N452WN

Part: SUPPORT — CRACKED (ZONE 200) · airframe 71,351 hrs · 42,913 cycles

FLIGHT DECK P-6 PANEL C/B SUPPORT CRACKED. REPAIRED FLT DECK P-6 PANEL C/B SUPPORT IAW M-24-125-00167-B, MEASUREMENT OF CRACK: L: 0.275 INCH.

Part: LIGHT — BROKEN (ZONE 200) · airframe 71,355 hrs · 42,914 cycles

BROKEN FLOOR LIGHTING PHOTOLUMINESCENT STRIP IN THE PAX CABIN (10 EA). REPLACED LIGHTS IAW MT 733-50-01, TTG8Q00FRFML.

Part: TRAY — BROKEN (ZONE 200) · airframe 71,355 hrs · 42,914 cycles

BROKEN TRAYS PAX SEATS, ROWS 10D, 12E, 14E, 15E, 16E, AND 18D RT SIDE. REPLACED THE TRAYS IAW CMM 25-21-45-3860, REV 6, PAGE 10088, FIGURE 4, ITEM 60, AND SOPM 20-50-01, REV 40.

Part: TEE ANGLE — DAMAGED (ZONE 600) · airframe 71,355 hrs · 42,914 cycles

ELONGATED HOLE ON TEE ANGLE TRAILING EDGE LOCATED AT ORSS250 APPROX, RT WING. REPLACED THE TEE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-20-01.

Part: ANGLE — ELONGATED (ZONE 600) · airframe 71,355 hrs · 42,914 cycles

ELONGATED HOLE ON TEE ANGLE TRAILING EDGE LOCATED AT ORSS250 APPROX, RT WING. REPLACED THE TEE ANGLE LOCATED TRAILING EDGE IAW SRM 51-10-02, ITEM 9, AND SRM 51-20-01.

Part: SUPPORT BEAM — CRACKED (ZONE 600) · airframe 71,355 hrs · 42,914 cycles

CRACK ON SUPPORT BEAM LOCATED TRAILING EDGE ORSS 280 ON THE RT WING. REPLACED THE SUPPORT BEAM IAW SRM 51-40-02-0G-0, AND DWG 115A3712, SHEET 6, REV B.

Part: SUPPORT ANGLE — ELONGATED (ZONE 500) · airframe 71,355 hrs · 42,914 cycles

ELONGATED HOLE TRAILING EDGE SUPPORT ANGLE LOC AT LEVEL ORSS 250 ON THE LT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND SRM 51-20-01.

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 71,355 hrs · 42,914 cycles

CRACKED DEFLECTION CONTROL RIB TRAILING EDGE SUPPORT ANGLE LOCATED AT ORSS 271, RT WING. REPLACED DEFLECTION CONTROL RIB TRAILING EDGE SUPPORT ANGLE IAW SRM 51-40-02-0G, AND SRM 51-10-02-0G, ITEM 9. CRACK MEASURED: L=0.550 INCH.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 71,355 hrs · 42,914 cycles

CRACKED AFT CORNER SCUFF PLATE, AFT CARGO BAY DOOR CUTOUT. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 71,355 hrs · 42,914 cycles

CRACKED DEFLECTION CONTROL RIB, TRAILING EDGE SUPPORT ANGLE LOCATED AT ORSS 270, LT WING. REPLACED THE DEFLECTION CONTROL RIB TRAILING EDGE SUPPORT ANGLE LOCATED ORSS 270 LT WING IAW SRM 51-40-02-0G, AND SRM 51-10-02-0G, ITEM 9. CRACK MEASUREMENT: L=0.550 INCH.

Part: RETAINER — MISSING (ZONE 100) · airframe 71,355 hrs · 42,914 cycles

MISSING CUT OUT DOOR RETAINER LOCATED ON UPPER SILL IN FWD CARGO BAY (2 EA). INSTALLED THE RETAINERS IAW SOPM 20-50-19.

Part: LENS — MISSING (ZONE 200) · airframe 71,355 hrs · 42,914 cycles

MISSING EMERGENCY LIGHT LENS ON THE BULL NOSE OVERHEAD STOWAGE BIN 11 LT SIDE. INSTALLED THE LENS IAW AMM 33-51-03-960-802.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 71,355 hrs · 42,914 cycles

CRACKED SUPPORT ANGLE FLOOR STRUCTURE, BS 695, LBL 24.75 IN PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, DWG 273A9110, SHEET 6, REV A, & DWG:111A6000, SHEET 178, REV-.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 71,355 hrs · 42,914 cycles

CRACKED SUPPORT ANGLE FLOOR STRUCTURE, BS 695, AND RBL 24.5. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 273A9110, SHEET 6, REV A, & DWG 111A6000, SHEET 178, REV-.

Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 71,355 hrs · 42,914 cycles

DELAMINATED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL ON THE BODY FAIRING IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: RIB — CRACKED (ZONE 100) · airframe 71,355 hrs · 42,914 cycles

CENTER TANK RIB CRACKED AT BS 540, LBL 25, WL 202. REPLACED VERTICAL STIFFENER RIB & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 111A2001, SHEET 77, REV-, & DWG 111A6000, SHEET 301, REV-.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 71,355 hrs · 42,914 cycles

CENTER TANK RIB CRACKED AT BS 540, LBL 25, WL 202. REPLACED VERTICAL STIFFENER RIB AND FASTENER LOCATED IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 111A2001, SHEET 77, REV-, & DWG 111A6000, SHEET 301, REV-.

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 71,355 hrs · 42,914 cycles

CRACKED LOWER SURFACE OF LEADING EDGE SLAT 2 NOSE SKIN AT ACTUATOR LOCATION, AROUND FASTENER AT LT WING. REPAIRED SLAT 2 LOWER SURFACE OF LEADING EDGE NOSE SKIN IAW SRM 57-42-01-2R-8, REPAIR 8, FIGURE 202, ALTERNATIVE 1, SHEET 2.

Part: ATTACH BRACKET — CRACKED (ZONE 600) · airframe 71,351 hrs · 42,913 cycles

FWD ATTACH BRACKET FOR INBD SUPPORT FOR PANEL 651AT ON R/H WING IS CRACKED. REMOVED AND REPLACED FWD ATTACH BRACKET FOR INBD SUPPORT FOR PANEL 651AT ON RT WING IAW SRM 51-40-02.

Part: FASTENER — CRACKED (ZONE 100) · airframe 71,351 hrs · 42,913 cycles

CENTER TANK RIB CRACKED AT STA 540 25LBL WL 202. BS 540 LBL 25 WL 202. FAULT RESOLVED IN OTHER FAULT SEE TTG8Q018YKSY.

Part: RIB — CRACKED (FUEL CELL) · airframe 71,351 hrs · 42,913 cycles

CENTER TANK RIB CRACKED AT STA 540 25LBL WL 202. BS 540 LBL 25 WL 202. FAULT RESOLVED IN OTHER FAULT SEE TTG8Q018YKSY.

Part: ISOLATOR MOUNT — BROKEN (ZONE 800) · airframe 71,351 hrs · 42,913 cycles

AFT PASSENGER ENTRY DOOR SLIDE AFT ATTACH POINT HAS TWO SLIDE ATTACH ISOLATORS BROKEN. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-A00729.

Part: SLIDE — LOOSE (ZONE 800) · airframe 69,458 hrs · 41,691 cycles

FA REPORT AFT ENTRY SLIDE LOOSE<[01] VERIFIED AFT ENTRY DOOR ESCAPE SLIDE VELCRO SECURED PER AMM 25-66-01

Part: COFFEEMAKER — SMOKE (ZONE 200) · airframe 69,028 hrs · 41,423 cycles

FA SAID #1 AFT COFFEE MAKER SMELLED OF SMOKE WHEN TURNED ON. <[01] R&R #1 AFT GALLEY COFFEE MAKER OPS CHECK GOOD REF AMM 25-30-01.

Part: SKIRT — WORN (ZONE 800) · airframe 68,969 hrs · 41,382 cycles

AFT GALLEY SERVICE DOOR ESCAPE SLIDE SKIRT WORN<[01] R&R AFT GALLEY SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01.<BR>REF. TTG8Q00YSHZK.;[02] INSPECTION C/W R&R AFT GALLEY SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01.<BR>REF. TTG8Q00YSHZK.

Part: DOOR — CRACKED (ZONE 700) · airframe 68,969 hrs · 41,382 cycles

L/H MLG STRUT DOOR IS CRACKED<[01] OK TO CONTINUE PER CDL 32-10-3 XC SP1B. REMOVED L/H MLG STRUT DOOR. REF AMM 32-13-11

Part: TAILPIPE — FIRE (NR 2 ENGINE) · airframe 67,898 hrs · 40,723 cycles

AFTER ENGINE SHUTDOWN; RAMP REPORTED TAIL PIPE FIRE IN THE EXHAUST NOZZLE #2 ENG NO ENGINE FIRE INDICATIONS IN THE FLIGHT DECK. FIRE DEPARTMENT ARRIVED AND DISCHARGED FIRE EXTINGUISHING AGENT HALTRON AFTER ENGINE SHUTDOWN RAMP REPORTED TAIL PIPE FIRE IN THE EXHAUST NOZZLE. NO ENGINE FIRE INDICATIONS IN THE FLIGHT DECK. FIRE DEPARTMENT ARRIVED AND DISCHARGED FIRE EXTINGUISHING AGENT HALTRON INTO EXHAUST NOZZLE AREA. FIRE WAS EXTINGUISHED.<[01] C/W INSPECTION AFTER AN ENGINE FIRE PER AMM 71-00-00. NO DAMAGE OR DEFECTS NOTED. FIRE EXTINGUISHING AGENT WAS DETERMINED TO BE SAFE FOR USE PER PPE AND NO FURTHER ACTION REQUIRED. DRY MOTORED #2 ENG PER AMM 71-00-00. NO DEFECTS NOTED AND A/C OK FOR SERVICE.<BR><BR>3839906

Part: SIGN — DETACHED (ZONE 200) · airframe 67,847 hrs · 40,693 cycles

EXIST SIGN OVER THE FO SIDE REAR EXIT FELL OFF<[01] RESECURED LENS IAW AMM 33-51-01

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 66,221 hrs · 39,671 cycles

FWD GALLEY BULKHEAD EXIT LIGHT LENS CAME OFF<[01] REPLACED FWD ENTRY EXIT LIGHT LENS PER SIP OPS CHECK NORMAL

Part: SKIRT — OUT OF ADJUST (L2 SLIDE) · airframe 65,652 hrs · 39,325 cycles

L2 DOOR SLIDE SKIRT RUBS ON SCUFF PLATE WHILE OPENING AND CLOSING THE DOOR<[01] ADJUSTED AFT ENTRY DOOR; DOOR MOUNTED ESCAPE SLIDE GIRT BAR Z-FOLD WITH MT 725-61-06 REF: TTG8Q00RB8CS;[02] VERIFIED ADJUSTMENT TO AFT ENTRY DOOR; DOOR MOUNTED ESCAPE SLIDE GIRT BAR Z-FOLD.

