N492HA

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 30,940 hrs · 46,391 cycles

COCKPIT EMERGENCY LIGHT INOP. RELAMPED CP EMERGENCY LIGHTS AND INSTALLED NEW BATTERY PACK AT B5-123, OPS TEST PER AMM 33-51-03 OK.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 30,445 hrs · 45,305 cycles

LEFT ENG COMPRESSOR STALL. REMOVED ENG1 BOOSTER BLEED VALVE (BBV) PER AMM 75-32-01 5/26/24 24713. INSTALLED BOOSTER BLEED VALVE IN SERVCABLE CONDITION ON #1 ENG PER AMM 75-32-01 UP TO STEP F.2.(E). REMOVED #1 ENG SN 13438 PER HAL TASKCARD E1128-717-72-0003-REMOVAL. INSTALLED #1 ENG ESN 13430 PER TASKCARD E1128-717-72-003-INSTALL. OK FOR SVC.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 30,441 hrs · 45,295 cycles

ENG L COMP STALL ON TAKE OFF @ 1600' (ATB). PERFORMED EEC 1 BITE - FC 801105 STARTER AIR VALVE OUT OF POSITION. REPLACED #1 ENGINE START VALVE PER AMM 80-11-03. OPS CHECK & LEAK CHECK NEED TO BE ACCOMPLISHED. BORESCOPE INSP PERFORMED NO FINDINGS AMM 72-33-00-200-801. GRND RUN #1 ENG LEAK CK GOOD PERFORMED INSP OF VIGV AND VSV NO FINDINGS AMM 72-33-34-200-801, BBVA RTS TEST AMM 75-32-01-741-801 TEST PASS.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 30,435 hrs · 45,280 cycles

ATB - ENG L. COMP STALL @ APPX 1500' ON CLIMBOUT. CONDITION IMPROVED ON POWER REDUCTION. NORMAL LANDING PERFORMED. COMPLETED INSPECTION OF THE ENGINE AFTER HIGH POWER SURGE AMM 72-00-200-801 UP TO STEP 2.E. (7) -N. DAMAGE FOUND NO DAMAGE NOTED. ENG 1 ON COMPRESSOR. EWG INSPECTION. ACCOMPLISHED TEST 4 ENG 1 POWER ASSURANCE CK. HIGH POWER RUN UP TEST CK 6000. OK FOR SERVICE. PER AMM 71-00-13

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 30,209 hrs · 44,791 cycles

#5 FAN BLADE #2 ENGINE MAJOR DAMAGE. REMOVED #2 ENG BLADE SET PER AMM72-38-15. 17601 3-29-24 PERFORMED INSPECTION OF #2 ENGINE FOR FOD PER AMM 72-00-00--200-809. INSTALLLED #2 ENGINE BLADE ASSEMBLY PER AMM 72-38-15.

Part: NONE — NONE · airframe 28,162 hrs · 40,318 cycles

BOTH OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. OK FOR SVC.

Part: CABLE — INOPERATIVE · airframe 27,223 hrs · 38,208 cycles

EMER EQ - LFT MAIN CABIN DOOR EMER SLIDE ARMING CABLE INOP // REMOVED AND REPLACED 1L DOOR EMERG SLIDE ARMING CABLE. SECURE OK TO CONTINUE.

Part: ENGINE — INOPERATIVE · airframe 27,083 hrs · 37,886 cycles

CREW REPORTED THAT INBND TO OGG THEY HAD ENG1 BRG OVHT MSG, PER FCOM PROCEDURES CREW SHUT DOWN AFFECTED ENG // MX TROUBLESHOOTING, FOUND METAL FINDINGS FROM OIL FILTER & FBC STRAINER. HAL PP ENGINEERING HAS DETERMINED THAT AN ENG CHANGE IS REQUIRED. MX CURRENTLY GATHERING EQUIPMENT, SPARE ENGINE AND PARTS FOR SHIPPING TO OGG (MAUI).

