N904WN
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
R2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED R2 DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801 OPS CHECK GOOD. VERIFIED R2 DOOR EXTERNAL EMERGENCY LIGHT REPLACEMENT IAW AMM 33-51-04-960-801. OPS CHECKED GOOD.
EMERGENCY LIGHT AT SEAT 16FED INOPERATIVE. REMOVED AND REPLACED 16DEF EMERGENCY AREA LIGHT BULB IAW AMM 33-51-03-960-801, OPS CHECKED GOOD. VERIFIED16DEF EMERGENCY AREA LIGHT BULB REPLACEMENT IAW AMM 33-51-03-960-801 OPS CHECK GOOD
FOS GRAB HANDLE (BY WINDSCREEN) BROKEN<[01] R&R GRAB HANDLE PER MM 56-11-11.
RIGHT OVER WING EXIT LIGHT DIM<[01] R&R CABIN EMERGENCY EXIT SIDEWALL BALLETS PER AMM 33-51-02
AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR CRACKED. R&R AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
AFT GALLEY SERVICE DOOR R2 ESCAPE SLIDE AFT TIE-LADDER NOT SECURED. SECURED THE SERVICE DOOR R2 ESCAPE SLIDE AFT TIE-LADDER W COTTER PIN REF AMM 25-66-01.
AFT ENTRY DOOR L2 ESCAPE SLIDE TIE-LADDER NOT SECURED. SECURED AFT ENTRY DOOR L2 SLIDE TIE-LADDER W COTTER PIN IAW AMM 25-66-01.
AFT GALLEY SERVICE DOOR R2 SLIDE GIRT HANGS TOO LOW. REPACKED AFT GALLEY SERVICE DOOR R2 SLIDE GIRT IAW AMM 25-66-01.
AFT ENTRY DOOR L2 SLIDE GIRT HANGS TOO LOW. REPACKED AFT ENTRY DOOR L2 SLIDE GIRT IAW AMM 25-66-01.
L1 LOWER FWD EMERGENCY EXIT LIGHT HAS BULB OUT. REMOVED AND REPLACED L1 LOWER FWD EMERGENCY EXIT LIGHT BULB IAW AMM 33-51-01-960-801.
L1 DOOR CLOSE HANDLE IS LOOSE AT SIDEWALL. TIGHTENED L1 DOOR CLOSE HANDLE AT SIDEWALL IAW AMM 52-11-31-400-802 STEP 3.G.(2).
L/H OVERWING EXIT AFT LIGHT LENS RETAINER IS DAMAGED. REMOVED AND REPLACED LT OVERWING EXIT LIGHT LENS IAW AMM 33-51-01-960-801 STEPS 2.C.1.A(3) AND 2 C(4).
RIGHT OVERWING EXIT FWD LIGHT LENS RETAINER IS DAMAGED. REMOVED AND REPLACED RT OVERWING EXIT LIGHT LENS IAW AMM 33-51-01-960-801 STEPS 2.C.1.A(3) AND 2.C(4).
AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE, REPAIRED IAW SRM 53-60-15-2R-1.
DURING OK TO CLOSE FOUND CORROSION ON FWD WET AREA LAV FITTING STA 312 APPROX LBL 55. REMOVED AND REPLACED TIEDOWN GIRT BAR AT BS 312 LBL 52; WL 208.1 IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G AND DWG 141A5220.
CORROSION ON FCB INTERCOSTAL BS 500 TO BS 500A, LBL 25, WL161. REMOVED AND REPLACED INTERCOSTAL FROM BS 500 TO BS 500A, LBL 25 IAW SRM 51-40-02, AND DWG 143A7505 REV -.
CRACK FOUND ON BAFFLE FWD CLIP AT BS 400, LBL 25. REMOVED AND REPLACED BAFFLE FWD CLIP AT BS 400, LBL 25 IAW SRM 51-40-02, AND DWG 143A7505 0081, REV -,
CRACKED BAFFLE AT BS 500A TO 500B, LBL 21, WL 161. REMOVED AND REPLACED THE BAFFLE FROM BS 500A TO 500B, LBL 21 IAW SRM 51-40-02, AND DWG 143A7505 REV -.
CRACKED INTERCOSTAL BS 312 - BS 328, LBL 45, WL 208.1. REMOVED AND REPLACED INTERCOSTAL BS 312- 328, LBL 45, WL 208.1 IAW SRM 51-40-02, AND DWG 141A5400.
CORROSION ON THE GIRT BAR AT BS 312, LBL 52, WL 208.1. REMOVED AND REPLACED TIE DOWN FOR GIRT BAR AT BS 312, LBL 52, WL 208.1 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DWG 141A5220.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 6 INCH AFT BS 500A, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
CRACK AT FSD BS 297.5 BELOW STR 6R. THIS JOBCARD WAS ATTENDED WITH THE FOLLOWING WO TTG8Q014JYV0.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 13'AFT STA.500C, LBL23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 7 INCH AFT BS 500C, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
AAFT CARGO BAY, LT SIDEPLATE SUPPORT BS 727 TO 847, LBL 21 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED ACB LT SIDEPLATE SUPPORT BS 727 TO 847 LBL 21 IAW SRM 51-40-02-0G-0 AND DWG 146A7500.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 2 INCH AFT BS 500C, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 10 INCH AFT BS 500B, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
AFT CARGO, RT SIDEPLATE SUPPORT BS 727 TO 767, RBL 21 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO 767, RBL 21 IAW SRM 51-40-02-0G-0, AND DWG 146A7500.
AFT CARGO, CORROSION TO FLOOR SUPPORT STRAP BS 887, RBL 17 TO LBL 17. REMOVED AND REPLACED ACB FLOOR SUPPORT STRAP BS 887 FROM RBL17 TO LBL17 IAW SRM 51-40-02, AND DWG 149A8104 0113, REV -.
ACB; CORROSION TO FWD SHIELD, BS 767 TO 787+5, RBL 21. REMOVED AND REPLACED NEW ON ACB FWD SHIELD FROM BS 767 TO 794, RBL 21 IAW SRM 51-40-02 AND DWG 146A0081 0028, REV A.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 6 INCH AFT BS 500B, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 6 INCH AFT BS 480, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 10 INCH AFT BS 480, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 10 INCH AFT BS 500, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 14 INCH AFT BS 500, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 18 INCH AFT BS 500, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 2 INCH AFT BS 500A, LBL 23, WL 156.5. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D, LBL 23 IAW SRM 51-40-02 AND DWG 143A7500 REV -.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 6 INCH AFT BS 500A, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 14 INCH AFT BS 500A, LBL 23, WL 156.5. THIS CARD WILL BE ACCOMPLISHED AT CARD TTG8Q014L3L6.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 17 INCH AFT BS 500, RBL 23, WL 156.5. REMOVED AND REPLACED FCB SUPPORT BETWEEN BS 492.4 TO 500A, RBL 23, WL156.5 IAW SRM 51-40-02 AND DWG 143A0080 REV-.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 9 INCH AFT BS 500, RBL 23, WL 156.5. THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q014L2U0.
FLOOR TO SIDEWALL SUPPORT ATTACH FRAME CORRODED 13 INCH AFT BS 500, RBL 23, WL156.5. THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q014L2U0.
FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW 241FF FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.
FWD FLOOR PANEL 222CF UPPER SKIN HAS AN AREA OF PULLED STRANDS NEAR FWD EDGE. REPAIRED THE FWD FLOOR PANEL 222CF IAW SRM 53-00-50-2R-1.
AFT CARGO FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.
MULTIPLE CORROSION AREAS ON LT SHIELD WEB AT BS 1016, LBL 4, BS 1016+12, LBL 4, BS 1016+14, LBL10 & LBL 13, BS 1016+12, LBL 18 AND BS 1016+5, LBL 30, WL 208.1. REPAIR PER EA 25-153-02201.
CRACK NOTED ON R1 DOOR CUT OUT STUB FRAME BS 291.5+9. 0.1 INCH ABOVE SEAL DEPRESSOR, APPROX LENGTH: 0.9 INCH. ENG TSR REQUIRED. REMOVED AND REPLACED STUB FRAME IAW SRM 51-40-02-0G-0 AND EA M-25153-01539, FIGURE 1.
CORROSION ON TENSION STRAP AT BS 1006, LBL 7, AND BS 1016+7, LBL 3, WL 208.1. REMOVED AND REPLACED AFT WET AREA TENSION STRAP FROM BS 1006 TO 1016+7; LBL 3 TO LBL 7, WL 208.1 IAW SRM 51-40-02-0G-0, AND DWG 147A5600 REV B.
FED INTERCOSTAL BETWEEN BS294.5-BS303.9 STR 16L WL216 IS CRACKED. REMOVED AND REPLACED FED INTERCOSTAL FROM BS 294.5 TO BS 303.9, S16L IAW SRM 51-40-02 AND DWG 141A8180 ID: 0027 REV C.
CRACK NOTED ON R1 BEAR STRAP BS 291.5+4, WL 266.5, APPROX. LENGTH: 1.9 INCH AND EXTENDING FROM STUB FRAME, REPAIRED IAW SRM 53-10-01-2R-6, AND EA M-25-153-01539.
