N7841A

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,788 hrs · 32,823 cycles

L/H OVERWING EXIT FWD EMERGENCY LIGHT INOP<[01] R&R EMERGENCY EXIT LIGHT PER AMM 33-21-00

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 58,709 hrs · 32,135 cycles

SEVERAL EMER LIGHTS INOP IN CABIN<[01] INSTALLED AFT GALLEY R/H EMERGENCY BATT. PACK AND POWER SUPPLY. IAW AMM 33-51-06. OPS CK GOOD.

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,674 hrs · 31,469 cycles

EMERGENCY EXIT SIGN ABOVE R1 DOOR DOES NOT ILLUMINATE<[01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND CHARGER ASSY. IAW AMM 33-51-06. NO FIX. SWAPPED LIGHT ASSYS. WITH KNOWN GOOD ASSEMBLIES IAW AMM 33-51-02. NO FIX. LIGHT ASSYS. SWAPPED TO ORIGINAL.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,674 hrs · 31,469 cycles

EMERGENCY EXIT SIGN ABOVE R1 DOOR DOES NOT ILLUMINATE<[01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND CHARGER ASSY. IAW AMM 33-51-06. NO FIX. SWAPPED LIGHT ASSYS. WITH KNOWN GOOD ASSEMBLIES IAW AMM 33-51-02. NO FIX. LIGHT ASSYS. SWAPPED TO ORIGINAL.

Part: FUSE — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,674 hrs · 31,469 cycles

EMERGENCY EXIT SIGN ABOVE R1 DOOR DOES NOT ILLUMINATE<[01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND CHARGER ASSY. IAW AMM 33-51-06. NO FIX. SWAPPED LIGHT ASSYS. WITH KNOWN GOOD ASSEMBLIES IAW AMM 33-51-02. NO FIX. LIGHT ASSYS. SWAPPED TO ORIGINAL. REPLACED CONNECTOR D40042P PER SWPM. EMERGENCY LIGHT OPS CHECK GOOD PER AMM 33-51-00

Part: STRIP — LOOSE (ZN 200 FUS TOP) · airframe 57,535 hrs · 31,381 cycles

ROW 9 FLOOR LIGHTING LOOSE.<[01] RESECURED STRIP PER M/M 33-51-15.

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 57,398 hrs · 31,296 cycles

CAPT SIDE AFT GIRT BAR LOOSE<[01] SECURED THE GIRT BAR IAW AMM 25-66-01

Part: SLIDER — OUT OF ADJUST (STAB) · airframe 56,887 hrs · 30,955 cycles

RIGHT LOWER AFT STAB SLIDER SEAL TRAILING EDGE NOT ENGAGED CORRECTLY<[01] REMOVED AND PROPERLY INSTALLED SLIDER SEAL PER AMM 55-30-00

Part: SLIDER — OUT OF ADJUST (STAB) · airframe 56,887 hrs · 30,955 cycles

LEFT LOWER AFT STAB SLIDER SEAL TRAILING EDGE NOT ENGAGED CORRECTLY<[01] REMOVED AND PROPERLY REISTALLED SLIDER SEAL PER AMM 55-30-00

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,177 hrs · 30,494 cycles

L2 DOOR ESCAPE SLIDE FELL OUT OF CONTAINER / [01] REPACKED L2 DOOR ESCAPE SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE.

Part: NONE — BROKEN (PAX CABIN) · airframe 55,886 hrs · 30,285 cycles

FWD EMERGENCY LIGHT BROKEN / [01] REMOVED AND REPLACED EXIT SIGN LENS PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 55,811 hrs · 30,240 cycles

EMERGENCY LIGHT AT THE OUTSIDE OF AFT SERVICE DOOR IS INOP / [01] RELAMPED REF AMM 33-51-04

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 55,078 hrs · 29,733 cycles

INOP EMERGENCY EXIT LIGHT RH SIDE AT PASSENGER CABIN (1 EA) 2022-239744 / [01] REPLACED EMERGENCY EXIT LIGHT RH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-01-960-801.PERFORMED OPERATIONAL TEST ..TEST IS OK .;[02] REPLACED EMERGENCY EXIT LIGHT RH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-01-960-801.PERFORMED OPERATIONAL TEST ..TEST IS OK .

Part: BATTERY PACK — INOPERATIVE · airframe 55,078 hrs · 29,733 cycles

INOP BATTERY PACK (M1674) AT FWD PASSENGER CABIN 2022-239729 / [01] REPLACED BATTERY PACK (M1674) AT FWD PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK;[02] REPLACED BATTERY PACK (M1674) AT FWD PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 55,078 hrs · 29,733 cycles

CRACK DORSAL FIN FRONT SPAR CROSSBEAM BRACKET AT STA 1016 INTERNAL CAVITY AT VERTICAL STAB 2022-239726 / [01] REPLACED DORSAL FIN FRONT SPAR CROSSBEAM BRACKET AT STA 1016 INTERNAL CAVITY AT VERTICAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 176A3001 SHEET 17 REV-.SEE INDIVIDUAL STEP SIGNOFF BELOW;[02] CERTIFIED STEP 1; COMPLETED. RII

Part: SKIN — BROKEN · airframe 55,078 hrs · 29,733 cycles

BROKEN EXTERNAL SKIN NUT PLATES BS 663 TO BS 706 BTW STR 1 TO STR 2R AT UPPER FUSELAGE ( (REFERENCE SRM 53-40-01-2R-1) 2022-239678 REPAIR SKIN LOC ON AREA ADF N.1 ANTENNA BS 663 TO BS 706 BTW STR 1 TO STR 2R AT UPPER FUSELAGE IAW B737-700 SRM SRM 53-40-01-2R-1 REPAIR 1 PARAGRAPH 4 F. MATERIAL USED: 2024-T3; 0.40 INCH. P/O: 2022-102468. PERFORMED BONDING TEST IAW SWPM 20-20-00. AND TEST IS OK. REPAIR SKIN LOC ON AREA ADF N.1 ANTENNA BS 663 TO BS 706 BTW STR 1 TO STR 2R AT UPPER FUSELAGE IAW B737-700 SRM SRM 53-40-01-2R-1 REPAIR 1 PARAGRAPH 4 F. MATERIAL USED: 2024-T3; 0.40 INCH. P/O: 2022-102468.

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CORROSION ON SHIELD LOCATED ON FWD CARGO COMPARTMENT BTW BS 492 TO BS 500A AND AT LEVEL OF RBL 21.8 2022-239648 / [01] REPLACED SHIELD AND FASTENERS LOCATED ON FWD CARGO COMPARTMENT BTW BS 492 TO BS 500A AND AT LEVEL OF RBL 21.8 I.A.W B737-700 SRM 51-40-02 AND DWG 143A0080; SHEET 15; REV -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] COMPLETE TASK CERTIFIED RII

Part: STIFFENER — CRACKED · airframe 55,078 hrs · 29,733 cycles

CRACK ON STIFFENER LOCATED ON FWD FACE OF VAPOR BARRIER LH BS663 BTW LBL 5.00 TO LBL 32 2022-239636 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N:A16165044; DUE DATE: 01/FEB/23.;[02] REPLACED NEW STIFFENER AND FASTENERS LOCATED ON FWD FACE OF VAPOR BARRIER LH BS663 BTW LBL 5.00 TO LBL 32 I.A.W B737-700 SRM 51-40-02 AND DWG 111A1000; SHEET 114; REV -. SEE INDIVIDUAL SIGN-OFF BELOW;[03] CERTIFIED STEP 2; COMPLETED. ITEM RII

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CORROSION ON SHIELD WEB LOCATED BTW BS767 TO BS 787 AT LEVEL STR 25R RBL 21.84 WL 156.1 AFT CARGO COMPARTMENT 2022-239585 / [01] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS767 TO BS 787 AT LEVEL STR 25R RBL 21.84 WL 156.1 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 SHEET 13 REV. A. PART NUMBER USED: 146A8127U1ATSMRO P.O:2022-149139.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS767 TO BS 787 AT LEVEL STR 25R RBL 21.84 WL 156.1 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 SHEET 13 REV. A. PART NUMBER USED: 146A8127U1ATSMRO P.O:2022-149139. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW RII COMPLETED

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CRACK ANGLE - SUPPORT LOCATED BULKHEAD BS 727 AT AFT CARGO COMPARTMENT 2022-239590 / [01] REPLACED ANGLE - SUPPORT LOCATED BULKHEAD BS 727 AT AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A2600 SHEET 236 REV-;[02] REPLACED ANGLE - SUPPORT LOCATED BULKHEAD BS 727 AT AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A2600 SHEET 236 REV-

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727D TO BS 767 WL 156.1 RBL 21.84 AT AFT CARGO COMPARTMENT 2022-239589 / [01] REPLACED NEW SUPPORT ZEE LOCATED LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AT AFT CARGO COMPARTMENT IAW B737-700 DRAWING 146A7500 REV: - <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED STEP 1; COMPLETED. ITEM RII

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CRACK STRINGER 23L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2022 - 239551 / PERFORMED PERMANENT REPAIR ON STRINGER 23L LOCATED BS 500D T0 BS 540 AT FWD CARGO COMPARTMENT;IAW SRM B737-700 SRM 53-00-03-2R-1 REPAIR 1 ;THIS REPAIR IS CAT A NOT FURTHER ACTION OR INSPECTION ARE REQUIRED. MATERIAL USED 7075-T0 0.040? CHANNEL AND ANGLES PO: 2021 189587.AND 7075-T0 0.036? SECTION STRINGER PO: 2021131796. CONVERTED FROM 7075T0 TO 7075T6.

