N263WN

Part: MEGAPHONE — NO DISCREPANCY (ZONE 200) · airframe 58,444 hrs · 35,206 cycles

MEGAPHONE IN AFT GALLEY INOPERATIVE. MEGAPHONE OPS CHECK GOOD IAW AMM 25-64-00

Part: SENSOR — FAULTY (ZONE 500 K FLAPS) · airframe 58,071 hrs · 34,958 cycles

LE FLAPS TRANSIT AT FLAPS 10 AND BEYOND. ALL LE DEVICES APPEARED EXTENDED; NO ASYMMETRY WAS DETECTED NOR ANY SKEW. PERFORMED BYTE CHECK, FOUND FAULT 27-81215. SLAT 8 INBD SENSOR FAULTY PER FIM 27-88 TASK 804. R AND R S8 INBD SENSOR PER AMM 27-88-11. OPS CHK GOOD.

Part: TRANSMITTER — MALFUNCTIONED (ZONE 500) · airframe 56,276 hrs · 33,854 cycles

ON APPROACH FLAP WOULD NOT GO BEYOND FLAPS 5 THE LEFT FLAP POSITION TRANSMITTER LAGGED THEN ASYMMETRY BYPASS INITIATED BUT LOOKS LIKE IT MIRROR UP AFTER. I WOULD CHANGE THE LEFT FLAP POSITION TRANSMITTER (T427) AND INDICATOR.<[01] PER FSEU FAULT HISTORY MSG 27-52261 AND AHM DATA; REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPS CHECK GOOD. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW AMM 27-58-02. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (FLAP SYS) · airframe 56,221 hrs · 33,820 cycles

FLAPS FAILED BETWEEN 1 AND 2; EXTENDED FLAPS TO 15 USING ALT FLAP EXTENSION. RNO MX FOUND LEFT POSITION TRANSMITTER CONNECTOR LOOSE BARELY FINGER TIGHT. CLEANED AND CORRECTLY SECURED. SHOULD BE A GOOD FIX.<[01] ACCOMPLISHED FSEU BITE PER FIM 27-51 TASK 801. FOUND NO ACTIVE FAULTS; FAULT HISTORY SHOWS FC 27-52259; TE FLAP SNSR L. CLEANED AND RESECURED LEFT POSITION FLAP TRANSMITTER CONNECTOR; REF AMM 27-58-01; CYCLED FLAPS MULTIPLE TIMES; NO DEFECTS NOTED; OPS CHECK GOOD.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 55,540 hrs · 33,399 cycles

R/H HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED FWD EDGE<[01] R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.

Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 55,539 hrs · 33,398 cycles

OVERWING EMERGENCY EXIT SIGN LOOSE / DANGLING<[01] REINSTALLED EMERGENCY EXIT SIGN PER AMM 33-51-02

Part: HANDLE — BROKEN (ZN 800 DOOR) · airframe 55,540 hrs · 33,399 cycles

AFT PASSENGER DOOR R2 DOOR HANDLE CAM SAFETY WIRE BROKEN.<[01] RE-SECURED AFT GALLEY SVC DOOR HANDLE CAM BOLTS AND SAFETY WIRE REF AMM 20-50-11.<BR>CORRECTION AFT GALLEY SERVICE DOOR.

Part: LAMP — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,294 hrs · 33,258 cycles

RIGHT AFT EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED LAMP IN REF TO AMM 33-51-00

Part: BULB — INOPERATIVE (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

RH EMERGENCY EXIT DORR LOWER EXIT LIGHT BULB OUT<[01] RELAMPED RH EMERGENCY EXIT DOOR LOWER EXIT LIGHT AND PERFORMED GOOD OPERATIONAL CHECK PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD SERVICE DOOR FWD LOWER EXIT LIGHT BULB OUT<[01] RELAMPED FORWARD SERVICE DOOR FWD LOWER EXIT LIGHT AND PERFORMED GOD OPERATIONAL CHECK PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

EMERGENCY BATTRIES PACK (M1672; M1673; N1668; M1670; 1675; M1674) FAIL TEST; DO NOT HOLD CHARGE EMERGENCY BATTRIES PACK (M1672 M1673 M1668 M1670 M1675 M1674) FAIL TEST DO NOT HOLD CHARGE<[01] REMOVED AND REPLACED EMERGENCY BATTRIES PACK (M1672; M1673; N1668; M1670; 1675; M1674) PER AMM 33-51-06-960-805 STEP 4 (A) TO 4 E(5);[02] CERTIFIED ACTION 1;[03] VERIFIED CORRECTIVE ACTION ITEM 1;[04] REMOVED AND REPLACED EMERGENCY BATTRIES PACK (M1672; M1673; N1668; M1670; 1675; M1674) PER AMM 33-51-06-960-805.<BR>PERFORMED GOOD TEST.;[05] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: INSERT — OUT OF POSITION (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FLOOR PANEL 241AF HAS NUMEROUS THROUGH INSERTS THAT DO NOT ALIGN WITH THE UNDERLYING STRUCTURE.<[01] NEW 241AF FLOOR PANEL FABRICATION HAS BEEN COMPLETED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

CRACK FOUND AT R1 DOOR ON STUB FRAME ABOVE SEAL DEPRESSOR BS 294+5 WL274<[01] REMOVED AND REPLACED STUB FRAME UPPER AREA R1 DOOR FWD SIDE PER SRM 51-40-02 AND DWG 141A8370 REV C;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: WEB — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

SHEAR WEB AT BS 1016 RBL 36 WL 208 HAS CORROSION AROUND FASTENER HOLES ON UPPER SURFACE<[01] REMOVED AND REPLACED NEW SHEAR WEB PN#147A5744-14 FROM BS986-BS1016 RBL 36 PER SRM 51-40-02; PER DWG#147A5730 REV C AND PER DWG# 147A000 REV A;[02] VERIFIED CORRECTIVE ACTION 1.

Part: SHIELD — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

CORROSION ON AFT CARGO DOOR CUT-OUT FWD SHIELD AT STA 767+2 & 767+15; WL 158; RBL 22.<[01] REMOVED AND REPLACED AFT CARGO DOOR CUT-OUT FWD SHIELD BS 767 TO BS294 RBL22 WL158 P/N 146A8127-12 LOT#1572705-1 IAW SRM 51-40-02 AND DWG 146A0081 REV A.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: WEB — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT SUB-TRHESHOLD WEB FROM STA 807 TO STA 827+8 RBL 27; WL 158.<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB P/N 146A8123U25 LOT# 1577334-1 IAW SRM 51-40-02 AND DWG 146A8340.;[02] UPDATE STEP 1.<BR>REMOVED AND REPLACED SUB-THRESHOLD WEB P/N 146A8123U25 LOT# 1577334-1 IAW SRM 51-40-02 AND DWG 146A8340. REV A;[03] VERIFIED CORRECTIVE ACTION 2; CARD COMPLETE.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD CABIN COMPARTMENT STRUCTURE AREA; AT BS294.5 TO BS303.9 L/H SIDE STRINGER 15; INTERCOSTAL WITH CRACK MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD ENTRY DOOR BS294.5 TO BS303.9 L/H SIDE; STR15L IAW B-737-700 SRM 51-10-02. SRM 51-40-02-0G-0 AND DWG# 141A8180 REV: C;[02] REJECT: NEW INTERCOSTAL INSTALLATION AT BS294.5 TO BS303.9 STGR 15L; TWO HI-LOCKS FOUND PARTIALLY INSTALLED AT LOWER SIDE. (MARKED) [TTG8Q00VYZXE];[03] THE FAULT WAS CORRECTED WITH THE CUSTOMER CARD #TTG8Q00VYZXE;[04] VERIFIED COMPLETION RII STEPS; CORRECTIVE ACTION 1.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727B+6 TO STA 767; RBL 22; WL 158.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL BS727 TO BS767 RBL22 WL158. IAW SRM 51-40-02-0G-0 & DWG 146A7500 REV: A;[02] VERIFIED RII CORRECTIVE ACTION 1.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727C+5 TO STA 787+2 LBL 22; WL 158.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727 TO STA 847 LBL 22; WL 158. IAW SRM 51-40-02 AND DWG 146A7500 REV: B;[02] REJECTED: STEP 2 CLOSED AMT NOT AUTHORIZED TO COMPLETE OUT STEPS DUE TO MPM REQUIREMENTS.<BR>RAISE STEP 11 INSTALL NUTPLATES AT FLOOR SIDEWALL SUPPORT;[03] REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847 LBL 22 WL 158 IAW SRM 51-40-02 AND DWG 146A7500 ID:0085 REV: A.;[04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

REJECT: CORROSION NOT REMOVED ON FCB AFT BULKHEAD RH SIDE SUPPORT TOP CORNER AT BS 500D; WL194<[01] REPAIRED PER EA 24-153-02618;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE; INTERCOSTAL BS 380 TO BS 400 WL 208 RBL 10 FOUND WITH CRACK (R/H) MARKED.<[01] REMOVED AND REPLACED (1EA.) ANGLE IN THE FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE BETWEEN BS 380 AND BS 400 WL 208 RBL 10 IAW SRM 51-10-02 & SRM 51-40-02 AND DWG# 143A5400; REV: A.;[02] VERIFIED CORRECTIVE ACTION; TASK COMPLETE.

Part: STRAP — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1028; WL 208.1 & LBL 3 APPROX.<[01] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION STRAP STA 1028; WL 208.1; LBL 3 IAW SRM 51-40-02-0G-0 AND DWG# 147A5600.;[02] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION STRAP STA 1028; WL 208.1; LBL 3 IAW SRM 51-40-02-0G-0 AND DWG# 147A5600 REV B;[03] VERIFIED RII CORRECTIVE ACTION 2.

