N13716

Part: GIRT BAR — OUT OF POSITION (ZONE 800) · airframe 82,623 hrs · 30,418 cycles

R1 GIRT BAR IS DRAGGING REMOVED DOOR 1R SLIDE AND PACKED ZEE FOLD AND INSTALLED AFFECTED SLIDE IAW AMM 26-66-01/401 FLAGGING RII. ACCOMPLISHED RII INSPECTION OF DR 1R SLIDE INSTALLATION PER GMM 09-25-05 AND AMM 25-66-01.

Part: LATCH — OUT OF TOLERANCE (ZONE 800) · airframe 82,536 hrs · 30,368 cycles

AFT ENTRY DOOR LIGHT CAME ON IN FLT. WENT OUT AFTER PUSHING ON THE HANDLE. HAPPENED 2 LEGS, FOUND L2 DOOR LOWER FWD AND AFT LATCH RECEIVERS OUT OF CLEARANCE, ADJUSTED L2 DOOR LOWER FWD AND AFT LATCH RECEIVERS IAW AMM 52-13-00-820-801 AND PERFORMED TORQUE HANDLE TEST IAW AMM 52-13-00-700-805. TORQUE HANDLE LATCHING AND UNLATCHING WITHIN RANGE. INSPECTED PER RII REQUIREMENTS PRESSURIZED CABIN REFERENCING AMM 05-51-91-790-801, L2 DOOR INTERIOR HANDLE STAYED LATCHED AND NO AFT ENTRY INDICATION OPS CHECKED GOOD.

Part: SENSOR — OUT OF TOLERANCE (ZONE 800) · airframe 82,340 hrs · 30,262 cycles

L1 DOOR INDICATED OPEN DURING CLIMB 5 TIMES. NOT FLICKERING. ON STEADY. NORMAL PRESSURE. HANDLE CL FOUND S199 OUT OF TOLERANCE. ADJUSTED SENSOR TO 21 MILS. LIGHT AND PSEU OPS CHECK GOOD. REF: AMM TASK 52-71-11-820-801.

Part: NUT — LOOSE (TARGET) · airframe 82,330 hrs · 30,257 cycles

WHEN TAXING FWD ENTRY LIGHT CAME ON. DOOR VERIFED CLOSE AND HANDLE FULL DOWN FORWARD ENTRY DOOR INDICATION IS INTERMITTENT WHEN ACTUATING THE INDICATION SWITCH. WHEN L1 DOOR IS CLOSED ITS FLUSH WITH FUSELAGE. DOOR IS FAIRED WITH THE FUSELAGE. VERIFIED THAT ALL EXTERIOR/INTERIOR DOOR HANDLES ARE IN THE PROPER CLOSED/FAIRED POSITION. M/L FOR FORWARD ENTRY DOOR INDICATION SENSOR FOUND TARGET JAMNUTS AT DOOR 1 LOOSE. ADJUSTED TARGET REFERENCE AMM 52-71-11-820-801 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 81,405 hrs · 29,789 cycles

30 ABC EMER AISLE LIGHT INOPERATIVE. EMERGENCY AISLE LIGHT 30 ABC SECURED INTO PLACE, LENS NOT BROKEN AND LIGHT IS INOPERATIVE. REMOVED AND REPLACED SEAT 30ABC EMERGENCY LIGHT HOUSING IAW IFM 25-22-59. OPS CHECK GOOD.

Part: LIGHT — DETACHED (ZONE 200) · airframe 81,405 hrs · 29,789 cycles

ROW 22ABC EMERGENCY LIGH IN AISLE FELL OUT. SWAPPED 22 ABC WITH 30 ABC, EMER LIGHT OPS CHECKS ARE NORMAL.

Part: DOOR — MALFUNCTIONED (L1) · airframe 81,105 hrs · 29,644 cycles

AIRCRAFT WONT PRESSURIZE DOOR 1L LOUD AIR LEAK ON ARRIVAL BACK TO THE GATE, GATE AGENT FOUND DOOR 1L NOT CLOSE PROPERLY DOOR BINDING AT ROLLER ASSY. OPS CHECKED 1L MULTIPLE TIMES IN REF TO AMM 52-11-00. DOOR OPERATES NORMAL AND NO BINDING. CHECKED RIG IN REF TO AMM 52-11-00-820-801. NO ADJUSTMENTS MADE OR NEEDED AT THIS TIME. DOOR HANDLE FOUND NOT TO BE SOFT LATCHING AND TESTED IN REF TO AMM 52-11-00-700-804. PRESSURIZED A/C IN REF TO AMM 05-51-91. NO LEAKS NOTED AT 1L DOOR. ALL DAMAGE AREAS NOTED IN PHOTOS ARE OLD. DOOR NOT BINDING NOW.

Part: STRIKER — WORN (ZONE 800) · airframe 81,083 hrs · 29,627 cycles

WHILE REMOVING DOOR 192 DR FOUND O/B LATCH HAS WORN THROUGH THE STRIKER PLATE.REMOVED SEAL AND RETAINER FOR ECS DOOR 192CR, BAGGED AND TAGGED PARTS. FOUND DAMAGE TO UPPER SURFACE OF CHORD AND MULTIPLE #40 HOLES PLUGGED ON BOTTOM. WILL NEED TO PERFORM SRM REPAIR 57-10-13-2R-3. INITIATED SFR. COMPLIED WITH STEPS 4 A THROUGH E OF SRM 57-10-13-2R-3. REMOVED 3 NUTPLATES AND REMOVED DAMAGE AS REQUIRED. REQUIRE NDT FOR CUTOUT EDGE AND ORIGINAL 5/32 NUTPLATE HOLES REF STEPS 4 F AND 4 G. IDENTIFIED REPAIR MATERIALS FOR ITEM 1 STRAP 7075-T6 0.125" PO # 6374129, ITEM 4 FILLER 7075-T6 0.125" PO # 6374129 AND ITEM 6 SHIM 7075-T6 0.090" PO # 8034319 PER SRM 57-10-13-2R-3 REPAIR STEP 4I TABLE 201. MATERIAL VERIFICATION IS REQUIRED. PERFORMED RII REQS OF NDT OF BLENDED DAMAGE AREA AND FASTNER HOLES AS PER. NDT HFEC. PER NDT PART 6 51-00-00 PROCEDURE 23 & 51-00-00. PROCEDURE 16 FOR HOLE PROBE , NO CRACKS NOTED. MATERIAL VERIFICATION REQUESTED. PERFORMED MATERIAL VERIFICATION OF IDENTIFIED REPAIR MATERIALS FOR ITEM 1 STRAP 7075-T6 0.125" PO # 6374129, ITEM 4 FILLER 7075-T6 0.125" PO # 6374129 AND ITEM 6 SHIM 7075-T6 0.090" PO # 8034319 PER SRM 57-10-13-2R-3 REP PERFORMED STEPS 4H THROUGH N(3) REF SRM 57-10-13-2R-3. ADD EMP:U125272 INSTALLED NUTPLATES, -4 FILLER AND STRIKER PLATE REF SRM 57-10-13-2R-3. REQUIRE OK TO INSTALL REPAIR STRAP ASSY ON LWR BEAM CHORD. OK TO INSTALL REPAIR STRAP REF SRM 57-10-13-2R-3 COMPLIED WITH STEPS J THROUGVERIFIED COMPLETION OF CHORD REPAIR REF SRM 57-10-13-2R-3

