N567CA

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,184 hrs · 25,377 cycles

EMERGENCY LIGHTING BATTERY PACK M10799 WILL NOT CHARGE, REF LP 43425-2. REMOVED AND REPLACED BATTERY PACK, AS PER B757 AMM 33-51-07.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,184 hrs · 25,377 cycles

ENTRY DOOR "L-1" EMERGENCY EXIT SIGN INOPERABLE, REF. LP 43423-2. REMOVED AND REPLACED THE BATTERY PACK AT BS 711, EQUIPMENT NR M10799, PER B757 AMM 33-51-07.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,000 hrs · 25,328 cycles

LT EMERGENCY EXIT HATCH OVER-HEAD EMERGENCY LIGHT INOPERABLE. CHARGED BATTERY PACK, PERFORMED OPERATIONAL CHECK OF LIGHTS. OPERATIONS CHECK NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 73,784 hrs · 25,029 cycles

RIGHT OVERWING EXIT SIGN COVER LOOSE. - RESECURED COVER PER AIRCRAFT MAINTENANCE MANUAL 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,535 hrs · 24,966 cycles

AFT CARGO DOOR EMERGENCY LIGHT INOPERATIVE. - REMOVED AND REPLACED LAMP PER B757 AIRCRAFT MAINTENANCE MANUAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,673 hrs · 25,003 cycles

NUMEROUS EMERGENCY EXIT PATH LIGHTING BULBS INOPERATIVE OR DIM. - REMOVED AND REPLACED LAMPS PER B757 AIRCRAFT MAINTENANCE MANUAL 33-51-11. OPERATIONAL CHECKS NORMAL.

Part: LINER — CORRODED (LT ENGINE) · airframe 73,535 hrs · 24,966 cycles

LEFT ENGINE HAS CORROSION DAMAGE AT 6 O'CLOCK POSITION UNDER LOW PRESSURE COMPRESSOR ROTOR PATH LINER - REMOVED AND REPLACED ENGINE PER AIRCRAFT MAINTENANCE MANUAL 71-00-02.

Part: LINER — CORRODED (RT ENGINE) · airframe 73,535 hrs · 24,966 cycles

RIGHT ENGINE HAS CORROSION DAMAGE AT 6 O'CLOCK POSITION UNDER LOW PRESSURE COMPRESSOR ROTOR PATH LINER - REMOVED AND REPLACED ENGINE PER AIRCRAFT MAINTENANCE MANUAL 71-00-02.

Part: DOUBLER — CORRODED (RT NACELLE) · corrosion level 2 · airframe 73,535 hrs · 24,966 cycles

CORROSION ON RIGHT ENGINE PYLON, INBOARD SIDE INTERIOR AT APPROXIMATELY POWERPLANT WATERLINE 140 POWERPPLANT STATION 152 TO 166, BEYOND ALLOWABLE LIMITS - ACCOMPLISHED CORROSION BLEND OUT REPAIR TO RIGHT ENGINE PYLON SKIN PER BOEING SERVICE REQUESTION SR 3-4547026910 INSTRUCTIONS.

Part: SKIN — DENTED (BS 580) · airframe 73,535 hrs · 24,966 cycles

SKIN DENT WITH CREASE, AT BODY STATION 580, BETWEEN STRINGERS 26R AND 27R, JUST BELOW THE FORWARD CARGO DOOR THRESHOLD - ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST ID # 3-4540838648.

Part: SKIN — DENTED (BS 580) · airframe 73,535 hrs · 24,966 cycles

DENT IN SKIN BELOW FORWARD CARGO DOOR CUTOUT AT BODY STATION 580, BETWEEN STRINGERS 28R AND 29R - ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST ID # 3-4540838648.

Part: SKIN — CORRODED (LT NACELLE) · corrosion level 2 · airframe 73,535 hrs · 24,966 cycles

CORROSION ON LEFT ENGINE PYLON INBOARD SIDE SKIN, ON INTERIOR, AT APPROXIMATELY POWERPLANT WATER LINE 140.94 POWERPLANT STATION 144.425 TO 170 - ACCOMPLISHED CORROSION BLEND OUT REPAIR TO LEFT ENGINE PYLON SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST SR 3-4547117692 INSTRUCTIONS.

