N289CT
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2021-05-21 – 2021-05-21 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2021-05-21 – 2021-05-21 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FORWARD ENTRY SLIDE HARD TO ARM AND PART OF SLIDE FELL OUT. RE-ATTACHED VELCRO AT BOTTOM OF FWD ENTRY DOOR SLIDE IAW AMM 25-66-01
PANEL 621PB CRACKED AT FWD I/B END. <[01] CRACK AT FWD I/B END OF PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6.; [02] VERIFIED CORRECTIVE ACTION #1.
VERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02-0G-0 AND DWG #176A3101 SHEET 4 REV-.
CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25' FROM FWD EDGE; 0.6' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 25' FROM FWD EDGE IAW SRM 55-10-01-2R-11 REPAIR 11.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
CRACKED INTERCOSTAL BS 312-328 RBL 30 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 RBL 30 WL 208.;[02] ALL TASKS STEPS COMPLETED;[03] JOB COMPLETE
CRACKED INTERCOSTAL BS 312-328 LBL45 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL BS 312-328 LBL45 WL 208.;[02] ALL TASK STEPS COMPLETED;[03] JOB COMPLETE
CORROSION ON FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE BS 320 AND 338 LBL 56 WL 208. <[01] REMOVED AND REPLACED FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
CRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. <[01] REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW AT BS 380-400 RBL 40 WL 208. VERIFIED SRM 53-00-04-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE ON CRACKED INTERCOSTAL BS 380-400 RBL 40 WL 208. REMOVED CRACKED INTERCOSTAL AT BS 380-400 RBL 40 WL 208 IAW SRM 51-40-02 INSTALLED NEW INTERCOSTAL AT BS 380-400 RBL 40 WL 208 IAW SRM 51-40-02; BOEING DWG#143A5400 REV:A PART FOUND TO BE OUT OF LIMITS DUE TO CRACK BEING IN THE HOLE IAW SRM 53-00-04-1A-1 TREATED AND PRIMED IAW SRM 53-00-04-1A-1 PARAGRAPH 2. E. (1) (2); [02] VERIFIED.
CORROSION ON STRAP BS 1028 RBL 18 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 18 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
CORROSION ON STRAP BS 1016-1026 RBL 3 WL 208. <[01] REMOVED AND REPLACED NEW STRAP BS 1016-1026 RBL 3 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730 REV:C; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
CORROSION ON FWD ENTRY DOOR MOP SILL BS 303 LBL 56 WL 208.<[01] REMOVED AND REPLACED FED MOPSILL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.
CORROSION ON STRAP BS 1017 LBL 3 WL 208. <[01] REMOVED AND REPLACED STRAP BS1017 LBL3 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV:B; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
FOLDING AND PEELING OFF INTERNAL FUSELAGE SKIN ON UPPER-FWD COUNTER FRAME OF R1 DOOR; DIMENSIONS OF 3' LONG; 1' DEEP; AND 3/32' PEELING OFF.<[01] DURING INSPECTION STUB FRAME FOUND CRACK AND GENERATED CCN TTG8Q00YSN5X THEREFORE DISCREPANCY REPORTED BEING NULL DUE TO STUB FRAME REQUIRED REPLACEMENT OF THE PART.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
CRACK FOUND ON R1 DOOR STUB FRAME 0.7' ABOVE SEAL DEPRESSOR; 0.6' FWD FROM DOOR CUT OUT. L: 0.5' MARKED. <[01] REMOVED CRACKED R1 DOOR STUB FRAME AND REPLACED ALL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV: D; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
CORROSION ON BS 303 FRAME LBL 56 WL 208. <[01] REPAIRED CORROSION ON BS 303 FRAME LBL 56 WL 208 PER EA 25-153-00457-WIP1; [02] VERIFIED ITEM 1.
CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156 <[01]. CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 767 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500 ID: 0113 REV: -
AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED <[01]. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.
CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156 <[01]. CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE L/H FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500 ID: 0113 REV: -; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED <[01]. FWD CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1.
CABIN FLOOR PANEL 232AF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 232AF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.; [02] VERIFIED CORRECTIVE ACTION #1.
CABIN FLOOR PANEL 221FF TOP SURFACE IS DELAMINATED. <[01] CABIN FLOOR PANEL 221FF TOP SURFACE WITH DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
CABIN FLOOR PANEL 241ACF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241ACF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
CABIN FLOOR PANEL 241UF HAS TOP SURFACE DELAMINATION. <[01] CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-0.; [02] ITEM 1 SHOULD READ: CABIN FLOOR PANEL 241UF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H SHIELD; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H SHIELD; BS 767 TO BS 794 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A7500 ID: 0031 REV: -;[02] CORRECTION ACTION 1. <BR><BR>CORROSION ON AFT CARGO BAY R/H SHIELD; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE R/H SHIELD; BS 767 TO BS 794 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A0081 ID: 0031 REV: -;[03] VERIFIED CORRECTIVE ACTION 2. CARD COMPLETE.
AFT CARGO BAY CARGO TRACK IS CRACKED BS747 AND BS727E RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS727+4 - BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500 REV:- ; DWG 147A7500 REV:- AND DWG 146A0061 REV:A;[02] REPAIRED AS PER SRM 53-00-53-2R-3 AND EA 25-153-00471.
CORROSION ON INNER CHORD AT BS 698 RBL 63 WL 208. (MARKED) <[01] REFER TO FAULT TTG8Q00YQ2WS WHERE EA 25-153-00417 WAS ADDED AS A SUBTASK; [02] VERIFIED CORRECTIVE ACTION 1.
CABIN FLOOR PANEL 231JF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231JF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0; [02] CORRECTION TO ITEM 1: FABRICATED NEW CABIN FLOOR PANEL 231JF IAW SRM 53-00-50-2R-0.; [03] VERIFIED CORRECTIVE ACTION ITEM 1 AND 2.
CABIN FLOOR PANEL 242DF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242DF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-150 IAW SRM 51-10-02-0G-0 PARA 9.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
CABIN FLOOR PANEL 241EF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 241EF WITH DISBONDED TOP SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.; [02] VERIFIED CORRECTIVE ACTION #1.
CABIN FLOOR PANEL 232FF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 232FF DISBONDED TOP SURFACE REPAIRED IAW SRM 53-00-50-2R-0.; [02] CORRECTION TO ITEM 1: FABRICATED NEW CABIN FLOOR PANEL 232FF IAW SRM 53-00-50-2R-0.; [03] VERIFIED CORRECTIVE ACTION ITEM 1 AND 2.
CABIN FLOOR PANEL 242BF HAS DELAMINATED TOP SURFACE. <[01] REPLACED DAMAGED 242BF FLOOR PANEL WITH SERVICEABLE PANEL P/N:144A5810-149 IAW SRM 51-10-02-0G-0 PARA 9.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
CABIN FLOOR PANEL 231ZF HAS DISBONDED TOP SURFACE. <[01] CABIN FLOOR PANEL 231ZF; WITH DISBONDED TOP SURFACE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION #1.
PANEL 621YB CRACKED ON O/B FWD. END <[01] PANEL 621YB WITH CRACK ON O/B FWD END WAS REPAIRED PER SRM 51-70-05-2R-6.
CABIN FLOOR PANEL 231MF HAS DISBONDED TOP SURFACE. <[01] 231MF FLOOR PANEL DISBOND DAMAGE ON UPPER AND LOWER SURFACE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]. ATTACHED CURE SHEETS TO THIS FAULT.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
CABIN FLOOR PANEL 242AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 242AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.
CABIN FLOOR PANEL 231XF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231XF; WITH TOP SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
CABIN FLOOR PANEL 241AF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241AF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0127.; [02] VERIFIED CORRECTIVE ACTION #1.
CABIN FLOOR PANEL 231YF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 231YF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
CABIN FLOOR PANEL 241BF HAS DELAMINATED TOP SURFACE. <[01] CABIN FLOOR PANEL 241BF WITH DELAMINATED TOP SURFACE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.
CABIN FLOOR PANEL 232RF HAS DELAMINATED TOP SURFACE. <[01] DAMAGE TO CABIN FLOOR PANEL 232RF WAS BEYOND ECONOMICAL REPAIR; FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION 1.
CORROSION ON STRAP AT MID CABIN BS696 RBL67 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE STRUCTURE ID/DRAWING'; [03] REMOVED CORROSION ON STRAP AT MID CABIN BS696 RBL67 WL203. BLEND WAS 1'X.5'. BLEND IS OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE. EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 07/25; [04] REMOVED CORROSION ON STRAP AT MID CABIN BS696 RBL67 WL203. BLEND WAS 1'X.5'. BLEND IS OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE. EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 07/25 REFER TO FAULT TTG8Q00YQ32J WHERE 25-153-00427 WAS ADDED AS A SUBTASK; [05] VERIFIED COMPLETION. CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
CORROSION ON STRAP AT MID CABIN BS703 RBL64 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE STRUCTURE ID/DRAWING'; [03] REMOVED CORROSION ON STRAP AT MID CABIN BS703 RBL64 WL203. BLEND WAS 1'X.6'. BLEND IS OUT OF LIMITS DUE TO NO LIMITS IN THE SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE. EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 07/25; [04] REMOVED CORROSION ON STRAP AT MID CABIN BS703 RBL64 WL203. BLEND WAS 1'X.6'. BLEND IS OUT OF LIMITS DUE TO NO LIMITS IN THE SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE. EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 07/25 REFER TO FAULT TTG8Q00YQ32J WHERE 25-153-00427 WAS ADDED AS A SUBTASK; [05] VERIFIED COMPLETION CORRECTIVE ACTION 4 AND MEASUREMENT TABLE.
CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] EDIT: 'DID NOT PROVIDE STRUCTURE ID/DRAWING'; [03] REMOVED CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. BLEND WAS 1'X.4'. BLEND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW WIP1; [04] REMOVED CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. BLEND WAS 1'X.4'. BLEND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02; [05] REMOVED CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203. BLEND WAS 1'X.4'. BLEND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE. EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 07/25 [06] REMOVED CORROSION ON STRAP AT MID CABIN BS692 RBL62 WL203 PER EA 25-153-00427-WIP1; ACCOMPLISHED ON TASK TTG8Q00YSS6F.; [07] VERIFIED CORRECTIVE ACTION #6.
