N475WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2015-12-23 – 2015-12-23 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2015-12-23 – 2015-12-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
NUMEROUS EMERGENCY LIGHTS IN THE CABIN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS M1673 (AFT LT GALLEY) AND M1674 (FWD RT GALLEY) IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
LEFT WING INBD FIXED TE SEAL BULKHEAD FITTING CRACKED. REMOVED AND REPLACED THE LT WING INBD FIXED TE SEAL BULKHEAD FITTING IAW SRM 51-40-02, AND DWG 115A2930, REV E.
FOUND MISSING LENSE ON OVERHEAD STOWAGE BIN EMERGENCY LIGHT AT LT ROW 4. INSTALLED NEW LENS ON OVERHEAD STOWAGE BIN EMERGENCY LIGHT AT SEAT ROW 4ABC IAW AMM 33-51-03-960-801, STEP D.(3)(C).
FWD ENTRY DOOR; DOOR TARGET ANGLE CRACK. REMOVED AND REPLACED FWD ENTRY DOOR; DOOR TARGET ANGLE IAW SRM 51-40-02 AND IPC 52-11-00-02B. REMOVED AND REPLACED FWD ENTRY DOOR TARGET ANGLE IAW SRM 51-40-02 AND IPC 52-11-00-02B.
FRAME STRAP AT BS 328 STR 20R-22R DOES NOT MATCH CONFIGURATION OF FIG 5 CUSTOMER CARD 5311-I-17336NG STEP 13, FOUND REPAIR AT BS 328 FRAME BETWEEN STRINGERS S-19 R AND S-24R CARD REQUIRES CONTACT ENGINEERING USING ESR OR TSR. VERIFIED PERFORM OP TEST OF IND LIGHT DIMM M469 IAW AMM 33-18-00-960-805, NO DEFECTS NOTED. INSPECTED AREA OF EA 24-153-03187 EXISTING REPAIR PER EA 26-153-01076. AMOC FOR AD 2025-15-01 TRACKING ON EA 26-153-01076-TRK..
POSSIBLE CRACK IN LT AC PACK BAY AFT UPPER CORNER. REPLACEMENT ATTACH ANGLE FABRICATED AND INSTALLED PER EA 26-157-01152.
CABIN SEAT RECLINE NEEDS TO BE INOP AT 11F (EXIT ROW). ADJUSTED SEAT 11F IAW AMM 25-22-00.
OVERHEAD EXIT SIGN ABOVE EXIT ROW FELL OFF<[01] REINSTALLED OVERHEAD EXIT SIGN ABOVE EXIT ROW IAW AMM 33-51-01
EMERGENCY LIGHTING BATTERY PACK AT R/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.;[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
RH EMERGENCY EXIT DOOR LIGHT COVER MISSING (MID-CABIN) (OVERWING EXIT)<[01] INSTALLED RH OVERWING EMERGENCY EXIT DOOR RH SIDE OF DOOR EXIT INDICATOR LENS IAW AMM 33-51-01. NO DEFECTS NOTED AT THIS TIME.
AFT SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] ADJUSTED CAM PLATE PER AMM 52-41-00
L/R OWE SLIDE LIGHT INOP ***CORRECTION TO TITLE*** L/H OWE SLIDE LIGHT INOP<[01] RECONNECTED LEFT FWD ESCAPE SLIDE LIGHT CONNECTOR AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801 STEP D (4).;[02] RELAMP L/R OWE SLIDE LIGHT AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801 STEP D (4).;[03] VERIFIED ACTION ITEMS 1 & 2;[04] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
FWD ENTRY EMERGENCY EXIT SLIDE LIGHT INOP<[01] REPLACED LAMP AT FWD ENTRY EMERGENCY EXIT SLIDE LIGHT IAW AMM 33-51-04-960-801; LIGHT CONTINUE INOP.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RECONNECTED FWD ENTRY EMERGNCY EXIT SLIDE LIGHT CONNECTOR AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801 STEP D (4).;[04] VERIFIED ACTION ITEM 3;[05] UPDATED MEASUREMENTS TABLE.;[06] VERIFIED CORRECTIONS ITEMS 3-5;[07] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
R/H OVERWING EXIT WINDOW LIGHT ASSY. HAS BURNED OUT EMERGENCY LIGHT BULB<[01] EMERGENCY LIGHT BULB REPLACED AT R/H OVERWING EXIT WINDOW LIGHT ASSY AND PERFORMED GOOD OPERATIONAL TEST IAW 33-51-01-960-801.;[02] CERTIFIED ACTION 1.;[03] CORRECTION CORRECTIVE ACTION NO. 1 REFERENCE IS AMM 33-51-01-960-801.;[04] VERIFIED CORRECTIVE ACTION STEP 1;3.
CORROSION ON PASSENGER CABIN STIFFENER AT BS 706+7 RBL 63 WL 202<[01] REFER TO FAULT TTG8Q00SN4XS WHERE EA 24-153-01070 WAS ADDED AS A SUBTASK.;[02] CORRECTED MEASUREMENT TABLE.;[03] UPDATED STEP 2.1 AND 2.3
PAX CABIN FLOOR ATTACH ANGLE CRACKED AT BS 693; RBL 22 WL203.<[01] COMPLETED STEPS 1 AND 2 REMOVED AND REPLACED CRACKED CABIN FLOOR ATTACH ANGLES AT BS 693 RBL 22 AND BL 0 ALL AT WL 203 VERIFIED ALL STEPS COMPLETE ALL IAW SRM 51-40-02-0G-0 AND BOEING DWG 273A9110;[02] VERIFIED CORRECTIVE ACTION 1
CORROSION ON STRAP AT MID PAX CABIN BS 711; RBL 63; WL 202. CORROSION ON STRAP AT MID PAX CABIN BS 706+2 RBL 63 WL 202.<[01] UPDATED STEPS 2;3 AND 4.;[02] UPDATED MEASUREMENTS TABLE;[03] PICTURES OF DAMAGE IS MISSING IN ATTACHMENTS.;[04] UPDATED STEP 2 AND 4;[05] EDITED STEP 4;[06] STEP 3 AND 4 AND 8 COMPLETE;[07] 'AS PER EA 24-153-01070; THE REWORK AND PART REPLACEMENT IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.'
PAX CABIN FLOOR PANEL BRAKE CRACKED AT BS 540; LBL 1 WL208.<[01] REMOVED AND REPLACED BREAK PANEL BS540 LBL1-LBL25 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 <BR>TASK COMPLETED;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE
PAX CABIN FLOOR PANEL BRAKE CRACKED AT BS 540; RBL 1 WL208.<[01] REMOVED AND REPLACED BREAK PANEL BS540 RBL1-RBL25 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 <BR>TASK COMPLETED;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PAX CABIN FLOOR PANEL SUPPORT BRACKET CRACKED AT BS 705; LBL 23 WL208.<[01] UPDATED STEP 1 AND COMPLETED STEP 3;[02] UPDATED STEP 4;[03] COMPLETED STEP 5.;[04] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] PAX CABIN FLOOR PANEL SUPPORT BRACKET AT BS 705; LBL 23 WL208 IAW SRM 51-40-02 AND BOEING DWG 144A5700 SH1.;[05] VERIFIED ACTION 4.<BR>JOB COMPLETE.
PAX CABIN FLOOR ATTACH ANGLE CRACKED AT BS 693; LBL 22 WL203.<[01] COMPLETED STEP 1 AND VERIFIED ALL STEPS COMPLETE REMOVED AND REPLACED CRACKED CABIN FLOOR ATTACH ANGLE AT BS 693 LBL 22 WL 203 IAW SRM 51-40-02-0G-0 AND BOEING DWG 273A9110;[02] VERIFIED ITEM 1
CRACKED INTERCOSTAL COMMON TO FLOOR BOARD HOLE AT BS 322 LBL 45 WL 208 (MARKED)<[01] REMOVED AND REPLACED INTERCOSTAL BS312-BS328 LBL45 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CABIN FLOOR PANEL 221GF CORNER IS DAMAGED AND INSERTS ARE CORRODED. (MARKED)<[01] PARTIAL STEP 1;[02] COMPLETED STEP 1;[03] REMOVED PASSENGER CABIN FLOOR PANEL 221GF PER AMM 53-21-00-000-801. CABIN FLOOR PANEL 221GF WITH CORNER DAMAGED AND INSERTS CORRODED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0.PARA 9.A.(1); AIPC 53-21-00-50D.ITEM [295]. INSTALLED FLOOR PANEL 221GF IAW AMM 53-21-00-400-801<BR>TOOLING ID: NCX001167<BR>DUE DATE: 06/2024;[04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
CORROSION ON BOTH FED GRIT BAR FITTING BRACKETS COMMON TO FED MOPSILL. (MARKED)<[01] UPDATED STEP 1;[02] UPDATED STEPS 2 AND 3;[03] REMOVED BOTH FED GRIT BAR FITTING BRACKETS COMMON TO FED MOPSILL PER SRM 51-40-02-0G-0. NSTALLED BOTH FED GRIT BAR FITTING BRACKETS COMMON TO FED MOPSILL PER SRM 51-40-02-0G-0-A00729 REMOVED CORROSION IN THE AREA OF 1' X 2' X 0.010' FROM ORIGINAL MATERIAL THICKNESS 0.070'. FOUND PART TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS AVAILABLE WORK ACCOMPLISHED PER SRM 51-10-02-0G-0.;[04] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
RIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT I/B SIDE OF RIB STAB STA 193.90; 17 INCHED FWD OF R/S<[01] UPDATED MEASUREMENT TABLE.;[02] REMOVED DAMAGE AND INSTALLED REPAIR @ RH HORIZONTAL STABILIZER LOWER SKIN @ STA 193.90 IAW SRM 55-10-01-2R-11.;[03] VERIFIED CORRECTIVE ACTION & MEASUREMENTS FIELDS
EXISTING REPAIR COMMON TO BS663 WL150 LBL16 VAPOR BARRIER WAS FOUND TO BE DISBONDED<[01] RECEIVED NEW VAPOR BARRIER. LOCATED AND DRILLED REPLACEMENT VAPOR BARRIER AS PER BOEING DRAWINGS 111A1151; 111A1001; 144A7100; 111A1000; 111A7000 AND 737-700 SRM 51-40-05-0G-0. REPLACEMENT VAPOR BARRIER WILL BE INSTALLED ON FAULT TTG8Q00SJFYV.
CORROSION AFT CARGO BAY INTERCOSTAL BS807+2 S-27R WL150<[01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02 AND DWG 146A8132.;[02] STEP # 2 COMPLETE; TASK CARD COMPLETE.
CORROSION AFT CARGO BAY INTERCOSTAL BS787+6 S-27R WL150<[01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02 AND DWG 146A8132.;[02] STEP # 2 COMPLETED TASK CARD COMPLETE.
CORROSION AFT CARGO BAY INTERCOSTAL BS767+3 S-27R WL150<[01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02 AND DWG 146A8132.;[02] STEP # 2 COMPLETE TASK CARD COMPLETE.
CORROSION AFT CARGO BAY INTERCOSTAL BS767+5 S-25R WL150<[01] INTERCOSTAL FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
G-4 GALLEY EXIT LIGHT LENS BROKEN.<[01] REMOVED AND REPLACED G-4 GALLEY EXIT LIGHT LENS PER AMM 33-51-01-960-801 STEPS 2.C.(1)(A); (4);[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.
CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] SHIELD FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A8123;146A0081.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A7500.
CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] VERIFIED COMPLETE ALL RII REQUIREMENTS.;[03] COMPLETE STEP 1; CARD COMPLETE.
AFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED<[01] COMPLETED STEP 5;6.;[02] REPAIRED AFT CARGO BAY FORWARD CORNER THRESHOLD BY WELDING; APPLIED CHEMICAL CONVERSION AND PRIMED; ALL PER SRM 53-60-15-2R-1;[03] VERIFIED CORRECTIVE ACTION 2
R/H HORIZONTAL STAB REMOVABLE L/E 4TH RIB FROM I/B END IS CRACKED<[01] REMOVED RH HORIZONTAL STABILIZER LEADING EDGE RIB #4 IAW SRM 51-40-02-0G-0.;[02] RELACED R/H HORIZONTAL STAB. REMOVEABLE L/E RIB; 4TH FROM I/B END IAW SRM 51-40-02 0G-0 PARA. 4 AND BOEING DWG. 186A1001.;[03] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
LH HORIZONTAL STABILIZER RIB AT STAB STA 129.50 IS CRACKED AT 2ND STIFFENER<[01] CUT AND REMOVED CRACK DAMAGE ON LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 129.50 AT 2ND STIFFENER FROM FRONT SPAR AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CRACKED STRINGER MAIN DISTRIBUTION BAY BS535 S-25L WL150<[01] CRACK FOUND TO BE OUT OUR LIMITS AS PER SRM 53-00-03-1A-1;REMOVED DAMAGED SECTION OF STRINGER 25 L/H BETWEEN BS 500D+11.5' TO BS 536 PER SRM 53-00-03-2R-1 PAR 4 ;STEP B ;FIG 205 AND REPAIRED IAW SRM 53-00-03-2R-1.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CRACKED STRINGER MAIN DISTRIBUTION BAY BS535 S-23R WL150<[01] CRACK FOUND TO BE OUT OUR LIMITS AS PER SRM 53-00-03-1A-1; REMOVED DAMAGED SECTION OF STRINGER 23 R/H BETWEEN BS 500D+12' TO BS 536 PER SRM 53-00-03-2R-1 AND REPAIRED PER SRM 53-00-03-2R-1 AND EA 24-153-00885.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.;[03] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00885.;[04] UPDATED CORRECTION-VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PANEL 192JR OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 192JR OUTER SKIN WAS DISBONDED NEAR CENTER OF PANEL AND REPAIRED IAW SRM 51-70-05-2R-2;[02] JOB COMPLETE.