Part: FRAME — CORRODED (BS 263 BULKHEAD) · corrosion level 2 · airframe 73,535 hrs · 24,966 cycles

CORROSION BEYOND LIMITS, COMMON TO THE FUSELAGE BODY STATION 263 NOSE WHEEL WELL BULKHEAD OUTBOARD CHORD VERTICAL FLANGE, BETWEEN LEFT BUTT LINE 10.6 TO LEFT BUTT LINE 18.8 - ACCOMPLISHED MAJOR REPAIR TO BLEND DAMAGE IN ACCORDANCE WITH BOEING SERVICE REQUEST ID NUMBER SR 3-4542883597.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 73,535 hrs · 24,966 cycles

STOWBIN BULLNOSE LIGHT @ 35DEF IS DISBONDED - REBONDED STOWBIN BULLNOSE LIGHT 35DEF IAW STANDARD OVERHAUL PROCEDURES MANUAL 20-50-92

Part: SKIN — DENTED (BS 578) · airframe 73,535 hrs · 24,966 cycles

DENT IN SKIN BELOW FORWARD CARGO DOOR CUTOUT, AT BODY STATION 578, BETWEEN STRINGERS 26R AND 27R - ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST ID # 3-4540838648.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,535 hrs · 24,966 cycles

WHITE EMERGENCY PATH LIGHTS OUT AT SEATS 3DEF, 7DEF (WHITE ONLY INOP), 11DEF, 14DEF, 19DEF, 24DEF, 29DEF, AND 31DEF - RELAMPED EMERGENCY PATH LIGHTS AT SEATS 3DEF, 7DEF, 11DEF, 14DEF, 19DEF, 24DEF, 29DEF, AND 31DEF PER AIRCRAFT MAINTENANCE MANUAL 33-51-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,535 hrs · 24,966 cycles

EXTERNAL EMERGENCY EXIT LIGHT AT L3 DOOR INOPERATIVE - RELAMPED EXTERNAL EMERGENCY LIGHT AT L3 DOOR PER AIRCRAFT MAINTENANCE MANUAL 33-51-06.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 73,510 hrs · 24,955 cycles

EMERGENCY EXIT LENS MISSING AT 16-17 RIGHT HAND. OKAY TO DEFER PER NATIONAL AIRLINES NEF MANUAL 25-20-01-N12, DISCREPANCY TRANSFERRED TO DEFERRED MAINTENANCE ITEM CONTROL NUMBER 191116-733. CLEAR LIGHT LENS MISSING ONLY.

Part: LIGHT — INTERMITTENT (ZONE 200) · airframe 73,090 hrs · 24,861 cycles

LEFT NUMBER 2 DOOR SLIDE ARMED LIGHT INTERMITTENT - REMOVED AND REPLACED SLIDE ARMED LIGHT BULBS PER AIRCRAFT MAINTENANCE MANUAL 25-66-00. OPERATION NORMAL.

Part: LENS — MISSING (CABIN) · airframe 73,028 hrs · 24,847 cycles

SEAT ROW 22 CLEAR EMERGENCY EGRESS LIGHT LENS MISSING. REPLACED LENS PER AIRCRAFT MAINTENANCE MANUAL 33-51-11.

Part: LENS — MISSING (CABIN) · airframe 73,028 hrs · 24,847 cycles

SEAT ROW 15D RED EMERGENCY EGRESS LIGHT LENS MISSING. REPLACED LENS PER AIRCRAFT MAINTENANCE MANUAL 33-51-11.

