N8514F

Part: BRACKET — DAMAGED (ZONE 600) · airframe 29,507 hrs · 14,715 cycles

RIGHT WING TRAILING EDGE TEE BRACKET LOCATED ABOVE PANEL 651FB, THE ROD ATTACH HOLES ARE ELONGATED. REMOVED AND REPLACED TWO EACH BEARIGS IAW SOPM 20-50-03. REMOVED AND REPLACED THE TEE BRACKET IAW SRM 51-40-02.

Part: BRACKET — DAMAGED (ZONE 600) · airframe 29,507 hrs · 14,715 cycles

RIGHT WING TRAILING EDGE TEE BRACKET LOCATED ABOVE PANEL 651FB. THE ROD ATTACH HOLES ARE ELONGATED. DUPLICATE WRITE UP. SEE TTG8Q019NG09 FOR FAULT CORRECTIVE ACTION IAW MPM 51-03-02.

Part: RIB — WORN (ZONE 600) · airframe 29,507 hrs · 14,715 cycles

RIGHT WING TRAILING EDGE, DEFLECTION CONTROL RIB UPPER TRAILING EDGE ATTACH BOLTS, SHIM PLATE AND FASTENER HOLES ARE WORN. REMOVED DAMAGE FROM DEFLECTION CONTROL RIB UPPER TAB IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .016". DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 57-51-02-1A-1. PERFORMED HFEC INSPECTION OF REPAIR AREA IAW NDT PART 6; 51-00-00. NO DEFECTS NOTED. LOCATED AND DRILLED A DOUBLER FOR TRAILING EDGE SUPPORT BEAM IAW SRM 57-51-02-2R-1. REMOVED AND REPLACED INBD & OTBD SERRATED PLATES IAW SRM 51-40-02. INSTALLED THE DOUBLER FOR T/E SUPPORT BEAM IAW SRM 57-51-02-2R-1. ADJUSTMENT CHECKED GOOD IAW AMM 57-50-01.

Part: WEDGE — DELAMINATED (ZONE 500 SLAT) · airframe 29,507 hrs · 14,715 cycles

NUMBER 1 SLAT DELAMINATED AT THE OTBD END ON THE LOWER PART OF THE T/E WEDGE. REMOVED AND INSTALLED A SERVICEABLE NR 1 SLAT IAW AMM. 27-81-21. RII COMPLETED.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,507 hrs · 14,715 cycles

LEFT SIDE VAPOR BARRIER ATTACH ANGLE, BS 663 CRACKED APPROX. LBL 34, REMOVED THE ATTACH ANGLE IAW SRM 57-10-10-2R-5. CLEANED UP CUT EDGE OF REMAINING ATTACH ANGLE IAW SRM 57-10-10-2R-5. C/W NDT INSP IAW PART 6 51-00-00 PROC 16 & PART 6 51-00-00 PROC 23 OF EXISTING HOLES WITHIN REPAIR AREA, NO DEFECTS. PERFORMED HFEC OF REPAIR AREA IAW NDT PART 6; 51-00-00. NO DEFECTS. LOCATED & DRILLED THE ATTACH ANGLE & REPAIR DOUBLER IAW SRM 57-10-10-2R-5. INSTALLED TANK FASTENERS COMMON TO THE ATTACH ANGLE IAW SRM 57-10-10-2R-5. INSTALLED FASTENERS IN VERTICAL LEG COMMON TO THE ATTACH ANGLE IAW SRM 57-10-10-2R-5, & EA M-24-157-02340. CAP SEALED TANK FASTENERS COMMON TO THE ATTACH ANGLE REPAIR IAW SOPM 20-50-19. REPAIRED THE VAPOR BARRIER ATTACH ANGLE IAW SRM 57-10-10-2R-5 & EA M-24-157-02340.

Part: HANDLE — LOOSE (ZONE 800) · airframe 28,692 hrs · 14,297 cycles

CR RR R1 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED R1 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED. SECURED R1 DOOR AIRFRAME SIDE ASSIST HANDLE IAW B737-800 AMM TASK 52-11-31-400-802.

Part: LENS — DETACHED (ZONE 200) · airframe 28,410 hrs · 14,135 cycles

INDOUND FA REPORTS EXIT EMERGENCY SIGN COVER HAS COME OFF AT MID CABIN. INSTALLED AILE EMERGENCY LENS REF AMM 33-51-03.

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 28,268 hrs · 14,058 cycles

FWD FLASHLIGHT WILL NOT TEST. R&R FLASHLIGHT BATTERY REF AMM 25-64-00 OPS CHECK GOOD

Part: LENS — MISSING (ZONE 200) · airframe 26,909 hrs · 13,360 cycles

F/AS REPORT EMERGENCY EXIT SIGN LIGHT LENSE MISSING ON ONE SIDE AT MID CABIN.<[01] REPLACED MID CABIN EMER. EXIT LIGHTED SIGN LENSE PER AMM 33.51.03; OPS CK NORMAL.

