N7881A
Registered owner: WELLS FARGO TRUST CO NA TRUSTEE, MD (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2022-09-29 – 2022-09-29 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2022-09-29 – 2022-09-29 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER. REMOVE AND REPLACED FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER IAW AMM 53-11-01-420-801, REJECT; FWD SERVICE DOOR FWD LOWER CORNER CUTOUT LEAK CHECK FAILED. IT HAS A HISSING SOUND FROM INSIDE & LEAK FROM OUTSIDE. REMOVED FSD SCUFF PLATE IAW AMM 53-11-01-000-801, INSTALLED FSD SCUFF PLATE IAW AMM 53-11-01-420-801. APPLIED PS 870 B1/2. WELDED THE DAMAGED AREAS ON SCUFF PLATE IAW SRM 53-10-15-2R-2 STEP 4.B(4). REFERRED TO BAC 5975 CLASS BPT INSPECTED WELDED AREAS IAW SOPM 20-20-02. NO CRACKS NOTED. SANDED THE REWORKED SURFACES AND EDGES OF SCUFF PLATE AS NECESSARY IAW SRM 53-10-15-2R-2 STEP 4.B.
DURING OK TO CLOSE, FOUND THE FLOORBEAM CRACKED AT BS 540, RBL 1 - 25. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A0060, REV B;
RIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED THE RT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE INBD SIDE IAW SRM 51-40-02, AND DWG 115A2781, REV B.
BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 45, WL 173. THE COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.
RIGHT HORIZONTAL STABILIZER NR 6 INSPAR RIB AT STABILIZER STATION 138.70; 3RD VERTICAL STIFFENER IS CRACKED. PERFORMED REPAIR AT HORIZONTAL STABILIZER NO 6 INSPAR RIB STABILIZER STATION 138.70 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4, REPAIR 4.
CRACKED STRINGER 7L, BS 296, LBL 41, WL 274. THE DAMAGE WAS REPAIRED IAW SRM 53-00-03-2R-1, REPAIR 1, AND EA 25-153-02976 WITH AN INSPECTION PROGRAM DEFINED IN 25-153-02976-INSP. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. CRACK NOTED. NO ALLOWABLE LIMIT FOUND FOR SPECIFIC LOCATION ON SRM 53-00-03-1A-1, ALLOWABLE DAMAGE 1, THEREFORE REPAIR IS NEEDED. REPAIR PROVIDED IAW SRM IS NOT APPLICABLE DUE TO LIMITATION GIVEN SRM 53-00-03-2R-1, REPAIR 1, PAR 1.C.(2) INITIAL STRINGER ON FWD AND AFT DIRECTIONS IS LESS THEN 20'. ENGINEERING WILL BE CONTACTED TO FURTHER REPAIR INSTRUCTIONS.
CRACKED FRAME BS 312 LBL 33 WL 282 ABOVE FWD ENTRY DOOR UPPER SILL WEB. REPAIRED IAW SRM 22-153-01244.
AFT ENTRY DOOR SLIDE GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FASTENER AFT ENTRY DOOR SLIDE GIRT BAR BRACKET IAW SRM 51-40-02-0G-0.
RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR RIB HAS POSSIBLE CRACK. CLEANED RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR IAW SOPM 20-30-03. REPAIRED SLAT IAW SRM 57-42-01-2R-8, REPAIR 8, ALTERNATIVE 1, FIG 202.
CORRODED FLOOR SUPPORT, BS 304, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5600, REV N.
CORRODED FLOORBEAM, BS 986, LBL 38-45, WL 208. REMOVED AND REPLACED THE FILLER IAW EXISTING REPAIR SRM 53-70-51-2R-6, ALT 4.
CORRODED FLOORBEAM, BS 986, RBL 38-45, WL 208. INSTALLED A REPAIR IAW SRM 53-70-51-2R-6, ALTERNATIVE 3, FIG 204, SHEET 1.
AFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.
AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ADF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241UF WITH UPPER SKIN AREAS OF PULLED STRANDS, REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
FWD FLOOR PANEL 221EF UPPER SURFACE DELAMINATED. THE FWD FLOOR PANEL 221EF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1,
AFT FLOOR PANEL 242UF FWD O/B CORNER IS CRACKED. AFT FLOOR PANEL 242UF WITH FWD O/B CORNER CRACKED WAS REPAIRED PER SRM 53-00-50-2R-1.
CRACKED INTERCOSTAL, BS 315, RBL 30, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -.
AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241AEF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
FLOOR PANEL 242XF IS SOFT IN THE MIDDLE OF PANEL.<[01] FLOOR PANEL 242XF WITH SOFT AREA IN THE MIDDLE OF PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.
AFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE. REPLACED AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 195.
WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN S19 & 20L. REMOVED AND REPLACED THE WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02, AND DWG 116A3010, REV-.
CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE THRESHOLD WEB IAW SRM 51-40-02, AND DWG:146A8340 REV-.
CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 727D+6, RBL 11.5, WL 156. EVALUATED CORROSION OF FLOOR STRAP. FOUND TO BE OUT OF LIMITS, RECEIVED NEW STRAP AND APPLIED WHITE ENAMEL ALL IAW SRM 51-10-02, AMM 51-21-73-370-804, AND ACO 5360-E-16462.
CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM. REMOVED, REPLACED, AND INSTALLED A NEW SHIELD IAW SRM 51-10-02, SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A0081, REV A.
CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED A NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 53-00-53-1A-2, SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A7500, REV-.
CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED A NEW AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 53-00-53-1A-2; SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500, REV-.
BS 663, LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT LBL 45, WL 165. REMOVED, REPLACED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0, AND DWG 111A1000, REV A.
FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, STEP 4.B.(4).
AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, STEP 4.B.(4).
EGPR SURROUND DOUBLER CRACKED BS 233, WL 175+8, ABOVE S24R. TRIMMED DAMAGED AREA; FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-15-2R-4, REPAIR 4, PARG 4 (B-M).
CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS 767 TO 787, RBL 21, WL 156. CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED, REPLACED, AND INSTALLED A NEW AFT CARGO BAY ATTACH ANGLE IAW SRM 51-10-02, SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A8123 REV -.
AFT ATTENDANCE PANEL EMERGENCY LIGHT SWITCH IS BROKEN. REMOVED AND REPLACED AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER IAW SWPM 20-84-14..
PANEL 194CL DELAMINATED ON OUTER SURFACE. PANEL 194CL REPAIRED IAW SRM 51-70-05-2R-2.
FWD SERVICE DOOR SLIDE BUSTLE TRIM HAS SHARP EDGE ON LOWER RIGHT CORNER.<[01] ADJ DOOR BUSTLE CORRECTED SHARP EDGE PER AMM 52-41-31. AC OK FOR SERVICE.
NOSE TIRE SEPARATION ON ROTATION AT ROTATION NOSEWHEEL VIBRATION INCREASED AND MATERIAL DEPARTED TO THE LEFT FROM THE NOSE WHEEL WELL AREA AND THE VIBRATION INCREASED. WE ELECTED TO LEAVE THE LANDING GEAR EXTENDED DUE TO THE UNKNOWN CONDITION OF THE NOSE GEAR. NO ABNORMAL ENGINE INDICATIONS OR SMELLS NOTED. AN EMERGENCY WAS DECLARED AND WE RETURNED TO DAL. THE LANDING WAS NOT OVERWEIGHT AND LANDING NORMAL EXCEPT FOR EXCESS NOSE GEAR VIBRATION.<[01] R AND R BOTH NLG WHEEL ASSY?S PER AMM 32-45-21. TIRE TREAD LOSS CONDITIONAL INSP ALSO PERFORMED REF TASK ID TTG8Q00X0W6T.
