N8648A
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ON LEFT ENG SHUTDOWN; FUEL FLOW DROPPED DOWN INITIALLY THEN CAME UP, THEN DISPLAYED ENG FAIL AND SHUT DOWN. REMOVED NR 1 ENGINE HMU IAW AMM 73-21-10, REMOVED NR 1 ENGINE SERVO FUEL HEATER IAW AMM 73-11-07, REMOVED MAIN OIL/FUEL HEAT EXCHANGER IAW AMM 79-21-02. PARTIALLY REMOVED NR 1 ENGINE FUEL PUMP IAW AMM 73-11-01. R & R NR 1 ENG FUEL PUMP PACKAGE PER MT 773-11-00. OPS CHECKED GOOD.
ON LEFT ENG SHUTDOWN; FUEL FLOW DROPPED DOWN INITIALLY THEN CAME UP; THEN DISPLAYED ENG FAIL AND SHUT DOWN. REMOVED NR 1 ENGINE HMU IAW AMM 73-21-10; REMOVED NR 1 ENGINE SERVO FUEL HEATER IAW AMM 73-11-07. REMOVED MAIN OIL/FUEL HEAT EXCHANGER IAW AMM 79-21-02. PARTIALLY REMOVED NR 1 ENGINE FUEL PUMP IAW AMM 73-11-01. R & R NR 1 ENG FUEL PUMP PACKAGE IAW MT 773-11-00. OPS CHECKED GOOD.
CREW REPORTED R2 DOOR SLIDE PROTRUDING FROM BOTTOM OF HOUSING. ADJUSTED THE SLIDE IN R2 DOOR IAW AMM 25-66-01 AND MT 725-61-06.
OVERHEAD EXIT SIGN DETACHED. RESECURED LIGHT ASSY IAW AMM 33-51-00.
EMERGENCY LIGHT ASSOCIATES TO BATTERY PACK M1676 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1676; PERFORMED GOOD TEST PER AMM 33-51-06-960-805.
AFT EMERGENCY DOOR DOOR EXIT SLIDE; CAPTS SIDE; DETACHED FROM DOOR CASE <[01]. RE-INSTALLED L2 DOOR SLIDE IAW AMM 25-66-01 AND MT 725-61-06.
CENTER CABIN CEILING EMER EXIT SIGN TAGS BROKEN <[01]. R&R EXIT SIGN ASSY CENTER CABIN PER MM 33-51-01.
AFT MEGAPHONE HANDLE SEPARATED FROM BELL<[01] REMOVED AND REPLACED AFT MEGAPHONE REF AMM 25-64-00.
PANEL 561AB INBD MOUNTING WAFFLE PLATE HAS EVIDENCE OF CRACKING. (MARKED)<[01] REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-10-02 AND 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
AFT RIGHT SIDE EMERGENCY LIGHTS DO NOT ILLUMINATE AT ROW 17 & 21<[01] R&R BATTERY PACKS AT M1695; M1671 & M1670 IAW AMM 33-51-06. OPS CHECK GOOD IAW AMM 33-51-00.;[02] VICTOR GARIBAY (TECHNICIAN); 06-SEP-2024 22:18 UTC<BR>R&R BATTERY PACKS AT M1695; M1671 & M1670 IAW AMM 33-51-06. OPS CHECK GOOD IAW AMM 33-51-00.
PANEL 344AB BLADE SEAL DELAMINATED AT ENDS.<[01] DRILLED UP AND INSTALLED NEW PANEL IAW SRM 51-40-02.;[02] C/W INSPECTION
PASSENGER CABIN STA 540 BL 0 INTERCOSTAL FLOOR SUPPORT CRACKED.<[01] LOCATED AND MATCH DRILLED INTERCOSTAL IAW SRM 51-10-02.;[02] VERIFIED C/A # 1 : JAMES LYNCH (TECHNICIAN); 28-AUG-2024 21:34 UTC<BR>LOCATED AND MATCH DRILLED INTERCOSTAL IAW SRM 51-10-02.;[03] REMOVED AND REPLACED INTERCOSTAL AT STA 540 BL0 IAW SRM 51-10-02;[04] VERIFIED C/A # 3 : JAMES LYNCH (TECHNICIAN); 28-AUG-2024 22:06 UTC<BR>REMOVED AND REPLACED INTERCOSTAL AT STA 540 BL0 IAW SRM 51-10-02
LEFT WING TRAILING EDGE: DEFLECTION RIB SUPPORT BEAM ATTACHMENT. THE 2 HORIZONTAL ATTACHMENT FASTENERS ARE LOOSE, BEAM & BRACKET HOLES ARE ELONGATED. CUT OUT DAMAGE IN CONTROL RIB UPPER TAB IAW SRM 57-51-02-2R-4. CUT OUT DAMAGE IN SUPPORT BEAM IAW SRM 57-51-02-2R-1. PERFORMED AN HFEC INSPECT ALONG CUT EDGES. REF NDT PART 6; 51-00-00; PROCEDURE 4 OR NDT PART 6; 51-00-00; PROCEDURE 23. NO DEFECTS NOTED. PERFORMED AN OPEN HOLE HFEC INSPECT OF THE INITIAL FASTENER HOLES IN REPAIR AREA. REF NDT PART 6; 51-00-00; PROCEDURE 16. NO DEFECTS NOTED. DRILLED REPAIR PARTS FOR UPPER TAB REPAIR IAW SRM 57-51-02-2R-4. DRILLED REPAIR PARTS FOR UPPER TAB REPAIR IAW SRM 57-51-02-2R-4. LOCATED & DRILLED REPAIR DOUBLER FOR UPPER BEAM IAW SRM 57-51-02-2R-1. INSTALLED REPAIR PARTS IAW SRM 57-51-02-2R-4 & SRM 57-51-02-2R-1.
R/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON LOWER I/B SURFACE<[01] OK TO INSTALL O/B AFT FLAP.;[02] REMOVED AND REPLACED R/H OUTBD AFT FLAP PER AMM 27-51-22.;[03] INSPECTED WORK PERFORMED ON C/A #2.;[04] REMOVED AND REPLACED R/H OUTBD AFT FLAP PER AMM 27-51-22. SEE C/A'S AND STEPS FOR INDIVIDUAL SIGN OFFS.;[05] RII - CW INSPECTION AS REQUIRED C/A #4
L/H WING O/B AFT FLAP HAS AREA OF DELAMINATION ON LOWER I/B SURFACE<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-21;[02] LINE #1 INSPECTED AS REQUIRED;[03] CORRECTIVE ACTION #1 SIGNED OFF USING INCORRECT REFERENCE. CORRECTIVE ACTION SHOULD READ; REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22;[04] INSPECTED AS REQUIRED <BR>SEE LINES 1;2;3; FOR CORRECTIVE ACTIONS;[05] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22. SEE C/A'S AND STEPS FOR INDIVIDUAL SIGN OFFS.;[06] C/W INSPECTION AS REQUIRED C/A #5
L/H WING #3 CANOE HAS MULTIPLE AREAS OF LARGE DELAMINATIONS ON O/B SIDE<[01] REMOVED #3 TRAILING EDGE SUPPORT FAIRING 'CANOE' FROM AIRCRAFT INVENTORY AND REPLACED WITH NEW SERVICEABLE #3 TRAILING EDGE SUPPORT FAIRING. TRAILING EDGE SUPPORT FAIRING TO BE INSTALLED AND ADJUSTED ON NRC# TTG8Q00VDBK6 IAW AMM 27-51-18.;[02] ALCOHOLIC BEVERAGES LIMIT;[03] INSPECTED WORK PERFORMED
L/H WING I/B MAIN FLAP HAS LARGE AREA OF DELAMINATION ON FIXED TRAILING EDGE WEDGE.<[01] REMOVED TRAILING EDGE WEDGE F.O.M.;[02] DRILLED NEW WEDGE ASSY 113A2550-603 PER SRM 51-10-02.;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1 AND #2;[04] PAINTED EXTERIOR FINISH PER AMM 51-21-99.;[05] REINSTALLED I/B FIXED TRAILING EDGE WEDGE PER SRM 51-40-02.;[06] REINSTALLED I/B FIXED TRAILING EDGE WEDGE PER SRM 51-40-02.;[07] C/W INSPECTION
FWD L/H EMERGENCY LIGHT BATTERY DISCHARGED.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY REF BOEING 737 AMM 33-51-06. OPS CHECKED GOOD.
