ALASKA AIRLINES, INC. AND/OR HAWAIIAN AIRLINES, IN

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 33,351 hrs · 51,645 cycles

FWD LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. GROUNDED - YES. OPS CHECK OK PER AMM 33-51-00.

Part: DOOR — BINDING (ZONE 800) · airframe 46,601 hrs · 14,597 cycles

FA SAYS THE L1 DOOR IS STICKY, HARD TO OPEN AND CLOSE. GROUNDED - YES. CHECKED L1 DOOR HANDLE TORQUE REF AMM 52-11-00, WELL W/IN LIMITS, HAD INCOMING FLIGHT CREW OPERATE DOOR MULTIPLE TIMES, NO PROBLEMS, NO HISTORY 30 DAYS.

Part: HOUSING — MISSING (ZONE 200) · airframe 64,682 hrs · 10,515 cycles

3R EMERGENCY EXIT SIGN FELL OFF. GROUNDED - YES. REMOVED AND REPLACED 3R EMERGENCY EXIT SIGN. OPS/SECURITY CHECK GOOD. OK FOR SVC.

Part: LIGHT SYS — INTERMITTENT (ZONE 200) · airframe 10,561 hrs · 3,003 cycles

FA REPORTS AFT EMERGENCY LIGHTS RANDOMLY TURNED ON WITHOUT BEING ACTIVATED. GROUNDED - YES. PERFORMED IFIM 33-51-00-810-817 OPS TEST PASS, COULD NOT DUPLICATE DEFECT,NO HISTORY 30 DAYS.

Part: SMOKE DETECTOR — NO DISCREPANCY (ZONE 200) · airframe 25,382 hrs · 5,247 cycles

INFO TO MX: SMOKE LAVATORY SMOKE ECAM DURING CRUISE, F/A REPORTS PAX VAPING IN MID CABIN LAC ON A/C L SIDE. NO VISABLE DAMAGE. GROUNDED - YES. INFO NOTED BY MX. OPS CHECK OK PER AMM 26-17-00. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 200) · airframe 20,770 hrs · 4,558 cycles

SMOKE MX MSG ON ECAM. ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY SMOKE (WITH MOD 30354 OR WITH MOD 33100) (DISPATCH WITH THE ABOVE MAINTENANCE STATUS MESSAGE DISPLAYED ON ECAM IS PERMITTED WITHOUT CFDS INTERROGATION) ). GROUNDED - YES. PERFORMED TSM TASK 26-16-00-810-821-A. GROUND SCAN SHOWS NO FAULTS. TEST PASSED. A/C OK FOR SVC. PLACARD REMOVED.

Part: HOLDER — FOD (GIRT BAR) · airframe 35,157 hrs · 52,098 cycles

FA REPORTS THAT 1L DOOR GRIT BAR IS HARD TO REMOVE FROM HOLDER. GROUNDED - YES. REMOVED DEBRIS FROM 1L GRIT BAR HOLDER AS REQUIRED. OPS CHECK GOOD. OK FOR SVC.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 18,084 hrs · 5,310 cycles

AFT LEFT EMERGENCY LIGHT FAILED FUNCTIONAL CHECK. GROUNDED - YES. REPLACED M1673 BATTERY POWER SUPPLY REF BOEING AMM TASK 33-51-06-960-802. OP TEST GOOD WITH AFT LEFT EMERGENCY LIGHTS ILLUMINATING AS REQUIRED. NO FURTHER DEFECTS.

Part: FLT CONTROLS — FAULTED · airframe 39,927 hrs · 65,955 cycles

A/C ROLLED 15* RIGHT WING DOWN WITH CLEAN CONFIG TRIM ( AILERON& RUDDER) WITH FLAPS 40* AND GEAR DOWN AFTER HANDS OFF CONTROLS FOR 10 SECS. GROUNDED - YES. ON DEFERRAL.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 17,690 hrs · 5,109 cycles

ROW 17ABC LOWER EMERGENCY EXIT LIGHT ASSY HAS BULBS INOP. GROUNDED - YES. RELAMPED 17ABC LWR EMERY EXIT LIGHT ASSY, OPS CHECK GOOD REF B737 AMM 33-51-04.