FWD GALLEY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK FOR THE FWD GALLEY EMERGENCY LIGHTS. OPS CHECK GOOD PER AMM 3351-06
PASSENGER CABIN: LEFT EVACUATION STRIP AT SEAT 1C IS SHORT.<[01] INSTALLED MISSING PHOTOLUMINESCENT STRIP PER AMM 33-51-15;[02] C/W INSPECTION PER AMM 33-51-15.
FORWARD GALLEY SERVICE DOOR (R1). AFT SLIDE RETAINER ISOLATOR CRACKED.<[01] REMOVED AND REPLACED PER SRM 51-40-02;[02] C/W INSPECTION PER SRM 51-40-02.
AFT CAPTAINS SIDE WHITE EXIT SIGN COVER BY ENTRY DOOR MISSING.<[01] INSTALLED NEW EMERGENCY EXIT SIGN IAW SIP.
LEFT FORWARD ENTRY DOOR PARTIALLY OPENED WITH SLIDE GIRT BARS STILL ARMED. RAFT FELL OUT OF BOX BUT DID NOT INFLATE.<[01] UPDATED PART REQ FOR SLIDE R&R;[02] R/R FWD ENTRY ESCAPE SLIDE IAW AMM 25-66-01.
AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET CRACKED<[01] REMOVED AND REPLACED AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET PER AMM 52-41-00
ONE FWD EMERGENCY FLASHLIGHT WILL NOT TEST. R & R THE FWD EMERGENCY FLASHLIGHT BATTERY PACK IAW MM 25-64-00. OPS NORMAL
COCKPIT EMERGENCY LIGHT DOES NOT COME ON / [01] REPLACED M1219 OPS CHECK GOOD PER AMM 33-51-00
EMERGENCY EXIT LIGHTS INOP AT FWD ENTRY DOOR OVERHEAD; 3FED; 6 FED AND EXTERIOR LIGHT AFT OF FWD SERVICE DOOR. / [01] REPLACED BATTERY PACK M1674 AND PERFORMED GOOD TEST OF BATTERY PACK AND ASSOCIATED LIGHTS PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION 1.
CORROSION FOUND AT AFT CARGO BAY RAIL BS 767+4 RBL 8 / [01] DUE CORROSION NOTED AT TWO(**) SEPARATE LOCATIONS ONE IN LIMITS AND ONE OUT OF LIMITS.<BR>RAISED NEW FAULT TTG8Q00BUGAD TO CAPTURE CORROSION LEVEL ONLY <BR><BR>**#1- AT AFT CARGO BAY RAIL BS 727D + 5' RBL 8; DAMAGED FOUND IN LIMITS DOCUMENTED AND RESOLVED ON FAULT# TTG8Q00BLW3Z <BR>**#2- AT AFT CARGO BAY RAIL BS 767 + 4' RBL 8; DAMAGED FOUND OUT OF LIMITS(REF: DAMAGE REPAIRED ON FAULT# TTG8Q00BLV4T.) <BR><BR>CORROSION AT AFT CARGO BAY RAIL BS 767 + 4; RBL 8- REPAIRED ON FAULT # TTG8Q00BLV4T.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED COMPLETE
PANEL 193AR IS DELAMINATED ON INNER SURFACE 7.5' AFT OF FWD EDGE; 20' OB OF IB EDGE / [01] IDENTIFIED MATERIAL OF PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 18; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.B(6)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 PER SRM 53-40-70-2R-1 PARA 4.B(1) AND 4.D(1); TABLE 202;[02] CORRECTION: INCORRECT TABLE REFERENCED<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 PER SRM 53-40-70-2R-1 PARA 4.B(1) AND 4.D(1); TABLE 201;[03] VALIDATED REPAIR PER SRM 51-70-05-2R-2;[04] VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBOND NOTED; REMOVED 2' DIA OF INNER SKIN AND PARTIAL DEPTH CORE; CLEANED REPAIR AREA IAW SRM 51-70-05-2R-2 PARA 4.A-B; [06] POTTED REPAIR AREA WITH BMS 5-28 TY 7 POTTING (CG1305) LOT AK1IP9146K AND SET FOR ROOM TEMP CURE IAW SRM 51-70-05-2R-2 PARA 4.D 'NOTE' AND SRM 51-60-05-2R-11 PARA 4.A-B;[07] COMPLETED SUCCESSFUL POTTING CURE AT ROOM TEMPERATURE; LIGHTLY SANDED REPAIR AREA FLUSH; AND CLEANED. FABRICATED AND INSTALLED REPAIR PLIES USING BMS8-79CL3ST120 LOT#1488452-1 AND BMS5-129TY2 GR05 LOT#1483858-1. INSTALLED VACUUM BAG; LEAKED CHECKED GOOD USING VACUUM GAUGE ID:E11543 S/N:UNKNOWN. IAW SRM 51-70-05-2R-11 PAR.4 B-E & SRM 51-70-05-2R-2 PAR.4 F-H;[10] REFINISHED REPAIR AREA IAW SRM 51-70-05-2R-2 PARAGRAPH 4.K
PANEL 193AL HAS DELAMINATION OF OUTER SURFACE ALOND LEADING EDGE; 38' OB OF IB EDGE / [01] IDENTIFIED MATERIAL OF PANEL 193AL IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 7; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.B(6)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 AND 51-70-14 PER SRM 53-40-70-2R-1 PARA 4.B(2) AND 4.D(2); TABLE 202;[02] VALIDATED REPAIR PER SRM 51-70-05-2R-6;[05] FABRICATED REPAIR PLIES FROM BMS 8-139 LOT 1481644-1 AND BMS 5-154 LOT 1463556-1; INSTALLED REPAIR PLIES IAW SRM 51-70-05-2R-6 PARA 4.E;[06] VACUUM BAGGED AND SET FOR CURE IAW SRM 51-70-05-2R-6 PARA 4.F-G<BR><BR>HOT BONDER NCX000526;[07] CURED REPAIR; UNBAGGED AND LIGHTLY SANDED IAW SRM 51-70-05-2R-6 PARA 4.G AND 4.I;[10] FABRICATED EXPANDED ALUMINUM FOIL MESH USING BMS 8-336 LOT#1360513-1; INSTALLED USING BMS 8-301 CL1 GR1 LOT#JH1GAA7833; VACUUM BAGGED; CHECKED FOR LEAKS AND SET TO CURE USING HEATCON HOTBONDER ID:ATS532 S/N:15092117 IAW SRM 51-70-14-2R-4 PAR 5D;F;I-K(1-11).;[11] COMPLETED THE FOIL MESH REPAIR & RESTORED THE FINISH IAW SRM 51-70-14-2R-14 PARA 5 . K STEPS 11-14. USING BMS10-103 PRIMER & BMS10-60 ENAMEL.;[12] VERIFIED CORRECTIVE ACTION STEPS 10 AND 11;[13] PANEL 193AL DELAMINATION OUTER SURFACE ALONG THE L/E 38' OB OF IB EDGE WAS REPAIRED IAW SRM 51-7-05-2R-6.;[14] REPAIR COMPLETE
BS 500A FRAME CRACKED AT FASTENER HOLE STR 26 L/H / TRIMMED OUT THE DAMAGED PART OF THE FRAME AT BS 500A LBL 24 L=1' W=1' IAW 53-30-07-0I-1 AND 53-30-07-2R-1 STEP 4. C. (1);[03] TRIMMED OUT THE DAMAGED PART OF THE FRAME AT BS 500A LBL 24 L=1' W=1' IAW SRM 53-30-07-2R-1 STEP 4. C. (1);[05] NDT HFEC INSPECTED TRIM OUT AND HOLES IAW SRM 53-30-07-2R-1 AND 737 NDTM PART 6 51-00-00 PROC 23 AND PROC 16; NO CRACKS NOTED AT TRIM OUT. SEVERAL DAMAGED/OUT OF ROUND HOLES NEED REPAIRED THEN HOLE NDT AGAIN. ID ISOOO450 SN N500D000M120071.;[06] PERFORMED OVERSIZE HOLES ON DAMAGED HOLES 1/32 AS REQUIRED ; FINAL DIAMETER 0.218' IAW SRM 51-40-05 FIGURE 3 TABLE A-BRECEIVED ; FORMED AND HEAT TREATED ; ITEM 1 REPAIR DOUBLER ON CUSTOMER RO NO : 862987-SWA ;MATERIAL USED 7075 T0 ; 0.063' LOT#1449291-1 <BR>IAW SRM 53-30-07-2R-1 REPAIR 1 LOCATED AND DRILLED -1 REPAIR ANGLE IAW SRM 53-30-07-2R-1 REPAIR 1 ALTERNATIVE 1;[14] REPAIR PART ITEM 2 STRINGER CLIP DOCUMENTED ON CUST SYSTEM ID:TTG8Q00BNPG1;FABRICATED; LOCATED AND DRILLED FILLER AND SHIM AT B/S 500A STR 26 L/H MATERIAL USED : 7075T6 #0.012' LOT#1086450 IAW SRM 53-30-07-2R-1 REPAIR 1 ALTERNATIVE 1<BR>OK TO APPLY PRIMER] OK TO INSTALL FILLER; SHIM ; NEW CLIP AND NEW CLIP; OUT OF SEQUENCE: APPLIED CHEMICAL CONVERSION AND PRIMER ON FILLER AND SHIM IAW SRM 53-30-07-2R-1 REPAIR 1 ALTERNATIVE 1 INSTALLED REPAIR PARTS AT FCB BS 500A BTW LBL 18 TO LBL 25 IAW SRM IAW SRM 53-30-07-2R-1 REPAIR 1 ALTERNATIVE 1. AND UPDATE STEP 1
CRACK IN RADIUS OF B.S. 312 FRAME JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / [01] VERIFIED SRM 53-00-07-1A-1 IS APPLICABLE FOR DAMAGE ON A FRAME;[02] CRACK IN BS 312 FRAME FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 FIG. 102 DETAIL E;[03] REQUEST NDI TO MARK END OF CRACK;[04] HFEC INSPECTED FRAME BS312 AND MARKED END OF CRACKED AS REQUESTED IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23. <BR>EQUIP USED: NORTEC 600 ID: ATS1465;[05] VERIFIED CORRECTIVE ACTION 1 AND 2.;[06] TRIMMED .400' FROM EDGE OF BS 312 FRAME TO REMOVE CRACK; MAINTAINING .5' RADIUS PER SRM 51-10-02;[07] REQUEST NDI TO HFEC TRIMMED EDGE TO ENSURE A CRACK FREE CONDITION;[08] HFEC INSPECTED TRIMMED EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23. <BR>EQUIP USED: IS000450 500D;[09] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[10] ADDITION TO ACTION 8; NO CRACKS FOUND.;[11] CARD COMPLETE;[12] VERIFIED COMPLETE
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727B+6; BS 727B+14; BS 727C+10; BS 727D+3; BS 727D+6; BS 727D+10; BS 727D+14. / [01] SRM 53-60-53-0I-2 IDENTIFICATION AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE ARE APPLICABLE<BR><BR>REMOVED CORROSION BY BLENDING FLOOR TO SIDEWALL SUPPORT UPPER SURFACE PER SRM 51-10-02. MATERIAL LOSS L=3.7'; W=1.0'; D=0.010'. ORIGINAL THICKNESS 0.040'; REMAINING THICKNESS 0.030'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL E.<BR>GAGE: ATS1672; S/N:65092939; DUE DATE 03/2023;[02] VERIFIED CORRECTIVE ACTION 1- BLEND OUT OF LIMITS.;[03] UPDATED MEASUREMENTS;[04] FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 21 IS REPLACED ON CUST. CARD TTG8Q00BLW4N;[05] VERIFIED STEP 2.
CORROSION ON MOP SILL AT AFT WET AREA BS992 - BS951 RBL50 WL208. / [01] REMOVED MULTIPLE AREAS OF CORROSION ON MOP SILL BS951-992 RBL50 WL208; DEEPEST BLEND FOUND AT BS 967+10 MEASURES 1'X1'X0.020'; ORIGINAL THICKNESS 0.080'; FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1.;[02] FOUND SRM 53-70-15-1A-1 APPLICABLE FOR ALLOWABLE DAMAGE LIMITS OF MOP SILL.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.;[04] REMOVED MOP SILL AT RBL50 WL208 FROM BS 894 TO 1006 PER SRM 51-40-02-0G-0;[05] COMPLETED LOCATING AND DRILLING OF AFT RH MOP SILL PER SRM 51-40-05.;[06] VERIFIED CORRECTIVE ACTION 5;[07] REQUEST OK TO INSTALL NEW AFT RH MOP SILL.;[08] OKAY TO INSTALL MOP SILL AT AT RBL50 WL208 FROM BS 894 TO 1006.;[09] SEALANT MIXED/APPLIED 11-APR-2022 14:00 UTC; INSTALLED 100% PERMENENT OR TEMP FASTENERS PRIOR TO BMS5-95 C20 SEALANT SQUEEZE-OUT TIME; REF. SOPM 20-50-19.;[10] VERIFIED CORRECTIVE ACTION ITEM 9 FOR SEALANT SQUEEZE-OUT.;[11] INSTALLED MOP SILL AT RBL50 WL208 FROM BS 894 TO 1006 PER SRM 51-40-02 AND DWGS 147A8501; 147A0004 AND 147A0060.;[12] VERIFIED CORRECTIVE ACTION ENTRY 11.;[13] UPDATED REPAIR TYPE;[14] CERTIFY;[15] VERIFIED ALL STEPS COMPLETE
CORROSION ON MOP SILL AT AFT WET AREA BS992 - BS967 LBL50 WL208. / [01] FOUND SRM 53-7--15-1A-1 APPLICABLE FOR ALLOWABLE DAMAGE LIMITS OF MOP SILL.;[02] REMOVED MULTIPLE AREAS OF CORROSION ON MOP SILL BS967-992 LBL50 WL208; DEEPEST BLEND FOUND AT BS 986+6 MEASURES 2'X1'X0.012'; ORIGINAL THICKNESS 0.080'; FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1.;[03] SRM CORRECTION; APPLICABLE SRM IS 53-70-15-1A-1;[04] VERIFIED CORRECTIVE ACTION 1-3;[05] REMOVED DAMAGED MOPSILL AT LH AFT L2 DOOR LOCATION IAW SRM CH 51-40-02.;[06] COMPLETED LOCATING AND DRILLING OF NEW AFT LH L2 DOOR MOP SILL PER SRM 51-40-05.;[07] UPDATED MEASUREMENTS TABLE;[08] VERIFIED CORECTIVE 6.;[09] OK TO INSTALL;[10] OKAY TO INSTALL MOP SILL AT L/H AFT ENTRY DOOR.;[11] SEALANT MIXED/APPLIED 11-APR-2022 14:00 UTC; INSTALLED 100% PERMENENT OR TEMP FASTENERS PRIOR TO BMS5-95 C20 SEALANT SQUEEZE-OUT TIME; REF. SOPM 20-50-19.;[12] VERIFIED CORRECTIVE ACTION ITEM 11 FOR SEALANT SQUEEZE-OUT.;[13] INSTALLED MOP SILL AT L/H AFT ENTRY DOOR PER SRM 51-40-02 AND DWGS 147A8501; 147A004 AND 147A0060.;[14] UPDATED PARTS;[15] CERTIFIED ACTION 13 JOB COMPLETE;[16] VERIFIED CORRECTIVE ACTION ENTRY 13.;[17] VERIFIED CARD COMPLETE.