FWD SERVICE DOOR GIRT BAR RETAINING CLIP MISSING RIVET<[01] INSTALLED MISSING RIVET IAW AMM 25-66-01
GIRT BAR RETAINING HOOK ON FORWARD GALLEY DOOR IS LOOSE<[01] C/W EA M-23-125-01839
R2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED R2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1
L2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED L2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1
MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1
MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1
MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK PERFORMED I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1
EMERGENCY LIGHT ASSEMBLY ON G4 DAMAGED<[01] REMOVED AND REPLACED LIGHT ASSEMBLY I/A/W ENCORE CMM 25-31-05; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1
LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL DETERIORATED AND BROKEN PIECE AT END TIP.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
RIGHT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL CRACKED<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL REF SRM 51-40-02-0G-0;[02] VERIFIED STEP #1
MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' HAS EXFOLIATING CORROSION THAT IS OUT OF LIMITS<[01] REPAIRED MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' REF SRM 53-70-51-2R-6;[02] RII VERIFIED STEP 1;[03] COMPLETED SME INSPECTION OF WORKMANSHIP AND PAPERWORK AUDIT.
MAIN CABIN FLOOR PANEL #221GF FWD SECTION TIP CRACKED<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221GF AS PER B737 SRM 53-00-50-2R-6 PARAG 3-G-M; MATERIAL USED PO#1798939; PO#1690463.;[02] VERIFIED AND INSPECTED STEP #1. PERMANENTLY APPLIED ON DAMAGE AREA OF MAIN CABIN FLOOR ACCESS PANEL 221GF.
LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 333AT BLADE SEAL CRACKED.<[01] REMOVED AND REPLACED BLADE SEAL AT LEFT HORIZONTAL STABILIZER UPPER GAP COVER PANEL REF SRM 51-40-02-0G-0;[02] VERIFIED STEP #1
MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM STA 986.5 LBL 2'- 44'<[01] REMOVED NUTPLATE FOR ACCESS AS PER SRM 51-40-02-0G-0. CLEANED CORROSION AS PER SRM 51-10-02-0G-0 <BR>ORIGINAL THICKNESS 0.150'; MATERIAL REMOVED FROM LBL 2' THROUGH LBL 43: 0.001'; MATERIAL REMAINING 0.149'.;[02] CLEANED CORROSION AT FLOOR BEAM STA 986.5 LBL 2'- 44' AS PER SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA; IAW B737 NDT PART 4 51-00-00 PREC. 3 TOOLS: 27MG; B/C 172139; CAL. DUE 30-MAR-2024.<BR>FROM LBL 2 - LBL 43; MIN. THICKNESS 0.149? & LBL 44; MIN. THICKNESS 0.123?. ORIGINAL THICKNESS 0.150'; MATERIAL REMOVED FROM LBL 2' THROUGH LBL 43: 0.001'; MATERIAL REMAINING 0.149'. THE CORROSION AT LBL 44' WAS FOUND WITH EXFOLIATING CORROSION AND MATERIAL REMOVED WAS 0.027'; MATERIAL REMAINING 0.123' AND IT IS OUT OF LIMITS. SEPARATE FAULT WAS CREATED TO REPAIR CORROSION SPOT AT LBL 44' WITH NUMBER TTG8Q00PYDEC;[03] RII--- VERIFIED AND INSPECTED STEP #2.
MAIN CABIN STA 540 RBL 2' FLOOR PANEL BREAK CRACK<[01] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 RBL 2' AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 RBL 2' AS PER SRM 51-40-02-0G-0; BOEING DWG #143A0060.;[03] VERIFIED STEP 2
MAIN CABIN STA 540 LBL 2' FLOOR PANEL BREAK CRACK<[01] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 LBL 2' AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 LBL 2' AS PER SRM 51-40-02-0G-0; BOEING DWG #143A0060.;[03] VERIFIED STEP 2
MAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00PDXP8.;[02] VERIFIED STEP 1
MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT STRAP STA 1016+11' RBL 17'<[01] CLEANED AFT WET AREA AT FLOOR SUPPORT STRAP STA 1016+11' RBL 17'AS PER SOPM REF 20-30-03;[02] CLEANED AFT WET AREA AT FLOOR SUPPORT STRAP STA 1016+11' RBL 17'AS PER SOPM REF 20-30-03. PERFORMED UT THICKNESS INSP ON REWORKED AREA; IAW B737 NDT PART 4 51-00-00 PREC. 3 TOOLS: ZX-6; B/C 174231; CAL. DUE 19-DEC-2023. MIN. THICKNESS 0.049?. EVALUATED REWORKED AREA: ORIGINAL MATERIAL 0.050 REMOVED MATERIAL 0.001 REMAINING MATERIAL 0.049'. REWORKED AREA WITHING LIMITS AS PER REF SRM 51-10-02-0G-0;[03] VERIFIED AND INSPECTED STEP #2.
VERTICAL FIN L/H HORIZONTAL BOX HINGE CUTOUT UPPER SLIDING SEAL FWD GUIDE TRACK TIP CRACKED<[01] REMOVED AND REPLACED BOX HINGE CUTOUT UPPER SLIDING SEAL TRACK AT L/H HORIZONTAL STAB REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
VERTICAL FIN R/H HORIZONTAL BOX HINGE CUTOUT UPPER SLIDING SEAL FWD GUIDE TRACK TIP CRACKED<[01] REMOVE AND REPLACE TRACK ASSY REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
MAIN CABIN BL 0' BETWEEN STA 344-360 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BL 0' BETWEEN STA 344-360 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED; STEP # 1.
MAIN CABIN BL 0' BETWEEN STA 277-294.5 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BL 0' BETWEEN STA 277-294.5 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED; STEP # 1.
MAIN CABIN LBL 11' BETWEEN STA 344-360 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN LBL 11' BETWEEN STA 344-360 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED; STEP # 1.
MAIN CABIN BL 0' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND BOEING AIRCRAFT DWG # 143A5400.;[02] VERIFIED STEP 1
MAIN CABIN RBL 12' BETWEEN STA 344-360 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN RBL 12' BETWEEN STA 344-360 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1
MAIN CABIN FWD WET AREA INNER CHORD SUPPORT ANGLE LBL 60' BETWEEN STA 294.5-328 UPPER SURFACE CORROSION<[01] REMOVED AND REPLACED SUPPORT ANGLE AT MAIN CABIN FWD WET AREA INNER CHORD LBL 60' BETWEEN STA 309 TO 343 SRM 51-40-02-0G-0 AND DWG141A8110;[02] VERIFIED STEP 1
L-1 DOOR CUTOUT FWD SLIDE MOUNT FITTING CORRODED<[01] REMOVED AND REPLACED FWD SLIDE MOUNT FITTING AT L1 DOOR. AS PER; 51-40-02-0G-0 AND AIPC 53-42-00-29.;[02] VERIFIED; STEP # 1.
L-1 DOOR CUTOUT AFT SLIDE MOUNT FITTING CORRODED<[01] REMOVED AND REPLACED AFT SLIDE MOUNT FITTING AT L1 DOOR. AS PER; 51-40-02-0G-0 AND AIPC 53-42-00-29.;[02] VERIFIED; STEP # 1.