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 81,083 hrs · 29,627 cycles

EMERGENCY LIGHT BATTERY PACK AT M1674 FAILS CAPACITY CHECK. PARTS NIS IN CLE. NEW BATTERY ON AOG. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M1674 IAW 737NG AMM TASK 33-51-06-960-805. OPS CHECK GOOD.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 81,033 hrs · 29,602 cycles

DURING WINDOW CLEAN FOUND CRACK ON R3 WINDOW FRAME, FORWARD LOWER CORNER.PHOTO ADDED. CRACK EXTENSE THE LENGTH OF POST 3, 2ND FASTENER UP FROM BOTTOM, WINDOW POST IS OUT OF LIMITS PER SRM 56-10-02 -1A-3 STEP 4.A.1 DETAILS A,B AND D . MADE CUT IN RH DOOR POST READY FOR INSP TO PERFORM HFEC PER AVO 14577 REV F STEP 5.C ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT INSPECTION ON R3 WINDOW FRAME EDGES OF TRIM OUT REF NDT PART 6, 51-00-00 PROCEDURE 23 AND AVO 14577 REV F STEP 5.C. NO LIMITED DEFECT NOTED. PER AVO 14577 REV H STEP 9. NEED TO VERIFY MATERIAL FOR -1 FILLER MADE FROM 7075 T6 CLAD, .250" PO # 2970119. AND -2 FILLER MADE FROM 7075 T6 CLAD, .100" PO # 1828461. PIC ATTATCHED. REF: AVO 14577 REV H STEP 9. VERIFIED MATERIAL FOR -1 FILLER MADE FROM 7075 T6 CLAD, .250" PO # 2970119. AND -2 FILLER MADE FROM 7075 T6 CLAD, .100" PO # 1828461. MILLED DOWN -1 FILLER FROM .250" TO .200" REF. AVO14577 REV. H.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 80,585 hrs · 29,403 cycles

DO TO UN COMMANDED POSS TE FLAP INDICATED JUST SHY OF 15. AIR RP EED WAS 210 KTS. FLAP 15 OVR SPD PHASE 1 FLAP INSPECTION REQUIRED DUE AIRSPEED 210 KTS. AT FLAPS 15 AS PER AMM 05-51-08/201. ACCOMPLISHED PHASE 1 INSPECTION OF TRAILING EDGE FLAPS PER MM 05-51-08-210-801. REFERENCE LOG PAGE 3856816 FOR DISCREPANCIES FOUND.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 79,139 hrs · 28,734 cycles

DIFF PRESSURE EXCEEDED LIMITATION. 8.5 AT FL380CREW FL380 DIFFERENTIAL PRESS WAS 8.5 AND RISING. WENT TO 8.9. M AX WAS 8.3 OPERATING LIMIT. DESCENDED DOWN TO FL 240. WENT DOWN TO 7.8 AND AND BACK UP TO 8.5 . AT 20000 WENT TO 8.0 AT 20000 C ABIN ALT WAS AT 0 AND SHOULD HAVE BEEN AROUND 3000FT. NEEDLE NEV ER WENT BELOW THE DIFFERENTIAL PRESSURE LIMITATION UNTIL THEY W ERE AT FL140. DIDN'T NOTICE ANY CHANGES WITH POWER SETTING AND 0 2 MASKS DID NOT DEPLOY. CA BELIEVES IT TO BE AN OVER PRESSURE. PRESSURIZED AIRCRAFT REF AMM 21-00-05-780-801 TO 4 PSID. NO HULL LEAKS FOUND. AFTER 4 PSID CLOSED OUTFLOW VALVE COMPLETLY AND TURNED BOTH PACKS OFF. AFTER 2 MINUTES PRESSURE WAS AT 2.5 AND RATE OF CHANGE NEVER EXCEEDED 1.5. ROTABLE PARTS CHANG ROTABLE PARTS CHANGE WAS INDICATED - TT # 1369988 SN OFF 9763 IPC REFERENCE # 21-31-00 VALVE, AIR, CAB OFF 29-2131-9-0007 0524 ON 29-2131-9-0007 9763 REMOVED AND REPLACED AFT OUTFLOW ASSEMBLY REF AMM 21-31-03-000/400-801. OUTFLOW VALVE ASSEMBLY FAILED PRESSURIZATION GROUND TEST REF AMM 21-31-00-700-802.SUSPECT OUTFLOW VALVE ASSEMBLY BAD FROM STOCK STILL REQUIRES REPLACEMENT.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 79,088 hrs · 28,709 cycles

BULLNOSE EMERGENCY LIGHTS AT 29ABC AND 26ABC INOP. RE-LAMPED LIGHT AT 26ABC REF MM 33-51-03. OPS CK OK. FOUND CONNECTOR D11338 LOCKING FEATURE BROKEN FOR LIGHT AT 29ABC. REMOVED AND REPLACED CONNECTOR REF SWPM 20-61-28 AND WDM 33-51-14-10. LIGHT OPS CK OK.

