N26215

Part: COVER — DAMAGED (ZONE 800 SLIDE) · airframe 82,472 hrs · 30,614 cycles

ESCAPE SLIDE COVER DAMAGED AT DOOR R2. R & R NEW SLIDE COVER AT R2 DOOR REF CMM 25-66-01-400-803.

Part: FIRE LOOP — DAMAGED (ZONE 400) · airframe 81,316 hrs · 30,063 cycles

1 ENG OVERHEAT ILLUM AND EXTINGUISHED FOR APPROX 5-10 SECONDS ON INITIAL CLIMB TOMC LOCKS LOG PAGE AFTER DUAL AIR RETURN WHILE PERFORMING INSPECTION WHEN REMOVING LEFT CORE HARNESS DETECTOR CERAMIC SHIELDING CRACKED AND BROKE APART ALSO FOUND RIGHT SIDE GROUNDING WIRE BROKEN OFF. IPC REF 26-11-02-01B SHEET 15 AND 19 ITEMS 565 AND 555 REMOVED ENG 1 CORE FIRE DETECTION HARNESSES REFERENCE AMM TASK 26-11-02-000-802. INSTALLED ENG 1 CORE FIRE DETECTION HARNESS MW0326 (LOOP B OF THE ENGINE CORE FIRE DETECTION CIRCUIT) IN REFERENCE AMM TASK 26-11-02-400-802. PENDING OPS CHECK. INSTALLED ENG 1 CORE FIRE DETECTION HARNESS MW0325 (LOOP A OF THE ENGINE CORE FIRE DETECTION CIRCUIT) IN REFERENCE AMM TASK 26-11-02-400-802. ENGINE FIRE DETECTION OPERATIONAL TEST GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 81,024 hrs · 29,925 cycles

EMERGENCY BATTERY PACK M1694 DOES NOT CHARGE. (REF: AAR NR 1000034040) REMOVED AND INSTALLED NEW POWER SUPPLY BATTERY PACK M1694 IAW B737 AMM 33-51-06-960-805 OP TEST GOOD (WORK ACCOMPLISHED BY V937546 AND AAR QC A-11 V931821) SDR IS COMPLIED WITH. SDR #1555

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 81,024 hrs · 29,925 cycles

EMERGENCY BATTERY PACK M1672 DOES NOT CHARGE. (REF: AAR NR 1000034039) REMOVED AND INSTALLED NEW POWER SUPPLY BATTERY PACK M1672 IAW B737 AMM 33-51-06-960-805 OP TEST GOOD (WORK ACCOMPLISHED BY V937546 AND AAR QC A-14 V935540) REMOVED AND REPLACE POWER SUPPLY BATTERY PACK. SDR #1554 CREATED BY UAL REP

Part: SKIN — CRACKED (ZONE 600 AILERON) · airframe 81,024 hrs · 29,925 cycles

FLIGHT TEST REQUIRED TO CHECK AILERON MANUAL REVERSION (ASYMMETRICAL FLIGHT CONTROL FORCES) TEST FLIGHT REQUIRED FOR SKIN REPAIR ACCOMPLISHED AT RH WING FORWARD OF RH AILERON REF ECRA 5721-01160 AND AMM 27-11-00-750-801 REPAIRED PER ECRA 5725-01160. UPDATE ESFR COMPLETED. APPROVED PLACARD APPROVED FOR TEST FLIGHT REQUIRED.

Part: WIRE — DISCONNECTED (ZONE 200) · airframe 80,584 hrs · 29,723 cycles

ROW 31 THOURGH ROW 37 EMERGENCY ESCAPE PATH LIGHTING INOP FOUND A WIRE DISCONNECTED AT ROW 31 RECONNECTED THE WIRE IAW AMM 33-51-11 OPS CHECK GOOD. C/W ALL IDT REQUIREMENTS PER GMM 09-10-05

Part: SPACER — MISSING (ZONE 100) · airframe 80,584 hrs · 29,723 cycles

#2 POWER FEEDER WIRE STAR SPACERS NOT INSTALLED PROPERLY UNDER SADDLE CLAMPS. NO. 2 IDG POWER FEEDER ELECTRICAL WIRING INTERCONNECTION SYSTEM (EWIS) INSPECTION (EZAP) {B737-20-3-0107} - REPOSITIONED WIRE SPACER AND WIRE CLAMP.

Part: FUSE — BLOWN (ZONE 200) · airframe 79,688 hrs · 29,289 cycles

EMERGENCY EXIT PATH LIGHTS INOP ON LH UP TO OVERWING EXITS. REPLACED FUSES IN PWR SPY M1676 AND M1695 IAW AMM 33-51-06-960-804. OPS CHECK GOOD IAW AMM 33-51-06-710-003.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 79,688 hrs · 29,289 cycles

MAIN CABIN STA 400 STR 5R FASTENER HOLE IS ELONGATED COMMON TO THE 143A1010-6 STRINGER CLIP OUTBOARD SIDE OF THE STRINGER. SUPPORT TASK NSA EMX N/R 00152. REPAIRED STRINGER 5R AT STA. 400 IAW B737-800 SRM 53-00-03-2R-3 FLIGHT CYCLES AFTER THRESHOLD IS REACHED SEE NSA EMX N/R 00152 UAL INSPECTION U274434 09/13/2024. REPAIR 3 FIGURE 202, THE THRESHOLD FOR THE START OF THE AND HANGER N/R 5428358 FOR WORK ACCOMPLISHED, CIR C/W. DATA WAS SUPPLEMENTAL INSPECTION IS 50,000 FLIGHT CYCLES AFTER TRANSCRIBED FROM NSA EMX N/R 00152.