Part: WEB — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT FLOOR WEB STA 1016; WL 208.1 & LBL 38 APPROX.<[01] ?REFER TO FAULT TTG8Q00VTXK7 WHERE EA 24-153-02532 WAS ADDED AS A SUBTASK?<BR>'FAULT RESOLVED ON OTHER FAULT' REPAIR REFERENCE IS SELECTED.;[02] VERIFIED CORRECTIVE ACTION 1; RII REQUIREMENTS TRANSFERRED TO TTG8Q00VTXK7 WHERE EA 24-153-02532 WAS ADDED AS A SUBTASK.

Part: SILL DRAIN — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD CABIN COMPARTMENT ON FLOOR WET AREA MOP SILL WITH CORROSION; BS294 TO BS312 WL208 LBL55 (MARKED).<[01] REMOVED AND REPLACED FORWARD CABIN COMPARTMENT ON FLOOR WET AREA MOP SILL WL208 LBL55 BS 277 - BS 360. PER SRM 51-40-02 AND DWG 141A8110.;[02] REMOVED AND REPLACED FORWARD CABIN COMPARTMENT ON FLOOR WET AREA MOP SILL WL208 LBL55 BS 277 - BS 360. PER SRM 51-40-02 AND DWG 141A8110 REV E.;[03] VERIFIED RII CORRECTIVE ACTION ITEM 2; CARD COMPLETE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD CABIN COMPARTMENT FLOOR STRUCTURE; BRACKET FOUND WITH CORROSION AT BS312 LBL55 WL208 MARKED.<[01] REMOVED AND REPLACED BRACKET AT BS 312 LBL 55 WL 208.1 IAW SRM 51-40-02; AMM 20-50-11 AND DWG 141A5220 REV:-;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.

Part: WEB — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT FLOOR WEB STA 1030; WL 208.1 & RBL 5 APPROX.<[01] REMOVED CORROSION AND REWORKED AFFECTED AREA AT PASSENGER CABIN AFT WET AREA; AT FLOOR WEB STA 1030; WL 208.1; RBL 5 APPROX. IAW EA 24-153-02532.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SILL DRAIN — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

PASSENGER CABIN WET AREA; AFT RH DOOR MOPSILL FOUND CORROSION AROUND SEVERAL FASTENER HOLES BTWN STA 967 TO 985; WL 208.1 APPROX.<[01] REMOVED AND REPLACED RH MOPSILL PN#147A8540U8 IAW SRM 51-40-02; PER DWG#147A8501 REV: A; DWG#147A0000 REV: A AND PER DWG#147A0600 REV: -;[02] VERIFIED CORRECTIVE ACTION 1.

Part: SHIELD — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

CORROSION ON FCB AFT SHIELD AT BS 500+24 RBL 25 WL 156.<[01] REMOVED AND REPLACED FCB AFT SHIELD <BR>IAW SRM 51-40-02 <BR>AND DWG # 143A0080 REV: -;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BS 380 TO BS 400 WL 208 LBL 13 FOUND WITH CRACK (L/H) MARKED.<[01] REMOVED AND REPLACED (1EA.) UPPER CHORD IN THE FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE BETWEEN BS 380 AND BS 400 WL 208 LBL 13 IAW SRM 51-10-02 & SRM 51-40-02 AND DWG# 143A5400; REV: A.;[02] VERIFIED CORRECTIVE ACTION; TASK COMPLETE.

Part: NUT PLATE — CORRODED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

MULTIPLE SPOT WITH CORROSION ON FCB FWD BULKHEAD CENTER SUPPORT NUTPLATE (6 EACH).<[01] REMOVED AND INSTALLED NEW 6EA RECEPTACLES<BR>IAW SRM 51-40-02 AND DWG 453A1600 REV -<BR>FCB FWD BULKHEAD CENTER SUPPORT<BR>BS400 LBL20-RBL20 WL158;[02] VERIFIED CORRECTIVE ACTION 1.

Part: STRAP — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1028; WL 208.1 & RBL 3 APPROX.<[01] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION STRAP STA 1028; WL 208.1 & RBL 3 IAW SRM 51-40-02-0G-0 AND DWG# 147A5730.;[02] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION STRAP STA 1028; WL 208.1 & RBL 3 IAW SRM 51-40-02-0G-0 AND DWG# 147A5730 REV C;[03] VERIFIED RII CORRECTIVE ACTION 2.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL FOUND WITH CRACK AT BS312 TO BS328 WL 208 RBL30 MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL P/N 141A5410-140. LOT:1574381-1. LOCATED BETWEEN BS.312 - BS.328 RBL.30 WL.208 IAW B-737-700. SRM 51-40-02. & DWG#141A5400 REV: -;[02] JOB COMPLETE.

Part: SUPPORT — CORRODED (ZOEN 100) · airframe 54,754 hrs · 32,941 cycles

CORROSION ON FCB AFT BULKHEAD RH SIDE SUPPORT TOP CORNER AT BS 500D; WL194.<[01] FAULT RESOLVED ON FAULT TTG8Q00VUEL8;[02] REPAIRED ON TTG8Q00VUEL8 PER EA 24-153-02618;[03] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

FCB ATTACH ANGLE CRACKED AT BS 500C LBL 26 WL 156.<[01] REMOVED AND REPLACE FCB ATTACH ANGLE BS 500C LBL 26 WL 156 P/N 143A7502-157 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV A.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: STRAP — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1027; WL 208.1 & RBL 18 APPROX.<[01] REMOVED AND REPLACED NEW PASSENGER CABIN AFT WET AREA TENSION STRAP BS 1027 RBL 18 IAW SRM 51-40-02-0G-0 AND DWG #147A5730.;[02] REMOVED AND REPLACED NEW PASSENGER CABIN AFT WET AREA TENSION STRAP BS 1027 RBL 18 IAW SRM 51-40-02-0G-0 AND DWG #147A5730 REV C;[03] VERIFIED RII CORRECTIVE ACTION 2.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FORWARD CABIN COMPARTMENT FLOOR STRUCTURE; INTERCOSTAL FOUND WITH CRACK AT BS 277 TO BS 294.5 WL 208 BL 0 MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL BS 277 TO BS 294.5 WL 208 BL 0. P/N 141A5410U3 LOT#240023 IAW SRM 51-40-02 AND DWG 141A5400 REV-;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241UF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 222DF; UPPER SKIN WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0008.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT CARGO COMPARTMENT FORWARD SCUFF PLATE IS CRACKED.<[01] ALL STEPS COMPLETED;[02] AFT CARGO BAY FWD SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1;[03] CORRECTED MEASUREMENTS;[04] CORRECTED MEASUREMENTS;[05] VERIFIED COMPLETE

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FWD FLOOR PANEL 222AF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222AF WITH AREA OF PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241YF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

FORWARD CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED.<[01] ALL STEPS COMPLETED;[02] REPAIRED FCB AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.<BR>WILL BE INSTALLED ON CUSTOMER CARD:TTG8Q00VRMF3.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] CHANGED IS FAULT ASSOCIATED TO FAILURE TYPE FROM NO TO YES ON BEHALF OF AMT;[04] CERTIFIED

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241ABF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AEF; UPPER SKIN; AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

BS 986 FLOOR BEAM HAS CORROSION AROUND FASTENER HOLE UPPER SURFACE; RBL 43<[01] REMOVED AND REPLACED REPAIR PART PER SRM 51-40-02 AS SHOWN IN SWA EA#1-753-33463 REV IR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT FLOOR PANEL 242XF CENTER AREA OF PANEL IS SOFT.<[01] AFT FLOOR PANEL 242XF WITH CENTER AREA OF PANEL BEING SOFT WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0007.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FWD FLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 231AF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 232BF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — DEBONDED (ZONE 200) · airframe 54,754 hrs · 32,941 cycles

FLOOR PANEL 231ZF LOWER SKIN HAS AREAS OF DISBONDS. (MARKED)<[01] FLOOR PANEL 231ZF LOWER SKIN WITH AREAS OF DISBONDS AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: RIB — CRACKED (ZONE 300) · airframe 54,754 hrs · 32,941 cycles

LT. HORIZONTAL STAB L/E PANEL 331B HAS CRACKED RIB AT LE STA 123.85 (MARKED). LT. HORIZONTAL STAB L/E PANEL 331B HAS CRACKED RIB AT LE STA 105.26 (MARKED).<[01] REMOVED AND REPLACED LT. HORIZONTAL STAB L/E PANEL 331B; RIB AT LE STA 105;26 IAW SRM 51-40-02 AND DWG 186A1001;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: FITTING — CRACKED (ZONE 100) · airframe 54,754 hrs · 32,941 cycles

APU DOOR LWR ROD AFT SUPPORT BRACKET FITING CRACKED<[01] REMOVED APU DOOR LWR ROD AFT SUPPORT BRACKET FITTING IAW SRM 51-40-02-0G-0. REMOVED AND REPLACED FITTING P/N 148A2694-2 LOCATED AT BS.1156; APU DOOR LWR ROD AFT IAW SRM 51-40-02; DWG# 148A2690 REV: B.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.

