N7836A

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 67,428 hrs · 30,675 cycles

FIRE WARNING LIGHT ILLUMINATES ON MASTER CAUTION RECALL ON BOTH SIDES WITH NO OTHER FIRE INDICATIONS / [01] RR CAPTAINS FIE WARNING LIGHT ASSY IAW MM 33-18-00

Part: SLIDE — OUT OF POSITION (AFT SERVICE DOOR) · airframe 67,234 hrs · 30,555 cycles

AFT SERVICE DOOR DROPPED FROM CASE / [01] INSP AFT SERVICE DOOR SLIDE AND ADJ BACK INTO CASE AS PER AMM 25-66-01

Part: PANEL — DAMAGED (FUSELAGE) · airframe 66,351 hrs · 29,985 cycles

PANEL 193B HAS SEVERAL ELONGATED HOLES / [01] REMOVED AND REPLACED PANEL PER SRM 51-40-02;[02] C/W INSPECTION

Part: GUARD — DAMAGED (LIGHT SWITCH) · airframe 66,351 hrs · 29,985 cycles

AFT GALLEY ATTENDANT LIGHT PANEL EMERGENCY EXIT LIGHT SWITCH GUARD IS DAMAGED. / [01] REMOVED AND REPLACED AFT GALLEY ATTENDANT LIGHT PANEL EMERGENCY EXIT LIGHT SWITCH GUARD IAW CMM 33-11-05.

Part: LIGHT — CORRODED · airframe 65,505 hrs · 29,478 cycles

EMERGENCY LIGHT OVER ROW 9ABC INOP ; / [01] OK FOR SERVICE PER MEL 33-15-02 SP1B. AUTHORIZATION 46865; [02] REMOVED AND REPLACED PACK CHARGER ASSY AND BATTERY PACK PER AMM 33-51-06. OPS. CHECK GOOD .

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 64,993 hrs · 29,186 cycles

CORROSION SUPPORT BRACKET LOCATED ON DOOR 315A AFT POSITION ON APU COMPARTMENT ; 2021-496960 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [02] REPLACED SUPPORT BRACKET LOCATED ON DOOR 315A AFT POSITION ON APU COMPARTMENT IAW B737-700 SRM 51-40-02; DWG 148A6355 REV: E AND DWG 148A6350 REV: A.; SRM 51-10-02 MATERIAL USED: ALUMINUM SHEET 2024T0 (0.050?) SEE INDIVIDUAL SIGNOFFS BELOW; [03] COMPLETE TASK CERTIFIED

Part: BRACKET — CORRODED (FUSELAGE) · airframe 64,993 hrs · 29,186 cycles

CORROSION SUPPORT BRACKET LOCATED ON DOOR 315A FWD POSITION ON APU COMPARTMENT ; 2021-496959 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [02] REPLACED SUPPORT BRACKET LOCATED ON 315A FWD POSITION ON APU COMPARTMENT MATERIAL USED ALUMINUM SHEET 2024T0 (0.050?); P.O. 2020-202345; SEE INDIVIDUAL SIGNOFFS BELOW; [03] REPLACED SUPPORT BRACKET LOCATED ON 315A FWD POSITION ON APU COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-09 AND DWG 148A6355 REV: E AND 148A6350 REV: A. MATERIAL USED ALUMINUM SHEET 2024T0 (0.050?); P.O. 2020-202345; SEE INDIVIDUAL SIGNOFFS BELOW; [04] COMPLETE

Part: ACCESS PANEL — ELONGATED (FUSELAGEQ) · airframe 64,975 hrs · 29,174 cycles

ELONGATED HOLE ACCESS PANEL 671BB TRAILING EDGE AT RT WING ; 2021-496921 / [01] TOOL USED : CALIPER P/N:500-197-30 S/N:A18229508 DUE DATE: 29-SEP-22; [02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 11/DEC/21.; [03] REPAIRED ACCESS PANEL 671BB TRAILING EDGE AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REP.9 TOOL USED SCALE PN:CL5000 SN: AE-37099 DUE DATE: 16/AUG/22; SCALE PN:CL5000 SN: AE-408753 DUE DATE: 19/MAR/22. SEE INDIVIDUAL SIGNOFFS BELOW; [04] TASK COMPLETED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 847 AND BS 727 S-25L AT WL 156 AFT CARGO COMPARTMENT ; 2021-496919 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 847 AND BS 727 S-25L AT WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 53-00-53-2R-6 REPAIR 6 AND DWG #146A7500; SHEET: 1; REV: B AND DWG #146A7502; SHEET: 1; REV: A<BR>MATERIAL USED P/N: BAC1496-377; PO: 2021 218987 1<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW; [02] COMPLETE TASK CERTIFIED RII

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 64,975 hrs · 29,174 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AFT CARGO COMPARTMENT ; 2021-496918 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG #146A7500 REV A. MATERIAL USED: BAC1496-377 P/O: 2021-218987. SEE INDIVIDUAL SING-OFF BELOW; [02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG #146A7500 RII CERTIFIED