CORROSION ON INNER CHORD AT MID CABIN BS696; BS704 RBL63 WL208. MARKED <[01] REMOVED CORROSION IN MULTIPLE AREAS AREAS BS695 RBL63 WL 208 BLEND WAS .080'X.070'X.003; BS696 RBL63 WL 208 WAS .009'X.007'X.003'; BS704 RBL63 WL 208 WAS 1'X.080'X.004'; BS 706 RBL63 WL 208 WAS 1.1'X.070'X.005'. BLENDS WERE OUT OF LIMITS DUE TO MORE THAN 3 FASTENERS IN A GROUP OF 10 REMOVED IAW SRM 53-40-13-1A-1 FIGURE 103 DETAIL F. DEPTH GAUGE ID ATS1225 DUE 07/2025 AND MAINTENANCE WAS ACCOMPLISHED ON STEPS 1-5 AND FAULT#TTG8Q00YSN0V; [02] VERIFIED RII ITEMS COMPLETE; [03] TASK COMPLETE.
CORROSION ON STRAP AT MID CABIN BS707 RBL63 WL203. MARKED <[01] REJECTED; AMT REQUEST FOR NDI TO VERIFY REMAINING THICKNESS OF PART. AMT DID NOT PROVIDE STRUCTURE ID/DRAWING AS REQUIRED IAW 737 NDTM PART 4; 51-00-00; PROC 2 STEP 4. C.; [02] REMOVED CORROSION ON STRAP AT MID CABIN BS707 RBL63 WL203. BLEND WAS 1'X.5'. BLEND IS OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE. EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 07/25; [03] REMOVED CORROSION ON STRAP AT MID CABIN BS707 RBL63 WL203. BLEND WAS 1'X.5'. BLEND IS OUT OF LIMITS DUE TO NO LIMITS IN SRM. TREATED AND PRIMED BLENDED AREAS IAW SOPM 20-41-02. UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2. SEE ATTACHED FILE 'REFER TO FAULT TTG8Q00YQ32J WHERE 25-153-00427 WAS ADDED AS A SUBTASK; [04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
R/H A/C BAY FWD PNEUMATIC APU BLEED AIR TO PACK VALVE DUCT MOUNT BRACKET CRACKED JUST OTBD OF KEEL BEAM BOX STRUCTURE. (SEE PIC)<[01] REMOVED AND REPLACED PER AMM 20-50-11.
RIGHT MLG WHEEL WELL; FWD. BULKHEAD; ABOVE BOOST PUMP; BRACKET CRACKED<[01] REMOVED AND REPLACED RIGHT MLG WHEEL WELL FWD BULKHEAD; ABOVE BOOST PUMP BRACKET IN REF SRM 51-10-02 AND 51-40-02.
R1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE PER AMM 52-41-11.
R1 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED R1 DOOR ASSIST HANDLE PER AMM 52-41-31.
LEFT MLG CENTER GEAR DOOR CRACKED AT FORWARD ATTACH POINT<[01] REMOVED LEFT MLG CENTER AND LOWER/INNER DOOR ASSEMBLY IN REF AMM 32-13-11.
FA REPORTS EMERG. BULLNOSE LIGHT LENS MISSING AT 12 ABC<[01] OK TO CONTINUE ON MEL 33-15-02 SP-1;[02] 01 - REMOVED AND REPLACED PER [AMM 33-51-03-960-803-NG (EMERGENCY AISLE LIGHT (EAL) - LENS REPLACEMENT - PERMANENT)]REPLACED MISSSING EMERG LIGHT LENSE AT 12 ABC. I/A/W AMM 33-51-03
EMERGENCY SLIDE GIRT BAR UNABLE TO BE ARMED AT FORWARD SERVICE ENTRY DOOR.<[01] REPOSITIONED FWD SERVICE DOOR SLIDE GIRT BAR FLAP REF AMM 25-6601.
CENTER ISLE EMERGENCY EXIT SIGN COVER FALLING DOWN<[01] R&R CENTER ISLE EMERGENCY SIGN LIGHT ASSY PER AMM 33-51-01.
AFT SERVICE DOOR SLIDE GIRT HANGS TOO LOW/VELCRO NOT ATTACHED.<[01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT PER AMM 25-66-01
NOSE LANDING GEAR HAS CORROSION ON AFT SIDE OF GEAR JUST ABOVE UPPER STEERING PLATE. (SEE ATTACHED PICTURES).<[01] CLEANED AND REMOVED PAINT ON AFT SIDE OF NLG JUST ABOVE STEERING PLATE TO IDENTIFY WHERE CORROSION REACHED IAW AMM 20-10-34.;[02] REMOVED AND REPLACED NLG ON TTG8Q004MQUG. RAISED A FAULT FOR THE OFF UNIT NLG SN# T9507Y0175 FOR VENDOR TO REPAIR. SEE TTG8Q00MX5V9 FOR FAULT RAISED AGAINST THE DISCREPANT NLG.
NOSE LANDING GEAR RH AXLE HAS CORROSION I/B OF SPACER AT THE 5 OCLOCK POSITION.<[01] REMOVED AND REPLACED NLG ON TTG8Q004MQUG. RAISED A FAULT FOR THE OFF UNIT NLG SN# T9507Y0175 FOR VENDOR TO REPAIR. SEE TTG8Q00MX5VF FOR FAULT RAISED AGAINST THE DISCREPANT NLG.
EMX LIGHT BATT PACK M01673 FAILED CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01673 PER AMM 33-51-06
EMX LIGHT BATT PACK M01672 FAILED CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01672 PER AMM 33-51-06
EMX LIGHT BATT PACK M01668 FAILED CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01668 PER AMM 33-51-06
EMX LIGHT BATT PACK M01670 FAILED CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06
EMX LIGHT BATT PACK M01674 FAILED CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01674 PER AMM 33-51-06
EMX LIGHT BATT PACK M01675 FAILED CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01675 PER AMM 33-51-06
194BR ACCESS PANEL #5 AFT TRACK BROKEN<[01] REMOVED AND REPLACED PANEL 194BR IAW AMM 53-51-21 AND AMM 20-50-11.
PASSENGER CABIN OWE CEILING EMERGENCY EXIT SIGN IS LOOSE<[01] RE-SECURED PASSENGER CABIN OWE CEILING EMERGENCY EXIT SIGN; PER AMM 33-51-01
FWD ENTRY DOOR GIRT BAR LOOSE IN BRACKET<[01] ADJUSTED FWD ENTRY DOOR GIRT BAR RETAINER CLIPS TO CONFORM FIGURE 602: SHEET 4 PER AMM 25-66-01.
O/H E/E AISLE SIGN NOT SECURE AT 11ABC/12DEF<[01] SECURED OH E/E AISLE SIGN AT 11 ABC/ 12DEF PER AMM 33-51-01
EMERG. EXIT LIGHT ON BULLNOSE AT ROW 14 ABC IS OUT<[01] REMOVED AND REPLACED BAD BULB AND PERFORMED GOOD OP TEST AS PER AMM33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION 1
FLIGHT DECK FLOOR REPAIR - CRACK NOTED IN THIRD LAYER OF FASTENER HOLE AT BS 254 LBL 4 WL 208. MARKED LOCATION.<[01] REMOVED FITTING SUPPORT BS 251 BETWEEN LBL 3.8 - LBL 15.3 FLIGHT DECK FLOOR WEB PER SRM 51-40-02;[02] LOCATED AND DRILLED NEW STIFFENER P/N:141A5136-11; LOT#1519516-1 AT BS 252; WL 208 BETWEEN LBL 3.8 AND LBL 15.3 PER SRM 51-40-05 AND DWG#141A5100 SH 158. OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION STEP 2. VERIFIED OK TO INSTALL.;[04] INSATALLED NEW STIFFENER P/N:141A5136-11 BS 252; WL 208 BETWEEN LBL 3.8 AND LBL 15.3 PER SRM 51-40-02 AND DWG#141A5100 SH 158.;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] COMPLETED STEP 2.;[07] VERIFIED STEP 2.;[08] STEP 1 COMPLETED;[09] VERIFIED STEP 1.;[10] REPAIRED BY REPLACEMENT STIFFENER P/N 141A5136-11 IAW SRM 51-10-02-0G-0 PARAGRAPH 9
LT WING L/E PANEL 521ZB O/B FWD CORNER IS CRACKED<[01] IDENTIFIED PANEL 521ZB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 2; SHEET1; TABLE 2; ITEM [1]. <BR><BR>CLEANED PANEL AND REMOVED FINISH ON TOOL SIDE TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. AND D<BR><BR>VISUAL INSPECTION FOUND DAMAGE AT O/B FWD CORNER AND ADDITIONAL DAMAGE AT I/B FWD CORNER TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4. A. (5) (A). <BR><BR>REMOVED (2 EA.) BACK-UP PLATES TO FACILITATE REPAIR IAW SRM 51-40-02-0G-0 PARA 4.E. FIG 8. <BR><BR>REMOVED BONDED ALUMINUM FOIL TO FACILITATE REPAIR IAW SRM 51-70-14-2R-3 PARA 4.A.(1).-(2). AS GIVEN IN SRM 57-41-01-2R-1 PARA 2.E.(2). <BR><BR>DAMAGE WILL BE REPAIRED PER SRM 51-70-05-2R-6 AS DIRECTED PER SRM 57-41-01-2R-1 PARA 4.E.;[09] FABRICATED REPAIR FOIL USING BMS8-289 LOT# 1507307-1; AND INSTALLED USING BMS5-128 (EA-956) ADHESIVE LOT# JH2FAL7046; VACUUM BAGGED REPAIR; WITH COMPLETED SUCCESSFUL BLEED DOWN TEST USING GAUGE ID: ATS2798 CAL/DUE: 10/2023; AND CURED UNDER HEATLAMP MONITORED USING THERMOMETER ID: ATS2209 CAL/DUE: 10/2023; REMOVED VACUUM BAG SYSTEM; TRIMMED AND CLEANED REPAIR EDGES IAW SRM 51-70-14-2R-3 PAR. 4.A.(3)-(5); & (11)(A)-(L).[
FWD CARGO BAY - SIDEWALL SUPPORT HAS CORROSION BS 400+17 RBL 18.<[01] VERIFIED APPLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] REMOVED CORROSION ON FWD CARGO BAY SIDEWALL SUPPORT AT BS 400+17 RBL 18 IAW SRM 51-10-02.<BR><BR>EVALUATED BLENDED AREA L=0.800' W=0.400' ORIGINAL THICKNESS 0.040' PER BAC1496-444 REMAINING 0.020' LOSS 0.020'; MAX MAT REMOVE ALLOWABLE 0.004'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D.<BR><BR>TOOL ID: ATS 1671 S/N: 65093024 DUE:07/2023;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT BS400 - BS420; RBL 18; BAC1496-444#7075T6; LOT# 1515896-1; PER SRM 51-40-05 AND DWG 143A7501.;[05] VERIFIED CORRECTIVE ACTION 4 AND THE MEASUREMENT TABLE.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW PART; PER SRM 51-20-01 AND SOPM 20-41-02.;[07] VERIFIED CORRECTIVE ACTION 6.;[08] UPDATE CORRECTIVE ACTION 7.
