N271LV

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 55,069 hrs · 38,976 cycles

R1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / INSTALLED R1 DOOR LOWER EXIT SIGN IAW AMM 33-51-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,964 hrs · 38,906 cycles

ISLE EMERGENCY LIGHT AT 16DEF IS INOP. / REPLACED EMERGENCY EXIT LIGHT LAMP AT SEAT ROW 16DEF IAW AMM 33-51-03-960-801 LIGHT CHECKS GOOD 'A'TAG D90421

Part: LIGHT — FAULTY (CABIN) · airframe 54,099 hrs · 38,383 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT TURNS ON WHEN CABIN LIGHTS TURNED ON THE BRIGHT SETTING / FOUND LIGHT IN QUESTION TO BE ENTRY DOOR THRESHOLD ILLUMINATION LIGHT. ILLUMINATION LIGHT OPS CHECK GOOD PER S.I.P. EMERGENCY EXIT. LIGHTS OPS CHECK GOOD PER M.M. CH. 33-51-00

Part: SMOKE DETECTOR — FAULTY (FWD LAV) · airframe 53,422 hrs · 37,927 cycles

SUPPLEMENTAL INFORMATION: FORWARD LAV SMOKE ALARM ACTIVATED FOR DURATION OF APPROACH & TAXI TO GATE. NO PASSENGERS WERE IN LAVATORY / CLOSING DMA #0405036 R&R FWD LAV SMOKE DETECTOR IAW AMM 26-14-01 CLEARING # 36546

Part: STRIP — DAMAGED (AFT CARGO) · airframe 53,217 hrs · 37,798 cycles

ACB FLOOR PANELS 140DF AND 140CF I/B CAP STRIPS ARE DAMAGED / RECEIVED 2EA NEW CAP STRIPS FOR ACB FLOOR PANELS 140DF AND 140CF. ACB FLOOR PANELS 140DF AND 140CF I/B CAP STRIPS WILL BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,217 hrs · 37,798 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP. CHARGED M1673 BATTERY PER AMM 33-51-06-610-802. PERFORMED SATISFACTORY EMERGENCY LIGHTS OPERATIONAL TEST PER AMM 33-51-00-710-801.

Part: FLOOR PANEL — DEFECTIVE (CABIN) · airframe 53,217 hrs · 37,798 cycles

PASSENGER CABIN FLOOR PANEL 241AAF, 3 FASTENER HOLES ALONG FWD EDGE DO NOT LINE UP WITH EXISTING STRUCTURE PASSENGER CABIN FLOOR PANEL 241AAF, 3 FASTENER HOLES ALONG FWD EDGE THAT DO NOT LINE UP WITH EXISTING STRUCTURE WERE RELOCATED IAW SRM 53-00-50-2R-6 56144U. 02/27/2020

Part: FLOOR PANEL — OUT OF ALIGNMENT (CABIN) · airframe 53,217 hrs · 37,798 cycles

PASSENGER CABIN FLOOR PANEL 241AAF; 3 FASTENER HOLES ALONG FWD EDGE DO NOT LINE UP WITH EXISTING STRUCTURE / PASSENGER CABIN FLOOR PANEL 241AAF; 3 FASTENER HOLES ALONG FWD EDGE THAT DO NOT LINE UP WITH EXISTING STRUCTURE WERE RELOCATED IAW SRM 53-00-50-2R-6 56144U. 02/27/2020

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 53,217 hrs · 37,798 cycles

DELAMINATION ON L/W I/B AFT FLAP LOWER SURFACE / DELAMINATION OF FIBERGLASS OVERLAY PLIES IN 3EA. AREAS ON L/W I/B AFT FLAP LOWER SURFACE WERE REMOVED AND REAPPLIED PER SRM 51-70-04-2R-0.

Part: SKIN — BENT (L1 DOOR) · airframe 53,217 hrs · 37,798 cycles

FWD ENTRY DOOR EXTERNAL SKIN IS BENT AT LOWER HINGE CUTOUT EDGE. L=5.65'; W=.8'; DEPTH .091 / EVALUATED DAMAGE ON FED EXTERNAL SKIN LOWER HINGE CUTOUT. L=5.6'; W=0.8' D=0.0091'. DAMAGE FOUND TO BE BEYOND THE LIMITS IAW SRM 52-10-01-1A-1. FIG 104. ACCOMPLISHED REPAIR IAW SRM 52-10-01-2R-5 REPAIR 5

Part: SKIN — DENTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A DENT BS 1006+3.7, 2.9" BELOW STR 14L, DENT MEASURES: L=2.3", W=1.9", Y=.004" W/Y=475 REPAIR ACCOMPLISHED ON ER NO 20-01888 REV IR & EA NO 1-753-36715 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — DENTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A DENT BS 992+6; .7' BELOW STR 14L; DENT MEASURES: L=.5'; W=.4'; Y=.004' W/Y=100 / DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1).(B) NO FURTHER ACTION OR INSPECTION IS REQUIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A DENT BS 992+4; 1' BELOW STR 14L; DENT MEASURES: L=.8'; W=.6'; Y=.003' W/Y=200 / DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1)(B) NO FURTHER ACTION OR INSPECTION IS REQUIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A DENT BS 992+6, .7" BELOW STR 14L, DENT MEASURES: L=.5", W=.4", Y=.004" W/Y=100 DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1).(B) NO FURTHER ACTION OR INSPECTION IS REQUIRED.

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

(SKYLINE DTIP) FUSELAGE SKIN REPAIR AT BS 1025, S-15L TO S-17AL REQUIRES ADDITIONAL REWORK. (REF ESR: 20-01837) FUSELAGE SKIN REPAIR AT BS 1025, S-15L TO S-17AL WAS REPAIRED IAW ATS ER 20-01871 REV IR DATED 28FEB2020 AND EA 1-753-36639 REV IR

Part: SKIN — DENTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A DENT BS 1006+3.7; 2.9' BELOW STR 14L; DENT MEASURES: L=2.3'; W=1.9'; Y=.004' W/Y=475 / REPAIR ACCOMPLISHED ON ER NO 20-01888 REV IR & EA NO 1-753-36715 REV IR

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

(SKYLINE DTIP) FUSELAGE SKIN REPAIR AT BS 1025; S-15L TO S-17AL REQUIRES ADDITIONAL REWORK. (REF ESR: 20-01837) / FUSELAGE SKIN REPAIR AT BS 1025; S-15L TO S-17AL WAS REPAIRED IAW ATS ER 20-01871 REV IR DATED 28FEB2020 AND EA 1-753-36639 REV IR

Part: SKIN — DENTED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A DENT BS 992+4, 1" BELOW STR 14L, DENT MEASURES: L=.8", W=.6", Y=.003" W/Y=200 DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1)(B) NO FURTHER ACTION OR INSPECTION IS REQUIRED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL156. REMOVED AND REPLACED FCB INTERCOSTAL SUPPORT ANGLE BS 500C FWD SIDE LBL 25 IAW SRM 51-40-02 AND DWG 143A7505 89004U 25FEB20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 420 TO BS. 480, LBL 23. / R&R SUPPORT IAW SRM.