Part: LENS — LOOSE (CALL LIGHT) · airframe 65,652 hrs · 39,325 cycles

UPPER CEILING PANEL BETWEEN LAV A DOOR AND COCKPIT DOOR ATTENDANT CALL LIGHT LENSE IS LOOSE<[01] REMOVED AND REPLACED LENS AT THE UPPER CEILING PANEL BETWEEN LAV A DOOR AND COCKPIT DOOR PER REF AMM 33-51-01-960-801. PERFORMED CALL LIGHT TEST FOUND NORMAL.;[02] CORRECTION STEP 1<BR>REMOVED AND REPLACED LENS AT THE UPPER CEILING PANEL BETWEEN LAV A DOOR AND COCKPIT DOOR PER REF AMM 33-51-01-960-801. PERFORMED CALL LIGHT TEST FOUND NORMAL PER AMM 23-42-00-710-802;[03] REMOVED AND REPLACED LENS AT THE UPPER CEILING PANEL BETWEEN LAV A DOOR AND COCKPIT DOOR PER REF AMM 33-51-01-960-801. PERFORMED CALL LIGHT TEST FOUND NORMAL PER AMM 23-42-00-710-802;[04] VERIFIED STEP 3

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,652 hrs · 39,325 cycles

MULTIPLE EMERGENCY LIGHTS IN PAX CABIN INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1672; M1674 AND M1675 AS PER REF B-737; AMM 33-51-06-960-805. OPERATIONAL TEST FOUND NORMAL.;[02] VERIFIED STEP 1.;[03] PERFORMED CONTINUITY CHECKS BETWEEN BATTERY PACK M1670 CONNECTOR D10716 PINS 3;4 BATTERY PACK M1673 CONNECTOR D10746 PINS 3;4 BATTERY PACK M1668 CONNECTOR D10712 PINS 3;4 UP TO DISCONNECT BRACKET AB0340A CONNECTOR D40196J PINS 1;2 FOUND NORMAL PER WDM 33-51-11 SHEET 2 FURTHER T/S REQUIRED;[04] CORRECTION TO STEP 3<BR>PERFORMED CONTINUITY CHECKS BETWEEN BATTERY PACK M1670 CONNECTOR D10716 PINS 3;4 BATTERY PACK M1673 CONNECTOR D10746 PINS 3;4 BATTERY PACK M1668 CONNECTOR D10712 PINS 3;4 UP TO DISCONNECT BRACKET AB0340A CONNECTOR D40196J PINS 1;2 FOUND NORMAL PER WDM 33-51-11 SHEET 2 FURTHER T/S REQUIRED<BR>TOOL: MULTIMETER<BR>B/C 176391<BR>CAL DUE 13 OCT 24;[05] VERIFIED STEP 4.;[06] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674/M1675 & BATTERY POWER SUPPLY M1670 & M1675 I/A/W BOEING AMM 33-51-06-960-805 & 33-51-06-960-806. OPERATIONAL TEST PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[07] VERIFIED STEP 6

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,652 hrs · 39,325 cycles

MULTIPLE EMERGENCY LIGHTS IN PAX CABIN INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1672; M1674 AND M1675 AS PER REF B-737; AMM 33-51-06-960-805. OPERATIONAL TEST FOUND NORMAL.;[02] VERIFIED STEP 1.;[03] PERFORMED CONTINUITY CHECKS BETWEEN BATTERY PACK M1670 CONNECTOR D10716 PINS 3;4 BATTERY PACK M1673 CONNECTOR D10746 PINS 3;4 BATTERY PACK M1668 CONNECTOR D10712 PINS 3;4 UP TO DISCONNECT BRACKET AB0340A CONNECTOR D40196J PINS 1;2 FOUND NORMAL PER WDM 33-51-11 SHEET 2 FURTHER T/S REQUIRED;[04] CORRECTION TO STEP 3<BR>PERFORMED CONTINUITY CHECKS BETWEEN BATTERY PACK M1670 CONNECTOR D10716 PINS 3;4 BATTERY PACK M1673 CONNECTOR D10746 PINS 3;4 BATTERY PACK M1668 CONNECTOR D10712 PINS 3;4 UP TO DISCONNECT BRACKET AB0340A CONNECTOR D40196J PINS 1;2 FOUND NORMAL PER WDM 33-51-11 SHEET 2 FURTHER T/S REQUIRED<BR>TOOL: MULTIMETER<BR>B/C 176391<BR>CAL DUE 13 OCT 24;[05] VERIFIED STEP 4.;[06] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674/M1675 & BATTERY POWER SUPPLY M1670 & M1675 I/A/W BOEING AMM 33-51-06-960-805 & 33-51-06-960-806. OPERATIONAL TEST PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[07] VERIFIED STEP 6

Part: FITTING — BROKEN (BS 1016 RBL 4) · airframe 65,652 hrs · 39,325 cycles

LOWER FUS. DRAIN FITTING AT STA. 1016; APPROX. RBL 4 IS BROKEN<[01] REMOVED AND REPLACED LOWER FUS. DRAIN FITTING AT STA. 1016; APPROX. RBL 4 AS PER SRM 51-40-02-0G-0 AND DWG#148A3320.;[02] VERIFIED STEP 1

Part: INSERT — MISSING (GIRT BAR FITTING) · airframe 65,652 hrs · 39,325 cycles

INSERT IS MISSING AT R-2 DOOR AFT GIRT BAR FITTING.<[01] REMOVED AND REPLACED INSERT AT R2 DOOR AFT GIRT BAR FITTING. AS PER; SRM 53-00-50-2R-3.;[02] VERIFIED STEP 1

Part: LIGHT — DETERIORATED (CABIN) · airframe 65,652 hrs · 39,325 cycles

PHOTOLUMINESCENT DETERIORATED/SCRATCHED THROUGHOUT THE CABIN<[01] REMOVED AND REPLACED MAIN CABIN PHOTOLUMINESCENT IN REF DRAWING# 33500007;[02] VERIFIED STEP 1

Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 65,652 hrs · 39,325 cycles

ACCESS PNL. # 323AR HAS PANEL LWR. POSITIONING METAL CLIP IS CRACKED . PANEL ATTACHED METAL CLIP IS CRACKED.<[01] REMOVED AND REPLACED RETAINER ON ACCESS PANEL 323AR. AS PER SRM 51-40-02-0G AND DWG 172A6122;[02] VERIFIED STEP # 1

Part: LIGHT — DAMAGED (RT OVERWING) · airframe 65,652 hrs · 39,325 cycles

R/H OVERWING EXIT DOOR LOWER EMERGENCY EXIT LIGHT ASSY DAMAGED<[01] REPLACED R/H OVERWING EXIT DOOR LOWER EMERGENCY EXIT LIGHT ASSY AS PER REF AMM TASK 33-51-01-960-802. PERFORMED OPERATIONAL TEST AS PER AMM REFERENCES 33-51-00-720-801 AND 33-51-00-710-801. TESTED NORMAL.;[02] VERIFIED STEP # 1

Part: SKIN — CRACKED (BS 312 S8R) · airframe 65,652 hrs · 39,325 cycles

R1-DOOR CUTOUT SKIN FWD STA 312 4' BELOW STR 8R APPEARED CRACK AROUND FASTENER<[01] INSTALLED REPAIR AT R1 DOOR CUTOUT BEARSTRAP SKIN REF SRM 53-10-01 ATR-6 4.N. AND FIGURE 202;[02] REFER TO EA 24-153-00239; BARCODE: TTG8Q00R6BKP;[03] 'DAMAGE REPAIRED PER 737-700 SRM 53-10-01-2R-6 (REPAIR 6) FIGURE 202. WEIGHT AND BALANCE CHANGE ACCOUNTED FOR VIA EA 24-153-00239.';[04] VERIFIED STEP 3

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,652 hrs · 39,325 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB #2 CRACK FROM I/B TO O/B<[01] REMOVED AND REPLACED #2 RIB AT RIGHT HORIZONTAL STAB L/E REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.

Part: ANGLE — CORRODED (BS 947) · airframe 65,652 hrs · 39,325 cycles

AFT CARGO COMP CORROSION AT FLOOR SUPPORT ANGLE STA 947.5 RBL 22'<[01] REMOVED AFT CARGO COMPT FLOOR SUPPORT ANGLE AT STA 947.5 FOR ACCESS TO REMOVE CORROSION PER REF SRM 51-40-02-0G-0.FOUND SEVERE EXFOLIATED CORROSION ON FLOOR SUPPORT ANGLE. OUT OF LIMITS PER REF SRM 51-10-02-0G-0.LOCATED AND DRILLED NEW SUPPORT ANGLE (PN:149A8118U29ATSMRO PO:2043476) PER REF SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG #149A8117.INSTALLED NEW SUPPORT ANGLE AT AFT CARGO COMP STA 947.5 PER REF SRM 51-40-02-0G-0 AND DWG# 149A8117.;[02] VERIFIED STEP # 1

Part: ANGLE — CORRODED (BS 787) · airframe 65,652 hrs · 39,325 cycles

AFT CARGO DOOR CUTOUT CORROSION AT STRAP UNDER FLOOR SUPPORT ANGLE STA 787 RBL 19'<[01] REMOVED AND REPLACED STRAP AT AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE LOWER AREA STA 787 RBL19 PER REF SRM 51-40-02-0G-0AND DWG#146A0081.;[02] VERIFIED STEP 1

Part: ANGLE — CORRODED (BS 847) · airframe 65,652 hrs · 39,325 cycles

AFT CARGO DOOR CUTOUT CORROSION AT STRAP UNDER FLOOR SUPPORT ANGLE STA 847 RBL 19'<[01] REMOVED AND REPLACED STRAP AT AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE LOWER AREA STA 847 RBL19 PER REF SRM 51-40-02-0G-0AND DWG#146A0081.;[02] VERIFIED STEP 1

Part: ANGLE — CORRODED (BS 947) · airframe 65,652 hrs · 39,325 cycles

AFT CARGO COMP CORROSION AT FLOOR SUPPORT ANGLE STA 947.5<[01] THIS JOB CARD WILL BE ACCOMPLISH ON TASK CARD#TTG8Q00QN1JX.;[02] VERIFIED STEP 1.

Part: STRAP — CORRODED (BS 787 S25R) · airframe 65,652 hrs · 39,325 cycles

ORROSION ** AT AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE LOWER NUTS STRAP AFT OF STA 787 S-25R MKD DOT<[01] REMOVED AND REPLACED STRAP AT AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE LOWER AREA AFT OF STA 787 S-25R PER REF SRM 51-40-02-0G-0AND DWG#146A0081.;[02] VERIFIED STEP 1

Part: STINGER — CORRODED (BS 540 S23L) · airframe 65,652 hrs · 39,325 cycles

AREA AFT OF FORWARD CARGO COMPARTMENT STA 540 STR 23L END CORRODED AND CRACK<[01] CORRECTION FOR STEP 1: CUT-OUT DAMAGE STRINGER AT FWD CARGO COMPARTMENT FROM STA 510 TO STA 540 STR 23L REF USED B737-700 SRM 51-40-02-0G-0 ; 51-10-02-0G-0 AND SRM 53-00-03-1A-1<BR>LATE ENTRY DUE TO THE CRACK STRINGER NEEDS TO BE REPAIRED. PENDING ENGINEERING INSTRUCTIONS;[02] WRITTEN IN ERROR;[03] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00098.';[04] (RII) VERIFIED STEP 3

Part: STINGER — CORRODED (BS 540 S23R) · airframe 65,652 hrs · 39,325 cycles

AREA AFT OF FORWARD CARGO COMPARTMENT STA 540 STR 23R END CORRODED AND CRACK<[01] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00099.';[02] VERIFIED STEP 1

Part: CHANNEL — CORRODED (BS 737 S25R) · airframe 65,652 hrs · 39,325 cycles

ORROSION ** AT AFT CARGO COMPARTMENT FLOOR Z CHANNEL INTERCOSTAL SUPPORT UNDER AROUND NUT PLATES S-25R STA 767+6' MKD DOT<[01] REMOVED CORROSION AT AFT CARGO COMPARTMENT FLOOR Z CHANNEL INTERCOSTAL SUPPORT S-25R STA 767 PER SRM 51-10-02-0-0.EVALUATED REWORKED AREA AT AFT CARGO COMPARTMENT FLOOR SUPPORT INTERCOSTAL STA 767+6 STR 25R MINIMUM THICKNESS NOTED 0.032;ORIGINAL MAT 0.050;MAT LOST 0.018 FOUND OUT OF LIMITS PER REF SRM 53-60-15-1A-1.LOCATED AND DRILLED NEW INTERCOSTAL AT AFT CARGO COMPARTMENT STA 767+6' STR 25R PER REF SRM 51-40-05-0G-0. INSTALLED NEW INTERCOSTAL AT AFT CARGO COMPARTMENT STA 767+6 STR 25R PER REF SRM 51-40-02-0G-0 AND DWG#146A0081.;[02] VERIFIED STEP # 1

Part: STINGER — CORRODED (BS 540 S26L) · airframe 65,652 hrs · 39,325 cycles

AREA AFT OF FORWARD CARGO COMPARTMENT STA 540 STR 26L END CORROSION AREA AFT OF FORWARD CARGO COMPARTMENT STA 540 STR 26L END EXFOLIATING CORROSION<[01] VERIFIED INSTALLATION;[02] ACCOMPLISHED EA: 24-153-00093/ 9015750.;[03] VERIFIED STEP 2

Part: STINGER — CRACKED (BS 540 S25L) · airframe 65,652 hrs · 39,325 cycles

AREA AFT OF FORWARD CARGO COMPARTMENT STA 540 STR 25L END CRACK<[01] WORK WAS ACCOMPLISHED PER EA # 24-153-00052-WIP1 TASK CARD # TTG8Q00QVGLU;[02] VERIFIED STEP 1

Part: ANGLE — CRACKED (BS 540 RBL 2) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN STA 540 RBL 2' FLOOR PANEL BREAK ANGLE CRACK<[01] THIS FAULT WAS RESOLVED ON CARD: TTG8Q00QKQGH.;[02] VERIFIED STEP 1

Part: STRINGER CLIP — CRACKED (BS 500C S26L) · airframe 65,652 hrs · 39,325 cycles

FWD CARGO COMP STA 500C STR 26L CLIP UNDER ZEE CHANNEL CRACK<[01] REMOVED AND REPLACED CLIP AT FWD CARGO COMPT STA 500C UNDER Z CHANNEL PER REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP # 1

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 65,652 hrs · 39,325 cycles

FWD CARGO COMPARTMENT STA 500D STR 19R GUSSET CRACK<[01] REMOVED AND REPLACED NEW GUSSET AT FWD CARGO COMPT FROM STA 500D STR 19R PER REF SRM 51-40-02-0G-0;[02] CORRECTION TO STEP 1:REMOVED AND REPLACED NEW GUSSET AT FWD CARGO COMPT FROM STA 500D STR 19R PER REF SRM 51-40-02-0G-0 AND DWG:#143A7902;[03] VERIFIED STEP 2.