Part: ACM — SEIZED · airframe 72,886 hrs · 24,796 cycles

DURING CRUISE FLIGHT, LEFT ENGINE BLEED OFF LIGHT ILLUMINATED. UNABLE TO MAINTAIN CABIN PRESSURIZATION. - TROUBLESHOT LEFT ENGINE BLEED AIR SUPPLY SYSTEM IN ACCORDANCE WITH FAULT ISOLATION MANUAL 36-10 FAULT TREE 813. LEFT ENGINE BLEED AIR SYSTEM CHECKED NORMAL. WHILE PERFORMING TEST OF CABIN PRESSURIZATION SUPPLY SYSTEM, FOUND THE RIGHT AIR CONDITIONING SYSTEM AIR CYCLE MACHINE DEFECTIVE. REPLACED THE AIR CYCLE MACHINE PER AIRCRAFT MAINTENANCE MANUAL 21-51-03. PERFORMED CABIN PRESSURIZATION SYSTEM TEST PER AIRCRAFT MAINTENANCE MANUAL 21-31-00. SYSTEM TESTED NORMAL. PERFORMED CABIN PRESSURIZATION CONTROL SYSTEM TEST PER AIRCRAFT MAINTENANCE MANUAL 21-31-02. SYSTEM TESTED NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 72,852 hrs · 24,783 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 10 - REPAIRED PINS/WIRES IN ACCORDANCE WITH STANDARD WIRING PRACTICES MANUAL 20-10-13.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,852 hrs · 24,783 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LEFT HAND AFT OVERWING EXIT DOOR - RELAMPED PER AIRCRAFT MAINTENANCE MANUAL 33-51-00, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,852 hrs · 24,783 cycles

EMERGENCY EGRESS LIGHT INOPERATIVE AT SEAT ROW 19 - RELAMPED PER AIRCRAFT MAINTENANCE MANUAL 33-51-11, OPS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 72,852 hrs · 24,783 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 23 - REPAIRED WIRING IN ACCORDANCE WITH STANDARD WIRING PRACTICES MANUAL 20-10-13.

Part: LENS — MISSING (CABIN) · airframe 72,734 hrs · 24,747 cycles

MID GALLEY EMERGENCY EVACUATION ALARM LENS COVER MISSING - DEFERRED PER MINIMUM EQUIPMENT LIST 25-63-02-01 - A SUPPLEMENT SERVICE DIFFICULTY REPORT WILL BE FILED UPON REPAIR. REPLACED LENS PER MAINTENANCE MANUAL 25-63-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,622 hrs · 24,719 cycles

EXTERIOR EMERGENCY EXIT LIGHT FOR MAIN ENTRY DOOR 4 LEFT (SLIDE LIGHT) INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 33-51-06. PERFORMED SATISFACTORY OPERATIONAL TEST OF EXIT LIGHT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,103 hrs · 24,574 cycles

OVERHEAD BIN EMERGENCY LIGHTS AT SEAT ROWS 19D, 21C, AND 24D ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PER AIRCRAFT MAINTENANCE MANUAL 33-51-07.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,103 hrs · 24,574 cycles

EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR PER AIRCRAFT MAINTENANCE MANUAL 33-51-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,103 hrs · 24,574 cycles

CEILING EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 31C PER AIRCRAFT MAINTENANCE MANUAL 33-51-05.

Part: LENS — MISSING (EXIT SIGN) · airframe 71,807 hrs · 24,487 cycles

RIGHT-HAND AFT OVER WING EMERGENCY HATCH EXIT SIGN MISSING LENS. INSTALLED LENS PER AIRCRAFT MAINTENANCE MANUAL CHAPTER 20-00-00.

Part: LENS — CRACKED (EXIT SIGN) · airframe 71,530 hrs · 24,414 cycles

DURING CABIN INSPECTION FOUND EMERGENCY EXIT SIGN ABOVE NUMBER 2 LEFT DOOR CRACKED. - DEFERRED PER MEL/NON-ESSENTIAL FURNISHINGS 25-20-01-N12. SUPPLEMENTAL SDR WILL BE FILED UPON REPAIR.

Part: CYLINDER — LOW PRESSURE (RT OVRWG SLIDE) · airframe 71,160 hrs · 24,291 cycles

DURING DAILY SERVICE CHECK INSPECTION, WHILE ACCOMPLISHING SQUIB TEST 2, FOUND RIGHT EMERGENCY ESCAPE LIGHT NOT TESTING. - PERFORMED TROUBLESHOOTING PER B757 FAULT ISOLATION MANUAL 25-65 FAULT TREE 803. FOUND RIGHT OVERWING ESCAPE SLIDE PRESSURE CYLINDER WITH LOW PRESSURE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY ESCAPE SLIDE PRESSURE CYLINDER ASSEMBLY IN ACCORDANCE WITH BOEING 757 AIRCRAFT MAINTENANCE MANUAL CHAPTER 25-65-02.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 71,123 hrs · 24,278 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY AISLE LIGHT AT BULLNOSE OF OVERHEAD BIN 6A INOPERATIVE. REMOVED AND REPLACED AISLE LIGHT LAMP AT BIN 6A OVERHEAD BULLNOSE IN ACCORDANCE WITH B757 AMM 33-51-05. OPERATIONAL CHECK OF LIGHT FOUND SATISFACTORY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,799 hrs · 24,182 cycles

SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 29. REPLACED THE SEAT MOUNTED EMERGENCY LIGHT IAW AMM 33-53-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,799 hrs · 24,182 cycles

SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 14. REPLACED THE LAMPS IAW AMM 33-53-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,799 hrs · 24,182 cycles

SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 15. REPLACED THE SEAT MOUNTED EMERGENCY LIGHT IAW AMM 33-53-11.

Part: LIGHT — INOPERATIVE (SEAT ROW 3) · airframe 70,799 hrs · 24,182 cycles

SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE, SEAT ROW 3. REPLACED THE EMERGENCY LIGHT IAW AMM 33-53-11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,617 hrs · 24,141 cycles

FLOOR LEVEL ESCAPE PATH LIGHTING AT SEAT ROWS 8 THROUGH 15 INOPERATIVE. CHARGED BATTERY PACKS PER AMM33-51-07 AND 24-22-00, OPERATIONAL CHECK FOUND SATISFACTORY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,617 hrs · 24,141 cycles

EMERGENCY EXIT LIGHTS DOOR 2 LEFT AND 2 RIGHT, LOWER EXIT LIGHTS AT EACH DOOR INOPERATIVE. CHARGED EMERGENCY EXIT LIGHT BATTERY PACKS PER AMM 33-51-07 AND 24-22-00, OPERATIONAL CHECK FOUND SATISFACTORY.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 70,588 hrs · 24,137 cycles

R2 DOOR ARMED LIGHT INOPERATIVE. RELAMPED R2 DOOR ARMED LIGHT, REFERENCE WIRING DIAGRAM 25-66-11. LIGHT OPERATES NORMAL.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 70,220 hrs · 24,063 cycles

DURING INSPECTION, FOUND THE LEFT OUTBOARD FLAP UPPER SURFACE WITH FIVE GOUGES IN THE SKIN, 32, & 38 INCHES FROM INBOARD END, AND 25 INCHES FROM TRAILING EDGE. ACCOMPLISHED INTERIM POTTED FILLER REPAIR OF LEFT OUTBOARD FLAP UPPER SKIN PANEL IAW EO 57-18111-1, REVISION IR.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 70,217 hrs · 24,063 cycles

FORWARD CARGO FLOOR PANEL #121AF HAS A PUNCTURE 1 X 1.2 INCHES. REPAIRED THE FLOOR PANEL IAW SRM 51-70-13-06-0, GENERAL FIGURE 1, DETAIL I, TABLE I.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 70,217 hrs · 24,063 cycles

LEFT WING UPPER SURFACE LWS 585, STRINGER 4L HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW MESSAGE MUA-MUA-8-0012-05B.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 70,188 hrs · 24,056 cycles

DURING ACCOMPLISHMENT OF SCHEDULED MAINTENANCE TASK FOUND EMERGENCY ISLE LIGHTS AND CEILING EMERGENCY EXIT SIGN LIGHTS IN ZONE WOULD NOT TEST. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK IAW AMM 33-51-07. EMERGENCY EXIT LIGHTS OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,887 hrs · 23,960 cycles

FORWARD GALLEY, CENTER, CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT POWER SUPPLY ASSEMBLY IAW AMM 33-51-07. OPERATIONAL CHECKED SATISFACTORY.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 69,477 hrs · 23,843 cycles

MAIN PASSENGER CABIN AT ROW 7 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWPM 20-61-00. LIGHT OPS CHECKED GOOD AMM 33-51-00

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 69,477 hrs · 23,843 cycles

MAIN CABIN AT ROW 10 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED THE ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWP 20-61-00. LIGHT OPS CHECKED GOOD IAW AMM 51-00.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 69,477 hrs · 23,843 cycles