MAIN CABIN FLOOR PANEL 221CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 221CF AND WILL BE INSTALLED ON T/C TTG8Q00PDYRA;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 222DF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL 222DF. INSTALLATION WILL BE ACCOMPLISHED ON TASKS CARD TTG8Q00PDYQU.;[02] VERIFIED STEP 1
FOUND CRACK AT AFT CARGO COMPT. AFT CORNER SCUFF PLATE.<[01] RECEIVED REPAIRED AFT CARGO COMPT AFT CORNER SCUFF PLATE FROM OUTSIDE VENDOR (PN: 146A8343-7 PO: 2043476). SCUFF PLATE WILL BE INSTALLED PER TASK CARD TTG8Q002GEYU.;[02] VERIFIED STEP 1
MAIN CABIN RBL 10' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE. AS PER; SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED STEP 1
MAIN CABIN LBL 46' BETWEEN STA 312-328 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN LBL 46' BETWEEN STA 312-328 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1
MAIN CABIN LBL 13' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE AT MAIN CABIN LBL 13' BETWEEN STA 380-400. IN ACCORDING WITH SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] REJECT: SEVERAL RIVETS NOT BUCK PROPERLY SEE N/R TTG8Q00Q253L;[03] CORRECTED REJECTION SEE WORK CARD TTG8Q00Q253L;[04] VERIFIED STEPS 1 AND 3
MAIN CABIN LH STA 303.9 INNER CHORD CRACK<[01] REMOVED AND REPLACED INNER CHORD AT MAIN CABIN L1 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP 1
REF. CARD: 23-153-02955-TLD. PERFORM PERMANENT REPAIR AT WTB FAIRING 193AL; L/E AREA WITH EROSION & DELAMINATION DAMAGE.<[01] REPAIRED DAMAGE AREA AT FAIRING PANEL #193AL AS PER SRM 51-70-04-2R-13 .MATERIAL USED BMS9-3-7781 PO#1738579;[02] VERIFIED STEP # 1
CRACK FOUND ON LT HORIZONTAL STAB. LOWER IN-SPAR SKIN AT STA. 193.90 RIB; 17' APPROX. FROM L/E; I/B ROW (CRACK LENGTH 0.50') CRACK FOUND ON LT HORIZONTAL STAB. LOWER IN-SPAR SKIN AT STA. 193.90 RIB 17' APPROX. FROM L/E I/B ROW (CRACK LENGTH 0.50')<[01] ACCOMPLISHED REPAIRS AT L/H HORIZONTAL STAB LOWER INSPAR SKIN AT STA 193.90 RIB 17'APROXIMATELY FROM L/E REF SRM 55-10-01-2R-11 REPAIR 11. REPAIR INSPECTION REQUIREMENTS ARE AS FOLLOWS: <BR>INSPECTION THRESHOLD IS 56;000 TOTAL FLIGHT CYCLES. A DETAILED VISUAL INSPECTION WILL BE REQUIRED AT AN INTERVAL OF 9;000 FLIGHT CYCLES AND AN EXTERNAL LOW FREQUENCY EDDY CURRENT (LFEC) INSPECTION AT INTERVAL OF 9;000 FLIGHT CYCLES.
LH WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATE PLATES HOLES ELONGATED<[01] REMOVED SERRATED PLATE AT LH WING DEFLECTOR RIB TO DEFLECTOR PANEL AS PER SRM 51-40-02 HOLES NOT ELONGATED FOUND WORN; AFTER EVALUATION ON DEFLECTED SUPPORT BEAM NO FASTENER HOLES ELONGATED NOTED ONLY FOUND SERRATED PLATE DAMAGED AS PER SRM 51-10-02-0G-0; INSTALLED NEW PARTS AT LH WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATE PLATES AS PER SRM 51-40-02-0G-0.;[02] CORRECTION OF STEP 1 INSTALLED NEW PARTS AT LH WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATE PLATES AS PER SRM 51-40-02-0G-0 AND DWG# 115A2000.;[03] CORRECTION ON STEP 2 REMOVED SERRATED PLATE AT LH WING DEFLECTOR RIB TO DEFLECTOR PANEL AS PER SRM 51-40-02 HOLES NOT ELONGATED FOUND WORN; AFTER EVALUATION ON DEFLECTED SUPPORT BEAM NO FASTENER HOLES ELONGATED NOTED ONLY FOUND SERRATED PLATE DAMAGED AS PER SRM 51-10-02-0G-0; INSTALLED NEW PARTS AT LH WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATE PLATES AS PER SRM 51-40-02-0G-0 AND DWG# 115A2000.;[04] CORRECTIONS ON STEPS 1-3 <BR>AFTER FURTHER EVALUATION ON L/H WING DEFLECTOR CONTROL RIB FOUND NO ELONGATED HOLES ONLY SERRATED PLATE DAMAGED (WORN) NOTED AS PER SRM 51-10-02-0G-0.<BR>REMOVED AND REPLACED SERRATED PLATE AT L/H WING DEFLECTOR CONTROL RIB TO DEFLECTOR PANEL AS PER SRM 51-40-02-0G-0 AND DWG 115A2000.;[05] VERIFIED STEP 4
PHOTOLUMINESCENT ESCAPE PATH LIGHTING STRIP AT ROW 1 DEF LOOSE<[01] RESECURED STRIP REF AMM 33-51-15
PANEL 193AL HAS LEADING EDGE DELAMINATION APPROXIMATELY 12 FROM TOP OF PANEL<[01] DELAMINATION DAMAGE FOUND ON PANEL 193AL LEADING EDGE 12? FROM TOP; FOUND TO BE OUT OF LIMITS IAW SRM 53-40-70 4. B. (6);[02] C/W EA 23-153-02955
193B PANEL HAS SEVERAL ELONGATED FASTENER HOLES.<[01] REMOVE AND REPLACED THE 193B PANEL PER AMM 53-51-21.;[02] C/W INSPECTION.
DOOR 2 RIGHT AFT SLIDE NEEDS TO BE REPOSITIONED<[01] PART REMOVED FOR SLIDE R AND R.;[02] REMOVED AND REPLACED AFT SERVICE DOOR SLIDE IAW MT 725-61-06-AS.
R2 SLIDE FLAPS EXPOSED<[01] ACCOMPLISHED MT 725-66-01
SEVERAL EMERGENCY LIGHTS INOP ON RH SIDE OF AIRCRAFT. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
EMERGENCY EXIT BULLNOSE LIGHTS OUT AT 14 A;B;C AND 17 A;B;C. / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY M1670 IAW AMM 33-51-06.