Part: ANGLE — CRACKED (BS 540 LBL 2) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN STA 540 LBL 2' FLOOR PANEL BREAK ANGLE CRACK<[01] THE PANEL BREAK WAS REPLACED ON CARD: TTG8Q00QKQZ5.;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 540 LBL1) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ STA 540 LBL1<[01] REMOVED AND REPLACED AT MAIN CABIN CENTER WING FLOOR SUPPORT BREAK ASSY STA 540 LBL 1 IAW SRM 51-40-02-0G-0.;[02] CORRECTION TO STEP #1<BR>PANEL BREAK ASSY WAS REMOVED AND REPLACE AT MAIN CABIN CENTER WING STA 540 LBL 1 AS PER SRM 51-40-02-0G-0 AND DWG 143A5240.;[03] VERIFIED STEP 2

Part: SEAT TRACK — CORRODED (BS 500A LBL45.5) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN CORROSION AT SEAT TRACK CROWN BOTTOM STA 500A+8' LBL 45.50<[01] GENERAL FAULT RESOLVED ON OTHER FAULT SEE TASK CARD # TTG8Q00QKFGN SEAT TRACK IS BEING REPLACED.;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (BS 500B-500C) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN CORROSION AT SEAT TRACK CROWN BOTTOM BETWEEN STA 500C- 500B LBL 45.50<[01] GENERAL FAULT RESOLVED ON OTHER FAULT SEE TASK CARD # TTG8Q00QKFGN SEAT TRACK IS BEING REPLACED.;[02] VERIFIED STEP 1

Part: FLOORBEAM — CRACKED (BS 540 LBL25-45) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN CENTER WING FLOOR SUPPORT BREAK TOP LAYER CRACKED @ STA 540 LBL25 TO LBL 45 MKD DOTS<[01] REMOVED AND REPLACED AT MAIN CABIN CENTER WING FLOOR SUPPORT BREAK TOP LAYER CRAKED STA 540 LBL 24.75 TO LBL 45.50 IAW SRM 51-40-02-0G-0.;[02] CORRECTION ON STEP # 1 : REMOVED AND REPLACED AT MAIN CABIN CENTER WING FLOOR SUPPORT BREAK TOP LAYER CRAKED STA 540 LBL 24.75 TO LBL 45.50 IAW SRM 51-40-02-0G-0. & IPC 53-42-11-66.;[03] VERIFIED STEP 2

Part: FLOOR SUPPORT — CRACKED (BS 540 RBL1) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ STA 540 RBL1<[01] REMOVED AND REPLACED AT MAIN CABIN CENTER WING FLOOR SUPPORT BREAK ASSY STA 540 RBL 1 IAW SRM 51-40-02-0G-0.;[02] CORRECTION TO STEPS #1 <BR>REMOVED AND REPLACED AT MAIN CABIN CENTER WING FLOOR SUPPORT BREAK ASSY STA 540 RBL 1 IAW SRM 51-40-02-0G-0 AND DWG 143A5240.;[03] VERIFIED STEP 2

Part: SEAT TRACK — CORRODED (BS 500 LBL 45.5) · airframe 65,652 hrs · 39,325 cycles

MAIN CABIN CORROSION AT SEAT TRACK CROWN BOTTOM STA 500-3' LBL 45.50<[01] GENERAL FAULT RESOLVED ON OTHER FAULT SEE TASK CARD # TTG8Q00QKFGN SEAT TRACK IS BEING REPLACED.;[02] VERIFIED STEP 1

Part: CHANNEL — CORRODED (BS 727-847) · airframe 65,652 hrs · 39,325 cycles

***CORROSION*** LH SIDE PLATE (Z CHANNEL) SHOWS SEVERAL SPOTS OF CORROSION FROM STA 847 TO STA 727. DOT 82-012.<[01] REMOVED AND REPLACED Z CHANNEL AT AFT CARGO COMPT FROM STA 727 TO STA 847 PER REF SRM 51-40-02-0G-0 AND DWG#146A7502.;[02] VERIFIED STEP # 1

Part: PLATE — CORRODED (BS 727 S25R) · airframe 65,652 hrs · 39,325 cycles

***CORROSION*** AFT CARGO RH SIDE SIDE PLATE (Z CHANNEL) HAS SPOT OF CORROSION AT STA 727+14.5 AND S25R. DOT 82-002.<[01] FAULT WILL BE RESOLVED PER TASK CARD TTG8Q00QK6EV;[02] VERIFIED STEP 1

Part: CHANNEL — CORRODED (BS 727 794) · airframe 65,652 hrs · 39,325 cycles

RH SIDE PLATE (Z CHANNEL) SHOWS SEVERAL SPOTS OF CORROSION FROM STA 794.3 TO STA 727. DOT 82-011.<[01] REMOVED AND REPLACED Z CHANNEL AT AFT CARGO COMPT FROM STA 727 TO STA 767 RBL 21 PER REF SRM 51-40-02-0G-0 AND DWG#146A7502.;[02] VERIFIED STEP # 1

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 65,652 hrs · 39,325 cycles

R/H WING ANTI-ICE DUCT SUPPORT ROD ATTACHED FITTING CRACKED @ WING TO BODY STA 540 MKD DOT<[01] REMOVED AND REPLACED R/H WING ANTI-ICE DUCT SUPPORT ROD ATTACHED FITTING AS PER SRM 51-40-02-0G-0.;[02] CORRECTION TO STEP #1<BR>REMOVED AND REPLACED R/H WING ANTI-ICE DUCT SUPPORT ROD ATTACHED FITTING AS PER SRM 51-40-02-0G-0 AND IPC 57-11-00-01.;[03] VERIFIED STEP 2

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 65,652 hrs · 39,325 cycles

AFT CARGO DOOR CUTOUT LOWER SILL FWD SCUFF PLATE CRACKED MKD DOT<[01] RECIEVED WELDED SCUFF PLATE FOR THE AFT CARGO COMPARTMENT FWD SIDE; PO # 2043476; ISSUE TAG # WN39251 SERIAL: NSI. SCUFF PLATES WILL BE INSTALLED ON TASK CARD NUMBER TTG8Q001UF7N STEPS 15- STEP 17.;[02] VERIFIED STEP 1

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 65,652 hrs · 39,325 cycles

AFT CARGO DOOR CUTOUT LOWER SILL AFT SCUFF PLATE CRACKED MKD DOT<[01] RECIEVED WELDED SCUFF PLATE FOR THE AFT CARGO COMPARTMENT AFT SIDE; PO # 2043476; ISSUE TAG # WN39250; SERIAL: NSI. SCUFF PLATES WILL BE INSTALLED ON TASK CARD NUMBER TTG8Q001UF7N STEPS 15- STEP 17.;[02] VERIFIED STEP 1

Part: FITTING — CRACKED (ZN 500 LEFT WING) · airframe 65,652 hrs · 39,325 cycles

L/W REAR SPAR T/E DEFLECTION CONTROL RIB FIXED PANEL T/E VERTICAL BULB SEAL FITTING CRACKED @ FASTENER TAIL MKD DOT<[01] REMOVED AND REPLACED L/W REAR SPAR T/E DEFLECTION CONTROL RIB FIXED PANEL T/E VERTICAL BULB SEAL BRACKET AS PER SRM 51-40-02-0G-0

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 65,652 hrs · 39,325 cycles

RH HORIZONTAL STABILIZER RIB #4 STIFFENER #3 CRACKED AT LOWER END.<[01] ACCOMPLISHED REPAIR OF RIGHT HORIZNTAL STAB RIB #4 STIFFENER 3 REF SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED STEP 1

Part: BULB — INOPERATIVE (ZN 800 DOOR) · airframe 65,302 hrs · 39,109 cycles

EXTERNAL EMERGENCY EXIT LIGHT AFT OF R2 DOOR WILL NOT ILLUMINATE.<[01] RELAMPED BULB PER AMM 33-51-02. OPS CHECK GOOD.

Part: PANEL — CRACKED (ZN 300 STABILIZE) · airframe 64,550 hrs · 38,619 cycles

VERTICAL FIN LEADING EDGE COMPOSITE IS CRACKED AND HAS MATERIAL MISSING BELOW LEADING-EDGE PANEL 322C.<[01] REPAIRED VERTICAL FIN LEADING EDGE COMPOSITE BELOW L/E PANEL 322C REF SRM 55-30-01-2R-13

Part: FAIRING — CRACKED (ZN 400 NACELLE/P) · airframe 63,888 hrs · 38,176 cycles

NO. 1 ENGINE AFT STRUT FAIRING T/E ASSY. HAS CRACK ON FWD FACE(HFEC VERIFIED)<[01] REMOVED DAMAGED NO. 1 ENGINE AFT STRUT FAIRING T/E ASSY AND LOCATED AND DRILLED NEW STRUT FAIRING T/E ASSY PER SRM 51-40-02;[02] ATTACHED PIC OF PYLON BRACKET KIT TAG; BN 372043; USED ON THIS A/C;[03] INSTALLED AFT STRUT FAIRING IAW SRM 51-40-02

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 63,713 hrs · 38,070 cycles

EMERGENCY WALKWAY (PHOTO LUMINESCENT) LIGHT STRIP AT 9DEF IS LOOSE FROM FLOOR. EMERGENCY WALKWAY LIGHT STRIP AT 9DEF IS LOOSE FROM FLOOR.<[01] SECURED EMERGENCY WALKWAY LIGHT STRIP AT 9DEF TO FLOOR PER AMM 25-27-15.;[02] C/W

Part: SLIDE — DEPLOYED (ZN 200 FUS TOP) · airframe 63,555 hrs · 37,964 cycles

SLIDE DEPLOYED IN AFT GALLEY<[01] RE-PACK AFT SVC DOOR SLIDE IAXWX MT 725-61-06

Part: CIRCUIT BREAKER — POPPED (ZN 200 FUS TOP) · airframe 63,490 hrs · 37,923 cycles

NOTICED EMER PANEL LTG CB WAS POPPED OUT BEHIND FO SEAT<[01] FOUND P6-3 D8 CB EMER PANEL LTG OUT. RESET PER MM 20-60-01. PERFORMED COCKPIT BACKGROUND LIGHTING TEST USING WDM 33-11-33 CB REMAINED SET; ALL LIGHTS OPS NORMAL

Part: BATTERY — INOPERATIVE (ZN 100 FUS LOWER) · airframe 63,132 hrs · 37,683 cycles

FELT ATTENDANT MEGAPHONE BATTERIES POSSIBLY INOP<[01] REMOVED AND REPLACED THE FWD MEGAPHONE BATTERIES. REF AMM 25-64-00

Part: LIGHT — BROKEN (CABIN) · airframe 62,728 hrs · 37,433 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01-960-802 STEPS 3.C.(1)-(4); (5)(B); AND (6)-(12)<BR><BR>PENDING STEPS 3.C. 13 & 14 , OPS CHECKED IAW AMM 33-51-01-960-802 STEPS 3.C. 13 & 14.

Part: GIRT BAR — OUT OF ADJUST · airframe 62,191 hrs · 37,073 cycles

FWD ENTRY DOOR HINGE AND GIRT BAR - FLT ATTD. REQUEST MX TO LOOK AT THEM. / [01] TIGHTENED FORWARD ENTRY DOOR UPPER HINGE TRIM COVER & ADJUSTED GIRT BAR RETENTION HOOKS PER SIP.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,622 hrs · 36,050 cycles

AFT ENTRY DOOR EMERGENCY EXIT SIGN LIGHT COVER MISSING / [01] INSTALLED AFT ENTRY DOOR EMERGENCY EXIT SIGN LIGHT LENS REF AMM 33-51-01

Part: STRIP — LOOSE (FWD CABIN) · airframe 60,341 hrs · 35,878 cycles

FIRST OFFICER SIDE; BETWEEN ROW 8 & 9; PHOTO LUMINESCENT EMERGENCY FLOOR LIGHTING STRIP LOOSE. / [01] RESECURED PHOTO LUMINESCENT STRIP AT ROW 8 ABC & 9 ABC PER AMM 33-51-15.