Part: FIRE DETECTOR — FAULTED (NR 1 ENGINE) · airframe 79,077 hrs · 29,025 cycles

INTERMTT ENG 1 OVRHT AT FL100..WENT AWAY ON ITS OWN ..RAN CHKLST NEVER REAPPEARED #1 ENG UPPER FAN FIRE DET ASSY (M1757), LOWER FAN FIRE DET ASSY (M1758), LEFT CORE DET ASSY (M1759) AND RIGHT CORE DET ASSY (M1760) PER AMM 26-11-01 DUE TO MULTIPLE SERVICE INTERRUPTIONS. THANKS. TECH SUPPORT UPDATE: THIS ITEM IS CHRONIC. SEVERAL GVI''S HAVE BEEN ACCOMPLISHED WITH NO FINDINGS AND CORE DET HARNESS WAS REPLACED, DUE TO HISTORY, PLEASE T/S PER FIM 26-10 TASK 805. IF NO DEFECTS ARE NOTED, PLEASE REPLACE THE REMOVED AND REPLACED E1 RIGHT CORE FIRE DETECTOR ASSY 26-11-01. REMOVED AND REPLACED E1 UPPER FAN FIRE DETECTOR ASSEMBLY.. REMOVED AND REPLACED E1 LOWER FAN FIRE DETECTOR ASSEMBLY. REF: REMOVED AND REPLACED E1 LEFT CORE FIRE DETECTOR REF MM 26-11-01. E1 ENGINE FIRE DETECTION OPS TEST TASK 26-11-00-710-801 IS PERFORMED ENGINE FIRE DETECTION OPS TEST PER OPS CK REQUIRED. OPS CK REQUIRED. REQUIRED BEFORE CLEARING LOG PAGE. AMM26-11-00-710-801, TEST PASSED NO FAULTS DETECTED AT THIS 1765867,

Part: WHEEL — VIBRATION (NLG) · airframe 78,274 hrs · 28,666 cycles

NOSE WHEEL VIBRATES AT TAKEOFF DURING TAXI TAKEOFF AND RETRACTION AIRCRFT REQUIRES REPOSITION TO CHANCE BOTH NLG PARTS TIRES 1 AND 2. ATTEMPTED LIFT CAUSED AIRCRAFT TO SHIFT ROTABLE PARTS CHANGE WAS INDICATED - TT # 1591606 SN OFF 0963 DRAMATICALY TO THE RIGHT. WHEEL, ASSY, NL OFF 29-3245-9-0002 0963 ON 29-3245-9-0002 1728 CHANGED NLG TIRE 1 AS PRECAUTION. INBOUND FLIGHT CREW REPORTED SEVERE VIBRATION COMING FROM NOSE LANDING GEAR, THAT STOPPED ONCE WHEELS WERE STOWED. CHANGED NLG TIRE 1 IN REFERENCE TO AMM 32-21-00.

Part: VALVE — LEAKING (ENG#1) · airframe 77,365 hrs · 28,216 cycles

ENG 1 OVHT PERFORMED ENGINE/APU CONTROL BITE NO FAULTS REF. AMM 26-10 TASK APPLIED PNEUMATICS FROM APU TO #1 ENG REF 801. AMM36-00-00-860-803,FOUND BAD LEAK AT HIGH STAGE VALVE SHAFT SEAL. BORROWED PART FROM SOUTHWEST AIRLINE TAG IN LOG BOOK ROTABLE PARTS CHANGE WAS INDICATED - TT # 1623300 SN OFF 6852 R/R HPV P/N 3214446-4 ,M&E 33-3612-4-0005. WORK PERFORMED IAW ACP POWER ASSURANCE CHECK REF AMM 71-00-00-700-813-F00 @ 65% N1, AMM TASK 36-11-06-000-801, 36 11-06-400-807 , PERFORMED INSTALL AND 75% N1. CHECKS OK. NO OVERHEAT INDICATION. TEST OPTION 2. NO LEAKS FOUND .PLACED A/C BACK INTO USUAL ADD EMP:U015521 CONDITION. VALVE, HIGH STA OFF 29-3611-9-0002 6852 ON 29-3611-9-0002 9607, OPS/ LEK CHK GOOD,PLACARD REMOVED. PARTS USED: 1534691,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1534691 SN OFF 9607 VALVE, HIGH STA OFF 29-3611-9-0002 9607 ON 29-3611-9-0002 3912

Part: DOOR — LEAKING (L1) · airframe 76,308 hrs · 27,725 cycles

RETURNED FOR VERY LOUD HISSING NOISE COMING FROM DOOR 1L PER CREW COMMENTS:LOUD HIISING NOISE FROM FWD LWR DOOR HINGE@ PERFORMED CABIN LEAK TEST REF AMM 05-51-91-790-801.FOUND FWD DOOR 1L.AIRCRAFT TO 30,000 FEET PRESSURIZED TO APPROX 8 PSI NO DOOR EXTERIOR LEAKING AND HISSING NOISE STILL PRESENT IN LOSS OF CABIN PRESSURE INTERIOR(SEE ATTACHED PHOTOS).LEAKING BEGAN @ APPROX .5 PSI AND CONTINUED TO APPROX 1.5. FOUND LOWER ACOUSTIC SEAL FWD AND AFT MISSING FASTENERS AND FWD LOWER FILLER SEAL NOT EVEN WITH STRUCTURE. REPLACED MISSING FATENERS AND RESEALED FILLER. NEED TO PRESSURIZE AIRPLANE FOR LEAK CHECK. PRESSURIZED AIRCRAFT, ACCOMPLISHED LEAK CHECK. NO LEAK NOTED.