Part: GIRT BAR — OUT OF ALIGNMENT (FWD SERVICE DOOR) · airframe 53,733 hrs · 32,323 cycles

FWD SERVICE DOOR GIRT BAR MISALLIGNED<[01] ADJUSTED FWD SERVICE DOOR GIRT BAR PER AMM 52-41-00

Part: ISOLATOR — BROKEN (DOOR SLIDE) · airframe 53,315 hrs · 32,067 cycles

FWD SERVICE DOOR AFT SLIDE ISOLATOR IS BROKEN<[01] R&R FWD SERVICE DOOR AFT SLIDE ISOLATOR IAW SRM 51-40-02.;[02] INSPECTED THE REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]

Part: ISOLATOR — CRACKED (PAX DOOR) · airframe 53,315 hrs · 32,067 cycles

AFT ENTRY DOOR FWD ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD UPPER AND LOWER ISOLATORS IAW SRM 51-40-02.;[02] COMPLIED WITH INSPECTION

Part: ACTUATOR — POPPED (ZN 100 FUS LOWER) · airframe 50,614 hrs · 30,345 cycles

FUEL IMBALANCE INFLIGHT; CROSSFEED VALVE CIRCUIT BREAKER FOUND POPPED<[01] FOUND CROSSFEED VALVE ACTUATOR STUCK IN OPEN POSITION. R&R VALVE ACTUATOR PER MM 28-22-21. SUCCESSFULLY TRANSFERRED @ 2000# OF FUEL TO REBALANCE AIRCRAFT.

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 50,404 hrs · 30,213 cycles

RT OVERWING EXIT EMERGENCY SIGN LENS LOOSE<[01] REPLACED LENS PER AMM 33-51-01;[02] VERIFIED INSTALLATION OF NEW EMERGENCY EXIT SIGN IAW AMM 33-51-01

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 50,404 hrs · 30,213 cycles

LT OVERWING EXIT EMERGENCY SIGN LENS LOOSE<[01] REPLACED LENS PER AMM 33-51-01;[02] VERIFIED INSTALLATION OF NEW EMERGENCY EXIT SIGN IAW AMM 33-51-01

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,174 hrs · 29,437 cycles

CRACK HORIZONTAL STAB LEADING EDGE RIB, HSS 114.55. REPLACED LEADING EDGE RIB IAW SRM 51-10-02, SRM 51-40-02, AND DWG 186A1001, REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,174 hrs · 29,437 cycles

CRACKED LEADING EDGE RIB, LE HSS 105.26, RT HORIZONTAL STAB. REPLACED THE RIB AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1304, SHEET 1, REV - .

Part: SUPPORT BRACKET — CRACKED (BS 540) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT BRACKET LT SIDE, BS 540 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, AND 51-10-02, ITEM 9.

Part: WEB — CORRODED (BS 294-312 S22L) · airframe 49,174 hrs · 29,437 cycles

CORROSION ON WEB, BS 294.5 - 312, S22L, WL 174.1 IN THE E/E BAY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 141A1350, SHEET 8, REV -.

Part: LIGHT — CRAZED (CABIN) · airframe 49,174 hrs · 29,437 cycles

CRAZING IN FOUR PHOTOLUMINESCENT FLOOR LIGHTING IN THE PASSENGER CABIN. REPLACED THE FOUR PHOTOLUMINESCENT PROXIMITY LIGHTS IAW AMM 33-51-15-400-802, AND DWG-33500007.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,174 hrs · 29,437 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM-33-51-06-960-805. TESTED OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,174 hrs · 29,437 cycles

INOP EMERGENCY EXIT LIGHT BATTERY PACK LT SIDE AT PASSENGER CABIN (1 EA) 2022-559981. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK LT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805 ; TEST IS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,174 hrs · 29,437 cycles

INOP LOWERED CEILING PANEL BATTERY PACK POSITION LT SIDE AT FWD GALLEY AREA (1 EA). REPLACED LOWERED CEILING PANEL BATTERY PACK IAW AMM 33-51-06-960; TEST IS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,174 hrs · 29,437 cycles

INOPERATIVE BATTERY PACK RT SIDE AT AFT GALLEY AREA. REPLACED THE BATTERY PACK IAW AMM-33-51-06-960-805. TESTED OK.

Part: SUPPORT — CORRODED (BS 727A-807 S25L) · airframe 49,174 hrs · 29,437 cycles

CORRODED SUPPORT ZEE, BS 727A - 807, S25L, WL 156. PERFORMED VISUAL INSPECTION, AND FOUND 9 POINT OF CORROSION.

Part: SUPPORT ANGLE — CRACKED (BS 727) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT ANGLE, BS 727, BL 0 - RBL 5 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 144A2600, SHEET 712, REV -.

Part: CARGO TRACK — CRACKED (BS 747) · airframe 49,174 hrs · 29,437 cycles

CRACK TRACK RBL 13.80, BS 747 AFT CARGO BAY. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3.

Part: STRAP — CORRODED (BS 794-807 S25R) · airframe 49,174 hrs · 29,437 cycles

CORROSION ON STRAP, BS 794 - 807, S25R. WL 157. REPLACED THE STRAP IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, AND DWG 146A8340, SHEET 24, REV A .

Part: SUPPORT — CORRODED (BS 727A-767 S25R) · airframe 49,174 hrs · 29,437 cycles

CORROSION SUPPORT ZEE LOCATED BS727A TO BS767 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT 2022-559945<[01] REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT. I.A.W 737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:146A7500 SHEET 85 REV A.

Part: INTERCOSTAL — CORRODED (BS 767-787 S25R) · airframe 49,174 hrs · 29,437 cycles

CORRODED INTERCOSTAL, BS 767 - 787, S25R, WL156. REPLACED THE INTERCOSTAL IAW SRM 51-40-02, DWG 146A0081, SHEET 31, REV -.

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT ANGLE, BS 907-927, S25-27R IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A7221, SHEET 24, REV -.

Part: SUPPORT BRACKET — BROKEN (PAX DOORWAY) · airframe 49,174 hrs · 29,437 cycles

BROKEN ENTRY DOORWAY LINNING, RT SUPPORT BRACKET IN THE FWD GALLEY AREA. REPLACED SUPPORT BRACKET ON FWD ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 51-10-02 AND DRAWING # 411A2113 REV. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1: <BR>REPLACED SUPPORT BRACKET ON FWD ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 51-10-02 AND DRAWING # 411A2113 REV -

Part: INTERCOSTAL — CORRODED (BS 747-767 S25R) · airframe 49,174 hrs · 29,437 cycles

CORRODED INTERCOSTAL, BS 747-767, S25R, WL 156. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND DWG 146A7500, REV A.

Part: SUPPORT ANGLE — CRACKED (BS 727B-727C) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT ANGLE, BS 727B-727C, LBL54 CEILING AREA IN AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, SRM 51-40-02, & DWG 149A9491, SHEET 38, REV -.

Part: SUPPORT BRACKET — MISSING (AFT PAX DOOR) · airframe 49,174 hrs · 29,437 cycles

MISSING LINING SUPPORT BRACKET AFT ENTRY DOOR LT AT AFT GALLEY AREA 2022-559938<[01] INSTALLED NEW LINING SUPPORT BRACKET AFT ENTRY DOOR LT AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING # 411A2113. REV -;[02] INSTALLED NEW LINING SUPPORT BRACKET AFT ENTRY DOOR LT AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING # 411A2113. REV -

Part: SUPPORT — CORRODED (BS 500-500C) · airframe 49,174 hrs · 29,437 cycles

CORRODED SUPPORT ZEE BETWEEN BS 500 - 500C, LBL 23, WL 156.5 IN THE FWD CARGO BAY. REPAIRED THE SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6.

Part: COLLAR — LOOSE (BS 727B LBL 45) · airframe 49,174 hrs · 29,437 cycles

LOOSE FASTENER FLOOR STRUCTURE COLLAR POSITION B AT BS727B LBL 45 AT PASSENGER CABIN. REPAIRED LOOSE FASTENER COLLAR IAW EA 22-153-03332, EA 22-153-03332-WIP1, AND 22-153-03332-WIP2.

Part: INTERCOSTAL — CORRODED (BS 492-500A) · airframe 49,174 hrs · 29,437 cycles

CORRODED INTERCOSTAL, BS 492.4 - 500A, RBL 23, WL 156.5 IN THE FWD CARGO BAY. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND DWG 143A0080, SHEET 11, REV-.

Part: SUPPORT ANGLE — CORRODED (BS 500D R/LBL23) · airframe 49,174 hrs · 29,437 cycles

SUPPORT ANGLE CORRODED, BS 500D, RBL 23 - LBL 23, WL156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A9481, SHEET 10, REV -.

Part: ANGLE — CRACKED (BS 500D S28R) · airframe 49,174 hrs · 29,437 cycles

CRACKED ANGLE, BS 500D, S28R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 126, REV A.

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 49,174 hrs · 29,437 cycles

CRACKED STRINGER 26L, BS 540 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1, ITEM 4, TABLE 201, 202, 203, AND FIGURE 206.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,174 hrs · 29,437 cycles

CRACKED HORIZONTAL STAB INSPAR RIB 4, HSS 120.30 AND 70 INCHES OF FROM SPAR. PERFORMED REPAIR IAW SRM 55-10-09-2R-5, REPAIR 5, FIGURE 204, DETAIL A.

Part: STRINGER — CRACKED (BS 540 S23R) · airframe 49,174 hrs · 29,437 cycles

CRACK STRINGER 23R, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1, ITEM 4, TABLE 201, 202, 203, FIGURE 206, AND 51-40-02-0G-0.

Part: SUPPORT ANGLE — CRACKED (HORIZONTAL STAB) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT ANGLE ON THE LT HORIZONTAL STAB. REPLACED CHANNEL BALANCE PANEL SUPPORT LOC ON TRAILING EDGE BTW SS138.70 TO SS166.66 AT LT HORIZONTAL STABILIZER AND FASTENERS. IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 185A1102 REV C.

Part: STRINGER — CRACKED (BS 540 S24R) · airframe 49,174 hrs · 29,437 cycles

CRACK STRINGER 24R, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1, ITEM 4, TABLE 201, 202, 203, AND FIGURE 206.

