N7884G

Part: OIL COOLER — LEAKING (ZN 100 FUS LOWER) · airframe 71,012 hrs · 30,851 cycles

APU AUTO SHUTDOWN EN ROUTE<[01] FOUND OIL LEAK AT APU OIL COOLER; R&R APU OIL COOLER IAW AMM 49-91-41; OPS CHECK GOOD

Part: SLIDE — OUT OF TOLERANCE (ZN 800 DOOR) · airframe 70,527 hrs · 30,533 cycles

FWD SERVICE DOOR SLIDE GAUGE NEEDLE IN RED BAND.<[01] REMOVED SLIDE PER MT 725-61-06.;[02] INSTALLED FWD SERVICE SLIDE PER MT 725-61-06. CKS OK.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,205 hrs · 30,324 cycles

CAPTS SIDE EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED L/H OVERWING EMERGENCY EXIT WINDOW LIGHT BALLAST PER AMM 33-21-00. OPS CHK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,279 hrs · 29,736 cycles

OVERHEAD FWD COVE LIGHT F/O INOP OVERHEAD FWD COVE LIGHT F/O INOPCENTER ISLE CEILING NEAR ROW 1 DEF OVERHEAD BIN. RELAMPED RECESSED CEILING LIGHT PER AMM 33-22-00

Part: NONE — INOPERATIVE · airframe 68,544 hrs · 29,249 cycles

BOTH OUTSIDE EMERGENCY LIGHTS AFT OF THE WING INOP / [01] REPLACED M1670 BATTERY PACK PER AMM 33-51-06. OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 68,058 hrs · 28,926 cycles

EMERGENCY LIGHTS AT OVERHEAD BIN LOCATION 6ABC;9ABC;14ABC;13DEF;11DEF;8DEF AND R/H OVERWING EXIT DOOR INTERIOR AND EXTERIOR INOP / [01] REMOVED AND REPLACED BATTERIES PACKS M1669 AND M2335 PER AMM 33-51-06-960-805. TEST NORMAL.;[02] VERIFIED STEP 1.

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 68,058 hrs · 28,926 cycles

FOUND AT FWD CARGO STA 520 STR 25 RT. SIDE INTERCOSTAL CRACKED / [01] REMOVED INTERCOSTAL FOR CRACK AT FWD CARGO STA 520 STR 25 RT 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] FABRICATED INTERCOSTAL AS PER BOEING DRAWING # 143A9803-58; MATERIAL USED 7075-0 .032' PO # 1734421.;[04] VERIFIED STEP 3;[05] HEAT TREATED FWD CARGO INTERCOSTAL AS PER DWD 143A9803 AND BAC5602;[06] VERIFIED STEP 5;[07] LOCATED AND OPENED NEW FASTENER HOLES AT INTERCOSTAL STA 520 AND STR. 25 RT. AS PER B737-7 SRM 51-40-05 AND BOEING DRAWING #143A9803-58.;[08] VERIFIED STEP 7;[09] TREATED AND PRIME NEW INTERCOSTAL AMM 51-21-72-370-804 AND SRM 51-20-01-0G-0;[10] VERIFIED STEP 9<BR>OK TO INSTALL NEW INTERCOSTAL AT FWD CARGO STA 520 STR 25 RT;[11] INSTALLED NEW INTERCOSTAL AT FWD CARGO STA 520 STR 25 RH SRM 51-40-02-0G-0;[12] VERIFIED STEP 11

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 68,058 hrs · 28,926 cycles

FOUND AFT CARGO COMPT; FWD CORNER SCUFF PLATE CRACKED AT MULTIPLE SPOTS. / [01] LOCATED AND OPENED NEW FASTENER HOLES AT NEW AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE AS PER B737-7 SRM 51-40-05-0G-0.;[02] SCUFF PLATE FWD CORNER WILL BE INSTALLED AT CARD TTG8Q004EXF7.;[03] VERIFIED STEPS 1 AND 2

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 68,058 hrs · 28,926 cycles

AFT OF FWD CARGO COMPARTMENT R/H SIDE WALL GUSSET CRACKED @ S-19R STA 500D MKD DOT / [01] REMOVED GUSSET AT AFT OF FWD CARGO RH SIDE WALL FOR CRACK S-19R STA 500D SRM 51-40-02-0G-0;[02] RECEIVED NEW PARTS PO#1774766 LOCATED NEW PART AND DRILLED NEW HOLES SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] TREATED AND PRIME AT NEW HOLES SRM 51-20-01 AND AMM 51-21-72-370-801;[05] OK TO INSTALL NEW GUSSET AT AFT OF FWD CARGO RH;[06] INSTALLED NEW GUSSET AT FWD CARGO RH SIDE WALL S29R STA 500D SRM51-40-02-0G-0;[07] VERIFIED STEP 6