Part: UNKNOWN — UNKNOWN (E&E) · airframe 75,871 hrs · 27,524 cycles

DURING MANUAL REVERSION CHECKS, WHEN SELECTING FLT CONT B TO ''STBY RUD'' WITH FLT CONT A ''OFF'' AIRCRAFT ROLLED RAPIDLY TO THE RIGHT, INDUCING ABOUT 6 UNITS RWD YOKE. UNABLE TO INPUT ENOUGH LEFT RUDDER TRIM TO COUNTER (STOPPED TRIMMING RUDDER AT 13 UNITS). AT LEAST A 6:1 FORCE RATIO ROLLING LEFT VS RIGHT. 3 UNITS LEFT AILERON REQUIRED TO MAINTAIN WINGS LEVEL. SUSPECT RUDDER HARD OVER. WHEN NORMAL HYDRAULIC POWER RESTORED AIRCRAFT SNAPPED BACK. 37-AMM-27-32-42. NORMAL OP CHECKS GOOD AND PERFORMED MANUAL REVE RSION CHECK WITH NO RUDDER MOVEMENT. CONDITIONAL INSPECTION FOR EXCESSIVE MANUEVERING ACCOMPLISHED ON AAR RFD NR 99967088 (WORK ACCOMPLISHED BY V931611 AND AAR QC V920285) ROTABLE PARTS CHANGE WAS INDICATED - TT # 1859839 SN OFF 0371 DURING TROUBLESHOOTING, WHEN SELECTING FLT CONT B TO STBY RUB WI PERFORMED CONTROL ROD ADJ CHECK FOR STANDBY RUDDER PCU IAW B737 PERFORMED CHECK OF AILERON SYSTEM, MEASUREMENTS ARE IN LIMITS, N TH FLT CONT A OFF, NOTICED A RAPID MOVEMENT OF THE RUDDER, APPRO AMM 27-21-00-820-810-002. ADJ CHECK PASSED. (WORK ACCOMPLISHED O DEFECTS FOUND IAW B737 AMM 27-11-00-820-805 AND AMM 27-11-00-8 XIMATELY 3 INCHES RUDDER TRAILING EDGE TO THE LEFT. DISCREPANCY BY V931611 AND AAR QC V923046) 20-803 (WORK ACCOMPLISHED BY V931611 AND AAR QC V923046) OCCURED 2 OUT OF 2 TRIES. REMOVED AND REPLACED SMYD NO. 2 IAW B7 ADD EMP:V931611 ADD EMP:V931611 ADD EMP:V931611 COMPUTER, STALL OFF 29-2732-9-0003 0371 ON 29-2732-9-0003 0520

Part: BATTERY PACK — FAILED (M1670) · airframe 75,869 hrs · 27,523 cycles

PASSENGER CABIN EMERGENCY LIGHTS, BATTERY PACK M1670 TEST NOT GO OD (REF AAR NR 99967010)

Part: BATTERY PACK — FAILED (M1673) · airframe 75,869 hrs · 27,523 cycles

PASSENGER CABIN EMERGENCY LIGHTS, BATTERY PACK M01673 TEST NOT GOOD (REF. AAR NR 99958634).

Part: FRAME — CRACKED (LH WINDOW) · airframe 75,869 hrs · 27,523 cycles

COMPLETE REQUIRED SFR FOR WINDOW REPAIR ON L/H WINDOW FRAME DUE TO CRACK LOCATED AT THE TOP UNDER MOD (REF: AAR NR 99959435) EA 5310-04554 REV B OP 007 REPAIR ACCOMPLISHED FOR CONFIG B REVIEWED AND APPROVED

Part: BATTERY PACK — FAILED (M1671) · airframe 75,869 hrs · 27,523 cycles

PASSENGER CABIN EMERGENCY LIGHTS, BATTERY PACK M1671 TEST NOT GOOD (REF. AAR NR 99967011).

Part: SKIN — CORRODED (AIR DUCT) · airframe 75,869 hrs · 27,523 cycles

CORROSION FOUND IN THE SKIN OF GROUND CONDITIONED AIR CONNECTION DUCT. REQUIRE EVALUATION (REF. AAR NR 99967000). ACCUMULATION OF 48,000 TOTAL AIRCRAFT FLIGHT CYCLES, PLANNING TO ELAGE SKIN AND KEEL BEAM DOUBLER REPAIR BETWEEN STA 500H AND STA PART 2 OF THE LATEST REVISION OF ECRA 5331-03018. CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR THE FUS 540, STR 26L AND STR 26R ON AIRCRAFT N26215 IN ACCORDANCE WITH ACCOMPLISHED REPAIR AT FUSELAGE LOWER SKIN AT THE AIR CONDITIONI NG GROUND CONNECTOR AREA, PER ECRA 5331-03018. ON OR BEFORE THE TOMC APPROVED DIP TO ON OR BEFORE THE ACCUMULATION OF 48,000 TOMC-APPROVAL FROM SC1ELBYC COMMENT TOTAL AIRCRAFT FLIGHT CYCLES, PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR THE FUSELAGE SKIN AND KEEL BEAM DOUBLER REPAIR BETWEEN STA 500H AND STA 540, STR 26L AND STR 26R ON AIRCRAFT N26215 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5331-03018. REVIEWED AND APPROVED QC QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: BATTERY PACK — FAILED (M1672) · airframe 75,869 hrs · 27,523 cycles

PASSENGER CABIN EMERGENCY LIGHTS, BATTERY PACK M01672 TEST NOT GOOD (REF. AAR NR 99958636).