ENTRY DOOR FWD LOWER EXIT SIGN LENS DAMAGED ; / [01] R+R LENS IAW AMM 33-51-01
FED FWD GIRT BAR FITTIN IS LOOSE ; / [01] TIGHTENED FED FWD GIRT BAR FFITTIN IAW AMM 25-66-02-400-801 STEPS 3.E.(1).(C); [02] INSPECTION COMPLETE
PANEL 193D HAS DELAMINATION TO OUTER SURFACE (MARKED) ; IDENTIFIED PANEL IAW SRM 53-40-70-0I-1 FIG 2 ITEM 12. DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A (6)(C). DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-2 & SRM 51-70-04-2R-11 (CORE POTTING) AS GIVEN IAW SRM 53-40-70-2R-1 PARA 4.B (1) TABLE 201. REMOVED DAMAGED OUTER SKIN AND PARTIAL DEPTH CORE; (1.1' IN DIAMETER; 5.5' FROM T/E; 13.25' FROM RT EDGE) IAW SRM 51-70-04-2R-2 PARA 4.A - 4.C. FABRICATED REPAIR PLIES USING BMS 9-3ST120 LOT#1352337-1; INSTALLED WITH BMS 8-301CL1 LOT#JH1GAA7833. LEAK CHECK GOOD AND SET TO CURE IAW SRM 51-70-04-2R-2 PARA 4G-I.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 23 BS 500A+14; BS 500B+10; BS 500C+6; BS 500C+10. BS 500C+14. REMOVED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. FABRICATED LOCATED AND DRILLED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0 AND DWG#143A7500; REV.-; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0; OK TO PRIME.; [07] VERIFIED CORRECTIVE ACTION 6. OKAY TO PRIME; [08] APPLIED PRIMER ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL23; FROM BS500A TO BS500D; IAW SOPM 20-41-02.; [09] VERIFIED CORRECTIVE ACTION 8; [10] COMPLETED STEPS 1 THRU 5; [11] VERIFIED COMPLETE STEPS 1 - 5.
CRACK ON FWD CARGO BAY GUSSET AT BS 500D L/H STRINGER 19. ; / [01] REMOVED FWD CARGO BAY GUSSET BS 500D L/H STRINGER 19 IAW SRM 51-40-02.; [02] RECEIVED NEW GUSSET P/N 143A9481-5; LOCATED AND DRILLED NEW GUSSET AT FWD CARGO BAY BS 500D L/H STR 19L IAW SRM 51-40-05-OG-0.; [03] VERIFIED CORRECTIVE ACTION 1 AND 2.; [04] OK TO INSTALL.; [05] OK TO INSTALL GUSSET PN 143A9481-5; [06] INSTALLED NEW GUSSET FWD CARGO BAY BS500D L/H STRINGER 19L IAW SRM 51-40-02-0G-0; DWG#143A7902; [07] RII- VERIFIED INSTALLATION OF THE FWD CARGO GUSSET AT BS500D STR19L PER SRM 51-40-02-0G-0; DWG#143A7902; [08] WORKSCOPE COMPLETE
CORROSION ON AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT AT RBL 21 BS 727C+2; BS 727C+8; BS 727C+15; BS 727D+14; BS 727E+6; BS 727E+14; BS 727E+18; BS 747+2; BS 747+18. REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-10-02 PARAGRAPH 15. FOUND TO BE OUT OF LIMITS ALLOWABLE DAMAGE IAW SRM 53-OO-53-1A-2 FIG 103 DETAIL 'E'. REMOVED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02. LOCATED AND DRILLED AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IAW DWG 146A7502; ID:0049 REV:- AND SRM 51-40-05. TREATED IAW SRM 51-20-01.
CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+3; BS 767+7; BS 767+11. ; / [01] DAMANGE FOUND ON ACB FWD SHIELD BS 767-797 RBL 22 WL164 P/N 146A8127-12 FOUND TO BE OUT OF LIMIT IAW SRM PART WILL BE REPAIRED BY REMPLACEMENT IAW SRM 51-10-02.; [02] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM; PART WILL BE REPLACED.; [03] VERIFIED CORRECTIVE ACTIONS 1-2.; [04] RECEIVED ON AFT CARGO BAY FWD DOOR SHIELD NEW AT RBL 22 BS767 TO BS794 ITEM 146A8127U12 PO #849483. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A0081; [05] VERIFIED CORRECTIVE ACTION 4; [06] ACB FWD SHIELD WILL BE REPLACED ON CUSTOMER CARD # TTG8Q004EY39; [07] VERIFIED ACB FWD SHIELD WILL BE REPLACED ON CUSTOMER CARD # TTG8Q004EY39.
CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 22 BS 847+1. DAMANGE FOUND ON ACB AFT SHIELD FOUND TO BE OUT OF LIMIT IAW SRM. LOCATED AND DRILLED NEW SHIELD IAW 737-700 SRM 51-40-05-0G-0 DWG 146A0081. REPLACED.
CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 23 BS 500+6. REMOVED AND EVALUATED SHIELD ON FWD CARGO BAY AFT DOOR, NO FOUND ALLOWABLE DAMAGE LIMITS; DUE NOT LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; STEP 9. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-05; AND DWG 143A8123. INSTALLED NEW SHIELD IAW SRM 51-40-02-0G-0-; AND DWG#143A0080 ID:0023 REV:-; [08] INSTALLED FWD CARGO BAY AFT DOOR SHIELD AT RBL 23; FROM BS 500 - BS 500A. IAW. SRM 51-40-02-0G-0-; AND DWG#143A0080 ID:0023 REV.
CORROSION ON AFT CARGO BAY SIDEWALL TO FLOOR SUPPORT AT LBL 21 BS 727C+10; BS 727D+2; BS 727E+14; BS 747+5; BS 767+7; BS 767+18; BS 787+7. FABRICATED NEW ACB FLOOR TO SIDE WALL SUPPORT AND FABRICATED REPAIR SPLICE. LOCATED AND DRILLED ALL PARTS IAW SRM 51-40-05 AND SRM 53-00-53-2R-5 REPAIR 5. REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, SRM 53-00-53-2R-5, REPAIR 5, DWG 146A7500, AND DWG 149A8102.
CORROSION ON AFT CARGO BAY THRESHOLD SUB WEB AT RBL 26 BS 787+13; BS 787+16; BS 787+19; BS 807+2; BS 827+1; BS 827+3; BS 827+6; BS 827+7. REMOVED CORROSION ON SUBTHRESHOLD WEB. FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1; PARAG. 4.G.(2) DETAIL G. COMPLETED STEPS 1-8. LOCATED AND DRILLED NEW ACB SUBTHRESHOLD WEB IAW SRM 51-40-05-0G-0 AND DWG 146A8340. INSTALLED NEW ACB SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG#146A8340; ID:0028; REV:-.
CORROSION ON AFT CARGO BAY FWD DOOR SHIELD TO FRAME ATTACH ANGLE AT RBL 25 BS 767. ; / [01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM; PART WILL BE REPLACED; [02] VERIFIED NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM; PART WILL BE REPLACED.; [03] REMOVED AND REPLACED NEW ATTACH ANGLE ON AFT CARGO BAY FWD DOOR SHIELD RBL 25 BS767. IAW SRM 51-40-02 AND DWG 146A0081; [04] VERIFIED REPLACED NEW ATTACH ANGLE ON AFT CARGO BAY FWD DOOR SHIELD RBL 25 BS767. IAW SRM 51-40-02 AND DWG 146A0081.; [05] VERIFIED ALL STEPS COMPLETE.