LH WING TO BODY FAIRING SUPPORT HAS CRACKED AROUND THE FASTENER. REMOVED AND REPLACED LT WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02 AND DWG 116A3010 ID: 0039 REV -.
BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT RBL 8, WL 167. REPAIRED IAW SRM 57-10-10-2R-5, REPAIR 5.
LEFT HORIZONTAL STAB REMOVABLE L/E PANEL 331A RIB NR 3 IS CRACKED. REMOVED AND REPLACED RIB 3 IAW SRM 51-40-02 & DWG 186A1001.
LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB NR 4 IS CRACKED. REMOVED AND REPLACED RIB #4; IAW SRM 51-40-02 & DWG 186A1001.
RIGHT WING T/E PANEL 651FB HAS CRACKED L ANGLE AT FWD EDGE 27' FROM O/B END. REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB BRACKET AT FWD EDGE 27' FROM O/B END IAW SRM 51-10-02-0G-0 PAR. 9; C. AND AIPC 57-50-00-38.
CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS 663, LBL 37, WL 165. CRACKED LOWER LT COMPOSITE BULKHEAD AT BS 663, LBL 37, WL 165 WAS REPAIRED IAW SRM 51-70-04-2R-10.
R/H HORIZONTAL STAB REMOVABLE L/E 341B RIB NR 3 IS CRACKED. REMOVED AND REPLACED RIB NR 3 IAW SRM 51-40-02 & DWG 186A1001.
LEFT WING T/E PANEL 561AB AFT PANEL SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED LEFT-HAND WING T/E PANEL 561AB BEAM ASSY IAW SRM 51-40-02 AND DWG# 115A3712 ID: 0005 REV: -.
RIGHT HORIZONTAL STAB REMOVABLE L/E 341B RIB NR 4 IS CRACKED. REMOVED AND REPLACED RIB NR 4 IAW SRM 51-40-02 & DWG 186A1001.
LEFT WING T/E UPPER SURFACE PANEL JUST INBD OF NR 5 SPOILER O/B L-CLIP COMMON TO DEFLECTION CONTROL RIB IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-40-02 & DWG 115A6200, LEFT WING T/E UPPER SURFACE PANEL JUST INBD OF NR 5 SPOILER OTBD L-CLIP COMMON TO DEFLECTION CONTROL RIB.
FOUND AN AISLE LIGHT INOPERATIVE BETWEEN ROWS 18-19 DEF. REPLACED LAMP AISLE LIGHT BETWEEN ROW 18-19 DEF AND GOOD TEST IAW AMM 33-51-03-960-802.
LEFT WING T/E ORSS 261 UPPER SURFACE PANEL JUST I/B OF #5 SPOILER TRANSVERSE WEB CRACKED AT O/B FASTENER. REMOVED AND REPLACED WEB; IAW SRM 51-40-02 & DWG 115A2512.
27-51 (F/T TROUBLESHOOTING TRAILING EDGE FLAPS SYSTEM). DUE TO A/C HISTORY OF THE TRAILING EDGE FLAPS NOT EXTENDING PROPERLY CHECK THE TRAILING EDGE FLAPS TRANSMISSION TORQUE TRIP INDICATORS EXTENDED PER FIM 27-51 TASK 849. IF ANY INDICATORS ARE EXTENDED DRAIN AND REFILL THAT FLAP TRANSMISSION PER AMM 12-22-51. IF NO FAULTS ARE FOUND DRAIN & REFILL THE ALL T/E FLAP TRANSMISSIONS PER AMM 12-22-51. (PICTURES SDS 27-51-00-014) <[01]. T/S PER FIM 27-51 TASK 849; FOUND #2 TRAILING EDGE FLAP TRANSMISSION TORQUE TRIP INDICATOR EXTENDED.; [02] RESET #2 TRAILING EDGE FLAP TRANSMISSION INDICATOR; THEN DRAIN AND REFILL THE TRANSMISSION PER AMM 12-22-51. OPS CHECK GOOD.
PASSENGER CABIN L1 DOOR BOTH GIRT BAR HANGER BRACKETS LOOSE<[01] RESECURED L1 DOOR GIRT BAR HANGER BRACKETS PER SRM 51-40-02
AFT MEGAPHONE INOP<[01] REPLACED MEGAPHONE BATTERIES IAW AMM 25-64-00. OPS CHECK GOOD AT THIS TIME.
ASD AFT GIRT BAR FITTING; AFT ADAPTER BOLT BROKEN OFF IN ANCHOR NUT<[01] REMOVED BROKEN FASTENER AND INSTALLED NEW FASTENER PER AMM 25-66-02-400-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
EXTERIOR L/H LOWER EMERGENCY EXIT LIGHT INOP AFT OF WING<[01] RELAMPED EXTERIOR L/H LOWER EMERGENCY EXIT LIGHT AFT OF WING AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION #1
PASSENGER CABIN FLOOR PANEL 222BF HAS PULLED STRANDS ON UPPER SURFACE.<[01] UPDATED MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 222BF WITH PULLED STRANDS ON UPPER SURFACE WAS REPAIRED PER SRM 53-00-20-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION #2<BR>VERIFIED MEASUREMENTS
PASSENGER CAIN FLOOR PANEL 221AF HAS PULLED STRANDS ON UPPER SURFACE.<[01] PULLED STRANDS ON UPPER SURFACE OF PASSENGER CABIN FLOOR PANEL 221AF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.
CORROSION ON BS 986 FLOOR BEAM LOWER FLANGE AROUND FLOOR PANEL HOLE RBL 5 WL 208.<[01] REMOVED DAMAGED AND REPAIRED FLOOR BEAM LOWER FLANGE AT BS 986 RBL 5 WL 208 PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1.;[02] REMOVED DAMAGED AND REPAIRED FLOOR BEAM UPPER FLANGE AT BS 986 RBL 5 WL 208 PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 WORK WAS ACCOMPLISHED ON STEPS 1-12
CORROSION ON BS 986 FLOOR BEAM LOWER FLANGE UNDER NUT PLATE LBL 44 WL 208.<[01] REMOVED DAMAGED AND REPAIRED FLOOR BEAM LOWER FLANGE AT BS 986 LBL 44 WL 208 PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.;[02] REMOVED DAMAGED AND REPAIRED FLOOR BEAM UPPER FLANGE AT BS 986 LBL 44 WL 208 PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. WORK WAS ACCOMPLISHED ON STEPS 1-12
CORROSION ON AFT R/H SHEAR WEB STRAP BS 1028 RBL 18 WL 208.<[01] VERIFIED CORRECTIVE ACTION ITEM AND MEASUREMENT FIELDS; CARD COMPLETE.
FWD ENTRY DOOR MOP SILL CRACKED AT BS 303 LBL 56 WL 208.<[01] PARTILA STEP 1;[02] UPDATED STEP 1.;[03] UPDATED STEP 2 AND 3;[04] COMPLETED STEPS 2.3.;[05] COMPLETED STEP 1AND 4.;[06] VERIFIED STEPS COMPLETE.
BS312 FRAME CRACKED IN RADIUS ABOVE FWD ENTRY DOOR<[01] ACCOMPLISHED M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L) ATTACHED SEE TTG8Q00N0XPJ.;[02] VERIFIED STEP 1.