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 64,975 hrs · 29,174 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS 807 AT LEVEL S-25R AFT CARGO COMPARTMENT ; 2021-496920 / [01] INSTALLED ANGEL-SUPPORT LOC. AT BS807 AT LEVEL STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 DWG 146A8120 SHEET 10 REV A PART USED:146A8125-9; [02] INSTALLED ANGLE-SUPPORT LOC. AT BS807 AT LEVEL STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 DWG 146A8120 SHEET 10 REV A PART USED:146A8125; [03] CORRECTED STEP 1; STEP2: INSTALLED ANGLE-SUPPORT LOC. AT BS807 AT LEVEL STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 DWG 146A8120 SHEET 10 REV A PART USED:146A8125; SEE INDIVIDUAL SIGNOFFS BELOW; [04] COMPLETE TASK CERTIFIED RII

Part: PLATE — CRACKED (L/H WING) · airframe 64,975 hrs · 29,174 cycles

CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 230 AT LT WING (1EA) ; 2021?496886 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 230 AT LT WING (1EA) IAW SRM B737-700 51-40-02 AND DWG 115A2001 REV B<BR>SEE INDIVIDUAL SIGNOFFS BELOW.; [02] VERIFIED TASK COMPLETE

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

DELAMINATED FLOOR PANEL 231YF AT PASSENGER CABIN ; 2021-496888 / [01] REPAIRED FLOOR PANEL 231YF AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.; [02] JOB COMPLETED. RII INSPECTION COMPLETED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CRACKED STRINGER 25R AND BS540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 25R BETWEEN BS 500C AND BS540 IAW SRM B737-700 SRM 53-00-03-2R-1; FIG 206.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

DELAMINATED FLOOR PANEL 242BF AT PASSENGER CABIN ; 2021-496887 / [01] REPLACED FLOOR PANEL 242BF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-1A-1; [02] COMPLETE TASK CERTIFIED

Part: PANEL — ELONGATED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

SUPPLEMENTAL INFORMATION: ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT ; 2021-496867 / [01] REPLACED ACCESS PANEL 141 JW AFT CC FABRICATED WITH MATERIAL A60SG4W 60144 PO# 2021-19183600101 IAW B737-700 AMM 25-52-01-201-801-NG AND DWG 25453A2510 REV:G; [02] COMPLETE TASK CERTIFIED

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CRACK ON STRINGER 26R, BS540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 26R AND BTW BS 500D TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1; FIG 206.

Part: LIGHT — DETERIORATED (CABIN) · airframe 64,975 hrs · 29,174 cycles

SUPPLEMENTAL INFORMATION: DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) ; 2021-496663 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 SOPM 20-50-12 DWG 33500007 REV.2; [02] COMPLETED

Part: NONE — MISSING (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

SUPPLEMENTAL INFORMATION: CUSTOMER REQUEST MISSING STUB 4 E/A ON ACCESS PANEL 121LW LOCATED AT FWD CARGO COMPARTMENT ; 2021-496784 / [01] INSTALLED STUB 4 EA LOCATED ON ACCESS PANEL 121LW LOCATED AT FWD CARGO COMPARTMENT; [02] INSTALLED STUB 4 EA LOCATED ON ACCESS PANEL 121LW LOCATED AT FWD CARGO COMPARTMENT IAW SRM 51-40-02; [03] CERTIFIED WORK PERFORMED

Part: FLOOR PANEL — ELONGATED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

SUPPLEMENTAL INFORMATION: CUSTOMER REQUEST ELONGATED HOLES 25 E/A LOCATED ON ACCESS PANEL 140AF LOCATED AT AFT CARGO COMPARTMENT. ; 2021-496763 / [01] FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT; FROM MATERIAL:2024-T3 CLAD ALUMINUM SHEET; P/N:2024-T3 0.071; P/O:2021-111049; IAW B737-700 AMM 25-52-01-201-801; DWG:453A2610-8;SHEET:8; REV: D.; [02] CERTIFIED WORK PERFORMED

Part: FLOOR PANEL — ELONGATED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

ELONGATED HOLES 18 E/A ON ACCESS PANEL 140BF LOCATED AT AFT CARGO COMPARTMENT. FABRICATE FLOOR PANEL 140BF IAW AMM 25-52-01-201-801, & DWG 453A2610-7, SHEET 7, REV C.