Part: WEB — CORRODED (BS 440-494) · airframe 53,217 hrs · 37,798 cycles

FORWARD CARGO BAY MULTIPLE SPOTS ON SUBTHRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 494, RBL 29. / R&R SUBTHRESHOLD WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** ON FLOOR RAIL AT AFT CARGO BAY BS767+5 LBL3 WL157. / ACCOMPLISHED REPAIR AT FLOOR RAIL AFT CARGO BAY BS767+5' LBL3 WL157 AS PER SRM 53-00-53-2R-2 ALT.#5. TABLE 205. FIG.203; DUE TO UPON REMOVAL CORROSION EVALUATED AREA AND FOUND TO BE OUT OF LIMITS AS PER SRM 53-00-53-1A-2 PARAGRAPH 4.A2 FIG.203. FABRICATED REINFORCING CHANNEL FROM BAC 1510-1355 LOT 1330259-2 MACHINE SHOP FABRICATION PO.NUMBER # 783578-SWA.

Part: SHIELD — CORRODED (BS 847-867) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. / R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - 500C LBL23 WL157. / SIDEPLATE CHANNEL SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2; MULTIPLES AREAS 1 X 1 MORE THAN 50% MATERIAL LOSS. FABRICATED SIDEWALL SUPPORT IAW SRM 53-30-53-01-2 BAC1496-444-7075-76 CLAD LOT# 1412169-1 AND DWG 143A 7500; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01. FABRICATED REPAIR SPLICE FROM EXTRUSION BAC1496-444# 7075-T6 LOT# 1412169-1 APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-00-53-2R-5. INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS400-500D LBL23 IAW SRM 51-40-02 AND DWG 143A7500 80641U 26FEB20. REMOVAL OF SIDEWALL SUPPORT AT FCB BS400-500D IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. / REMOVED AND REPLACED ON INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS 500B FWD SIDE LBL 25 IAW SRM 51-40-02 AND DWG 143A7505 REV B P/N 143A7502U159. 80641U 27FEB20

Part: FLOOR SUPPORT — BENT (BS 787) · airframe 53,217 hrs · 37,798 cycles

BENT FLOOR SUPPORT AT AFT CARGO BAY BS787+8 RBL17 WL 157. / REPLACED FLOOR SUPPORT AT ACB. BS 787+8' RBL 77 WL 157 AS PER SRM 51-40-02-0G-0 AND DRAWING# 146A7500 I.D 0004.; FLOOR SUPPORT WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE AS PER SRM 53-00-53-1A-2

Part: SUPPORT — CORRODED (BS 887-947) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887 TO BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.

Part: SHIELD — CORRODED (BS 420) · airframe 53,217 hrs · 37,798 cycles

FORWARD CARGO BAY ON FORWARD SHIELD CORRODED AT BS. 420+2.5, RBL 24. / R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** AROUND THE FASTENER ON AFT FLOOR TO BULKHEAD PANEL SUPPORT ANGLE BS947 LBL7 WL178. / REPLACE BULKHEAD PANEL SUPPORT ANGLE AT BS 947 LBL 7 WL 178 AS PER. DWG. 149A8118 AND SRM 51-40-02-0G-0. 59868U FEB-28-20.

Part: SHIELD — CORRODED (BS 767-787) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. / R&R SHIELD PER SRM AND DWG.

Part: FRAME SPLICE — CORRODED (BS 787) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY FRAME CORRODED AT BS. 787, RBL 25. / R&R FRAME SPLICE IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 727, RBL 21. / R&R SUPPORT PER SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS500B AFT SIDE LBL25 WL156. REMOVED AND REPLACED ON INTERCOSTAL ANGLE AT FWD CARGO BAY BS 500B AFT SIDE LBL 25 IAW SRM 51-40-02 AND DWG 143A7505 REV A 80641U 27FEB20 P/N 143A7502U5 PO# 755718.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY FLOOR RAIL CORRODED AT BS. 767+5, LBL 3. / REPAIRED FLOOR RAIL PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY ON TRACK AROUND THE FASTENER CORRODED AT BS. 927+8, RBL 13. / R&R FLOOR TRACK IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS807 - BS727 LBL21 WL157. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO BS 847 LBL 21 WL 157 P/N 146A7502-27 IAW SRM 51-40-02-0G-0 AND DRAWING # 146A7500 AND 146A7502 59861U 27FEB20

Part: BRACKET — CRACKED (BS 663) · airframe 53,217 hrs · 37,798 cycles

BRACKET P/N 272A9112-31 @B.S. 663 RBL40 CRACKED / REMOVED; LOCATED; DRILLED AND INSTALLED BRACKET P.N. 272A9112-31 PER SRM 51-40-02 PAR.D(6); SRM 51-40-05 FIG.4; SRM 51-40-02 PAR D(1-5) AND DWG.111A7000 AND DWG.272A9112. APPLIED CHEM.CONVERSION COATING AND PRIMED BRACKET PER SRM 51-20-01 PAR.5C AND SOPM 20-41-02 PAR.6(A)(1). 91195U 2-26-20 MATERIAL USED IS AND 10138-1205 2024-T3511 LOT# 21933877. 91195U 2-26-20

Part: SKIN — GOUGED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A GOUGE BS 400+2.4; STR 27R / FUSELAGE SKIN GOUGE BS 400+2.4; STR 27R REPAIRED IAW ATS ER 20-01914; REV IR; DATED 10-MAR-2020 AND PER EA NO: 1-753-36694 REV IR 55981U 11MAR20

Part: ANGLE — CORRODED (BS 1124) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** APU TRANSITION DUCT ATTACH FLANGE STA 1124 R/H SIDE / REMOVED AND INSTALLED A NEW APU TRANSITION DUCT ATTACH STIFFENER ANGLE PER SRM 51-40-01-0G-0 AND DWG # 148A8650

Part: SKIN — CORRODED (BS 480 S28L) · airframe 53,217 hrs · 37,798 cycles

CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 480+18; 6.5' BELOW STR 28L / BLENDED CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 480+18 6.5' BELOW STR 28 L/H INSPECTED & EVALUATED PER EA 1-753-36709 REV IR & ATS ER 20-01892 REV IR THIS EA THE DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITH REPETATIVE INSPECTIONS APPLIED DENT DOT IAW MPM 52.03.01.02 PARA 2.D(1)(B) & PARA 3