#2 ENG O/B FAN COWL LOWER FWD END CRACK FOUND<[01] REMOVED AND REPLACED #2 ENG O/B FAN COWL REF AMM 71-11-02;[02] TSR #2024004698
CENTER EXIT SIGN; OVERWING; AFT COVER MISSING.<[01] INSTALLED MISSING EXIT SIGN LENS IAW AMM 33-51-01.
#1 ENG FAILURE PASSING 10;000<[01] REMOVED AND REPLACED #1 ENGINE PER MT 771-00-01;[02] C/W INSPECTION OF REMOVED AND REPLACED #1 ENGINE PER MT 771-00-01
MID CABIN EMER EXIT LIGHT LENS FELL OFF<[01] SECURED LENS PER S.I.P.
FWD GALLEY LIGHT FLICKERING AND HAVING FOUL ODOR FLIGHT ATTENDANT REPORTS SMELL COMING FROM FWD GALLEY WORK LIGHT AND SMELL WENT AWAY AFTER PULLING BREAKER<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56 AND FIM 21-00 TASK 806 F/A REPORTED SULPHER SMELL DIMINISHED AFTER REMOVING POWER FROM FWD UNDER GALLEY WORK LIGHT. R/R FWD GALLEY WORK LIGHT PER CMM 25-31-67;[02] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56 AND FIM 21-00 TASK 806 F/A REPORTED SULPHER SMELL DIMINISHED AFTER REMOVING POWER FROM FWD UNDER GALLEY WORK LIGHT. R/R FWD GALLEY WORK LIGHT PER CMM 25-31-67
CADMIUM PLATING MISSING ON ALL L/H MLG FWD TRUNNION FITTING BUSHINGS.<[01] REMOVED AND REPLACED ALL 4 L/H MLG FWD. TRUNNION FITTING BUSHINGS PER. AMM REF. 20-10-02 AND REF. 757-RCB-04-01 (DVI - MLG FWD TRUNNION FITTING (-700 AND -800))
CADMIUM PLATING MISSING ON ALL R/H MLG FWD TRUNNION FITTING BUSHINGS<[01] REMOVED AND REPLACED ALL 4 R/H MLG FWD. TRUNNION FITTING BUSHINGS PER. AMM REF. 20-10-02 AND EA. 1-A57-3246 REV.16.
SEAT 14D RECLINES WHEN IT SHOULDN'T<[01] LOCKED OUT RECLINE HYDROLOC AT EMERGENCY EXIT SEAT 14D IAW AMM 25-22-00.
CENTER AISLE EMERGENCY EXIT LENS MISSING-AFT SIDE<[01] INSTALLED CENTER AISLE EMERGENCY EXIT LENS AFT SIDE AS PER REF AMM 33-51-01
T/E LH OTBD AFT FLAP DELAMINATED/MISSING PAINT.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22;[02] C/W T/C;[03] VERIFIED R&R AND ADJUSTMENT TEST OF FLAP
FWD GALLEY MEGAPHONE BROKE.<[01] SECURED FWD GALLEY MEGAPHONE HANDLE. OPS TEST PER AMM 25-64-00 OK. ACFT OK FOR SERVICE.
EXIT ROW SIGN CEILING AFT SIDE LENSE; FELL OFF.<[01] SECURED SIGN PER SIP
LEFT AFT HORIZONTAL SLIDING SEALS OUT OF TRACK<[01] REMOVED AND REINSTALLED LEFT AFT HORIZONTAL SLIDING SEAL PER AMM 53-31-31. RAN STABILIZER OPS CHECK NORMAL
R1 SLIDE IS HANGING DOWN. REPOSITIONED R1 SLIDE PER AMM25-66-01 AND MT725-66-01.
BLUE F/A CALL LIGHT UNDER AFT EXIT SIGN INOP / [01] OK TO CONTINUE PER MEL 21-10-01 SP1B
EMERGENCY LIGHTS ASSOCIATED WITH M1670 DO NOT ILLUMINATE. / [01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK M1670 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805 AND AMM 33-51-06-960-806.;[02] VERIFIED CORRECTIVE ACTION #1
EMERGENCY LIGHT RH AFT OVERWING ESCAPE LIGHT DOES NOT ILLUMINATE. / [01] REMOVED AND REPLACED BULB AND PERFORMED GOOD OP TEST AS PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION 1
CRACK ON FWD CARGO BAY O/B BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500H+1. / [01] CLIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED BAFFLE ANGLE AT BS 500H+1 LBL 24 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW BAFFLE ANGLE AT BS 500H+1 LBL 24 PER SRM 51-40-05-0G-0 AND DWG 143A7505;[05] OK TO INSTALL BFFLE ATTACH ANGLE;[06] VERIFIED CORRECTIVE ACTION STEPS 4 AND 5. VERIFIED OK TO INSTALL.;[07] INSTALLED BAFFLE ATTACH ANGLE AT BS 500H+1 LBL 24 PER SRM 51=40-02-0G-0 AND DWG 143A7505;[08] VERIFIED CORRECTIVE ACTION #7;[09] VERIFIED CORRECTIVE ACTION #7
CORROSION ON FLOOR SUPPORT BS 947+1 LBL26 WL 208 / [01] VERIFIED NO SRM APPLICABILITY FOR THIS PART.;[02] VERIFIED THAT THERE IS NO SRM APPLICABLE FOR THIS FLOOR SUPPORT.;[03] VERIFIED CORRECTIVE ACTION #1;[04] REMOVED CORROSION ON FLOOR SUPPORT. ORIGINAL THICKNESS 0.200'. AMOUNT OF CORROSION REMOVED 0.035'. REMAINING THICKNESS 0.165' . OUT OF LIMITS PER NO SRM ALLOWABLE DAMAGE FOR THIS FLOOR SUPPORT.;[05] VERIFIED CORRECTIVE ACTION #4;[06] LOCATED AND DRILLED HOLES IN NEW INTERCOSTAL IAW SRM 51-40-05 AND DWG 147A5650 ID: 0013 AND ATTACHED ADHESIVELY BONDED NUT PLATES PER SRM 51-40-10-2R-0. REQUESTING OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION #6<BR>MEASUREMENT TABLE VERIFIED;[08] INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02-0G-0 AND DWG 147A5650 ID: 0013 .;[09] INSTALLED INTERCOSTAL AT BS 947+1 LBL26 WL208 IAW SRM51-40-02-0G-0 AND DWG 147A5650;[10] CERTIFIED CORRECTION OF BS947+1 LBL26 WL208 . ADDED;[11] CORRECTIVE 4 ADDED REMOVAL OF INTERCOSTAL AT BS 947+1 LBL26 WL208;[12] CERTIFIED REMOVAL OF INTERCOSTAL AS PART OF CORRECTIVE ACTION 4;[13] VERIFIED INSTALLATION OF INTERCOSTAL AT BS 947+1 LBL26 WL208;[14] VERIFIED INSTALLATION OF INTERCOSTAL AT BS 947+1 LBL26 WL208; CARD COMPLETE
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 460+2. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 460+2' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 400 TO BS 500I ON FAULT TTG8Q00E5E0E.;[02] VERIFIED ACTION #1;[03] VERIFIED MEASUREMENT FIELD