Part: HANDLE — LOOSE (SERVICE DOOR) · airframe 49,174 hrs · 29,437 cycles

LOOSE SERVICE DOOR CONTROL HANDLE MECHANISM. TIGHTENED SERVICE DOOR CONTROL HANDLE MECHANISM IAW AMM 52-41-11-400-801, STEP 3 F, 5, H, - 3 F, 5, N.

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 49,174 hrs · 29,437 cycles

CRACKED ACCESS PANEL 661BB ON THE RT WING TE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.

Part: INTERCOSTAL — CRACKED (BS 500B-500C) · airframe 49,174 hrs · 29,437 cycles

CRACKED INTERCOSTAL, BS 500B - 500C, S26L IN THE FWD CARGO BAY. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS500B TO BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 82 REV - .

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 49,174 hrs · 29,437 cycles

CRACKED GUSSET, BS 500D, S19L IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 174, REV-.

Part: SUPPORT ANGLE — CRACKED (BS 400 S26L) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT ANGLE, BS 400, S26L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 143A7505, REV -.

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 49,174 hrs · 29,437 cycles

CRACK VAPOR BARRIER BS 663, L/H SIDE AT MAIN WHEEL WELL COMPARTMENT.

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 49,174 hrs · 29,437 cycles

CRACKED SUPPORT ANGLE BS 695,BL 0. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 273A9110, SHEET 6, REV A.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 49,174 hrs · 29,437 cycles

CRACKED ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.

Part: BRACKET — CRACKED (BS 540 BL0-RBL24) · airframe 49,174 hrs · 29,437 cycles

CRACKED FLOORBEAM, BS 540, BL 0 - RBL 24. REPLACED TEE BRACKET ON THE FLOORBEAM IAW SRM 51-10-02, ITEM 9.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 49,174 hrs · 29,437 cycles

CRACKED ACCESS PANEL 521QB ON THE LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-10, REPAIR 10.

Part: ACCESS PANEL — CRACKED (BODY FAIRING) · airframe 49,174 hrs · 29,437 cycles

CRACK ACCESS PANEL 191D BODY FAIRING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 49,174 hrs · 29,437 cycles

CRACKED VAPOR BARRIER LH SIDE BS 663. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 47,720 hrs · 28,487 cycles

FWD LH MOUNTING BRACKET FOR KEEL BEAM PANEL 192E IS CRACKED. / [01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02.

Part: BALLAST — SMOKE (CABIN LIGHT) · airframe 47,592 hrs · 28,410 cycles

DURING DESCENT INTO BWI. ; FA. REPORTED STRONG ELECTRICAL SMELL EMANATING FROM FWD. GALLEY. IMMEDIATELY DISSIPATED AFTER GALLEY SWITCH TURNED OFF. / [01] FWD. GALLEY CEILING LIGHT FOUND TO BE INOP. REMOVED AND REPLACED BALLAST ASSY. IAW M/M 33-26-02;[02] CONDITIONAL INSPECTION. DONE IAW M/M 05-51-56 AND FIM TASK 21-00 TASK 806 NO OTHER DEFECTS NOTED

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 47,397 hrs · 28,275 cycles

R-2 DOOR EXTERNAL SLIDE LIGHT INOP / [01] RELAMPED REF AMM 33-51-04

Part: LIGHT — DISCONNECTED (CABIN) · airframe 46,043 hrs · 27,465 cycles

SUPPLEMENTAL INFORMATION: LEFT HAND OVERWING EXIT EMERGENCY EXIT INDEXER LIGHT DOES NOT WORK ; / [01] CONNECTED THE WIRING CORRECTLY AS PER WDM 33-51-13 PAGE 1 SHEET 1 NO OTHER FAULTS NOTED.; [02] ALSO GOOD OP TEST OF LIGHT AS PER AMM 33-51-00-710-801; [03] CERTIFIED ALL WORK COMPLETED AS PER LISTED REFERENCES.; [04] VERIFIED GOOD OP TEST OF LIGHT AS PER AMM 33-51-00-710-801.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 46,043 hrs · 27,465 cycles

AFT CARGO COMPARTMENT AFT SCUFF PLATE CRACKED. REPAIR WELDED CRACKED CORNER IAW SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4).

Part: BRACKET — BROKEN (R/H WING) · airframe 46,043 hrs · 27,465 cycles

WHILE INSTALLING PANEL 651FB FOUND BROKEN ATTACH BRACKET AT RT WING REAR SPAR LOWER CORD AT IRSS 211. ; / [01] REMOVED AND REPLACED BRACKET AT DISCREPANCY AREA P/N 115A5552-2 PO# 729677 /2.1 IAW SRM 51-40-02 AND AIPC 57-50-00-23; [02] VERIFIED CORRECTIVE ACTION 1

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL 21; WL 154; BS 727E+18. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT, MEASURES L=0.750, W=0.300, D=0.008'. ORIGINAL 0.040', REMOVED=0.008', REMAINING THICKNESS 0.032'. THE SIDEWALL SUPPORT IS OUT OF LIMITS. IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, STEP 4.2A. INSPECTED AND VERIFIED ACTION 1;2. THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q006Q898. .

Part: PLATE — CORRODED (AFT CARGO) · airframe 46,043 hrs · 27,465 cycles

AFT CARGO DOOR FWD HINGE LOWER SERREGATATED PLATE HAS SURFACE CORROSION (DOOR SIDE) ; AFT CARGO DOOR FWD HINGE LOWER SERREGATATED PLATE HAS SRFACE CORROSION (DOOR SIDE) / [01] REMOVED AND REPLACED AFT CARGO DOOR FWD HINGE LOWER SERRATED PLATE PER AIPC 52-31-00-15 AND SOPM 20-50-01.; [02] VERIFIED REPLACEMENT OF AFT CARGO DOOR FWD HINGE LOWER SERRATED PLATE PER AIPC 52-31-00-15 AND SOPM 20-50-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL 21; WL 154; BODY STATIONS: 727D+14; 727D+20; 727E+1; 727E+2; 727E+6; 727E+9; 727E+10; 727E+11; 727E+14; AND 727E+17. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT MEASURES :BS727E 9:L=0.950';W=0.250';D=0.009'.ORIGINALTHICKNESS=0.040';MATERIAL REMOVED= 0.009'; REMAINING MATERIAL THICKNESS=0.031'.THE SIDEWALL SUPPORT IS OUT OF LIMITS. I.A.W. SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2; STEP 4.2A. ACCOMPLISHED ON CARD TTG8Q006Q898.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 21;WL 154; BODY STATIONS: 767+18.5 AND 787+14. ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT DISCREPANCY AREA FOUND TO BE OUT LIMITS AT BS 767+18.5 L=1.5' W=0.7' D=0.012' ORIGINAL THICKNESS 0.040' PERS RSM 53-00-1A-2 FIG 103 DETAIL C USED TOOL ID ATS 1671 DATE DUE 01/2022; [02] INSPECTED AND VERIFIED ACTION 1; [03] ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED WITH NC TTG8Q006Q8B1; [04] ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED ON FAULT TTG8Q006Q8B1; [05] VERIFIED ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED ON FAULT TTG8Q006Q8B1.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 21;WL 154; BODY STATIONS:727E+10; 727E+12; 727E+18; 747+1.5; 747+2; 747+5; 747+6; 747+8; AND 747+10. ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT DISCREPANCY AREA. FOUND TO BE OUT OF LIMITS L=1.5' W=0.400'; D=0.014' ORIGINAL THICKNESS 0.040' IAW SRM 53-00-53 1A-2 FIG 103 DETAIL C USED TOOL ID ATS1672 DATE DUE 01/20/22; [02] INSPECTED AND VERIFIED ACTION 1; [03] ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED WITH NC TTG8Q006Q8B1; [04] ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED ON FAULT TTG8Q006Q8B1; [05] VERIFIED ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED ON FAULT TTG8Q006Q8B1.

Part: NONE — CORRODED (FUSLEAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON UNDERSIDE OF INTERCOSTAL BELOW FLOOR SUPPORT STRAP, AT BS 767+6; RBL 20; WL 154. REMOVED CORROSION ON INTERCOSTAL WEB, MEASURES:L=1.900'; W=0.600'; D= 0.020'; ORIGINAL THICKNESS:0.050'; MATERIAL LOSS:0.020'; REMAINING THICKNESS:0.030'. THE WEB INTERCOSTAL IS OUT OF LIMITS IAW SRM 53-60-15-1A-1, ALLOWABLE DAMAGE 1, TABLE 101, STEP 4.G(2). REMOVED INTERCOSTAL WEB IAW SRM 51-40-02. LOCATED AND DRILLED A NEW INTERCOSTAL WEB IAW SRM 51-40-05, AND DWG 146A0081. INSTALLED NEW INTERCOSTAL WEB IAW SRM 51-40-02 AND DWG 146A0081.

Part: BULKHEAD — CRACKED (CENTER WING) · airframe 46,043 hrs · 27,465 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT RBL 36, WL 154. FABRICATED REPAIR PLIES AND INSTALLED IAW SRM 51-70-04-2R-10 PARA 4D.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STATION 747+18; RBL 21; WL 154 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT RBL21, WL 154, BS 747E+18, MEASURES L=0.600'; W=0.500'; D=0.007'. ORIGINAL THICKNESS=0.040', MATERIAL REMOVED, 0.007', REMAINING MATERIALTHICKNESS 0.033'. THE SIDEWALL SUPPORT IS OUT OF LIMITS. I.A.W. SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2; STEP 4.2A. TOOL USED MICROMETER ID:ATS1671; DUE DATE: 01/2022.; [02] INSPECTED AND VERIFIED ACTION 1; [03] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q006Q898..