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

CHAFING ON FLOOR RAIL AT FWD CARGO BAY BS500A LBL8 WL157. / REMOVED DAMAGE FROM FCB FLOOR RAIL BS500A LBL8 WL157 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 SEAT CHANNEL EXTRUSION BAC1510-1355 7050-T76511 LOT# 1330259-2 TO MACHIN SHOP AND RECIEVED CHANNEL SPLICE P/N HFAB53-AN-011 PO#783578 LOCATED AND DRILLED FABRICATED FILLER #1 P/N BAC1509-100146 7050-T76511 LOT#1411423-1 IAW SRM 53-00-53-2R-2 AND SRM 51-40-05-0G-0 APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-20-01-0G-0 AND INSTALLED IAW SRM 53-00-53-2R-2 REPAIR 2 AND SRM 51-40-02-0G-0

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - 500C LBL23 WL157. SIDEPLATE CHANNEL SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2, MULTIPLES AREAS 1 X 1 MORE THAN 50% MATERIAL LOSS. FABRICATED SIDEWALL SUPPORT IAW SRM 53-30-53-01-2 BAC1496-444-7075-76 CLAD LOT# 1412169-1 AND DWG 143A 7500, APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01. FABRICATED REPAIR SPLICE FROM EXTRUSION BAC1496-444# 7075-T6 LOT# 1412169-1 APPLIED CHEMICAL CONVERSION COATING

Part: SKIN — CORRODED (BS 500A S28L) · airframe 53,217 hrs · 37,798 cycles

CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 500A+3; 6.5' BELOW STR 28L / BLENDED CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 500A+3 6.5' BELOW STR 28 L/H INSPECTED & EVALUATED PER EA 1-753-36709 REV IR & ATS ER 20-01892. REV IR AS PER THIS EA THE DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITH REPETATIVE INSPECTION APPLIED DENT DOT IAW MPM 52.03.01.02 PARA 2.D(1)(B) & PARA 3

Part: SKIN — GOUGED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

FUSELAGE SKIN HAS A GOUGE BS 400+2.4, STR 27R FUSELAGE SKIN GOUGE BS 400+2.4, STR 27R REPAIRED IAW ATS ER 20-01914, REV IR, DATED 10-MAR-2020 AND PER EA NO: 1-753-36694 REV IR 55981U 11MAR20

Part: HANDLE — CRACKED (OVERWING EXIT) · airframe 53,217 hrs · 37,798 cycles

R/H OVER WING EXIT DOOR RELEASE HANDLE ASSEMBLY IS CRACKED REMOVED AND REPLACED R/H OVERWING EXIT DOOR RELEASE HANDLE ASSEMBLY IAW AMM 52-22-51-400-801 3.C.(2) (E-F) AND AMM 52-22-51-000-801 2.B.(1)(D-G) 59576U 07MAR20

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS494 - 500A RBL23 WL157. REMOVED AND REPLACED ON AFT SHIELD AT FCB FROM BS 494 TO BS 500A RBL 23 WL157, P/N 143A8126-12 IAW SRM 51-40-02 AND DWG 143A0080.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241ABF HAS DAMAGED UPPER SURFACE PLIES / AFT CABIN FLOOR PANEL 241ABF WITH DAMAGED UPPER SURFACE PLIES WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241ZF HAD DAMAGED UPPER SURFACE PLIES REMOVED FLOOR PANEL 241ZF IAW AMM TASK 53-21-00-000-801. 57885U 02-19-2020 10537C 02/19/20 REPAIRED DAMAGED UPPER SURFACE PLIES, PANEL 241ZF IAW SRM 53-00-50-2R-1 10537C 02/23/20: OK TO INSTALL FLOOR PNL 241ZF 56303C 25FEB20 INSP 15 25FEB20 INSTALLED FLOOR PANEL 241ZF IAW M/M 53-21-00-400-801

Part: SKATE ANGLE — CHAFED (BS 1007-1016) · airframe 53,217 hrs · 37,798 cycles

SKATE ANGLE IS CHAFED AT 1007-1016; W.L. 306; L.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3200U11; BS 1007 TO BS 1016; LBL 14; WL 306 IAW SRM 51-40-02 AND DWG 147A0030 REV A. 89004U; 29FEB20.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 53,217 hrs · 37,798 cycles

SKATE ANGLE IS CHAFED AT 1007-1016; W.L. 306; R.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3200U12 BS 1007 TO BS 1016; RBL14; WL 306 IAW SRM 51-40-02 AND DWG 147A0030 REV A. 89004U; 29FEB20.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,217 hrs · 37,798 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / ACCOMPLISHED REPAIR AT ACB AFT CORNER SCUFFPLATE IAW ENGINNERING AUTHORIZATION EA.#1-A53-2076 REV.11. THE AFT CORNER INSTALLATION IT'S GOING TO BE ACCOMPLISHED WITH CUSTOMER CARD# 753-140-00-024.

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

SKATE ANGLE IS CHAFED AT 1108-1110, W.L. 306, L.B.L. 14. REPAIRED SKATE ANGLE AT BS 1108-1110, WL 306 LBL 14 IAW SRM 53-80-71-2R-6

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

SKATE ANGLE IS CHAFED AT 1108-1110, W.L. 306, R.B.L. 14. REMOVED AND CUT CLOSURE ANGLE 5" FWD AND AFT OF DAMAGE CUT AT BS 1108-1110, WL306, RBL14 IAW 53-80-71-2R-6. ACCOMPLISHED REPAIR IAW SRM 53-80-71-2R-6. APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-20-01 AND SOPM 20-44-04. APPLIED EXTERIOR FINISHES IAW AMM 51-21-00 APPLIED RESISTANT TEFLON COATING IAW SOPM 20-44-09

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241YF HAS DAMAGED UPPER SURFACE PLIES / REMOVED FLOOR PANEL 241YF IAW AMM TASK 53-21-00-000-801 PARA 2E(1)-(3). 57885U 02-19-2020 10537C 02/19/20 DUE TO EXTENT OF DAMAGE TO PANEL 241YF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 & AIPC 53-21-00-26 ITEM 66. 57885U 02-19-2020 10537C 02/19/20 OK TO INSTALL FLOOR PNL 241YF 56303C 25FEB20 INSP 15 25FEB20 INSTALLED FLOOR PANEL 241YF IAW M/M 53-21-00-400-801

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

SKATE ANGLE IS CHAFED AT 1108-1110; W.L. 306; L.B.L. 14. / REPAIRED SKATE ANGLE AT BS 1108-1110; WL 306 LBL 14 IAW SRM 53-80-71-2R-6

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241ZF HAS DAMAGED UPPER SURFACE PLIES / REMOVED FLOOR PANEL 241ZF IAW AMM TASK 53-21-00-000-801. 57885U 02-19-2020 10537C 02/19/20 REPAIRED DAMAGED UPPER SURFACE PLIES; PANEL 241ZF IAW SRM 53-00-50-2R-1 10537C 02/23/20: OK TO INSTALL FLOOR PNL 241ZF 56303C 25FEB20 INSP 15 25FEB20 INSTALLED FLOOR PANEL 241ZF IAW M/M 53-21-00-400-801