Part: SLIDE — OUT OF POSITION · airframe 60,304 hrs · 35,856 cycles

AFT RH DOOR SLIDE ASSY RETAINING LATCH CAME APART. / [01] REINSTALLED AFT RH SERVICE DOOR SLIDE PACK PER AMM 25-66-01. ACFT OK FOR CONTINUED SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 60,081 hrs · 35,724 cycles

FWD GALLEY EMERGENCY FLASH LIGHTS TEST INOP. / [01] REMOVE AND REPLACED FWD GALLEY EMERGENCY FLASH LIGHTS BATTERIES PER AMM 25-64-00-900-806. TEST NORMAL.<BR>AAR TAGS WN12381 AND E78705.; [02] VERIFIED STEP 1

Part: SUPPORT BRACKET — CORRODED (LH WING) · airframe 60,081 hrs · 35,724 cycles

LEFT WING BOOST PUMP TANK # 1 LOWER BONDING STRAP AND SUPPORT BRACKET CORRODED ; / [01] REMOVED SUPPORT BRACKET AT LT WING BOOST PUMP TANK # 1 LOWER BONDING AS PER B737-700 SRM 51-40-02-0G-0.; [02] BONDING TESTER USED BC 168698 EXP APR 2022; [03] CLEANED CORROSION AT SUPPORT BRACKET AS B737-700 SRM 51-10-02-OG-0. ORIGINAL MATERIAL 0.050' MATERIAL REMOVED 0.025 ' ; MATERIAL REMAINING 0.025'. FOUND CORROSION OUT OF LIMITS AS PER B737-700 SRM 57-20-10-1A-3.; [04] REMOVED AND REPLACED SUPORT AND NEW BONDING STRAP REF B-737-700-SRM 51-40-02-0G-0; AMM 28-22-41-400-802; [05] VERIFIED REPLACEMENT AND BONDING TEST NORMAL; [06] SAFETY WIRE MISSING ON LOWER SUPPORT; [07] CORRECTION ON STEP 3. ORIGINAL MATERIAL 0.063' ; MA

Part: FITTING — CRACKED (RH WING) · airframe 60,081 hrs · 35,724 cycles

R/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED I/B SIDE MKD ; / [01] REMOVED SEAL FITTING AT R/W REAR SPAR T/E REF B-737-700 SRM 52-40-02-0G-0; [02] LOCATED AND DRILLED SEAL FITTING AT R/W REAR SPAR T/E REF B-737-700 SRM 52-40-05-0G-0; [03] VERIFIED STEP 1; 2.; [04] O.K. TO INSTALL NEW FITTING..; [05] INSTALLED NEW FITTING AT RIGHT WING REAR SPAR T/E DEFLECTION CONTROL RIB I/B SIDE IAW B 737-7 SRM 51-40-02-0G-0; [06] VERIFIED STEP 5...

Part: RIB — CRACKED (LH HOR STAB) · airframe 60,081 hrs · 35,724 cycles

L/H HORIZONTAL FRONT SPAR L/E FAIRING CRACKED @ INNER RIB # 1 EDGE MKD ; / [01] PERFORMED HFEC INSP. ON L/H HORIZ. STAB. FRONT SPAR L/E FAIRING INNER RIB #1 EDGE IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED; EQUIP: NORTEC 600 CAL DUE: 10/22 B/C 166317; [02] REMOVED L/H HORIZONTAL FRONT SPAR L/E CRACKED INNER #1 RIB IAW B 737-7 SRM 51-40-02-0G-0; [03] VERIFIED STEP 2..O.K. TO INSTALL NEW RIB...; [04] INSTALLED NEW LEFT HAND FRONT SPAR L/E INNER #1 RIB IAW B 73-7 SRM 51-40-02-0G-0; [05] VERIFIED STEP 4..

Part: LIGHT — INOPERATIVE · airframe 60,081 hrs · 35,724 cycles

RIGHT OVERWING EXIT SIGN INTERIOR AND EXTERIOR LIGHT ARE INOPERATIVE ; / [01] PERFORMED TROUBLESHOOTING; FOUND BATTERY PACK (M1669) DEFECTIVE AS PER B737 FIM 33-50 TASK 801.; [02] VERIFIED STEP 1; [03] REMOVED AND REPLACED R/H WING EMERGENCY BATTERY PACK; M1669 AND PERFORMED OPS-CHECK AS PER B737 AMM 33-51-06-960-805. TEST FOUND NORMAL.; [04] REMOVED AND REPLACED R/H WING EMERGENCY BATTERY PACK; M1669 AND PERFORMED OPS-CHECK AS PER B737 AMM 33-51-06-960-805. TEST FOUND NORMAL. <BR> <BR><BR> <BR>:; [05] VERIFIED STEP 3;4

Part: LIGHT — BROKEN (CABIN) · airframe 60,081 hrs · 35,724 cycles

LAVATORY A EMERGENCY EXIT SIGN BROKEN ; / [01] REMOVED AND REPLIED LAVATORY A EMERGENCY EXIT SIGN IN REF B737-700 AMM 33-51-01-960-802; [02] VERIFIED INSTALLATION;<BR>CORRECTION STEP 1. CHANGE REPLIED FOR REPLACED

Part: NONE — CORRODED (CABIN FLOOR) · airframe 60,081 hrs · 35,724 cycles

SUPPLEMENTAL INFORMATION: CORROSION SPOTS ON AFT CABIN FLOOR STRAP B.S. 1016 TO AFT APB LBL 3' ; / REMOVED SPOTS OF CORROSION AT AFT CABIN FLOOR STRAP STA 1016 TO AFT LBL 3' AS PER SRM 51-10-02-0G-0. EVALUATE DAMAGE. ORIGINAL MATERIAL 0.071' MATERIAL LOST 0.020' MATERIAL REMAINING 0.051' FOUND OUT OF LIMITS AS PER SRM 53-70-51-1A-1 FIG. 103 DET. M. USED CALIPER ID 165957 CALIBRATION DUE: 26-OCT-22. LATE ENTRY: INSTALLED PROTECTION OF EWIS AT STA 1016 TO AFT BETWEEN LBL 20' AND RBL 20' AS PER AMM 20-60-07-913-801. REMOVED STRAP P/N 147A5620-3 AT MAIN CABIN STATION 1016 AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW FLOOR STRAP AT STA 1016 TO AFT LBL 3' AS PER B-737 700 SRM 51-40-05-0G-0. INSTALLED AFT CABIN FLOOR STRAP AT STA 1016 LBL 3' AS PER B737-700 SRM 51-40-02-0G-0.; [11] VERIFIED INSTALLATION; [12] C/W; [13] EWIS PROTECTION REMOVAL ON CARD TTG8Q001VQGW FOR FOD PROTECTION AND CARD TTG8Q001RHGU FOR AFT WET AREA RESTORATION

Part: NONE — CORRODED (L2 DOOR) · airframe 60,081 hrs · 35,724 cycles

SUPPLEMENTAL INFORMATION: *** CORROSION *** L2 DOOR LWR SILL WITH SIGNS OF EXFOLIATION. / [01] REMOVED CORROSION AT L-2 LOWER SILL .FOUND OUT LIMITS SEVERAL SIDE REWORKED AREA [EXFOLIATION] IAW B737 SRM 51-10-02-0G-0.; [02] FOUND OUT LIMITS BY SRM 53-70-15-1A-1 D/D # 1 FIG103 DETAIL D.; [03] CORRECTION STEP 1; ORIGINAL MATERIAL 0.071.MATERIAL LOOS 0.023 MATERIAL REMAINING 0.045.FOUUND OUT LIMITS .USED TOOL CALIPER B/C174207.; [04] CORRECTION STEP 1 ;ORIGINAL MATERIAL 0.071.MATERIAL LOSS 0.026.MATERIAL REMAINING 0.045. FOUND OUT LIMITS .USED TOOL CALIPER B/C174207.IAW SRM 53-70-15-1A- A/D #1 FIG 103 DETAIL D.; [05] VERIFIED STEPS 1 AND 4; [06] FABRICATED NEW LOWER SILL AT L-2 DOOR ] LOCATED AND DRILLED HOLES AT SHEAR TIE LBL 50 IN REFERENCE. B-737 SRM 51-40-02-0G-0.; [12] EDIT WORK CAPTURE- FABRICATED NEW LOWER SILL AT L-2 DOOR .MATERIAL USED 7075 -T6 0.071 CLAD P/O 1747908. INSTALLED 4 ANGLE SUPPORT LOWER SELL AND 4 UPPER CLIP AND PUT ON POSITION L-2 SILL AND STARED INSTALL FASTENERS IAW B737 SRM %1_40-02-0G-0.;

Part: PANEL — ELONGATED (FUSELAGE) · airframe 60,081 hrs · 35,724 cycles

AFT WING-TO-BODY FAIRING PANEL 194E HAS SEVERAL ELONGATED HOLES. ; / [01] PREPARED DAMAGED AREA; NO WATER NOTE AND FULL THE ELONGATED HOLES WITH LAMINATING RESIN AND CHOPPED FIBERS. REF B737-700 SRM 53-40-70-2R-1; SRM 51-70-04-2R-9 PARAGRAPH 4 AND SRM 51-70-04-2R-0 PARAGRAPH 4.; [02] VERIFIED PREPARATION.<BR>OK TO INSTALL REPAIR; [03] APPLIED THE FABRIC REPAIR PLIES AT DAMAGED AREA. REF B737-700 SRM 53-40-70-2R-1; SRM 51-70-04-2R-9 PARAGRAPH 4 AND SRM 51-70-04-2R-0 PARAGRAPH 4.; [04] VERIFIED REPAIR.<BR>OK TO TOP COAT; [05] APPLIED TOP COAT AT REPAIR AREA. REF B737-700 SRM 53-40-70-2R-1; SRM 51-70-04-2R-9 PARAGRAPH 4; SRM 51-70-04-2R-0 PARAGRAPH 4 AND AMM 51-21-99-300-802.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,081 hrs · 35,724 cycles

CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.9 16' AFT OF FWD EDGE I/B OF I/B FASTENER ROW. ; / REMOVED EXITED L DOUBLE AND FASTENER FOR ACCESS REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 193.9 16' IAW B737 SRM 51-40-02-0G-0.; [03] PERFORMED HFEC INSP ON LH HORIZ STAB LWR SKIN STA 193.9 16' AFT OF FWD EDGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED (LENGTH 1.0 INCHES)<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [04] REMOVED CRACK AT L/H HORIZONTAL STAB LOWER SKIN STA 193-9 16'.DIMESION CUTOUT 1.600' LONG AND W 1'.ED 0.350'IAW B737 SRM 55-10-01-2R-11 REPAIR 11.; [05] STEP 4 VERIFIED; [06] PERFORMED HFEC INSP ON CUT OUT LH HORIZ STAB LWR SKIN STA 193.9 16' AFT OF FWD EDGE IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [07] PERFORMED ROTO INSP ON ALL THE EXISTING HOLES IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [08] PERFORMED COUNTERSINK INSP ON ALL THE EXISTING COUNTERSUNK HOLES IAW B737 NDT P6 53-30-00 PROC.3; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [09] DIMENSION EXIST REPAIR STA 184.7 .CUT OUT LONG 1.700' AND W 1'.AD 0.350 IAW B737 . SRM %%-10-01-2R 11 REPAIR 11.; [10] STEP 9 VERIFIED; [11] ISSUED SUMMARY EA 22-155-00140-1 REV 2; [12] EA-COMPONENT' REPAIR REFERENCE TO CLOSE THE OPEN FAULT TTG8Q00A8A8Z. <BR> <BR>EA-COMPONENT' REPAIR REFERENCE TO CLOSE THE OPEN FAULT TTG8Q00A8A8Z.; [13] VERIFIED WORK CARD COMPLETION

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,081 hrs · 35,724 cycles

CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.9 24' AFT OF FWD EDGE I/B OF I/B FASTENER ROW CRACK LENGHT 107' ; CORRECTION: CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.9 24' AFT OF FWD EDGE IB OF IB FASTENER ROW CRACK LENGHT 1.7' / [01] REMOVED PAINT FOR ACCESS REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 193.9 24' IAW B737 AMM51-21-11-150-801.; [02] REMOVED EXISTED DOUBLE AND FASTENERS FOR ACCESS REPAIR AT L/H HORIZONTAL STAB STA 193.9 24' IAW SRM 51-40-02-0G-0.; [03] PERFORMED HFEC INSP ON LH HORIZ STAB LWR SKIN STA 193.9 IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED (LENGTH 1.7 INCHES)<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [04] REMOVED CRACK AT L/H HORIZONTAL STAB STA 193.9 24'. DIMENSION CUTOUT LONG 2.200 W 1' .AD .350 ' IAW B737 SRM 55-10-01-11 2R REPAIR 11.; [05] STEP 4 VERIFIED; [06] PERFORMED HFEC INSP ON CUT OUT LH HORIZ STAB LWR SKIN STA 193.9 24' AFT OF FWD EDGE IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [07] PERFORMED ROTO INSP ON ALL THE EXISTING HOLES IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [08] PERFORMED COUNTERSINK INSP ON ALL THE EXISTING COUNTERSUNK HOLES IAW B737 NDT P6 53-30-00 PROC.3; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 07/22; [09] SELECT THE ?FAULT RESOLVED ON OTHER FAULT? REPAIR REFERENCE TO CLOSE FAULT TTG8Q00A8ATQ; [10] VERIFIED WORK CARD COMPLETION

Part: WEB — CORRODED (FUSELAGE) · airframe 60,081 hrs · 35,724 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO DOOR CUT OUT LOWER WEB HAS NUMEROUS SPOTS OF CORROSION ; AFT CARGO DOOR CT OT LOWER WE HAS NMEROS SPOTS OF CORROSION / [01] LOCATED AND DRILLED NEW PART AT AFT CARGO DOOR CUT OUT LOWER WEB REF B-737-700-SRM 51-40-05-0G-0; [02] VERIFIED LOCATED AND DRILLED OF NEW WEB; [03] LATE ENTRY <BR>AFT CARGO DOOR CUT OUT LOWER WEB HAS EXFOLIATING CORROSION FOUND TO BE OUT OF LIMITS AS PER B 737-7 SRM 53-00-53-1A-2; [04] INSTALLED NEW NUT PLATES IAW B 737-7 SRM 51-40-02-0G-0; [05] SUMMARY=AFT CARGO DOOR CUT OUT LOWER WEB HAS EXFOLIATING CORROSION FOUND TO BE OUT OF LIMITS AS PER B 737-7 SRM 53-00-53-1A-2 LOCATED AND DRILLED NEW PART AT AFT CARGO DOOR CUT OUT LOWER WEB REF B-737-700-SRM 51-40-05-0G-0 INSTALLED NEW NUT PLATES IAW B 737-7 SRM 51-40-02-0G-0 WEB TO BE INSTALLED ON ITEM # TTG8Q004DS7E; [06] VERIFIED STEPS 3;4;AND5.

