N8642E
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2021-10-08 – 2021-10-08 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2021-10-08 – 2021-10-08 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EXTERIOR FUSELAGE, AFT OF L2 DOOR, EMERGENCY LIGHT BURNED OUT. REPLACED THE LAMP IAW AMM 33-51-04-960-801.
CRACKED ACCESS PANEL 551GB, TRAILING EDGE LT WING. REPAIRED THE ACCESS PANEL 551GB IAW SRM 51-70-05-2R-10, REPAIR 10.
CRACKED ANGLE OF ACCESS PANEL 844DZ OF DOOR GALLEY AT AFT GALLEY AREA. REPLACED THE ACCESS PANEL ANGLE ON GALLEY DOOR AREA DUE TO NO FOUND ALLOWABLE DAMAGE FOR CRACK IAW SRM 52-10-02-1A-4, SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 411A2119, SHEET 71, REV-. MEASUREMENT OF CRACK: L=0.262 INCH.
CRACKED ANGLE ON ACCCESS PANEL 834DZ OF THE ENTRY DOOR. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 411A2119, SHEET 72, REV-. MEASUREMENT OF CRACK: L=0.453 INCH.
CRACK SUPPORT ANGLE, BS 500I, STR 28R IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE, AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 320, REV-.
CRACKED SUPPORT ANGLE, BS 500I, STR 28L REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7902, SHEET 320, REV-.
BROKEN LENS OF EMERGENCY LIGHT, STRONGHBACK ROW 24-25 RT SIDE. REPLACED THE LENS IAW AMM 33-51-03-960-803, STEP 4.D, ITEM (1) & (2).
CRACKED ACCESS PANEL 551GB T/E LT WING. REPAIRED THE ACCESS PANEL 551GB IAW SRM 51-70-05-2R-10, REPAIR 10.
CRACKED WEB, ORSS 271 RT WING T/E. REPLACED THE WEB IAW SRM 51-10-02, STEP 9, SRM 51-40-02-0G-0, & DWG 115A2512, SHEET 16, REV-.
CRACKED SUPPORT ANGLE, BS 867, S26 - 27L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A.
ELONGATED HOLES ON SUPPORT ZEE BTW BS 727C - 747, RBL 21 IN THE AFT CARGO BAY. TOOK INITIAL MEASUREMENTS OF HOLES ON THE SUPPORT ZEE, HOLE NR 1: D=0.246, HOLE NR 2: D=0.247, HOLE NR 3: D=0.246. REAMED HOLE NR 1: D=250, HOLE NR 2: D=0.250, HOLE NR 3: D=0.250. FOUND WITHIN TOLERANCE IAW SRM 51-40-05-0G-0, TABLE A, FIGURE 4, SHEET 2, & DWG 146A7502, SHEET 54, REV -.
CORRODED WEB - INTERCOSTAL BS 747 - 767, RBL 21, WL 155 IN THE AFT CARGO BAY. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND DWG 146A7500, SHEET 236, REV-.
CORRODED SHIELD WEB, BTW BS 767 - 794.3, RBL 21, WL 155 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A.
CRACKED PAX CABIN FLOOR SUPPORT BTW BS 380 - 400, LBL 51. REPLACED THE FLOOR SUPPORT & FASTENERS IAW SRM 51-40-02-0G, SRM 51-10-02 PARAGRAPH 9, & DWG 143A5400, SHEET 183, REV -.
CRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV-.
CORRODED ANGLE, BS 986.5 + 10, RBL 42, WL 208.1. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, DWG 147A5700, SHEET 123, REV A, SRM 51-10-02, STEP 9 ITEM A.
CRACKED ANGLE, BS 500G, RBL 21, IN THE CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.
CRACKED ANGLE, BS 500G, RBL 21 AFT SIDE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, 138, & 139, REV-.
CRACKED GUSSET ANGLE, BS 500I, S19R. REPLACED THE GUSSET & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7902, SHEET 256, REV B.
CRACKED ANGLE, BS 440, LBL 21. IN THE CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 138, REV -.
CRACKED ANGLE, BS 500H, RBL 21 FWD SIDE IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.
CRACKED ANGLE, BS 500H, RBL 21 AFT SIDE IN THEFWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.
CRACKED ANGLE, BS 500H, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, DWG 143A7505, SHEET 138, REV -.
CRACKED ANGLE, BS 400, LBL 21, IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505,SHEET 137, REV-.
CRACKED SCUFF PLATE AFT CORNER IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 & 4 - 7.
CORRODED FLOOR STRAP, AFT POSITION BULKHEAD IN THE FWD CARGO BAY. REPLACED THE FLOOR STRAP IAW SRM 51-40-02-0G-0.
PULL HANDLE EXPOSED ON AFT SERVICE DOOR SLIDE<[01] FOUND VELCRO PULL HANDLE COVER TUCKED UP IN SLIDE COVER ;PULLED DOWN AND PUT INTO PLACE PER SIP
R2 DOOR SLIDE FELL OUT OF COVER. REINSTALLED SLIDE IAW AMM 25-66-00 AND TASK CARD 725-61-06
EMERGENCY EXIT LIGHT BATTERY PACK M1695 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.;[02] WN50315;[03] VERIFIED C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1694 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR><BR>WN50316;[02] VERIFIED C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1673 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN50318;[02] VERIFIED C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1671 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR><BR>WN50317;[02] VERIFIED C/W
040-001 BRACKET ON AFT SIDE OF # 1 ENGINE O/B COWL IS WORN AND CRACKED. HAS STREAMER ATTACHED.<[01] REMOVED WORN AND CRACKED BRACKET ON AFT SIDE OF #1 ENG O/B COWL AND REPLACED WITH NEW BRACKET; PN 314-2264-7 ATAG A307566; IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED ITEM 1<BR>C/W
R1 DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED R1 DOOR LINER ASSIST HANDLE IAW AMM-52-41-31-400-802 PG 3 STEP F ITEM 2;[02] VERIFIED ITEM 1<BR>C/W
R2 DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED R2 DOOR LINER ASSIST HANDLE IAW AMM-52-41-31-400-802 PG 3 STEP F ITEM 2;[02] VERIFIED ITEM 1<BR>C/W
L1 DOOR EMERGENCY SLIDE AFT GIRL BAR HOLDER LOOSE <[01]. REPLACED FWD L1 DOOR SLIDE AFT GIRT BAR HOLDER FWD RIVET PER SIP. REF AMM 25-66-01. OK FOR SVC.
