N479HA
Registered owner: HAWAIIAN AIRLINES INC, HI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
1L DOOR HARD TO CLOSE. GROUNDED - YES. FOUND EXCESS SEALANT INHIBITING/BLOCKING DOOR STOPS 1L. REMOVED EXCESS SEALANT. LUBRICATED DOOR HANDLE MECHANISM, BOYNNET, AND CAM FOLLOWER. OPS, LEAK, AND SECURITY CHECK OF 1L GOOD. OK FOR SVC. REF 21-30-00 REF FIM 52-10-801.
FWD ENTRY DOOR HANDLE HARD TO CLOSE. GROUNDED - YES. MED OP CHECKS GOOD. OK FOR SERVICE.
BOARDING DOOR HARD TO CLOSE. GROUNDED - YES. REMOVED DEBRIS FROM MAIN ENTRY DOOR. OPS CHECK GOOD. OK FOR SERVICE.
CABIN AND COCKPIT EMERGENCY LIGHTS NOT WORKING. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY SUPPLIES 221CC, 221FC, & 222AR, OPS CHKD OK. OK FOR SERVICE. AMM 33-51-03.
MAIN CABIN DOOR INSIDE HANDLE DIFFICULT TO MOVE. GROUNDED - YES. LUBRICTED MED HANDLE. OPS CHECK GOOD.
CAT WALK EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY ASSY. B5-260 PER AMM 33-51-03. OPERATIONAL CHECKED OK.
OVERWING EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. AC OK TO CONTINUE SERVICE.
"INFO TO MX" RTO;BTB TAKEOFF AND THROTTLE ADVANCE LEFT ENGINE N1 STAGNANT. L ENGINE N1 AT 25 WHEN R ENGINE AT N1 55. REMOVED AND REPLACED FUEL PUMP ENG #1 REF AMM 73-12-01. LEAK CHECK FAIL. FUEL PUMP LEAKING (BAD FROM STOCK) S/N #0431. REMOVED BAD FUEL PUMP AT ENG 1 PER AMM 73-12-01-000-801. UP TO STEP D. INSTALLED FUEL PUMP PER AMM 73-12-01. PENDING LEAK AND OPS CHECK UP TO STEP F(2). LEAK CHECK PASSED OPS CHECK GOOD OF #1 ENG FUEL PUMP PER AMM 73-12-01-400-801. COMPLETED REMAINING STEPS OF AMM 73-12-01-400-801
LVL 2- ENG L COMP STALL ON EAD DURING LANDING ( NO OTHER INDICATIONS). PERFORMED FIM 72-00 TASK 803, REMOVED AND REPLACED LH ENG N2 SHARED SPEED PROBE PER AMM 77-12-01, OPS AND LEAK CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.
POSSIBLE CRACK IN LOWER PORTION OF CO PILOT WINDSHEILD APPROX 1 INCH. REMOVED RIGHT AND CENTER FAIRING COVER AND WINDSHEILD WIPER AMM 56-11-02-801 25000. REMOVED AND REPLACED RIGHT SIDE WINDSHEILD IAW AMM 56-11-02 UP TO PARA 4E (6). ACCOMPLISHED REMAINING STEPS. OPS LEAK CHECK GOOD.
CAPTAIN SIDE WINDSHIELD CRACKED IN FLIGHT. REMOVED AND INSTALLED NEW CAPTAIN SIDE WINDSHIELD PER AMM 56-11-02 UP TO STEP E (7).(B) NEED TO CONTINUOUS FROM E.(8) PERFORMED LEAK CHECK AND PRESSURIZATION CHECK GOOD.PER AMM 56-11-02.NEED TO CONTINUE OPS CHECK ANTI ICE E.18. REMOVED CAPTAIN SIDE WINDSHIELD FOR HEAT ELEMENT TEST .HEATING TEST OK. REINSTALLED CAPTAIN SIDE WINDSHIELD PER AMM 56-11-02 UP TO STEP E. (7)(B). COMPLETED REMAINING STEPS IAW AMM 56-11-02-420-801 .OPS CHECK OK. LEAK CHECK OK .WINDSHIELD WIPER OPS CHECK OK.HYDROPHOBIC COATING APPLIED OK FOR SVC
MULTIPLE CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY (B5-231, B5-119, B5-259 & B5-227) PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SVC
BTB L ENGINE COMPRESSOR STALL ON TAKEOFF ROLL AS SOON AS TAKEOFF POWER APPLIED LOUD BANG. REMOVED L/H ENG PER T/C E1128-717-71-003-REMOVAL W/O 280784
ATB - DUAL FMS FAIL INFLIGHT. PERFORMED FIM 34-63 TASK 830 "FMS DUAL FAIL". VIA 1 & 2 RTS PER AMM 31-43-00-741-803, TESTS OK. REMOVED AND REPLACED FCC-1 AS PRECAUTIONARY PER AMM 22-01-03. AIRCRAFT OK FOR SERVICE.