Part: SEAL — DAMAGED (LH HOR STAB) · airframe 60,081 hrs · 35,724 cycles

L/H HORIZONTAL STAB. UPPER T/E PANEL # 333AT HAS METAL SLIDING SEAL WORN ; / [01] REMOVED AND REPLACED METAL SLIDING SEAL AT PANEL 333AT IAW B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT R/H SIDE PLATE SUPPORT ZEE; HAS MANY SPOTS OF CORROSION FROM STA 767 TO 727. ; / [01] REMOVED CORROSION AT AFT CARGO R/H Z CHANNEL FROM 727-767 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED 1; [03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.036'<BR>TOOL USED : OLYMPUS 27MG B/C 172139 04/22; [04] MAT EVALUATION ORIGINAL MATERIAL 0.040' AFTER REWORKED MATERIAL REMAINING 0.036' MATERIAL LOST 0.004'' FOUND TO BE WITH IN LIMITS AS PER B737-700 SRM 53-00-53-1A-2 4A FIG 103 DETAIL A;B;AND C; [05] VERIFIED STEPS 3 AND 4 ;OK TO TREAT AND PRIME.; [06] TREATED AND PRIMED AREA AT AFT CARGO COMP FLOOR R/H SIDE PLATE SUPPORT ZEE CHANEL FROM STA 767 TO 727 IAWAMM51-21-41-370-802 AND AMM51-21-72-370-802.; [07] SUMMARY :REMOVED CORROSION AFT CARGO COMP R/H SIDE PLATE ZEE STA 767 TO STA 727.IAW SRM 51-10-02-0G-0.PERFORMER INSP ON REWORKED ARE NDT P451-00-00 PROC3.FOUND AREA TO BE LIMITS IAW SRM A/D 53-00-53-1A 4A FIG 103 DETAIL A;B;C.TREATED AND PRIMED AREA IAW AMM51-21-41-370-802 AND AMM51-21-72-370-802.; [08] VERIFIED STEPS 6 AND 7; [09] CORRECTED MEASURING TABLE

Part: FITTING — CORRODED (AFT CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR AREA BS 767 - 787, RT RAIL AT CARGO NET ATTACH FITTING HAD CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3, ORIGINAL MATERIAL 0.070', MATERIAL REMAINING 0.068', FOUND TO BE WITH IN LIMITS IAW SRM 53-00-53-1A-2 4A, FIG 103, DETAIL A;B;AND C. TREATED AND PRIMED IAW B737 AMM51-21-41-370-802 AND AMM51-21-72-370--802.

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR AREA AT STA 927 L/H RAIL TOP AREA HAS CORROSION. REMOVED CORROSION AT AFT CARGO FLOOR AREA IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3. MATERIAL 0.086' AFTER REMAINING 0.077' MATERIAL LOST 0.009' FOUND TO BE WITH IN LIMITS IAW SRM 53-00-53-1A-2 4A FIG 103 DETAIL A;B;AND C. TREATED AND PRIMED AREA IAW AMM51-21-41-370-802 AND AMM 51-21-72-370-802.

Part: ATTACH FITTING — CORRODED (AFT CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR AREA BS 907 RT RAIL HAS CORROSION AT NET ATTACH FITTING. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3, PERFORMED EVALUATION WITH UT THICKNESS AT REWORKED AREA AND ADJACENT STRUCTURE. IAW NDT PART 4 51-00-00 PROCE 3. MIN THICK 0.048'. ORIGINAL MATERIAL THICKNESS 0.070'. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. FIG. 103; DETAIL G.; [06] ADDING TO STEP 1. REMOVED RT TRACK -NET ATTACH FITTING IAW SRM 51-40-02-0G-0. REPLACEMENT OF RT TRACK-NET ATTACH FITTING WILL BE ACCOMPLISH ON TASK TTG8Q00A4AA4.

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR AREA BETWEEN BS 927 - 947.5 RT RAIL CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3. ORIGINAL MATERIAL THICKNESS 0.070'; MATERIAL LOSS 0.011'; REMAINING MATERIAL 0.059'. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. FIG. 103; DETAIL G. REPLACED IAW SRM 51-40-02-0G-0 AND DRAWING 147A7500.

Part: FLOORBEAM — CORRODED · airframe 60,081 hrs · 35,724 cycles

CORROSION AROUND FASTENER HOLES ON FLOORBEAM UPPER FLANGE BS 986.5, RBL 28'-46'. EVALUATED REWORKED AREA ORG. MAT.0.150' MAT REMAINING 0.100' MAT REMOVED 0.050' FOUND TO BE OUT OF LIMITS IAW SRM=53-70-51-11A-1. LOCATED AND DRILLED HOLES IAW B737 SRM 53-70-51-2R-4 REPAIR4, FIG204, SHEET 2. REPAIRED IAW SRM 51-40-05-0G-0 AND 53-70-51-2R-4 REPAIR 4.

Part: DOOR — CRACKED (RMLG) · airframe 60,081 hrs · 35,724 cycles

RT GEAR FIXED DOOR CRACKED. REMOVED DOOR ASSY IAW AMM 32-13-11-000-803. INSTALLED A NEW MLG DOOR ASSY IAW AMM 32-13-11-420-803 FROM STEP 7.0 UP TO AND INCLUDING STEP 7.H.(3)(D)1)A).

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 60,081 hrs · 35,724 cycles

CORROSION SPOT ON AFT CABIN WET AREA FLOORBEAM UPPER FLANGE AT BS 986.5 R.BL. 5'. REMOVED CORROSION IAW SRM 53-70-51-1A-1-A00108. PERFORMED UT THICKNESS INSP. IAW NDT PART 4; 51-00-00; PROCEDURE 3. MIN. THICKNESS 0.137'. FOUND TO BE OUT OF LIMITS IAW SRM=53-70-51-11A-1. REPAIR ACCOMPLISH ON TASK CARD TTG8Q00A436K.

Part: NONE — CORRODED (FUSELAGE) · airframe 60,081 hrs · 35,724 cycles

CORROSION SPOTS ON CABIN FLOOR WEB AFT WET AREA B.S. 1006+9 L.BL. 40'. (51-002). REMOVED CORROSION AT AFT CABIN FLOOR WEB AT STA 1006+9 AND LBL 40' IAW SRM 53-70-51-1A-1-A00108. REMOVED SHEAR WEB CORROSION WAS EXFOLIATING WEB IS OUT OF LIMITS IAW 51-40-02-0G-0. LOCATED & DRILLED A NEW WEB IAW SRM 51-40-05-0G-0 AND DWG 147A5600. PARTIALLY INSTALLED FLOOR WEB IAW SRM 51-40-02-0G-0. COMPLETED INSTALLATION OF CABIN FLOOR WEB IAW SRM 51-40-02-0G-0 AND DWG 147A5600.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 60,081 hrs · 35,724 cycles

CORROSION SPOT ON AFT CABIN WET AREA FLOOR BEAM UPPER FLANGE AROUND FASTENER HOLE B.S.986.5 L.BL. 43'. REMOVED CORROSION IAW B 737-7 SRM 53-70-51-1A-1-A00108. EVALUATED REWORKED AREA ORG. MAT.0.150' MAT REMAINING 0.102' MAT REMOVED 0.048' FOUND TO BE OUT OF LIMITS IAW SRM=53-70-51-11A-1. REMOVED SPLICE IAW SRM 51-40-02-0G-0, PERFORMED SHOT PEENING PROCEDURE AT TRIM OUT IAW PER SOPM 20-10-03. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 53-70-51-2R-4 REPAIR 4, SECTION 47 ;PAGE TABLE 201. INSTALLED NEW SHEAR TIE ITEM 7 REPAIR SRM 53-70-51-2R-4 REPAIR 4.

Part: FLOOR PANEL — DETERIORATED (AFT CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR PNL 140 DF DETERIORATED ; / [01] FABRICATED AFT CARGO FLOOR PANEL 140 DF AS PER B737-700 AMM 25-52-01-201-801; [02] VERIFIED STEP 1..

Part: FLOOR PANEL — DETERIORATED (FUSELAGE) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR PNL 140 BF DETERIORATED ; / [01] REPLACED AFT CARGO FLOOR PANEL 140BF IN REF B-737 700 AMM 25-52-01-201-801-NG.; [02] VERIFIED STEP 1

Part: FLOOR PANEL — DETERIORATED (FUSELAGE) · airframe 60,081 hrs · 35,724 cycles

AFT CARGO FLOOR PNL 140AF DETERIORATED ; / [01] REPLACED AFT CARGO FLOOR PANEL 140AF IN REF B-737 700 AMM 25-52-01-201-801-NG.; [02] CORRECTION FOR STEP #1 TO READ FABRICATED NEW AFT CARGO FLOOR PANEL 140AF IN REF B-737 700 AMM 25-52-01-201-801-NG; [03] VERIFIED STEPS 1 AND 2..

Part: RIB — CRACKED (FWD ENTRY DOOR) · airframe 60,081 hrs · 35,724 cycles

ABOVE FWD ENTRY DOOR FWD CORNER AT BS 312 THERE`S A CRACKED RIB. FABRICATED UPPER CHORD REPAIR IAW SRM 53-10-07-2R-1 REPAIR 1, TRIMMED OUT CRACK AREA IAW SRM 53-10-07-2R-1 REPAIR 1. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. ACCOMPLISHED HEAT TREATMENT ON REPAIR PART PER BOEING 737-700 SRM 53-10-07-2R-1 REPAIR 1 AND BAC5602. TREATED AND PRIMED REPAIR PART AND REPAIR AREA PER BOEING 737-700 SRM 51-20-01-0G-0 AND SOPM 20-41-02. INSTALLED REPAIR PART PER BOEING 737-700 SRM 53-10-07-2R-1 REPAIR 1

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,081 hrs · 35,724 cycles

FWD WET AREA STATION 312 - 328 INTERCOSTAL CRACKED RBL 30 ; / [01] PERFORMED HFEC AND CONFIRMED CRACK ON UPPER SECTION OF INTERCOSTAL AT FWD WET AREA BETWEEN STA 312 AND STA 328 AT RBL 30 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH : 0.787' ( AT 12 AND 6 O'CLOCK POSITION GOING THROUGH FASTENER HOLE).; [02] REMOVED AND REPLACED INTERCOSTAL AT STA 312- STA 328 RBL 30 IN REFERENCE B-737 700 SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0.; [03] ADDING DRWG # 141A5400.; [04] VERIFIED STEPS 2 AND 3.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,081 hrs · 35,724 cycles

CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 17' AFT OF FWD EDGE;I/B OF I/B FASTENER ROW. CRACK LENGTH 1'. ; CRACK FOND AT RT HORIZONTAL STAILIZER LOWER SKIN STAB STA 193.90; 17' AFT OF FWD EDGE;IB OF IB FASTENER ROW. CRACK LENGTH 1'. / [01] REMOVED PAINT WITH STRIPER FOR ACCESS TO REPAIR IAW B 737-7 AMM 51-21-11-150-801; [02] REMOVED DAMAGED AREA AT R/H HORIZONTAL STAB SKIN STA 193.90 .PENDING NDT IAW B737 SRM55-10-01-2R-11 REPAIR 11.] FABRICATED DOUBLER AND FILLER .MATERIAL USED 2024 T-3 0.080 ALUMINUM CLAP AND 0.063 2024 T3 ALUMINUM CLAP AND LOCATED AND DRILLED DOUBLER AND FILLER IAW B737 SRM 55-10-01-2R-11 REPAIR 11.; [07] CORRECTION STEP #5 USED TOOL #172329.; [08] VERIFIED 1 AND 2; [09] CORRECTION: VERIFIED CUT EDGES OF INITIAL PARTS HAVE SURFACE SMOOTHNESS 63 MICRO INCHES RA AND CUT EDGES OF REPAIR PARTS HAVE SURFACE SMOOTHNESS OF 125 MICRO INCHES IAW SRM 55-10-01-11-REPAIR 11.; [10] VERIFIED 6 AND 9. OK TO TREAT AND PRIME; [11] TREATED AND PRIMED REPAIR AND AREA AT RT HORIZONTAL STAB LOWER SKIN STA 193.90 17' AFT OF FWD EDGE I/B IAW AMM 51-00-58-201. AND AMM51-21-72-370-802.; [12] MIXED 0870B002BM SEALANT 10;00PM 01/07/2022 SQUEEZED OUT BY TIME 12;00 01/02/22.; [13] LATE ENTRY: OK TO INSTALL; [14] INSTALLED REPAIR AT R/H HORIZONTAL STAB LOWER SKIN STA 193.90 17' AFT OF FWD EDGE ;I/B OF I/B FASTENERS IAW B 737 SRM 5555-10-01-2R 11 REPAIR 11.;RESTORED TOP COAT ON AREA L/H LOWER SKIN HORIZONTAL STAB REPAIR IAW B737 AMM51-21-73-370-803.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,081 hrs · 35,724 cycles

TWO CRACKS FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA193.90:(1) 16' AFT OF FWD EDGE;I/B OF I/B FASTENER ROW.CRACK LENGTH1'(2) 24'AFT OF FWD EDGE I/B OF I/B FASTENER ROW.CRACK LENGTH 1.7' ; TWO CRACKS FOND AT LT HORIZONTAL STAILIZER LOWER SKIN STAB STA193.90:(1) 16' AFT OF FWD EDGE;IB OF IB FASTENER ROW.CRACK LENGTH1'(2) 24'AFT OF FWD EDGE IB OF IB FASTENER ROW.CRACK LENGTH 1.7' / [01] CRACKS AT LOWER SKIN AT LEFT HORIZONTAL STABILIZER BETWEEN STA 184 AND STA 193 MOST FORWARD CRACK MEASURES 1' LONG AND SECOND MOST AFT CRACK MEASURES 1.200'FOR ENGINEERING SUPPORT; [02] COMPLETED ALL STEPS.

Part: FLOOR PANEL — DISTORTED (FWD CARGO BAY) · airframe 60,081 hrs · 35,724 cycles

FWD CARGO FLOOR PANEL 120CF IS WORN AND DISTORTED ; / [01] FABRICATED FLOOR CARGO PANEL#120CF AT FWD CARGO COMPARTMENT IN REF B737-700 AMM25-52-01-201-801.

Part: SLIDE — FAILED (R1 DOOR) · airframe 59,875 hrs · 35,598 cycles

SUPPLEMENTAL INFORMATION: R1 DOOR SLIDE FALLING OUT OF COVER. ; / [01] REINSTALLED SLIDE PER AMM 25-66-01.

Part: SUPPORT — CRACKED (L/H WING) · airframe 59,819 hrs · 35,564 cycles

LH WING FIXED TRAILING EDGE BULKHEAD SUPPORT IS CRACKED AT LOWER RADIUS THROUGH BOLT HOLE. ; / [01] COMPLETED SRM REPAIR STEPS UP TO AND INCLUDING 57-51-02 4. N.; [02] REMOVED AND REPLACED LH WING FIXED TRAILING EDGE BULKHEAD SUPPORT PER AMM 70-20-02; [03] ENTERED IN ERROR REFERENCE CARD #TTG8Q009D9QG; [04] REMOVED AND REPLACED LH WING FIXED TRAILING EDGE BULKHEAD SUPPORT PER AMM 70-20-02; [05] L/E ACTIVATION COMPLETED

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 57,934 hrs · 34,441 cycles

L/H A/C BAY; AFT UPPER CORNER OF BAY; BS 662; LBL40.0'; CRACK IN WING CENTER SECTION LOWER SKIN TO BS 663 BULKHEAD ATTACH ANGLE; MARKED IN BLACK / REMOVED CRACKED ATTACH ANGLE STA 663 L/H LBL 65 TO LBL 35 AND REPAIRED IAW SRM 57-10-10-2R-5 APPLIED CIC IAW AMM 51-21-91-670-802.

Part: ATTACH ANGLE — CRACKED (BULKHEAD) · airframe 57,934 hrs · 34,441 cycles

EVIDENCE OF CRACK FOUND AT CENTER WING BOX STA 663 RBL 8.5. CTR WING LWR EXT SURFACE. / REPAIRED CENTER WING LOWER EXTERNAL SURFACE VAPOR BARRIER ATTACH ANGLE AT STA 663 RBL 8.5 IAW SRM 57-10-10-2R-5. ACCOMPLISHED LEAK CHECK IAW AMM 28-11-00-400-801. LEAK CHECK GOOD.

Part: PANEL — PULLED (FUSELAGE) · airframe 57,934 hrs · 34,441 cycles

CABIN FLOOR BOARD 231XF FACE SHEET PLY PULLED OFF / REPAIRED FWD RIGHT CORNER CORE ON PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-10; SRM 53-00-50-2R-0

Part: FLOORBOARD — PULLED (CABIN) · airframe 57,934 hrs · 34,441 cycles

CABIN FLOOR BOARD 232SF FACE SHEET PLY PULLED OFF / REPAIRED DAMAGE TO UPPER SURFACE SHEET ON FLOOR BOARD 232 SF 737-700 SRM 53-00-50-2R-0 REV 72 REPAIR AND SRM 53-00-50-2R-1 REV REPAIR 1. TAP TEST GOOD

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,934 hrs · 34,441 cycles

BS 663; RBL 45; IN CABIN; CRACK NOTED VISUALY AT HORIZONTAL FLANGE OF CENTER WING TANK UPPER SKIN LOWER CHORD REPAIRED CENTER WING TANK UPPER SKIN LOWER CHORD AT BS 663 RBL 45 IAW AAR EA 210069 IR AND SWA EA 2115700758 REV IR

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 57,934 hrs · 34,441 cycles

CABIN FLOOR BOARD 241AF FACE SHEET PLY PULLED OFF / REPAIRED CABIN FLOORBOARD 241AF UPPER FACE SHEET PLIES MISSING IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 57,934 hrs · 34,441 cycles

CABIN FLOOR BOARD 231ZF FACE SHEET PLY PULLED OFF / REPAIRED CABIN BOARD 2312F SHEET PLY PULLED OFF ON UPPER SURFACE IAW SRM 53-00-50-2R11 AND SRM 53-00-50-2R-0 REPAIR GENERAL

Part: FLOORBOARD — PULLED (CABIN) · airframe 57,934 hrs · 34,441 cycles

CABIN FLOOR BOARD 232RF FACE SHEET PLY PULLED OFF / REPAIRED DAMAGE TO UPPER SURFACE FACE SHEET ON FLOOR BOARD 232 RF 737-700 SRM 53-00-50-2R-0 REV 72 REPAIR GENERAL AND SRM 53-00-50-2R-1 REV 72 REPAIR 1. TAP TEST GOOD

Part: FLOORBOARD — PULLED (CABIN) · airframe 57,934 hrs · 34,441 cycles

CABIN FLOOR BOARD 241CF FACE SHEET PLY PULLED OFF / REPAIRED CABIN FLOOR BOARD 241CF UPPER FACE SHEET IAW B737 SRM 53-00-50-2R-1

Part: SKIN — CRACKED (BS 235) · airframe 57,934 hrs · 34,441 cycles

RH FUSELAGE EXTERNAL POWER RECEPTACAL LOWER CUTOUT AT STA 235.8 ABOVE STR 24R CRACKED AT FASTENER / CUT AND REMOVED DAMAGED PORTION OF ELECTRICAL GROUND POWER RECEPTACLE R/H FUSELAGE LOWER CUTOUT AT STA 235.8 ABOVE STR 24R FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-10-15-2R-4

Part: GIRT BAR — DISPLACED (FWD SERVICE DOOR) · airframe 56,768 hrs · 33,750 cycles

FORWARD SERVICE DOOR EMERGENCY SLIDE GIRT TO LONG / ATTACHED GRIT PER MT 725-61-06

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,270 hrs · 33,438 cycles

LEFT AFT EMERGENCY EXIT IDENTIFIER LIGHT & CENTER AFT OVER HEAD EMERGENCY LIGHT INOP / R&R BATTERY PACK OPS CK OK REF AMM 33-51-06

Part: MOTOR — INOPERATIVE (STAB TRIM) · airframe 55,330 hrs · 32,865 cycles

DECLARED EMERGENCY------------------------------------------------AFTER DEPARTURE OUT OF HRL FIRST OFFICER NOTICED STABILIZER TRIM SWITCH WOULD NOT WORK. CAPTAIN SWITCHES INOPERATIVE. AS WELL. AUTOPILOT TRIM INOPERATIVE. MANUAL TRIM WAS OPERATIVE. COMPLIED WITH APPROPRIATE CHECKLISTS & FLAPS 15 IND. BRAKE COOLING CHECKED. OTHER THAN MANUAL TRIM THE A/C FLEW FINE. / R&R HORIZONTAL STABILIZER TRIM MOTOR PER AMM.

Part: ACTUATOR — FAILED (FUEL SYSTEM) · airframe 32,756 hrs · 55,169 cycles

CROSS FEED FUEL VALVE FAILED OPEN. / R&R FUEL TANK CROSS-FEED VALVE ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,142 hrs · 32,737 cycles

L2 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP. / RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,142 hrs · 32,737 cycles

R/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R BATTERY PACK PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,142 hrs · 32,737 cycles

L/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R POWER SUPPLY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,142 hrs · 32,737 cycles

L/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R BATTERY PACK PER AMM.

Part: BAND — MISSING (FLASHLIGHT) · airframe 55,142 hrs · 32,737 cycles

AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT SECURITY BAND MISSING. / INSTALLED BAND (SHIELD) PER DWG AND SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,142 hrs · 32,737 cycles

R/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R POWER SUPPLY PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,142 hrs · 32,737 cycles

L1 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP. / RELAMPED LIGHT IAW AMM.

Part: BRACKET — CRACKED (FWD CARGO LH) · airframe 55,142 hrs · 32,737 cycles

FWD CARGO COMPARTMENT L/H FWD OF STA 500A; BETWEEN S-24L AND S-25L BRACKET NOTED CRACKED / REMOVED AND REPLACED BRACKET (CUP) PNO 7531258 AT FWD CARGO L/H FWD STA 500A BETWEEN STR 25L AND STR 24L IRW B737 SRM 51-40-02-0G-0 AND DWD 143A7505

Part: SUPPORT — CRACKED (AFT CARGO COMPT) · airframe 55,142 hrs · 32,737 cycles

AFT CARGO COMPARTMENT AFT OF STA 947.5 BL+10' ABOVE LBL 26L FLOOR ANGLE SUPPORT CRACKED NOTED. / REMOVED AND REPLACED FLOOR ANGLE SUPPORT AT AFT CARGO COMPR. AFT OF STA 947 BT 10' ABOVE LBL 26L PER REF: SRM 51-40-02-0G-0 B737-700.