CRACKED INTERCOSTAL BS 380-400 RBL 39 WL 208.<[01] UPDATED MEASUREMENT TABLE AND ACCOMPLISHED STEP 1.;[02] REMOVED AND REPLACED INTERCOSTAL BS 380-400; RBL 39; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 143A5400.;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED MEASUREMENT TABLE
CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208.<[01] UPDATED MEASUREMENT TABLE AND ACCOMPLISHED STEP 1.;[02] COMPLETED STEP 4;[03] REMOVED AND REPLACED INTERCOSTAL BS 380-400 LBL 14 WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 143A5300.;[04] VERIFIED INSTALL; TASK COMPLETE
CORROSION ON OUTER FUSELAGE CROWN SKIN COMMON TO FASTENER ROWS FROM STATION 1016 TO 1016+17; STRINGER 0; STRINGER S-1R; STRINGER S-1L; AND BL 12 LEFT AND RIGHT. CORRECTION TO FAULT NAME LOCATION SHOULD BE STR 1 AND STR 2L AND STR 2R LBL 12 AND RBL 12<[01] VERIFIED CORRECTIVE ACTION STEP 1; 2;3.;[02] VERIFIED STEP 9.1;[03] REMOVED CORROSION AROUND 47 FASTENER HOLES BS 1016 TO BS 1016+22; STR 1; STR 2R; STR 2L; RBL12; AND LBL12. REMOVED .5'X.5'X.006' LOWEST READING. ORIGINAL THICKNESS IS .080'; REMOVED AND REPLACED FASTENERS IN REWORKED AREA; ALL PER SRM 53-00-01-1A-1; SRM 53-80-01-0L-1; AND EA 23-153-02671. ' AS PER EA 23-153-02671; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.';[04] VERIFIED CORRECTIVE ACTION #3
RH CABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AT BS 639+10; 706+5; RBL 45; WL 208<[01] UPDATED MEAUSREMNTS TABLE; STEP 1 AND 2.;[02] VERIFIED CORRECTIVE ACTION STEP 1 AND STEPS 1 AND 2.;[03] UPDATED MEASURMENTS TABLE;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] TOOLING USED ON STEP 2 ID:ATS2472 CAL DATE:12/20/22 DUE DATE:12/31/23;[06] UPDATED STEP 3;[07] REJECTION. DURING OK TO INSTALL SEAT TRACK; FOUND SCRIBE MARKS ON BEAM FROM BS 540 TO BS 727B RBL 45 WL 208 [TTG8Q00N8BCX];[08] UPDATED STEP 4;[09] REMOVED AND REPLACED R/H CABIN SEAT TRACK AT BS 540-727B AND WAS ACCOMPLISHED ON FAULT# TTG8Q00NABR2 AND PER BOEING DWG# 144A5300 REV: E AND AMM 20-50-11-910-801;[10] REMOVED AND REPLACED R/H CABIN SEAT TRACK AT BS 540-727B PER BOEING DWG# 144A5300 REV: E AND AMM 20-50-11-910-801;[11] VERIFIED CORRECTIVE ACTION 10;[12] CARD COMPLETE
CORROSION ON LAV MOUNT FLOOR SUPPORT BS 294-312 LBL 11 WL 208.<[01] UPDATED STEP 1;[02] UPDATED STEP 3;[03] UPDATED STEP 2;[04] UPDATED MEASUREMENT TABLE;[05] UPDATED PARTS TABLE;[06] UPDATED STEPS 5 AND 6;[07] REMOVED AND REPLACED DAMAGE LAV.MOUNT FLOOR SUPPORT I.A.W SRM 51-40-02-0G-0; BOEING DWGS 141A5502;141A5600.;[08] VERIFIED CORRECTIVE ACTION 7;[09] VERIFIED MEASUREMENT TABLE
CORROSION ON AFT ENTRY DOOR MOP SILL BS 967-986 LBL 52 WL 208.<[01] COMPLETED STEP 4<BR><BR>REMOVED CORROSION ON AED MOP SILL BS 967-986 LBL 52 WL 208 AND WORK WAS ACCOMPLISHED ON STEPS 1-4;[02] VERIFIED CORRECTIVE ACTION ITEM AND MEASUREMENT FIELDS; CARD COMPLETE.
CRACKED INTERCOSTAL BS 380-400 RBL 9 WL 208.<[01] UPDATED MEASUREMENT TABLE AND ACCOMPLISHED STEP 1.;[02] COMPLETED STEP 4;[03] REMOVED AND REPLACED INTERCOSTAL BS 380-400; RBL 9; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 143A5300.;[04] VERIFIED REMOVAL OF CRACKED PART IN STEP 1;[05] TASK CARD COMPLETE
CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] UPDATED MEASUREMENT TABLE.;[02] ACCOMPLISHED STEPS 1 AND 2.;[03] REMOVED AND REPLACE CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 141A5400.
CORROSION ON FWD ENTRY DOOR MOP SILL ATTACH ANGLE BS 317 -340 LBL 60 WL 208.<[01] UPDATED TABLE MEASUREMENTS;[02] UPDATED MEASUREMENTS TABLE;[03] UPDATED STEP 1.;[04] UPDATED STEPS 2 AND 3;[05] STEP 1 7 2 COMPLETE; STEP 3 IN PARTIAL.;[06] UPDATED STEP 4.;[07] STEP 4 IN PARTIAL.;[08] UPDATED STEP 4.;[09] STEP 4 COMPLETE.;[10] UPDATED STEP 3;[11] COMPLETED STEP 3;[12] UPDATED MEASUREMENT TABLE;[13] REMOVED CORROSION ON FED MOP SILL ATTACH ANGLE BS 317-340 LBL 60 WL 208 AND WORK WAS ACCOMPLISHED ON STEPS 1-5
CORROSION ON AFT SERVICE DOOR MOP SILL VERTICAL AND HORIZONTAL FLANGES BS 964-993 RBL 48 WL 208.<[01] REMOVED; REPLACED AND INSTALLED NEW SERVISE DOOR MOPSILL PER SRM 51-40-02-0G-0 AND DWG 147A8501.
CORROSION ON BS 986 FLOOR BEAM COMMON TO A PREVIOUS REPAIR RBL 36-45 WL 208.<[01] REMOVED AND REPLACED PREVIOUS REPAIR AT BS 986 RBL 36-50 WL 208 PER SRM 51-40-02-0G-0 ALL PER ORIGINAL REPAIR RECORD ON NRC G300314 PER SWA EA-1-753-29038 REV IR AND SRM 53-70-51-2R-4 REPAIR 4.;[02] REMOVED AND REPLACED PREVIOUS REPAIR AT BS 986 RBL 36-50 WL 208 PER SRM 51-40-02-0G-0 ALL PER ORIGINAL REPAIR RECORD ON NRC G300314 PER SWA EA-1-753-29038 REV IR AND SRM 53-70-51-2R-4 REPAIR 4. WORK WAS ACCOMPLISHED ON STEPS 1-7;[03] VERIFIED CORRECTIVE ACTION COMPLETE
CORROSION ON AFT L/H SHEAR WEB STRAP BS 1018-1028 LBL 3 WL 208.<[01] VERIFIED CORRECTIVE ACTION ITEM AND MEASUREMENT FIELDS; CARD COMPLETE.
FWD L/H WINDSCREEN EMERGENCY FLASHLIGHT NOT WORKING NEEDS REPLACEMENT.<[01] REPLACED FLASHLIGHT ASSEMBLY FROM FWD L/H WINDSCREEN; BOTTOM FLASHLIGHT. PER AMM 25-64-00-200-802-NG-01. FUNCTIONAL CHECK GOOD.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 231GF HAS DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE FABRICATED NEW FLOOR PANEL 231GF OUT OF BMS4-17 TY6 LOT#1531501-1 AND INSTALLED INSERTS WITH BMS5-107 LOT#1537008-1. CURED INSERTS UNDER HEAT LAMP USING THERMOMETER ID:ATS2209 DUE:10/23 AND PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE); 5.S; AND BDWG 143A5810-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] ATTACHED INSERT CURE SHEET TO FAULT.;[04] VERIFIED CORRECTIVE ACTION ITEM 3. JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221FF HAS DELAMINATION<[01] REPAIRED FLOOR PANEL 221FF DELAMINATION IAW SRM 53-00-50-2R-1 AND BDWG 141A5810-157.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CORRECTIVE ACTION 1
PASSENGER CABIN FLOOR PANEL 241YF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241YF WITH DELAMINATION ON UPPER SKIN WAS REPAIRED PER SRM 53-00-50-2R-1. <BR><BR>ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CORRECTIVE ACTION 1
PASSENGER CABIN FLOOR PANEL HAS DELAMINATION PASSENGER CABIN FLOOR PANEL 241ZF HAS DELAMINATION.<[01] ACCOMPLISHED DELAMINATION REPAIR ON FLOORBOARD 241ZF AS PER 53-00-50-2R-1;[02] ACCOMPLISHED DELAMINATION REPAIR ON FLOORBOARD 241ZF AS PER SRM 53-00-50-2R-1;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED CORRECTIVE ACTION 2
PASSENGER CABIN FLOOR PANEL 242UF HAS 1 BAD INSERT AND DELAMINATION.<[01] REPAIRED PASSENGER CABIN FLOOR PANEL 242UF AND REPLACED BAD INSERT IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 241XF HAS DELAMINATION.<[01] PASSENGER CABIN FLOOR PANEL 241XF WITH DELAMINATION ON UPPER SKIN WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221EF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 221EF WITH DELAMINATION ON UPPER SURFACE WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 242AF HAS DELAMINATION<[01] ACCOMPLISHED FABRICATION OF 242AF FLOORBOARD PANEL IAW SRM 53-00-50-2R-0 ALONG WITH DWG 144A5810 SHEET 189;[02] VERIFIED CORRECTIVE ACTION 1
PASSENGER CABIN FLOOR PANEL 221DF HAS DELAMINATION. (MARKED)<[01] REPAIRED PASSENGER CABIN FLOOR PANEL 221DF DELAMINATION IAW SRM 53-00-50-2R-1 AND BDWG 141A5810-59.;[02] VERIFIED CORRECTIVE ACTION #1;[03] ATTACHED CURE SHEETS TO THIS FAULT RECORD.
CRACK AFT CARGO BAY CARGO TRACK BS767 AND BS727E RBL13 WL156<[01] VERIFIED STEP 5;6 IN PARTIAL.;[02] VERIFIED STEP 6 COMPLETE AND MEASUREMENT TABLE.;[03] REMOVED OLD DAMAGED CARGO BAY TRACK BS 727+4 TO 887 RBL 13; LOCATED; DRILL AND INSTALLED NEW CARGO TRACK PER SRM 51-40-02-0G-0; DWG; 146A7500; SRM 53-00-53-2R-3 REPAIR 3 AND EA 23-153-02547;[04] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 3 AND MEASUREMENT TABLE.
