N477HA

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 31,656 hrs · 74,039 cycles

ATO - RTO OGG RUNWAY 02 DUE TO HYD R TEMP HI ALERT AT APPROX 40 KTS. CYCLED FLT CONTROLS TO CLEAR ALERT. SUBSEQUENT TAKEOFF NORMAL. NOTED BY MX. NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: SEAL — DAMAGED (L1 DOOR) · airframe 31,142 hrs · 72,930 cycles

LOUD SQUEAL BY 1L DOOR AIRBORNE IN CRUISE FOR 10 MINUTES THAT WENT AWAY DURING DESCENT. PERFORMED SEAL REPAIR TO FWD LOWER CORNER OF MED PER E105-C10707-INI. DUE TO ACCOMPLISHING E105, PERFOMRED LEAK CHK PER AMM 21-30-00-790-801. NO DEFECTS NOTED. OK TO COMTINUE.

Part: NONE — NONE · airframe 30,410 hrs · 71,286 cycles

FORWARD PAX ENTRY DOOR MAKING LOUD SQUEALING NOISE AFTER TAKEOFF AND IN-FLIGHT ALSO DESCENT // REPAIRED MED DOOR SEAL FWD LWR CORNER PER SRM 52-10-17. LEAK CHECK GOOD. OK FOR SVC.

Part: DUCT — DAMAGED (APU) · airframe 30,129 hrs · 70,665 cycles

FOUND LOWER APU INLET DUCT SEVERELY DAMAGED. // REMOVED TOP SIDE OF LOWER APU INLET DUCT PER AMM 49-16-01. INSTALLED TOP SIDE OF LOWER APU INLET DUCT PER AMM 49-16-01. OK FOR SERVICE. SECURITY CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 30,100 hrs · 70,609 cycles

UNCOMMANDED PASSENGER O2 MASK DEPLOYMENT ROW 22. //RE-SECURED PASSENGER O2 MASK SEAT 22 A/B/C IN ACCORDANCE WITH B717 AMM 35-23-06. NO DEFECTS FOUNDED. OK FOR SERVICE.

Part: SENSOR — MALFUNCTIONED (SMOKE WARNING) · airframe 30,047 hrs · 70,497 cycles

CARGO SMOKE TEST WON'T START. // CARGO TEST SWITCH CHECK OK. SWAPPED VIA #1 AND #2 CONDITION SAME, REINSTALLED VIA'S IN ORIGINAL POSITIONS. VIA #1 AND #2 R.T.S. PASS. RED TRIANGLE SHOWS FOR ACFT DETECTOR. REMOVED AND REPLACED AFT CARGO CHANNEL FORE SMOKE DETECTOR SENSOR PER AMM 26-13-01. PERFORMED OPERATIONAL TESTS FOR FIRE DETECTION. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (SMOKE TEST) · airframe 30,047 hrs · 70,497 cycles

CARGO SMOKE TEST WON'T START. // RESET VIA'S OPS CHECK GOOD IAW AMM 31-43-00-741-803.

Part: LIGHT — NOT REPORTED (CABIN) · airframe 29,757 hrs · 69,844 cycles

17 B EMERGENCY FLOOR EXIT LIGHT NEEDS TO BE REPLACED. // REMOVED AND REPLACED EMERGENCY FLOOR EXIT LIGHT, SECURED CHECK OK

Part: PROBE — DEFECTIVE (ENGINE) · airframe 29,757 hrs · 69,844 cycles

SELECT FADEC ALTERNATE (L) ILLUMINATED DURING CLIMB OUT - ABOUT 1,300 FEET C/W QRH PROCEDURES, LIGHT DID NOT GO OUT - RETURNED TO DEPARTING AIRPORT. // PER FIM 73-21 TASK 814, REMOVED AND REPLACED P2/T2 PROBE PER AMM 73-21-05. REPAIR CONFIRMATION SATISFACTORY. OK FOR SVC.

Part: ROD END — CRACKED (SLAT ACTUATOR) · airframe 29,371 hrs · 68,970 cycles

WHEN THE SLATS EXTEND: THE AIRCRAFT TURNS TO THE LEFT. THAT'S ALSO VERIFIED WITH THE FLIGHT CONTROLS TURNING LEFT. NOTE: THE RIGHT WING COME UP. FOUND RH INBD SLAT ACTUATOR ROD END CRACKED. REMOVED AND REPLACED ACTUATOR PER AMM 27-82-04-400-802.

