N480HA

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,767 hrs · 76,207 cycles

TAIL CATWALK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BOTH THE EMERGENCY LIGHT BATTERY AND BATTERY POWER SUPPLY UNIT PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 31,906 hrs · 74,290 cycles

INTERMITTENT L HYD PUMP FAIL. REMOVED AND REPLACED LH ENGINE DRIVEN HYD PUMP PER B717 AMM 29-11-01. CONDITION SAME. REMOVED AND REPLACED LH ENGINE EDP LOW PRESSURE SWITCH PER B717 TSM 29-10 TASK 801. NO FAULTS NOTED. OPS CHECK NORMAL. OK FOR SVC.

Part: NONE — NONE · airframe 31,215 hrs · 72,790 cycles

ATB- ENG L FADEC ALTERNATE (AIRBORNE) WOULD NOT RESET // PERFORMED FIM 71-00 TASK 812. NO FAULTS FOUND. RAN #1 ENG TWICE. BOTH RUNS NO DEFECTS NOTED. OK FOR SVC.

Part: PIN — BROKEN (L1 LIFE RAFT) · airframe 29,364 hrs · 68,623 cycles

DOOR 1L LIFERAFT PIN BROKEN. RESECURED GIRT BAR AT 1L DOOR. OPERATIONS CHECK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,030 hrs · 67,902 cycles

EXTERIOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. // REMOVED AND REPLACED OVER WING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. OK FOR SERVICE

Part: CONTROL UNIT — UNKNOWN (ANTI SKID SYS) · airframe 27,477 hrs · 64,462 cycles

ATB - ANTI-SKID FAIL. // REMOVED AND REPLACED BCU PER AMM 37-45-01. RTS TEST PASSED. OK FOR SVC.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,644 hrs · 62,643 cycles

DENT AND GOUGE FOUND ON LEFT HAND AFT FUSELAGE BETWEEN STATION 927-946 STRINGER 18-15L.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 26,328 hrs · 61,959 cycles

LAVATORY SMOKE ALERT DISPLAYED. MOVED LAVATORY SMOKE DETECTOR TEST SWITCH TO OFF POSITION. MESSAGE CLEARED. OK FOR SERVICE.

Part: THERMOCOUPLE — MALFUNCTIONED (APU) · airframe 26,295 hrs · 61,884 cycles

DURING CLIMB OUT, A LEVEL 2 APU EGT HIGH LIGHT ILLUMINATED INTERMITTENT. APU THERMOCOUPLE 1 OPEN CIRCUIT MESSAGE. REMOVED AND REPLACED NR 1 APU THERMOCOUPLE IAW AMM 49-72-02. OPS AND RTS CHECKED GOOD.

Part: RETRACT CYLINDER — FAULTY (LT MLG) · airframe 25,694 hrs · 60,582 cycles

AFTER T/O L&R MAIN GEAR INDICATED UNSAFE. REMOVED & REPLACED LT MAIN LANDING GEAR RETRACT CYLINDER.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 25,169 hrs · 59,417 cycles

COMPRESSOR STALL LEFT ENG, LOUD BANG/SMELLED FUMES THEN ENG L COMP STALL ON EAD. ENGINE CHANGE IN WORK.

Part: ENGINE — DAMAGED (LEFT) · airframe 25,051 hrs · 59,160 cycles

LEFT ENGINE HAD SEVERE DAMAGE.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,826 hrs · 58,649 cycles

ODOR THROUGH TAKEOFF TO 3000FT, THE ELECTRICAL BURNING ODOR EVENTUALLY WENT AWAY. CHECKED CIRCUIT BREAKERS, TURNED ON ALL FLIGHT DECK LIGHTS, CHECKED E & E BAY, RAN LEFT AND RIGHT A/C PACKS WITH APU, ALSO WITH LEFT ENGINE. NO ELECTRICAL ODOR AT ANYTIME. OK FOR SERVICE.