Part: BATTERY PACK — FAILED (M01672) · airframe 77,049 hrs · 27,779 cycles

EMERGENCY LIGHT BATTERY PACK CHECK FAILED AT MULTIPLE LOCATIONS REF TO PEMCO NR 14390.0028 (S/N182999) REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT MULTIPLE LOCATIONS IAW B737 AMM 33-51-06. OPS TEST GOOD. (S/N182999) WORK PERFORMED BY V922334, ENTERED BY V927860

Part: BATTERY PACK — FAILED (M01668) · airframe 77,049 hrs · 27,779 cycles

EMERGENCY LIGHT BATTERY PACK CHECK FAILED AT MULTIPLE LOCATIONS REF TO PEMCO NR 14390.0028 (S/N206127) REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT MULTIPLE LOCATION IAW B737 AMM 33-51-06. OPS CHECK GOOD. (S/N 206127)

Part: BATTERY PACK — FAILED (M01670) · airframe 77,049 hrs · 27,779 cycles

EMERGENCY LIGHT BATTERY PACK CHECK FAILED AT MULTIPLE LOCATIONS REF TO PEMCO NR 14390.0028 (S/N269312) REMOVED AND REPALCED EMERGENCY LIGHT BATTERY PACKS AT MULTIPLE LOCATIONS IAW B737 AMM 33-51-06 OPC TEST GOOD.

Part: BATTERY PACK — FAILED (M01673) · airframe 77,049 hrs · 27,779 cycles

EMERGENCY LIGHT BATTERY PACK CHECK FAILED AT MULTIPLE LOCATIONS REF TO PEMCO NR 14390.0028 (S/N218109) REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT MULTIPLE LOCATIO NSIAW B737 AMM 33-51-06. OPS CHECK GOOD. (S/N 218109)

Part: BATTERY PACK — FAILED (M01675) · airframe 77,049 hrs · 27,779 cycles

EMERGENCY LIGHT BATTERY PACK CHECK FAILED AT MULTIPLE LOCATIONS REF TO PEMCO NR 14390.0028 (S/N229876) REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT MUTIPLE LOCATIONS IAW B737 AMM 33-51-06. OPS TEST GOOD. (S/N 229876)

Part: BATTERY PACK — FAILED (M01674) · airframe 77,049 hrs · 27,779 cycles

REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT MULTIPLE LOCATIONS IAW AMM 33-51-06. OPS CHECK GOOD. REF TO PEMCO NR 14390.0028 (S/N 249215) REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT MUTIPLE LOCATIONS IAW B737 AMM 33-51-06. OPS TEST GOOD. (S/N 249215).

Part: BATTERY PACK — FAILED (M01669) · airframe 77,049 hrs · 27,779 cycles

EMERGENCY LIGHT BATTERY PACK CHECK FAILED AT MULTIPLE LOCATIONS REF TO PEMCO NR 14390.0028 (S/N260765) REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT MULTIPLE LOCATION IAW B737 AMM 33-51-06 OPS CHECK GOOD.(S/N 260765)

Part: STRINGER — CORRODED (AFT CARGO SEC47) · airframe 77,049 hrs · 27,779 cycles

AFT CARGO SECT 47, FWD OF BS927 STRINGER 21R CORRODED. REF TO PEMCO NR 14390.0595 SUPPLEMENTAL INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AFTER FLIGHT CYCLES AFTER THE THRESHOLD HAS BEEN REACHED. REPAIR PARTS INSTALLATION OF REPAIR, AND REPETITIVE INSPECTION EVERY 2,350 DO NOT EXCEED 5LBS. REMOVED AND REPAIRED DAMAGE SECTION AT AFT CARGO SECTION 47, BETWEEN BS 907 TO BS 927 S-21R PER B737-700 SRM 53-00-03-2R-3. TOMC APPROVED DIP AT AFT CARGO SECTION 47, BETWEEN BS 907 TO BS TOMC-APPROVAL FROM SC1ELBYC COMMENT 927 S-21R PER B737-700 SRM 53-00-03-2R-3. SUPPLEMENTAL INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AFTER INSTALLATION OF REPAIR, AND REPETITIVE INSPECTION EVERY 2,350 FLIGHT CYCLES AFTER THE THRESHOLD HAS BEEN REACHED. REPAIR PARTS DO NOT EXCEED 5LBS. APPROVED RECORDS UPDATE APPROVED INIT: 50000 FC INIT WILL ITO TO RIR RIR: 2350 FC ...VC/U392424

Part: FLOORBEAM — CORRODED (FWD WET AREA) · airframe 77,049 hrs · 27,779 cycles

FWD WET AREA, FLOOR BEAM AT RBL14 AND STA 294.5 HAS CORROSION ON UPPER SURFACE. FWD WET AREA FLOOR BEAM AT RBL 14 STA 294.5, EVALUATED, REMOVED DAMAGE, AND REPLACED IAW B737 SRM 53-10-51-1A-1, 51-40-02-06-730-802, 20-10-01-400-801, 20-10-09-400-801, AND 22-11-92-820-801.

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 77,049 hrs · 27,779 cycles

ELB LP CREATED FOR ESFR REPORTING. PEMCO NR 14390 0615 FOR AFT GALLEY FLOOR BEAM REPLACMENT. ESFR CREATED #1034286.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 77,049 hrs · 27,779 cycles

ELB LP CREATED FOR ESFR REPORTING. PEMCO NR# 14390 0073 FOR REPLACMENT OF FOWARD CARGO DOOR SKIN. EFSR# 1034288

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 77,049 hrs · 27,779 cycles

ELB LP CREATED FOR ESFR REPORTING. PEMCO NR# 14390 0074 FOR REPLACMENT OF AFT CARGO DOOR SKIN. EFSR CREATED. EFSR# 1034287