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT RBL 21; WL 154; BS 727+13; 727A+2; 727A+12; 727A+19; 727B+2; 727B+10; 727B+15; 727C+1; AND 727C+5. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT. MEASURES BS727B+10: L=0.930'; W=0.350'; D=0.010'.ORIGINAL THICKNESS 0.040'. MATERIAL REMOVED= 0.010'. REMAINING MATERIAL THICKNESS=0.030'.THE SIDEWALL SUPPORT IS OUT OF LIMITS. IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2; STEP 4.2A.. ACCOMPLISHED ON CARD TTG8Q006Q898.

Part: BULKHEAD — CRACKED (CENTER WING) · airframe 46,043 hrs · 27,465 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 36, WL 154. REPAIRED IAW SRM 51-70-04-2R-10 PARA 4 STEPS C ; D & E.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION FWD CARGO BAY FWD SHIELD BS420 TO BS420+17 RBL24 WL156 ; / [01] REMOVED SHIELD LOCATED BTW BS 420- BS 440 RBL 24 WL 156 IAW SRM 51-40-02. PART NO HAVE ENTRIES IN SRM BY ALLOWABLE DAMAGE MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAG 9.C.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] RECEIVED SHIELD WITH P/N 143A8126-21. LOCATED AND DRILLED AT FWD CARGO BAY FWD SHIELD BTW BS 420- BS 440 RBL 24 WL 156 IAW SRM 51-40-05; DWG#143A0080; [04] VERIFIED CORRECTIVE ACTION ENTRY 3.; [05] OK TO INSTALL; [06] OK TO INSTALL; [07] INSTALLED AT FWD CARGO BAY FWD SHIELD BTW BS 420- BS 440 RBL 24 WL 156 IAW SRM 51-40-02 & DWG# 143A0080.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION FWD CARGO BAY AFT SHIELD BS 492.4 TO BS 500+18 RBL25 WL156 ; / [01] REMOVED AT FWD CARGO BAY AFT SHIELD BTW BS 492.4 - BS 500A; PER SRM51-40-02; PART NO HAVE ENTRIES IN SRM BY ALLOWABLE DAMAGE MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAG 9.C; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] LOCATED AND DRILLED NEW AFT SHIELD P/N 143A812U31 TO FWD CARGO BAY BTW BS 492.4 TO BS 5001+18 RBL25 WL156 IAW SRM 51-40-05-0G-0 AND DWG 143A0080.; [04] OK TO INSTALL SHIELD AT FWD. CARGO BAY AFT SHIELD.; [05] VERIFIED CORRECTIVE ACTIONS 3 AND 4.; [06] INSTALLED AT FWD CARGO BAY AFT SHIELD WITH P/N 143A8126-31; LOT. 1470603. BTW BS 492.4 - BS 500A; RBL 25; WL. 156 IAW SRM 51-40-02. DWG# 143A0080.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 480+14 TO BS 440+6 LBL25 WL156 ; / [01] REMOVED CORROSION AT FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BTW BS 440+6 TO BS 480+14; LBL 25 WL 156 PER SRM 51-10-02; MAX.MATERIAL LOSS; MEASURE L=1.4' X W= 1.' X D= 0.020' REMAINING THICKNESS IS 0.020'; ORIG.THICKNESS 0.040' BAC1496-444. PER SRM 53-30-53-0I-2 IDENTIFICATION 2 TABLE 2 ITEM[1] REWORKED AREA FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARAG.4.A.(2) DETAIL D FIG.103. RECEIVED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT MAT. IAW SRM 51-40-02-0G-0 AND DWG#143A7500.

Part: NONE — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON ON FLOOR TO SIDEWALL SUPPORT AT RBL 21; WL 154; BODY STATIONS 727E+18; 727E+19; 747; 747+2; 747+5; 747+6; 747+8; 747+10; 747+12; AND 747+14 ; / [10] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY; BETWEEN BS727 TO BS767; RBL21; WL154. IAW SRM 51-40-02-0G-0 AND DWG#146A7500; [11] VERIFIED INSTALLATION OF R/H FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 21 WL 154 PER SRM 51-40-02 AND DWG #146A7500; [12] TASK COMPLETE

Part: SUPPORT — CORRODED (FUSLEAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 400 TO BS 420+6 LBL25 WL156 ; / [01] REMOVED CORROSION AT FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BTW BS 400 TO BS 420+6 LBL 25 WL 156 PER SRM 51-10-02; MAX.MATERIAL LOSS; MEASURE L=1.4' X W= 1.' X D= 0.025' REMAINING THICKNESS IS 0.015'; ORIG.THICKNESS 0.040' BAC1496-444. PER SRM 53-30-53-0I-2 IDENTIFICATION 2 TABLE 2 ITEM[1] REWORKED AREA FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARAG.4.A.(2) DETAIL D FIG.103. USED TOOL. ID:1671. S/N: 65093024. DUE DATE:01/2022.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] THIS TASK CARD WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD TTG8Q006Q82K.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON AFT CARGO DOOR CUTOUT FWD SHIELD AT RBL 22; WL 154; BS: 767+4; 767+6.5; AND 767+10.5, THE SHIELD DOESN'T HAVE ALLOWABLE DAMAGE LIMITS ON SRM. VERIFIED CORROSION OUT OF LIMITS DUE TO NO LIMITS IN SRM. LOCATED AND DRILLED A NEW SHIELD IAW SRM 51-40-05, DWG 146A0081. INSTALLED NEW FWD SHIELD LOCATED ON AFT CARGO BAY DOOR CUTOUT BTW AT BS767 TO BS 794; RBL22; WL154. IAW.SRM 51-40-02 AND DWG#146A0081.; [08] UPDATED PARTS INFORMATION; [09] VERIFIED INSTALLATION AFT CARGO BAY FWD SHIELD BS767 TO BS 794; RBL22; WL154. IAW.SRM 51-40-02 AND DWG#146A0081; [10] TASK COMPLETE; [11] CHANGED THE CORRODED ELEMENT PART NUMBER TO 146A8127-12.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 21;WL 154; BODY STATIONS:727+13; 727B+8; 727C+18; 727D+3; 727D+8; 727D+10; 727D+14; 727D+18; 727E+4; 727E+8 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT DISCREPANCY AREA. FOUND OUT OF LIMITS L=2' W=0.500; D=0.024 ORIGINAL THICKNESS O;040 BE OUT LIMIT IAW SRM 53-00-53 1A-2 USED TOOL ID ATS1672 DATE DUE 03/2021/03/2022; [02] INSPECTED AND VERIFIED ACTION 1; [03] ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED WITH NC TTG8Q006Q8B1; [04] ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED ON FAULT TTG8Q006Q8B1; [05] VERIFIED ALL PROCESS IN THIS CARD WILL BE ACCOMPLISHED ON FAULT TTG8Q006Q8B1.; CHANGED CORRODED STRUCTURE PART NUMBER FROM 146A7500 TO 146A7502-1.

Part: NONE — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON CARGO NET TIE-DOWN BRACKET AT BS 787 TO 787+4; LBL 17; WL 154. REMOVED CORROSION ON CARGO NET TIE-DOWN BRACKET. REWORKED AREA L=4' W= 1.2' D= 0.045' ORIGINAL THICKNESS .250' AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW ACB TIE DOWN TRACK FROM BS 727 + 4 TO BS 867 LBL 17 IAW SRM 51-40-05 AND DWG 146A7500. REMOVED ACB TIE DOWN TRACK IAW SRM 51-40-02. INSTALLED NEW ACB TIE DOWN TRACK IAW SRM 51-40-02 AND DWG 146A7500.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 21;WL 154; BS 747+14; 747+18; 747+18.5; 767+4.5; 767+5.5; 767+7; 767+10; 767+12; 767+14; 767+18. REMOVED CORROSION & FOUND OUT LIMITS AT BS 747+14 .L=1.7' W=0.600' D=0.024' ORIGINAL THICKNESS 0.040 IAWSRM53-00-1A-2 FIGU 103 DETAIL C. INSPECTED AND VERIFIED ACTION 1. PARTIAL LOCATED 7 DRILLED FLOOR SIDE WALL SUPPORT. LOCATED AND DRILLED FLOOR SIDE WALL SUPPORT NEW ZEE ASSEMBY IAW SRM 51-40-05. INSTALLED NEW FLOOR SIDE WALL SUPPORT IAW SRM 51-40-02-0G-0; DWG 146A7500 .

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL 22; WL 154; BODY STATIONS 867+6; 867+9; 887+4 AND 907+10. ; / [10] INSTALLED FLOOR SIDE WALL SUPPORT AT AFT BS867-BS947 RBL 22 WL 154. IAW 737F-700 SRM 51-40-02-0G-0; DWG 146A7500 AND DWG 147A7500 . ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [11] VERIFIED CORRECTIVE ACTION 10.

Part: PANEL — CORRODED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

PANEL 651GB AFT SUPPORT ROD; LOWER ROD END BEARING IS CORRODED ; / [01] REMOVED AND REPLACED PANEL 651GB AFT SUPPORT ROD IAW SOPM 20-50-03.

Part: PANEL — PULLED (R/H WING) · airframe 46,043 hrs · 27,465 cycles

RT WING T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES. FABRICATED REPAIR PLIES, AND INSTALLED IAW SRM 51-70-04-2R-9.PARA 4.J-M.

