N27239

Part: SKIN — CRACKED (ZONE 300 ELEV) · airframe 79,296 hrs · 29,660 cycles

PUNCTURE FOUND AT LT ELEVATOR UPPER SURFACE LOCATED 10 INCHES FOR FWD EDGE AND 103 INCHES FROM I/B EDGE. APPLIED PERMANENT REPAIR ON DAMAGED AREA ON LT ELEVATOR UPPER SURFACE LOCATED 10 INCHES FOR FWD EDGE AND 103 INCHES FROM I/B EDGE REF SRM 51-70-04-2R-1 PARAG 4-F & SRM 51-70-04-2R-0 REPAIR GENERAL PARAG 4-N-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

FOUND CORROSION AT LT MLG FAILSAFE STRAP EXTERNAL AT STA 663.75 WL199. PERFORMED A REPAIR TO THE OUTER SURFACE OF THE BS 663.75 REAR SPAR BULKHEAD FRAME LT FAILSAFE STRAP NEAR WL 199 IAW AAR-MIA ESR-WI NO.: 2023704-15-12772 AND EC/RA 5340-02240. INITIATE A DIP LOGPAGE TO READ AS FOLLOWS: AFTER THE ACCUMULATION OF 49,900 TOTAL ACFT FLT CYCLES, BUT BEFORE 50,000, PERFORM AN INSPECTION OF OUTER SURFACE OF BS 663.75 REAR SPAR BULKHEAD FRAME LT FAILSAFE STRAP NEAR WL 199 ON ACRT N27239 IAW PART 2 OF LATEST REVISION OF ECRA 5340-02240.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 79,293 hrs · 29,659 cycles

LEFT VAPOR BARRIER UPPER ATTACHED ANGLE CRACKED AT LBL 7, BS 663. REMOVED AND FABRICATED A NEW UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5, FIGURE 202, DETAIL B, SHT 4.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 79,293 hrs · 29,659 cycles

CABIN AFT WET AREA FLOORBEAM CORRODED BS 967, RBL 16. REPAIR ACCOMPLISHED IAW ESR-WI 2023704-10-12752 AND EC/RA 5370-01193.

Part: DECK PLATE — DAMAGED (ZONE 200) · airframe 79,293 hrs · 29,659 cycles

FLIGHT DECK ENTRY FLOOR SKIN CORNER EDGE DAMAGED AT LBL 11, BS 277. REPAIRED FLIGHT DECK ENTRY FLOOR SKIN PANEL CORNER EDGE AT LBL11 STA 277 IAW SRM 53-10-51-2R-2.

Part: PRESSURE BLKHD — CRACKED (ZONE 100) · airframe 79,372 hrs · 29,702 cycles

FOUND CRACK AT BS 1016 AFT PRESSURE BULKHEAD, 2" ABOVE WL 208.1 AND LBL 3. REPAIRED THE DAMAGED AFT PRESSURE BULKHEAD WEB IAW ESR-WI 2023704-24-12817 AND EC/RA 5380-01428,

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

CORROSION CABIN AFT WET AREA FLOORBEAM STA 947.5, LBL9. (REF AAR N/R 97533673) REMOVED THE DAMAGED FLANGES OF THE UPPER TEE OF THE FLOORBEAM BETWEEN LBL 34.5 TO RBL 32.9, INSTALLED NEW TEE ANGLE AND REPAIR PARTS IAW SRM 53-70-51-2R-5 REPAIR 5 WITH THE DEVIATIONS APPROVED IN EC/RA 5370-01194 AND AAR-MIA ESR-WI 2023704-13-12761.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

CORROSION ON CABIN AFT WET AREA FLOORBEAM STA 986.5 BETWEEN BL-0 AND RBL 54. REMOVED CORRODED EXISTING TEE CHORD REPAIR AT STA 986.5 FROM RBL 54 TO LBL 50 IAW SRM 51-40-02-0G-0, CUT AND REMOVED THE REMAINING DAMAGE FLANGE FROM LBL 50 TO LBL 54 IAW SRM 53-70-51-2R-4. INSTALLED NEW T-CHORD REPAIR AND ASSOCIATED REPAIR PARTS FROM LBL 55 TO RBL 55 AS PER SRM 53-70-51-2R-4 AND EC/RA 5370-01192.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 79,293 hrs · 29,659 cycles

MAIN CABIN FLOOR SUPPORT WEB CRACKED AT RBL 39 STA 663.75 REMOVED AND CUT THE WEB DAMAGED FROM STA 663.75 BETWEEN RBL38 TO RBL60. INSTALLED NEW WEB AND REPAIR PARTS AT STA 663.75 BETWEEN RBL 30 TO RBL 60 IAW B737 SRM 53-40-51-2R-2 AND SRM 51-40-02-0G-0.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

AFT PASSANGER CABIN STA 947 RBL 54 (R2 DOOR) INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED INNER CHORD AT AFT PASSENGER CABIN STA 946 RBL 54" (R2 DOOR) IAW SRM 51-40-02-0G-0 AND DWG 147A8501.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

AFT CABIN STA 986 LBL 55 WEB UNDER L/H INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED WEB AT AFT CABIN STA 986 LBL 55 WEB UNDER L/H INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501 SHEET 23.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

CORROSION ON CABIN FWD WET AREA R1 DOOR LOWER INNER CHORD BETWEEN STA 294 AND STA 328. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED INNER CHORD, AT CABIN FWD WET AREA R1 DOOR. LOCATED AND DRILLED NEW INNER CHORD, INSTALLED NEW INNER CHORD AT CABIN FWD WET AREA R1 DOOR LOWER I.A.W. DWG 141A8310 & SRM 51-40-02-0G-0 G.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