MAIN CABIN AT ROW 3 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWP 20-61-00. LIGHT OPS CHECKED GOOD IAW AMM 33-51-00

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 69,477 hrs · 23,843 cycles

MAIN CABIN AT ROW 30 EMERGENCY AISLE LIGHT INOPERATIVE. RESEATED ENRGENCY LIGHT CONNECTOR AT SEAT ROW 3 IAW SWPM 20-61-00. THE LIGHT OPS CHECKED GOOD IAW AMM 33-51-00

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,351 hrs · 23,796 cycles

EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 34 DOES NOT ILLUMINATE. RELAMPED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 34 IN ACCORDANCE WITH AMM 33-51-11 LIGHT TESTS GOOD.

Part: LAMP — MISSING (EMERGENCY LIGHTS) · airframe 68,890 hrs · 23,627 cycles

EGRESS LIGHT LENS MISSING AT SEATS 18D AND 34D - 18D AND 34D. LAMPS MISSING AT SEATS 5D, 18D, AND 34D - SEATS 5D, 18D, AND 34D EGRESS LIGHT LAMPS REPLACED.

Part: TRANSCOWL — DAMAGED (LT ENGINE) · airframe 68,864 hrs · 23,612 cycles

LT ENGINE INBOARD C-DUCT HAS 1.5" X 3" DAMAGE TO CARBON FIBER ON UPPER EDGE, AT THE CENTER HINGE AREA. ACCOMPLISHED ERO 5430ERO2238 TEMPORARY REPAIR.

Part: SWITCH — DIRTY (EMERGENCY LIGHT) · airframe 68,843 hrs · 23,601 cycles

L1 DOOR EXIT LIGHT INOPERATIVE. TROUBLESHOT SYSTEM IAW WIRING DIAGRAIM MANUAL 33-51-12. CLEANED AND SECURED EMERGENCY LIGHT SWITCH, ON P-5 PANEL. SYSTEM OPS CHECKED SATISFACTORY IAW AMM 33-51-00.

Part: CONTROL MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,772 hrs · 23,578 cycles

SEVERAL AREAS OF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS AND CONTROL MODULES IAW MM 33-51-07.

Part: CHANNEL — CORRODED (BS 355) · corrosion level 2 · airframe 68,772 hrs · 23,578 cycles

BS 355, STRINGER 17R, HAT CHANNEL HAS UPPER SURFACE CORROSION. REMOVED AND REPLACED THE HAT CHANNEL IAW SRM 51-40-02. DRAWING 141N8422.

Part: TEE FITTING — CRACKED (BS 1720) · corrosion level 2 · airframe 68,772 hrs · 23,578 cycles

RIGHT SHEAR PANEL AFT CORNER CRACKED AND CORRODED AT BS 1720 AFT BULKHEAD IN MAIN CABIN. REMOVED AND REPLACED THE TEE FITTING ANGLE IAW SRM 51-40-04. DRAWING 146N8722.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,772 hrs · 23,578 cycles

LEFT MAIN LANDING GEAR WHEEL WELL AFT INBOARD CORNER SUPPORT FROM AFT BULKHEAD TO CORNER BULKHEAD CORRODED. REMOVED AND REPLACED CORNER SUPPORT BARCKET IAW SRM 51-40-02. DRAWING 144N8161.

Part: STRUCTURE — CORRODED (BS 1094) · corrosion level 2 · airframe 68,772 hrs · 23,578 cycles

LEFT MAIN LANDING GEAR WHEEL WELL FORWARD DOOR CUTOUT, OUTBOARD SIDE HAS CORROSION. REPAIRED WING TO BODY FAIRING OUTER CHORD AT BS 1094 IAW ENGINEERING ORDER FAS EA 16259.

