N23707

Part: PANEL — NOT SEATED (ZONE 800) · airframe 82,172 hrs · 30,247 cycles

MID CABIN EMERGENCY EXIT DOOR, LOWER PANEL NOT FLUSH. OPENED EMERGENCY EXIT DOOR IAW AMM 52-22-00-580-801. RESEATED PANEL AND CLOSED EMERGENCY EXIT DOOR IAW AMM 52-22-00-580-803, PANEL FLUSH. ACFT OK FOR SERVICE.

Part: FLAG — FALSE ACTIVATION (PFD) · airframe 82,106 hrs · 30,206 cycles

FO PFD DISPLAYING SPD AND ALT FLAGS TESTED RIGHT ADR SYSTEM REF. TO 34-21-00, TESTED GOOD.

Part: SLIDE — MISINSTALLED (ZONE 800) · airframe 81,646 hrs · 29,978 cycles

EXCESS SLIDE MATERIAL HANGING DOWN FROM DOOR 1R. REPACKED SLIDE IAW AMM TASK 25-66-01-000-801 & 25-66-01-400-804. OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 81,044 hrs · 29,690 cycles

ROW 2 AB AISLE PATH EMERGENCY LIGHTING INOP. R&R'ED EMERGENCY PATH SEAT LIGHT ASSY. @ SEATS 2 A/B IAW AMM 33-51-11. NOT IDT REQUIRED

Part: PLATE — WORN (ZONE 200) · airframe 80,688 hrs · 29,528 cycles

O /B STRIKER PLATE FOR H/P PNEUMATIC DOOR 192 DR WORN THROUGH AND COMMING OFF. CHORD IS WORN INTO SLIGHTLY BY O/B LATCH AS WELL.REMOVED ECS SEAL RETAINER AND WORN/LOOSE STRIKER PLATE. LOCATION IS INCORRECT RESULTING IN OUTBOARD LATCH FOR DOOR 192 DR WEARING INTO ATTATCH FWD RIVIT AND DAMAGING CHORD BEYOND LIMITS.WILL NEED TO DO CHORD REPAIR SRM 57-10-13-2R-3. CREATED SFR 12:30 2/19/25 PICTURE ADDED COMPLIED WITH STEPS A THROUGH D REF SRM 57-10-13-2R-2 REPAIR 3. COMPLIED WITH STEP E REF SRM 57-10-13-2R-2 REPAIR 3. .... ****. HFEC INSPECTION IS REQUIRED**** ADD EMP:U125272 IDENTIFIED REPAIR MATERIALS FOR STRAP 7075-T6 0.0125" AND FILLER 7075-T6 0.125", BOTH MATERIALS' P.O. NUMBERS ARE 6374129 PER SRM 57-10-13-2R-3 REPAIR 3. MATERIAL VERIFICATION IS REQUIRED. UPDATED FOR RII REQUIREMENT UPDATED FOR RII REQUIREMENT. AS PER MAJOR REPAIR REQ 737. SRM. 57-10-13-2R-3. REPAIR 3 , PERFD. HFEC OF. PNUE DOOR 192 STRIKER AREA / REPAIR AREA. AS PER. 737 NDT. PART 6, 51-00-00 PROCEDURE 23 . NO DEFECTS NOTED. UPDATED FOR RII REQUIREMENT. PERFD RII MATERIAL VERIFICATION AS PER 737 SRM 57-10-13-2R-3. REPAIR 3 , MATERIAL TYPE , THICKNESS AND PO # ALL VERIFIED . OK TO FAB REPAIR PART FROM STOCK AT THIS TIME. PERFORMED FLAP PEENING ON THE REPAIR AREA PER SOPM 20-10-03 PARA 4 STEP H. THE PRIOR UPDATE REF IS SRM 57-10-13-2R-3 REPAIR 3. STARTED TO FABRICATE REPAIR PARTS PER SRM 5REPAIRED DAMAGE TO CHORD REF SRM 57-10-13-2R-3 REPAIR 3. FILLED OUT SFR AND SDR AS REQUIRED WITH REPAIR INFORMATION.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 80,688 hrs · 29,528 cycles

EMERGENCY LIGHTS POWER SUPPLY M1674 FAILS CAPACITY CHECK. REFERENCE AMM 33-51-06-200-801 FOR DISPOSITION. BATTERY PACKS WERE DEEP CYCLED PRIOR TO CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER M.M. 33-51-06-200-801, 33-51-06-960-805 FOR THE M1674 POWER SUPPLY.OP CHECKS GOOD.

