N276WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
POST FLIGHT, FOUND SMOKE COMING FROM LEFT MAIN WHEEL BRAKE ASSY. BRAKE TEMP READINGS UNABLE TO BE TAKEN PRIOR TO 15 MINUTES AFTER ACFT ARRIVED AT GATE. ACFT BRAKES REQUIRED TO COOL MINIMUM GROUND TIME. IAW MPM 53.5.2.2
CLOSE ASSIST HANDLE BROKE F/E DOOR. REPLACED ASSIST HANDLE ON FORWARD ENTRY DOOR IAW AMM 25-21-31.
PASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED.<[01] R&R AFTER SLIDE MOUNT ISOLATOR PER SRM 51-40-02;[02] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
RIGHT WING UPPER PANEL SUPPORT, FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-A00729.
AFTER LAV SMOKED ALARM ACTIVATED INTERMITTENTLY DURING FINAL DESCENT AND AT THE GATE. NO SIGNS OF SMOKE. OK TO CONTINUE PER MEL 26-16-01 XB;AFT LAVATORY SMOKE DETECTION SYSTEM. WITH SP 1B & 3 AND AUTHORIZATION NUMBER 296463. R & R AFT LAVATORY SMOKE DETECTOR IAW AMM 26-14-01.
FWD ENTRY DOOR ASSIST HANDLE STRAP WILL NOT SECURE TO DOOR TRIM<[01] REPLACED HANDLE ?WARNING? STRAP PER SIP OPS CHECKS GOOD
FWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE, TIGHTENED HARDWARE. PER AMM 20-50-11.
ENG #1 OVERHEAT DURING CLIMB THROUGH 9K COMPLETED QRC/QRH LIGHT EXTINGUISHED<[01] PERFORMED FIM TASK 26-10 TASK 810 NO FAULTS FOUND. REMOVED AND REPLACED ENGINE & APU FIRE DETECTION CONTROL MODULE AS PER AMM 26-10-01. AIRCRAFT STILL REQUIRES HIGH POWER ENGINE RUN.E58067.;[02] PERFORMED POWER ASSUARANCE TEST 5 AT 65% N1 AND FOUND TO BE WITHIN LIMITS PER AMM 71-00-00. OPS CHECK PASSED.
ENROUTE NOTICED ELECTRICAL BURN SMELL THEN RECEIVED A 'TRANSFER BUS OFF' LIGHT AND 'SOURCE OFF' LIGHT ON NO.2 SIDE. RAN QRH AND DURING CHECKLIST GOT A 'DRIVE' LIGHT ON NO2 SIDE. COMPLIED WITH QRH AND FA'S CALLED TO SAY CABIN HAD SMOKE. RAN QRH AND SMOKE CLEARED. LANDED AT NEAREST SUITABLE WHICH WAS DTW<[01] REPLACED GCU 2 REF. AMM 24-21-81. GCU 2 OPS CHECKS FAILED. WILL NEED ANOTHER GCU DUE TO CATASTROPHIC FAILURE. WIRING CHECKS FOUND 10 OHMS TO GROUND IN ALL THREE CIRCUITS OF PMG WITH GCU 2 OUT OF RACK AND IDG CONNECTOR DP1205 DISCONNECTED. ALSO 47 OHMS TO GROUND AT D10892B (PIN 55) WITH CONNECTOR DP1206 DISCONNECTED AT IDG. THIS MIGHT BE FROM POSSIBLE CORROSION AT CONNECTOR DP1234. WILL NEED TO DEFER IDG 2 PER MCC.;[02] OK TO CONTINUE PER MEL 24-1-02; SP1. (SEE MXI FOR COMPLETE DETAILS OF WORK PERFORMED.);[03] TROUBLESHOT PER WDM 24-11-21. FOUND CONNECTOR D30116 WITH HIGH RESISTANCE AND CORRODED. D30116 REQUIRES REPLACEMENT.;[04] REMOVED AND REPLACED W1264-3001 WIRE ASSEMBLY IAW SWPM 20-10-11. REMOVED AND REPLACED D30116 IAW SWPM 20-61-00. OPS CHECK GOOD IAW AMM 24-11-00; 71-00-00; 80-11-01; A/C OK FOR SERVICE.
ENROUTE NOTICED ELECTRICAL BURN SMELL THEN RECEIVED A 'TRANSFER BUS OFF' LIGHT AND 'SOURCE OFF' LIGHT ON NO.2 SIDE. RAN QRH AND DURING CHECKLIST GOT A 'DRIVE' LIGHT ON NO2 SIDE. COMPLIED WITH QRH AND FA'S CALLED TO SAY CABIN HAD SMOKE. RAN QRH AND SMOKE CLEARED. LANDED AT NEAREST SUITABLE WHICH WAS DTW<[01] REPLACED GCU 2 REF. AMM 24-21-81. GCU 2 OPS CHECKS FAILED. WILL NEED ANOTHER GCU DUE TO CATASTROPHIC FAILURE. WIRING CHECKS FOUND 10 OHMS TO GROUND IN ALL THREE CIRCUITS OF PMG WITH GCU 2 OUT OF RACK AND IDG CONNECTOR DP1205 DISCONNECTED. ALSO 47 OHMS TO GROUND AT D10892B (PIN 55) WITH CONNECTOR DP1206 DISCONNECTED AT IDG. THIS MIGHT BE FROM POSSIBLE CORROSION AT CONNECTOR DP1234. WILL NEED TO DEFER IDG 2 PER MCC.;[02] OK TO CONTINUE PER MEL 24-1-02; SP1. (SEE MXI FOR COMPLETE DETAILS OF WORK PERFORMED.);[03] TROUBLESHOT PER WDM 24-11-21. FOUND CONNECTOR D30116 WITH HIGH RESISTANCE AND CORRODED. D30116 REQUIRES REPLACEMENT.;[04] REMOVED AND REPLACED W1264-3001 WIRE ASSEMBLY IAW SWPM 20-10-11. REMOVED AND REPLACED D30116 IAW SWPM 20-61-00. OPS CHECK GOOD IAW AMM 24-11-00; 71-00-00; 80-11-01; A/C OK FOR SERVICE.
ENROUTE NOTICED ELECTRICAL BURN SMELL THEN RECEIVED A 'TRANSFER BUS OFF' LIGHT AND 'SOURCE OFF' LIGHT ON NO.2 SIDE. RAN QRH AND DURING CHECKLIST GOT A 'DRIVE' LIGHT ON NO2 SIDE. COMPLIED WITH QRH AND FA'S CALLED TO SAY CABIN HAD SMOKE. RAN QRH AND SMOKE CLEARED. LANDED AT NEAREST SUITABLE WHICH WAS DTW<[01] REPLACED GCU 2 REF. AMM 24-21-81. GCU 2 OPS CHECKS FAILED. WILL NEED ANOTHER GCU DUE TO CATASTROPHIC FAILURE. WIRING CHECKS FOUND 10 OHMS TO GROUND IN ALL THREE CIRCUITS OF PMG WITH GCU 2 OUT OF RACK AND IDG CONNECTOR DP1205 DISCONNECTED. ALSO 47 OHMS TO GROUND AT D10892B (PIN 55) WITH CONNECTOR DP1206 DISCONNECTED AT IDG. THIS MIGHT BE FROM POSSIBLE CORROSION AT CONNECTOR DP1234. WILL NEED TO DEFER IDG 2 PER MCC.;[02] OK TO CONTINUE PER MEL 24-1-02; SP1. (SEE MXI FOR COMPLETE DETAILS OF WORK PERFORMED.);[03] TROUBLESHOT PER WDM 24-11-21. FOUND CONNECTOR D30116 WITH HIGH RESISTANCE AND CORRODED. D30116 REQUIRES REPLACEMENT.;[04] REMOVED AND REPLACED W1264-3001 WIRE ASSEMBLY IAW SWPM 20-10-11. REMOVED AND REPLACED D30116 IAW SWPM 20-61-00. OPS CHECK GOOD IAW AMM 24-11-00; 71-00-00; 80-11-01; A/C OK FOR SERVICE.
AT CRUISE; A NOTICEABLE ELECTRICAL SMELL WAS NOTICED THROUGHOUT ENTIRE PLANE. SHORTLY AFTER; TRANSFER BUS LIGHT ILLUMINATED; FOLLOWED BY SOURCE OFF LIGHT; FOLLOWED BY DRIVE LIGHT - ALL CHECKLISTS WERE FOLLOWED AND COMPLIED WITH<[01] WHILE PERFORMING FIM TASK 05-51-56-200-801 SMOKE OR FUMES IN CABIN (CONDITIONAL INSPECTION); ISOLATED THE SMELL TO THE EE COMPARTMENT. FOUND #2 GCU FAILED WITH EXTREME BURNED ELECTRICAL SMELL. CHANGED #2 GCU PER 24-21-81 AMM. OPS CHECK NORMAL NO FAULTS FOUND.;[02] CORRECTED VALUES.