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,058 hrs · 28,926 cycles

EXTERNAL POWER RECEPTACLE CUTOUT; FWD; LOWER INNER DOUBLER CRACKED. / [01] REMOVE EPR DOOR FOR INNER DOUBLER REPLACE ACCESS REF USED SRM 53-10-15-2R-4 STEP4.A(1);[[17] PERFORMED HFEC AT CUT OUT AS PER NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS<BR>[NORTEC 600 ; B/C 166316 ; CALIB.DUE- 10/22];[18] PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIONS AT REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS. [NORTEC 600 ; B/C 166316 ; CALIB.DUE- 10/22];[19] PERFORMED HFEC COUNTERSINK INSPECTION ON ALL REMOVED FASTENER LOCATIONS AT REPAIR AREA IAW NDTM PART 6; 53-30-00; PROCEDURE 3. NO CRACKS. [NORTEC 600 ; B/C 166316 ; CALIB.DUE- 10/22];[20] LOCATED AND DRILLED NEW EGPR INNER DOUBLER REF USED SRM 51-40-05-0G-0;[25] INSTALLED EGPR DOUBLER AND PARTIALLY INSTALLED FASTENERS AT EGPR EXTERIOR SKIN REF USED SRM 51-40-02-0G-0 AND DWG#141A3702;

Part: FITTING — CRACKED · airframe 68,058 hrs · 28,926 cycles

R/W RAR SPAR T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED @ FASTENER TAIL INB. MKD DOT / [01] REMOVEDND REPLACED BULB SEAL FITTING AT R/W REAR SPART T/E DEFLECTION CONTROL RIB PANEL VERTICAL. REF. SRM. 51-40-02-0G-0-A00279.;[02] CORRECTION FOR STEP #1 SHOULD READ: REMOVED AND REPLACED BULB SEAL FITTING AT R/W REAR SPAR T/E DEFLECTION CONTROL RIB PANEL AS PER B737-700 51-40-02-0-A00279;[03] VERIFIED STEP 3.

Part: SUPPORT ANGLE — CRACKED (LH WING) · airframe 68,058 hrs · 28,926 cycles

L/W REAR SPAR T/E LOWER SUPPORT ANGLE CRACKED @ INB END BELOW SPOILER NO-5 MKD DOT / [01] REMOVED SUPPORT ANGLE AT LW REAR SPAR T/E FOR CRACK SRM 51-40-02-0G-0;[02] RECEIVED NEW ANGLE PP#115A3758-9 LOCATED NEW ANGLE AND DRILLED NEW HOLES SRM 51-40-05-0G-0;[03] VERIFIED STEPS:1 AND 2.;[04] TREATED AND PRIME AT NEW HOLES AMM 51-21-41-370-802 AND 51-21-72--370-804;[05] VERIFIED STEP 4<BR>OK TO INSTALL NEW ANGLE AT L/W REAR SPAR T/E;[06] INSTALLED NEW ANGLE AT L/W REAR SPAR T/E REF SRM 51-40-02-0G-0;[07] VERIFIED STEP 6

Part: FITTING — LOOSE (LH WING) · airframe 68,058 hrs · 28,926 cycles

L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL FITTING LOCATION ' A ' HAS PLAY / [01] RESECURED FASTENERS AT RT WING DEFLECTION CONTROL RIB AS PER B737-7 SRM 57-51-02-2R-4 FIG 202 DETAIL A-A;[02] VERIFIED STEP 1

Part: PLATE — CRACKED (LH WING) · airframe 68,058 hrs · 28,926 cycles

L/W REAR SPAR FIXED T/E LOWER WIGGLE FITTING SHEARED FASTENERS POSSIBLE CRACKED O/B OF FLAP TRACK NO-3 MKD DOT / [01] REMOVED AND REPLACED WIGGLE PLATE AT L/W REAR SPAR O/B OF OF FLAP TRACK #3 AS PER B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: FITTING — LOOSE (RH WING) · airframe 68,058 hrs · 28,926 cycles

R/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL FITTING LOCATION ' A ' HAS PLAY / [01] RESECURED FASTENERS AT RT WING DEFLECTION CONTROL RIB AS PER B737-7 SRM 57=51-02-2R-4; FIG. 202 DETAIL A-A;[02] VERIFIED STEP 1