Part: HANDLE — LOOSE (ZONE 800) · airframe 26,442 hrs · 13,103 cycles

AFT SERVICE DOOR; DOOR ASSIST HANDLE LOOSE<[01] RE SECURED AFT SERVICE DOOR ASSIST HANDLE REF AMM 25-21-25

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 26,358 hrs · 13,054 cycles

FWD CARGO AFT CORNER SCUFF PLATE HAS SMALL CRACK.<[01] INSTALLED FWD CARGO DOOR AFT SCUFF PLATE PER AMM 53-11-02.;[02] INSPECTED WORK ABOVE

Part: GUSSET — CRACKED (ZONE 100) · airframe 26,358 hrs · 13,054 cycles

FWD CARGO GUSSET CRACKED AT BS500I STR19R.<[01] REMOVED DAMAGED GUSSET AT BS 500I AND STR19R FOR REPLACEMENT PER SRM 51-40-02.;[02] LOCATED; DRILLED; AND DEBURRED NEW REPLACEMENT GUSSET PER SRM 51-40-05.;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1 AND #2. OK TO INSTALL NEW GUSSET.;[04] REMOVED AND REPLACED FWD CARGO CRACKED GUSSET PER SRM 51-40-02.;[05] INSPECTED AS REQUIRED. CORRECTIVE ACTION #4

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 527C L/H IS INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: SEAL — CRACKED (ZONE 300) · airframe 26,358 hrs · 13,054 cycles

LEFT HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL CRACKED.<[01] REMOVED AND REPLACED L/H HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL AND PERFORMED CLEARANCE AND OPS CHECK PER PER SRM 51-40-02 AND AMM 53-31-31.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Part: SEAL — CRACKED (ZONE 300) · airframe 26,358 hrs · 13,054 cycles

RT HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL AND PERFORMED CLEARANCE AND OPS CHECK ALL WORK PER PER SRM 51-40-02 AND AMM 53-31-31.;[02] CORRECTIVE ACTION #1 C/W

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

CABIN FLOOR SUPPORT FOR PANEL 231XF CRACKED BS537 RBL1 .<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT. SRM 51-40-02;[02] CORRECTIVE ACTION #1 C/W.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

CABIN FLOOR SUPPORT FOR PANEL 231XF CRACKED BS537 LBL1 .<[01] REMOVED PANEL 231UF TO ACCESS REPAIR.;[02] REMOVED AND REPLACED CABIN FLOOR SUPPORT. SRM 51-40-02;[03] CORRECTIVE ACTION #2 C/W.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 50 HAS CORROSION ON UPPER SURFACE.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED DAMAGED INTERCOSTAL AT STA. 947-967; RBL50 IAW SRM 51-40-02.;[04] LOCATED AND DRILLED REPLACEMENT INTERCOSTAL PER SRM 51-40-05.;[05] INSPECTED WORK ACCOMPLISHED IN C/A #3. REMOVED DAMAGED INTERCOSTAL AT STA. 947-967; RBL50 IAW SRM 51-40-02. INSPECTED WORK ACCOMPLISHED IN C/A #4. LOCATED AND DRILLED REPLACEMENT INTERCOSTAL PER SRM 51-40-05.;[06] INSTALLED NEW INTERCOSTAL PER SRM 51-40-02;[07] C/W RII REQUIREMENT FOR C/A 6; INSTALLED NEW INTERCOSTAL PER SRM 51-40-02

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 25 HAS CORROSION ON UPPER SURFACE.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. DAVID BELL (TECHNICIAN); 16-DEC-2024 18:06 UTC<BR>EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED DAMAGED INTERCOSTAL AT STA 947-967; RBL 25 IAW SRM 51-40-02.;[04] LOCATED AND DRILLED REPLACEMENT INTERCOSTAL PER SRM 51-40-05.;[05] INSPECTED WORK ACCOMPLISHED IN C/A #3. LONNIE HERMANN (TECHNICIAN); 17-DEC-2024 10:19 UTC REMOVED DAMAGED INTERCOSTAL AT STA 947-967; RBL 25 IAW SRM 51-40-02.<BR><BR>AND<BR><BR>INSPECTED WORK ACCOMPLISHED IN C/A #4. RICHARD BLACKBURN (TECHNICIAN); 21-DEC-2024 07:39 UTC<BR>LOCATED AND DRILLED REPLACEMENT INTERCOSTAL PER SRM 51-40-05.;[06] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[07] C/W INSPECTION<BR>REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

