N486HA

Part: FRAME — CORRODED (ZONE 100) · airframe 34,165 hrs · 79,311 cycles

NUMEROUS CORROSION ON FRAME 1138 (M). CUTOUT APPROX 4 INCHES OF OUT OF LIMITS CORROSION ON STA 1138 FRAME BETWEEN LEFT L29 AND L30, HFC CUTOUT NO CRACKS NOTED. REMOVED REMAINING S/C AT STA 1138 FRAME , CLEANED AND TREATED PRIME AND PAINTED PER SRM 51-10-04 M

Part: BRACKET — CORRODED (ZONE 10) · airframe 34,165 hrs · 79,311 cycles

SURFACE CORROSION ON "L" BRACKET UNDER MAINT PLATFORM STATION 1095 . MARKED. 1. REMOVED TEE EXTRUSION FROM WALKWAY STRUCTURE. FABRICATED NEW TEE PER BOEING DRAWING# 9915537. TREATED, PRIMED AND PAINTED PER SRM 51-22-01. INSTALLED NEW TEE PER BOEING DRAWING# 9915537.

Part: SPRING — FAULTED (ZONE 700) · airframe 33,704 hrs · 78,318 cycles

AFTER T/O LEFT GEAR UNSAFE LIGHT ILLUMINATE WITH GEAR HANDLE UP. REMOVED AND REPLACED UP LATCH SPRING FOR LEFT MLG DOOR. OPS CHK AND SECURITY CHK OK. OK FOR SVC.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 33,170 hrs · 77,143 cycles

ENG R COMP STALL IN CRUISE. COMPLIED WITH QRH PROCEDURE. "ENGINE VIB HI" AT HIGH POWER SETTINGS. PREPPED FOR BOROSCOPE INSP. PER AMM 72-00-00-200-801 TO STEP 2E(7). REMOVED 5 BYPASS PANEL AND 4 OF THE CORE COMPRESSOR PANELS PER FOM. 20807. COMPLETED BORESCOPE OF STAGE 2 & 3 LPC - NO DAMAGE FOUND 5895 BORESCOPED HPC, COMB CHAMBER NGVS HPT LPT PICS SENT TO POWERPLANT ENGINEERING. PERFORMED HIHG POWER RUN. NO COMPRESSOR STALL OR HI VIB NOTED. DURING BORESCOPE FOUND MISSING MATERIAL AROUND FUEL NOZZLE HEAT SHIELD, NO 2 ENGINE. OK TO CONTINUE PER AMM 72-40-00-200-801. ENG #2 NEEDS TO BE REPLACED WITHIN 60 CYCLES.

Part: ENGINE — FAULTED (LEFT) · airframe 32,942 hrs · 76,651 cycles

FLIGHT DECK CREW AND CABIN HEARD 2 LOUD POPS. ENG LEFT COMPRESSOR STALL ALERT CAME ON. CREW FOLLOWED QRH CHECKLIST, LEFT ENGINE WAS SHUT DOWN. ENG GAUGES SHOWED ERRATIC INDICATIONS. TGT WENT TO 940. REMOVED #1 ENG PER TC E1128-717-72-003-REMOVAL. INSTALLED #1 ENG PER TC E1128-717-72-003-INSTALL. OPS CK LEAK CK GOOD. OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,927 hrs · 76,618 cycles

FWD ATTENDANT WORK LIGHT AND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSEMBLY AND POWER SUPPLY PER AMM 33-51-03. OPS CHECK GOOD. OKAY FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,763 hrs · 76,260 cycles

EMER LT. NOT STAY ON. REMOVED AND REPLACED 13 EA CABIN EMERGENCY EXIT LIGHT BATTERIES PER AMM 33-51-03/401. OPS TEST GOOD. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,526 hrs · 75,754 cycles

EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY POWER SUPPLY PER AMM 33-51-06. OPERATION GOOD.

Part: NONE — NONE · airframe 30,741 hrs · 71,781 cycles

EMERGENCY LIGHTS IN CEILING FROM ROW 4 TO 11 INOP AND CEILING TAIL CONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY B5-116 AND B5-227. OPS CHK GOOD OK FO SERVICE PER 33-51-03

Part: NONE — NONE · airframe 30,184 hrs · 70,538 cycles

ATB - ENG R SYS FAIL ON CLIMBOUT // REFERENCE LOG PG 878257-2 FOR CH B REPLACED LUG ATT1043-2, PERFORMED WIRING CHECKS PER FIM 73-21 TASK 875 FOR CH A ALL WIRING CHECKS OK. MECH 5970 2/23/22 OPS CHECK PENDING. OPS CHECK OK OK FOR SVC