Part: FITTING — ERODED (LH WING) · airframe 68,058 hrs · 28,926 cycles

L/W REAR SPAR LOWER FIXED T/E STIFFENER LOWER FITTING HAS DRILLED HOLE @ ORSS 261 O/B OF FLAP TRACK NO-3 MKD DOT / [01] MEASURED DAMAGED AREA AT L/H WING REAR SPAR LOWER AREA OF STIFFNER ORSS 261 AS PER B737-7 SRM 57-20-90-1A-2 ; HOLE DIAMETER= .215' DEPTH= .083'.;[02] PERFORMED HFEC AROUND PERIMETER OF DAMAGED AREA IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. [NORTEC 600 ; B/C 166316 ; CALIB.DUE- 10/22] NOTE: DAMAGE POSSIBLE CAUSE IS FRICTION RESULTING IN SURFACE EROSION WITH MATERIAL LOSS. THERE IS NO 'HOLE' PRESENT.;[03] PERFORMED UT THICKNESS ON AFFECTED AREA AS PER NDTM PART 4; 51-00-00 PROCEDURE 3. MINIMUM FOUND: 0.140'<BR>[OLYMPUS 27MG; B/C 172139; CALIB.DUE-4/23];[04] VERIFIED STEP 1;[05] FOUND DAMAGED AREA TO BE OUT OF LIMITS AT LT WING REAR SPAR STIFFENER LOWER AREA ORSS 261 AS PER B737-7 SRM 57-20-90-1A=2; FIG 103 DETAIL C-C.MATERIAL LOSS =.083' NOMINAL MAT. = .140' MAT. REMAINING = .057';[06] VERIFIED STEP 5;[07] ACCOMPLISHED REPAIR AT L/W REAR SPAR SUPPORT BRACKET ORSS 261 AS PER EA M-21-157-00525 AND TTG8Q00DT78J.;[08] VERIFIED STEP 7

Part: FITTING — DAMAGED (RH WING) · airframe 68,058 hrs · 28,926 cycles

R/W REAR SPAR FIXED T/E LOWER STIFFENER FITTING LOWER SURFACE DRILLED HOLE @ ORSS 261 MKD DOT / [01] MEASURED DAMAGED HOLE AT RT WING REAR SPAR FIXED T/E LOWER STIFFNER ATREA ORSS 261 AS PER B737-7 SRM 57-20-90-1A-2;DEPTH = .044' WITDTH = .210';CALIPER B/C 159930.;[02] PERFORMED HFEC AROUND PERIMETER OF DAMAGED AREA IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. [NORTEC 600 ; B/C 166316 ; CALIB.DUE- 10/22] NOTE: DAMAGE POSSIBLE CAUSE IS FRICTION RESULTING IN SURFACE EROSION WITH MATERIAL LOSS. THERE IS NO 'HOLE' PRESENT.;[03] PERFORMED UT THICKNESS ON AFFECTED AREA AS PER NDTM PART 4; 51-00-00 PROCEDURE 3. MINIMUM FOUND:0.140'<BR>[OLYMPUS 27MG; B/C 172139; CALIB.DUE-4/23];[04] VERIFIED STEP 1;[05] FOUND DAMAGED AREA TO BE OUT OF LIMITS AT RT. WING REAR SPAR STIFFENER LOWER AREA ORSS 261 AS PER B737-7 SRM 57-20-90-1A-2 FIG. 103 DETAIL C-C MATERIAL LOSS = .044' NOMINAL MAT.= ;140' MAT. REMAINING = .096';[06] VERIFIED STEP 5;[07] ACCOMPLISHED REPAIR AT R/W SUPPORT BRACKET ORSS 261 AS PER EA M-21-157-00525 AND TTG8Q00DUIZD.;[08] VERIFIED STEP 7

Part: SUPPORT ANGLE — CORRODED (LH WING) · airframe 68,058 hrs · 28,926 cycles

CORROSION ** L/W REAR SPAR LOWER T/E SUPPORT ANGLE BELOW SPOILER PANEL NO- 5 MKD DOT / [01] REF TASK CARD: TTG8Q00DRWEU FOR ANGLE REPLACEMENT.;[02] VERIFIED STEP #1

Part: FITTING — CRACKED (LH WING) · airframe 68,058 hrs · 28,926 cycles

R/W REAR SPAR LOWER T/E WIGGLE FITTING CRACKED ;SHEARED FASTENERS O/B FLAP TRACK NO-6 / [01] REMOVED AND REPLACED WIGGLE PLATE AT L\H WING T/E O/B OF FLAP TRACK #6 AS PER B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: BATTERY PACK — INOPERATIVE (L/H CABIN) · airframe 68,055 hrs · 28,924 cycles

MULTIPLE EMERGENCY EXIT LIGHTS INOP. / [01] R+R LH FWD BATTERY PACK AND RH AFT BATTERY PACK/POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (R/H CABIN) · airframe 68,055 hrs · 28,924 cycles

MULTIPLE EMERGENCY EXIT LIGHTS INOP. / [01] R+R LH FWD BATTERY PACK AND RH AFT BATTERY PACK/POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (R/H CABIN) · airframe 68,055 hrs · 28,924 cycles

MULTIPLE EMERGENCY EXIT LIGHTS INOP. / [01] R+R LH FWD BATTERY PACK AND RH AFT BATTERY PACK/POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.