CORROSION ON FLOOR SUPPORT AT AFT WET AREA BS947+13 LBL41 WL208. / [01] REMOVED CORROSION FROM SUPPORT AT BS 947+13 LBL41 MAX MAT. LOSS OF .025 FOUND TO BE OUT OF LIMITS USING TOOL ID # ATS1225 S/N UNK. CAL DATE 07/2021 DUE 07/2022 IAW SERM CH 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW SUPPORT FOR LBL41 BS947-967 IAW SRM CH 51-40-05 OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION #1; 2;[04] INSTALLED SUPPORT AT BS 947- 927 LBL41 WL 208 IAW SRM CH 53-40-02 AND DRAWING #140A9870 SHT 11.;[05] VERIFIED CORRECTIVE ACTION #4;[06] VERIFIED CORRECTIVE ACTION #4
CORROSION ON WEB AT AFT WET AREA BS986+8 RBL39 WL208. / [01] REMOVED CORROSION ON WEB AT BS986+8 RBL39 WL 208 IN A 1.5'X1.5'X.005 ORIGINAL THICKNESS .020 OUT OF LIMITS PER SRM 53-70-51-1A-1STEP 4-C 2 FIG 103;[02] REMOVED WEB AT BS 986 TO 1016; RBL 37 TO RBL 47 PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW WEB AT BS986-1016 RBL37-47; PER SRM 51-40-05.;[04] VERIFIED CORRECTIVE ACTION 3.;[05] OK TO INSTALL WEB AT BS986-1016; RBL37-47; WL 208.;[06] OK TO INSTALL GIVEN;[07] INSTALLED WEB AT BS986-1016; RBL37-47; WL 208 PER SRM 51-40-02 AND DWG 147A5730 AND 147A0000.;[08] VERIFIED CORRECTIVE ACTION ENTRY 7.;[09] UPDATED REPAIR TYPE;[10] UPDATED REPAIR TYPE;[11] UPDATED CORROSION LEVEL;[12] CERTIFY;[13] VERIFIED STEPS COMPLETE
CORROSION ON FLOOR SUPPORT AT AFT WET AREA BS997 RBL7 WL208. / [01] VERIFIED APPLICABILITY FOR SRM 53-70-51-1A-1.<BR>REMOVED CORROSION ON FLOOR SUPPORT ; RBL7 WL 208 IN A 1.3X1.9' AREA; MAX DEPTH .025'. ORIGINAL THICKNESS IS .080'. FOUND TO BE OUT LIMITS PER SRM 53-70-51-1A-1; MEASURED WITH DIAL DEPTH GAUGE ID: ATS2677.;[02] VERIFIED CORRECTIVE ACTION #1; OUT OF LIMITS;[03] REMOVED INTERCOSTAL AT RBL7 WL208 FROM BS 886;5 TO 1006 PER SRM 51-40-02-0G-0;[04] INTERCOSTAL LOCATION IS RBL7; WL208; FROM BS 986.5 TO 1006.;[05] LOCATED AND DRILLED INTERCOSTAL AT BS 986.5-1006; RBL 7 PER DWG 147A5730 AND SRM 51-40-05. INTERCOSTAL TO BE INSTALLED ON TTG8Q00BLVCP.;[06] VERIFIED CORRECTIVE ACTION ENTRY 5.
CORROSION ON FLOORBEAM AT AFT WET AREA BS986.5 LBL44 TO RBL44 WL208. / [01] REMOVED CORROSION ON FLOOR BEAM AT BS 986 W/L 208 RBL44 2'X3'X.100 ;RBL7 REMOVED 1.6X1.5X.050; AT LBL 42 REMOVED 1.5X1.5X.042 ALL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 STEP 4-H 2 FIG 103;[17] FABRICATED REPAIR PARTS TWO SECTIONS T-CHORD [1] MADE OF BAC1505-101474 #7050-T76511; LOT# 1385019-1 FROM RBL 50 TO LBL 50; TWO EA. ANGLES [2] MADE OF BAC1490-2811#7075 T62 .071' LOT # 1488279-1; TWO EA. ANGLES (3) MADE OF BAC1490-2887#7075 T62 .080' LOT # 1361302-1 AND TWO EA. STRAPS [4] MADE OF 7075 T6 .080' LOT # 1379745-2. LOCATED AND DRILLED ALL PARTS OF REPAIR AND APPLIED CHEMICAL CONVERSION COATING IAW EA 22-153-01043 REV A AND SRM 53-70-51-2R-4 ALTERNATIVE 1.<BR>REQUEST OK TO APPLY PRIMER.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 887+5; BS 947. / [01] REMOVED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 947 TO 867 RH;IAW SRM 51-40-02.;[02] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS887+5;BS947;AT DISCREPANCY AREA ;FOUND TO BE OUT LIMITS MEASURES:L=1.300;W=.900;D=.024';ORIGINAL TICKNESS:0.040';;REMAINING TICKNESS:.016';MATERIAL LOSS:0.024';IAW SRM 53-00-53-1A-2 PARAG 4 A(2) DETAIL C FIG.103.TOOL USED:ATS1671;S/N65093024;DUE:10/2022.;[03] CUSTOMER CARD TTG8Q00BLW5S IS FOR DOCUMENTATION OF CORROSION REMOVAL AND FABRICATION ONLY.;[04] UPDATED MEASUREMENTS;[05] VERIFIED CORRECTIVE ACTION 2.;[06] LOCATED AND DRILLED NEW SIDEWALL SUPPORT WITH P/N BAC1496-377;7075-T62;LOT#1484618-1;IAW SRM 53-70-53-0I-2 AND DWG#147A7500 REV B.OK TO TREAT AND PRIME.;[07] VERIFIED CORRECTIVE ACTION 6.<BR>OK TO TREAT AND PRIME;[08] QUIMICAL CONVERSION AND PRIMER SIDEWALL SUPPORT BS887 TO 947; IAW AMM 51-21-41;AND 51-21--72.;[09] APPLIED CHEMICAL CONVERSION AND PRIMER SIDEWALL SUPPORT BS887 TO 947; IAW AMM 51-21-41;AND 51-21--72.;[10] VERIFIED CORRECTIVE ACTION 9.;[11] INSTALLED NUTPLATES ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS887 TO BS947;IAW SRM 51-40-02 AND DGW#147A7500.ALL MAINTENANCE ACTION ARE COMPLETED REQUIRE FINAL BUY OFF.;[12] VERIFIED CORECTIVE ACTION 11.
CORROSION ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT RBL 3 BS 947. / [01] VERIFIED APPLICABILITY OF SRM 51-10-02-0G-0;[02] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR ACB AFT LOWER BULKHEAD SUPPORT; PART TO BE REPAIRED BY REPLACMENT PER SRM 51-10-02-0G-0;[03] VERIFIED CORRECTIVE ACTIONS 1-2. NO LIMITS IN SRM; PART TO BE REPLACED.;[04] LOCATED AND DRILLED HOLES IN NEW RECEIVED PART #149A8118U29 LOT# 1487879-1 PO# 863744 IAW SRM 51-40-05-0G-0 GENERAL - FASTENER HOLE SIZES AND DWG 149A8110 REV:-;[05] LOCATED AND DRILLED HOLES IN NEW RECEIVED PART #149A8118U29 LOT# 1487879-1 PO# 863744 IAW SRM 51-40-05-0G-0 GENERAL - FASTENER HOLE SIZES AND DWG 149A8110 REV:-<BR><BR>OK TO APPLY CHEMICAL CONVERSION AND PRIME BARE METAL;[06] VERIFIED UPDATED STATEMENT;[07] MEASUREMENTS;[08] MEASUREMENTS UPDATE;[09] VERIFIED CORRECTIVE ACTION ENTRIES 5-8. OK TO PRIME GIVEN.;[10] APPLIED CHEMICAL CONVERSION COATING; PRIME AND TOP COAT AT HOLES BARE METAL IAW AMM 51-21-41; AMM 51-21-72 AND AMM 51-21-73;[11] VERIFIED CORRECTIVE ACTION ENTRY 10. CARD COMPLETE.
CORROSION ON AFT CARGO BAY RAIL AT LBL 3 BS 867+3; BS 867+12. / [01] SRM 53-00-53-1A-2 IA APPLICABLE REMOVED DAMAGE ON EDGE AFT CARGO BAY TIE DOWN RAIL IN 2EA. LOCATIONS AT LBL 17; BS 867+3 AND BS 867+12 IN AREA OF: BS867 +3' 1.2'X.036' FOUND TO BE IN LIMITS<BR>BS867+12' 1.2'X.048' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR 2.TABLE 101; PAR 4.B(2) FIG 103 C AND SRM 51-10-02-0G-0<BR><BR>CALIPER<BR>PER1999<BR>S/N UNKNOWN 04/2022;[02] UPDATED MEASUREMENTS;[03] VERIFIED CORRECTIVE ACTION 1.;[04] APPLIED CHEMICAL CONVERSION COATING AND BMS 10-11 PRIMER TO AFT CARGO BAY RAIL AT LBL 3 BS 867+3 IAW AMM 51-00-58/201 AND AMM 51-21-72-370-804;[05] VERIFIED CORRECTIVE ACTION 4.;[06] REMOVED DAMAGED SECTION OF AFT CARGO RAIL FROM LBL 3 BS 847 - BS 887 IAW SRM 51-10-02-0G-0;[07] LOCATED AND DRILLED NEW SECTION OF AFT CARGO RAIL FROM LBL 3 BS 847 - BS 887 P/N: 146A7501U5 PO# 824827/1 RECEIPT # 1459147 IAW SRM 51-10-05 AND DWG 146A7503 REV:- AND DWG 146A7500 REV :-<BR>OK TO INSTALL NEW PART;[08] FIXED PART NUMBER IN MEASUREMENT CHART;[09] VERIFIED CORRETIVE ACTIONS 7 AND 8.<BR>OK TO INSTALL;[10] INSTALLED NEW SECTION OF AFT CARGO RAIL FROM LBL 3 BS 847 - BS 887 IAW SRM 51-10-02 AND DWG 146A7503 REV:- AND DWG 146A7500 REV :-;[11] VERIFIED CORRECTIVE ACTION 10;[12] VERIFIED ALL STEP ACCOMPLISHED
CORROSION ON AFT CARGO BAY INTERCOSTAL AT RBL 22 BS 867+3. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE AND IDENTIFICATION IAW SRM 53-60-53-01-2 AND SRM 51-10-02-0G-0;[02] THREE IS NO SRM ALLOWABLE DAMAGE FOR ACB INTERCOSTAL. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02.<BR>RECEIVED A NEW INTERCOSTAL PN 146A7505-7 FROM STORES REF PO 864199.<BR>LOCATED AND DRILLED NEW PART IAW SRM 51-40-05 AND DWG 146A7500 REV: -<BR>OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION ENTRY 4. OK TO INSTALL GIVEN.;[06] MEASUREMENTS;[07] INSTALLED NEW PART IAW SRM 51-40-02 AND DWG 146A7500 REV: -.<BR>TASK COMPLETE.;[08] UPDATED MEASUREMENTS;[09] VERIFIED CORRECTIVE ACTION ENTRY 7.;[10] VERIFIED CORRECTIVE ACTION ENTRY 8. CARD COMPLETE.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 20 BS 867+17. / [01] REMOVED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 20 BS 867 TO 947 RH;IAW SRM 51-40-02.;[02] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 20 BS 867+17;AT DISCREPANCY AREA;FOUND TO BE OUT LIMITS MEASURES: L=1.00;W=.400;D=.013;ORIGINAL TICKNESS:0.040';REMAINING TICKNESS:0.027;MATERIAL LOSS:0.013';IAW SRM 53-00-53--1A-2;PARAG 4A-2 DETAIL C FIG.103;TOOL USED:ATS1671;S/N 65093024;DUE:10/2022.;[03] CUSTOMER CARD TTG8Q00BLWP5 IS FOR DOCUMENTATION OF CORROSION REMOVAL AND FABRICATION ONLY.;[04] VERIFIED CORRECTIVE ACTION 2.;[05] CUSTOMER CARD TTG8Q00BLW5P IS FOR DOCUMENTATION OF CORROSION REMOVAL AND FABRICATION ONLY;[06] LOCATED AND DRILLED NEW SIDEWALL SUPPORT WITH P/N BAC1496-377;7075-T62;LOT#1484618-1;IAW SRM 53-70-53-0I-2;51-10-05 AND DWG#146A7500.OK TO TREAT AND PRIME.;[07] VERIFIED CORRECTIVE ACTION 6.<BR>OK TO TREAT AND PRIME;[08] QUIMICAL CONVERSION COATING AND PRIMER SIDEWALL SUPPORT BS 867 TO 887;IAW AMM 51-21-41 AND 51-21-72.;[09] APPLIED CHEMICAL CONVERSION COATING AND PRIMER SIDEWALL SUPPORT BS 867 TO 887;IAW AMM 51-21-41 AND 51-21-72. OK TO INSTALL SPLICE;[10] VERIFIED CORRECTIVE ACTION 9.;[11] INSTALLED SPLICE ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 20 BS867 TO BS887;IAW SRM 51-40-02 AND DGW#146A7500;ALL MAINTENANCE ACTION ARE COMPLETED REQUIRE FINAL BUY OFF.;[12] VERIFIED CORRECTIVE ACTION 11
CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+15. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.;[03] RECEIVED NEW ACB AFT SHIELD<BR>ITEM # : 146A8127Y10ATSMRO<BR>PO# : 848298/1;[04] LOCATED; DRILLED; AND COUNTERSANK NEW SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 146A8127 ID:0007 REV:-;[05] VERIFIED CORRECTIVE ACTION 3 AND 4
CORROSION ON AFT CARGO BAY THRESHOLD AT RBL 25 BS 787+11; BS 787+13; BS 807+2; BS 827+2; BS 827+8. / [01] ENTERED MEASUREMENTS;[02] SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 IS APPLICABLE FOR THIS AIRCRAFT.<BR><BR>REMOVED CORROSION DAMAGE IAW SRM 51-10-02-0G-0.;[03] BS827+8'; 0.90'L X 0.70'W. REMOVED 0.008'. REMAINING MATERIAL - 0.042'<BR><BR>BS827+2'; 1.00'L X 0.90'W. REMOVED 0.004'<BR>REMAINING MATERIAL - 0.046'<BR><BR>BS807+2'; 0.50'L X 0.30'W. REMOVED 0.002'.<BR>REMAINING MATERIAL - 0.048'<BR><BR>BS787+13'; 1.10'L X 0.80'W. REMOVED 0.011'<BR>REMAINING MATERIAL - 0.039'<BR><BR>BS787+11'; 1.00'L X 0.04'W. REMOVED 0.005'<BR>REMAINING MATERIAL 0.045';[04] CORROSION DAMAGE FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-15-1A-1; TABLE 101; 4G (2) (B) FIGURE 103; DETAIL D AND SRM 53-60-15-0L-1; TABLE 4; ITEM [2].<BR><BR>REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0.<BR><BR>DEPTH GAGE:<BR>ATS2473<BR>S/N UNKNOWN<BR>CAL DUE 07/2022;[05] VERIFIED CORRECTIVE ACTION #2; 3; 4;[06] LOCATED AND DRILLED NEW ACB THRESHOLD WEB IAW SRM 51-40-05-0G-0 AND DWG 146A8340;[07] VERIFIED CORRECTIVE ACTION ENTRY 6. CARD COMPLETE.