Part: SIGN — LOOSE (ZONE 200) · airframe 80,688 hrs · 29,528 cycles

EMERGENCY LIGHTS CEILING MOUNTED EXIT LOCATOR LIGHT ASSY AT ROW 21 IS LOOSE AND APPEARS TO HAVE SEVERL INOP BULBS DURING OPERATIONAL CHECK. SECURED EMERGENCY LIGHT CEILING MOUNTED EXIT LOCATOR LIGHT ASSY AT ROW 21 REF SRM 51-40-02 AND RELAMPED SEVERAL INOP BULBS REF AMM 33-51-01

Part: PANEL — INFLT SEPARATION (ZONE 100) · airframe 79,452 hrs · 28,929 cycles

PDA 1 PANEL 194BR RIGHT SIDE AFT OF W/W DEPARTED AIRCRAFT. ARRIVED FROM EWR. REF LOG 9015927 PANEL IS 194CR; PART NUMBER 149A7552-2 INSTALLED AFT WING TO BODY FAIRING PANEL 194CR IAW 53-51-21 PARTS USED: 29-5351-3-0028,QTY :1 ADD EMP:401055

Part: SEAT TRACK — CORRODED (LT O/B SEAT TRK) · airframe 76,586 hrs · 27,640 cycles

AFT WET AREA STA 907 TO STA 927 LT O/B SEAT TRACK HAS CORROSION REF AAR N/R 9205146 CLEANED SEAT TRACK AT AFT WET AREA FOUND OUT OF LIMITS PER REF DWG 147A5300 SRM 53-00-52-1A-1 FIG 103 RERMOVED SEAT TRACK LBL 45.50 FROM STA 887 TO STA 927 LOCATED DRILLED AND INSTALLED NEW SEAT TRACK PER REF B737 SRM 51-40-02-0G-0 AND DEG 10N01455 AND

Part: UNKNOWN — CORRODED (STA312 - STA325) · airframe 76,586 hrs · 27,640 cycles

ELECTRICAL AND ELECTRONICS COMPARTMENT STA 312 TO STA 325 STR 23L HAS EVIDENCE OF CORROSION REF AAR N/R 9204786 REQUIREMENTS FOR THE STR 23L LOWER AUXILIARY SILL OUTER CHORD REPAIR BETWEEN STA 312 AND STA 325 ON AIRCRAFT N23707 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5311-03050 WORK ACCOMPLISHED BY V894495 ELECTRICAL AND ELECTRONICS COMPARTMENT STA 312 TO STA 325 STR23L REPAIRED IN REF TO ESR/RES NO.2021347-16-5139 AND ECRA5311-03050 UPON THE ACCOMULATION OF 48,000 TOTSL AIRCRAFT CYCLES PLANNING TO CONTACT ENGINEERING FOR THE INSP AUXILIARY SILL OUTER CHORD BETWEEN STA 312 AND STA 325 ON AIRCRAFT N23707 IAW PART 2 OF THE LATEST REV OF ECRA 5311-03050 UPON THE ACCUMULATION OF 50,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION OF THE REPAIR TO THE STR 23L LOWER TOMC APPROVED DIP CARRY. PERFORMED INTERIM REPAIR PER PART 1. TOMC-APPROVAL FROM SC1ELBYC COMMENT PLACED ON DIP TO PERFORM AN INSPECTION OF THE REPAIR TO THE STR 23L LOWER AUX SILL OUTER CHORD BETWEEN STA 310 AND 325 IAW PART 2 OF THE LATEST REVISION REF ECRA 5311-03050 UPON ACCUMULATION OF 50,000 TOTAL AC FC. REF ASSOCIATED DIP LP 5536346 FOR PLANNING TO CONTACT ESC. TOMC UPDATE: TYPO CORRECTION: STA 312 NOT STA 310. QC REVIEWED RECORDS UPDATE QC REVIEWED T/A : 50,000 TAFC............PK/U394517

Part: PANEL — DENTED (STA 259) · airframe 76,586 hrs · 27,640 cycles

FLIGHT DECK FLOOR SKIN PANEL HAS A DENT AT STA 259 REF AAR N/R 9205005 AT STA 259 LBL 11 EVALUATED DENT FOUND OUT OF LIMITS PER REF B737 SRM 53-01-51-11-1 ALLOWABLE DAMAGE 1 DETAIL D REMOVED EXISTING REPAIR PER SRM 53-40-02-0G-0 REPAIR FLIGHT DECK FLOOR WBC AT STA 250 TO 270 PER ECRA2021347-19-5169 REV P1 ON OR BEFORE JUNE 8, 2025, PLANNING TO CONTACT ENGINEERING FOR LATEST REVISION OF EC/RA 5322-01122. INSPECTION REQUIREMENTS FOR THE FLIGHT DECK FLOOR WEB DOUBLER WORK ACCOMPLISHED BY V937697. STRUCTURAL FILLER REPAIR FORWARD OF STA 260 BETWEEN LBL 10 AND BL 0 ON AIRCRAFT N23707 IN ACCORDANCE WITH PART 2 OF AT STA 259 LBL 11 EVALUATED DENT FOUND OUT OF LIMITS PER REF B737 SRM 53-01-51-11-1 ALLOWABLE DAMAGE 1 DETAIL D REMOVED EXISTING REPAIR PER SRM 53-40-02-0G-0 REPAIR FLIGHT DECK FLOOR WBC AT STA 250 TO 270 PER ECRA2021347-19-5169 REV P1 ADD EMP:V894498