INTERCOSTAL LOCATED BETWEEN STAS 947-967; LBL 50 CORRODED ON UPPER SURFACE.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED DAMAGED INTERCOSTAL AT STA 947-967; LBL 50 IAW SRM 51-40-02.;[04] MATCH DRILLED NEW INTERCOSTAL PER SRM 51-40-05.;[05] INSPECTED MATCH DRILLING OF PART;[06] RII. OK TO INSTALL NEW INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 50.;[07] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[08] C/W INSPECTION REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241F HAS PULLED FIBERS.<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 241F PER AMM 53-21-00. PANEL INSTALL ON SWA TASK CARD#TTG8Q00X75B6.;[02] VERIFIED REPLACEMENT OF PANEL 241F. VERIFIED PANEL TO BE INSTALLED ON TTG8Q00X75B6.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 221DF HAS PULLED FIBERS.<[01] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] REMOVED AND REPLACED PANEL 221DF I.A.W. AMM 53-21-00;[03] C/W INSPECTION

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 242RF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242RF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75JU.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242RF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75JU.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 232BF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE CARD TTG8Q00X75E3 FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241YF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241YF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75CV.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241YF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75CV.

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 242F HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242F PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AS.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242F PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AS.

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241ABF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241ABF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75BG.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241ABF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75BG.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 221FF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KG FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 222AF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED PANEL 222AF I.A.W. AMM 53-21-00;[02] C/W INSPECTION

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241AAF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241AAF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75BJ.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241AAF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75BJ.

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241XF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241XF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AY.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241XF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AY.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 221GF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KE FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241E HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241E PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75B8.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241E PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75B8.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 221EF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KJ FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 232AF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE CARD TTG8Q00X75E5 FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 242UF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242UF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75JQ.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242UF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75JQ.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 242SF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242SF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75JS.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242SF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75JS.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 231BF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75K2 FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 222BF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED PANEL 222BF I.A.W. AMM 53-21-00.;[02] C/W INSPECTION

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 222DF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KA FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 231AF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75K4 FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 221CF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KN FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 242D HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242D PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AW.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242D PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AW.

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 242E HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242E PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AU.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 242E PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75AU.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 231CF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75K0 FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241ZF HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241ZF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75C4.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241ZF PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75C4.

Part: ACCESS PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 241D HAS PULLED FIBERS.<[01] REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241D PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75BC.;[02] VERIFIED. REMOVED AND REPLACED WITH NEW CABIN FLOOR PANEL 241D PER AMM 53-21-00. PANEL TO BE INSTALL ON SWA TASK CARD# TTG8Q00X75BC.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

PASSENGER CABIN FLOOR ACCESS PANEL 222CF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KC FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]

Part: ANGLE — CRACKED (ZONE 100) · airframe 26,358 hrs · 13,054 cycles

FORWARD CARGO FLOOR STRUCTURE STRINGER CLIP AT STA 500I AND RBL 21.00 HAS CRACK AT RIVET.<[01] DISPLACED BAFFLE AND RH LOWER BULKHEAD CHORD AT STA. 500I. PER SRM 51-40-02.;[02] REMOVED OLD STRINGER CLIP; LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #2. OK TO INSTALL NEW STRINGER CLIP.;[04] REMOVED AND REPLACED STRINGER CLIP AT STA 500I RBL 21 PER SRM 51-40-02.;[05] C/W INSPECTION AS REQUIRED C/A #4;[06] REPLACED AND INSTALLED NEW STRINGER CLIP PER SRM 51-40-02.;[07] INSPECTED AS REQUIRED. CORRECTIVE ACTION #6

Part: ANGLE — CRACKED (ZONE) · airframe 26,358 hrs · 13,054 cycles

FORWARD CARGO FLOOR STRUCTURE STRINGER CLIP AT STA 500I AND LBL 21.00 HAS CRACK AT RIVET.<[01] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.;[02] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.;[03] STEPS 1 THRU 4 ARE NOT SIGNED AND NO SRM REFERENCES NOTED;[04] CHANGED STEPS 1-4 FROM COMPLETE TO PARTIAL FOR INSPECTION FOR INSPECTION BUY OFF.;[05] CERTIFIED;[06] UPDATED THE STEPS WITH SRM REFERENCE.;[07] VERIFIED THE SRM REFERENCE WAS ON STEPS 1-4. NO DEFECTS NOTED.;[08] VERIFIED THE CARD IS COMPLETE AND SIGNED OFF AS REQUIRED.

Part: TIE DOWN — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

FWD LAV. I/B TIE-DOWN FITTING AT STA 303 LBL 13 HAVE CORROSION INTERNALLY IN FASTNER HOLE. REMOVED AND REPLACED FWD LAV INBOARD TIE DOWN FITTING AT STA 303 LBL 13 PER SRM 51-40-02.