EMERGENCY EXIT LOCATOR FWD OF FWD SERVICE DOOR HAS INOP BULBS<[01] RELAMPED EMERGENCY EXIT LOCATOR FWD OF FWD SERVICE DOOR; PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
EMERGENCY EXIT LOCATOR FWD OF L/H OWE HAS INOP BULBS<[01] RELAMPED EMERGENCY EXIT LOCATOR FWD OF FWD SERVICE DOOR; PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
ASSOCIATED EMERGENCY LIGHTS WITH BATTERY PACK M1674 DO NOT TURN ON<[01] REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF M1673 EMERGENCY BATTERY PACK PER AMM 33-51-06-960-805<BR><BR>CARD COMPLETE;[02] UPDATED PART REQUIREMENTS;[03] ALL STEPS COMPLETED FOR CC# TTG8Q00YA1Q0;[04] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
L732 AFT LEFT ESCAPE SLIDE LIGHT DOES NOT TURN ON.<[01] RELAMPED AFT L/H ESCAPE SLIDE LIGHT AND PERFORME3D INSTALLATION TEST PER AMM 33-51-04-960-801; LIGHT STILL INOP; PERFORMED GOOD CONTINUITY CHECK OF WIRING FOR AFT L/H ESCAPE SLIDE LIGHT PER WDM 33-51-14; UPON FURTHER INVESTIGATION; FOUND FUSE F2 ON EMERGENCY LIGHT BATTERY CHARGER M1673 TO BE BAD; REPLACED FUSE F2 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801; LIGHT NOW ILLUMINATES<BR><BR>MULTIMETER CAL ID: ATS1511 CAL DUE: 05/2025;[02] JOB COMPLETE.
FCB FWD CORNER SCUFF PLATE CRACKED<[01] ALL STEPS COMPLETED
ELONGATED FASTENER HOLE ON BUFFLE AT BS500 TO BS500A LBL25 WL156<[01] REMOVED AND REPLACED BAFFLE AT BS 500 TO BS 500A<BR>IAW SRM 51-40-02 & DWG# 143A7505 REV: -<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE
CRACKED BUFFLE AT BS500A TO BS500B LBL25 WL156 CORRECT LOCATION IS BS500B TO BS500C<[01] REMOVED AND REPLACED BAFFLE ASSY P/N 143A7510-11 BETWEEN BS500B AND BS500C; LBL25 IAW SRM 51-40-02 AND DWG 143A7505 REV B.;[02] REJECT - CRACK FOUND @ BRACKET AFT OF FRAME STA 500C WL156 LBL25; LOWER FASTENER;[03] PICTURE ATTACHED FOR CORRECTIVE ACTION ENTRY 2.;[04] REMOVED AND REPLACED BAFFLE ASSY P/N 143A7510-11<BR>BS500B AND BS500C; LBL25 IAW SRM 51-40-02 <BR>AND DWG 143A7505 REV B.;[05] VERIFIED CORRECTIVE ACTION COMPLETE
ELONGATED FASTENER HOLE ON INTERCOSTAL AT BS440 TO BS460; LBL25; WL156<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 440 TO BS 460 LBL 25 WL 156 IAW SRM 51-40-02 AND DGW# 143A7505 REV:-<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE
DURING HFEC INSPECTION OF STUB FRAME FOUND CRACK ABOVE SEAL DEPRESSOR BS 291.5 + 8 WL266 L: 1.7' MARKED.<[01] REJECTED: DURING OK TO INSTALL NEW STUB FRAME; FOUND FASTENER HOLE DAMAGE OUT OF TOLERENCE AND NOT TRUE AND ROUND. LOCATED AT FSD FWD FRAME UPPER FITTING STA 296 APPROX. COMMON TO REPAIR AREA; MARKED;[02] REPAIRED THE DAMAGED FASTENER HOLE AT FSD FWD FRAME UPPER FITTING STA 296 IAW ER: 25-153-00100-WIP1;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] AS PER EA 25-153-00100; THE REPAIR IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.;[05] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CRACKED STRINGER S-11L AT FWD CABIN BS294 WL251.<[01] REMOVED AND REPLACED STRINGER 11L AT FWD CABIN BS294 TO 259.5 1AW B737-7 SRM 51-40-02-0G-01 AND DWG# 141A3120 SHEET 7 REV-B.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727B S-6L IAW SRM 51-40-02 AND DWG#146A1102 ID: 0001 REV:D;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
CRACKED STR CLIP AT PAX CABIN BS767 S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS767 S-6L IAW SRM 51-40-02 AND DWG#143A1010 ID: 0001 REV:C;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
CRACKED STR CLIP AT PAX CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727E S-5L IAW SRM 51-40-02 AND DWG#146A1112 ID: 0001 REV:C;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
SECTION 46 FUSELAGE SKIN HAS A BLEND AT BS 787+4 AND 5' BELOW STR 24R WITHIN 10 INCHES OF AFT CARGO DOOR CUTOUT<[01] REPAIRED PER EA 24-153-03589;[02] VERIFIED CORRECTIVE ACTION COMPLETED.
AFT CARGO; FWD SHIELD CLIP AT BS 767 RBL 26 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED AFT CARGO FWD SHIELD CLIP AT BS767 RBL26 IAW SRM 51-40-02 AND DWG 146A0081 ID:0028 REV:A;[02] VERIFIED CORRECTIVE ACTION
CORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL23 WL156.<[01] REMOVED AND REPLACED SHIELD IAW SRM 51-40-05 & DWG# 143A0080 REV: CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1.
AFT CARGO ENTRY THRESHOLD BS 807 TO 847 RBL26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED ACB THRESHOLD WEB AT BS 794.25 TO BS847 IAW SRM 51-40-02 AND DWG 146A8340 ID:0024 REV: A.; [02] VERIFIED CORRECTIVE ACTION COMPLETE.
AFT CARGO; ZEE SIDE PLATE BS 727 TO 767 RBL 26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 767 RBL 26 IAW SRM 51-40-02 AND DWG 146A7500 ID 85; AND INTERCOSTAL BS 747 TO BS 767 RBL 26 IAW SRM 51-40-02 AND DWG 146A7500 ID 88.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500 - BS500D LBL23 WL156.<[01] REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT; P/N 143A7501U183; BS400 TO BS500D LBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 REV. B.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT; P/N 143A7501U183; BS400 TO BS500D LBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 REV. B.
CORROSION ON FWD SHIELD AT FCB BS420 - BS440 RBL23 WL156. MARKED<[01] REMOVED AND REPLACED SHIELD FCB BS 420 - BS 440. IAW SRM 51-40-02 AND DWG # 143A0080 REV: CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
AFT CARGO; AFT SHIELD BS 847 TO 867 RBL 26 HAS CORROSION. (MARKED)<[01] STEP 4 OK TO APPLY CIC.;[02] OK TO APPLY CIC;[03] REMOVED AND REPLACED ACB AFT SHIELD; P/N 146A8127-10; BS847 TO BS867 RBL26 IAW SRM 51-40-02 AND DWG 146A0081 REV A;[04] REJECTED STEP 2 ITEM 5; INCORRECT INSTALLATION OF FASTENERS.;[05] REMOVED AND REPLACED FASTENERS AS REQUIRED; IAW SRM 51-40-02 AND DWG 146A0081; ACB AFT SHIELD BS847 TO BS867 RBL26;[06] RII VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
AFT CARGO; ZEE SIDEPLATE BS 727 TO 847 LBL 26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT ANGLE BS 727 TO BS 847; LBL 26; IAW SRM 51-40-02-0G-0 AND DWG# 146A7500;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
AFT CARGO; SIDEPLATE INTERCOSTAL BS 767 TO 787 HAS CORROSION (MARKED). RBL 23<[01] REMOVED AND REPLACED NEW AFT CARGO; WEB BS 767 TO BS 787 RBL21 IAW SRM 51-40-02 AND DWG 146A0081 ID:0028 REV:A;[02] VERIFIED CORRECTIVE ACTION 1
AFT CARGO; ZEE SIDEPLATE BS 867 TO 947 RBL 26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT BS887 TO BS947 RBL26 IAW SRM 51-40-02 AND DWG 147A7500 ID:0029 REV: -;[02] VERIFIED CORRECTIVE ACTION COMPLETE
AFT CARGO; CROSS BEAM FRAME AT BS 947.5 RBL 20 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED ACB FRAME BS 947 BETWEEN STR 23L AND STR 23R IAW SRM 51-40-02-0G-0 AND DWG # 147A1047 REV :D;[02] VERIFIED CORRECTIVE ACTION
AFT CARGO; FWD SHIELD BS 767 TO 794 RBL 26 HAS CORROSION. (MARKED)<[01] REMOVED AND REPLACED AFT CARGO FWD SHIELD BS767 TO BS794 RBL26 IAW SRM 51-40-02 AND DWG 146A0081 ID:0028 REV: A;[02] VERIFIED CORRECTIVE ACTION
PANEL BREAK CRACKED BS 540 BL 0 - RBL 25 WL 207<[01]. REMOVED AND REPLACED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 IAW SRM 51-40-2 AND IAW DWG# 143A5240 REV: -;[02] VERIFIED CORRECTIVE ACTION.