Part: UNKNOWN — CORRODED (STR 23L) · airframe 76,586 hrs · 27,640 cycles

ELECTRICAL AND ELECTRONICS COMPARTMENT STA 312 TO STA 325 STR 23L HAS EVIDENCE OF CORROSION REF AAR N/R 9204786 REQUIREMENTS FOR THE STR 23L LOWER AUXILIARY SILL OUTER CHORD REPAIR BETWEEN STA 312 AND STA 325 ON AIRCRAFT N23707 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5311-03050 WORK ACCOMPLISHED BY V894495 ELECTRICAL AND ELECTRONICS COMPARTMENT STA 312 TO STA 325 STR23L REPAIRED IN REF TO ESR/RES NO.2021347-16-5139 AND ECRA5311-03050 UPON THE ACCOMULATION OF 48,000 TOTSL AIRCRAFT CYCLES PLANNING TO CONTACT ENGINEERING FOR THE INSP.

Part: STRINGER — CORRODED (S-22L STA 1016) · airframe 76,586 hrs · 27,640 cycles

AFT CABIN BELOW WET AREA DEFOLIATE CORR AT STRINGER AND TERMINAL S-22L STA 1016 MKD DOT 061. REF AAR N/R 9204798. FOUND CORROSION OUT OF LIMITS, CUTOUT DAMAGED SECTION FROM TO 1016 S-22L PER REF B737 SRM 53-00-03-2R-1 REPAIR 1. STA 977.5 TO STA 1016 S-22L PER REF SRM 53-00-03-2R-1. INSTALLED NEWFITTING AT STR 22L STA 1016 PER REF SRM PERFORMED HFEC AND PROBE INSPECTION. FABRICATED SPLICE, 51-40-02-0G-0. EXTRUSION AND INSTALLED REPAIR PARTS AT AFT WET AREA STA 977.5 WORK ACCOMPLISHED BY V913200.

Part: SKIN — DENTED (STA 259) · airframe 76,586 hrs · 27,640 cycles

FLIGHT DECK FLOOR SKIN PANEL HAS A DENT AT STA 259 REF N/R 9205005 AT STA 259 LBL 11 EVALUATED DENT FOUND OUT OF LIMITS PER REF B737 SRM 53-01-51-11-1 ALLOWABLE DAMAGE 1 DETAIL D REMOVED EXISTING REPAIR PER SRM 53-40-02-0G-0 REPAIR FLIGHT DECK FLOOR WBC AT STA 250 TO 270 PER ECRA2021347-19-5169 REV P1.

Part: BEAM — CORRODED (STA 986) · airframe 76,586 hrs · 27,640 cycles

AFT WET AREA STA 986 AT RBL 17 TO RBL 48: FLOOR BEAM UPPER FLANGE PREVIOUS REPAIR HAS CORROSION (DOT 56-011). (REF AAR N/R 9204644) REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED NEW REPAIR AT AFT WET AREA STA 986.5 BETWEEN RBL 48 TO RBL 50 PER REF. B737-700 SRM 53-90-51-2R-4.

Part: FLOOR SUPPORT — CORRODED (STA 951) · airframe 76,586 hrs · 27,640 cycles

AFT WET AREA STA 951 AT RBL 26 TO RBL 49: FLOOR SUPPORT ANGLE HAS CORROSION (DOT 56-012). (REF AAR N/R 9204645) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT AFT WET AREA STA 951 AT RBL 26 TO RBL 49 AS PER REF. SRM 51-40-02-0G-0 AND DRWG#147A5650 REV."E"

Part: STRINGER — CORRODED (STR 22L STA 1016) · airframe 76,586 hrs · 27,640 cycles

AFT CABIN BELOW WET AREA DEFOLIATE CORR AT STRINGER AND TERMINAL S-22L STA 1016 MKD DOT 061. REF AAR N/R 9204798. FOUND CORROSION OUT OF LIMITS, CUTOUT DAMAGED SECTION FROM TO 1016 S-22L PER REF B737 SRM 53-00-03-2R-1 REPAIR 1. STA 977.5 TO STA 1016 S-22L PER REF SRM 53-00-03-2R-1. INSTALLED NEWFITTING AT STR 22L STA 1016 PER REF SRM PERFORMED HFEC AND PROBE INSPECTION. FABRICATED SPLICE, 51-40-02-0G-0. EXTRUSION AND INSTALLED REPAIR PARTS AT AFT WET AREA STA 977.5

Part: INTERCOSTAL — CORRODED (STA328-STA344) · airframe 76,586 hrs · 27,640 cycles

PASSENGER CABIN FLOOR STRUCTURE FWD WET AREA INTERCOSTAL STA328 TO STA344 LBL12 HAS SURFACE CORROSION (REF AAR NR 9204617)

Part: PRESSURE WEB — CRACKED (CTR REAR SPAR) · airframe 76,586 hrs · 27,640 cycles

CRACK FOUND ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB AT LBL 40.00 TO LBL 31.83 (DOT 002). REF AAR N/R 9204444. INSPECTION INTERVAL 36,000 FLIGHT CYCLES. WORK ACCOMPLISHED BY V896697. REPAIRED WEB AT CENTER WING REAR SPAIR IN REF SRM 57-10-10-2R-3 STA 663, LBL 31.83 TO LBL 45.0. ACCOMPLISHED INSPECTION 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION HIGH FREQUENCY EDDY CURRENT AND LOW FREQUENCY EDDY CURRENT.