WING CENTER SECTION CORROSION ON STRAP AT BS 685+13; RBL 65; WL 204. (MARKED) CORRECTION TO FAULT NAME CORROSION IS LOCATED ON ANGLE AT BS 685+13 RBL 65 WL 204.<[01] REMOVED CORROSION ON STRAP AT BS 685+13; RBL 65; WL 204 IN AN AREA OF 0.6'X1'X0.0013' IAW SRM 51-10-02-0G-0; TOOL USED ID:ATS400; DUE:09/2023;[02] INSPECTED AND VERIFIED CORROSION REMOVAL.;[03] COMPLETED MEASUREMENT TABLE.;[04] WING CENTER SECTION STRAP AT BS 685+13; RBL 65; WL 204 FOUND TO HAVE NO ALLOWABLE DAMAGE ENTRY; THEREFORE; DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 51-10-02-0G-0. REPAIRED DAMAGE ON WING CENTER SECTION CORROSION ON STRAP AT BS 685+13; RBL 65; WL 204 PER EA 23-153-02680.;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4 AND MEASUREMENT TABLE.
WING CENTER SECTION FLOOR BEAM SUPPORT CRACKED AT BS 540; WL 208; RBL 44. (MARKED)<[01] UPDATED STEPS 1 AND 2 AND OK TO INSTALL STEP 1;[02] REMOVED AND REPLACED WING CENTER SECTION FLOOR BEAM SUPPORT AT BS 540; RBL 25 - RBL 45; WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED MEASUREMENT TABLE
WING CENTER SECTION FLOOR BEAM SUPPORT CRACKED AT BS 540; WL 208; RBL 1. (MARKED)<[01] REMOVED BEAM SUPPORTON WING CENTER SECTION AT BS 540; WL 208; RBL 1 IAW SRM SRM 51-40-02;[02] UPDATED STEP 1;[03] REMOVED AND INSTALLED NEW PART 143A5240U34 FLOOR BEAM SUPPORT ON BS 540; WL 208; RBL 1 IAW SRM 51-40-02 DWG 143A0060.;[04] VERIFIED CORRECTIVE ACTION 3
WING CENTER SECTION FLOOR BEAM SUPPORT CRACKED AT BS 540; WL 208; LBL 1. (MARKED)<[01] REMOVED BEAM SUPPORTON WING CENTER SECTION AT BS 540; WL 208; LBL 1 IAW SRM 51-40-02;[02] UPDATED STEP 1;[03] REMOVED AND INSTALLED NEW PART 143A5240-33 FLOOR BEAM SUPPORT ON BS 540; WL 208; LBL 1 IAW SRM 51-40-02 DWG 143A0060.;[04] COMPLETED MEASUREMENT TABLE.;[05] VERIFIED CORRECTIVE ACTION 3;[06] VERIFIED MEASUREMENT TABLE
WING CENTER SECTION FLOOR BEAM SUPPORT CRACKED AT BS 540; WL 208; LBL 44. (MARKED)<[01] REMOVED AND INSTALLED NEW PART PN 143A5240U31 FLOOR BEAM SUPPORT ON BS 540; WL 208; LBL 44 IAW 51-40-02 DWG 143A0060. AND TABLE MEASUREMENTS COMPLETED;[02] VERIFIED TASK COMPLETE.;[03] REMOVED AND INSTALLED NEW PART PN 143A5240U31 FLOOR BEAM SUPPORT ON BS 540; WL 208; LBL 44 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 143A0060. AND TABLE MEASUREMENTS COMPLETED
CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26.5 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY SUB THRESHOLD WEB PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8340.
CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727A TO BS787 LBL22 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE BS727+4 TO BS847 LBL22 WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500 AND DWG 146A0061;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB R/H STA 663+2 RBL 39+0.7 L: 0.5'<[01] UPDATED STEPS 2-7.;[02] STEP 15 IN PARTIAL.;[03] CRACK FOUND TO BE OUT OF LIMITS ON HORIZONTAL PRESSURE DECK WEB R/H STA 663+2 RBL 39+0.7 NO ALLOWABLE LIMITS IN SRM; REPAIRED AREA IAW SRM 53-40-51-2R-2; REPAIR 2;[04] VERIFIED CORRECTIVE ACTION #3<BR>VERIFIED MEASUREMENTS
CRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. MARKED<[01] REMOVED DAMAGED STRINGER SECTION BS 535 STRINGER 25 R/H; FABRICATED NEW REPAIR PARTS; LOCATED DRILLED AND INSTALLED ALL PER SRM 51-40-02-0G-0; SRM 53-00-03-2R-1; EA 23-153-02537; AND DWG 143A3241.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
CRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<[01] TASK CARD COMPLETE.
L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] UPDATED STEP 4 AND 5;[02] VERIFIED STEPS 4;9;10;11 IN PARTIAL.;[03] VERIFIED STEPS 9;10; COMPLETE.;[04] VERIFIED STEP 11 IN PARTIAL.;[05] CRACK ON UPPER ATTACH ANGLE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION AND REPAIRED L/H BS663 UPPER ATTACH ANGLE ON VAPOR BARRIER LBL8 WL167.68 IAW SRM 57-10-10-2R-5 AND DWG 111A1000.;[06] VERIFIED STEP 11 COMPLETE.;[07] VERIFIED STEP 4;12; COMPLETE.;[08] VERIFIED STEP 13;14 COMPLETE AND MEASUREMENT TABLE; CARD COMPLETE.
FWD CARGO FIBERGLASS FLOOR PANEL HAS 14 INCH CRACK<[01] REPAIRED FLOOR PANEL IAW AMM 25-52-01 OK FOR CONT SERVICE
AFT ENTRY DOOR ESCAPE SLIDE SKIRT BINDS ON LOWER DOOR FRAME WHEN ATTEMTING TO CLOSE<[01] REINSTALLED GIRT BAR AND ESCAPE SLIFE SKIRT AND OPS CHK NORMAL PER AMM 25-66-01
FWD ENTRY DOOR ESCAPE SLUDE GIRT BAR HANGING TO LOW<[01] REPOSITIONED GIRT BAR FLAP PER M/M 25-66-01.
FWD ENTRY DOOR ASSIST HANDLE BROKEN<[01] R&R?D FWD ENTRY DOOR ASSIST HANDLE REF AMM 52-11-31.
EMERGENCY LIGHTS INOP AT L1 LINER EXIT; L1 LOWER EXIT AND R1 LINER EXIT<[01] FOUND EMERGENCY LIGHTS WERE OPERATING WHEN SWITCH WAS IN THE ARMED POSITION AS WELL. REPLACED EMERGENCY LIGHT SWITCH PER WDM 33-51-11 & SWPM 20-83-11. SWITCH OPERATES NORMAL. FOUND FUSES BAD ON FWD LH EMERGENCY POWER SUPPLY (M1675). FOUND L1 LOWER WALL EXIT LIGHT ASSEMBLY SHORTED PER WDM 33-51-12. R&R L1 LOWER WALL EXIT LIGHT PER AMM 33-51-01. FOUND BAD LAMPS ON R1 LINER EXIT LIGHT; RELAMPED PER AMM 33-51-01. REPLACED LH AND RH EMERGENCY POWER SUPPLIES AND BATTERY PACKS PER AMM 33-51-06. OPS CHECKED EMERGENCY LIGHTS PER AMM 33-51-00. EMERGENCY LIGHTS GOOD.
FWD ENTRY DOOR BRACKET FOR GIRT BAR IS LOOSE . BAR FALLS OUT / [01] ADJUSTED FWD ENTRY DOOR SLIDE GIRT BAR BRACKETS PER S.I.P. OPS CHKS GOOD
FWD GALLEY MEGA PHONE INOP. / [01] REPLACED BATTERY PER SIP.
FWD ENTRY DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT HOUSING BROKEN / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT HOUSING AS REQUIRED. OPS CHECK NORMAL. AMM 33-51-01
FWD ENTRY DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REPLACED LENSE REF AMM 33-51-01
SMELL COMING FROM BEHIND COFFEE MAKER ( FWD GALLEY ) / [01] C/W CONDITIONAL INSPECTION PER 05-51-56; VERIFIED SMELL COMING FROM BEHIND THE COFFEE MAKER; NO SMELL NOTED AFTER DE ACTIVATING THE COFFEE MAKER. OK TO CONTINUE PER MEL 25-10-01. SP1B AND SP2;[02] R&R?D FWD COFFE MAKER PER A.M.M. 25-30-01- OP?S CK GOOD;[03] ITEM CLEARED ON LOG PAGE 2080251
RH OVER WING EXIT SIGN AFT LIGHT INOP / [01] RELAMPED RH OVER WING EXIT SIGN AFT LIGHT PER AMM 33-51-01. OPS CK GOOD
2 AFT CABIN POBS USED IN FLIGHT DUE TO A POSSIBLE LEAK IN AN OVERHEAD BIN OR CEILING COMPARTMENT. 2 AFT CABIN POBS USED IN FLIGHT DUE TO A POSSIBLE LEAK IN AN OVERHEAD BIN OR CEILING COMPARTMENT. / [01] SERVICED BOTH AFT POB?S REF. AMM 12-15-21.<BR><BR>REF. LOG PAGE 2130609 FOR FURTHER ACTION.