AFT FLOOR PANEL 241WF UPPER SURFACE DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241WF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-22 ITEM #185.;[02] VERIFIED JOB COMPLETE
AFT FLOOR PANEL 241ADF LOWER SURFACE DELAMINATED.<[01] LOWER SURFACE DELAMINATION ON AFT FLOOR PANEL 241ADF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1
AFT CABIN FLOOR PANEL 241UF UPPER SURFACE DELAMINATED.<[01] FLOOR PANEL 241UF WITH UPPER SURFACE DAMAGE WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 146A5810 ID:0054;[02] VERIFIED JOB COMPLETE
AFT FLOOR PANEL 241AEF UPPER SURFACE FWD EDGE CRACKED<[01] AFT FLOOR PANEL 241AEF AND UPPER SURFACE FWD EDGE WAS CRACKED AND REPAIRED IAW SRM 53-00-50-2R-1 ALONG WITH 147A5810 SHEET: 351;[02] AFT FLOOR PANEL 241AEF AND UPPER SURFACE FWD EDGE WAS CRACKED AND REPAIRED IAW SRM 53-00-50-2R-1 ALONG WITH DWG: 147A5810 SHEET: 351;[03] VERIFIED JOB COMPLETE
PASSENGER CABIN FLOOR PANEL 241BF UPPER SURFACE DELAMINATED<[01] REPLACED PASSENGER CABIN FLOOR PANEL 241BF WITH SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM #65.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANEL 231XF UPPER SURFACE DELAMINATED<[01] FLOOR PANEL 231XF WITH UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0126;[02] VERIFIED TASK COMPLETE
PASSENGER CABIN FLOOR PANEL 232RF UPPER SURFACE DELAMINATED<[01] 01 - REMOVED AND REPLACED FLOOR PANEL 232RF DUE TO EXCESSIVE DELAMINATION PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE DELAMINATED<[01] FLOOR PANEL 241AF WITH UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0127;[02] VERIFIED JOB COMPLETE
PASSENGER CABIN FLOOR PANEL 241DF UPPER SURFACE DELAMINATED<[01] FLOOR PANEL 241DF WITH UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0128;[02] VERIFIED JOB COMPLETE
PASSENGER CABIN FLOOR PANEL 241EF UPPER SURFACE DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241EF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM #105.;[02] VERIFIED JOB COMPLETE
PASSENGER CABIN FLOOR PANEL 241FF UPPER SURFACE DELAMINATED<[01] REPLACED PASSENGER CABIN FLOOR PANEL 241FF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABN FLOOR PANEL 242AF UPPER SURFACE DELAMINATED.<[01] REPLACED PASSENGER CABIN FLOOR PANEL 242AF WITH SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANE 242DF UPPER SURFACE DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242DF WAS REPLACED WITH A NEW PANEL DUE TO EXCESSIVE UPPER SURFACE DELAMINATED PLIES IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM 135.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABN FLOOR PANEL 242BF UPPER SURFACE DELAMINATED.<[01] PASSENGER CABIN FLOOR PANEL 242BF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM #85.;[02] VERIFIED JOB COMPLETE
PASSENGER CABIN FLOOR PANEL 231FF UPPER SURFACE DELAMINATED<[01] 04 - REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.
CORROSION DAMAGE ON THE STRAP FLOOR STRUCTURE AFT WET AREA AT STA 1016+3.5 RBL 2.75 (MARKED)<[01]. THE CORROSION DAMAGE ON THE AFT WET AREA TENSION STRAP BS 1016+3.5 RBL 2.75 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS PART AND IT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9 ITEM C. REMOVED AND REPLACED THE TENSION STRAP IAW SRM 51-40-02 AND DWG# 147A5730 REV C;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
CORROSION DAMAGE ON THE WEB FLOOR STRUCTURE AFT WET AREA AT STA 1016+14.5 RBL 1.5 (MARKED)<[01] AREA OF CORROSION DAMAGE ON THE WEB FLOOR STRUCTURE AFT WET AREA AT STA 1016+14.5 RBL 1.5 REWORKED; TREATED; AND RESTORED IAW EA 24-153-03525.;[02] VERIFIED CORRECTIVE ACTION COMPLETE
INBOARD FLANGE OF THE STA 312 FRAME HAS A CRACK IN THE RADIUS LOCATED DIRECTLY ABOVE THE L/H ENTRY DOOR AT WL 282.<[01] REPAIRED INBOARD FLANGE OF THE STA 312 FRAME ABOVE THE L/H ENTRY DOOR AT WL 282 IAW EA# M-22-153-01244.;[02] VERIFIED CORRECTIVE ACTION COMPLETE;[03] NDT LABOR ROW NOT NEEDED; FINISHED LABOR ROW.
RH PANEL 192BR PANEL DELAMINATED WITH HOLE<[01] C/W EA 24-153-01186
CREW REPORTS #1 ENGINE ACCOUSTICLE PANELPEELED UP AROUND 3 OR 4 OCLOCK POSITION<[01] REMOVED AND REPLACED #1 ENG AFT ACOUSTICAL PANEL 7-9 O?CLOCK POSITION PER AMM 72-23-02 REMOVED AND REPLACED #1 ENG 8 O?CLOCK POSITION STRUT PROFILE PER AMM 72-23-02
CABIN O/H BIN BULLNOSE EMERGENCY LIGHT ASSY LOOSE AT 12ABC<[01] SECURED CABIN O/H BIN BULLNOSE EMERGENCY LIGHT LENS ASSY AT 12ABC PER AMM 33-51-03.
CABIN - EMERGENCY LIGHT BULB OUT AT ROW 22<[01] REMOVED AND REPLACED EMERGENCY AISLE LIGHT BULB AT ROW 22 PER AMM 33-51-03
CABIN - TWO EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK<[01] REMOVED AND REPLACED FWD LH AND AFT RH BATTERY PACKS. OPS CHECK GOOD. REF: AMM 33-51-06;[02] REMOVED AND REPLACED FWD LH AND AFT RH BATTERY PACKS. OPS CHECK GOOD. REF: AMM 33-51-06
RH HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31
OUT OF POSITION PHOTOLUMINESCENT STRIP ON ROW 11C AT PASSENGER CABIN 2023-83862<[01] INSTALLED CORRECTLY PHOTOLUMINESCENT STRIP ON ROW 11C AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802.;[02] INSTALLED CORRECTLY PHOTOLUMINESCENT STRIP ON ROW 11C AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802.