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500+5; BS 500+10; BS 500+15; BS 500+20; BS 500A+7; BS 500A+11; BS 500B+7; BS 500B+11; BS 500B+15; BS 500B+20. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500B+7' REMOVED 0.025' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 400 TO BS 500I ON FAULT TTG8Q00E5E0E.;[02] VERIFIED ACTION #1;[03] VERIFIED MEASUREMENT FIELD
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500D+20; BS 500E+2; BS 500E+7; BS 500E+11; BS 500E+15; BS 500E+20; BS 500F+2; BS 500F+11; BS 500F+15; BS 500F+20. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500E+15' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 400 TO BS 500I ON FAULT TTG8Q00E5E0E.;[02] VERIFIED ACTION #1;[03] VERIFIED MEASUREMENT FIELD
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500C+2; BS 500C+7; BS 500C+11; BS 500C+15; BS 500C+20; BS 500D+2; BS 500D+6; BS 500D+11. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500C+20' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023.;[02] REMOVED LH FLOOR TO SIDEWALL SUPPORT FROM BS 400 TO BS 500I PER SRM 51-40-02-0G-0.;[03] VERIFIED ACTION #1;2;[04] THE DAMAGE WAS REPAIRED PER 737-800 SRM 53-00-53-2R-5 (REPAIR 5) AND EA 22-153-02538.;[05] VERIFIED ALL WORK COMPLETED.;[06] VERIFIED ALL WORK COMPLETED.;[07] VERIFIED MEASUREMENT TABLE COMPLETED.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500G+2; BS 500G+6; BS 500G+11; BS 500H+2; BS 500H+7; BS 500H+11; BS 500H+15. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500G+11' REMOVED 0.025' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 400 TO BS 500I ON FAULT TTG8Q00E5E0E.;[02] VERIFIED ACTION #1;[03] VERIFIED MEASUREMENT FIELD
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2; BS 500A+6; BS 500A+11; BS 500A+15; BS 500B+7; BS 500B+11. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500B+7'' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 500A TO BS 500I ON FAULT TTG8Q00E5E11;[02] VERIFIED CORRECTIVE ACTION 1<BR><BR>VERIFIED MEASUREMENTS TABLE
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500B+16; BS 500B+20; BS 500C+2; BS 500C+7; BS 500C+11; BS 500C+16; BS 500C+20; BS 500D+2; BS 500D+7; BS 500D+11. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500C+20' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023;[02] VERIFIED CORRECTIVE ACTION 1<BR><BR>VERIFIED MEASUREMENTS TABLE;[03] REMOVED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT R/H BS 500A TO 500I RBL 24 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT R/H BS 500A TO 500I RBL 24 PER SRM 51-40-05-0G-0 AND DWG 143A7500<BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION #4<BR>VERIFIED MEASUREMENT TABLE <BR>OK TO INSTALL GIVEN;[06] INSTALLED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT R/H BS 500A TO 500I RBL 24 PER SRM 51-40-02-0G-0 AND DWG 143A7500;[07] COMPLETED STEP 1;[08] VERIFIED CORRECTIVE ACTIONS 6 AND 7;[09] VERIFIED CORRECTIVE ACTIONS 6 AND 7
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500D+15; BS 500D+20; BS 500E+2; BS 500E+7; BS 500E+11; BS 500E+15; BS 500E+20; BS 500F+4; BS 500F+7; BS 500F+11. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500E+20' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 500A TO BS 500I ON FAULT TTG8Q00E5E11;[02] VERIFIED CORRECTIVE ACTION 1<BR><BR>VERIFIED MEASUREMENTS TABLE
CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 480+14. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1<BR><BR>VERIFIED MEASUREMENTS TABLE;[03] REMOVED DAMAGED SHIELD AT RBL 24 BS 492 -BS 500A PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHIELD AT RBL 24 BS 492 -BS 500A PER SRM 51-40-05-0G-0 AND DWG 143A0080.<BR>OK TO INSTALL;[05] VERIFIED ACTION #4; OK TO INSTALL GIVEN;[06] UPDATED OK TO INSTALL SHIELD;[07] OK TO INSTALL GIVEN ON CORRECTIVE ACTION #5;[08] INSTALLED SHIELD AT RBL 24 BS 492 -BS 500A PER SRM 51-40-02-0G-0 AND DWG 143A0080;[09] VERIFIED CORRECTIVE ACTION #8
CORROSION ON FSD MOPSILL THRESHOLD SUPPORT ANGLE BS294.5+11-BS312+4 RBL56 WL 209 / [01] SRM APPLICABILITY 53-10-15-1A-2. REMOVED CORROSION ON FSD MOPSILL THRESHOLD SUPPORT ANGLE AT BS 312+4 -BS 312+5 PER SRM 51-10-02. MAXIMUM MATERIAL REMOVED WAS 1'X1'X .011'. FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2. DIAL DEPTH GAUGE ID:ATS2677 S/N: UNKNOWN DATE:11/2021 DUE: 11/2022. UPDATED MEASUREMENT TABLE.;[02] VERIFIED ACTION #1;[03] REMOVED FSD MOPSILL THRESHOLD SUPPORT ANGLE PER SRM 51-40-02.;[04] LOCATED AND DRILLED NEW SUPPORT ANGLE FOR BS 294.5 TO BS 332 RBL 56 WL 209 IAW SRM 51-40-05-0G-0 OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION #4 OK TO INSTALL;[06] INSTALLED FSD MOP SILL THRESHOLD SUPPORT ANGLE BS 294.5 TO BS 332 RBL 56 WL 209 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 APPLIED FILLET SEAL IAW AMM 51-31-00-390-804;[07] VERIFIED CORRECTIVE ACTION ITEM 6.;[08] VERIFIED MEASUREMENTS. VERIFIED FAULT COMPLETE
CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 24 BS 420+12; BS 420+17. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1<BR><BR>VERIFIED MEASUREMENTS TABLE;[03] REMOVED DAMAGED FWD CARGO BAY SHIELD AT RBL24 BS 420-BS440 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHIELD AT RBL24 BS 420-BS440 PER SRM 51-40-05-0G-0 AND DWG 143A0080;[05] OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 3-5 OK TO INSTALL;[07] INSTALLED NEW SHIELD AT RBL24 BS 420-BS440 PER SRM 51-40-02-0G AND DWG 143A0080;[08] VERIFIED INSTALLATION OF NEW SHIELD AT RBL24 BS 420-BS440;[09] CARD COMPLETE;[10] VERIFIED INSTALLATION OF NEW SHIELD AT RBL24 BS 420-BS440; CARD COMPLETE
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500G+2; BS 500G+7; BS 500G+15; BS 500G+20; BS 500H+2; BS 500H+7; BS 500H+11; BS 500H+15. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500H+7'' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 500A TO BS 500I ON FAULT TTG8Q00E5E11;[02] VERIFIED CORRECTIVE ACTION 1<BR><BR>VERIFIED MEASUREMENTS TABLE
INTERCOSTAL IS CRACKED BS344+6 BL 0 WL 208 / [01] REMOVED CRACKED INTERCOSTAL AT BS344+6 BL 0 WL 208 PER SRM 51-40-02. UPDATED MEASUREMENT TABLE.;[02] RECEIVED A NEW INTERCOSTAL PO#879133 LOCATED HOLES; DRILLED; AND DEBURRED IAW SRM 51-40-05 AND BOEING DWG 141A5400. ALSO; OK TO INSTALL.;[03] VERIFIED ACTION #1-2; OK TO INSTALL GIVEN;[04] INSTALLED INTERCOSTAL AT BS 344+6 BL0 WL 208 PER SRM 51-40-02-0G-0 AND DWG #141A5400;[05] VERIFIED INSTALLATION OF INTERCOSTAL AT BS 344+6 BL0 WL 208;[06] VERIFIED ALL STEPS COMPLETE;[07] CARD COMPLETE;[08] CARD COMPLETE;[09] VERIFIED ALL STEPS COMPLETE
CRACKED INTERCOSTAL AT FWD WET AREA BS344+9 LBL11. / [01] REQUEST NDI TO VERIFY CRACK FREE CONDITION ON INTERCOSTAL AT FWD WET AREA BS344+9 LBL11.;[02] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23 <BR>-MINIMITE ID: ATS1411 CAL DUE: 07/23;[03] UPON FURTHER INVESTIGATION INTERCOSTAL AT FWD WET AREA BS344+9 LBL11 WL 208 WAS FOUND TO BE IN CRACK FREE CONDITION.;[04] HFEC INSPECTED SURFACE AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED TO BE 0.6'. FOUND ADJACENT TO THE AFT FASTENER HOLE. MARKED ENDS OF CRACK.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23;[05] UPDATED MEASUREMENT TABLE.;[06] REMOVED CRACKED INTERCOSTAL AT FWD WET AREA BS344+9 LBL11 WL 208 PER SRM 51-40-02.;[07] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS344+9 LBL11 WL208 PER SRM 51-40-05 AND DWG#141A5400. REQUEST OK TO INSTALL.;[08] VERIFIED ACTION #6-7 OK TO INSTALL GIVEN;[09] INSTALLED INTERCOSTAL AT FWD WET AREA BS344+9 LBL 11 PER SRM 51-40-02-0G-0 AND DWG 141A5400;[10] VERIFIED INSTALLATION OF INTERCOSTAL AT FWD WET AREA BS344+9 LBL 11;[11] RII INSPECTION ACCOMPLISHED;[12] ALL STEPS COMPLETE
CRACKED INTERCOSTAL AT FWD WET AREA BS344+9 RBL12. / [01] REQUEST NDI TO VERIFY CRACK FREE CONDITION ON INTERCOSTAL AT FWD WET AREA BS344+9 RBL12.;[02] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23 <BR>-MINIMITE ID: ATS1411 CAL DUE: 07/23;[03] UPON FURTHER INVESTIGATION INTERCOSTAL AT FWD WET AREA BS344+9 RBL12 WL 208 WAS FOUND TO BE IN CRACK FREE CONDITION.;[04] HFEC INSPECTED SURFACE AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>2 CRACKS NOTED; BOTH ARE 0.6'. ONE ADJACENT TO THE FWD FASTENER HOLE; AND ONE ADJACENT TO THE AFT FASTENER HOLE. MARKED ENDS OF CRACKS.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23;[05] UPDATED MEASUREMENT TABLE.;[06] REMOVED INTERCOSTAL AT FWD WET AREA BS344+9 RBL12 WL 208 PER SRM 51-40-02.;[07] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS344+9 RBL12 WL 208 PER SRM 51-40-05; DWG#141A5400. AND REQUEST OK TO INSTALL.;[08] INADVERTENTLY UPDATED INSPECTORS LABOR ROW. (CORRECTIVE ACTION 6.);[09] INADVERTENTLY UPDATED INSPECTORS LABOR ROW. (CORRECTIVE ACTION 7.);[10] REMOVED; LOCATED; AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS344+9 RBL12 WL 208 PER SRM 51-40-02; SRM 51-40-05; AND DWG#141A5400. REQUEST OK TO INSTALL.;[11] VERIFIED CORRECTIVE ACTION #10<BR>OK TO INSTALL GIVEN;[12] INSTALLED NEW INTERCOSTAL AT FWD WET AREA BS344+9 RBL12 WL 208 PER SRM 51-40-02; DWG#141A5400
INTERCOSTAL IS CRACKED BS277+6 BL 0 WL 208 / [01] CRACK DAMAGED INTERCOSTAL 0.950 IN LENGTH NEXT TO MIDDLE FASTENER HOLE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1 FIG 105.(A) PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REMOVED CRACK DAMAGED INTERCOSTAL AT BS 277 TO BS 294.5 BL 0 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 OK TO INSTALL;[04] OK TO INSTALL GIVEN.;[05] INSTALLED NEW INTERCOSTAL AT BS 277 TO BS 294.5 BL0 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A5400;[06] VERIFIED CORRECTIVE ACTIONS STEP 5.