Part: SLAT TRACK — CORRODED (RT WING NR 6) · airframe 46,043 hrs · 27,465 cycles

RH L/E SLAT #6; OUTBOARD TRACK UPPER SURFACE CORRODED. ; / [01] DEACTIVATED LEADING EDGE FLAPS AND SLATS IAW AMM 27-81-00-040-801.; [02] REMOVED #6 MAIN SLAT TRACK IAW AMM 27-81-21-000-801.; [03] DISCONNECTED LWR ROD END TO #6 MAIN SLAT ACTUATOR IAW AMM 27-81-21-000-802 STEP 4.E.(6)(A) NOTE.; [04] REMOVED PANEL AT SLAT STA. 458.50 IAW AMM 27-81-21-000-801 STEP 4.E.(3).; [05] INSTALLED NEW #6 MAIN SLAT TRACK IAW AMM 27-81-21-400-802 STEPS 5G(1)-(2)(A)3); 5G(3)-(6)(A)2). ALL TORQUES AND SAFETIES VERIFIED AND ALL CLEARANCE CHECKS ALSO VERIFIED. PRIOR TO INSTALLATION OF #6 MAIN SLAT TRACK RECEIVED AN OK TO INSTALL SLAT TRACK.<BR>CAL TOOLS USED:<BR>ATS2321<BR>S/N: 0119121014<BR>DUE: 05/2022<BR><BR>PER2148<BR>S/N: 0420503937<BR>DUE: 02/2022; [06] CHECK ADJUSTMENT AS REQUIRED AND PERFORM LEADING EDGE FLAP AND SLAT SYSTEM OPERATION WITH PRIMARY CONTROL OF #6 SLAT; [07] VERIFIED STEPS 1-5 AND CORRECTIVE ACTION 5; [08] ENTERED PART AND MEASURMENT INFORMATION; [09] CHECKED ADJUSTMENT OF #6 SLAT AND PERFORMED LEADING EDGE FLAP AND SLAT SYSTEM OPERATION WITH PRIMARY CONTROL PER AMM 21-81-21-400-802 STEP 5G(7)-(10). CHECKS GOOD; [10] VERIFIED ADJUSTMENT AND OPERATION OF #6 SLAT PER AMM 21-81-21-400-802 STEP 5G(7)-(10). CHECKS GOOD

Part: SLAT TRACK — CORRODED (RT WING NR 5) · airframe 46,043 hrs · 27,465 cycles

RH L/E #5 SLAT; INBOARD MAIN TRACK UPPER SURFACE; PLATING WORN; PITTING AND LIGHT CORROSION ; / [01] DEACTIVATED LEADING EDGE FLAPS AND SLATS IAW AMM 27-81-00-040-801.; [02] DISCONNECTED #5 I/B MAIN SLAT TRACK IAW AMM 27-81-21-000-802 STEPS 4.E.(1)-(5); [03] COMPLETED REMOVAL OF #5 I/B MAIN SLAT TRACK IAW AMM 27-81-21-000-801 STEP 4.E. (6); [04] VERIFIED PARTIAL STEP 1.; [05] VERIFIED CLEARANCE OF #5 MAIN SLAT TRACK SIDE GUIDES AND STOPS IAW AMM 27-81-21-400-802 STEP 5F.(3)(C); CHECKED OUT GOOD.; [06] VERIFIED COMPLETE STEP 2.; [07] REINSTALLED #5 I/B MAIN SLAT TRACK IAW AMM 27-81-21-400-802 STEPS 5G (1);(2)(A)1)-3); STEPS 5G(3)-(5)(D)2) & (6)(C)1)&2); [08] CAL. TOOLS USED:<BR>I.D. ATS2321<BR>S/N: 0119121014<BR>DUE: 05/2022<BR><BR>I.D. PER2148<BR>S/N: 0420503937<BR>DUE:02/2022; [09] VERIFIED UPDATED STEP 1.; [10] ADJUST #5 I/B SLAT AS REQUIRED AND PERFORM LEADING EDGE FLAP AND SLAT SYSTEM OPERATION WITH PRIMARY CONTROL.; [11] ENTERED PART AND MEASURMENT INFORMATION; [12] CHECKED ADJUSTMENT OF #5 SLAT AND PERFORMED LEADING EDGE FLAP AND SLAT SYSTEM OPERATION WITH PRIMARY CONTROL PER AMM 21-81-21-400-802 STEP 5G(7)-(10). CHECKS GOOD; [13] COMPLETED STEPS 1-3; [14] TAK COMPLETE

Part: PANEL — PULLED (R/H WING) · airframe 46,043 hrs · 27,465 cycles

RT WING T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES. FABRICATED REPAIR PLIES AND INSTALLED, LEAK CHECKED GOOD IAW SRM 51-70-04-2R-9.PARA 4.J-M.

Part: PANEL — PULLED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES. FABRICATED REPAIR PLIES. INSTALLED THE REPAIR PLIES. VACUUM BAGGED AND SET FOR CURE IAW SRM 51-70-04-2R-9 PARA 4. ACCOMPLISHED UT INSPECTION IAW NDTM D6-37239 PART 4; 51-00-02. NO DISBONDS FOUND.

Part: PANEL — PULLED (FUSELAGE) · airframe 46,043 hrs · 27,465 cycles

PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES. FABRICATED REPAIR PLIES. INSTALLED REPAIR PLIES IAW SRM 51-70-04-2R-9 PARA 4.J-M. RESISTANCE CHECKED GOOD IAW AMM 51-21-71-370-801 PARA 3.D(2-4) AND 3.D(7)(A). FASTENER HOLES WERE LOCATED AND COUNTERSINKED USING TEMPLATE PRIOR TO REFINISH IAW SRM 51-70-04-2R-9.PARA 4.N.

Part: NONE — CRACKED (R1 DOOR) · airframe 46,043 hrs · 27,465 cycles

FORWARD SERVICE DOOR #4 BEAM IS CRACKED ON THE INBOARD FLANGE APPROXIMATELY 14 INCHES AFT OF THE INNER SKIN LEADING EDGE. / [01] FWD SERVICE DOOR #4 BEAM WAS REPAIRED ON WORK ORDER #543255 PO #P1506289-1; [02] VERIFIED FWD SERVICE DOOR #4 BEAM WAS REPAIRED ON WORK ORDER #543255 PO #P1506289-1

Part: BATTERY — FAULTY (CABIN) · airframe 46,043 hrs · 27,465 cycles

LIGHTS RELATED TO M1674 BATTERY PACK DO NOT ILLUMINATE. ; / [01] INSTALLED BATTERY AS PER AMM 33-51-06-960-805 STEP 4.D.(5); [02] INSTALLED AND PERFORMED GOOD OP CHECK OF M1674 BATTERY PACK AS PER AMM 33-51-06-960-805 STEP 4.D.(6); [03] VERIFIED INSTALLED AND PERFORMED GOOD OP CHECK OF M1674 BATTERY PACK AS PER AMM 33-51-06-960-805 STEP 4.D.(6).

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 45,510 hrs · 27,131 cycles

LEFT WING I\B MID FLAP O\B T\E WEDGE LOWER SURFACE DELAM APPROX 15'X9' AT THE AFT EDGE STARTS 9' I\B OF THE AFT END. / LEFT WING I\B MID FLAP O\B T\E WEDGE LOWER SURFACE DELAM APPROX 15'X9' AT THE AFT EDGE STARTS 9' I\B OF THE AFT END. COMPLIED WITH EA: 1-757-16816 BY DRYING AREA; CLEAN ING THE DAMAGED AREA; DO A DETAILED INSPECTION OF THE DAMAGED AREA; ACCOMPLISH A TAP TEST OF ADJACENT AREA; ACCOMPLISH BOND TEST OF ADJACENT AREA; DRILL 0.125' DIAMETER HOLES ON 0.5' SPACING THROUGH OUT THE DISBOND AREA; INJECT BMS 5-141 ADHESIVE OR EAUIVALENT; AND APPLY TWO LAYERS OF ALUMINUM FOIL TAPE (SPEED TAPE) TO THE AREA. REPETITIVE INSPECTION ACTION: SPEC LIMIT START: 01/30/2020; INSPECTION THRESHOLD: 8DAYS; REPEAT INSPECTION INT: 8 DAYS. ACTION REQUIRED: PERFORM VISUAL INSPECTION TO ENSURE DAMAGE HAS NOT GROWN OR CHANGED. IF ADDITIONAL DAMAGE IS FOUND CONTACT ENGINEERING BEFORE FURTHER FLIGHT. REPLACE SPEED TAPE IF DEGRADED. PERMANENT REPAIR LIMIT: SPEC LIMIT START: 01/30/2020; PERM REPAIR REQMNT: 118

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,510 hrs · 27,131 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK AT LOCATIONS M01669I AND M01672. R&R BATTERY PACKS AT M01669 AND M01672 PER AMM.

Part: HANDLE — BROKEN (L1 DOOR) · airframe 44,665 hrs · 26,600 cycles

FORWARD ENTRY DOOR ASSIST HANDLE BROKEN. / R&R HANDLE IAW AMM.

Part: SKIRT — WORN (R2 DOOR SLIDE) · airframe 43,406 hrs · 25,791 cycles

R2 DOOR ESCAPE SLIDE SKIRT WORN. / R&R SLIDE PER TASK CARD.

Part: GUARD — FAULTY (LIGHT SWITCH) · airframe 42,892 hrs · 25,473 cycles

EMERGENCY EXIT LIGHTS SWITCH GUARD WON'T STAY DOWN. R&R SWITCH GUARD IAW SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,286 hrs · 25,103 cycles

R1 DOOR GIRT BAR HARD TO HOOK, OUT OF POSITION. REPOSITIONED SLIDE PER AMM & MT.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 42,033 hrs · 24,956 cycles

RT AFT DOOR EXIT SIGN AFT AIRCRAFT FELL OFF. R&R LENS PER MM.