PNEUMATIC DUCT CLAMP SUPPORT BRACKET IS CRACKED AT B.S. 540+6; R.B.L. 8; W.L. 160. LOCATED UNDER PANEL 192CR. / [01] REMOVED DAMAGED PNEUMATIC DUCT CLAMP SUPPORT BRACKET AT BS 540+6; RBL 8; WL 160 AND REPLACED WITH NEW PART #212A1116-1 IAW SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED COMPLETION OF TASK.
PASSENGER CABIN FLOOR PANEL; 221BF; AFT OUTBOARD CORNER IS MISSING. / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-6.<BR>REMOVED 7EA THROUGH INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-6 PARA 3B.<BR>REMOVED DAMAGED SKIN AND CORE AROUND AFT O/B CORNER; CLEANED REPAIR AREA IAW SRM 53-00-50-2R-6 PARA 3C-E.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-6.;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2. OKAY TO PROCEED PER SRM 53-00-50-2R-6.;[04] FABRICATED CORE PLUG OUT OF BMS 8-124 CL4 TY5 GR5 LOT#1283769; AND FABRICATED UPPER SURFACE REPAIR PLIES OUT OF BMS 9-3 ST 1581 LOT#1475360-2 IAW SRM 53-00-50-2R-6 PAR 4F. OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4<BR><BR>OK TO INSTALL CORE PLUG AND REPAIR PLIES;[06] INSTALLED REPAIR PARTS USING BMS 8-201 TY IV LOT#1486456-1; AND BMS 5-28 TY 19 LOT#AK1KP5968K; VACUUM BAGGED; CHECKED FOR LEAKS USING PRESSURE GAGE ID:ATS2583 S/N:5432766772 IAW SRM 53-00-50-2R-6 PAR 3G(1);H(1).;[07] VERIFIED CORRECTIVE ACTION 6;[08] CURED REPAIR WITH THERMOMETER ID:ATS2208 S/N:43300740WS; UNBAGGED AND SANDED CORE PLUG SMOOTH TO SURFACE; FABRICATED LOWER SURFACE REPAIR PLIES<BR>FROM BMS 9-3H2 LOT#1475360-2 IAW SRM 53-00-50-2R-6 PARA 3I-K.<BR>OK TO INSTALL;
CRACK ON AFT CARGO BAY RAIL AT RBL 13 BS 727E. / EVALUATED DAMAGE ON AFT CARGO BAY RAIL AT RBL 13 BS 727E. CRACK DIMENSIONS : L= 0.300' AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 <BR>TOOL USED CALIPER ; ID:ATS2500; DATE DUE 03/2023; REMOVED CARGO TRACK LOCATED BTW B/S 727 TO B/S 767+11' RBL 13 IAW SRM 51-40-02;REMOVED CARGO TRACK LOCATED BTW B/S 727 TO B/S 887 RBL 13 IAW SRM 51-40-02; LOCATED AND DRILLED TRACK ASSY PN 654A0004-1350 COMMON TO FRAMES AND BAFFLE FROM BS727 TO BS 747 AND BS 767 TO BS 887;RBL 13 IAW BOEING DWG 146A7500 AND SRM 51-40-05; INSTALLED TRACK ASSY COMMON TO FRAMES AND BAFFLE FROM BS727 TO BS 747 AND BS 767 TO BS 887;RBL 13 IAW BOEING DWG 146A7500 AND SRM 51-40-02PERFORMED CUT THE TRACK BETWEEN FRAMES LOACTED B/S 747 TO B/S 767 RBL 13;VERIFIED APPLICABILITY OF REPAIR FOR CORRECTIVE ACTION ITEM 12. VERIFIED TRACK CUT BETWEEN FRAMES BS 747 AND BS 767 CORRECTIVE ACTION ITEM 13.NO OTHER DAMAGE IN REPAIR AREA.;[16] HFEC INSPECTED OPEN HOLE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16.<BR>NO CRACKS NOTED <BR>EQUIP USED: NORTEC 600 ID: ATS1465 EQUIP USED: MINIMITE ID: ATS240;LOCATED AND DRILLED TRACK SPLICE ; P/N 146A7506-20 LOT# 1461883-2 IAW SRM 53-00-53-2R-3 REPAIR 3 AND OK TO INSTALL REPAIR PARTINSTALLED [2} TRACK SPLICE BTW B/S 747 TO B/S 767 RBL 13 IAW SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 20 BS 727A+12; BS 727B+6; BS 727C+6; BS 727C+8; BS 727C+10; BS 727D; BS 727D+2; BS 727D+5; BS 727D+8; BS 727D+10. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 20 BETWEEN BS727A+12 INCHES . THE LOWEST REMAINING THICKNESS .033' ON BLENDED AREA L=2.2'X W=1'XD=0.007' ORIG. MAT. THK.=.040' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2 STEP 4A FIG. 103 DETAIL D ;SRM 53-60-53-01-2 TOOL USED ID:ATS1672 ;S/N:65092939; DUE:03/2023 <BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q00BLV44;[02] UPDATED MEASUREMENTS;[03] UPDATED STEPS;[04] VERIFIED STEPS 1-9 AND CORRECTIVE ACTION 1.
FWD CARGO BAY INTERCOSTAL BS 460-480 WL 156 LBL 24 IS CRACKED / [01] REMOVED FCB INTERCOSTAL BS 460-480 LBL24 WL 156 I.A.W SRM 51-40-02-0G-0;[02] RECEIVED NEW INTERCOSTAL P/N:143A7510-13 LOT: 1478990-1 PO/N:852014/1 AND LOCATED AND DRILLED AT FCB ON BS 460 TO 480 WL 156 LBL 24 IAW SRM 51-40-05 AND DWG: 143A7505 ID:0004 REV:-. REQUES OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION ENTRY 2. OK TO INSTALL GIVEN.;[04] INSTALLED INTERCOSTAL AT FCB ON BS 460 TO 480 WL 156 LBL 24 IAW SRM 51-40-02 AND DWG: 143A7505 ID:0004 REV:-.;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED COMPLETE
CORROSION ON AFT CARGO BAY BULKHEAD SUPPORT ATTACH ANGLE AT LBL 10 BS 847+19. / [01] INVESTIGATED DAMAGE PER SRM 51-10-02-0G-0.FOUND SUPPORT ANGLE TO BE CRACKED; NOT CORRODED.;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED AND REPLACED CRACKED SUPPORT ANGLE AY B.S. 867; LBL10 PER SRM 51-40-02-0G-0 AND DWGS 149A8102 SHT 16 AND 149A8104 SHT 1.;[04] VERIFIED CORRECTIVE ACTION 3;[05] VERIFIED COMPLETE
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+13 RBL3 WL208. / [01] REMOVED CORROSION ON TENSION STRAP AT BS 1016+13; RBL3 IN A 3'X1' AREA; MAX DEPTH .003'. ORIGINAL THICKNESS IS .050'. FOUND TO BE WITHIN LIMITS PER SRM 53-70-51-1A-1.;[02] REMOVED CORROSION ON TENSION STRAP AT BS 1016+13; RBL3 IN A 3'X1' AREA; MAX DEPTH .003'. ORIGINAL THICKNESS IS .050'. FOUND TO BE WITHIN LIMITS PER SRM 53-70-51-1A-1; MEASURED WITH DIAL DEPTH GAUGE CAL ID: ATS2677.;[03] REMOVED CORROSION ON TENSION STRAP AT BS 1016+13; RBL3 IN A 3'X1' AREA; MAX DEPTH .016'. ORIGINAL THICKNESS IS .050'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1; MEASURED WITH DIAL DEPTH GAUGE CAL ID: ATS2677; AND DENT GAUGE CAL ID: ATS2595.;[04] VERIFIED CORRECTIVE ACTION #3; OUT OF LIMITS;[05] REMOVED TENSION STRAP AT BS 1006-1030; RBL3; WL208 PER SRM 51-40-02-0G-0.;[06] LOCATED AND DRILLED NEW 147A5744-1 STRAP AT BS 1006-1030; RBL3; WL208 PER DWG 147A5730 AND SRM 51-40-05. OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION #6;[08] INSTALLED NEW TENSION STRAP AT AFT WET AREA BS.1006 TO 1030 RBL3 ; WL208 IAW SRM 51-40-02 AND DWG 147A5730 REV:C;[09] CERTIFY;[10] VERIFIED CORRECTIVE ACTION 8;[11] VERIFIED ALL STEPS COMPLETE.
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016; 1029 LBL3 WL208. / [01] CORROSION ON TENSION STRAP AT BS 1016; LBL3 MEASURES 3'X1'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 DUE TO 100% MATERIAL LOSS.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED TENSION STRAP AT BS 1006-1030; LBL3; WL208 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW 147A5620-3 STRAP AT BS 1006-1030; LBL3; WL208 PER DWG 147A5600 AND SRM 51-40-05. OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION #4;[06] STARTED INSTALLING 147A5620-3 STRAP AT BS 1006-1030; LBL3; WL208 PER DWG 147A5600 AND SRM 51-40-02-0G-0.;[07] COMPLETED INSTALLATION OF 147A5620-3 STRAP AT BS 1006-1030; LBL3; WL208 PER DWG 147A5600 AND SRM 51-40-02-0G-0.;[08] VERIFIED CORRECTIVE ACTION 7.;[09] COMPLETE
CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 24 BS 767+8; BS 767+12. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.;[03] RECEIVED NEW ACB FWD SHIELD<BR>ITEM# : 146A8127U12ATSMRO<BR>PO# : 859290/1;[04] LOCATED; DRILLED; AND COUNTERSANK NEW SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND ;DWG 146A8127 ID:0008 REV:-;[05] VERIFIED CORRECTIVE ACTION 3 AND 4
CORROSION ON AFT CARGO BAY DOUBLER ATTACHED TO TENSION STRAP AND INTERCOSTAL AT RBL 20 BS 787+9. / [01] NO ALLOWABLE LIMITS GIVEN PER SRM. REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0. LOCATED AND DRILLED NEW STRAP PER SRM 51-40-05-0G-0 AND DWG 146A8128. APPLIED CHEMICAL CONVERSION COATING TO BARE METAL PER AMM 51-21-41-370-802.;[02] REQUEST OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.;[04] INSTALLED REPLACEMENT NUT PLATE STRAP AT B.S. 787-787+7 PER SRM 51-40-02-0G-0 AND DWG 146A8120 SHT 19.;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED ALL STEP ACCOMPLISHED
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 20 BS 767+6; BS 767+8; BS 767+10; BS 767+18; BS 787; BS 787+6. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 20 BETWEEN BS727D+14 INCHES . THE LOWEST REMAINING THICKNESS 0.033' ON BLENDED AREA L=3'X W=2.2'XD=0.007' ORIG. MAT. THK.=.040' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2 STEP 4A FIG. 103 DETAIL D ;SRM 53-60-53-01-2 TOOL USED ID:ATS1672 ;S/N:65092939; DUE:03/2023; THE LOWEST REMAINING THICKNESS 0.033' ON BLENDED AREA L=3'X W=2.2'XD=0.007' ORIG. MAT. THK.=.040' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2 STEP 4A FIG. 103 DETAIL D ;SRM 53-60-53-01-2 TOOL USED ID:ATS1672 ;S/N:65092939; DUE:03/2023 FABRICATED; LOCATED AND DRILLED AFT FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 847 LBL 20 AND SPLICER ANGLE AT BS 727E+10 LBL 20 MADE FROM EXTRUSION BAC1496-377 #7075T62 LOT#1484618-1 IAW SRM 51-40-05-0G-0- AND SRM 53-00-53-2R-5 REPAIR-5 OK TO TREAT AND PRIME;FABRICATED; LOCATED AND DRILLED AFT FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 847 LBL 20 AND SPLICER ANGLE AT BS 727E+10 LBL 20 MADE FROM EXTRUSION BAC1496-377 #7075T62 LOT#1484618-1 IAW SRM 51-40-05-0G-0- AND SRM 53-00-53-2R-5 REPAIR-5 DWG 146A750APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804 INSTALLED NEW SPLICE REPAIR ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727E+10 LBL20 IAW SRM 53-00-53-2R-5 REPAIR 5 AND SRM 51-40-02.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 20 BS 727D+14; BS 727E+14; BS 727E+18; BS 747+2; BS 747+6; BS 747+10; BS 747+14; BS 747+18; BS 767; BS 767+3. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 20 BETWEEN BS727D+14 INCHES . THE LOWEST REMAINING THICKNESS .035' ON BLENDED AREA L=2'X W=1'XD=0.005 ORIG. MAT. THK.=.040' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2 STEP 4A FIG. 103 DETAIL D ;SRM 53-60-53-01-2 TOOL USED ID:ATS1672 ;S/N:65092939; DUE:03/2023<BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q00BLV44;[02] UPDATED MEASUREMENTS;[03] UPDATED STEPS;[04] VERIFIED PARTIAL STEPS 2-9.;[05] VERIFIED CORRECTIVE ACTION 1.