OVERHEAD EMERGENCY LIGHT LENS COVER 4-5 ABC BROKE<[01] 05 - OK TO CONTINUE PER [MEL 33-15-02;INTERIOR EMERGENCY EXIT LIGHTING SYSTEM - EMERGENCY AISLE LIGHTS]. REPLACED LENS ON OVERHEAD EMERGENCY LIGHT 4-5 ABC. OP CHECKS GOOD IAW SIP
LEFT AFT OVER WING EXIT EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED M1670 EMERGENCY LIGHT BATTERY PER AMM 33-51-06.
THE FOLLOWING EXTERNAL EMERGENCY EXIT LIGHTS ARE INOP: LH OWE AFT; RH OWE AFT; L2 DOOR; RH AFT FUSELAGE; LH AFT FUSELAGE.<[01] REMOVED BATTERY PACKS M1670; M1671 AND M1673 BATTERY PACKS; REPLACED WITH SERVICEABLE UNITS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.;[02] JOB COMPLETE.
R/H O/B AFT FLAP DELAMINATED ON I/B END<[01] REMOVED; REPLACED; AND ADJUSTED R/H O/B AFT FLAP PER AMM 27-51-22.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-5.
BODY RIB CRACKED ON RH A/C BAY AT BS 540+18; RBL37.WL136(APPROX.)<[01] 'REPAIRED PER EA 24-157-01843 WITH AN INSPECTION THRESHOLD DEFINED IN 24-157-01843-DTI1 AND 24-157-01843-DTI2.';[02] VERIFIED CORRECTIVE ACTION #1
PANEL BREAK AT BS 540 RBL 2 IS CRACKED<[01] REMOVED AND REPLACED PANEL BREAK PER SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] CARD COMPLETE
PANEL BREAK AT BS 540 LBL 2 IS CRACKED<[01] REMOVED CRACKED PANEL BREAK AT BS 540 LBL 2 IAW SRM 51-40-02-0G-0.<BR>OBTAINED AND INSTALLED NEW PANEL BREAK AT BS 540 LBL 2 IAW SRM 51-40-02-0G-0 AND DRW 143A0060;[02] UPDATED MEASUREMENTS;[03] VERIFIED CORRECTIVE ACTION #1
#1 ENGINE I/B FAN COWL OIL TANK ACCESS DOOR SHIELD CRACKED<[01] REMOVED AND REPLACED ACCESS DOOR SHIELD IAW SRM 51-40-02.;[02] PARTS REMOVED / INSTALLED;[03] REJECTION OF CORRECTIVE ACTION 1 AND STEP 1: 1EA BAD RIVET AT LOWER END OF #1 ENGINE I/B FAN COWL OIL TANK ACCESS DOOR SHIELD. SEE TTG8Q00UH35J
LEFT OUTBOARD AFT FLAP INBOARD SIDE UPPER AND LOWER SURFACE DELAMINATED.<[01] REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP REF AMM 27-51-11. REQUIRES OPS CHECK.;[02] REMOVED AND REPLACED LEFT OB AFT FLAP REF AMM 27-51-22-400-801; THRU STEP F.(5)(G). OB AFT FLAP ADJUSTMENT REQUIRED.;[03] COMPLIED WITH FLAP ADJUSTMENT IAW AMM 27-51-26
PHOTO ILLUMINATION STRIP AT ROW 1 FED DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01; SP #1;[02] REPLACED PHOTO ILLUMINATION STRIP AT ROW 1DEF PER AMM 33-51-15. MEL CLEARED.
FWD MEGAPHONE IS INOP.<[01] REMOVED AND REPLACED FWD MEGAPHONE PER AMM 25-64-00. OPS CHECK NORMAL.
L/H FWD EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT L/H FWD CEILING AND BATTERY PACK AT 8 ABC AIR GRILLE LOCATIONS; PER AMM 33-51-06. EMERGENCY EXIT LIGHTS OP?S CHECK GOOD.
L/H FWD EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT L/H FWD CEILING AND BATTERY PACK AT 8 ABC AIR GRILLE LOCATIONS; PER AMM 33-51-06. EMERGENCY EXIT LIGHTS OP?S CHECK GOOD.
CREW REPORTS FWD SLIDE L1 DOOR FELL OUT OF CONTAINER<[01] REINSTALLED L1 DOOR SLIDE PER MT 725-61-06
RIGHT FWD ISLE EMERGENCY LIGHTS IN-OP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M2335 LOCATION PER AMM 33-51-06. OPS CHECK GOOD.
RH OVER WING EMERGENCY LIGHT INOP<[01] RELAMPED RH OVER WING EMERGENCY LIGHT PER AMM 33-51-04
ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT R2 DOOR INOP<[01] R/R AFT R/H BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.