FORWARD SERVICE DOOR GIRT BAR STICKING ; / [01] ADJUSTED AND CLEANED GIRT BAR CLIP PER MM25-66-01
AFT CARGO DOOR CUT OUT CORNER CASTING AFT SCUFF PLATE CRACKED. ; / [01] INSTALLED REPLACEMENT AFT SCUFF PLATE PER MM 53-11-02 UP TO APPLYING FAIRING COMPOUND; [02] INSPECTION COMPLETE ON AFT CARGO DOOR AFT SCUFF PLATE INSTALLATION. FINAL BUYOFF STILL PENDING APPLICATION OF FAIRING COMPOUND.; [03] APPLIED FAIRING COMPOUND PER AMM 53-11-02. LEAK CHECK GOOD PER AMM 05-51-91; [04] INSTALLED REPLACEMENT AFT SCUFF PLATE PER MM 53-11-02 ;APPLIED FAIRING COMPOUND PER AMM 53-11-02. LEAK CHECK GOOD PER AMM 05-51-91 C/W INSPECTION
AFT CARGO DOOR CUT OUT CORNER CASTING FWD SCUFF PLATE CRACKED. ; / [01] INSTALLED REPLACEMENT FWD SCUFF PLATE PER M/M 53-11-02 UP TO APPLYING FAIRING COMPOUND; [02] INSPECTION COMPLETE ON AFT CARGO DOOR FWD SCUFF PLATE INSTALLATION. FINAL BUYOFF STILL PENDING APPLICATION OF FAIRING COMPOUND.; [03] APPLIED FAIRING COMPOUND PER AMM 53-11-02. LEAK CHECK GOOD PER AMM 05-51-91; [04] INSTALLED REPLACEMENT FWD SCUFF PLATE PER M/M 53-11-02 ;APPLIED FAIRING COMPOUND PER AMM 53-11-02. LEAK CHECK GOOD PER AMM 05-51-91 C/W INSPECTION
PANEL 561BB HAS SEVERAL CRACKED FASTENER HOLES ALONG TRAILING EDGE. ; / [01] REMOVED DAMAGE IAW SRM 51-70-05-2R-8; [02] PREPPED AREA FOR INSTALLATION OF REPAIR PLIES.; [03] VERIFIED; [04] REPAIRED DAMAGE FASTENER HOLES PER SRM 51-70-05-2R-8 & TTG8Q006LZY0; [05] INSPECTED WORK PERFORMED IN CORRECTIVE ACTION #4. WILLIAM BOUNLUTAY (TECHNICIAN); 02-OCT-2021 20:31 UTC<BR>REPAIRED DAMAGE FASTENER HOLES PER SRM 51-70-05-2R-8 & TTG8Q006LZY0
LEFT HAND AILERON HAS SEVERAL CORRODED WEIGHTS. 2 ON THE LOWER AND AT LEAST 1 ON UPPER SIDE. ; / [01] REMOVED AND INSTALLED NEW LEFT AILERON ADJUST WEIGHT (UPPER) AND AILERON FIXED WEIGHT (LOWER) AT THE MOST INBOARD POSITION OF BAY NO. 5 PER. SRM 51-60-01-0G-0 AND M.M. 20-50-11; [02] VERIFIED REMOVED AND INSTALLED NEW LEFT AILERON ADJUST WEIGHT (UPPER) AND AILERON FIXED WEIGHT (LOWER) AT THE MOST INBOARD POSITION OF BAY NO. 5 PER. SRM 51-60-01-0G-0 AND M.M. 20-50-11; [03] REMOVED AND INSTALLED NEW LEFT AILERON ADJUST WEIGHT (UPPER) AND AILERON FIXED WEIGHT (LOWER) AT<BR>THE SECOND INBOARD POSITION OF BAY NO. 5 PER. SRM 51-60-01-0G-0 AND M.M. 20-50-11
AFT SVC DOOR LOWER DUST/SWEEPER SEAL BRACKET CRACKED. ; / [01] REMOVED AND REPLACED AFT SVC DOOR LOWER DUST/SWEEPER SEAL BRACKET PER REF. AMM 52-13-31 AND SRM 51-40-02.; [02] REMOVED AND REPLACED AFT SVC DOOR LOWER DUST/SWEEPER SEAL BRACKET PER REF. AMM 52-41-31 AND SRM 51-40-02.; [03] REMOVED AND REPLACED AFT SVC DOOR LOWER DUST/SWEEPER SEAL BRACKET PER REF. AMM 52-41-31 AND SRM 51-40-02.; [04] REMOVED AND REPLACED AFT SVC DOOR LOWER DUST/SWEEPER SEAL BRACKET PER REF. AMM 52-41-31 AND SRM 51-40-02.; [05] REMOVED AND REPLACED AFT SVC DOOR LOWER DUST/SWEEPER SEAL BRACKET PER REF. AMM 52-41-31 AND SRM 51-40-02. C/W INSPECTION
CORROSION ON FLOORBOARD SPLICE TEE AT STA 727D+6 AFT CARGO COMP ; / [01] REMOVED AND REPLACED TEE STRAP PER SRM 51-40-02
BALLFLE AT STA 500A TO 500B RBL22 CRACKED AT AFT FLANGE ; / [01] C/W FASTENER HOLE INSPECTION. PER<BR>SRM 53-30-53-2R-1 REPAIR 1<BR>737 NDT PART 6;51-00-00; PROCEDURE 16; [02] REMOVED AND DISCARDED DAMAGED BAFFLE. OBTAINED NEW BAFFLE FROM STOCK PART # 143A7510-12 AND MODIFIED NEW BAFFLE PER SRM 53-30-53-2R-1; [03] INSTALLED NEW MODIFIED BAFFLE PER SRM 53-30-53-2R-1; [04] INSPECTED INSTALLED NEW MODIFIED BAFFLE PER SRM 53-30-53-2R-1
RT HORZ STAB RIB 129.50 LOWER I/B CORD HAS CRACK INDICATION IN ONE HOLE AFT OF VERTICAL STIFFENER. CUT OUT LOWER CHORD DAMAGE IAW SRM 55-10-09-2R-5. ACCOMPLISHED NDT ON DAMAGE CUT-OUT AREA.. NO DEFECTS NOTED PER NDT PART 6; 51-00-00 PROCEDURE 23. ALL OTHER NDT WAS ACCOMPLISHED ON TASK CARD TTG8Q006JF36. LAID OUT AND PILOT DRILLED RIB AND T-SECTION IAW SRM 55-10-09-2R-5. LAID OUT AND PILOT DRILLED RIB AND T-SECTION IAW SRM 55-10-09-2R-5. C/W INSPECTION. FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-5. INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5. REPAIRED RIB IAW SRM 55-10-09-2R-5.
R/H LOWER HORIZONTAL STAB INSPAR SKIN; STAB STA 193.9 HAS A 1' CRACK 18' FROM THE REAR SPAR.(CRACK ENDS HAVE BEEN MARKED AND 2EA. CUT OUT THE DAMAGED AREA PER SRM 55-01-2R-11.; [02] VERIFIED DAMAGE REMOVAL PER NDT PART 6 51-00-00 PROCEDURE 23. CUT OUT THE DAMAGED AREA PER SRM 55-10-01-2R-11. VERIFIED DAMAGE CUTOUT CORRECTIVE ACTION 1 PER NDT PART 6 51-00-00 PROCEDURE 23 AND SRM 55-10-01-2R-11. MADE REPAIR PARTS PER SRM 55-10-01-2R-11. INSPECTED WORK PERFORMED ON C/A #5. TREATED AND PAINTED REPAIR PARTS PER SRM 55-10-01-2R-11.INSPECTED WORK PERFORMED ON C/A #7. COMPLETED REPAIR IAW SRM 55-10-01-2R-11.
KEEL BEAM ACCESS PANEL 193B FASTENER HOLES ENLARGED. ; / [01] REMOVED AND REPLACED PANEL 193B PER SRM 51-40-02; [02] C/W INSPECTION
R/H LOWER HORIZONTAL STAB INSPAR SKIN; STAB STA 193.9 HAS A 1' CRACK 18' FROM THE REAR SPAR. CUT OUT THE DAMAGED AREA PER SRM 55-01-2R-11. VERIFIED DAMAGE REMOVAL PER NDT PART 6 51-00-00 PROCEDURE 23. CUT OUT THE DAMAGED AREA PER SRM 55-10-01-2R-11. VERIFIED DAMAGE CUTOUT CORRECTIVE ACTION 1 PER NDT PART 6 51-00-00 PROCEDURE 23 AND SRM 55-10-01-2R-11. MADE REPAIR PARTS PER SRM 55-10-01-2R-11. INSPECTED WORK PERFORMED ON C/A #5. TREATED AND PAINTED REPAIR PARTS PER SRM 55-10-01-2R-11. INSPECTED WORK PERFORMED ON C/A #7. COMPLETED REPAIR IAW SRM 55-10-01-2R-11. INSPECTED REPAIR IAW SRM 55-10-01-2R-11.