Part: NUT PLATE — CORRODED (ZONE 100) · airframe 26,358 hrs · 13,054 cycles

AFT CARGO FLOOR SUPPORT STRAP STA 887; RBL 20 NUT PLATE HAS CORROSION.<[01] REMOVED AND REPLACED CORRODED NUT PLATE ON AFT CARGO FLOOR SUPPORT STRAP PER SRM 51-40-02.;[02] C/W INSP. REMOVED AND REPLACED CORRODED NUT PLATE ON AFT CARGO FLOOR SUPPORT STRAP PER SRM 51-40-02.

Part: WEB — CORRODED (ZONE 100) · airframe 26,358 hrs · 13,054 cycles

AFT CARGO DOOR THRESHOLD WEB STA 794-847; RBL 27 HAS CORROSION.<[01] REMOVED SURFACE CORROSION ON DOOR SILL WEBBING AT STA 794-847. REMOVED OVER .015. PART FOUND TO BE OUT OF LIMITS. REF SRM 53-60-15-1A-1.;[02] REMOVED DOOR SILL WEBBING. SRM 51-40-02;[03] LOCATED AND DRILLED NEW THRESHOLD WEB PER SRM 51-40-02;[04] COUNTERSUNK; ALODINED AND PRIMED FASTENER HOLES ONTO NEW THRESHOLD WEB PER SRM 51-40-08; SOPM 20-43-03 AND 20-44-04 <BR>INSTALLED NUTPLATES ONTO NEW THRESHOLD WEB PER SRM 51-40-02;[05] INSPECTED WORK ABOVE;[06] OK TO INSTALL AFT CARGO DOOR THRESHOLD WEB;[07] INSTALLED NEW AFT CARGO DOOR THRESHOLD WEB PER SRM 51-40-02;[08] VERIFIED<BR>INSTALLED NEW AFT CARGO DOOR THRESHOLD WEB PER SRM 51-40-02

Part: TIE DOWN — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

FWD LAV. I/B TIE-DOWN FITTING AT STA 280 LBL 13 HAVE CORROSION INTERNALLY IN FASTNER HOLE. REMOVED AND REPLACED FWD LAV INBOARD FITTING AT STA 280 LBL 13 PER SRM 51-40-02

Part: FLOORBEAM — COCKED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

AFT R/H LAV; FLOOR BEAM UNDER AFT OUTBOARD MOUNT; HAS EVIDENCE OF CORROSION AT STA. 947.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. DAVID BELL (TECHNICIAN); 16-DEC-2024 21:14 UTC<BR>EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REPAIRED DAMAGE PER SRM 53-70-51-2R-5. REF CARD TTG8Q00XLZ40; EA'S M-24-153-02031 AND M-24-153-02022 FOR FOR INDIVIDUAL STEPS AND SIGN-OFFS.;[04] RII: INSPECTED WORK IN CA# 3

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

AFT L/H LAV; FLOOR BEAM UNDER AFT OUTBOARD MOUNT; HAS EVIDENCE OF CORROSION AT STA. 947.<[01] EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. DAVID BELL (TECHNICIAN); 16-DEC-2024 18:47 UTC<BR>EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REPAIRED DAMAGE PER SRM 53-70-51-2R-5. REF CARD TTG8Q00XLZ40; EA'S M-24-153-02031 AND M-24-153-02022 FOR FOR INDIVIDUAL STEPS AND SIGN-OFFS.;[04] REPAIRED DAMAGE PER SRM 53-70-51-2R-5. REF CARD TTG8Q00XLZ40; EA'S M-24-153-02031 AND M-24-153-02022 FOR FOR INDIVIDUAL STEPS AND SIGN-OFFS.;[05] RII: INSP WORK PERFORMED IN CA# 3.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

AFT R/H LAV; FLOOR BEAM UNDER AFT INBOARD MOUNT; HAS EVIDENCE OF CORROSION AT STA. 947.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.[14] OK TO INSTALL REPAIR PARTS ON STA 947 FLOOR BEAM;[15] INSTALLED RH AND LH STA 947 FLOOR BEAM STRINGER CLIPS PER SRM 51-40-02.;[16] C/W INSPECTION AS REQUIRED C/A # 15 - INSTALLED RH AND LH STA 947 FLOOR BEAM STRINGER CLIPS PER SRM 51-40-02.;[17] REPAIRED DAMAGE PER SRM 53-70-51-2R-5 AND EA'S M-24-153-02031 AND M-24-153-02022.;[18] RII: INSPECTED WORK PERFORMED IN CA #17.<BR>17. MICHAEL PETERSON (TECHNICIAN); 28-DEC-2024 17:47 UTC<BR>REPAIRED DAMAGE PER SRM 53-70-51-2R-5 AND EA'S M-24-153-02031 AND M-24-153-02022.