CRACK ON FWD CARGO BAY FRAME TO INTERCOSTAL ATTACH ANGLE AT LBL 23 BS 400. ; / [01] DAMAGE FOUND ON INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL23; FOUND TO BE OUT OF LIMITS DUE TO O LIMITS ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9.C.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOVED FWD CARGO BAY FRAME TO INTERCOSTAL ATTACH ANGLE CRACKED AT LBL 23 BS 400 IAW SRM 51-40-02.; [04] RECEIVED NEW ANGLE WITH ITEM#143A7502U155; LOT#1478785-5; LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05 AND DWG#143A7505. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION ENTRIES 3. AND 4.<BR><BR>OK TO INSTALL NEW ANGLE; [06] INSTALLED NEW FCB FRAME TO INTERCOSTAL ATTACH ANGLE BS400 LBL23 IAW
AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED ; / [01] WELDED CRACK ON ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL ID; E10583; SN;KJ256554; [02] VERIFIED ACTION 1; [03] PT INSPECTED WELD AREA IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP USED: RADIOMETER ID: ATS2561-1;2;3; [04] SANDED WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] OK TO INSTALL; [07] OK TO INSTALL; [08] INSTALLED ACB AFT CORNER SCUFF PLATE PER 53-11-02-420-801).; [09] VERIFIED CORRECTIVE ACTION 8
FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED ; / [01] WELDED CRACK ON RADIUS OF FCB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N;KJ256554; [02] VERIFIED ACTION 1; [03] PT INSPECTED WELD AREA IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP USED: RADIOMETER ID: ATS2561-1;2;3; [04] SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA 4.B.(5); [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] REQUEST OK TO INSTALL FWD CORNER SCUFF PLATE; [07] OK TO INSTALL FWD CORNER SCUFF PLATE; [08] INSTALLED THE FWD CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE IAW AMM TASK 53-11-02-420-801; [09] VERIFIED CORRECTIVE ACTION 8
AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED ; / [01] WELDED CRACK ON ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL ID; E10583; SN;KJ256554; [02] VERIFIED ACTION 1; [03] PT INSPECTED WELD AREA IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP USED: RADIOMETER ID: ATS2561-1;2;3; [04] SANDED WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] OK TO INSTALL; [07] OK TO INSTALL; [08] INSTALLED ACB FWD CORNER SCUFF PLATE PER 53-11-02-420-801).; [09] VERIFIED CORRECTIVE ACTION 8
RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 3RD VERTICAL STIFFENER IS CRACKED. ; / REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 3RD VERTICAL STIFFENER IAW SRM 53-10-09-2R-4 REPAIR-4; [03] REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR-4; [04] VERIFIED CORRECTIVE ACTIONS 1-3.<BR><BR>APPLICABILITY AND DAMAGE REMOVAL.; [05] HFEC INSPECTED DAMAGE CUTOUT AND OPEN HOLES IN REPAIR AREA PER 737NDT PART 6 51-00-00 PROCEDURES 23 AND 16. NO CRACKS FOUND. TOOL N600 ATS1465.; [06] FABRICATED [1] T-SECTION MADE FROM 60-5872#7075-T76511 EXTRUSION ; AMS-QQ-A-200/15 ; LOT# 1476286-1 ; FABRICATED [2] ANGLE MADE FROM BAC1490-2793 # 7075T62 EXTRUSION LOT# 1474027-1 AND FABRICATED (2EA) [3] SHIMS MADE FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR-4; OK TO TREAT AND PRIME ALL REPAIR PARTS AND CUTOUT; [07] VERIFIED CORRECTIVE ACTION ENTRY 6.<BR><BR>OK TO TREAT AND PRIME; [08] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.;] INSTALLED REPAIR PARTS PER SRM 55-10-09-2R-4; [11] RII- VERIFIED INSPAR RIB REPAIR PER SRM 55-10-09-2R-4.; [12] VERIFIED RIB REPAIR IS COMPLETE PER SRM 55-10-09-2R-4. RIB WILL BE REINSTALLED ON TTG8Q00A83QY
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 2ND VERTICAL STIFFENER IS CRACKED. ; / VERIFIED THE APPLICABILITY OF SRM 55-10-09-2R-4; [03] VERIFIED CORRECTIVE ACTIONS 1; 2. <BR><BR>VERIFIED APPLICABILITY AND DAMAGE REMOVAL.FABRICATED -1 T-SECTION FROM 60-5872#7075-T76511 EXTRUSION ; AMS-QQ-A-200/15 ; LOT# 1476286-1 ; FABRICATED -2 ANGLE FROM BAC1490-2793 # 7075T62 EXTRUSION LOT# 1474027-1 ; FABRICATED -3FILLER FROM 7075T6 0.050' LOT#5087747-1 CLAD . AND FABRICATED (2EA) -4 SHIMS FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATE; DRILLED AND APPLIED A CHEMICAL CONVERSION COATING TO ALL REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ; OK TO PRIME; [11] VERIFIED CORRECTIVE ACTION 10; [12] PERFORMED A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA (INCLUDING UNDERLYING STRUCTURE ) FOR CORROSION ; EXISTING REPAIRS OR ANY OTHER DEFECTS ; IAW SRM 55-10-09-2R-5 REPAIR 5; [13] VERIFIED CORRECTIVE ACTION 12. NO CORROSION; EXISTING REPAIRS; OR DEFECTS NOTED; [14] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO ALL REWORKED AREAS AND ALL REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ; OK TO INSTALL; [15] VERIFIED CORRECTIVE ACTION ENTRY 14.<BR><BR>OK TO INSTALL REPAIR PARTS; [16] INSTALLED REPAIR PARTS AND APPLIED FILLET SEAL TO REPAIR PARTS IAW SRM 55-10-09-2R-5 STEP 4.N - R.; [17] VERIFIED CORRECTIVE ACTION ENTRY 16.; [18] REPAIRED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB STA120.30; 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.
RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 4TH VERTICAL STIFFENER IS CRACKED. ; / REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR-4; [04] VERIFIED CORRECTIVE ACTION 1-3;<BR><BR>APPLICABILITY AND DAMAGE REMOVAL.; [05] HFEC INSPECTED CUTOUT IN STIFFENER PER 737NDT PART 6 51-00-00 PROCEDURE 23. FOUND CRACK IN WEB AND MARKED IN RED INK. TOOL N600 ATS1465.;FABRICATED [1] T-SECTION MADE FROM 60-5872#7075-T76511 EXTRUSION ; AMS-QQ-A-200/15 ; LOT# 1476286-1 ; FABRICATED [2] ANGLE MADE FROM BAC1490-2793 # 7075T62 EXTRUSION LOT# 1474027-1 AND FABRICATED (2EA) [4] SHIMS MADE FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR-5; OK TO TREAT AND PRIME ALL REPAIR PARTS AND CUTOUT; [11] FABRICATED (3)FILLER 7075 T6 0.050' CLAD LOT# 1407842-2 APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-5 ] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-5 OK TO INSTALL.; [15] VERIFIED SRM APPLICABILITY STEP 8 FOR FLANGE REPAIR AND STEP 14. OK TO INSTALL REPAIR PARTS; [16] INSTALLED REPAIR PARTS PER SRM 55-10-09-2R-5; [17] RII- VERIFIED REPAIR OF THE R/H HORZ. INSPAR RIB ON 4TH STIFFENER PER SRM 55-10-09-2R-5.; [18] VERIFIED RIB REPAIR IS COMPLETE PER SRM 55-10-09-2R-5. RIB WILL BE REINSTALLED ON TTG8Q00A83QY
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 4TH VERTICAL STIFFENER IS CRACKED. ; / CUT AND REMOVED THE DAMAGE FROM THE 4TH VERTICAL STIFFENER OF THE L/H HORIZONTAL STABILIZER RIB STA 120.30 IAW SRM 55-10-09-2R-4 ; REPAIR 4FABRICATED -3FILLER FROM 7075T6 0.050' LOT#5087747-1 CLAD . AND FABRICATED (2EA) -4 SHIMS FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATE; DRILLED AND APPLIED A CHEMICAL CONVERSION COATING TO ALL REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ; OK TO PRIME; [11] VERIFIED CORRECTIVE ACTION 10; [12] PERFORMED A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA (INCLUDING UNDERLYING STRUCTURE ) FOR CORROSION ; EXISTING REPAIRS OR ANY OTHER DEFECTS ; IAW SRM 55-10-09-2R-5 REPAIR 5; [13] VERIFIED CORRECTIVE ACTION 12. NO CORROSION; EXISTING REPAIRS; OR DEFECTS NOTED; [14] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO ALL REWORKED AREAS AND ALL REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ; OK TO INSTALL; [15] VERIFIED CORRECTIVE ACTION ENTRY 14.<BR><BR>OK TO INSTALL REPAIR PARTS; [16] INSTALLED REPAIR PARTS AND APPLIED FILLET SEAL TO REPAIR PARTS IAW SRM 55-10-09-2R-5 STEP 4.N - R.; [17] VERIFIED CORRECTIVE ACTION ENTRY 16.; [18] REPAIRED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB STA120.30; 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.; [19] VERIFIED CORRECTIVE ACTION ENTRY 18.