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 26,329 hrs · 36,156 cycles

EMER EQ - MAIN ENTRY DOOR WILL NOT CLOSE PROPERLY -REPEAT WRITE UP // ACCOMPLISHED AMM 52-11-01/501 ADJUSTMENT TEST DOOR ,PASSENGER FORWARD ENTRY TEST OPS CK OK NO FAULTS NOTED REINSTALLED SLIDE SHUTE PER AMM 25-61-01/401

Part: LOCK — OBSTRUCTED (PAX DOOR) · airframe 26,318 hrs · 36,132 cycles

EMER EQ - MAIN ENTRY DOOR WILL NOT CLOSE PROPERLY // FOUND SAFETY WIRE ON LOCK ADJUSTMENT ARM CAUSING JAM. REMOVED AND REPLACED SAFETY. OPS CHECK OK. OK FOR SERVICE. REF AMM 52-11-01

Part: ENGINE — FAILED (RIGHT) · airframe 26,057 hrs · 35,558 cycles

ATB-RT ENGINE COMP STALL RT ENGINE OIL PRESS 0. REMOVED & REPLACED #2 ENG PER W/O 181624 REF TASK CARD E1128-717-72-003-INSTALL OPS/LEAK CHECK OK.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 25,974 hrs · 35,374 cycles

MISSING EMERGENCY LIGHT COVER AT ROW 11 RT. COVER DOES NOT HOLD ONTO ASSEMBLY. REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT ASSEMBLY AT ROW 11 RTM, PER AMM 33-51-08-400-801.

Part: FRAME — CORRODED (BS 1098) · corrosion level 2 · airframe 25,972 hrs · 35,372 cycles

492 C CHECK. CORROSION DISCOVERED ON THE STA 1098.868 FRAME TEE (PN 9971144-61) AT L-28L. THE CORROSION WAS MECHANICALLY REMOVED WITH MORE THAN 50% MATERIAL LOST IN THE VERTICAL FLANGE AND PITTING CORROSION 100% THROUGH THE AFT HORIZONTAL FLANGE. INSTALLED VERTICAL FASTENERS ONLY IN REPAIR, PER E105-492088-PERM FIGURE 2. 09/11/20 MECH 11006; INSP 4760. INSTALL REPAIR PARTS E105-492088-PERM. SEAL AREA PENDING AND PRIME AND PAINT FASTENER PENDING. EDGE SEALED AROUND REPAIRED AREA. 0 PRIME AND PAINT FASTENERS PENDING. PRIMED AND PAINT, PER SRM 51-22-01.

Part: STRUCTURE — CORRODED (BS 974) · corrosion level 2 · airframe 25,972 hrs · 35,372 cycles

492 C CHECK. SM S/C AROUND STA 974 AND LONG 30 (M). REMOVED CORROSION, PER B717SRM 51-10-04-OG-O. FOUND TO BE BEYOND LIMITS, PER SRM 53-00-090-1A 0 FIG 103 M66 SUBMITTED. PENDING INSTALLATION OF FASTENERS TREAT PRIME AND PAINT POST REPAIR. INSTALLED LOCK FASTENERS, PER B717SRM 51-41-05-OG-O. INSTALLED RIVETS, PER B717SRM 51-41-02-OG-O. TREATED PRIMED AND PAINTED AREA, PER B717 SRM 51-22-01-OG-O. BLEND OF FRAME AT STA 974 LONGERON DUE TO CORROSION (E105-492092-PERM).

Part: FORMER — CORRODED · corrosion level 2 · airframe 25,972 hrs · 35,372 cycles

492 C CHECK. CORROSION UNDERNEATH BONDING WIRE ON LEFT FILLET FORMER 4TH BACK FROM FWD (M). REMOVED CORROSION, PER SRM 51-10-04. FOUND TO BE OUT OF LIMITS. M66 SUBMITTED. CORROSION BLEND ON THE WING TO FUSELAGE FILLET FORMER AT Y=636 SURFACE CORROSION BLEND. REPAIRED PER E105-492083-PERM.

Part: DOUBLER — CRACKED (BS 1178 BULKHEAD) · airframe 25,972 hrs · 35,372 cycles

492 C CHECK, DURING ROUTINE MAINTENANCE TASKS, HWI DISCOVERED A CRACK IN THE STA 1178 BULKHEAD DOUBLER (PN 9911839-265) AND SKIN PANEL (PN 5912141-77), JUST INBOARD OF L-3L. MINOR REPAIR. E105-492092-PERM C/W DATE 09/10/20, MECH 019536. PENDING INSTALLATION OF FASTENERS TREAT PRIME AND PAINT POST REPAIR. INSTALLED HI-LOC FASTENERS, PER B717SRM 51-41-05-OG-O. INSTALLED RIVETS, PER B717SRM 51-41-02-OG-O. TREATED PRIMED AND PAINTED AREA, PER B717 SRM 51-22-01-OG-O. DATE 08/28/20, MECH 019536.

Part: BEAM — CRACKED (NR 6) · airframe 25,972 hrs · 35,372 cycles

492 C CHECK. SMALL CRACKS ON THE MED NR 6 BEAM (P/N: 9955757-503) AT/NEAR THE BAYONET CRANK FITTING BOLT HOLE. REPAIRED MED NR 6 BEAM, PER E105-B10650-PERM 08/17/2020.

