N7813P

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 66,304 hrs · 35,438 cycles

MULTIPLE EMERGENCY LIGHTS IN MID CABIN LEFT SIDE INOP<[01] REPLACE BATTERY PACK AND CHARGER ASSY (M1668) REF AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 66,304 hrs · 35,438 cycles

MULTIPLE EMERGENCY LIGHTS IN MID CABIN LEFT SIDE INOP<[01] REPLACE BATTERY PACK AND CHARGER ASSY (M1668) REF AMM 33-51-06. OPS CHECK GOOD.

Part: SEAT BACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 65,643 hrs · 35,053 cycles

SEAT @12B EXIT ROW RECLINES; EXIT ROW NOT MEANT TO RECLINE<[01] LOCKED OUT RECLIBE @12B PER SIP

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 65,391 hrs · 34,898 cycles

FWD GALLEY FA FLASHLIGHT INOP<[01] REMOVED AND REPLACED FWD GALLEY FA FLASHLIGHT BATTERY PER AMM 25-64-00.

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,552 hrs · 34,398 cycles

MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHT FOUND INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY AT M1670 PER AMM 33-51-06. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT M1670; M1672; M1673; M1674; AND M1675. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,552 hrs · 34,398 cycles

MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHT FOUND INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY AT M1670 PER AMM 33-51-06. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT M1670; M1672; M1673; M1674; AND M1675. OPS CHECK GOOD.

Part: LIGHT — INACCURATE (ZN 200 FUS TOP) · airframe 63,818 hrs · 33,954 cycles

LH EXIT SIDE WALL LT FOR OVER WING INOP<[01] RE-LAMPED L/H EXIT LT FOR OVER WING PER AMM 33-51-04 OPS C.K GOOD

Part: FUSE — INOPERATIVE (CABIN) · airframe 62,812 hrs · 33,364 cycles

INOP EMERGENCY LIGHT 6 EA ADJACENT TO RT SIDE EMERGENCY DOOR AT PASSENGER CABIN 2022-533483 / [01] REMOVED AND REPLACED FUSE (3 EA) ON EMERGENCY EXIT LIGHT BATTERY PACK M1668 AND M1669 AND PERFORMED TEST IAW B737-700 AMM 33-51-06-960-804. TEST IS OK.;[02] TASK CARD COMPLETE.

Part: FUSE — INOPERATIVE (OVERWING EXIT) · airframe 62,812 hrs · 33,364 cycles

OVER WINGS INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP 2022-533510 / [01] REMOVED AND REPLACED FUSE (3 EA) ON EMERGENCY EXIT LIGHT BATTERY PACK M1668 AND M1669 AND PERFORMED TEST IAW B737-700 AMM 33-51-06-960-804. TEST IS OK.;[02] TASK CARD COMPLETE.

Part: ANGLE — CRACKED (ZN 400 NACELLE/P) · airframe 62,812 hrs · 33,364 cycles

CRACK ON ANGLE RH FAN COWL ENGINE 2 AT 5 O CLOCK 2022-533466 / [01] REPLACED ANGLE ON RH FAN COWL ENGINE 2 AT 5 O'CLOCK IAW B737-700 51-40-02 AND CMM 71-13-30 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE ON RH FAN COWL ENGINE 2 AT 5 O'CLOCK IAW B737-700 51-40-02 AND CMM 71-13-30 SEE INDIVIDUAL SIGN OFF BELOW

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 62,812 hrs · 33,364 cycles

CRACK ON RIB LOCATED AT L/E STA. 114.55 ON RT HORIZONTAL STABILIZER LEADING EDGE. 2022-533454 / [01] REPLACED RIB LOCATED AT L/E STA. 114.55 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW SRM B77-700 51-10-02 ITEM 9 AND DWG 186A1305 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED RIB LOCATED AT L/E STA. 114.55 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW SRM B77-700 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1305 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED RIB LOCATED AT L/E STA. 114.55 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW SRM B77-700 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1305 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 62,812 hrs · 33,364 cycles

CRACK ON RIB LOCATED AT L/E STA. 95.96 ON RT HORIZONTAL STABILIZER LEADING EDGE. 2022-533452 / [01] REPLACED RIB LOCATED AT L/E STA. 95.96 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV. ?A?. SEE INDIVIDUAL SIGN-OFFS BELLOW;[02] REPLACED RIB LOCATED AT L/E STA. 95.96 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV. ?A?. SEE INDIVIDUAL SIGN-OFFS BELLOW<BR>RII

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 62,812 hrs · 33,364 cycles

CRACK ON RIB LOCATED AT L/E STA. 105.26 ON RT HORIZONTAL STABILIZER LEADING EDGE. 2022-533453 / [01] REPLACED RIB LOCATED AT L/E STA. 105.26 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV. ?A?. SEE INDIVIDUAL SIGN-OFFS BELLOW;[02] REPLACED RIB LOCATED AT L/E STA. 105.26 ON RT HORIZONTAL STABILIZER LEADING EDGE IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV. ?A?. SEE INDIVIDUAL SIGN-OFFS BELLOW<BR>RII

Part: ANGLE — CRACKED (ZN 400 NACELLE/P) · airframe 62,812 hrs · 33,364 cycles

CRACK ON ANGLE RH FAN COWL ENGINE 1 AT 5 O CLOCK 2022-533449 / [01] FAULT RESOLVED ON OTHER FAULT TTG8Q00F9DEJ;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00F9DEJ

Part: NONE — BROKEN (L1 DOOR) · airframe 62,812 hrs · 33,364 cycles

BROKEN HANDLE ASSIST FWD ENTRY DOORWAY LINING (1EA) 2022-533321 / [01] REPLACED HANDLE ASSIST FWD ENTRY DOORWAY LINING (1EA) I.A.W B737-700 AMM 52-11-31-400-802 STEP 3G ITEM 4 (D);[02] CORRECTED STEP 1 REPLACED HANDLE ASSIST FWD ENTRY DOORWAY LINING (1EA) I.A.W B737-700 AMM 25-21-31-402-802 STEP 3B ITEM (6).;[03] CORRECTED STEP 2 REPLACED HANDLE ASSIST FWD ENTRY DOORWAY LINING (1EA) I.A.W B737-700 AMM 25-21-31-420-802 STEP 3B ITEM (6).;[04] REPLACED HANDLE ASSIST FWD ENTRY DOORWAY LINING (1EA) I.A.W B737-700 AMM 25-21-31-420-802 STEP 3B ITEM (6).

