N483HA

Part: LIGHT — MISSING (ZONE 200) · airframe 41,187 hrs · 71,175 cycles

DMI# 406046 EMERGENCY ESCAPE FLOOR PATH STRIP MISSING 6" AT ROW 17AB ( PHOTOLUMINESCENT MARKING SYSTEM ). GROUNDED - YES. INSTALLED EMERGENCY PATH GLOWSTRIP AT 17AB. OPS CHECK GOOD. SECURITY CHECK GOOD. PLACARD REMOVED. MIC SHEET UPDATED.

Part: RESERVOIR — FAILED (HYDRAULIC SYSTEM) · airframe 4,532 hrs · 69,701 cycles

HYD R PRES LO IN FLIGHT SYSTEM WOULD NOT REPRESSURIZE, LEAD TO EMERGENCY GEAR EXT. FOUND RH HYDRAULIC RESERVOIR BLOWN / STUCK. REMOVED AND REPLACED RH HYDRAULIC RESERVOIR PER AMM 29-12-01-400-801 UP TO STEP D(8). OPS CHECK + LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — NOISE · airframe 39,909 hrs · 68,332 cycles

DURING TAKEOFF ROLL AT ABOUT 70 KNTS LOUD BANG ON THE RIGHT SIDE OF AC ALL SYSTEM INDICATIONS APPEAR TO BE NORMAL TKAEOFF ROLL ABORTED TAKEOFF AND BTB. PERFORMED INSPECTIONS OF LANDING GEAR HYD INLET OUTLET FLIGHT CTLS ENGINEERING REPORTED NO DEFECTS FAULTS ON ROLLS ROYVE PORTAL. ENG RUN NORMAL NO DEFECTS NOTED OK TO CONTINUE PER FIM 05-50 TASK 809.

Part: RADOME — NO DISCREPANCY (ZONE 100) · airframe 39,724 hrs · 67,933 cycles

DIV - BIRD STRIKE DEPARTING OGG. INSPECTED AIRCRAFT PER AMM 05-52-01-210-801, NO DAMAGE FOUND. NOTED BOTTOM OF RADOME L/H HAS A MARK BUT NO REMENANTS OR DAMAGE FROM BIRD. OK FOR SVC.

Part: COALESCER BAG — ODOR (ZONE 100) · airframe 39,661 hrs · 67,792 cycles

AFTER #2 ENG START (AT THE GATE) + R PACK SWITCH ON ... FA REPORTED BURNING RUBBER SMELL IN FWD GALLEY. PILOT ASSITED WITH RUNNING #2 ENG AND RT PACK. ENGINE AMM 71-00-04 SMELL PERSISTS. 18922 9/16/24. REMOVED AND REPLACED LT + RT COELESCER BAGS. OPS CK GOOD. LEAK CK GOOD. IAW AMM 21-54-08.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 39,537 hrs · 67,524 cycles

PRIOR TO PUSH, BURNING RUBBER SMELL FROM CEILING VENT BEHIND COCKPIT DOOR. AWAITING MORE INFORMATION AND RESOLUTION.

Part: INDICATION SYS — FALSE INDICATION (HYD SYSTEM) · airframe 38,829 hrs · 65,973 cycles

HYD L TEMP HI INDICATION DURING TAXI ONTO RUNWAY EXIT RUNWAY RETURN TO GATE AFTER CYCLING FLIGHT CONTROLS AND INDICATION REMAINING. PERFORMED FIM 29-30 TASK 803 TO STEP D(2) NEED TO CONTINUE FROM STEP D(3) ENG RUN 24094 4/2/24 RAN #1 ENG & OPERATED L HYD SYSTEM PER FIM 29-30, NO HYD TEMP HI NOTED. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,705 hrs · 65,696 cycles

OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PER AMM 31-51-06. OPS CHECK GOOD. OK FOR SERVICE.