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 41,414 hrs · 24,578 cycles

TOILET SERVICE DOOR 145AL HAS CORROSION BELOW BONDING WIRE END. / REMOVED AND REPLACED TOILET SERVICE DOOR 145AL PER AMM 52-49-07. FIT CHECK GOOD.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,414 hrs · 24,578 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 101.9, 2ND VERTICAL STIFFENER FROM THE FRONT SPAR. REPAIRED RIB PER SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 41,414 hrs · 24,578 cycles

R/H WING: STIFFENER ON PANEL ABOVE DEFLECTION RIB IS CRACKED. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (R/H WING) · airframe 41,414 hrs · 24,578 cycles

R/H WING: INTERCOSTAL ON PANEL ABOVE DEFLECTION RIB IS CRACKED. / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

OVERHEAD L1 DOOR UPPER SILL BEAM FRAME CRACKED AT BS 312, STR 5L. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

MAIN CABIN FLOOR SUPPORT CRACKED BETWEEN BS 500D TO BS 520, BL 0. REPAIRED SUPPORT PER SRM.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 41,414 hrs · 24,578 cycles

VERTICAL FIN RIGHT SKATE ANGLE CHAFFED BETWEEN BS 1005 TO BS 1016. R&R ANGLE PER SRM.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 41,414 hrs · 24,578 cycles

VERTICAL FIN LEFT SKATE ANGLE CHAFFED BETWEEN BS 1005 TO BS 1016. R&R ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

SHEAR TIE CORRODED AT BS 947, BETWEEN STR 26L TO STR 27L. R&R SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,414 hrs · 24,578 cycles

STA 947 BULKHEAD PANEL LOWER ATTACH ANGLE CORRODED IN SEVERAL PLACES. / :REMOVED AND REPLACED BULKHEAD PANEL LOWER ATTACH ANGLE AT STA.947 PER SRM. 51-40-02

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 41,414 hrs · 24,578 cycles

LOWER PRESSURE WEB CRACKED AT BS 663, RBL 48. R&R WEB PER SRM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 41,414 hrs · 24,578 cycles

VERTICAL PRESSURE WEB LOWER ANGLE CRACKED AT BS 663, RBL 32. REPAIRED ANGLE PER EA.

Part: BEAM — CORRODED (CABIN) · airframe 41,414 hrs · 24,578 cycles

CORROSION STA 328 RBL 45.5 AT BASE OF SEAT TRACK. / REPAIRED BS 328 FLOOR BEAM AT RBL 42.5 PER SRM 53-10-51-2R-7 AND EA 1-753-33521.SEE CARD ' TASK AND WIPS' FOR INDIVIDUAL SIGN OFFS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 50 RBL 50. REPAIRED FLOORBEAM PER SRM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 41,414 hrs · 24,578 cycles

R/H STAB FWD UPPER SLIDER SEAL CRACKED. / REMOVED AND REPLACED RH STAB UPPER FWD SLIDER SEAL PER AMM 53-31-31 FWD AND AFT LINK ASSEMBLY WILL BE CONNECTED TO PEDESTAL ON NR G597708

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,414 hrs · 24,578 cycles

RH HORIZONTAL STAB L/E 4TH INTERNAL RIB ATTACH ANGLE IS CRACKED. / R/H HORIZONTAL STABILIZER REPLACED ON NRC G597397 AND G597708.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 41,414 hrs · 24,578 cycles

PANEL 193D HAS 2 SMALL AREAS OF DELAMINATION ON OUTER SURFACE.(MARKED) / REPAIRED PER SRM 51-70-05-2R-11.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 41,414 hrs · 24,578 cycles

CABIN FLOOR PANEL SUPPORT INTERCOSTAL UPPER LEG CRACKED AT FLOOR BOARD HOLE STA.387 BL0. / REMOVED AND REPLACED CABIN FLOOR PANEL SUPPORT INTERCOSTAL UPPER LEG AT STA 387 BL0 AS REQUIRED PER SRM 51-10-02 AND SRM 51-40-02. PLEASE SEE SUBTASKS FOR ADDITIONAL SIGNOFFS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. REPAIRED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 12. REPAIRED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED AT NUTPLATE HOLE STA 344-360 BL0 / REMOVED AND REPLACED INTERCOSTAL AT STA 344-360 BL0 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

R2 DOOR Z ANGLE CORRODED BETWEEN BS 957 TO BS 996. R&R Z ANGLE PER SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 41,414 hrs · 24,578 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 29. REPAIRED WEB PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

FLOORBEAM CORRODED AT BS 328, RBL 51. REPAIRED FLOORBEAM PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

FLOOR SUPPORT CORRODED AT BS 294+5, LBL 12. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

FLOOR SUPPORT NUTPLATE HOLE CORRODED BETWEEN BS 294.5 TO BS 312, LBL 12. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED AT NUTPLATE HOLE STA 328-344 LBL46 / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED AT NUTPLATE HOLE STA 277-294.5 BL0 / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 12. REPAIRED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 33. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 41,414 hrs · 24,578 cycles

INTERCOSTAL CRACKED AT NUTPLATE HOLE STA 321-328 LBL46 / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 41,414 hrs · 24,578 cycles

AFT CARGO COMPARTMENT; UPPER SURFACE OF CARGO FLOOR ANGLE HAS CORROSION AROUND FASTENER HOLE AT APPROX. STA.812 RBL.22. MARKED / REMOVED AND REPLACED AFT CARGO COMPARTMENT; STRAP ; AT STA.812 - 847 ; RBL.22. PER SRM.51-40-02

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 41,414 hrs · 24,578 cycles

AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE ;UPPER SURFACE; HAS CORROSION AROUND FASTENER HOLES FROM STA.727E TO STA.747. MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA.727 TO STA.767 PER SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19L. R&R CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 41,414 hrs · 24,578 cycles

AFT CARGO COMPARTMENT; SUPPORT ANGLE CRACKED. LOCATED BELOW THE WASTE TANK POST AT APPROX. STA.867 LBL.8. MARKED / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 41,414 hrs · 24,578 cycles

AFT CARGO COMPARTMENT; LEFT TRANSITION ANGLE ;UPPER SURFACE; HAS CORROSION AROUND FASTENER HOLE AT STA.727C+6'. MARKED / REMOVED AND REPLACED L/H TRANSITION ANGLE FROM STA. 727 - 847 PER SRM 51-10-02;INSTALLED FASTENERS PER SRM 51-40-02

Part: ANGLE — CORRODED (FWD ENTRY DOOR () · airframe 41,414 hrs · 24,578 cycles

FORWARD ENTRY DOOR (L-1) INBOARD THRESHOLD SUPPORT 'Z' ANGLE HAS CORROSION ON THE UPPER HORIZONTAL SUPPORT AT STA 318 TO 340 LBL 59. MARKED / FORWARD ENTRY DOOR (L-1) INBOARD THRESHOLD SUPPORT 'Z' ANGLE; WAS REMOVED AND REPLACED ON N/R G597664. CORROSION QUESTIONS ANSWERED.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 41,414 hrs · 24,578 cycles

AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE ;UPPER SURFACE; HAS CORROSION AROUND FASTENER HOLES FROM STA.755 TO STA.766. MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA.727 TO STA.767 PER SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19R. R&R GUSSET PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,414 hrs · 24,578 cycles

L1 DOOR Z ANGLE CRACKED IN RADIUS, AT BS 303.9, WL 208. R&R Z ANGLE PER SRM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 41,414 hrs · 24,578 cycles

RIGHT HORZ STAB FWD UPPER SLIDER SEAL CRACKED ON BOTH LEADING AND TRAILING EDGES. / RIGHT HORZ STAB FWD UPPER SLIDER SEAL REMOVED AND REPLACED ON NR G598639

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 41,414 hrs · 24,578 cycles

RT HORIZONTAL STABILIZER RIB STA 120.3, 3RD VERTICAL STIFFENER FROM FRONT CRACKED. R&R HORIZONTAL STABILIZER PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,414 hrs · 24,578 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120, 3RD RIB FROM THE FRONT. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,414 hrs · 24,578 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120, 3RD VERTICAL GUSSET FROM FORWARD END CRACKED AT LOWER CONTOUR. REPAIRED RIB PER SRM.

Part: NONE — BULGED (RT HORIZ STAB) · airframe 41,414 hrs · 24,578 cycles

RIGHT STAB UPPER SKIN BULGING ABOVE TAB TRIM MECHANISM UPPER ATTACH BRACKET. STAB STA 57.9. LOCATED 62.5 INCHES AFT OF THE FWD SPAR. (MARKED) / NEW R/H STAB. WAS ORDERED OUT OF STOCK AND INSTALLED ON N/R G597708. TAG NO: 364699 PN ON: 186A2000-41 SN ON: SAIC0390 PN OFF: SN OFF: 000186

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,414 hrs · 24,578 cycles

RIGHT WING UPPER PANEL MOUNT SUPPORT BRACKET CRACKED NEAR WING ROOT STA 663 / REMOVED AND REPLACED AS PER SRM 51-40-02

Part: SUPPORT STRUT — CRACKED (RT WING) · airframe 41,414 hrs · 24,578 cycles

R/H WING PANEL 651BB SUPPORT STRUT CRACKED / REMOVED AND REPLACED SUPPORT STRUT PER SRM 51-40-02.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 40,497 hrs · 24,003 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,745 hrs · 23,533 cycles

AFT GALLEY EXIT SIGN MISSING THE LENS. REPLACED THE LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,721 hrs · 22,276 cycles

L2 DOOR EXTERIOR SLIDE LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 36,756 hrs · 21,696 cycles

AFT LT EMERGENCY BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 36,756 hrs · 21,696 cycles

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

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 36,363 hrs · 21,460 cycles

FORWARD GALLEY EMERGENCY EXIT SIGN COVER CAME OFF. REINSTALLED THE LENS IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 35,441 hrs · 20,909 cycles

LT EMERGENCY DOOR EXIT SIGN LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,868 hrs · 20,568 cycles

SEAT ROW 16 & 18 EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,868 hrs · 20,568 cycles

AFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,806 hrs · 20,537 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,806 hrs · 20,537 cycles

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

Part: STRAP — FRAYED (CABIN) · airframe 34,742 hrs · 20,496 cycles

RT OVERWING EMERGENCY EXIT DOOR ASSIST STRAP FRAYED. R&R STRAP PER AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 34,742 hrs · 20,496 cycles

FLOOR SUPPORT STRAP CRACKED AT BS 540, BETWEEN RBL 0 TO RBL 24.5. R&R STRAP PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 34,742 hrs · 20,496 cycles

LT EMERGENCY EXIT ESCAPE STRAP CORRODED. R&R STRAP PER MM.