AFT PASSANGER CABIN BS 947 LBL 54 (L2 DOOR) INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED INNER CHORD AFT PASSENGER CABIN STA 946 LBL 54" L2 DOOR AS PER SRM 51-40-02-0G-0 AND DWG 147A8501 SHEET 67.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

FWD PASSANGER CABIN BS 312 LEFT SIDE (L1 DOOR) INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FWD PASSANGER CABIN (L1 DOOR) INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 1.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,293 hrs · 29,659 cycles

AFT CABIN STA 986 RBL 55 WEB UNDER R/H INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED WEB AT AFT CABIN STA 986 RBL 55 UNDER R/H INNER CHORD IAW SRM 51-40-02-G0-0 AND DWG 147A8501 SHEET 25.

Part: ACTUATOR — FAULTED (AILERONS) · airframe 79,285 hrs · 29,655 cycles

THREE UNCOMMANDED RIGHT ROLL INPUTS MADE WHILE ON COMMAND A AUTO PILOT. THE FIRST HAPPENED THRU CHECKED DFCS BITE NO FAULTS NOTED, ALSO CHECKED SMYD COMPUTERS ALSO NO FAULTS NOTED. TEC SUPPORT RECOMMENDS AUTO PILOT A AILERON ACTUATOR REPLACEMENT REMOVED AND REPLACED AILERON AUTOPILOT ACTUATOR A REF. AMM 22-11-25-400-801 LEAK CHECKS AND OPS CHECKS GOOD. INSP INSTALLATION OF THE AILERON A/P ACRUATOR A IN REF TO AMM 22-11-25-400-801. ACTUATOR LKS OPS CHECKS GOOD.

Part: COVER — DETACHED (ZONE 200) · airframe 79,205 hrs · 29,617 cycles

20C EMERGENCY EXIT LIGHTING MISSING FOUND 20C RED EMERG LIGHT COVER MISSING. REPLACED REF MM 33-51-11. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 79,109 hrs · 29,576 cycles

RT WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FUSE 4 ON BATTERY PACK M1695. OPS CHECK GOOD. REF AMM 33-51-06.

Part: LAVATORY — ODOR (ZONE 200) · airframe 78,392 hrs · 29,245 cycles

EXTREME SEWER SMELL ON TAXI OUT OF LGA AND ORD ...BOTH FLTS...D ISAPPATE AFTER TAKEOFF.AFT GALLE DEBRIEFED FLIGHT CREW, SPECIFIED SMELL WAS DURING TIME ON APU BLEED, RAN APU AND BLEED AIR MULTIPLE TIMES, NO SMELL NOTED. PER CREW LAV E WAS WORST SMELL, REMOVED AND INSTALLED LAV E TOILET SHROUD IN REF AMM 38-32-01, NO FOREIGN MATERIAL NOTED AT THIS TIME

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 78,377 hrs · 29,237 cycles

REMOVED L1 DOOR SLIDE TO F.O.M REINSTALLED ESCAPE SLIDE PACK AND COVER ON L1 DOOR REF AMM 25-66-01-400-803 OPS CHECK GOOD VERIFIED ESCAPE SLIDE PACK AND COVER ON L1 DOOR REF AMM 25-66-01-400-803 OPS CHECK GOOD

Part: BULB — BURNED OUT (ZONE 200) · airframe 77,295 hrs · 28,736 cycles

RT OVERWING EMERGENCY EX IT LIGHT BURNED OUT PLACED NEW SERVICEABLE BULB IN THE AFT RH OVERWING OUTSIDE PATH LIGHT AS REQUIRED , NO ADDITIONAL DEFECTS NOTED , LIGHT NOW WORKS NORMAL.

Part: TIRE — FAILED (ZONE 700) · airframe 76,800 hrs · 28,497 cycles

03 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT.#3 MLG TIRE FAILURE REMOVED AND REPLACED NUMBER THREE TIRE IN REF WITH AMM 32-45-11. TEMPORARILY INSTALLED SAFTY BOLTS ON AXLE NUT ON RUNWAY DO TO BAD HARDWARE. NEW CORRECT HARDWARE SENT TO MCO NORTH HANGAR OFFICE. IPC REF 32-41-11-03. INSTALLED NEW SAFTEY HARDWARE REF AMM 32-45-11 R&R'D THE #3 MLG TIRE REF AMM 32-45-11, AND INSTALLED NEW HARDWARE SAFTEY BOLTS. 04 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT.#4 MLG WHEEL ASSY NEEDS TO BE CHANGED DUE TO #3 MLG TIRE FAILURE. REMOVED AND REPLACED MLG #4 TIRE REF AMM 32-45-11.