Part: ANGLE — CRACKED (LH WING) · airframe 55,078 hrs · 29,733 cycles

CRACK ANGLE TRAILING EDGE LOCATED WS253.00 LT WING 2022-239498 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS253.00 LT WING IAW SRM B737-700 51-40-02;[02] REPLACED ANGLE TRAILING EDGE LOCATED WS253.00 LT WING IAW SRM B737-700 51-40-02<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED ANGLE TRAILING EDGE LOCATED WS253.00 LT WING IAW SRM B737-700 51-40-02 <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CORRODED (RH WING) · airframe 55,078 hrs · 29,733 cycles

CORROSION ANGLE MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT RT WING 2022-239511 / [01] REPLACED ANGLE LOC. MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT RT WING I.A.W B737-700 SRM 51-40-02 AND DWG 115A2511 REV A.SEE INDIVIDUAL SING-OFF BELOW.;[02] REPLACED ANGLE LOC. MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT RT WING I.A.W B737-700 SRM 51-40-02 AND DWG 115A2511 REV A.SEE INDIVIDUAL SING-OFF BELOW.

Part: LIGHT — DETERIORATED · airframe 55,078 hrs · 29,733 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2022-239428 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM-33-51-15-400-802;[02] COMPLETE TASK CERTIFIED

Part: FLOOR PANEL — ELONGATED (FWD CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

ELONGATED HOLE FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2022-239458 / [01] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801;[02] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801.<BR>TASK COMPLETED

Part: ANGLE — CRACKED (RH WING) · airframe 55,078 hrs · 29,733 cycles

CRACK TRAILING EDGE ANGLE LOCATED IRSS140.00 AT RT WING 2022-239496 / [01] REPLACED ANGLE LOCATED IRSS140.00 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG # 115A2000.;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE LOCATED IRSS140.00 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG # 115A2000 RV:B;[03] REPLACED ANGLE LOCATED IRSS140.00 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG # 115A2000 RV:B

Part: SUPPORT — CORRODED (LH WING) · airframe 55,078 hrs · 29,733 cycles

CORROSION ANGLE MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT LT WING 2022-239497 / [01] REPLACED ANGLE LOC. MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT LT WING . IAW SRM B737-700 51-40-02 AND DWG 115A2511 REV A.;[02] REPLACED ANGLE LOC. MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT LT WING . IAW SRM B737-700 51-40-02 AND DWG 115A2511 REV A. SEE INDIVIDUAL SING-OFF BELOW.;[03] REPLACED ANGLE LOC. MAIN LANDING GEAR SUPPORT BEAM LOCATED WBL94.24 AT LT WING . IAW SRM B737-700 51-40-02 AND DWG 115A2511 REV A. SEE INDIVIDUAL SING-OFF BELOW.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CRACK ON SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-239237 / [01] TOOL USED; DIGITAL CALIPER P/N: 500-196-30 S/N:A21033538 DUE DATE:02-FEB-23;[02] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW

Part: PANEL — DELAMINATED (WTB) · airframe 55,078 hrs · 29,733 cycles

DELAMINATED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR 2022-239313 / [01] TOOL USED: CALIPER: P/N:500-197-30 S/N:15120589 DUE DATE:28-NOV-22;[02] TOOL USED: HOT BONDER PN: HCS9000B-AV SN: 18164925 DUE DATE: 16-JAN-23;[03] TOOL USED SCALE PN SCA-301 SN AE-412125 DUE DATE: 14-MAR-23;[04] TOOL USED: HOT BONDER PN: HCS9000B-AV SN: 18164925 DUE DATE: 16-JAN-23;[05] TOOL USED SCALE PN SCA-301 SN AE-412125 DUE DATE: 14-MAR-23;[06] TOOL USED MULTIMETER 1000V AC RMS P/N:FLUKE 1587 S/N:38200035 DUE DATE 08-SEP-22.;[07] REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REPAIR 2 . SEE INDIVIDUAL SIGNOFFS BELOW.;[08] JOB COMPLETED

Part: SUPPORT ANGLE — CRACKED (PAX CABIN) · airframe 55,078 hrs · 29,733 cycles

CRACK SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24 AT PASSENGER CABIN 2022-239181 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL BL0 TO LBL24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9;[02] CERTIFIED STEP 1; COMPLETED. ITEM RII

Part: PLATE — CRACKED (AFT CARGO BAY) · airframe 55,078 hrs · 29,733 cycles

CRACK PLATE LOCATED ON BS 867 AND BTW STR 26L TO STR 27L AFT CARGO COMPARTMENT 2022-239186 / [01] REPLACED PLATE AND FASTENERS LOC. ON BS 867 AND BTW STR 26L TO STR 27L AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND DWG 149A8102; SHEET 12; REV C;[02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: SKIN — CRACKED (RH WING) · airframe 55,078 hrs · 29,733 cycles

CRACK EXTERNAL SKIN ACTUATOR FITTING AT SLAT STATION 322.71 AT RT WING 2022-239229. PERFORMED PERMANENT REPAIR EXTERNAL SKIN ACTUATOR FITTING AT SLAT STATION 322.71 SLAT 7 AT RT WING MATERIAL USED ALUMINUM SHEET 7075-T6 0.071? P/O: 2021-203793; ALUMINUM SHEET 7075-T6 0.063? P/O 2021-152041 IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; FIGURE 202; SHEET 2 ALTERNATIVE 1 SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR EXTERNAL SKIN ACTUATOR FITTING AT SLAT STATION 322.71 SLAT 7 AT RT WING MATERIAL USED ALUMINUM SHEET 7075-T6 0.071? P/O: 2021-203793; ALUMINUM SHEET 7075-T6 0.063? P/O 2021-152041 IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; FIGURE 202; SHEET 2 ALTERNATIVE 1.

Part: ANGLE — CRACKED (PAX CABIN) · airframe 55,078 hrs · 29,733 cycles

CRACK ANGLE LOCATED BS695 AT LEVEL BL0 TO RBL24 AT PASSENGER CABIN 2022-239182 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE LOC BS695 AT LEVEL BL0 TO RBL24 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 AND DWG 273A9110; SHEET 5; REV. A. SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED ANGLE LOC BS695 AT LEVEL BL0 TO RBL24 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 AND DWG 273A9110; SHEET 5; REV. A. SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT ANGLE — ELONGATED (PAX CABIN) · airframe 55,078 hrs · 29,733 cycles

ELONGATED HOLE SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24 TO RBL45 AT PASSENGER CABIN 2022-239180 / REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL RBL24 TO RBL45 AT PASSENGER CABIN IAW B737-700 SRM 51-40-01-0G-0 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 143A5240-32 P.O: 2022-133185. CORRECTED CORRECTIVE ACTION. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL RBL24 TO RBL45 AT PASSENGER CABIN IAW B737-700 SRM 51-40-01-0G-0 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 143A5240-32 P.O: 2022-133185. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL RBL24 TO RBL45 AT PASSENGER CABIN IAW B737-700 SRM 51-40-01-0G-0 AND SRM 51-10-02 ITEM 9.