Part: ACCESS PANEL — CRACKED (L/H HORIZ. STAB.) · airframe 64,975 hrs · 29,174 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB ; 2021-496780 / [01] REPLACED SEAL-PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-40-02; [02] VERIFIED TASK COMPLETE

Part: ACCESS PANEL — CRACKED (R/H HORIZ. STAB.) · airframe 64,975 hrs · 29,174 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB ; 2021-496744 / [01] REPLACED SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STABILIZER IAW SRMB737-700 51-40-02; [02] VERIFIED TASK COMPLETE

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CRACK ANGLE VERTICAL LOCATED BS 695 BL0 AND WL 208.1 AT PASSENGER CABIN. REPLACED ANGLE VERTICAL LOCATED BS 695 BL0 AND WL 208.1 AT PASSENGER IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 3 REV-.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CRACK ANGLE LOCATED BS 540 ; BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN ; 2021-496765 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 540 BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; [02] CORRECTIVE ACTION 1 CORRECTED <BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 540 BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 <BR>SEE INDIVIDUAL SING-OFFS BELOW; [03] CERTIFIED WORK PERFORMED RII<BR>SEE INDIVIDUAL SIGNOFFS BELLOW

Part: WEB — CRACKED (CABIN) · airframe 64,975 hrs · 29,174 cycles

SUPPLEMENTAL INFORMATION: CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT STA 663 PLUS 8 INCHES AND RBL 42; CENTER PAX CABIN. CRACK LENGTH 0. 300 INCHES APPROX. ; 2021-496552 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 01-DEC-21; [02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 01-DEC-21; [03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22; [04] PERFORMED PERMANENT REPAIR ON PRESSURE WEB LOC BTW BS 663 TO BS 675 AND BTW RBL 30 TO RBL 60 I.A.W. B737-700; SRM 53-40-51-2R-2; REPAIR 2.<BR>SEE INDIVIDUAL SIGNOFFS BELOW; [05] CERTIFIED WORK PERFORMED RII<BR>SEE INDIVIDUAL SIGNOFFS BELLOW

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CUSTOMER REQUEST CORROSION ON AFT EXTERNAL SKIN BS1016 AND BTW STR 23L TO STR 25L LOWER FUSELAGE ; 2021-496476 / [01] TOOL USED ULTRASONIC EQUIPMENT PN: 25DLPLUS; SN: 071504410; DUE DATE: 20-NOV-21; [02] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULTS TTG8Q0093TQ1 AND TTG8Q0093TQU; [03] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULTS TTG8Q0093TQ1 AND TTG8Q0093TQU

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 64,975 hrs · 29,174 cycles

CRACK FRONT SPAR INSPAR RIB STAB STA 101.90 LOCATED AT 38 INCHES RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOC. ON INSPAR RIB STAB STA 101.90; AT 38 INCHES FROM FRONT WEB RT HORIZONTAL STABILIZER. I.A.W B737-700 SRM 51-40-02 AND SRM 55-10-09-2R-4 REPAIR 4; ITEM 4; FIGURE 202;SHEET 1. MATERIAL USED. ANGLE P/N: BAC1490-2738; P/O: 2021-185455; PROFILE P/N: BAC1505-101208; P/O: 2021-187268; SHEET P/N: 7075-T6 0.010; P/O: 2021-552973.

Part: DOUBLER — CRACKED (GROUND POWER DOO) · airframe 64,975 hrs · 29,174 cycles

CRACK ON INTERNAL DOUBLER SKIN, BS 277, 4 INCH ELECTRICAL GROUND POWER RECEPTACLE LOWER FUSELAGE. REPAIRED SKIN IAW SRM 53-10-15-2R-5 REPAIR 5.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,975 hrs · 29,174 cycles

CRACK ON SURROUND DOUBLER LOWER POSITION BTW BS277 TO BS235 ELECTRICAL GROUND POWER RECEPTACLE LOWER FUSELAGE. PERFORMED PERMANENT REPAIR AT SURROUND DOUBLER OF EPGR LOWER POSITION BTW BS277 TO BS235, WL 175 IAW SRM 53-10-15-2R-4 REPAIR 4 FIGURE 204 SHEETS 3; 4.

Part: ATTACH FITTING — DAMAGED (NR 1 NACELLE) · airframe 63,602 hrs · 28,377 cycles

#1 PYLON AFT O/B PRECOOLER ATTACH FITTING HAS DAMAGE TO THE BORE ; /

Part: ATTACH FITTING — DAMAGED (NR 1 NACELLE) · airframe 63,602 hrs · 28,377 cycles

#1 PYLON AFT O/B PRECOOLER ATTACH FITTING HAS DAMAGE TO THE BORE ; /

Part: LIGHT — DISLODGED (FWD GALLEY) · airframe 63,089 hrs · 28,065 cycles

FORWARD GALLEY EMERGENCY EIT LIGHT COVER FELL OFF. R & R FWD GALLEY R1 DOOR EMERGENCY EXIT LIGHT ASSY REF MM 33-51-01; OPS CK GOOD. OKAY FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,938 hrs · 27,973 cycles

EMERGENCY LIGHT INOPERABLE AT SEAT ROW 16DEF. RELAMPED EMERGENCY EXIT LIGHT AT SEAT ROW 16DEF, PER AMM 33-51-03.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 61,952 hrs · 27,370 cycles