COCKPIT OVERHEAD EMERGENCY LIGHT DOESNT STAY ON (ILLUMINATES MOMENTARILY) WHEN "EMER LT" SWITCH IS PLACED "ON". ALL OTHER EMER LIGHTS APPEAR OPERATIONAL. REMOVED AND REPLACED EMERGENCY BATTERY AND EMERGENCY BATTER POWER SUPPLY PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SERVICE. UNIT CHANGED IS B5-123
FWD 1/3 OVHD EMER CEILING LTS INOP. REMOVED AND REPLACED EMER LIGHT BATTERIES ON EMER LIGHT BATTERY POWER SUPPLIES B5-227, B5-230 AND B5-259. OPS CHECK OK PER AMM 33-51-00. OK FOR SERVICE.
PER LINE MX MANGEMENT PILOT / CREW REPORT DIRTY SOCK SMELL FROM A/C SYS FOUND OIL LEAKING IN APU. REMOVED AND REPLACED APU PER TASK CARD 717-49-HWI-04-01, OPS CHECK GOOD.
FIRST FLIGHT ATTENDANT REPORTS ODOR SMELL COMING FWD AIR CONDITIONING DUCT//REPLACED BOTH AC WATER SEPARATORPER AMM 21-54-01. SECURITY CHECK OK. NO ODOR SMELL NOTED THROUGHOUT CABIN
ELECTRICAL ODOR THROUGHOUT CABIN & COCKPIT.// OPERATED #1 &2 ENGINE WITH L/R PACKS & HAD SLIGHT SMELL OF OIL, REPLACED COALESSER BAGS PER AMM 21-54-08-400-801 PERFORMED PACK BURN PER AMM 21-54-00.FOUND GASPER BOOSTER FAN TO BE SOURCE OF ELECTRICAL SMELL.REPLACED PER AMM 21-23-01.OPS CHECKED GOOD NO SMELL REMAIN.OK FOR SERVICE.
EMER EQ - LIFE PRESERVER AT PASSENGER SEAT 16B HAS BEEL PULLED OUT FROM HOUSING // REMOVED AND REPLACED LIFEVEST SEAL. SECURITY CHECK GOOD. OK FOR SVC.
ATB - INFLIGHT SEL FADEC ALT AND ENGINE L SYSTEM FAULT WITH ACCOMPANYING LOUD BANG FROM ENGINE. REMOVED AND REPLACED NR 1 ENGINE EEC, IAW AMM 73-21-01/401. SECURITY CHECK GOOD. OPERATIONS CHECK GOOD. PERFORMED IDLE RUN, TEST GOOD.
FOUND #1 ENGINE ACCESS PANEL 412CR DE-LAMINATED. // REMOVED AND REPLACED #1 ENGINE ACCESS PANEL 412CR PER AMM 74-20-04 SECURITY CHECK GOOD OK FOR SERVICE.
AIR DIVERSION - R ENG SYS FAIL. // INSPECTED #2 ENG TGT HARNESS AND FOUND TERMINAL T1040-2 LEG BROKEN. REMOVED AND REPLACED PER 71-52-01. OPS CK PENDING. RAN ENGINES FOR 4 MINUTES -- NO FAULTS NOTED ( AMM 71-00-11 ). OK FOR SERVICE.