FWD CARGO BAY - FWD SHIELD HAS CORROSION RBL 23 BS 420+16; BS 420+18.<[01] NO ALLOWABLE DAMAGE LIMITS; IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9 C.;[02] VERIFIED CORRECTIVE ACTION 1;[03] LOCATED AND DRILLED NEW FCB FWD SHIELD RBL 23 IAW SRM 51-40-05 AND DWG#143A8126 . INSTALLATION OF THIS PART WILL BE ON FAULT [TTG8Q004DRF3];[04] COMPLETED MEASUREMENT TABLE;[05] VERIFIED CORRECTIVE ACTIONS 3; 4 AND MEASUREMENT TABLE.
CRACK ON AFT CARGO BAY LOWER BULKHEAD SUPPORT ATTACH ANGLE AT BS 847+19 LBL 10.<[01] REMOVED AND REPLACE ON AFT CARGO BAY P/N 149A8109-114 AT BS847+19; LBL 10 I.A.W. SRM 51-10-02-0G-0. ITEM 9.C. SRM 51-40-02-DWGS#149A8102; 149A8104 REV: B.;[02] CORRECTED: REMOVED AND REPLACE ON AFT CARGO BAY LOWER BULKHEAD SUPPORT ATTACH ANGLE WITH P/N 149A8109-114 AT BS.847+19; LBL 10 I.A.W. SRM 51-10-02-0G-0. ITEM 9.C. SRM 51-40-02-DWGS#149A8102; 149A8104 REV: B.;[03] VERIFIED CORRECTIVE ACTION STEP 2.;[04] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
LT STAB L/E HAS CRACKED RIB AT L/E STA 95.96<[01] REMOVED AND REPLACED RIB AT DISCREPANCY AREA IAW SRM 51-40-02 AND DWG 186A1001;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
AFT CARGO BAY FWD CORNER SCUFF PLATE CRACK<[01] WELDED CRACK ON AFT CARGO BAY FWD SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIP USED; WELDING MACHINE E10583; CAL DUE DATE 01/24.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2504-A; B; C CAL DUE: 05/23;[04] SANDED REPAIR AREA PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(5);[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-60-15-2R-1 STEP 4.B.(6) & (7);[07] VERIFIED CORRECTIVE ACTION 6;[08] INSTALLATION OF ACB FWD CORNER SCUFF PLATE IS DOCUMENTED ON CUSTOMER CARD #TTG8Q0027ZQP STEPS 15 AND 17;[09] VERIFIED COMPLETE STEP 8.<BR>VERIFIED MEASUREMENTS.
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION LBL 21.5 BS 807+2; BS 807+8; BS 807+10; BS 807+14; BS 807+18; BS 827+2; BS 827+6; BS 827+14; BS 827+18; BS 827+19.<[01] VERIFIED APPLICABILITY FOR IDENTIFICATION IAW SRM 53-60-53-0I-2<BR>AND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] ALL STEPS COMPLETED <BR>THIS FAULT WILL BE ACCOMPLISHED ON CARD #TTG8Q00HU6BV;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
FWD WET AREA INTERCOSTAL BS 277-294 BL 0; WL 208 IS CRACKED<[01] EVALUATED CRACK AT DISCREPANCY AREA WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; PART REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9.;[02] REMOVED FWD WET AREA INTERCOSTAL FROM BS-277 - BS-294; BL-0; WL-208 P/N 141A5410-3 PER SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] LOCATED AND DRILLED NEW INTERCOSTAL P/N:141A5410U3AAR PO#899637 PER SRM 51-40-05-0G-0. OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO INSTALL.;[06] INSTALLED NEW INTERCOSTAL P/N:141A5410U3AAR PO#899637 AT BS-277 - BS-294; BL-0; WL=208 PER SRM 51-40-02-0G-0 DWG#141A5410;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
WING TO BODY FAIRING PANEL 191CL HAS A DISBOND<[01] IDENTIFIED PANEL 191CL IAW SRM 53-30-70-0I-1 FIGURE 2 ITEM [8]. BEFORE SANDING AWAY THE PAINT LAYERS IN DISCREPANT AREA; TAP TESTED THE DISCREPANT AREA IAW SRM 53-30-70-1A-1 PARAGRAPH 2.A.(1).(A) WITH NO DISBONDS NOTED. SANDED AWAY MULTIPLE PAINT LAYERS IN THE DISCREPANT AREA IAW AMM 51-21-99-300-802 PARAGRAPH 3.C.(3).(A-D); TAP TESTED AREA AGAIN IAW SRM 53-30-70-1A-1 PARAGRAPH 2.A.(1).(A); WITH NO DISBONDS NOTED. OK TO REFINISH REPAIR AREA.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REFINISHED DISCREPANT AREA IAW AMM 51-21-99-300-802 PARAGRAPH 3.C.(3).;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
R?H FLOOR TO SIDEWALL SUPPORT ANGLE IS CORRODED AT FASTENER HOLES UPPER SURFACE; BS867+2; RBL22; WL164<[01] REMOVED CORROSON ON FLOOR TO SIDEWALL SUPPORT AT RBL22;WL154;BS867+2.MEASURES:L=.8.W=8;D=.007';ORIGINAL TICKNESS IS 0.040';REMAINING TICKNESS IS 0.033';FOUND AREA OUT OF LIMITS;IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2;PARAG.4 A(2) DETAIL D FIG.103.TOOL USED ATS2473;S/N UNKNOWN;DUE:08/2023.;[02] ADD TO CORRECTIVE ACTION 1 MATERIAL ID TO RH SIDEWALL SUPPORT;IAW SRM 53-70-53-0I-2 IDENTIFICATION 2;TABLE 2 FIG.2;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] RECEIVED ZEE CHANNEL P/N 146A7502-56 LOT:1515046-1.<BR>LOCATED AND DRILLED ZEE CHANNEL BTW. BS 867 - BS 887 RBL 22 WL 164 IAW SRM 51-40-05 DWG# 146A7500.<BR> THE INSTALLATION WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD #TTG8Q004G46G STEP# 33;[05] VERIFIED CORRECTIVE ACTION 4.;[06] VERIFIED CORRECTIVE ACTION 4.
R/H FLOOR TO SIDEWALL SUPPORT IS CORRODED AT FASTENER HOLES UPPER SURFACE; BS867+5; RBL22; WL164<[01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL22;WL164;BS867+5.MEASURES:L=.6;W=.6;D=.009';ORIGINAL TICKNESS IS 0.040';REMAINING TICKNESS IS 0.031'.FOUND AREA OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2;PARAG.4A(2) DETAIL D FIG.103 AND SRM 53-70-53-0I-2 IDENTIFICATION 2.TOOL USED ATS 2473;S/N UNKNOWN;DUE:08/2023.;[02] ALL PROCESS WILL BE COMPLETED WITH CARD#TTG8Q00HTZSK.;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] THE INSTALLATION WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD #TTG8Q004G46G STEP# 33.;[05] VERIFIED CORRECTIVE ACTIONS 4 AND MEASUREMENT TABLE .
R/H FLOOR TO SIDEWALL SUPPORT IS CORRODED AT FASTENER HOLES UPPER SURFACE; BS867+8; +11; +15; RBL22; WL164<[01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL22;WL164;BS867+8.MEASURES:L=.7;W=.7;D=.010';ORIGINAL TICKNESS IS 0.040';REMAINING TICKNESS IS 0.030';FOUND AREA OUT OF LIMITS;IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2;PARAG 4A(2) DETAIL D FIG.103 AND SRM 53-70-53-0I-2 IDENTIFICATION 2;TABLE 2 FIG 2.TOOL USED ATS2473;S/N UNKNOWN;DUE:08/2023.;[02] ALL PROCESS WILL BE COMPLETED WITH CARD#TTG8Q00HTZSK.;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] THE INSTALLATION WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD #TTG8Q004G46G STEP# 33;[05] CORRECTED MEASUREMENT TABLE #17.;[06] VERIFIED CORRECTIVE ACTIONS 4; 5 AND MEASUREMENT TABLE.
AFT BULKHEAD LOWER SUPPORT ANGLE IS CORRODED; BS947; LBL11-RBL24; WL186<[01] REMOVED AFT BULKHEAD LOWER SUPPORT ANGLE LOCATED BTW. BS 947 RBL 20.0 -LBL 8.1 IAW SRM 51-40-02.;[02] EVALUATE DAMAGE: AFT BULKHEAD LWR SUPPORT NOT HAS ALLOWABLE DAMAGE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAG. 9.C.;[03] VERIFIED CORRECTIVE ACTION 2 .;[04] INSTALLED NEW SUPPORT BRACKET ASSY. AS PER SRM 51-40-02 AND DWG 149A8117.;[05] VERIFIED CORRECTIVE ACTION 4;[06] UPDATED MEASUREMENT TABLE;[07] VERIFIED MEASUREMENT TABLE
TAIL CONE SKIN HAS A DISBOND AT BS 1156+13.5' AND 7' LOWER FROM TAIL CONE ACCESS DOOR CUT OUT SKIN LOWER EDGE<[01] IDENTIFIED TAIL CONE IAW SRM 53-80-70-0I-1 FIGURE 2 TABLE 2 ITEM 1<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-80-70-1A-1 PAR.4 B(4)<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 51-70-04-2R-4 AS DIRECTED BY SRM 53-80-70-2R-1 PAR.4 B(1) TABLE 201 <BR><BR>REMOVED DAMAGE TO BOTH SKINS AND FULL DEPTH HONEYCOMB CORE MEASURING 1.5'DIA; CLEANED SURROUNDING AREA; WITH NO CONTAMINATION NOTED IAW SRM 51-70-04-2R-4 PAR.4 A-C;[02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-04-2R-4.;[03] VERIFIED CORRECTIVE CTION 1 AND 2.;[04] FABRICATED REPAIR PLIES FOR THE INNER SURFACE FROM BMS9-3 ST1581 LOT# 1495277-1. FABRICATED CORE PLUG FROM BMS8-124 CL4 TY5 GR3 LOT# 1052601. INSTALLED REPAIR PLIES ON INNER SURFACE USING BMS8-301 CL1 GR1 LOT# JH2EAA8895; AND INSTALLED THE CORE PLUG USING BMS5-28 TY7 LOT# AK1AP8072K. VACUUM BAGGED INNER SURFACE PLIES WITH CORE PLUG. LEAK CHECKED BAGGED GOOD USING VACUUM GAUGE ID: E11543 CAL DUE: 09/2023 AND SET INNER SURFACE AND CORE PLUG TO CURE IAW SRM 51-70-04-2R-4 PARAGRAPH 4.D-F.;
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION RBL 21.5 BS 727C; BS 727C+13.5; BS 727D+5; BS 727+10.5; BS 727E+14.<[01] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2.;[02] REMOVED CORROSION ON AFT CARGO SIDEWALL SUPPORT AT RBL21.5;BS727E+14.MEASURES:L=2.2;W=.9;D=.012';ORIGINAL THICKNESS IS 0.040';REMAINING TICKNESS IS 0.028';FOUND AREA OUT OF LIMITS;IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2;PARAG 4A(2) DETAIL D FIG.103;TOOL USED ATS2473;S/N UNKNOWN;DUE:08/2013.;[03] VERIFIED CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.;[04] RECEIVED ZEE CHANNEL WITH P/N 146A7502-51 LOT: 1519347-1.<BR>THE INSTALLATION WILL BE ACCOMPLISHED WITH CUSTOMER CARD# TTG8Q004G46G STEP# 33.<BR>ALL MAINTENANCE ACTION ARE COMPLETE REQUEST FINAL BUY OFF.;[05] VERIFIED STEPS 1;2;3;4;5 AND CORRECTIVE ACTION 4.