Part: SUPPORT ROD — BROKEN (#1 ENGINE) · airframe 67,950 hrs · 28,857 cycles

#1 ENGINE O/B FAN COWL AFT SUPPORT ROD IS BROKEN. / [01] REMOVED AND REPLACED #1 ENG O/B FAN COWL AFT SUPPORT ROD SWIVEL BASE BRACKET IN REF TO CMM 71-13-30. OPS TEST NORMAL AT THIS TIME

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 67,626 hrs · 28,641 cycles

EXTERIOR EMERGENCY LIGHT BY R2 DOOR INOP / [01] RELAMPED EXTERIOR EMERGENCY LIGHT BY R2 DOOR IAW AMM 33-51-04. OPS CHECK GOOD.

Part: LENS — FAILED · airframe 67,520 hrs · 28,571 cycles

AFT EMERGENCY LIGHT LENS FELL OFF / [01] REPLACED AFT EMERGENCY LIGHT LENS PER AMM 33-51-14. OPS CHK GOOD.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 66,132 hrs · 27,716 cycles

SUPPLEMENTAL INFORMATION: PNL 193D HAS (1) HOLE ELONGATED ; / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 66,132 hrs · 27,716 cycles

SUPPLEMENTAL INFORMATION: PNL 194E HAS (4) EACH HOLES DELAMINATED ; / [01] INSTALLED NEW PANEL IAW AMM 53-51-21

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 66,132 hrs · 27,716 cycles

SUPPLEMENTAL INFORMATION: PNL 193D HAS (4) EACH HOLE DELAMINATED ; / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,179 hrs · 26,576 cycles

EMERGENCY EXIT LENS ON RT OVERWING EXIT DOOR MISSING / REPLACED EMERGENCY EXIT LENS ON RT OVERWING IAW AMM 33-51-01

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,798 hrs · 26,358 cycles

FOUND MULTIPLE LH EMER EXIT LIGHTS INOP AT LH OVER WING EXIT / REMOVED & REPLACED LH EMER EXIT ROW EMERGENCY BATTERY PACK & CHARGER ASSY PER AMM 33-51-06. OP CHECK GOOD

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,798 hrs · 26,358 cycles

FOUND MULTIPLE LH EMER EXIT LIGHTS INOP AT LH OVER WING EXIT / REMOVED & REPLACED LH EMER EXIT ROW EMERGENCY BATTERY PACK & CHARGER ASSY PER AMM 33-51-06. OP CHECK GOOD

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 62,884 hrs · 25,819 cycles

RIGHT OVERWING EMERGENCY EXIT LOCATOR SIGN IS INOPERATIVE. TROUBLESHOT RIGHT OVERWING EMERGENCY LIGHT, FOUND RIGHT OVERWING SIGN DISCONNECTED. RECONNECTED RIGHT OVERWING EMERGENCY LIGHT PER WDM 33-51-13. PERFORMED GOOD OPERATIONS TEST PER AMM 33-51-01-960-801 STEP 2.B.(2).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,884 hrs · 25,819 cycles

ALL EMERGENCY LIGHTS ATTACHED TO M1673 DO NOT ILLUMINATE. REPLACED M1673 BATTERY PACK AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,884 hrs · 25,819 cycles

ALL EMERGENCY LIGHTS CONNECTED TO M1674 DO NOT ILLUMINATE. REPLACED M1674 BATTERY PACK AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 62,884 hrs · 25,819 cycles

FOUND L1 DOOR EMERGENCY ESCAPE SIGN LIGHT WIRE W4142-0152 BROKEN AT GROUND BLOCK. RETERMINATED W4142-0152 INTO GD3782 PER SWPM 20-90-15 & WDM 33-51-21. PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-01-960-801 STEP 2.B.(2).

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 62,884 hrs · 25,819 cycles

FORWARD CARGO BAY FWD SCUFF PLATE IS CRACKED / LOCATED AND DRILLED FORWARD CARGO BAY; FWD SCUFF PLATE IAW SRM 51-60-05-0G-0; IFG 9; SRM 51-40-08-0G-0; FIG; PG4 AND COUNTERSICKED; INSTALLATION OF FORWARD CARGO BAY; FWD SCUFT PLATE WILL BE PREFORMED ON TASKCARD# 753-140-00-01Y 6679U 24AUG20

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 62,884 hrs · 25,819 cycles

FORWARD CARGO BAY AFT SCUFF PLATE IS CRACKED / RECEIVED NEW FORWARD CARGO BAY AFT SCUFF PLATE; LOCATED AND DRILLED FORWARD CARGO BAY AFT SCUFF PLATE PER SOPM# 51-40-05-0G-0 TO BE INSTALLED ON CUSTOMER CARD# 753-140-00-01Y. 57609U 25AUG20

Part: SKIN — DENTED (BS 1016) · airframe 62,884 hrs · 25,819 cycles

FUSELAGE SKIN HAS A DENT LOCATED AT BS1016+10'; 2' ABOVE S-7L. DAMAGE WAS REPAIRED PER REF B787 SRM 53-80-01-2R-5 REPAIR 5.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 62,884 hrs · 25,819 cycles

LT INBOARD AFT FLAP HAS SKIN DAMAGE ON LOWER SURFACE 5.5' FROM OUTBOARD END; 6' FROM T/E. LT INBOARD AFT FLAP SKIN DAMAGE ON LOWER SURFACE 5.5' FROM OUTBOARD END; 6' FROM T/E WAS REPAIRED IAW SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.