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241AEF HAS DAMAGED AFT EDGE / DAMAGE TO THE AFT EDGE ON CABIN FLOOR PANEL 241AEF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-4. 59198U 2.21.20.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241XF HAS DAMAGED UPPER SURFACE PLIES / AFT CABIN FLOOR PANEL 241XF WITH DAMAGED UPPER SURFACE PLIES WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

SKATE ANGLE IS CHAFED AT 1108-1110; W.L. 306; R.B.L. 14. / REMOVED AND CUT CLOSURE ANGLE 5' FWD AND AFT OF DAMAGE CUT AT BS 1108-1110; WL306; RBL14 IAW 53-80-71-2R-6. ACCOMPLISHED REPAIR IAW SRM 53-80-71-2R-6. APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-20-01 AND SOPM 20-44-04. APPLIED EXTERIOR FINISHES IAW AMM 51-21-00 APPLIED RESISTANT TEFLON COATING IAW SOPM 20-44-09

Part: FLOOR PANEL — DAMAGED (AT CABIN) · airframe 53,217 hrs · 37,798 cycles

AFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE PLIES / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 241AAF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 & AIPC 53-21-00-2G ITEM 150. 57885U 02-19-2020

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 53,217 hrs · 37,798 cycles

THE INTERNAL HORIZONTAL PRESSURE DECK WEB IS CRACKED AT BS 675 LBL35. / ACCOMPLISHED REPAIR AT INTERNAL HORIZONTAL PRESSURE DECK WEB BS 675 LBL 35 AS PER SRM 53-40-51-2R-2 FIG.201 REPAIR #2; PRESSURE DECK WEB WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE AT SRM B737-700; SA-M 1008 COMPLETED.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 53,217 hrs · 37,798 cycles

CRACKED FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 24.5. / R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 53,217 hrs · 37,798 cycles

THE INTERNAL HORIZONTAL PRESSURE DECK WEB IS CRACKED AT BS 675 LBL35. ACCOMPLISHED REPAIR AT INTERNAL HORIZONTAL PRESSURE DECK WEB BS 675 LBL 35 AS PER SRM 53-40-51-2R-2 FIG.201 REPAIR #2, PRESSURE DECK WEB WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE AT SRM B737-700, SA-M 1008 COMPLETED.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 53,217 hrs · 37,798 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 24.5. / R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 53,217 hrs · 37,798 cycles

RIGHT HAND LOWER COMPOSITE BULK HEAD WAS CRACKED AT BS. 663, RBL 53. / R&R VAPOR BARRIER PER SRM, AMM, & DWG.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 53,217 hrs · 37,798 cycles

RH ELEVATOR TE UPPER SKIN, PREVIOUS REPAIR DAMAGED, 72" FROM IB END AFTER REMOVING PREVIOUS REPAIR 72" FROM I/B END ON R/H ELEVATOR T/E UPPER AND LOWER SKIN, ACCOMPLISHED REPAIR ON 4EA AREAS PER SRM 51-70-04-2R-9 AND SRM 51-70-04-2R-6.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 53,217 hrs · 37,798 cycles

RH ELEVATOR TE UPPER SKIN; PREVIOUS REPAIR DAMAGED; 72' FROM IB END / AFTER REMOVING PREVIOUS REPAIR 72' FROM I/B END ON R/H ELEVATOR T/E UPPER AND LOWER SKIN; ACCOMPLISHED REPAIR ON 4EA AREAS PER SRM 51-70-04-2R-9 AND SRM 51-70-04-2R-6.

Part: RETAINER — CRACKED (LT WING TE) · airframe 53,217 hrs · 37,798 cycles

LEFT WING T/E UPPER SEAL RETAINER IS CRACKED 3' BELOW FIXED T/E PANEL 10' I/B OF DEFLECTION RIB ORSS269. / REMOVED AND REPLACED LEFT WING T/E UPPER SEAL RETAINER AT 3' BELOW FIXED T/E PANEL 10' I/B OF DEFLECTION RIB ORSS 269 P/N 115A2982-9. IAW. SRM 51-40-02. AIPC. 57-50-00-25. 88920U 20FEB20

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 53,217 hrs · 37,798 cycles

RIGHT WING TRAILING EDGE HAD CRACKED SUPPORT ANGLE 1" INBOARD OF DEFLECTION RIB ORSS 281. / REMOVED AND REPLACED SUPPORT ANGLE IAW SRM.

Part: RETAINER — CRACKED (RT WING TE) · airframe 53,217 hrs · 37,798 cycles

RIGHT WING FIXED T/E PANEL VERTICAL BULB SEAL RETAINER IS CRACKED 9' I/B OF DEFLECTION RIB. MARKED / REMOVED AND REPLACED RIGHT WING FIXED T/E PANEL VERTICAL BULB SEAL RETAINER P/N 115A2953-2 AT 9' I/B OF DEFLECTION RIB. IAW SRM 51-40-02 AND AIPC 57-50-00-25 88920U 22FEB20

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 53,217 hrs · 37,798 cycles

LEFT WING TRAILING EDGE HAD CRACKED SUPPORT ANGLE 1" INBOARD OF DEFLECTION RIB ORSS. 281. REMOVED AND RESTORED SUPPORT ANGLE IAW SRM.

Part: STRUCTURE — DENTED (COCKPIT) · airframe 53,217 hrs · 37,798 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; W.L. 207.54; R.B.L. 4 - L.B.L. 14. / REPAIRED FLIGHT DECK FLOOR AT B.S.255; W.L.207.54; R.B.L.4 - L.B.L 14. IAW EA 1-A53-33179 REV IR. AND BOEING DWG 141A0631 55981U 10MAR20

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 53,217 hrs · 37,798 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255, W.L. 207.54, R.B.L. 4 - L.B.L. 14. REPAIRED FLIGHT DECK FLOOR AT B.S.255, W.L.207.54, R.B.L.4 - L.B.L 14. IAW EA 1-A53-33179 REV IR. AND BOEING DWG 141A0631 55981U 10MAR20

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,798 hrs · 36,890 cycles

EMERGENCY LIGHT OUT AT 22DEF. RELAMPED & OPS CK'S GOOD IAW AMM 33-51-03.

Part: SIGN — LOOSE (CABIN) · airframe 51,767 hrs · 36,865 cycles

EMERGENCY EXIT OVERHEAD SIGN MID CABIN LOOSE. SECURED LIGHT ASSEMBLY IAW MM.