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION LBL 21.5 BS 727D+3; BS 727D+9; BS 727D+10.<[01] VERIFIED APPLICABILITY FOR IDENTIFICATION IAW SRM 53-60-53-0I-2<BR>AND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21.5 BS 727D+9<BR>DIMENSIONS L=0.600' W= 0.800' DEPTH:0.015'<BR>ORIGINAL MATERIAL THICKNESS 0.040' IAW BAC 1496-377 REMAINING THICKNESS : 0.025'<BR>AND FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2<BR>TOOL USED: ID ATS 2473 S/N: UNKNOWN DUE: 08/2023;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] FABRICATED LOCATED AND DRILLED <BR>NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE <BR>FROM BS727 TO BS847 LBL 21.5<BR>PER SRM 51-40-05-0G-0; SRM 53-00-53-2R-6 AND DWG 143A7502 MATERIAL USED BAC1496-377#7075T62 LOT: 1515191-1<BR>OK TO TREAT AND PRIME ON<BR>NEW FLOOR TO SIDEWALL SUPPORT AND NEW SPLICE;[06] VERIFIED CORRECTIVE ACTION 5.;[07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER<BR>ON FLOOR TO SIDEWALL SUPPORT AND SPLICE<BR>IAW SRM 51-20-01 AND SRM SOPM 20-41-02 <BR>OK TO INTALL REPAIR SPLICE;[08] VERIFIED CORRECTIVE ACTION 7.<BR>OK TO INTALL REPAIR SPLICE;[09] INSTALLED SPLICE REPAIR ON SIDEWALL SUPPORT <BR>BETWEEN BS 727E AND BS 747 LBL 21.5 <BR>IAW SRM 53-00-53-2R-6 <BR>ALL MAINTENANCE TASKS HAVE BEEN COMPLETED;[10] UPDATE ITEM 19 ON MEASUREMENT TABLE;[11] VERIFIED MEASUREMENT TABLE;[12] VERIFIED CORRECTIVE ACTION 9 AND 10
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION AT LBL 21.5 BS 747+2; BS 747+8; BS 747+10 BS 747+14 BS 747+15; BS 767+7.BS 767+9; BS 767+14; BS 767+18; BS 787.<[01] VERIFIED APPLICABILITY FOR IDENTIFICATION IAW SRM 53-60-53-0I-2<BR>AND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] ALL STEPS COMPLETED <BR>THIS FAULT WILL BE ACCOMPLISHED ON CARD #TTG8Q00HU6BV;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION AT LBL 21.5 BS 787+1; BS 787+2; BS 787+5 BS 787+6 BS 787+10; BS 787+14.BS 787+18.<[01] VERIFIED APPLICABILITY FOR IDENTIFICATION IAW SRM 53-60-53-0I-2<BR>AND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] ALL STEPS COMPLETED <BR>THIS FAULT WILL BE ACCOMPLISHED ON CARD #TTG8Q00HU6BV;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION LBL 21.5 BS 727B+6; BS 727C; BS 727C+2; BS 727C+10; BS 727C+14; BS 727C+18; BS 727D+3.<[01] VERIFIED APPLICABILITY FOR IDENTIFICATION IAW SRM 53-60-53-0I-2<BR>AND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] ALL STEPS COMPLETED <BR>THIS FAULT WILL BE ACCOMPLISHED ON CARD #TTG8Q00HU6BV;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION AT RBL 21.5 BS 747+8; BS 747+12 BS 747+12 BS 747+14; BS 747+18.5.<[01] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2.;[02] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL21.5;BS747+8;MEASURES:L=.5;W=.5;D=.011';ORIGINAL TICKNESS IS 0.040';REMAINING TICKNESS IS 0.029';FOUND AREA OUT OF LIMITS;IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2;PARAG 4 A(2) DETAIL D FIG.103;TOOL USED ATS 2473;S/N UNKNOWN;DUE:08/2023.;[03] ALL PROCESS WILL BE COMPLETED WITH CARD#TTG8Q00HU5FY.;[04] VERIFIED CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.;[05] RECEIVED ZEE CHANNEL WITH P/N 146A7502-51 LOT: 1519347-1.<BR>THE INSTALLATION WILL BE ACCOMPLISHED WITH CUSTOMER CARD# TTG8Q004G46G STEP# 33.<BR>ALL MAINTENANCE ACTION ARE COMPLETE REQUEST FINAL BUY OFF.;[06] VERIFIED STEPS 1;2;3;4 AND CORRECTIVE ACTION 5.
AFT CARGO BAY - SIDEWALL SUPPORT HAS CORROSION AT RBL 21.5 BS 767+2; BS 767+3.5 BS 767+7.5 BS 767+11; BS 767+15; BS 767+19.<[01] VERIFIED APPLICABILITY OF SRM 51-10-02 STEP#9.;[02] THIS PART DOES NOT HAVE ALLOWABLE DAMAGE LIMITS;IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP#9.;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] RECEIVED NEW PART (FORWARD SHIELD) WITH P/N 146A8127-12 LOT. 1518989-1.<BR>LOCATED AND DRILLED FWD SHIELD IAW SRM 51-40-05 AND DWG#146A0081<BR> THE INSTALLATION WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD #TTG8Q004G46G STEP#35.;[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE
AFT CABIN FLOOR PANEL 242UF HAS A DELAMINATION ON THE LOWER SKIN AFT EDGE AT GIRT BAR ATTACH POINT<[01] IDENTIFIED PANEL 242UF MATERIAL IAW SRM 53-00-50-0I-1 FIG 6; TABLE 6.<BR><BR>FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F. <BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 53-00-50-2R-1. <BR><BR>CLEANED PANEL IAW SRM 53-00-50-2R-0 PARA 5. A. (1). <BR><BR>REMOVED DAMAGED PLIES ON LOWER SKIN AFT EDGE AT GIRT BAR ATTACH POINT WITH NO MOISTURE; CONTAMINATION OR DAMAGED CORE NOTED. <BR><BR>INSERTS NEAR REPAIR WERE REMOVED ON TTG8Q00HST79.<BR><BR>ALL IAW SRM 53-00-50-2R-1 PARA 3. A. - F. <BR><BR>O.K. TO POT.;[02] VALIDATED REPAIR PER SRM 53-00-50-2R-1;[03] VERIFIED ITEMS 1;2 CORRECTIVE ACTIONS. <BR>OK TO POT.;[04] APPLIED POTTING BMS5-28 TYPE 19 LOT#AK2JP8366K AND CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023; SANDED POTTING SMOOTH; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FROM BMS9-3H2ST1581 LOT#1495277-1; OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3G-K(1);[05] INSPECTED AND VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL REPAIR PLIES.<BR><BR>VERIFIED MEASUREMENTS TABLE.;[06] INSTALLED REPAIR PLIES USING BMS8-201 LOT#AK2EP8210K; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2107 CAL DUE DATE 04/2023 IAW SRM 53-00-50-2R-1 PARA 3K(1)-L(1)
FWD CABIN FLOOR PANEL 222BF HAS A DELAMINATION ON O/B EDGE APPROXIMATELY 4' AFT OF FWD EDGE<[01] IDENTIFIED 222BF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 2; TABLE 2.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL BE PERFORMING WORK IAW SRM 53-00-50-2R-1 <BR><BR>LIGHTLY SANDED DAMAGED SURFACE; CLEANED; AND PREPARED FOR REPAIR IAW SRM 53-00-50-2R-1 PARA 3.A-F.;[08] FILLED EXPOSED CELLS USING BMS 5-28 TY19 LOT: AK2JP8366K<BR>CURED POTTING COMPOUND USING THERMOMETER ATS2209 DUE: 10/2023<BR>LIGHTLY SANDED POTTING COMPOUND SMOOTH. CLEANED AND PREPARED PANEL SURFACE FOR REPAIR PLIES.<BR>FABRICATED REPAIR PLIES USING BMS 9-3 TYH2 LOT: 1513216-1 IAW SRM 53-00-50-2R-1 PARA 3.G-K;[09] OK TO INSTALL REPAIR PLIES.;[10] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 8 AND 9. OKAY TO INSTALL REPAIR PLIES.;[11] INSTALLED REPAIR PLIES USING RESIN BMS 8-201 TY3 LOT: AK2EP8210K<BR>ASSEMBLED VACUUM BAG USING VACUUM GAUGE ATS2441 DUE: 08/2023 IAW SRM 53-00-50-2R-1 PARA 3.K-L.(1).(A)<BR><BR>STILL NEEDS 5X5 TEST.;
FWD CABIN FLOOR PANEL 221BF HAS BROKEN TANG ON AFT I/B END<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-6.<BR>REMOVED 5EA THROUGH INSERTS TO FACILITATE REPAIRS IAW SRM 53-00-50-2R-6 PARA 3.B.<BR>REMOVED DAMAGED SKINS AND CORE; CLEANED REPAIR AREA IAW SRM 53-00-50-2R-6 PARA 3C-E.[04] FABRICATED CORE PLUG USING BMS 8-124C4T5G9 LOT#1287137 AND UPPER SURFACE REPAIR PLIES USING BMS 9-3H2 LOT#1495277-1 IAW SRM 53-00-50-2R-6 PARA 3F-G.<BR>OK TO INSTALL.;[10] INSTALLED LOWER REPAIR PLIES USING BMS 8-201TY3 LOT#AK2EP8210K; VACUUM BAGGED; LEAK CHECK GOOD WITH VACUUM GAUGE ID:ATS2798 CAL DUE 10/2023 IAW SRM 53-00-50-2R-6 PARA 3K-L.