Part: COVER — ABNORMAL · airframe 29,989 hrs · 70,097 cycles

EMER EQ - SLIDE - FORWARD SERVICE DOOR GIRT BAR DISCONNECTED FROM EMERGENCY SLIDE // RESECURED FWD SVC DOOR COVER. FOUND SLIDE COVER DISENGAGED. SECURITY CHK GOOD. OK FOR SVC

Part: CYLINDER — DEFECTIVE (MLG DOOR) · airframe 29,008 hrs · 67,877 cycles

LANDING GEAR DOOR - GEAR DOOR OPEN ALERT LOWERING LANDING GEAR. ALERT REMAINS FOR 15 SECONDS BEFORE EXTINGUISHING. // REMOVED + REPLACED L/H MLG DOOR ACTUATOR CYLINDER PER AMM 32-34-03. OPS / LEAK CHECK OK

Part: RING — CORRODED (NR 1 ENGINE) · airframe 28,396 hrs · 66,524 cycles

OPEN - ENGINE 1 SYSTEM FAIL, UNABLE TAKEOFF POWER. // ACCOMPLISHED BOROSCOPE, FOUND VSV RING AND SUSPECTED CORROSION CAUSING VSV RING TO BIND. REPLACEMENT OF ENGINE IN WORK.

Part: RELAY — FAILED (ELEVATOR) · airframe 28,379 hrs · 66,492 cycles

AUTO TRIM FAIL ILLUMINATED DURING DESCENT APPROXIMATED 10000 FEET. WARNING WENT OUT AFTER LANDING.// REMOVED AND REPLACED ELV UP AND DOWN TRIM REPLAY PER 27-43-0. RTS PASSED PER 22-00-00. ALL TEST PASSED. OK FOR SERVICE.

Part: CABLE — OUT OF POSITION (TAILCONE) · airframe 28,348 hrs · 66,423 cycles

TAIL CONE JETTISON KEVLAR CABLE ROUTED INCORRECTLY FROM PAINT. // RE-ROUTED TAIL CONE RELEASE KEVLAR CABLE PER AMM 53-52-01, SECURITY CHECK OK.

Part: FLOOR SUPPORT — CORRODED (BS 1037) · corrosion level 2 · airframe 27,993 hrs · 65,684 cycles

FOUND CORROSION ON FLOORTRACK OF RH SIDE OF FUSELAGE AT STA 1037//REPAIRED FLOOR PANEL SUPPORT PER E105-486293-PERM

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,953 hrs · 65,591 cycles

BATTERIES FOR EMERGENCY PER NOT CHARGING. REMOVED AND REPLACED 3 BATTERIES PER AMM 24-34-01. BATTERIES CHECK GOOD.

Part: WATER SEPARATOR — ODOR (CABIN AIR) · airframe 27,680 hrs · 64,992 cycles

ON GROUND BURNING OIL SMELL WHEN PACKS ON APU. APU BLEED AIR MODULATING VALVE. REMOVED AND REPLACED BOTH WATER SEPERATORS FOR AIR CONDITIONING. APU COMPARTMENT INSPECTED. NO OIL LEAK. REACTIVATED APU BLEED AIR VALVE AND PERFORMED APU RUN, CHECKED NO OIL SMELL IAW AMM 21-54-01. OK FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 27,011 hrs · 63,483 cycles

ATB / RIGHT MAIN GEAR "RED" INDICATION UPON RETRACTION. THREE GREEN ON DOWN POSITION.// REMOVED AND REPLACED MLG DOWN/LOCK PROX SENSOR ASSY PER AMM TASK 32-61-04-000-801.

Part: UNKNOWN — ODOR (AIR CON SYSTEM) · airframe 26,805 hrs · 63,024 cycles

FA'S REPORT FOUL SMELL COMING FROM CABIN A/C.PERFORMED FIM 21-22 TASK 815. NO DEFECTS NOTED. AS PRECAUTION REPLACED BOTH COALESCER BAGS PER AMM 21-54-08. OPS TEST OK. NO FURTHER ODOR NOTED.

Part: SENSE LINE — CONTAMINATED (NR 1 ENGINE) · airframe 26,495 hrs · 62,351 cycles

IN ALT (FADEC) WITH THROTTLES AT IDLE, ENG 1 STUCK AT 71% N1 FOLLOWED BY ENG COMP STALL LEFT, AFTER 3 MIN ENG WENT TO IDLE. PERFORMED WIRING CHECK ON OIL PRESSURE TRANSDUCER (CHANNEL B) PER 79-33-802. WIRING OK. DISCONNECTED P30+P50 LINES, EEC TO P50 MANIFOLD BLEW OUT, WATER IN P#) LINE RECONNECTED PER AMM 73-21-06-000-801. PERFORMED CONTINUITY CHECK WIRE HARNESS NR L ENG FMU TO EEC CHANNELS A AND B PER WDW 73-24-01 SHIELD TO GROUND CHECKED OK, PER FIM 72-00 TASK 801. PERFORMED BORESCOPE ON NR 1 ENG COMPRESSOR SECT, PER AMM 72-00-00-200-801, NO DEFECTS WERE NOTED, BUT NOTICED THE CONNECTOR "A/F" ON THE FMU HAD A LOOSE BACK SHELL. TIGHTENED BACK SHELL AND CONNECTOR. PERFORMED HIGH POWER RUN AND OPS CHECK GOOD, NO DEFECTS NOTED, COULD NOT DUPLICATE DISCREPANCY.