Part: FLAP — DELAMINATED (L/H WING) · airframe 49,996 hrs · 35,742 cycles

LEFT OUTBOARD AFT FLAP LOWER SURFACE HAS DAMAGE. DAMAGE IS OUT OF LIMITS DUE TO DELAMINATION TOO CLOSE TO OTHER DAMAGE AND TOO CLOSE TO SPAR WEB / REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22 POS L/H OTBD PN OFF 113A3700-7 SN OFF 00057 PN ON 113A3700-25 SN ON 004078

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,165 hrs · 35,192 cycles

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

Part: LANYARD — LOOSE (R1 DOOR) · airframe 48,984 hrs · 35,080 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD WIRE LOOSE. SECURED LANYARD PER SIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,009 hrs · 34,442 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1675 INOP. R&R BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,009 hrs · 34,442 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1674 INOP. R&R BATTERY PER MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 48,009 hrs · 34,442 cycles

G4 GALLEY EMERGENCY EXIT LIGHT CONNECTORS DAMAGED. REPAIRED CONNECTOR PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500 TO BS 500A, LBL 24. R&R INTERCOSTAL IAW DWG AND SRM.

Part: PANEL — CRACKED (AFT FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

APU INLET UPPER PANEL IS CRACKED P/N (315A2040-24) / APU INLET UPPER AFT PANEL WAS REMOVED ON CC# 753-430-00-01B. RECIEVED NEW APU INLET AFT UPPER PANEL P/N 353A2040-24. LOCATED; DRILLED; COUNTERSANK AND ASSEMBLED PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; SRM 51-40-02-0G-0; IPC 49-15-00-01 AND BOEING DWG # 353A2010. INSTALLATION WILL BE ACCOMPLISHED ON CC# 753-430-00-01Y.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

SUPPORT CORRODED AT BS 267, BL 0. R&R SUPPORT IAW DWG AND SRM.

Part: FITTING — CORRODED (AFT CARGO COMPT) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** AFT CARGO COMPARTMENT EQUIPMENT BAY DRAIN MAST SUPPORT FITTING HAS CORROSION; BS992; WL182; LBL22. / REMOVED AND REPLACED DRAIN MAST SUPPORT FITTING DUE TO CORROSION PER SRM 51-40-02-0G-00 & DWG # 147A7443

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY INTERCOSTAL WEB CORRODED AT BS 847, STR 25R. R&R WEB PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

FUSELAGE INTERCOSTAL CORRODED AT STA 306, STR 23L. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 48,009 hrs · 34,442 cycles

LT HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED LT HORIZ STAB UPPER FWD SLIDE SEAL LAW AMM 53-31-31-802 84036U 29JUN18

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

CREASE BEAM WEB CORRODED AT BS 727D+11, RBL 60. R&R CREASE BEAM IAW DWG AND SRM.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

FAIRING PANEL 193AR; INBOARD INNER SKIN HAS CHAFF DAMAGE AND COMMON TO DAMAGE AREA ARE FASTENERS HOLES THAT ARE ELONGATED. / FAIRING PANEL 193AR; INBOARD INNER SKIN WITH CHAFF DAMAGE AND COMMON TO DAMAGE AREA WERE FASTNER HOLES THAT WERE ELONGATED WAS REPAIRED IAW SRM 51-70-05-2R-6. 57545U 7-6-18

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 48,009 hrs · 34,442 cycles

RT HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED RT HORIZ STAB UPPER FWD SLIDE SEAL IAW SOPM 20-50-01 LOCATE AND DRILL IAW SRM 50-40-05 84036U 29JUN18. INSTALLED RT HORIZ STAB UPPER FWD SLIDE SEAL IAW AMM 53-31-31-400-801 STEP 3.D. & E. 56790U 09JUL18 OPS CHECK GOOD

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,009 hrs · 34,442 cycles

RT WING OUTBD AFT FLAP DELAMINATED ON UPPER SUFACE. R&R FLAP PER MM.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** FCB FLOOR PANEL 120CF EDGE HAS SURFACE CORROSION. / REMOVED CORROSION; CORROSION LENGTH IS GREATER THAN 3' OUT OF LIMITS. FABRICATED A NEW ALUMINUM FLOOR PANEL 2024-T3; .071 LOT # 1347031-3 PER SRM 53-30-53-0I-1; SRM 51-10-02-0G-0; AND SOPM 20-43-03 93046U 22JUN18

Part: SCUFF PLATE — CRACKED (FWD SERVICE DOOR) · airframe 48,009 hrs · 34,442 cycles

FSD THRESHOLD CRACKED AT AFT CORNER / REPAIRED FSD THRESHOLD IAW EA 1-A53-2076 REV 11

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** ACB; FLOOR PANEL 140CF HAS EDGE SURFACE CORROSION. / REPLACED THE ACB FLOOR PANEL 140CF WITH NEW PANEL FABRICATED FROM 2024T3 .071 CLAD LOT # 1347031-1 AND APPLIED FINISH PER DWG 453A2610 & SOPM 20-43-03 & AMM 51-21-72-370-804 & SRM 53-60-53-01-1 56708U 26JUN18

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** FCB FLOOR PANEL 120AF EDGE HAS SURFACE CORROSION. / FABRICATED OF REPLACEMENT PANEL FWD PIT 120AF I.A.W SRM 51-30-01-0G-0 PPGA & PPG 7; TREATED (CHEM.CONV.COAT) & PRIMED I.A.W SRM 51-00-58-201 PG 2;(C) AMM 27-72-370-801 PG 2 'D;' SWB TASK 2 TABLE 709 + DWG 453A1610 56708U 26JUN18 MAT USED WAS 2027-T3 .071 CLAD LOT# 1322082-2 56708U 26JUN18

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 790 TO BS 847, RBL 13.84. R&R FLOOR TRACK PER SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** ACB; FLOOR PANEL 140DF HAS EDGE SURFACE CORROSION. / ACB FLOOR PANEL 140DF CORROSION FOUND OUT OF LIMITS DUE TO LENGTH EXCEEDING 3' PER SRM 53-00-53-1A-1 STEP 5.A.(B). FABRICATED FLOOR PANEL FROM .071' 2024-T3 LOT # 1347031-3; COUNTERSUNK PANEL; APPLIED CHEMICAL CONVERSION COATING AND PRIMED PANEL BOTTOM SIDE PER SRM 53-70-53-01-1; DWG 453A2610; SRM 51-40-05-0G-0; MM 51-21-41-370-801; SRM 51-40-08-0G-0 AND MM 51-21-72-370-804.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 787. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 747 TO BS 767. R&R SUPPORT PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 855 TO BS 867, RBL 20. R&R SHIELD ASSEMBLY PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT PER SRM & DWG.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** FCB FLOOR PANEL 120BF EDGE HAS SURFACE CORROSION. / REPLACED FCB FLOOR PANEL 120 BF WITH NEW PANEL FABRICATED FROM 2024 T3 # 0.71 LOT # 1347031-3 PER DWG 453A1610 AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER SOPM 20-43-03 AND AMM 51-21-72-370-804. 57546U 26JUN18

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 48,009 hrs · 34,442 cycles

HORIZONTAL PRESSURE DECK COMMON TO WEB CRACKED AT BS 665, BETWEEN RBL 41 TO RBL 45. REPAIRED WEB PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY LOWER SUPPORT ANGLE CRACKED COMMON TO PANEL 141QW FORWARD STANCHION. R&R ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 48,009 hrs · 34,442 cycles