Part: STRAP — CRACKED (AFT CARGO) · airframe 62,812 hrs · 33,364 cycles

CRACK ON STRAP LOCATED BS 767 AND BS 787; S- 25L AND S-25R AFT CARGO COMPARTMENT 2022-533428 / [01] REPLACED STRAP LOCATED BS 767 AND BS 787; S- 25L AND S-25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;[02] CORRECTED STEP 1 REPLACED STRAP LOCATED BS 767 AND BS 787; S- 25L AND S-25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TOOL USED CALIPER P/N 500-196-30 S/N B21140348 DUE DATE 16-JUL-23;[03] TASK CARD COMPLETED

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 62,812 hrs · 33,364 cycles

CRACK ON STIFFENER OF INSPAR RIB 129.5 AND 25 INCH FROM LEADING EDGE AT LT HORIZONTAL STABILIZER 2022-533438 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 14-MAY-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 14-MAY-23;[03] REPAIRED STIFFENER OF INSPAR RIB 129.5 AND 25 INCH FROM LEADING EDGE AT LT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5 REPAIR 5 SEE INDIVIDUAL STEP SIGN OFF BELOW.;[04] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — BROKEN (FWD ENTRY DOOR) · airframe 62,812 hrs · 33,364 cycles

BROKEN HANDLE ASSIST FWD ENTRY DOORWAY LINING (1EA) 2022-533325 /

Part: PLATE — CRACKED (L/H WING) · airframe 62,812 hrs · 33,364 cycles

CRACK INBOARD TRAILING EDGE CORRUGATED PLATE LOCATED AT LEVEL OF IRSS 215 AT LT WING 2022-533347 / [01] REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE AT LEVEL IRSS 215 LT WING. IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 115A2001. REV. ?B?. SEE INDIVUDUAL SIGNOFF BELOW.;[02] REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE AT LEVEL IRSS 215 LT WING. IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 115A2001. REV. ?B?. <BR>SEE INDIVUDUAL SIGNOFF BELOW.

Part: ANGLE — CRACKED (R/H HORIZ. STAB.) · airframe 62,812 hrs · 33,364 cycles

CRACK BLADE RETAINER ANGLE ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER (1 EA) 2022-533359 / [01] REPLACED BLADE RETAINER ANGLE ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND 51-10-02;[02] REPLACED BLADE RETAINER ANGLE ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND 51-10-02 TOOL USED: DIGITAL CALIPER P/N: 500-196-30 <BR>S/N: A20231600 DUE DATE:12/SEP/23;[03] REPLACED BLADE RETAINER ANGLE ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND 51-10-02 TOOL USED: DIGITAL CALIPER P/N: 500-196-30 <BR>S/N: A20231600 DUE DATE:12/SEP/23

Part: ANGLE — CRACKED (VERT. STAB.) · airframe 62,812 hrs · 33,364 cycles

CRACK LEADING EDGE ANGLE LOC. BS 1016 AND BTW STR2L TO STR2R AT VERTICAL STABILIZER 2022-533290 / [01] REPLACED NEW LEADING EDGE ANGLE (SPRING ) LOC. BS 1016 AND BTW STR2L TO STR2R AT VERTICAL STABILIZER AND STRAP 2E/A I.A.W.B737-700 SRM 51-40-02 176A3101 REV? SEE INDIVIDUAL SING OFF BELLOW.;[02] REPLACED NEW LEADING EDGE ANGLE (SPRING ) LOC. BS 1016 AND BTW STR2L TO STR2R AT VERTICAL STABILIZER AND STRAP 2E/A I.A.W.B737-700 SRM 51-40-02. AND DWG 176A3101 REV? SEE INDIVIDUAL SING OFF BELOW .

Part: ANGLE — CRACKED (R/H WING) · airframe 62,812 hrs · 33,364 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED AT DEFLECTION CONTROL RIB AREA AND ORSS 278 AND WS 278.5 AT RT WING 2022-533302 / [01] REPLACED TRAILING EDGE SUPPORT ANGLE AND FASTENERS LOCATED AT DEFLECTION CONTROL RIB AREA AND ORSS 278 AND WS 278.5 AT RT WING. IAW B737-700 SRM 51-40-02; AND DWG 115A2930. REV. ?-?.;[02] CORRECTED STEP 1.<BR>REPLACED TRAILING EDGE SUPPORT ANGLE AND FASTENERS LOCATED AT DEFLECTION CONTROL RIB AREA AND ORSS 278 AND WS 278.5 AT RT WING. IAW B737-700 SRM 51-40-02; AND DWG 115A6200. REV. ?A?;[03] JOB TASK CARD COMPLETED.

Part: BRACKET — CRACKED (L/H WING) · airframe 62,812 hrs · 33,364 cycles

CRACK SUPPORT BRACKET TRAILING EDGE AREA AT LEVEL OF ORSS 271 AT LT WING 2022-533287 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AREA AT LEVEL OF ORSS 271 AT LT WING IAW SRM B737-700 51-40-02 TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A21042066 DUE DATE: 30-JUN-23;[02] TASK CARD COMPLETED

Part: BRACKET — CRACKED (L/H WING) · airframe 62,812 hrs · 33,364 cycles

CRACK SUPPORT BRACKET LOCATED AT TRAILING EDGE DEFLECTION CONTROL RIB AREA AND WS 278.5 AND ORSS 278 AT LT WING 2022-533286 / [01] REPLACED SUPPORT BRACKET LOCATED AT TRAILING EDGE DEFLECTION CONTROL RIB AREA AND WS 278.5 AND ORSS 278 AT LT WING IAW SRM 737-700 51-40-02 AND DWG 115A6200 TOL USED DIGITAL CALIPER PN: 500-196-30 SN: A20231600 DUE DATE 12-SEP-23;[02] REPLACED SUPPORT BRACKET LOCATED AT TRAILING EDGE DEFLECTION CONTROL RIB AREA AND WS 278.5 AND ORSS 278 AT LT WING IAW SRM 737-700 51-40-02 AND DWG 115A6200 TOL USED DIGITAL CALIPER PN: 500-196-30 SN: A20231600 DUE DATE 12-SEP-23

Part: PLATE — BROKEN (L/H WING) · airframe 62,812 hrs · 33,364 cycles

BROKEN CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL OF ORSS 261 AT LT WING 2022-533289 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL OF ORSS 261 AT LT WING IAW SRM B737-700 51-40-02; 51-10-02 ITEM 9 AND DRAWING 115A2001. REV.B; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL OF ORSS 261 AT LT WING IAW SRM B737-700 51-40-02; 51-10-02 ITEM 9 AND DRAWING 115A2001. REV.B; <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: PLATFORM — BROKEN (R/H WING) · airframe 62,812 hrs · 33,364 cycles

BROKEN CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL OF ORSS 261 AT RT WING 2022-533299 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL OF ORSS 261 AT RT WING IAW SRM B737-700 51-40-02 AND 115A2001 REV -;[02] TASK COMPLETED

Part: BRACKET — BROKEN (R/H WING) · airframe 62,812 hrs · 33,364 cycles

BROKEN TRAILING EDGE SUPPORT BRACKET AT ORSS 271 AT RT WING 2022-533301 / [01] REPLACED TRAILING EDGE SUPPORT BRACKET AND FASTENERS AT ORSS 271 AT RT WING. IAW B737-700 SRM 51-40-02. AND DWG 115A6200. REV. ?A?;[02] CORRECTED STEP 1. <BR>REPLACED TRAILING EDGE SUPPORT BRACKET AND FASTENERS AT ORSS 271 AT RT WING. IAW B737-700 SRM 51-40-02. AND DWG 115A2930. REV. ?-?.;[03] JOB TASK CARD COMPLETED.