Part: CHECK VALVE — LEAKING (HYD SYSTEM A) · airframe 75,100 hrs · 26,891 cycles

CAPT ADVISED LOSS OF SYS "A'' HYD QTY. (U147655) LOCKED L/P UNLOCKED FOR UPDATE LOG PAGE LOCKED AFTER MX UPDATE VERBALLY NOTIFIED BY FLIGHT CREW HYD PAGE DISLAYED 20% HYD QTY IN FLIGHT , THEREAFTER HYD SIX PACK FLASHED HEARD NOISE AND VIBRATION , BLOCKED ON THE GATE HYD PAGE DISPLAYED 44% RF . APPEARS EVIDENCE IN WHEEL WELL AREA OF LEAKS . T/S REQUIRED. UNLOCKED FOR SIGNOFF DURING #1 ENG RUNS NOTICED HYD FLUID COMING FROM HYD SYS A MODULAR PACKAGE ASSY HYD PRESSURE SYSTEM CHECK VALVE, REPLACED CHECK VALVE ORING RAN #1 MOTOR OPS CHECKS GOOD REF AMM 29-11-71. PICTURES

Part: NONE — NONE (LAV E) · airframe 74,648 hrs · 26,687 cycles

LAV E CONTINUOSLY FLUSHING IN FLT LAV D DOES NOT FLUSH BOTH REAR LAVS INOP FOUND WATER TO AFT LAV TURNED OFF. OPS CHK LAV NUMEROUS TIMES NO FAULTS FOUND REF AMM

Part: NONE — NONE (L CENTER TANK) · airframe 74,234 hrs · 26,501 cycles

THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/07/22. LEFT CENTER TANK FUEL BOOST PUMP LIGHT COMES ON FOR 10 SEC THEN OFF THEN ON. REPLACED PWR SWITCH RELAY K09902 PERFORMED OPS ON LT CTR PUMP NORMAL UFI START SEQUENCE. RAN PUMP FOR 15 MINUTES MOVED FUEL NORMAL.

Part: CONTROL UNIT — FAULT MESSAGE (NA) · airframe 72,954 hrs · 26,009 cycles

AUTOBRAKE FAIL MSG UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. EVALUATE, CONTACT TOMC. MAC METER INITIATED FOR WITH VENDOR ID V902239 MAC RELATED WORK ORDER 000000003042072 AND PRTR CORREA, LINY (V902239) REMOVED AND REPLACED ANTISKID/AUTOBRAKE CONTROL UNIT REFERENCE AMM 32-42-21-400-801. OPS CHK GOOD. CORREA, LINY (V902239) REMOVED AND REPLACED ANTISKID/AUTOBRAKE CONTROL UNIT REFERENCE AMM 32-42-21-400-801. OPS CHK GOOD. ADD EMP:V902239 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1922544 SN OFF 0110 CONTROL, AUTOBR OFF 29-3242-9-0002 0110 ON 29-3242-9-0002 1058

Part: FSEU — FAILED (NA) · airframe 72,954 hrs · 26,009 cycles

LE FLAPS TRANSIT LIGHT FLASHING INTERMITTENTLY IN FLIGHT WITH FL APS RETRACTED FSEU BITE CONFIRMED MESSAGE 27-81205 SLAT 3 PROX INBD FAULT LAST AND TRAILING EDGES. VERIFIED PROPER OPERATION OF STICK SHAKERS. COLLARED CB ON P 18-2 PANEL " STALL WARNING ASY MODE". APPLIED PLACED ON MEL. DDP COMPLIED WITH. LEG. INTERMITTENT FAULT. VERIFIED PROPER OPERATION OF LEADING REMOVED BULBS FROM INDICATOR LIGHTS ON P2 PANEL AS REQUIRED. PLACARD ON OVERHEAD PANEL AS REQUIRED. ITEM PLACED ON MEL. ADD FAULT: 27-81205 DISPATCH DESK: 31 NAME: SS DATE: 23-APR-22- NOC DESK: 7 NAME: DZ DATE: 23-APR-22- APPROVED ACCOMPLISHED FSEU BITE CHECK AND FOUND MULTIPLE LEGS WITH FAULT CODE 27-53280, REF. FIM 27-51 TASK 823 AND REF. AMM 27-51-01 REMOVED AND REPLACED FSEU. OPS CHECK GOOD. ADD EMP:U142517 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1810111 SN OFF 1793 UNIT, FLAP & SL OFF 29-2751-9-0024 1793 ON 29-2751-9-0049 5431

Part: NONE — CRACKED (R1 WINDOW) · airframe 72,698 hrs · 25,911 cycles

R1 WINDOW FRAME HAS 3/4" LONG CRACK IN UPPER RH CORNER. ACCOMPLISHED AVO 9601 STEPS B PER NDT PART 6 51-00-00 PROCEDURE 23, CRACK IS CONDITION 1 PER AVO. ACP. RII INSPECTION IAW GMM 09-25-05 & AVO9605 PART1 B1A FIG. ACCOMPLISHED RII INSPECTION, VERFIED FASTENER INSTALLATION OF #2 ACCOMPLISHED RII INSPECTION, VERFIED FASTENER INSTALLATION OF RH 13.4 STEP 2. VERIFIED CRES SHIM HAS NOT BEEN CUT THROUGH AT ANY WINDOW AND ENSURED SLIDEING WINDOW CLEARED PER AVO 09605 PAR C #2 WINDOW AND ENSURED SLIDEING WINDOW CLEARED PER AVO 09605 PAR LOCATION. NO DEFECTS NOTED. PART 1. ALSO VERIFIED KIT P/N PER AVO 09605 PAR D PART 1. C PART 1 AND 2 . ALSO VERIFIED KIT P/N PER AVO 09605 PAR D PART 1. ACP. RII INSPECTION IAW GMM 09-25-05. INCORRECT AVO REFERENCED IN ABOVE STATEMENT. SHOULD READ AVO9605. REMOVED RIGHT SIDE FASTENERS AND SEPARATED RIGHT SIDE 1AND 2 CUT THE RIGHT SIDE NUMBER 1 WINDOW FRAME PER AVO 9604 PART 1 PAR REMOVED RIGHT SIDE FASTENERS AND SEPARATED RIGHT SIDE 1AND 2 CUT THE RIGHT SIDE NUMBER 1 WINDOW FRAME PER AVO 9605 PART 1 PAR VERIFY R/H REPAIR KIT AS P/N 002A0003-234 WCJO 0057128 PER AVO RE-INSTALLED RH SIDE FASTENERS REMOVED IN STEP A.1. CHECKED RE-INSTALLED RH SIDE FASTENERS REMOVED IN STEP A.1. CHECKED WINDOW FRAMES PER AVO9604 PART 1 INTERIM REPAIR PAR A PART 1 AND B STEP 1A. WINDOW FRAMES PER AVO9605 PART 1 INTERIM REPAIR PAR A PART 1 AND B STEP 1A. 09605 PAR D. NUMBER 2 WINDOW AND ENSURED WINDOW CLEARED ALL FASTENERS. PER NUMBER 2 WINDOW AND ENSURED WINDOW CLEAR