Part: TIRE — FAILED (ZONE 700) · airframe 31,738 hrs · 10,207 cycles

TIRES 1 AND 4 BLOWN ON LANDING. GROUNDED - YES. ANTISKID WAS ON MEL WHEN INCIDENT OCCURRED. DUE TO TIRE BLOWOUT, REQUIRES CONDITIONAL INSP. PERFORMED TIRE BURST COND INSP REF AMM 05-51-54. DUE TO MULTIPLE FLAT SPOT TIRES PERFORMED FLAT SPOTTED COND INSP IAW AMM 05-51-16 STEP D/E. DURING CONDITIONAL INSP, FOUND RT MAIN LANDING GEAR INNER/CENTER DOOR DAMAGED REF L/P 61373794 FOR ADDITIONAL WORK. REF L/P 61373795 FOR 1 AND 2 MLG TIRE CHANGE. REF L/P 61373796 FOR 3 AND 4 MLG TIRE CHANGE. REF L/P 61373797 FOR #1 AND #4 MLG BRAKE CHANGE.

Part: BOLT — MISSING (ZONE 800) · airframe 77,228 hrs · 41,510 cycles

UNABLE TO OPEN L1 DOOR. GROUNDED - YES. DOOR STUCK PARTIALLY OPEN. CANNOT OPEN OR CLOSE. LOWER DOOR GATE IS STUCK. DURING INSPECTION FOUND VERTICAL ROD ATTACHMENT BOLT MISSING. REINSTALLED ATTACHMENT BOLT REF AMM 52-16-12. DOOR OPENS NORMALLY NOW. CHECKED L1 FORWARD ENTRY DOOR ADJUSTMENT CHECK. NO ADJUSTMENTS MADE. L1 DOOR ADJUSTMENT CHECK SATISFACTORY. PERFORMED L1 FORWARD ENTRY DOOR SYSTEM TEST. TEST PASSED PER AMM 52-11-00-820-801 FORWARD ENTRY DOOR ADJUSTMENT PER AMM 52-11-00-700-804. FORWARD ENTRY DOOR SYSTEM TEST.

Part: TEMP STRIP — PEELING (ZONE 900) · airframe 5,356 hrs · 795 cycles

TEMP STRIP IN FC LAV PEELING OFF. GROUNDED - YES. REMOVED AND REPLACED FC LAV TEMP STRIP. CHECKS OK. OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 36,032 hrs · 83,450 cycles

OVERWING EMERGENCY LIGHTS OUT. GROUNDED - YES. REPLACED OVERWING EMERGENCY LIGHT BATTERY PER AMM 33-51-06-400-801. OPS CHECK GOOD, OK FOR SERVICE.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 67,226 hrs · 20,577 cycles

WHILE PERFORMING T/C 78233001 FOUND BATTERY PACK M1673 FAILING CAPACITANCE CHECK. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1673 REF SMM 33-51-14-103 AND AMM 33-51-06. INSTALL TEST OK.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 67,226 hrs · 20,577 cycles

EMERGENCY AISLE LIGHT AT SEAT ROW 26ABC INOP. GROUNDED - YES. RELAMPED AISLE LIGHT AT SEAT ROW 26ABC AS REQ. OPS NORMAL.

Part: LIGHT — DETACHED (ZONE 200) · airframe 18,938 hrs · 5,706 cycles

FLOOR TRACK LIGHT TAPE PEELING NEAR L1. GROUNDED - YES. REMOVED AND REPLACED 2 FT OF PHOTOLUMINESCENT STRIP REF AMM 33-51-15.

Part: SMOKE DETECTOR — FAILED (ZONE 100) · airframe 35,898 hrs · 40,239 cycles

DMI# 407243 CARGO SMOKE AFT FAIL - LAST CARGO SMOKE DETECTOR AMBER [F]. LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM DETECTOR UNITS [ONE DETECTOR AT EACH LOCATION MAY BE INOPERATIVE AND THE REMAINING PORTIONS OF THE SMOKE DETECTION SYSTEM MAY STILL BEUSED.] . GROUNDED - YES. REMOVED AND REPLACED AFT CARGO COMPARTMENT SMOKE DETECTOR PER AMM 26-41-01. OPS CHECK GOOD. PLACARD REMOVED MIC SHEET CLEARED.