Part: FMU — MALFUNCTIONED (NR 1 ENGINE) · airframe 26,498 hrs · 62,355 cycles

DIVERSION - APPROACHING OUT CRUISE ALTITUDE OF 25000' WE HAD A "ENG L SYS FAIL AND ENG L FADEC ALTN" PERFORMED QRH LEFT ENG INDICATING HAD A X TALKED TO MTN AND DIVERTED TO THE NEAREST AIRPORT, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACE NR 1 ENG FMU PER AMM 73-21-03-000-801 AND AMM 73-21-03-400-801 UP TO STEP 3.F(2), LEAK CHECK PENDING. OPS CHK PENDING. REMOVED AND REPLACED NR 1 EEC PER AMM 73-21-01-000-801 & 73-21-01-400-801. RETURN TO SERVICE OK. COMPLETED REMAINING STEPS FOR FMU LEAK AND OPS CHECK PER AMM 73-21-03-400-801. LEAK CHECK AND OPS GOOD.

Part: EEC — FAULTY (LT ENGINE) · airframe 26,495 hrs · 62,350 cycles

DURING CRUISE AT FL250 AMBER X DISPLAYED ON LEFT EPR AND SELECT FADEC L ALTN DISPLAYED. BONDING CHECK OFF NR 1 ENG EEC CHECK OK. REMOVED AND REPLACED EEC CONTROLLER NR 1 LT PER AMM 73-21-01-410-801 RTS OK.

Part: CONNECTOR — DAMAGED (RESERVOIR) · airframe 25,981 hrs · 61,211 cycles

RIGHT HYD TEMP HIGH DURING TAXI OUT. REMOVED AND REPLACED THE RT HYD RESERVOIR HIGH WARNING TEMP PLUG IAW WDM 29-33-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: RESERVOIR — CONTAMINATED (HYDRAULIC SYS) · airframe 25,404 hrs · 59,934 cycles

ON TAXI OUT, "HYD R TEMP HI" MASTER CAUTION. BLEED RIGHT HYD RES. CYCLED ALL KNURLED KNOBS. RAN PUMPS MESSAGE DID NOT RETURN.

Part: FUEL LINE — LEAKING (APU) · airframe 25,335 hrs · 59,784 cycles

AFTER STARTING APU, NOTICE A STRONG FUEL ODOR, SHUT APU DOWN AND FUEL ODOR WENT AWAY. FOUND FUEL LEAKING FROM APU FCU HARD LINE TO FUEL NOZZLE. REMOVED AND REPLACED FCU HARD LINE PER AMM 49-32-01. LEAK CHK OPS OK. ODOR NO LONGER PRESENT. OK FOR SVC.

Part: RELAY — FAILED (TRIM MOTOR) · airframe 24,124 hrs · 57,079 cycles

BURNING ODOR NOTICED AFTER LANDING. PERFORMED FIM 21-22-815 FOR ODOR. RAN NR 1 & 2 ENGINES SPERATELY. AS NR 1 AND 2 PACKS ISOLATED, COULD NOT DUPLICATE ON GROUND. OPS OF PACKS NORMAL ON GROUND. OK TO CONTINUE. NO EVIDENCE OF ODOR. ON SUBSEQUENT FLIGHT FA REPORTED AN ODOR. PRIMARY STAB DRIVE RELAY IN FWD CARGO WAS FOUND BURNED. REMOVED AND REPLACED THE NOSE DOWN TRIM MOTOR RELAY IAW AMM 27-41-03-400-801. RAN TRIM MOTOR OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 23,482 hrs · 55,662 cycles

WHILE ENROUTE, RED GEAR UNSAFE LIGHT ILLUMINATED ON RT GEAR AND ON CONFIGURATION PAGE. PERFORMED INSPECTION OF RT MLG DOOR LATCH IAW AMM 32-34-01. NO DEFECTS NOTED. PERFORMED INSPECTION OF RT MLG PROXIMITY SENSOR. ADJUSTED SENSOR IAW AMM 32-61-00. OK FOR SERVICE.