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 3RD VERTICAL STIFFENER IS CRACKED. ; / CUT AND REMOVED THE DAMAGE FROM THE 3RD VERTICAL STIFFENER OF THE L/H HORIZONTAL STABILIZER RIB STA 120.30 IAW SRM 55-10-09-2R-4 ; REPAIR 4; [03] VERIFIED CORRECTIVE ACTION 1; 2.<BR><BR>VERIFIED APPLICABILITY AND DAMAGE REMOVAL FABRICATED -2 ANGLE FROM BAC1490-2793 # 7075T62 EXTRUSION LOT# 1474027-1 ; AND FABRICATED (2EA) -4 SHIMS FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATED ; DRILLED AND APPLIED A CHEMICAL CONVERSION COATING TO ALL REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4 ; OK TO PRIME; [07] VERIFIED CORRECTIVE ACTION 6; [08] PERFORMED A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA (INCLUDING UNDERLYING STRUCTURE ) FOR CORROSION ; EXISTING REPAIRS OR ANY OTHER DEFECTS ; IAW SRM 55-10-09-2R-4 REPAIR 4; [09] VERIFIED CORRECTIVE ACTION 8. NO CORROSION; EXISTING REPAIRS; OR DEFECTS NOTED; [10] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO ALL REWORKED AREAS AND ALL REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4 ; OK TO INSTALL; [11] VERIFIED CORRECTIVE ACTION ENTRY 10. <BR><BR>OK TO INSTALL REPAIR PARTS; [12] INSTALLED REPAIR PARTS AND APPLIED FILLET SEAL TO REPAIR PARTS IAW SRM 55-10-09-2R-4 STEP 4.M - Q.; [13] VERIFIED CORRECTIVE ACTION ENTRY 12.; [14] REPAIRED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB STA120.30; 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.
RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 2ND VERTICAL STIFFENER IS CRACKED. ; / REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 2ND VERTICAL STIFFENER IAW SRM 53-10-09-2R-4 REPAIR-4; [03] REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR-4; [04] VERIFIED CORRECTIVE ACTIONS 1-3.<BR><BR>APPLICABILITY AND DAMAGE REMOVAL; [05] HFEC INSPECTED CUTOUT IN STIFFENER PER 737NDT PART 6 51-00-00 PROCEDURE 23. FOUND CRACK IN WEB AND MARKED IN RED INK. TOOL N600 ATS1465.; [06] REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB WEB STA. 120.30 2ND IAW SRM 55-10-09-2R-4 REPAIR-4; [07] HFEC REQUEST AT RH HORIZONTAL STABILIZER INSPAR RIB WEB TO ENSURE NO CRACKS EXIST FABRICATED [1] T-SECTION MADE FROM 60-5872#7075-T76511 EXTRUSION ; AMS-QQ-A-200/15 ; LOT# 1476286-1 ; FABRICATED [2] ANGLE MADE FROM BAC1490-2793 # 7075T62 EXTRUSION LOT# 1474027-1 AND FABRICATED (2EA) [3] SHIMS MADE FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR-4; OK TO TREAT AND PRIME ALL REPAIR PARTS AND CUTOUT;] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.CHEMICAL CONVERSION AND PRIMER APPLICATION PER SRM 55-10-09-2R-4. INSTALLED REPAIR PARTS PER SRM 55-10-09-2R-4; [VERIFIED RIB REPAIR IS COMPLETE PER SRM 55-10-09-2R-4. RIB WILL BE REINSTALLED ON TTG8Q00A83QY.
R/H INBD MAIN FLAP BROKEN NUTPLATE AT RIB ATTACH POINT (MARKED) 24.5' INBD OF OTBD EDGE ON LEADING EDGE ; / [01] REPLACED BROKEN NUT PLATE. WITH A NEW ONE IAW SRM 51-40-02 DWG 113A2100. REV B
L/H EMERGENCY EXIT ROW EMERGENCY ROPE COVER LOOSE AT ROW 11. / SECURED COVER PER AMM.
FORWARD CABIN FLOOR BOARD PANEL 221BF CORNER TAB BROKEN, BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR BOARD 221BF IAW SRM.
PASSENGER CABIN STRINGER CLIP BRACKET CRACKED IN RADIUS AT BS. 259, STR. 8L. / R&R STRINGER CLIP PER SRM AND DWG.
CRACK AT STA 540 INTERCOSTAL AFT SIDE ABOVE FASTENER LBL 0-24. / REMOVED AND REPLACED STA 540 INTERCOSTAL LBL 0-24 IAW BOEING DWG 143A0060 REV:- AND B737 SRM 51-40-02-0G-0
PASSENGER CABIN; STA 277; STR 10R; FWD SIDE OF FRAME. STRINGER CLIP IS CRACKED COMMON TO FRAME. / REMOVED AND REPLACED PASSENGER CABIN STA 277 STR 10R; FWD SIDE OF FRAME; STRINGER CLIP IAW DWG 141A1110 REV- AND B-737 SRM 51-40-02 A TAG WN 6387 P/N 141A125-92
CABIN PANEL 241AAF TOP SURFACE PLY IS DAMAGED IN SEVERAL AREAS. / REPAIRED UPPER FACESHEET MISISNG FIBERS ON FLOORBOARD PANEL (241AAF) WITH WET-LAY-UP REPAIR I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-M (REV 69)
CABIN PANEL 242TF UPPER FACE PLIES ARE DAMAGED 7' FROM AT EDGE. / REPAIRED UPPER FACESHEET MISSING FIBERS ON FLOORBOARD PANEL (242TF) I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-M (REV 69)
CABIN PANEL 241XF LOWER SURFACE PLY IS DAMAGED AT BL 0 10' FROM AFT EDGE / REPAIRED LOOSE PLIES ON LOWER SURFACE OF FLOORBOARD PANEL (241 XF) WITH WET-LAY-UP REPAIR IAW B737-700 SRM 53-00-50-2R-1 (3) A-M (REV 69)
CABIN PANEL 241XF TOP SURFACE PLY IS DAMAGED AT SEVERAL LOCATIONS / REPAIRED UPPER FACESHEET AT MISSING PLIES AREAS ON FLOORBOARD PANEL (241 XF) WITH WET-LAY-UP REPAIR IAW B737-700 SRM 53-00-50-2R-1 (3) A-M (REV 69)
EMPENAGE TAIL CONE LEFT HAND SIDE WHERE ELEVATOR SEAL RUBS HAS AN AREA OF DELAMINATION / REPAIRED EMPENAGE TAIL CONE 4H SIDE AREA OF DECLAMINATION I/A/W B737-700 SRM'S 53-80-70-2R-1 REV 69+51-70-04-2R-1 REV 69+ 51-70-04-2R-0 REV 69 AND B737-700 AMM 51-21-99-300-801 REV 69 (A22759)(A50534)(A13438)
CABIN PANEL 242UF TOP SURFACE PLY IS DAMAGED 16' FROM AFT EDGE. / REPAIRED UPPER FACESHEET WITH MISSING FIBERS ON FLOORBOARD PANEL (242 VF) WITH WET-LAY-UP REPAIR I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-M (REV 69)
R1 DOOR #5 BEAM FOUND TO BE CRACKED. / R&R #5 BEAM IAW SRM AND DWG.