Part: BATTERY PACK — INOPERATIVE · airframe 55,078 hrs · 29,733 cycles

INOP BATTERY PACK (M 1669) IN MIDDLE PASSENGER CABIN 2022-239085 / [01] REPLACED BATTERY PACK (M1669) IN MIDDLE PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK;[02] REPLACED BATTERY PACK (M1669) IN MIDDLE PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 55,078 hrs · 29,733 cycles

INOP BATTERY PACK (M 1675) IN FWD PASSENGER CABIN 2022-239083 / [01] REPLACED BATTERY PACK (M1675) IN FWD PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK;[02] REPLACED BATTERY PACK (M1675) IN FWD PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 55,078 hrs · 29,733 cycles

NOP BATTERY PACK (M 1668) IN MIDDLE PASSENGER CABIN 2022-239084 / [01] REPLACED BATTERY PACK (M 1668) IN MIDDLE PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK;[02] REPLACED BATTERY PACK (M 1668) IN MIDDLE PASSENGER CABIN IAW AMM 33-51-06-960-805 AND TEST IS OK

Part: LIGHT — MISSING · airframe 55,072 hrs · 29,729 cycles

ROW 11 LOWER SIDEWALL EXIT LIGHT LENS MISSING(LEFT SIDE)(11B) / [01] INSTALLED NEW LENS IAW AMM 33-51-01

Part: INDICATOR — FAULTED (E&E BAY) · airframe 54,984 hrs · 29,672 cycles

BOTH TRAILING EDGE AND LEADING EDGE FLAPS FAILED TO EXTEND WITH 3 ATTEMPTS. EXTENDED NORMALLY UPON A 4TH ATTEMPT. / [01] FOUND #6 FLAP TRANSMISSION WITH NO OIL AND TORQUE TRIP INDICATOR POPPED. FLUSHED; SERVICED; & RESET TORQUE TRIP INDICATOR ON #6 FLAP TRANSMISSION. DRAINED AND FILLED #1;#2; #3; #4; #5; #6; #7; & #8 FLAP TRANSMISSION OIL PER AMM 12-22-51. OPS & LK CK NORMAL PER AMM 27-51-00. NO FURTHER DEFECTS NOTED.<BR>E130865

Part: FLAP SYSTEM — FAILED · airframe 54,962 hrs · 29,653 cycles

FLAPS DID NOT EXTEND AIRBORNE WHEN FLAP LEVER WAS MOVED TO FLAPS 5. ALTERNATE FLAPS USED TO EXTEND TO 15 / [01] PERFORMED FSEU BITE; PREVIOUS/CURRENT LEG FAULT 27-51402 PRESENT. PERFORMED FIM 27-51 TASK 847. REMOVED AND REPLACED FLIGHT CONTROL PANEL PER AMM 27-09-45; OPS CHECK GOOD. PERFORMED T/E OPS CHECK PER AMM 27-51-00; CHECKS GOOD. PERFORMED L/E FLAP OPS CHECK PER AMM 27-81-00; CHECKS GOOD. PERFORMED GVI OF FLAP T/E SYSTEM PER AMM 27-51-00; NO DEFECTS FOUND.

Part: INDICATOR — FAULTED (TE FLAPS) · airframe 53,944 hrs · 29,047 cycles

ON APPROACH WHEN SELECTING FLAPS 5 I NOTICED A SPLIT FLAP BETWEEN 0-1. THE LEADING EDGE FLAP CAME OUT PARTIALLY BUT WE HAD L/E FLAP ORANGE TRANSIT LIGHT ON + TRAILING EDGE FLAPS STOPPED HALFWAY ; BETWEEN 0 + 1 AFTER ALL CHECKLIST WERE RAN WE LANDED FLAPS UP AT 189 KNOTS. LANDING WAS SMOOTH AND UNEVENTFUL. THE CHECKLIST HAD ME PUT THE FLAP HANDLE TO THE UP POSITION + AFTER LANDING THE LE ORANGE TRANSIT LIGHT WENT OUT. / [01] PERFORMED FIM TASK 27-51 TASK 813; FOUND L/H FLAP TRANSMITTER FAULTED & FLAP POS IND TO LAG. R&R L/H FLAP TRANSMITTER PER AMM 27-58-01 & R&R FLAP POSITION IND PER AMM 27-58-02. OPS CHK GOOD AT THIS TIME. REF LP 1941527 FOR CONDITIONAL INSP.

Part: TRANSMITTER — FAULTED (TE FLAPS) · airframe 53,944 hrs · 29,047 cycles

ON APPROACH WHEN SELECTING FLAPS 5 I NOTICED A SPLIT FLAP BETWEEN 0-1. THE LEADING EDGE FLAP CAME OUT PARTIALLY BUT WE HAD L/E FLAP ORANGE TRANSIT LIGHT ON + TRAILING EDGE FLAPS STOPPED HALFWAY ; BETWEEN 0 + 1 AFTER ALL CHECKLIST WERE RAN WE LANDED FLAPS UP AT 189 KNOTS. LANDING WAS SMOOTH AND UNEVENTFUL. THE CHECKLIST HAD ME PUT THE FLAP HANDLE TO THE UP POSITION + AFTER LANDING THE LE ORANGE TRANSIT LIGHT WENT OUT. / [01] PERFORMED FIM TASK 27-51 TASK 813; FOUND L/H FLAP TRANSMITTER FAULTED & FLAP POS IND TO LAG. R&R L/H FLAP TRANSMITTER PER AMM 27-58-01 & R&R FLAP POSITION IND PER AMM 27-58-02. OPS CHK GOOD AT THIS TIME. REF LP 1941527 FOR CONDITIONAL INSP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,803 hrs · 28,966 cycles

SUPPLEMENTAL INFORMATION: CABIN EMERGENCY LIGHT AT 13DEF INOP. ; / [01] RELAMPED EMERGENCY EXIT AREA LIGHT AT 13DEF IAW AMM 33-51-03.

Part: ANTI-SKID VALVE — FAULTED (RT MLG) · airframe 53,232 hrs · 28,635 cycles

RIGHT BRAKE EXCESSIVE SHUTTERING BEFORE COMING TO A STOP ; / [01] RAR RH INBD AND RH OUTB ANTI SKID VALVE PER AMM 32-42-31. OPS CHECK GOOD.

Part: BRAKE ASSY — FAULTED (RT MLG) · airframe 53,226 hrs · 28,630 cycles

BRAKE HAVE EXCESSIVE SHUTTERING COMING TO A STOP ; / [01] ACCORDING TO THE HISTORY OF SHUTTERING. R/R #3 MLG BRAKE ASSY PER AMM 32-41-41. AND PERFORMED A/C RUN-TAXI; NO SHUTTERING ON BRAKE NOTED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,555 hrs · 27,684 cycles

MULTIPLE EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1670, IAW AMM 33-51-06. OPERATIONS TEST OK.

Part: SKIN — DEBONDED (RUDDER) · airframe 50,759 hrs · 27,203 cycles

LT RUDDER CONDUCTIVE STRIP DISBONDED AT LOWER AFT END 32' INCHES FROM TIP OF THE RUDDER, 19' INCHES FROM THE FWD EDGE 3' INCHES FROM THE AFT EDGE IN ZONE 3 MOD. REMOVED AND INSTALLED RUDDER, IAW B737 AMM 27-21-11 POS ONLY PN OFF: 173A0103-7 PN ON: 173A0103-8 SN OFF: SB0804 SN ON: SB1144.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,129 hrs · 26,791 cycles

RIGHT HAND OVER WING EXIT HATCH AFT EXIT LIGHT DOES NOT ILLUMINATE WITH EMERGENCY LIGHTS SWITCH SELECTED ON / REMOVED AIR RETURN GRILL TO ACCESS EMERGENCY EXIT POWER SUPPLY M1668 AND REPLACED F1 FUSE AND RE-INSTALLED EMERGENCY EXIT LIGHT BATTERY PACK ONTO M1668. POWER SUPPLY IAW AMM 33-51-06-960-804 STEP 3.D.(1);(2)(C);(3). OK TO INSTALL AIR RETURN GRILL AT L/H BS603 LEAD 253 03JUN20 INSP 15 03JUN20 RE-INSTALLED AIR RETURN GRILL AND CONNECTED D12448 TO EMERGENCY EXIT LIGHT L1365 IAW AMM 33-51-00-960-804 STEP 3.D.(5)(C) AND SWPM 20-30-12 AND WDM 33-51-21. PERFORMED GOOD FUNCTIONAL TEST OF EMERG. EXIT LIGHT L1358 AT R/H OWE AFT IAW AMM 33-51-06-960-804 STEP 3.D.(4).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,129 hrs · 26,791 cycles

EMERGENCY EXIT LIGHTS L1359 & L1189 AT LT OWE (INSIDE CABIN) HAVE BULBS OUT. REMOVED & REPLACED AND PERFORMED GOOD FUNCTIONAL TEST OF APPLICABLE EMERGENCY EXIT LIGHT BULBS FOR L1359 AND L1189 LIGHTS AT LT OWE (INSIDE CABIN) IAW AMM 33-51-01-960-801 STEP 2C (1)(A)4)(E);(2) AND (4).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

FCB BS 500-500A LBL 24 INTERCOSTAL CRACKED. REMOVED AND INSTALLED NEW FCB BS 500 - 500A LBL 24 INTERCOSTAL ITEM 143A7510-15 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DWG 143A7505.