CORROSION ON AFT CARGO BAY RAIL AT RBL 13 BS 727D+5; BS 787+16. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FOR IDENTIFICATION IAW SRM 53-60-53-01-2 IDENTIFICATION 2;[02] WORK ACCOMPLISHED ON CUST SYSTEM ID: TTG8Q00BLW42 FOR CORROSION AT B/S 727D RBL 13 ; CARGO TRACK MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[03] REMOVED CORROSION ON CARGO TRACK LOCATED AT B/S 787 +16 RBL 13 ; DIMENSIONS L:3 W: 1' DEEPTH: 0.035' IAW SRM 51-10-02 PARAGRAPH 15 . <BR>EVALUATED REWORKED AREA ; REMAINING THICKNNES : 0.035'AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 DETAIL D<BR>TOOL USED MICROMETER ; ID:ATS601; DATE DUE 05/2022;[04] REMOVED CARGO TRACK LOCATED BTW B/S 767+11 TO B/S 887 RBL13 IAW SRM 51-40-02;[05] WORK ACCOMPLISHED ON CUST SYSTEM ID: TTG8Q00BLW42;[06] VERIFIED WORK WILL BE ACCOMPLISHED ON CARD TTG8Q00BLW42;[07] VERIFIED ITEMS 1 - 3 CORRECTIVE ACTIONS.;[08] FIXED MEASUREMENT TABLE
CORROSION ON AFT CARGO BAY STRINGER CLIP AT RBL 15 BS 787. / [01] ENTERED MEASUREMENTS;[02] B737-700 SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS EVALUATION.<BR>NO ALLOWABLE DAMAGE GIVEN IN SRM; REPAIR BY REPLACEMENT IAW SRM 51-10-02.<BR>REMOVED DAMAGED CLIP IAW SRM 51-40-02.;[03] VERIFIED CORRECTIVE ACTION #2;[04] LOCATED AND DRILLED NEW CLIP P/N 146A1010-27 IAW SRM 51-40-05-0G-0; OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4.;[06] INSTALLED NEW STRINGER CLIP P/N 146A1010-27; PO# 863035 IAW 51-40-02-0G-0 AND DWG. 146A1262 REV A ON ACB BS 787; RBL 15.;[07] CERTIFIED ACTION 6.;[08] VERIFIED CORRECTIVE ACTION 6.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727D+18; BS 727E+3; BS 727E+6; BS 727E+10; BS 747+3; BS 747+12; BS 747+15. / [01] SRM 53-60-53-0I-2 IDENTIFICATION AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE ARE APPLICABLE<BR><BR>REMOVED CORROSION BY BLENDING FLOOR TO SIDEWALL SUPPORT UPPER SURFACE AT MULTIPLE AREAS PER SRM 51-10-02. MAXIMUM MATERIAL LOSS L=6.8'; W=0.9'; D=0.011'. ORIGINAL THICKNESS 0.040'; REMAINING THICKNESS 0.029'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL E.<BR>GAGE: ATS1672; S/N:65092939; DUE DATE 03/2023;[02] VERIFIED CORRECTIVE ACTION 1- BLEND IS OUT OF LIMITS;[03] LOCATED AND DRILLED FLOOR TO SIDEWALL SUPPORT FROM BS 727+4 TO BS 767; RBL 21 PER SRM 51-40-05 AND DWG# 146A7500. FROM EXTRUSION BAC1496-377#7075T62 LOT #1477731-1. OK TO TREAT AND PRIME;[04] VERIFIED CORRECTIVE ACTION 3.;[05] TREATED AND PRIMED FLOOR TO SIDEWALL SUPORT SECTION PER SRM 51-20-01 AND SOPM 20-41-02;[06] VERIFIED CORRECTIVE ACTION 5.;[07] UPDATED MEASUREMENTS;[08] FABRICATED FLOOR TO SIDEWALL SUPPORT FROM BS 727+4 TO BS 767; RBL 21 PER SRM 51-40-05 AND DWG# 146A7500. FROM EXTRUSION BAC1496-377#7075T62 LOT #1477731-1.;[09] VERIFIED CORRECTIVE ACTION 8.
CORROSION ON AFT CARGO BAY STRINGER CLIP AT RBL 15 BS 767. / [01] ENTERED MEASUREMENTS;[02] B737-700 SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS EVALUATION.<BR>NO ALLOWABLE DAMAGE GIVEN IN SRM; REPAIR BY REPLACEMENT IAW SRM 51-10-02.<BR>REMOVED DAMAGED CLIP IAW SRM 51-40-02.<BR>RECEIVED A NEW CLIP PN 146A1010-27 FROM STORES REF PO 845011.<BR>LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05 AND DWG 146A1263 REV: A.<BR>OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION #2;[04] INSTALLED NEW CLIP IAW SRM 51-40-02 AND DWG 146A1263 REV: A.;[05] VERIFIED CORRECTIVE ACTION #4
CRACKED INTERCOSTAL AT B.S. 312-328; L.B.L. 47; W.L. 208.1. / [01] REMOVED INTERCOSTAL BS 312 TO BS 328 LBL 47; WL; 208.1 IAW SRM 51-40-02-0G-0 LOCATE AND DRILLED NEW INTERCOSTAL IAW 51-40-05-0G-0; AND OK TO INTALL;[02] REMOVED INTERCOSTAL BS 312 TO BS 328 LBL 47; WL; 208.1 IAW SRM 51-40-02; LOCATE AND DRILLED NEW INTERCOSTAL IAW 51-40-05-0G-0 AND OK TO INTALED;[03] CERTIFY;[04] VERIFIED CORRECTIVE ACTION 1.;[05] INTALLED NEW INTERCOSTAL BS 312 TO BS 328 LBL 47 WL 208.1 IAW SRM 51-40-02-0G-0 AND DWG # 141A5400 ID 0026 RV:-;[06] INSTALLED NEW INTERCOSTAL AT BS 312 TO BS 328 LBL 47 WL 208.1 IAW 51-40-02-0G-0 AND DWA # 141A5400 AD0026 RV:-;[07] CERTIFY;[08] VERIFIED CORRECTIVE ACTION #6
CRACKED INTERCOSTAL AT B.S. 312-328; R.B.L. 33; W.L. 208.1 / [01] REMOVED INTERCOSTAL BS 312 TO 328 RBL; 33; WL. 208.1 IAW SRM 51-40-02-0G-0 LOCATE AND DRILLED NEW INTERCOSTAL IAW 51-40-05-0G-0 ; AND OK TO INSTALL;[02] CERTIFY;[03] VERIFIED CORRECTIVE ACTION 1; OK TO INSTALL GIVEN.;[04] INSTALED NEW INTERCOSTAL BS 312 TO BS 328 RBL 33 WL 208.1 IWA SRM 51-40-02-0G-0 AND DWG # 141A5400 ID0039 REV:-;[05] VERIFIED CORRECTVE ACTION 4;[06] VERIFIED STEPS COMPLETE;[07] CERTIFY
CRACKED INTERCOSTAL AT BS 294.5-312; RBL 15; WL 208.1. INSTALLED FOD PROTECTION FROM BS277 - BS328, BL 0 - RBL 30, WL 198 IAW AMM 20-60-07-913-801. REMOVED ALL FASTENERS FROM INTERCOSTAL IAW SRM 51-40-02-0G-0. REMOVED STIFFENER AT BS 312 RBL 24 AND INTERCOSTAL AT BS 294.5-BS312 RBL 36 IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0. INSTALLED THE INTERCOSTAL IAW SRM 51-40-02 AND DRAWING 141A5400 SH. 9.
AFT CARGO DOOR; FWD SCUFF PLATE IS CRACKED / [01] WELDED 3 CRACKED AREAS ON SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N; KJ256554;[02] VERIFIED CORRECTIVE ACTION 1.;[03] PT INSPECTED WELDS IAW SOPM 20-20-02.<BR>NO CRACKS NOTED <BR>EQUIP USED: RADIOMETER ID: ATS2561-1;2;3;[04] SANDED REPAIR AREAS PER SRM 53-60-15-2R-1 PARA 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4.
FWD CARGO BAY INTERCOSTAL BS 440-460 WL 156 LBL 24 IS CRACKED / [01] REMOVED FCB INTERCOSTAL BS 440-460 LBL24 WL 156 I.A.W SRM 51-40-02-0G-0;[02] RECEIVED NEW INTERCOSTAL P/N:143A7510-9 LOT:1453381-1 AND LOCATED AND DRILLED AT FCB ON BS 440 TO 460 WL 156 LBL 24. IAW SRM 51-40-05 AND DWG: 143A7505; ID:0003 ;REV:A. REQUEST OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION ENTRY 2. OK TO INSTALL GIVEN.;[04] INSTALLED INTERCOSTAL AT FCB ON BS 440 TO 460 WL 156 LBL 24. IAW SRM 51-40-02 AND DWG: 143A7505; ID:0003 ;REV:A.;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED COMPLETE
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 400+2; BS 400+6; BS 400+10; BS 400+14; BS 420+13; BS 440+2; BS 440+6; BS 460+2; BS 460+7; BS 460+10. / [01] REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS400+2 MEASURED1.5'L X 0.8'W AND 0.0055'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS400+6 MEASURED1.5'L X 0.8'W AND 0.010'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS400+10 MEASURED1.3'L X 0.9'W AND 0.0085'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS400+14 MEASURED1.2'L X 0.6'W AND 0.007'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2[05] LOCATED AND DRILLED NEW FWD CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT AND SPLICE BS 400 TO BS 500D LBL 24 WL 156 IAW SRM 51-40-05; DWG 143A7501; DWG 143A7500 AND SRM 53-00-53-2R-5<BR><BR>MATERIAL USED BAC1496-444#7075T62;EXTRUSION;LOT#1485
CRACK ON FWD CARGO BAY INTERCOSTAL AT RBL 23 BS 400+1. / [01] REMOVED FCB INTERCOSTAL AT RBL 23 BS 400 - BS 420 I.A.W SRM 51-40-02-0G-0;[02] LOCATED AND DRLLED ON FWD CARGO BAY NEW INTERCOSTAL BS 400 TO BS 420 RBL 23 WL 156 P/N 143A7510-34 LOT#1487853-1 PO#863642/1 IAW SRM 51-40-05 AND DWG143A7505 REV:B. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION ITEM 2. OKAY TO INSTALL NEW INTERCOSTAL AT RBL 23 BS 400 - BS 420 GIVEN.;[04] INSTALLED ON FWD CARGO BAY NEW INTERCOSTAL BS 400 TO BS 420 AT RBL 23 WL 156 IAW SRM 51-40-02 AND DWG 143A7505 REV:B.;[05] SRM 53-00-53-1A-2 IA IS APPLICABLE; NO ALLOWABLE DAMAGE PER SRM; PART TO BE REPLACED IAW SRM 51-10-02 PAR.9<BR><BR>LOCATED AND DRLLED ON FWD CARGO BAY NEW INTERCOSTAL BS 400 TO BS 420 RBL 23 WL 156 P/N 143A7510-34 LOT#1487853-1 PO#863642/1 IAW SRM 51-40-05 AND DWG143A7505 REV:B. OK TO INSTALL;[06] UPDATED MEASUREMENTS;[07] VERIFIED CORRECTIVE ACTION ITEMS 4 AND 5. INSTALLATION OF INTERCOSTAL AND SRM APPLICABILITY.