Part: LOCK PIN — UNSECURE (DOOR SLIDE) · airframe 29,335 hrs · 68,886 cycles

SLIDE CASE CAME OFF JAMMING DOOR. RE-SECURED OVER CENTER LOCKING PIN. OPS CK GOOD. SECURITY CK GOOD. OK FOR SVC.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 29,086 hrs · 68,310 cycles

ATB / ATB, ELECTRICAL SMELL REPORTED BY FA'S. TROUBLESHOT SMELL TO GASPER BOOSTER FAN. C/B POPPED. REMOVED AND REPLACED GASPER BOOSTER FAN PER AMM 21-23-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 28,624 hrs · 67,264 cycles

AT 1,000 FT "DISARM SPOILERS CAME ON AFTER TAKE OFF. THEN ON APPROACH "CLIMB THRUST" FLASHED IN THE AIR. PULLED C/BS K-32 L 323. // PERFORMED FIM 27-60TASK 1 802. NO DEFECTS NOTED. PERFORMED AFS RTS. TEST PASSED, OK FOR SVC. RESET CB'S K32 & L32.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 27,672 hrs · 65,173 cycles

DECLARED EMERGENCY FOR IN-FLIGHT HYDRAULIC FLUID LOSS. REMOVED AND REPLACED AUX PUMP HOSE.

Part: PLENUM — CRACKED (LT A/C PACK) · airframe 27,273 hrs · 64,258 cycles

AFT FA REPORTED THAT THE JUMP SEAT AND BULKHEAD DOOR GETS PROGRESSIVELY HOTTER DURING FLIGHT. SEAT BECOMES UNCOMFORTABLY HOT BY THE END OF THE FLIGHT. FOUND THE LT PACK PLENUM CRACKED. REMOVED AND REPLACED THE LT RAM AIR INLET PLENUM IAW AMM 21-29-21. OPS & LEAK CHECKED OK.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 27,249 hrs · 64,207 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN LENS DETACHED. INSTALLED A NEW EMERGENCY SIGN LENS. LIGHT OPS CHECKED OK.

Part: WIRE — UNSECURE (LT ENGINE) · airframe 26,824 hrs · 63,273 cycles

ATB, EN ROUTE TO DESTINATION, LT ENGINE SYS FAIL ALERT. FLASHING X ON TGT GAUGE. NO CURRENT FAULTS NR 1 EEC FAULT REVIEW SHOWS CODE 772103. TGT CIRCUIT FAULT CH-A/CH-B DISAGREE. REPAIRED WIRE 2A00G20 TO T1040-2 PER SWPM 20-20-01 AND SECURED WIRE CONNECTION AT T1041-2. OPS CHECKED PENDING. OPS CHECKED GOOD ON ENG. RUN PER FIM 77-21 TASK 803.

Part: COTTER PIN — OUT OF POSITION (FLAP DRUM) · airframe 26,757 hrs · 63,124 cycles

AT FLAP POSITION, SLATS EXTENDED 8, FLAPS 13, RECEIVED A DISAGREE 3, & 4 ALERT. DURING TROUBLESHOOTING, FOUND NO CABLE MOVEMENT WHEN SELECTING FLAPS 0 TO 13. FOUND A COTTER KEY ON K-2 DRUM BINDING ON CABLE GUIDE. REPOSITION COTTER KEY. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 24,967 hrs · 59,133 cycles

ATB, OUT OF 1200 FT ENG R COMP STALL LOUD BANG, SHOOK VIOLENTLY RETURNED TO AIRPORT. FOUND POSSIBLE LIGHT BIRD MATERIAL ON NR 2 ENG INLET COWL AND TAIL CONE AREA. PERFORMED FIM 72-00 TASK 801 AND AMM 72-00-00-200-801 INSP OF THE ENGINE AFTER SURGE BORESCOPE HP SECTION STAGE 1 THRU 10 NO DAMAGE OR DEFECTS NOTED. NR 2 ENG RUN PENDING CLOSE UP PENDING. PERFORMED BIRD STRIKE VISUAL INSPECTION PER AMM 05-52-01-210-801 AND INSPECTION OF ENGINE AFTER BIRD STRIKE ON NR 2 ENGINE PER AMM 72-00-00-200-804 NO DAMAGE OR DEFECTS NOTED OK FOR SERVICE.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 24,853 hrs · 58,879 cycles