Part: SUPPORT — CRACKED (BS 460-480) · airframe 50,129 hrs · 26,791 cycles

BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT IN FWD CARGO BAY ;BS 460-480 IS CRACKED / REPLACED BATTLE UNDER L/H FLOOR TO SIDEWALL SUPPORT IN FWD BS 460 - 480 PER REF SRM 51-40-02-0G AND DWG NBR 143A7505

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 50,129 hrs · 26,791 cycles

RT FWD VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT BS 1016 REMOVED AND REPLACED RT FWD SKATE ANGLE AT BS 1016 IAW SRM 544002; DWG 147A0030 AND DWG 147A0070. APPLIED DECORATIVE EXTERIOR PAINT IAW AMM 512199300801

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 50,129 hrs · 26,791 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS 500D S-19R WL 193 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG # 143A7902

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B AFT SIDE LBL24 WL156. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BSS 500B AFT SIDE LBL 24 WL 156 PER REF SRM 51-40-02-0G AND DWG NR 143A7502; 143A7505.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON FLOOR SUPPORT SPLICE AT ACB BS767+6 LBL19 - RBL19 WL157. CORROSION ON FLOOR SUPPORT SPLICE AT ACB BS767+6 LBL19-RBL19 WL157 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. DENT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED NEW FLOOR SUPPORT SPLICE AT BS767+6 LBL19-RBL19. PN 146A9401-4; PO 771569 IAW DWG 146A7500.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON AFT BULKHEAD TO FLOOR PANEL SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL23 WL157. REMOVED AND REPLACED AFT BULKHEAD TO FLOOR PANEL SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL23 WL157 PER REF SRM 51-40-02-0G AND DWG NR 143A9481.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON RAIL AT ACB BS 727D+6 RBL7 WL157. REPAIRED RAIL AT ACB BS 727D+6 RBL17 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 50,129 hrs · 26,791 cycles

***CORROSION*** ON FWD SHIELD AT ACB BS767 -787 RBL22 WL159. / REMOVED AND REPLACED ON FWD SHIELD AT ACB FROM BS767-787 RBL22-WL159 PO #761893/1 IAW SRM 51-40-02 AND DWG 146A0081

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON RAIL AT ACB BS 727D+6 RBL13 WL157. REMOVED AND REPLACED CARGO TRACK (RAIL) FROM BS 727+4' TO BS 887 RBL13 WL157 ITEM 7531329. IAW SRM 51-40-02; SRM 53-00-53-2R-3; DWG 146A7500 AND DWG 146A7501.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON RAIL AT ACB BS 727D+6 LBL17 WL157. REMOVED AND REPLACED CARGO TRACK (RAIL) AT ACB FROM BS 737+4' TO BS867; LBL17; WL157 P/N 146A7501-1 AND PO 753396 IAW SRM 51-40-02 AND DWG 146A7500.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS500D LBL24 WL157. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL BS400-500D WITH REPAIR SPLICE AT BS490; LBL24 WL157 IAW SRM 51-40-02; SRM 53-00-53-2R-6 AND DWG 143A7500.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 LBL24 WL155. REMOVED AND REPLACED ANGLE AT INTERCOSTAL BS400 LBL24 WL155 PER REF SRM 51-40-02-0G AND DWG NR 143A7505.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS500D LBL29 WL158. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE AT AFT BULKHEAD FCB BS500D LBL29 WL158 PER REF SRM 51-40-02-0G AND DWG NR 143A9481.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 50,129 hrs · 26,791 cycles

***CORROSION*** ON AFT SHIELD AT FCB BS494 - BS500 RBL24 WL157. / CORROSION ON FCB AFT SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS PER SRM PART REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0 PAR. 9C REMOVED AND REPLACED FCB AFT SHIELD BS 454 - 500A RBL 24 WL 157 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG # 143A0080

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,129 hrs · 26,791 cycles

CORROSION ON RAIL AT FCB BS500+6 LBL18 WL157. REMOVED AND REPLACED ON RAIL AT FCB BS396 TO BS500D LBL18 IAW 51-40-02 AND DWG 143A7500 NEW RAIL P/N.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 50,129 hrs · 26,791 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19L WL 193 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG # 143A7902

Part: GUSSET — CRACKED (BS 500D S21L) · airframe 50,129 hrs · 26,791 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-21L WL177. MARKED / FCB AFT BULKHEAD SUPPORT GUSSET AT BS 500D S-21L WL177 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS PER SRM REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0 PAR. 9C. REMOVED AND REPLACED FCB AFT BULKHEAD GUSSET BS500D S-21L WL177 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG #143A7902

Part: SHIELD — CORRODED (AFT CARGO) · airframe 50,129 hrs · 26,791 cycles

***CORROSION*** ON AFT SHIELD AT ACB BS847 - BS867 RBL21 WL165. / CORROSION FOUND ON ACB AFT SHIELD BS 847 - 867 RBL-21 WL=165 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLACMENT IAW SRM 51-10-02-0G-0 PAR 9C LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0 AND DWG # 146A0081 REV-A AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG # 146A0081 REV-A

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,129 hrs · 26,791 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 4TH VERTICAL STIFFENER IS CRACKED. REPAIRED RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,129 hrs · 26,791 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 2ND VERTICAL STIFFENER IS CRACKED. REPAIRED RT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 50,129 hrs · 26,791 cycles

PANEL BREAK SUPPORT AT BS 540; BL 0- RBL 25 IS CRACKED. / REMOVED & REPLACED PANEL BRAKE SUPPORT-36 PER SRM 51-40-02-0G-0 & AIPC 53-31-00-05 PG 31 59899U 13MAY20

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 50,129 hrs · 26,791 cycles

LT FWD VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT BS 1016. REMOVED AND REPLACED LT FWD SKATE ANGLE AT BS 1016 IAW SRM 514002; DWG 147A0030 AND DWG 147A0070. APPLIED DECORATIVE EXTERIOR; PAINT IAW AMM 512199300801

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 50,129 hrs · 26,791 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED LT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 3RD VERIFIED STIFFENER IAW SRM 55-10-09-2R-5.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 50,129 hrs · 26,791 cycles

LT AFT VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT BS 1025 AND BS 1132. REMOVED AND REPLACED LH AFT VERTICAL FIN TO BODY SKATE ANGLE AT BS1016 BS 1132 IAW SRM 514002 DWG 148A8300 AND DWG 148A3590.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 50,129 hrs · 26,791 cycles

RT AFT VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT SEVERAL AREAS FROM BS 1025- BS 1132. REMOVED AND REPLACED RH AFT VERTICAL FIN TO BODY SKATE ANGLE AT BS 1016 BS 1132 IAW SRM 514002 DWG 148A8300 AND DWG 148A3590

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,129 hrs · 26,791 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED RT HORIZONTAL STABILIZER INSPAR RIB STAB STA 120.30 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 50,129 hrs · 26,791 cycles

CRACK AROUND THE FASTENER AT LEFT WING NO.1 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. / REMOVED AND REINSTALLED SERVICEABLE #1 SLAT PER MM 27-81-21-400-801 ADJUSTED AND FUNCTINALLY TEST PER MM27-81-00-820-803 OPS CHECK GOOD VERIFIED ALL TORQUES SAFTIES AND CLEARANCES. REPAIR OF #1 SLAT ACCOMPLISHED ON WORK ORDER # 533360; CUSTOMER P.O. # 0570128-ANR (POS: #1; TAG NO.: 704817; P/N OFF/ON: 114A5010-3; S/N OFF/ON: 000798)

Part: SKIN — CRACKED (LE SLAT) · airframe 50,129 hrs · 26,791 cycles

CRACK AROUND THE FASTENER AT RIGHT WING NR 6 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. TRIMMED OUT THE DAMAGE PART OF RIGHT WING NR 6 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIB AND INSTALLED REPAIR PARTS IAW SRM 57-42-01-2R-8.