Part: HARNESS — FAULTY (#1 ENGINE) · airframe 61,500 hrs · 32,555 cycles

DURING CLIMB #1 ENG EGT EXCEEDED LIMITS OF 930 DEGREES + (AMBER BAND) RETURNED TO NORMAL WHEN POWER REDUCED. STAYED IN AMBER BAND FOR APPROX. 2 MIN. / [01] INVESTIGATED EGT INDICATION SYSTEM WITH TECH FOREMAN AND FOUND FAULTY J10 HARNESS ON#1 ENG. R&R J10 HARNESS PER AMM 73-21-06 AND M-21-177-01860. NO FURTHER DEFECTS NOTED. <BR><BR>REF BARCODE TTG8Q00BVMFN & TTG8Q006VYY9 FOR TROUBLESHOOTING AND PARTS REPLACEMENT.

Part: PANEL — ELONGATED · airframe 60,897 hrs · 32,213 cycles

PANEL 194E HAS SEVERAL OUT OF ROUND HOLES. ; / [01] FABRICATED NEW PANEL; BACK DRILLED HOLES PER 51-40-05; COUNTER SINK PER 51-40-08 AND APPLIED DECORATIVE FINISH PER AMM 51-21-99.

Part: NONE — CRACKED (FUSELAGE) · airframe 60,897 hrs · 32,213 cycles

VERTICAL CLIP @ 727 PANEL 193 HAS CRACK APPROX. 2.0' LONG. ; / [01] FABRICATED NEW CLIP AND INSTALLED PER SRM 51-40-02 AND 51-40-05

Part: ENGINE — FAULTY (L/H WING) · airframe 60,522 hrs · 32,004 cycles

FUEL IMBALANCE INDICATION. FUEL LEAK CONFIRMED. LEFT SIDE ; / [01] PERFORMED #1 ENGINE GVI AND ENG IDLE RUN PER AMM 71-00-00. NO LEAKS OR DEFECTS NOTED. (PER MOC SUSPECT L/H #1 MAIN TANK FUEL QUANTITY INDICATION FAULT)

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,928 hrs · 31,141 cycles

RAMP REPORTED A CRACK IN THE EXTERNAL POWER DOOR CUTOUT. / PERFORMED REPAIR 4--ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER PER SRM 53-10-15-2R-4

Part: BRACKET — STUCK (R1 DOOR GIRT BAR) · airframe 58,404 hrs · 30,863 cycles

R1 DOOR GIRT BAR STOWAGE BRACKET STICKS / CLEANED BRACKET PER SIP

Part: TRUNNION — CORRODED (RT MLG) · airframe 58,006 hrs · 30,652 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING -UPPER OUTBOARD LUG-OUTER FACE HAS CORROSION / ACCOMPLISHED EA 1-A57-3246 AND MT 757-RCB-04-01 ON RIGHT MLG FWD TRUNNION FITTING UPPER OUTBD LUG OUTER FACE. (SPOT FACED) REF. D&M ENTERPRISES A/R WO. SSR #1263

Part: TRUNNION — CORRODED (RT MLG) · airframe 58,006 hrs · 30,652 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING- LOWER OUTBOARD LUG-OUTER FACE HAS CORROSION. / ACCOMPLISHED E.A. 1A-57-3246 AND MT 757-RCB-04-01 ON RIGHT MLG FWD TRUNNION FITTING LOWER OUTBD LUG; OUTER FACE. (SPOT FACED.) REF. D&M ENTERPRISES A/R W.O. SSR#1263.

Part: TRUNNION — CORRODED (LT MLG) · airframe 58,006 hrs · 30,652 cycles

L/H MLG FWD TRUNNION FITTING-UPPER INBOARD LUG- OUTER FACE HAS CORROSION / ACCOMPLISHED E.A. 1-A57-3246 AND MT 757-RCB-04-01 ON LEFT MLG FWD TRUNNION FITTING UPPER INBD LUG OUTER FACE. (SPOT FACED.) REF D&M ENTERPRISES A/R W.O. SSR#1262

Part: TRUNNION — CORRODED (LT MLG) · airframe 58,006 hrs · 30,652 cycles

L/H MLG FWD TRUNNION FITTING-LOWER INBOARD LUG- OUTER FACE HAS CORROSION. / ACCOMPLISHED E.A. 1-A57-3246 AND MT 757-RCB-04-01 ON LEFT MLG FWD TRUNNION FITTING LOWER INBD LUG OUTER FACE. (SPOT FACED.) REF. D&M ENTERPRISES A/R W.O. SSR# 1262

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 57,662 hrs · 30,458 cycles

BOTH LEFT OVERWING HATCH EMERGENCY LIGHTS DO NOT ILLUMINATE. TIGHTENED LOOSE CONNECTOR D12452, PER WDM 33-51-13 AND SWPM 20-61-28. PERFORMED A SATISFACTORY PASSING TEST OF BOTH LEFT OVERWING HATCH EMERGENCY LIGHTS, PER AMM 33-51-01-960-801.

Part: SIGN — INOPERATIVE (AFT CABIN) · airframe 57,662 hrs · 30,458 cycles

AFT SERVICE ENTRY DOOR EXIT LOCATOR SIGN IS INOPERABLE. REMOVED AFT SERVICE ENTRY DOOR EXIT LOCATOR SIGN FOUND JIFFE SPLICES HOOKED UP TO LIGHT ASSEMBLY NOT TO AIRCRAFT. CONNECTED LIGHT TO AIRCRAFT CONNECTORS D10086 AND D10088, AS PER WDM 33-51-22. REINSTALLED AFT SERVICE DOOR EXIT LOCATOR AND PERFORMED A GOOD OPERATIONAL CHECK OF EMERGENCY LIGHTS, AS PER AMM 33-51-00-720-801 PARA 3D (1) THROUGH (4) (A)3) AND 3D (4)(B)3).

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 57,662 hrs · 30,458 cycles

FWD SERVICE DOOR ESCAPE SLIDE LIGHT IS INOPERABLE. TROUBLESHOT FOUND W4142-0052-18 PULLED FROM GD 3880-DC FOR FWD SERVICE DOOR ESCAPE SIDE LIGHT, RETERMINATED W4148-0051-18. PERFORMED GOOD EMERGENCY LIGHTS OPERATIONAL CHECK, AS PER SWPM 20-90-15; WDM 33-51-12 AND AMM 33-51-00-720-801.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 57,662 hrs · 30,458 cycles

LOWER EXIT INDICATOR SIGN FOR RT OVERWING DOOR IS INOPERABLE. REMOVED LOWER EXIT INDICATOR SIGN LEASE FOR RT OVERWING DOOR FOUND WIRING DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY, AS PER AMM 33-51-01-960-802. PERFORMED A GOOD TEST OF THE LIGHT ASSEMBLY AND A GOOD EMERGENCY LIGHTING OPERATIONAL TEST, AS PER AMM 33-51-01-960-802 PARA 3C (7) AND AMM 33-51-00-710-801.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,662 hrs · 30,458 cycles

LT OVERWING EXIT EMERGENCY EXIT LIGHT ABOVE DOOR IS INOPERABLE. REPLACED FUSE ON POWER SUPPLY M1668. PERFORMED GOOD OPERATIONAL TEST OF LT OVERWING EXIT EMERGENCY LIGHT ABOVE DOOR, PER AMM 33-51-06-960-804; AMM 33-51-00-710-801 AND WDM 33-51-13.