Part: NONE — CRACKED (L1 WINDOW) · airframe 72,698 hrs · 25,911 cycles

L1 WINDOW FRAME HAS 3/4" LONG CRACK IN UPPER LH CORNER. ACCOMPLISHED AVO 9601 STEPS B PER NDT PART 6 51-00-00 PROCEDURE 23, CRACK IS CONDITION 1 PER AVO. ACP. RII INSPECTION IAW GMM 09-25-05 & AVO9604, PART 1B 1, FIG. 12.4 STEP 2. VERIFIED CRES SHIM HAS NOT BEEN CUT THROUGH AT ANY LOCATION. NO DEFECTS NOTED. REMOVED LEFT SIDE FASTENERS AND SEPARATED LEFT SIDE 1AND 2 CUT THE LEFT SIDE NUMBER 1 WINDOW FRAME PER AVO 9604 PART 1 PAR RE-INSTALLED LH SIDE FASTENERS REMOVED IN STEP A.1. CHECKED WINDOW FRAMES PER AVO9604 PART 1 INTERIM REPAIR PAR A PART 1 AND B STEP 1A. NUMBER 2 WINDOW AND ENSURED WINDOW CLEARED ALL FASTENERS. PER 2. AVO 9604 PAR C PART 1 AND 2. ACP RII INSPECTION IAW GMM 09-25-05 & AVO 9604 ORG. PART 1 D. VERIFIED CORRECT KIT, P/N 002A0003-223. NO DEFECTS NOTED. VERIFY REPAIR KIT P/N 002A0003-233 PER AVO 9604 PAR D. PAGE 4. WC JO 0057128 INSTALLED REPAIR WASHERS AT 25 LOCATIONS PER AVO 9604 FIG 21.04 DRILLED UP REPAIR DOULBER AND TRIPLER, OK TO INSTALL PER AVO 9604 PAR D. OK TO INSTALL REPAIR PIECES PER AVO9604 PAR. D VERIFIED GAP CREATED BY THE CUT IN THE OUTER FLANGE OF THE #1 WINDOW FRAME FILLED WITVERIFIED GAP CREATED BY THE CUT AVO9604 PG 2 D REPAIR INSTALLATI WINDOW FRAME FILLED WIT E. AVO9604 PG 2 D REPAIR INSTALLATI FILLED GAP CREATED BY THE CUT IN THE OUTER FLANGE OF THE 1# WINDOW FRAME WITH EC-3587B PER FIG 24 REF AVO9604 PG 2 D REPAIR INSTALLATION , ST3# ACP. RII INSPECTION IAW GMM 09-25-05 & AVO9604 PART

Part: PROCESSOR — FAULTED (FUEL QTY) · airframe 70,582 hrs · 25,031 cycles

FUEL QUANTITY INDICATION, FLIGHT COMPARTMENT ERROR OR BLANK CENT ER TANK UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V898293 MAC RELATED WORK ORDER 000000003012045 AND PRTR GILHARRY, ABRAHAM (V898293) APPROVED, DDP''S C/W GILHARRY, ABRAHAM (V898293) APPROVED, DDP''S C/W DISPATCH DESK: 80 NAME: MS DATE: 18-JUN-21- NOC DESK: 7 NAME: DZ DATE: 18-JUN-21- DEFERRED DIRECTLY BY TOMC REMOVED AND REPLACED FQPU REF AMM 28-41-81 OPS CHECK GOOD. PLACARDS REMOVED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1027339 SN OFF 8045 PROCESSOR, FUEL OFF 29-2841-9-0003 8045 ON 29-2841-9-0003 2787

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA540 LBL40.87 IS CRACKED. B737-57-4-1262 - LP - 5867975 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW UNIT ED ECRA 5714-01203 REV ORIGINAL AND B737-700 SRM 51-40-02. SSFR REPORT, FOR 46-0024,ENTEREDBY UAL INSPECTION U354653, DATE 3/11/ 2021. ALL INSP REQ C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. B737-57-4-1262 - LP - 5868043 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW UNIT ED ECRA 5714-01203 REV ORIGINAL AND B737-700 SRM 51-40-02 SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651 3/11/2021 ALL INSP REQ, C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING STA540 RBL54.60 IS CRACKED. B737-57-4-1262 - LP - 5867971 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW UNIT ED ECRA 5714-01203 REV ORIGINAL AND B737-700 SRM 51-40-02 SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651 3/11/2021

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA540 RBL6.14 IS CRACKED. B737-57-4-1262 - L P - 5867976 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW UNITE D ECRA 5714-01203 REV ORIGINAL AND B737-700 SRM 51-40-02. SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, DATE 3/1 1/2021. ALL INSP REQ C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA540 LBL15.04 IS CRACKED. B737-57-4-1262 -L P- 5867973 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW UNIT ED ECRA 5714-01203 REV ORIGINAL AND B737-700 SRM 51-40-02, SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653, DATE 3 /11/2021 ALL INSP REQ C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA540 RBL32.40 IS CRACKED. B737-57-4-1262 - LP - 5868041 REMOVED AND REPLACED SHEAR FITTING IAW UNITED ECRA 5714-01203 RE V ORIGINAL AND B737-700 SRM 51-40-02 AT STA 540 RBL 32.40 SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653 3/11/2021 ALL INSP REQ. C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. B737-57-4-1262 - LP - 5867974 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 AND SUPP ORT BRACKET IAW UNITED ECRA 5714-01202 REV ORIGINAL. SSFR REPORT , FORM 46-0024, ENTERED BY UAL INSPECTION U354653, DATE 3/11/202 1 ALL INSP REQ C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT SPA540 RBL15.04 IS CRACKED. B737-57-4-1262 - LP - 5868040 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW UNIT ED ECRA 5714-01203 REV ORGINAL AND B737-700 SRM 51-40-02 SSFR RE PORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651 3/11/2021 ALL INSP REQ. C/W