R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IS CRACKED / [01] REMOVED AND REPLACE R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IAW SRM 51-40-02-OG-0 STEP 4.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500A+12; BS 500A+14; BS 500A+18; BS 500B+2; BS 500B+6; BS 500B+18; BS 500B+19; BS 500C+2; BS 500C+5; BS 500C+14. / [01] REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS500A+12 MEASURED1.4'L X 1.0'W AND 0.010'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS500B+18 MEASURED2.5'L X 1.5'W AND 0.0045'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS500B+19 MEASURED1.8'L X 0.8'W AND 0.0065'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2[05] NEW FCB LH FLOOR TO SIDEWALL SUPPORT BS 400- BS 500D WILL BE FABRICATED ON CUSTOMER CARD: TTG8Q00BL4G9;[06] VERIFIED ITEMS 4;5 CORRECTIVE ACTIONS.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 460+14; BS 480+6; BS 480+10; BS 500+5; BS 500+10; BS 500+14; BS 500+18; BS 500A+2; BS 500A+6; BS 500A+10. / [01] REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS480+6 MEASURED1.7'L X 0.9'W AND 0.010'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS480+10 MEASURED1.3'L X 0.9'W AND 0.0065'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT AT BS500A+2 MEASURED1.8'L X 0.8'W AND 0.005'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2[05] NEW FCB LH FLOOR TO SIDEWALL SUPPORT BS 400- BS 500D WILL BE FABRICATED ON CUSTOMER CARD: TTG8Q00BL4G9;[06] VERIFIED ITEM 5 CORRECTIVE ACTIONS.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2; BS 500A+6; BS 500A+10; BS 500A+14; BS 500A+18; BS 500B+6. / [01] SRM 53-00-53-1A-2 IS APPLICABLE<BR><BR>REMOVED CORROSION IN 6EA LOCATIONS ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT RBL24 PER SRM 51-10-02-0G-0 IN AREA OF:<BR><BR>BS500A+02' 1.5'X.80'X.007'<BR>BS500A+06' 1.6'X1.1'X.006'<BR>BS500A+10' 1.4'X1.1'X.003'<BR>BS500A+14' 1.6'X.80'X.002'<BR>BS500A+18' 1.3'X.80'X.003'<BR><BR>BS500B+6' 1.5'X.80'X.003'<BR><BR>FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS500A+2' AND BS500A+6' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2<BR><BR>DEPTH GAUGE<BR>ATS401<BR>S/N UNKNOWN<BR>10/2022;[02] VERIFIED REWORK OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] FABRICATED NEW FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT RBL24 BS 500A - 500D USING BAC1496-444 LOT#1485395-1 AND LOCATED AND DRILLED HOLES IAW SRM 51-40-05-0G-0 AND DWG 143A7500 REV:A<BR><BR>OK TO APPLY CHEMICAL CONVERSION COATING AND BMS10-11 PRIMER;[04] VERIFIED ITEM 3 CORRECTIVE ACTIONS. OK TO APPLY CHEMICAL CONVERSION COATING AND PRIMER;[05] APPLIED CHEMICALCONVERSION COATING AND BMS 10-11 PRIMER TO FABRICATED FCB FLOOR TO SIDEWALL SUPPORT RBL24 BS500A-500D IAW AMM 51-21-72-370-804 AND AMM 51-00-58/201;[06] INSTALLED NUTPLATES ON FABRICATED FCB FLOOR TO SIDEWALL SUPPORT RBL24 BS500A-500D IAW SRM 51-40-02-0G-0 AND DWG 143A7500 REV:A;[07] VERIFIED CORRECTIVE ACTIONS 5 AND 6.
CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 500+2; BS 500+6; BS 500+10; BS 500+14. / [01] NO ALLOWAVLE DAMAGE PER SRM. REPAIR BY REPLACEMENT OF PART;[02] LOCATED AND DRILLED NEW FWD CARGO BAY AFT DOOR SHIELD P/N 143A8126-31 AT BS 500 TO BS 500A ; RBL 24 IAW SRM 51-40-05-0G-0 AND DWG 143A0080; ID: 0010; REV:A;[03] VERIFIED CORRETIVE ACTIONS 1 AND 2;[04] ADDED PARTS INSTALLED REQUIREMENT;[05] VERIFIED COMPLETE
CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 24 BS 420+3. / [01] NO ALLOWABLE DAMAGE PER SRM. REPAIR BY REPLACEMENT OF PART;[02] RECEIVED NEW SHIELD<BR><BR>ITEM # : 143A8126U21ATSMRO<BR>PO# : 855387/1;[03] LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0 AND DWG 143A8126 ID:0011 REV:A;[04] VERIFIED CORRECTIVE ACTION 3.;[05] UPDATED MEASURMENTS;[06] TASK CARD COMPLETE;[07] VERIFIED TABLE MEASUREMENTS. TASK CARD COMPLETE.
CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 45 BS 500C+11; BS 500D; BS 500D+18. / [01] COMPLETED STEPS 1 - 3;[02] UPDATED MEASUREMENTS;[03] COMPLETED STEPS 1 - 3;[04] PARTIAL UPDATE TO STEP 4;[05] PARTIAL UPDATE TO STEP 4;[06] COMPLETED STEP 4;[07] PARTIAL STEP 4;[08] COMPLETED STEP 4
UPON COMPLETION OF CCN:5241-I-14079-NG; FOUND 1 INCH CRACK ON FORWARD SERVICE DOOR COMMON TO THE #5 BEAM. AREA MARKED / [01] UPDATED PART REMOVAL.;[02] UPDATED PARTS;[03] RECEIVED SERVICEABLE DOOR FROM OSS WO# 548552;[04] CORRECTION TO ITEM 3; FSD REPAIRED ON CUSTOMER RO# P2758269-1 SEE ATTACHMENT.;[05] VERIFIED CORRECTIVE ACTION 3 AND 4
#3 SLAT NOSE SKIN IS CRACKED AT ACTUATOR ATTACH RIB AT FASTENER. MARKED / [01] REMOVED SLAT COVE PANELS 523CB; 523DB; 523EB IAW SOPM 20-50-01.;[02] REMOVED SLAT FLEX SKIN IAW SRM 57-4201 2R-8.;[03] VALIDATED APPLICABILITY OF SRM 57-42-01-2R-8.;[04] REMOVED FASTENERS AS REQUIRED AND CUT OUT DAMAGED AREA OF SLAT NOSE SKIN IAW SRM 57-42-01-2R-8 PARA.4.;[05] VERIFIED CORRECTIVE ACTIONS 3 AND 4;[06] ACCOMPLISHED HFEC INSPECTION IAW NDTM D6-37239 PART 6; 51-00-00 PROC 16. SRM 51-42-01-2R-8 REPAIR 8 STEP 4.C. NO DAMAGE FOUND. TOOL I.D. IS000450 500D; ATS2407 MINIMITE;[07] FABRICATED REAIR DOUBLER FROM 7075-T62 CLAD; .071'; LOT# 1478276-1. REPAIR FILLER FROM 7075-T62 CLAD; .063'; LOT# 1418646-2. APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS AND BARE AREAS OF SLAT NOSE SKIN. INSTALLED COUNTER SINK REAIR WASHERS TO SLAT NOSE SKIN AS REQUIRED. WORK DONE IAW SRM 57-42-012R-8 PARA. 4. F.
FORWARD SERVICE DOOR GIRT BAR BRACKET LOOSE. / [01] ADJUSTED GIRT BAR BRACKETS PER S.I.P.
CENTER WHEEL WELL PANEL 193D HAS MULTIPLE ELONGATED FASTENER HOLES. ; / [01] REMOVED AND REPLACED CENTER WHEEL WELL PANEL 193D<BR>I/A/W AMM 53-51-21
LEFT A/C BAY; BS 663; LBL 15.0 TO 19.0; WL 50 TO 67; SEVERAL CRACKS IN BULKHEAD WED SKIN ABOVE EXH. AIR DUCT CUTOUT AROUND ATTACH FASTENERS. BONDED REPAIR PLIES. IAW SRM 51-70-04-2R-10 PAR4D-G REV 74. RESTORED FINISHES IAW SRM 57-10-10-2R-2 REPAIR 2.
FUEL PANEL 532JB HAS FRETTING CORROSION AT RING MATTING SURFACE. REMOVED DAMAGE ALLOWABLE .020'' REMOVED .004'' FOUND TO BE IN LIMITS. PERFORMED FLAP PEEN IAW SRM 57-20-01-2R-1 REPAIR 1 PARAGRAPH 4.H. APPLIED ALODINE TO REWORK AREA IAW SRM 57-20-01-2R-1 PARAGRAPH 4.J.
FOUND CRACK IN L/H A/C BAY STA 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 40 ; / [01] REMOVED STIFFENER ON FWD SIDE OF STA 663 LBL 40 TO FOM IAW SRM 51-40-02-0G-0; [02] REMOVED U-CHANNEL ON FWD SIDE STA 663 LBL 43-65 TO FOM IAW SRM 51-40-02-0G-0; [03] CUT AND REMOVED DAMAGED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5; [04] PERFORMED DVI OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5; [05] RECIEVED -1 REPLACEMENT ANGLE FROM BACKSHOP ON WORK ORDER 42971-5000-0001. RECIEVED -2 SPLICE ANGLE FROM BACKSHOP ON WORK ORDER 42971-5000-0002; [06] VERIFIED STEP 4.; [07] PERFORMED NDT IAW B737 NDT PT.6; 51-00-00 PROC. 16. NO DEFECTS NOTED . TOOL# 36303 CAL DUE 13APR22.; [08] VERIFIED ITEMS 3 AND 5; [09] FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5; [10] VERIFIED ITEM 9.<BR>OK TO TREAT AND PRIME.; [11] TREATED AND PRIMED REPAIR PARTS AND CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5; [12] VERIFIED ITEM 11.<BR>OK TO INSTALL REPAIR PARTS.
FOUND CRACK IN L/H A/C BAY STA 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 40. REMOVED STIFFENER ON FWD SIDE OF STA 663 LBL 40 TO FOM IAW SRM 51-40-02-0G-0. CUT AND REMOVED DAMAGED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED NDT IAW NDT PT.6 51-00-00 PROC 16. NO DEFECTS NOTED . FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED AND PRIMED REPAIR PARTS AND CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. STIFFENER REMOVED ON STEPS 1 AND 2 INSTALLED REPAIR PARTS U CHANNEL AND STIFFENER IAW SRM 57-10-10-2R-5 REPAIR 5.
FUEL PANEL 532QB HAS FRETTING CORROSION AT RING MATTING SURFACE. REMOVED DAMAGE AND EVALUATED MATERIAL LOSS TO BE .007'; ORIG .275'; REMAINING .268' IAW SRM 57-20-01-2R-1. ROTO PEENED FUEL PANEL IAW SRM 57-20-01-2R-1 4H. RESTORED FINISH ON FUEL PANEL 532QB IAW SRM 57-20-01-2R-1. 4J-K.
NR 3 FLAP TRACK CANOE FAIRING CRACKED ON AFT INBD EDGE WHERE IT MEETS TAIL CONE. REMOVED FLAP TRACK AFT & TAILCONE FAIRING IAW AMM 27-51-18-000-802. FOUND CRACK ON AFT EDGE. REPAIRABLE IAW SRM 57-53-70-2R-4 REV. 74 TABLE 201. REMOVED DAMAGE & PREPPED AREA FOR REPAIR IAW SRM 51-70-04-2R-10REV. 74 PARA. 4 AND SRM 51-70-04-2R-0 REV. 74 PARA. 4 APPLIED AND BONDED REPAIR PLIES TO AREA AND CURED AT 200F FOR 3.75HRS THERMOMETER #30347 DUE 4/29/22 BOND IS SATISFACTORY/ NO DEFECTS IAW SRM 51-70-04-2R-10 REV. 74 PARA. 4 AND SRM 51-70-04-2R-0 REV. 74 PARA. 4 FIBERGLASS (A10273) RESIN (A54377) RESIN SWEPT AREA TO FILL IN IRREGULARITIES FOR AERODYNAMIC SMOOTHNESS IAW SRM 51-70-08-0G-0 AND CURED FOR 1HR @ 150F THERMOMETER #30347 DUE 4/29/22 SEALER RESIN (A71242) REMOVED AND RE-INSTALLED 5EA. NUTPLATES TO FACILITATE MAINTENANCE IAW SRM 51-40-02-0G-0 REV. 74 PARA. 4. SOLID SHANK RIVETS (A88275) *REQUESTING OKAY TO RESTORE FINISH TO REPAIR AREA* STEP 3 OK. OK TO PAINT RESTORED FINISH TO REPAIR AREA ON #3 FLAP TRACK CANOE FAIRING IAW AMM 51-21-99-300-801 REV. 75 PRIMER (A35225) PAINT (A74783) STEP 5 OK OK TO INSTALL #3 AFT FLAP TRACK FAIRING INSTALLED #3 AFT SUPPORT FAIRING IAW B737 AMM 27-51-18-400-802 STEPS 5.G.1 THROUGH 5.G.2.
FUEL PANEL 532QB HAS FRETTING CORROSION AT RING MATTING SURFACE ; / [01] REMOVED DAMAGE AND EVALUATED MATERIAL LOSS TO BE .007'; ORIG .275'; REMAINING .268' IAW SRM 57-20-01-2R-1 TOOL ID 41391 CAL DUE 09-08-22; [02] VERIFIED ITEM 1; [03] ROTO PEENED FUEL PANEL IAW SRM 57-20-01-2R-1 4H.; [04] VERIFIED ITEM 3; [05] FOR ABOVE STEP 1 USED 10X MAG TO VERIFY DAMAGE REMOVAL IAW SRM 57-20-01-2R-1.<BR>FOR ABOVE STEP 3 USED AAR TOOL 7995 CAL DUE 04-09-22.; [06] RESTORED FINISH ON FUEL PANEL 532QB IAW SRM 57-20-01-2R-1. 4J-K.; [07] OK TO TREAT<BR><BR>VERIFIED STEP 6 <BR><BR>AUDIT C/W
FUEL PANEL 532CB HAS FRETTING CORROSION AT RING MATTING SURFACE. REMOVED DAMAGE ALLOWABLE .020'' REMOVED .012'' FOUND TO BE IN LIMITS. PERFORMED FLAP PEEN IAW SRM 57-20-01-2R-1 REPAIR 1 PARAGRAPH 4.H. APPLIED ALODINE TO REWORK AREA IAW SRM 57-20-01-2R-1 PARAGRAPH 4.J.
