N475WN

Part: SEAT — OUT OF ALIGNMENT (ZONE 200) · airframe 69,585 hrs · 41,531 cycles

CABIN SEAT RECLINE NEEDS TO BE INOP AT 11F (EXIT ROW). ADJUSTED SEAT 11F IAW AMM 25-22-00.

Part: SIGN — DETACHED (ZONE 200) · airframe 68,471 hrs · 40,863 cycles

OVERHEAD EXIT SIGN ABOVE EXIT ROW FELL OFF<[01] REINSTALLED OVERHEAD EXIT SIGN ABOVE EXIT ROW IAW AMM 33-51-01

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 68,208 hrs · 40,697 cycles

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)]

Part: LENS — MISSING (ZONE 200) · airframe 67,112 hrs · 40,000 cycles

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.

Part: PLATE — LOOSE (AFT DOOR HANDLE) · airframe 65,956 hrs · 39,282 cycles

AFT SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] ADJUSTED CAM PLATE PER AMM 52-41-00

Part: CONNECTOR — OUT OF ADJUST (EMERGENCY LIGHTS) · airframe 65,737 hrs · 39,139 cycles

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.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,737 hrs · 39,139 cycles

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.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 65,737 hrs · 39,139 cycles

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.

Part: STIFFENER — CORRODED (ZN 200 FUS TOP) · airframe 65,737 hrs · 39,139 cycles

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

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.'

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 65,737 hrs · 39,139 cycles

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

Part: SUPPORT BRACKET — CRACKED (BS 705 LBL23) · airframe 65,737 hrs · 39,139 cycles

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.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 65,737 hrs · 39,139 cycles

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.

Part: ATTACH ANGLE — CRACKED (BS 693 RBL 22) · airframe 65,737 hrs · 39,139 cycles

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

Part: ATTACH ANGLE — CRACKED (BS 693 LBL22) · airframe 65,737 hrs · 39,139 cycles

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

Part: BRACKET — CORRODED (GIRT BAR) · airframe 65,737 hrs · 39,139 cycles

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.

Part: FLOOR SUPPORT — CRACKED (BS 322 LBL45) · airframe 65,737 hrs · 39,139 cycles

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.

Part: FLOOR PANEL — CORRODED (ZN 200 FUS TOP) · airframe 65,737 hrs · 39,139 cycles

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.

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 65,737 hrs · 39,139 cycles

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

Part: VAPOR BARRIER — DEBONDED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 65,737 hrs · 39,139 cycles

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.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: THRESHOLD — CRACKED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,737 hrs · 39,139 cycles

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.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 65,737 hrs · 39,139 cycles

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.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: SKIN — DEBONDED (ZN 100 FUS LOWER) · airframe 65,737 hrs · 39,139 cycles

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.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 65,137 hrs · 38,764 cycles

FWD GALLEY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK FOR THE FWD GALLEY EMERGENCY LIGHTS. OPS CHECK GOOD PER AMM 3351-06

Part: ISOLATOR — CRACKED (ZN 800 DOOR) · airframe 64,145 hrs · 38,157 cycles

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.

Part: LIGHT — MISSING (ZN 200 FUS TOP) · airframe 64,145 hrs · 38,157 cycles

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.

Part: SIGN — MISSING (ZN 200 FUS TOP) · airframe 63,373 hrs · 37,664 cycles

AFT CAPTAINS SIDE WHITE EXIT SIGN COVER BY ENTRY DOOR MISSING.<[01] INSTALLED NEW EMERGENCY EXIT SIGN IAW SIP.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 63,078 hrs · 37,479 cycles

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.

Part: BRACKET — CRACKED (ZN 800 DOOR) · airframe 62,250 hrs · 36,951 cycles

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

Part: BATTERY PACK — NO TEST (FWD FLASHLIGHT) · airframe 61,732 hrs · 36,606 cycles

ONE FWD EMERGENCY FLASHLIGHT WILL NOT TEST. R & R THE FWD EMERGENCY FLASHLIGHT BATTERY PACK IAW MM 25-64-00. OPS NORMAL

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 60,239 hrs · 35,607 cycles

COCKPIT EMERGENCY LIGHT DOES NOT COME ON / [01] REPLACED M1219 OPS CHECK GOOD PER AMM 33-51-00

Part: NONE — INOPERATIVE · airframe 59,744 hrs · 35,276 cycles

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.

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: STRINGER CLIP — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: TENSION TIE — CORRODED (WET AREA) · airframe 59,744 hrs · 35,276 cycles

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.