CREW REPORTED THAT AFTER TAKEOFF, THE RT ENGINE COMPRESSOR STALLED AT 1000 FT, ALERT WENT AWAY AFTER FIVE SECONDS. ENGINE NORMAL INDICATIONS. NO LIMITATIONS EXCEEDED. ACFT RETURNED TO DEPARTURE. ACCOMPLISHED FIM TASK 72-00TASK 801, NO DEFECTS NOTED. LPC CHECKED GOOD, TAILCONE CHECKED GOOD. ACCOMPLISHED EEC 2 REMOVAL AND REPLACEMENT IAW AMM 73-21-01, OPS CHECKED GOOD, NO DEFECTS NOTED ON GROUND. OK FOR SERVICE.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 24,370 hrs · 57,800 cycles

HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED AT 19000 FT AFTER LEVEL OFF. RE-PRESSURE DID NOT WORK. R & R NR 1 EDP IAW AMM TASK 29-11-01-000-801. OPS AND LEAK CHECK GOOD.

Part: HYDRAULIC SYSTEM — CONTAMINATED (LEFT) · airframe 24,281 hrs · 57,598 cycles

LT HYD TEMP HI, ABORT ON TAKEOFF. BLEED LEFT HYD SYS AND QTY CK OK TO CONTINUE IAW AMM 12-13-01, AND AMM 29-00-00, BOTH HYD SYST. CK OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (RT MLG DOOR) · airframe 23,323 hrs · 55,445 cycles

GEAR DOOR "OPEN" ALERT APPEARED DURING APPROACH, THEN DISAPPEARED. R & R RT MLG DOOR ACTUATOR IAW AMM 32-34-03, UP TO STEP 3.D. 1, D. COMPLETED REMAINING STEPS OF AMM 32-34-03. OK FOR SERVICE.

Part: STRUCTURE — CORRODED (BUTE DOOR) · corrosion level 2 · airframe 23,059 hrs · 54,862 cycles

LEFT WING NR-2 BUTE DOOR INBD AND OTBD EDGES CHAFED AND SURFACE CORROSION. CORROSION, BLENDED OUT CHAFED AND CORRODED AREAS AT LT WING NR 2 BUTE DOOR AT BOTH INBD AND OTBD EDGES IAW SRM 51-10-04-OG-0. PERFORMED VT THICKNESS INSPECTION OF NR 2 BUTE DOOR AS FOLLOWS: OTBD EDGE ORIGINAL THICKESS .100, REMAINING .092, MATERIAL LOSS .008. INBD EDGE ORIGINAL MATERIAL, .040, REMAINING MATERIAL .021 MATERIAL LOSS .019. REF: NDT SPM 04-00-06. SRM 57-50-01-3. AFTER FURTHER EVALUATION FOUND INBD DOOR EDGE OUT OF LIMITS IAW SRM 57-00-00. REPAIRED L/W NR-2 BUTE DOOR INBD & OTBD EDGES IAW RES-WI CARD NR E105-477279-PERM AND SRM 51-10-04,57-00-00 AND NDT SPM 04-00-06, SRM 57-50-01-3.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 22,784 hrs · 54,257 cycles

FWD CARGO DOOR LOWER EDGE SKIN PULLED OUT BELOW DOOR HANDLE 30 INCHES FROM FWD EDGE 3' X .7500, .065 BENT OUTWARD. REPAIRED IAW DPS 2.70-13. DOOR SKIN. HFEC OK, NO CRACKS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,759 hrs · 54,199 cycles

EMERGENCY EXIT LIGHTS AT LT & RT AFT OVERWING EXITS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY B5-119 IAW AMM 33-51-03. OPS CHECK OK. OK FOR SERVICE.

Part: TIRE — DAMAGED (LT MLG) · airframe 21,735 hrs · 51,910 cycles

LEFT INBD MAIN GEAR TIRE DAMAGED. REMOVED AND REPLACED THE NR 2 MW ASSY IAW 32-41-01-000-803 AND AMM 32-41-01-400-802.

Part: ENGINE — MAKING METAL (LEFT) · airframe 17,888 hrs · 43,147 cycles

LT ENGINE HIGH VIBRATION, 6. METAL FOUND IN TAILPIPE. OPEN

Part: ACM — INOPERATIVE (LEFT) · airframe 16,513 hrs · 39,905 cycles

LEFT PACK OVERHEAT LIGHT ON TAXI IN WITH ODOR OF SMOKE. R & R LEFT ACM IAW AMM 21-53-01. LEAK AND OPS CHECKED GOOD.