Part: SKIN — CRACKED (LT NR 8 SLAT) · airframe 50,129 hrs · 26,791 cycles

CRACK AROUND THE FASTENER AT RIGHT WING NO.8 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. / REMOVED; INSTALLED SERVICEABLE; ADJUSTED AND FUNCTIONAL TESTED #8 SLAT IAW MM 27-81-21-000-801 AND MM 27-81-21-000-801 AND MM 27-81-21-400-801 FUNCTIONAL CHECK GOOD VERIFIED ALL TORQUES SAFETYS AND CLEARANCES (POS: #8; TAG NO.: 702418; P/N OFF/ON: 144A5010-4; S/N OFF: 000796; S/N ON: 001646)

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,129 hrs · 26,791 cycles

LEFT & RIGHT OVER WING EMERGENCY LIGHTS INOP / REMOVED & REPLACED R/H & L/H EMERGENCY SIGN BATTERY AT STA @40 REF AMM 33-51-06

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO COMPARTMENT. STA 727D+4; RBL 21 TO LBL 21; WL 155; FLOOR PANEL SPLICE STRAP HAS CORROSION ON UPPER AND LOWER SURFACE. / REPLACED NEW TEE ASSY ON AFT CARGO COMPARTMENT; STA 727D+4 RBL 21-LBL 21; WL 155; IAW BOEING DWG #146A7500 TY: DWG; ID: 0037 REV: C & SRM 51-40-02.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED / WELDED AFT CARGO DOOR AFT CORNER SCUFF PLATE IAW SHOP WORK REQUEST 40430/1600/003

Part: PLATE — CRACKED (RT WING TE FLAP) · airframe 49,742 hrs · 26,554 cycles

R/H WING FIXED TRAILING EDGE OUTBOARD OF #6 FLAP TRACK HAD CRACKED WAFFLE PLATE. / R&R WAFFLE PLATE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 927-967) · airframe 49,742 hrs · 26,554 cycles

R2 DOOR CREASE BEAM CORRODED BETWEEN BS. 927 TO BS. 967. / R&R R2 DOOR CREASE BEAM IAW SRM AND DWG.

Part: SKIN — INCORRECT (BS 611-615) · airframe 49,742 hrs · 26,554 cycles

SKIN INTERNAL BETWEEN BS. 611 TO BS. 615, BETWEEN STR. 1 TO STR. 2R REQUIRED REPLACEMENT. / R&R FUSELAGE SKIN IAW EA.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 49,742 hrs · 26,554 cycles

AFT PIT RH Z ANGLE HAS MULTIPLE AREAS OF CORROSION BETWEEN STA 747 TO STA 767. EVALUATED CORROSION ON AFT CARGO RH Z ANGLE FROM STA 747 TO STA 767; WL 160 AND RBL 20. FOUND TO BE OUT OF LIMITS DUE TO CORROSION ON FASTENER HOLES IAW SRM 5300531A2 FIG 103 SHEET 2 DET D. PART REPLACEMENT ACCOMPLISHED ON Y167612 146A7502-30.

Part: STRAP — CORRODED (BS 1016) · airframe 49,742 hrs · 26,554 cycles

AFT WET AREA FLOOR STRUCTURE STRAP CORRODED AT BS. 1016+11, BL 0. / R&R STRAP PER SRM AND DWG.

Part: PAN — CORRODED (LAVATORY BS 1016) · airframe 49,742 hrs · 26,554 cycles

AFT WET AREA; STA 1016 + 6'; LBL 15; WL 208; LAV PAN CORRODED AT FASTENER HOLE. / EVALUATED CORROSION ON LAV PAN IN AFT WET AREA AT STA 1016+6'; LBL 15 AND WL 208. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA IAW SRM 51-10-02-0G-0 STEP 9. REMOVED AND REPLACED LAV PAN; P/N 147A5620-15; IAW BOEING DRAWING 147A5600 REV B AND SRM 51-40-02-0G-0 STEP 4 AND 7 147A5620-15

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,742 hrs · 26,554 cycles

UPON EVAL OF FLOORPANEL 241AEF DELAM WAS FOUND ON UPPER SURFACE / REPLACED FLOOR PANEL 241AEF WITH NEW IAW IPC 53-21-00-26 AND DWG 815A0044-2 FLOOR PANEL 241AEF WILL BE INSTALLED ON JPANEL-241-CLOSE.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO COMPARTMENT PANEL 140AF HAS CORROSION AROUND THE EDGES / CORROSION DAMAGE EXCEEDS 20'; OUT OF LIMITS; FABRICATED NEW PNL 140AF P/N 453A2610-34; ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED FLOOR PANEL P/N 453A2610-34 CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG NO 453A2610; SHT 22023 REV B. IAW SRM 53-00-53-1A-1 FIG 102; AMM 51-21-41-370-803; AMM 51-21-72-370-804. ATAG A11774 453A2610-34.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO COMPARTMENT PANEL 140BF HAS CORROSION AROUND THE EDGES / AFT CARGO COMP PANEL 140BF CORROSION FOUND TO BE 'OUT OF LIMITS' WITH MAX LENGTH OF 20' EXCEEDED IAW SRM 53-00-53-1A-1 FABRICATED NEW PANEL IAW BOEING DWG #453A2610 REV. K AND SRM 51-40-05-0G-0

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO COMPARTMENT PANEL 140DF HAS CORROSION AROUND THE EDGES / CORROSION DAMAGE ON PNL 140DF EXCEEDS 20'; OUT OF LIMITS; FABRICATED NEW PNL 140DF; P/N 453A2610-20; ACCOMPLISHED CONFROMITY INSPECTION AND VERIFIED FLOOR PANEL P/N 453A2610-20 CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG NO 453A2610 SHT 13 & 14 REV B; IAW SRM 53-00-53-1A-1 FIG 102; BOEING DWG NO 453A2610 REV K; AMM 51-21-41-370-803; AMM 51-21-72-370-804 ATAG 11768 453A2610-20.

Part: FRAME SPLICE — CORRODED (BS 967) · airframe 49,742 hrs · 26,554 cycles

AREA AFT OF AFT CARGO PIT; STA967; RBL18; WL183 FRAME SPLICE PLATE; JUST FWD OF OUTFLOW VALVE CUTOUT; HAS CORROSION ON UPPER LIP OF PLATE. / REMOVED CORROSION AT AFT CARGO STA 967 RBL 18 WL 183 FRAME SPLICE PLATE IAW SRM 53-00-04-1A-1. VERIFIED MATERIAL LOSS ORIGINAL .056 REMOVED .010 REMAIN .046 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED AAR TOOL #36647 DUE 06/07/20 IAW SRM 53-00-07-1A-1 AND SRM 53-70-07-01-1. FABRICATED NEW FRAME SPLICE IAW SRM 51-40-05-0G-0 AND BOEING DWG 147A0002 AND DWG 147A1100. INSTALLED FABRICATED FRAME SPLICE IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A0002 (SPLICE PLATE) 147A1100-20

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

PASSENGER CABIN AFT WET AREA FLOOR PANEL 242XF HAS FIBER AND CORE DAMAGE / REPLACED PNL242XF IAW 53-00-50-2R-1 REV 69 51-00-05 NDT EVALUATED AND FOUND FIBER DAMAGE AND CORE DAMAGE REPAIRED IAW B737 SRM 53-00-50-2R-0 REV 69 (A89485)(A98054)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

PASSENGER CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS FIBER DAMAGE / REPAIRED UPPER SURFACE PLY ON FLOORBOARD 241AAF IAW SRM 53-00-50-2R-1; PG'S 1;2 STEPS 3(A-N) A05073;A10203

Part: ANGLE — CORRODED (BS 727-847) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO PIT L/H Z ANGLE HAD MULTIPLE AREAS CORRODED BETWEEN BS. 727+3 TO BS. 847, WL 158. / R&R Z ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 49,742 hrs · 26,554 cycles

AFT CARGO PIT LH Z ANGLE STA 767+3' TO STA 847; WL 158 HAS MULTIPLE AREAS OF CORROSION REMOVED CORROSION FROM AFT CARGO LH Z ANGLE STA 767+3 TO 847 IAW B737 SRM 5110020G0 FOUND TO BE OUT OF LIMITS ORIG .040 REMAIN .020' LOSS .020' IAW B737 SRM 53005312. ZANGLE REPLACED ON NRC Y167533 PN 146A.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

PASSENGER CABIN FLOOR PANEL 242VF UPPER SURFACE HAS FIBER DAMAGE / WORK PERFORMED ON WORK CARD # 40428/2700/0019

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #008; CABIN FLOOR PANEL 241BF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED 5 AREAS WITH DENT DAMAGE AT UPPER FACESHEET ONLY ON FLOORBOARD 241BF IAW B737 SRM 53-00-50-2R-1; PAR 3(A; C; E; K1; L1; M1) -REV 69 & SRM 53-00-50-2R-0; PAR (5)- REV 69.

