N601AP

Part: AMPLIFIER — MALFUNCTIONED (NR 2)

FLT 564 - HNL - NR 2 COMPASS SYSTEM BECAME INOPERATIVE WITH GEAR RAISED. STARTED WORKING AGAIN WITH THE GEAR DOWN. REPLACED NR 2 INSTRUMENT AMPLIFIER. OPS CHECK GOOD. (M)

Part: WHEEL — OUT OF BALANCE (NLG)

HNL - FLT 186 - FOUND SEVERE NOSE SHIMMY AT START OF TAKEOFF, RETURNED TO THE RAMP. REMOVED AND REPLACED BOTH NOSE TIRE ASSEMBLIES. SPIN CHECKS OK. INSPECTED NOSE LANDING GEAR AND NO DEFECT NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: VALVE — FAILED (NR 1 ENGINE)

FLT 147 - KOA - NR 1 START VALVE WILL NOT OPEN, NO LIGHT NO PRESSURE DROP NO ENGINE ROTATION. REMOVED AND REPLACED LEFT ENGINE START VALVE. SECURITY CONDITION CHECK, GOOD, GROUND RUN, OPERATIONAL CHECK GOOD. (M)

Part: SPRING — BROKEN (ELEVATOR)

FLT 282 - HNL - PRIMARY STAB INOP DURING CLIMB-OUT, RESET C/B PER SOP. NO CHANGE. AIRCRAFT MADE AN UNEVENTFUL LANDING IN HNL. FOUND TWO EACH SPRINGS AT ELEVATOR SECTOR BROKEN. REPLACED SPRINGS, OPS CHECK GOOD. (M)

Part: CONTROL CABLE — OUT OF ADJ (MLG)

FLT 241 - HNL - UNABLE TO RAISE LANDING GEAR HANDLE AFTER TAKEOFF. ABNORMAL PROCEDURES ADHERED TO GEAR WAS RETRACTED, NO GROUND MODE PROBLEM, FLIGHT NORMAL. ADJUSTED ANTI-RETRACTION CABLE SYSTEM PER DC-9 MM 32-31-1. OPS AND GEAR SWING CHECK OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

HNL - (LOG PAGE NR A165002) - CEILING EMERGENCY LIGHT ABOVE ROW 25/26 IS INOPERATIVE. REPLACED THE EMERGENCY LIGHT FIXTURE AND THE OPERATIONAL CHECK WAS OK. (X)

Part: BATTERY — DISCHARGED (CABIN)

HNL - (LOG PAGE NR A165001) - BOTH LEFT AND RIGHT VENTRAL STAIR EMERGENCY LIGHTS ARE INTERMITTENT. REPLACED THE EMERGENCY LIGHT BATTERIES AND THE OPERATIONAL CHECK WAS OK. (X)

Part: SPLICE — CORRODED (BS 598-579)

HNL - MODERATE/HEAVY CORROSION, ON LONGERON 30 SPLICE BETWEEN STATION 598 AND 579. REPLACED SPLICE PER HAL 105, FILE NR 59125. (M)

Part: TURBINE — FAILED (NR 2 ENGINE)

HNL - FLT 158 - ON TAKEOFF ROLL FROM HNL, THE NR 2 ENGINE TURBINE CAME APART. IN PROCESS OF INSPECTING A/C FOR DAMAGE AND CHANGING OUT THE NR 2 ENGINE. (M)

Part: O-RING — FAILED (CABIN DOOR SLIDE)

FLT 158 - HNL - FORWARD SERVICE DOOR SLIDE DID NOT DEPLOY PRESS ZERO. INSPECTION OF BOTTLE REVEILED THE MAIN 'O' RING COULD HAVE CAUSED THE PRESSURE TO LEAK OUT OF THE BOTTLE. WHEN A NEW BOTTLE WAS INSTALLED AND SLIDE TESTED, IT DEPLOYED AS ADVERTISED. REMOVED AND REPLACED RIGHT FWD DOOR SLIDE. (M)

Part: BATTERIES — DISCHARGED (CABIN)

HNL - FORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES, OPS OK. (M)

Part: BATTERIES — DISCHARGED (CABIN)

HNL - FORWARD HALF OF EMERGENCY TRACK LIGHT WILL NOT ILLUMINATE WITH SWITCH 'ON' OR ARM. RECHARGED THE BATTERIES AND THE OPERATIONAL CHECK WAS OK. (M)

Part: WHEEL — SHIMMY (NLG)

FLT 317 - ITO - SEVERE NOSE WHEEL SHIMMY ON TAKEOFF ROLL, 70 KTS. ABORTED TAKEOFF, CLEARED RUNWAY WITHOUT INCIDENT. REPLACED NOSE WHEEL AND TIRE ASSEMBLY, LEFT AND RIGHT, LUBED NOSE GEAR ASSEMBLY. CHECKED NOSE GEAR CONDITION AND SECURITY. OK FOR SERVICE. SPIN CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

HNL - AFT SECTION OF CABIN EMERGENCY FLOOR PATH LIGHTING INOP. REMOVED AND REPLACED MID CABIN AFT CONTROL MODULE. OPS CHECK OK. (M)

Part: BATTERY — DISCHARGED (CABIN)

HNL - FORWARD CABIN EMERGENCY LIGHTING INOP. REPLACED POWER BATTERY PACK. OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

HNL - FORWARD MID CABIN EMERGENCY LIGHTING INOP. REPLACED POWER BATTERY PACK. OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

HNL - FORWARD EMERGENCY LIGHT INOP. REPLACED POWER BATTERY PACK. OPS CHECK OK. (M)

Part: CONTROL BOX — OVERHEAT (THROTTLE QUAD)

HNL - FLT 519 - STRONG ELECTRICAL BURNING SMELL IN COCKPIT. SEEMS TO BE CENTERED AT THROTTLE QUADRANT. REPLACED AUTO SPOILER ACTUATOR, CONTROL BOX AND INTERLOCK BOX. THE OPERATIONAL CHECK WAS GOOD. REFERENCE HALA96122.