FWD CABIN FLOOR PANEL 221GF HAS BROKEN TANG ON FWD O/B END<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-6.<BR>REMOVED 7EA THROUGH INSERTS TO FACILITATE REPAIRS IAW SRM 53-00-50-2R-6 PARA 3.B.<BR>REMOVED DAMAGED SKINS AND CORE AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-6 PARA 3C-F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-6.;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2.<BR><BR>VERIFIED MEASUREMENTS TABLE.;[04] FABRICATED CORE PLUG USING BMS 8-124C4T5G9 LOT#1287137 AND UPPER SURFACE REPAIR PLIES USING BMS 9-3H2 LOT#1495277-1 IAW SRM 53-00-50-2R-6 PARA 3F-G.<BR>OK TO INSTALL.;;[10] INSTALLED LOWER REPAIR PLIES USING BMS 8-201TY3 LOT#AK2EP8210K; VACUUM BAGGED; LEAK CHECK GOOD WITH VACUUM GAUGE ID:ATS2797 CAL DUE 10/2023 IAW SRM 53-00-50-2R-6 PARA 3K-L.
FWD CABIN FLOOR PANEL 222DF HAS A TORN OUT FASTENER HOLE ON THE O/B EDGE<[01] IDENTIFIED FLOOR PANEL 222DF MATERIAL IAW SRM 53-00-50-0I-1 FIG. 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS AND REQUIRES A PERMANENT REPAIR IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE IS REPAIRABLE PER SRM 53-00-50-2R-1.<BR> <BR>REMOVED DAMAGED SKIN AT DISCREPANT LOCATION MEASURING 1.0 X 2.0. CLEANED; AND REQUESTING OKAY TO APPLY POTTING IAW SRM 53-00-50-2R-1 PARAGRAPH 3.C-F.;[02] VALIDATED REPAIR PER SRM 53-00-50-2R-1;[03] VERIFIED ITEMS 1;2 CORRECTIVE ACTIONS. OKAY TO APPLY POTTING IAW SRM 53-00-50-2R-1 PARAGRAPH 3.C-F.;[04] APPLIED POTTING COMPOUND BMS5-28 TY19 LOT#AK2JP8366K TO EXPOSED CORE IAW SRM 53-00-50-2R-1 PARAGRAPH 3.G;[05] CURED POTTING; SANDED FLUSH; CLEANED REPAIR AREA AND FABRICATED REPAIR PIES FROM BMS9-3 STYLE 1581 LOT NUMBER 1513216-1 IAW SRM 53-00-50-2R-1 PARAGRAPH 3.H-J AND K.(1).(A) OK TO INSTALL REPAIR PLIES.;[06] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 THRU 5.<BR><BR>VERIFIED MEASUREMENTS TABLE.;[07] INSTALLED PLIES WITH BMS8-201 TYPE III LOT NUMBER AK2EP8210K VACUUM BAGGED PLIES AND VERIFIED A SATISFACTORY 5X5 USING VACUUM GAUGE ID: E11543 DUE: 09/2023 IAW SRM 53-00-50-2R-1 PARAGRAPH 3.K.(1).(B-C) AND L.(1).
FWD CARGO BAY - SIDEWALL SUPPORT HAS CORROSION BS 500C+13 RBL 23<[01] VERIFIED APPLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] REMOVED CORROSION ON FWD CARGO BAY SIDEWALL SUPPORT AT RBL 23 BS 500C+13 IAW SRM 51-10-02.<BR><BR>EVALUATED BLENDED AREA L=0.900' W=0.700' ORIGINAL THICKNESS 0.040' PER BAC1496-444 REMAINING 0.025' LOSS 0.015'; MAX MAT REMOVE ALLOWABLE 0.004'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D<BR><BR>TOOL ID: ATS1671 S/N: 65093024 DUE:07/2023;[03] VERIFIED ACTIONS 1 AND 2;[04] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT BS500A - BS500D; RBL 23; BAC1496-444#7075T6; LOT# 1515896-1; PER SRM 51-40-05 AND DWG 143A7501.;[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW PART; PER SRM 51-20-01 AND SOPM 20-41-02.;[07] VERIFIED CORRECTIVE ACTION 6.;[08] UPDATE CORRECTIVE ACTION 7.
CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 29 BS 440+7; BS 440+17. (MARKED)<[01] VERIFIED APPLICABILITY IAW SRM 53-30-15-0L-1 FOR IDENTIFICATION AND SRM 53-30-15-1A-1 FOR ALLOWABLE DAMAGE.<BR>STEPS 1 AND 2 PARTIAL.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] LOCATED AND DRILLED NEW FWD CARGO BAY THRESHOLD AT RBL 29 BS 440 TO BS 495 I.A.W SRM 51-40-05-0G-0 AND DWG 143A8122.;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] JOB CARD WILL BE ACCOMPLISHED ON N/C TTG8Q00HSBYJ;[06] JOB CARD WILL BE ACCOMPLISHED ON CARD 5330-E-16461-NG [TTG8Q004DRF3];[07] UP DATED PARTS REQUIREMENTS;[08] VERIFIED CORRECTIVE ACTION STEPS5;6 AND 7. TASK CARD COMPLETE.;[09] VERIFIED MEASUREMENT TABLE.
FWD CARGO BAY - SIDEWALL SUPPORT HAS CORROSION BS 500+14 RBL 24<[01] NO ALLOWABLE DAMAGE LIMITS; IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9 C.;[02] VERIFIED CORRECTIVE ACTION 1;[03] LOCATED AND DRILLED NEW AFT SHIELD BS 495 TO BS 500A I.A.W SRM 51-40-05-0G-0 AND DWG 143A8126.;[04] VERIFIED CORRECTIVE ACTION 3 AND VERIFIED MEASUREMENT TABLE.;[05] PART WILL BE INSTALLED ON AD CARD 5330-E-16461-NG (TTG8Q004DRF3);[06] VERIFIED CORRECTIVE ACTION STEP 5. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 440+5; BS 440+14; BS 460. (MARKED)<[01] VERIFIED APPLICABILITY IAW SRM 53-30-15-0L-1 FOR IDENTIFICATION AND SRM 53-30-15-1A-1 FOR ALLOWABLE DAMAGE.<BR>STEPS 1-3 PARTIAL.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] JOB CARD WILL BE ACCOMPLISHED ON N/C TTG8Q00HSCL0;[04] UPDATED MEASUREMENTS FIELD.;[05] VERIFIED CORRECTIVE ACTION #3.
FWD CARGO BAY - SIDEWALL SUPPORT HAS CORROSION LBL23 BS 500A+2; BS 500A+6; BS 500A+10; BS 500A+14.<[01] VERIFIED APPLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] REMOVED CORROSION ON FWD CARGO BAY SIDEWALL SUPPORT AT LBL 23 BS 500A+6 IAW SRM 51-10-02.<BR><BR>EVALUATED BLENDED AREA L=1.100' W=0.800' ORIGINAL THICKNESS 0.040' PER BAC1496-444 REMAINING 0.020' LOSS 0.020'; MAX MAT REMOVE ALLOWABLE 0.004'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D.<BR>TOOL ID: ATS2827 S/N: UNKNOWN DUE:01/31/24;[03] JOB CARD WILL BE ACCOMPLISHED ON N/C TTG8Q00HS4VM;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET HAS A CRACK AT BS 500D S-19L WL193. MARKED<[01] NO ALLOWABLE DAMAGE PER SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9 C.;[02] REMOVED FROM FCB AFT BULKHEAD SUPPORT GUSSET AT STA 500D S-19L WL 193 IAW SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION 1;2 AND THE MEASUREMENT TABLE.;[04] RECEIVED ON FWD CARGO BAY AFT BULKHEAD NEW SUPPORT GUSSETAT BS 500D S-19L WL 193 P/N 143A9481-6. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7902.<BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4.<BR>OK TO INSTALL.;[06] INSTALLED ON FWD CARGO BAY AFT BULKHEAD NEW SUPPORT GUSSET BS 500D S-19L WL 193 IAW SRM 51-40-02 AND DWG 143A7902;[07] VERIFIED CORRECTIVE ACTION 6.
CORROSION ON FWD CARGO BAY - L/H AFT BULKHEAD TO SIDEWALL ANGLE AT BS 500D LBL 34 LBL 37 LBL 41 LBL 44 LBL 47 LBL 50 LBL 53<[01] VERIFIED APPLICABILITY SRM 53-30-08-0I-1 FOR IDENTIFICATION AND SRM 53-30-08-1A-1 FOR ALLOWABLE DAMEGE.<BR><BR>REMOVED CORROSION ON FWD CARGO BAY L/H AFT BULKHEAD TO SIDEWALL ANGLE AT BS 500D LBL 44. IAW SRM 51-10-02<BR><BR>EVALUATED DAMAGE REMOVAL AT BLENDED AREA L=0.860' W=0.700' ORIGINAL THICKNESS= 0.071'; REMAINING =0.050'; MATERIAL LOSS= 0.021'; MAX MAT REMOVE ALLOWABLE =0.015'; FOUND TO BE OUT OF LIMITS<BR> IAW SRM 53-30-08-1A-1 PARA 4A (2) FIG 103 DETAIL C.<BR>TOOL ID: ATS2827 S/N: UNKNOWN DUE:01/31/2024.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] LOCATED AND DRILLED NEW FCB L/H AFT BULKHEAD TO SIDEWALL ANGLE IAW SRM 51-40-05 AND DWG # 143A9485 ; OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3.<BR>OK TO INSTALL.;[05] FCB L/H AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D WILL BE INSTALLED ON FAULT [TTG8Q004DRF3];[06] VERIFIED CORRECTIVE ACTION 5.