Part: FITTING — CRACKED (BS 540) · airframe 69,907 hrs · 24,796 cycles

SHEAR FITTING AT STA540 LBL6.14 IS CRACKED. B737-57-4-1262 - L P 5867972 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW UNITE D ECRA 5714-01203 REV ORIGINAL AND B737-700 SRM 51-40-02. SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653, DATE 3/1 1/2021 ALL INSP REQ C/W

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 67,471 hrs · 23,801 cycles

ESCAPE SLIDE CABLE AT DOOR 1R NOT ATTACHED FOUND SAFETY TREAD BROKEN. REMOVED AND REPLACED DOOR 1R SLIDE PACK. REF AMM 25-66-01-400-801 AND REDENDER SAFE CK LIST ACP RII INSPECTION OF #1R SLIDE ASSY. INSTALLATION, REF. GMM 09- 25-05. TRACKING # 1296321 SN OFF 0344 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1296321 SN OFF 0344 IPC REFERENCE # IPC 25-66-00-02.

Part: CONTROL MODULE — MALFUNCTIONED (COCKPIT) · airframe 67,095 hrs · 23,666 cycles

PRESSURIZATION PANEL WENT COMPLETELY BLANK APPROX 12000 REMOVED AND REPLACED CABIN PRESSURE CONTROL MODULE REF AMM 21-31-02. ALL TESTS PASSED. NO FAULTS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1165252 SN OFF 7041 PANEL, PRESS, C OFF 29-2131-9-0006 7041 ON 29-2131-9-0006 0136.

Part: CAP — MISSING (CABIN) · airframe 63,033 hrs · 21,969 cycles

END CAP FOR EMERGENCY EXIT LIGHT ABOVE 21C NEEDS TO BE REINSTALLED T ASSY AND OPS CK OK TO CONTINUE. REMOVED AND REPLACED ROW 21C WITH NEW EMERGENCY RED LIGHT.

Part: UNKNOWN — MALFUNCTIONED (THRUST REVERSER) · airframe 62,759 hrs · 21,869 cycles

REVERSE THRUST LEVER HAS LOST MOTION, NO THRUST REVERSER OPERATION ENGINE 2 RT ENG WOULD NOT GO INTO REV REVERSER LIGHT ON CANNOT DUPLICATE FAULT, OPS CHECK NORMAL. OK TO CONTINUE.

Part: FRAME — CORRODED (BS 303) · airframe 62,493 hrs · 21,762 cycles

FRAME AT STA 303.9 AFT FLANGE 2IN UP FROM FLOOR LEVEL HAS CORROSION ACCOMPLISHED INTERIM REPAIR AT FRAME STA 303.9 AFT FLANGE INNER CORD IAW UNITED ECRA 5310-07308 PART 1 INITIATE A DIP TO ACCOMPLISH INSPECTION PER PART 2 OF ECRA 5310- 07308 ON OR BEFORE THE AIRCRAFT REACHES 75,000 TOTAL AIRCRAFT CYCLCES. PLANNING TO CONTACT ENGINEERING AFT 72,000 BUT BEFORE 73, 000 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE INSPECTION REQUIRMENTS.

Part: BULKHEAD — CRACKED (BS 663) · airframe 62,493 hrs · 21,762 cycles

CRACK INDICATION OBTAINED FROM HFEC INSP ON CENTER WING BOX REAR SPAR VERTICAL PRESSURE DECK BETWEEN RBL40 RBL 45.64 LOCATED BETWEEN WL200.6 WL 192 PAR BETWEEN RBL 40-RBL45-64. BETWEEN WL 200.6-WL 192. REF B737-7 SRM 57-10-10 FIG 204. REPAIRED CRACKED VERICAL PRESSURE DECK ON CENTER WING BOX REAR S DIP TO REQUIRE INSPECTION AT 56000 F/C AFTER REPAIR INSTALLATION PER PARA 6 TABLE 204 TOMC APPROVED INSPECTION REQUIREMENTS PER SRM 57-10-10 REPAIR 3 PARBETWEEN RBL 40-RBL45-64. BETWEEN WL 200.6-WL 192. REF B737-7 SRM 57-10-10 FIG 204. THIS IS A CATEGORY B REPAIR AND REQUIRES I NSPECTION AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION PER PARA 6 TABLE 204

Part: FLOORBEAM — CORRODED (BS 986) · airframe 62,493 hrs · 21,762 cycles

AFT CABIN FLOORBEAM HAS CORROSION ON UPPER FLANGE BS 986.5, RBL 17 - 44. ACCOMPLISHED A REPAIR IAW ECRA 5321-01429.

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 61,239 hrs · 21,249 cycles

EMERGENCY EXIT SIGN COVERS IN THE MID CABIN BOTH CAME OFF. SECURED THE SIGN COVERS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,379 hrs · 20,879 cycles

EMERGENCY LIGHTS AT ROWS 22L THRU 28L INOP. REMOVED AND REPLACED BATTERY PACK AT SEAT 26ABC. REF AMM 33-51-06-960-805 C/W IDT REQUIREMENTS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,913 hrs · 20,312 cycles

AFT GALLEY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,607 hrs · 20,186 cycles

AFT GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT, OPS CHECKED OK

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,900 hrs · 18,645 cycles

INBOARD AFT SEAT TRACK FLANGE HOLE AT 45.5 RBL, JUST FWD OF FLOORBEAM AT STATION 727B HAS A CRACK INDICATION WHEN HFEC HOLE INSP IS PERFORMED IAW EA 5320-02076 REV F OP 4 STEP 6.4, ONE OF 4 HOLES INSP AD 2013-23-04. REPAIRED CRACK TRACK IAW ECRA 5320-02475. SEE ALL TASK & WIPS FOR WC.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,900 hrs · 18,645 cycles