EMERGENCY BATTERIES FAILED CAPACITY CHECK AT LOCTIONS M01669 AND M01672 / REMOVED AND REPLACED EMERGENCY BATTERIES AT LOCTIONS M01669 AND M01672 PER AMM 33-51-06

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 61,952 hrs · 27,370 cycles

FORWARD SERVICE DOOR ESCAPE SLIDE DISLODGED. REPOSITIONED SLIDE PER MT #725-61-06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,078 hrs · 26,240 cycles

M1670 EMERGENCY EXIT LIGHT DO NOT WORK. / REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1670 AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LIGHT BATTERY PACK M1670 AS PER AMM 33-51-06-960-805.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,078 hrs · 26,240 cycles

R/H OVER WING EXIT DOOR WINDOW LIGHT FWD EMERGENCY LIGHT IS OUT. / RELAMPED R/H OVERWING EXIT DOOR WINDOW LIGHT FWD EMERGENCY LIGHT AND PERFORMED GOOD TEST PER AMM 33-21-00-960-801.

Part: LIGHT — BROKEN (CABIN) · airframe 60,078 hrs · 26,240 cycles

EMERGENCY EXIT LIGHT HAS BROKEN BULB AFT LWR O/B FACE OF FWD LAV. / REPLACED BROKEN BULB ON EMERGENCY EXIT LIGHT AT AFT LWR O/B FACE OF FWD LAV AND PERFORMED GOOD TEST OF THE NEW LAMP PER AMM 33-51-01-960-801.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 60,078 hrs · 26,240 cycles

FWD CARGO BAY FWD SCUFF PLATE IS CRACKED / REMOVED AND INSTALLED NEW FWD CARGO BAY FWD SCUFF PLATE ITEM #7530065 IAW AIPC 53-13-00-08; AMM 53-11-02-420-801 OK TO INSTALL FROM CUSTOMER CARD # 753-140-00-01Y STEP 3. A1

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 60,078 hrs · 26,240 cycles

FWD CARGO BAY AFT SCUFF PLATE IS CRACKED / RECEIVED NEW FWD CARGO BAY AFT SCUFF PLATE ITEM # 7530065. INSTALLED ON CUSTOMER CARD #753-646-63-01

Part: FLASHLIGHT — DEFECTIVE · airframe 60,078 hrs · 26,240 cycles

AFT OUTBOARD FLASHLIGHT WILL NOT TURN OFF. / REMOVED AND REPLACED FLASH LIGHT ASSY AFT O/B IAW SOPM 20-50-01.

Part: SKIN — DEBONDED (SPOILER) · airframe 60,078 hrs · 26,240 cycles

FOUND DISBOND ON #5 SPOILER UPPER SURFACE. MARKED IN RED / REPAIRED DISBOND ON #5 SPOILER UPPER SURFACE PER SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-2.

Part: ANGLE — CRACKED (BS 294) · airframe 60,078 hrs · 26,240 cycles

ANGLE CRACKED AROUND AFT FASTENER OF VERTICAL FLANGE AT STA 294 + 1" WL 208, OTB SIDE OF INBD CREASE BEAM CHORD (MOP SILL) FWD LWR CORNER OF FSD SURROUND STRUCTURE. / INSTALLED NEW CLIP PN 141A8312-3 PER DWG 141A8310 AND SRM 51-40-02.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 60,078 hrs · 26,240 cycles

PANEL 193AL HAS A DELAMINATION ON THE INNER SURFACE SKIN / PANEL 193AL DELAMINATION ON THE INNER SURFACE SKIN WAS REPAIRED IAW SRM 51-70-05-2R-1. 56144U 10/24/2019.

Part: BLOCK — CORRODED (EMERGENCY LIGHT) · airframe 60,078 hrs · 26,240 cycles

GROUND BLOCK GD03810S (WITH WIRES) AT BS 1006 STRINGER 11 R/H IS CORRODED. / REMOVED AND REPLACED GROUND BLOCK GD03810S AS PER SRM 51-40-02-0G-0. PERFORMED DOOR WARNING SYSTEM TEST FOR THE AFT SERVICE DOOR AS PER AMM 52-71-00-730-801. OPERATIONAL TEST FOR EMERGENCY EXIT LIGHTS WILL BE PERFORMED ON T991308.

Part: SHIELD — CORRODED (BS 500-500A) · airframe 60,078 hrs · 26,240 cycles

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

Part: SUPPORT — CRACKED (BS 500D) · airframe 60,078 hrs · 26,240 cycles

FRAME TO STRINGER GUSSET SUPPORT CRACKED AT BS. 500D, STR. 19L. / R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 60,078 hrs · 26,240 cycles

AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. / R&R SUPPORT PER DWG AND SRM.