Part: ACTUATOR — UNSERVICEABLE (LEFT YAW DAMPER) · airframe 39,926 hrs · 65,954 cycles

ON LANDING, ACFT GAVE AN UNCOMMANDED LT WING DOWN. PILOT FLYING ABLE TO COUNTER WITH RT INPUT. WING ROLLED A FEW DEGREES BUT THE YOKE DID AN UNCOMMANDED LT INPUT OF ABOUT 30 DEGREES. GROUNDED - YES. VERIFIED LT SLAT DRIVE CYLINDER ROD ENDS ARE EQUAL. VERIFIED LEFT WING SLAT DRIVE CABLE TENSIONS WITHIN SERVICABLE LIMITS IAW AMM 27-8-00. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-02. BITE CHKD OK. OK FOR SERVICE.

Part: ISOLATOR MOUNT — CRACKED (ZONE 800) · airframe 62,188 hrs · 19,278 cycles

R1 DOOR AFT SLIDE ATTACH POINT FOUND WITH DAMAGED MOUNT (ISOLATOR). GROUNDED - YES. REMOVED R1 DOOR SLIDE AFT BACKPLATE, REMOVE AND REPLACED UPPER MOUNT (ISOLATOR), REINSTALLED BACKPLATE AND SLIDE MOUNT BRACKET IAW B737-800 SRM 51-40-02.

Part: LIGHT SYS — MALFUNCTIONED (ZONE 200) · airframe 61,469 hrs · 9,609 cycles

EMERGENCY LIGHTS REMAINED ON FOR THE ENTIRE FLIGHT. OFF SWITCH IN COCKPIT HAD NO EFFECT. GROUNDED - YES. PERFORMED BITE TEST OF CIDS AND EPSU SYSTEMS BITE TEST OK. PERFORMED FAULT ISOLATION TEST IAW AMM 33-51-00-810-803-A. OPS TEST PASSED. NO DEFECTS NOTED. SWITCH OPERATES LIGHTS NORMALLY. OK FOR SERVICE.

Part: BATTERY — FAULTED (ZONE 200) · airframe 50,854 hrs · 8,091 cycles

EPSU BATTERY 15WL FAULTING. GROUNDED - YES. REMOVED AND REPLACED BATTERY 15WL PER AMM 33-51-30 MECH 21315 07/31/2026. PENDING OPS. OPS TEST OK PER AMM 33-51-30. OK FOR SVC.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 14,359 hrs · 4,097 cycles

FWD CARGO COMPARTMENT AT AFT BULKHEAD FLOOR LEVEL STATION 520, THERE IS CORRODED CHORD/FRAME UNDER PANEL 121HW. GROUNDED - YES. CORROSION ON FLOOR SUPPORT AND RAIL ASSEMBLIES ARE FOUND TO BE OUT OF LIMITS IAW SRM 51-10--02. DUE TO NO ALLOWABLE LIMITS PERMITTED, REMOVED AND REPLACED SUPPORT ASSEMBLY AND RAIL ASSEMBLY IAW SRM 51-40-02-0G-0, REV 26 10.

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 44,473 hrs · 13,988 cycles

EMERGENCY LIGHT ON AFT BULL NOSE LH SIDE REMAINS ON. GROUNDED - YES. REPLACED POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.

Part: BATTERY PACK — UNSECURE (ZONE 200) · airframe 41,718 hrs · 72,335 cycles

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE. GROUNDED - YES. RESECURED EMERGENCY LIGHTS BATTERY PACK IN FWD GALLEY - OPS CHK OK ON GND - OK FOR SVC.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,690 hrs · 5,109 cycles

AFT CARGO COMPT RIGHT SIDE TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS727J+13 AND BS727+4. GROUNDED - YES. BLENDED AWAY CORROSION ORIGINAL THICKNESS .040 MAT LOSS AT GREATEST .006 IN VARIOUS PLACES, NEW THICKNESS .034 AREAS OUT OF LIMITS. COMPLETED REPAIR PER B737-MAX9 SRM 53-00-53-2R-5, SRM 51-40-02, AND BWDG 146A7500 REV.-.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,690 hrs · 5,109 cycles

AFT CARGO COMPT RIGHT SIDE TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS767 AND BS727J+13. GROUNDED - YES. BLENDED AWAY CORROSION. ORIGINAL THICKNESS .040, MAT LOSS IN VARIOUS LOCATIONS AT .009, NEW THICKNESS IN VARIOUS LOCATION .031. AREAS OUT OF LIMITS COMPLETED REPAIR PER B737-MAX9 SRM 53-00-53-2R-5, SRM 51-40-02, BDWG 146A7500 REV-.