AT CRUISE F/A HEARD A BANG NOISE MID CABIN. COCKPIT AND CABIN THEN SMELLED FAINT SMELL OF SMOKE. RUN QRH; SMELL IMMEDIATELY CLEARED OUT.<[01] PERFORMED CONDITIONAL INSPECTION FOR SMOKE IN CABIN PER AMM 05-51-56. DETERMINED CAUSE OF SMOKE & ODOR TO BE A DEFECTIVE LT PACK ACM. ACM REPLACED PER AMM 21-51-04. REFER TO LOGPAGE #2101069 FOR CORRECTIVE ACTION & PARTS REPLACEMENT.
EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2816 ARE INOP. / [01] REMOVED NON-OPERATIONAL BATTERY PACK; INSTALLED AND PERFORMED GOOD INSTALLATION TEST OF NEW BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 1.;[03] VERIFIED CORRECTIVE ACTIONS #1 AND #2
EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1675 ATE INOP<[01] REMOVED AND REPLACED M675 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1;[03] PERFORMED GOOD TEST OF NEW BATTERY PACK PER AMM 33-51-06-960-805 STEPS 4.E.6.A-C.;[04] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 3
EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP<[01] REMOVED AND REPLACED M1672 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1;[03] PERFORMED GOOD TEST OF NEW BATTER PACK PER AMM 33-51-06-960-805 STEPS 4.E.6.A-C.;[04] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 3.;[05] VERIFIED CORRECTIVE ACTION #3
EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATYERY PACK M1676 ARE INOP<[01] REMOVED AND REPLACED M1676 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1;[03] PERFORMED GOOD TEST OF NEW BATTER PACK PER AMM 33-51-06-960-805 STEPS 4.E.6.A-C.;[04] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 3;[05] VERIFIED CORRECTIVE ACTION #3
FLASHLIGHT BRACKET BROKEN AT AFT R/H ATTENDANCE SEAT OUTBOARD POSITION / [01] REPLACED FLASHLIGHT ASSY PER AMM 25-64-00-200-802 STEPS (4); (6); (7);[02] REPLACED FLASHLIGHT BRACKET ASSY PER AMM 25-64-00-200-802 SEC 10 B STEPS (3); (4); (6); (7) & AMM SWAD633A101-SWA SEC 2;[03] EDIT ITEM 1 AMM REFERENCE TO READ AMM 25-64-00-200-802; STEP 10. B.(4); (6); AND (7).
CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 1; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL1 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGEL PO#876312; LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL1 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED;[03] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED
CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 41; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 RBL41 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGLE PO# 876805 LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 RBL41 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE
CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 9; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL1 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGEL PO#876312; LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL1 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED;[03] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED
FWD ENTRY MOPSILL IS CRACKED COMMON TO 303 FRAME ON VERTICAL FLANGE LBL 54; WL 209. / [01] NOT ALLOWABLE LIMITS FOUND ON SRM FOR CRACK ON BS303 FED MOPSILL LBL54 WL209 REPLACEMENT OF THE PART IS APPLICABLE PER SRM 51-10-02-0G-0 PAR. 9.C;[02] REMOVE FED MOPSILL I.A.W SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FED MOPSILL I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 140A9810 OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL THE FED MOP SILL.;[05] VERIFIED MEASUREMENT TABLE.;[06] INSTALLED NEW FED MOPSILL BS270-BS356 WL209 LBL54 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 140A9810 COMPLETED ALL REMOVED AND REPLACED TASK;[07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED MEASUREMENTS
FWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283. MARKED. / [01] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; CRACK NOTED AND MARKED ENDS.<BR>EQUIP ID. NORTEC 500D S/N IS000681 DUE 02/23;[02] REMOVED CRACK IN FRAME IN FWD CABIN STA 312; 11' BELOW STR 4L; WL 283. AREA REMOVED IS .300' BY .200' ON ENDV OF FRAME PER SRM 51-10-02-0G-0.;[03] VISUALLY INSPECTED BLEND AREA- NO CRACK NOTED VISUALLY.;[04] CORRECTED DIMENSION IN TABLE;[05] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; NO CRACK NOTED.<BR>EQUIP ID. NORTEC 500D IS000681 DUE 02/23;[06] PERFORMED .040' INSURANCE CUT ON 312 FRAME CUTOUT PER SRM 51-10-02-0G-0.;[07] PERFORMED .040' INSURANCE CUT ON 312 FRAME CUTOUT TRIMMED EDGES PER SRM 51-10-02-0G-0.;[08] EDITED TABLE;[09] ADDED TRIMMED EDGES TO STATEMENT;[10] VERIFIED CORRECTIVE ACTION 7 AND MEASUREMENT TABLE.;[11] REPAIRED DAMAGE ON FWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283 PER EA 22-153-02216.;[12] VERIFIED CORRECTIVE ACTION #11