Part: SKIN — CRACKED (ZONE 500) · airframe 76,800 hrs · 28,497 cycles

SUSPECTED CRACK IN LH WING LOWER OUTBOARD SKIN, AT OTBD MOST FASTENER OF S-9 BETWEEN WSTA 564.5 AND WSTA 591.5. INSPECTION VERIFY CRACK IN LH WING LOWER OUTBOARD SKIN PANEL AND STRIPPED PAINT AS REQUIRED IN AREA THAT CRACK WAS FOUND. S-9 CRACK BETWEEN WSTA 564.5 AND WSTA 591.5 APPLIED SECOND COAT OF PAINT STRIPPER TO SKIN WHERE CRACK WAS APPLIED THE 3RD COAT OF PAINT STRIPPER ON THE SKIN WHERE THE INDICATED. MCO TIME 0900 SUSPECTED CRACK IS LOCATED AT 4:00 PM 9/10/24. VERIFIED CRACK WITH HIFC PART 6, 51-00-00 PRCOEDURE 23. IN LH WING LOWER OUTBOARD SKIN PANEL AND S-9 CRACK BETWEEN WSTA 564.5 AND WSTA 591.5 CRACK FOUND TO BE 1.7 IN LONG. REMOVED REMAINDER OF PAINT STRIPPER, CLEANED, AND REQUESTING INSPECTION TO VERIFY CRACK VERIFIED REMOVAL OF REMAINING FASTENERS AT FRONT SPAR PER AVO # 239-24-09-08-01 STEP A.2. REMOVED FASTENER ON STR 8 AND 9. AND PARTIAL FRONT SPAR PER AVO VERIFIED REMOVED FASTENER ON STR 8 AND 9. AND PARTIAL FRONT SPAR REMOVED REMAINING FASTENERS AT FRONT SPAR PER AVO # REMOVED REMAINING FASTENERS AT FRONT SPAR PER AVO # # 239-24-09-08-01. PER AVO # 239-24-09-08-01. 239-24-09-08-01. 239-24-09-08-01. PO# 14497302330, ORIGINAL THICKNESS 0.160 MILLED DOWN TO 0.130 FOR FILLER CORRECTION. VERFIED: PERFORMED TRIM OUT OF DAMAGED PORTION OF SKIN. PER AVO: ACOMPLISHED HFEC INSPECTION OF TRIMMED EDGES PER 737 NDT MANUAL VEREFIED PERFORMED AN INSURANCE CUT AROUND EDGE OF THE TRIM-OUT. VEREFIED HFEC SURFACE INSPECTION PER 737NDT MANUAL PART 6, PERFORMED HFEC PART 6,5

Part: HMU — NONE (ENGINE 1) · airframe 72,328 hrs · 26,456 cycles

CREW REPORTED E1 FAILURE DURING CLIMB THRU FL210. ALL TAKE OFF P ARAMETERS NORMAL. ENGINE STARTED SLOW ROLL BACK AT FL210. CREW F LLOWED QRH, SHUT DOWN ENGINE CREW DEBRIEF: NORMAL T/O PARAMETERS; E1 SLOW ROLL BACK REF FIM 73-31 TASK 803 FOR FUEL FLOW WAS NOT DETECTED DURING ACCOMPLISHED OVERWEIGHT LANDING INSPECTION PER AMM ACCOMPLISHED INSPECTION OF ENGINE AFTER WINDWILLING PER AMM DURING CLIMB THRU FL210. CREW REPORTED WINDMILL TIME 20 MINUTES START ATTEMPT, AT STEP F.(2) WIRE AND VOTAGE CHECKED OK. 05-51-35-210-801. NO SIGNS OF DAMAGE OR LEAKAGE, OK FOR SERVICE 71-00-00-210-802-F00. REPORTED WINDWILL TIME OF 20 MINUTES, NO WITH OIL PRESSURE. LANDING WT 149963 NORMAL LANDING NO HARD BRAK FURTHER ACTION REQUIRED ING. ALL E1 PARAMETERS ROLL BACK AT SAME RATE. ENG FAIL ON PER FIM TASK 73-31 TASK 803 STEP F.(2)F. NEXT STEP IS REPLACEMENT OF HMU ADD FAULT: 73-11551 REF LOG PAGES #3939111 AND #3939102 FOR CORRECTIVE ACTION TAKEN OPS CHECK GOOD ON GROUND RUN IAW AMM 71-00-00

Part: SKIN — CORRODED (STA540/BL0) · airframe 72,317 hrs · 26,450 cycles

B737-06-3-0026, FUSELAGE EXTERNAL SKIN HAS CORROSION BLISTER AT STA 540 AND BL0. REFER TO PEMCO NR 13291.0282. FEBRUARY 14, 2025. INITIATING DTA DIP PER EC/RA 5330-07054 TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/RA 5330-07054 ON OR BEFORE RE-INSP BY Q966 RE-INSP BY Q966 ACCOMPLISHED REPAIR PER PEMCO EA PD37-53-3430 AND EC/RA 5330-07054 AS TRANSCRIBED ON PEMCO NR 13291.0282

Part: INDICATOR — UNRELIABLE (FO SIDE) · airframe 70,457 hrs · 25,634 cycles

AIRSPEED AND ALT UNRELI ABLE AT FL350 F/O INST WERE NOT RELIABL E VISUAL INSPECTION. PUMP THE AIRCRAFT UP AND VERIFY ALL AIRSPEED AND ALT INDICATORS ARE WORKING NORMAL. FO AIRSPEED AND ALT RETURNED TO NORMAL ONCE THEY HIT LOWER TALKED TO CREW THEY REPORTED THAT AIRSPEED AND ALT WENT BACK TO ALTITUDE. CHECK PROPE HEATS AND MAKE SURE THEY ARE GETTING HOT NORMAL AS THEY GOT CLOSER TO LANDING. MOST LIKELY THE F/O PROBE ENOUGH. MOST LIKELY PROBS GOT ICE ON THEM AND MELTED AT LOWER IS NOT HEATING UP CORRECTLY AND GOT ICE ON IT WHEN THEY WERE AT ALTITUDE. DIDNT SEE ANY WEAR OR DAMADGE ON PROBES WHEN DOING ALTITUDE. RECOMEND CHECKING THE HEAT ON ALL THE PROBES AND THEN ACCOMPLISHED PITOT HEAT TEST REF. 30-31-00-730-801 AND STATIC REF. AMM TASK 34-21-01-400-801. AND TOTAL AIR SYSTEM PRESSURIZATION REF. AMM TASK ROTABLE PARTS CHANGE WAS INDICATED - TT # 1813307 SN OFF 3250 34-11-00-790-802 NO FAULTS NOTED AT THIS TIME. REMOVED AIR DAYA REF UNIT. INSTALLED SERVICEABLE AIR DATA UNIT. OPS CHECK GOOD ADD EMP:U112733 UNIT, ADIRU, AI OFF 60-3421-9-0001 3250 ON 60-3421-9-0001 5051