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #010; CABIN FLOOR PANEL 242AF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED UPPER SURFACE PLY ON FLOORBOARD 242AF IAW SRM 53-00-50-2R-1; PG'S 1;2; & FOUND DENTS 3EA TO BE WITHIN LIMITS IAW SRM 53-00-1A-1; PG 2; ITEMS C (1;2;3) A05073; A10203

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #012; CABIN FLOOR PANEL 242BF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED CABIN FLOOR PANEL 242BF PUNCTURE 2' AFT OF FWD EDGE AND 2 1/2' O/B FROM I/B EDGE IAW B737 SRM 53-00-50-2R-1 REV 69 AND B737 SRM 53-00-50-2R-0 REV 69; AND MULTIPLE DENTS ON UPPER SURFACE

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #013; CABIN FLOOR PANEL 242DF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED PNL 242DF SEVERAL DENTS ON UPPER SURFACE. IAW B737-700 SRM 53-00-50-2R-1 REV 64; SRM 53-00-50-2R-0 REV 69 A98054; A36551

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #007; CABIN FLOOR PANEL 232RF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED DENTS THAT WERE OUT OF LIMITS IAW SRM 53-00-50-2R-2 ITEM 3 (A THROUGH M ) ON PASSENGER CABIN FLOORBOARD 232 RF; UPPER SURFACE

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #015; CABIN FLOOR PANEL 241EF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED CABIN FLOOR PANEL #241EF OF 1(EA) DENT IAW B737-700 SRM 53-00-50-2R-0 REV 69 AND B737-700 SRM 53-00-50-2R-4 REV 69 AND 2(EA) DENTS IAW B737-700 SRM 53-00-50-1A-1 REV 69. A89485; A36551; A98054; A29895

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #004; CABIN FLOOR PANEL 231YF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED DAMAGE ON FLOOR PANEL 231YF. BLENDED REPIAR PLIES IN 3EA LOCATIONS. CURED; TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-0 REV 69; SRM 53-00-50-2R-1 REV 69

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 49,742 hrs · 26,554 cycles

DOT #003; CABIN FLOOR PANEL 231ZF HAS SEVERAL DENTS; UPPER SURFACE. / DENTS REPAIRE DON UPPER FLOOR BOARDS SURFACE ON FLOOR BOARD 231 ZF. IAW SRM 53-00-50-2R-2 ITEM 3 STEPS A THROUGH N

Part: STIFFENER — CRACKED (BS 663) · airframe 49,742 hrs · 26,554 cycles

FOUND DURING FCBS REPAIR SURVEY MLG WHEEL WELL CENTER WING REAR SPAR STA 663 RBL 27 APPROXIMATE WL 153 VERTICAL STIFFENER IS CRACKED 2.5 INCHES LONG / REMOVED DAMAGED STIFFENER IN MLG WHEEL WELL @ STA 663 RBL 27 WL 153' AND INSTALLED NEW STIFFNER P/N 11A 308-16 ATAG # WN6395 I/A/W SRM 51-40-02-0G-0 & BOEING DWG 11A 100 SHEET 114 REV -.

Part: HANDLE — CRACKED (FWD CARGO DOOR) · airframe 49,742 hrs · 26,554 cycles

DURING INSPECTION OF THE REPAIR SURVEY FOR THE FWD CARGO DOOR; FOUND DOOR HANDLE CRACKED ON THE INSIDE AROUND RIVET BUCKTAIL (MARKED) / REMOVED CRACKED FWD CARGO DOOR HANDLE PAN AND INSTALLED NEW HANDLE PART IAW EA 200170 REV P1; IR & SWA EA 1-752-2698 REV IR & BOEING DWG 143A61110 REV C. A-TAG # WN7227.

Part: STIFFENER — CRACKED (AFT SERVICE DOOR) · airframe 48,678 hrs · 25,879 cycles

AFT SERVICE DOOR LOWER ATTACHMENT SKIRT FOR THE DOOR LINER HAS BOTH STIFFENERS CRACKED / REMOVED AND REPLACED AFT SERVICE DOOR LOWER ATTACHMENT SKIRT PER SRM 51-40-02.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 46,764 hrs · 24,636 cycles

ONE EMERGENCY FLASH LIGHT STRAP BROKEN. R&R STRAP IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,632 hrs · 24,542 cycles

EXTERNAL POWER CUTOUT MID/FORWARD LIP CRACKED. REPAIRED CUTOUT PER EA.

Part: FASTENER — LOOSE (EMERGENCY EXIT) · airframe 46,596 hrs · 24,514 cycles

LT OVERWING EXIT HANDLE COVER LOOSE. INSTALLED HARDWARE PER AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 46,386 hrs · 24,383 cycles

RT SIDE WINDOW OVERHEAT CAME ON. FIRST OFFICER SAW A FLASH IN BOTTOM CORNER OF WINDOW. R&R NR 2 WINDOW IAW MT.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 45,877 hrs · 24,047 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 45,877 hrs · 24,047 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 45,877 hrs · 24,047 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 45,877 hrs · 24,047 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SIGN — MISSING (CABIN) · airframe 45,454 hrs · 23,781 cycles

R1 DOOR EXIT SIGN MISSING DIRECTIONAL ARROW. R&R SIGN PER AMM.

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 45,111 hrs · 23,555 cycles

L2 DOOR SLIDE OUT OF POSITON. REPOSITIONED GIRT BAR IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,089 hrs · 23,544 cycles

R1 DOOR EMERGENCY SLIDE OUT OF POSITION. R&R SLIDE PER MT AND EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 44,920 hrs · 23,445 cycles

R2 DOOR SLIDE GIRT BAR LOOSE. REPOSITIONED SLIDE IAW MT.

Part: SENSOR — FAULTY (LT MLG) · airframe 44,869 hrs · 23,407 cycles

AIR TURNBACK, AFTER TAKEOFF, LANDING GEAR WAS SELECTED TO UP. LEFT MAIN GEAR INDICATION OR FWD PAROL INDICATED GREEN "LEFT GEAR" OVERHEAD PAROL GEAR LIGHTS WERE EXTINGUISHED. RUN "GEAR" DISAGREE "QRM PROCEDURE. R&R SENSOR PER AMM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 44,741 hrs · 23,321 cycles

R1 DOOR GIRT BAR BRACKET LOOSE. REPOSITIONED RETAINER IAW AMM.

Part: SEAL — BUCKLED (HORIZONTAL STAB) · airframe 44,347 hrs · 23,083 cycles

RIGHT HORIZONTAL STAB LOWER FORWARD SLIDER SEAL IS BUCKLED; TORN. / REMOVED AND REPLACED SLIDER SEAL PER AMM 27-41-11

Part: CONNECTOR — DISCONNECTED (EXTERIOR LIGHT) · airframe 44,269 hrs · 23,030 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RECONNECTED CONNECTOR IAW AMM.

Part: PANEL — DELAMINATED (RT WING) · airframe 44,269 hrs · 23,030 cycles

SERVERAL AREAS OF DISBOND OVER CORE FOUND ON T/E PANEL 661BB / REPAIRED SEVERAL AREAS OF DISBOND OVER CORE ON T/E PANEL 661BB I.A.W 737 SRM 57-51-01-2R-1 TABLE 201; I.A.W SRM 51-70-05-2R-1.

