NEW PACIFIC AIRLINES, INC.

Part: BATTERY PACK — INOPERATIVE (ZONE 200)

FWD GALLEY EMERGENCY LIGHT INOP.

Part: STOP FITTING — GOUGED (ZONE 200)

L4 DOOR FWD FRAME UPPER STOP FITTING IS GOUGED.

Part: SLEEVE — DENTED (THRUST REVERSER)

NR 2 ENGINE INBD THRUST REVERSER SLEEVE HAS A DENT 18 INCHES FROM TOP EDGE AND 15 INCHES FROM FWD EDGE.

Part: HEAT SHIELD — CRACKED (ZONE 700)

LEFT MLG BODY DOOR OUTER SURFACE HEAT SHIELD COVER IS CRACKED AND DELAMINATED.

Part: APU — OIL CONSUMPTION (ZONE 100) · airframe 82,511 hrs · 27,887 cycles

HIGH OIL CONSUMPTION AUTO SHUTDOWN ACTIVATED

Part: SIGN — NO TEST (ZONE 200)

R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC, AND EXIT SIGN INOPERATIVE, NO TEST.

Part: SKIN — DEBONDED (ZONE 300)

RIGHT UPPER SURFACE SKIN PATCH DE-BONDED.

Part: SKIN — DENTED (ZONE 600 SLAT)

RIGHT WING NR 6 SLAT TRAILING EDGE UPPER SKIN.

Part: SIGN — INOPERATIVE (ZONE 800)

L3 DOOR EXIT IND SIGN INOPERATIVE.

Part: SIGN — INOPERATIVE (ZONE 200)

AFT GALLLEY RIGHT SIDE EMERGENCY EXIT SIGN INOPERATIVE, WON'T TURN ON.

Part: HYDRAULIC LINE — GOUGED (ZONE 400)

LEFT NACELLE REVERSE FLOW CHECK CONTROL LINE FOUND GOUGED.

Part: ACCESS PANEL — DELAMINATED (ZONE 600)

RIGHT UPPER WING ACCESS PANEL 611KT FOUND DELAMINATED.

Part: SKIN — DENTED (ZONE 200)

DENT ON FUSELAGE SKIN STA 846 BETWEEN S-4L AND S-5L.

Part: SKIN — DAMAGED (ZONE 600)

RIGHT WINGTIP HAS LIGHTING STRIKE.

Part: FAIRING — DAMAGED (ZONE 600)

EVIDENCE OF DAMAGE AT EDGE OF CANOE PANEL 672HB.

Part: SKIN — DENTED (ZONE 100)

DENT ON PREVIOUS BLEND ON FUSELAGE SKIN AT STA 481 BETWEEN STR 27L-28-L.

Part: SKIN — DENTED (ZONE 300)

VERTICAL STABILIZER LH LOWER SIDE OF RUDDER HAS DENT

Part: SKIN — DENTED (ZONE 100)

DENT ON FUSELAGE SKIN AT STA 531 BETWEEN STR 28L AND 28R

Part: HINGE — DAMAGED (ZONE 600)

LH ENG OB LOWER BLOCKER FLAP #6 FROM 12 OCLOCK POSITION LOWER HINGE ATTACHEMENT PLATE HAS MISSING PIECE

Part: SKIN — DENTED (ZONE 100)

DENT ON FUSELAGE SKIN STA 1697 BETWEEN S-18L AND S-19L.

Part: BATTERY PACK — NO TEST (ZONE 200)

R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC INOP LIGHT ALONG WITH EXIT SIGN.

Part: SWITCH — BROKEN (ZONE 200)

DURING INSTALLATING AFT 3 LH DOOR LINNERS FJOUND SLIDE LIGHT INDICATIO SWITCH BROKEN

Part: FUSE — FAILED (ZONE 200) · airframe 81,956 hrs · 27,923 cycles

AFT GALLEY R/H SIDE EMERGENCY EXIT MAKER INOP

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 81,956 hrs · 27,923 cycles

EMERGENCY MARKER AT R3 DOOR INOPERATIVE.

Part: LIGHT — BROKEN (ZONE 200) · airframe 81,956 hrs · 27,923 cycles

DURING INSTALLING AFT 4 R/H DOOR LINERS FOUND SLIDE LIGHT INDICATOR SWITCH CONNECTOR BROKEN

Part: PANEL — DELAMINATED (ZONE 300) · airframe 80,893 hrs · 27,304 cycles

DURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 0004399709 IAW SRM 51-40-08, B757-200SRM 51-40-05, TREATED AND PRIMED HOLES FOR THE FASTENERS AND SURROUNDING EDGES ONPANEL 321CL IAW B757-200 SRM 51-20-01, OK TO INSTALL PANEL 321CLPN: 175N2001U4 SN: 0004399709

Part: PANEL — DELAMINATED (ZONE 300) · airframe 80,893 hrs · 27,304 cycles

DURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 0004399709 IAW B757-200 SRM 51-40-08, B757-200SRM 51-40-05, TREATED AND PRIMED HOLES FOR THE FASTENERS AND SURROUNDING EDGES ONPANEL 321CL IAW B757-200 SRM 51-20-01, OK TO INSTALL PANEL 321CL PN: 175N2001U4 SN: 0004399709

Part: SKIN PANEL — DELAMINATED (ZONE 300) · airframe 81,936 hrs · 27,916 cycles

SKIN PANEL DELAMINATION

Part: SWITCH — FAILED (HYD PUMP) · airframe 48,172 hrs · 52,395 cycles

#2 ENG HYD PUMP CAUTION LIGHT CAME ON IN FLIGHT.