Part: SUPPORT FITTING — DAMAGED (UNKNOWN) · airframe 38,038 hrs · 65,236 cycles

ATB - ON GEAR RETRACTION, LEFT AND RIGHT MAIN GEAR LIGHTS WENT FROM GREEN TO DARK. NOSE GEAR LIGHT WENT FROM GREEN TO RED AND REMAINED RED. LOUD NOISE HEARD FROM FLIGHT DECK. QRH COMPLETE, GEAR EXTENDED AND SHOWED THREE GREEN. FOUND NLG CYLINDER SUPPORT FITTING DAMAGE DUE TO UPPER BOLT MISSING. REMOVED AND REPLACED NLG CYLINDER SUPPORT FITTING (P/N 5912386-501) PER DRAWING 9911509 AND 9910073 AND SRM 51-40-03. OPS CHECK AND LEAK CHECK OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,038 hrs · 65,235 cycles

ATB - NOSE GEAR WOULD NOT RETRACT AFTER TAKE OFF. PERFORMED B717 FIM TASK 32-30 TASK 802. NO DAMAGE, NO LEAKS NOTED. NFT. PER FIM 32-30 TASK 802 FAULTS WAS INTERMERITTENT. CYCLED GEAR 6 TIMES. NO FAULTS FOUND. OK FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,861 hrs · 63,848 cycles

BRAKE PRES LO INDICATED WHEN SETTING THE PARKING BRAKE W/ HYD AUX AND TRANS PUMPS IN THE OFF POSITION AT THE GATE. REMOVED AND REPLACED THE LEFT BRAKE ACCUMULATOR PER TASK 32-44-01. OPS CHECKED NORMAL AND OK FOR SERVICE.

Part: PROBE — FAILED · airframe 60,994 hrs · 36,561 cycles

ATB ENG L FADEC ALTN DISPLAYED. FAULTING 732116 P20/T20 PROBE. REMOVED AND REPLACED P20/T20 PROBE PER FIM 73-21 TASK 816. RTS TEST FPR P20/T20 PROBE FAILED. AS 17605 7/13/22. REQUIRES FURTHER T/S. PERFORMED WIRING CK REF FIM 7321 TASK 816 STEP F ALL WIRES CK GOOD NO SHORT TO GND. (CONT TO LP 938845/2) CBS PULLED & COLLARED FOR EEC 1 A/B (U41,W32,X32) 18614 07/13/2022 NEED TO CONT T/S. RESET C/B'S U41, W32, X32. REMOVED AND REPLACED EEC ON #1 ENG PER AMM 73-21-01. OPS CHECK GOOD-OK FOR SERVICE.

Part: SLIDE — DEFECTIVE · airframe 35,847 hrs · 59,409 cycles

EMER EQ - UPON ARRIVAL FOUND MED SLIDE PARTIALLY DEPLOYED. // REPLACED L1 DOOR SLIDE PER AMM 25-61-01. SECURITY CHECK GOOD. OK FOR SVC.

Part: SENSE LINE — CRACKED (LT ENGINE) · airframe 35,330 hrs · 58,241 cycles

ATB - LEFT ENGINE COMPRESSOR STALL FOLLOWED BY ENG L SYS FAIL IN FLIGHT. // FAULT CODE 732178. PERFORMED FIM 73-21 TASK 873, FOUND P30 SENSE LINE P/N BRH17623 CRACKED. REMOVED LINE. 13971 08/04/21. INSTALLED P30 SENSE LINE PER AMM 72-00-41. PERFORMED HIGH POWER RUN, OPERATIONAL CHECK GOOD, NO DEFECTS NOTED. OK FOR SERVICE.

Part: FAIRING — CRACKED (LPT) · airframe 34,868 hrs · 57,232 cycles

CRACKS, FOUND 2 CRACKS ON TOP LPT FAIRING. REPLACED TOP LPT FAIRING, PER AMM 72-03-03/401. SECURITY CHECK OKAY.

Part: WINDSHEAR SYS — ILLUMINATED · airframe 34,215 hrs · 56,890 cycles

ABORT T/O WIND SHEAR ALERT. NO BRAKE OVERHEAT INDICATED 100 C HIGHEST TEMP. PERFORMED AMM TASK 05-53-01-200-801. INSPECTION OK. OK FOR SERVICE. CREW REPORTS HIGH WIND GUST ON T/O ROLL FOR SUSPECT OF WIND SHEAR ALERT.