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

SKIN DAMAGED BS 295.5-305.9 L/H 4' BELOW STR 19 / TRIMMED OUT DAMAGED SKIN AT BS 295.5-305.9 L/H 4' BELOW STR 19 AND INSTALLED REPAIR PER EA 1-753-32827 REV IR AND ER 18-02901 REV IR

Part: STIFFENER — CRACKED (WHEEL WELL LH) · airframe 44,269 hrs · 23,030 cycles

STIFFENER CRACKED BS 663 L/H LOWER VAPOR BARRIER. (111A1308-7) / REMOVED CRACKED STIFFENER & INSTALLED NEW STIFFENER P/N 111A1308015 IAW 51-40-02-0G-0 & BOEING DWG 11131308 AT BS 663 LT

Part: BEAM — DAMAGED (AFT CARGO COMPT) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO FLOOR BEAM DAMAGED AT BS 791 RBL 8 AROUND FASTENER HOLE / EVALUATED DAMAGE AT BS 791 RBL 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED DAMAGED AREA IAW SRM 53-00-53-2R-2; FABRICATED; LOCATED & DRILLED REPAIR PARTS IAW SRM 53-00-53-2R-2; TREATED & PRIMED REPAIR PARTS IAW AMM 51-21-41-370-801 & 51-21-72-370-804; INSTALLED REPAIR PARTS IAW SRM 53-00-53-2R-2 & 51-40-02-0G-0 REPAIR SPLICE LOCSTED B2 789-792 ROL 8.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 44,269 hrs · 23,030 cycles

FWD CARGO DOOR CUTOUT. AFT LOWER CORNER SCUFF PLATE CRACKED / LOCATED AND DRILLED. REPLACEMENT FWD CARGO DOOR CUTOUT. AFT LOWER CORNER SCUFF PLATE AND COUNTER SUNK IAW B737-700 SRM 51-40-08-0G-0 AND SRM 51-40-05-0G-0. SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD #753-140-00-01Y. SCUFF PLATE ITEM #7530065 PO #688128

Part: PLATE — CRACKED (RT WING) · airframe 44,269 hrs · 23,030 cycles

RT WING WIGGLE PLATE JUST INBOARD OF ENGINE PYLON ON FIXED TRAILING EDGE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: TRIM TAB — DAMAGED (ELEVATOR RH) · airframe 44,269 hrs · 23,030 cycles

R/H ELEVATOR TRIM TAB DAMAGED AT TRAILING EDGE APPROX 31 INCHES O/B FROM I/B EDGE (MARKED) / REMOVED & REINSTALLED R/H ELEVATOR TRIM TAB AMM 27-31-31-000-801 & 27-31-31-400-801. REPAIRE REPAIRED ELEVATOR TRIM TAB IAW A.T.S. ER 18-02846 REV IR & SWA EA 1-755-4137 REV IR. VERIFIED ADJUSTMENT OF ELEVATOR TAB IAW AMM 27-31-34-400-801; NO ADJUSTMENT REQUIRED. PER FORMED OPS CHECKS IAW AMM 27-31-00-700-802 & 27-31-00-700-806. ALL OPS CHECKS GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 44,269 hrs · 23,030 cycles

CABIN FLOOR PANEL 221BF HAS DAMAGE ON O/B AFT CORNER / REPAIRED CABIN FLOOR PANEL 221BF O/B CORNER IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-6 AND SRM 53-00-50-2R-0

Part: STRIP — ELONGATED (AFT CARGO COMPT) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO; AFT L/H CAP STRIP HAS ELONGATED HOLES. / FABRICATED REPLACEMENT AFT CARGO; AFT L/H CAP STRIP FROM 2024 T3 .063' LOT #5045345 PER DWG #453A2611 AND SRM 51-40-05-0G-0. APPLIED ALODINE; PRIMER; AND PAINT PER AMM 51-21-41-370-802; AMM 51-21-72-370-801 AND AMM 51-21-73-370-803

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

INTERCOSTAL CRACKED AT BS 277, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO LOWER MAIN DOOR SILL INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 792, RBL 20. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO LOWER MAIN DOOR SILL INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 854, RBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO LOWER MAIN DOOR SILL INTERCOSTAL CORRODED BETWEEN BS 792 TO BS 847, RBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FLOORBEAM CORRODED AT BS 344, BETWEEN LBL 28 TO RBL 11. REPAIRED FLOORBEAM IAW EA AND ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 44,269 hrs · 23,030 cycles

RT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. R&R AFT FLAP IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

INTERCOSTAL CRACKED BETWEEN BS 500A TO BS 500B, LBL 23. R&R INTERCOSTAL PER EA AND ER.

Part: STRAP — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO COMPARTMENT STRAP CORRODED BETWEEN BS 812 TO BS 816, RBL 19. R&R STRAP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO COMPARTMENT TOP SURFACE OF FRAME CORRODED AT BS 787, RBL 19.5. REPAIRED FRAME PER EA AND ER.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 774, RBL 20. R&R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO COMPARTMENT TOP SURFACE ON FLOOR SUPPORT ANGLE CORRODED AT BS 793.5, RBL 2.5. REPAIRED ANGLE IAW SRM.

Part: NONE — CRACKED (MAIN CABIN) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: L1 DOOR THRESHOLD REVEAL PANEL CRACKED / REMOVED REVEAL. LOCATED & DRILLED NEW REVEAL IAW SRM 51-40-05 & DWG 141A8221; APPLIED PAINT IAW AMM 51-21-73; INSTALLED NEW REVEAL IAW DWG 141A8220 & SRM 51-40-02 57171U 22MAY18

Part: FLAP — DELAMINATED (LT WING) · airframe 44,269 hrs · 23,030 cycles

LT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO FLOOR SUPPORT ANGLE CORRODED AT BS 791, LBL 128. REPAIRED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FLOOR TO SIDEWALL SUPPORT Z ANGLE CORRODED BETWEEN BS 727 TO BS 847, LBL 22. R&R CHANNEL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO FLOOR SUPPORT ANGLE CORRODED AT BS 767+6, LBL 2.5. REPAIRED ANGLE PER EA.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** AT AFT R/H BULKHEAD ANGLE BS 500D RBL 25.5 / REMOVED IAW SRM 51-40-02-0G-0 INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 143A9485 PART RECIEVED 7530202 PO #688039 BS500D RH BULKHEAD ANGLE

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO COMPARTMENT LAV PAN CORRODED AT BS 855, LBL 31. R&R CHANNEL IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO SIDEWALL SUPPORT ANGLE CORRODED AT BS 787, BETWEEN LBL 30 TO LBL 41. R&R SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO FLOOR SUPPORT TRACK CORRODED AT BS 767+5.5, LBL 8. REPAIRED TRACK PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

AFT CARGO FLOOR SUPPORT TRACK CORRODED AT BS 767+4.5, RBL 8. REPAIRED FLOOR BEAM IAW SRM.

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT LOWER STANCHION CLIP ATTACHED TO FRAME IS CRACKED AT STA. 867 LBL 11 WL 164 / REMOVED AND REPLACED CRACKED BRACKET @ STA867 LBL11 WL 164 WITH NEW BRACKET 149A8109-114 PER SRM 51-40-02 & DWG 149A8102

Part: GUSSET — CRACKED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL 222BF HAS 3 AREAS OF DISBOND (MARKED / FABRICATED REPLACEMENT CABIN FLOOR PANEL 222BF IAW SRM 53-00-50-2R-0 PARA 4A TABLE 204 AND PER BOEING DRAWING #141A5810 REV:C. PANEL IDENDIFICATION PER SRM 53-00-50-01-1 FIG. 2 SH1 TABLE 2. BMS 4-17 TY VI LOT #5066655-1. INSERTS: SL 5182A3; SL 2334-3; SL 618-3; SL 5111A3; CB3023AAFCR. INSERTS INSTALLED PER BAC 5085 PARA 8.3.1.2 AND PER BAC 5583 PARA 8.3.3.2. BMS 5-107 LOT #AK7FP4931K; BMS 5-28 TY 19 LOT #AK7JP2908K

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

SUPPORT L ANGLE FOR THRESHOLD PLATE CORRODED AT BS 310.5, RBL 57. R&R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL CRACKED BETWEEN BS 460 TO BS 480, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — DEBONDED (FWD CABIN) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL 222BF HAS O/B FWD CORNER DISBONDED / WORK ACCOMPLISHED ON NRC N132541

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL 241DF HAS LARGE AREAS OF MISSING FIBERGLASS ON UPPER SURFACE / FABRICATED REPLACEMENT CABIN FLOOR PANEL 241DF PER SRM 53-00-50-01-1 SRM 53-00-50-2R-0 TABLE 204 AND BOEING DWG #144A5810-9

Part: FLOOR PANEL — DEBONDED (AFT CABIN) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL 222AF HAS O/B AFT CORNER DISBONDED / REPAIRED DISBOND ON O/B AFT CORNER OF CABIN FLOOR PANEL 222AF. IAW SRM 53-00-50-2R-9 & SRM 53-50-50-2R-0 80734U 14MAY18

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

TOP SURFACE OF FLOOR SUPPORT CORRODED AT BS 312-3, RBL 10. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL 241AF HAS LARGE AREAS OF MISSING FIBERGLASS ON UPPER SURFACE / FABRICATED REPLACEMENT FLOOR PANEL 241AF PER SRM 53-00-50-01-1 AND BOEING DWG 144A5810-8; SRM 53-00-50-2R-0 TABLE 204

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FLOORBEAM CORRODED AT BS 294.5, LBL 11. REPAIRED FLOORBEAM IAW ER AND EA.