Part: SKIN — CRACKED (LH WING) · airframe 75,869 hrs · 27,523 cycles

FOUND CRACK ON L/H WING LOWER SKIN BETWEEN RIB 19 AND 20, STR 9. INSPECTION PERFORMED PER STEP 1 ITEM B. (REF:AAR NR 99959471) (MAJOR REPAIR - SDR REPORTABLE) THIS WORK IS COMPLETED IAW EA 230047 REV. IR AND EC/RA 5725-0112 0 ESFR NO. 1031757 (WORK ACCOMPLISHED BY V916729 AND AAR QC A-72 V931821). ADD EMP:V916729

Part: DOOR — DENTED (AFT CARGO DOOR) · airframe 75,869 hrs · 27,523 cycles

DENT AT AFT CARGO DOOR AFT OF CUTOUT APPROX 27 INCHES ABOVE FROM BOTTOM OF CUTOUT REQUIRE PERMANENT REPAIR LOG 8072013 (REF AAR NR 99959146) DIP APPLIED, REINSPECT INITIAL AT 50,000 CYCLES AND REPETITIVE INSPECTION AT 3,500 CYCLES PER SRM 53-00-01-2R-24 FIGURE 204. REPAIRED AFT CARGO DOOR AFT OF CUTOUT APPROX 27 INCHES ABOVE FROM BOTTOM OF CUTOUT. IAW SRM B737-800 53-00-01-2R-24. PERFORM REQUIRE INSPECTION PER B737 SRM 53-00-01-2R-24 STEP 5 ITEM A(B) (WORK ACCOMPLISHED BY V936445 AND AAR QC V918045) ADD EMP:V936445

Part: UNKNOWN — CORRODED (STA 887) · airframe 75,869 hrs · 27,523 cycles

POSSIBLE CORROSION ON AFT CARGO STA 887 STRG 27L (REF AAR NR 99958861) REPAIRED STGR 27LH STA 887 IAW B737-800 SRM 51-10-02-0G-0, SRM 53-00-03-1A-1, SRM 51-40-0G-0, SRM 53-00-03-2R-1, AMM 51-21-00-100-801 (WORK ACCOMPLSIHED BY V9396011 AND AAR QC V918045)

Part: SKIN — CRACKED (L WING LWR SKIN) · airframe 75,869 hrs · 27,523 cycles

FOUND CRACK ON L/H WING LOWER SKIN BETWEEN RIB 19 AND 20, STR 9. INSPECTION PERFORMED PER STEP 1 ITEM B. (REF:AAR NR 99959471) (MAJOR REPAIR - SDR REPORTABLE)

Part: STRINGER — CORRODED (STA887/S27L) · airframe 75,869 hrs · 27,523 cycles

POSSIBLE CORROSION ON AFT CARGO STA 887 STRG 27L (REF AAR NR 99958861)

Part: SKIN — CRACKED (STA 129.50) · airframe 75,869 hrs · 27,523 cycles

VALIDATED CRACK INDICATION ON RH LOWER SKIN HORIZONTAL STAB AT STA 129.50 S/M ADVISE ON REPAIR (REF AAR NR 99959398)

Part: SKIN — UNKNOWN (AFT CARGO DOOR) · airframe 75,869 hrs · 27,523 cycles

AFTER INSPECTION ON AFT CARGO REPAIR DOUBLER PER EA 5100-02345 REV. E OP 16 FOUND DAMAGE ON DOUBLER (REF: AAR NR 99959126) REMOVED & REPLACED AFT CARGO DOOR SKIN IAW B737-800 SRM 51-40-02 -0G-0 STEP 4. AND STEP 7.,SRM 52-30-01-01-1, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, B737-800 AMM 51-21-72-370- 804 (WORK ACCOMPLISHED BY V936445 & AAR QC A-76 V920285)

Part: UNKNOWN — DAMAGED (STA 395.5) · airframe 75,869 hrs · 27,523 cycles

REF LOGPAGE 6161264 FOUND AREA TO BE REWORKED AS LIGHTNING DAMAGE NOT AS A DENT AS ORIGINAL DESCRIPTION ON BS 395 STRINGER 20 L/H (REF. AAR NR 99958964). OF EC/RA 5331-03008 (WORK ACCOMPLISHED BY V916729 AND AAR QC V938209) THIS WORK IS COMPLETED PER EA 230024 REVISION IR AND EC/RA 5331-03008., ON OR BEFORE MARCH 3, 2025 PERFORM AN INSPECTION OF THE EXTERNAL DOUBLER/TRIPLER REPAIR AT STA 395.5, STR 20L ON AIRCRAFT N26215 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION ADD EMP:V916729