Part: SUPPORT CHANNEL — CRACKED (ZONE 100) · airframe 68,772 hrs · 23,578 cycles

RIGHT MAIN LANDING GEAR FORWARD OUTBOARD LOWER DOOR CUTOUT STRUCTURE (WING TO BODY FAIRING) CRACKED UNDER PROXIMITY SENSOR. REMOVED AND REPLACED SUPPORT CHANNEL IN ACCORDANCE WITH B757 SRM 51-40-08

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 68,496 hrs · 23,491 cycles

DURING ACCOMPLISHMENT OF TASK CARD 33-001-00-01, FOUND L1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY, M731 IAW AMM 33-51-07. OPS CHECK GOOD.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR) · airframe 68,372 hrs · 23,450 cycles

WHILE ACCOMPLISHING TASK CARD 52-004-00-05, FOUND R2 DOOR EMERGENCY POWER ASSIST RESERVOIR WITH LOW PRESSURE. R & R RT NR 2 DOOR POWER ASSIST RESERVOIR IAW AMM 52-11-30.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,447 hrs · 23,170 cycles

BATTERY CHARGER OVER ROW 28ABC LOW VOLTAGE. R & R EMERGENCY LIGHT BATTERY ASSY-POWER SUPPLY ASSY IAW AMM 33-51-07. OPS TESTED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,447 hrs · 23,170 cycles

BATTERY POWER SUPPLY OVER THE L-2 DOOR LOW VOLTAGE. R & R EMERGENCY LIGHT BATTERY ASSY-POWER SUPPLY ASSY IAW AMM 33-51-07. OPS TEST GOOD.

Part: BATTERY PACK — DEPLETED (EMERGENCY LIGHTS) · airframe 67,447 hrs · 23,170 cycles

L-2 DOOR EMERGENCY LIGHT BATTERY ASSEMBLY VOLTAGE LOW. R & R EMERGENCY LIGHT BATTERY ASSEMBLY IAW AMM 33-51-07. OPS TEST GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,447 hrs · 23,170 cycles

R2 DOOR EMERGENCY LIGHT BATTERY ASSY VOLTAGE LOW. R & R R-2 DOOR LIGHT BATTERY ASSEMBLY IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,133 hrs · 23,087 cycles

LEFT MAIN ENTRY DOOR, NR 2 EXTERIOR EMER EXIT ESCAPE LIGHT INOPERATIVE. REPLAMPED LT MAIN ENTRY DOOR NR 2 EMER ESCAPE LIGHT IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,133 hrs · 23,087 cycles

LEFT EMER EXIT DOOR NR 3 EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE. RELAMPED LT EMER EXIT DOOR NR 3 EXTERIOR ESCAPE LIGHT IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: RESERVOIR — EMPTY (PAX DOOR ASSIST) · airframe 67,092 hrs · 23,076 cycles

DURING ACCOMPLISHMENT OF TC 52-004-00-04, IT WAS NOTED THAT THE LT NR 2 MAIN ENTRANCE DOOR EMERGENCY POWER ASSIST RESERVOIR PRESSURE GAUGE READS EMPTY. R & R POWER ASSIST RESERVOIR IAW AMM 52-11-30.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,066 hrs · 23,071 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. TROUBLESHOT IAW AMM 33-51-07. FOUND BATTERY PACKS DISCHARGED. R & R THE BATTERY PACKS IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHT) · airframe 66,823 hrs · 23,027 cycles

WITH EMERGENCY LIGHT SWITCH ARMED, VARIOUS EMERGENCY LIGHTS IN THE CABIN GO ON AND OFF AT RANDOM TIMES, WITH SWITCH IN ON POSITION, ALL OVERHEAD EMERGENCY LIGHTS COME ON, BUT ONLY SOME FLOOR PATH LIGHTS WORK. R & R POWER SUPPLY ASSY IAW AMM 33-51-07. EMERGENCY LIGHTS OPERATIONALLY CHECK GOOD.

Part: WINDOW — FAILED (R1) · airframe 66,858 hrs · 23,023 cycles

F/O R-1 WINDOW SHATTERED IN FLIGHT. SHOWS SIGNS OF ARCING AND IS DEFORMED. R & R R-1 WINDOW IAW AMM 56-10-01. ALSO REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD.

Part: SUPPORT BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 66,635 hrs · 22,962 cycles

WING TO BODY FAIRING SUPPORT BRACKET LOCATED AT BS 1300 S20R IS CRACKED IN TOP CORNER. CRACK LENGTH MEASURED TO BE .750". REMOVED DAMAGE AND INSTALLED REPAIR ANGLE, FILLER IAW SRM 53-60-71, FIG. 201, REPAIR 1.