CORROSION ON R/H AFT BULKHEAD TO SIDEWALL SUPPORT/FWD CARGO BAY AT BS 500D RBL 34 RBL 37 RBL 41 BL 44 RBL 47 RBL 50 RBL 53<[01] VERIFIED APPLICABILITY SRM 53-30-08-0I-1 FOR IDENTIFICATION AND ARM 53-30-08-1A-1 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON FCB R/H AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D RBL 53 IAW SRM 51-10-02.<BR><BR>EVALUATED DAMAGE REMOVAL AT BLENDED AREA L=1.150' W=0.590' ORIGINAL THICKNESS= 0.071'; REMAINING =0.050'; MATERIAL LOSS= 0.021'; MAX MAT REMOVE ALLOWABLE =0.015'; FOUND TO BE OUT OF LIMITS<BR> IAW SRM 53-30-08-1A-1 PARA 4A (2) FIG 103 DETAIL C.<BR>TOOL ID: ATS2827 S/N: UNKNOWN DUE:01/31/2024.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] LOCATED AND DRILLED NEW FCB R/H AFT BULKHEAD TO SIDEWALL ANGLE IAW SRM 51-40-05 AND DWG # 143A9485 ; OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3.<BR>OK TO INSTALL.;[05] FCB R/H AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D WILL BE INSTALLED ON FAULT [TTG8Q004DRF3];[06] VERIFIED CORRECTIVE ACTION 5.
FWD CARGO BAY - INTERCOSTAL HAS A CRACK BS 500B+6 LBL 25<[01] NOT ALLOWABLE DAMAGE FOUND ON SRM PART THAT DO NOT ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED ON FWD CARGO BAY - INTERCOSTAL AT BS 500B TO BS 500C LBL25 IAW SRM 51-40-02;[03] RECEIVED ON FWD CARGO BAY NEW INTERCOSTAL BS 500B TO BS 500C LBL25 P/N 143A7510-11.LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7505.<BR>OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTIONS 3 AND MEASUREMENT TABLE.<BR>OK TO INSTALL.;[05] INSTALLED ON FWD CARGO BAY NEW INTERCOSTAL BS 500B TO BS 500C LBL 25 IAW SRM 51-40-02 AND DWG 143A7505;[06] VERIFIED CORRECTIVE ACTIONS 5.
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET HAS A CRACK AT BS 500D S-19R WL193. MARKED<[01] NO ALLOWABLE DAMAGE PER SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9 C.;[02] REMOVED FROM FCB AFT BULKHEAD SUPPORT GUSSET AT STA 500D S-19R WL 193 IAW SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION 1;2 AND THE MEASUREMENT TABLE.;[04] RECEIVED ON FWD CARGO BAY AFT BULKHEAD NEW SUPPORT GUSSET BS 500D S-19R WL193 P/N143A9483-5. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7902<BR>OK TO INSTALL;[05] VERIFIED STEP 4.<BR>OK TO INSTALL.;[06] INSTALLED ON FWD CARGO BAY AFT BULKHEAD NEW SUPPORT GUSSET AT BS 500D S-19R WL 193 IAW SRM 51-40-02 AND DWG 143A7902;[07] RII VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED ITEM 6 CORRECTIVE ACTION.;[09] VERIFIED MEASUREMENTS TABLE AND JOB COMPLETE
FWD CARGO BAY - INTERCOSTAL HAS A CRACK BS 500A+2 RBL 24<[01] NOT ALLOWABLE DAMAGE FOUND ON SRM. PART DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED ON FWD CARGO BAY INTERCOSTAL AT BS 500A TO BS 500B RBL 24 IAW SRM 51-40-02;[03] RECEIVED FWD CARGO BAY NEW ITERCOSTAL BS500A - BS500B RBL 24 P/N 143A7510-12 PO#878716. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7505.<BR>OK TO INSTAL;[04] VERIFIED CORRECTIVE ACTION STEPS 1;2 AND 3. VERIFIED OK TO INSTALL.;[05] INSTALLED ON FWD CARGO BAY NEW INTERCOSTAL BS 500A TO BS 500B RBL 24 IAW SRM 51-40-02 AND DWG 143A7505;[06] VERIFIED CORRECTIVE ACTION STEP 5.;[07] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
FWD CARGO BAY - SIDEWALL SUPPORT HAS CORROSION LBL24.5 BS 440+6; BS 440+10; BS 440+14; BS 440+18; BS 460+2; BS 460+6; BS 460+10; BS 460+14.<[01] VERIFIED APPLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] REMOVED CORROSION ON FWD CARGO BAY SIDEWALL SUPPORT AT LBL 24.5 BS 440+14 IAW SRM 51-10-02.<BR><BR>EVALUATED BLENDED AREA L=0.600' W=0.600' ORIGINAL THICKNESS 0.040' PER BAC1496-444 REMAINING 0.025' LOSS 0.015'; MAX MAT REMOVE ALLOWABLE 0.004'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D.<BR>TOOL ID: ATS2827 S/N: UNKNOWN DUE:01/31/24;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] FABRICATED AND DRILLED NEW - SIDEWALL SUPPORT LBL24.5 BS 396 -BS 500D WITH NEXT MATERIAL BAC1496-444#7075T62 LOT 1515896-1 I.A.W.SRM 51-40-05-0G AND DWG 143A7500; FABRICATED NEW SPLICE REPAIR WITH NEXT MATERIAL BAC1496-444#7075T62 LOT 1515896-1 I.A.W SRM 53-00-53-2R-6; APPLIED CHEMICAL CONVERSION COATING DRILLED NEW - SIDEWALL SUPPORT LBL24.5 BS 396 -BS 500D AND SPLICE REPAIR I.A.W SRM 51-20-0G-0.
FWD CARGO BAY - SIDEWALL SUPPORT HAS CORROSION LBL 23 BS 500+3; BS 500+5; BS 500+6; BS 500+10; BS 500+13; BS 500+17.<[01] VERIFIED APPLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] REMOVED CORROSION ON FCB SIDEWALL SUPPORT AT LBL 23 BS 500+13 IAW SRM 51-10-02.<BR><BR>EVALUATED BLENDED AREA L=0.600' W=0.500' ORIGINAL THICKNESS 0.040' PER BAC1496-444 REMAINING 0.020' LOSS 0.020'; MAX MAT REMOVE ALLOWABLE 0.004'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D.<BR>TOOL ID: ATS2827 S/N: UNKNOWN DUE:01/31/24;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] JOB CARD WILL BE ACCOMPLISHED ON N/C TTG8Q00HS4VM;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
FWD CARGO BAY - INTERCOSTAL CLIP HAS A CRACK BS 400+1 LBL 24.5<[01] NOT ALLOWABLE DAMAGE FOUND ON SRM PART DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED ON FWD CARGO BAY INTERCOSTAL CLIP BS400 TO BS420 LBL24.5 IAW SRM 51-40-02;[03] RECEIVED ON FWD CARGO BAY -NEW INTERCOSTAL CLIP BS 400+1 LBL24.5 P/N 143A7502-155. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7502.<BR>OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.<BR>OK TO INSTALL.;[05] INSTALLED ON FWD CARGO BAY NEW INTERCOSTAL CLIP BS 400+1 LBL 24.5 IAW SRM 51-40-02 AND DWG 143A7505;[06] VERIFIED CORRECTIVE ACTION 5.
FLOOR SUPPORT HAS A CRACK BS 540 LBL 44<[01] VERIFIED APPLICABILITY NOT ALLOWABLE ITEMS THAT DO NOT HAVE ENTRIES ARE CALLEDREPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED FLOOR SUPPORT AT BS 540 LBL 25 TO LBL45 IAW SRM 51-40-02;[03] RECEIVED NEW FLOOR SUPPORT AT BS 540 LBL25 TO LBL45 P/N 143A5240-32 PO#905537. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A5240.<BR>OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION ITEM 3; OK TO INSTALL.;[05] INSTALLED FLOOR SUPPORT AT BS 540 LBL25 - LBL45 IAW SRM 51-40-02 AND DWG 143A0060;[06] VERIFIED CORRECTIVE ACTION 5 AND THE MEASUREMENT TABLE.
CRACK ON FRAME BS 312 BETWEEN STR-4L AND UPPER MAIN SILL .<[01] REPAIRED FRAME BS 312 BETWEEN STR-4L AND UPPER MAIN SILL ON FAULT #[TTG8Q00HTL5N];[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS. <BR>VERIFIED MEASUREMENTS.
CORROSION RIGHT OWE THRESHOLD SUPPORT RBL 71 WL 221<[01] CORROSION ON RIGHT OVER WING EXIT THRESHOLD SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS FOUND IN THE SRM FOR THIS ITEM AND IT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9 C;[02] REMOVED RIGHT OWE THRESHOLD SUPPORT RBL 71 WL 221 IAW SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.;[04] LOCATED AND DRILLED NEW R/H OVER WING THRESHOLD SUPPORT RBL 71 WL 221 IAW SRM 51-40-05 AND DWG # 411A2854 OK TO INSTALL;[05] VERIFIED ORRECTIVE ACTION 4 AND THE MEASUREMENT TABLE. OK TO INSTALL THRESHOLD SUPPORT.;[06] INSTALLED RIGHT OWE THRESHOLD SUPPORT RBL 71 WL 221 IAW SRM 51-40-02 AND DWG # 144A8201;[07] VERIFIED CORRECTIVE ACTION 6. WORKSCOPE IS COMPLETE.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1675; M1672. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATION M1675 AND M1672 PER AMM 33-51-06. OPS CHECK GOOD.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1675; M1672. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATION M1675 AND M1672 PER AMM 33-51-06. OPS CHECK GOOD.
CABIN L/H EMERGENCY HATCH HANDLE SURROUND CRACKED<[01] REMOVED AND REPLACED LH EMERGENCY EXIT HATCH HANDLE SURROUND IAW AMM 52-22-51
LEFT WING #1 SLAT LOWER SKIN CRACKED AT ACTUATOR MOUNT FITTING CRACK IS APPROX .5 LONG AND 2 FWD OF THE AFT EDGE. REMOVED #1 SLAT PER AMM 27-81-21 THRU STEPS 2G(10);[02] R/R #1 SLAT PER AMM 27-81-21. R/R LEFT WING #1 SLAT PER AMM 27-81-21. R/R LEFT WING #1 SLAT PER AMM 27-81-21.
EMERGENCY SLIDE ON R1 DOOR PARTIALLY DETACHED. REINSTALLED IAW MM 25-66-01
PASSING 32;500 #1 ENGINE PEGGED AT 5.0 VIB / [01] REMOVED AND REPLACED #1 ENGINE REF AMM 71-00-02 AMD MT 771-00-01
COCKPIT DOME LIGHT EMERGENCY LIGHTS BULB DOES NOT ILLUMINATE / [01] REMOVED AND REPLACED M1675 EMERGENCY LIGHTS POWER SUPPLY REF AMM 33-51-06.