***CORROSION*** ACB; FLOOR PANEL 140AF HAS EDGE SURFACE CORROSION. / REMOVED CORROSION; CORROSION LENGTH IS GREATER THAN 3'; OUT OF LIMITS. FABRICATED A NEW ALUMINUM FLOOR PANEL 2024T3 # 0.071 LOT # 1347031-3 PER DWG 453A2610; SRM 53-00-53-1A-1; SRM 51-10-02-0G-0; SOPM 20-43-03; AMM 51-21-72-370-804 93046U 26JUN18

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

STRINGER CLIP CORRODED AT BS 500B, STR 27R. R&R CLIP PER DWG AND SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AUXILIARY POWER UNIT INLET CUTOUT UPPER DOUBLER CORRODED AT BS 1088. R&R DOUBLER PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

FORWARD CARGO LT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R ANGLE IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 945, RBL 20. R&R SUPPORT PER SRM & DWG.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

VAPOR BARRIER CRACKED AT BS 663, RBL 13. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 48,009 hrs · 34,442 cycles

VAPOR BARRIER CRACKED AT BS 663, RBL 54. REPAIRED BARRIER IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 48,009 hrs · 34,442 cycles

FORWARD SIDE OF UPPER ATTACH ANGLE CRACKED AT BS 662, RBL 42. REPAIRED ANGLE PER EA AND ER.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 47,825 hrs · 34,325 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 47,825 hrs · 34,325 cycles

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

Part: TAB — BROKEN (RT WING) · airframe 47,488 hrs · 34,114 cycles

MOUNTING TAB FOR R/H WING TRAILING EDGE FIXED PANEL; AFT OF THE ENGINE IS BROKEN OFF OF THE DEFELCTION CONTROL RIB. / ACCOMPLISHED A PERMANENT REPAIR REF SRM 57-51-02-2R-3 REPAIR 3.

Part: PANEL — BROKEN (LT WING) · airframe 46,582 hrs · 33,575 cycles

LEFT WING TRAILING EDGE FIXED PANEL 551CT LIFTED/ BRAKET BROKEN / CLOSING DMA 0511329 REPAIR LT WING TRAILING FIXED UPPER PANEL AND REPAIRED UPPER SUPPORT BEAM PER SRM 57-51-02-2R1; AMM 57-50-01 REMOVED AND REINSTALLED UPPER PANEL REF EA 1-757-14730; NRC D248422 CLSING 39500

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,106 hrs · 32,016 cycles

RIGHT FORWARD OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 43,067 hrs · 31,391 cycles

RT OVERWING EXIT LIGHT LENS COVER MISSING LOCATED LOWER LEFT OF THE DOOR. INSTALLED COVER PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 42,349 hrs · 30,967 cycles

AFT CABIN CEILING ACCESS PANEL EMERGENCY EXIT SIGN MOUNTS BROKEN. R & R SIGN IAW AMM.

Part: RIB — CRACKED (LT WING) · airframe 42,349 hrs · 30,967 cycles

LEFT WING TRAILING EDGE INBOARD OF DEFLECTOR RIB UPPER PANEL FORWARD WEB, OUTBOARD ATTACH ANGLE COMMON TO THE DEFLECTOR RIB CRACKED. R & R THE RIB IAW SRM AND DWG.

Part: WEB — CORRODED (BS 982-989) · airframe 42,349 hrs · 30,967 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 982 - 989, RBL 47. R & R THE WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

FRAME STRINGER CLIP CRACKED AT BS 360, STR 8R. R & R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

FRAME STR CLIP CRACKED AT BS 380, STR 8L. R & R CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 360) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 42,349 hrs · 30,967 cycles

FRAME AT CRACKED AT BS 380, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

FLOORBEAM T-CAP CORRODED AT BS 947, RBL 11. REPAIRED T-CAP IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 727D) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 559) · airframe 42,349 hrs · 30,967 cycles

FRAME CRACKED AT BS 559, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 727D) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 480) · airframe 42,349 hrs · 30,967 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 42,349 hrs · 30,967 cycles

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

Part: STRAP — CORRODED (BS 1012) · airframe 42,349 hrs · 30,967 cycles

FLOOR SUPPORT STRAP CORRODED AT BS 1012, LBL 0. R & R THE STRAP IAW SRM AND DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 42,349 hrs · 30,967 cycles

LEFT HORIZONTAL STABILIZER STIFFENER CRACKED 11 INCHES FROM FORWARD SPAR 92.7. REPAIRED THE STIFFENER IAW SRM.

Part: CREASE BEAM — CORRODED (BS 291-332) · airframe 42,349 hrs · 30,967 cycles

R1 DOOR UPPER SURFACE OF CREASE BEAM CORRODED BETWEEN BS 291 TO 332, RBL 58. R & R CREASE BEAM IAW DWG & SRM.

Part: BRACKET — CORRODED (BS 312-348) · airframe 42,349 hrs · 30,967 cycles

L1 DOOR THRESHOLD MOUNT BRACKET CORRODED BETWEEN BS 312 TO 348, LBL 66. R & R BRACKET IAW SRM & DWG.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 42,349 hrs · 30,967 cycles

LEFT HORIZONTAL STAB CRACKED, 20 INCHES AFT FROM FORWARD SPAR WS 92.70. REPAIRED THE STAB IAW SRM.

Part: CREASE BEAM — CORRODED (BS 947-1006) · airframe 42,349 hrs · 30,967 cycles

R2 DOOR CREASE BEAM ANGLE CORRODED BETWEEN BS 947 - 1006. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 328-340) · airframe 42,349 hrs · 30,967 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 340, LBL 45. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: WEB — CRACKED (BS 295) · airframe 42,349 hrs · 30,967 cycles

R1 DOOR CUTOUT SURROUND LOWER WEB CRACKED AT BS 295, RBL 55. R & R THE WEB IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 42,349 hrs · 30,967 cycles

FORWARD LAVATORY EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: ANGLE — CORRODED (BS 312-360) · airframe 42,349 hrs · 30,967 cycles

L1 DOORWAY UPPER SURFACE OF CREASE BEAM ANGLE CORRODED BETWEEN BS 312 - 360, LBL 58. R & R THE ANGLE IAW DWG.

Part: SEAT TRACK — CORRODED (BS 747-767) · airframe 42,349 hrs · 30,967 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 767 - 747. R & R THE SEAT TRACK IAW SRM.

Part: WEB — CORRODED (BS 792-847) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT SILL WEB CORRODED BETWEEN BS 792 TO 847, RBL 26. R & R THE SILL WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 42,349 hrs · 30,967 cycles

FORWARD CARGO BAY STRINGER CLIP 19L CRACKED AT BS 500D. R & R THE STRINGER CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE STA 727C+10-STA 797, STR 25L CORRODED UPPER SURFACE. REPAIRED Z-CHANNEL IAW SRM.