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 75,869 hrs · 27,523 cycles

AFTER INSPECTION ON AFT CARGO REPAIR DOUBLER PER EA 5100-02345 REV. E OP 16 FOUND DAMAGE ON DOUBLER (REF: AAR NR 99959126) REMOVED & REPLACED AFT CARGO DOOR SKIN IAW B737-800 SRM 51-40-02 -0G-0 STEP 4. AND STEP 7.,SRM 52-30-01-01-1, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, B737-800 AMM 51-21-72-370- 804 (WORK ACCOMPLISHED BY V936445 & AAR QC A-76 V920285)

Part: SKIN — DENTED (AFT CARGO DR) · airframe 75,869 hrs · 27,523 cycles

DENT AT AFT CARGO DOOR AFT OF CUTOUT APPROX 27 INCHES ABOVE FROM BOTTOM OF CUTOUT REQUIRE PERMANENT REPAIR LOG 8072013 (REF AAR NR 99959146)

Part: BEAM — CORRODED (STA 344) · airframe 75,869 hrs · 27,523 cycles

FLOOR STRUCTURE TRANSVERSE BEAM WITH CORROSION ON STA. 344 LBL 56 AND LBL 11 (REF. AAR NR 99959059). PERFORMED REPAIR AT FLOOR STRUCTURE TRANVERSE BEAM ON STA 344 LBL 56 & LBL 11 IAW B737-800 SRM 53-10-51-2R-10 REPAIR 10. (WORK ACCOMPLISHED BY V938333 AND AAR QC A-54 V918832)

Part: DOOR SILL — CORRODED (DOOR 1L) · airframe 75,869 hrs · 27,523 cycles

DOOR SURROUND STRUCTURE SILL ANGEL WITH CORROSION ON L1 (REF. AAR NR 99959066). REMOVED AND PLACED CHORD NEW ON DOOR SURROUND STRUCTURE SILL ANGLE ON L1 IAW B737-800 DWG 1A1A8110, SRM 51-40-02-0G-0 (WORK ACCO MPLISHED BY V940184 AND AAR QC V938209)

Part: FLOORBEAM — CORRODED (RBL 28-38) · airframe 75,869 hrs · 27,523 cycles

AFT PASSENGER COMPARTMENT WET AREA, FLOOR BEAM 986.5 WITH CORROSION BTW RBL 28 TO RBL 38 (REF. AAR NR 99959070). REPAIRED FLOOR BEAM STA 986.5 IAW B737-800 SRM 53-70-51-2R-4 REP AIR 4 ALTERNATIVE 1 (WORK ACCOMPLISHED BY V940286 AND AAR QC V91 8045)

Part: SKIN — NONE (LH STR20/ BS395) · airframe 75,869 hrs · 27,523 cycles

REF LOGPAGE 6161264 FOUND AREA TO BE REWORKED AS LIGHTNING DAMAGE NOT AS A DENT AS ORIGINAL DESCRIPTION ON BS 395 STRINGER 20 L/H (REF. AAR NR 99958964).

Part: DOOR SILL — CORRODED (DOOR 1L) · airframe 75,869 hrs · 27,523 cycles

DOOR SURROUND STRUCTURE SILL ANGEL WITH CORROSION ON L1 (REF. AAR NR 99959066).

Part: BEAM — CORRODED (RBL 28) · airframe 75,869 hrs · 27,523 cycles

AFT PASSENGER COMPARTMENT WET AREA, FLOOR BEAM 986.5 WITH CORROSION BTW RBL 28 TO RBL 38 (REF. AAR NR 99959070).

Part: SCREW — MISSING (INBOARD FLAP) · airframe 72,649 hrs · 26,206 cycles

PDA 3 SEVEN SCREWS MISSING FROM INDOARD FLAP, OUTBOARD TRACK TAILCONE FAIRING. % FROM LEFT WING, 2 FROM RIGHT WING SHOULD SAY 5 FROM LEFT WING FAIRING. SEE LP 7778796 AND 7778803 FOR DISPOSITION

Part: SCREW — LOOSE (FUEL VENT PANEL) · airframe 72,298 hrs · 26,068 cycles

FUEL LEAK LEFT WING SUSPECTED AFTER AIRCRAFT BEHIND US REPORTED FUEL LEAKING ON TAKEOFF FOUND SOME LOOSE SCREWS ON FUEL VENT PANEL. TIGHTENED SCREWS REF AMM 28-11-11. NO LEAK NOTED.

Part: SHROUD — DELAMINATED (NR 2 ENGINE) · airframe 71,425 hrs · 25,700 cycles

ON-WING- FAN BLADE ULTRASONIC INSPECTION AND BROACHED DISK LUBRICATION - #2ENG ABRAIDABLE SHROULD HAS MISSING MATERIAL WITH DELAMINATION AT 6 OCLOCK POSITION. DAMAGE AND REPAIR FOR 50 FLIGHT CYCLES OR 125 HOURS STEP (F)2. REF AMM 72-24-02-200-801-F00 AND FOUND TO BE WITHIN ALLOWABLE IN REFERENCE WITH AMM 72-24-02 A REPAIR IS REQUIRE PRIOR TO 50 CYCLES OR 125 HOURS.DIP LIMIT Y MISSING MATERIAL AT 6 O''CLOOCK 2 AREAS .5X.3 AND .25X.25 FAN CASE PARENT METAL SHOWS THROUGH.INSPECTED AND FOUND TO BE WITHIN LIMITS TO CONTINUE-IN-SERVICE FOR 50 FLIGHT CYCLES OR 125 DIP LIMIT Y HOURS REF AMM 72-24-02-200-801-F00 STEP (F) 2 QC QC REVIEWED RECORDS UPDATE - AP T/A : 50FC/125 FH..........AP/U366012