Part: TENSION TIE — CORRODED (WET AREA) · airframe 59,744 hrs · 35,276 cycles

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

Part: RAIL — CRACKED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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

Part: PANEL — MISSING (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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;

Part: WEB — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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.

Part: RAIL — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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.

Part: WEB — CORRODED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: INTERCOSTAL — CRACKED (BS 294-312) · airframe 59,744 hrs · 35,276 cycles

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.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: SUPPORT BRACKET — CRACKED · airframe 59,744 hrs · 35,276 cycles

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.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: STRINGER CLIP — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: ATTACH ANGLE — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 59,744 hrs · 35,276 cycles

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

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: NONE — CRACKED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: TENSION TIE — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 59,744 hrs · 35,276 cycles

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

Part: SHIELD — CORRODED (AFT CARGO) · airframe 59,744 hrs · 35,276 cycles

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

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,744 hrs · 35,276 cycles

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

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SIDEWALL SUPPORT — CRACKED (FWD CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 59,744 hrs · 35,276 cycles

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.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 59,744 hrs · 35,276 cycles

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

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: BRACKET — CRACKED (R/H WING) · airframe 59,744 hrs · 35,276 cycles

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

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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.

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 59,744 hrs · 35,276 cycles

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

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 59,744 hrs · 35,276 cycles

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

Part: NONE — CRACKED (R1 DOOR) · airframe 59,744 hrs · 35,276 cycles

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

Part: DOUBLER — CRACKED (L/H WING) · airframe 59,744 hrs · 35,276 cycles

#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.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 59,570 hrs · 35,159 cycles

FORWARD SERVICE DOOR GIRT BAR BRACKET LOOSE. / [01] ADJUSTED GIRT BAR BRACKETS PER S.I.P.

Part: PANEL — ELONGATED (MLG WW) · airframe 59,100 hrs · 34,882 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 58,806 hrs · 34,711 cycles

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.

Part: PANEL — CORRODED (FUSELAGE) · airframe 58,806 hrs · 34,711 cycles

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

Part: PANEL — NONE (FUSELAGE) · airframe 58,806 hrs · 34,711 cycles

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.

Part: PANEL — NONE (FUSELAGE) · airframe 58,806 hrs · 34,711 cycles

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.

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 58,806 hrs · 34,711 cycles

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.

Part: ANGLE — CRACKED (CENTER WING) · airframe 58,806 hrs · 34,711 cycles

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.

Part: PANEL — NONE (FUSELAGE) · airframe 58,806 hrs · 34,711 cycles

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.

Part: FAIRING — CRACKED (#3 FLAP TRACK) · airframe 58,806 hrs · 34,711 cycles

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.

Part: PANEL — CORRODED (FUSELAGE) · airframe 58,806 hrs · 34,711 cycles

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.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 57,388 hrs · 33,875 cycles

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.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,007 hrs · 33,646 cycles

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

Part: COVER — MISSING (CABIN) · airframe 56,743 hrs · 33,496 cycles

EMERG. EXT SIGN COVER FELL OFF. OVERWING EXIT ON FO'S SIDE / REINSTALLED R/H OVERWING EMERGENCY EXIT SIGN COVER PER SIP

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 56,238 hrs · 33,192 cycles

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).

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 55,872 hrs · 32,972 cycles

LT WING EMERGENCY EXIT LIGHT LENS BROKEN. R & R LT WING EMERGENCY EXIT LENS, IAW AMM 33-51-11.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 55,707 hrs · 32,864 cycles

LT AFT EMERGENCY LIGHT C/B POPPED. REMOVED AND REPLACED AFT LEFT EMERGENCY CHARGER AND BATTERY, PER AMM33-51-06.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 55,506 hrs · 32,733 cycles

FOUND R AFT LIGHTING EMERENCY LIGHT CB POPPED ON PREFLIGHT / RESET RIGHT AFT LIGHTING EMERGENCY CHARGER & OPS CHECKED NORMAL PER AMM 33-51-00

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,070 hrs · 32,448 cycles

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.

Part: SIGN — UNSECURE (CABIN) · airframe 55,067 hrs · 32,446 cycles

CAPT SIDE OVERWING EXIT LOWER 'EXIT' SIGN FELL OFF. RE-INSTALLED SIGN IAW SIP

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,947 hrs · 32,366 cycles

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

Part: SUPPORT — CRACKED (COCKPIT) · airframe 54,947 hrs · 32,366 cycles

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

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

***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

Part: STRAP — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 54,947 hrs · 32,366 cycles

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

Part: STRAP — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

***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.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 54,947 hrs · 32,366 cycles

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

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: WEB — CORRODED (CARGO DOOR) · airframe 54,947 hrs · 32,366 cycles

***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.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 54,947 hrs · 32,366 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,947 hrs · 32,366 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

***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

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 54,947 hrs · 32,366 cycles

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.