Part: FLOOR PANEL — PUNCTURED (PAX CABIN) · airframe 57,662 hrs · 30,458 cycles

PASSENGER CABIN FLOOR PANEL 241EF IS PUNCTURED. DUE TO THE EXTENT OF DAMAGE FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241EF USING BMS 4-23TY2 LOT NR 1428456-1. INSTALLED INSERTS USING BMS 5-107 LOT NR 1445148-1 AND PART MARKED, IAW SRM 53-00-50-2R-0 PARA 1A(NOTE); 5S AND DWG 144A5810-10. 57066U 11/7/20.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 57,662 hrs · 30,458 cycles

RIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. / REMOVED AND REPLACED RIGHT HAND HORIZ. STAB FOWARD UPPER SLIDE SEAL PLATE P/N 181A8025-2 IAW SRM 51-40-02 AND AIPC 53-31-31-03 88920U 10NOV20

Part: STRAP — DAMAGED (BS 794) · airframe 57,662 hrs · 30,458 cycles

STRAP ON TOP OF BS 794 FRAME IS DAMAGED ON UPPER SURFACE; RBL 18; WL 154 / REMOVED AND INSTALLED NEW STRAP ON ACB BS 794 STR 18R TO STR 25R ITEM 7531466 PO # 752858 IAW SRM 51-40-02; SRM 53-60-15-1A-1 DWG 146A8200; DWG 146A7500 AND DWG 146A8120; SRM 51-40-05 80641U 12NOV20

Part: HOOK — CORRODED (LT OVRWG STRAP) · airframe 57,662 hrs · 30,458 cycles

CORROSION LT OWE EXIT LATCH ESCAPE STRAP HOOK, ENTIRE SURFACE AND SPRING. REMOVED AND REPLACED LT OWE EXIT LATCH ESCAPE STRAP HOOK, IAW AMM 25-61-10-000-802 AND AMM 25-61-10-400-802.

Part: STRAP — CORRODED (ESCAPE HATCH) · airframe 57,662 hrs · 30,458 cycles

CORROSION RT OWE EXIT HATCH ESCAPE STRAP HOOK, ENTIRE SURFACE AND SPRING. REMOVED AND INSTALLED NEW RT EMERGENCY EXIT HATCH ESCAPE STRAP, IAW AMM 25-61-11 AND SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS 787 TO 793 RBL 24 WL 156. REMOVED & REPLACED NEW INTERCOSTAL P/N 146A8123-17 AT AFT CARGO BAY BS 787 TO 793 RBL 24 WL 156, IAW DWG 146A8120 DWG 146A0081 & SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 57,662 hrs · 30,458 cycles

COCKPIT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 255 LBL 4 WL 208, MARKED. REMOVED AND REPLACED INTERCOSTAL COCKPIT FLOOR SUPPORT AT BS 255 LBL 4 WL 208, IAW SRM 51-40-02-0G-0 DWG 141A5100 59205U 10NOV20.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 57,662 hrs · 30,458 cycles

RH VERTICAL FIN TO BODY CLOSURE ANGLE (SKATE ANGLE) CHAFED SEVERAL AREAS BS 1040 TO BS 1064 / REMOVED & REPLACED RH VERTICAL FIN TO BODY CLOSURE ANGLE (SKATE ANGLE) FROM BS 1016 TO BS 1156 IAW DWG 148A8300 & SRM 51-40-02-0G-0

Part: CARGO TRACK — BENT (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

BENT RAIL AT AFT CARGO BAY BS 727A+12 RBL 3 WL 156. ACCOMPLISHED THE REPAIR ON ACB AT RAIL BS 727+4 TO BS 727C RBL 3, IAW SRM 53-00-53-2R-4; SRM 51-40-02 AND DWG 146A7500. 80641U 09NOV20.

Part: FLOORBEAM — CORRODED (BS 727D R-LBL 19) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 LBL19 TO RBL19 WL156. / REMOVED AND REPLACED NEW FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 LBL19 TO RBL19 WL156 ITEM# 146A9401-8 IAW SRM 51-10-02-0G-0 SRM 51-40-02-0G-0; AIPC 53-42-11-30

Part: SHIELD — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22 WL156. / REMOVED AND INSTALLED NEW ON FWD SHIELD AT ACB BS 767 - BS 787 RBL 22. IAW SRM 51-40-02; SRM 51-20-01; SRM 51-40-05 AND DWG 146A0081 80641U 12NOV20

Part: SUPPORT — CRACKED (BS 727) · airframe 57,662 hrs · 30,458 cycles

CRACKED FWD BULKHEAD PANEL SUPPORT AT AFT CARGO BAY BS727 RBL3 WL163. / A.C.B. AT BS727; RBL3; WL163. REMOVED BULKHEAD PANEL SUPPORT PER SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ITEM 7531203 PER SRM 51-40-05. OK TO INSTALL 89021C 03NOV20 INSP 33 03NOV20. INSTALLED NEW SUPPORT PER SRM 51-40-02 AND DWG #144A2600

Part: FRAME — DENTED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

DENT ON FRAME AT AFT CARGO BAY BS 727B S-24R WL 159. REPAIRED FRAME BS 727B STR 24R, PER SWA EA20-153-02319 REV IR (ATS ER 20-03546 REV IR).

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 57,662 hrs · 30,458 cycles

LH VERTICAL FIN TO BODY CLOSURE ANGLE (SKATE ANGLE) CHAFED SEVERAL AREAS BS 1040 TO BS 1064 / L/H VERTICAL FIN TO BODY CLOSURE ANGLE (SKATE ANGLE) CHAFED SEVERAL AREAS BS1040 TO BS1064 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED NEW L/H SKATE ANGLE IAW DWG# 148A8300 AND IAW DWG# 148A3590

Part: CARGO TRACK — BENT (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

BENT RAIL AT AFT CARGO BAY BS 787 RBL 8 WL 156. REPAIRED ACB RAIL BETWEEN BS 779 TO BS 800 RBL 8 WL 156, PER SRM 53-00-53-2R-2 REPAIR 2.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS807 LBL22 WL156. / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 - BS 807 LBL 22; WL 156; MAX MATERIAL REMOVED IN AREA 1.7' X 1.1' X MORE THAN 50% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT P/N 146A7502-1 IAW SRM 51-40-02. DWG 146A7500 AND DWG 149A8102

Part: FRAME — DENTED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

DENT ON FRAME AT AFT CARGO BAY BS 827 LBL 26 WL 162. REPAIRED FRAME BS 827 BETWEEN STR 24L AND 25L, PER SWA EA 20-153-02325 REV IR (ATS ER 20-03550 REV IR).