FUEL PANEL 532BB HAS FRETTING CORROSION AT RING MATTING SURFACE. REMOVED DAMAGE ON FUEL PANEL 532BB LOSS .006' MAX ALLOWED .020' WITHIN LIMITS IAW SRM 57-20-01-2R-1. ROTO PEENED FUEL PANEL IAW SRM 57-20-01-2R-1 4H. RESTORED FINISH ON FUEL PANEL 532BB IAW SRM 57-20-01-2R-1.
COCKPIT EMERGENCY DOME LIGHT INOP ; / FOUND LOOSE CONTACT OF WIRE W2114 - A-AG AT GROUNDING BLOCK GB261. RESEATED CONTACT REF SWPM 20-90-15. PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF AMM 33-51-00. OPS CHECK NORMAL.
2 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST. / REMOVED AND REPLACED 2 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1669 AND M1672 PER AMM 33-51-06 AND ENG DWG 33500005
EMERG. EXT SIGN COVER FELL OFF. OVERWING EXIT ON FO'S SIDE / REINSTALLED R/H OVERWING EMERGENCY EXIT SIGN COVER PER SIP
EXIT/SALIDA PLASTIC SIGN COVER FOR OVERWING EXIT ROW 12 IS BROKEN AND WILL NOT STAY ATTACHED. R & R, PER AMM 33-51-01 (COVER).
LT WING EMERGENCY EXIT LIGHT LENS BROKEN. R & R LT WING EMERGENCY EXIT LENS, IAW AMM 33-51-11.
LT AFT EMERGENCY LIGHT C/B POPPED. REMOVED AND REPLACED AFT LEFT EMERGENCY CHARGER AND BATTERY, PER AMM33-51-06.
FOUND R AFT LIGHTING EMERENCY LIGHT CB POPPED ON PREFLIGHT / RESET RIGHT AFT LIGHTING EMERGENCY CHARGER & OPS CHECKED NORMAL PER AMM 33-51-00
LT PAX CABIN EMERGENCY EXIT LIGHTS (OVER WING INSIDE & OUSIDE) INOP. REPLACED LT OVER WING EMERGENCY EXIT LIGHTS BATTERY PACK REF AMM 33-511-06.
CAPT SIDE OVERWING EXIT LOWER 'EXIT' SIGN FELL OFF. RE-INSTALLED SIGN IAW SIP
DURING INSTALLATION THE FIRST OBSERVER SEAT FOUND HINGE CRACKET AT FIRST OBSERVER SEAT SUPPORT / REMOVED AND REPLACED FIRST OBSERVER SEAT SUPPORT ASSY AS PER B737-7 SRM 51-40-02-0G-0
AFT CARGO DOOR AFT CORNER SCUFF PLATE CRACKED ON OUTER SIDE / REPAIRED AFT CARGO DOOR - AFT ORNER SCUFF PLATE IRW EA # 1-A53-2076 REV 11 BY OUTSIDE VENDOR J.L WELDING INC W.O #15891
***CORROSION *** FRETTING - BS 663 RT LOWER KEEL BEAM WL 148.5 WTB FAIRING SUPPORT BRACKET. [DOT 124-041] / REPLACED WTB FAIRING SUPPORT @ BS663 RT LOWER KEEL BEAM WL 148.5 AS PER B737-700 SRM 51-40-02-0G-0
CORROSION FOUND AFT CARGO 'T' STRAP STA 887 LBL 9 TO RBL 21 AND WL 153.8 / REMOVED CORRODED 'T' STRAP AND INSTALLED NEW STRAP; AFT CARGO COMPARTMENT STA 887; PER REF DRAWING #146A7500 AND MPL 146A7500-16
FWD CARGO COMPARTMENT AFT BULKHEAD CENTER BILGE AREA FLANGE SUPPORT ANGLE AT STA 5OOD SHOWS HAVING CORROSION. DOT 82-041. / REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT STA 500D AT FWD CARGO COMPARTMENT AFT BULKHEAD (FROM LBL 25' TO RBL 25') IRW B737-700 SRM 51-40-02-0G-0 / 51-40-05-0G-0 / 53-00-53-1A-2
R/H HORIZONTAL STABILIZER INSPAR RIB ASSY 4 CRACKED AT STIFFENER #4 / INSTALLED REPAIR AT HORIZONTAL STABILIZER INSPAR RIB LOWER CHORD R/H HORIZONTAL RIB #4 STIFFENER #4; PER REF B737 SRM 55-10-09-2R-5 REP 5
R/H HORIZONTAL STABILIZER INSPAR RIB ASSY 4 CRACKED AT STIFFENER #2 / INSTALLED REPAIR AT LOWER CHORD RIB #4 STIFFENER #2 PER REF 737 SRM 55-10-09-2R-5 REP 5
CORROSION FOUND AFT CARGO RH Z CHANNEL RBL 21 FROM STA 727 TO STA 767;WL 153.8 / REMOVED CORROSION ON R/H 'Z' CHANNEL FROM STA 727 TO STA 767 WL 153.8 FOUND EXFOLIATOR CORROSION OUT OF LIMITS IAW B737 SRM 51-10-00-0G-0 AND SRM 53-00-1A-2; FABRICATED; LOCATED AND DRILLED NEW 'Z' CHANNEL IAW B737-700 SRM 51-40-05-0G-0; TREATED AND PRIMED AND INSTALLED NEW Z CHANNEL AT AFT CARGO COMP; R/H BETWEEN STA 727 TO STA 767 WL 153.8
FWD CARGO COMPARTMENT AFT BULKHEAD RT CIRCUNFERENTIAL FLANGE SUPPORT ANGLE AT STA 5OOD SHOWS HAVING CORROSION AT THE I/B END. DOT 82-040. / REMOVED CIRCUNFERENTIAL FLANGE FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW CIRCUNFERENTIAL FLANGE AS REQUIRED. REF B737 SRM 51-40-02-0G-0
CORROSION - AFT CARGO RT SIDEWALL BS 907 S24-R AT 2 PLACES AROUND FASTENER HOLES AS MARKED. [DOT 124-037] / REMOVED AND REPLACED CORRORED FRAME SPLICE AT STA 907 AND STRINGER 24 R/H AFT CARGO R/H SIDEWALL; MATERIAL USED 7075-0; .056' HEAT TREATED TO 7075 T6; PER REF DRAWING 147A9409 AND BAC 5602 AND SRM 51-40-02-0G-0
***CORROSION*** AFT CARGO BS 767+3 FLOOR SUPPORT STRAP DOT 124-040.RBL 21' TO LBL 21' AND WL 153.8 / FOUND EXFOLIATION CORROSION ON FLOOR SUPPORT STRAP OUT OF LIMITS AT STA 767 +3; REMOVED AND REPLACED STRAP AS PER REF B737-700 SRM 51-40-02-0G-0.
FWD CARGO COMPARTMENT AFT BULKHEAD LT CIRCUNFERENTIAL FLANGE SUPPORT ANGLE AT STA 5OOD SHOWS HAVING CORROSION AT THE I/B END. DOT 82-042. / REMOVED AND REPLACED AFT BULKHEAD CIRCUNFERENTIAL FLANGE SUPPORT ANGLE (OR RAIL) AT FWD CARGO COMPARTMENT STA 500D LEFT SIDE IRW B737-700 SRM 51-40-02-0G-0 / 51-40-05-0G-0 / 53-00-53-1A-2 AND DRWG #143A9481
AFT CARGO FWD BULKHEAD CENTER LOWER PANEL SUPPORT CHANNEL BRACKET IS CRACKED. [DOT 124-032] / REMOVED CRACK SUPPORT CHANNEL AND INSTALLED NEW BRACKET; AFT CARGO COMPARTMENT FWD BULKHEAD; PER REF 737 SRM 51-40-02-0G-0 AND DRAWING #144A9401
CORROSION FOUND AFT CARGO LH Z CHANNEL LBL 21 FROM STA 727 TO STA 847. / REMOVED AND REPLACED L/H 'Z' CHANNEL SECTION FROM STA 757 SPLICE REPAIR PER SRM 53-00-53-2R-5 TO STA 847 PER REF SRM 51-40-02-0G-0 AND DRAWING # 146A7500
CORROSION FOUND ON RH SHIELD SUPPORT AT RBL 21 STA 767 TO 787 + 10. / REMOVED CORRODED SHIELD SUPPORT ON AFT CARGO BETWEEN STA 767 AND STA 787+10; AND INSTALLED NEW SHIELD; PER REF B737 SRM 51-40-02-0G-0 AND DRAWING #146A8127
***CORROSION*** FWD CARGO STA 420 TO STA 440 STR25R RBL24 SHIELD SUPPORT HAS CORROSION / REMOVED AND REPLACED SHIELD STA 420-440 STR25R; RBL24 AT FWD CARGO REF B737-7 SRM 51-40-02-0G-0 & DRAWING # 143A0080
***CORROSION*** FWD CARGO STA 500A TO STA 500D STR25R RBL24 Z-CHANNEL HAS CORROSION / REMOVED AND REPLACED Z CHANNEL (SIDE PLATE ASSEMBLY) AT FWD CARGO R/H FROM STA 500A TO STA 500D IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING NO. 143A7500; Z CHANNEL FABRICATED ON DEFECT #W144177.
LT HORIZONTAL STABILIZER L/E NUMBER 3 RIB IS CRACKED AT THE RIVET HOLE. DOT 82-034. / REMOVED AND REPLACED DAMAGED RIB (P/N 186A1303-1) STA: 95.96 ON LT HORIZ STAB L/E PANEL; RIB #3 PER REF B737 SRM 51-40-02-0G-0 AND #PL186A001.
FWD CARGO COMPARTMENT STA 500D STR 21L APROX WL 178 GUSSET CRACKED / REMOVED OLD CRACKED GUSSET AND REPLACED WITH NEW GUSSET AT FWD CARGO COMP STA 500D STRINGER 21L AND RESEALED AS REQUIRED REF # B737 SRM 51-40-02-0G-0 AND 51-31-00-201
***CORROSION*** FWD CARGO STA 400 TO STA 500D STR25L LBL24 Z-CHANNEL HAS CORROSION / REMOVED; REPLACED AND INSTALLED NEW SIDE PLATE 'Z' CHANNEL AT FWD CARGO COMPARTMENT IN REF B737-700 SRM 51-40-02-0G-0 AND DRAWING #143A7501
***CORROSION*** FWD CARGO STA 440 TO STA 480 +12 STR25R RBL24 LWR WEB CARGO DOOR HAS CORROSION / REMOVED AND REPLACED FWD CARGO DOOR LOWER WEB BETWEEN STA 440 & STA 492 REF B737-700 DWG 143A8120_AND DWG 143A8330.
AS PER CUSTOMER REQUEST THERE IS A DENT AT STA 257 AND LBL14 AT THE FLIGHT DECK FLOOR THAT NEEDS TO BE REPAIRED. DOT 82-036. / REPAIRED FLIGHT DECK FLOOR WEB AT BS260 IRW EA #1-A53-33179 REV IR
RIGHT SIDE FWD OF VAPOR BARRIER WEB HORIZONTAL ANGLE ANGLE CRACKED APPROX. STA.663; RBL 12 / REMOVED AND REPLACED RT SIDE VAPOR BARRIER WEB ANGLE AT APPROX STA 663 RBL 12 IAW 737-700 SRM 57-10-2R-5
T HORIZONTAL STABILIZER L/E RIB NUMBER 9 IS RACKED BY THE FASTENER HOLE AS MARKED. DOT 2-035. / REMOVED AND REPLACED DAMAGED RIB ON R/H HORIZONTAL STABILIZER L/E RIB #9 STA 151.75' (P/N 186A1401-2) PER REF B737 SRM 51-40-02-0G-0 AND PL186A1308.
AFT CARGO COMPT. FWD SCUFF PLATE CORNER CRACKED / WELDED AFT CARGO COMPARTMENT FWD SCUFF PLATE CORNER BY SL WELDING W/O 15888; P.O. 412709
***CORROSION*** FWD CARGO STA 400 TO STA 420 STR25R RBL24 Z-CHANNEL HAS CORROSION / REMOVED AND REPLACED 'Z' CHANNEL SECTION AT FWD CARGO BETWEEN STA 396 ABD STA 420 RBL 24 IRW 737-700 SRM 51-40-02-0G-0 AND BOEING DWG# 143A7500. 'Z' CHANNEL SECTIOIN WAS FABRICATED ON DEFECT NO. W144180
***CORROSION*** FWD CARGO STA 480+12 TO STA 500A STR25R RBL24 SHIELD SUPPORT HAS CORROSION / REMOVED AND REPLACED SHIELD SUPPORT FWD CARGO STA 480 + 12' TO STA 500A STR25R RBL 24 IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING NO. 143A8126 (PART WAS FABRICATED ON W144178) AND DRAWING # 143A0080. CA 18533 4/25/20
FWD CARGO COMPARTMENT STA 500D STR19L APROX WL 190 GUSSET CRACKED / REMOVED OLD CRACKED GUSSET AND REPLACED WITH NEW GUSSET AT FWD CARGO COMP STA 500D STA19L WL APPROX 190 RESEALED REF 737 SRM 51-40-02-0G-0 AND 51-31-00-0G-0 ALSO SRM 51-20-01-1A-1
FWD CARGO COMPARTMENT STA 500C STR25L LBL 25 ANGULAR CRACKED AT LWR FASTENER HOLE / REMOVED AND REPLACED CRACK CLIP ON FWD CARGO COMPARTMENT STA 500C STRINGER 25L PER REF DRAWING #143A7505 AND SRM 51-40-02-0G-0
FWD CARGO COMPARTMENT STA 500D STR19R APROX WL 190 GUSSET CRACKED / REMOVED OLD CRACKED GUSSET AND REPLACED WITH NEW GUSSET AT STA 500D STR19R AS REQUIRED ALSO RESEALED AREA REF # B737 SRM 51-10-02-0G-0 AND SRM 51-31-00-201.