KEEL BEAM ACCESS PANEL 194E HAS NUMEROUS FASTENER HOLES ELONGATED AND ENLARGED. ; / [01] REMOVED DAMAGE AT ELONGATED HOLES PER SRM 51-70-05-2R-8.; [02] C/W DAMAGE REMOVAL INSPECTION PER SRM 51-70-05-2R-8.; [03] DUPLICATE WRITE UP FAULT WILL BE REPAIRED ON FAULT # TTG8Q006KUA0.; [04] C/W INSPECTION
KEEL BEAM ACCESS PANEL 194E HAS NUMEROUS FASTENER HOLES ELONGATED AND ENLARGED. ; / [01] REMOVED DAMAGE AT ELONGATED HOLES PER SRM 51-70-05-2R-8.; [02] C/W DAMAGE REMOVAL INSPECTION PER SRM 51-70-05-2R-8.; [03] DUPLICATE WRITE UP FAULT WILL BE REPAIRED ON FAULT # TTG8Q006KUA0.; [04] C/W INSPECTION
PANEL 55FB HAS CRACKED SUPPORT BRACKET ; / [01] REMOVED AND REPLACED SUPPORT BRACKET ON PANEL 551FB PER SRM 51-40-02; [02] REMOVED AND REPLACED SUPPORT BRACKET ON PANEL 551FB PER SRM 51-40-02 C/W INSPECTION
FWD CARGO RH TRANSITION ANGLE FROM STA 500A-500D; WL 156.5 AT RBL 24 HAS AREAS OF CORROSION AT FASTENER HOLES. (MARKED) ; / [01] WHILE REMOVING CORROSION ;FOUND AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.[.012] REMOVED; [02] MATCH DRILLED REPLACEMENT TRANSITION ANGLE PER SRM 51-40-02. INSTALLATION ON FAULT 5330-E-16461-NG (CPCP/AD MOC - FWD CARGO COMPARTMENT FLOOR STRUCTURE CORROSION PROTECTION) [TTG8Q004E4SE]; [03] C/W INSPECTION
FWD CARGO RH TRANSITION ANGLE FROM STA 492.4-500A; WL 156.5 AT RBL 24 HAS AREAS OF CORROSION AT FASTENER HOLES. (MARKED) ; / [01] REMOVED CORROSION.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. .022 REMOVE .010 REMAINING; [02] C/W INSPECTION; [03] MATCH DRILLED REPLACEMENT TRANSITION ANGLE PER SRM 51-40-02. INSTALLATION ON FAULT 5330-E-16461-NG (CPCP/AD MOC - FWD CARGO COMPARTMENT FLOOR STRUCTURE CORROSION PROTECTION) [TTG8Q004E4SE]; [04] C/W INSPECTION
PANEL 561CB HAS CRACKED FASTENER HOLES ; / [01] REMOVED DAMAGE PER EA 21-157-02762; [02] VERIFIED REMOVED DAMAGE PER EA 21-157-02762; [03] PERFORMED 250 DEG. PREPREG CURE; PER EA 21-157-02762; [04] VERIFIED PERFORMED 250 DEG. PREPREG CURE; PER EA 21-157-02762; [05] REPAIRED PER EA 21-157-02762
L/H TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 767-787 ; / [01] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [02] PROCURED NEW ANGLE; PART WILL BE INSTALLED ON 5360-E-16462-NG IAW SRM 51-10-02.
L/H TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 727E-747 ; / [01] C; [02] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [03] PROCURED NEW ANGLE; PART WILL BE INSTALLED ON 5360-E-16462-NG IAW SRM 51-10-02.
L/H TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 787-795 ; / [01] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [02] PROCURED NEW ANGLE; PART WILL BE INSTALLED ON 5360-E-16462-NG IAW SRM 51-10-02.
L/H TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 747-767 ; / [01] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [02] PROCURED NEW ANGLE; PART WILL BE INSTALLED ON 5360-E-16462-NG IAW SRM 51-10-02.
RIGHT TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 747-767. REMOVED CORROSION IAW SRM 51-10-02 AREA IS WITHIN LIMITS IAW SRM 53-00-53-1A-2. APPLIED ALODIE IAW AMM 51-21-41 AND APPLIED PRIMER PER AMM 51-21-72. PART INSTALLED ON CARD 5360-E-16462-NG.
PANEL 561AB HAS CRACKED FASTENER HOLES ; / [01] REMOVED DAMAGE PER EA 21-157-02762; [02] VERIFIED REMOVED DAMAGE PER EA 21-157-02762; [03] REPAIRED DAMAGE PER EA 21-157-02762; [04] VERIFIED DAMAGE REPAIRED PER EA 21-157-02762 C/W; [05] APPLIED RESIN SEALER PER SRM 51-70-08.; [06] VERIFIED APPLICATION OF RESIN SEALER PER SRM 51-70-08.; [07] REPAIRED DAMAGE PER EA 21-157-02762; [08] ROBERT TOWNS (TECHNICIAN); 01-OCT-2021 09:23 UTC <BR>REPAIRED DAMAGE PER EA 21-157-02762 INSPECTED; [09] REPAIRED DAMAGE PER EA 21-157-02762; [10] REPAIRED DAMAGE PER EA 21-157-02762
RUDDER BEAM ARM BALANCE WEIGHT CORRODED.(PICS IN ATTACHMENTS) ; / [01] REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER REF CMM55-40-09 / SRM51-60-07; [02] REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER REF CMM55-40-09 / SRM51-60-07
L/H TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 727B+10 ; / [01] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [02] PROCURED NEW ANGLE; PART WILL BE INSTALLED ON 5360-E-16462-NG IAW SRM 51-10-02.; [03] REMOTE HELP
FWD CARGO RH TRANSITION ANGLE FROM STA 420-440; WL 156.5 AT RBL 24 HAS AREAS OF CORROSION AT FASTENER HOLES. (MARKED) ; / [01] REMOVED CORROSION ;FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.REMAINING MATERIAL THICKNESS .027; [02] C/W INSPECTION; [03] MATCH DRILLED REPLACEMENT TRANSITION ANGLE PER SRM 51-40-02. INSTALLATION ON FAULT 5330-E-16461-NG (CPCP/AD MOC - FWD CARGO COMPARTMENT FLOOR STRUCTURE CORROSION PROTECTION) [TTG8Q004E4SE]; [04] C/W INSPECTION
FWD CARGO LH TRANSITION ANGLE FROM STA 500-500D; WL 156.5 AT LBL 24 HAS AREAS OF CORROSION AT FASTENER HOLES. (MARKED) ; / [01] WHILE REMOVING CORROSION ;FOUND AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.[0.0 08] REMOVED; [02] LOCATED AND DRILLED HOLES FROM STA 490 TO STA 500D LBL 24(EXISTING SPLICE). PER SRM 51-40-05; [03] APPLIED ALODINE TO PARTS PER SRM 51-20-01; [04] VERIFIED CORRECTIVE ACTIONS 2 AND 3; [05] MATCH DRILLED REPLACEMENT TRANSITION ANGLE PER SRM 51-40-02; INSTALLATION ON FAULT 5330-E-16461-NG (CPCP/AD MOC - FWD CARGO COMPARTMENT FLOOR STRUCTURE CORROSION PROTECTION) [TTG8Q004E4SE]; [06] C/W INSPECTION.
RIGHT HORIZONTAL STAB. INSPAR RIB ASSY 5 (STAB STA 129.50); STIFFENER 2 CRACKED. ACCOMPLISHED HFEC OF WEB SECTION AFTER VERTICAL RIB REMOVAL FOUND WEB AREA HAS A CRACK INDICATION PER NDT PART 6 51-00-00 PROC. 23 REMOVED FASTENERS FOR RIB REMOVAL TO FOM. REMOVED RIB AND CUT OUT DAMAGE IAW SRM 55-10-09-2R-4. REMOVED RIB AND CUT OUT DAMAGE IAW SRM 55-10-09-2R-4. INSPECTED AND VERIFIED DAMAGE REMOVAL FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-5. OK TO INSTALL REPAIR PARTS. VERIFIED FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-5. INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5. INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5. REPAIRED RIB CRACK IAW SRM 55-10-09-2R-5.
EMERGENCY LIGHT ON RT FWD OF AFT CARGO INOPERABLE. SA-M 767 NR H19884-1 RELAMPED EMERGENCY LIGHT, PER M/M 35-51-01. OPERATIONS CHECK GOOD.