Part: FLOORBEAM — CORRODED · airframe 55,142 hrs · 32,737 cycles

**CORROSION** FLOOR BEAM STA 328; RBL 44; WL 208.1 / THIS ITEM WAS ACCOMPLISHED ON N/R; S/N W.135684 THIS ITEM NOW CLOSED.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 55,142 hrs · 32,737 cycles

***CORROSION*** NOTED ON TEE SUPPORTSURFACE AT AFT CARGO COMPARTMENT STA 772 / REMOVED CORROSION AT AFT CARGO TEE SUPPORT STA 772. MEASURES: ORIGINIAL THICKNESS .070';MINIMUM THICKNESS FOUND .031'. MATERIAL LOST .039' FOUND OUT OF LIMITS.REPLACED TEE SUPPORT P/N 146A9401.16 AS PER REF B737-700 SRM 53-00-53-1A-2.AND WILL BE INSTALLED ON CUSTOMER ORDER -JPANEL-141-CLOSE

Part: FLOORBEAM — CORRODED (BS 328) · airframe 55,142 hrs · 32,737 cycles

FLOOR BEAM AREA CORRODED AT BS. 328, BETWEEN RBL 43 TO RBL 47. REPAIRED THE FLOORBEAM TEE CAP IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 55,142 hrs · 32,737 cycles

CORROSION--AFT CARGO STA 887 FLOOR PANELS SPLICER HAS EVIDENCE OF CORROSION AT SEVERAL ATTACH HOLES / ACCOMPLISHED INSPECTION AT AFT CARGO FLOOR PANEL SPLICER STA 887; FOUND DEEP CORROSION OUT OF LIMITS. REMOVED AND REPLACED FLOOR PANEL TEE SPLICER AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #146A7500

Part: FLOOR SUPPORT — CORRODED (BS 294.5-312) · airframe 55,142 hrs · 32,737 cycles

FLOOR SUPPORT CORRODED BETWEEN BS. 294.5 TO BS. 312, LBL 13. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,142 hrs · 32,737 cycles

L/H HORIZONTAL STABILIZER #4 RIB STIFFENER #3 CRACKED. / REPAIRED #3 STIFFENER PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 55,142 hrs · 32,737 cycles

**CORROSION **STA 344; BL0 TO LBL 3 AT FLOOR BEAM / REMOVED CORROSION AT CABIN FLOOR BEAM STA 344; BL0 TO LBL 3. MEASURES: ORIGINAL MATERIAL .180'; MINIMUM MATERIAL NOTED 0.145'; MATERIAL LOST 0.035'. FOUND OUT OF LIMITS AS PER REF. B737-700 SRM 53-10-51-1A-1. REPARIED FLOOR BEAM AS PER BEAM AS PER REF. B737-700 SRM 53-10--51-2R8 AND DWG 141A5505

Part: INTERCOSTAL — CRACKED (BS 294.5) · airframe 55,142 hrs · 32,737 cycles

INTERCOSTAL CRACKED AT BS. 294.5, BL 0. / R&R INTERCOSTAL IAW DWG.

Part: FLOOR SUPPORT — CORRODED (BS 294-312) · airframe 55,142 hrs · 32,737 cycles

INTERCOSTAL CORRODED BETWEEN BS. 294 TO BS. 312, LBL 13. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 312-348) · airframe 55,142 hrs · 32,737 cycles

L/H INNER CREASE BEAM CORRODED BETWEEN BS. 312 TO BS. 348.2. / R&R CREASE BEAM PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 55,142 hrs · 32,737 cycles

FLOORBEAM CORRODED AT BS 312 BETWEEN LBL 32 TO RBL 22. REPAIRED FLOORBEAM IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,142 hrs · 32,737 cycles

L/H HORIZONTAL STABILIZER #4 RIB #2 STIFFENER CRACKED. / REPAIRED #2 STIFFENER PER SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 55,142 hrs · 32,737 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 47. / R&R INTERCOSTAL IAW DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 55,142 hrs · 32,737 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO BAY) · airframe 55,142 hrs · 32,737 cycles

*** CORROSION*** FWD CARGO COMP STA 500D STR 25 FROM LBL 23 TO RBL 23 FLOOR SUPPORT HAS CORROSION / REMOVED AND REPLACED #002 SUPPORT FWD CARGO COMPARTMENT STA 500D STR 25 FROM LBL23 TO RBL 23 IN REF B-737-700 SRM 51-40-02-0G-0.

Part: GUSSET — CRACKED (BS 500D) · airframe 55,142 hrs · 32,737 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM.

Part: PLATE — CORRODED (FWD CARGO BAY) · airframe 55,142 hrs · 32,737 cycles

*** CORROSION*** FWD CARGO COMP STA 400 TO 500D STR 25 LBL 23 L/H SIDE PLATE HAS CORROSION / REMOVED CORROSION AT FWD CARGO L/H SIDE PLATE FROM STA400 TO 500D ORIGINAL .040' MAT LOST .010' MAT REMAINING .030' FOUND TO BE OUT OF LIMITS IAWS B737 SRM 53-00-53-1A-2 FIG 103 DETAIL C (STA 480+4' AND STA 500A+12') REMOVED AND REPLACED L/H SIDE PLATE FROM STA 396 TO STA 500D IAW B737 SRN 51-40-02-06-0 AND 533-00-53-2R-5

Part: GUSSET — CRACKED (BS 500D) · airframe 55,142 hrs · 32,737 cycles

FORWARD CARGO COMPARTMENT FORWARD GUSSET CRACKED AT BS. 500D, STR. 21L. / R&R GUSSET IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,142 hrs · 32,737 cycles

L/H HORIZONTAL STABILIZER #4 RIB CRACKED AT #4 STIFFENER. / REPAIRED #4 STIFFENER PER SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

FLOOR PANEL 241RF DELAMINATED / REMOVED AND REPLACED FLOOR PANEL 241RF REF. B737-700 B-DW A46A5810 SRM 53-00-50-12-0

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

FLOOR PANEL 241DF DELAMINATED / REPLACED CABIN FLOOR PANEL 241DF FOR NEW PANEL P/N 7530622 AND WILL BE INSTALLED ON JPANEL231-CLOSE

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

FLOOR PANEL 231XF DELAMINATED / REPLACED FLOOR PANEL 231XF IAW B737 AMM 53-21-00-400-801 WILL BE ACCOMPLISHED ON JPANEL 231 CLOSE

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

ACCESS PANEL 521ZB DELAMINATED. DOT 221-02 / CLEANED AND REQUIIRED AT ACCESS PANEL 521ZB PER B737-700 SRM 51-70-0G-2R-6 MATERIAL USED P.O. 1190381; P.O. 1624260 AND P.O. 614988

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

FLOOR PANEL 241NF DELAMINATED / REMOVED & REPLACED AND INSTALLED NEW FLOOR PANEL # 241NF AT MAIN CABIN IN REF. B-737-700 DW 146A5810; AMM 53-21-00-000-801/53-21-00-400-801

Part: ACCESS PANEL — BROKEN (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

ACCESS PANEL 194BR ; CORNER BROKEN. DOT 221-01 / CLEANED AND REPAIRED DAMAGE AREA ON CORNER OF ACCESS PANEL 194BR SIZE 2' DIAMETER WITH A PERMANENT WET LAY UP REPAIR AS PER B737 SRM 51-70-04-2R-10 REPAIR #10 MATERIAL USED PO # 1624260 AND PO # 1129190. PRIME AND TOP COAT REPAIRED AREA ON ACCESS PANEL 194BR AS PER B737 AMM 51-21-99-300-802.

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 55,142 hrs · 32,737 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN RBL 38 TO RBL 60. / REPAIRED WEB PER SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 55,142 hrs · 32,737 cycles

FLOOR PANEL 241KF DELAMINATED / FABRICATED NEW FLOOR PANEL 241KF MAT. USED GILL FAB 5424-400001BB-G; PER REF. BOEING DWG 146A5810

Part: RETAINING CLIP — LOOSE (L2 DOOR) · airframe 54,480 hrs · 32,299 cycles

L2 DOOR GIRT BAR LOOSE AND FELL OUT. ADJUSTED GIRT BAR CLIPS PER AMM.

Part: LIGHT — DETACHED (CABIN) · airframe 54,200 hrs · 32,113 cycles

R1 DOOR EMERGENCY EXIT SIGN FELL OFF. R & R THE LIGHT ASSEMBLY HOUSING IAW MM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 53,510 hrs · 31,655 cycles

HORIZONTAL STABILIZER LEFT UPPER FORWARD SLIDING SEAL CRACKED / REMOVED AND REPLACED HORIZONTAL STABILIZER LEFT UPPER FORWARD SLIDING SEAL PER AMM. 53-31-31

Part: WEDGE — BROKEN (LT WING) · airframe 53,510 hrs · 31,655 cycles

LEFT WING #2 SLAT LOWER SKIN T/E ALUMINUM FILLER IS BROKEN OFF AT O/B END. / REPAIRED LEFT WING #2 SLAT LOWER SKIN T/E ALUMINUM FILLER AT O/B END REF SRM 57-42-01-2R-6

Part: NONE — CRACKED (AC BAY) · airframe 53,510 hrs · 31,655 cycles

FLOOR BOARD SUPPORT BREAK PANEL IN AIR CONDITIONING DISTRIBUTION BAY STATION 540 RIGHT OF CENTER LINE CRACKED. / R&R'D FLOOR BOARD SUPPORT BREAK PANEL IN AIR CONDITIONING DISTRIBUTION BAY STATION 540 RIGHT OF CENTER LINE PER SRM 51-10-02.

Part: NONE — CRACKED (AC BAY) · airframe 53,510 hrs · 31,655 cycles

FLOOR BOARD SUPPORT BREAK PANEL IN AIR CONDITIONING DISTRIBUTION BAY STATION 540 LEFT OF CENTER LINE CRACKED. / R&R'D FLOOR BOARD SUPPORT BREAK PANEL IN AIR CONDITIONING DISTRIBUTION BAY STATION 540 LEFT PER SRM 51-10-02.

Part: LENS — MISSING (CABIN) · airframe 53,249 hrs · 31,483 cycles

RT OVER WING EXIT LIGHT LENS FORWARD OF DOOR MISSING. R&R LENS PER MM.

Part: PRESSURE SWITCH — LOW PRESSURE (HYD PUMP) · airframe 52,963 hrs · 31,297 cycles

AIR TURNBACK, SYSTEM A ELECTRIC HYDRAULIC PUMP LOW PRESSURE PUMP, LIGHT COME ON. R & R THE A SYSTEM PRESSURE SWITCH IAW AMM.

Part: FSEU — FAULTY (E&E BAY) · airframe 52,244 hrs · 30,857 cycles

AIR TURNBACK, ON TAKEOFF ROLL (APPROX 90 KNOTS), RECEIVED TAKEOFF WARNING WITH LE FLAPS TRANSIT LIGHT FLICKERING ON & OFF. AFTER FLAP RETRACTION, LEADING EDGE TRANSIT LIGHT STAYED ON WITH NR 4 LE FLAP INDICATING FULL EXTENSION ASYMMETRY NOTED WITH AUTOPILOT OFF. R&R FLAP SLAT ELECTRONIC UNIT PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 50,495 hrs · 29,743 cycles

RT EXIT SIGN LENS MISSING AT ROW 12. INSTALLED LENS IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,013 hrs · 29,444 cycles

FORWARD SERVICE EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,457 hrs · 29,072 cycles

RIGHT EMERGENCY EXIT SIGN INOPERATIVE. R & R BATTERY IAW AMM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 49,457 hrs · 29,072 cycles

RIGHT EMERGENCY SIGN BROKEN. R & R THE SIGN AMM.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 49,045 hrs · 28,798 cycles

SUPPLEMENTAL INFORMATION: NO.2 CANOE ACCESS PANEL 543CL CRACKED. / REPLACED NO.2 CANOE ACCESS PANEL 543CL PER SOPM 20-50-01

Part: PLATE — CRACKED (RIGHT WING) · airframe 49,045 hrs · 28,798 cycles

RIGHT WING WIGGLE PLATE UNDER PANEL 651EB (ABOVE #6 FLAP TRACK) IS CRACKED ON INBD SIDE / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02; SEE BELOW FOR INDIVIDUAL SIGN-OFFS.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 49,045 hrs · 28,798 cycles

AFT CARGO LEFT HAND TRANSITION ANGLE HAS CORROSION FROM STA. 827 TO STA. 727 / REMOVED AND REPLACED L/H TRANSITION ANGLE PER SRM 51-40-02.

Part: FLAP — DELAMINATED (LH OUTBD AFT FLA) · airframe 49,045 hrs · 28,798 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED ON UPPER AND LOWER SURFACES AT AFT INBOARD CORNER. / REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22. TAG NO: 346440 PN ON: 113A3700-23 SN ON: 003211 PN OFF: SN OFF: 001467

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 49,045 hrs · 28,798 cycles

PRESSURE BULKHEAD WEB ATTACH ANGLE CRACKED AT BS 663, RT SIDE AT INBOARD NUTPLATE HOLE. REPAIRED THE ATTACH ANGLE IAW EA.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 49,045 hrs · 28,798 cycles

RUDDER COUNTER WEIGHT IS CORRODED / REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER CMM 55-40-09.

Part: FLAP — DELAMINATED (RH OUTBD AFT FLA) · airframe 49,045 hrs · 28,798 cycles

R/H O/B AFT FLAP IS DELAMINATED AT I/B LOWER SURFACE / REMOVED AND REPLACED R/H O/B AFT FLAP IAW AMM 27-51-22. TAG NO: 352131 PN ON: 113A3700-24 SN ON: 002006 PN OFF: SN OFF: 1468

Part: TRACK — WORN (CABIN) · airframe 49,045 hrs · 28,798 cycles

PASSENGER SEAT TRACK LBL 45 (1) UPPER CROWN IS WORN FROM SEAT MOUNT CONTACT. LOCATED AT STA 520. / REPAIRED AT STA 520 SEAT TRACK #1 PER SRM 53-00-52-2R-4

Part: BRACKET — CRACKED (RIGHT WING) · airframe 49,045 hrs · 28,798 cycles

RIGHT WING; BULB SEAL RETAINER FWD. OF THE CURVED BULB SEAL RETAINER IS CRACKED. LOCATED ABOVE THE #2 PYLON AFT END. MARKED / REMOVED AND REPLACED BULB SEAL RETAINER ATTACH BRACKET PER SRM 51-40-02.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 49,045 hrs · 28,798 cycles

FWD CARGO THRESHOLD AFT SCUFF PLATE IS CRACKED. / THRESHOLD PLATE REPAIRED ON RO # 7530065-AOR. PLATE TO BE INSTALLED ON ROUTINE TASK CARDS 753-646-62-01 AND 753-646-63-01.