Part: GIRT BAR — UNSECURE (DOOR) · airframe 32,047 hrs · 50,981 cycles

GIRT BAR BECAME NOT STOWED PROPERLY. RE-SECURED GIRT BAR AS REQUIRED. OK FOR SVC.

Part: INSULATION — DAMAGED (A/C BAY) · airframe 32,026 hrs · 50,937 cycles

AFT FLIGHT ATTENDANT JUMPSEAT IS ABNORMALLY HOT. REMOVED AND REPLACED AFT ACCESSORY COMP A/C SYSTEM DAMAGED HEAT INSULATION IAW AMM 20-60-25, OK FOR SERVICE.

Part: AILERON SYS — STICKING · airframe 32,016 hrs · 50,914 cycles

AILERON TRIM WAS STICKING MULTIPLE TIMES WHEN MOVED LEFT WING DOWN. PERFORMED AN OPS CHECK OF AILERON TRIM. NO FAULTS NOTED. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,984 hrs · 50,844 cycles

EMERGENCY LIGHT ABOVE MAIN ENTRY DOOR WOULD NOT ILLUMINATE. REMOVED AND REPLACED 6V EMERGENCY BATTERY POWER SUPPLY AND CORRECTED SHORT.

Part: COALESCER BAG — ODOR (CABIN) · airframe 31,659 hrs · 50,134 cycles

NOTICED ODOR DURING CLIMB OUT, FOR APPROXIMATELY 5 MINUTES, AN OILY MUSTY ODOR. REMOVED AND REPLACED BOTH LT AND RT COALESCER BAGS IAW AMM 21-54-08. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (STICK PUSHER) · airframe 31,178 hrs · 49,086 cycles

AIR TURNBACK DUE TO A STICK PUSHER FAILED MESSAGE. TROUBLESHOT WITH NO FAULTS FOUND.

Part: VIA — MALFUNCTIONED (NR 1) · airframe 31,178 hrs · 49,085 cycles

RETURNED TO DEPARTURE AFTER GEAR RETRACTION. RADIO ALTIMETER BEGAN TO ALERT. STICK PUSHER FAILED, WINDSHEAR DETECT FAILED, BANK ANGLE SHOWED RAD AT 30 DEGREE LIMIT. CONTINUITY CHECKED DATA BUSS WIRES FROM RA NR 1 R5-1006B G2 AND G3 TO VIA 31 AND VIA NR 2. CHECKED WIRES FROM RA NR 2 DATA BUSS TO VIA NR 1 AND VIA 2. CONTINUITY CHECKED DATA TRASMITTER WIRES FROM RA NR 1 TO FCC NR 1 AND NR 2 R5-1006B B2 AND B3. CONTINUITY CHECKED DATA TRANSMITTER WIRES FROM RA NR 2 R5-1006B B2, B3 TO FCC NR 1 AND FCC NR 2. MEGGED BOTH RA NR 1 TRANSMITTERS AND REC ANTENNA COAX. BOTH CHECKED OK. REPLACED RA NR 1 TRANSMITTER AND REC ANTENNAS. CHECKED OK IAW MM 34-42-02. BOTH VIA NR 1 AND 2 RTS CHECKED OK IAW MM 31-43-00. BOTH FCC NR 1 AND 2 RTS CHECKED OK IAW MM 22-00-00. REMOVED AND REPLACED THE GROUND SENSE RELAY R2-5003 IAW WDM 34-45-11. SECURITY CHECKED GOOD. REPLACED THE NR 1 VIA IAW AMM 31-43-01 AND REPLACED THE NR 1 RADIO ALTIMETER TRANSCEIVER IAW AMM 34-42-01. OPS CHECKED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,915 hrs · 48,497 cycles

UNUSUAL ODOR STARTING FROM LAST 3 ROWS OF AIRCRAFT AND AFT. NO ODORS FOUND DURING INSPECTION OF AIRCRAFT INTERIOR OF THE LAST 3 ROWS, AFT GALLEY AND LAV. OKAY FOR SERVICE.

Part: HANDSET — OVERHEATED (FA STATION) · airframe 30,343 hrs · 47,210 cycles

F/A HANDSET HOT, BURNING ODOR. REMOVED AND REPLACED THE HANDSET IAW AMM 23-41-07, AND OPS CK OKAY IAW AMM 23-41-07.