CRACK ON FWD CARGO BAY O/B BAFFLE TO FRAME ATTACH ANGLE AT RBL 24 BS 500H+1. / [01] CLIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED FWD CARGO BAY O/B BAFFLE TO FRAME ATTACH ANGLE AT BS 500H+1 RBL24 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW ATTACH ANGLE BS 500H+1 RBL 24 PER SRM 51-40-05-0G-0 AND DWG 143A7505;[05] OK TO INSTALL ATTACH ANGLE;[06] VERIFIED CORRECTIVE ACTION STEPS 4 AND 5.;[07] INSTALLED ATTACH ANGLE AT BS 500H+1 RBL 24 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[08] VERIFIED CORRECTIVE ACTION #7;[09] VERIFIED CORRECTIVE ACTION #7
FLOOR PANEL 222BF HAS TORN PLIES ON UPPER SURFACE IN SEVERAL LOCATIONS (MARKED) / [01] IDENTIFIED MATERIAL IAW SRM 53-00-50-0I-1 TABLE 2 FIG 2.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1<BR><BR>REMOVED DAMAGE TO UPPER SURFACE PLIES THEN CLEANED REPAIR AREA. FABRICATED REPAIR PLIES FROM BMS9-3 H2 ST 1581 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3C-F;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2.<BR>OKAY TO INSTALL REPAIR PLIES.;[04] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 3 LOT#AK2CP8139K; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2107 CAL DUE DATE 09/2022 IAW SRM 53-00-50-2R-1 PARA 3K-L;[05] VERIFIED CORRECTIVE ACTION ITEM 4.;[06] CURED REPAIR PLIES UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/2022; UNBAGGED; AND TRIMMED EXCESS MATERIAL IAW SRM 53-00-50-2R-1 PAR.3 M(1);[07] VERIFIED CORRECTIVE ACTION 6<BR><BR>VERIFIED MEASUREMENTS TABLE;[08] UPLOADED CURE SHEET AND VERIFIED COMPLETION OF REPAIRS IAW SRM 53-00-50-2R-1;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED CORRECTIVE ACTION 8
CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+3; BS 767+7; BS 767+11; BS 767+15; BS 767+19. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.<BR>VERIFIED MEASUREMENTS.;[03] REMOVED DAMAGED AFT CARGO BAY FWD DOOR SHIELD AT BS767- BS794 RBL 21 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW AFT CARGO BAY FWD DOOR SHIELD AT BS767- BS794 RBL 21 PER SRM 51-40-05-0G-0 AND DWG 146A0081.<BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION #4<BR>OK TO INSTALL GIVEN;[06] INSTALLED AFT CARGO BAY FWD DOOR SHIELD AT BS767- BS794 RBL 21 PER SRM 51-40-02-0G-0 AND DWG 146A0081.;[07] VERIFIED CORRECTIVE ACTION #6
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727J+14; BS 727J+18; BS 747; BS 747+6; BS 747+18. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727I+18' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767 ON FAULT TTG8Q00E4Q8G.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767 ON FAULT TTG8Q00E4Q8G.;[03] VERIFIED MEASUREMENTS.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727H+6; BS 727H+9; BS 727H+13; BS 727I+3; BS 727I+10; BS 727I+14; BS 727I+18; BS 727J+2; BS 727J+6; BS 727J+10. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727I+3' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767 ON FAULT TTG8Q00E4Q8G.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767 ON FAULT TTG8Q00E4Q8G.;[03] VERIFIED MEASUREMENTS.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727A+10; BS 727B+10; BS 727C+6; BS 727C+12; BS 727C+16; BS 727E; BS 727E+6; BS 727E+13; BS 727E+20; BS 727F. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727C+12' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS. <BR>VERIFIED MEASUREMENTS.;[03] REMOVED R/H FLOOR TO SIDEWALL SUPPPORT AT BS 727 TO 767 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 727 TO 767 RBL21 PER SRM 51-40-05-0G-0 AND DWG 146A7500;[05] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT;[06] VERIFIED CORRECTIVE ACTION #4<BR>OK TO INSTALL FLOOR TO SIDEWALL SUPPORT GIVEN;[07] INSTALLED R/H FLOOR TO SIDEWALL SUPPORT AT BS 727 TO 767 RBL21 PER SRM 51-40-02-0G-0; DWG 146A0061 AND 1467500;[08] VERIFIED CORRECTIVE ACTION #7
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727F+2; BS 727F+6; BS 727F+9; BS 727F+13; BS 727F+16; BS 727G; BS 727G+16; BS 727G+20; BS 727H; BS 727H+2. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727F+16' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767 ON FAULT TTG8Q00E4Q8G.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 767 ON FAULT TTG8Q00E4Q8G<BR>VERIFIED MEASUREMENTS.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727J+14; BS 727J+18; BS 747+6; BS 747+10; BS 747+14; BS 767; BS 767+5; BS 787+6. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 767+5' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL21; WL156 PER SRM 53-00-53-2R-5 STEP 4.B. SRM 51-40-02-0G-0; FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL21;WL156 AND SPLICES REPAIRS AT BS727F+8' - BS727E+18' AND BS727H+8' - 727H+18' USING BAC1496-377#7075T62 LOT# 1500263-1 PER SRM 53-00-53-2R-5 STEP 4. I. SRM 51-40-05-0G AND DWG 146A7500. AMM 51-21-41-370-802;APPLIED PRIMER TO ACB FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-2R-5 STEP 4. J. INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL21; WL156 AND SPLICES REPAIRS AT BS727F+8' - BS727E+18' AND BS727H+8' - 727H+18' PER SRM 53-00-53-2R-5; SRM 51-40-02-0G AND DWG 146A7500.;[10] VERIFIED CORRECTIVE ACTION ITEM 9. REPAIR COMPLETE.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727B+6; BS 727C+16; BS 727E+21; BS 727F+9; BS 727G+6; BS 727G+9; BS 727G+20; BS 727H+6; BS 727I+5; BS 727I+19. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727G+6' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. FLOOR TO SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED FROM BS 727 + 4' TO BS 847 ON FAULT TTG8Q00E4Q8F .;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE
CORROSION ON AFT CARGO BAY NUT PLATE BRACKET ATTACH TO LOWER SIDE OF INTERCOSTAL AT RBL 19 BS 787+4. / [01] CORROSION ON NUTPLATE STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.;[03] UPDATED MEASUREMENT TABLE.;[04] VERIFIED CHANGED PRIMARY TO 2-SDRY AND CORROSION FROM LEVEL 2; TO LEVEL 1.;[05] REMOVED DAMAGED AFT CARGO BAY NUT PLATE BRACKET AT BS787- BS793 RBL19 PER SRM 51-40-02-0G-0;[06] LOCATED AND DRILLED NEW AFT CARGO BAY NUT PLATE BRACKET AT BS787- BS793 RBL19 PER SRM 51-40-05-0G-0 AND DWG 146A0081.<BR>OK TO INSTALL;[07] VERIFIED CORRECTIVE ACTION #6<BR>OK TO INSTALL GIVEN;[08] INSTALLED AFT CARGO BAY NUT PLATE BRACKET AT BS787- BS793 RBL19 PER SRM 51-40-02-0G-0 AND DWG 146A0081.;[09] VERIFIED CORRECTIVE ACTION #8<BR>MEASUREMENT TABLE VERIFIED
CORROSION ON AFT CARGO BAY THRESHOLD AT RBL24 BS787+11; RBL27 BS787+18; RBL27 BS807+1; RBL27 BS807+4; RBL27 BS807+7; RBL27 BS807+16; RBL27 BS827+2; RBL27 BS827+4; RBL27 BS827+9; RBL21 BS827+18. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 787 RBL 24 REMOVED .016' IN AREA OF 1'X 1' ORIGINAL THICKNESS .045' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING ATS TOOL ID: ATS2678 EXP 04/2023;[02] VERIFIED CORRECTIVE ACTION ITEM 1. AREA OF DAMAGE REMOVED EXCEEDS LIMITATION PER SRM 53-60-15-1A-1.;[03] REMOVED SUB-THRESHOLD WEB AT BS 792-847 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SUB-THRESHOLD WEB BS 792-847 PER SRM 51-40-05-0G-0 AND DWG 146A8340. OK TO INSTALL SUB-THRESHOLD;[05] VERIFIED CORRECTIVE ACTION ITEM 4. OKAY TO INSTALL SUBTHRESHOLD GIVEN.;[06] INSTALLED SUB-THRESHOLD WEB BS 792-847 PER SRM 51-40-02-0G-0 AND DWG 146A8340;[07] VERIFIED CORRECTIVE ACTION ITEM 6.;[08] ALL WORK COMPLETE.;[09] VERIFIED MEASUREMENT TABLE;[10] VERIFIED TASK COMPLETE
FWD CARGO BAY DOOR CUTOUT THRESHOLD HAS AREAS OF CORROSION. (MARKED) / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 465 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING ATS TOOL ID ATS2678 EXP 4/2023;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED FWD CARGO BAY DOOR CUTOUT THRESHOLD WEB PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SUB-THRESHOLD WEB BS 440-BS 480+12' PER SRM 51-40-05-0G-0; AND DWG 143A8330. OK TO INSTALL SUB-THRESHOLD WEB;[05] VERIFIED CORRECTIVE ACTION ITEM 4. OKAY TO INSTALL NEW SUBTHRESHOLD GIVEN.;[06] INSTALLED SUB-THRESHOLD WEB AT BS 440-480+12' PER SRM 51-40-02-0G-0 AND DWG 143A8330;[07] VERIFIED CORRECTIVE ACTION ITEM 6.;[08] ALL STEPS COMPLETED;[09] VERIFIED FAULT COMPLETE;[10] VERIFIED MEASUREMENTS. FAULT COMPLETE.
CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+16. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.<BR>VERIFIED MEASUREMENTS.;[03] REMOVED DAMAGED AFT CARGO BAY AFT DOOR SHIELD AT BS847-BS867 RBL21 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHIELD AT BS847-BS867 RBL21 PER SRM 51-40-05-0G-0 AND DWG 146A0081.<BR>OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION #4<BR>OK TO INSTALL GIVEN;[06] INSTALLED SHIELD AT BS847-BS867 RBL21 PER SRM 51-40-02-0G-0 AND DWG 146A0081.;[07] VERIFIED CORRECTIVE ACTION #6;[08] ALL STEPS COMPLETED;[09] TASK COMPLETE
#2 ENGINE PRIMARY EXHAUST NOZZLE PERFORATED FACE SHEET HAS A CRACK IN ZONE 2 AT THE 6:00 POSITION MEASURING 1 INCH IN LENGTH; 13 INCHES FWD OF THE AFT WELD LINE. / [01] REMOVED AND REPLACED #2 ENGINE PRIMARY EXHAUST NOZZLE IAW AMM 78-11-01.
FWD ENTRY DOOR SLIDE CAME LOOSE WHEN DOOR OPENED / [01] RESECURED FWD ENTRY DOOR SLIDE. AMM 25-66-01
AFT L/H EMERGENCY LIGHTING INOP / [01] REMOVED AFT GALLEY EMERGENCY LIGHT BALLAST BATTERY PACK; IAW B737 AMM 33-51-06;[02] R&R AFT LEFT EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK NORMAL
L/H OUTBOARD TRAILING EDGE AFT FLAP; LOWER INBOARD CORNER IS DELAMINATING. AREA MEASURES 6.75?L & 3.5?H ; / [01] REMOVED AND REPLACED L/H O/B AFT FLAP; RIG AND OPS CHK GOOD PER MM 27-51-22; [02] INSPECTED WORK ABOVE; [03] INSPECTED WORK ABOVE; [04] REMOVED AND REPLACED L/H O/B AFT FLAP; RIG AND OPS CHK GOOD PER MM 27-51-22.<BR>SEE STEP 1 FOR WORK COMPLETED AND SIGN-OFF.
FWD CARGO RH INTERCOSTAL ABOVE AC MIX MANIFOLD IS CRACKED . ; / [01] REMOVED AND REPLACED FWD CARGO RH INTERCOSTAL ABOVE AC MIX MANIFOLD PER SRM 51-40-02 AND AMM 20-50-11.
EMERGENCY EXIT SIGN COVER BY FORWARD GALLEY GARBAGE CAN FELL OFF. / RESECURED COVER; AS REQUIRED; LIGHT OP'S CKD GOOD. REF 33-51-03
#2 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON CLIMNBOUT. FOLLOWED BY B SYSTEM QTY. ON DESCENT 1 ENGINE DRIVEN 'A' SYSTEM PUMP LOW PRESSURE LIGHT. / REPLACED #2 ENGINE HYDRAULIC PUMP PER M/M 29-11-11 OPS CHECKS AND LEAK CHECKS OK. REPLACED #2 ENGINE CASE DRAW FILTER AND #2 ELECT HYD PUMP CASE DRAIN FILTERS PER M/M 29-11-51 LEAK CHECKS O.K. REMOVED AND REPLACED #1 ELECT CASE DRAIN FILTERS PER M/M 29-11-51 RAN BOTH ENGINES PER M/M 71-00-00 ALL PRESSURES NORMALPN OFF/ON: 849589 S/N OFF: MX780418 S/N ON: MX791278ISSUE # 3477884
CREW REPORTED TO MX L1-R1 ENTRY/SERVICE DOOR GIRT BAR SUPPORT MATERIAL EXCESSIVE / REPACKED L1 ENTRY & R1 SERVICE DOOR GIRT BAR MATERIAL PER MT # 725-61-06
CREW REPORTED TO MX L1-R1 ENTRY/SERVICE DOOR GIRT BAR SUPPORT MATERIAL EXCESSIVE / REPACKED L1 ENTRY & R1 SERVICE DOOR GIRT BAR MATERIAL PER MT # 725-61-06
L1 DOOR EVAC SLIDE BOTTLE GAGE NEEDLE IN RED. R & R L1 DOOR EVAC SLIDE, PER MT 725-61-06 & MM 25-66-01P/N OFF 5A3307-7 S/N OFF BNG10543P/N ON 5A3307-7 S/N ON BNG16822.
PASSENGER CABIN FLOOR PANEL 231QF; UPPER SURFACE HAS FIBERS RIPPED UP. REPAIRED UPPER SURFACE; FIBERS PULLED AND PUNCTURES; ON FLOOR PANEL 231QF IAW SRM 53-00-50-2R-1 REV. 70 AND SRM 53-00-50-2R-0 REV. 70. REINSTALLED INSERTS IAW BAC5085 REV. E
PASSENGER CABIN FLOOR PANEL 232DF; UPPER SURFACE HAS FIBERS RIPPED UP. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 232DF IAW 737-800 SRM 53-00-50-2R-1 REV. 70 REPAIR 1 AND SRM 53-00-50-2R-0 REV. 70 REPAIR GENERAL. TAP TEST GOOD.