Part: FRAME — CORRODED (E&E COMPARTMENT) · airframe 76,586 hrs · 27,640 cycles

ELECTRICAL AND ELECTRONICS COMPARTMENT FRAME STA312+7 STRINGER 21L TO LONGERON22L HAS EVIDENCE OF CORROSION (REF AAR NR 9204606)

Part: LONGERON — CORRODED (E&E COMPARTMENT) · airframe 76,586 hrs · 27,640 cycles

ELECTRICAL AND ELECTRONICS COMPARTMENT STA294.5+7 LONGERON 23L HAS EVIDENCE OF CORROSION (REF AAR NR 9204599)

Part: BULKHEAD WEB — CRACKED (LBL 40.00 TO LBL) · airframe 76,586 hrs · 27,640 cycles

CRACK FOUND ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB AT LBL 40.00 TO LBL 31.83 (DOT 002). REF AAR N/R 9204444. INSPECTION INTERVAL 36,000 FLIGHT CYCLES. WORK ACCOMPLISHED BY V896697. REPAIRED WEB AT CENTER WING REAR SPAIR IN REF SRM 57-10-10-2R-3 STA 663, LBL 31.83 TO LBL 45.0. ACCOMPLISHED INSPECTION 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION HIGH FREQUENCY EDDY CURRENT AND LOW FREQUENCY EDDY CURRENT ADD EMP:V896697

Part: DOOR — CORRODED (STA312TO STA344) · airframe 76,586 hrs · 27,640 cycles

PASSENGER CABIN FLOOR STRUCTURE FWD WET AREA AT FWD ENTRY DOOR STA 312 TO STA 344 HAS SURFACE CORROSION REF AAR N/R 9204618 REMOVED AND REPLACED PASSENGER CABIN FLOOR STRUCTURE FWD WET AREA AT ENTRY DOOR STA 312 TO 344 LBL56 REF B737 SRM 51-40-02-0G-0 INNER CHORD WORK ACCOMPLISHED BY V894071

Part: ANGLE — CORRODED (DOOR SIL I/B) · airframe 76,586 hrs · 27,640 cycles

PASSENGER CABIN WET AREA ENTRY DOOR SIL I/B ANGLE HAS SURFACE CORROSION REF AAR N/R 9204624 REMOVED AND REPLACED ANGLE PASSENGER CABIN FWD WET AREA ENTRY DOOR SIL I/B AS PER REF B737 SRM 51-10-02-06-0 AND SRM 51-40-02-0G-0 WORK ACCOMPLISHED BY V894071

Part: STIFFENER — CRACKED (RIB STA 101.90) · airframe 76,586 hrs · 27,640 cycles

LEFT HORIZONTAL STAB. RIB STA 101.90, STIFFENER NO.4 HAVE EVIDENCE CRACKED. (REF AAR N/R 9204507) REMOVED FRUNT WEB FOR ACCESS TO REMOVE RIB AT STA 101.90 REF SRM 51-40-02 REMOVED RIB AND REPAIRED STIFFENER NO.4 REF SRM 55-10-09-2R-4 REINSTALLED RIB AND FRUNT WEB AT STA 101.90 REF SRM 51-40-02 WORK ACCOMPLISHED BY V938928

Part: ANGLE — CORRODED (DOOR SILL) · airframe 76,586 hrs · 27,640 cycles

PASSENGER CABIN WET AREA ENTRY DOOR SIL I/B ANGLE HAS SURFACE CORROSION REF AAR N/R 9204624. REMOVED AND REPLACED ANGLE PASSENGER CABIN FWD WET AREA ENTRY DOOR SIL I/B AS PER REF B737 SRM 51-10-02-06-0 AND SRM 51-40-02-0G-0 WORK ACCOMPLISHED BY V894071

Part: DOOR — CORRODED (STA 312 TO STA 3) · airframe 76,586 hrs · 27,640 cycles

PASSENGER CABIN FLOOR STRUCTURE FWD WET AREA AT FWD ENTRY DOOR STA 312 TO STA 344 HAS SURFACE CORROSION REF AAR N/R 9204618 REMOVED AND REPLACED PASSENGER CABIN FLOOR STRUCTURE FWD WET AREA AT ENTRY DOOR STA 312 TO 344 LBL56 REF B737 SRM 51-40-02-0G-0 INNER CHORD WORK ACCOMPLISHED BY V894071

Part: DRAIN LINE — LEAKING (POTABLE WATER) · airframe 75,264 hrs · 27,011 cycles

LARGE POTABLE WATER SPILL DETECTED 1/14/23 IN AFT CARGO BELOW CENTER FLOOR FROM FUSELAGE POTABLE WATER TANK OVERFLOW DRAIN PORT HOSE AT AFT SIDE OF AFT CARGO AFT BULKHEAD STA. 947 TO AFT CARGO FWD BULKHEAD STA. 727 FROM S25L-S25R. PERFORMED EC/RA 2011-01000 CARGO COMPARTMENT SPILL SECTIONS 1. THROUGH 2.A. TO AFT CARGO AREA BENEATH FLOORS DURING SCHEDULED MAINTENANCE VISIT.