REF CARD #I14079 FORWARD SERVICE DOOR #4 BEAM FOUND TO BE CRACKED DURING NDT INSP. / REMOVED FORWARD SERVICE DOOR #4 BEAM AND INSTALLED NEW #4 BEAM FOR FORWARD SERVICE DOOR IAW SRM 51-40-02-0G-0 AND BOEING DWG # 141A6535 REV:C
RIGHT WING #6 FLAP TRACK FORWARD FAIRING 642AB OUTBOARD SEAL RETAINER IS CRACKED / REMOVED AND REPLACED RT WING #6 FLAP TRACK FORWARD FAIRING 642AB OUTBOARD SEAL RETAINER IAW B737 SRM 51-40-02-0G-0 STEP 9 AND B737 IPC 27-51-18-02 P. 7. ATAG A73917
R/H HORIZONTAL STABILIZER LEADING EDGE 341B RIB CHORD CRACKED AT LEADING EDGE STA. 123.85. / R&R RIB IAW SRM AND DWG.
FWD CARGO COMPARTMENT FLOOR PANEL 120AF HAS CORROSION AROND THE OUTSIDE EDGES / REMOVED AND EVALUATED CORROSION ON PANEL 120AF ORIGINAL MATERIAL THICKNESS .071' LOSS OF .004' WITH .067' REMAINING. BLEND FOUND TO BE OUT OF LIMITS DUE TO LENGTH OF BLEND OVER 20' PER SRM 53-00-53-1A-1. FABRICATED REPLACEMENT PANEL 120AF PART #453A1610-14 PER DWG 453A1610 REV C
R/H HORIZONTAL STABILIZER LEADING EDGE 341B RIB EVIDENCE OF CRACKED AT LEADING EDGE STA. 291.21. / R&R RIB IAW SRM AND DWG.
L/H HORIZONTAL STABILIZER LEADING EDGE 331B RIB CRACKED AT LEADING EDGE STA. 188.94. / R&R RIB IAW SRM AND DWG.
L/H HORIZONTAL STABILIZER LEADING EDGE 331B RIB CHORD CRACKED AT LEADING EDGE STA. 105.26. / R&R RIB IAW SRM AND DWG.
FWD CARGO COMPARTMENT FLOOR PANEL 120CF HAS CORROSION AROND THE OUTSIDE EDGES / REMOVED AND EVALUATED CORROSION ON PANEL 120CF. ORIGINAL MATERIAL THICKNESS .071' LOSS OF .005' WITH .066' REMAINING. BLEND FOUND TO BE OUT OF LIMITS DUE TO LENGTH OF BLEND OVER 20' PER SRM 53-00-53-1A-1. FABRICATED REPLACEMENT PANEL 120CF PART #453A1610-32 PER DWG 453A1610 REV C
R/H HORIZONTAL STABILIZER LEADING EDGE 341B RIB CRACKED AT LEADING EDGE STA. 160.04. / R&R RIB IAW SRM AND DWG.
R/H HORIZONTAL STABILIZER LEADING EDGE 341B RIB CRACKED AT LEADING EDGE STA. 179.64. / R&R RIB IAW SRM AND DWG.
R/H HORIZONTAL STABILIZER LEADING EDGE 341B RIB CRACKED AT LEADING EDGE STA. 198.23. / R&R RIB IAW SRM AND DWG.
AFT CARGO COMPARTMENT STA 767 TO 793 RBL 22 WL 158; SHIELD IS CORRODED TOP AND BOTTOM SIDES. / REMOVED AND EVALUATED CORROSION ON AFT CARGO FWD SHIELD. ORIGINAL THICKNESS .050' LOSS OF .014' WITH .036' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRW 53-00-53-1A-2. REMOVED AND REPLACED SHIELD PART# 146A8127-12 PER SRW 51-40-02-0G-0 AND DWG 146A0081 REV-- REMOVABLE COMPONENT P/N 146A8127-12
AFT CARGO COMPARTMENT STA 767-787 RBL 22 WL 158; SHEILD SUPPORT ANGLE IS CORRODED AT NUTPLATES. / REMOVED AND EVALUATED CORROSION ON SHIELD SUPPORT ANGLE ORIGINAL THICKNESS .050' LOSS OF .012' WITH .038' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED -53 SUPPORT ANGLE PER SRM 51-40-02-0G-0 AND DWG 146A123 REV-
AFT CARGO COMPARTMENT Z CHANNEL CORRODED BETWEEN BS. 727E+10 TO BS. 807, LBL 22. / R&R Z-ANGLE PER SRM.
AFT CARGO COMPARTMENT STA 867 LBL 10; BULKHEAD PANEL SUPPORT BRACKET IS CRACKED AT BOTTOM. / REMOVED AND REPLACED SUPPORT BRACKET PART #149A8109-114 PER SRM 51-40-02-0G-0 AND DWG 149A8109 REV B
AFT CARGO COMPARTMENT STA 793 RBL 22 WL 158; NUT PLATE STRAP IS CORRODED ON BOTTOM. / REMOVED AND REPLACED NUTPLATE STRAP PART #146A8128-22 PER SRM 51-40-02-0G-0 AND DWG 146A8128 REV- AT STA 799 RBL 22.
AFT CARGO COMPARTMENT STA 793 RBL 22 WL 158; NUT PLATE STRAP IS CORRODED ON BOTTOM. / REMOVED AND REPLACED NUTPLATE STRAP PART #146A8128- 21 AT STA 793 RBL 22 PER SRM 51-40-02-0G-0 AND DWG 146A8128 REV-
FWD CARGO COMPARTMENT STA 727 BL0; FWD BULKHEAD PANEL SUPPORT BRACKET IS CRACKED. / REMOVED AND REPLACED BRACKET AT STA 727 BLO PER SRM 51-40-02-0G-0 AND AIPC 53-11-01-26A
AFT CARGO COMPARTMENT STA 727A-727B LBL22 WL 158; INTERCOSTAL IS CORRODED ON UPPER FLANGE AT FASTENER HOLES. / REMOVED AND EVALUATED CORROSION. ORIGINAL MATERIAL THICKNESS .030' LOSS OF .020' WITH .010' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED -1 INTERCOSTAL PER SRM 51-40-02-0G-0 AND DWG 146A7502 REV-
AFT CARGO COMPARTMENT STA 747-767 RBL 22 WL 158; INTERCOSTAL IS CORRODED ON UPPER FLANGE AT NUTPLATES. / REMOVED AND EVALUATED CORROSION ON INTERCOSTAL STA 747-767 RBL 22. ORIGINAL THICKNESS .030' LOSS OF .010' WITH .020' REMAINING BLENDS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED INTERCOSTAL PART # 146A7505-2 PER SRM 51-40-02-0G-0 AND DWG 146A7502 REV- REMOVEABLE COMPONENT P/N 146A7505-2
FORWARD CARGO PIT BAFFLE CLIP AFT SIDE OF BS. 500C FRAME, LBL 24 CRACKED. / R&R BAFFLE CLIP IAW SRM & DWG.