Part: BOLT — MISSING (RH INBRD FWD FLA) · airframe 70,622 hrs · 25,372 cycles

PDA 2 RIGHT WING INBOARD FLAP FWD CANOE FAIRING MISSING 2 EACH ATTACH BOLTS PICTURE UPDATE REF L/P 6268454 REPLACED MISSING BOLTS AS REQUIRED. OK TO CONTINUE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. SPT- 7002946 REMOVED & REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW EC/RA 5714-01148 REV ORIGINAL & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION COMPLETED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. SPT- 7002942 REMOVED & REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW EC/RA 5714-01144 REV ORIGINAL & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SPT- 7002947 REMOVED & REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW EC/RA 5714-01149 REV ORIGINAL & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 RBLO 15.04 IS CRACKED. SPT- 7002945 REMOVED & REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW EC/RA 5714-01147 REV ORIGINAL & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. SPT- 7002944 REMOVED & REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW EC/RA 5 714-01146 REV ORIGINAL & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. SPT- 7002939 REMOVED & REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW EC/RA 5 714-01141 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-800 AM M 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. SPT- 7002940 REMOVED & REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW EC/RA 5714-01142 REV ORIGINAL & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. SPT- 7002941 REMOVED & REPLACED SHEAR FITTING AND TUBE BRACKET IAW EC/RA 5714 -01143 REV ORIG AT STA 540 LBL 32.40 & APPLIED VAPOR BARRIER IAW B737-800 AMM 28-11-00. SSFR REPORT, FORM 46-0024, ENTERED BY UA L INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,516 hrs · 24,947 cycles

SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. SPT - 7002943 REMOVED & REPLACED SHEAR FITTING AT STA 540 LBL 54.60 IAW EC/RA 5714-01145 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-800 A MM 28-11-00. SSFR REPORT, 46-0024, ENTERED BY UAL INSPECTION 4/1/2020 INSPECTION ACCEPTED

Part: SKIN — DENTED (BS 450) · airframe 69,340 hrs · 24,878 cycles

FWD CARGO COMPARTMENT DOOR CUTOUT APROX STA 450 UPPER FWD EDGE HAS DENT REF AAR N/R 99873551 DENT FOUND OUT OFLIMITS PER B737 SRM 53-00-01 AD5 NO DAMAGE PERMITTED AT THE EDGE OF DOOR CUTOUT. ACCOMPLISHED REPAIR AT FWD UPPER CORNER APPROX STA 450 PER B737 SRM 53-00-01 REPAIR 21 FIG 202 THIS A CAT B REPAIR THAT NEEDS INSPECTION PER PARA 5 WITH A THRESHOLD OF 50,000 FC AFTER INSTALLATION OF REPAIR

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 69,340 hrs · 24,878 cycles

REF ELB LP 4484477 FWD CARGO DOOR HAS AN OUT OF LIMITS DENT 10IN ABOVE DOOR HANDLE AND 3IN AFT OF DOOR HANDLE CENTER LINE REF AAR N/R 99873705 ACCOMPLISHED PERMINENT REPAIR AT FWD CARGO DOOR PER REF B737 SRM 52-00-00 REP 2 FIG 201 CAT A REPAIR

Part: ACTUATOR — CRACKED (NR 1 SPOILER) · airframe 65,113 hrs · 23,224 cycles

UPON LANDING IN DEN, HYDRAULIC PRESSURE INDICATION ZERO SYSTEM A LOST SYSTEM A. FOUND NUMBER 1 SPOILER CASTING CRACKED. REMOVED ACTUATOR. PROVIDED CLEARANCE TO INSTALL NR 1 SPOILER ACTUATOR. VERIFIED PART NUMBER ALSO. CLEARED AREA TO INSTALL NR 1 SPOILER ACT. REPLACED NR 1 FLIGHT SPOILER. ALSO INSPECTED #1 ENG AND A SYS ELECTRIC PUMP CASE DRAIN FILTER. NO DEBRIS FOUND.

Part: INTERLOCK VALVE — FAULTY (GROUND SPOILERS) · airframe 61,899 hrs · 21,950 cycles

LANDING GEAR LEVER DOES NOT MOVE TO THE UP POSITION IN FLIGHT, IS FREE TO MOVE TO THE UP POSITION WHEN THE LOCK OVERRIDE IS USED. EMERGENCY DECLARED. PSEU BITE CHECK INDICATED GROUND SPOILER INTERLOCK VALVE FAILURE. INSTALLED GROUND SPOILER INTERLOCK IAW 27-62-61-400-801. OPS CHECKED GOOD. JACKED ACFT IAW AMM 07-11-01-580-815, AND PERFORMED THE LANDING GEAR CONTROL SYSTEM TEST IAW AMM 32-31-00-730-802. PERFORMED GEAR SWING. LANDING GEAR LEVER OPS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 60,838 hrs · 21,551 cycles

AFT EMERGENCY EXIT SEAT LIGHT AT 15C BROKEN. REPLACED BOTH LIGHT BULBS AND LENS. EMERGENCY EXIT LIGHTS AT 15C OPS CHECK NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 60,838 hrs · 21,551 cycles

EMERGENCY EXIT SEAT LIGHT AT 29C BROKEN. REPLACED SEAT EXIT LIGHT LENS, OPS NORMAL.