Part: RELAY — INOPERATIVE (STAB TRIM) · airframe 75,211 hrs · 26,987 cycles

STAB TRIM INOPERATIVE. UNABLE TO ENGAGE AUTOPILOT. REPLACED STAB TRIM CONTROL RELAY, R64 IN J4 JUNCTION BOX. OPERATED GROUND TEST OFTHE SYSTEM, GROUND TEST PASSED AND CHECKED OK IAW TASK 27-41-71-700-801.

Part: WINDSHEAR SYS — NONE (NA) · airframe 71,728 hrs · 25,574 cycles

RTO DUE WINDSHEAR AT 96 KTS REVIEWED PARAMETERS IAW 05-51-07-210-801. NO MTC ACTION REQUIRED

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. SPT 5429188 REMOVED AND REPLACED SHEAR FITTING ATSTA 540 RBL 6.14 IAW EC/RA 5714-01127 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 A MM 28-11-00 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. SPT 5429190 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW EC/R A 5714-01129 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP 98 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. SPT 5429193 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW EC/RA 5714-01122 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT 46-0024 ENTERED BY UAL INSP 3/2 9/2020 RII

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. SPT 5429197 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 54.60 IAW EC/R A 5714-01126 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT FORM 46-0024 ENTERED BY UAL 98 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. SPT 5429189 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW EC/R A 5714-01128 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP 98 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. SPT 5429194 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW EC/R A 5714-01123 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP 98 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. SPT 5429195 REMOVED AND REPLACED SHEAR FITTING AND TUBE BRACKET IAW EC/RA 57 14-01124 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT ENTERED BY UAL INSP 3/29/2020 RII

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. SPT 5429196 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW EC/R A AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPOR T 46-0024 ENTERED BY UAL INSP 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. SPT 5429191 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW EC/R A 5714-01130 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP 98 3/29/2020 RII.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,613 hrs · 24,767 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SPT 5429192 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW EC/R A 5714-01131 REV ORIGINAL AND APPLIED VAPOR BARRIER IAW B737-700 AMM 28-11-00 SSFR FORM REPORT 46-0024 ENTERED BY UAL INSP 98 3/29/2020 RII.

Part: ACCESS DOOR — DAMAGED (A/C BAY) · airframe 68,091 hrs · 24,238 cycles

ACCESS DOOR FOR AIRSTART CONNECTION DAMAGED, FOUND OPEN ON ARRIVAL. ACPD ECRA TEMP REPAIR, PLACED ON DIP DIP APPROVED, ACCOMPLISHED INTERM REPAIR REPLACE TAPE AFTER EACH TIME DOOR IS OPENED AND REPAIR PER PART 3 WITHIN 2 LANDINGS TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC REMOVED AND REPLACED AIR CONDITION ACCESS DOOR ASSY. P/N 59-5351-3-0002. REF. IPC 52-49-00-01. DIP CLOSED. TOMCQC REV PERFORMED QC REVIEWED.

Part: LANDING GEAR — MALFUNCTIONED · airframe 66,076 hrs · 23,406 cycles

ALL GEAR WOULD NOT RETRACT ON TAKEOFF AFTER DEBRIEFING CAPTAIN HE COMENTED THAT AFTER GETTING ON GROUND HE WAS ASKED TO CK MANUAL EXTENSION ACESS DOOR AND HE FELT LIKE DOOR MIGHT NOT HAVE BEEN SHUT WHILE PRESSING ON DOOR HE HEARD A AUDIBLE CLICK BUT IS NOT POSITIVE NOTE PSEU HAS ZERO FAULTS AND ZERO FAULT HISTORY PERFORMED REPAIR CONFIRMATION PER FIM 32-30-00-810-815 STEP { G} . SWUNG GEAR SEVERAL TIMES WITH NO FAULTS.

Part: SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 61,383 hrs · 21,416 cycles

LEFT OVERWING EMER EXIT ILLUMINATED. ACP TS PROCEDURE IAW FIM 52-20-00-810-806, ADJUSTED SW S1104 IAW AMM 52-71-22-820-805, ACP OPS TEST IAW AMM 52-22-00-710-802, OPS CK GOOD.