Part: STRAP — CORRODED (CABIN) · airframe 34,742 hrs · 20,496 cycles

RT EMERGENCY EXIT ESCAPE STRAP CORRODED. R&R STRAP PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 34,742 hrs · 20,496 cycles

E&E BAY FLOOR SUPPORT CRACKED AT BS 312 TO 328, LBL 47. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 34,742 hrs · 20,496 cycles

CENTER WING SECTION REAR SPAR LOWER VAPOR BARRIER WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW EA.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 33,945 hrs · 20,026 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MAINTENANCE.

Part: COVER — LOOSE (CABIN) · airframe 33,476 hrs · 19,754 cycles

FORWARD ENTRY DOOR LOWER RT CORNER EMER EXIT LIGHT COVER LOOSE. R & R COVER IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 33,294 hrs · 19,646 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. REPAIRED GIRT BAR IAW EA.

Part: FLAP — LOOSE (L2 DOOR) · airframe 33,305 hrs · 19,655 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR VELCRO FLAP LOOSE. SECURED FLAP IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 32,639 hrs · 19,254 cycles

MID CABIN EMER EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 32,111 hrs · 18,964 cycles

CENTER AISLE OVERHEAD EMER EXIT LIGHT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 31,645 hrs · 18,683 cycles

RIGHT EMER EXIT COVER LENS LOOSE. SECURED LENS IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,345 hrs · 17,898 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT M1673. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,345 hrs · 17,898 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT M1668. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,345 hrs · 17,898 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT M1669. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,345 hrs · 17,898 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT M1672. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,345 hrs · 17,898 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT M1674. R & R BATTERY IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 29,060 hrs · 17,171 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,010 hrs · 16,561 cycles

RIGHT HORIZONTAL STABILIZER STAB RIB STATION 147.9 AFT ATTACH TAB THAT ATTACHES TO TE SPAR INBD & OTBD SIDES CRACKED. REPAIRED RIB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

FORWARD CABIN FLOOR INTERCOSTAL CRACKED AT BS 284 RBL 2.0. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

RIGHT FLANGE SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

LEFT FLANGE SEAT TRACK CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

AFT FASTENER HOLE RT FLANGE SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

FLOORBEAM CORRODED UPPER SURFACE AT BS 986.5 BL 0. REPAIRED FLOORBEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

LEFT FLANGE SEAT TRACK CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

FORWARD CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 328 TO 344 LBL 46.0. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

RIGHT FLANGE SEAT TRACK CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

LEFT FLANGE SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

LEFT FLANGE SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

FORWARD CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, RBL 31.0. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

RIGHT FLANGE SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 28,010 hrs · 16,561 cycles

AFT CARGO DOOR SKIN CREASED 20.75 INCHES FROM FWD EDGE BETWEEN 18 & 26 INCHES FROM TOP. R & R SKIN IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,010 hrs · 16,561 cycles

FORWARD CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 LBL 46.0. R & R INTERCOSTAL IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 26,408 hrs · 15,621 cycles

AFT EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 25,688 hrs · 15,201 cycles

RIGHT WW FWD CTR SECTION BULKHEAD CRACKED 4 INCHES ON THE VAPOR BARRIER, 12 INCHES FROM THE BOTTOM & 8 INCHES FROM THE OTBD END. REPAIRED BARRIER IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 25,688 hrs · 15,201 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.90, 29 INCHES AFT OF THE FWD SPAR. REPAIRED SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 25,205 hrs · 14,908 cycles

RT EMERGENCY EXIT LENS COVER LENS MISSING. INSTALLED COVER IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 24,186 hrs · 14,317 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: LIGHT — UNSECURE (CABIN) · airframe 23,370 hrs · 13,836 cycles

OVERHEAD EMERGENCY EXIT LIGHT FELL OUT AT ROW 11. R&R LIGHT IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 22,597 hrs · 13,400 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITION SLIDE PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,212 hrs · 12,587 cycles

L2 + R2 DOOR EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED L2 + R2 DOOR EXTERIOR EMERGENCY LIGHTS IAW AMM TASK 33-51-04-960-801. OPS CHECK GOOD.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 21,088 hrs · 12,522 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE IS CRACKED AT STA 867 LBL 10. REMOVED AND REPLACED PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,088 hrs · 12,522 cycles

PASSENGER CABIN FLOOR, INTERCOSTAL FROM BL 0 -RBL 24 CRACKED AT STA 540. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,088 hrs · 12,522 cycles

PASSENGER CABIN FLOOR, INTERCOSTAL FROM BL 0 -LBL 24 CRACKED AT STA 540. REMOVED AND REPLACED PASSENGER CABIN FLOOR, INTERCOSTAL FROM BL 0 -LBL 24 CRACKED AT STA 540 PER SRM.

Part: FAIRING — DAMAGED (FUSELAGE) · airframe 21,089 hrs · 12,522 cycles

WING TO BODY FAIRING FWD UPPER 191 FL CRACKED. REPAIRED DAMAGED AREA PER SRM 51-70-05 REPAIR 10.

Part: LENS — LOOSE (CABIN) · airframe 21,089 hrs · 12,522 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT LENS NOT SECURE. REMOVED AND REPLACED PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 21,089 hrs · 12,522 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS NOT SECURE. REMOVED AND REPLACED PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,005 hrs · 12,469 cycles

LEFT EEPLS INOP AT ROW 11. REMOVED & REPLACED EEPLS PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 20,895 hrs · 12,394 cycles

OVERWING EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 20,739 hrs · 12,287 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 20,409 hrs · 12,069 cycles

R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,077 hrs · 11,867 cycles

EEPLS INOP AT ROW 9. REMOVED AND REPLACED EEPLS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,044 hrs · 11,852 cycles

EEPLS INOP AT ROW 1. REPLACED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 20,044 hrs · 11,852 cycles

EEPLS COVER BROKEN AT ROW 1. REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,337 hrs · 11,451 cycles

LEFT EEPLS INOP ROW 15C. REMOVED AND REPLACED EEPLS IAW AMM.

Part: BLADE — OUT OF BALANCE (NR 2 ENGINE) · airframe 18,901 hrs · 11,196 cycles

AIR TURNBACK - NUMBER 2 ENGINE VIBRATION INDICATED 4.0 IN CLIMB BOX STARTED FLASHING WHEN AT FL300. PERFORMED ONBOARD FAN TRIM BALANCE PER AMM. REBALANCED FAN BALANCE WEIGHTS POS 22 / & 29

Part: COVER — CRACKED (CABIN) · airframe 18,896 hrs · 11,188 cycles

RT EEPLS COVERS CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 18,896 hrs · 11,188 cycles

LT EEPLS COVERS CRACKED AT ROW 19. REMOVED AND REPLACED COVER PER AMM.

Part: DUCT — LOOSE (CABIN) · airframe 17,874 hrs · 10,594 cycles

DIVERSION/DECLARED EMERGENCY - IN FLIGHT, RT SIDEWALL AND WINDOW WERE HOT AND SMELL OF SMOKE AT ROW 8. SECURED DISTRIBUTION DUCTS IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 17,694 hrs · 10,491 cycles

DURING SCHEDULED CV CHECK FOUND, OVERWING EMERGENCY EXIT LIGHT SPACERS CRACKED. REMOVED AND REPLACED EEPLS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 16,524 hrs · 9,791 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 15. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 16,524 hrs · 9,791 cycles

DURING SCHEDULED HC1 CHECK, FOUND EELPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LENS — DEFECTIVE (CABIN) · airframe 15,041 hrs · 8,927 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS INOP AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 14,791 hrs · 8,794 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 14,137 hrs · 8,415 cycles

DURING SCHEDULED HC2 CHECK, FOUND LOWER L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,137 hrs · 8,415 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 14 TO ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 14,003 hrs · 8,340 cycles

EEPLS LENS MISSING AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 12,044 hrs · 7,194 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 12,044 hrs · 7,194 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,044 hrs · 7,194 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,524 hrs · 6,880 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: COVER — MISSING (CABIN) · airframe 11,246 hrs · 6,703 cycles

AFT EMERGENCY EXIT DOOR SIGN LIGHT COVER MISSING. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 6,902 hrs · 4,045 cycles

FOUND FWD CABIN EEPLS LIGHT LOOSE. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 6,790 hrs · 3,975 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS LOOSE AT FWD SECTION. REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 6,790 hrs · 3,975 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT LOOSE AT NR 1 POSITION. REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 6,630 hrs · 3,886 cycles

FOUND LT FWD EMERGENCY EXIT FLOOR LIGHT COVER MISSING. REPLACED COVER PER MM.

Part: LENS — OUT OF POSITION (R2 DOOR) · airframe 6,521 hrs · 3,815 cycles

DURING SCHEDULED RON CHECK, R2 DOOR EMERGENCY LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: LENS — MISSING (CABIN) · airframe 6,500 hrs · 3,802 cycles

FOUND FWD EMERGENCY EXIT LIGHT MISSING LENS. REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 4,027 hrs · 2,315 cycles

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