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

AFT GALLEY SERVICE DOOR; Z ANGLE HAS EVIDENCE OF CORROSION AT STA. 986 +6.<[01] REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4.;[02] BLENDED CORROSION AFT GALLEY SERVICE DOOR Z ANGLE; ORIGINAL MATERIAL THICKNESS IS 0.080'; MATERIAL LOSS WAS 0.022; MAX ALLOWED IS 0.008'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1;[03] REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4;[04] C/W INSPECTION OF C/A LINES 1; 2 & 3; VERIFIED REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

AFT GALLEY SERVICE DOOR; Z ANGLE HAS EVIDENCE OF CORROSION. ( STA. 947 TO STA. 967)<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1.;[02] REMOVED AFT GALLEY SERVICE DOOR Z ANGLE PER SRM 53-70-15;[03] LOCATED DRILLED AND COUNTERSINK HOLES ON NEW A ANGLE PER SRM 53-10-05.;[04] LOCATED DRILLED AND COUNTERSINK HOLES ON NEW A ANGLE PER SRM 53-10-05. COMPLIED WITH INSPECTION.;[05] TREATED AND PRIMED BARE METAL ON NEW CHORD AND AIRCRAFT PER SRM 51-20-01 INSTALLED NEW RH Z? ANGLE FASTENER FROM STA 887+7 TO 987 PER SRM 51-40-02;[09] INSTALLED REMAINING FASTENERS FROM STA 987 TO 1006 PER SRM 51-40-02;[10] REMOVED AND REPLACED AFT GALLEY SERVICE DOOR; Z ANGLE PER SRM 51-40-02. SEE STEPS 1-9 FOR INDIVIDUAL SIGN OFFS;[11] WRONG SRM REFERENCE C/A 3. SRM 53-10-05 DOES NOT EXIST.;[12] C/W WITH RII REQUIREMENT FOR C/A 8; 9 & 10.;[13] REF C/A 3 AND C/A 11. TYPO ON REFERENCE USED SHOULD READ SRM 51-40-05 FOR FASTENER HOLE SIZES USED WHILE DRILLING NEW PART<BR><BR>3. LOCATED DRILLED AND COUNTERSINK HOLES ON NEW AN ANGLE PER SRM 51-10-05. SRM 51-40-05 FOR FASTENER HOLE SIZES USED WHILE DRILLING NEW PART. LOCATED DRILLED AND COUNTERSINK HOLES ON NEW AN ANGLE PER SRM 51-10-05.

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

AFT GALLEY SERVICE DOOR Z ANGLE HAS EVIDENCE OF CORROSION AROUND FASTENERS HOLES.<[01] REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4.;[02] BLENDED CORROSION AFT GALLEY SERVICE DOOR Z ANGLE; ORIGINAL MATERIAL THICKNESS IS 0.080'; MATERIAL LOSS WAS 0.022; MAX ALLOWED IS 0.008'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1;[03] REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4;[04] C/W INSPECTION OF C/A LINES 1; 2 & 3. VERIFIED AFT GALLEY SERVICE DOOR Z ANGLE REMOVAL AND REPLACEMENT WILL BE ACCOMPLISHED ON TTG8Q00XLYB4.

Part: THRESHOLD — CRACKED (ZONE 200) · airframe 26,358 hrs · 13,054 cycles

FORWARD SERVICE DOOR THRESHOLD HAS CRACK AT TOP; FORWARD EDGE. FORWARD SERVICE DOOR THRESHOLD HAS CRACK AT TOP FORWARD EDGE.<[01] REPLACED FORWARD SERVICE DOOR THRESHOLD WITH NEW THRESHOLD. UP-SIZED PILOT HOLES AND COUNTERSUNK I/A/W SRM 51-40-05 AND SRM 51-40-08.;[02] VERIFIED. REPLACED FORWARD SERVICE DOOR THRESHOLD WITH NEW THRESHOLD. UP-SIZED PILOT HOLES AND COUNTERSUNK I/A/W SRM 51-40-05 AND SRM 51-40-08.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,169 hrs · 12,946 cycles

SEVERAL EMERGENCY LIGHTS ARE INOP IN THE CABIN ON BOTH RH AND LH SIDE<[01] M1670<BR>M1676;[02] REMOVED AND REPLACE EMERGENCY LIGHT BATTERY AND CHARGER AT LOCATIONS M1670 AND M1676 PER AMM 33-51-06

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,131 hrs · 12,932 cycles

FWD INBD JUMPSEAT FLASHLIGHT INOP.<[01] REMOVED AND REPLACED FWD INBD JUMP SEAT FLASHLIGHT BATTERY REF B737 AMM 25-64-00 OP/C GOOD

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 24,316 hrs · 11,959 cycles

FWD ENTRY FLASHLIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY FLASHLIGHT AND BATTERY IAW AMM 25-64-00. THIS CLEARS MEL 25-12-01.