Part: WASHER — DAMAGED (NLG) · airframe 22,089 hrs · 52,498 cycles

NLG LOWER SPRING BEVEL WASHER BELOW TRUNNION DAMAGED AND REMOVED. R & R NLG BELLEVILLE WASHER IAW AMM 32-21-01. SERVICE AND LUBRICATED NLG STRUT. SECURITY CHECK GOOD OK FOR SERVICE.

Part: TIRE — SEPARATED (MLG) · airframe 20,722 hrs · 49,454 cycles

TIRE RECAP PEELING RT MAIN INBD TIRE. REPLACED NR 3 MAIN TIRE IAW AMM 32-41-01. CONDITION & SECURITY OK, TORQUE & SPIN CK OK AND CHECKED DENTS ON T/E FLAP. DENT NR 1-1" X 1.5" X .0625"-7" FROM T/E & 33" FROM INBD EDGE ON T/E FLAP. DENT NR 2-1" X 2" X .0312"-9" FROM L/E & 29" FROM INBD EDGE ON T/E FLAP. INSPECTED BOTH DENTS & FOUND NO CRACKS, SHARP EDGES, CREASES, OR GOUGES. ACFT OK FOR SERVICE. NO OTHER DAMAGE NOTED ON ACFT. ACFT OK IAW FORM E105-486203-INI. INSPECTED NR 1 & NR 2 ENGINE INLET & COWLINGS & NO DAMAGE NOTED. ACFT OK TO CONTINUE.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 20,667 hrs · 49,336 cycles

EMERGENCY LIGHT WIRES 6F FOUND LOOSE DURING PREFLIGHT. SECURED EMERGENCY LIGHT WIRE AT 6F. SECURITY, OPS CHECKED GOOD. OK FOR SERVICE.

Part: ENGINE — VIBRATION · airframe 20,417 hrs · 48,779 cycles

ENGINE VIBRATION HIGH ALERT FOLLOWED BY SUDDEN GROWLING NOISE, CLIMBING THROUGH 5000 FEET LT N2 VIB. REACHED 6.2 AND DROPPED LOWER WITH REDUCED POWER. ALL OTHER ENGINE INDICATIONS NORMAL. AIR TURN BACK.

Part: BOLT — FAILED (SLAT DRIVE) · airframe 20 hrs · 47,713 cycles

DURING AN A-CHECK, FOUND A MISSING NAS6204-9, BOLT COMMON TO THE RT WING SLAT DRIVE ASSY. CONFIRMED THAT THE BOLT WAS MISSING BECAUSE OF THE NAS679A4. NUT WAS DETACHED FROM THE UNSCATHED BOLT. AND AFTER CHASING THE MISSING BOLT, DISCOVERED THAT THE AFT DRIVE SUPPORT PLATE, THAT IS COMMON TO THE 5971724-2 ASSY, WAS COMPLETELY SEVERED IN HALF. AFTER REMOVAL OF THE 5971724-2 SLAT DRIVE ASSY, THEN DISCOVERED THAT THE MATING BRACKET, REF PN 9919398-8, COMMON TO THE WING L/E SUPPORT INSTALLATION AT XRS 148.125, WAS ALSO CRACKED NEAR THE ATTACHMENT LOCATION THAT FAYS WITH THE SLATE DRIVE ASSY, CURRENTLY IN THE PROCESS OF REPLACING BOTH PART ASSEMBLIES.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 19,842 hrs · 47,465 cycles

PRIMARY TRIM FAILED DURING FLIGHT. ALT TRIM OK. TROUBLESHOT PRIMARY TRIM FAULT IAW FIM TASK 27-40, TASK 801, PERFORMED OPS CHECK OF THE PRIMARY TRIM DRIVE MOTOR IAW AMM TASK 27-41-10-710-801. OPS CHECK NORMAL ON GROUND, OK FOR SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 19,842 hrs · 47,465 cycles

PRIMARY TRIM FAILED DURING FLIGHT. ALTERNATE TRIM OK. TROUBLESHOT PRIMARY TRIM FAULT IAW FIM TASK 27-40 TASK 801, PERFORMED OPS CHECK OF THE PRIMARY TRIM DRIVE MOTOR IAW AMM TASK 27-41-10-710-801, OPS CHECKED NORMAL ON GROUND, OK FOR SERVICE.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 19,692 hrs · 47,121 cycles

DURING FLIGHT, RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE. R & R RT MAIN GEAR ACTUATOR HOSE ASSY SERVICED HYDRAULICS. LEAK TESTED GOOD. OK FOR SERVICE. HYDRAULIC PRESSURE GOOD.

Part: FAN — UNKNOWN (OIL COOLING) · airframe 18,951 hrs · 45,504 cycles

APU AUTO SHUTDOWN. R & R APU OIL COOLING FAN ASSEMBLY IAW AMM 49-50-01, LEAK AND OPS CHECKED GOOD.