Part: FAN — FAILED (NR 1 ADIRU) · airframe 24,816 hrs · 58,628 cycles

AFTER TAKEOFF TO 3000 FT, HAD AN ELECTRICAL BURNING ODOR, EVENTUALLY WENT AWAY. FOUND THE NR 1 ADIRU FAN FROZEN AND BURNED. REPLACED THE FAN IAW AMM 34-43-05. OPS CHECKED OK.

Part: LATCH — OUT OF ADJUST (RT MLG) · airframe 23,904 hrs · 56,604 cycles

OPEN: ATB, RT GEAR UNSAFE LIGHT AFTER TO. MX NEEDS TO ADJUST THE RT MLG UPLOCK LATCH AND OPS CHK. MX IS REPLACING THE DOWN LOCK ELEC CONDUIT.

Part: LATCH — OUT OF ADJUST (RT MLG DOOR) · airframe 23,904 hrs · 56,604 cycles

RIGHT GEAR UNSAFE LIGHT ILLIMINATED AFTER TAKE OFF. ACCOMPLISHED FUNCTIONAL TEST OF MAIN & NOSE GEAR IAW AMM 32-30-00-720-801. OPS CHECKED OK. FOUND MAIN GEAR RT DOOR LATCH ROLLER TO HOOK CLEARANCE OUT OF LIMITS. ADDED A SHIM BETWEEN MLG DOOR AND DOOR LATCH. INSPECTED AND ADJUSTED MAIN LANDING GEAR LATCH CLEARANCES IAW AMM 32-34-01-820-801. ALL CLEARANCES WITHIN LIMITS. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 23,764 hrs · 56,286 cycles

EMERGENCY LIGHT IN COCKPIT DOES NOT ILLUMINATE WHEN ON POSITION. R & R BATTERY AT B5-123 IAW WDM 33-51-12. OPS CHECK GOOD. OK FOR SERVICE.

Part: DUCT — DISCONNECTED (LT A/C PACK) · airframe 23,780 hrs · 56,251 cycles

F/A REPORTED AFT DOOR HOT TO FEEL. FOUND LEFT PACK DISHCHARGE ELBOW DUCT DISSCONECTED. REATTACHED DUCT RAN PACK, NO LEAK NOTED OK TO CONTINUE SECURITY CHECK GOOD, PACK OP'S CHECK GOOD NO FAULTS NOTED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 23,280 hrs · 55,234 cycles

MAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN STA 646-823, RBL 22. BLENDED OUT SCRATCHES AND GOUGES AT MAIN CABIN SEAT TRACK BETWEEN STA 646-823, RBL 22. NDT AREA IAW NDT SPM PT4 04-00-07, ORIGINAL MST .100 WITH MST LOSS OF .042, MST REMAINING .58, FOUND TO BE OUT OF LIMITS IAW 53-20-52. REMOVED 4 EA CLIPS FOR ACCESS STA 775, 794 AND 813 LBL 22 IAW SRM 51-40-02. CUTOUT DAMAGE SEAT TRACK FROM STA 823 TO 756 IAW SRM 53-20-52, LOCATED AND DRILLED NEW SEAT TRACK, IAW 51-10-00, INSTALLED SEAT TRACK SRM 51-40-02. INSTALLED 4 EA CLIPS IAW SRM 51-40-02 AND SRM 53-20-52-2R REPAIR 5.

Part: TAB — CRACKED (FUSELAGE) · airframe 23,280 hrs · 55,234 cycles

MAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53-10-15-2R-1, REPAIR 1.

Part: TAB — CRACKED (FUSELAGE) · airframe 23,280 hrs · 55,234 cycles

MAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53-10-15-2R-1, REPAIR 1.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,280 hrs · 55,234 cycles

FUSE AFT CARGO COMPARTMENT LOWER DOOR PAN BS 974 HAS EXFOLIATED CORROSION. REPAIRED PAN AT AFT CARGO COMPARTMENT LOWER DOOR, BS 974 TO 954 IAW SRM 53-20-15-2R-7, REPAIR 7. REMOVED DAMAGE AFT CARGO DOOR LOWER DOOR PAN IAW SRM 51-40-07, REMOVED 2 EA STRAPS FOR ACCESS IAW SRM 51-400-07. REMOVED 2 EA SPLICES FOR ACCESS IAW SRM 51-40-07, LOCATED, DRILLED NEW DOOR PAN IAW SRM 51-40-08. INSTALLED DOOR PAN IAW SRM 51-40-02, INSTALLED 2 EA STRAPS AND 2 EA SPLICES IAW 51-40-07.