Part: SPAR — CRACKED (ZN 300 STABILIZE) · airframe 23,151 hrs · 11,322 cycles

LH HORIZONTAL STAB FRONT SPAR LOWER CHORD DEFLECTED AT STA 234.23 LENGTH 11 WIDTH 0.67 DEPTH 0.062<[01] PERFORMED HFEC NO DAMAGE NOTED PER NDT PART 6 51-00-00 PROCEDURE 23.;[02] REPAIRED PER 23-155-03701 (COMPONENT - SWA - REPAIR - LHS HORIZONTAL STAB FRONT SPAR LOWER CHORD REPAIR AT STAB STA 234 (PN: 186A1000-45; SN: KAI001149) ? TIME LIMITED) [TTG8Q00QL1MT];[03] C/W RII INSPECTION

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 21,973 hrs · 10,642 cycles

LT HORIZONTAL UPPER FRONT SLIDING SEAL IS CRACKED.<[01] R+R SLIDING SEAL REF AMM 53-31-31

Part: FLAP SYSTEM — LOCKED (ZN 500 LEFT WING) · airframe 20,479 hrs · 9,807 cycles

FLAPS WOULD NOT EXTEND BEYOND5 DURING APPROACH<[01] RE-SET-?ELECTRIC FLAPS? TO NORMAL & SET TRIM TAB WITHIN GREEN BAND & CYCLED FLAPS FULL UP/DOWN SEVERAL TIMES PER AMM 27-81-00 OPS NORMAL. OK FOR CONTINUED SERVICE;[02] RE-SET-?ELECTRIC FLAPS? TO NORMAL & SET TRIM TAB WITHIN GREEN BAND & CYCLED FLAPS FULL UP/DOWN SEVERAL TIMES PER AMM 27-81-00 OPS NORMAL. OK FOR CONTINUED SERVICE. CHECKED BOTH FLAP TRANSMISSION INDICATORS - NORMAL;[03] C/W

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,944 hrs · 9,498 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1675 INOPERATIVE. REPLACED THE BATTERY PACK M1675. PERFORMED A GOOD TEST IAW AMM 33-51-06-960-805.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 19,944 hrs · 9,498 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2816 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M2816. PERFORMED A GOOD OPS TEST IAW AMM 33-51-06-960-805.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 19,944 hrs · 9,498 cycles

NR 7 FWD FLAP TRACK FAIRING HAS WIND EROSION DAMAGE AT CENTER MOUNT FASTENER HOLES. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1, PARA 4 D 1. SRM 57-53-70-2R-3, PARA 4 B 2 AND 5 E 3. REMOVED SURFACE FINISHES AND DELAMINATED PLIES TO A REGULAR SHAPE. TAP TESTED AREA, NO DEBONDS NOTED. FWD FLAP TRACK FAIRING WAS REPAIRED IAW SRM 57-53-70-2R-3.

Part: WEB — CRACKED (RT WING) · airframe 19,944 hrs · 9,498 cycles

RIGHT WING; TRANSVERSE WEB ABOVE NR 2 PYLON AFT TIP IS CRACKED ON UPPER LEG AT O/B ATTACH RIVET LOCATION. REMOVED THE TRANSVERSE WEB IAW SRM 51-40-02-0G-0. INSTALLED A NEW TRANSVERSE WEB IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, & AIPC 57-50-00-36A.

Part: PANEL — CRACKED (BS 540) · airframe 19,944 hrs · 9,498 cycles

CRACKED BREAK PANEL STA 540, LBL 1, WL 208. REPLACED CRACKED BREAK PANEL BS 540, BL 0 - LBL 25, WL 208 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0.

Part: SUPPORT PLATE — CORRODED (BS 500D-500F) · airframe 19,944 hrs · 9,498 cycles

FWD CARGO BAY, RT FLOOR TO SIDEWALL PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES, BS 500D+7 - 500F+11, RBL 24.5, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE DAMAGED SUPPORT PLATE AND REPAIRED SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550.

Part: PLATE — CORRODED (BS 500C-500F) · airframe 19,944 hrs · 9,498 cycles

FWD CARGO BAY, LEFT FLOOR TO SIDEWALL PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES BS 500C+12 - 500F+3, LBL 24.5, WL156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. CUT AND REMOVED DAMAGED SECTION IAW SRM 53-0053-2R-5 STEP 4. B, AND EA M-22-153-01550. FABRICATED, LOCATED, AND INSTALLED REPAIR AND TAPERED FILLERS IAW SRM 53-00-53-2R-5 STEP 4. L THRU N, DWG 143A7500, AND EA M-22-153-01550. REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550.