Part: SCREW — MISSING (EMERGENCY LIGHT) · airframe 62,884 hrs · 25,819 cycles

LEFT HAND OVERWING EMERGENCY EXIT FLOOD LIGHT LENS IS MISSING A SCREW; LOCATED ON EXTERIOR OF FUSELAGE JUST AFT OF LEFT HAND EMERGENCY EXIT. LEFT HAND OVER WING EMERGENCY EXIT FLOOD LIGHT LENS MISSING SCREW WILL BE INSTALLED ON DEFECT NUMBER U178904.

Part: SKIN — DENTED (BS 440) · airframe 62,884 hrs · 25,819 cycles

FUSELAGE SKIN DENT AT BS440+13'; 1' ABOVE S-7L. DENT MEASURES AT L=2'; W=1.5'; Y=.040'; W/Y=37.5. REPAIRED AT FUSELAGE SKIN DENT AT BS 440+13'; 1' ABOVE S-7L IAW SRM 53-00-01-2R-3 REPAIR 3 CATEGORY B.

Part: SKIN — DENTED (BS 312) · airframe 62,884 hrs · 25,819 cycles

FUSELAGE SKIN HAS MULTIPLE DENTS ON PREVIOUS REPAIR DOUBLER; BS 312 BETWEEN STR 20R-23R. REMOVED DENTED REPAIR DOUBLER; BS 312 BETWEEN STR 20R-23R AND REPLACED REPAIR PER SRM 53-00-01-2R-36 REPAIR 36.

Part: SHEAR TIE — CORRODED (BS 360) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON SHEAR TIE AT BS 360 BETWEEN STRINGER 25 AND 26 LT. CORROSION ON SHEAR TIE AT BS 360 BETWEEN STR25L-26L FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C. REMOVED AND REPLACED BS360 SHEAR TIE BETWEEN STR25L-26L IAW DWG #141A1171 AND IAW DWG #141A3502.

Part: FRAME — CRACKED (BS 259) · airframe 62,884 hrs · 25,819 cycles

CRACK ON FRAME AT FLIGHT DECK BS259.5 1' BELOW S-12L WL241. MARKED / CRACK ON BS259.5 FRAME; 1' BELOW S-12L WL241 WAS REPAIRED IAW ATS ER 20-03076 REV IR DATED 24AUG20 AND EA-20-153-01536 REV IR.

Part: STRINGER CLIP — CHAFED (BS 259 S16L) · airframe 62,884 hrs · 25,819 cycles

CHAFING ON STRINGER CLIP BS259 S-16L WL216. MARKED / REMOVED AND REPLACED STR CLIP STA.259 STR 16L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20

Part: STRINGER CLIP — CHAFED (BS 259 S10L) · airframe 62,884 hrs · 25,819 cycles

CHAFING ON STRINGER CLIP BS259 S-10L WL253. MARKED / REMOVED AND REPLACED STR CLIP STA.259 STR 10L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20

Part: STRINGER CLIP — CHAFED (BS 259 S8L) · airframe 62,884 hrs · 25,819 cycles

CHAFING ON STRINGER CLIP BS259 S-8L WL263. MARKED / REMOVED AND REPLACED STR CLIP STA;259 STR 8L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG;141A0720. 91195U 8-16-20

Part: CHANNEL — CORRODED (BS 270-259) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON INTERCOSTAL SUPPORT CHANNEL BS270 - BS259 BL0 WL208. MARKED / REMOVED AND REPLACED INTERCOSTAL SUPPORT CHANNEL FROM BS270 TO BS259; BL0; WL208 IAW SRM 51-40-02; DWG 140A9810 AND EA 1-A53-13812 REV 2 DATED 8FEB11.

Part: WEB — CORRODED (BS 253) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON WEB BS253.6 WL207.54 LBL46. MARKED / REMOVED AND REPLACED WEB AT BS253.6; WL207.54 LBL46 IAW SRM 51-40-02-0G-0 AND DWG 141A0631.