CRACKED INTERCOSTAL STA 344-360; RBL 13; WL 208. / [01] REMOVED INTERCOSTAL STA 344-360; BL0; WL 200-208 FOR ACCESS PER SRM 51-40-02-0G-0.;[02] REMOVED DAMAGED INTERCOSTAL STA 344-360; RBL 13; WL 208 PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED AND DEBURRED NEW INTERCOSTAL STA 344-360; RBL 13; WL 200-208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. OK TO INSTALL BOTH INTERCOSTALS; AT 344-360 AT BL0; RBL 13.;[04] VERIFIED CORRECTIVE ACTION 3.;[05] VERIFIED MEASUREMENT TABLE;[06] INSTALLED A NEW INTERCOSTAL AT BS 344-360 RBL13 WL208 IAW SRM 51-40-02; AND BOEING DWG 141A5400. ALSO; REINSTALLED INTERCOSTAL FOR ACCESS AT BS 344-360 BL0 WL208 IAW SRM 51-40-02 AND BOEING DWG 141A5400.;[07] VERIFIED CORRECTIVE ACTION #6;[08] VERIFIED CORRECTIVE ACTION #6
CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 50; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL50 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGLE PO# 876805 LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL50 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE
CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL13 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGLE PO# 876805 LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL13 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE
CORROSION ON FWD SERVICE DOOR MOPSILL SCUFFPLATE ATTACH ANGLE STA 302-326; RBL 57- RBL 59; WL 209. / [01] REMOVED NUT PLATES COMMON TO FWD SERVICE DOOR MOP SILL SCUFF PLATE ATTACH ANGLE IAW SRM 51-40-02-0G-0 BLENDED CORROSION FROM ATTACH ANGLE IN SEVERAL SPOTS BS 302 TO 326 RBL 57 -59 WL 209 1' X 1' MAX REMOVED .012 FROM ORIGINAL .090 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-2 STEP 4.A FIG 102 USING DIAL INDICATOR ATS2678 S/N UNKNOWN CAL DUE 04/2023;[02] VERIFIED CORRECTIVE ACTION ITEM 1;[03] REMOVED CORRODED FWD SERVICE DOOR MOP SILL SCUFF PLATE ATTACH ANGLE AT BS 302-326 RBL 57 WL 209 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED AND COUNTERSUNK AND DEBURRED NEW FWD SERVICE DOOR MOPSILL SCUFFPLATE ATTACH ANGLE STA 302-326; RBL 57-RBL 59; WL 209 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0. OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4.;[06] VERIFIED MEASUREMENT TABLE.;[07] INSTALLED NEW FWD SERVICE DOOR MOPSILL SCUFFPLATE ATTACH ANGLE STA 302-326; RBL 57-RBL 59; WL 209 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 COMPLETED ALL REMOVED AND REPLACED TASK;[08] VERIFIED ITEM 7 CORRECTIVE ACTIONS.;[09] VERIFIED MEASUREMENTS.;[10] CHANGED MAJOR TO MINOR IN TABLE;[11] CHANGED MAJOR TO MINOR IN TABLE
CORROSION ON FLOOR SUPPORT STA 949; LBL 25; WL 208; UPPER SURFACE. / [01] NO LIMITS FOUND ON SRM FOR SPECIFIC DAMAGE SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT FIELD;[03] REMOVED FLOOR SUPPORT BS947-BS967 LBL25 WL208 I.A.W SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW FLOOR SUPPORT BS947-BS967 LBL25 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650. OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4. OK TO INSTALL FLOOR SUPPORT.;[06] INSTALLED NEW FLOOR SUPPORT BS 947-967 LBL25 WL 208 PER SRM 51-40-02-0G-0;[07] CORRECTED STEP 1;[08] CERTIFIED CORRECTION;[09] VERIFIED CORRECTIVE ACTION #6 AND STEP 1;[10] VERIFIED CORRECTIVE ACTION #6 AND STEP 1
CORROSION ON FLOOR SUPPORT STA 949; RBL 23.5; WL 208; UPPER SURFACE. / [01] NO LIMITS FOUND ON SRM FOR SPECIFIC DAMAGE SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT FIELD;[03] REMOVED FLOOR SUPPORT BS947-BS967 RBL24 WL208 I.A.W SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW FLOOR SUPPORT BS947-BS967 RBL24 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650. OK TO INSTALL;[05] VERIFIED CORRECTIVE BACTION 4 AND MEASUREMENT TABLE.;[06] INSTALLED FLOOR SUPPORT BS947-BS967 RBL24 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650.;[07] VERIFIED CORRECTIVE ACTION #6 AND STEP 1;[08] VERIFIED CORRECTIVE ACTION #6 AND STEP 1
CORROSION ON FLOOR SUPPORT STA 949; LBL 52; WL 208; UPPER SURFACE. / [01] NO LIMITS FOUND ON SRM FOR SPECIFIC DAMAGE SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT FIELD;[03] REMOVED DAMAGED FLOOR SUPPORT STA 947-986; LBL 52; WL 208 PER SRM 51-40-02-0G-0.;[04] REMOVED FLOOR SUPPROT STA 950; LBL 25-LBL 52; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.;[05] REMOVED DAMAGED FLOOR SUPPORT STA 947-967; LBL 52; WL 208 PER SRM 51-40-02-0G-0.;[06] CORRECTED BODY STATION 947-967.;[07] LOCATED AND DRILLED NEW FLOOR SUPPORT BS947-BS967 LBL52 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650. OK TO INSTALL;[08] VERIFIED CORRECTIVE ACTION 7. OK TO INSTALL FLOOR UPPORT.;[09] INSTALLED FLOOR SUPPORT BS947-BS967 LBL52 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650.;[10] VERIFIED CORRECTIVE ACTION #9 AND STEP 1;[11] UPDATED PARTS USED INFO.;[12] VERIFIED CORRECTIVE ACTION #9 AND STEP 1
G4B R/H STRAP BACKSIDE BOTTOM HAS CORROSION / [01] G4B R/H STRAP CONNECTOR ANGLE HAS NO LIMITS ON CORROSION; OUT OF LIMITS AND SRM 51-10-02-0G-0 IS APPLICABLE REPLACEMENT OF PART.;[02] REMOVED AND REPLACED G4B R/H STRAP CONNECTOR ANGLE PER SOPM 20-50-01.;[03] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 2. VERIFIED MEASUREMENT FIELDS ARE ACCURATE & COMPLETE.
AFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET BROKEN BS867 LBL10 WL166 / [01] REMOVED AND REPLACED ACB LAV TANK BULKHEAD LOWER BRACKET BS 867; LBL 10; WL 166 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 149A8104; DWG#149A8102.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED COMPLETE
AFT CARGO BAY CARGO FLOOR SPLICE STRAP HAS CORROSION BS727I +6 RBL20 WL156 / [01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 727I+6 RBL 20 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] RECEIVED NEW AFT CARGO BAY CARGO FLOOR SPLICE STRAP BS727I +6 RBL20 WL156 ON PO # 833679 INSTALL WELL BE ON CARD # TTG8Q00CX314;[04] VERIFIED CORRECTIVE ACTION #3
AFT CARGO BAY CARGO FLOOR SPLICE STRAP HAS CORROSION BS767+6 RBL20 WL156 / [01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 767+6 RBL 20 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] RECEIVED NEW AFT CARGO BAY CARGO FLOOR SPLICE STRAP BS767+6 RBL20 WL156 ON PO # 835775 INSTALL WELL BE ON CARD # TTG8Q00CX310;[04] VERIFIED CORRECTIVE ACTION #3
AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727F TO BS767 RBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727I+10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATD 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] VALIDATED APPLICABILITY OF SRM 53-00-53-2R-5;[04] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727E +12' - BS767; RBL21; WL156 PER SRM 51-40-02-0G-0; SRM 53-00-53-2R-5;[05] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727E +12' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+7' - BS727E+17' USING BAC1496-377#7075T62 LOT # 1494598-1 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5; AMM 51-21-41-370-802;[06] VERIFIED CORRECTIVE ACTION #5<BR>VERIFIED MEASUREMENTS;[07] APPLIED PRIMER TO FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-2R-5; AMM 51-21-72-370-804;[08] OK TO INSTALL REPAIR PARTS;[09] VERIFIED CORRECTIVE ACTION 7 AND 8; OK TO INSTALL;[10] INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT BS727E +12' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+7' - BS727E+17' PER SRM 51-40-02-0G AND DWG 146A7500; SRM 53-00-53-2R-5;[11] VERIFIED CORRECTIVE ACTION #10;[12] VERIFIED CORRECTIVE ACTION #10
AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS747 TO BS847 LBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 21 WL 21; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATD 2678 DUE 04/2023;[02] CORRECTION TO STEP 1; WL IS 156;[03] VERIFIED ACTION #1;2;[04] VALIDATED APPLICABILITY OF SRM 53-00-53-2R-5;[05] REMOVED DAMAGED PART OF THE ACB L/H FLOOR TO SIDEWALL SUPPORT BS727J+10 TO BS847; LBL21; WL156. PER SRM 53-00-53-2R-5 STEP 4. B & C.;[06] FABRICATED ACB L/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS BS727J+10 TO BS847; LBL21; WL156. PER DWG 146A7500 AND SRM 53-00-53-2R-5 STEPS 4. D. THRU H. FROM BAC1496-377#7075T62 EXT. CLAD LOT#1494598-1. SLICE LOCATION BS727J+10.;[07] VERIFIED CORRECTIVE ACTION #5; 6<BR>VERIFIED MEASUREMENTS;[08] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO ACB FABRICATED L/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS PER SRM 53-00-53-2R-5 STEP 4. I. AND J. OK TO INSTALL.;[09] VERIFIED CORRECTIVE ACTION #8;[10] INSTALLED FABRICATED ACB L/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS BS727J+10 TO BS847; LBL21; WL156. PER DWG 146A7500 AND SRM 53-00-53-2R-5 STEPS 4. K THRU N.;[11] VERIFIED CORRECTIVE ACTION #10
AFT CARGO BAY SHIELD FWD OF CARGO DOOR HAS AREAS OF CORROSION BS767 TO BS787 RBL21 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 767 TO BS 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] REMOVED ACB SHIELD BS767 TO BS793 RBL21 WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED; DRILLED AND DEBURRED NEW SHIELD BS767 TO BS793 RBL21 WL156 PER SRM 51-40-05-0G-0. AND DWG 146A0081.;[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL NEW SHIELD.;[07] OK TO INSTALL NEW SHIELD.;[08] INSTALLED NEW SHIELD BS767 TO BS793 RBL21 WL156 PER SRM 51-40-02-0G-0. AND DWG 146A0081.;[09] VERIFIED CORRECTIVE ACTOIN 8;[10] ADDED PARTS;[11] VERIFIED MEASUREMENTS
AFT CARGO BAY ATTACH ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 HAS AREAS OF CORROSION / [01] EVALUATED CORROSION ON ATTACH ANGLE UNDER SHIELD BS 767 TO BS 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] REMOVED ACB ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED; DRILLED AND DEBURRED NEW ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 PER SRM 51-40-05-0G-0 AND DWG 146A8123.;[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL NEW ANGLE UNDER SHIELD.;[07] OK TO INSTALL NEW ANGLE UNDER SHIELD.;[08] INSTALLED NEW ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 PER SRM 51-40-02-0G-0 AND DWG 146A8123.;[09] VERIFIED CORRECTIVE ACTION 8;[10] ADDED PARTS;[11] VERIFIED MEASUREMENTS