Part: CARGO TRACK — CORRODED (BS 787-827) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO TRACK CORRODED BETWEEN BS 787 TO 827, RBL 13. R & R THE CARGO TRACK IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (BS 727 BULKHEAD) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT FORWARD BULKHEAD SUPPORT BRACKET CRACKED AT BS. 727, STR. 27R. R & R THE SUPPORT BRACKET IAW SRM & DWG.

Part: RIB — BROKEN (RT WING) · airframe 42,349 hrs · 30,967 cycles

RIGHT WING TRAILING EDGE INBOARD OF THE DEFLECTOR RIB BROKEN. R & R THE RIB IAW SRM AND DWG.

Part: SUPPORT STRAP — CORRODED (BS 787-847) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT SUPPORT STRAP CORRODED BETWEEN BS 787 TO 847, RBL 20. R & R THE SUPPORT STRAP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 727D-BS 767, STR 25R. R & R Z-ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BS 947) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO BAY SIDEWALL SUPPORT ANGLE CORRODED AT BS 947, BETWEEN STRINGERS 21 - 25R. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: FLAP — CRACKED (RT WING) · airframe 42,349 hrs · 30,967 cycles

RIGHT WING OTBD L/E FLAP, OTBD OF ACTUATOR AFT INNER FLANGE CRACKED. REPAIRED FLANGE IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 42,349 hrs · 30,967 cycles

LEFT WING AFT LOWER SPAR WIGGLE PLATE CRACKED INBOARD OF SAIL TAIL WS 253. R & R THE PLATE IAW SRM.

Part: SPAR — CORRODED (LT WING) · airframe 42,349 hrs · 30,967 cycles

LEFT WING FRONT SPAR CORRODED AT THE NR 1 LOWER BOOST PUMP. REPAIRED IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT CENTER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 42,349 hrs · 30,967 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD SCUFF PLATE CRACKED. R & R SCUFF PLATE DWG & SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 41,576 hrs · 30,522 cycles

L2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 41,379 hrs · 30,398 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MT.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 41,132 hrs · 30,254 cycles

R1 DOOR ESCAPE SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,712 hrs · 30,014 cycles

RIGHT EMER LIGHTS INOPERATIVE, BETWEEN ROWS 16 - 19. R & R BATTERY PACK IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 40,640 hrs · 29,970 cycles

AFT GALLEY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,645 hrs · 29,369 cycles

LEFT EMER EXIT HATCH, EMER EXIT LIGHT LENS. R & R LIGHT ASSEMBLY IAW AMM.

Part: PLATE — CRACKED (RT WING) · airframe 39,645 hrs · 29,369 cycles

RIGHT WING LOWER TE SHELF PANEL SUPPORT PLATE WIGGLE CRACKED. R & R WIGGLE PLATE IAW SRM & MM.

Part: COVER — MISSING (CABIN) · airframe 39,352 hrs · 29,208 cycles

LEFT OVERHEAD BIN EMER EXIT LIGHT COVER MISSING AT ROW 17. INSTALLED COVER IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 39,256 hrs · 29,150 cycles

CENTER CABIN OVERHEAD EMER EXIT SIGN LOOSE. R & R LIGHT ASSEMBLY AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 38,011 hrs · 28,425 cycles

R2 DOOR EMER EXIT LIGHT SIGN LENS MISSING. R & R LENS SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,416 hrs · 28,082 cycles

LEFT PAX CABIN EMER LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,416 hrs · 28,082 cycles

RIGHT PAX CABIN EMER LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SEAL — BLOWN (AC BAY) · airframe 37,159 hrs · 27,938 cycles

DECLARED EMER, CABIN ALTITUDE WARNING AT FL400. PERFORMED AN EMER DECENT. GOT CONTROL OF PRESS PASSING 14000 FT. BEFORE DECENT DIFFERENTIAL PRESS WAS 5.8 PSI & CABIN ALTITUDE WAS 9500 FT. FOUND FLEX SEAL IN RT PACK BAY AT PRESS BULKHEAD BLOWN. R & R FLEX SEAL IAW MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 36,484 hrs · 27,567 cycles

AIR TURN BACK, FUMES REPORTED BY AFT FLIGHT ATTENDANT, SMELLED LIKE BURNING PLASTIC COMING THRU GASPER VENTS. R & R AFT NR 2 COFFEE MAKER IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 36,317 hrs · 27,474 cycles

RIGHT OVERWING EXIT EMER FLOOR LIGHT MISSING. INSTALLED LIGHT IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,973 hrs · 27,250 cycles

AFT BULKHEAD CRACKED AT BS 663 LBL 22. R & R BULKHEAD IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,973 hrs · 27,250 cycles

MAIN CABIN RT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW FAS EA & SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,973 hrs · 27,250 cycles

MAIN CABIN NR 1 WINDOW FRAME LT UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW FAS EA & SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,973 hrs · 27,250 cycles

SEAT TRACK 727B CRACKED AT BS 727B LBL 24.75 FWD INBD AT AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,973 hrs · 27,250 cycles

RIGHT E - F WINDOW POST 2ND HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,973 hrs · 27,250 cycles

SEAT TRACK CRACKED AT BS 727B LBL 45.5 FWD INBD AT FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,973 hrs · 27,250 cycles

LEFT WING NR 2 SLAT CRACKED AT FASTENERS ON THE LOWER SURFACE OF THE LE SLAT NOSE SKIN OF ACTUATOR RIBS. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,973 hrs · 27,250 cycles

LEFT WING NR 3 SLAT CRACKED LOWER SURFACE OF THE LE SLAT NOSE SKIN OF ACTUATOR RIBS. REPAIRED NR 3 SLAT IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 35,973 hrs · 27,250 cycles

RIGHT WING NR 7 SLAT CRACKED. REPAIRED NR 7 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,973 hrs · 27,250 cycles

RIGHT WING NR 5 SLAT CRACKED AT FASTENERS ON THE LOWER SURFACE OF THE LE SLAT NOSE SKIN OF ACTUATOR RIBS. REPAIRED NR 5 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,973 hrs · 27,250 cycles

RIGHT WING NR 8 SLAT CRACKED AT FASTENERS ON THE LOWER SURFACE OF THE LE SLAT NOSE SKIN OF ACTUATOR RIBS. REPAIRED NR 8 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,973 hrs · 27,250 cycles

LEFT WING NR 1 SLAT CRACKED AT FASTENERS ON THE LOWER SURFACE OF THE LE SLAT NOSE SKIN OF ACTUATOR RIBS. REPAIR NR 1 SLAT IAW SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 34,264 hrs · 26,305 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: LIGHT — UNSECURE (CABIN) · airframe 31,687 hrs · 24,766 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT FELL OFF. R & R LIGHT ASSY IAW MM .

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,541 hrs · 24,680 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT OUTSIDE INOP. RELAMPED IAW MM.