AFT CARGO BAY FLOOR PANEL 140EF CORRODED / REPLACED AFT CARGO BAY FLOOR PANEL 140EF; VERIFIED MATERIAL AS 2024 T3 .071; AND FABRICATED REPLACEMENT PANEL IAW AMM 25-52-01. TREATED BACK SIDE OF PANEL IAW AMM 51-21-41. APPLIED PRIMER IAW AMM 51-21-72. AND BOEING DWG 453A2610 REV: C C06779
AFT CARGO BAY FLOOR PANEL 140BF CORRODED / FOUND CORROSION TO BE GREATER THAN 20' IN LENGTH. FOUND FLOOR PANEL 140BF TO BE OUT OF LIMITS. VERIFIED MATERIAL FOR NEW PANEL TO BE 2024 T3 .071' ATAG C06782. FABRICATED NEW FLOOR PANEL 140BF. ALODINED AND PRIMED PANEL IAW SRM 53-00-53-1A-1; AMM 25-52-01-201-801; AMM 51-21-41-370-802; AMM 51-21-72-370-804 DWG 453A2610 REV K
AFT CARGO BAY FLOOR PANEL 140DF CORRODED / EVALUATED CORROSION EXCEEDS THE LIMITS IAW SRM 53-00-53-1A-1; VERIFIED MATERIAL 2024 T3 .071 CLAD IAW AMM 25-52-01-201-801(C) ATAG C006782; FABRICATED AFT FLOOR PANEL 140DF IAW AMM 25-52-01-201-801(C) TRETED AND PRIME IAW AMM 25-52-01-201-801 IAW BOEING 453A2410 REV: K WORK ACCOMPLISHED
AFT CARGO BAY FLOOR PANEL 140CF CORRODED / EVALUATED CORROSION ON FAT CRAGO BAY FLOOR PANEL 140CF; FOUND LENGTH OF CORROSION DAMAGE EXCEEDS 20' MAXIMUM - OUT OF LIMITS IAW SRM 53-00-53-1A-1; FABRICATED NEW FLOOR PANEL 140CF IAW AMM 25-52-01-201-801 AND BOEING DWG 453A2610 REV C ATAG CO6780
FWD CARGO PIT PANEL 120CF HAS SEVERAL AREAS OF CORROSION; MARKED. / EVALUATED CORROSION ON FWD CARGO FLOOR PANEL 120CF; CORROSION EXCEEDED 20 INCHES. OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND BOEING DRAWING 453A1610 SH 65 REV D. TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804
FWD CARGO PIT PANEL 120AF HAS LARGE AREA OF CORROSION; MARKED. / EVALUATED CORROSION DAMAGE ON FWD CARGO PIT PANEL 120AF; LENGTH OF DAMAGE EXCEES THE 20' MAXIMUM ALLOWED - OUT OF LIMITS; FABRICATED NEW PANEL 120AF IAW AMM 25-52-01-201-801 AND BOEING DWG 453A1610 REV F ATAG A68671
FWD CARGO PIT PANEL 120BF HAS SEVERAL AREAS OF CORROSION; MARKED. / EVALUATED CORROSION ON FWD CARGO PIT FLOOR PANEL 120BF CORROSION EXCEEDED 20 INCHES. OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND BOEING DRAWING 453A1610 SH 10 EV E. TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804ATAG # CD6783
FWD PIT STA 500I LATERAL FLOOR SUPPORT UPPER SURFACE CORRODED FROM LBL 24 TO RBL24 AT WL 155 / EVALUATED CORROSION ON LOWER BULKHEAD SUPPORT AT STA 500I LBL 24 - RBL 24 NO PUBLISHED LIMITS IN SRM. REMOVED AND REPLAED RAIL ASSY IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A9481 REV - ATAG WN4193
AFT CARGO BAY UPPER CORNER DOOR SCUFF PLATE CORRODED / REPLACED AFT CARGO BAY CORNER DOOR SCUFF PLATE FWD SIDE (HOCKEY STICK) IAW B737 AIPC 25-52-10-04 & AMM 25-52-10-400-801. NO WRITTEN LIMITS REPAIR BY REPLACEMENT IAW B737 SRM 51-10-02-0G-0 P/N 453A2611-1 ATAG A75260
AFT CARGO BAY FLOOR PANEL 140AF CORRODED / EVALUATED AFT CARGO BAY FLOOR PANEL #140AF CORROSION EXCEEDS MORE THAN 20 INS. OUT OF LIMITS I/A/W 737-800 SRM 53-00-53-1A-1 FIG 102. FABRICATED PANEL #140AF I/A/W 737 AMM 25-52-01-201-801; 737 AMM 51-21-41-370-802; AND 737 AMM 51-21-72-370-804
FWD PIT RIGHT Z ANGLE UPPER SURFACE CORRODED IN SEVERAL AREAS FROM STA 500A TO 500I RBL 24 AND WL 155. REMOVED CORROSION & EVALUATED ON FWD PIT RT Z ANGLE STA 500A - 500I RBL 24 WL 155 AS OUT OF LIMITS IAW SRM 51-10-02-0G-0 & SRM 53-00-00-53-1A-2. REMOVED OUT OF LIMITS Z ANGLE SECTION FROM STA 500B+12' - 500I. VERIFIED NEW Z-ANGLE AS PN BAC1446-444 7075 T62 ATAG #A57840 IAW SRM 53-00-53-2R-5. LOCATED & DRILLED REPAIR PARTS IAW SRM 53-00-53-2R-5 STEPS 4 (D TO H). TREATED AND PRIMED IAW SRM 53-00-53-2R-5. INSTALLED Z-ANGLE; SPLICE; AND REPAIR PARTS. SPLICE LOCATED AT STA 500B+12' IAW SRM 53-00-53-2R-5. APPLIED CIC IAW SRM 53-00-53-2R-5 P/N 143A7501-188
FWD PIT LEFT Z ANGLE UPPER SURFACE CORRODED STA 480 TO STA 500E LBL 24 AT WL 155. REMOVED CORROSION FROM FWD CARGO COMPARTMENT; LT Z ANGLE; STA 480-500E IAW SRM 51-10-02-0G-0 SECTION 15. VERIFIED LIMITS ORIGINAL THICKNESS .040'; LOSS OF .008' REMAINING .032' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIGURE 103. ACCOMPLISHED Z-ANGLE REPAIR AT STA 480 - 500E IAW SRM 53-00-53-2R-5 P/N 143A7501-187.
EXTERNAL POWER DOOR CUTOUT LOWER LATCH FLANGE METAL IS TORN COMMON TO FWD ATTACH FASTENER. ACCOMPLISHED DOUBLER REPAIR AT ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER AT LOWER LATCH I.A.W SRM 53-10-15-2R-4.
CABIN FLOOR PANEL 241BF HAS DAMAGE AT FWD EDGE. MARKED / REPAIRED CABIN FLOOR PANEL 241BF FWD EDGE IAW B737 SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0 A36551 A33703 A68437.
CABIN FLOOR PANEL 241FF HAS DAMAGE 22' FROM AFT EDGE; SPANNING THE WIDTH OF PANEL. MARKED / REPAIRED CABIN FLOOR PANEL 241FF 22' FROM AFT EDGE SPANNING THE WIDTH OF PANEL AS MARKED IAW B737 SRM 53-00-50-2R-1 REV 70 AND B737 SRM 53-00-50-2R-0 REV 70.
L\H WING FIXED T\E AT SAIL TAIL; L-ANGLE ATTACHED TO INBD SIDE OF DEFLECTOR RIB CRACKED. / REMOVED AND REPLACED L/H WING FIXED T/E AT SAIL TAIL L-ANGLE ATTACHED TO I/B SIDE OF DEFELCTOR RIB IAW SRM 51-40-02-0G-0 AND DWG: 115A6200 REV: A MPN: 115A6260-1 ATAG: A75282
CABIN FLOOR PANEL 241EF HAS DAMAGE 22' FROM AFT EDGE; SPANNING THE WIDTH OF PANEL. MARKED / REPAIRED CABIN FLOORBOARD PANEL 241EF 22' FROM AFT EDGE SPANNING WIDTH OF PANEL AS MARKED IAW B737 SRM 53-00-50-2R-1 REV 70 AND B737 SRM 53-00-50-2R-0 REV 70
CABIN FLOOR PANEL 241CF HAS DAMAGE AT AFT INBOARD CORNER. MARKED AND REPAIRED CABIN FLOOR PANEL 241CF DAMAGE AFT INBOARD CORNER AS MARKED IAW B737 SRM 53-00-50-2R-10 REV 70 AND B737 SRM 53-00-50-2R-0 REV 70. A68437.