Part: BEAM — CRACKED (R1 DOOR) · airframe 60,126 hrs · 21,256 cycles

R1 DOOR LOWER TORQUE BOX BEAM IS CRACKED REF ECRA 5210-02788. VERIFIED WITH EDDY CURRENT. REMOVED AND INSTALLED NEW LOWER TORQUE BOX BEAM PER BAC DRAWING 141A6516 AND ECRA 5210-02788.

Part: BEAM — CORRUPTED (R1 DOOR) · airframe 60,126 hrs · 21,256 cycles

R1 DOOR UPPER TORQUE BOX BEAM IS CRACKED REF ECRA 5210-02788, VERIFIED WITH EDDY CURRENT. REMOVED AND REPLACED NEW LOWER TORQUE BOX BEAM PER BAC DRAWING 1 41A6516 AND ECRA 5210-02788.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 60,126 hrs · 21,256 cycles

FOUND 0.5" CRACK IN LEFT WHEEL WELL CENTER WING REAR SPAR VERTICAL PRESSURE WEB AT STA 663, 2"O/B OF LBL 31.83, 4" BELOW WL 200.6 (MARKED). CUT OUT DAMAGE AND INSTALLED REPAIR REF SRM 57-10-10 REPAIR 3 ALTERNATIVE 01, INSPECTION REQUIRED AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND 36,000 FLIGHT CYCLES THEREAFTER REF TABLE 203 PARA 6 OF SRM 57-10-10 REPAIR 3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,126 hrs · 21,256 cycles

PAX CABIN FWD ENTRY STRUCTURE, STRINGER 4L IS DAMAGED AND HAS 1.5" CRACK AT BS 303.9. INSTALLED NEW STRINGER WEB P/N 141A8130U38 AND FABRICATED GUSSET STRAP FROM 7075-T6 .063" REF BAC DWG 141A8130 ITEM 9, INSTALLED REF SRM 51-40-02.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,230 hrs · 20,885 cycles

R1 OVERWING EMERGENCY EXIT LIGHT DOES NOT ILUMINATE. REPLACED THE FUSE. OPS NORMAL.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAP) · airframe 57,334 hrs · 20,190 cycles

FLAPS WOULD ONLY EXTEND TO THE FLAPS 2 POSITION IN NORMAL. HAD TO USE ALTERNATE FLAPS TO EXTEND THE FLAPS TO 30. FLAPS WHERE SYMMETRIC. TROUBLE SHOT IAW FIM 27-51-00. R & R RT FLAP TRANSMITTER IAW AMM TASK 27-58-01. OPERATIONAL TESTS PASSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,817 hrs · 19,995 cycles

FORWARD LEFT DOORWAY LINING, EMER EXIT SIGN WILL NOT ILLUMINATE. R & R M1675 BATTERY PACK PN D717-01-100, SN 9 6096 WITH SERVICEABLE M1675 BATTERY PACK PN D717-01-100, SN 146848 IAW AMM 33-51-06. SYS OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 56,114 hrs · 19,732 cycles

ON APPROACH, FLAPS WERE EXTENDED TO 1. WE HAD A FLAP ASYMMETRY PRIOR TO FLAP 1, INDICATED NO ROLL. TRIED TO EXTEND FLAPS WITH ALTERNATE SYS, FLAPS INDICATED 5 ONLY. FWD PANEL HAD LE FLAPS TRANSIT. UNABLE TO DUPLICATE RAN TASKS 27-51-00-740-801, 27-51-00-810-803 & 27-51-00-810-802, NO FAULTS FOUND.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 53,529 hrs · 18,817 cycles

ON APPROACH AT SELECTION OF FLAP 1, YAW DAMP KICKED OFF. IT RESET & AT FLAPS 5 SELECTION WE SAW FLAPS WERE STUCK AT LT 1. RAN CHECKLIST & LANDED FLAPS UP. TOUCHDOWN SPEED 189 KTS. NO FLAP OR GEAR WERE OVER SPEED. PERFORMED FIM TASK 32-61-00-810-815 FOR PSEU FAULTS 32-62009 & 32-62010. GND CHECKS GOOD, ACFT OK TO CONTINUE. FAULT DATA, FAULT CODE 1. 32-62009 & FAULT CODE 2. 32-62010. FAULT COMMENTS LANDING FLAP A & B FAULT.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,113 hrs · 17,981 cycles

L2 DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED LENS ASSEMBLY, ALL TEST PASSED AMM 33-51-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

RT WING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,144 hrs · 17,238 cycles

SUPPORT TASK EMERGENCY LIGHT INOPERATIVE AT RT WING AFT LIGHT WHILE TROUBLE SHOOTING FOUND EMERGENCY EXIT LIGHT BATTERY PACK AFT TO BE INOPERATIVE. REMOVED & REPLACED BATTERY PACK IAW BOEING 7 37-700/800/900 AMM TASK 33-51-06-960-805. OPERATION CHECKED GOOD IAW BOEING 737-700/800/900 AMM TASK 33-51-06-960-805

Part: CHARGER — FAILED (E&E BAY) · airframe 43,908 hrs · 15,394 cycles

ELEC LIGHT ON OVERHEAD FOUND BATTERY CHARGER C/B E-1 ON P-92 TRIPPED IN MAIN ELECT COMP WITH ELECTRICAL ODOR DISSIPATING THROUGH AIRCRAFT COCKPIT OVERHEAD PANEL ELECT BITE TEST SHOWS BATTERY CHARGER INOP R&R BATTERY CHARGER AND MAIN AIRCRAFT BATTERY. BATTERY AND CHARGER TESTS GOOD. ELECT PANEL BITE TEST GOOD. CONTINUED ON 8652593 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1484824 SN OFF 00578 TT # 1383696 SN OFF 00296 BATTERY, AIRCRAFT OFF 29-2431-9-9001 0578 ON 29-2431-9-9001 6811 CHARGER, BATTERY OFF 29-2431-9-0002 0296 ON 29-2431-9-0002 2679.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,601 hrs · 15,282 cycles