Part: ACTUATOR — OVERHEAT (THROTTLE QUAD)

HNL - FLT 519 - STRONG ELECTRICAL BURNING SMELL IN COCKPIT, SEEMS TO BE CENTERED AT THROTTLE QUADRANT. REPLACED AUTO SPOILER ACTUATOR, CONTROL BOX AND INTERLOCK BOX. THE OPERATIONAL CHECK WAS GOOD. (M)

Part: INTERLOCK BOX — OVERHEAT (THROTTLE QUAD)

HNL - FLT 519 - STRONG ELECTRICAL BURNING SMELL IN COCKPIT. SEEMS TO BE CENTERED AT THROTTLE QUADRANT. REPLACED AUTO SPOILER ACTUATOR, CONTROL BOX AND INTERLOCK BOX. THE OPERATIONAL CHECK WAS GOOD. REFERENCE HALA96122.

Part: TR UNIT — INOPERATIVE (NR 2 ENGINE)

HNL - FLT 108 - RIGHT ENGINE REVERSE UN-LOCK LIGHT CAME ON AFTER GEAR RETRACTION. RETURNED TO HNL FOR LANDING. LIGHT WENT OUT AFTER LANDING. PLACARD NR 2 REVERSE INOP. LOCKED OUT REVERSER AND DMI NR 98226 ISSUED. ITEM ENTERED ON 1414. (M)

Part: UPLATCH ROLLERS — WORN (MLG DOORS)

HNL - FLT 381 - GEAR DOOR OPEN LIGHT CAME ON IN-FLIGHT. PLACED HYDRAULIC PUMPS TO HIGH AND LIGHT WENT OUT. OCCURRED 3 TIMES. REMOVED AND REPLACED BOTH UPLATCH ROLLERS, LT AND RT GEAR DOORS. TIGHTENED HOOK GUARD, LT MLG. (X)

Part: TIRE — SHIMMY (NLG)

ITO - FLT 121 - VIOLENT NOSE WHEEL SHIMMY AT APPROXIMATELY 75 KNOTS. APPLIED FORWARD YOKE PRESSURE WITH NOSE WHEEL STEERING INPUT. NO CHANGE. ABORTED THE TAKEOFF. VISUALLY CHECKED NOSE LANDING GEAR AND SURROUNDING AREA. NO DEFECTS NOTED. REMOVED AND REPLACED NOSE TIRE ASSEMBLIES. (X)

Part: UPLOCK GUIDE — BENT (LT MLG)

HNL - FLT 317 - GEAR UPLATCH FAILED TWICE ON CLIMB-OUT. RED LEFT GEAR UNSAFE LIGHT CAME ON. STRAIGHTENED AND SECURED LEFT GEAR UPLOCK ACTUATOR GUIDE AND SPRING. CLEANED ALL PROX SENSORS. GEAR SWING CHECKED OK. (M)

Part: CONNECTOR — FAILED (NR 2 FIRE LOOP)

HNL - FLT 202 - B-LOOP RIGHT ENGINE FIRE DETECTOR IS INOPERATIVE. RESPLICED NEW LOOP CONNECTOR. THE OPERATIONAL CHECK WAS OK. (X)

Part: LE RIBS — CRACKED (VERT STAB)

IN C-CHECK, UPON REMOVAL OF VERTICAL STABILIZER LEADING EDGE FOR DPM 119846, 3 ADDITIONAL CRACKS FOUND IN RIBS LEFT SIDE NR 2, NR 7 AND NR 8 FROM BOTTOM. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 55-02 FIG 19. (M)

Part: L/E RIBS — CRACKED (VERT STAB)

IN C-CHECK, FOUND CRACKS ON VERTICAL STABILIZER LEADING EDGE RIBS ZFS = 142 AND 148, RIGHT LOWER ENDS. REMOVED CRACKED VERTICAL STABILIZER LEADING EDGE RIBS, ZFS = 142 AND 148 PER SRM 53-05-84. FABRICATED, TREATED AND PRIMED REPAIR ANGLES PER SRM 51-10-02, 51-10-03 AND INSTALLATION COMPLETE PER 53-03-84. (M)

Part: FRAME — CORRODED (BS 1305)

SBA - AN .5 INCH BY .5 INCH AREA OF EXFOLIATION EXISTS ON FRAME FLANGE AT STATION 1305 STRINGER 14R. REMOVED CORROSION PER SRM 51-10-3. MATERIAL LOSS OUT OF LIMITS PER SRM 53-01 FIG 1. FABRICATED ANGLES AND FILLER PER SRM 53-01 FIG 2, ALODINED, PRIMED AND INSTALLED PER 53-01. (M)

Part: EEL WIRE — DISCONNECTED (CABIN)

HNL - SECTION OF FLOOR EMERGENCY LIGHTS INOPERABLE. RECONNECTED WIRE 7-10. OPERATIONAL CHECK GOOD. (M)

Part: EEL POWER PACK — DISCHARGED (COCKPIT)

HNL - COCKPIT EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY LIGHT POWER PACK. OPERATIONS CHECK OK. (M)

Part: EEL — INOPERATIVE (CABIN)

HNL - ITEM FROM M-71, LOG PAGE NR 138673. THE EMERGENCY LIGHT AT THE ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS OKAY. (X)