Part: SHIELD — CORRODED (BS 847-867) · airframe 60,078 hrs · 26,240 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 60,078 hrs · 26,240 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+7, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 60,078 hrs · 26,240 cycles

LOWER COMPOSITE BULKHEAD HORIZONTAL STIFFENER CRACKED AT BS. 663, LBL 9. / R&R STIFFENER IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,078 hrs · 26,240 cycles

FLIGHT DECK STRINGER CLIP CRACKED AT AFT SIDE OF BS. 259.5, STR. 8L. / R&R STRINGER CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,078 hrs · 26,240 cycles

L/H HORIZONTAL STABILIZER INSPAR #4 RIB STAB. STA. 120.3, STIFFENER #4 FROM FRONT CRACKED. / REPAIRED #4 RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 60,078 hrs · 26,240 cycles

R/H HORIZONTAL STABILIZER INSPAR #4 RIB STAB. STA. 120.3, STIFFENER #3 FROM FRONT CRACKED. / REPAIRED INSPAR #4 RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 60,078 hrs · 26,240 cycles

R/H HORIZONTAL STABILIZER INSPAR #1 RIB STAB. STA. 92.70, STIFFENER #2 FROM FRONT CRACKED. / REPAIRED #1 RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 60,078 hrs · 26,240 cycles

R/H HORIZONTAL STABILIZER INSPAR #1 RIB STAB. STA. 92.70, STIFFENER #3 FROM FRONT CRACKED. / REPAIRED #1 RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,078 hrs · 26,240 cycles

L/H HORIZONTAL STABILIZER INSPAR #4 RIB STAB. STA. 120.3, STIFFENER #3 FROM FRONT CRACKED. / REPAIRED INSPAR #4 RIB IAW EA AND ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 60,078 hrs · 26,240 cycles

R/H HORIZONTAL STABILIZER INSPAR #1 RIB STAB. STA. 92.70, #1 STIFFENER FROM FRONT CRACKED. / REPAIRED #1 RIB IAW SRM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 60,078 hrs · 26,240 cycles

LOWER COMPOSITE BULKHEAD VERTICAL STIFFENER CRACKED AT BS. 663, RBL 29. / R&R VERTICAL STIFFENER PER SRM AND DWG.

Part: BEAM — CRACKED · airframe 60,078 hrs · 26,240 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR #4 BEAM WAS REPAIRED ON WORK ORDER #527604.

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 48,524 hrs · 32,492 cycles

RAMP REPORTED TO CAPTAIN; LARGE TEAR IN AFT CARGO FLOOR PANEL 140CF / R & R AFT CARGO FLOOR PANEL IAW M/M 25-52-10 (140CF)

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 57,715 hrs · 24,715 cycles

L2 DOOR GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 57,005 hrs · 24,254 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 57,005 hrs · 24,254 cycles

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

Part: PANEL — DELAMINATED (LH PYLON) · airframe 56,971 hrs · 24,229 cycles

SUPPLEMENTAL INFORMATION: #1 ENG PYLON PANEL 43/ER LOWER FWD SIDE HAS 4' X 4' TO SKIN MISSING DELAMAINTED. / CLOSING ACTION LOG #0062832 R/R #1 ENGINE PYLON PANEL 431ER REF AMM 54-53-02. CLEARING #14357

Part: LIGHT — LOOSE (CABIN) · airframe 56,150 hrs · 23,702 cycles

RT ESCAPE PATH STRIP LOOSE BETWEEN ROW 8 TO ROW 10. SECURED STRIP PER SIP.

Part: LENS — BROKEN (CABIN) · airframe 55,737 hrs · 23,453 cycles

RT AFT DOOR EXIT SIGN BROKEN. R&R LENS PER MM.

Part: RETAINER — LOOSE (R1 GIRT BAR) · airframe 54,145 hrs · 22,449 cycles

R1 DOOR GIRT BAR RETENTION LOOSE. ADJUSTED THE RETAINERS IAW SIP.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,127 hrs · 22,434 cycles

R1 DOOR EXIT LIGHT INOP. R&R BATTERY CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,127 hrs · 22,434 cycles

RT EMERGENCY LIGHT ON STOWAGE BINS INOP BETWEEN ROW 3 TO ROW 11. R&R CHARGER IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 54,127 hrs · 22,434 cycles

LT EMERGENCY EXIT BIN LIGHT DAMAGED AT ROW 23. R&R LIGHT ASSEMBLY PER AMM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY LT FRAME SIDEWALL ATTACH SUPPORT ANGLE CORRODED AT BS 787 FASTENER HOLES. R&R ANGLE PER SRM & DWG.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 54,127 hrs · 22,434 cycles

RT WING T/E UPPER AFT PANEL AFT OF #2 PYLON AFT UPPER SEAL RETAINER IS CRACKED. / REMOVED RT WING T/E UPPER AFT PANEL ART OF #2 PYLON AFT UPPER SEAL RETAINER PER SOPM 20-50-01. 4318R 19DEC17 INSTALLED SERVICEABLE AFT UPPER SEAL RETAINER ON R/H WING T/E UPPER AFT PANEL AFT OF #2 PYLON IAW SOPM 20-50-01; SRM 51-40-02-0G-0 AND IPC REFERENCE 57-50-00-25. 57048U 21DEC17