Part: INDICATOR — MISSING (ZONE 900) · airframe 5,165 hrs · 773 cycles

LAV 4L TEMPERATURE INDICATOR STRIP IN WASTE BIM IS MISSING. GROUNDED - YES. FOUND STRIP DETACHED. RESTORED IN THE CORRECT POSITION OK. AMM 26-24-02.

Part: RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,359 hrs · 2,977 cycles

FWD CARGO PIT, AFT BULKHEAD LOWER RAIL HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT, AFT BULKHEAD LOWER RAIL IAW SRM 51-40-02, SRM 51-40-05, AMM 50-10-04, AND DWG 143A9481 REV-.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,690 hrs · 5,109 cycles

AFT PIT LEFT TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS727J+13 AND BS727+4 AS MARKS. GROUNDED - YES. BLENDED AWAY CORROSION, ORIGINAL THICKNESS .040, MAT LOSS AT GREATEST .017, NEW THICKNESS AT LOWEST .023. AREAS OUT OF LIMITS PER B737-MAX9 SRM 53-00-53-1A-2. ACCOMPLISHED REPAIR PER B737-MAX9 SRM 53-00-53-2R-5, SRM 51-40-02 AND BDWG 146A7500.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,690 hrs · 5,109 cycles

AFT PIT LEFT TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS747 AND BS727J+13. GROUNDED - YES. BLENDED AWAY CORROSION, ORIGINAL THICKNESS .040, MAT LOSS AT LOWEST .007 NEW THICKNESS .033, AREAS OUT OF LIMITS PER B737-MAX9 SRM 53-00-53-1A-2. COMPLETED REPAIR PER B737-MAX9 SRM 53-00-53-2R-5 SRM 51-40-02 AND BWDG 146A7500.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,690 hrs · 5,109 cycles

FWD CARGO PIT R/H TRANSITION PANEL STARTING AROUND STA 500C AND CONTINUING AFT TO REAR BULKHEAD PANEL HAS NUMEROUS AREAS OF CORROSION, GROUNDED - YES. BLENDED AWAY CORROSION ORIGINAL THICKNESS .040, MAT. LOSS AT GREATEST .009, NEW THICKNESS AT LOWEST .031, AREAS OUT OF LIMITS PER B737-MAX9 SRM 53-00-53-1A-2. COMPLETED AND INSTALLED REPAIR PER B737-MAX9 SRM 53-00-53-2R-5, SRM 51-40-02 AND BDWG 143A7500.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,578 hrs · 14,568 cycles

FWD WET AREA FLOOR SUPPORT HAS CORROSION BETWEEN BS 294-312, BL 0. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT LIMITS, REMOVED AND REPLACED FWD WET AREA FLOOR SUPPORT BETWEEN BS 294-312 BL 0 IAW B737-800 SRM 51-40-02-0G-0 STEP 4. B & 7. W= 2" O=.170" R= .144" L=3". D=.026".

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,578 hrs · 14,568 cycles

AFT WET AREA FLOOR SUPPORT STRUCTURE IS CORRODED BETWEEN BS 947-967 LBL 20. GROUNDED - YES. REMOVED AND REPLACED AFT WET AREA FLOOR SUPPORT STRUCTURE BETWEEN BS 947-967 LBL 20 IAW B737-800 SRM 51-40-02-0G-0, STEP 7.B & C. W: 2" / O: .066" /R: .034" /L: 2" /D: .032".