Part: STRAP — CORRODED (BS 767) · airframe 19,944 hrs · 9,498 cycles

CORROSION AFT CARGO BAY FLOOR SPLICE STRAP BS 767+6, RBL 3, WL 156, AROUND FASTENER HOLES. CORROSION FOUND TO BE OUT OF LIMITS. A NEW AFT CARGO BAY FLOOR SPLICE STRAP WILL BE INSTALLED ON CARD TTG8Q00FEJCV.

Part: ATTACH ANGLE — CORRODED (BS 767-787) · airframe 19,944 hrs · 9,498 cycles

CORROSION ON THE AFT CARGO ATTACH ANGLE UNDER SHIELD AT MULTIPLE AREAS UNDER NUT PLATES BS 767 - 787, RBL 21, WL 156. FOUND TO BE OUT OF LIMITS. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0. LOCATED, DRILLED, DEBURRED, AND INSTALLED NUT PLATES TO THE NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, DRAWING 146A8123, AND DWG 146A0081. INSTALLED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0, DWG 146A8123, AND DWG 146A0081.

Part: SHIELD — CORRODED (BS 767-794) · airframe 19,944 hrs · 9,498 cycles

CORROSION ON THE AFT CARGO BAY RT SHIELD FWD OF CARGO DOOR AT MULTIPLE AREAS AROUND FASTENER HOLES, BS 767 - 794, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS. REMOVED THE SHIELD IAW SRM 51-40-02-0G-0. LOCATED, DRILLED, AND DEBURRED A NEW SHIELD IAW SRM 51-40-05-0G-0, AND DRAWING 146A0081. INSTALLED THE NEW SHIELD IAW SRM 51-40-02-0G-0, AND DWG 146A0081.

Part: SUPPORT — CORRODED (BS 727D-847) · airframe 19,944 hrs · 9,498 cycles

CORROSION ON AFT CARGO BAY LT FLOOR TO SIDE WALL SUPPORT PLATE AROUND MULTIPLE FASTENER HOLES BS 727D - 847, LBL 22, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE DAMAGED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-4-05-0G-0. INSTALLED THE NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, DWG 146A0061, AND DWG 146A7500.

Part: SUPPORT — CORRODED (BS 727E-767) · airframe 19,944 hrs · 9,498 cycles

CORROSION ON THE AFT CARGO RT FLOOR TO SIDEWALL SUPPORT PLATE AT MULTIPLE AREAS AROUND FASTENER HOLES BS 727E - 767, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND SRM 51-40-05-0G-0. INSTALLED THE NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, DWG 146A0061, AND DWG 146A7500.

Part: SUPPORT — CORRODED (BS 887-907) · airframe 19,944 hrs · 9,498 cycles

CORROSION ON THE AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE AT MULTIPLE AREAS AROUND FASTENER HOLES, BS 887 - 907, RBL 21, WL 168. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED A REPAIR IAW SRM 53-00-53-2R-5, EA M-22-153=01550, AND SRM 51-40-02-0G-0. INSTALLED THE FLOOR TO SIDEWALL SUPPORT, AND SPLICE IAW SRM 53-00-53-2R-5, SRM 51-40-02-0G-0, DWG 146A7502, DWG 147A7500, AND EA M-22-153-01550. REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 19,944 hrs · 9,498 cycles

LEFT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN HAS AREA OF DELAMINATION. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 57-53-01-1A-1, PARA 4 A 7, AND FIG 102. REMOVED AREA OF DELAMINATED SKIN IAW SRM 51-70-10-2R-0, PARA, 6 & 7. REMOVED AND REPLACED THE WEDGE IAW SOPM 20-50-01, DRAWING 113A2500, & AMM 20-50-11-910-801.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 19,944 hrs · 9,498 cycles

LEFT WING OTBD AFT FLAP LOWER SKIN WAS DELAMINATED AT AFT I/B CORNER. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A-2, PARA 4 A 9. FIG 102. REMOVED AND REPLACED THE FLAP IAW AMM 27-51-22-000-801, STEPS 2D, AND AMM 27-51-22-400-801, STEPS 3.

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 19,944 hrs · 9,498 cycles

LEFT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL 8 WL 167.68. INSTALLED A REPAIR IAW SRM 57-10-10-2R-5.

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 19,944 hrs · 9,498 cycles

RIGHT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 8, WL 167.68. REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5. INSTALLED A REPAIR IAW SRM 57-10-10-2R-5.

Part: GIRT BAR — STUCK (SERVICE DOOR) · airframe 18,207 hrs · 8,486 cycles

SERVICE DOOR GIRT BAR STUCK / [01] STRAIGHTENED GIRT BAR HOOK PER SIP.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 6,777 hrs · 15,038 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE AT L2 DOOR. RELAMPED PER AMM 33-51-04. OPS. OK.