Part: STICK SHAKER — MALFUNCTIONED (STALL WARNING) · airframe 30,220 hrs · 46,935 cycles

STICK PUSHER FAILED. PERFORMED FCC 1 & 2 RTS AND SYSTEM TEST. NO FAULTS.

Part: SENSOR — UNKNOWN (ELEVATOR POSITIO) · airframe 29,970 hrs · 46,384 cycles

ELEVATOR SPLIT MESSAGE WAS DISPLAYED ON APPROACH TO LAND, SPEED 160KTS, FLAPS 18 GEAR DOWN. MESSAGE EXTINGUISHED AT 145KTS. ACCOMPLISHED FIM 27-30-804, R & R THE LEFT ELEVATOR POSITION SENSOR IAW AMM 27-34-01.

Part: FILTER — LEAKING (FUEL SYSTEM) · airframe 29,667 hrs · 45,713 cycles

FUEL LEAKING FROM RIGHT ENGINE AFTER LANDING. FUNCTIONAL TEST OF THE EMERGENCY SHUTDOWN SYSTEM OK IAW AMM 76-20-00-720-801. REMOVED AND REPLACED LP FUEL FILTER HOUSING IAW AMM 73-11-01. OPS OK. LEAK CHECKED OK.

Part: UNKNOWN — ODOR (GALLEY) · airframe 29,298 hrs · 44,881 cycles

ELECTRIC TYPE BURNING ODOR IN AFT GALLEY AREA. NO ELECRICAL BURNING ODOR PRESENT IN AFT GALLEY AREA. ACFT OK FOR SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 28,805 hrs · 43,787 cycles

CARGO SMOKE TEST DID NOT TEST AT ALL. OPS CHECKED CARGO SMOKE TEST IAW AMM TASK 26-13-01-710-801. FAULT MESSAGE, CARGO SMOKE FWD, APPEARED. TROUBLESHOT IAW FIM TASK 26-13, TASK 803. R & R NR 8 SMOKE DETECTOR IN FWD CARGO IAW AMM 26-13-01. ALL TESTS PASSED OK.

Part: TIRE — SEPARATED (NR 2) · airframe 28,227 hrs · 42,517 cycles

NR 2 MLG TIRE THREAD SEPARATED ON T/O ROLL. R & R NR 2 MLG TIRE IAW AMM 32-41-01. SPIN, PRESSURE AND SECURITY CHECK GOOD. FOUND 1 DENT, 1 BROKEN AND 1 LOOSE RIVET AT PANEL 530CF.1 DENT 12" AFT OF PANEL. REMOVED PANEL 530CF FOR DAMAGE ACCESS. REPLACED 2 EA RIVETS ON PANEL 530CF IAW SRM 51-41-02. 6" X 6" DENT .215 DEPTH ON LT INBD FLAP T/E PANEL. HFEC SKIN NO CRACKS. NO LOOSE FASTENERS, BOROSCOPE RIB IAW E105-483175-INI. NO DAMAGE NOTED. COMPLIED WITH E105-483175-INI.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI SKID SYS) · airframe 41,781 hrs · 27,905 cycles

ANTISKID RT FAIL ALERT DURING LANDING ROLL OUT. DID AMM 32-45-00 RTS NO FAULTS NOTED. OK TO CONTINUE.

Part: SPRING — NOT REPORTED (PROXIMITY SENSOR) · airframe 27,842 hrs · 41,635 cycles

LEFT UNSAFE LIGHT AFTER RETRACTING THE LANDING GEAR AFTER TAKEOFF. UPON INSPECTION LT MLG DOOR TARGET ARM SPRING BROKEN. INSPECTED LT MLG UP AND LATCHED PROXIMITY SENSOR AND TARGET. NO DEFECTS NOTED. REPLACED LT MLG TARGET ARM SPRING. NO ADJUSTMENTS MADE. CONDITION AND SECURITY GOOD. OK FOR SERVICE.