Part: NONE — NONE · airframe 69,947 hrs · 25,424 cycles

THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022040600896 SUBMITTED ON 04/06/22. NEAR NO. 3 SLAT ON LOWER EDGE HAS A MISSING PANEL. REPLACED MISSING SLAT PANEL PER EA 00-0592-3-4149. FUNCTION TESTED SLATS ALL FUNCTION TESTED UP AND DOWN OK AT THIS TIME

Part: PITOT SYSTEM — CLOGGED (PITOT) · airframe 68,690 hrs · 24,903 cycles

REJECTED T/O IAS DISAGRE E JUST AFTER 100 KNOTS A/T FAILED THEN A/S CAPT SIDE REMOVED CAPT AND FO PITOT ADM QUICK DISCONNECT FLUSHED PITOT SYSTEM FOUND MUD DOBBER LOGDGED ON THE CAPT PITOT. CLEARED PITOT SYSTEM LINES AND PERFORMED AIRSPEED LEAK TEST. OPS CHK NORMAL. REF AMM 34-11-00 ACP SECURITY OF CAPT AND FO PITOT ADM QUICK DISCONNECT. DUE TO REJECTED TAKE-OFF, PERFORMED "HIGH ENERGY STOP CONDITIONAL INSPECTION - IN CAUTION RANGE", REF AMM 05-51-07 AND EC/RA 0500-01012. WHEELS, TIRES, BRAKES, AND BLOCKER DOORS ARE IN GOOD CONDITION. FOREIGN OBJECT FOUND ON THE CAPT PITOT WAS SOME SORT OF BLACK EXOSKELETON INSECT. WAS CONFIRMED BY MY LEAD.

Part: LIGHT — BROKEN (CABIN) · airframe 68,027 hrs · 24,632 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK - FLOOR PROXIMTY LIGHTS ON SEATS 12C AND 29C INOP. REMOVED AND REPLACED WHITE LIGHT ON SEATS 12C & 29C OPS CHECKED GOOD REF. AMM 33-51-11-960-802.

Part: FIRE DETECTOR — INTERMITTENT (NR 2 ENGINE) · airframe 68,027 hrs · 24,632 cycles

NO2 ENG OVHT. FOLLOWED QRH. SHUT ENG DOWN CREW DEBRIEF OVERHEAT WAS HIGH NACELLE TEMP. LIGHT. REMOVED AND REPLACED AFT RIGHT ENGINE FIRE DETECTOR ASSEMBLY PER AMM TASK 26-11-01-000-802. OPS CHECKS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1085427 SN OFF 1792 DETECTOR, FIRE, OFF 29-2611-9-0004 1792 ON 29-2611-9-0004 5562 DETECTOR, FIRE, OFF 29-2611-9-0003 1813 ON 29-2611-9-0003 4887 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1306612 SN OFF 1813 AMM26-11-01/401. REPLACED #2 ENG. LOWER CORE FIRE DETECTOR LOOP IAW REMOVED REPLACED LOWER FAN CASE FIRE DETECTION LOOP P/N902016-01 . FIRE TEST PASSES. REF AMM 26-11-01/401 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1013916 SN OFF 1447 DETECTOR, FIRE, OFF 29-2611-9-0002 1447 ON 29-2611-9-0002 6426 DETECTOR, FIRE, OFF 29-2611-9-0001 1871 ON 29-2611-9-0001 2014 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1160242 SN OFF 1871 OPERATIONAL TEST AMM 26-11-01-400-802, 26-11-00-710-801. REMOVED AND REPLACED UPPER FAN FIRE LOOP AND PERFORMED RAN ENGINE FOR 5 MINUTES WITH BLEED ON AND PACKS LIGHT REMAINED EXTINGUISHED. PERFORMED BITE ON BOX NO FAULTS REF. AMM 26-11-00-710-801, 71-00-00-800-803-F00.

Part: TIRE — DAMAGED (MLG) · airframe 68,004 hrs · 24,622 cycles

PDA 3 PDA 3 #3 TIRE HAS MISSING CHUNK, WILL TO C/W AMM 05-51-54, AND REPLACE TIRE. ACTIVITIES ACCOMPLISHED INSPECTION REF: MM 05-51-54. CHUNK MEASURES 1/8" DEEP AND 3/4" ROUND. NO DAMAGE NOTED. LOG PAGE 6613853 FOR TIRE CHANGE.