ENGINE LEFT FUEL PRESSURE ON STATUS PAGE., OK TO CONTINUE, DEFERED PER MEL 73-33-01
ON TAKEOFF OR FINAL GETTING STRONG CHEMICAL SMELL IN COCKPIT. // REMOVED & REPLACED LEFT PACK COALESCER BAG PER AMM 21-54-08. NO SMELL FROM PACK LEFT OR PACK RIGHT. OK FOR SVC.
"AFT EMERGENCY EXIT LIGHT INOP'. // RELAMPED AFT EMERGENCY EXIT LIGHT AS REQUIRED. OPS CHECK GOOD. OK FOR SERVICE.
BINDING IN YOKE AT ABOUT 30 DEG. OF LEFT YOKE. ACCOMPLISHED FIM TASK 27-10-803 CLEANED AND LUBED AILERON TRANSITION SECTOR. AILERON CONTROL SYSTEM TEST OK.
INFLIGHT BRAKE OVERHEAT QRH PROCEDURES WERE COMPLETED.// INSPECTED ALL MLG BRAKES NO DEFECTS NOTED PER 32-43-01, BRAKES COOLED DOWN TO DISPATCH ABLE LEVEL WHEN BLOCKED IN.
OPEN - RIGHT WING NR 5 SLAT RETRACT CABLE (204A) FOUND SEVERED. REPAIR IN WORK.
RECEIVED A BLEED AIR LT FAIL, WHILE CLIMBING THRU 10,000. RETURNED TO DEPARTURE. REPLACED THE LT PM SENSOR IAW AMM 36-12-04. ENGINE RUN CHECKED GOOD. WIRING CHECKED FROM PM SENSOR TO PSC CHECKED GOOD.
LEFT SLAT BY WING TIP, IT'S NOT FLUSH LIKE OTHER SIDE. INSPECTED LT SLAT AND FOUND NR 5 SLAT RETRACT CABLE FRAYED. REMOVED NR 5 SLAT CABLE PER AMM 27-81-02-000-801. INSTALLED NR 5 SLAT RETRACT CABLE 194A PER AMM 27-81-02-400-801. REMOVAL AND INSTALLATION OF NR 5 SLAT RETRACT CABLE 194A. ADJUSTMENT/RIGGING PENDING. COMPLETED ADJUSTMENT/RIGGING AND ALL REMAINING STEPS OF INSTALLATION PER AMM 27-81-02-400-801. OPS TEST GOOD.
NR 3 MLG TIRE DELAMINATED. TIRE PRESSURE AT REMOVAL 170PSI. R & R NR 3 MLG TIRE IAW AMM 32-41-01. SPIN CK OK.
AFT CARGO SMOKE ALERT ILLUMINATED INFLT. BOTH BOTTLES DISCHARGED, LOWER CARGO COMP FIRE SUPPRESSION SYS. R & R CARGO COMPARTMENT FIRE EXTINGUISHER CONTAINER 1 AND 2 IAW AMM 26-22-01. PERFORMED CARGO FIRE EXT ADJUSTMENT/TEST NO FAULTS DEFECTS NOTED, OK FOR SERVICE.
DURING DEPARTURE, SELECTED GEAR UP, LT MAIN UNSAFE, RED, CONDITION INDICATION. CYCLED ONCE, ALL OK. REPLACED MLG DOWN/LOCKED PROXIMITY SENSOR. GROUND OPS CHECK OK, 32-61-04.
F/A UNABLE TO OPEN L1 DOOR. TRIED SEVERAL TIMES. DOOR HAD TO BE OPENED FROM OUTSIDE. PERFORMED VERTICAL ADJUSTMENT OF DOOR IAW 52-11-01. OPS & LEAK CHECKED OK. OK FOR SERVICE.
HYDRAULIC RT QTY LOW, ZERO QTY, RT, DECLARED AN EMERGENCY. R & R RT MLG RETRACT CYLINDER GLAND HYD LINE IAW AMM 32-33-05. LEAK CHECKED OK. AN UNEVENTFUL LANDING WAS MADE.