Part: RETAINER — CRACKED (LEFT WING) · airframe 49,045 hrs · 28,798 cycles

LEFT WING; CURVED BULB SEAL RETAINER ABOVE THE #1 PYLON IS CRACKED. MARKED / REMOVED AND REPLACED SEAL SUPPORT ANGLE PER SRM 51-40-05; SRM 51-20-01; SRM 51-40-02.

Part: NONE — CRACKED (LEFT WING) · airframe 49,045 hrs · 28,798 cycles

LEFT WING TRAILING EDGE; GREEN ATTACH CLIP CRACKED; LOCATED UNDER THE FORWARD INBD. CORNER OF UPPER WING PANEL 551AT. MARKED / REMOVED AND REPLACED GREEN ATTACH CLIP PER SRM 51-40-02

Part: RETAINER — CRACKED (RIGHT WING) · airframe 49,045 hrs · 28,798 cycles

RT WING FIXED LOWER T/E PANEL 651GB AFT SEAL RETAINER IS CRACKED AND WORN. / :REMOVED AND REPLACED BULB SEAL RETAINER ON PANEL 651GB PER SRM 51-40-02.

Part: COVER — MISSING (EXIT SIGN) · airframe 46,966 hrs · 27,475 cycles

OVERWING CEILING EXIT SIGN COVER MISSING. SECURED COVER PER SIP.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 45,838 hrs · 26,799 cycles

FORWARD EMERGENCY EXIT SIGN LENS LOOSE. SECURED THE LENS IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,147 hrs · 24,582 cycles

FORWARD GALLEY EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,147 hrs · 24,582 cycles

LEFT EMER EXIT HATCH LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

CHORD CRACKED AT BS 540, STRINGER 22R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 42,147 hrs · 24,582 cycles

VERTICAL STABILIZER VERTICAL FIN SUPPORT ANGLE CRACKED ON REAR SPAR, AT BS 1016. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

BULKHEAD WEB CRACKED AT BS 663.75, LBL 18. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

MAIN WW COMPARTMENT ANGLE CRACKED AT BS 663.75, LBL 31. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 8R. R & R TIE CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 294.5 - 312, BL 0. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FORWARD GALLEY AREA, WEB INTERCOSTAL CRACKED, BETWEEN BS 312 - 326, RBL 34. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FORWARD GALLEY AREA, INTERCOSTAL WEB CRACKED, BETWEEN BS 326 - 344, LBL 48. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, BL 0. REPAIRED INTERCOSTAL IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,147 hrs · 24,582 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT ON STAB STATION 92.70. REPAIRED RIB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FORWARD GALLEY AREA, WEB INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, LBL 11. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FORWARD GALLEY AREA, WEB INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, RBL 12. REPAIRED INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 727B, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

RIGHT SIDE NR 3 WINDOW FRAME E - F, POST CRACKED IN HOLE NR 7. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

LEFT SIDE NR 3 WINDOW FRAME E - F, POST CRACKED IN NR 8 OPEN FASTENER HOLE. REPAIRED POST IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

RIGHT SIDE NR 3 WINDOW FRAME E - F, POST CRACKED IN HOLE NR 8. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

LEFT SIDE NR 3 WINDOW FRAME E - F, POST CRACKED IN HOLE NR 6. REPAIRED POST IAW ACO.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 42,147 hrs · 24,582 cycles

AFT CARGO COMPARTMENT TRACK CRACKED AT BS 767, RBL 13.80. REPAIRED TRACK IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

ANGLE CRACKED AT STATION 500C, STRINGER 26L. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

GUSSET CRACKED AT STATION 500D, STRINGER 19R. R & R GUSSET IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

GUSSET CRACKED AT STATION 500D, STRINGER 19L. R & R GUSSET IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FORWARD CARGO COMPARTMENT SUPPORT ANGLE CRACKED, AT BS 500B, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

ANGLE CRACKED AT STATION 500B, STRINGER 26L. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,147 hrs · 24,582 cycles

FORWARD CARGO COMPARTMENT, ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,147 hrs · 24,582 cycles

RIGHT WING NR 8 LE SLAT, SKIN CRACKED AT STATION 451.97. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,209 hrs · 24,029 cycles

AFT LT EMER LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,209 hrs · 24,029 cycles

FORWARD LT EMER LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,209 hrs · 24,029 cycles

FORWARD RT EMER LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,054 hrs · 23,366 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,644 hrs · 20,843 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,644 hrs · 20,843 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,644 hrs · 20,843 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 147.9 BETWEEN 9.5 INCHES & 17 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,644 hrs · 20,843 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.7 16.5" FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,644 hrs · 20,843 cycles

FLOOR PANEL SUPPORT CRACKED AT BS 537.45 BETWEEN BL 0 TO LBL 24.75. R & R SUPPORT IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 35,644 hrs · 20,843 cycles

LT WING AFT OF PYLON FAIRING UPPER SHELF ANGLE CTR FWD L BRACKET CRACKED. R & R L BRACKET IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,644 hrs · 20,843 cycles

FLOOR PANEL SUPPORT CRACKED AT BS 537.45 BETWEEN BL 0 TO RBL 24.75. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,644 hrs · 20,843 cycles

FLOOR PANEL SUPPORT CRACKED AT BS 537.45 BETWEEN RBL 24.75 TO RBL 45.50. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,644 hrs · 20,843 cycles

FLOOR PANEL SUPPORT CRACKED AT BS 537.45 BETWEEN LBL 24.75 TO LBL 45.50. R & R SUPPORT IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 35,644 hrs · 20,843 cycles

LT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,644 hrs · 20,843 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 120.3, 18.75 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,644 hrs · 20,843 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.5 10" FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 35,221 hrs · 20,591 cycles

INFLIGHT SHUTDOWN DECLARED EMERGENCY ON APPROACH, AIRCRAFT SHUDDERED & VIBRATED EXCESSIVELY OBSERVED OFF SCALE HIGH N1 & OFF SCALE HIGH EGT. NR 1 ENG SHUT DOWN ENG IN FLIGHT. R & R NR 1 ENG IAW TC.

Part: HMU — FAULTY (NR 1 ENGINE) · airframe 35,248 hrs · 20,609 cycles

AIR RETURN ON TAKEOFF NR 1 ENG WOULD NOT GO ABOVE APPROXIMATELY 62%. R & R NR 1 ENG HMU MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 34,864 hrs · 20,372 cycles

RT UPPER CORNER WINDOW POST C-D FRAME CRACKED .700 INCHES IN LENGTH. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 34,856 hrs · 20,367 cycles

FLIGHT DECK NR 1 WINDOW FRAME RT SIDE CRACKED AT UPPER OTBD CORNER, LOCATED JUST ABOVE PREVIOUS CRACK. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 34,565 hrs · 20,191 cycles

LT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STAB BS 184.70 9.75" FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 34,565 hrs · 20,191 cycles

FIRST OFFICERS UPPER CORNER WINDOW POST C-D CRACKED .700 INCHES IN LENGTH. REPAIRED POST IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 34,137 hrs · 19,942 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: SIGN — DETACHED (CABIN) · airframe 32,632 hrs · 19,028 cycles

FORWARD EXIT SIGN FELL OFF. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,342 hrs · 18,858 cycles

LEFT AFT EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED PER AMM. LEFT AFT EMERGENCY LIGHTS BATTERY PACK M1672

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,342 hrs · 18,858 cycles

RIGHT FWD CENTER EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED PER AMM RIGHT FWD CENTER EMERGENCY LIGHTS BATTERY PACK M1670.

Part: COVER — BROKEN (CABIN) · airframe 31,167 hrs · 18,135 cycles

LEFT EEPLS COVER BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 30,102 hrs · 17,494 cycles

EMERGENCY LIGHT FLOOR LENS COVER CRACKED AT ROW 20. REMOVED AND REPLACED COVER PER M/M.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 30,102 hrs · 17,494 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 29,138 hrs · 16,917 cycles

RT AFT GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,138 hrs · 16,917 cycles

RIGHT AFT GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,857 hrs · 16,742 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: CAP — MISSING (CABIN) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT EEPLS INOP. REMOVED AND REPLACED EEPLS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD LAV, AFT FACING WALL EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CREASE BEAM VERTICAL STRAP CORRODED AT BS 298. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CREASE BEAM ATTACH ANGLE UPPER SURFACE CORRODED BETWEEN BS 298 TO BS 325. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND STUB FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,695 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,423 hrs · 16,487 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP BETWEEN ROW 1 AND ROW 2. R&R EEPLS PER MM.

Part: FAN — FAULTY (A/C BAY) · airframe 28,395 hrs · 16,473 cycles

DIVERSION/DECLARED EMERGENCY - FLIGHT ATTENDANTS REPORTED FUMES & MIST IN CABIN. ELECTRICAL SMELL LASTED A FEW MINUTES THEN DISSIPATED. REMOVED AND REPLACED RECIRCULATION FAN AND FILTER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,386 hrs · 16,468 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LOOSE AT ROW 18. SECURED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 28,058 hrs · 16,273 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER CRACKED AT ROW 16. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 28,058 hrs · 16,273 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER CRACKED AT ROW 5. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 28,058 hrs · 16,273 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER CRACKED AT ROW 20. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 28,058 hrs · 16,273 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,669 hrs · 14,874 cycles

DURING SCHEDULED HC1 CHECK, FOUND CRACK ON RT HORIZONTAL STAB LWR SPAR SKIN, STA 129.5 +34 INCHES AFT OF LEADING EDGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,669 hrs · 14,874 cycles

DURING SCHEDULED HC1 CHECK, FOUND CRACK ON RT HORIZONTAL STAB LWR SPAR SKIN, STA 129.5 +25 INCHES AFT OF LEADING EDGE. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 24,810 hrs · 14,379 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 22,216 hrs · 12,872 cycles

DURING SCHEDULED 6Y CHECK, FOUND HORIZONTAL STABILIZER SKIN CRACKED AT STA 139. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 22,203 hrs · 12,864 cycles

DURING SCHEDULED 6Y CHECK, FOUND RT WING NR 6 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 22,203 hrs · 12,864 cycles

DURING SCHEDULED 6Y CHECK, FOUND RT WING NR 7 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: COVER — MISSING (CABIN) · airframe 21,827 hrs · 12,627 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER MISSING AT ROW 10. INSTALLED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 21,703 hrs · 12,557 cycles

LEFT EEPLS LENS LOOSE AT ROW 11. SECURED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,463 hrs · 13,413 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 101.90 TO STA 147.90. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 20,621 hrs · 11,886 cycles

EEPLS COVER LOOSE AT ROW 11. SECURED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,471 hrs · 11,800 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 18,441 hrs · 10,581 cycles

AFT ENTRY BULKHEAD EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 18,441 hrs · 10,581 cycles

L2 EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 16,894 hrs · 9,634 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 139. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,651 hrs · 9,490 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,287 hrs · 9,260 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,506 hrs · 8,215 cycles

EEPLS INOP AT ROW 1. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,479 hrs · 8,200 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (ROW 3 ABC) · airframe 14,437 hrs · 8,176 cycles

EEPLS MISSING LENS AT ROW 3 ABC. INSTALLED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,408 hrs · 8,159 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,398 hrs · 8,153 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 7 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 9,680 hrs · 5,432 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT EXTERIOR LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 9,542 hrs · 5,337 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 7,282 hrs · 4,052 cycles

FWD END OF EEPLS TRACK BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: CAP — LOOSE (EMERGENCY LIGHTS) · airframe 7,170 hrs · 3,978 cycles

EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS END CAP PER MM.

Part: COVER — MISSING (EEPLS) · airframe 7,105 hrs · 3,941 cycles

EEPLS COVER MISSING AT FWD END. INSTALLED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 6,971 hrs · 3,860 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 6,604 hrs · 3,651 cycles

EEPLS TRACK COVER MISSING AT FWD END. INSTALLED COVER PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 6,500 hrs · 3,578 cycles

EEPLS TRACK LENS LOOSE AT ROW 3. SECURED LENS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 6,500 hrs · 3,578 cycles

FWD END OF EEPLS TRACK COVER LOOSE. SECURED COVER PER MM.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 6,379 hrs · 3,512 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 WINDOW HEAT CONTROLLER PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 6,358 hrs · 3,502 cycles

EEPLS TRACK COVER OUT OF POSITION AT FWD END. SECURED COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 170 hrs · 114 cycles

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