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,578 hrs · 14,568 cycles

AFT WET AREA FLOORBEAM BS 986 HAD CORROSION AT OTBD MOST HOES, RT SIDE. GROUNDED - YES. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6. W= 1" O= .150 R= .140 L= 1" D= .010.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,578 hrs · 14,568 cycles

AFT WET AREA FLOOR BEAM 986 HAS CORROSION AT OTBD MOST HOLES, LT AND SIDE. GROUNDED - YES. REPAIRED AFT WET AREA FLOORBEAM IAW SRM 53-70-51-2R-6. W= 1" O= .150 R= .106 L= 1 1/2" D= .044.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 70,076 hrs · 21,176 cycles

FWD WET AREA INTERCOSTAL STA 328 TO STA 344 LBL 47 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL I.A.W. B737-800 S.R.M. 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 70,076 hrs · 21,176 cycles

FWD WET INTERCOSTAL STA 277 TO STA 294.5 BL-0 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL I.A.W. B737-800 S.R.M. 51-40-02-0G-0.

Part: LENS — MISSING (ZONE 200) · airframe 12,346 hrs · 3,592 cycles

L2/17F EXIT SIGN MISSING IN FLIGHT. GROUNDED - YES. INSTALLED NEW COVER ON LOWER FORWARD EXIT SIGN REF AMM 33-51-01.

Part: SKIN — CRACKED (ZONE 300) · airframe 70,556 hrs · 21,317 cycles

LEFT HAND HORIZ STAB LOWER SKIN STA 138.70 HAS CRACK INBOARD OF RIB AFT OF FRONT SPAR AS MARKED. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB LOWER SKIN AT STA 138.70 USING MAT 2024-T3 .100 FOR THE DOUBLER AND 2024-T3 .063 FOR THE FILLER PER B737-800 SRM 55-10-01-2R-11. REPAIR IS A CAT "B" WITH AN INSPECTION THRESHOLD OF 56,000 TFC AND AN INTERVAL INSPECTION OF 9,000FC.

Part: SKIN — CRACKED (ZONE 300) · airframe 70,556 hrs · 21,317 cycles

LEFT HORZ STAB LOWER SKIN STA 167.10 HAS CRACK INBOARD OF RIB FORWARD OF THE REAR SPAR AS MARKED. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB LOWER SKIN AT STA 167.10 USING MAT 2024-T3 .100 FOR THE DOUBLER AND 2024-T3 .063 FOR THE FILLER PER B737-800 SRM 55-10-01-2R-11. REPAIR IS A CAT "B" WITH AN INSPECTION THRESHOLD OF 56,000 TFC AND AN INTERVAL INSPECTION OF 9,000FC.

Part: SKIN — CRACKED (ZONE 300) · airframe 70,556 hrs · 21,317 cycles

LEFT HAND HORZ STAB LOWER SKIN BETWEEN STA 120.30 AND 129.50 HAS CRACK JUST FORWARD OF THE REAR SPAR AS MARKED. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB LOWER SKIN BETWEEN STA 120.30 AND 129.50 USING MAT 2024-T3 .100 FOR THE DOUBLER AND 2024-T3 .071 FOR THE FILLER PER B737-800 SRM 55-10-01-2R-11 REPAIR IS A CAT "B" WITH AN INSPECTION THRESHOLD OF 56,000 TFC AND AN INTERVAL INSPECTION OF 9,000 FC.

Part: PCU — FAULTY (LEFT MLG WHEEL W) · airframe 44,797 hrs · 14,115 cycles

AIRCRAFT ROLLED RIGHT AS AIRSPEED INCREASED USED EXCESSIVE AILERON TRIM, ATTEMPTED TO COMPENSATE WITH RUDDER TRIM. AT CRUISE THERE WAS (FL360) SHUDDERING AT .78 SLOWED TO .75 AND SHUDDERING WAS SIGNIFICANTLY LESS. USED AILERON TRIM W/ A/P OFF BUT DID NOT CORRECT SITUATION. GROUNDED - YES. DIVERSION - PERFORMED LEFT AND RIGHT AILERON INSPECTION REF 27-11 TASK 802. ITEM A THRU D. NO DEFECTS NOTED. REMOVED AND REPLACED UPPER AILERON PCU (SYS B) REF AMM 27-11-71. REMOVED & REPLACED LOWER AILERON PCU (SYS A) REF AMM 27-11-71. ACCOMPLISHED BLEED, LEAK CHK, ADJUSTMENT, OPERATIONAL, AND TRAVEL TESTS FOR BOTH PCUS REF SAME AMM. ALL TESTS PASSED. ACCOMPLISHED RUDDER TRIM SYSTEM TEST REF AMM 27-21-00, NO DEFECTS NOTED.