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS767 RBL22 WL156. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BETWEEN BS 727-BS 767 RBL 22 WL 156 PER SRM 51-40-02 AND DWG 146A7500

Part: SUPPORT — DAMAGED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

FLOOR TO SIDEWALL SUPPORT HAS DAMAGE AT AFT CARGO BAY BS867 - BS887 RBL21 WL164. / REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 867-BS 887 EBL 21 WL 164. ITEM# 7535224 IAW SRM 53-00-53-01-2; SRM 53-00-53-1A-2; SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; DWG# 146A7500 57319U 11-05-20

Part: SHIELD — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL20 WL164. / REMOVED AND INSTALLED NEW AFT SHIELD AT AFT CARGO BAY BS847-BS 867 RBL 20 WL 164 ITEM# 7531255 IAW SRM 51-10-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG#145A8127; DWG# 146A0081 57319U 11-05-20

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS 727A-BS 727B LBL 17 WL 154. REMOVED AND REPLACED INTERCOSTAL 146A7505-3 AT AFT CARGO BAY BS 727A-BS 727B LBL 17 WL 154, IAW SRM 51-40-05 AND DWG 146A7500.

Part: FLOOR PANEL — BENT (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

BENT FLOOR PANEL SUPPORT AT AFT CARGO BAY BS794 RBL7 WL156. / REMOVED AND REPLACED FLOOR PANEL SUPPORT AT ACB BS794 RBL17 WL156 P/N 146A9401U42 PO# 806906 IAW SRM 51-40-02 AND AIPC 53-42-11-30 89004U 02NOV20

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS 807-BS 787 RBL 6 WL 153. REMOVED CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS 807-BS 787 RBL 6 WL 153 MEASURED 19' X 2.3' X .010'. ORIGINAL MATERIAL THICKNESS .045', FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-15-1A-1 STEP 4C (2) FIG 103. REMOVED AND REPLACED INTERCOSTAL P/N 146A8132-17, IAW SRM 51-40-02 AND DWG 146A8130.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,662 hrs · 30,458 cycles

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-27R WL 150, MARKED. ACCOMPLISHED STRINGER REPAIR, IAW SRM 53-00-03-2R-1 REPAIR 1.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS500D LBL23 WL157. / REMOVED & REPLACED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY FROM BS 400-BS 500D IAW DWG 143A7500 & SRM 51-40-02-0G-0

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 480 S-27L WL 152. REMOVED & REPLACED NEW STRINGER CLIP P/N 143A1010-11 AT FWD CARGO BAY BS 480 S-27L WL 152, IAW DWG 143A1220 & SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 WL157. / REMOVED AND INSTALLED FLOOR TO SIDEWALL SUPPORT AT FCB BS 400 BS 420 FROM BAC1496-444-7075T62C LOT# 1440365-1 LOCATED AND DRILLED IAW SRM 53-00-53-1A-2; SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; DWG 143A7501 AND DWG 143A7500 80641U 05NOV20

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 500B LBL 6 WL 152. REMOVED & REPLACED STRINGER CLIP AT FWD CARGO BAY BS 500B LBL 6 WL 152, IAW DWG 143A1223 & SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 500B RBL 6 WL 152. REMOVED & REPLACED NEW STRINGER CLIP P/N 143A1010-15 AT FWD CARGO BAY BS 500B RBL 6 WL 152, IAW DWG 143A1223 & SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 500C RBL 6 WL 152. REMOVED & REPLACED NEW STRINGER CLIP P/N 143A1010-15 AT FWD CARGO BAY BS 500C RBL 6 WL 152, IAW DWG 143A1224 & SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CRACKED (BS 500B) · airframe 57,662 hrs · 30,458 cycles

CRACKED INTERCOSTAL ATTACH ANGLE BS500B FWD SIDE RBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE BS 500B FWD SIDE RBL 25. WL 156. AS PER SRM 51-40-02-0G-0. AND DRAWING #143A7505; INTERCOSTAL ATTACH ANGLE WAS EVALUATED AND FOUND TO BE OUT OF LIMITS AS PER SRM 53-00-53-1A-2; PART REPAIRABLE BY REPLACEMENT AS PER SRM 51-70-02-0G-0 PARAGRAPH. 9.C.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON CLIPS AT FWD CARGO BAY BS 460-BS 470 LBL 6 WL 152. CLIPS AT FWD CARGO BAY BS 460 & 470 LBL 6 WL 152 DAMAGE WAS REPAIRED, INSPECTED & EVALUATED, PER EA-20-153-02261 REV IR DATED 11/20/2020 & ATS ER 20-63571 REV IR DATED 11/20/2020 REFER TO NRC U236936.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-26R WL 153, MARKED. REPAIRED CRACKED STRINGER AT BS 540 S-26R WL 153, PER SRM 53-00-03-2R-1 REPAIR 1.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON INTERCOSTAL SUPPORT CHANNEL AT BS 259-270 LBL 3-RBL 2 WL 208.1. REMOVED AND REPLACED SUPPORT CHANNEL AT BS 259-BS 270 LBL 3-RBL 2 WL 208.1, PER SRM 51-40-02; SRM 51-40-05 AND DWG 141A5210. REMOVED CORROSION ON SUPPORT CHANNEL MEASURED 8' X 3' X .007 FOUND TO BE OUT OF LIMITS, PER SRM 53-10-51-1A-1.

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 500C LBL 6 WL 152. REMOVED & REPLACED NEW STRINGER CLIP P/N 143A1010-15 AT FWD CARGO BAY BS 500C LBL 6 WL 152, IAW DWG 143A1224 & SRM 51-40-02-0G-0.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS440 - BS420 RBL23 WL157. / REMOVED AND REPLACED FWD SHIELD AT FWD CARGO BAY BS420-440 RBL23 WL157 AS PER SRM 51-40-02-0G-0 AND DRAWING # 143A0080; SHIELD WAS EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMIT ON SRM AS PER SRM 53-00-53-1A-2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,662 hrs · 30,458 cycles

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-26L WL 153, MARKED. REPAIRED STR 26L STA 510-540 WL 153, PER SRM 53-00-03-2R-1, SRM 51-40-02; SRM 51-20-01, SOPM 20-41-02 AND DWG 143A3241. 91195U 11-8-20.