Part: TIRE — FAILED (NR 4) · airframe 18,003 hrs · 43,333 cycles

NR 4 TIRE FAILURE CAUSED NR 2 ENG ATTRITION LINING DAMAGE AT 3 PLACES FROM 10 TO 11 0'CLOCK POSITION. INSTALLED NR 2 ENG IAW HAL M143-717. OPS AND LEAK CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE) · airframe 18,003 hrs · 43,333 cycles

ON TAKEOFF CLIMB AT 1000FT MSL RT ENGINE SYS FAIL CAUTION LIGHT CAME ON. YELLOW X CAME ON OVER TGT. TGT FLUCTUATED 10-20 DEG NO EXEEDANCE. EEC-2 FAULT CODE 772103. ACCOMPLISHED FIM 77-21, TASK 803. BITE CHECK EEC-2. NO FAULTS NOTED ON GROUND RUN OK TO CONTINUE.

Part: TIRE — SEPARATED (NR 4) · airframe 17,077 hrs · 41,176 cycles

NR 4 MAIN TIRE, RECAP SHOWING. OTBD TREAD SEPARATED. R & R NR 4 MAIN TIRE IAW AMM 32-41-01, SPIN CHECKED GOOD.

Part: BRAKE — OVERHEATED (NR 1 MLG) · airframe 16,109 hrs · 38,893 cycles

HOT BRAKES AT NR 1 MLG REACHED AT 450 DEGREES. FAN COOLED NR 1 MLG BRAKE. OK TO CONTINUE IAW AMM 32-47-00, INSPECTED BRAKES & FUSE PLUG. CHECKED OK, NO FAULTS NOTED.

Part: DETECTION SYS — MALFUNCTIONED (CARGO BAY) · airframe 14,988 hrs · 36,288 cycles

ON PREFLIGHT AFTER CARGO SMOKE TEST BUTTON RELEASED "ABENT 1 DISCH" BUTTONS CONTINUED TO FLASH & CARGO SMOKE ANNUNICATED ON EAD & ATR PAGE. RESET NR 1 VIA PERFORMED CARGO SMOKE TEST IAW MM26-13-01-710-801. OPS CHECKED NORMAL.

Part: EEC — FAILED (RT ENGINE) · airframe 13,765 hrs · 33,425 cycles

ENROUTE "ENG R SYS FAIL" LIGHT CAME ON - ATB. ACCOMPLISHED RT EEC BITE PROCEDURE 73-21, TASK 801. SHOW FAULT CODE 732165 & 166 & MX MSG 732140, START SWITCH LATCH CIRCUIT CH-B. FIM 73-21, TASK 839 START SW LATCH CIR CH-B ACC IAW FIM NR2 ENG EEC NEEDS REPLACE 5743. R & R RT EEC IAW AMM 73-21-01. GROUND RUN OPS CHECK OK. NO FAULTS.

Part: CONNECTOR — DEFECTIVE (HYDRAULIC SYS) · airframe 13,523 hrs · 32,843 cycles

ATB - AFTER T/O MESSAGE HYD R TEMP HI ILLUMINATED. REPLACED ELECTRICAL PLUG FOR RIGHT HYD TEMP HI SWITCH. OPS CHECK OK, WDM 29-33-01.

Part: HINGE — CRACKED (APU DOOR) · airframe 13,472 hrs · 32,727 cycles

APU RT ACCESS DOOR HINGE CRACKED AFT END. REMOVED CRACKED HINGE, REPAIRED IAW M-105 PRIMED AND PAINTED HINGE. PICKED UP FASTENER HOLES ON NEW DOOR HINGE. INSTALLED DOOR.

Part: FASTENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,472 hrs · 32,727 cycles

LEVEL 2 CORROSION ON HI - LOKS BETWEEN STATION 1053 AND 1076, LONGERON 25R. REPLACED CORRODED FASTENERS. PRIMED AND PAINTED PER SRM 51-22-01.

Part: FASTENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,472 hrs · 32,727 cycles

LEVEL 2 CORROSION ON FASTENERS AT LONG 22 RT END FITTING, STA 1053. REPLACED RUSTED FASTENERS. PRIMED AND PAINTED PER SRM 51-22-01.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,472 hrs · 32,727 cycles

LEVEL 2 CORROSION ON END CAP AT STATION 1053 LONGERON 23RT. REMOVED AND REPLACED END CAP PRIMED AND PAINTED PER SRM 51-22-01.

Part: FORMER — CORRODED (BS 116) · corrosion level 2 · airframe 13,472 hrs · 34,727 cycles

LEVEL 2 CORROSION ON FORMER AT STA 1116 AT LONG 24RT. REMOVED FORMER, FABRICATED FORMER IAW DWG 9957714. INSTALLED FORMER AT STA 1116, LONG 24RT.

