-57-0066.

Part: WEDGE — DELAMINATED (NR 3 SLAT) · airframe 66,658 hrs · 19,936 cycles

NR 3 SLAT T/E WEDGE DELAMINATED 30.5" FROM INBD END AT AFT EDGE AREA .8750" X 6". REF AD 91-22-51, SB 757-57-0066.

Part: WEDGE — DELAMINATED (NR 7 SLAT) · airframe 66,660 hrs · 19,936 cycles

NR 7 SLAT T/E WEDGE AFT EDGE DELAMINATION 33.75" FROM OTBD END AREA 2.1875" X 1.5". REF AD 91-22-51, SB 757-57-0066.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 66,606 hrs · 19,906 cycles

DURING CLIMB OUT AT 600 FT, NR 1 COMPRESSOR STALL.