Part: FITTING — WORN (EMERGENCY EXIT) · airframe 66,635 hrs · 22,962 cycles

RIGHT AFT OVERWING EMERGENCY EXIT DOOR LWR FWD GUIDE FITTING WORN. R & R RT AFT OVERWING EMERGENCY EXIT DOOR FWD PIVOT FITTING IAW CMM 52-21-45.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,635 hrs · 22,962 cycles

CABIN SEAT EMERGENCY LIGHTS INOPERATIVE IN ZONE 4. R & R POWER SUPPLY MODULE IAW AMM 33-51-11, LIGHTS CHECKED GOOD.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

RT FUSELAGE WING TO BODY FAIRING LOWER MOUNTING BRACKET SURFACE CORROSION. REMOVED, FABRICATED AND INSTALLED OVERWING FAIRING LOWER MOUNT BRACKET IAW SRM 51-20-01, 51-30-01, FIG 3, 51-40-02 AND 51-40-05. BRACKET FABRICATED IAW DWG 149N7550RG.

Part: ATTACH BRACKET — CRACKED (L1 DOOR) · airframe 66,635 hrs · 22,962 cycles

L1 DOOR HINGE COVER ATTACH BRACKET CRACKED, BETWEEN UPPER AND LOWER HINGE DOOR. REMOVED THE ATTACH BRACKET, FABRICATED A NEW BRACKET, INSTALLED NEW BRACKET IAW SRM 51-40-02. BRACKET FABRICATED IAW DWG 141N8315.

Part: VERTICAL SUPPORT — CRACKED (LT MLG WW) · airframe 66,635 hrs · 22,962 cycles

LEFT WW AFT BULKHEAD INBD LOWER VERTICAL SUPPORT CRACKED. CRACK LENGTH 1.5". REMOVED, LOCATED & DRILLED AND INSTALLED NEW VERTICAL SUPPORT IN LT MAIN GEAR WW AFT BULKHEAD IAW SRM 51-40-02, 51-40-05 & DWG 144N2503.

Part: FLOOR SUPPORT — CORRODED (BS 1680) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

MAIN CABIN FLOOR SUPPORT UPPER SIDE CORRODED SEVERAL AREAS FROM BS 1680 RBL 54. REPAIRED IAW SRM 53-60-51, REPAIR 2 & 51-40-02.

Part: VERTICAL SUPPORT — CRACKED (ZONE 100) · airframe 66,635 hrs · 22,962 cycles

RIGHT WW AFT BULKHEAD INBD LOWER VERTICAL SUPPORT CRACKED. CRACK IS LENGTH 1.5 INCHES. REMOVED CRACKED RT W/W AFT BULKHEAD INBD LOWER VERTICAL SUPPORT AND REPLACED WITH NEW VERTICAL SUPPORT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

MAIN CABIN FLOORBEAM BS 1660, RBL 54 CORRODED AT UPPER SIDE. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-51, REPAIR 8, 51-40-05, 51-40-02 AND 51-20-01.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

FUSELAGE BODY FAIRING PANEL FRAME CORRODED AT NR 198AR. REMOVED FRAME AT FUSELAGE BODY FAIRING, FABRICATED NEW-FRAME INSTALLED NEW FRAME IAW SRM 51-40-02, DWG 149N7553, REV C, SRM 51-40-05, BAC 5602, SRM 51-20-01, AMM 51-21-01-7 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

MAIN CABIN FLOORBEAM IS CORRODED AT BS 1681, RBL 25 ON LOWER FLANGE. CUTOUT DAMAGE, FABRICATED AND INSTALL REPAIR IAW SRM 53-60-51, REPAIR 3 & 51-40-02.

Part: DECK PLATE — CORRODED (BS 1681) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

MAIN CABIN DECK PLATE AT BS 1681, RBL 12 IS CORRODED. CUTOUT DAMAGED AREAS IAW SRM 51-10-02. FABRICATED AND INSTALLED THE REPAIR AND FILLERS IAW SRM 53-60-51, REPAIR 2, 51-40-05 & 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

L4 DOOR SILL LOWER SIDE CORRODED AT DRAIN HOLES. R & R DOOR SILL IAW SRM 51-40-02.