Part: PAN — CORRODED (BS 974) · corrosion level 2 · airframe 23,280 hrs · 55,234 cycles

AFT CARGO COMPARTMENT LOWER DOOR PAN BS 974 HAS EXFOLIATED CORROSION.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,280 hrs · 55,234 cycles

CORROSION ON FALSE TRACK STA 1002, RBL 18. REMOVED -65 AND -67 SUPPORTS IAW SRM 51-41-01. REMOVED CORROSION FROM SUPPORTS, -65 SUPPORT WITHIN LIMITS, -67 SUPPORT OUT OF LIMITS IAW SRM 53-00-00, FIG 103. REINSTALLED -65 SUPPORT AND NEW -67 SUPPORT IAW SRM 51-41-01.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 23,280 hrs · 55,234 cycles

CRACK ON GROUND CONDITION AIR ACCESS DOOR LANDING, FWD INBD CORNER AND AFT INBD CORNER. R & R CRACKED DOUBLER AT GROUND CONDITIONED AIR ACCESS DOOR LANDING IAW DWG 5911429, REV 02 AND SRM 51-41-02, LEAK CHECK GOOD IAW AMM 21-22-07.

Part: HF COMM — MALFUNCTIONED · airframe 23,271 hrs · 55,232 cycles

HF RADIO UNABLE TO UNDERSTAND TRANSMISSIONS FROM OTHER ACFT AND FROM ATC, VERY GARBLED. TRIED 3 DIFFERENT FREQUENCIES ALL SAME. SET HF FOR USB OPERATION. OPS CHECKED NR 1 HF IAW AMM 23-11-00-710-801. OPS CHECKED GOOD. OK FOR SERVICE.

Part: HYDRAULIC SYSTEM — CONTAMINATED · airframe 22,673 hrs · 53,890 cycles

ATO- HYD L TEMP HIGH ON T/O ROLL. MAINTENANCE FOUND EXCESSIVE AIR IN HYDRAULIC SYS RESERVOIR, BLEED OFF HYD SYS. CHECKED BYPASS VALVES. OPS CHECK GOOD, ACFT RELEASED.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED · airframe 22,673 hrs · 53,890 cycles

ABORTED TAKEOFF. HYD LOW TEMP HIGH ON T/O ROLL. MAINTENANCE FOUND EXCESSIVE AIR IN HYD SYS RES. BLEED OFF HYD SYS. CHECKED BYPASS VALVES. OPS CHECK GOOD, ACFT RELEASED.

Part: SENSOR — FAULTED (RT ENGINE) · airframe 22,195 hrs · 52,806 cycles

DURING CLIMB, ENROUTE, LEVEL 1 ENGINE RT SYS. FAIL ALERT DISPLAYED ON SECONDARY ENGINE PAGE. FOUND FAULT CODE 771202, R & R HP SPEED PROBE SENSOR U1019 IAW AMM 77-12-01. OPS AND LEAK CHECK GOOD.

Part: MOTOR — INOPERATIVE (PRIMARY TRIM) · airframe 22,050 hrs · 52,486 cycles

PRIMARY TRIM INOPERATIVE. R & R PRIMARY STABILIZER TRIM MOTOR IAW AMM 27-41-10-400-801.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 19,521 hrs · 46,843 cycles

RT INBD FLAP T/E HAS IMPACT DAMAGE. OPEN

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 19,396 hrs · 46,564 cycles

LEFT ENGINE FUEL PRESSURE LEVEL ALERT DISPLAYED DURING TAXING FOR TAKEOFF. R & R LT ENGINE LOW PRESSURE SWITCH. OPS CHECK COMPLETE, LEAK CHECK COMPLETE IAW AMM 73-33-01.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 19,374 hrs · 46,527 cycles

DIVERSION TO ALTERNATE STATION. RED GEAR UNSAFE LIGHT ON RT GEAR AFTER ROTATION CYCLED GEAR DOWN/UP AND ALL INDICATIONS NORMAL. R & R LT MAIN GEAR UP & LATCH PROXIMITY SENSOR IAW AMM 32-61-02. FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION SYS CHECKED GOOD.