Part: WIRE — BROKEN (MAINIFOLD) · airframe 14,941 hrs · 36,233 cycles

ON TAXI OUT, TAIL MANIFOLD FAIL LT ILLUMINATED COMPLIED WITH PROCEDURE. REINSTALLED RT HORIZ SENSOR (P1-1022A & B) CONNECTOR & SAFETIED. CLOSED PANEL. FOUND WIRE FRNR41021A-20 BROKEN AT CLAMP NEAR RECEPTACLE R5-1248 ON HORIZ STAB CTR SECTION. REPLACED LT HORIZ SENSOR ASSY D1-1021 COND SAME. PODS FAULT CODE 362160.//REPAIRED WIRE FRNR41021A-20 IAW SWPM 20-10-03. CONTINUITY CHECK GOOD. PERFORMED PODS RTS TEST. TEST PASSED. NO FAULTS NOTED IAW AMM 36-23-00.

Part: THROTTLE — FLUCTUATES (LT ENGINE) · airframe 14,484 hrs · 35,152 cycles

ATB - CLIMBING THROUGH 14,000' ENGINE L SYS FAIL LIGHT CAME ON. WHILE THROTTLE INDICATOR WAS FLUCTUATING ALONG W/THROTTLE. R & R THROTTLE MODULE IAW AMM 76?-01 7010/5295 ENG RUN PEND NR 1 ENGINE RUN ACCOMPLISHED ALL INDICATIONS NORMAL NO FAULTS FOUND, OK FOR SERVICE.

Part: ACCUMULATOR — RUPTURED (HYD SYSTEM) · airframe 13,729 hrs · 33,394 cycles

INTERMITTENT BRAKE PRESS LOW AFTER PUSHBACK. FOUND RT SYS BRAKE ACCUMULATOR AT 0 PRESS AND LEAKING. (RUPTURED DIAPHGRAM) REPLACED RT SYS BRAKE ACCUMULATORS IAW AMM32-44-01. OPS CK AND LEAK CK OK.

Part: ENGINE — FAILED (LEFT) · airframe 13,130 hrs · 31,996 cycles

LEFT ENG SYS FAIL. REMOVED AND REPLACED LT ENGINE. OPS AND LEAK CHECK GOOD.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 12,795 hrs · 31,227 cycles

NO CARGO SMOKE TEST. RESET C/B CARGO SMOKE TEST OK.

Part: CONTROL CABLE — BROKEN (LT SLAT) · airframe 12,759 hrs · 31,147 cycles

LT OUTBOARD SLAT NOT FULLY RETRACTED DURING WALK AROUND. FOUND NR 5 RETRACT CABLE NR 194A BROKEN. REPLACED RUN NR 194A PER DRW 5910451. ADJUSTED LT SLAT CABLES PER AMM 27-80 00.

Part: ENGINE — FAILED (NR 1) · airframe 12,454 hrs · 30,450 cycles

OPEN - ATB - AT TAKEOFF APPROX 10K FT NR 1 ENGINE FAILED, IFSD. ENGINE CHANGE IN WORK.

Part: MOTOR — INOPERATIVE · airframe 10,418 hrs · 25,604 cycles

PRIMARY TRIM INOP. REMOVED AND REPLACED PRIMARY TRIM MOTOR PER AMM 27-41-10. OPS AND SECURITY CK OK.

Part: ENGINE — FAILED (RIGHT) · airframe 9,541 hrs · 23,479 cycles

ATO - RT ENGINE FAILED 110 KNOTS ON TAKEOFF. FOUND RT ENGINE BLOWN. REMOVED RT ENGINE ASSY PER AMM144. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (SMOKE DETECTOR) · airframe 9,380 hrs · 23,080 cycles

FWD CARGO SMOKE DETECTOR "PUSH" SWITCH FLASHING. ACCOMP FIM 26-11 TASK 803 GND CK OK NO FAULTS. OK FOR SERVICE.