FMS FROZE AFTER TAKEOFF. NO THRUST CHANGE. NO NAV FUNCTION. UNABLE TO TUNE RADIO. NO AUTOPILOT. NO AUTO TUNE NAV RADIO. NO FMS SPEED BUGS. RESET NR 1 AND NR 2 VIA'S AND MCDU'S. OPS CHECKED OK IAW AMM 31-43-00 AND AMM 31-65-01.
DURING REVERSE THRUST AFTER LANDING, THROTTLES IN EMERGENCY REVERSE. RT ENGINE HAD COMPRESSOR STALL FOR ABOUT 15 SECONDS, ALERT WAS DISPLAYED ON EAD. NO LIMITATIONS WERE EXCEEDED. ENGINE RESPONDED NORMAL AFTER. INSPECTED NR 2 ENGINE IAW AMM 72-00-00-200-801. NO DAMAGE FOUND. PERFORMED FIM 72-00-TASK 801, REPLACED EEC 2, NO FAULTS NOTED. EEC TEST PASSED. PERFORMED HIGH POWER RUN, CHECK OK. OK FOR SERVICE. REPLACED EEC 2 IAW 73-21-01.
DURING FLIGHT F/A ADVISE SOME NOISE WHEN GEAR RETRACTED, NO ABNORMAL INDICATIONS. FOUND NR 4 MAIN TIRE RECAP SEPARATED FROM CORE, R & R NR 4 TIRE IAW AMM 32-41-01.
UPON PREFLIGHT OBSERVED RT ENGINE FIRE LEVEL 3 ALERT DISPLAYED WITH AURAL WARNING, FOLLOWED BY ENGINE DETECTION RT FAILED LEVEL 1 ALERT. R & R RT ENGINE FCDU IAW AMM 26-11-01. OPS CHECKED NORMAL. NO DEFECTS NOTED.
ON CLIMBOUT YAW DAMP FAIL LIGHT. ACCOMPLISHED FIM 22-23 TASK 801. R & R NR 1 FCC COMPUTER, GROUND CHECKED OK IAW AMM 22-01-03.
AIR TURN BACK - ON CLIMB, IGNITION CAME ON, LT ENG WITH SLIGHT PWR SURGE. REPAIR IN WORK. OPEN
R1 DOOR SLIDE FAILED DEPLOYMENT SYS CHECK. SLIDE DID NOT DROP OUT OF ACFT. REMOVED SHIM FROM LINER COVER DOOR CLIP. ACCOMPLISHED OPS CHECK OF SERVICE DOOR SLIDE DEPLOYMENT SYS, NO DEFECT. REF AMM 25-61-03 & 25-61-00.
FWD CARGO LOWER PAN BY DOOR WAY HAS CORROSION FWD TO AFT END. REMOVED DAMAGED LOWER FWD CARGO PAN IAW SRM 51-41-00-06-0. INSTALLED NEW (1EA) LOWER PAN ASSY IAW SRM 53-20-15-2D-6.
OPEN - AFT CARGO DOOR FWD EDGE 13" FROM BOTTOM DAMAGED, IN WORK.
TEMPORARY NR 2 ENGINE DISPLAYED FOLLOWED BY A LOSS OF THRUST, ENG REGAINED NORMAL THRUST. INSPECTED NR 1 & NR 2 ENG INLETS & EXHAUSTS. NO DEFECTS NOTED. PERFORMED FAULT REVIEW OF EEC 1 & EEC 2. NO FAULTS NOTED. PERFORMED RTS ON BOTH EEC 1 & EEC 2 RTS PASSED. NO FAULTS NOTED.
A FEW MINTURES AFTER TAKE-OFF, F/A'S SMELLED & SAW SMOKE IN FWD CABIN NEAR "MOOD" LIGHTS. F/A'S SAID IT LASTED ABOUT 5 MINS THEN DISAPATED. TURNED OFF GALLEY POWER. DISPATCH NOTIFIED. OK TO CONTINUE TO HNL. INSP WIRNG IAW AMM 20-30-00. NO DEFECTS NOTED. NO SIGNS OF BURNED COMPONENTS & WIRING IN PANEL 221FC. FOUND 2 LIGHT BULBS BURNED OUT. R & R LAMPS IN MOOD LITES. OPS CK OK.