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** LAVATORY SERVICE DOOR BONDING JUMPER ATTACH POINT CORRODED / LAVATORY SERVICE DOOR BONDING JUMPER ATTACH PAINT CORRODED. REMOVED 1'X3'X.025 AT GROUND HOLE LOCATION; FOUND TO BE OUT OF LIMITS. DAMAGE LESS THAN 20X FROM HOLE REMOVED AND INSTALLED NEW CFE-7523161 DOOR PER SRM 52-40-01-1A-4; SRM 51-40-02; AMM 52-49-07-000-801 AND AMM 52-49-07-400-801. 28DEC17 57546U

Part: FRAME — CORRODED (AFT CARGO COMPT) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** CORROSION ON AFT CARGO BAY FORWARD BULKHEAD FRAME AT BS 727+4; LBL 10 TO LBL 12; WL 155 TO WL 154. / CORROSION AT ACB FWD. BULKHEAD FRAME BS 727+4'; LBL 10 TO LBL 12; WL 155 TO WL 154; REMOVED 2' X 1.5' X 0.004' NO LIMITS GIVEN IN SRM. REPAIRED PER ATS ER 17-05580 REV IR; SWA EA 1-753-32112 REV IR

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

FORWARD CARGO BAY AFT BULKHEAD RT LOWER SUPPORT CORRODED AT BS 500D, RBL 25. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 847, BETWEEN LBL 21 TO RBL 23. R&R SUPPORT PER SRM & DWG.

Part: FLAP — DELAMINATED (LH OUTBD AFT FLA) · airframe 54,127 hrs · 22,434 cycles

LEFT WING O/B AFT FLAP TAILING EDGE IS SEPARATED AT I/B END / SEPARATION OF THE WEDGE ON THE I/B END AT THE LEFT WING O/B AFT FLAP WAS REPAIRED AT CSD ON WORK ORDER 502834. FLAP WAS REMOVED FROM THE AIRCRAFT & WILL BE REINSTALLED ON NRC T735092

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY FORWARD FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 767, BETWEEN RBL 21 TO RBL 23. R&R SUPPORT PER SRM AND DWG.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 54,127 hrs · 22,434 cycles

RIGHT WING TRAILING EDGE SEAL RETAINER AT FWD SIDE OF FALSE WEB AFT OF #2 PYLON CRACKED / REMOVED AND REPLACED RT WING T/E SEAL RETAINER @ FWD SIDE OF FALSE WEB AFT OF # 2 PYLON (TRANSVERSED PANEL) PER SRM 51-40-02-0G-0 AND IPC. 57-50-00-25 ITEM 272.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 460 TO BS 500C+7, BETWEEN LBL 23 TO LBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS 775, RBL 20. R&R WEB ASSEMBLY PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, BETWEEN RBL 21 TO RBL 23. R&R SUPPORT PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY AFT BULKHEAD LOWER CENTER SUPPORT CORRODED AT BS 947, BETWEEN LBL 10 TO RBL 23. R&R SUPPORT PER DWG & SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 789, BETWEEN RBL 21 TO RBL 23. R&R SHIELD PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL IAW DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

FORWARD CARGO BAY FORWARD BULKHEAD LOWER CENTER SUPPORT CORRODED AT BS 396, RBL 18. R&R FRAME ASSEMBLY PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW DWG.

Part: FRAME — CORRODED (AFT CARGO COMPT) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** CORROSION ON AFT CARGO BAY FORWARD BULKHEAD FRAME AT BS 727+4; RBL 10 TO RBL 12; WL 155 TO WL 154. / CORROSION AT ACB FWD BULKHEAD FRAME 72714U; RBL 10 TO RBL 12; WL 155 TO WL 154. 2' X 1.5'X0.002 NO LIMITS GIVEN IN SRM; REPAIRED PER ATS ER - 17-05580 REV IR; SWA EA 1-753-32112 REV IR

Part: BRACKET — CRACKED (R/H WING) · airframe 54,127 hrs · 22,434 cycles

SUPPLEMENTAL INFORMATION: RIGHT WING TRAILING EDGE SEAL RETAINER/SUPPORT BRACKET AT AFT SIDE OF FALSE WEB AFT OF #2 PYLON CRACKED AT LOWER FASTENER HOLE / ALL WORK ACCOMPLISHED ON NRC DEFECT NO. T735086 WINGS 5049; SEE COPY ATTACHED. 57048U 21DEC17

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY AFT RT HAND AFT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 930, BETWEEN RBL 21 TO RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL 140BF ALONG L/H & R/H EDGES / FABRICATED ACB 140BF FLOOR PANEL REPLACEMENT FROM CONOLITE 0.090 LOT # 1315698-1 PER: AMM 25-52-01-201-801. ITEM F.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 54,127 hrs · 22,434 cycles