OUTBOARD AFT SEAT TRACK FLANGE HOLE AT LBL 45.50 JUST FWD OF FLOORBEAM AT STATION 727B HAS A CRACK INDICATION, WHEN HFEC HOLE INSPECTION IS PERFORMED. REFER TO EA 5320-02076 REV F OP 3 STEP 3.6. ONE OF 4 HOLES INSPECTED AD 2013-23-04 REPAIRED CRACK ON SEAT TRACK 45.50 LBL AT STATION 727B IAW ECRA 5320-02475. SEE ALL TASK & WIP FOR WC.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,900 hrs · 18,645 cycles

OUTBOARD AFT SEAT TRACK FLANGE HOLE AT 45.5 RBL, JUST FWD OF FLOORBEAM AT STATION 727B HAS A CRACK INDICATION WHEN HFEC HOLE INSP IS PERFORMED IAW EA 5320-02076 REV F OP 4 STEP 3.6 & 6.4, ONE OF FOUR HOLE INSPECTED ON STEP AD 2013-23-04. REPAIRED CRACK ON SEAT TRACK IAW ECRA 5320-02475. SEE ALL TASK & WIPS FOR WC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,900 hrs · 18,645 cycles

WHILE PERFORMING HFEC HOLE INSPECTION FOR EA 5310-05878 OP 2 STEP 6 & 7 FOUND CRACK INDICATION IN SKIN LOCATED AT STATION 540 BETWEEN STRINGER 22L & 23L, AFT HOLE SECOND ONE DOWN FROM TOP. FUSELAGE SKIN AT STATION 540 BETWEEN STRINGER 22L & 23L HAS BEEN REPAIRED IAW EA 5310-05878 REV A OP 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,900 hrs · 18,645 cycles

DAMAGE FOUND AT STATION 787, STRINGER 26 IS OUT OF LIMITS IAW SRM 53-00-01 FIG G PG 115, W=2" Y=.082 = 24.39 MIN IS 30 INTERIM REPAIR PERFORMED AT STATION 787 - 807 FUSELAGE SKIN BETWEEN STRINGER 26R & 27L IAW ECRA 5331-02032 PART 1 53-DIP ISSUED. INSPECTION THRESHOLD ON OR BEFORE 50,000 TOTAL FC PLANNING TO CONTACT ENGINEERING AFTER 43,000 TOTAL FC BUT BEFORE 44,000 TOTAL FC FOR INSPECTION REQUIREMENTS.

Part: RIB — DAMAGED (LT HORIZ STAB) · airframe 54,900 hrs · 18,645 cycles

NEED TO MAKE A CUT TO LT HORIZONTAL STAB, LOWER SURFACE TO FACILITATE REPAIR ON RIB & WEB AT LT STAB 111.10 STIFFENER. SRM 55-10-01 REPAIR 11 INSPECT REPAIR TABLE 204. DETAIL VISUAL & LFEC, INITIAL THRESHOLD 56,000 FLIGHT CYCLES THEN REPEAT EVERY 9,000 FLIGHT CYCLES.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,900 hrs · 18,645 cycles

CRACK FOUND ON BULKHEAD CHORD BETWEEN STRINGER 22R & 23R, AFT ROW SECOND FASTENER DOWN. TYPICAL REPAIR PERFORMED IAW EA 5310-05878 REV A. OPERATIONS 5 TO FUSELAGE SKIN AT STATION 540 BETWEEN STRINGER 22R & 23R.

Part: SPAR — DAMAGED (LT HORIZ STAB) · airframe 54,900 hrs · 18,645 cycles

NEED TO MAKE A CUT TO LT HORIZONTAL STAB LOWER SURFACE TO FACILITATE REPAIR ON RIB & WEB AT LT STAB 111.10, STIFFENER 3 & WEB. IAW NR 9738049 SRM 55-10-01 REPAIR 11, INSPECT REPAIR TABLE 204. DETAIL VISUAL & LFEC, INITIAL THRESHOLD 56,000 FLIGHT CYCLES THEN REPEAT EVERY 9,000 FLIGHT CYCLES.

Part: SPAR — CRACKED (CENTER WING) · airframe 49,673 hrs · 16,643 cycles

CENTER WING BOX REAR SPAR WEB AT STATION 663 ON LT SIDE FOUND 11/2 INCH CRACK AT LBL 41 & AMP; WL 194 & 11/2 INCH CRACK AT LBL 43 & AMP; WL 197. REPAIR CARRIED OUT IAW SRM 57-1010,REPAIR 3, ALTERNATE 2, PAGE 20 4 THRU PAGE 210.

Part: BULKHEAD WEB — CRACKED (BS 663)

DURING INSPECTION OF VERTICAL PRESSURE WEB AT BS 663, FOUND TWO CRACKS 1.5 INCHES LONG AT LBL 41, WL 194 AND 1.5 INCHES LONG AT LBL 43, WL 197. REPAIRED VERTICAL PRESSURE WEB IAW SRM 57-10-10. REPAIR NR 3, ALTERNATE NR 2.

Part: FRAME — CRACKED (BS 727D) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE IN FRAME BS 727D BETWEEN STRINGER 8 AND 9R. REPAIRED FRAME AND REINSTALLED BRACKET IAW EA 5310-04716, REV D.

Part: FRAME — CRACKED (STA 727A) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE IN FRAME BS 727A RT BETWEEN STRINGER 8 AND 9. REPAIRED FRAME AND REINSTALLED BRACKET IAW EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 747) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE IN FRAME STATION 747, BETWEEN STRINGER 8 AND 9R. INSTALLED FRAME REPAIR IAW EA 5310-04716, FIG 3, REV D.

Part: FRAME — CRACKED (BS 747) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE IN FRAME BS 747. FRAME REPAIRED IAW EA 5310-04716, REV D, OP 1.

Part: FRAME — CRACKED (BS 520) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE IN FRAME BS 520 BETWEEN STRINGERS 8 AND 9R. REPAIRED IAW EA 5310-04716, REV D, OP 1.

Part: FRAME — CRACKED (BS 500A) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT RIVET HOLE, FRAME BS 500A BETWEEN STRINGERS 8 AND 9R. INSTALLED REPAIR DOUBLERS ON FRAME IAW EA 5310-047 16, REV D OP 1.

Part: FRAME — CRACKED (BS 500A) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE ON FRAME, BS 500C BETWEEN STR 8 AND 9R. FRAME REPAIRED IAW EA 5310-04716 OP 1, REV D.