SUPPORT TASK - BRACKET AT FRAME 440R BEETWEN STRINGER 8 AND 9. REPAIRED PER ECRA5310-05428. SEE BACK OF NR FOR PARTIAL WORK ACCOMPLISHED.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 43,601 hrs · 15,282 cycles

SUPPORT TASK BRACKET AT FRAME 400R STR 8 AND 9 CRACKED. REPAIRED PER ECRA5310-05428, PARTIAL WORK ACCOMPLISHED BACK OF NR.

Part: PCU — FAULTY (AILERON) · airframe 36,926 hrs · 12,891 cycles

AILERON CONTROL WHEEL SLOW TO RESPOND WHEN TURNED TO THE RIGHT. REMOVED AND INSTALLED B SYS PCU PER AMM 27-11-71-400-801, ROTABLE PARTS CHANGE WAS INDICATED - TT 1371744, S/N OFF 00346 UNIT, POWER CON OFF 29-2711-9-0004 0346 ON 29-2711-9-0004 1188.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,910 hrs · 12,880 cycles

FUSELAGE SKIN DAMAGED ON BOTTOM EDGE OF AFT CARGO DOOR CUTOUT LOCATED UNDER THE OUTBOARD SILL PLATE. REPAIRED AFT CARGO DOOR CUTOUT LOWER FUSELAGE SKIN PER ECRA 5331-01471, REINSPECT PER PART 2 EC5331-01471AT INTERVALS NOT TO EXCEED 500 FLT CYCLES PERMANENT REPAIR PER PART 3 EC5331-01471 AFTER 15870 CYCLES BUT BEFORE 15880 TOTAL A/C FLT CYCLES REF DIP 001347.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,312 hrs · 12,323 cycles

CABIN FLOOR PANEL 241UF DELAMINATED. FABRICATED PAX CABIN FLOOR PANEL 241UF REF EC/RA 5320-01448.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,082 hrs · 11,890 cycles

L-1 DOOR BATTERY PACK FAILED TEST. REMOVED AND REPLACED L-1 DOOR BATTERY PACK PER AMM 33-51-06, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,627 hrs · 9,380 cycles

L2 DOOR EMERGENCY EXIT SIGN FAILED TO ILLUMINATE UPON TEST. REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 AND WDM 33-51-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,090 hrs · 7,800 cycles

INSPECTION FOUND THE EXTERIOR FUSELAGE SKIN CORRODED ADJACENT TO THE DRAIN AT STA 727E, BL 0. THE CORRODED AREA WAS TRIMMED OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-03444.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,493 hrs · 7,949 cycles

INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN INTERCOSTAL BETWEEN STA 270-294, RBL 2. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 511-20-01 AND 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,493 hrs · 7,949 cycles

INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN INTERCOSTAL BETWEEN STA 312 AND 328, RBL 30. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,493 hrs · 7,949 cycles

INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BETWEEN STA 328 AND 344 NEAR L-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,493 hrs · 7,949 cycles

INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BETWEEN STA 312 AND 320, LBL 64, NEAR L-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-20-01 AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,493 hrs · 7,949 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 360-380, LBL 22. A REPAIR WAS INSTALLED IAW ECRA 5321-01253.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,493 hrs · 7,949 cycles

INSPECTION FOUND AFT GALLEY FLOOR SUPPORT AFT OF RT GALLEY MOUNT CORRODED AT STA 986.5 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 3147A5710.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,090 hrs · 7,800 cycles

INSPECTION FOUND CORROSION ON SKIN AROUND CENTER DRAIN PLUG BETWEEN STA 727E AND 727F. REPAIRED IAW ECRA 5330-03444 AND PLACED ON DIP TO PERFORM PERMANENT REPAIR PER PART 3 WITHIN 12 MONTHS.

Part: SKIN — DENTED (AFT CARGO DR) · airframe 14,959 hrs · 5,088 cycles

INSPECTION FOUND THE AFT CARGO DOOR OUTER SKIN DENTED FORWARD OF THE DOOR HANDLE AT STA 808. THE CUTOUT WAS 3.35" X 7.5" AFTER THE DENTED AREA WAS REMOVED. THE AREA WAS REPAIRED IAW ECRA 5210-01629.

Part: SKIN — DENTED (STA 460-480) · airframe 14,959 hrs · 5,088 cycles

INSPECTION FOUND A DENT AND GOUGE IN THE FUSELAGE SKIN BELOW THE FORWARD CARGO DOOR CUTOUT BETWEEN STA 460 AND 480 FROM S26R TO S27R. THE SKIN WAS REPAIRED IAW ECRA 5330-03204.

Part: LIFE RAFT — DISCHARGED (OVERHEAD) · airframe 7,816 hrs · 2,570 cycles

INSPECTION FOUND AFT OVERHEAD RAFT PRESSURE LOW. THE AFT OVERHEAD RAFT WAS REMOVED AND REPLACED IAW MM 25-64-00.