AFT CARGO BAY SUBTHRESHOLD WEB HAS CORROSION AT BS807 RBL26 WL156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 807 RBL 26 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] REMOVED ACB SUBTHRESHOLD WEB BS. 794-847 RBL 26 WL 156 PER SRM 51-40-02.;[04] LOCATED; DRILLED; DEBURRED; AND INSTALLED NUT PLATES ON NEW ACB SUB THRESHOLD WEB BS 794 TO BS847; RBL 26; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#146A8120; DWG#146A8340.;[05] VERIFIED CORRECTIVE ACTION #4; MEASUREMENT FIELD VERIFIED;[06] OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION 6 OK TO INSTALL;[08] INSTALLED NEW ACB SUB THRESHOLD WEB BS 794 TO BS 847; WL 156 PER DWG 146A8340 AND SRM 51-40-02-0G-0.;[09] VERIFIED CORRECTIVE ACTION #8;[10] VERIFIED CORRECTIVE ACTION #8
FWD CARGO BAY CENTER THRESHOLD WEB HAS CORROSION BS462 RBL28 WL156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 462 RBL 28 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] REMOVED FCB SUBTHRESHOLD WEB BS 440-492 RBL 28; WL 156 PER SRM 51-40-02.;[04] LOCATED; DRILLED; AND DEBURRED NEW FCB CENTER SUB THRESHOLD WEB BS 440 TO BS 492; RBL 28; WL 156 IAW SRM 51-40-05-0G-0; DWG#143A8330; DWG#143A8120.;[05] VERIFIED CORRECTIVE ACTION 4 AND MEQSUREMENT TABLE.;[06] OK TO INSTALL;[07] INSTALLED FWD CARGO BAY CENTER THRESHOLD WEB HAS CORROSION BS462 RBL28 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A8330;[08] CORRECTION: INSTALLED NEW FWD CARGO BAY CENTER SUB THRESHOLD WEB BS 440 TO BS 492; RBL 28 WL 156 IAW SRM 51-40-02-0G-0 AND 143A8330;[09] VERIFIED CORRECTIVE ACTION 6.<BR>OK TO INSTALL.;[10] UPDATED PARTS TABLE;[11] VERIFIED CORRECTIVE ACTION 8;[12] VERIFIED MEASUREMENT TABLE
LEFT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / [01] REMOVED LH UPPER SLIDE SEAL IAW AMM 53-31-31-000-802<BR>ASSEMBLED SEAL PLATE; TIE BAR; AND CORNER PLATES IAW AMM 53-31-31-400-802 STEPS 3.F (1-18);[02] VERIFIED CORRECTIVE ACTION #1;[03] INSTALLED SEAL PLATE IN TRACKS PER AMM 53-31-31-400-802 STEPS 3.F(19)-(21)<BR>TOOL ID ATS392 DUE 01-2023;[04] VERIFIED CORRECTIVE ACTION #3;[05] INSTALLED SLIDING SEAL IAW AMM 53-31-31-400-802 STEPS 3.F(22)-(28);G;[06] VERIFIED CORRECTIVE ACTION #5
#6 FLAP TRACK AFT FAIRING HAS DELAMINATED AREA AT O/B SIDE / [01] IDENTIFIED #6 AFT FLAP TRACK FAIRING PANEL 642BB IAW SRM 57-53-70-0I-3 FIGURE 1-2; 4 AND 14; ITEM 1; TABLE 3 AND 12<BR><BR>DAMAGE IS OUT OF ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1 FIGURE 101 AND 104; ZONE 1; PARA 4.A(5)<BR><BR>ENGINEERING IS REQUIRED DUE TO THE SIZE OF THE DAMAGE IS MORE THAN 3' DIA PER SRM 57-53-70-2R-1 PARA 4.A(1) AND 4.B(1); FIGURE 204; ZONE 1 AND TABLE 201<BR><BR>VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - MULTIPLE DISBONDS NOTED; REMOVE 2EA AREAS OF DISBONDS; AREA #1; REMOVED 4.5' X 8.8' OF OUTER OB SURFACE PLY (1 PLY); AREA #2; [07] DUE TO DAMAGE IS OUT OF REPAIRABLE LIMITS ON #6 AFT FLAP TRACK FAIRING THE PART WAS REPLACED WITH A SERVICEABLE UNIT. IAW SRM 57-53-70-1A-1 AND AIPC 27-51-18-01 ITEM 425 AFT TAIL CONE AND AFT MOUNT STRUCTURE WILL BE TRANSFERRED TO NEW UNIT FROM OFF UNIT ON FAULT TTG8Q00DRFYY.
L/H BS663 UPPER ATTACH ANGLE CRACKED ON VAPOR BARRIER LBL8 WL167.68 / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 REPAIR 5 AND UPDATED MEASUREMENT TABLE [12] INSTALLED LH BS663 UPPER ATTACH ANGLE REPAIR PARTS LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. BOND CHECK GOOD. TOOL ID:ATS1751 S/N:DC004716 DUE:10/2022. CAP SEALING AND LEAK CHECK ON INTERNAL SIDE FUEL TANK FASTENERS WILL BE ACCOMPLISHED ON CC#TTG8Q00DLKRU.;[13] VERIFIED CORRECTIVE ACTION 12;[14] FILLET SEALED; CAP SEALED EXTERNAL SIDE OF REPAIR AND APPLIED CIC TO BS663 LH UPPER ATTACH ANGLE REPAIR PARTS LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5.;[15] REMOVED PROTECTION OF EWIS @ LH BS 663 UPPER ATTACH ANGLE ON FWD AND AFT SIDE OF VAPOR BARRIER IAW AMM 20-60-07-913-801.;[16] VERIFIED CORRECTIVE ACTIONS 14 AND 15
FWD CARGO AC DISTRIBUTION BAY RIGHT FLOOR BREAK PNL ASSEMBLY CRACKED ; / [01] REMOVED AND REPLACED R/H BREAK PANEL ASSEMBLY IN FWD CARGO AC DISTRIBUTION BAY AS PER SRM 51-40-02
LEFT WING FORWARD EMERGENCY EXTERIOR LIGHT INOPERABLE. REMOVED AND REPLACED LEFT WING FORWARD EMERGENCY EXTERIOR LIGHT BULB, IN REF TO AMM 33-51-04. OPERATIONS CHECKS GOOD.