Part: FRAME — CRACKED (BS 727A) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE ON FRAME BS 727A BETWEEN STR 8 AND 9L. FRAME REPAIRED IAW EA 5310-04716, REV D, OP 1.

Part: FRAME — CRACKED (BS 440) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE, IN FRAME BS 440. REPAIRED IAW EA 5310-04716, REV D, OP 1.

Part: FRAME — CRACKED (BS 400) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE OF FRAME, BS 400. REPAIRED FRAME IAW 5310-04716.

Part: FRAME — CRACKED (BS 400) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE FRAME BS 400 BETWEEN STRINGER 8 AND 9R. REPAIRED IAW EA 5310-04716, REV D, OP 1.

Part: FRAME — CRACKED (BS 380) · airframe 47,437 hrs · 15,837 cycles

CRACK INDICATION AT INBD RIVET HOLE FRAME BS 380 REPAIRED IAW EA 5310-04716, REV D, OP 1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,908 hrs · 12,849 cycles

SUPPORT TASK; FWD O/H RIGHT BATTERY PACK FOR EMERGENCY LIGHTS INOP. REMOVED & REPLACED BATTERY PACK AT M01674 POWER SUPPLY AND OPS CHECKED GOOD IAW B737-700AMM 33-51-09-960-806.

Part: RIB — CORRODED (HORIZ STAB) · airframe 32,515 hrs · 10,546 cycles

RIGHT-HAND HORIZONTAL STABILIZER OUTBOARD CLOSURE RIB HAS SURFACE CORROSION AT SCREW HOLES - 3 EA AT UPPER SURFACE AND 2 EA AT LOWER SURFACE AREA. BLENDED OUT ALL CORROSION, PERFORMED HFEC OF BLENDED AREAS AND REFINISHED PER ECRA 5510-01933 MIN REMAINING THICKNESS IS .060 INCH.

Part: BUSHING — CORRODED (RT MLG) · airframe 32,515 hrs · 10,546 cycles

RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD LOWER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,515 hrs · 10,546 cycles

STATION 986.5 FLOORBEAM UPPER CHORD HAS CORROSION AT LBL 38. REPAIRED PER EC/RA 5321-01330.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,515 hrs · 10,546 cycles

STATION 986.5 FLOORBEAM UPPER CHORD HAS CORROSION AT LBL 44. REPAIRED PER EC/RA 5321-01330 REVISION A.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,515 hrs · 10,546 cycles

STATION 986.5 FLOORBEAM HAS CORROSION ON UPPER CHORD RBL 23 FWD FLANGE AT PREVIOUS REPAIR. REMOVED AND REPLACED REPAIR FILLER PER SRM 53-00-51 REPAIR 1.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,515 hrs · 10,546 cycles

STATION 986.5 FLOORBEAM UPPER CHORD AFT FLANGE HAS CORROSION LBL 26. REPAIRED PER EC/RA 5321-01330 REVISION A.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 32,515 hrs · 10,546 cycles

STATION 986.5 FLOORBEAM UPPER CHORD FORWARD FLANGE LBL 26 CORROSION ON PREVIOUS REPAIR. REMOVED AND REPLACED REPAIR FILLER PER SRM 53-00-51 REPAIR 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

MAIN DECK FLOOR SUPPORT AT STATION 540 RBL 2 IS CRACKED. REMOVED AND REPLACED MAIN DECK FLOOR SUPPORT AT STATION 540 RBL 2 PER EC/RA 5321-01551.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

FRAME CRACKED AT STATION 380 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 380 S8R AND S9R PER EC/RA 5310-04777.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

FRAME CRACKED AT STATION 827 BETWEEN S8R AND S9R. REPAIRED FRAME STATION 827 S8R AND S9R PER EC/RA 5310-04777.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

FRAME CRACKED AT STATION 867 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 867 BETWEEN S8R AND S9R PER EC/RA 5310-04777.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

FRAME CRACKED AT STATION 440 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 440 S8R AND S9R PER EC/RA 5310-04777.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

FRAME CRACKED AT STATION 727D BETWEEN S8L AND S9L. REPAIRED FRAME AT STATION 727D BETWEEN S8L AND S9L PER EC/RA 5310-04777.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

MAIN DECK FLOOR SUPPORT AT STATION 540 LBL 2 IS CRACKED. REMOVED AND REPLACED MAIN DECK FLOOR SUPPORT AT STATION 540 LBL 2 PER EC/RA 5321-01551.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,515 hrs · 10,546 cycles

FRAME CRACKED AT STATION 480 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 480 S8R AND S9R PER EC/RA 5310-04777.

Part: BUSHING — CORRODED (RT MLG) · airframe 32,515 hrs · 10,546 cycles

RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD UPPER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D.

Part: BUSHING — CORRODED (LT MLG) · airframe 32,515 hrs · 10,546 cycles

LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD LOWER BUSHING FACE) HAS CORROSION. REWORKED OUTBOARD LOWER BUSHING FACE PER ECRA 5741-01106.

Part: BUSHING — CORRODED (LT MLG) · airframe 32,515 hrs · 10,546 cycles

LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD UPPER BUSHING FACE) HAS CORROSION. REWORKED OUTBOARD UPPER BUSHING FACE PER ECRA 5741-01106.

Part: BUSHING — CORRODED (LT MLG) · airframe 32,515 hrs · 10,546 cycles

LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD UPPER BUSHING FACE) HAS CORROSION. REWORKED INBOARD UPPER BUSHING FACE PER ECRA 5741-01106.

Part: BUSHING — CORRODED (LT MLG) · airframe 32,515 hrs · 10,546 cycles

LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD LOWER BUSHING FACE) HAS CORROSION. REWORKED INBOARD LOWER BUSHING FACE PER ECRA 5741-01106.

Part: BUSHING — CORRODED (RT MLG) · airframe 32,515 hrs · 10,546 cycles

RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD LOWER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D.

Part: BUSHING — CORRODED (RT MLG) · airframe 32,515 hrs · 10,546 cycles

RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD UPPER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,409 hrs · 8,243 cycles

INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 986.5, LBL 64 TO RBL 64. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.