Part: STRINGER CLIP — CHAFED (BS 259 S6L) · airframe 62,884 hrs · 25,819 cycles

CHAFING ON STRINGER CLIP BS259 S-6L WL273. MARKED / REMOVED AND REPLACED STR. CLIP STA. 259 STR 6L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20

Part: WEB — CORRODED (BS 278) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON UPPER WEB AT BS278 LBL18 8' WL 184.5 BELOW NOSE WHEEL WELL TOP PANEL, ACCESS PANEL 113BW. MARKED / REMOVED CORROSION ON UPPER WEB AT BS 278, LBL 18, ORIGINAL THICKNESS IS .050'; MAX MAT REMOVED 1.5'X1.6'X.011' REMAINING THICKNESS IS .039' WEB FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED UPPER WEB BETWEEN BS268 TO BS 288; 8' BELOW NOSE WHEEL WELL TOP PANEL #113 BW IAW SRM 51-40-02 AND DWG #141A7500 84632U 14AUG20.

Part: BEAM — CORRODED (BS 270) · airframe 62,884 hrs · 25,819 cycles

CORROSION AT COCKPIT ON FWD SIDE OF BS270 LATERAL BEAM LBL11 - RBL11 WL208. MARKED/REPAIRED BS270 LATERAL BEAN LBL11-RBL11; WL208 PER EA 1-A53-13812 REV.2.

Part: STRINGER CLIP — CHAFED (BS 259 S12L) · airframe 62,884 hrs · 25,819 cycles

CHAFING ON STRINGER CLIP BS259 S-12L WL243. MARKED / REMOVED AND REPLACED STR.CLIP STA.259 STR 12L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20

Part: FLOOR SUPPORT — CORRODED (BS 727A-727B) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON INTERCOSTAL AT ACB BS727A TO 727B LBL17 WL154. REMOVED CORROSION FROM ACB INTERCOSTAL BS727A-TO-727B LBL-17 WL-154 IN AREA L=1'; W=0.8' MORE THAN 50% MATERIAL THICKNESS LOST ORIGINAL MATERIAL THICKNESS 0.045' FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 STEP 4C FIG 103-D. LOCATED AND DRILLED NEW INTERCOSTAL ITEM #146A7505 U3 IAW SRM 51-40-05-0G-0 AND DWG #146A7505 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG #146A7500 AND DWG #146A1201.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON INTERCOSTAL AT AREA AFT OF ACB BS947 - BS967 RBL43 WL190. / REMOVED CORROSION ON INTERCOSTAL AT AREA AFT OF BS947-BS967 RBL967 WL190 IAW SRM 51-10-02. MAX MATERIAL IN 1.25'LX0.75'WX0.009' DEPTH AREA FROM AN ORIGINAL THICKNESS 0.040' MATERIAL LOSS 0.009'. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 ALLOWABLE DAMAGE 1. REMOVED AND REPLACED INTERCOSTAL BS947-967 RBL43 IAW SRM 51-40-02 AND IAW DWG #147A8801.

Part: FLOOR SUPPORT — DAMAGED (BS 727A-727B) · airframe 62,884 hrs · 25,819 cycles

DAMAGED INTERCOSTAL AT ACB BS727A - 727B LBL3 WL156. REMOVED AND INSTALLED NEW INTERCOSTAL AT ACB BS727A- 727B LBL3 ITEM 146A7505 PO# 744027, IAW SRM 51-40-02; SRM 51-40-05; DWG 146A0061 DWG 146A7510, 80641U 12AUG20.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,884 hrs · 25,819 cycles

CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS919 RBL13 WL172. / REMOVED AND REPLACED NEW SUPPORT ANGLE IN ACB BS919 RBL13 WL172 BEHIND WATER SERVICE PANEL PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND BOEING DRAWING # 147A7221. 57006U 12AUG20

Part: CARGO TRACK — CORRODED (BS 888) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON RAIL AT ACB BS888 LBL7 WL168. / REMOVED CORROSION FROM ACB RAIL BS888 LBL-7-WL-168 IN AREA OF L=1.4' W=0.9; D=0.039' DEEP FOUND TO BE OUT OF LIMIT IAW SRM 53-00-33-1A-2 STEP 4.A.(2) FIG 103-D FABRICATED NEW RAIL MADE FROM BAC1509- 100146 #7050T 76511 LOT #1382910-1 AT BS867-BS947 LBL-8 WL-168 IAW DW #147A7501 APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 31-20-01-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG #147A7500 REV-B

Part: CARGO TRACK — CRACKED (BS 727E-767) · airframe 62,884 hrs · 25,819 cycles

CRACKED FLOOR TRACK AT ACB BS727E - BS767 LBL17 WL155. / EVALUATED CRACK ON FLOOR TRACK BS727E-BS767 LBL17 WL155 CRACK EXCEEDS MORE THEN .10' FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED ACB FLOOR TRACK BS727-867 LBL17 WL155 I.A.W SRM 53-00-53-1A-2; SRM 51-40-02-0G-0 AND BOEING DWG# 146A7500

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON RAIL SUPPORT ANGLE AT ACB BS727C LBL8 WL154. / REMOVED AND REPLACED RAIL SUPPOR ANGLE AT ACB BS 727C LBL 8 WL 154 PO # 800791-SWA IAW SRM 51-40-02 AND DWG 146A1310

Part: FLOOR SUPPORT — CORRODED (BS 927-947) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON INTERCOSTAL AT AREA AFT OF ACB BS927 - BS947 RBL46 WL187. REMOVED AND REPLACED NEW INTERCOSTAL AT BS927-947 RBL46 WL187 IN ACB PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 53-70-15-1A-1 AND BOEING DRAWING #147A8801. 57006U 17AUG20.