LH WING #6 SPOILER LOWER SURFACE DENT #8 DISBONDED / REPAIRED #8 DENT WITH DISBOND ON LOWER SKIN OF #6 SPOILER. IAW B737800 SRM 5770010I1; SRM 5770012R2; SRM 5170102R2; SRM 5170102R0; AMM 512199300801.
AFT CARGO BAY FLOOR PANEL 140DF CORRODED / EVALUATED CORROSION ON AFT CARGO BAY FLOOR PANEL 140DF AND FOUND ACCUMULATED LENGTH OF DAMAGE TO BE MORE THAN 20' MAXIMUM ALLOWED - OUT OF LIMITS IAW SRM 53-00-53-1A-1; FABRICATED NEW PANEL 140DF IAW AMM 25-52-01-201-801 AND BOEING DWG 453A2610 REV B; TO BE INSTALLED ON SA-M 565S TASK CARD PANEL SIGN OFF SHEET ATAG A11784
AFT CARGO BAY FLOOR PANEL 140EF CORRODED / EVALUATED CORROSION ON AFT CARGO BAY FLOOR PANEL 140EF; LENGTH OF TOTAL ACCUMULATED DAMAGE EXCEEDED 20' MAXIMUM ALLOWEABLE LENGTH - OUT OF LIMITS IAW SRM 53-00-53-1A-1; REPLACED WITH NEW/FABRICATED PANEL 140EF IAW AMM 25-52-01-201-801; TO BE INSTALLED ON SA-M 565S PANEL SIGN OFF SHEET; AND BOEING DWG 453A2610-SHT 38 REV. C. P/N 453A2610-58 ATAG A68668
AFT CARGO BAY FLOOR PANEL 140BF CORRODED / FOUND CORROSION TO BE MORE THAN 20' IN LENGTH WHICH IS OUT OF LIMITS. FABRICATED NEW PANEL 140BF I/A/W AMM 25-52-01-201; SRM 53-00-53-1A AND DRAWING 453A2610 REV. K
AFT CARGO BAY FLOOR PANEL 140AF CORRODED / EVALUATED CORROSION ON AFT CARGO PIT FLOOR PANEL 140AF CORROSION EXCEEDED THE 20 INCH ALLOWABLE LIMITS; OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND BOEING DRAWING 453A2610 SHEET 26 REV. E; TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804
AFT CARGO BAY FLOOR PANEL 140CF CORRODED / EVALUATED CORROSION ON AFT CARGO PANEL 140CF CORROSION EXCEEDS THE 20 INCH ALLOWABLE LIMITS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND BOEING DRAWING 453A2610 SHEET 11 REV C TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804
FWD PIT STA 500A TO STA 500I RIGHT Z ANGLE UPPER SURFACE CORRODED AT RBL 23 AND WL157 / REMOVED CORROSION FROM FWD CARGO BAY RH ZEE ANGLE STA 500A TO STA 500I RBL 23 WL157 IAW SRM 51-10-02-0G-0 AND USED 10X MAG GLASS NO DEFECTS NOTED EVALUATED MATERIAL LOSS TO BE .020' ORIGINAL T = .040' LIMIT = .004' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FABRICATED NEW ZEE ANGLE IAW SRM 53-00-53-2R-5 INSTALLED NEW ZEE ANGLE IAW SRM 51-40-02-0G-0 AND DWG 143A7500 REV - APPLIED CIC TO BOTTOM AND TOP SURFACES IAW AMM 51-21-91-620-802 P/N 143A7501-88
FWD PIT FLOOR PANEL 120DF CORRODED IN MANY LOCATIONS ON TOP SIDE OF AFT AND RH EDGES. / EVALUATED FWD PIT FLOOR PANEL 120DF CORROSION EXCEEDED LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801
AFT CARGO COMPARTMENT; FRAME; WL157; LBL21; BS747; CORRODED / AFT CARGO FRAME 747 LBL 21 CORRODED. BLENDED AND REMOVED CORROSION AND CHECKED WITH 10X MAG I/A/W 51-10-02-0G-0 SRM. 'OUT OF LIMITS' THICKNESS IS .063 MAT LOSS .010 REMAINING .053 I/A/W SRM 53-00-07-1A-1 FIG 102 DETAIL C. FABRICATED REPAIR DOUBLER TRIMMED; DEBURRED; DRILLED ALL FASTENER HOLES I/A/W SRM 53-60-07-2R-2 REPAIR 2. TREATED AND PRIMED NEW DOUBLER I/A/W SRM 51-21-72-370-804; SRM 51-21-07-06-0. INSTALLED NEW DOUBLER I/A/W SRM 51-40-02-0G-0 ALSO SRM 51-40-05-0G-0. APPLIED C.I.C TO REPAIR I/A/W AMM 51-21-91-620-802 (P/N 146A1265-61)
FWD PIT STA 500I BULKHEAD PANEL LWR SUPPORT ANGLE UPPER SURFACE CORRODED FROM LBL 20 TO RBL 23 / FWD PIT STA 500I BULKHEAD PANEL LOWER SUPPORT ANGLE UPPER SURFACE CORRODED FROM LBL 20 TO RBL 23 REMOVED AND REPLACED WITH NEW ANGLE P/N 143A9485Y35 IAW SRM 51-40-05-0G-0 AND BOEING DWG'S 143A9485 (PL) REV F AND 143A9481 REV - REMOVED CORROSION; VISUALLY INSPECTED AREA WITH 10X MAG NO DEFECTS NOTED IAW 51-1-02-0G-0 ORIG 'T' .071' LOSS OF .005' REMAINING .066' NO SRM ALLOWABLE LIMITS ATAG WN2583