AFT PASSENGER FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE PLIES / REPAIRED UPPER SURFACE PLIES ON AFT PASSENGER FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-1. 56749U 19DEC17

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 54,127 hrs · 22,434 cycles

AFT PASSENGER FLOOR PANEL 241YF HAS DAMAGED UPPER SURFACE PLIES / REPAIRED AFT PASSENGER FLOOR PANEL 241YF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-9 56749U 20DEC17

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL 140AF ALONG L/H & R/H EDGES / FABRICATED AFT CARGO BAY FLOOR PANEL 140AF REPLACEMENT FROM CONOLITE .090 LOT # 1315698-1 PER AMM 25-52-01-201-801 ITEM F. 57636U 21DEC17

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL 140DF ALONG L/H & R/H EDGES / FABRICATED AFT CARGO BAY FLOOR PANEL 140DF REPLACEMENT FROM CONOLITE 0.090 LOT # 1315698-1; MATERIAL I.D. A90RG1W: AMM 25-52-01-201-801; ITEM F. 88641U 21DEC17

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 54,127 hrs · 22,434 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL 140CF A LONG L/H & R/H EDGES / 140CR ACB FLOOR PANEL FOUND TO BE OUT OF LIMITS. CORROSION MORE THAN MAXIMUM OF 3.0 INCHES PER SRM 53-00-53-1A-1 LOCATED AND DRILLED REPLACEMENT PANEL ACB 140CF PER SRM 51-40-05 AND PER SRM 53-70-53-01-1 LOT # 1310914-4. APPLIED CHEMICAL CONVERSION COATING AND PRIMED PER SRM 51-20-01.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 54,127 hrs · 22,434 cycles

AFT PASSENGER FLOOR PANEL 241ABF HAS DAMAGED UPPER SURFACE PLIES / REPAIRED DAMAGED UPPER SURFACE PLIES ON AFT PASSENGER FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-1. 57066U 12/19/17

Part: STRIP — CRACKED (AFT CARGO BAY) · airframe 54,127 hrs · 22,434 cycles

AFT L/H OF CARGO DOOR CAP STRIP IS CRACKED AT FASTENER HOLE ( MARKED) / REMOVED DAMAGED CAP STRIP. FORMED & FABRICATED NEW CAP STRIP FROM 2024-T3 .063 CLAD LOT # 1317399-1 PER DWG 453A1611. NEW CAP STRIP TO BE INSTALLED ON CUST CARD NBR JPANEL-121-CLOSE.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY L/H #2 FLOOR TO SIDEWALL CAP STRIP BS 727D+6 - 767+6 HAS CORROSION AT SEVERAL FASTENER HOLE LOCATIONS ( MARKED) / REPLACED #2 FLOOR TO SIDEWALL CAP STRIP BS 727D+6 - 767+6 IAW AMM 25-52-10-400-801 57636U

Part: CAP — CORRODED (AFT CARGO BAY) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY R/H #1 FLOOR TO SIDEWALL CAP STRIP BS 727 - 727D + 6 HAS CORROSION AT SEVERAL FASTENER HOLE LOCATIONS ( MARKED) / REMOVED DAMAGED CAP STRIP. FABRICATED NEW CAP STRIP FROM 2024-T3 .063 CLAD LOT # 1317399-1 PER DWG 453A2611. NEW CAP STRIP TO BE INSTALLED ON CUST CARD NBR JPANEL-141-CLOSE

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY L/H #1 FLOOR TO SIDE WALL CAP STRIP BS 727 - 727D+6 HAS CORROSION AT SEVERAL FASTENER HOLE LOCATIONS ( MARKED) / REPLACED AFT CARGO BAY FLOOR TO SIDEWALL CAP STRIP BS 727-727D+6 IAW AMM 25-52-10-400-801 57636U

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 54,127 hrs · 22,434 cycles

VERTICAL PRESSURE DECK CRACKED AT BS 663, LBL 33. REPAIRED DECK PER ER AND EA.

Part: CAP — CORRODED (AFT CARGO BAY) · airframe 54,127 hrs · 22,434 cycles

AFT CARGO BAY L/H #3 FLOOR TO SIDEWALL CAP STRIP BS 767+6 - 847 HAS CORROSION AT SEVERAL FASTENER HOLE LOCATIONS ( MARKED) / REPLACED #3 FLOOR TO SIDEWALL CAP STRIP BS 767+6-847 IAW AMM 25-52-10-400-801 57636U

Part: SKIN — CRACKED (LE SLAT) · airframe 54,127 hrs · 22,434 cycles

RT WING NR 8 SLAT SKIN CRACKED AT FASTENER HOLE ON SLAT NOSE SKIN AT ACTUATOR RIB ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: GLOWSTRIP — DIM (CABIN) · airframe 53,371 hrs · 21,948 cycles

AFT GALLEY PHOTO LUMINESCENT STRIP DIM. R&R STRIP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 50,988 hrs · 20,516 cycles

LEFT OVERHEAD BIN EMERGENCY LIGHT LENS COVER MISSING AT ROW 9. R & R THE LENS IAW SIP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,067 hrs · 19,946 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW AMM.