EVIDENCE OF DAMAGE TO LH OUTBOARD HORIZONTAL STAB. REMOVED PAINT AT DEFECT LOCATION BY STRIPPING METHOD PER M/M 51-21-11. CLEANED AND INSPECTED AREA AND FOUND NO DAMAGE. REAPPLIED ALODINE;PRIMER AND PAINT PER M/M 51-21-99.
EVIDENCE OF DAMAGE TO RH OUTBOARD HORIZONTAL STAB. REMOVED RT HORIZONTAL STAB IAW AMM 27-41-11. INSTALLED RT HORIZONTAL STAB IAW MM 27-41-11 UP TO AND INCLUDING STEP 3. F.(6). (D) 4. COMPLETED INSTALLATION OF RT HORIZONTAL STAB, ALL TASKS COMPLETED IAW AMM 27-41-11.
LEFT ELEVATOR DAMAGED. INSTALLED THE LEFT ELEVATOR IAW AMM 27-31-11-400-801 G 12(3 A)3 (B) 12345 (C) 12 AND 3.
RIGHT HAND SHIELD PLATE HAS CORROSION ON AROUND NUT PLATE HOLES FROM STA 497 TO STA 500A. / REMOVED AND REPLACED SHIELD PLATE PER SRM 51-40-02 ( P/N # 143A8126U13 ) .
R/H WING PANEL 661CB HAS MULTIPLE SMALL CRACKS AROUND FASTENER HOLES ALONG THE ENTIRE TRAILING EDGE. / REPAIRED DAMAGED FASTENER HOLES PER EA 21-157-00876 AND SRM 51-70-05-2R-8.
R/H WING PANEL 661AB HAS MULTIPLE SMALL CRACKS AROUND FASTENER HOLES ALONG THE ENTIRE TRAILING EDGE. / REPAIRED IAW SRM 51-70-05-2R-8 & EA 21-157-00876
R/H WING PANEL 661BB HAS MULTIPLE SMALL CRACKS AROUND FASTENER HOLES ALONG THE ENTIRE TRAILING EDGE. / REPAIRED FASTENER HOLES PER EA 21-157-00876 AND SRM 51-70-05-2R-8. RESTORED SURFACE FINISH PER AMM 51-21-99.
L/H WING PANEL 561AB HAS MULTIPLE SMALL CRACKS AROUND FASTENER HOLES ALONG THE ENTIRE TRAILING EDGE. / REPAIRED IAW SRM 51-70-05-2R-8 & EA 21-157-00876
L/H WING PANEL 561BB HAS MULTIPLE SMALL CRACKS AROUND FASTENER HOLES ALONG THE ENTIRE TRAILING EDGE. / REPAIRED FASTENER HOLES PER EA 21-157-00876 AND SRM 51-70-05-2R-8. RESTORED SURFACE FINISH PER AMM 51-21-99.
L/H WING PANEL 561CB HAS MULTIPLE SMALL CRACKS AROUND FASTENER HOLES ALONG THE ENTIRE TRAILING EDGE. / REPAIRED IAW SRM 51-70-05-2R-8 AND EA#21-157-00876
CENTER CABIN FLOOR BOARD 241BF HAS SEVERAL DENTS AND AN AREA OF FIBER GLASS DAMAGE ON TOP. / REMOVED AND REPLACED CABIN FLOOR BOARD 241BF PER AMM 53-21-00.
CENTER CABIN FLOOR BOARD 242BF HAS SEVERAL DENTS AND AN AREA OF FIBER GLASS DAMAGE ON TOP. / REMOVED AND REPLACED CABIN FLOOR BOARD 242BF PER AMM 53-21-00.
CENTER CABIN FLOOR BOARD 242AF HAS SEVERAL DENTS AND AN AREA OF FIBER GLASS DAMAGE ON TOP. / REMOVED AND REPLACED CABIN FLOOR BOARD 242AF PER AMM 53-21-00.
# 1 SEAT TRACK F.S. 520 HAS WEAR MARKS ON LUG. / REPAIRED SEAT TRACK PER SRM 53-00-52-2R-4.
WAFFLE PLATE JUST O/B OF PANEL 651D CRACKED. / REMOVED AND REPLACED WIGGLE PLATE (P/N #115A2781-4 .) PER SRM 51-40-02 .
LH WING REAR SPAR LOWER CHORD PANEL WAFFLE PLATE CRACKED JUST IB OF #3 FLAP TRACK (MARKED) / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-10-02;AND SRM 51-40-02.
RUDDER ARM BALANCE WEIGHT CORRODED / REMOVED AND REPLACED RUDDER ARM BALANCE WEIGHT PER CMM 55-40-09 AND TORQUE PER SRM 51-60-07-0G-0
RT EMERGENCY EXTERNAL GROUND FLOOD LIGHT LENS COVER DETACHED INTERNALLY TO HOUSING. R & R RT EMERGENCY EXTERNAL GROUND FLOOD LIGHT LENS COVER, PER SIP.
OPS FOUND L1 DOOR SLIDE PACK DISPLACED / RE-INSTALLED L1 DOOR SLIDE PACK PER MAINT TASK 725-61-06
OVERWING ESCAPE GROUND ILLUMINATION LIGHT ON RT SIDE AND AISLE LIGHTS AT STA 560 AND 640 INOPERATIVE. FOUND EMERGENCY EXIT LIGHT BATTERY PACK M1670 AT STA 727 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD REF AMM 33-51-06.
CLEANERS REPORTED L1 SLIDE FELL OUT OF COVER. / RESECURED SLIDE IN COVER AT L1 DOOR AS REQUIRED PER AMM 25-66-01. A/C OK FOR SERVICE
EMERGENCY EXIT ROW LIGHT INOPERATIVE 12 F. (SIDEWALL LIGHT) / R&R BALLAST IAW AMM.
AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / RELAMPED LIGHT IAW AMM.
L2 DOOR GIRT BAR BRACKET LOOSE. R&R THE GIRT BAR FASTENERS IAW SRM.
R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
RT BULLNOSE EMERGENCY LIGHT COVER MISSING AT ROW 16. INSTALLED LENS PER AMM.
AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED. / REPAIRED PER EA 1-A53-2076 REV 11
RT HORIZONTAL STABILIZER RIB AT STAB. STA. 120.30, 4TH VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.
RT HORIZONTAL STABILIZER RIB AT STAB. STA. 120.30, 2ND VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.
INTERCOSTAL UPPER FLANGE BENT BETWEEN BS. 500D TO BS. 520, LBL 7. R&R INTERCOSTAL PER SRM & DWG.
DENT; WITH A .800' AREA OF DELAMINATION (MARKED); ON #6 SPOILER UPPER SKIN; 6' FROM LE; 12' FROM THE OB EDGE / DENT; WITH A .800' AREA OF DELAMINATION ON #6 SPOILER UPPER SKIN 6' FROM L/E; 12' FROM THE O/B EDGE REPAIRED IAW SRM 51-70-10-2R-0 PER SRM 57-70-01-2R-1; AND IAW SRM 51-70-10-2R-2
DENT; WITH A .800' AREA OF DELAMINATION (MARKED); ON #5 SPOILER UPPER SKIN; 8' FROM LE; 8' FROM THE OB EDGE / DENT; WITH A .800' AREA OF DELAMINCATION ON #5 SPOLIER UPPER SKIN 8' FROM L/E 8' FROM THE O/B EDGE REPAIRED IAW SRM 57-70-10-2R-0 PER SRM 57-70-10-2R-1 AND IAW SRM 51-70-10-2R-2
AFT CARGO BAY VERTICAL WEB CORRODED BETWEEN BS. 767 TO BS. 787, RBL 21. R&R VERTICAL WEB PER SRM & DWG.
LOWER FAIRING FORMER AT BS 663 LBL 27 IS CRACKED / REPAIRED PER: EA 1-757-16257 REV IR AND ATS ER 19-02997 REV IR
AFT CARGO BAY SHIELD SUPPORT ANGLE CORRODED BETWEEN BS. 767 TO BS. 787, RBL 21. R&R ANGLE PER SRM & DWG.
LT MLG WHEEL WELL VAPOR BARRIER HAS A 15' CRACK AT LBL35. / LT MLG WHEEL WELL VAPOR BARRIER 15' CRACK AT LBL35 WAS REPAIRED IAW SRM 51-70-04-2R-10
SUPPORT ANGLE CRACKED BETWEEN BS. 380 TO BS. 400, RBL 11. R&R SUPPORT ANGLE PER SRM & DWG.
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #5 (UPPER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR #5 UPPER BEAM REPAIRED ON JOB #523232
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE 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. / FORWARD SERVICE DOOR #4 LOWER BEAM REPAIRED ON JOB #523232
AFT CARGO BAY SUB THRESHOLD CLOSE OUT WEB CORRODED BETWEEN BS. 795 TO BS. 837, RBL 28. R&R WEB PER SRM & DWG.
AFT CARGO BAY FLOOR BOARD SPLICE PLATE CORRODED AT BS. 767+6, WL 156. R&R SPLICE PLATE IAW SRM.
AFT CARGO BAY SHIELD CORRODED BETWEEN BS. 767 TO BS. 792, RBL 21. R&R SHIELD PER SRM AND DWG.
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS. 727C+10" TO BS 847 WL 156 LBL 21. R&R FLOOR TO SIDEWALL SUPPORT IAW SRM AND DWG.
PANEL 193AR HAS PUNCTURES & DELAMINATED AREA ON THE INNER SURFACE OF THE CORE AREA. / PANEL 193AR WITH PUNCTURES AND DELAMINATED AREA ON THE INNER SURFACE OF THE CORE AREA WAS REPAIRED IAW SRM 51-70-05 REPAIRS 2 AND 11. 59702U 05/06/19
AFT CARGO BAY SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. R&R SHIELD PER SRM & DWG.
AFT CARGO BAY FLOOR BOARD SPLICE PLATE CORRODED AT BS. 887, WL 156. R&R TEE ASSEMBLY PER DWG AND SRM.
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727+6 TO BS. 767, RBL 21. R&R SUPPORT PER SRM & DWG.
AFT CARGO BAY FLOOR BOARD SPLICE PLATE CORRODED AT BS. 727D, WL 156. R&R SPLICE PLATE IAW SRM.
FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED AT LOWER DOORWAY SILL BETWEEN BS. 460 TO BS. 480, RBL 27. R&R WEB PER SRM & DWG.