FLAPS DID NOT MOVE WHEN FLAPS 5 SELECTED; FLAPS MOVED TO 15 IN ALTERNATE. CFR ROLLED. /
SUPPLEMENTAL INFORMATION: FLAP HANDLE MOVED TO POSITION 5 FLAP GAUGE INDICATED 0 / PERFORMED FIM 27-51-TASK 836. NO FAULTS FOUND ON FSEU. TRAILING EDGE FLAP TEST PERFORMED IAW AMM 27-51-00. NO DEFECTS NOTED. NO PREVIOUS HISTORY; AC OK FOR SERVICE
FLAPS DID NOT MOVE WHEN FLAPS 5 SELECTED; FLAPS MOVED TO 15 IN ALTERNATE. CFR ROLLED. /
FLAPS DID NOT MOVE WHEN FLAPS 5 SELECTED; FLAPS MOVED TO 15 IN ALTERNATE. CFR ROLLED /
FLAPS DID NOT MOVE WHEN FLAPS 5 SELECTED; FLAPS MOVED TO 15 IN ALTERNATE. CFR ROLLED. /
SUPPLEMENTAL INFORMATION: STIFFENER END IS CRACKED AT KRAS 226 / INSTALLED NEW STIFFNER AT INBD FIXED L/E KRAS 226 TO KRAS 206 PER SRM 51-40-02-0G-0 AND BOEING DWG # 116A4008 92385U 03/31/20
STIFFENER END IS CRACKED AT KRAS 226 /
L1 DOOR ESCAPE SLIDE GIRT BAR RETAINER CLIP FELL OFF. / INSTALLED RETAINER CLIP PER AMM.
EMERGENCY EXIT SIGN MID CABIN CEILING BROKEN. / R&R SIGN PER AMM.
DECLARED EMERGENCY-------------------------------------------------FLAPS 1 DEGREE AND 2 DEGREE WERE SELECTED AND NEITHER LEADING EDGE DEVICES OR THE TRAILING EDGE FLAPS EXTENDED. ALTERNATED FLAP EXTENSION WAS USED. / R&R R/H FLAP POSITION INDICATOR IAW AMM.
DECLARED EMERGENCY-------------------------------------------------FLAPS 1 DEGREE AND 2 DEGREE WERE SELECTED AND NEITHER LEADING EDGE DEVICES OR THE TRAILING EDGE FLAPS EXTENDED. ALTERNATED FLAP EXTENSION WAS USED. / R&R R/H FLAP POSITION TRANSMITTER IAW AMM.
EMERGENCY EXIT SIGN MID-CABIN LOOSE. / RE-ATTACHED SIGN IAW AMM.
***CORROSION*** FIRST OFFICER'S FWD INBOARD AND OUTBOARD SEAT TRACKS HAVE CORROSION / REMOVED AND REPLACED FO'S FWD INBOARD AND OUTBOARD SEAT TRACKS IAW AMM 25-11-11-400-801 STEPS 3.D.(2)(3)(D)(4-8) AND SOPM 20-50-01 56572U 06SEPT19 PRIOR TO REPLACEMENT OF FO'S SEAT TRACKS; EVALUATED PER AMM 25-11-11-601; FOUND NO AMM LIMITS FOR CORROSION.
***CORROSION*** CAPTAINS'S FWD INBOARD AND OUTBOARD SEAT TRACKS HAVE CORROSION / REMOVED AND REPLACED CAPTS FWD INBOARD AND OUTBOARD SEAT TRACKS IAW AMM 25-11-11-400-801 STEPS 3.D.(2)(3)(D)(4)(5)(6-8) AND SOPM 20-50-01 56572U 06SEPT19 PRIOR TO CAPTAINS SEAT TRACK REPLACEMENT; EVALUATED PER AMM 25-11-11-601; FOUND NO AMM LIMITS FOR CORROSION.
LT OVERWING EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED BULBS PER AMM.
R1 DOOR EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED BULBS PER AMM.
BATTERY CHARGER M1673 PRESS TO TEST BUTTON INOP. R&R EMERGENCY LIGHTS POWER SUPPLY PER AMM.
CLIP AT COMMON TO CREASE BEAM WEB CRACKED AT BS. 292, RBL 54. R & R THE CLIP PER SRM AND DWG.
R1 DOOR STUB FRAME CRACKED AT FASTENER COMMON TO MOPSILL AT BS. 294, RBL 54. R&R STUB FRAME PER SRM AND DWG.
RT HORIZONTAL STABILIZER STA 129.50, INSPAR RIB CRACKED AT 1ST STIFFENER. REPAIRED 1ST STIFFENER IAW SRM.
FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS. 460 TO BS. 480, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.
FWD CARGO BAY AFT SCUFF PLATE IS CRACKED / REMOVED AND REPLACED NEW FCB AFT SCUFF PLATE PN# 654A0004-338; PO# 758415 IAW SRM 51-40-02: IAW AMM 53-11-02-020-801 AND IAW AMM 53-11-02-420-801
FWD CARGO BAY FWD SCUFF PLATE IS CRACKED / ACCOMPLISHED FCB FWD SCUFF PLATE REPAIR AND RE-INSTALLED IAW EA #1-A53-2076 REV 11
ACB AFT CAP STRIP IS BROKEN / REMOVED AND REPLACED AFT CAP STRIP ACB IAW SRM 57-40-02-0G-0 AND IPC 25-52-10-02.
AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE CORRODED AT BS. 947, BETWEEN LBL 11 TO RBL 22. R&R ANGLE IAW DWG AND SRM.
***CORROSION*** IN MULTIPLE PLACES IN ACB ON L/H FLOOR TO SIDEWALL SUPPORT STA 727-847 LBL 22 WL 158 / REMOVED DAMAGE AT ACB FLOOR TO SIDEWALL SUPPORT BS727-727E+10 1' X 1' X .003' FROM AN ORIGINAL THICKNESS OF .040' FOUND TO BE WITHIN LIMITS; IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT BS 727E+10-847 WITH THE REPAIR SPLICE LOCATED AT BS727E+10 IAW SRM 53-00-53-2R-5 AND DWG# 146A7500 AND DWG# 146A7502.
FLOOR TRACK AROUND FASTENER HOLE CORRODED AT BS 787+11, RBL 14. R&R TRACK SECTION PER SRM AND EA.
AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO 787+7, RBL 22. R&R SHIELD IAW SRM & DWG.
FRAME TO STRINGER GUSSET SUPPORT CRACKED AT BS. 500D, STR. 21L. R&R SUPPORT PER SRM AND DWG.
FRAME TO STRINGER GUSSET SUPPORT CRACKED AT BS. 500D, STR. 19L. / R&R SUPPORT PER SRM & DWG.
FRAME TO STRINGER GUSSET SUPPORT CRACKED AT BS. 500D, STR. 19R. / R&R STRINGER GUSSET SUPPORT PER SRM AND DWG.
AFT CARGO BAY ON UNDERSIDE OF INTERCOSTAL TO SHIELD ANGLE CORRODED BETWEEN BS. 767 TO BS. 787, RBL 20. R&R ANGLE IAW SRM AND DWG.
FLOOR SPLICE CORRODED AT BS. 887, BETWEEN RBL 22 TO LBL 10. R&R FLOOR SPLICE IAW SRM.
***CORROSION*** B.S. 986.5 FLOOR BEAM; UPPER SURFACE; AT R.B.L. 30-40; W.L. 208.1. / CORROSION ON BS 986. 5 FLOOR BEAM UPPER SURFACE AT RBL 30-40; WL 208.1 WAS REPAIRED IAW ATS ER 19-04365 REV IR DATED 20AUG19 AND EA 1-753-35433 REV IR
AFT CABIN FLOOR PANEL 241XF DAMAGED, BETWEEN BS. 887 TO BS. 1016, UPPER SKIN. / REPAIRED FLOOR PANEL 241XF IAW SRM.
RT HORIZONTAL STABILIZER STA 129.50, INSPAR RIB CRACKED AT 3RD STIFFENER. REPAIRED 3RD STIFFENER IAW SRM.
FWD PASSENGER CABIN FLOOR PANEL 221BF HAS BROKEN AFT O/B CORNER / FWD PASSENGER CABIN FLOOR PANEL 221BF WITH BROKEN AFT O/B CORNER WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA.9.A(1).
FORWARD PASSENGER CABIN FLOOR PANEL 222DF DAMAGED BETWEEN BS. 270 TO BS. 420, UPPER SURFACE SKIN. / REPAIRED FLOOR PANEL 222DF IAW SRM.
FORWARD PASSENGER CABIN FLOOR PANEL 222BF DAMAGED, BETWEEN BS. 270 TO BS. 420 UPPER SURFACE SKIN. / REPAIRED FLOOR PANEL 222BF IAW SRM.
FORWARD PASSENGER CABIN FLOOR PANEL 221DF DAMAGED, BETWEEN BS. 270 TO BS. 420 UPPER SURFACE SKIN. / REPAIRED FLOOR PANEL 221DF IAW SRM.
AFT CABIN FLOOR PANEL 242VF DAMAGED, BETWEEN BS. 887 TO BS. 1016, SKIN INBOARD EDGE LOWER SURFACE. REPAIRED FLOOR PANEL 242VF IAW SRM.
AFT CABIN FLOOR PANEL 242RF DAMAGED, BETWEEN BS. 887 TO BS. 1016, UPPER SKIN ON AFT EDGE. / REPAIRED FLOOR PANEL 242RF IAW SRM.