PASSENGER CABIN SEAT TRACK AT STA 520 AND LBL 45.75 THERE IS A SPOT WORN ON UPPER TOP CROWN. DOT 82-028. / REPAIRED SEAT TRACK @ PASSENGER CABIN @ STA 520 & LBL45.75 AS PER B737-700 SRM 53-00-52-22-4
PASSENGER CABIN LH SIDE SEAT TRACK AT STA 520 AND LBL 24.75 THERE IS A SPOT OF THE UPPER CROWN TOP WORN. DOT 82-027. / INSTALLED SEAT REPAIR PASSENGER CABIN BETWEEN STA 500C AND STA 520 LBL 24.75 PER REF 737 SRM 53-00-52-2R-4 / EA # 1-A53-11779 REV1.
LT HORIZONTAL STABILIZER PANEL 333AB RED THIN RUBBER SEAL ATTACHED TO THIN METAL ANGLE IS DEBONDED DOT 124-023 / REMOVED AND REPLACED LT HORIZONTAL STAB PANEL 333AB (2EA) SEAL ASSY IN REF TO BOEING SRM 51-40-02-0G-0
CRACK INDICATION FOUND AT MAIN CABIN STA 663 LBL31 OF HORIZONTAL PRESSURE DECK WEB.APPROX LENGTH OF CRACK:1'. / INSTALLED REPAIR AT MAIN CABIN STA 663 HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663.75AND STA 675 LBL 30 AND LBL 60 IRW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203.
CRACK INDICATION FOUND AT MAIN CABIN STA 663 RBL42 OF HORIZONTAL PRESSURE DECK WEB.APPROX LENGTH OF CRACK:0.75'. / INSTALLED CATEGORY A REPAIR AT MAIN CABIN - HORIZONTAL PRESSURE DECK WEB STA 663 RBL 42 IRW B737-700 SRM 53-40-51-2R-2 REPAIR 2
WING CENTER SECTION REAR SPAR VAPOR BARRIER CRACKED STA.663.75; RBL 30'; WL 170 / REPAIRED DAMAGE AQREA AT REAR SPAR VAPOR BARRIER AS PER BOEING 737 SRM 51-70-04-2R-10 REPAIR 10 MATERIAL USED HCS2410-030 P/O 1150387 PWS EY3804AB P/O 1675204.
R/H HORIZONTAL STABILIZER INSPAR RIB ASSY 4 CRACKED AT STIFFENER #3 / REPAIRED R/H HORIZONTAL STAB. INPAIR #4 AT STIFFENER #3 AS PER REF B737-700 SRM 55-10-09-2R-4
CABIN FLOOR PANEL 231XF UPPER SURFACE HAS PEELED FIBERS. [DOT 124-006] / REPLACED FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-0 CP 18533 4/16/20
CABIN FLOOR PANEL 241AF UPPER SURFACE HAS PEELED FIBERS. [DOT 124-007] / REPLACED FLOOR PANEL 241AF AT MAIN CABIN IAW B737-700 SRM 53-00-50-2R-0
RIGHT EMERGENCY EXIT HATCH CUTOUT FWD LOWER CORNER HAS CORROSION SPOTS. MARKED 29-10 /
SUPPLEMENTAL INFORMATION: RIGHT EMERGENCY EXIT HATCH CUTOUT FWD LOWER CORNER HAS CORROSION SPOTS. MARKED 29-10 / CLEANED AREA TREATED + PRIMED AS REQUIRED AT R/H EMERGENCY EXIT CUTOUT FWD LOER CORNER DAMAGE NOTED PAINT DAMAGE ONLY REF B737 SRM 51-20-01-0G-0.
RIGHT WING TO BODY FAIRING 191AR VERTICAL SUPPORT FRAME CRACKED AT STA 500. / REMOVED AND REPLACED RIGHT WING TO BODY 191AR VERTICAL SUPPORT FRAME AT STA 500 PER SRM 51-40-02.
L/H WING OUTBOARD AFT FLAP INBOARD AFT LOWER SKIN CORNER DELAMINATED. / R&R L/H AFT FLAP ASSEMBLY PER AMM.
L1 DOOR SLIDE FELL OUT. REINSTALLED SLIDE PER MT.
EMERGENCY EXIT LIGHT COVER BROKEN ON R/H SIDE EMERGENCY EXIT DOOR. / R&R LIGHT COVER IAW AMM.
FORWARD GALLEY FLASHLIGHT RETENTION STRAP BROKEN. INSTALLED RETENTION STRAP PER AMM.
AIR TURNBACK, ON CLIMBOUT FIRST OFFICER'S R1 WINDOW ARCED THEN CRACKED. R&R R1 WINDOW PER AMM.
LT.WING-FIXED UPPER TRAILING EDGE CLOSE OUT PANEL BETWEEN #5 FLT SPOILER AND INBD GROUND SPOILER-HAS BULB SEAL ATTACH BRACKET CRACKED;UNDERNEATH PANEL. / REMOVED AND REPLACED PER AMM. 20-50-11
LT MAIN LANDING MIDDLE GEAR DOOR CRACKED AT STIFFENER. REPAIRED DOOR IAW AMM.
R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
FLIGHT DECK " EMERGENCY LIGHT" IN CEILING INOP. INSTALLED LAMP IAW AMM.
DURING RE-INSTALLATION OF LEADING EDGE SLAT COVE PANEL 623DB FOUND CRACKED AT LOWER I/B FASTENER HOLE / REPLACED R/H L/E SLAT #6 COVE PANEL 623DB IAW BOEING DWG 114A5030 REV B P/N 114A8131-8
AFT PIT FLOOR LT Z-ANGLE CORRODED BETWEEN BS 727D TO BS 792, LBL 20. R&R Z-ANGLE IAW SRM.
FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED AT BS 328, LBL 46. R&R INTERCOSTAL IAW DWG AND SRM.
LH WING LOWER INBOARD FIXED TRAILING EDGE PANEL 551GB; UPPER SURFACE SEAL RETAINER BRACKET; OUTBOARD HOLE IS WORN AND CRACKED. / REMOVED AND REPLACED NEW SEAL RETAINER BRACKET TO L/H WING LOWER INBOARD FIXED TRAILING PANEL 551GB IAW B737-700 DWG 115A2714 REV:-; SRM 51-40-02-0G-0 ATAG# WN3775
AFT CARGO DOOR CUT OUT LOWER SILL AFT CORNER SCUFF PLATE CASTING CRACKED ALONG BULLNOSE. REPAIRED SCUFF PLATE IAW EA.
EMERGENCY LIGHT CHECK FLIGHT DECK CEILING LIGHT INOP. RELAMPED LIGHT IAW AMM & SIP.
RIGHT WING #6 L/E SLAT; NOSE SKIN AT ACTUATOR RIBS; CRACK ADJACENT TO OTBD - CTR FASTENER HOLE; MRK'D. / REPAIRED R/H WING; #6 L/E SLAT NOSE SKIN IAW B737 SRM 57-42-01-212-8 ALL DAMAGE REMOVED VERIFIED WITH HFEC
LT LOWER FUSELAGE EMERGENCY LIGHT INOP. R&R POWER SUPPLY IAW AMM.
EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1675. R & R THE BATTERY PACK IAW MM.
EXTERNAL POWER DOOR CUTOUT AFT LOWER EDGE CRACKED. REPAIRED CUTOUT PER SRM.
EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1672. R & R THE BATTERY PACK IAW MM.
EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1670. R & R THE BATTERY PACK IAW MM.
EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1673. R & R THE BATTERY PACK IAW MM.
EMERGENCY LIGHTING BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1674. R&R BATTERY PACK PER MM.
SUPPLEMENTAL INFORMATION: RMLG WHEEL WELL FWD BULKHEAD OUTBOARD STIFFENER UPPER PANEL SUPPORT CLIP IS BROKEN / R & R STIFFENER PER SRM 51-10-02 & SRM 51-40-02
SUPPLEMENTAL INFORMATION: RIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R RIGHT HORIZ STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.
L/H WING FLAP SEAL BRACKET UNDER PNL 551 GB IS CRACKED / R&R BRACKET AS PER SRM 51-40-02
FORWARD EMERGENCY FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW SIP.
L2 DOOR EXIT SIGN INOPERTIVE. REPLACED THE LAMPS IAW AMM.
INFLIGHT SHUTDOWN, RT FUEL QUANTITY ERRATIC. FOUND FAULT CODE 28-41208, AS CURRENT FAULT AND ON PREVIOUS 20 + LEGS. R & R NR 2 TANK COMPARTMENT PROBE IAW AMM.
L1 DOOR CUTOUT LOWER INBD CHORD CRACKED AT BS 312. R & R CHORD IAW SRM AND DWG.
FORWARD CARGO PIT INTERCOSTAL CLIP CRACKED AT BS 500D, RBL 6. R & R CLIP IAW SRM AND DWG.
FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.
FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.
FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.
FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.
FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.
FORWARD WET AREA FLOORBEAM CORRODED AT BS 285, BETWEEN BL 0 TO LBL 7. REPAIRED THE FLOORBEAM IAW EA.
R2 DOOR CUTOUT LOWER INNER CHORD CORRODED AT BS 986.5. R & R CHORD IAW SRM AND DWG.
LOWER BULKHEAD FRAME CRACKED AT BS 540, STRINGER 22R. REPAIRED FRAME IAW EA.
RIGHT WING NR 7 SLAT L/E SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM AND EA.
MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 33 TO RBL 34. REPAIRED WEB IAW SRM.
LEFT EXTERNAL EMER LIGHT JUST AFT OF FLAP INOPERATIVE. RELAMPED LIGHT IAW SIP.
R1 DOOR EMER EVAC SLIDE GIRT BAR CLIP BROKEN. REPAIRED CLIP IAW AMM.
RIGHT MLG INNER DOOR CRACKED AT AFT DOOR & FWD HINGE. R & R DOOR IAW AMM.
L1 DOOR EMER EXIT LIGHT HOUSING CRACKED. R & R LIGHT IAW AMM.
MAIN WHEEL WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B LBL 45.5. REPAIRED BEAM IAW ACO & EA.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B RBL 24.75. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B LBL 24.75. REPAIRED BEAM IAW EA.
LEFT WING OTBD AFT FLAP INBD LOWER CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.
LEFT WING ORSS 271 APPROX BELOW TE FIXED PANEL, TE VERTICAL RIB AFT BUMPER SEAL ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG.
RIGHT NR 3 WINDOW FRAME E - F POST SECOND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW SI & ACO.
AFT EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.
FORWARD EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.
MID CABIN EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.
EMERGENCY EXIT LIGHT LENS AFT OF LT AFT WING TO BODY FAIRING DIRTY. R & R LENS IAW AMM.
EMERGENCY EXIT LIGHT LENS AFT OF RT AFT WING TO BODY FAIRING DIRTY. R & R LENS IAW AMM.
L2 DOOR EMERGENCY EXIT SIGN BASE CRACKED. R&R LIGHT ASSEMBLY IAW AMM.
FWD EEPLS LOOSE AT FORWARD BALLMAT AREA. SECURED EEPLS IAW MM.
INFLIGHT SHUTDOWN /AIR TURNBACK/ DECLARED EMERGENCY. AT APPROX 13000FT NR 2 ENGINE EXPERIENCED 3 LOUD BANGS EGT EXCEEDANCE MANUALLY SHUTDOWN NR 2. REMOVED AND REPLACED NR 2 ENGINE PER MT & AMM.
LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
LEFT EEPLS COVER CRACKED AT ROW 13. REMOVED AND REPLACED COVER PER MM.
R1 DOOR EMERGENCY EXIT LIGHT INOP. CLEANED CONNECTOR PER AMM.
FLOOR SUPPORT BEAM CORRODED BETWEEN BS 787+4 TO BS 847, RBL 13. REPAIRED BEAM IAW SRM.
FRAME CORRODED AT BS 268.8, LBL 7. REPAIRED FRAME IAW SRM.
L1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW EA.
R1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW EA.
L2 DOOR EMERGENCY EVAC SLIDES PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.
R1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR HOLDER LOOSE. REMOVED AND REPLACED FASTENER PER MM.
LT EMERGENCY FLOOR LIGHTING MISSING COVER AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV2 CHECK FOUND, R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE INOP. REMOVED AND REPLACED GIRT BAR PER MM.
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERY FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PER MM.
FWD CABIN EEPLS COVER MISSING. INSTALLED COVER PER MM.
DURING SCHEDULED MV3 CHECK, FOUND LT EEPLS WIRE LOOSE BETWEEN ROW 11 TO ROW 13. SECURED WIRE PER MM.
DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 12.5. REPAIRED FLOORBEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 8. REPAIRED FLOORBEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, RBL 8. REPAIRED FLOORBEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, RBL 14. REPAIRED FLOORBEAM PER EA.
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.
DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 13 TO ROW 23. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 5 TO ROW 10. REMOVED AND REPLACED COVER PER MM.
FWD EEPLS LIGHT LENS LOOSE. SECURED LENS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.
DURING SCHEDULED HC1 CHECK, RT MID EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, RT AFT EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT ELEVATOR DELAMINATED AT UPPER SURFACE STATION 265.45. REPAIRED ELEVATOR PER SRM.
DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK FAILED LONG TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, AFT LEFT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
EEPLS TRACK COVER LOOSE AT FWD END. REMOVED AND REPLACED COVER PER MM.
AIR TURNBACK/DECLARED EMERGENCY. BURNING RUBBER FUMES AND ODOR IN CABIN. PERFORMED VISUAL INSPECTIONS, NO DEFECTS NOTED. REMOVED AND REPLACE LEFT AND RIGHT A/C PACK WATER SEPARATOR BAGS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
FWD END OF EEPLS LENS MISSING. INSTALLED LENS PER MM.
FWD FLOOR EMERGENCY EXIT LIGHT BROKEN. REPAIRED WIRING, REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED EEPLS PER MM.
DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT SIGN LENS CRACKED IN AFT GALLEY. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED RON CHECK, FOUND EEPLS FLOOR TRACK INOP AT ROW 1. REMOVED AND REPLACED EEPLS FLOOR TRACK COVER PER MM.