ELONGATED HOLE VAPOR VARRIER SUPPORT ANGLE 4(E/A) AT MAIN WHEEL WELL COMPARTME 2023-83835<[01] DRILLED OVERSIZE HOLES VAPOR VARRIER SUPPORT ANGLE 4(E/A) AT MAIN WHEEL WELL COMPARTME INITIAL DIAMETER HOLE 0.175' AND FINAL DIAMETER HOLES 0.187' IAW B737-700 SRM 51-40-05 TOOL USED P/N: 8647A42; S/N: B22058354; DUE DATE: 27-AUG-23;[02] CORRECTED STEP 1<BR>DRILLED OVERSIZE HOLES VAPOR VARRIER SUPPORT ANGLE 4(E/A) AT MAIN WHEEL WELL COMPARTME INITIAL DIAMETER HOLE 0.175' AND FINAL DIAMETER HOLES 0.187' IAW B737-700 SRM 51-40-05 TOOL USED CALIPER P/N: 8647A42; S/N: B22058354; DUE DATE: 27-AUG-23;[03] TASK CARD COMPLETED <BR>DRILLED OVERSIZE HOLES VAPOR VARRIER SUPPORT ANGLE 4(E/A) AT MAIN WHEEL WELL COMPARTME INITIAL DIAMETER HOLE 0.175' AND FINAL DIAMETER HOLES 0.187' IAW B737-700 SRM 51-40-05 TOOL USED CALIPER P/N: 8647A42; S/N: B22058354; DUE DATE: 27-AUG-23
ELONGATED HOLE VAPOR VARRIER PLATES(4EA) LT SIDE AT MAIN WHEEL WELL COMPARTME 2023-83827<[01] DRILLED OVERSIZE 12 HOLES ON 4(E/A) REINFORCEMENT PLATES OF VAPOR BARRIER LH SIDE OF MAIN WHEEL WELL IAW B737-700 SRM 51-40-05.SEE INDIVIDUAL STEP SIGNOFF BELLOW;[02] TASK CARD COMPLETED <BR>DRILLED OVERSIZE 12 HOLES ON 4(E/A) REINFORCEMENT PLATES OF VAPOR BARRIER LH SIDE OF MAIN WHEEL WELL IAW B737-700 SRM 51-40-05.SEE INDIVIDUAL STEP SIGNOFF BELLOW
CORROSION ON ACCESS PANEL 193B SUPPORT STRUCTURE AT BODY FAIRING 2023-83805<[01] TOOLS USED: POWER PACK P/N: PE1068; S/N: PE0118-94826; DUE DATE: 16-MAY-23; MULTIMETER P/N: FLUKE 87; S/N: 42180184; DUE DATE: 21-FEB-23; THERMOMETER P/N: 2278-20; S/N:AE-410983 ; DUE DATE: 06-JAN-24.;[02] REPLACED SUPPORT STRUCTURE ( FRAME ) LOC ON ACCESS PANEL 193B AT BODY FAIRING IAW B737-700 SRM 51-10-02. THE REMOVAL AND REINSTALLATION IS DOCUMENTED ON FAULT TTG8Q00HDB27. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED SUPPORT STRUCTURE ( FRAME ) LOC ON ACCESS PANEL 193B AT BODY FAIRING IAW B737-700 SRM 51-10-02. THE REMOVAL AND REINSTALLATION IS DOCUMENTED ON FAULT TTG8Q00HDB27. SEE INDIVIDUAL SIGNOFFS BELOW... RII ITEM
CORROSION STRAP LOCATED BS 727D PLUS 5 INCH BETWEEN RBL 21 AND LBL 21 WL156 AT AFT CARGO COMPARTMENT 2023-83791<[01] REPLACED STRAP LOCATED BS 727D PLUS 5 INCH BETWEEN RBL 21 AND LBL 21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A9401 SHEET 1; REV C:. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED STEP 1; COMPLETED<BR>ITEM RII
CORROSION STRAP LOCATED AT BS 767 PLUS 5 INCH BETWEEN S-25R AND S-25L WL 156 AT AFT CARGO COMPARTMENT 2023-83781<[01] REPLACED STRAP LOCATED AT BS 767 PLUS 5 INCH BETWEEN S-25R AND S-25L WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A9401 SHEET 1; REV C: . SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED STRAP LOCATED AT BS 767 PLUS 5 INCH BETWEEN S-25R AND S-25L WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A9401 SHEET 2; REV C: . SEE INDIVIDUAL SIGNOFFS BELOW;[03] CERTIFIED STEP 2 COMPLETED<BR>ITEM RII
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 AND BS 787 S-25R RBL 21 WL 156 AT AFT CARGO COMPARTMENT 2023-83789<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 767 AND BS 787 S-25R RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A0081 SHEET 31 REV- ?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] CORRECTED STEP 1<BR>REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 767 AND BS 794.25 S-25R RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A0081 SHEET 31 REV- ?SEE INDIVIDUAL SIGN OFF BELOW?.;[03] CERTIFIED STEP 2 COMPLETED<BR>ITEM RII
CORROSION SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R RBL 21 WL 156 AT AFT CARGO COMPARTMENT 2023-83788<[01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 221861811; DUE DATE: 08-NOV-23.;[02] REPLACED SUPPORT ZEE LOCATED RBL 21 BETWEEN BS727+4 TO BS 767 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ;DWG 146A7500 SHEET: 85; REV: A. SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTIVE ACTION CERTIFIED RII
CRACK TRACK LBL 17.24 AT BS 767 WL 156 AFT CARGO COMPARTMENT 2023-83757<[01] TOOL USED PN NORTEC 600D; SN 200048001; DUE DATE 30-MAR-23;[02] TOOL USED CALIPER P/N: 500-193-30 S/N: 0000291 DUE DATE: 12-OCT-23.;[03] PERFORMED REPAIR TRACK EXTRUSION;SPLICES (CHANNEL) (2EA) AND FASTENERS LOCATED ON LBL 17.24 BTW BS 747+10.5 INCH AND BS 767+9 INCH AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 STEP 4; O TO P (1) (D) <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[04] CORRECTED STEP 3<BR>PERFORMED REPAIR LOCATED ON LBL 17.24 BTW BS 747+10.5 INCH AND BS 767+9 INCH AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGNOFFS BELOW;[05] CORRECTED STEP 3 <BR>PERFORMED REPAIR LOCATED ON LBL 17.24 BTW BS 747+10.5 INCH AND BS 767+9 INCH AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGNOFFS BELOW
CRACK TRACK RBL 13.84 BS 727E WL 156 AFT CARGO COMPARTMENT 2023-83756<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 200048001; DUE DATE 30-MAR-23;[02] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBL 13.84 BETWEEN BS 727D+ 11? AND BS 767+9? WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK CARD COMPLETED <BR>PERFORMED PERMANENT REPAIR ON CARGO TRACK RBL 13.84 BETWEEN BS 727D+ 11? AND BS 767+9? WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII
CRACK ANGLE - SUPPORT LOCATED AT BS 907 PLUS 11 INCH BETWEEN S-25R AND S-26R AFT CARGO COMPARTMENT 2023-83771<[01] REPLACED ANGLE-SUPPORT AND FASTENER; LOCATED AT BS 907 PLUS 11 INCH BETWEEN S-25R AND S-26R AFT CARGO COMPARTMENT; IAW B737-700 SRM 51-40-02 AND DWG 147A7221 SHEET 8; REV C: . SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED ANGLE-SUPPORT AND FASTENER; LOCATED AT BS 907 PLUS 11 INCH BETWEEN S-25R AND S-26R AFT CARGO COMPARTMENT; IAW B737-700 SRM 51-40-02 AND DWG 147A7221 SHEET 8; REV C: . SEE INDIVIDUAL SIGNOFFS BELOW
CRACK ANGLE - SUPPORT LOCATED AT BS 907 PLUS 6 INCH BETWEEN S-25R AND S-26R AFT CARGO COMPARTMENT 2023-83770<[01] REPLACED ANGLE-SUPPORT AND FASTENER; LOCATED AT BS 907 PLUS 6 INCH BETWEEN S-25R AND S-26R AFT CARGO COMPARTMENT; IAW B737-700 SRM 51-40-02 AND DWG 147A7221 SHEET 8; REV C: . SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED ANGLE-SUPPORT AND FASTENER; LOCATED AT BS 907 PLUS 6 INCH BETWEEN S-25R AND S-26R AFT CARGO COMPARTMENT; IAW B737-700 SRM 51-40-02 AND DWG 147A7221 SHEET 8; REV C: . SEE INDIVIDUAL SIGNOFFS BELOW
CRACK TRACK RBL 13.84 LOCATED AT BS 767 WL 156 AFT CARGO COMPARTMENT 2023-83755<[01] REPAIR DOCUMENTED ON TTG8Q00HHRKZ.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPAIR DOCUMENTED ON TTG8Q00HHRKZ. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.5 INCHES 2023-83746<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210136503; DUE DATE: 11-APR-23;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 11-APR-23;[03] INSPECTION REJECT IN STEP 9 SEE TTG8Q00HQ1LC;[04] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL LOWER INSPAR SKIN STATION 193.90 RIB 17.500 INCH FROM FRONT SPAR INBD SIDE OF RIB. IAW BOEING 737-700 SRM 51-40-02 AND B737-700 SRM 55-10-01-2R-11 REPAIR 11 TABLE 202 FIGURE 204; DETAIL B; SEE INDIVIDUAL SIGN OFF BELOW.;[05] CERTIFIED STEP 4; COMPLETED<BR>ITEM RII
INOP BATTERY PACK ON BS 727C STR 17 L AT PASSENGER CABIN 2023-83745<[01] REPLACED BATTERY PACK ON BS 727C STR 17 L AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-06-960-805 AND PERFORMED OPERATIONAL TEST OF THE NEW BATTERY PACK; TEST IS OK.;[02] CORRECTIVE ACTION CERTIFIED
CORROSION ON PLATE LOCATED BS 847 RBL 21.80 AND WL 156 AT AFT CARGO COMPARTMENT 2023-83748<[01] REPLACED PLATE LOCATED BS 847 RBL 21.80 AND WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] REPLACED PLATE LOCATED BS 847 RBL 21.80 AND WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.
CRACK ANGLE LOCATED AT BS 500A S-26L WL 156 FWD FACE FRAME FWD CARGO COMPARTMENT 2023-83713<[01] REPLACED ANGLE LOCATED AT BS 500A S-26L WL 156 FWD FACE FRAME FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505; SHEET 81; REV: -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE LOCATED AT BS 500A S-26L WL 156 FWD FACE FRAME FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505; SHEET 81; REV: -. SEE INDIVIDUAL SIGN OFFS BELOW... RII ITEM
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 492 AND BS 500A AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT 2023-83711<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 492 AND BS 500A AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 23; REV-. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 492 AND BS 500A AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 23; REV-. SEE INDIVIDUAL SIGNOFFS BELOW. AS RII
CORROSION SUPPORT ZEE LOCATED BETWEEN BS 500A AND BS 500D. AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT 2023-83712<[01] REPLACED SUPPORT ZEE AND FASTENER; LOCATED BETWEEN BS 500A AND BS 500D. AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7500 SHEET 59; REV -. SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK GUSSET LOCATED AT BS 500D S-19R WL 200 FWD CARGO COMPARTMENT 2023-83717<[01] REPLACED GUSSET LOCATED AT BS 500D S-19R WL 200 FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 AND DWG 143A7902 SHEET 209; REV-. ?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
ELONGATED HOLE ACCESS PANEL 343CB AT RT HORIZONTAL STABILIZER 2023-83715<[01] TOOL USED CALIPER PN: 500-97-30; SN: B20189362; DUE DATE: 27/DEC/23.;[02] TOOL USED; HOT BONDER PN: HCS9200B-AV; SN: 18185847; DUE DATE: 24/SEP/23;[03] TOOL USED; SCALE PN: 1863T62; SN: AE-40571; DUE DATE: 09/JUN/23.;[04] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE DATE: 20-JUL-23.;[05] TOOL USED: MULTIMETER P/N: FLUKE 87 S/N: 37640204 DUE DATE: 14-DEC-23.;[06] REPAIRED ACCESS PANEL 343CB AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED.