Part: INTERCOSTAL — CORRODED (BS 1087) · corrosion level 2 · airframe 13,472 hrs · 32,727 cycles

LEVEL 2 CORROSION ON FORMER AND INTERCOSTAL AT STA 1087 AT LONGERON 24 RT. REMOVED FORMER, FABRICATED , PRIMED AND PAINTED. INSTALLED FORMER IAW M-105, FILE B10091, REV E.

Part: EXHAUST DUCT — LEAKING (APU) · airframe 13,472 hrs · 32,727 cycles

EVIDENCE OF EXHAUST LEAK AT APU ELBOW TO LOWER BELLOWS FLANGE AREA. FOUND SEARED BOLTS ON ELBOW FLANGE. REMOVED ELBOW. FOUND ELBOW FLANGE CRACKED 360 DEGREES. REMOVED 5 EA NUT PLATES WITH SHEARED STUDS AND REPLACED NUT PLATES. INSTALLED ELBOW ASSY IN THE EXHAUST IAW AMM 49-81-02-400-801. LEAK CHECK OK.

Part: BRACE — CRACKED (FUSELAGE) · airframe 13,472 hrs · 32,727 cycles

CRACK IN SIDEWALL CROSS BRACE BEHIND ACCESS PANEL 181HR. AFT CARGO COMP. R & R SIDEWALL CROSS BRACE. SECURITY CHECK OK.

Part: ATTACH BRACKET — CRACKED (TE FLAP) · airframe 13,472 hrs · 32,727 cycles

ATTACH BRACKET CRACKED, FOR RT FLAP MID HINGE FWD FAIRING (BRACKET MOUNTED ON FOOTBALL PANEL, 620EB. REMOVED AND REPLACED BRACKET FOR FWD FLAP MID HINGE FAIRING.

Part: ENGINE — STALLED (NR 2) · airframe 12,919 hrs · 31,450 cycles

UPON CLIMB-OUT PAST 18,500' HAD ALERT "ENGINE RIGHT COMP STALL". DUE TO MULTIPLE COMPRESSOR STALLS, HAD TO SHUT DOWN ENGINE. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (SUPPLY TEMP) · airframe 12,399 hrs · 30,249 cycles

DURING START LEVEL 2 LT TEMP HI ON. REMOVED AND REPLACED (L) SUPPLY TEMP SENSOR IAW AMM 36-13-07. OPS AND LEAK CHECK OK.

Part: SWITCH — OUT OF POSITION (SMOKE TEST) · airframe 12,371 hrs · 30,185 cycles

LAV SMOKE SIGN ON AFT LAV ILLUMINATED. FOUND TEST SW IN TEST POS RESET SW. OPS CK GOOD.

Part: ENGINE — SMOKE (NR 2) · airframe 12,176 hrs · 29,725 cycles

WHITE SMOKE FROM NR 2 ENG. RETURNED TO GATE. PERFORMED GENERAL VISUAL INSP OF NR 1 AND NR 2 ENGINES. NO FAULTS NOTED. PERFORMED NR 1 AND NR 2 ENG RUNS IAW AMM 71-00-04, NO FAULTS NOTED ON GROUND. PARAMETERS NORMAL, OK TO CONTINUE.

Part: RETAINER — CRACKED (NT 2 PYLON) · airframe 11,686 hrs · 28,601 cycles

NR 2 ENGINE PYLON T/E FWD LOWER GAP SEAL RETAINER CRACKED. REPAIRED PER HAL M-105 FILE NR 486106.

Part: ISOLATOR — GOUGED (NR 2 NACELLE) · airframe 11,686 hrs · 28,601 cycles

GOUGE ON NR 2 ENGINE FWD UPPER ISOLATOR. REMOVED AND REPLACED NR 2 FWD UPPER ISOLATOR PER TASK 71-20-05-000-801, 71-20-05-400-801.

Part: SEAL — DAMAGED (NR 2 NACELLE) · airframe 11,686 hrs · 28,601 cycles

1 INCH CRACK ON THE NR 2 ENGINE LOWER APRON FIRE SEAL L/E 2ND FASTENER HOLE. REPAIRED PER HAL-M-105. FILE NR B10196.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 10,804 hrs · 26,540 cycles

LAVATORY SMOKE DETECTOR WARNING LIGHT STAYS ON. FUNCTIONAL TEST OF THE LAVATORY SMOKE DETECTORS PER FIM 26-14-01. NO FAULTS FOUND. OPS CK GOOD OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,774 hrs · 26,455 cycles