Part: ANGLE — CORRODED (MAIN CABIN) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** FWD ENTRY THRESHOLD PLATE SUPPORT Z ANGLE HAS CORROSION STA. 338.5' LBL 64 WL 209 (MARKED) / REMOVED CORROSION ON FWD ENTRY THRESHOLD PLATE SUPPORT Z-ANGLE BY MECHANICAL MEANS REMOVED .030 FOUND TO BE OUT OF LIMITS I.A.W.- SRM 53-10-15-1A-1. REMOVED Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW Z-ANGLE I.A.W. SRM 51-40-05-0G-0. INSTALLED NEW Z-ANGLE IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV:E LOT #5068786.

Part: PANEL — CRACKED (RT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: R/H WING TRAILING EDGE PANEL 661AB HAS MANY CRACKED ATTACH FASTENER HOLES (MARKED) / REPAIRED MANY CRACKED ATTACH FASTENER HOLES ON R/H WING TRAILING EDGE PANEL 661AB PER SRM 51-51-01-2R-1 TABLE 202 AND SRM 51-70-05-2R-6

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FORWARD CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FORWARD CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 460 TO BS 500D, LBL 23. R&R SUPPORT IAW SRM & DWG.

Part: PANEL — CRACKED (LT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: L/H WING TRAILING EDGE PANEL 561BB HAS MANY CRACKED ATTACH FASTENER HOLES (MARKED) / REPAIRED SEVERAL CRACKED FASTENER HOLES ON L/H WING T/E PANEL 561BB IAW SRM 57-51-01-2R-1 AND SRM 51-70-05-2R-6

Part: PANEL — CRACKED (RT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: R/H WING TRAILING EDGE PANEL 661BB HAS MANY CRACKED ATTACH FASTENER HOLES (MARKED) / REPAIRED R/H WING TRAILING EDGE PANEL 661BB CRACKED FASTENER HOLES I.A.W 737 SRM 57-51-01-2R-1 PARA 1;4D TABLE 202; 250Ï¿½F CURE PER 737 SRM 51-70-05-REPAIR 6

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 44,269 hrs · 23,030 cycles

LT LOWER VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FORWARD CARGO BAY AFT SIDE SHIELD CORRODED BETWEEN BS 482 TO BS 500A, RBL 23. R&R SHIELD IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 44,269 hrs · 23,030 cycles

FORWARD CARGO BAY SIDE SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 23. R&R SHIELD PER SRM AND DWG.

Part: NONE — CRACKED (RT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: RH WING SUPPORT GUSSET FOR UPPER TRAILING EDGE PANEL IS CRACKED AT LOWER TRANSVERSE WEB ATTACH POINT. APPROXIMATELY 10 INCHES INBOARD OF AFT DEFLECTION ARM. / REMOVED & REPLACED RH WING SUPPORT GUSSET FOR UPPER TRAILING EDGE PANEL IAW SRM 51-40-02-0G-0 STEP 4; SRM 51-40-045-0G-0 FIG 3; AND DWG 115A2930 REMOVED & REPLACED RH WING R/H WING TRANSVERSE WEB IAW SRM 51-40-05-0G-0 FIG 3; SRM 51-40-02-0G-0 STEP 4; & DWG 115A2930

Part: NONE — CRACKED (RT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: RH WING TRAILING EDGE COVE SEAL RETAINER ABOVE #2 PYLON AFT TIP IS CRACKED AT WEB ATTACH POINT. / R/H WING TRAILING EDGE COVE SEAL RETAINER ABOVE #2 PYLON WAS REMOVED & REPLACED ON CUST. NRC DEFECT N132506

Part: PANEL — CRACKED (RT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: R/H WING TRAILING EDGE PANEL 661CB HAS MANY CRACKED ATTACH FASTENER HOLES (MARKED) / REPAIRED SEVERAL CRACKED FASTENER HOLES ON R/H WING T/E PANEL 661CB IAW SRM 57-51-01-2R-1 AND SRM 51-70-05-2R-6

Part: PANEL — CRACKED (LT WING) · airframe 44,269 hrs · 23,030 cycles

SUPPLEMENTAL INFORMATION: L/H WING TRAILING EDGE PANEL 561AB HAS MANY CRACKED ATTACH FASTENER HOLES (MARKED) / REPAIRED MANY CRACKED ATTACH FASTENER HOLES ON L/H WING TRAILING EDGE PANEL 561AB PER SRM 57-51-01-2R-1 TABLE 202 AND SRM 51-70-05-2R-6

Part: SLIDE — LOOSE (L1 DOOR) · airframe 42,479 hrs · 21,891 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE ASSEMBLY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 40,159 hrs · 20,456 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 40,159 hrs · 20,456 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER AMM.

Part: BONDING JUMPER — LOOSE (L1 DOOR SLIDE) · airframe 38,092 hrs · 19,231 cycles

L1 DOOR SLIDE COVER BONDING JUMPER LOOSE ON BACKING PAN. SECURED THE BONDING JUMPER IAW IAW TC.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 38,092 hrs · 19,231 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, SECOND VERTICAL STIFFENER. R & R RIB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887. R & R SUPPORT IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

RIGHT AUXILIARY POWER UNIT AIR INLET LOWER CHORD CORRODED BETWEEN BS 1112 TO BS 1147. R & R CHORD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 947, RBL 20. R & R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS 947, BETWEEN LBL 20 TO RBL 20. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. R & R SUPPORT IAW DWG AND SRM.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY ON FRAME SPLICE CORRODED AT BS 867, RBL 22. R & R SPLICE IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 784, RBL 20. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 20. R & R SUPPORT IAW SRM AND DWG.

Part: POST — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

RT 3 WINDOW E-F POST CRACKED AT 2ND FASTENER HOLE FROM BOTTOM. REPAIRED POST IAW ACO.

Part: BEAM — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

R1 DOOR STUB BEAM CRACKED AT BS 293, WL 209. R & R STUB BEAM IAW SRM.

Part: WINDOW FRAME — CRACKED (L3 WINDOW) · airframe 38,092 hrs · 19,231 cycles

L3 WINDOW E-F POST CRACKED. REPAIRED THE POST IAW ACO.

Part: FRAME — CORRODED (BS 847) · airframe 38,092 hrs · 19,231 cycles

FRAME CORRODED AT BS 847, STRINGER 1. REPAIRED THE FRAME IAW EA AND ER.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

LEFT COCKPIT NR 1 WINDOW FRAME CRACKED FROM THE RADIUS TO INTERNAL SURFACE. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME IAW EA.

Part: PLATE — CRACKED (RT WING) · airframe 38,092 hrs · 19,231 cycles

RIGHT WING WAFFLE PLATE CRACKED JUST INBD OF NR 2 PYLON AFT TIP. R & R WAFFLE PLATE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (LT WING) · airframe 38,092 hrs · 19,231 cycles

LEFT WING TRANSVERSE WEB CRACKED JUST INBD OF MAIN FLAP PROGRAM ROLLER SUPPORT ARM AT UPPER OTBD FASTENERS. R & R WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: BEAM — CRACKED (RT WING) · airframe 38,092 hrs · 19,231 cycles

RIGHT WING LOWER T/E BEAM CRACKED AT RSS 287. R & R BEAM IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FORWARD CARGO DOOR CUT OUT SUB THRESHOLD CORRODED IN SEVERAL AREAS. REPAIRED SUB THRESHOLD IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

INTERCOSTAL CRACKED AT BS 398, RBL 41. R & R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

L/H FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 400 - 500D. R & R SUPPORT IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

LEFT EMERGENCY DOOR ON CREASEBEAM WEB INNER CHORD CORRODED BETWEEN BS 620 TO BS 663, WL 208. REPAIRED CHORD IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: BULKHEAD — CANNING (BS 1016) · airframe 38,092 hrs · 19,231 cycles

BULKHEAD OIL CANNED AT BS 1016, BETWEEN BL 0 TO STRINGER 3R. REPAIRED THE BULKHEAD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

AFT SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,092 hrs · 19,231 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.