Part: FLANGE — CRACKED · airframe 25,972 hrs · 35,372 cycles

492 C CHECK. CRACKED END FLANGE OF THE KEEL TO CANTED PANEL ATTACH FORMER AT Y=715. REMOVED FORMER FOR REPAIR. 08/18/2020 MECH 16912 M66 SUBMITTED 2. REPAIRED PER E105-492093-PERM UP TO STEP 6. 8-26-20 MECH 16148 INSP 7924 INSTALLATION PENDING. COMPLETED E105-492093-PERM. DATE: 08/27/2020 MECH:16148 RII: 5295 INSTALLATION PENDING. INSTALLED PER DRAWING 9923454. DATE: 08/20/2020 MECH: 21048 RII: 2659.

Part: OXYGEN MASK — FAILED (CAPTAIN'S) · airframe 25,701 hrs · 34,773 cycles

BTB - CAPTAIN OXYGEN MASK LEAKING AT HEADSTRAP AND UNABLE TO BROADCAST ON ON VHF1 OR VHF2,MULTIPLE RESET ATTEMPTS UNSUCESSFUL // REPLACED FAULTY O2 MASK. LOG PAGE # 810474.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 25,375 hrs · 34,027 cycles

FOUND A DENT L-1/2 " W 1/4 " D 0.006 " WITH A CRACK 9/32 " LONG AT THE CENTER OF THE DENT DAMAGE LOCATED ON L/H AFT MOVEABLE VANE 15 1/2 " FROM INBOARD EDGE 12 3/16 " FROM TRAILING EDGE UNDER SIDE OF VANE. // PERFORMED COIN TAP TEST AROUND THE AFFECTED AREA NO DEFECTS NOTED. REMOVED L/H AFT MOVABLE FLAP VANE PER AMM 27-50-03-00-802. ADJUSTMENT OUT OF LIMITS PER SUB TASK 27-50-03-820-003 L/H AFT MOVEABLE AND TRACK INBD. REMOVED PER AMM 27-50-03. REPLACED INBD TOP SIDE LOAD BEARING PER OVERHAUL MANUAL 27-50-01. REMOVED AND REPLACED INBD, O/B SIDE LOAD BEARING REF. OHM 27-50-1. INSTALLED NEW L/H AFT MOVEABLE VANE I/B TRACK PER CMM 27-50-01. INSTALLED AFT MOVABLE VANE PER AMM 27-50-03. ADJUSTED L/H FWD AND AFT MOVABLE VANE PER AMM 27-50-03-200-801. OPS CHECK GOOD NO BINDING. OK FOR SERVICE

Part: PUMP — FAILED (ZONE 500) · airframe 25,321 hrs · 33,908 cycles

ETOPS OPEN - BTB, HYDRAULIC FAIL //PER FIM REPLACE ENG HYD PUMP I.A.W. AMM 29-11-01-400-801. OPS AND LK CK GOOD. OK FOR SVC. REF LOG PAGE DEFECT 764801

Part: DOUBLER — DENTED (LT ELEVATOR) · airframe 23,830 hrs · 30,611 cycles

LH ELEVATOR HAS A DENT, 1" X 1" ON THE TOP, O/B SIDE, IN BETWEEN XE 225.834 AND XE 204.114, OR HINGE POINTS 5 AND 6

Part: CONTROL UNIT — FALSE INDICATION · airframe 23,525 hrs · 29,939 cycles

AT ABOUT 1200 FT. EMERGENCY POWER CAME ON IN FLT, DURING SHORT FINAL, PERFORMED OPS TEST OF EPCU IAW AMM 24-21-02-700-801. OPS CHECKED OK, OK FOR SERVICE.

Part: ENGINE — WARNING MESSAGE (RIGHT) · airframe 22,883 hrs · 28,508 cycles

CREW REPORTED THE RT ENGINE LOW OIL PRESSURE WARNING AND ENGINE RT SYS FAIL ALERT MESSAGE. REMOVED AND REPLACED THE NR 2 ENGINE IAW M143-717. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: COMPRESSOR BLADE — MISSING (RT ENGINE) · airframe 20,770 hrs · 26,368 cycles

ATB/ RIGHT ENGINE COMP STALL ON EICAS AUDIBLE BANG HEARD BY CREW. BORESCOPE REQUIRED. REMOVED HIGH PRESSURE COMPRESSOR FAIRING AND 6 EA PLUGS. REMOVED HP TURBINE STAGE 2, LP TURBINE STAGE 1, LP TURBINE STAGE 2 PLUGS. REMOVED BREATHER OUTLET. BORESCOPED NR 2 ENGINE HPC THROUGH ACCESS PORT "D", FOUND A BLADE MISSING ON STAGE 3 HPC AT ROOT AREA. REMOVED AND REPLACED RIGHT ENGINE. OPS CHECK GOOD.