FAIRING PANEL #195CR HAS SMALL CRACK AT THE AFT LOWER RADIUS MARKED / FAIRING PANEL #195CR SMALL CRACK AT THE AFT LOWER RAIDUS WAS REPAIRED IAW SRM 51-70-04-2R-6 56144U 05/03/2019
FAIRING PANEL #195CL HAS SMALL CRACK AT THE AFT LOWER RADIUS MARKED / FAIRING PANEL # 195CL SMALL CRACK AT THE AFT LOWER RADIUS WAS REPAIRED IAW SRM 51-70-04-2R-0 56114U 05/03/2019
FLOOR SUPPORT IS CRACKED BS 540 BL0-RBL25 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS 540 BL0- RBL 25 WL208 IAW ARM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INSTALL 13656R 28APR19 INSP 28 28APR19 INSTALLED NEW FLOOR SUPPORT AT BS 540 BL0-RBL25 WL208 IAW SRM 51-40-02-0G-0 AND IPC 53-31-00-05 13656R 28APR19
INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS. 380 TO BS. 400, BL 0. R&R ANGLE PER SRM & DWG.
FLOOR SUPPORT IS CRACKED BS 540 BL0-LBL25 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS 540 BL 0 - LBL 25 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INSTALL 1365R 28APR19 INSP 28 28APR19 INSTALLED NEW FLOOR SUPPORT AT BS 540 BL 0 - LBL 25 WL 208 IAW SRM 51-40-02-0G-0 AND IPC 53-31-00-05 13656R 28APR19
RT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED THE RT HORZ STAB UPPER FWD SLIDE SEAL IAW MM 53-31-31-000-802. 4077C 03MAY19. INSTALLED NEW RT HORIZ STAB UPPER FWD SLIDE SEAL IAW MM 53-31-31-400-802 STEPS 3.E.;3.F.
LT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED THE LT HORZ STAB UPPER FWD SLIDE SEAL IAW MM 53-31-31-000-802; 4077C 03MAY19. INSTALLED NEW LT HORIZ STAB UPPER FWD SLIDE SEAL IAW MM 53-31-31-400-802 STEP 5.3.E; 3.F.
R2 DOOR MOPSILL AT THRESHOLD ATTACH FLANGE CORRODED AT BS. 970, RBL 52. R&R MOPSILL PER SRM & DWG.
L1 DOOR MOPSILL INNER CHORD CRACKED AT BS. 303, LBL 53. R&R MOPSILL PER DWG AND SRM.
FLOOR SUPPORT CRACKED BETWEEN BS. 277 TO BS. 294, BL 0. R&R FLOOR SUPPORT IAW SRM & DWG.
RT HORIZONTAL STABILIZER RIB AT STAB. STA. 120.30, 3RD VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.
LT HORIZONTAL STABILIZER RIB AT STAB. STA. 120.30, 2ND VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.
FLOOR SUPPORT CRACKED BETWEEN BS. 312 TO BS. 328, LBL 45. R&R FLOOR SUPPORT PER DWG AND SRM.
LT WING LWR T/E PANEL AFR SUPPORT BRACKET IS CRACKED AT I/B END; JUST O/B OF THE #1 PYLON. / REMOVED AND REPLACED LT WING LWR T/E PANEL AFT SUPPORT BRACKET AT I/B END JUST O/B OF THE #1 PYLON. IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-17 89812U 04-18-19
ANGLE CRACKED BS290- 294 RBL 52 WL 208 / REMOVED AND REPLACED ANGLE AT BS 290-294 RBL 52 WL 208 PER DWG 141A8310 AND SRM 51-40-02-0G 91201U 25APR19
LT WING O/B ANGLE IS CRACKED FOR THE TRANSVERS WEB. REMOVED AND REPLACED LT WING OUTBD ANGLE FOR THE TRANSVERS WEB IAW SRM.
GIRT BAR ATTACH FITTING CORRODED AT BS. 312, LBL 52. R&R FITTING PER SRM.
EMERGENCY AISLE LIGHT INOP AT ROW 23. RELAMPED LIGHT IAW AMM.
LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.
RT OVER WING EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY BACK PER MM.
LT BULLNOSE EMERGENCY LIGHT INOP AT ROW 20. RELAMPED LIGHT PER AMM.
15 IN CRACK ON THE LEFT MAIN LANDING GEAR WHEEL WELL AT APPROXMATELY LBL35. AN INTERIM REPAIR WAS ACCOMPLISHED PER SRM 737-700; 57-10-10-1A2. THIS A/C HAS SPLIT SCIMITAR WINGLETS INTALLED. / 737NG SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 IS APPLICABLE AND ACCEPTABLE FOR USE ON A/C N289CT WITH SPLIT SCIMITAR WINGLETS CONFIGURATION PER EA 1-757-15904. SEE NRC D276051 FOR RE-INSPECT INTERVALS.
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
EMERGENCY LIGHT BATTERY M1675 FAILED TEST. R&R BATTERY PACK PER MM.
EMERGENCY LIGHT BATTERY M1673 FAILED TEST. R&R BATTERY PACK PER MM.
EMERGENCY LIGHT BATTERY M1672 FAILED TEST. R&R BATTERY PACK PER MM.
R1 DOOR EVAC SLIDE GIRT BAR FWD COLLAR SPACER LOOSE. R&R COLAR PER MM.
L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
R1 DOOR SLIDE INADVERTENTLY FELL OUT OF ITS CASE, DID NOT DEPLOY, STILL OPERATIONAL. SECURED THE SLIDE IAW MT.
FORWARD L/H BATTERY FAILED TIME TEST. / R&R BATTERY PER AMM.
LT MLG WHEEL WELL HAS A 15' VAPOR WEB CRACK AT 35LBL / INTERIM REPAIR OF VAPOR WEB IN LT MLG WHEEL WHEEL (WELL) AT 35LBL PER SRM 57-10-10-1A-2 STEP 2C3. REINSPECT EVERY 600 FLIGHT CYCLES
L1 DOOR SLIDE FOUND LOOSE. SECURED THE SLIDE IAW MT.
RT MAIN LANDING GEAR FORWARD TRUNNION PIN UPPER INBOARD ATTACHMENT LUG FITTING CORRODED. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD TRUNNION PIN UPPER INBOARD ATTACHMENT LUG FITTING CORRODED. REPAIRED FITTING PER EA.
LEFT EMERGENCY EXIT ESCAPE ROPE HOOK CORRODED. R & R THE ROPE IAW AMM.
RIGHT EMERGENCY EXIT ESCAPE ROPE HOOK CORRODED. R & R THE ROPE IAW AMM.
L2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.
BULKHEAD WEB CRACKED AT BS 663, LBL 42. REPAIRED THE BULKHEAD WEB IAW SRM AND SWA EA.
R1 DOOR LOWER EXIT SIGN COVER BROKEN. R & R THE LIGHT ASSEMBLY IAW MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
RIGHT MAIN WW CEILING CRACKED AT BS 663.75, RBL 43. REPAIRED CEILING IAW EA.
AIR TURN BACK & DECLARED EMER. NR 2 TIRE BLOWN AT TAKEOFF, LOST A HYD. R & R NR 2 MAIN TIRE IAW MM.
LEFT HORIZONTAL STABILIZER RIB 92.70, NR 3 STIFFENER CRACKED AT LOWER EDGE. REPAIRED STIFFENER IAW SRM.
LEFT HORIZONTAL STABILIZER RIB 147.90, CRACKED AT FWD INBD LOWER CASTING EDGE. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB 101.90, FWD LOWER CORNER OF CASTING CRACKED. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB 129.50, NR 3 STIFFENER CRACKED AT LOWER EDGE. REPAIRED STIFFENER IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB 92.7, STIFFENER CRACKED. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB 120.30, NR 2 STIFFENER CRACKED AT LOWER EDGE. REPAIRED STIFFENER IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 46. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, RBL 31. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 46. R & R INTERCOSTAL IAW SRM.
AFT GALLEY DOOR LOWER Z ANGLE CORRODED. R & R Z ANGLE IAW SRM.
L1 DOOR SLIDE GIRT BAR HOOK CLIP LOOSE. SECURED CLIP IAW SRM.
R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.
KEEL BEAM PANEL 192E FWD LT ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.
MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. R & R SIGN IAW SIP.
R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW MT.
R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW MM.289.
RT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW SIP.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW M/M.
LT EMERGENCY LIGHTS BATTERY CHARGER NUT CLIP MISSING AT STA 727 C+13. REMOVED & REPLACED CHARGER PER AMM.
RT WING O/B AFT FLAP O/B CENTER TRACK LOSE OUT FILLER CRACKED. R&R AFT FLAP IAW SRM & AMM.
RIGHT HORIZONTAL STABILIZER LOWER SURFACE AT STAB STA 184.70 A .9" CRACKED 7" FROM THE REAR SPAR. REPAIRED STABILIZER IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER SURFACE, AT STAB STA 129.50 A .9" CRACKED 8" FROM THE REAR SPAR. REPAIRED STABILIZER IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER SURFACE REAR SPAR, CRACKED 3" INBD OF STAB, STA 101.90. REPAIRED STABILIZER IAW MM.
AFT CARGO COMPARTMENT FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN STA 847 TO STA 867, RBL 20. R & R SUPPORT IAW SRM AND DWG.
AFT CARGO COMPARTMENT FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN STA 727D TO STA 847, LBL 20. R & R SUPPORT IAW SRM.
AFT CARGO COMPARTMENT FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN STA 727B TO STA 767, RBL 20. R & R SIDEWALL SECTION IAW SRM AND AMM.
FWD CARGO BAY BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 20 TO LBL 20. R & R ANGLE IAW SRM.
FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 396 TO BS 500D, LBL 24. REPAIRED PLATE IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SURFACE AT REAR SPAR, A 2.7" CRACKED 2.2" INBD OF STAB STA 101.90. REPAIRED STABILIZER IAW SRM.
R1 DOOR GIRT BAR TO HARD TO ENGAGE. REMOVED AND REPLACED R1 DOOR SLIDE PER MM.
R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
FWD ENTRY EMERGENCY SLIDE LIGHT INOP. RELAMPED FWD ENTRY EMERGENCY SLIDE LIGHT IAW AMM 33-51-04-960-801.
LT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.
RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.
RT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
LEFT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, LBL 67. REMOVED AND REPLACED WEB IAW SRM.
L1 DOOR EMERGENCY EXIT LIGHT PATH BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
OVERWING EEPLS COVER MISSING. INSTALLED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP BETWEEN ROW 10 TO ROW 13. SECURED WIRES PER MM.
DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS INOP AT ROW 2. SECURED WIRE PER MM.
L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.