BTB - UPON TAXI OUT F/A REPORT SMOKE IN CABIN WITH ODOR. POSSIBLE ELECTRIC. ACCOMPLISHED INSPECTION PER AMM 21-00-00-710-805, 803 AND 801 NO SMOKE IN CABIN OR ODOR. NO ELECTRICAL ODOR NOTED, CABIN ELECTRICAL SYS CHECK OK. APU AND ENG RUN FOR AIR CONDITION CHECK, OK FOR SERVICE.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 10,490 hrs · 25,776 cycles

OPEN - PACK L OVERHEAT ALONG WITH A BURNING SMELL, GRINDING, RATTLING NOISES AND VIBRATION. OK TO CONTINUE PER C 21-51-01.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 9,597 hrs · 23,632 cycles

LIGHTNING STRIKE DAMAGE, RIGHT WING TIP TRAIL EDGE. REMOVED RT WING TIP. INSTALLED WING TIP ASSY PER AMM 57-30-01. SECURITY CK AND OPS CK OK.

Part: SKIN — DAMAGED (LT WING AILERON) · airframe 9,597 hrs · 23,632 cycles

LIGHTNING STRIKE DAMAGE, L WING AILERON STATIC WICK AND AILERON BURNED TOP SIDE. REMOVED AND REPLACED LT AILERON AND TAB ASSY PER AMM 27-10-01. FUNCTIONAL CK OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,597 hrs · 23,632 cycles

LIGHTNING STRIKE LIH-HNL MID CHANNEL. NOTHING NOTICED IN COCKPIT HOWEVER FA'S SAY THEY SMELLED A HINT OF SMOKE AFTER STRIKE AND THEN NOTHING. INSP AIRFRAME AND ENGS PER MM 05-52-03. DEFECTS ENTERED IN LOG BOOK. INSP OF WX RADAR AND GIS ANT CK OK. INSPECTION OF IRS AND STBY COMPASS CK OK. INSP OF CABIN AND GALLEY LIGHTING AND EQUIPMENT FOUND NO DEFECTS OR ODOR. COMPLIED WITH M-584-717, LIGHTNING STRIKE INSP.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 8,812 hrs · 21,766 cycles

ATO - AFTER TAKEOFF, THRUST SET AND PRIOR TO 80 KTS CREW HEARD LOUD BAG. TOT OVERTEMP TO 1064 DEG AND COMPRESSOR STALL ALERT ILLUMINATED. ABORTED T/O AND RETURNED TO GATE. REMOVED ENG PER HAL M144-717. INSTALLED NR 1 ENG PER HAL M143-717. GRD RUN-UP AND LEAK CHECK OK.

Part: SWITCH — MALFUNCTIONED (RUDDER CONTROL) · airframe 8,543 hrs · 21,133 cycles

AFTER ENGINE START RUDDER PWR OFF ALERT ILLUMINATED WITH BOTH ENGINES RUNNING, AUX AND HYD TRANS PUMPS ON. CHECKED RUDDER OPERATION WHICH APPEARED NORMAL. PERFORMED FIM 27-20-00-810, NO DEFAULT NOTED OK FOR SERVICE, 2ND BTB: SWAP TO ACFT 476, ACFT 486. REMOVED AND REPLACED RUDDER CONTROL MANUAL SWT. OPS CHECK OK ACFT RELEASE FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 8,362 hrs · 20,683 cycles

NR 1 MAIN TIRE SEPARATION LEFT SIDE ON T/O. FOUND TIRE PRESS TO BE 190 PSI. REPLACED NR 1 MAIN TIRE PER MM 32-41-01. COND CK GOOD. WITH DAMAGE TO THE FOLLOWING:LEFT FLY DOOR AFT EDGE BENT UP ABOUT 9". REMOVED LHS FLY DOOR. REPAIRED FLY DOOR EDGE BENT DAMAGE PER HAL-M105 FILE #486075. CLEARANCE CHK PEND. CLEARANCE CHK NOT REQ DUE TO SAME DOOR INSTALLED. LT MAIN LANDING GEAR SPLASH GUARD BENT UP AFT OF NR 1 TIRE. REPLACED SPLASH GUARD AND BENT DOUBLER PLATE. DENT ON LOWER LT FLAP BELOW LE EDGE CAP BY LFS 105,5 1/2" BY 6 1/2"AND DENT ON LOWER LEFT FLAP XFL5 110 5" BY 6". BOTH REPAIRED PER HAL M 105 FILE NR 486078, INTRIM REPAIR. HONEYCOMB GOUGED NOSE COWL INLET 11 O'CLOCK 5" BY 1-1/2". PERF AMM 72-34

Part: CABLE — BROKEN · airframe 8,246 hrs · 20,398 cycles

DURING FLAP RETRACTION AFTER LANDING FLAP/SLAT DISAGREE ALERT ILLUMINATED. FOUND FLAP BUSS CABLE RUN 33B AND 34A BROKEN. REVD CABLES, FABRICATED CABLES 33B AND 34A PER AMM 91-10-05 AND AMM 20-00-03. INSTALLED AND ADJUSTED PER AMM 27-50-00. OPS CHK OK. (CHECK OUT THIS MODEL, I THINK IT MIGHT REALLY BE A 717200, OR WRONG N#).