Part: BATTERY — HOT (ZONE 100) · airframe 51,090 hrs · 56,213 cycles

AUX BATT HOT WARNING LIGHT CAME ON MOMENTARILY TWICE ON INITIAL CLIMB OUT. WE FOLLOWED FLIGHT OPS READ FILE NO. 2504. TURNED AUX BATT SWITCH OFF.

Part: FMS — INOPERATIVE (NR 1) · airframe 51,076 hrs · 56,206 cycles

CAPTS FMS SCREEN WENT BLANK. UNRESPONSIVE TO ANY INPUT.

Part: DOOR SEAL — LEAKING (ZONE 800) · airframe 51,046 hrs · 56,192 cycles

LOUD SQUEAL COMING FROM THE CARGO DOOR. VERIFIED BY F/A.

Part: WHEEL — OUT OF BALANCE (ZONE 700) · airframe 48,051 hrs · 52,281 cycles

NOSE WHEEL SHIMMY ON TAKEOFF.

Part: GAUGE — INTERMITTENT (ZONE 200) · airframe 48,051 hrs · 52,281 cycles

#2 ITT GAUGE INTERMITTENTLY INOP

Part: TOILET — CLOGGED (ZONE 900) · airframe 48,051 hrs · 52,281 cycles

LAVATORY "FLUSH" INTERMITTENTLY INOP

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 80,739 hrs · 27,226 cycles

RIGHT/FWD (R1) WINDSHIELD ARCHING IN FLIGHT, THEN SHATTERED. CORRECTIVE ACTION: REPLACED R1 WINDOW IAW B757-200 AMM 56-11-01, OPS CHECKED GOOD.

Part: SKIN PANEL — CRACKED (ZONE 200) · airframe 82,227 hrs · 27,734 cycles

WHILE PERFORMING INSPECTIONS PER AD 2017-20-05, PARA (G), BOEING SB 757- A CRACK MEASURING 1.2" IN LENGTH WAS FOUND ON FUSELAGE SKIN PANEL P/N 141N3312-7 AT THE S-4R LAP SEAM BETWEEN BS 418 AND 439. DAMAGE WAS REPAIRED IAW BOEING MESSAGES C04-C04-25-0006-01C THROUGH -10B, 8100-9 DTD. 02/20/2025, REF. ID 202502150036-0004.

Part: TORQUE SENSOR — MALFUNCTIONED (ZONE 100) · airframe 46,021 hrs · 50,272 cycles

FLAP DRIVE CAUTION LIGHT ILLUMINATED AFTER TAKEOFF W/FLAPS SELECTED 5 DEGREES.

Part: SWITCH — FAILED (ZONE 200) · airframe 82,227 hrs · 27,734 cycles

DURING A3 CHECK THE L4 DOOR OVERHEAD EMERGENCY LIGHT SWITCH DID WAS FOUND NOT TO WORK PER BOEING TASK CARD B757-LUMP-33-001-00-0. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHTS TEST SWITCH AT L4 DOOR PER B757 AMM 25-21-06-004-103, AMM 25-21-06-404-086. OPS CHECK GOOD PER B757 AMM 33-51-00-715-003.

Part: BUSHING — MISALIGNED (ZONE 700) · airframe 50,928 hrs · 56,118 cycles

LEFT MAIN GEAR DOOR HANGING DOWN 1 INCH IN CRUISE FLIGHT. F/A SAID THE DOOR CAME COMPLETELY UP DURING DESCENT.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 47,959 hrs · 52,193 cycles

CENTER AISLE MAIN ENTRANCE DOOR CEILING EMERGENCY EXIT SIGN INOP.

Part: WIRE HARNESS — INOPERATIVE (ZONE 200) · airframe 58,327 hrs · 64,572 cycles

"ALT GEAR IND FAIL" ANNUNCIATOR CAME ON IN FLIGHT. RIGHT MAIN ALT LIGHT WAS INOP.

Part: ELEC CONNECTOR — DIRTY (HYD PUMP) · airframe 56,046 hrs · 59,410 cycles

DISCREPANCY: #1 HYDRAULIC PUMP 'HOT CAUTION' LIGHT FLICKERING ON. CORRECTIVE ACTION: SWAPPED TO SECONDARY TEMP SENSOR ON #1 SPU AND REPLACED CANNON PLUG 2921-P1 AND OPS CHECKED GOOD IAW DASH-8-100 AMM 29-11-14.

Part: CLAMP — LOOSE (ZONE 600)

RIGHT, #3 DE-ICE BOOT DOES NOT INFLATE. DE-ICE LIGHT DOES NOT ILLUMINATE.

Part: GENERATOR — FAULTED (RIGHT) · airframe 82,080 hrs · 27,658 cycles

RIGHT GEN CONT OFF ILLUMINATED ON TAKEOFF

Part: DEICE SYSTEM — LOW PRESSURE (ZONE 300) · airframe 55,870 hrs · 59,255 cycles

DEICE BOOT FAILURE OF TAIL RHS OUTBOARD SECTION 6 RIGHT HAND SIDE - INDICATION LIGHT DOES NOT ILLUMINATE DURING OPERATION IN AUTO NOR IN MANUAL

Part: GENERATOR — WARNING LIGHT (NR 2 DC) · airframe 45,895 hrs · 50,115 cycles

#2 DC GEN CAUTION LIGHT ILLUMINATED. RESET FAILED.

Part: DEICE SYSTEM — LOW PRESSURE (ZONE 400) · airframe 55,811 hrs · 59,204 cycles

#1 ENGINE INTAKE DEICE INOP

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 80,451 hrs · 27,028 cycles

WEATHER RADAR FAILED IN FLIGHT IN BOTH AUTO AND MANUAL

Part: BATTERY PACK — WEAK (ZONE 200) · airframe 80,450 hrs · 27,027 cycles

SEVERAL EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN SWITCHED ON