Part: ATTACH FITTING — MISSING (LT MLG DOOR) · airframe 67,710 hrs · 24,507 cycles

PDA 3 LT MLG FLYING DOOR ATTACH HARDWARE IS COMPLETELY MISSING AT AFT LOWER ATTACH POINT AND THE DOOR IS LOOSE PHOTO ADDED REMOVED LT MLG FLYING DOOR ASSLY (CENTER & INNER DOOR ASSLY) -- REQUEST CDL 32E. DISPATCH DESK: 26 NAME: DK DATE: 06-JUN-21- TOMC APPROVED FOR CDL 32E FOR ACFT 0239. CDL APPLIED. ROUTED REMOVED DOOR ASSLY TO MOR STORES RON HOLD. LP OPEN DETAISL AWAITED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,901 hrs · 24,188 cycles

PAX CABIN SEAT 20 L/H RED EMERGENCY LIGHT LENS BROKEN. REF. AAR N/R: 9737524 GENERATED BY: V915555 REMOVED AND REPLACED AT SEAT ROW 20 L/H EMERGENCY LIGHT LENS ( RED ) REF. B737 AMM 33-51-11-960-801 AND DRWG#3350DD14973 REV."A" OPERATIONAL TEST NORMAL.REF. AAR N/R:9737521 WORK ACCOMPLISHED BY: V892138, INSPECTED BY: V915555 ADD EMP:V892138

Part: INTERPHONE — FAILED · airframe 66,702 hrs · 24,116 cycles

RADIO 2 INOPERABLE COULD NOT HEAR ATC ON COMM 1 OR 2 CAN HEAR/TRANSMIT ON COM 1 IN ALTN MODE ONLY. REMOVED REU PER B737-789 AMM23-51-01-000-801. INSTALLED A SERVICABLE REU, PER B737-789 AMM 23-51-01-000-802 UP TO STEP F. REU INSTALLATION TEST. REU MFG P/N: 5140-1-7, S/N OFF: 2576, S/N ON: 2236. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1996240 SN OFF 2576 UNIT, ACCY, AUD OFF 29-2351-9-0001 2576 ON 29-2351-9-0001 2236. PERFORMED REU INSTALLATION TEST, PER AMM 23-51-01. OPERATIONS CHECK GOOD.

Part: BUSTLE — LOOSE (R1 DOOR SLIDE) · airframe 66,644 hrs · 24,096 cycles

ESCAPE SLIDE PACK BUSTLE LOOSE DOOR 1R EXCESS SLIDE MATERIAL BETWEEN BAR AND PACK SHOW ING INSPECTED 1R DOOR ESCAPE SLIDE FOR EXCESS SLIDE MATERIAL BETWEEN BAR AND PACK, FOUND IT NORMAL IN ARMED AND DISARMED POSITION, NO DISCREPANCIES NOTED.

Part: SKIN — DENTED (BS 794) · airframe 64,787 hrs · 23,403 cycles

FUSELAGE AFT CARGO DOOR CUTOUT UPPER EXTERNAL EDGE HAS A DENT AT BS 794.3 + 8" S-18R + 3" (REF NR 99854117) REPAIRED AFT CARGO DOOR CUT-OUT UPPER EXTERNAL SKIN DENT AT BS794.3 + 8" AND STR 18R + 3" AS PER B737 SRM 53-00-01 FIG 202. ADD EMP:V900430 INSP C/W

Part: SKIN — DENTED (FUSELAGE) · airframe 64,787 hrs · 23,403 cycles

FOUND DENT IN FUSELAGE SKIN APPROXIMATELY 6" AFT AND 3" ABOVE THE FORWARD CARGO DOOR FORWARD UPPER CUTOUT.NO DMG DOT IN THE AREA. ON OR BEFORE THE AIRCRAFT REACHES 34000 TOTAL AIRCRAFT FLIGHT CY CLES PERFORM AN INSPECTION PER PART 2 OF ECRA 5331-02497. PLANNI NG TO CONTACT EG AFTER 31000 CYCLES BUT BEFORE 320000 CYCLES. ACCOMPLISH PERMANENT REPAIR PER PART 3 OF ECRA 5331-02491 WITHIN 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 45,000 TOTAL FLIGHT CYCLES BUT BEFORE 48,000 FLIGHT CYCLES FOR PERMANENT REPAIR REQUIREMENTS IN REFERENCE WITH ECRA 5331-02491 TOMC-APPROVAL FROM SC1ELBYC COMMENT INSP C/W CORRECTING SOURCE REFERENCE TO ECRA 5331-02497 WITH CORRECTED CRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART2 OF ECRA LIMITAIONS OF:ON OR BEFORE THE AIRCRAFT REACHES 34,000 TOTAL AIR BUT BEFORE 32,000 CYCLES FOR THE INSPECTION REQUIREMENTS. 5331-02497.

Part: FLOORBEAM — SCRATCHED (BS 328) · airframe 64,787 hrs · 23,403 cycles

FWD CABIN BS 328 FLOOR BEAM HAS SCRATCHED FROM RBL 12 TO RBL 48. (REF NR 99853400) REPAIRED FLOOR BEAM AT STA 328 BL "0" TO RBL 63 AS PER BOEING 737 DRM 53-10-51 REPAIR 7 AND RES 2015289-15 AND EC/RA 5311-02319

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 64,787 hrs · 23,403 cycles

2EA CRACKS FOUND IN INSPECTION AREA CENTER WING BOX REAR SPAR VE RTICAL PRESSURE WEB BETWEEN RBL40 AND RBL45.64, BETWEEN WL200.6 AND WL192.0, CRACKS MARKED ACCOMPLISHED CATEGORY "B" REPAIR AT CENTER WING BOX REAR SPAR VE RTICAL PRESSURE WEB BETWEEN RBL 40 AND RBL 45.64 BETWEEN WL.200. 6 AND WL 192.0 AS PER B-737-800 SRM.57-10-10-REPAIR 3 ALTERNATIV ES 2 FIG.204 AND TABLE 202.(FOR DETAILS SEE PARTIAL WORK). THIS REPAIR REQUIRES SUPPERMENTAL INSPECTION AS GIVEN IN TABLE 202 ADD EMP:V917221 REPAIRS, FIG 204.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 64,787 hrs · 23,403 cycles