FWD PIT STA 500+6' FLOOR SHIELD UPPER SURFACE CORRODED AT RBL 23 AND WL157. / REMOVED CORROSION FROM PIT STA 500+6' FLOOR SHEILD UPPER SURFACE AT RBL 23 AND WL 157; ORIGINAL THICKNESS .050' REMAINING .045' LOSS .005' NO ALLOWABLE LIMITS ON PART OUT OF LIMITS. BACK SHOP FORMED AND HEAT TREATED PART ON WORK ORDER # 41323-1400-0001 I/A/W BOEING DWG 143A8126 REV - FABRICATED NEW FLOOR SHEILD I/A/W BOEING 143A8125- REV.- REPLACED FLOOR SHEILD I/A/W 737-800 SRM 51-40-02-0G-0 AND BOEING DWG REV. -143A0080- REV - P/N 143A8126-38
FWD PIT FLOOR PNL 120CF HAS CORROSION ON UPPER SURFACE ALONG LH AND RH EDGES / FWD PIT FLOOR PNL 120CF HAS CORROSION ON UPPER SURFACE ALONG LH AND RH EDGES EVALUATED CORROSION FOUND IT EXCEEDS 20' OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 VERIFIED NEW MATERIAL P# 2024-T3-071 A TAG # A68671 IAW SRM 51-20-01-0G-0 PRIMED IAW AMM 51-21-72-370-804
FWD PIT FLOOR PNL 120AF HAS CORROSION ON UPPER SURFACE ALONG FWD AND RH EDGES / EVALUATED CORROSION ON UPPER SURFACE ALONG FWD AND RH EDGES OF FWD PIT FLOOR PNL 120AF; TOTAL ACCUMLATED CORROSION DAMAGE FOUND TO EXCEED 20' MAXIMUM LENGTH ALLOWED - OUT OF LIMITS; IAW SRM 53-00-53-1A-1; FABRICATED NEW FLOOR PANEL 120AF IAW AMM 25-52-01-201-801; TO BE INSTALLED ON SA-M 565S CARD PANEL SIGN OFF SHEET ATAG A63683
CABIN FLOOR PANEL 241AF FWD R/H CORNER IS MISSING CORE MATERIAL. REPAIRED CABIN FLOOR PANEL 241AF FWD R/H CORNER MISSING CORE IAW B737 SRM 53-00-50-2R-4 REV 69 ABD B737 SRM 53-00-50-2R-0 REV 69. A64736 A94414 A03261
AFT CARGO COMPARTMENT; Z-ANGLE; WL156; LBL20; BS727E +15' - 727F +15'; CORRODED MULTIPLE LOCATIONS / AFT CARGO Z-ANGLE L/H SIDE STA 727E TO 727F+15' CORRODED BLENDED AND REMOVED CORROSION ON Z-ANGLE AND CHECKED WITH 10X MAG I/A/W SRM 51-10-02-0G-0 THICKNESS IS .040; MAT LOSS IS .014; MAT REMINING IS .026 'OUT OF LIMITS' I/A/W SRM 53-00-53-2R-5 REPAIR 5. CUT AND REMOVED DAMAGED SECTION 727E TO 727J+10; FABRICATED NEW SECTION; DRILLED; DEBURRED; TRIMMED I/A/W SRM 53-00-563-2R-5. TREATED AND PRIMED AND INSTALLED NUT-PLATES I/A/W SRM 53-00-53-2R-5 STEP I;J;K;M. INSTALLED I/A/W SRM 53-00-53-2R-5 REPAIR 5 STEPS L. APPLIED C.I.C I/A/W SRM 53-00-53-2R-5 STEP N. P/N 146A7502-31
FWD PIT STA 500B TO 500G LEFT Z ANGLE CORRODED AT LBL 23 AND WL157 / REMOVED CORROSION AND EVALUATED MATERIAL LOSS ON FWD CARGO LH Z ANGLE FROM STA 500B TO 500G ORIGINAL 'T' .040' LOSS .010' REMAINING 'T' .030' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 REPAIRED LH Z ANGLE FROM STA 500B TO STA 500G IAW SRM 53-00-53-2R-5 P/N 143A7501-187
RH A/C PACK BAY. HORIZONTAL ANGLE COMMON TO LOWER CENTER FUEL TANK AT STATION 663 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. / REPIARED R/H STA 663 HORIZONTIAL ATTACH ANGLE 3RD FASTENER O/B OF KEEL BEAM VERTICAL ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5.
DIVERSION------------------------------FUMES & SMOKE IN CABIN. / INSPECTED A/C PER AMM 05-5156 & FIM 21-00-806. THE ONLY ISSUE FOUND IS LH RECIRE FAN BURNT UP & CAUSING SMOKEY SMELL (REF) LP# 1371078 FOR RECIRE FAN MEL A/C OK FOR SERVICE.
FLASHLIGHT IN FWD GALLEY INOP. / REPLACED BATTERY ON FWD GALLEY FLASHLIGHT PER SIP.
L1 DOOR LATCH LEFT ON DOOR BELOW SLIDE LOOSE. / R&R SLIDE PER MT.
ROW 15 OVERWING EXIT ROW LIGHT FLUTTERED. R&R LIGHT IAW AMM.
RT EMERGENCY LIGHTS INOP BETWEEN ROW 6 TO ROW 14. R&R BATTERY PACK PER AMM AND WDM.
R2 DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MT.
AFT MEGAPHONE INOP. R&R MEGAPHONE PER MM.
LT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED / R&R'D LT HORIZ STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.AMT 67660 INSP P44
R1 DOOR EMERGENCY EXIT LIGHTED SIGN LENS CRACKED. R & R THE LENS IAW MM.
AFT RT OTBD FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW CMM.