Part: SLIDE — DAMAGED (SERVICE DOOR) · airframe 16,978 hrs · 41,053 cycles

SERVICE DOOR SLIDE LOWER RELEASE PIN, MISSING TAMPER STRING. R & R FWD SERVICE DOOR EMERGENCY SLIDE IAW AMM 25-61-03 CONDITION & SECURITY CHECK OK. OK FOR SERVICE.

Part: CONTROL VALVE — DEFECTIVE (MLG) · airframe 15,971 hrs · 38,691 cycles

GEAR DOOR OPEN ALERT CAME ON APPROX 10 SEC AFTER GEAR EXTENTION, STAYED ON F/O APPROX 6SEC. PERFORMED AMM 32-33-00-720-801, FUNCTIONAL TEST OF THE LANDING GEAR HYD CONTROL SYS. GEAR RETRACTION, DOOR RETRACT NORMAL, AND ON GEAR EXTENSION, LT DOOR SLOW TO CLOSE. SUSPECT GEAR SELECTOR VALVE DEFECTIVE. R & R LANDING GEAR CONTROL VALVE IAW AMM 32-31-01. OPS AND LEAK CHECK GOOD. NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,340 hrs · 37,236 cycles

F/A REPORTED STRONG ELECTRICAL ODOR IN FWD CABIN AFTER ENGINE START. INSPECTED E/E, AFT ACCESS COMPT, APU COMPT, BAG BINS, WHEEL WELLS, CABIN O/H COMPTS. CLOSED MED, RAN BOTH ENGS. TURNED APU AIR OFF. NO SMOKE NOTED VISUALLY OR SMELLED. ALL SHIPS BATTERIES CHECKED GOOD. ALL FWD CABIN LIGHTS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: DUCT — DISLODGED (AIR CON) · airframe 13,954 hrs · 33,971 cycles

ENROUTE, DUCTING FOR EXTERNAL AC CAME LOOSE, LOST PRESSURIZATION. REINSTALLED FLEX HOSE COUPLING TO RIGID TUBING IN EXTERNAL AIR CONDITIONING DUCT ABOVE CHECK VALVE. OPS AND LEAK CHECK GOOD. SECURITY CHECK GOOD IN RT A/C PACK. OK FOR SERVICE.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 13,912 hrs · 33,899 cycles

TAIL CONE RELEASE HANDLE LT SIDE CABLE ASSY HAS SEVERAL BROKEN STRANDS AND IS RUSTED AT TERMINAL END. REMOVED TAIL CONE RELEASE HANDLE, LT SIDE CABLE ASSY REF B717 AMM 20-00-02. INSTALLED TAIL CONE LT INTERNAL RELEASE HANDLE CABLE ASSY REF B717 M/M 53-52-01. ACCOMPLISHED FUNCTIONAL TEST OF THE TAIL CONE RELEASE SYSTEM, REF B717 M/M 53-52-01, OPS CHECKS NORMAL.

Part: EEC — FAULTED (NR 1 ENGINE) · airframe 13,796 hrs · 33,643 cycles

SELECT FADEC ALTN ALERT DURING CLIMB LT ENG. OK TO CONTINUE IAW A 73-21-01.CODE 73-21-05. R & R NR 1 ENG EEC ASSY IAW AMM 73-21-0111. OPS CK OK, NO FAULTS NOTED.