Part: LIGHT — DETACHED (ZONE 200) · airframe 40,641 hrs · 12,450 cycles

FA REPORTS LIGHT FROM CEILING FELL OUT AND IS DANGLING (EMERGENCY LIGHT). GROUNDED - YES. REMOVED, REPLACED, AND TESTED EMERGENCY LIGHT AISLE LIGHT ABOVE ROW 25 RIGHT PER AMM 33-51-03-960-805 - OPS NORMAL.

Part: WINDSHEAR SYS — ACTIVATED · airframe 35,651 hrs · 82,828 cycles

TAKEOFF ABORTED AT 80 KTS DUE TO WINDSHEAR ALERT ON FLIGHT 1185. GROUNDED - YES. PERFORMED FIM 34-45-TASK 801. NO FAULTS NOTED. OK TO CONTINUE.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 70,076 hrs · 21,176 cycles

FWD CARGO STRINGER CLIP STA 500I STRINGER 26R CRACKED. GROUNDED - YES. REPLACED CLIP ON FWD CARGO STA 500I AND STR 26R IAW B-737-800 SRM 51-40-02-0G-0 PAR 7.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 70,076 hrs · 21,176 cycles

AFT CARGO R/H CARGO TRACK AT RBL 13 CRACKED AT STA 727D, 727E, 727G, 727I AND 747. GROUNDED - YES. REMOVED AND INSTALLED NEW CARGO TRACK AT RBL 13 FROM STA 727A TO STA 887 IAW B737-800 SRM 51-40-02-0G-0.

Part: SMOKE DETECTOR — FAULTED (ZONE 100) · airframe 2,419 hrs · 295 cycles

DETECTOR 7L, FWD CARGO STATUS MSG. GROUNDED - YES. IAW FIM 26-10-F6-67A-421A-A, CYCLED C/B FOR CARGO SMOKE DETECTOR, GORUND TEST PASSED A/C OK FOR SERVICE.

Part: ELECTRONIC UNIT — FAULTED (ZONE 100) · airframe 184 hrs · 52 cycles

ON DESCENT THROUGH 12000FT, AFT CARGO FIRE WARN CAME ON. THE LIGHT WENT OUT BEFORE A CHECKLIST WAS STARTED... MAYBE 10 SEC. UPON TOUCHDOWN ON RWY LIGHT AND WARNING CAME ON AGAIN. QRC & QRH WERE RAN, HALON WAS DISCHARGED INTO AFT CARGO. THE CREW ADVISED ATC AND THE PORT FIRE DEPARTMENT RESPONDED ON THE TAXIWAY AND VERIFIED NO FIRE PRESENT. GROUNDED - YES. ACCOMPLISHED AFT CARGO ELECTRONICS UNIT (CEU) BITE TEST, NO FAULT FOUND. PRECAUTIONARY REMOVED AND REPLACED AFT CARGO ELECTRONICS UNIT (CEU) AND ALL SIX AFT SIX CARGO SMOKE DETECTORS. REF AMM 26-16-02/401. ACCOMPLISHED CARGO ELECTRONICS UNIT INSTALLATION TEST PER AMM 26-16-02-710-801 AND CARGO SMOKE DETECTION OPERATIONAL TEST PER AMM 26-16-00-70-801. TEST PASSED. REF TASK CARDS 26-360-00 FOR REPLACEMENT OF BOTH CARGO FIRE BOTTLES, OPS AND LEAK CHECKS GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 40,029 hrs · 12,280 cycles

AFT EXIT ROW LEFT OVERWING LIGHT INOPERATIVE. GROUNDED - YES. REMOVED & REPLACED LEFT AFT EXIT ROW OVERWING LAMP IAW AMM 33-51-04. OPS CHECK GOOD.