Part: ANTI-SKID SYS — CHATTERING (LT MLG) · airframe 8,530 hrs · 21,013 cycles

BTB - LEFT BRAKE CHATTERING WHEN APPLIED. ACCOMPLISHED FIM 32-40 TASK 804 FOUND INTERNAL FAULT ON BCU 32431E AND 32431D. REMOVED AND REPLACED BCU PER AMM 32-45-01 ACCOMPLISHED RTS PER ANTI-SKID CHECK OK BLED BRAKES PER AMM 32-43-01. LEAK CHECK OK SERVICED FLUID AS REQUIRED TAXIED CHECK OK.

Part: WHEEL — CRACKED (MLG) · airframe 7,896 hrs · 19,488 cycles

NR 3 MAIN TIRE WORN. UPON FURTHER INSPECTION FOUND OUTER WHEEL HALF TO BE CRACKED. REPLACED NR 3 MAIN TIRE ASSY PER AMM32-41-01. BRAKE CHECK OK, SPIN CHECK OK. P/N 3910797-513, S/N ON B0652, OFF B0769.

Part: LIMITER — FAILED (RUDDER) · airframe 7,874 hrs · 19,431 cycles

BTB: FWD PITOT FAIL LEVEL 1 NO TAKEOFF ALERT. REMOVED AND REPLACED RUDDER LIMITER PITOT IAW AMM 34-1 1-02. OPS CHECK OK. LEAK CHECK OK IAW AMM 34-11-00.

Part: GENERATOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 7,749 hrs · 19,125 cycles

BTB - ENG R SYS FAIL ANNUNCIATION LIGHT ILLUMINATED. ACCOMP FIM TASK 73-21 TSK 812 FOUND RT ENG DEDICATED GEN STATOR CHANNEL -A- FAULT CODE 732111. REMOVED NR 2 ENG DEDICATED GEN STATOR PER AMM 73-21-04. INSTALLED SERVICEABLE DGS PER AMM 73-21-04 ENGINE RUN & LEAK CHECK GOOD. NO FAULTS NOTED. OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (AILERON TRIM) · airframe 7,605 hrs · 18,779 cycles

BTB - ON PUSH BACK "AILERON TRIM FAIL" ILLUMINATED. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR PER AMM 27-12-03, OPS CK OKAY.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 7,466 hrs · 18,435 cycles

SMALL CRACK TOP OF CAPTAIN WINDSHIELD. REMOVED AND REPLACED CAPTAIN WINDSHIELD PER MM 56-11-02. LEAK CHECK AND FUNCTIONAL TEST OF WINDSHIELD ANTI-ICING CHECKS OK IAW AMM 50-11-02.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 7,464 hrs · 18,429 cycles

DURING APPROACH AUTO THROTTLES ARE NOT HOLDING THE SELECTED SPEED, OFTEN ALLOWING IT TO DROP 5 KTS TO REF WITHOUT ADVANCING THROTTLES, MUST BE OVERRIDDEN MANUALLY. PERFORMED FIM 22010 TASK 801. GND CHECK OK. OK FOR SERVICE.

Part: ATTACH ANGLE — CRACKED (PYLON) · airframe 7,421 hrs · 18,325 cycles

APPROX 1.25 INCH CRACK ON UPPER PYLON TRAILING EDGE ATTACH ANGLE AT STA CANTED 1178 LT. REPAIRED PER HALM105 FILE 477101.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 7,418 hrs · 18,317 cycles

TAKEOFF INITIAL POWER APPLICATION COMPRESSOR STALL - BANG & -ENGINE LEFT COMPRESSOR STALL- ALERT FOLLOWED BY HIGH TGT. SHUTDOWN ENGINE WITH FUEL LEVER. REMOVED NR 1 ENGINE PER HAL M144-717. INSTALLED ENGINE PER HAL M143-717. GROUND RUN CHECKED GOOD. OK FOR SERVICE.

Part: COWLING — CRACKED (NR 1) · airframe 7,421 hrs · 18,325 cycles

APPROX 3 INCH LONG CRACK ON LT UPPER COWL ATA FAN AIR OUTLET. REMOVED & REPLACED TOP COWL ASSY PER AMM71-12-01. P/N 715-4010-509, S/N ON 279001, OFF 247001.

Part: INTERFACE UNIT — MALFUNCTIONED (NR 1) · airframe 7,273 hrs · 18,057 cycles

SECOND BTB - VIA FAULT. REMOVED AND REPLACED NR 1 VIA, GROUND CHECK OK PER MM 31-43-01-4.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 7,413 hrs · 18,305 cycles

ATB - AIR SYS FAULT ILLUMINATED AFTER 5 MIN IN FLIGHT. REMOVED AND REPLACED FAN AIR VLV PER AMM 36-13-04, OPS CHECK OKAY. NO FAULTS INDICATED.