Part: SKIN — DAMAGED (BS 342) · airframe 13,709 hrs · 33,442 cycles

ON WALK AROUND F/O NOTICED DENT JUST BELOW AFT STATIC PORT ON RT SIDE OF ACFT. FOUND CREASE BELOW AFT STATIC PORT APPROX 7" X 3/4', DEPTH .020" AT STA 342 BETWEEN L28R-29R. THE DAMAGE IS WITHIN LIMITS IAW SG 09530000 DWG ID 31. SILVER DOT WAS APPLIED. NO CRACKS FOUND.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,254 hrs · 32,378 cycles

11D EMERGENCY PATH LIGHT INOP. REPLACED 11D EMERGENCY LIGHT BULB AND LENS. OPS CK GOOD.

Part: LATCH — SHEARED (MLG DOOR) · airframe 12,986 hrs · 31,762 cycles

"GEAR DOOR OPEN" LIGHT ILLUMINATED AT GATE. FOUND UPLATCH SHEARED OFF. INSPECTED LT MLG. REMOVED AND REPLACED LT GEAR DOOR UP LATCH ARM. OPS CHK OK. NO OTHER DEFECTS NOTED IAW MM 32-34 01.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,797 hrs · 31,338 cycles

LEVEL 2 CORROSION ON THE LOWER TCAS ANTENNA BASE. REPAIR IN WORK.

Part: LONGERON — CRACKED (BS 1116 L12R) · airframe 12,332 hrs · 30,266 cycles

CRACK, 2 1/2 INCH LONG ON AFT ACCY, FUSELAGE FRAME STATION 1116, LONGERON 12R. REPAIR IN WORK.

Part: ACTUATOR — MALFUNCTIONED · airframe 12,332 hrs · 30,266 cycles

ENROUTE TO LIH OTBD SPOILER FAIL LIGHT ILLUMINATED IN FLIGHT. RETURNED TO HNL. SECU FAULT REVIEW FOUND SPOILER HOLD DOWN FAULT LT OTBD LVDT PROBABLY CAN'T HOLD DOWN ACTUATOR. REMOVED LT OTBD SPOILER HOLD DOWN ACTUATOR PER AMM 27-67-06-400-801 STEP 3A-F(3) (C). COMPLETED SPOILER HOLD ACTUATOR INSTALL IAW AMM 27-67-06-400-801 STEPS 4-11. SPOILER SYS OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — INOPERATIVE (NOSE COWL) · airframe 12,238 hrs · 30,054 cycles

"ENG R ANTI-ICE DISAG" LEVEL ALERT ILLUMINATED DURING IN-FLIGHT ANTI-ICE CHECK. REMOVED AND REPLACED RT ENG NOSE COWL ANTI-ICE VALVE IAW AMM 30-21-01. OPS CK GOOD.

Part: DOUBLER — CRACKED (BS 1178) · airframe 12,186 hrs · 29,933 cycles

OPEN - FUSELAGE, FS 1178 LT AND RT, DOUBLER AND SKIN, HAS A 2 INCH CRACK ON DOUBLER, AND A 2 INCH CRACK ON THE FUSELAGE SKIN PANEL AT CANTED STA 1178.225, LONGERON 3 LEFT AND 3 RIGHT. REPAIR IN WORK.

Part: MODULE — MALFUNCTIONED (AILERONS) · airframe 10,349 hrs · 25,514 cycles

AILERON STUCK 1/2 WAY LEFT OF CENTER IN FLIGHT. CKED FREEDOM OF MOVEMENT OF AILERON, NO DEFECT NOTED. FOUND AILERON TRIM IND OF CONFIG PG 1/2 LWD OF CENTER. ACCOMP FIM 27-10-00 TASK 801 MAINTENANCE MSG ON ATCL WAS NR 43 ACCOMP FIM 27-10-00 TASK 812. REPLACED AIL AND RUDDER TRIM CTL MODULE PER AMM 27-10-07.

Part: CONTROL UNIT — FAILED (ANTI SKID SYS) · airframe 10,122 hrs · 24,981 cycles

ANTI-SKID FAIL IN FLT - ATB. REPLACED BCU PER AMM 32-45-01. RETURN TO SERVICE TEST PASSED.