CRACK GUSSET LOCATED AT BS 500D S-19L WL 200 FWD CARGO COMPARTMENT 2023-83716<[01] REPLACED GUSSET AND FASTENERS LOC LOCATED AT BS 500D S-19L WL 200 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED GUSSET AND FASTENERS LOC LOCATED AT BS 500D S-19L WL 200 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -. SEE INDIVIDUAL SIGNOFFS BELOW
CRACK WEB - INTERCOSTAL LOCATED BS344 PLUS 9INCH BL0 AND WL208 AT FWD GALLEY AREA 2023-83689<[01] REPLACED WEB INTERCOSTAL LOC. BTW BS344 TO BS360 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 32; REV -<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED WEB INTERCOSTAL LOC. BTW BS344 TO BS360 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 32; REV - ITEM RII <BR>SEE INDIVIDUAL SIGNOFF BELOW
CORROSION ON STRAP LOCATED BS1016 PLUS 7INCH LBL3 AND WL 208 AT AFT GALLEY AREA 2023-83685<[01] REPLACED STRAP LOCATED BS1016 PLUS 7INCH LBL3 AND WL 208 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 AND DWG 147A5600 SHEET 32 REV B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED STRAP LOCATED BS1016 PLUS 7INCH LBL3 AND WL 208 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 AND DWG 147A5600 SHEET 32 REV B. SEE INDIVIDUAL SIGN OFF BELOW. RII
CRACK FLOOR BEAM LOCATED BS967 RBL49 AND WL208 AT AFT GALLEY AREA 2023-83684<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: DIGITAL CALIPER: P/N: 500-197-30; S/N: 15121570; DUE DATE: 05-NOV-23.;[04] REPAIRED FLOOR BEAM LOCATED BS967 BTW RBL 30.00 AND RBL 50.00 AND AT WL 208.1 IAW EA 23-153-00374 REV. 1; EA 23-153-00374-WIP1 REV. 1 AND EA 23-153-00374-WIP2 REV. 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] CERTIFIED STEP 4; COMPLETED<BR>ITEM RII
CRACK WEB - INTERCOSTAL LOCATED BS344 PLUS 9INCH RBL12 AND WL208 AT FWD GALLEY AREA 2023-83691<[01] REPLACED WEB - INTERCOSTAL LOCATED BS344 PLUS 9 INCH RBL12 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 13 REV- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BS344 PLUS 9 INCH RBL12 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 13 REV- <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW
CRACK STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-83688<[01] UT TOOL USED PN: 45MG ; SN: 221859911. DUE DATE: 07-NOV-23;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 500D; S/N N500X11290U021704 DUE DATE: 01-FEB-23;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23;[04] PERFORMED REPAIR LOCATED ON STRINGER 23R BTW BS 500D TO BS 540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW;[05] PERFORMED REPAIR LOCATED ON STRINGER 23R BTW BS 500D TO BS 540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW RII
CRACK WEB LOCATED BS277 PLUS 7INCH BL0 AND WL208 AT FWD GALLEY AREA 2023-83693<[01] REPLACED WEB LOCATED BTW BS277 TO BS 294; BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CORROSION SUPPORT BRACKET LOCATED BS312 LBL54 AND WL208 AT FWD GALLEY AREA 2023-83692<[01] REPLACED SUPPORT BRACKET LOCATED BS312 LBL54 AND<BR>WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02<BR>AND 51-10-02. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT BRACKET LOCATED BS312 LBL54 AND <BR>WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 <BR>AND 51-10-02. SEE INDIVIDUAL SIGN OFF BELOW.RII CERTIFIED
CRACK LEADING EDGE RIB LOCATED AT LE STA 95.96 RT HORIZONTAL STAB 2023-83670<[01] REPLACED RIB LEADING EDGE LOCATED AT LE STA 95.96 RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 186A1001 SHEET 19 REV- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED STEP 1; COMPLETED
CORROSION PLATE LOCATED BS792 RBL21.80 AND WL156 AT AFT CARGO COMPARTMENT 2023-83622<[01] REPLACED PLATE LOCATED BS792 RBL21.80 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] REPLACED PLATE LOCATED BS792 RBL21.80 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.
DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (4 EA) 2023-83618<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (4 EA) IAW AMM 33-51-15-400-802;[02] CERTIFIED WORK PERFORMED.
CRACK CENTER SCUFF PLATE LOCATED AT LEVEL WL 156.4 FWD CARGO COMPARTMENT 2023-83631<[01] TOOL USED DIGITAL CALIPER P/N:700-113-10;S/N:0019306;DUE DATE:21/NOV/23;[02] REPAIRED THE CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.C. STEP 2 AND STEPS 4 TO 7. AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELLOW;[03] TASK COMPLETED
MISSING STUD HANDLE DOOR AT AFT CARGO COMPARTMENT 2023-83592<[01] INSTALLED STUD HANDLE DOOR AT AFT CARGO COMPARTMENT IAW AMM 52-31-14-400-801;[02] COMPLETED
CRACK SUPPORT ANGLE LOCATED AT BS 695 RBL 24.5 WL 208.1 CENTER SECTION 2023-83568<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED SUPPORT ANGLE LOCATED AT BS 695 RBL 24.5 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-10-02 DWG 111A6000 REV. - AND DWG 273A9110 REV. A<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.5 WL208.1 CENTER SECTION 2023-83569<[01] REPLACED STIFFENER FLOOR STRUCTURE AND FASTENERS BS540 BETWEEN BL0 TO LBL24.5 IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 SHEET 43 REV ?.SEE INDIVIDUAL STEP SIGN BELOW;[02] REPLACED STIFFENER FLOOR STRUCTURE AND FASTENERS BS540 BETWEEN BL0 TO LBL24.5 IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 SHEET 43 REV ?.SEE INDIVIDUAL STEP SIGN BELOW<BR>STEP 4 AND STEP 5 COMPLETED
CRACK VAPOR BARRIER LBL 51 BS 663 AT MAIN WHEEL WELL COMPARTME (CUSTOMER REQUEST ) 2023-83463<[01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17 OCT 23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-409559 DUE DATE: 06 JUN 23.;[04] TOOL USED SCALE P/N 91847 S/N AE-409322 DUE DATE 06 JUN 23;[05] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 16122983 DUE DATE 24 JAN 24;[06] REPAIRED VAPOR BARRIER LBL 51 BS 663 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED. RII COMPLETED.
CRACK VAPOR BARRIER RBL 41 BS 663 AT MAIN WHEEL WELL COMPARTME (CUSTOMER REQUEST ) 2023-83464<[01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17 OCT 23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 22-JAN-24;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-409559 DUE DATE: 06 JUN 23.;[04] TOOL USED SCALE P/N 1863T62 S/N AE-40571 DUE DATE 09 JUN 23;[05] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 23 JAN 24.;[06] REPAIRED VAPOR BARRIER RBL 41 BS 663 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED. RII COMPLETED.
PERFORATION FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2023-83427<[01] REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT AIW B737-700 AMM 25-52-01-201-801;[02] CERTIFIED WORK PERFORMED.
CENTER AISLE; LH OVERWING EXIT SIGNS INOP. / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON LH SIDE; FWD OF OVERWING EXIT DOOR IN REFERENCE WITH AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
CABIN EMERGENCY EXIT ROW TRAY TABLE SAFETY LATCH IS BROKEN AT SEAT 11C / [01] REMOVED AND REPLACED CABIN EMERGENCY EXIT ROW TRAY TABLE SAFETY LATCH AT SEAT 11C PER CMM 25-21-42
CABIN SIDE WALL LIGHT AT LEFT OVER WING EMERGENCY EXIT INOP. REMOVED AND REPLACED LIGHT BALLAST AT CABIN SIDE WALL LIGHT LEFT OVER WING EMERGENCY EXIT PER AMM 33-21-00
FWD ENTRY DOOR EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED COVER IAW AMM 33-51-01;[02] INSPECTED
FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW AND NOT BILINGUAL / [01] REMOVED AND REPLACED COVER IAW AMM 33-51-01;[02] INSPECTED
EMERGENCY LIGHT ON RIGHT SIDE ROWS 2 AND 3 INOP / [01] R+R FWD RIGHT ON CEILING BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.