RUDDER PITOT FAIL, RAT PROBE FAIL, AOA HEAT R FAIL, AOA HEAT LT FAIL DURING CLIMBOUT. R & R DCU PER AMM 31-43-02 OPS CHECK OK.
"Z" ANGLE CRACKED AT NR 3 LWR COWL LATCH CUTOUT. AFT CORNER BELOW GUSSET. NR 1 ENG CHANGE. REPAIRED DAMAGE AREA IAW HAL M105 NR 479141. PERMANENT REPAIR.
ARB - "ENG L SYS FAIL" ALERT ILLUMINATED DURING INITIAL CLIMB. PERF FIM 73-33 TASK 802. FOUND MSG 733401 LT FUEL FILTER IMPENDING BLOCKAGE. REMOVED AND REPLACED LP FILTER PER AMM 73-11-01. OPS AND LK CK OK.
HEARD A LOUD BANG ON TAKEOFF. N1 & N2 SEIZED ON NR 1 ENGINE. NR 1 ENGINE WAS REMOVED AND REPLACED. LPT 3 BLADE EXHIBITED SIGNS OF FATIGUE IN THE SHANK NECK AND RELEASED BELOW PLATFORM RESULTING IN THE FAILURE OF THE REMAINING LPT3 TURBINE BLADES. (S)
ATB - RT AIR SYS FAULT DURING CLIMB AND INTERMITTENT LT AIR SYS PRESSURE LOW. REPAIR IN WORK.
LEFT ENG FIRE LOOP B DOES NOT TEST. FOUND LOOSE CONNECTOR ON FIRE LOOP B REPLACED CONNECTOR PER WDM 26-11-00, OPS OKAY PER AMM 26-11-00, OPS CK GOOD.
ENG R SYS FAIL. REMOVED AND REPLACED RIGHT ENGINE T-30 THERMOCOUPLE PER AMM 73-21-07. ALSO REMOVED AND REPLACED RIGHT ENGINE DEDICATED GENERATOR PER AMM 73-21-04. ENGINE RUN UP AND RTS CHECK OK. OK FOR SERVICE.
LEVEL 1 CORROSION ON RT I/B FLAP ACTUATOR AFT FAIRING. REPAIR IN WORK.
LEVEL 2 CORROSION VERTICAL STAB RAM AIR INLET SCOOP 2 REPAIR DOUBLERS LEFT AND RIGHT SIDE. REPAIR IN WORK.
CONTACT DAMAGE ON MED DOOR HINGE, FROM FUSELAGE FRAME.//REPAIR IN WORK.
GOUGES ON NR 1,NR 2, NR 3 AND NR 4, AFT MED STOPS SILL SIDE. REPAIR IN WORK.
LEVEL 1 CORROSION ON VERTICAL STAB FWD LOWER L/E NUT PLATES (9EA). REPAIR IN WORK.
CRACK ON RT SIDE OUTBOARD SEAT TRACK SUPPORT BRACKET EAR, UNDER FLOOR BOARD AT FUSELAGE STA 737.00. REPAIR IN WORK.
LEVEL 1 CORROSION, FWD CARGO PIT STA 465, ON FRAME AROUND FASTENERS, L 29R. REPAIR IN WORK.
LEVEL 1 CORROSION, ON RADOME INTERNAL FORMER RING. REPAIR IN WORK.
LEVEL 1 CORROSION, ON RADOME RT HINGE CUT OUT AREA (2 EA). REPAIR IN WORK.
LEVEL 1 CORROSION, ON LT ENGINE PYLON T/E ASSY LOWER SURFACE. REPAIR IN WORK.
LEVEL 1 CORROSION IN FWD CARGO PIT (AFT BULKHEAD), STA 686 FRAME. REPAIR IN WORK.
LEVEL 2 CORROSION, RADOME STA 37 PRESSURE BULKHEAD LT SIDE O/B INTERCOSTAL (STIFFENER). REPAIR IN WORK.