Part: ACTUATOR — DAMAGED (MLG) · airframe 8,104 hrs · 20,048 cycles

LEFT MAIN GEAR RETRACT ACTUATOR PISTON HAS CHROME CHIPPING OFF AT THE LOWER END WHERE SEAL CONTACTS PISTON WHEN GEAR IS RETRACTED. REMOVED AND REPLACED ACTUATOR PER MM 32-33-01.

Part: BUSHING — DAMAGED (RT MLG) · airframe 8,104 hrs · 20,048 cycles

RT GEAR FWD TRUNNION NR 2 SPACER PITTED AT APPROX 10 O'CLOCK POSITION. REMOVED AND REPLACED NR 3 BUSHING AND SPACER ON RT MLG HOUSING BORE PER CMM 57-40-1. EDGE SEAL PENDING. SEALED EDGE PER BOEING OVERHAUL MANUAL 57-40-1.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · airframe 8,104 hrs · 20,048 cycles

LT GEAR AFT TRUNNION NR 3 BUSHING PITTED AT APPROX 10 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 BUSHING AND SPACER ON LT MLG HOUSING BORE PER CMM 57-40-1. EDGE SEAL PENDING. SEALED EDGE PER BOEING OVERHAUL MANUAL 57-40-1.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 8,046 hrs · 19,910 cycles

DURING LEFT ENGINE START ALL PARAMETERS NORMAL WITH EXCEPTION OF SLIGHTLY HIGH TGT. ALL INDICATIONS NORMAL AT IDLE, BUT LINE SERVICE SIGNALED FOR SHUTDOWN DUE TO SMOKE COMING FROM ENGINE EXHAUST. TRIED SUBSEQUENT N2 ROTATION. FOUND NR 1 ENG STARTER FAILED. REPLACED NR 1 ENG STARTER PER AMM 80-11-01. GRD OPS CK OKAY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 7,273 hrs · 18,019 cycles

ELEC FAULT DISPLAYED ON ECEC PAGE SYNPTIC. OK TO CONTINUE PER FIM 24-20-809. OPS CHECK GOOD. NO FAULTS NOTED.

Part: STRUCTURE — GROUND DAMAGE · airframe 6,683 hrs · 16,593 cycles

PER BOARDING AGENT, JET BRIDGE CONTACTED BOTTOM OF MED. LOWER FWD OF DOORS EDGE DAMAGE 1/8 DEEP BY 10" LONG. OK TO CONTINUE PER M105FILE NR 486050. XCRIBED TO DPM P14542367

Part: ENGINE — MALFUNCTIONED (LEFT)

LT ENGINE PARAMETERS STARTED TO FLUCTUATE APPROX 7000 FT ON CLIMBOUT. WENT FROM CLB1 TO MCT PWR, IGN SYMBOL CAME ON. FMS PAGE CHANGED TO CONFIRM ENG OUT ALL FLUCTUATIONS WERE SMALL AND DID NOT SHUTDOWN ENGINE. ACCOMPLISHED FIM 73-22, TASK 807 EEC, INPUTS FRM FXX BLEED WORD FAULT CROSS CHECK FML (CH B) DUE EEC NR 1 BITE INFO, NO FAULTS NOTED. DFDR DOWNLOADED AND GIVE TO ENGINEERING FOR ANALYSIS. REF LOG PGS 114675 & 114801, ITEMS 70,71,72, AND 73. (WP13200509843) (K)

Part: LINE — RUPTURED (HYD SYSTEM)

ATB - EN ROUTE TO OGG GOT HYD RT PRESS LOW LIGHT FOLLOWED BY HYD RT QT LOW LIGHT HYD QUANTITY WHEN TO ZERO. RETURNED TO HNL AND PERFORMED APPROPRIATE QRH AND CHECK LIST. FOUND AUX PUMP PRESSURE LINE RUPTURED. REPLACED AUX PUMP PRESS LINE, LEAK OPS CHECK PENDING. OPS AND LEAK CHECK OK. (M)

Part: PIVOT — CRACKED (APU DOOR)

FOUND CRACK APPROXIMATELY 2 INCHES ON UPPER APU DOOR FLANGE AT BASE OF PIVOT ROD. REPLACED APU DOOR ASSEMBLY. OPS CHECK OK. (M)

Part: DUCT — CRACKED (COMPRESSOR)

HNL - FOUND LEFT COMPRESSOR OUTLET DUCT CRACKED. REPLACED DUCT. OPS CHECK OK. (M)