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 500 LBL 6 WL 152. REMOVED & REPLACED NEW STRINGER CLIP P/N 143A1010-15 AT FWD CARGO BAY BS 500 LB 6 WL 152, IAW DWG 143A1221 & SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — BENT (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

BENT INTERCOSTAL AT FWD CARGO BAY BS 500B-BS 500C RBL 24 WL 156. REMOVED AND REPLACED INTERCOSTAL AT FCB BS 500B TO BS 500C RBL 24 WL 156, AS PER SRM 51-40-02-0G-0 AND DRAWING NR 143A7505. INTERCOSTAL WAS EVALUATED AND FOUND TO BE OUT OF LIMITS, AS PER SRM 53-00-53-1A-2. PART REPAIRABLE BY REPLACEMENT, AS PER SRM 51-70-02-0G-0 PARAGRAPH 9C.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 57,662 hrs · 30,458 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / DAMAGE FOUND ON FCB GUSSET BS500D STR-19L FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACMENT IAW SRM 51-10-02-0G-0 PAR-9C LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-05-0G-0 AND INSTALLED IAW BOE.DWG #143A7902 REV-E

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 57,662 hrs · 30,458 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / DAMAGE FOUND ON FCB GUSSET BS 500D STR- 19R FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL REPAIRE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-05-0G-0 AND INSTALLED IAW BOE. DRW.# 143A7902 REV-E

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500D - BS500A RBL23 WL157. / REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT AT FCB BS 500D-500A RBL 23 WL 157 AS PER SRM 51-40-02-0G-0 AND DRAWING #143A7500; SIDEWALL SUPPORT WAS EVALUATED AND FOUND TO BE OUT OF LIMITS AS PER SRM. 53-00-53-1A-2. PARAGRAPH. 4A. FIG.103 DETAIL 'D'. MAX MATERIAL REMOVED IT'S MORE THAN 50% OF ALLOWABLE LIMIT

Part: STRINGER CLIP — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS 500A LBL 6 WL 152. REMOVED & REPLACED NEW STRINGER CLIP P/N 143A1010-15 AT FWD CARGO BAY BS 500A LBL 6 WL 152, IAW DWG 143A1222 & SRM 51-40-02-0G-0.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 57,662 hrs · 30,458 cycles

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL157. / REMOVED AND INSTALLED ON AFT SHIELD AT FCB BS500-BS500A RBL23 ITEM 7531855 PO# 806203 IAW SRM 51-40-05; SRM 51-40-02; DWG 143A8126 AND DWG 143A0080 80641U 03NOV20

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 57,662 hrs · 30,458 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4-LBL 14 WL 207.54. REPAIRED FLIGHT DECK FLOOR AT BS 255 RBL 4-LBL 14 WL 207.54, PER EA NO.1-A53-33179 REV 1 DATE 28MAY2019.

Part: TRIM PANEL — MISSING (R2 DOOR SLIDE) · airframe 57,658 hrs · 30,457 cycles

AFT SERVICE DOOR EMERGENCY SLIDE COMPARTMENT OUTER TRIM CORNER MISSING. REMOVED AND REPLACED TRIM CORNER, PER SRM 51-40-02.

Part: FUSE — INOPERATIVE (CABIN) · airframe 56,626 hrs · 29,808 cycles

** L/H OVER WING EXIT AFT EGRESS LIGHT INOP / REPLACED FUSE IN EMERGENCY LIGHT BATTERY POWER CHARGER M1670; L/H OVERWING EXIT AFT EGRESS LIGHT OPS CHECK GOOD; PER AMM TASK 33-51-06-960-804 AND WDM 33-51-22.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,626 hrs · 29,808 cycles

** L/H AND R/H EGRESS LIGHTS AFT OF WINGS INOP / TROUBLESHOOTING; LAMP REPLACEMENT; WIRE REPAIR; OPS CKS AND CLOSE UP FOR L/H AND R/H EGRESS LIGHTS AFT OF WINGS IAW AMM(S) 25-21-45; 25-21-46; 33-51-00 WDM 33-51-13; SWPM 20-30-12 OPS CK GOOD AND AMM 33-51-04

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,626 hrs · 29,808 cycles

***CORROSION*** ON BULKHEAD SUPPORT BS 947 WL170 LBL 10 / BULKHEAD SUPPORT BS 947 WL 170 LBL 10 CORRODED FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0 STEP 9 REMOVED DAMAGE PART AND INSTALLED NEW PART IAW SOPM 20-50-01 RECEIVED PART 7532170 P.O. 787648 & DWG 149A8117.

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 56,529 hrs · 29,759 cycles

FWD ENTRY DOOR LOWER EMER EXIT LIGHT LENS MISSING DIRECTIONAL ARROW INSTALLED NEW EXIT SIGN ON FWD ENTRY DOOR WITH DIRECTIONAL ARROW REF AMM 33-51-01

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 56,529 hrs · 29,759 cycles

FWD SERVICE DOOR LOWER EMER EXIT LIGHT LENS MISSING DIRECTIONAL ARROW INSTALLED NEW DIRECTIONAL SIGN BY FWD SERVICE DOOR REF AMM 33-51-01

Part: INDICATOR — STUCK (FLAP SYSTEM) · airframe 55,842 hrs · 29,335 cycles

DECLARED EMERGENCY, FLAPS STUCK AT 5 DEG DURING LANDING CONFIGURATION. RAN FLAP DISAGREE CHECKLIST AND LANDED FLAPS 15. R&R FLAP POSITION INDICATOR PER AMM.

Part: TRANSMITTER — STUCK (TE FLAPS) · airframe 55,842 hrs · 29,335 cycles

DECLARED EMERGENCY, FLAPS STUCK AT 5 DEG DURING LANDING CONFIGURATION. RAN FLAP DISAGREE CHECKLIST AND LANDED FLAPS 15. R&R LEFT NR 1 FLAP POSITION TRANSMITTER IAW AMM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 54,820 hrs · 28,711 cycles

L1 DOOR GIRT BAR HARD TO DISARM. / REPAIRED GIRT BAR ASSEMBLY PER EA.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,766 hrs · 28,673 cycles

L/H AFT EMERGENCY LIGHT INOP. / RESET CONNECTOR PER AMM.

Part: COVER — UNSECURE (CABIN) · airframe 54,414 hrs · 28,453 cycles

LT OVERWING EXIT SIGN LIGHT FELL OFF. R&R OVERWING EXIT SIGN COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,999 hrs · 28,199 cycles

L1 DOOR ESCAPE SLIDE OUT OF POSITION. / REPOSITIONED SLIDE PER MT.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 53,931 hrs · 28,159 cycles

AFT CARGO BAY AFT SCUFF PLATE IS CRACKED / REPLACED AFT CARGO BAY AFT SCUFF PLATE. LOCATED AND DRILLED NEW AFT CARGO BAY AFT SCUFF PLATE PER REF AMM 53-11-02-020-801 AND AMM 53-11-02-420-801.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 53,931 hrs · 28,159 cycles

AFT CARGO BAY FWD SCUFF PLATE IS CRACKED / REMOVED AND REPLACED AFT CARGO BAY FWD SCUFF PLATE IAW AMM TASK 53-11-02-020-801 AND AMM TASK 53-11-02-420-801.

Part: LIGHT — CRACKED (CABIN) · airframe 53,931 hrs · 28,159 cycles

EMERGENCY EXIT LIGHT COMMON TO THE FORWARD GALLEY CRACKED. R&R LIGHT IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 53,931 hrs · 28,159 cycles

EMERGENCY EXIT LIGHT COMMON TO THE FORWARD LAV CRACKED. R&R LIGHT IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 53,931 hrs · 28,159 cycles

FORWARD CARGO BAY AFT SCUFF PLATE IS CRACKED / REMOVED FCB AFT CUFF PLATE IAW AMM 53-11-02; LOCATED & DRILLED SCUFF PLATE IAW SRM 51-40-05. INSTALLATION OF SCUFF PLATES WILL BE ACCOMPLISHED ON CUSTOMER CARD # 753-140-00-01Y

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 794.3 TO BS. 837, RBL 24. R&R WEB IAW SRM AND DWG.