Part: STRINGER — CRACKED (LT WING) · airframe 14,281 hrs · 6,381 cycles

FIXED LEADING EDGE STRINGER #1 L/H AT WS 206-WS 227 IS CRACKED. /

Part: CLOSEOUT PANEL — CHAFED (WING LE) · airframe 14,281 hrs · 6,381 cycles

INBD LEADING EDGE SKIN ASSY CLOSEOUT PANEL IS CHAFFED /

Part: RIB — CRACKED (WING) · airframe 14,281 hrs · 6,381 cycles

FIXED LEADING EDGE RIB AT WS227 IS CRACKED /

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 13,029 hrs · 5,732 cycles

LEFT WING O/B AFT FLAP IS DELAMED AT 1/B AFT CORNER; 11' X 10.5' / REMOVED & REPLACED LEFT WING O/B AFT FLAP FAW AMM 27-51-22.POS L/H O/B P/N OFF 113A3700-23 S/N OFF 002961 P/N ON 113A3700-19 S/N ON 001398AMT 135306

Part: FLASHLIGHT — NOT SEATED (AFT GALLEY) · airframe 12,524 hrs · 5,482 cycles

FLASHLIGHT IN THE AFT GALLEY WAS INOPERATIVE. RESEATED THE AFT FLASHLIGHT IAW SIP.

Part: BATTERY PACK — INOPERATIVE (AFT FLASHLIGHT) · airframe 12,482 hrs · 5,463 cycles

AFT O/B EMERGENCY FLASHLIGHT INOP / REPLACED EMERGENCY FLASHLIGHT BATTERY IN AFT GALLEY PER MM 25-64-00.

Part: DOOR FRAME — CRACKED (EXTERNAL POWER) · airframe 12,283 hrs · 5,371 cycles

EXTERNAL POWER/COMMS PANEL DOOR FRAME CRACKED WILL NOT LATCH. / PERFORMED PERMANENT REPAIR ON EXTERNAL GROUND POWER RECEPTACLE LOWER DOUBLER AT LATCH. PERFORMED HFEC ON WORKED AREA AND FOUND NO CRACKS OR DEFECTS AT THIS TIME. REF SRM 53-10-15-2R-4 REPAIR #4.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,852 hrs · 5,142 cycles

AFT RIGHT INBD FLASHLIGHT DOES NOT TEST. ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / CLEARING DMA LOG PAGE# 0413464 REMOVED AND REPLACED AFT RH INBD FLASHLIGHT. OPS CK GOOD. AMM 25-64-00. CLOSING# 75952

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,653 hrs · 5,052 cycles

AFT OUTBOARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. / CLOSING ACTION LOG# 0413462 R&R FLASHLIGHT BATTERY PER 25-64-00 CL# 75266

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,637 hrs · 5,047 cycles

AFT OUTBOARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 9,168 hrs · 3,971 cycles

FORWARD JUMP SEAT INBOARD EMERGENCY FLASHLIGHT LED INDICATOR NOT FLASHING GREEN. R&R BATTERY PACK IAW CMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,684 hrs · 2,876 cycles

FORWARD EMERGENCY FLASHLIGHT TEST FUNCTION INOP. R&R FLASHLIGHT ASSEMBLY PER AMM.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 4,965 hrs · 2,150 cycles

LEFT SECONDARY HANDLE ON EMERGENCY EXIT DOOR WAS FOUND LOOSE. SECURED THE COVER IAW SIP.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR SLIDE) · airframe 4,285 hrs · 1,843 cycles

R1 DOOR SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED THE GIRT BAR IAW SIP.

Part: CONTROL MODULE — FAULTY (LAVATORIES) · airframe 3,890 hrs · 1,668 cycles

LAVATORYIES STOPPED WORKING IN FLIGHT. R & R THE LOGIC CONTROL MODULE IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 3,257 hrs · 1,387 cycles

LEFT EMERGENCY EXIT SIGN LIGHT LENS BROKEN NEAR THE AFT LAV. R & R THE LENS IAW AMM.

Part: LATCH — BROKEN (CABIN) · airframe 2,553 hrs · 1,079 cycles

FORWARD FLASH LIGHT PANEL LATCH BROKEN. R&R FLASHLIGHT ASSEMBLY IAW CMM.

Part: LATCH — BROKEN (CABIN) · airframe 2,553 hrs · 1,079 cycles

AFT RT FLASHLIGHT PANEL LATCH BROKEN. R&R FLASHLIGHT PANEL ASSEMBLY IAW CMM.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 537 hrs · 246 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED THE SLIDE ASSEMBLY IAW MT.