Part: CONTROL UNIT — FAILED (DCU) · airframe 10,123 hrs · 24,982 cycles

ANTI-SKID FAIL AFTER GEAR EXTENSION - ATB. TROUBLESHOT IAW FIM 32-45, TASK 807. REMOVED AND REPLACED DCU IAW AMM 31-43-02. OPS CHECK GOOD. MIC SHEET CLEARED. PLACARD REMOVED.

Part: PUMP — MALFUNCTIONED (RT ENGINE) · airframe 9,750 hrs · 24,117 cycles

AIRBORNE - RT HYD QTY LOW LIGHT, WILL BE LANDING ON 8R. WILL DO AN ALT GEAR EXTENSION AND WAIT FOR MAINT AND LINE SERVICE OUT THERE. CREW DECLARED AN EMERGENCY. LANDED AT HNL, WHERE AN UNEVENTFULL LANDING WAS MADE. T/S RT HYD SYSTEM. REMOVED AND REPLACED RT ENG HYD PUMP PER AMM 29-11-01. REMOVED AND REPLACED HYD FILTERS PER AMM29-12-12 AS PRECAUTIONARY STEP. OK FOR SERVICE.

Part: NONE — NONE (NONE) · airframe 9,275 hrs · 22,951 cycles

ATB AFTER ROTATION AND DURING CLIMB-OUT TOWER REPORTED VAPOR TRAILING FROM LEFT SIDE OF AIRCRAFT. RETURNED FOR NORMAL LANDING. DE-BRIEFED CREW AND THEY REPORTED NO ENG ABNORMALITIES. PERFORMED ENG EXCEED BITE PER FIM 71-00 TASK 801, NO EXCEEDANCE NOTED. PERFORMED PNEUMATIC SYSTEM BITE PER FIM 36-10 TASK 801. PERFORMED CABIN PRESS CONT SYS BITE PER FIM 21-30 TASK 801, NO FAULTS FOUND. PERFORMED ENG IDLE RUN AND LEAK CHECK PER AMM 71-00-11. NO LEAK NOTED, ALL PARAMETERS NORMAL VISUALLY CHECKED FOR HYD LEAKS NONE NOTED. HYD QTY GOOD. VISUALLY CHECKED FOR FUEL LEAKS, NONE NOTED VISUALLY CHECKED APU FOR LEAKS, NONE NOTED ACFT OK FOR SERVICE.

Part: CONNECTOR — DIRTY (DISPLAY) · airframe 9,238 hrs · 22,855 cycles

ATB - AFTER TAKEOFF, LOST NR 1DU NR 6 DU STARTED TO FAIL NR 4 CU FAILED FOR A FEW MINUTES. REMOVED AND CLEANED CONNECTORS OF DU'S 1, 4 AND 6. GND OPS CHK OK 31-43-01.

Part: ACCUMULATOR — RUPTURED (RT HYD SYSTEM) · airframe 9,138 hrs · 22,614 cycles

RT HYDRAULIC SYSTEM ACCUMULATOR RUPTURED. REPLACED RT HYDRAULIC SYSTEM ACCUMULATOR PER AMM 29-12-05. LEAK CK CK.

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 8,810 hrs · 21,804 cycles

BTB: ENG L SYS FAIL LIGHT CAME ON DURING START. INTERMITTANT FAULT START CIRCUIT (FUEL SW CIRCUIT) ERASED FAULT. PERFORMED EEC 1 RTS TEST PASSED.