RIGHT OVERWING EXIT WINDOW LIGHT INOP. / [01] RELAMPED RIGHT OVER WING EXIT WINDOW LIGHT REFF AMM 33-51-04 <BR>LOG PAGE 1723544
AFT L/H EMERGENCY LIGHT INOP / RELAMPED L/H AFT EMERGENCY LIGHT PER AMM 33-51-21
EMERGENCY BATTERY PACK DEFECTIVE AT POSITION M1670. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1670. PERFORMED INSTALLATION TEST NORMAL, AS PER REF B737 AMM 35-51-06-960-805.
LEFT WING AFT SPAR LOWER CAP BRACKET CRACKED AT PANEL 551DB OUTER EDGE SUPPORT BEAM FWD ATTACHMENT / REMOVED AND REPLACED LEFT WING AFT SPAR LOWER CAP BRACKET AT PANEL 551DB OUTER EDGE SUPPORT BEAM FWD ATTACHMENT REF B-737-700 SRM 51-40-02-0G-0
LEFT MAIN WHEEL WELL VAPOR BARRIER ANGLE CRACKED AT STA 663; WL 158; LBL 7'. / REPLACEMENT OF NEW ANGLE AT LEFT MAIN WHEEL WELL VAPOR BARRIER AT STA 663; WL 158 LBL 7' WILL BE ACCOMPLISHED ON NRC W198726
2 EACH DENTS LOCATED AT STA 188 AND STA 211 S-24L, REFERENCE DEFECTS: 0211796 AND 0211797. ACCOMPLISHED CATEGORY 'B' REPAIR, IAW B737 SRM 53-10-01-2R-8 REPAIR 8 AT STA 188 AND 211, S-24L.
RIGHT WING REAR SPAR FIXED T/E DEFLECTION CONTROL PANEL WEB VERTICAL SEAL RETAINER CRACKED INB MKD DOT 60-011 / REMOVED AND REPLACED FITTING AT R/WING REAR SPAR FIXED T/E DEFLECTION CONTROL PANEL WEB PER REF SRM 51-40-02-0G-0
FWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED / RECEIVED NEW SCUFF PLATE FOR AFT CORNER OF FWD CARGO COMPARTMENT; INSTALLATION WILL BE ACCOMPLISHED ON CARD J753-646-63-01.
HORIZONTAL STAB INSPAR NR 5 AT STAB STA 129.50 STIFFENER NR 3 LOWER SECTION CRACKED. ACCOMPLISHED REPAIR FOR HORIZONTAL STAB RIB NR 5 AT STIFFENER NR 3 LOWER SECTION AS PER REF B737-7 SRM 55-10-09-2R-4. PERFORMED NDT AFTER REWORK; NO FURTHER CRACKS NOTED IAW B737 NDT PART 6 51-00-00 PROC 23. TREATED AND PRIMED AREA OF REPAIR AS PER B737-7 AMM 51-00-58-201 AND 51-21-72-370-803.
FWD SVC DOOR UPPER HANDLE BROKEN / REPLACED UPPER/LOWER SVC DOOR ASST. HANDLE ATTACH BRACKET PER AMM 52-41-00
AFT LEFT PASSENGER DOOR EXTERNAL SLIDE, OVERWING LIGHT INOPERATIVE. RELAMPED LIGHT PER AMM.
RIGHT FWD UPPER WING TO BODY FAIRING 191AR AFT MIDDLE SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED RIGHT FWD UPPER WING TO BODY FAIRING 191AR AFT MIDDLE SUPPORT BRACKET PER SRM 51-40-02.
R2 DOOR ESCAPE SLIDE FELL OUT OF IT'S CONTAINER SLIDE DID NOT DEPLOY, STILL OPERATIONAL. R&R SLIDE IAW MT.
L/H HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED / R AND R NEW L/H UPPER SLIDER SEAL PER SRM 51-40-02.
AFT CARGO R/H SIDE FWD CAP STRIP IS CORRODED. / REMOVED AND REPLACED AFT CARGO R/H SIDE FWD CAP STRIP PER AMM 25-52-10.
AFT CARGO R/H SIDE SECOND CAP STRIP IS CORRODED. / REMOVED AND REPLACED AFT CARGO R/H SIDE SECOND CAP STRIP PER AMM 25-52-10.
AFT CARGO L/H SIDE AFT CAP STRIP IS CORRODED. / REMOVED AND REPLACED AFT CARGO L/H SIDE AFT CAP STRIP PER AMM 25-52-10.
AFT CARGO L/H SIDE MIDDLE CAP STRIP IS CORRODED. / REMOVED AND REPLACED AFT CARGO L/H SIDE MIDDLE CAP STRIP DUE TO CORROSION WITH NEW SERVICEABLE CAP-STRIP IAW SRM 51-10-02/ TASK 25-52-10-400-801
:AFT CARGO L/H SIDE FWD CAP STRIP IS CORRODED. / REMOVED; AND REPLACED CAP STRIP. REF. AMM. 25-52-10.
RT EMERGENCY LIGHT BATTERY PACK DAMAGED AT BASE M1674 AT BS 322. R&R BATTERY PACK PER AMM.
LT EMERGENCY LIGHT BATTERY PACK DAMAGED AT BASE M1675 AT BS 322. R&R BATTERY PACK PER AMM.
RT HORIZONTAL STABILIZER RIB AT STA 120.30 FASTENER HOLE 8 LOWER FLANGE CRACKED ON RIB ONLY. REPAIRED RIB PER EA.
RT HORIZONTAL STABILIZER RIB AT STA. 120.30 FASTENER HOLE NR 1 (HOLE DIAMETER .232) LOWER FLANGE DAMAGED AND ELONGATED ON RIB ONLY. REPAIRED LOWER FLANGE HOLE PER EA.
RT HORIZONTAL STABILIZER RIB AT STA 120.30 FASTENER HOLE 27 LOWER FLANGE CRACKED ON RIB ONLY. REPAIRED RIB PER EA.
RT HORIZONTAL STABILIZER RIB AT STA 120.30 FASTENER HOLE 35 LOWER FLANGE CRACKED ON RIB ONLY. REPAIRED RIB PER EA.
RT HORIZONTAL STABILIZER STAB STA 120.3 LOWER T-FLANGE CRACKED AT RIB 4. REPAIRED RIB IAW SRM AND EA.
RT HORIZONTAL STABILIZER STA 120.3 RIB NR 4 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.
RT HORIZONTAL STABILIZER STA 120.3 LOWER T-FLANGE CRACKED AT RIB 3. REPAIRED RIB PER SRM.
RT HORIZONTAL STABILIZER STA 120.3 RIB NR 2 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.
RT HORIZONTAL STABILIZER STA 120.3 RIB NR 3 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.
R/H STIFFENER TEE BULB IN APU TORQUE BOX HAS CORROSION AT STA 1125 AROUND AFT LOWER PLENUM ASSY BOLT HOLE. / REMOVED CORROSION FROM STIFFENER FOUND TO BE OUT OF LIMITS PER SRM 53-80-13-1A-2. REMOVED AND REPLACED RIGHT STIFFENER; PART NUMBER: 148A8640-14 PER SRM 51-40-02. ATA CODE IS CORRECT AS 53-98 FOR CORRODED PART. REFERENCE CARD FOR WORK ACCOMPLISHED AND INDIVIDUAL SIGN OFFS.
FOUND ELONGATED HOLE IN TOP OF FRAME AT STA. 907 RBL 8 IN AFT CARGO COMPARTMENT. / REPAIRED PER EA # 1-753-34194.
AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED. R&R WEB PER SRM.
AT THE WATER SERVICE DOOR 146AR; THE FUSELAGE SKIN HAS CORROSION IN THE AREA OF THE LATCHES / ACCOMPLISHED EA NO: 1-753-34207
LEFT HORIZONTAL STABILIZER REAR SPAR LOWER ATTACH LUG HAS CORROSION ON AFT SIDE ADJACENT TO BUSHING FLANGE. / REPAIRED AS PER EA# 1-755-4321.
RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER LUG HAS CORROSION ON AFT SIDE ADJACENT TO BUSHING FLANGE. / REPAIRD PER EA. 1-755-4322
AFT CARGO FLOOR SUPPORT STRAP CORRODED AT BS 727D+4, AROUND NUTPLATE HOLES. R&R STRAP PER SRM.
FORWARD CARGO COMPARTMENT LT TRANS ANGLE SUPPORT INTERCOSTAL AFT BRACKET CRACKED AT BS 500C. R&R BRACKET PER SRM.
R/H CUSP WEB FROM STA 887 TO STA 907 HAS ELONGATED HOLE. / REMOVED; AND REPLACED WEB. REF. SRM. 51-40-02
#1 SEAT TRACK HAS CORROSION IN THE TRACK AT STA.727.(MARKED) / REMOVED AND REPLACED #1 SEAT TRACK (PART # 144A5350-3) AT STA. 540 TO 727 PER SRM 51-40-02
R1 DOOR NR 4 BEAM CRACKED .75" ADJACENT TO INBOARD TORQUE BOX MOUNT BOLT. R&R DOOR PER SRM.