FORWARD CARGO PIT STA 500D BULKHEAD STRUCTURE RIGHT CURVED LOWER CHORD RBL 25 WL 157 HAS CORROSION AROUND LOWER FASTENER HOLE / REPLACED FORWARD CARGO STA 500D RH COVERED BLKHD SUPPORT PN 143A9485-34 I/A/W SRM 51-40-02-0G-0 & DWG 143A7902 SHEET 209.
FORWARD CARGO PIT BAFFLE CLIP FORWARD SIDE OF BS. 500C FRAME LBL 24 CRACKED. / R&R BAFFLE CLIP IAW SRM & DWG.
FORWARD CARGO DOOR SURROUND STRUCTURE FORWARD SHIELD CORRODED AT BS. 420+17, RBL 24, AROUND NUTPLATE ON UPPER AND LOWER SURFACE. / R&R SHIELD IAW SRM & DWG.
FORWARD CARGO PIT R/H SIDE PLATE HAD CORROSION ON UPPER SURFACE BETWEEN BS. 500A TO BS. 500D, RBL 24. / R&R R/H Z-ANGLE PER SRM AND DWG.
FORWARD CARGO DOOR SURROUND STRUCTURE LOWER SILL WEB CORRODED BETWEEN BS. 440 TO BS. 492, RBL 28, ON UPPER SURFACE. / R&R SILL WEB IAW SRM & DWG.
FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM, DWG, AND AMM.
FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW SRM, DWG, AND AMM.
L-2 DOOR LOWER HINGE PANEL 834DZ AFT VERTICAL SUPPORT BRACKET IS CRACKED / REMOVED AND REPLACED L2 DOOR LOWER HINGE PANEL 834DZ; ASSEMBLY; IAW SRM 51-40-02-0G-0 STEP 8E; 9B ATAG: IM 1047
R/H WING TRAILING EDGE PANEL 661CB INTERNAL AFT MATING SURFACE HAD SEVERAL FASTENER HOLES CRACKED. / REPAIRED PANEL 661CB IAW SRM.
R/H WING TRAILING EDGE PANEL 661AB INTERNAL AFT MATING SURFACE HAD SEVERAL FASTENER HOLES CRACKED. / REPAIRED PANEL 661AB IAW SRM AND AMM.
R-2 DOOR LOWER HINGE PANEL 844DZ AFT VERTICAL SUPPORT BRACKET IS CRACKED IN RADIUS / REMOVED AND REPLACED R2 DOOR PANEL 844DZ ASSEMBLY ON W/O 40254-8500-0002; Y142045.
R-2 DOOR LOWER HINGE PANEL 844DZ HAS CORROSION AROUND FORWARD NUTPLATE / REMOVED AND REPLACED R2 DOOR ACCESS PANEL 844DZ; ASSEMBLY; IAW SRM 51-40-02-0G-0 STEP 8E; 9B.
LEFT WING LEADING EDGE PANEL 521HB FORWARD INBOARD CORNER IS CRACKED AT FASTENER HOLE / REPAIRED AND RESTORED PAINT FINISH TO PNL 521 HB FWD INBD CORNER FASTNER HOLE ELONGATED AND CRACKED MARKED. IAW B737-700 SRM 51-41-01-2R-1 REV 69; SRM 51-70-04-2R-9 REV 69; SRM 51-70-04-2R-0 REV 69; AMM 51-21-99-300-802 REV 69; AMM 51-21-99-300-801 REV 69. A33188; A19242; A13438; A44971
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1668, M1669, M1672 AND M1675. R&R BATTERIES PER AMM.
L2 DOOR SLIDE GIRT NEEDS REPACKED. REPACKED SLIDE PER MT AND AMM.
LEFT CENTER FUEL PUMP LOW PRESSURE LIGHT ON W/2800 LBS. FUEL IN TANK. R&R LT CENTER BOOST PUMP PER AMM.
L2 DOOR SLIDE PARTIALLY OUT OF BOX, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW AMM & MT.
R2 DOOR SLIDE CAME OUT OF HOUSING. R&R SLIDE PER MT.
R1 DOOR EMERGENCY ESCAPE SLIDE SKIRT LOOSE FROM SHROUD. SECURED SLIDE PER MM.
R2 DOOR SLIDE LOOSE. SECURED THE HOOK AND LOOP STRIP IAW AMM.
FLOOR SUPPORT CRACKED AT BS 540, BETWEEN RBL 20 TO RBL 40. R&R SUPPORT PER SRM.
VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB PER SRM.
R1 DOOR EMERGENCY EXIT LIGHTED SIGN LENS BROKEN. R & R THE LENS IAW SIP.
LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.
L2 DOOR EMERGENCY EXTERIOR LIGHT INOP. RELAMPED LIGHT PER AMM.
FLOOR SUPPORT BRAKE ASSY PANEL AT STA 540 LEFT OF BL 0 CRACKED / REMOVED AND REPLACED FLOOR SUPPORT BRAKE ASSY PANEL AT STA 540 LEFT OF BL 0 IAW SRM 51-40-02
LT WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER IAW EA.
L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOCKING CLIP BROKEN. R&R CLIP PER AMM.
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
LEFT MID-CABIN EMERGENCY BULLNOSE LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
L1 DOOR AFT EMERGENCY LIGHT LENS DIRTY. R & R THE LENS IAW AMM.
AFT CARGO DOOR FORWARD EMERGENCY LIGHT LENS DIRTY. R & R THE LENS IAW AMM.
RIGHT OVERHEAD BINS BULLNOSE EMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 3 TO 4. R & R THE BATTERY PACK IAW AMM.
LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATVE. R & R THE FUSE IAW AMM.
R1 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
STRINGER CLIP 26L CORRODED AT BS 727E. R & R THE STRINGER CLIP IAW SRM.
AFT CARGO DOOR SUB THRESHOLD WEB CORRODED. R & R THE WEB IAW SRM.
FRAME SPLICE CORRODED AT BS 787, BETWEEN STRINGERS 24 - 25R. R & R THE FRAME SPLICE IAW SRM.
RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 847 - 867. R & R THE SUPPORT IAW SRM.
AFT CARGO BAY RT CARGO TRACK CORRODED AROUND FASTENER HOLES BETWEEN BS 787 - 827. R & R THE CARGO TRACK IAW SRM AND DWG.
AFT CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 847. R & R THE SUPPORT IAW DWG & SRM.
AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 767. R & R THE SUPPORT IAW DWG & SRM.
FORWARD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A - 500D, RBL 24. R & R THE SUPPORT IAW SRM.
FORWARD CARGO BAY FLOOR-TO- SIDEWALL SUPPORT CORRODED BETWEEN BS 400 - 480, LBL 24. R & R THE SUPPORT IAW SRM.
LEFT WING REAR SPAR WIGGLE PLATE ASSEMBLY CRACKED AT RSS 216. R & R WIGGLE PLATE ASSEMBLY IAW SRM.
R/H WING REAR SPAR WIGGLE PLATE ASSEMBLY CRACKED AT RSS 216. R & R THE WIGGLE PLATE ASSEMBLY IAW SRM.
LEFT HORIZONTAL STABILIZER RIB AT CRACKED AT STA 92.70, 2ND STIFFENER FROM FORWARD END. REPAIRED RIB IAW SRM.