Part: SUPPORT — CORRODED (MLG WW) · airframe 61,257 hrs · 21,354 cycles

MAIN WHEEL WELL KEEL BEAM LOWER SUPPORT CORRODED AT BL 0 FWD OF AFT BULKHEAD. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-12, FABRICATED WEB IAW DRAW 144A7134 AND INSTALLED IAW DWG 144A7134, AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 727B-887) · airframe 61,257 hrs · 21,354 cycles

CABIN SEAT TRACK UPPER CTR AREA HAS CORROSION LEFT OTBD BS 727B - 887. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REP 5, FIG 202, AND ECRA 5340-01789.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 61,257 hrs · 21,354 cycles

EXTERNAL POWER CAVITY INTERNAL DOUBLER HAS A CRACK APPROX 1IN AT FWD CUTOUT. REMOVED AND REPLACED EXTERNAL POWER INTERNAL DOUBLER REF SRM 51-40-02 AND DWG 141A3722.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,257 hrs · 21,354 cycles

CABIN FLOORBEAM HAS CORROSION AROUND LAV MOUNT BS 947 RBL 54. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT LIMITS IAW EC/RA 5321-01330. REPAIRED FLOORBEAM AT STA 947 FROM RBL 34 TO RBL 58 UPPER FLANGE AREA IAW SRM 53-70-51 REPAIR 5 ALTERNATIVE 2 FIG 206

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,524 hrs · 19,464 cycles

SUPPORT TASK, EMER LIGHT AT 7DEF, AREA LIGHT, INOPERATIVE. RELAMPED L1065 AT STATION 500+20, WL 274 & RBL 30. OPERATIONAL CHECKED GOOD IAW AMM 33-51-03.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 56,524 hrs · 19,464 cycles

SUPPORT TASK LT DRAG ANGLE CRACKED AT BS 540, STRINGER 22L EXTERNAL FUSELAGE. R & R DRAG LINK ASSEMBLY.AT STATION 540, LT SIDE STRINGER 22L IAW SRM 51-40-02 & DWG 143A0060.

Part: FUSE — FAILED (CABIN) · airframe 54,313 hrs · 18,587 cycles

RIGHT SIDE OVERWING ESCAPE GND ILLUMINATION LIGHT INOPERATIVE. REPLACED EMER EXIT LIGHT BATTERY PACK M1670 FUSE & OPERATIONS CHECKS GOOD IAW AMM 33-51-06-960-804.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,313 hrs · 18,587 cycles

WHILE ACCOMPLISHING EA 5320-02076 REV E OP 3 THE MAIN CABIN SEAT TRACK SPLICE LOCATION STATION 727B, RBL 24.75 HAS CRACKS ON THE SEAT TRACK HOLES COMMON TO THE SPLICE STRAP. THE SPLICE STRAP ALSO HAS CRACKED HOLES & THE REPAIR IAW THE EA DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. REPAIRED SEAT TRACK STATION 727B, RBL24.75 IAW ECRA 5320-02389.

Part: SKIN — WORN (FUSELAGE) · airframe 54,313 hrs · 18,587 cycles

UPPER FUSELAGE EXTERIOR SKIN IS WORN AT STATION 857 LBL-2. INSTALLED REPAIR DOUBLE AT FS 847 - 867 IAW ECRA 5330-050 03 PART 1. ACCOMPLISH AN INSPECTION OF CROWN SKIN REPAIR IAW ECRA 5330-05003 IAW PART 2 ON OR BEFORE 50,000 TOTAL ACFT FLIGHT CYCLES. CONTACT ENGINEERING AFTER 45,000 TOTAL ACFT FLIGHT CYCLES BUT BEFORE 47,000 TOTAL ACFT FLIGHT CYCLES FOR INSPECTION DETAILS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,313 hrs · 18,587 cycles

WHILE ACCOMPLISHING EA 5320-02076 REV E OP 3 THE MAIN CABIN SEAT TRACK SPLICE LOCATION STATION 727B, LBL 45.50 HAS CRACKS ON THE SEAT TRACK HOLES COMMON TO THE SPLICE STRAP. THE SPLICE STRAP ALSO HAS CRACKED HOLES & THE REPAIR IAW EA DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. REPAIRED SEAT TRACK STATION 727B, LBL45.50 IAW ECRA 5320-02389.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,313 hrs · 18,587 cycles

WHILE ACCOMPLISHING EA 5320-02076 REV E OP 3 THE MAIN CABIN SEAT TRACKS SLICE LOCATION STATION 727B, RBL45.50 HAS CRACKS ON THE SEAT TRACK HOLES COMMON TO THE SPLICE STRAP. THE SPLICE STRAP ALSO HAS CRACKED HOLES & THE REPAIR IAW THE EA DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. REPAIRED SEAT TRACK STATION 727B, RBL 45.50 IAW ECRA 5320-02839.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,313 hrs · 18,587 cycles

WHILE ACCOMPLISHING EA 5230-02076 REV E OP 3, THE MAIN CABIN SEAT TRACK SPLICE LOCATION STATION 727B, LBL 24.75 HAS CRACKS ON THE SEAT TRACK HOLES COMMON TO THE SPLICE STRAP. THE REPAIR IAW THE EA DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. REPAIRED SEAT TRACK STATION 727B, LBL 24.75 IAW ECRA 5320-02389.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 54,313 hrs · 18,587 cycles

WHEN PREFORMED C SCAN EDDY CURRENT INSPECTION ON LT HORIZONTAL STAB LOWER SKIN FOUND CRACK INDICATION ON STATION SS101.90. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR DOUBLER & FILLER ON LT HORIZONTAL STAB LOWER SKIN AT STATION SS101.90.