AFT CABIN FLOOR PANEL 241AEF DAMAGED, BETWEEN BS. 887 TO BS. 1016. SKIN ON FORWARD EDGE. / REPAIRED FLOOR PANEL 241AEF IAW SRM.
RT WING TRAILING EDGE PANEL SUPPORT WIGGLE PLATE CRACKED IN PHENOLIC COMMON AREA JUST INBOARD OF #8 FLAP SUPPORT WS. 432. R&R WIGGLE PLATE ASSEMBLY IAW SRM.
R1 DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. REPAIRED DOOR IAW WO.
L/H BS. 663 VAPOR BARRIER CRACKED MID SPAN. REPAIRED VAPOR BARRIER IAW SRM.
VERTICAL PRESSURE WEB CRACK AT BS 663 LBL 32 WL 188. REPAIRED IAW SRM.
EMERGENCY LIGHT BATTERY M1673 FAILED CAPACITY TEST. R&R BATTERY PER MM.
EMERGENCY LIGHT BATTERY M1670 FAILED CAPACITY TEST. R&R BATTERY PER MM.
LT OVERWING EXIT LIGHT INOP. RELAMPED LAMP PER MM.
NR 1 ENG LPT GUIDE VANE SECTION CRACKED. R&R NR 1 ENG PER MM.
R1 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.
STIFFENER EXTENSION AT STA 663; RBL 25.00 CRACKED. / INSTALLED STIFFENER EXTENSION AT STA 663; RBL 25.00 PER SRM 51-40-02 AND DRAWING NUMBER 111A1000.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITON. REPOSITIONED GIRT IAW MT.
PASSENGER CABIN FLOOR STRUCTURE;STA 540 EXPANSION JOINT CRACKED RBL 0-25' AT INBD FASTNER / REMOVED AND REPLACED FLOOR BREAK AT STA 540 RBL 0-25 REF DRW# 143A0060 REV -
PASSENGER CABIN FLOOR STRUCTURE;STA 540 EXPANSION JOINT CRACKED LBL -25' AT INBD FASTNER / REMOVED AND REPLACED FLOOR PANEL BREAK STA 540 LBL O-25 REF DRW #1430060 REV-
L1 DOOR SLIDE LOOSE. SECURED THE SLIDE IAW MT.
EMERGENCY LIGHT BATTERY M1670 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
EMERGENCY LIGHT BATTERY M1668 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
EMERGENCY LIGHT BATTERY M1674 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
EMERGENCY LIGHT BATTERY M1675 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
EMERGENCY LIGHT BATTERY M1669 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
EMERGENCY LIGHT BATTERY M1673 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
EMERGENCY LIGHT BATTERY M1672 FAILED CAPACITY TEST. R & R BATTERY IAW MM.
INTERCOSTAL CORRODED, BETWEEN BS 747 - 767, UNDER RT TRANSITION ANGLE. R & R INTERCOSTAL IAW SRM.
AFT GALLEY RT FLOOR WEB CRACKED AT BS 986.5, RBL 45. R & R WEB IAW SRM.
AFT CARGO FLOOR SUPPORT CORRODED, AT BS 812, RBL 20. R & R SUPPORT IAW SRM & DWG.
AFT CARGO FLOOR SUPPORT, CORRODED AT BS 819, RBL 20. R & R SUPPORT IAW SRM & DWG.
AFT CARGO FLOOR PANEL SPLICE STRAP, CORRODED AT BS 727D+5. REPAIRED STRAP IAW SRM.
AFT GALLEY FLOORBEAM T CAP, CORRODED AT BS 986, RBL 40. REPAIRED T CAP IAW SRM.
RIGHT HORIZONTAL STABILIZER STAB STATION 92.70, FWD INSPAR RIB CRACKED AT FWD SPAR. REPAIRED RIB IAW EA.
AFT CARGO DOOR THRESHOLD WEB CORRODED, BETWEEN BS 794 - 847. R & R WEB IAW SRM & DWG.
FLOOR SUPPORT CORRODED AT BS 827, RBL 20. R & R SUPPORT IAW SRM & DWG.
AFT GALLEY FLOORBEAM, CORRODED AT BS 986, RBL 6. REPAIRED BEAM IAW EA.
AFT GALLEY FLOORBEAM, CORRODED AT BS 986, LBL 43. REPAIRED BEAM IAW EA.
AFT CARGO FLOOR PANEL SPLICE STRAP CORRODED AT BS 887. R & R STRIP IAW SRM.
R2 DOOR Z ANGLE CORRODED, BETWEEN BS 945 - 986. R & R Z ANGLE IAW SRM.
AFT GALLEY FLOOR WEB CORRODED, BETWEEN BS 1016 - 1030, RBL 3. R & R WEB IAW SRM.
L1 DOOR WET AREA INTERCOSTAL CRACKED AT BS 322, LBL 46. R & R INTERCOSTAL IAW SRM.
R1 DOOR SLIDE CONTAINER INADVERTENTLY FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. INSTALLED SLIDE IAW MT.
RIGHT OVERWING EXIT SIGN LENS LOOSE. SECURED LENS IAW SIP.
DIVERSION, HYD B ENG DRIVEN PUMP LOW PRESS ILLUMINATED IN FLIGHT. R & R NR ENG DRIVEN HYD PUMP IAW MM.
EXTERNAL ELEC PANEL DOOR CUT OUT CRACKED ON THE BOTTOM FWD CORNER. REPAIRED CUT OUT IAW EA.
RIGHT OVERWING EXIT SIGN LOOSE. SECURED EXIT SIGN IAW MM.
RIGHT OVERWING EMER ROW EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
LEFT EMERGENCY EXIT LIGHT COVER LOOSE. R & R COVER ASSEMBLY IAW MM SIP.
LT WING CTR SECTION REAR SPAR VAPOR WEB CRACKED IN BAY 7L AT LBL 32. REPAIRED WEB IAW EA.
FRAME CRACKED AT STATION 540, BETWEEN STRINGER 22R TO STRINGER 23R. REPAIRED FRAME IAW EA.
AFT CARGO LT SIDE PLATE CORRODED BETWEEN STATION 727E TO STATION 767, LBL 22. REPAIRED PLATE IAW SRM.
RT HORIZONTAL STABILIZER LOWER SKIN CRACKED STATION 101.5 10.5" AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER LOWER SKIN CRACKED STATION 97.5 AT REAR SPAR. REPAIRED SKIN IAW SRM.
LT EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW WDM & AMM.
LT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.
RT EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW WDM & AMM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.
LT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
AFT GALLEY, LOWER LEFT EMERGENCY EXIT SIGN & RT OVERDOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED AFT LEFT CHARGER ASSY IAW MM POS A/LH TAG NO. P/N OFF/ON D717-02-030 S/N OFF 33415 S/N ON NSN
EMERGENCY LIGHTS AT SEATS 17/19 A-C WILL NOT LIGHT. REMOVED AND REPLACED BATTERY PACK OVERRIDE PANEL PER MM, OPS CHECK NORMAL.
L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.
AFT EEPLS INOP. REMOVED AND REPLACED FUSE PER MM.
EEPLS LENS MISSING AT ROW 20. INSTALLED LENS PER MM.
LEFT EEPLS INOP BETWEEN ROW 20 TO 23. REMOVED AND REPLACED BATTERY PACK IAW MM.
LEFT EEPLS COVER MISSING AT ROW 11. INSTALLED COVER PER M/M.
EEPLS LENS MISSING AT ROW 3. INSTALLED LENS PER MM.
LT EMERGENCY EXIT LIGHT BROKEN AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER M/M.
CENTER EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT PER SRM.
LT EEPLS LENS MISSING AT ROW 11. INSTALLED LENS PER MM.
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS BROKEN BETWEEN ROW 6 TO ROW 10. REMOVED AND REPLACED LENS IAW MM.
DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.
DECLARED EMERGENCY - DURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO 1590. NR 1 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON AS WELL AS MASTER CAUTION AND HYDRAULIC ANNUNCIATOR LIGHT. REMOVED AND REPLACED FEEL COMPUTER AND ENGINE DRIVEN HYDRAULIC PUMP PER MM.
R1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER EA.
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.
LT EEPLS COVER DAMAGED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS MISSING FWD END CAP. INSTALLED END CAP PER MM.
EEPLS LENS BROKEN FROM TRACK. REMOVED AND REPLACED LENS PER MM.
ABORTED TAKEOFF DUE TO LOUD BANG HEARD AND AIRPLANE STARTED TO TURN LEFT. NR 1 ENGINE SHOWED ENGINE FAILED ON EGT N1'S WAS APPROX 84 PERCENT AND LOW GROUND SPEED. REMOVED AND REPLACED NR 1 ENGINE PER MM.
FOUND EGRESS LIGHT UNSECURED AT ROW 1 SEAT A. REMOVED AND REPLACED LIGHT ASSY PER MM.
FOUND EGRESS LIGHT LOOSE AT ROW 1. REPAIRED LIGHT ASSY PER MM.
FOUND FWD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.