Part: PUMP — FLUCTUATES (LT HYD SYSTEM) · airframe 8,700 hrs · 21,533 cycles

LT HYDRAULIC PUMP FAIL. PRESSURE FLUCTUATED BETWEEN 3000 PSI AND ZERO AT FLIGHT IDLE. TURNED LT ENG DRIVEN PUMP OFF AND TURNED ON TRANSFER PUMP, PRESSURE AND QTY NORMAL.//R/R LEFT ENG HYD PUMP PER M/M 29-11-01 GRD RUN GOOD CHECKED PLUG P1-3355 PIN A TO PLUG P1-7824B PIN B3 WIRING CHKD OK, CHECKED S-32 CHECK OK PER 717 FIM 29-10 TASK 801 HHAL5743/580.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 8,700 hrs · 21,533 cycles

BTB - HYD L PUMP FAIL LT ON. REMOVED AND REPLACED LT HYD ENG, DRIVEN PUMP PER AMM 29-11-01. OPS CHECK OK, LEAK CHECK OK. SECURITY CHECK OK.

Part: BLEED VALVE — MALFUNCTIONED (APU) · airframe 8,347 hrs · 20,683 cycles

BTB - NO AIR ON APU ON START. PERFORMED APU RTS TEST FAILED BLEED CONTROL VALVE OPEN CIRCUIT FAULT. PERFORMED FIM 49-50-00-810-804 REF WDM 49-30-004. PERFORMED REPAIR CONFIRMATION RTS PASSED.

Part: WIRE — DAMAGED (STICK SHAKER) · airframe 8,298 hrs · 20,566 cycles

FLT CREW REPORTS, STALL WARNING FAULT LEVEL ONE ALERT ANNUNCIATED, NO TAKEOFF. FOUND WIRES TO FO STICK SHAKER N/G. REPAIRED WIRES PER SWPM 20-10-03. RTS FOR STALL WARNING SYSTEM CHECK OK.

Part: APU — EXPLODED (APU BAY) · airframe 8,239 hrs · 20,421 cycles

ON PARKING AT KOA PILOTS SMELLED FAINT SMOKE THEN NOTICED VISIBLE SMOKE COMING OUT OF A/C VENTS. SECURED BOTH PACKS, EXPEDITED DEPLANING OF PAX THEN APU BLEW UP. NO FIRE INDICATION ON PANEL, DISCHARGED BOTH BOTTLES. REMOVED AND REPLACED NR 2 FIRE BOTTLE PER AMM 26-21-01 FUNC/ADJ PER AMM26-21-01-720-801OK REM NR 1 FIRE BOTTLE ASSY PER MM REINSTL ORIG NR 1 BOTTLE DISCHARGE. FERRIED A/C TO HNL. INSTALLED NR 1 FIRE BOTTLE AND SQUIBS.

Part: WARNING SYSTEM — MALFUNCTIONED (THRUST REVERSER) · airframe 8,185 hrs · 20,280 cycles

BTB - NR 2 T/R FAULT LIGHT ILLUMNATED. ACCOMPLISHED FIM 78-34 AND TASK 806 AND TASK 78-30-0, 0-702-801. NO FAULTS NOTED. OK FOR SERVICE.

Part: PIVOT — LOOSE (NLG STEERING) · airframe 7,984 hrs · 19,810 cycles

BTB - AFTER ENG START UNABLE TO TURN STEERING TO RT. STEERING WAS JAMMED ONLY TO RT SIDE. AFTER INSPECTION BY MAINT JAM WAS NOT REMAINING AND WERE ABLE TO RETURN TO GATE. FOUND NLG STEERING BYPASS LEVER PIVOT BOLT LOOSE. RESECURED AND RESAFETIED BOLT. CHECKED STEERING, FULL DEFLECTION LT AND RT. OK.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 7,900 hrs · 19,608 cycles

BTB - "AIR SYSTEM R PRESS LO" ALERT AFTER ENG START. PERORMED FIM 36-10-00-310-505 PSC BITE CHECK NO FAULTS NOTED. OPS CK GOOD.