Part: BLADE — MISSING (NR 2 HPC) · airframe 22,500 hrs · 27,667 cycles

NR 2 ENGINE COMPRESSOR STALLED IN FLIGHT. REMOVED HIGH PRESSURE COMPRESSOR FAIRING AND SIX PLUGS. REMOVED HP TURBINE STAGE 2, LP TURBINE STAGE 1, LP TURBINE STAGE 2 PLUGS. REMOVED BREATHER OUTLET. BOROSCOPED THE NR 2 ENGINE HPC THROUGH ACCESS PORT D FOUND A BLADE MISSING ON STAGE 3 HPC AT ROOT AREA. REPLACED THE NR 2 ENGINE.

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 22,036 hrs · 26,628 cycles

VIOLENT BUFFETING AND ROLLING MOMENTS IN BOTH DIRECTIONS ON FLAP EXTENSION. NO INDICATIONS. RETRACTED, EXTENDED AGAIN SLOWLY. OPS NORMAL SECOND ATTEMPT.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 26,469 hrs · 21,965 cycles

RT ENGINE COMPRESSOR STALLED, FOLLOWED BY ENGINE VIBRATION HIGH. SHUT DOWN THE ENGINE. ENGINE CHANGE IN WORK.

Part: PITOT HEAD — OBSTRUCTED · airframe 19,760 hrs · 21,505 cycles

ON TAKEOFF ROLL AT 80 KTS F/O'S AIRSPEED INDICATOR STARTED DROPPING OFF DUE TO A BEE IN F/O'S PITOT TUBE. CONFIRMED BEE STUCK TO F/O'S PITOT PROBE, CLEARED LINE IAW AMM 34-11-00-171-801, LEAK CHECK OK IAW AMM 34-11-00-790-801. NO BRAKE OVERHEAT NOTED DURING BRAKING, NO HIGH ENERGY STOP REQUIRED IAW AMM 05-53-01, OK FOR SERVICE.

Part: TIRE — SEPARATED (NR 3) · airframe 19,106 hrs · 18,698 cycles

NR 3 MAIN TIRE CAP COMING OFF. TIRE SEPARATED ON TAKEOFF. R & R NR 3 MAIN WHEEL AND TIRE IAW TASK 32-41-01-400-802. SPIN CHECK OK. OPS CHECK OK, ACFT OK FOR SERVICE.

Part: SWITCH — MALFUNCTIONED (SMOKE TEST) · airframe 18,277 hrs · 18,177 cycles

LAVATORY SMOKE TEST STAYS ON AFTER TEST. RESET TEST SWITCH FOR LAVATORY SMOKE. MESSAGE EXTINGUISHED. NO DEFECTS NOTED. OK FOR SERVICE.

Part: DISPLAY — INOPERATIVE (NR 1) · airframe 16,403 hrs · 13,937 cycles

NR 1 MCDU/FMC WENT BLANK AFTER TAKE OFF. REPLACED NR 1 MCDU. OPS CHECKED OK IAW MM 31-65-01.

Part: SHUTOFF VALVE — INOPERATIVE (ANTI SKID SYSTEM) · airframe 17,926 hrs · 13,749 cycles

DURING START ANTI-SKID FAIL, RETURNED TO GATE, BRAKE RETURN LINE SHUTOFF VALVES. FOUND RT BRAKE LINE, SHUTOFF VALVE INOPERATIVE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 13,962 hrs · 8,342 cycles

STATIS MESSAGE FOR LAVATORY SMOKE ON. RESET SMOKE DETECTOR AFT LT, TEST SMOKE DETECTOR CHECKED GOOD.

Part: PUMP — FAILED (LAVATORY) · airframe 13,499 hrs · 7,281 cycles

LAVATORY SMOKE ALERT WITH ODOR. RETURN TO GATE, AFT RT LAVATORY LOCKED CLOSED. R & R CHEMICAL INJECTION PUMP AND ENVIROMENTAL CLEAN, OPS AND LEAK CHECKED OK IAW AMM 38-32-01.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 13,489 hrs · 7,266 cycles

AFT EMERGENCY EXIT SIGN ILLUMINATED. R & R AFT EXIT DOOR POWER SUPPLY. OPS CHECKED EMERGENCY LIGHTING, OK.