CRACK ON RT MLG I/B DOOR, FWD "Z" CHANNEL. REPAIR IN WORK.
LEVEL 1 CORROSION AND PAINT PEELING ON LT ENG UPPER COWL EXTERIOR SURFACE. REPAIR IN WORK.
LEVEL 1 CORROSION AT STATION 37 PRESSURE BULKHEAD, HORIZONTAL SKIN (SHELF). REPAIR IN WORK.
LEVEL 1 CORROSION ON LT ENG, LOWER COWLING FWD NR 1RIB, I/B REPAIR DOUBLER. REPAIR IN WORK.
LEVEL 2 CORROSION, ON RADOME PRESSURE BULKHEAD RT SIDE O/B INTERCOSTAL, (STIFFENER). REPAIR IN WORK.
CRACK ON LT SIDE OTBD SEAT TRACK SUPPORT EAR, UNDER FLOORBOARD AT FUSELAGE STA 437.00. REPAIR IN WORK.
CRACK ON O/B SECTION OF L-2 FORMER LEFT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK.
LEVEL 1 CORROSION, LT HORIZ STAB, LOWER SURFACE OF L/E PANEL. REPAIR IN WORK.
LEVEL 1 CORROSION, NUMEROUS FASTENERS HOLES, ON LOWER SURFACE OF THE LT HORIZ STAB L/E PANEL. REPAIR IN WORK.
CRACK ON O/B SECTION OF MOST FWD FORMER RIGHT WING BELOW CENTER SECTION, VIEW FROM 2ND WITNESS HOLE. REPAIR IN WORK.
LEVEL 1 CORROSION NR 1 ENGINE SEVEN PLACES ON LOWER COWL CHANNEL NEAR GUIDE PIN HOLES. REPAIR IN WORK.
.25 INCH DEEP GOUGE ON NR 1 ENGINE, TOP COWL CHANNEL AT 1ST GUIDE PIN. REPAIR IN WORK.
LEVEL 1 CORROSION, LOCK FASTENERS ON TOP OF LT HORIZ STAB, L/E PANEL. REPAIR IN WORK.
LEVEL 1 CORROSION L/E TIP OF RT HORIZ STAB. REPAIR IN WORK.
LEVEL 1 CORROSION ON BELLY, JUST LEFT OF MLG DOOR BY PASS CUTOUT. REPAIR IN WORK.
LEVEL 1 CORROSION AND PAINT PEEL, NR 1 ENGINE, TOP COWL EXTERIOR AT FAN AIR VALVE EXIT AND 1 PLACE AT COWL HALF. REPAIR IN WORK.
LEVEL 1 CORROSION AROUND FASTENER TAILS LEFT WING BELOW CENTER SECTION. REPAIR IN WORK.
LEVEL 1 CORROSION ON TOP COWL NR 1 ENGINE, ALONG L/E AND HINGE EDGE. REPAIR IN WORK.
LEVEL 1 CORROSION AND PAINT PEEL NR 1 ENGINE, LOWER COWL, EXTERIOR. REPAIR IN WORK.
CRACK ON O/B SECTION OF NR 3 FORMER LT WING BELOW CENTER SECTION, VIEWED FROM 4TH WITNESS HOLE. REPAIR IN WORK.
CRACK ON O/B SECTION OF MOST FWD FORMER LEFT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK.
LEVEL 1 CORROSION ON INNER SURFACE OF RT MLG OUTBOARD DOOR. REPAIR IN WORK.
CRACK ON O/B SECTION OF FORMER NR 2 RIGHT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK. REPAIR IN WORK.
LEVEL 1 CORROSION ON THE EXTERIOR SURFACE OF THE RT MLG OTBD DOOR. REPAIR IN WORK.
LEVEL 1 CORROSION IN AFT CARGO BAY, ON FASTENER ON LEFT CARGO TIE DOWN TRACK AT STA 851. REPAIR IN WORK.
LEVEL 1 CORROSION ON VERTICAL STAB RT EXTERIOR SURFACE AFT OF HORIZ STAB ROLLER TRACK. REPAIR IN WORK.