Part: CABLE — BROKEN (NR 5 SLAT) · airframe 27,574 hrs · 41,023 cycles

LEADING EDGE SLATS ON LT WING, NOT RETRACTING PROPERLY. FOUND NR 5 SLAT CABLE RUNS 194A BROKEN. REPLACED NR 5 SLAT CABLE RUNS IAW DWG 5910451. ADJUSTED CABLES IAW AMM 27-80-380-802. ALSO REPLACED PULLEYS, STA Z0S 530.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 270,309 hrs · 40,421 cycles

CARGO SMOKE DISCHARGE LIGHTS ILLUMINATED, ALL). RESET NR 1 & NR 2 VIA C/B'S BITE CHECK OK. OPS CHECKED CARGO SMOKE TEST IAW AMM 26-13-01 CHECKED GOOD, NO DEFECTS NOTED.

Part: WARNING LIGHT — ILLUMINATED (CABIN AIR) · airframe 26,592 hrs · 39,625 cycles

DURING DESCENT THROUGH FL190, AIR SYS RT LOW FOLLOWING QRH PROCEDURES. PERFORMED FIM TASK 36-10, TASK 801. NO FAULTS NOTED, OK FOR SERVICE.

Part: BLADE — MISSING (COMPRESSOR) · airframe 26,434 hrs · 38,452 cycles

NR 1 ENGINE HAD AN COMPRESSOR STALL IN CRUISE. ACCOMPLISHED BORESCOPE. FOUND BLADE MISSING THIRD STAGE HPC AND NUMEROUS DAMAGE AFT SECTION AS WELL. REMOVED AND INSTALLED NR 1 ENGINE. OPS AND LEAK CHECK OK. OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 229) · airframe 25,188 hrs · 35,617 cycles

DAMAGE AT BS 229 BETWEEN LONGERONS 24 -25R. VISUAL AND HFEC CHECKED OK, NO CRACKS NOTED. REPAIRED IAW E105-483132. LEAK CHECKED OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,712 hrs · 29,886 cycles

FWD F/A EMERGENCY FLASHLIGHT UPPER INOPERATIVE. R & R FLASHLIGHT, OPS CHECKED OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,712 hrs · 29,886 cycles

FWD F/A EMERGENCY FLASHLIGHT UPPER INOPERATIVE. R & R FLASHLIGHT, OPS CHECKED OK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 22,505 hrs · 29,407 cycles

LAVATORY "SMOKE" ILLUMINATED AT GATE - AFT LT LAV. PERFORMED FIM TASK 26-14. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 22,505 hrs · 29,407 cycles

RT AFT LAV SMOKE DETECTOR CHIMES ON. REPLACED AFT LAV SMOKE DETECTOR - OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENGINE) · airframe 20,339 hrs · 24,314 cycles

L ENG SELECT FADE ATT ALERT ILLUMINATED FOLLOWED PROCEDURE IN QRH //FOUND T30 FAULT MSG 732181 & 732182 REPAIRED WIRE AT U1043 ON T1043-1. OPS CK PEND. ACCOMP AMM SUB TASK 73-21-07-741-001 ENG RUN NO FAULTS NOTED RTS #1 EEC NO FAULTS NOTED. CK OK FOR SVC. OPS CK OK.

Part: WARNING LIGHT — ILLUMINATED · airframe 20,294 hrs · 24,206 cycles

CLIMBOUT AT 1000'AGL, RUNWAY 8 IN ITO "DISARM SPOILERS" ALERT STICK PUSHER FAIL & WINDSHEAR DET FAIL ALERTS DISPLAYED. ALL ALERTS CLEARED AFTER APPROX 15-20 SECONDS. FOUND NO CURRENT FAULTS ON MCDU. SPOILER RTS-PASSED. INSPECTED & OPERATED SPOILERS. OPS CK GOOD. NO FAULTS NOTED. COND & SECURITY CK GOOD OF SPLRS. NO ALERTS REMAIN. OK FOR SERVICE.

Part: SPOILER SYS — FAILED (INBOARD) · airframe 20,070 hrs · 23,669 cycles

SPOILER INBD FAILED, ACCOMPLISHED FIM 27-60 TASK 808. FOUND FAULT CODE (276023) SECU INTERNAL FAULT. R & R SECU IAW AMM 27-61-01 RTS TEST PASSED. NO FAULTS NOTED OK FOR SVC.