Part: DRAIN LINE — OUT OF POSITION (COCKPIT WINDOW) · airframe 50,353 hrs · 17,071 cycles

AFTER TAKEOFF FIRST OFFICER WINDOW DRAIN TUBE WAS CAUGHT IN WINDOW & NOISE WAS SO LOUD WE RETURNED FOR LANDING PRESSURIZATION WAS NORMAL. REPOSITIONED DRAIN TUBE & CLOSED WINDOW.

Part: WIRE — CUT (SMOKE DETECTOR) · airframe 49,050 hrs · 16,586 cycles

FWD LAV SMOKE DETECTOR REPORTED INOP BY F/A FOUND WIRE W1008-0260-22 CUT 2" FROM CB C1125 BEHIND THE P18-3 CB PANEL REF WDM 26-14-11 P.6. SPLICED WIRE USING RACHEM IAW SWP 20-10-13. FWD LAV SMOKE DETECTOR, OPS GOOD.

Part: FLOOR SUPPORT — CRACKED (BS 747-767) · airframe 46,626 hrs · 15,718 cycles

AFT CARGO BAY BS 747 AND 767 AT RBL 9 FLOOR SUPPORT CRACKED AT ATTACHING POINTS. INSTALLED REPAIR REF ECRA 5321-01802.

Part: SKIN — DAMAGED (BS 685 S1R) · airframe 46,626 hrs · 15,718 cycles

SUPPORT TASK, LIGHTNING STRIKE AT STA 685, STR 1R + 6" STA 685 AT STR 1R+ 6". REPAIRED IAW ECRA 5331-01616.

Part: BULKHEAD — CORRODED (BS 727) · airframe 46,626 hrs · 15,718 cycles

AFT CARGO BAY FWD BULKHEAD AREA, BS 727, APU BLEED AIR DUCT OPENING AREA EXFOLIATION FOUND. PERFORMED INTERIM REPAIR IAW EC/RA 5311-01560, PART 1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 46,626 hrs · 15,718 cycles

LT STABILIZER LOWER INNER SPAR SKIN CRACKED AT STA 147.90 8.5" AFT OF FWD SPAR. REPAIR MADE AT STA 147.90 IAW SRM 55-10-01, REPAIR 11 INITIAL ALSO NOTE THAT AFTER INITIAL INSP AT 56,000 FLT CYC, REPEAT INSPECTION TO BE ACCOMPLISHED AT 56,000 FLT CYC AFTER REPAIR INSP AT EVERY 9,000 FLT CYC ARE REQUIRED IAW TABLE 204. REINSPECT CATAGORY "B" REPAIR STA 147.90, 8.5 AFT FWD SPAR WITHIN 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION DV & LFEC & WITHIN EVERY 9,000 FLIGHT CYCLES THEREAFTER (NDT PART 6) IAW SRM 55-10-01, REPAIR 11, TABLE 204, PG 216, DIP CTL 16511.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 46,626 hrs · 15,718 cycles

LT STABILIZER LOWER INNER SPAR SKIN CRACKED AT STA 138.70, 10" FWD OF REAR SPAR REPAIR MADE AT STA 138.70 IAW SRM 55-10-01, REPAIR 11. INITIAL ALSO NOTE THAT AFTER INITIAL INSP IS ACCOMPLISHED AT 56,000 FLT INSP REQUIRED AT 56,000 FLT CYC AFTER REPAIR IAW TABLE 204 CYC AFTER REPAIR REPEAT INSP AT EVERY 9000 FLT CYC ARE RE PAGE 216 REQUIRED. REINSPECT CATAGORY "B" REPAIR WITHIN 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION DV & AMP; LT FEC AND WITHIN EVERY 9,000 FLIGHT CYCLES THEREAFTER (NDT PART 6) IAW SRM 55-10-01, REPAIR 11, TABLE 204, PG 216. DIP CTL 16510.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 46,626 hrs · 15,718 cycles

LT STABILIZER LOWER INNER SPAR SKIN CRACKED AT STA 157.10 9.5" FWD OF REAR SPAR REPAIR MADE IAW SRM 55-10-01, REPAIR 11 INITIAL INSP REQUIRED AT 56,000 FLT CYC AFTER REPAIR FOLLOWED BY REPEAT INSP EVERY 9,000 FLT CYC THERE AFTER QC. REINSPECT CATAGORY "B" REPAIR STA 157.10 9.5 FWD REAR SPAR WITHIN 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION DV & AMP; WITHIN EVERY 9,000 FLIGHT CYCLES THEREAFTER (NDT PART 6) SRM 55-10-01, REPAIR 11, TABLE 204, PG 216. DIP CTL 16512.

Part: FRAME — CRACKED (BS 440) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME 440L, STRINGER 8L-9L. REPAIRED IAW EA 5330-04716, REV C, OP 1.