LEVEL 1 CORROSION, RT HORIZ STAB 1 RUSTED NUT O/B AFT SIDE OF HORIZ INTERNAL STRUCTURE AT STA XHS 221. REPAIR IN WORK.
LEVEL 1 CORROSION ON RT HORIZ 2. RUSTED NUTS AFT SIDE OF HORIZ INTERNAL STRUCTURE AT STA XHS 103. REPAIR IN WORK.
LEVEL 1 CORROSION, ON LT HORIZ STAB INBD L/E LOWER INBD ATTACH AFT END. REPAIR IN WORK.
LEVEL 1 CORROSION, NUMEROUS FASTENERS ON OTBD END OF LT HORIZ STAB INNER BOX AREA. REPAIR IN WORK.
3 GOUGES ON NR 1 ENGINE, TOP COWL INTERIOR, NEAR FAN AIR VALVE EXIT. REPAIR IN WORK.
RT MLG DOOR HAS SURFACE CORROSION ON OUTER SKIN. REPAIR IN WORK.
SURFACE CORROSION AND PAINT PEELING ON LT MLG DOOR ON LEADING EDGE, REPAIR IN WORK.
RT MLG DOOR RAMP CRACKED AT INBD MOUNT BRACKET. REPAIR IN WORK.
2 CRACKS ON RIGHT MLG DOOR CUTOUT JUST ABOVE DOOR SENSOR. REPAIR IN WORK.
LT MLG DOOR HAS SURFACE CORROSION ON OUTER SKIN. REPAIR IN WORK.
NUMEROUS BOLT HEADS CORRODED ON LT ENGINE, ON TRAPEZOIDAL PANEL ABOVE AND I/B SIDE OF FWD MOVEABLE VANE. REPAIR IN WORK.
RT MLG DOOR INTERCOSTAL CRACKED SEEN INSIDE FWD MID ACCESS PANEL. REPAIR IN WORK.
BTB - ENG L SYS FAIL SW TAXI OUT ALERT. INTERROGATED MCDU PER FIM TASK 77-12-00-810-802. REMOVED AND REPLACED N2 SHAFT SPEED HPC PROBE. OPS AND LEAK CHECK OK. OK FOR SERVICE.
ENG L SYS FAIL DISPLAYED. FOUND 10P BOX FAULT ON EEC FAULT REVIEW AND CURRENT FAULT REMOVED AND REPLACED 10P PER MM 73-21-11, COND SAME. REMOVED AND REPLACED NR 1 EEC ASSY PER AMM 73-21-01. NO FAIL NOTED ON ENG RUN.
T/O ABORT DUE TO STABILIZER AURAL WARNING, EAD TURNING RED. PERFORMED RTS ON NR 1 AND NR 2 VIA AND NR 1 AND NR 2 FCC STAB TRIM. ALL TEST PASS PER MM 31-61-00 AND 22-10-00 OK FOR SERVICE.
LEFT SYSTEM HYD ACCUMULATOR RUPTURED. TROUBLESHOT LT SYS, FOUND PTU INOP. REMOVED AND REPLACED PTU PER AMM 29-22-01. OPS CK OK. SERVICED ACCUM FOUND OK.
RIGHT AT RETRACTION IN HNL, NOTICED A SLIGHT NOISE AT LIFT OFF, NO OTHER INDICATION NOTICED. AFTER PARKING IN LIHUE RAMP NOTICED THE NR 1 TIRE SHREDDED. LOOKS LIKE IT WENT THRU THE NR 1 ENGINE. REPLACED NR 1 MAIN TIRE BORESCOPE INSP OF NR 1 AND 3 LP COMP BLADES, NO DAMAGE NOTED.
ATB - AFTER T/O SMELLED ACID ODOR, WHICH SEEMED TO DISSIPATE THEN BECAME STRONGER CLIMBING THRU 1100' RETURNED TO AIRPORT. INSPECTED NR 1 AND NR 2 ENG FOR LEAKS. NO LEAKS NOTED. NR 1 ENG WAS JUST CHANGED. INSPECTED BOTH PACKS FOR LEAKS. NO LEAKS NOTED. REPLACED NR 1 PACK COALESCER BAG. HIGH POWER RAN UP CK OK. NO ODOR NOTED.