Part: NUT PLATE — CORRODED (AFT CARGO BAY) · airframe 53,931 hrs · 28,159 cycles

***CORROSION*** NUTPLATE STRAP ON LOWER SURFACE OF INTERCOSTAL BS 787+8 TO 787+15 RBL 21; WL 156 HAS CORROSION. / REMOVED AND REPLACED NUTPLATE STRAP ON LOWER SURFACE OF INTERCOSTAL BS 787+8 TO 787 H5 RBL21; WL156 PER SRM 51-40-02 AND DWG 146A8340. 59503U 13MAY19

Part: SKIN — DELAMINATED (RT WING) · airframe 53,931 hrs · 28,159 cycles

2 EACH DISBONDS FOUND ON THE #7 SPOILER. DISBONDED AREAS CIRCLED IN RED / REPAIRED 2 EACH DISBONDS ON THE #7 SPOILER IAW SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0

Part: FITTING — DAMAGED (R1 DOOR) · airframe 53,931 hrs · 28,159 cycles

R1 DOOR GIRT BAR FITTINGS DAMAGED. INSTALLED FITTING IAW AMM.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

PANEL 193AL OUTER SKIN HAS LARGE DISBONDED DENT JUST BELOW 'WARNING'. (MARKED) / PANEL 193AL OUTER SKIN WITH LARGE DISBONDED DENT JUST BELOW 'WARNING' AS MARKED WAS REPAIRED PER SWA EA# 1-753-34858 REV#1 DATED 20-MAY-2019 AND ATS ER# 19-03107 REV A DATED 20-MAY-2019.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 53,931 hrs · 28,159 cycles

VERTICAL PRESSURE WEB LOWER ATTACH ANGLE CRACKED AT BS. 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE IAW ER AND EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 53,931 hrs · 28,159 cycles

VERTICAL PRESSURE WEB CRACKED AT BS. 633, LBL 35. REPAIRED WEB IAW ER AND EA.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 53,931 hrs · 28,159 cycles

PANEL 343AT SHARK FIN CRACKED / REMOVED & REPLACED BLADE SEAL IAW SRM 51-40-02 & IPC 55-10-52; PANEL 242AT

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

INTERCOSTAL UPPER SURFACE UNDER FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 827 TO BS. 847, LBL 24. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

INTERCOSTAL UPPER SURFACE UNDER FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727A TO BS. 727B, RBL 24. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

INTERCOSTAL UPPER SURFACE UNDER FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727A TO BS. 727B, LBL 24. R&R INTERCOSTAL PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

INTERCOSTAL UPPER SURFACE UNDER FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 747 TO BS. 767, RBL 24. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

INTERCOSTAL CRACKED BETWEEN BS. 328 TO BS. 344, LBL 47. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 53,931 hrs · 28,159 cycles

CRACKED INTERCOSTAL AT B.S. 312-328; L.B.L 47; W.L. 208.1. / REMOVED AND REPLACED INTERCOSTAL AT BS 312-BS328 LBL 47; WL 208.1 IAW SRM 57-40-02-0G-0 DWG 141A5400

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

INTERCOSTAL CRACKED AT FASTENER HOLE BETWEEN BS. 277 TO BS. 294.5, RBL 1. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

MOPSILL CORRODED BETWEEN BS. 277 TO BS. 360, LBL 60. R&R MOPSILL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FORWARD ENTRY DOOR INBOARD THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS. 312 TO BS. 344, LBL 60. R&R ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, CABIN FLOOR PANEL 241ADF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. BS. 887 TO BS. 1016). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, FORWARD CABIN FLOOR PANEL 221EF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 270 TO BS 420). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, AFT CABIN FLOOR PANEL 242UF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 887 TO BS. 1016). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, FORWARD CABIN FLOOR PANEL 222CF DAMAGED UPPER SURFACE PLIES, (BETWEEN BS. 270 TO BS. 420). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, AFT CABIN FLOOR PANEL 242TF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 887 TO BS. 1016). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, AFT CABIN FLOOR PANEL 241XF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 887 TO BS. 1016). REPAIRED FLOOR PANEL PER SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

CABIN FLOOR PANEL SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 20. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, CABIN FLOOR PANEL 241ABF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 887 TO BS. 1016). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 53,931 hrs · 28,159 cycles

FWD CABIN FLOOR PANEL 221GF FWD O/B TANG BROKEN / FWD CABIN FLOOR PANEL 221GF WITH FWD O/B TANG BROKEN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE. IAW SRM 51-10-02-0G-0. PARA 9.A.(1)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, FORWARD CABIN FLOOR PANEL 222DF DAMAGED UPPER SURFACE PLIES, (BETWEEN BS. 270 TO BS. 420). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, FORWARD CABIN FLOOR PANEL 221CF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 270 TO BS. 420). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,931 hrs · 28,159 cycles

SUPPLEMENTAL INFORMATION, CABIN FLOOR PANEL 242VF UPPER SURFACE PLIES DAMAGED, (BETWEEN BS. 887 TO BS. 1016). REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 53,931 hrs · 28,159 cycles

FWD CABIN FLOOR PANEL 221BF AFT O/B TANG BROKEN / DUE TO EXTENT OF DAMAGE ON PANEL 221BF; REPLACED PANEL IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 53-21-00-19B ITEM 45

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FORWARD CARGO BAY INTERCOSTAL CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 6. R&R INTERCOSTAL PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FORWARD CARGO BAY L/H FLOOR-TO-SIDEWALL SUPPORT CORRODED BETWEEN BS. 440 TO BS. 480, LBL 24. INSTALLED SUPPORT PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED AT BS. 767+3, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FRAME CRACKED AT BS. 727A, STR. 8R. REPAIRED FRAME PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. R&R SUPPORT IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 53,931 hrs · 28,159 cycles

***CORROSION*** AT FLOOR SUPPORT STRAP BS 767 +5 RBL 20 TO LBL 20 / RECEIVED NEW SERVICEABLE PART. PART TO BE INSTALLED ON JPANEL-141-CLOSE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

AFT CARGO BAY AFT SHIELD CORRODED AT BS. 847 +8, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

AFT CARGO BAY LAV BULKHEAD GUSSET CRACKED ON LOWER END AT BS. 867, LBL 11. R&R GUSSET IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 53,931 hrs · 28,159 cycles

CARGO BAY FLOOR TRACK CORRODED AT BS. 927+7, RBL 13. R&R FLOOR CARGO TRACK PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 22. REPAIRED SUPPORT PER SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 53,931 hrs · 28,159 cycles

***CORROSION*** AT FLOOR SUPPORT STRAP BS 887 RBL 20 TO LBL 9 / REMOVED AND REPLACED FLOOR SUPPORT STRAP WITH NEW; PER DWG 146A7500; DWG 147A7500; SRM 51-40-02