AFT CABIN BS 986.5 RBL 43 HAS CORROSION AROUND FASTENER HOLE AS MARKED. [DOT 124-013] REF. AAR N/R: 99853333 REMOVED "TEE" CAP OUT OF LIMITS AT STA 986.5 LBL 38 TO RBL 50. FABRICATED "TEE" CAP AND INSTALLED STA 986.5,LBL 38 RBL 50 AS PER B-737-800 SRM 51-40-02,51-40-05,51-20-01 & EC/RA#5321-01498

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

L\H HORIZONTAL STAB RIB AT STA.92.70 #3 STIFFNER CRACKED AT LWR END. REF. AAR N/R: 99853795 ORIGINATED BY EMPLOYEE V915555 PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB STA 92.70,#3 AND HORIZONTAL STAB RIB STA 92.70 INSTALLATION WILL BE ACCOMPLI SHED ON TASK CARD #99854119. STIFFNER IAW B737-800 SRM 55-10-09.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

L\H HORIZONTAL STAB RIB AT STA.92.70 #2 STIFFNER CRACKED AT LWR END. REF. AAR N/R: 99853794 ORIGINATED BY EMPLOYEE V915555 PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB RIB STA 92.70, #2 AND HORIZONTAL STAB RIB STA 92.70 INSTALLATION WILL BE ACCOMPLI SHED ON TASK CARD #99854119. STIFFENER IAW B737-800 SRM 55-10-09.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

L\H HORIZONTAL STAB RIB AT STA.92.70 #4 STIFFNER CRACKED AT LWR END. REF. AAR N/R: 99853796 ORIGINATED BY EMPLOYEE V915555 PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB STA 92.70, #4 AND HORIZONTAL STAB RIB STA 92.70 WILL BE ACCOMPLISHED ON TASK CARD # 99854119 STIFFENER IAW B737-800 SRM 55-10-09.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

LT HORIZONTAL STABILIZER INSPAR RIB 2 - #4 STIFFENER IS CRACKED AT LOWER END. PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB RIB STA 92.70, #1 STIFFENER IAW B737-800 SRM 55-10-09.REINSTALLED RIB AFTER REPAIR WAS ACCOMPLISHED REF. USED SRM 51-40-02.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

R/H HORIZONTAL STABILIZER IN-SPAR RIB STA 101.90 CRACK LOCATED AT TRANSITION RADIUS OF VERTICAL STIFFENER #1. (MKD 126-22) REF. AAR N/R: 99853702 ORIGINATED BY EMPLOYEE V898275 REPAIRED RIB AT STA 101.90 AT #1 VERTICAL STIFFNER AS PER B737- 800 SRM55-10-09 REAPIR 4 FIG 202 SHEET 1,DETAIL "A",RE-INSTALLED RIB AFTER WORK WAS ACCOMPLISHED REF. USED 51-40-02 DATA WAS TRANSCRIBED FROM PAPER DOCUMENT: AAR N/R: WORK ACCOMPLISHED BY MECHANIC ADD EMP:INSPECTION ACCOMPLISHED BY

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

R/H HORIZONTAL STABILIZER IN-SPAR RIB STA 101.90 CRACK LOCATED AT TRANSITION RADIUS OF VERTICAL STIFFENER #3 . (MKD 126-024) REF. AAR N/R: 99853705 ORIGINATED BY EMPLOYEE REPAIRED RIB AT STA 101.90 AT SIFFNER #3 AS PER B737-800 SRM 55- 10-09 FIG 202 DETAIL"B" REAPAIR 4,REINSTALLED RIB AFTER WORK WAS ACCOMPLISHED REF.USED SRM 51-40-02. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT: AAR N/R: 99853705 WORK ACCOMPLISHED BY MECHANIC : ADD INSPECTION ACCOMPLISHED BY Q.C INSPECTOR :

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,787 hrs · 23,403 cycles

R/H HORIZONTAL STABILIZER IN-SPAR RIB STA 101.90 CRACK LOCATED AT TRANSITION RADIUS OF VERTICAL STIFFENER #2. (MKD 126-023) REF. AAR N/R: 99853704 ORIGINATED BY EMPLOYEE V898275 REPAIRED RIB AT STA 101.90 AT #2 VERTICAL STIFFNER AS PER B737- 800 SRM 55-10-09 REPAIR 4,FIG 202 DETAIL"B",REINSTALLED RIB AFTE R WORK WAS ACCOMPLISHED REF.USED SRM 51-40-02. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT: AAR N/R: 99853704 WORK ACCOMPLISHED BY MECHANIC : ADD INSPECTION ACCOMPLISHED BY Q.C INSPECTOR :

Part: NONE — NONE (NONE) · airframe 61,938 hrs · 22,290 cycles

CAPTAIN INADVERTENTLY OPERATED THE O2 MASK PASSANGER SWITCH SEAT ROWS 8ABC,8DEF,10ABC,10DEF,11ABC 12ABC,22DEF,23DEF,24ABC,24DEF,25DEF,26ABC,26DEF,27ABC 28ABC,28DEF,29ABC,30ABC,31DEF,38ABC MUST BE PLACED ON MEL NOC DESK: 05 NAME: ALAN DATE: 09-NOV-18- TOMC APPROVED SEAT ROWS LISTED ON THE TOP, PLACED ON MEL REPLACED USED O2 GENERATOR IN PSUS REF AMM 35-22-11 ADD EMP:U307987,U126394,U222030 REF L/P 8239061 INSPECTED INSTALLATION OF O2 GENERATORS IN LISTED LOCATIONS

Part: FAN — FAILED (RECIRCULATION) · airframe 60,060 hrs · 21,540 cycles

CLIMBING FROM FL330 TO FL370 FWD ZONE TEMP INCREASED 10C. ACCOM PANIED BY FOUL CONTIN FROM LP 6535354: ODOR IN CABIN. TURNED OFF RECIRC FANS. ORDOR DISSIPATED EVALUATE ODOR AND DEBRIEF CREW. PERFORM ZONE TEMP BITES, FOUND LEFT RECIRCULATION FAN CIRCUIT BREAKER OUT, WOULD NOT RESET. FOUND LEFT RECIRCULATION FAN AT FAULT. REMOVED AND REPLACED THE RECIRCULATION FAN IAW AMM 21-25-02. OPS CHECKED GOOD.