ON NR 1 ENGINE CHANGE, LT PYLON APRON UPPER AFT LATCH CUTOUT IS CRACKED. REPAIRED CRACK PER HAL M105 B10192.
ON NR 1 ENGINE CHANGE, LT PYLON APRON LOWER AFT LATCH CUTOUT HAS 2 CRACKS. REPAIRED NR 1 ENGINE LOWER AFT LATCH CRACKS PER HAL M105 B10192.
CABIN CREW REPORTS ACIDIC ODOR IN THE CABIN CAUSING HEADACHE AND SORE THROAT. REMOVED AND REPLACED APU START PURGE VALVE PER AMM 49-31-12-(6597). OPS CHECK GOOD, NO ODORS DETECTED.
WING ICE LEFT FAIL. CHECKED PNEUMATIC BOX CLEARED ANTI-ICE MSG. OK TO CONTINUE.
BTB - RT ENGINE NO IGNITE, 2ND ATTEMPT START ABORTED. REMOVED AND REPLACED R ENG B IGNITER PER AM 74-20-04 OPS CK OK.
BTB - DURING TAXI CHECK, ELEVATOR POWER CHECK UNSUCCESSFUL. ELEVATOR FWD MOTION RESTRICTED. SEAL ON LEFT HORIZ STAB I/B OF I/B ELEVATOR HINGE BOLT DAMAGED. COLUMN DISCONNECTED. REMOVED FOREIGN OBJECT BETWEEN LEFT ELEVATOR AND HORIZONTAL STAB. CHECKED COND AND SECURITY AND OPERATION OF ELEVATOR AND CONTROL COLUMN PER FIM 27-30-00-810-803. OPS CHKS GOOD. STRAIGHTENED SEAL, REINSTALLED SEAL. RESET CONTROL COLUMN DISCONNECT PER AMM 27-31-10-440-801.
AFTER ENGINE START, ENG LT AND RT SYS FAIL LIGHT ILLUMINATED. PERFORMED FIM 73-22-807, NO ACTIVE FAULTS RTS OF EECS 1 AND 2 IS OK. OK FOR SERVICE.
ON APP INTO HNL GOT HYD R PRESS LO LT AND HYD R QTY LO LT. R HYD QTY WENT TO ZERO. WE PERFORMED THE HYD R QTY LO CK-LIST. LANDED, STOPPED ON RWY AND GOT TOWED INTO GATE. VERIF HYD QTY AT 4.0 QTS. RMVD AND REPLACED RT GRD SVC HYD PIPING TEE P/N 7922150-502. LK AND SEC CK OK. REMOVED AND REPLACED HYD SYS FLTR ELEMENT (RT) IAW AMM TASK 29-12-12. SERVICED RT SYSTEM IAW AMM TASK 12-13-01. LEAK CK OK.
BTB - RT ENG WOULD NOT START. RTS IGNITION SYSTEM PER FIM 73-21 TASK 801, OPS CHECK GOOD. OK FOR SERVICE.
AFT CARGO SMOKE DETECTOR POSITION NR 11 INOP. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR NR 11 PER AMM 26-13-01, GND CK GOOD.
FLT 240 - HNL - PRIMARY TRIM FAILURE, NO ALERT. ON CLIMB-OUT AND RETURN TO HNL, TRIM STARTED WORKING AGAIN ON SHORT FINAL APPROACH. TRIED USING PRIMARY TRIM SEVERAL TIMES IN FLIGHT. RAN F/O, CAPTAIN CONTROL, DID NOT WORK. REMOVED AND REPLACED HORIZONTAL STABILIZER PRIMARY TRIM MOTOR PER AMM 27-41-10. OPS CHECK OK FROM BOTH CAPTAINS AND F/O'S SWITCHES. (M)
RAMS: 2 EACH CRACK ON APU DOOR INLET BOX. AT TOP AFT INBOARD CORNER OF BOX (IN AREA OF AFT SUPPORT STRUT). IN WORK.