Part: SHIELD — CORRODED (BS 420-440 S25R) · airframe 54,947 hrs · 32,366 cycles

***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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

***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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 54,947 hrs · 32,366 cycles

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.

Part: SUPPORT — CORRODED (BS 480-500A) · airframe 54,947 hrs · 32,366 cycles

***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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

***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.

Part: WEB — DENTED (COCKPIT) · airframe 54,947 hrs · 32,366 cycles

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

Part: SEAL — DEBONDED (HORIZONTAL STAB) · airframe 54,947 hrs · 32,366 cycles

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

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 54,947 hrs · 32,366 cycles

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

Part: VAPOR BARRIER — CRACKED (BS 663.75) · airframe 54,947 hrs · 32,366 cycles

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.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 54,947 hrs · 32,366 cycles

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

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 54,947 hrs · 32,366 cycles

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.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 54,947 hrs · 32,366 cycles

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

Part: FLOOR PANEL — PEELING (CABIN) · airframe 54,947 hrs · 32,366 cycles

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

Part: NONE — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

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.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,947 hrs · 32,366 cycles

RIGHT EMERGENCY EXIT HATCH CUTOUT FWD LOWER CORNER HAS CORROSION SPOTS. MARKED 29-10 /

Part: SKIN — DELAMINATED (TE FLAP) · airframe 54,242 hrs · 31,891 cycles

L/H WING OUTBOARD AFT FLAP INBOARD AFT LOWER SKIN CORNER DELAMINATED. / R&R L/H AFT FLAP ASSEMBLY PER AMM.

Part: FRAME — CRACKED (RT WG-BDY FAIRIN) · airframe 54,242 hrs · 31,891 cycles

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.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 53,144 hrs · 31,192 cycles

L1 DOOR SLIDE FELL OUT. REINSTALLED SLIDE PER MT.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 52,403 hrs · 30,713 cycles

EMERGENCY EXIT LIGHT COVER BROKEN ON R/H SIDE EMERGENCY EXIT DOOR. / R&R LIGHT COVER IAW AMM.

Part: STRAP — BROKEN (FWD FLASHLIGHT) · airframe 52,372 hrs · 30,691 cycles

FORWARD GALLEY FLASHLIGHT RETENTION STRAP BROKEN. INSTALLED RETENTION STRAP PER AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 51,098 hrs · 29,870 cycles

AIR TURNBACK, ON CLIMBOUT FIRST OFFICER'S R1 WINDOW ARCED THEN CRACKED. R&R R1 WINDOW PER AMM.

Part: SEAL — CRACKED (LT WING) · airframe 50,005 hrs · 29,196 cycles

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

Part: DOOR — CRACKED (LT MLG) · airframe 50,005 hrs · 29,196 cycles

LT MAIN LANDING MIDDLE GEAR DOOR CRACKED AT STIFFENER. REPAIRED DOOR IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,969 hrs · 28,541 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,752 hrs · 28,387 cycles

FLIGHT DECK " EMERGENCY LIGHT" IN CEILING INOP. INSTALLED LAMP IAW AMM.

Part: PANEL — CRACKED (SLAT) · airframe 48,752 hrs · 28,387 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · airframe 48,752 hrs · 28,387 cycles

AFT PIT FLOOR LT Z-ANGLE CORRODED BETWEEN BS 727D TO BS 792, LBL 20. R&R Z-ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,752 hrs · 28,387 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED AT BS 328, LBL 46. R&R INTERCOSTAL IAW DWG AND SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 48,752 hrs · 28,387 cycles

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

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 48,752 hrs · 28,387 cycles

AFT CARGO DOOR CUT OUT LOWER SILL AFT CORNER SCUFF PLATE CASTING CRACKED ALONG BULLNOSE. REPAIRED SCUFF PLATE IAW EA.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 48,752 hrs · 28,387 cycles

EMERGENCY LIGHT CHECK FLIGHT DECK CEILING LIGHT INOP. RELAMPED LIGHT IAW AMM & SIP.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,752 hrs · 28,387 cycles

LT LOWER FUSELAGE EMERGENCY LIGHT INOP. R&R POWER SUPPLY IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 48,752 hrs · 28,387 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,076 hrs · 27,955 cycles

EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1672. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 48,076 hrs · 27,955 cycles

EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1673. R & R THE BATTERY PACK IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,076 hrs · 27,955 cycles

EXTERNAL POWER DOOR CUTOUT AFT LOWER EDGE CRACKED. REPAIRED CUTOUT PER SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,076 hrs · 27,955 cycles

EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1675. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,076 hrs · 27,955 cycles

EMERGENCY LIGHTING BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1674. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 48,076 hrs · 27,955 cycles

EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED AT LOCATION M1670. R & R THE BATTERY PACK IAW MM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 48,071 hrs · 27,952 cycles

SUPPLEMENTAL INFORMATION: RIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R RIGHT HORIZ STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: NONE — BROKEN (WHEEL WELL RH) · airframe 48,071 hrs · 27,952 cycles

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

Part: BRACKET — CRACKED (LT WING) · airframe 45,956 hrs · 26,652 cycles

L/H WING FLAP SEAL BRACKET UNDER PNL 551 GB IS CRACKED / R&R BRACKET AS PER SRM 51-40-02

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 45,246 hrs · 26,218 cycles

FORWARD EMERGENCY FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,358 hrs · 25,084 cycles

L2 DOOR EXIT SIGN INOPERTIVE. REPLACED THE LAMPS IAW AMM.

Part: PROBE — DEFECTIVE (WING) · airframe 42,750 hrs · 24,747 cycles

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.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

L1 DOOR CUTOUT LOWER INBD CHORD CRACKED AT BS 312. R & R CHORD IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

FORWARD CARGO PIT INTERCOSTAL CLIP CRACKED AT BS 500D, RBL 6. R & R CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (BS 285) · airframe 42,517 hrs · 24,609 cycles

FORWARD WET AREA FLOORBEAM CORRODED AT BS 285, BETWEEN BL 0 TO LBL 7. REPAIRED THE FLOORBEAM IAW EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 42,517 hrs · 24,609 cycles

R2 DOOR CUTOUT LOWER INNER CHORD CORRODED AT BS 986.5. R & R CHORD IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,517 hrs · 24,609 cycles

RIGHT WING NR 7 SLAT L/E SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM AND EA.

Part: FRAME — CRACKED (BS 540 BULKHEAD) · airframe 42,517 hrs · 24,609 cycles

LOWER BULKHEAD FRAME CRACKED AT BS 540, STRINGER 22R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 42,517 hrs · 24,609 cycles

MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 33 TO RBL 34. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,718 hrs · 22,421 cycles

LEFT EXTERNAL EMER LIGHT JUST AFT OF FLAP INOPERATIVE. RELAMPED LIGHT IAW SIP.

Part: FITTING — BROKEN (R1 DOOR) · airframe 37,795 hrs · 21,891 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR CLIP BROKEN. REPAIRED CLIP IAW AMM.

Part: DOOR — CRACKED (RT MLG) · airframe 36,188 hrs · 20,975 cycles

RIGHT MLG INNER DOOR CRACKED AT AFT DOOR & FWD HINGE. R & R DOOR IAW AMM.

Part: LIGHT — CRACKED (L1 DOOR) · airframe 35,907 hrs · 20,807 cycles

L1 DOOR EMER EXIT LIGHT HOUSING CRACKED. R & R LIGHT IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,907 hrs · 20,807 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B RBL 24.75. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,907 hrs · 20,807 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B LBL 45.5. REPAIRED BEAM IAW ACO & EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,907 hrs · 20,807 cycles

MAIN WHEEL WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,907 hrs · 20,807 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B LBL 24.75. REPAIRED BEAM IAW EA.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 35,907 hrs · 20,807 cycles

LEFT WING ORSS 271 APPROX BELOW TE FIXED PANEL, TE VERTICAL RIB AFT BUMPER SEAL ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 35,907 hrs · 20,807 cycles

LEFT WING OTBD AFT FLAP INBD LOWER CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,907 hrs · 20,807 cycles

RIGHT NR 3 WINDOW FRAME E - F POST SECOND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW SI & ACO.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,015 hrs · 20,299 cycles

MID CABIN EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,015 hrs · 20,299 cycles

AFT EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,015 hrs · 20,299 cycles

FORWARD EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW MM.

Part: LENS — DIRTY (EXTERIOR) · airframe 35,011 hrs · 20,298 cycles

EMERGENCY EXIT LIGHT LENS AFT OF RT AFT WING TO BODY FAIRING DIRTY. R & R LENS IAW AMM.