AFT CARGO PIT R/H FLOOR STRUCTURE SHIELD; FWD ATTACH ANGLE AT STA 767 HAS CORROSION. RBL 21; WL 156.1 / REMOVED CORROSION FROM AFT CARGO GUSSET AT STA. 767 RBL 21 IAW B737 SRM 51-10-02 ORIGINAL MATERIAL THICKNESS .063 IAW BOEING DWG 146A8125 REV M MATERIAL REMOVED .008 REMAINING MATERIAL .055 GUSSET WAS FOUND OUT OF LIMITS IAW B737 SRM 53-60-15-1A-1 VERIFIED BY TOOL 36646 DUE 05OCT20 RECEIVED PART NEW PART 146A8125U39 ATAG# A56129 LOCATED DRILLED + DEBURRED GUSSET IAW B737 SRM 51-40-05 INSTALLED NEW GUSSET AT STA. 767 RBL 21 AST CARGO IAW B737 SRM 51-40-02
AFT CARGO PIT LT Z ANGLE HAS VARIOUS SPOTS OF CORROSION (MARKED IN RED) FROM STA 727G TO 807.LBL 21; WL 156.1. REMOVED CORROSION FROM AFT CARGO BAY LT ZEE ANGLE LBL 21 WL 156.1 STA 727G TO STA 807 AND INSPECTED W/ 10X MAG GLASS. NO DEFECTS NOTED. VERIFIED LIMITS TO BE = .004' MATERIAL LOSS = .020' ORIGINAL T = .040'. SECTION OF ZEE ANGLE BETWEEN 747 TO 847 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED NEE ZEE ANGLE AND REPAIR PARTS IAW SRM 53-00-53-2R-5. INSTALLED NEW ZEE ANGLE STA 727J+11' TO STA 847 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV. APPLIED CIC TO LOWER AND UPPER SURFACE IAW AMM 51-21-91-620-802 P/N 146A7502-31.
BODY FAIRING PANEL 194CL HAS A DENT WITH DISBOND.REQUIRE REPAIR / REPAIRED AND APPLIED DECORATIVE FINISH ON BODY FAIRING PANEL 194CL DENT WITH DISBOND IAW B737 SRM 51-70-04-2R-1 REV 70; B737 SRM 51-70-04-2R-0 REV 70 AND B737 AMM 51-21-99-300-801 REV 72. A36551 A51560 A53133
LEFT WING INBOARD OF PYLON; UPPER FIXED LEADING EDGE SKIN; 6TH FASTENER ( INBOARD TO OUTBOARD) DAMAGED AT LOWER SIDE OF FASTENER HOLE. MARKED. / LH WING INBD; OF PYLON; UPPER FIXED LE SKIN; 6TH FASTENER (INBD. TO OUTBD) ATTACH STRAP HOLE DAMAGED; REPAIRED HOLE; AND INSTALLED FASTNER. REPAIR. IAW EA 200451 IR SND SWA EA 20-157-01508. IR.
LEFT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. MARKED/ LT PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STA 663; 3RD FASTENER O/B OF KEEL BEAM CUTOUT DAMAGE; INSTALLED REPAIR IAW SRM 57-10-10-2R-5; REPAIR 5. LEAK CHECKED REPAIR AREA. LEAK CHECK GOOD IAW AMM 28-11-00-400-801.
R1 DOOR FLOOR FITTING FOR GIRT BAR WAS LOOSE. / SECURED FITTING PER SIP.
R2 DOOR SLIDE WAS COMING OUT OF THE CASING. / REPACKED SLIDE PER MT AND MM.
R1 DOOR GIRT BAR LOOSE. SECURED GIRT BAR HANGER PER SIP.
AFT ELECTRONICS COMPARTMENT LEFT OTBD FLOOR BOARD SUPPORT INTERCOSTAL BETWEEN BS 312 AND BS 328 CRACKED AT CENTER FASTENER ATTACH POINT / REMOVED AND REPLACED FLOORBOARD SUPPORT INTERCOSTAL BETWEEN BS 312 AND BS 328 PER SRM 51-40-02
AFT ELECTRONICS COMPARTMENT L/H OUTBOARD FLOOR BOARD SUPPORT INTERCOSTAL BETWEEN BS. 312 TO BS. 328 CRACKED AT CENTER FASTENER ATTACH POINT. / R&R INTERCOSTAL PER SRM.
AFT ELECTRONICS COMPARTMENT L/H OUTBOARD FLOOR SUPPORT BETWEEN BS. 312 TO BS. 328 CRACKED AT CENTER FASTENER ATTACH POINT. R & R THE FLOOR SUPPORT IAW SRM.
RT AFT EMERGENCY EXIT DOOR LIGHT FAILED TO ILLUMINATE. RELAMPED LIGHT PER AMM.
RT WING DEFLECTION CONTROL RIB SUPPORT CLIP CRACKED. R&R CLIP SRM.
SUPPORT CLIP AT THE R/H WING DEFLECTION CONTROL RIB IS CRACKED / REMOVED AND REPLACED CLIP REF SRM 51-40-02 (INSPECTOR 39215)
RT AFT OVERWING EXTERIOR EMERGENCY LIGHT LENS BROKEN. R&R LENS PER AMM.
AFT EMERGENCY FLASH LIGHT STRAP MISSING. / INSTALLED STRAP PER MM.
EMERGENCY BULLNOSE LIGHT COVER MISSING AT ROW 2. INSTALLED LIGHT PER MM.
OVERWING EMERGENCY EXIT SIGN BROKEN ON LANDING. R & R THE SIGN IAW MM.
OVERWING ROW EMERGENCY EXIT SIGN BROKEN. R & R THE SIGN IAW SIP.
R1 DOOR AFT GIRT BAR BRACKET OUT OF ADJUST. ADJUSTED THE BRACKET IAW SIP.
OVERWING EXIT DOORS CEILING EXIT SIGN LENS MISSING. R & R THE SIGN IAW SIP.
AFT EMERGENCY FLASHLIGHT HAD A BROKEN SAFETY STRAP. R & R THE STRAP IAW SIP.
OVERWING OVERHEAD EMERGENCY EXIT SIGN PLACARD MISSING. INSTALLED THE SIGN IAW SIP.
OVERHEAD OVERWING EXIT SIGN LIGHT PLATE COVER LOOSE. SECURED THE COVER IAW MM.
R1 DOOR ESCAPE SLIDE AFT RETAINING CLIP OUT OF ADJUST. ADJUSTED HOOK IAW SIP.
MID CABIN EMERGENCY EXIT SIGN FELL OFF. ATTACHED THE SIGN IAW MM.
MID PLATE EMERGENCY EXIT SIGN COVER FELL OFF. SECURED THE LIGHT COVER IAW SIP.
OVERWING OVERHEAD EMERGENCY EXIT LENS LOOSE. SECURED THE LENS IAW AMM.
LT OVERHEAD BIN EMERGENCY LIGHT LENS COVER CRACKED AT ROW 12. R&R COVER PER AMM.
MID CABIN CEILING EXIT SIGN LOOSE. SECURED SIGN IAW AMM.
R1 DOOR EXTERIOR EMER EXIT LIGHTS FAULTY. R & R BATTERY PACK IAW MM.
R1 DOOR INTERIOR EMER EXIT LIGHTS FAULTY. R & R BATTERY PACK IAW MM.