Part: WARNING LIGHT — FALSE ACTIVATION (STALL WARNING) · airframe 19,972 hrs · 23,434 cycles

ON SHORT FINAL 04R/800'/AP & AT OFF FLAPS 40 DEG STABILIZED AT 147 KTS. THE AMBER & RED FOOT OF SPEED TAPE ZOOMED UP TO 160 KTS CAUSING STALL WARNING & STICKSHAKER TO TURN ON. IMMEDIATELY ADDED POWER, AFTER 3-5 SECONDS & AMBER & RED FOOT WENT BACK TO NORMAL LANDED (HAD A FALSE STALL WARNING ERRONEOUSLY). DOWNPOWERED AC STALL WARNING CHECK OK IAW MM 27-38-00 FCC NR 1 & NR 2 BITE CHECK OK IAW MM 22-00-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,901 hrs · 23,267 cycles

EMERGENCY LIGHTS FROM ROWS 1 TO 6 DON'T COME ON. REMOVED & REPLACED BATTERY CHARGER/POWER SUPPLY AND BATTERY PACK IAW AMM 33-53-03. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 203-242) · corrosion level 2 · airframe 19,698 hrs · 22,807 cycles

LEVEL 2 CORROSION FOUND ON FWD CABIN SEAT TRACK, BETWEEN STA 203-242 RBL 21 INCH. REMOVED CORROSION AT FWD CABIN SEAT TRACK BETWEEN STA 203 TO STA 242 RBL 21 INCH. FOUND TO BE OUT OF LIMITS PER REF B717 SRM 53-20-52. REMOVED SEAT TRACK AT STA 203 - 265.5 RBL 21 INCH IAW DC9 SRM 53-05, FIG 4F. INSTALLED SEAT TRACK SECTION AT STA 203 TO STA 265.5 RBL 22 AS PER B717 SRM 53-05 FIG 4F.

Part: DETECTION SYS — NO TEST (NR 1 FIRE) · airframe 18,919 hrs · 20,937 cycles

FIRE TEST NR 1 FIRE HANDLE NO LIGHT. REPLACED LT ENG A LOOP.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 18,814 hrs · 20,679 cycles

MODERATE CORROSION ON THE LT WING REAR SPAR LWR TANG AT ARS 164 (AREA I/B FLAP ACT FITTING). ACCOMPLISHED PERMANENT REPAIR AS PER MESSAGE HWI 09-0047-08B AND DWG NR J060271.

Part: SPAR — CORRODED (TE FLAP) · airframe 18,814 hrs · 20,679 cycles

MODERATE CORROSION ON REAR SPAR LWR TANG AT XRS 267 (AREA O/B FLAP ACT FITTING). ACCOMPLISHED PERMANENT REPAIR PER BOEING MSSG. NR HWI 09-0047-08B AND DRWG NR J060271.

Part: STRUT — DISCHARGED (NLG) · airframe 17,832 hrs · 18,281 cycles

ATB - NOSE DID NOT RETRACT AFTER TAKEOFF. FOUND NOSE STRUT COMPRESSED NO LEAKS NOTED. REPLACED AIR CHARGING VALVE SERVICED STRUT PER MM32-21-01, RETRACTION CK GOOD.

Part: BRACKET — CRACKED (RT SPOILER)

RIGHT OUTBOARD SPOILER BRACKET CRACKED. REPAIRS IN WORK. (M)

Part: RELAY — INOPERATIVE (STAB TRIM)

PRIMARY TRIM INOPERATIVE. REPLACED PRIMARY TRIM DOWN BRAKE RELAY IAW MM. GROUND CHECK, OK.

Part: TIRE — VIBRATES (NLG)

KOA - FLT 157 - UNUSUAL SOUND HEARD FROM NOSE GEAR AREA DURING TAKEOFF ROLL. ABORTED TAKEOFF. RETURNED TO GATE. REPLACED NOSE TIRES, SPIN/SECURITY CHECK OK. PER MM 32-42-21. TAXI CHECK OK. (M)