Part: FAN — FAULTY (CABIN) · airframe 49,200 hrs · 19,429 cycles

ON INITIAL CLIMBOUT, AN ELECTRICAL ODOR CAME FROM WHAT SEEMED THE EYE BALL OUTLETS AND LASTED APPROXIMATELY 4 MINUTES. R & R RECIRCULATION FAN IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 48,277 hrs · 18,895 cycles

LOWER FWD ENTRY DOOR EMER EXIT SIGN LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,929 hrs · 18,689 cycles

RIGHT EXTERNAL OVERWING EMER EXIT LIGHT INOPERATIVE AFT OF WING. RELAMPED LIGHT IAW AMM.

Part: LIGHT — FAULTY (EXTERIOR) · airframe 47,929 hrs · 18,689 cycles

LEFT EXTERNAL OVERWING EMER EXIT LIGHT FAULTY. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,929 hrs · 18,689 cycles

RIGHT EXTERNAL OVERWING EMER EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

VERTICAL WEB ATTACH CLIP CRACKED AT BS 827, RBL 24. R & R CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

LOWER SURFACE OF CREASE WEB CORRODED, BETWEEN BS 706 - 716, STRINGER 17R. REPAIRED WEB IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE WEB CORRODED, BETWEEN BS 716 - 727, STRINGER 17R. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

INTERCOSTAL CRACKED BETWEEN BS 500 - 500A, RBL 24. R & R INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FRAME WEB CRACKED AT BS 727, WL 200 RT, 1ST INBD HOLE IN 10 O CLOCK POSITION. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

SKIN CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R. REPAIRED SKIN IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM INBOARD CHORD CORRODED AT BS 639, RBL 64. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM INBD CHORD CORRODED AT BS 597, RBL 64. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM INBD CHORD CORRODED AT BS 544, RBL 64. REPAIRED CHORD IAW ER & EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,929 hrs · 18,689 cycles

EMERGENCY EXIT LIGHT POWER SUPPLY INOPERATIVE AT BS 603, RBL 67. R & R POWER SUPPLY IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17R. R&R WEB PER SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CHANNEL FITTING CORRODED BETWEEN BS 348 - 351, STRINGER 17L. R & R FITTING IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 827 - 847, STRINGER 17L. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 767 - 787, STRINGER 17L. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 867 - 887, STRINGER 17L. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AIRSTAIR DOORSTOP INTERCOSTAL UPPER HOLE CRACKED AT BS 333.36. R&R INTERCOSTAL IAW ACO AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 847 - 867, STRINGER 17L. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 787 - 807, STRINGER 17L. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 747 - 767, STRINGER 17L. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 639 - 663, STRINGER 17L. REPAIRED WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 727E - 747, STRINGER 17L. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 807 - 827, STRINGER 17L. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

STRINGER CLIP CORRODED AT BS 887, STRINGER 10L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

CREASE BEAM INBD CHORD CORRODED, BETWEEN BS 947 - 993, LBL 49. R & R CHORD IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

STRINGER CLIP CORRODED AT BS 706, STRINGER 9R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

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

Part: PLATE — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 400 TO 500D, LBL 24. R & R SUPPORT PLATE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 400 TO BS 420, RBL 24. R&R SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 755, LBL 18. R&R SUPPORT PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED, BETWEEN BS 270 - 294, BBL. 0. R & R INTERCOSTAL IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 492 TO 500A, RBL 24. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 755 TO BS 847, LBL 18. R&R SUPPORT PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED AT FLOOR BOARD NUT PLATE HOLE BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AFT CARGO DOORWAY, LOWER THRESHOLD INBD STRAP, LOWER SURFACE CORRODED AT BS 791, RBL 19. R & R STRAP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 767 - 794, RBL 20. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AFT CARGO DOORWAY, LOWER THRESHOLD WEB CORRODED, BETWEEN BS 795 - 847, RBL 19. R & R WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED AT BETWEEN BS 344 TO BS 360, BBL 0. R&R INTERCOSTAL PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 47,929 hrs · 18,689 cycles

AFT CARGO DOORWAY LOWER THRESHOLD INBD STRAP, UPPER SURFACE CORRODED, BETWEEN BS 770 - 860, RBL 19. R & R STRAP IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 47,929 hrs · 18,689 cycles

RIGHT WING TRANSVERSE WEB BULB SEAL TRACK BRACKET CRACKED, AT LOWER BOLT HOLE. R & R BRACKET IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 47,929 hrs · 18,689 cycles

AFT ENTRY CEILING PANEL EXIT SIGN BROKEN AT MOUNTING POINTS. R & R SIGN IAW AMM.