Part: OVEN — ARCED (GALLEY) · airframe 59,766 hrs · 21,432 cycles

FLIGHT ATTENDANTS REPORT SMOKE SMELL IN FWD GALLEY WENT AWAY WHEN CAP TURNED OFF CABIN UNTIL OVRHD INSP PER AMM 05-51-26-800-801C1. FOUND SIGNS OF ARCHING BEHIND OVEN CONTROLLER AT OVEN POS 204. REMOVED AND REPLACED OVEN PER AMM 25-34-00-400-801C3. OPS CHKS GOOD. NO OTHER DISCREPANCIES NOTED IN FWD GALLEY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,694 hrs · 21,400 cycles

EMERGENCY LIGHT FOR SEAT ROWS 15, 20, AND 21 INOPERATIVE. REMOVED AND REPLACED THE CHARGER AND BATTERY PACK IAW AMM 33-51-06-960-806. LIGHTS OPS CHECKED NORMAL. ACFT OK TO CONTINUE.

Part: LENS — MISSING (EXIT SIGN) · airframe 57,593 hrs · 20,575 cycles

EMERGENCY EXIT SIGN AT DOOR 2R MISSING. INSTALLED EXIT LENS COVER AT 2R.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,580 hrs · 20,571 cycles

FIRST CLASS SEAT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, ALL LIGHTS OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,462 hrs · 20,524 cycles

TWO EMERGENCY OVERHEAD SIGNS FOUND INOPERATIVE AT THE R1 DOOR AND FIRST CLASS AREA. REPLACED THE LAMPS, RESET SYSTEM, OPS CHECKED NORMAL.

Part: TIRE — BLOWN (NR 2 MLG) · airframe 53,407 hrs · 18,960 cycles

ON TAKEOFF, ADVISED BLOWN TIRE ON TAKEOFF. OVERWEIGHT LANDING, 151.3 WEIGHT. SINK RATE 600 FPM, REF SPEED 149K. REPLACED NR 2 MLG TIRE & WHEEL ASSEMBLY IAW AMM 32-45-11. SEE LOG PAGE 8355523 FOR BURST INSPECTION WHEEL OFF B0086.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 51,022 hrs · 18,122 cycles

SEAT TRACK FLANGE CRACKED AT RBL 24.75, OTBD AFT SPLICE STRAP HOLE AD RELATED 2013-23-04 AMDT 39-17659. REPAIRED SEAT TRACK FLANGE ECRA 5320-0 2509 REV ORIGINAL.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 33,478 hrs · 11,929 cycles

UPON MOVING FLAP HANDLE FROM UP POSITION FLAP INDICATOR SHOWED SPLIT (ONE NEEDLE UP, OTHER DOWN) AND YAW DAMP KICKED OFF, FOLLOWED QRH BUT WERE ONLY ABLE TO GET LED, NO TRAILING EDGE FLAPS. APPROACH AND LANDING UNREMARKABLE. SPEED 167K, MAX BRAKE GW 135K. FOUND RT FLAP TRANSMITTER CONNECTOR AND RECEPTACLE CORRODED. REPLACED FLAP TRANSMITTER PER 27-58-01-400 AND TESTED PER MM 27-51-00-730. REF N/R 4318074 FOR RECEPTACLE REPLACEMENT. OPERATIONAL CHECK SATISFACTORY. ROTABLE PARTS CHANGE WAS INDICATED - TT 1384749, S/N OFF 03448 TRANSMITTER, FL OFF 29-2759-9-0001 3448, ON 29-2759-9-0001 3031.

Part: SIGN — BROKEN (CABIN) · airframe 31,747 hrs · 11,333 cycles

AFT LOUVERED CEILING PANEL EMERGENCY EXIT SIGN BROKEN. REPLACED AFT CEILING PANEL EMERGENCY EXIT SIGN IAW AMM 33-51-01. OPS CHECKED GOOD WORK PERFORMED BY SL755.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

CABIN STATION 400 RT FRAME CRACKED BETWEEN STR 8-9 RIGHT. REPAIRED PER ECRA 5310-04933.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

CABIN STATION 400 LEFT FRAME CRACKED BETWEEN STR 8-9 LEFT. REPAIRED PER ECRA 5310-04933.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

CABIN STATION 500A RIGHT FRAME CRACKED BETWEEN STR 8-9 RT. REPAIRED PER ECRA 5310-04933.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

CABIN STATION 500C RIGHT FRAME CRACKED BETWEEN STR 8-9 RT. REPAIRED PER ECRA 5310-04933.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

CABIN STATION 440 LT FRAME CRACKED BETWEEN STR 8 - 9 LEFT. REPAIRED PER ECRA 5310-04933.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

RIGHT SIDE TRANSITION RAIL HAS CORROSION FROM STA 727G TO 787. REMOVED AND REPLACED RT SIDE TRANSITION PANEL FROM STA 727G TO 787 REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

FLOOR INTERCOSTAL CRACKED AT BL-11 STA 344 TO 360. REMOVED AND REPLACED INTERCOSTAL BL-11 STA 344-360. REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