Part: STRINGER CLIP — CORRODED (BS 727D) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON STRINGER CLIP AT ACB BS727D LBL15 WL154. REMOVED AND REPLACED NEW CLIP AT BS727 LBL15 WL154 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-10-02-0G-0. 57006U 12AUG20.

Part: SUPPORT — CORRODED (BS 727-807) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - 807 LBL21 WL156. / REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT ACB BS 727-BS 847 LBL 21 WL 156 ITEM # 7532037 IAW SRM 53-60-53-01-2; SRM 53-00-53-1A-2 SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500

Part: STRINGER CLIP — CORRODED (BS 727C) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON STRINGER CLIP AT ACB BS727C LBL15 WL154. / REMOVED AND REPLACED ON STRINGER CLIP AT ACB BS 727C LBL 15 NEW ITEM 146A1010-34 PO# 800189 IAW SRM 51-40-05; SRM 51-40-02 AND DWG 146A1202. 80641U 15AUG20

Part: ATTACH ANGLE — CORRODED (BS 767) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON STRINGER ATTACH ANGLE AT ACB BS767 RBL6 WL151. / REMOVED AND REPLACED ON STRINGER ATTACH ANGLE AT ACB BS 767 RBL 6 ITEM 146A1320-13 PO # 800187 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 146A7810 80641U 18AUG20

Part: SHIELD — CORRODED (AFT CARGO) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON FWD SHIELD AT ACB BS767 - BS787 RBL22 WL156. / CORROSION FOUND ON ACB FWD SHIELD BS 767 - BS 787 RBL-22 WL-156 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLAEMENT IAW SRM 51-10-02-0G-0. PAR-9C LOCATED AND DRILLED NEW SHIELD ITEM # 7531132 IAW SRM 51-40-05-0G-0 AND DWG # 146A0081 AND INSTALLED IAW SRM 51-40-02-0G0 AND DWG # 146A0081 REV-A

Part: CHANNEL — DAMAGED (BS 727A-727B) · airframe 62,884 hrs · 25,819 cycles

DAMAGED RAIL AT ACB BS727A - 727B LBL3 WL156. REPAIRED RAIL AT ACGB BS727A-727B LBL 3 WL 156. REMOVED AND REPLACED CHANNEL SECTION BS 727+8 TO BS 727C LBL 3 WITH CHANNEL SPLICE AT BS 727C RBL 3 IAW SRM 53-00-53-2R-4. 89064U 17AUG20.

Part: ANGLE — CORRODED (BS 947) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS947 RBL53 WL199. DAMAGE FOUND ON ACB STRINGER CLIP AFT OF BS 947 FRAME RBL-53 WL-199 FOUND TO BE OUT OF LIMIT, DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLACMENT IAW SRM 51-10-02-0G-0. FABRICATED STRINGER CLIP MADE FROM BAC 1493-853 # 7075T62C LOT # 1344261-1 IAW SRM 51-40-05-0G-0 AND DWG # 147A3500-61 AND DWG # 147A3500. APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-20-01-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG # 147A0020

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727B - 767 RBL21 WL156. / REMOVED AND REPLACED NEW FLOOR TO SIDEWALL SUPPORT AT ACB BS727-BS767 RBL21 PER SRM 51-40-02-0G-0; BOEING DRAWING 146A7500; SRM 53-00-53-1A-2 AND SRM 51-10-02. 57006U 11AUG20

Part: CARGO TRACK — CORRODED (BS 747) · airframe 62,884 hrs · 25,819 cycles

CORROSION ON TRACK TIEDOWN AT ACB BS747 RBL13 WL156. REMOVED CORROSION ON TRACK TIE DOWN AT ACB BS747 RBL13 WL156. REWORKED AREAS L=0.5 W=0.25 D=0.045' TOP SURFACE AND L=1.8' W=0.8' D=0.028 BOTTOM SURFACE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB TRACK BS727+4 TO BS 887 WITH SPLICE AT BS747+8; RBL13 IAW SRM 51-40-02; SRM 53-00-53-2R-3 REF DWG 146A7500 89004U 14AUG20.

Part: SEAT TRACK — DAMAGED (BS 727-727C) · airframe 62,884 hrs · 25,819 cycles

DAMAGED RAIL AT ACB BS727A - 727B RBL3 WL156. / REMOVED AND REPLACED RAIL SECTION BS 727+8 TO BS 727C RBL 3 WL 156 FABRICATED AND INSTALLED SPLICE CHANNEL AT BS 727C FABRICATED FROM CHANNEL 7530199 IAW SRM 53-00-53-2R-4 .