Part: RETAINER — CRACKED (LEFT WING) · airframe 53,931 hrs · 28,159 cycles

VERTICAL BULB SEAL RETAINER IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE NO.1 PYLON. MARKED / REMOVED AND REPLACED VERTICAL BULB SEAL RETAINER AT LEFT WING FIXED T/E PANEL JUST AFT OF THE NO. 1 PYLON. P/N. 115A2953-1 IAW. SRM 51-40-02 AND AIPC. 57-50-00-25 88920U 26APR19

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 53,931 hrs · 28,159 cycles

***CORROSION*** AT AFT CENTER LWR BULKHEAD SUPPORT BS 947 RBL 19 TO LBL 10 / REMOVED EXISTING BULKHEAD SUPPORT AT STA 947 RBL 19- LBL 10; REPLACED WITH NEW BULKHEAD SUPPORT PN 149A8118-30 IAW SRM 51-40-02; DWG 149A8117 59230C 07MAY19

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FRAME CRACKED AT BS. 787, STR. 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FLOORBEAM CORRODED AT BS. 987, BETWEEN LBL 44 TO RBL 44. REPAIRED FLOORBEAM IAW ER AND EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 24. R&R SHIELD PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,931 hrs · 28,159 cycles

FORWARD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 24. R&R SUPPORT IAW DWG & SRM.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 53,931 hrs · 28,159 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L. 36; W.L. 154. / L/H VAPOR BARRIER INSTALLED ON NRC T913482. 91195U 5-4-19

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 53,931 hrs · 28,159 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L. 30; W.L. 148. / L/H VAPOR BARRIER INSTALLED ON NRC T913482. 91195U 5-4-19

Part: SKIN — CRACKED (LE SLAT) · airframe 53,931 hrs · 28,159 cycles

LT WING #1 LEADING EDGE SLAT NOSE SKIN CRACKED AROUND THE FASTENER AT WSTA. 434+8. REPAIRED #1 SLAT SKIN IAW EA AND ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,931 hrs · 28,159 cycles

RT STOW BIN EMERGENCY LIGHT INOP AT ROW 7. R&R LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,910 hrs · 28,146 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,763 hrs · 28,061 cycles

LT EMERGENCY SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,704 hrs · 26,221 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING RED ARROW ON COVER AT LOWER AREA. R & R THE LENS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,613 hrs · 25,595 cycles

LT FORWARD EMERGENCY BATTERY PACK FAILED TIME TEST. R&R BATTERY PACK PER AMM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 48,935 hrs · 25,177 cycles

AFT PRESSURE BULKHEAD AFT SIDE WEB OIL CANNING AT BS 1016, BETWEEN STR 2L TO STR 3L. REPAIRED WEB PER EA AND SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 48,156 hrs · 24,685 cycles

L1 DOOR SLIDE OUT OF POSITION. POSITIONED THE SLIDE IAW TC.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 47,644 hrs · 24,383 cycles

FORWARD P5 OVERHEAD PANEL THE EMERGENCY EXIT LIGHT SWITCH GUARD BROKEN. R & R SWITCH GUARD IAW SOPM.

Part: FRAME — CRACKED (BS 727) · airframe 47,644 hrs · 24,383 cycles

FRAME CRACKED AT BS 727, WL 200. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727) · airframe 47,644 hrs · 24,383 cycles

RIGHT LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED THE FRAME IAW EA.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 47,644 hrs · 24,383 cycles

LEFT WING NR 2 LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB CRACKED. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 47,644 hrs · 24,383 cycles

RIGHT WING NR 7 LEADING EDGE SLAT NOSE SKIN LOWER SURFACE ACTUATOR ATTACH RIB CRACKED AT SLAT STATION 322.71. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 47,644 hrs · 24,383 cycles

RIGHT WING NR 5 LEADING EDGE SLAT NOSE SKIN ACTUATOR RIB CRACKED AT SLAT STATION 85.19. REPAIRED THE SLAT SKIN IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,789 hrs · 23,856 cycles

RIGHT OVERWING EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,360 hrs · 21,938 cycles

AFT GALLEY EXIT SIGN LIGHT BROKEN. R & R SIGN IAW SIP.

Part: RADIO ALTIMETER — FAULTY (COCKPIT) · airframe 42,914 hrs · 2,672 cycles

AIR TURN BACK, AFTER TAKEOFF AT FLAPS 5 WITH GEAR UP CONFIGURE WARNING SOUNDED. RECYCLED GEAR CONFIG WARNING HORN OFF AT ALL THRUST SETTING WITH GEAR DOWN. R & R NR 2 RADIO ALTIMETER IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,390 hrs · 20,812 cycles

R1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,377 hrs · 20,806 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 41,006 hrs · 20,604 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE IAW MT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,258 hrs · 20,178 cycles

STRINGER CRACKED AT BS 440, STRINGER 21R. REPAIRED STRINGER IAW EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,258 hrs · 20,178 cycles

SKIN CRACKED AT BS 420, BETWEEN STRINGER 20R - 21R. R & R SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,608 hrs · 19,219 cycles

LEFT EMER EXIT LIGHT LOWER FWD BULB INOPERATIVE. RELAMPED IAW MM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

FORWARD CARGO BAY BAFFLE UNDER LT FLOOR TO SIDEWALL SUPPORT CRACKED BETWEEN BS 500C TO BS 500D. R & R BAFFLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L TO STRINGER 9L. REPAIRED FRAME IAW EA.

Part: LENS — DIRTY (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

L2 DOOR EXTERIOR EMER EXIT LIGHT LENS DIRTY. CLEANED LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

RIGHT OVERWING EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

R2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

FORWARD CARGO BAY BAFFLE UNDER LT FLOOR TO SIDEWALL SUPPORT BETWEEN BS 500B TO BS 500C CRACKED. R & R BAFFLE SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: LENS — DIRTY (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

FORWARD ENTRY DOOR EXTERIOR EMER EXIT LENS DIRTY. RELAMPED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

LEFT OVERWING EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: LIGHT — FAULTY (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

FORWARD ENTRY DOOR EXTERIOR EMER EXIT LIGHT FAULTY. RELAMPED LIGHT IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

FORWARD CARGO FLOOR SUPPORT CORRODED AT STATION 500D, LBL 25. R & R SUPPORT IAW SRM.

Part: LENS — DIRTY (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

LEFT OVERWING EXTERIOR EMER EXIT LIGHT LENS DIRTY. R & R LENS IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

L2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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

Part: LENS — DIRTY (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

RIGHT OVERWING EXTERIOR EMER EXIT LIGHT LENS DIRTY. R & R LENS IAW MM.

Part: CONVERTER — FAILED (CABIN) · airframe 38,608 hrs · 19,220 cycles

R1 DOOR OVERHEAD EMER EXIT LIGHT BATTERY AT BS 318, RBL 38 FAILED TEST. R & R CONVERTER D40042J IAW MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

STRINGER CLIP CORRODED AT BS 396, LBL 6. R & R CLIP IAW SRM & DWG.

Part: LENS — DIRTY (EXTERIOR) · airframe 38,608 hrs · 19,220 cycles

R2 DOOR EXTERIOR EMER EXIT LIGHT LENS DIRTY. R & R LENS IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,608 hrs · 19,220 cycles

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