Part: FILTER — DIRTY (COCKPIT) · airframe 7,409 hrs · 18,296 cycles

ATB - INFLT OVER LNY - AIR SYS FAULT. PER DISPATCH LDG OGG. FLT DIVERT TO OGG, PSC BITE SHOWED -L FAN AIR VLV- FAULT. REMOVED, CLEANED AND REINSTALLED INLINE FILTERS IN THE LEFT FAN AIR VALVE AND LEFT PRSOV PILOT VALVE. OPS CHECK GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 7,409 hrs · 18,296 cycles

AFTER PARKING, FLIGHT ATTENDANTS ADVISED SMOKE SMELL BRIEFLY NOTICED SHORTLY BEFORE PARKING. OBSERVED STRONG ODOR OF ELECTRICAL SMOKE IN FWD CARGO AFTER PARKING. AFTER REMOVAL OF BAGS FROM FWD PIT. NO SMELL NOTED. ACCOMPLISHED GEN CHECK PER AMM24-21-00-710-802. OPS CHECKS OK.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 7,380 hrs · 8,223 cycles

EMERG LIGHT ROW 8 INOP, WIRE PULLED OUT OF PLUG. SECURED WIRE AT ROW 8 SEAT CONNECTOR. LIGHT OPS CHECK OK.

Part: DISPLAY — FAULTED (COCKPIT) · airframe 7,353 hrs · 18,163 cycles

CAPT'S AND F/O MCDU FREEZE UP. REBOOTED VIA NR 1 AND NR 2 OPERATIONAL CHECK OK.

Part: BEARING — FAILED (ENGINE)

ON CLIMBOUT AT 16,00 FEET GOT (ENG R SURGE) LIGHT. FOLLOWED BY SOME SMOKE IN CABIN. FOLLOWED BY (ENG R SYS FAIL) LIGHT AND (R OIL FILTER) LIGHT. REDUCED POWER ON RT ENGINE RETURNED FOR LANDING. RT ENGINE INDICATIONS WERE NORMAL AFTER POWER REDUCTION. HOWEVER AFTER LANDING SOME VIBRATIONS. ENGINE SHUTDOWN AFTER LANDING. FOUND METAL IN GEAR BOX SUMP SUSPECT BEARING FAILURE ENGINE REPLACED. TEARDOWN REPORT TO FOLLOW. (K)

Part: MODULE — STUCK (RUDDER TRIM)

AILERON TRIM STUCK IN LT WING DOWN. REMOVED AND REPLACED AILERON AND RUDDER TRIM CONTROL MODULE IAW SRM. (K)

Part: ENGINE — SHUTDOWN (NR 2)

FLT 514 - OGG - NR 2 ENGINE INFLIGHT SHUTDOWN, RETURNED TO LIH, WHERE AN UNEVENTFUL LANDING WAS MADE. REPAIR IN WORK. (M)

Part: FRAME — CORRODED (FUSELAGE)

HNL - FOUND LEVEL 2 CORROSION ON THE LOWER HORIZONTAL LEG OF THE 5971057-3 AND 4 FRAMES AT BS 852. CORROSION WAS 100 PERCENT THROUGH HORIZONTAL LEG OF THE FORM AT THE SCREW ATTACH POINTS ON THE LOEWR SIDE. DAMAGE WAS REMOVED BY TRIMMING AND INSTALLING AN ANGLE DOUBLER. (M)

Part: SKIN — CORRODED (RT WING AILERON)

HNL - LEVEL 2 CORROSION ON RIGHT AILERON UNDER THE 9957571-23 RUBSTRIP IS BETWEEN XA 374.00 AND XA 382.125. THE CORROSION AFFECTED THE 995757-34 DOUBLER AND 9957571-36 SKIN. THESE 2 PARTS HAD 100 PERCENT CORROSION PENETRATION. THE AILERON WAS REPLACED PER BOEING MM. (M)

Part: SHAFT — CRACKED (APU DOOR)

MAINTENANCE ENTRY: APU DOOR SHAFT WELD, CRACKED. REMOVED DOOR AND ROUTE TO AOH. NO ACCEPTABLE REPAIR, OK TO CONTINUE PER CDL ENTERED ON MIC SHT (DOOR REMOVED).