Part: FRAME — CRACKED (BS 500) · airframe 46,626 hrs · 15,718 cycles

DURING INSPECTION OF OP4, NOTICED FRAME 500C RT CRACKED AND NO REPAIR WAS PERFORMED. VISUAL INSPECTION SHOWS RIVET CLOSEST TO RADIUS HAS 2 CRACKS. REPAIRED IAW EA 5330-04716, REV C, OP 1.

Part: FRAME — CRACKED (BS 747) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 747R, STRINGER 8L-9L. REPAIRED IAW EA 5330-04716, REV C, OP 1.

Part: FRAME — CRACKED (BS 480) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME 480L, STRINGER 8L-9L REPAIRED IAW EA 5330-04716, REV C, OP 1.

Part: FRAME — CRACKED (BS 727D S8-9L) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT BS 727D, STRINGER 8-9L. REPAIRED FRAME IAW EA 5310-04716, FIG 3, REV C. OP1.

Part: FRAME — CRACKED (BS 747L) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 747L, STRINGER 8L-9L FWD RIVET REPAIRED REF EA 5310-0716, REV C, OP 1.

Part: FRAME — CRACKED (BS 787 S8-9L) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT BS 787 LT STRINGER 8-9L. REPAIRED FRAME IAW EA 5310-04716, REV C, OP 1.

Part: FRAME — CRACKED (BS 867L) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 867 LT STRINGER 8L-9L. REPAIRED FRAME REF EA 5310-04716.

Part: FRAME — CRACKED (BS 400) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STATION 400 LEFT. REPAIRED FRAME IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 500C) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STATION 500C LEFT. REPAIRED FRAME IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 440) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 440 R STRINGER 8L-9L FWD RIVET. COMPLETED REPAIR IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 500) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 500 AL, STRINGER 8L - 9L INSTALLED REPAIR REF EA 5310-04716, REV C.

Part: FRAME — CRACKED (BS 500A) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 500A RT STRINGER 8L-9L FWD RIVET INDICATION. INSTALLED REPAIR IAW EA 5310-04716, REV C.

Part: FRAME — CRACKED (BS 400R) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT STA 400R STRINGER 8L-9L. COMPLETE REPAIR IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 480 S8-9L) · airframe 46,626 hrs · 15,718 cycles

CRACK IN FRAME AT BS 480, STRINGER 8L-9L INSTALLED SERVICEABLE REPAIR ANGLES IAW EA5310-04716, REV C.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,213 hrs · 13,831 cycles

EMERGENCY EXIT SEAT LIGHT INOP AT ROWS 11/12/14/20. REMOVED AND REPLACED BATTERY PACK FOR ROWS 11, 12, 14, 20 IAW AMM 33-51-06-960-805, ALL OPS CHECKS GOOD. CFOR SDR REPORTING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,422 hrs · 10,640 cycles

R-1 DOOR EMERGENCY INSIDE LIGHT INOP. REPLACED BATTERY PACK PER 33-51-06-960-805.

Part: FLOORBEAM — CORRODED (STA 986.5) · airframe 24,637 hrs · 8,064 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 43 TO RBL 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01306.

Part: PIN — CORRODED (RT HOR STAB) · airframe 19,219 hrs · 6,331 cycles

INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT TOP ATTACH PIN CORRODED. THE ATTACH PIN WAS REPLACED IAW EA 5510-01696.

Part: PIN — CORRODED (LT HOR STAB) · airframe 19,219 hrs · 6,331 cycles

INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT TOP ATTACH PIN CORRODED. THE ATTACH PIN WAS REMOVED AND REPLACED IAW EA 5510-01696.

Part: PIN — CORRODED (RT HOR STAB) · airframe 19,219 hrs · 6,331 cycles

INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT CENTER AND AFT LOWER ATTACH PINS CORRODED. THE ATTACH PINS WERE REPLACED IAW EA 5510-01696.

Part: PIN — CORRODED (LT HOR STAB) · airframe 19,219 hrs · 6,331 cycles

INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER AND AFT MIDDLE ATTACH PINS CORRODED. THE ATTACH PINS WERE REPLACED IAW EA 5510-01696.

Part: APU — FLAMED OUT (APU BAY)

APU REMOVED FROM AIRCRAFT WHEN APPARENT THERMAL DAMAGE WAS NOTED AT TAIL SECTION OF AIRCRAFT. UPON RECEIPT OF APU AT HONEYWELL REPAIR STATION THE APU WAS EVALUATED IN A TEST CELL. FLAMES OUT THE TAILPIPE WERE NOTED DURING TEST CELL OPERATION OF THE APU. CURRENTLY ROOT CAUSE ANALYSIS IS BEING PERFORMED TO DETERMINE THE FAILRE MODE OF THE APU.

Part: FITTING — CRACKED (LT ELEV TAB)

INSPECTION FOUND A .75 INCH CRACK IN LT ELEVATOR TAB MAST ARM FITTING. THE LT ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-31-00 AND 27-31-31. THE TAB WAS RIGGED AND OPERATION WAS NORMAL.