Part: LENS — DIRTY (EXTERIOR) · airframe 35,011 hrs · 20,298 cycles

EMERGENCY EXIT LIGHT LENS AFT OF LT AFT WING TO BODY FAIRING DIRTY. R & R LENS IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 32,877 hrs · 19,028 cycles

L2 DOOR EMERGENCY EXIT SIGN BASE CRACKED. R&R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,819 hrs · 19,001 cycles

FWD EEPLS LOOSE AT FORWARD BALLMAT AREA. SECURED EEPLS IAW MM.

Part: ENGINE — FAILED (RIGHT) · airframe 30,047 hrs · 17,417 cycles

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.

Part: LENS — MISSING (CABIN) · airframe 29,977 hrs · 17,375 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 29,429 hrs · 17,010 cycles

LEFT EEPLS COVER CRACKED AT ROW 13. REMOVED AND REPLACED COVER PER MM.

Part: CONNECTOR — DIRTY (CABIN) · airframe 29,368 hrs · 16,967 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. CLEANED CONNECTOR PER AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,130 hrs · 16,817 cycles

FLOOR SUPPORT BEAM CORRODED BETWEEN BS 787+4 TO BS 847, RBL 13. REPAIRED BEAM IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,130 hrs · 16,817 cycles

FRAME CORRODED AT BS 268.8, LBL 7. REPAIRED FRAME IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 29,130 hrs · 16,817 cycles

R1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 29,130 hrs · 16,817 cycles

L1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 29,120 hrs · 16,810 cycles

L2 DOOR EMERGENCY EVAC SLIDES PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 28,503 hrs · 16,452 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR HOLDER LOOSE. REMOVED AND REPLACED FASTENER PER MM.

Part: COVER — MISSING (CABIN) · airframe 27,861 hrs · 16,075 cycles

LT EMERGENCY FLOOR LIGHTING MISSING COVER AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,248 hrs · 15,717 cycles

DURING SCHEDULED MV2 CHECK FOUND, R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 26,358 hrs · 15,181 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: GIRT BAR — DEFECTIVE (R1 DOOR) · airframe 24,510 hrs · 14,152 cycles

R1 DOOR EMERGENCY EVAC SLIDE INOP. REMOVED AND REPLACED GIRT BAR PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 24,016 hrs · 13,873 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERY FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,962 hrs · 13,832 cycles

FWD CABIN EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 23,812 hrs · 13,745 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT EEPLS WIRE LOOSE BETWEEN ROW 11 TO ROW 13. SECURED WIRE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,311 hrs · 12,862 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 8. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,311 hrs · 12,862 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, RBL 14. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,311 hrs · 12,862 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, RBL 8. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,311 hrs · 12,862 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 773, LBL 12.5. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,945 hrs · 12,661 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,945 hrs · 12,661 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 19,134 hrs · 10,972 cycles

DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — CRACKED (CABIN) · airframe 18,554 hrs · 10,624 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 13 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 18,554 hrs · 10,624 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 5 TO ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 18,494 hrs · 10,586 cycles

FWD EEPLS LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 18,272 hrs · 10,465 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,329 hrs · 9,910 cycles

DURING SCHEDULED HC1 CHECK, RT MID EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,329 hrs · 9,910 cycles

DURING SCHEDULED HC1 CHECK, RT AFT EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,143 hrs · 9,798 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 15,583 hrs · 8,855 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 14,945 hrs · 8,490 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,484 hrs · 7,053 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK FAILED LONG TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,484 hrs · 7,053 cycles

DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 12,484 hrs · 7,053 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT ELEVATOR DELAMINATED AT UPPER SURFACE STATION 265.45. REPAIRED ELEVATOR PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,484 hrs · 7,053 cycles

DURING SCHEDULED HC1 CHECK, AFT LEFT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 5,680 hrs · 3,135 cycles

EEPLS TRACK COVER LOOSE AT FWD END. REMOVED AND REPLACED COVER PER MM.

Part: COALESCER BAG — ODOR (A/C BAY) · airframe 5,079 hrs · 2,816 cycles

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.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 4,902 hrs · 2,730 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,801 hrs · 2,125 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 3,070 hrs · 1,728 cycles

FWD END OF EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 2,996 hrs · 1,683 cycles

FWD FLOOR EMERGENCY EXIT LIGHT BROKEN. REPAIRED WIRING, REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 2,988 hrs · 1,679 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED EEPLS PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 2,411 hrs · 1,348 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT SIGN LENS CRACKED IN AFT GALLEY. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,156 hrs · 1,212 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS FLOOR TRACK INOP AT ROW 1. REMOVED AND REPLACED EEPLS FLOOR TRACK COVER PER MM.