FLOOR INTERCOSTAL CRACKED BL 0 STA 344 TO 360. REMOVED AND REPLACED INTERCOSTAL BL 0 STA 344 TO 360 REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

FLOOR INTERCOSTAL CRACKED BL-31R STA 312 TO 328. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

FLOOR INTERCOSTAL CRACKED AT BL-46 STA 312 TO 328. REMOVED AND REPLACED FLOOR INTERCOSTAL AT BL-46L STA 312 TO 328 REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 31,506 hrs · 11,235 cycles

FLOOR INTERCOSTAL CRACKED BL 0 STA 277 TO 294. REMOVED AND REPLACED FLOOR INTERCOSTAL AT BL 0 STA 277 TO 294. REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,506 hrs · 11,235 cycles

FLOOR INTERCOSTAL CRACKED AT BL-46L STA 328 TO 344. REMOVED AND REPLACED FLOOR INTERCOSTAL AT BL- 46L STA 328 TO 344 REF SRM 51-40-02.

Part: LIFE RAFT — DISCHARGED (DOOR) · airframe 27,689 hrs · 9,930 cycles

FWD AND AFT LIFE RAFT ASSY'S INOP. BOTTLES HAVE ZERO PSI. PLACED RAFTS ON PLACARD A/C OVERWATER RESTRICTED.

Part: ELEMENT — INOPERATIVE (MLG W/W) · airframe 24,966 hrs · 9,029 cycles

THE WHEEL WELL FIRE WARNING LIGHT AND BELL ACTIVATED AFTER LANDING GEAR RETRACTED. THE LANDING GEAR WAS EXTENDED AND THE WARNING LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. T/S IAW FIM 26-18-00 FOUND M270 WW DETECTOR AT FAULT. THE DETECTOR WAS REPLACED IAW MM 26-18-02. ALSO REPLACED OVERHEAT DETECTION UNIT AS A PRECAUTIONARY MEASURE IAW MM REF 26-18-01. ALSO REPLACED NR 3 MLG BRAKE. PERFORMED WW OVERHEAT DETECTION SYSTEM OPERATIONAL TEST WITH NO FAULTS FOUND.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 23,888 hrs · 8,656 cycles

L1 CHORD CORRODED. REPAIRED IAW SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 23,888 hrs · 8,656 cycles

CORRODED BEAM AT STA 986.5. REPAIRED IAW ECRA 5321-01450.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 23,888 hrs · 8,656 cycles

R2 CHORD CORRODED. REPAIRED IAW SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,715 hrs · 6,381 cycles

FWD EMERGENCY LIGHTS TO COCKPIT INOPERATIVE. REPLACED FWD EMERGENCY LIGHT BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,384 hrs · 17,724 cycles

LAST SECTION OF AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED AND TESTED BATTERY PACK.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN FORWARD CARGO PIT. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 14,791 hrs · 5,255 cycles

INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN FORWARD CARGO BIN BETWEEN STA 500 AND 500A. THE CORRODED SECTION OF Z-CHANNEL WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53.

Part: WEB — CRACKED (FAIRING) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND A 5 INCH CRACK IN O/B WEB ON RIGHT W/W AFT SKI JUMP FAIRING. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: WEB — CRACKED (FAIRING) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND A CRACK IN O/B WEB OF LEFT W/W AFT SKI JUMP FAIRING. THE WEB WAS REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (FAIRING) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND A 5 INCH CRACK IN LOWER OUTBOARD AND LOWER I/B CHORDS ON RIGHT W/W AFT SKI JUMP FAIRING. THE CHORDS WERE REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (FAIRING) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND A 5 INCH CRACK IN LOWER I/B CHORD AND IN LOWER O/B CHORD ON LEFT W/W AFT SKI JUMP FAIRING. NEW CHORDS WERE INSTALLED IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN AFT CARGO AREA AT STA 727+4 TO 767. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND RIGHT INTERCOSTAL UNDER Z-CHANNEL IN FORWARD CARGO PIT CORRODED AT STA 500D AND 500E. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 143A7510.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND LEFT Z-CHANNEL IN AFT CARGO AREA CORRODED AT STA 727+4 TO 847. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND LEFT STANCHION SUPPORT ASSEMBLY IN FORWARD PIT AT AFT BULKHEAD CORRODED AT STA 500I. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND THE LEFT Z-CHANNEL IN FORWARD CARGO AREA CORRODED AT ZONE 110. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND INTERCOSTAL CORRODED UNDER Z-CHANNEL IN FORWARD CARGO AREA AT RIGHT SIDE, STA 500E-500F. THE INTERCOSTAL WAS REPLACED IAW DRAWING 143A7510 AND SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND A 2 INCH CRACK IN RIGHT INTERCOSTAL AT STA 500G-500H. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-20-01, 51-40-02, AND DRAWING 143A7510.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND PANEL 121HW LOWER SUPPORT FRAME CORRODED AT AFT BULKHEAD OF FORWARD CARGO AREA. THE SUPPORT FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND A 2 INCH CRACK IN AFT PIT FLOOR RAIL AT STA 727I, RBL 13-84. THE FLOOR RAIL WAS REPAIRED IAW SRM 53-00-53.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 14,785 hrs · 5,252 cycles

INSPECTION FOUND PANEL 121EW LOWER SUPPORT FRAME CORRODED AT AFT BULKHEAD OF FORWARD CARGO AREA. A NEW SUPPORT FRAME WAS INSTALLED IAW SRM 51-40-02 AND 51-10-02.