Part: DECK PLATE — CORRODED (BS 1681) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

MAIN CABIN DECK PLATE IS CORRODED AT BS 1681, RBL 25. CUTOUT DAMAGED AREAS IAW SRM 51-10-02. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW SRM 53-60-51, REPAIR 2, 51-40-05 & 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 66,635 hrs · 22,962 cycles

MAIN CABIN FLOORBEAM, BS 1680, RBL 34 CORRODED AROUND FASTENERS HOLES LOWER AREA. CUT OUT DAMAGED AREAS IAW SRM 51-10-02. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW SRM 53-60-51, REPAIR 2, 51-40-05 & 51-40-02.

Part: SKIN — DAMAGED (NR 9) · airframe 66,635 hrs · 22,962 cycles

NR 9 SLAT HAS TWO CREASES ON LOWER SURFACE, APPROXIMATELY 18 INCHES FROM OTBD END. REPAIRED NR 9 SLAT IAW SRM 57-43-02, REPAIR 1, FIG 201.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 66,610 hrs · 22,954 cycles

RIGHT NR 1 DOOR SLIDE ARMED LIGHT INOPERATIVE. TRANSFERRED TO DMI CONTROL NR 2035 IAW MEL 25-66-04-02. FOUND GIRT BAR FWD END OUT OF POSITION. REPOSITIONED GIRT BAR & DOOR SLIDE ARMS & DISARMS OK IAW AMM 25-66-10 GIRT BAR NAD FLOOR FITTING MAINTENANCE PRACTICES.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 66,469 hrs · 22,926 cycles

DURING SLIDE SURVIVAL KIT HARNESS, L1 DOOR SLIDE BUSTLE & SLIDE FELL ON STAIR TRUCK, SLIDE DID NOT DISCHARGE. AT DEPARTURE TIME THE FLIGHT ATTENDANT INFORMED MX THAT SHE COULD NOT ARM THE L1 DOOR. TROUBLESHOOTING REVEALED THE SURVIVAL KIT ATTACHMENT LANYARD WAS FOULED IN THE GIRT BAR. AFTER THE STRAP WAS CLEARED THE RIG OF THE GIRT BAR WAS CHECKED & WHEN THE DOOR WAS CRACKED OPEN TO VERIFY PROPER ENGAGEMENT OF THE GIRT BAR, THE DOOR WAS PULLED OPEN BY GND OPERATION PERSON. THE DOOR ASSIST BOTTLE DISCHARGED. SLIDE VERIFIED IN SERVICEABLE CONDITION & REINSTALLED.

Part: GOVERNOR — FAULTY (ZONE 400) · airframe 66,297 hrs · 22,887 cycles

THRUST LEVER 01 DIFFICULT TO MOVE IN FWD & REVERSER THRUST. R & R FUEL FLOW GOVERNOR IAW AMM 73-21-01, CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,923 hrs · 22,808 cycles

MID CABIN & AFT GALLEY FLOOR PATH LIGHTING INOPERATIVE. BATTERY PACKS INOPERATIVE. R & R BATTERY PACKS IAW AMM 33-51-07.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,193 hrs · 22,624 cycles

FORWARD CABIN EMERGENCY LIGHT AT R1 DOOR AND CENTER AISLE DO NOT ILLUMINATE AFTER INITIAL POWER UP.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 65,193 hrs · 22,624 cycles

MID CABIN EMERGENCY LIGHT AT L2 DOOR DOES NOT ILLUMINATE AFTER INTIAL POWER UP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,048 hrs · 22,532 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE AT L-1 DOOR AND AFT LOWER BAGGAGE DOOR. REPLACED LAMP IAW AMM 33-51-01, TEST OK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR SLIDE) · airframe 64,869 hrs · 22,420 cycles

DURING SERVICE CHECK, FOUND R2 DOOR EVACUATION SLIDE PRESSURE LOW.

Part: SLIDE RAFT — NO TEST (R4 DOOR) · airframe 64,791 hrs · 22,380 cycles

DURING MINI-EVACUATION DEMONSTRATION, R4 DOOR SLIDE/RAFT DEPLOYED, BUT DID NOT INFLATE AUTOMATICALLY.