R1 DOOR NR 5 BEAM CRACKED .50" ADJACENT TO INBOARD TORQUE BOX MOUNT BOLT. R&R DOOR PER SRM.
BS 270 LATERAL INTERCOSTAL UPPER CHORD AFT FLANGE AT LBL 8 HAS ELONGATED FASTENER HOLE. / MARKED AS MAJOR REPAIR AND RII. REPAIRED PER EA 1-753-34089. SEE EA FOR INDIVIDUAL SIGN OFFS.
BS 270 LATERAL INTERCOSTAL UPPER CHORD AFT FLANGE AT RBL 8 HAS ELONGATED FASTENER HOLE. / MARKED AS MAJOR REPAIR AND RII. REPAIRED PER EA 1-753-34089. SEE EA FOR INDIVIDUAL SIGN OFFS.
BS 270 LATERAL INTERCOSTAL UPPER CHORD AFT FLANGE AT BL 0 HAS ELONGATED FASTENER HOLE. / MARKED AS MAJOR REPAIR AND RII. REPAIRED PER EA 1-753-34089. SEE EA FOR INDIVIDUAL SIGN OFFS.
INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, RBL 0. R&R INTERCOSTAL PER SRM.
AFT CARGO DOOR SKIN UNDER CENTER THRESHOLD CORRODED. REPAIRED THRESHOLD PER EA.
CABIN FLOOR PANEL 221BF AFT OB CORNER BROKEN / NEW FLOORBOARD INSTALLED ON TASK CARD: JPANEL-221-CLOSE
FORWARD CARGO THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 492. R&R WEB PER SRM.
INTERCOSTAL CRACKED AT BS 540, BETWEEN RBL 24.5 TO RBL 45.5. R&R INTERCOSTAL PER SRM.
INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 0. R&R INTERCOSTAL PER SRM.
AFT CARGO DOOR STRUCTURE WEB UNDER THRESHOLD CORRODED ON UPPER SURFACE BETWEEN BS 847 TO BS 867. R&R WEB PER SRM.
AFT CARGO FLOOR STRUCTURE SUPPORT RAIL CORRODED AROUND FASTENER HOLES AT BS 945, RBL 8. R&R SUPPORT RAIL PER SRM AND DWG.
AFT CARGO FLOOR STRUCTURE STRAP CORRODED 7" AFT OF BS 767 TO 6" FORWARD OF BS 867, RBL 19. R&R STRAP PER SRM.
AFT CARGO FLOOR STRUCTURE RIGHT TRANSITION ANGLE STA 847 TO STA 867 HAS VARIOUS SIGNS OF CORROSION. (MARKED) / REMOVED AND REPLACED TRANSITION ANGLE FROM STA 847 TO STA 867 (MPN 146A8127Y10) I.A.W SRM 51-40-02. ALT P/N 146A8127-10. SHIELD IDENTIFICATION ALSO DETERMINED TO BE 0.050' 7075-76 PER SRM 53-60-15-0I-1 TABLE 4 ITEM 7.
AFT CARGO FLOOR PANEL ATTACH STRIP AT STA 767 +4' HAS CORROSION / REPLACED STRAP PER SRM 51-40-02 PART NUMBER 146A9401-16 SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS.
AFT CARGO FLOOR STRUCTURE RIGHT TRANSITION ANGLE 7' FWD OF STA 927 HAS SIGNS OF CORROSION. (MARKED) / REMOVED AND REPLACED TRANSITION ANGLE (PART NUMBER 453A2611-3) DUE TO CORROSION FROM STA 727 TO 767 IAW SRM 53-00-51-2R-1
AFT CARGO LEFT TRANSITION ANGLE HAS CORROSION FROM STA 727D TO 847 / REMOVED LEFT SIDE TRANSITION ANGLE (PART NUMBER 146A7502-27) DUE TO CORROSION FROM STA 727 TO 847 AND INSTALLED NEW TRANSITION ANGLE IAW SRM 53-00-51-2R1. SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS.
AFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION FROM STA 727D - 847 / REMOVED AND INSTALLED NEW TRANSITION ANGLE (PART NUMBER 147A7502-51 FROM STA 727 TO 847 IAW SRM 53-00-51-2R-1. SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS.
AFT CARGO FLOOR STRUCTURE SUPPORT RAIL CORRODED AROUND FASTENER HOLE 2.5" FORWARD OF BS 294.5, RBL 3. R&R ANGLE PER SRM & DWG.
AFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION AT STA 727B + 14' / REMOVED AND REPLACED TRANSITION ANGLE (PART #453A2611-9) DUE TO CORROSION FROM STA 727 TO 767 IAW SRM 53-00-51-2R-1
FORWARD CARGO CORNER GUSSET BRACKET CRACKED AT BS 500D, STR 18L. R&R BRACKET PER SRM.
FORWARD CARGO CORNER GUSSET BRACKET CRACKED AT BS 500D, STR 18R. R&R GUSSET PRE SRM.
INTERCOSTAL CRACKED AT BS 540, BETWEEN RBL 24.5 TO CENTER. R&R INTERCOSTAL PER SRM.
INTERCOSTAL CRACKED AT BS 540, LBL 24.5 TO CENTER. R&R INTERCOSTAL PER SRM.
INTERCOSTAL CRACKED AT BS 540, BETWEEN LBL 24.5 TO LBL 45.5. R&R INTERCOSTAL PER SRM.
AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED. R&R WEB PER SRM.
FWD CABIN STA 312/328 ;RBL 31 FLOOR INTERCOSTAL IS CRACKED ON TOP FLANGE. / REMOVED AND REPLACED NEW INTERCOSTAL ( 141A5410U140 ) PER SRM 51-40-02
FORWARD INBOARD EDGE WEB CRACKED AT BS 295, STR 16L. R&R WEB PER SRM.
PASSENGER CABIN STA 827 STR 11R STRINGER CLIP CRACKED AT RADIUS. (MARKED) / REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.
SUPPLEMENTAL INFORMATION: AFT SERVICE DOOR SURROUND STRUCTURE LOWER Z ANGLE HAS VARIOUS AREAS OF CORROSION. (MARKED) / REMOVED; AND REPLACED AFT SERVICE DOOR Z ANGLE. REF. SRM. 51-40-02. SEE WIPS AND TASK FOR INDIVIDUAL SIGN OFFS.
SUPPLEMENTAL INFORMATION: PASSENGER CABIN STA 807 STR 11R STRINGER CLIP CRACKED AT RADIUS. (MARKED) / REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.
FORWARD CARGO BRACKET CRACKED AT BS 500D, STR 19R. R&R BRACKET PER SRM.
FORWARD CARGO BRACKET CRACKED AT BS 500D, STR 19L. R&R BRACKET PER SRM.
PASSENGER CABIN STA 787 STR 11R STRINGER CLIP CRACKED AT RADIUS. (MARKED) / REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT DOOR THRESHOLD; AFT CORNER PIECE HAS CRACK. / THRESHOLD PLATE REPAIRED ON REPAIR ORDER # RA15B5. PLATE TO BE INSTALLED ON ROUTINE TASK CARD # 753-140-00-02Y.
SUPPLEMENTAL INFORMATION: RT WING UPPER T/E SHELF PANEL O/B OF #7 SPOILER ANGLED BULB SEAL BRKT ON FWD SIDE CRACKED. / REMOVED AND REPLACED CRACK BRACKET PER SRM 51-40-02.
SUPPLEMENTAL INFORMATION: RT WING UPPER T/E SHELF PANEL O/B OF 7 SPOILER MIDDLE SUPPORT BRKT CRACKED. / REMOVED AND REPLACED CRACK BRACKET PER SRM 51-40-02.
SUPPLEMENTAL INFORMATION: RT WING WAFFEL PLATE CRACKED ABOVE PANEL #651DB / REMOVED AND REPLACED RT WING WAFFEL PLATE PER SRM 51-40-02.
RT AFT GIRT BAR ATTACHED BRACKET CORRODED AROUND FASTENER HOLE AT BS 986.5, RBL 43. REPAIRED FLOOR BEAM T CAP PER EA.
SUPPLEMENTAL INFORMATION: RH HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED / REMOVED AND REPLACED R/H HORIZONTAL STAB FWD UPPER SLIDER SEAL AND OPS CHECKED PER AMM 53-31-31
SUPPLEMENTAL INFORMATION: LEFT WING UPPER FIXED TRAILING EDGE PANEL ABOVE INBOARD DEFLECTION RIB; PANELS MIDDLE SEAL RETAINER CRACKED ON FWD UPPER SIDE. / REMOVED & REPLACED SEAL RETAINER ASSY. PER SOPM 20-50-01 & SRM 51-40-02.
SUPPLEMENTAL INFORMATION: LEFT WING UPPER FIXED TRAILING EDGE PANEL ABOVE INBOARD DEFLECTION RIB; AFT UPPER SEAL RETAINER CRACKED ON AFT UPPER SIDE. / REMOVED & REPLACED SEAL RETAINER ASSY. PER SOPM 20-50-01.