Part: BLEED VALVE — FAILED (APU) · airframe 7,895 hrs · 19,597 cycles

BTB: APU VALVE DISAGREE LEVEL 1 ALERT CAME ON AFTER SHUTTING DOWN APU ON TAXI OUT. REPLACED APU BLEED AIR VALVE PER AMM 36-16-02.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 7,654 hrs · 19,014 cycles

BAGGAGE SERVICE FOUND DENT & SCRATCH ALONG RT SIDE OF FUSELAGE APPROX L 19R FROM STA 253-357. BLENDED DENT AND SCRATCH AREA PER SRM 51-10-4, PERFORMED EDDY CURRENT INSP DENT AREA. NO CRACKS NOTED. DAMAGE FOUND TO BE CONDITION 3 PER SRM 53-00-01, PERMANENT REPAIR TO BE ACCOMP W/I 4500 FLT HRS. ALODINED AND PAINTED AREA PER SRM 51-10-4 MPCW XCRIBED TO MIC SHEET PLACARD START TIME 7654 PERMANENT REPAIR ACCOMP BY 12154.

Part: IGNITER — UNKNOWN (RT ENGINE) · airframe 7,586 hrs · 18,846 cycles

BTB - RT ENG DOES NOT LIGHT OFF IN AUTO. REMOVED AND REPLACED RT ENG B IGNITOR PLUG IAW AMM 74-20-04. OPS CHECK GOOD. OK FOR SERVICE.

Part: COMPRESSOR WHEEL — DAMAGED (ENGINE) · airframe 7,216 hrs · 17,955 cycles

DUE TO TREND ENGINE TO BE BORESCOPED. FOUND NR 3 HIGH PRESSURE COMPRESSOR PLATFORM DAMAGE AND DAMAGE NR 4 STAGE BLADES. ENGINE TO BE REPLACED.

Part: PUMP — FAILED (AUX HYD SYS)

DURING EO 29-02-02-11 REV A, FOUND AUX PUMP ELECTRICAL CONNECTOR ON PUMP MELTED, NEED TO REPLACE PUMP. AIRCRAFT SIDE PLUG DISCONNECTED FROM PUMP. REMOVED AND REPLACED AUX HYD PUMP IAW AMM 29-21-01, OPS AND LEAK CHECK GOOD. (M)

Part: CONTROL UNIT — MALFUNCTIONED (OVERSPEED PROTEC)

RIGHT ENIGNE SYSTEM FAIL LIGHT CAME ON. PERFORMED WIRING CHECK PER FIM 73-21. ALL OK. REMOVED AND REPLACED NR 2 INDEPENDANT OVERSPEED PROTECTOR (IOP) PER MM 73-21-11. CHECK OK. RTS CHECKED OK. OK FOR SERVICE. (M)

Part: GENERATOR — FAILED (LEFT)

FLT 541 - HNL - NUMEROUS POEWR INTERUPTIONS ON DESCENT TO HNL. NO BREAK POWER TRANSFER APPEAR INOPERATIVE. EMERGENCY LIGHTS ON (5 TIMES). INTERMITTENT ANNUNCIATOR LIGHTS, DCU FAIL. NR 1 ENGINE VIBE HIGH, INDICATED 5.0 PLU (AMBER) FOR NR 1 N1 ON ONE OCCASSION. LEFT GENERATOR APPEARED FAILED. RIGHT GENERATOR WAS POWERING LEFT AC BUSS. REPLACED LEFT GENERATOR ASSEMBLY. OPS CHECK LEAK CHECK NORMAL. (M)

Part: GEARBOX — FAILED (RT ENGINE)

FLT 180 - HNL - FOUND RIGHT ENGINE FAIL LIGHT CAME ON IN FLIGHT. REMOVED NR 2 ENGINE GEARBOX, ACCESSORY PER MM 72-61-00. INSTALLED GEARBOX PER MM 72-61-00 PARA E2P. LEAK AND OPS CHECK GOOD, PER TEST 5 TASK 71-0014-710-802. (M)

Part: DUCT — CRACKED (APU)

CRACK ON APU INLET DOOR DUCT. REPAIRED PER HAL M105 FILE.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS)

HNL - FLT 520 - RIGHT HYDRAULIC TEMPERATURE HIGH LIGHT ON. REMOVED AND REPLACED AUX PUMP OPS CHECK, LEAK CHECK OK, PER MM 29-21-01. (M)