Part: WEB — CRACKED (LT MLG WW) · airframe 31,422 hrs · 24,592 cycles

LEFT MAIN WHEEL WELL CRACKED AT FS 663, LBL 34 AND LBL 41. REPAIRED WEB IAW SRM.

Part: PANEL — CRACKED (LT WING) · airframe 30,967 hrs · 24,315 cycles

LEFT WING TO BODY FAIRING PANEL 191FL CRACKED AT UPPER EDGE. REPAIRED PANEL PER SRM.

Part: FLAP — CRACKED (LT WING) · airframe 30,967 hrs · 24,315 cycles

LEFT WING NR 2 KRUEGER FLAP CRACKED AT INBOARD CORNER. REMOVED AND REPLACED NR 2 LEFT KRUEGER FLAP IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 30,554 hrs · 24,064 cycles

ENTRY WAY EXIT LIGHT BY FWD ENTRY COVER BROKEN. REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT BASE & COVER IAW M/M.

Part: HOOK — LOOSE (L1 DOOR) · airframe 29,849 hrs · 23,629 cycles

FWD ENTRY DOOR SLIDE GIRT BAR HOOKS ARE LOOSE. REMOVED AND REPLACED PER SRM 51-40-02 FWD ENTRY DOOR SLIDE GIRT BAR HOOK RIVETS C/W T/C 725-61-06.

Part: LENS — MISSING (R2 DOOR) · airframe 29,849 hrs · 23,629 cycles

CABIN AFT SERVICE DOOR (R2) SLIDE LENS IS MISSING. REMOVED AND REPLACED PER AMM CABIN AFT SERVICE DOOR (R2) SLIDE LENS C/W T/C 725-61-06.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,335 hrs · 23,320 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 29,212 hrs · 23,236 cycles

FORWARD LEFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 29,212 hrs · 23,236 cycles

AFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 29,212 hrs · 23,236 cycles

AFT RIGHT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 29,212 hrs · 23,236 cycles

CENTER RIGHT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,212 hrs · 23,236 cycles

FORWARD RIGHT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: FSEU — FAULTY (E&E BAY) · airframe 28,858 hrs · 23,018 cycles

DECLARED EMERGENCY -- LEADING EDGE TRANSIT LIGHT REMAINED ILLUMINATED WHEN FLAP 5 SELECTED. NO LEADING EDGE DEVICES INDICATED ANY EXTENSION. REPLACED LEADING EDGE FLAP AND SLAT HYD FUSE EXTEND AND FSEU PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 28,746 hrs · 22,949 cycles

R1 DOOR EMERGENCY EVAC SLIDE IN ADVERTANTLY FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,052 hrs · 22,568 cycles

SIDEWALL LIGHT ABOVE RT OVERWING EXIT INOP. RELAMPED LIGHT ABOVE RT OVERWING EXIT PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 27,744 hrs · 22,401 cycles

RT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,671 hrs · 22,351 cycles

FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 26,979 hrs · 21,953 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,308 hrs · 23,302 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 25,533 hrs · 21,120 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 24,817 hrs · 20,698 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS COVER BASE. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: RING — WORN (THRUST REVERSER) · airframe 22,353 hrs · 19,274 cycles

REFERENCE SERVICE BULLETIN 737-78-1072, 20MAR2002, REV 00. THE 315A2222-5 CASCADE RING ASSEMBLY IS WORN AND HAS MATERIAL MISSING MEASURING 1.15 INBOARD / OTDB X .16 FWD / AFT X .0085 DEEP ON THE LOWER END FROM CONTACT WITH THE 315A2563-7 LOWER ATTACH FITTING. THE 315A2563-7 LOWER ATTACH FITTING HAS WEAR MEASURING 1.35 X .070 DEEP C/T THE FORWARD UPPER FLANGE. THERE ARE AREAS OF MATERIAL WEAR / GOUGING WITH LARGEST MEASURING APPROX .80 X .40 X .060 DEEP WITHIN THE 315A2222-5 RING ASSEMBLY INBOARD RADIUS. THE AFT MOST BACB30LE6K29 BOLT C/T THE 315A2222-5 CASCADE RING ASSEMBLY AND 315A2402-5 LATCH BEAM FITTING IS MISSING AND THE OPEN HOLE IS ELONGATED MEASURING .514 X .417 ON OUTBOARD SIDE OF -1 BEAM AND .499 X .438 ON INBOARD SIDE OF -1 BEAM. HOLE SHOULD MEASURE .4040 / .4160. THE FWD MOST BACB30LE6K29 BOLT C/T THE 315A2222-5 CASCADE RING ASSEMBLY AND 315A2402-5 LATCH BEAM ASSEMBLY IS SHEARED IN TWO AT THE FAYING SURFACES OF THE -5 RING AND -1 BEAM. ALSO, C/T THE SAME HOLE LOCATION, THERE IS AN APPROX .800 DIA X .005 AREA OF WEAR, (RESEMBLING A COUNTERBORE) AROUND THE HOLE C/T THE -1 BEAM INBOARD SIDE. AFTER REMOVAL OF THE SHEARED BOLT, THE OPEN HOLE IS ELONGATED MEASURING .377 / .392 ON OUTBOARD SIDE OF -1 BEAM AND .377 DIA. ON INBOARD SIDE OF -1 BEAM. HOLE SHOULD MEASURE .3750 / .379. UNABLE TO INSPECT BORES DUE TO OUT OF ROUND CONDITION. EDDY CURRENT INSPECTION PER NDT MANUAL REVEALS NO CRACK-LIKE INDICATIONS ON THE INBOARD OR OUTBOARD SURFACES. UNABLE TO INSPECT BORES DUE TO OUT OF ROUND CONDITION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 328, LBL 9. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 328, BETWEEN RBL 13 TO RBL 55. REPAIRED T-CAP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CORRODED AT BS 510B, RBL 10. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CORRODED AT BS 510B, RBL 10. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CORRODED AT BS 506B, BBL 0. REPAIRED SKIN PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD PRESSURE BULKHEAD WEB CRACKED AT BS 663.75, RBL 36. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 492, STR 26R. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND CABIN SIDEWALL PANEL LOWER AFT CORNER EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 22,354 hrs · 19,274 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 21,853 hrs · 18,958 cycles

L1 DOOR EMERGENCY EXIT SIGN LIGHT LENS MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,215 hrs · 16,094 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD FLIGHT ATTENDANTS FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FITTING — CORRODED (LT WING) · airframe 15,439 hrs · 15,025 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 15,439 hrs · 15,025 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 14,675 hrs · 14,638 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,804 hrs · 14,111 cycles

DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,718 hrs · 14,059 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 20 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 11,303 hrs · 12,617 cycles

DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 9,845 hrs · 11,435 cycles

R1 DOOR EVACUATION SLIDE LOOSE. REPOSITIONED SLIDE ASSY PER MM.