FWD CARGO AFT SCUFF PLATE CRACKED. / THRESHOLD SCUFF PLATE REPAIRED ON REPAIR ORDER # RA15B4. PLATE TO BE INSTALLED ON ROUTINE TASK CARD 753-140-00-01Y.
L1 DOOR SLIDE CAME LOOSE UPON OPENING. REINSTALLED SLIDE PACK PER TASK CARD.
CENTER AISLE FLOOR BOARD SOFT AND DELMINATED MOD / REMOVED & REPLACED CENTER AISLE FLOOR BOARD IN REF TO AMM 53-21-00
R1 DOOR EMERGENCY ESCAPE SLIDE FAILED INSPECTION CRITERIA. R&R SLIDE PER MT.
L1 DOOR EMERGENCY ESCAPE SLIDE FAILED INSPECTION CRITERIA. R&R SLIDE PER MT.
RIGHT OVERWING EXIT OVERHEAD SIGN INOPERATIVE. R & R THE POWER SUPPLY IAW AMM.
R1 DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
RT FORWARD CABIN FLOOR ESCAPE PATH STRIP DELAMINATED AT ROW 1. R&R STRIP PER DWG.
VERTICAL SEAL RETAINER IN TRAILING EDGE OF R/H WING JUST ABOVE #2 ENGINE AFT PYLON FAIRING IS CRACKED. / REMOVED AND REPLACED SEAL RETAINER AS REQUIRED I.A.W. SRM 51-40-02.
LEFT MAIN WHEEL WELL STA 663 STIFFENER OUTBD OF RAM AIR EXHAUST DUCT CRACKED / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02
LT FORWARD CABIN FLOOR ESCAPE PATH STRIP DELAMINATED AT ROW 1. R&R STRIP PER DWG.
L1 DOOR EXIT SIGN LIGHT COVER MISSING RED ARROW ON LIGHT COVER. R & R THE COVER IAW AMM.
R1 DOOR EMERGENCY EXIT SIGN LIGHT COVER MISSING RED ARROW AT ENTRANCE. / R&R COVER PER AMM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET BROKEN. SECURED BRACKET PER SIP.
LT EMERGENCY LIGHT LENS LOOSE AT ROW 14. SECURED LENS IAW AMM.
LT BIN EMERGENCY LIGHT INOP AT ROW 1. RECONNECTED CONNECTOR PER WDM & AMM.
CENTER AISLE MID CABIN EXIT LIGHT ASSEMBLY CRACKED. R&R LIGHT ASSEMBLY PER AMM.
STRINGER CLIP CRACKED AT BS 706, STR 3L. R&R CLIP PER SRM.
STRINGER CLIP CRACKED AT BS 727C, STR 6L. R&R CLIP PER SRM.
L2 WINDOW ARCED. R&R L2 WINDOW PER MT.
RIGHT OVERWING EXIT DOOR LIGHT LENS BROKEN. R & R LENS IAW MM.
RIGHT LOWER OVERWING EMER EXIT SIGN LIGHT LOOSE. SECURED LIGHT IAW AMM.
RIGHT PHOTO LUMINESCENT FLOOR STRIP DELAMINATED AT ROW 1. R & R STRIP IAW MM.
EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M167. R & R BATTERY PACK IAW AMM.
EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY PACK IAW AMM.
FORWARD ENTRY DOOR Z ANGLE CRACKED AT FRAME BS 303. R & R Z ANGLE IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 328 - 344, LBL 45. R & R INTERCOSTAL IAW SRM.
AFT CARGO DOOR THRESHOLD WEB CORRODED BETWEEN BS 794 - 847 ON UPPER SURFACE. R & R WEB IAW SRM.
AFT CARGO DOOR THRESHOLD STRAP CORRODED BETWEEN BS 803 - 839 ON UPPER SURFACE. R & R STRAP IAW SRM.
RIGHT HORIZONTAL STABILIZER CRACKED ON LOWER IN SPAR SKIN AT STAB STATION 101.9 & APPROX 7" FWD OF REAR SPAR. REPAIRED SKIN IAW CCO.
RIGHT OVERHEAD BULLNOSE EMER EXIT LIGHT LOOSE AT ROW 3. SECURED LIGHT IAW MM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 44.5, HOLE D. REPAIRED FLANGE IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 23.75, HOLE D. REPAIRED FLANGE IAW EA.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 23.75, HOLE D. REPAIRED FLANGE IAW EA.
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 45, AT FWD NUTPLATE HOLE. REPAIRED INTERCOSTAL IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 25.75, HOLE D. REPAIRED FLANGE IAW EA.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 44.5, HOLE D. REPAIRED FLANGE IAW EA.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 46.5, HOLE D. REPAIRED FLANGE IAW EA.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 23.75, HOLE D. REPAIRED FLANGE IAW EA.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 23.75, HOLE D. REPAIRED FLANGE IAW EA.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 23.75, HOLE D. REPAIRED FLANGE IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 25.75, HOLE D. REPAIRED FLANGE IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 46.5, HOLE D. REPAIRED FLANGE IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 44.5, HOLE D. REPAIRED FLANGE IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 23.75, HOLE D. REPAIRED FLANGE IAW SRM.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 46.5, HOLE D. REPAIRED FLANGE IAW SRM.
LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST 8 LOWER CORNER FASTENER HOLE CRACKED. REPAIRED POST IAW EA.
SKIN CRACKED AT BS 540, BELOW STRINGER 22L, FASTENER HOLE E. REPAIRED SKIN IAW EA.
LEFT WW PRESS WEB CRACKED AT BS 663, LBL 45. REPAIRED WEB IAW SRM.
SKIN CRACKED AT BS 540, BELOW STRINGER 22R, FASTENER HOLE B. REPAIRED SKIN IAW EA.
SKIN CRACKED AT BS 540, BELOW STRINGER 22L, FASTENER HOLE A. REPAIRED SKIN IAW EA.
SKIN CRACKED AT BS 540, BELOW STRINGER 22R, FASTENER HOLE G. REPAIRED SKIN IAW EA.
RT OVERWING EMEGENCY EXIT SIDE WALL LIGHT INOPERATIVE. RELAMPED IAW MM.
CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSEMBLY PER MM.
FLOOR SUPPORT CRACKED BS 540, BETWEEN BL 0 TO RBL 25. REMOVED AND REPLACED SUPPORT PER SRM.
RIGHT INTERCOSTAL CORRODED AT STA 772, RBL 20. REMOVED AND REPLACED INTERCOSTAL IAW SRM.
CORROSION AFT CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT STA 727B+10 - 807, LBL 22 AND WL 155. REPAIRED FLOOR SUPPORT PER SRM.
RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 847 TO BS 867, RBL 22 AND WL 164. REMOVED AND REPLACED SUPPORT PER SRM.
CORROSION AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT BETWEEN STA 767 TO STA 787, RBL 22 AND WL 156. REMOVED AND REPLACED FLOOR SUPPORT PER SRM.
CORROSION AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT STA 727A - 767, RBL 22 AND WL 155. REPAIRED FLOOR SUPPORT IAW SRM.
FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO LBL 25. REMOVED AND REPLACED SUPPORT PER SRM.
LEFT WING INBD MAIN FLAP LOWER T/E WEDGE LOWER SURFACE CRACKED. REPAIRED WEDGE PER EA.
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BETWEEN BS 500 TO BS 500D, LBL 23. REPAIRED FLOOR SUPPORT BAC.
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BETWEEN BS 500A AND BS 500D, RBL 23. REPAIRED FLOOR SUPPORT PER SRM AND DWG.
RIGHT WING T/E COVE SEAL RETAINER CRACKED ABOVE NR 2 PYLON AFT TIP. REMOVED AND REPLACED RETAINER IAW SRM.
LEFT WING T/E COVE SEAL RETAINER CRACKED ABOVE NR 1 PYLON AFT TIP. REMOVED AND REPLACED RETAINER IAW SRM.
BODY STATION 663 BULKHEAD, LOWER RIGHT FIBERGLASS WEB, IS CRACKED JUST I/B OF HYDRAULIC "B" SYSTEM GROUND SERVICE DISCONNECT MODULE BRACKET. REPAIRED WEB PER EA.
RIGHT MLG W/W, BS 663, RBL 42, WL 200 PRESSURE WEB CRACKED. REPAIRED WEB PER SRM.
EMERGENCY EXIT FLOOR LIGHT LENS MISSING AT ROW 3. INSTALLED LENS PER M/M.
EEPLS BROKEN BETWEEN ROW 1 TO ROW 3. REMOVED AND REPLACED EEPLS IAW MM.
EEPLS LENS MISSING. INSTALLED LENS PER MM.
LT EEPLS LENS BROKEN AT ROW 20. REMOVED AND REPLACED LENS PER MM.
FWD FLOOR EMERGENCY LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN IAW SRM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS CRACKED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS DIRTY AT ROW 16. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
FWD EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.
DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS LENS CRACKED AT ROW 2. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED END CAP PER MM.
DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
L1 DOOR LOWER EMERGENCY EXIT SIGN LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
FWD GALLEY EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM.
EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.