Part: SUPPORT — CORRODED (BS 400-420) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** IN FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 400-420; R.B.L. 23; W.L. 154. / REMOVED AND INSTALLED IN FCB FLOOR TO SIDEWALL SUPPORT 135 400-420 RBL23 NEW ITEM BAC1496-444 #707ST62 CLAD LOT NO. 1389311-2 IAW SRM 51-40-02; SRM 51-40-05; SRM 53-30-53-01-2; DWG 143A7501 AND DWG 143A7500. 80641U 11AUG20

Part: BOOT — DAMAGED (RADOME) · airframe 62,884 hrs · 25,819 cycles

NOSE RADOME BOOT IS DAMAGED. / REMOVED DAMAGED RADOME BOOT AND INSTALLED NEW RADOME BOOT IAW AMM 53-52-00-000-802 AND AMM 53-52-00-400-802. 6645U 08/13/20.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** IN FORWARD CARGO BAY ON SHIELD SUPPORT AT B.S. 494-500A; R.B.L. 23; W.L. 154. / REMOVED AND REPLACED IN FORWARD CARGO BAY SHIELD SUPPORT FROM BS 494 TO BS 500A RBL 23 WL 154 IAW SRM 51-40-02 AND DWG 193A0080

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 62,884 hrs · 25,819 cycles

CORROSION IN FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 400-500D; L.B.L. 23; W.L. 154. REMOVED AND INSTALLED NEW IN FCB ON FLOOR TO SIDEWALL SUPPORT AT BS400-500D LBL23 FROM BAC 1496-444 #7075T62 CLAD LOT #1437457-1 IAW SRM 51-40-02 SRM 53-30-12-01-2; SRM 53-00-53-2R-6; SRM 51-20-01 AND DWG 143A7500; 143A7501 80641U 15AUG20.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** IN FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 500A-500D; R.B.L. 23; W.L. 154. / REMOVED AND INSTALLED NEW IN FCB FLOOR TO SIDEWALL SUPPORT AT BS500A-500D RBL23 ITEM BAC 1496-444 #7075T62 LOT# 1435481-1 IAW SRM 51-40-02; SRM 53-30-53-01-2; SRM 51-40-05; AMM 51-21-72-370-804; DWG 143A7500. 80641U 13AUG20

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 62,884 hrs · 25,819 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS597 S-5L. MARKED / REMOVED AND REPLACED STRINGER CLIP STA.597 S&R 5L PER SRM 51-40-02; SRM 51-40-05 AND DWG. 144A1103; 91195U 8-8-20.

Part: STRINGER CLIP — CRACKED (BS 639) · airframe 62,884 hrs · 25,819 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS639 S-8R WL282. MARKED/REMOVED AND REPLACED STRINGER CLIP STA.639 STRINGER 8R PER SRM 51-40-02; SRM 51-40-05 AND DWG. 144A1108; 91195U 8-8-20.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 62,884 hrs · 25,819 cycles

PASSENGER CABIN FLOOR PANEL 232RF UPPER SURFACE HAS MULTIPLE AREAS OF DAMAGE. MARKED PASSENGER CABIN FLOOR PANEL 232RF WITH UPPER SURFACE HAS MULTIPLE AREAS OF DAMAGE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY2 LOT # 1399953-1; BMS 5-107 LOT # AK9GP5303K-2 DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0. PARA. 1.A. NOTE; 5.S.(1); DWG 144A5810-17.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 62,884 hrs · 25,819 cycles

PASSENGER CABIN FLOOR PANEL 232SF HAS DAMAGE ON UPPER SURFACE 52' FROM FWD EDGE; 1' FROM OUTBOARD EDGE. DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 232SF FABRICATED NEW PANEL FROM BMS 4-23 TY2 LOT # 1437364-1 IAW SRM 53-00-50-2R-0 PARA 1A NOTE & TABLE 204 & DWG 144A5810-14. 57885U 08-03-2020 10537C 08/03/20 INSTALLED INSERTS USING BMS 5-107 LOT # AK9GP5303K-1 IAW SRM 53-00-50-2R-0. PARA. 5.S.(1); DWG 144A5810-14.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 62,884 hrs · 25,819 cycles

PASSENGER CABIN FLOOR PANEL 241CF HAS DAMAGE ON UPPER SURFACE 13' FROM AFT EDGE; 1' FROM IB EDGE. DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 241CF; FABRICATED NEW PANEL FROM BMS 4-23 TY2 LOT # 1399953-1 IAW SRM 53-00-50-2R-0 PARA 1A NOTE; TABLE 204 & DWG 144A5810-21. 57885U 08-04-2020 10537C 08/04/20 INSTALLED ALL INSERTS USING BMS 5-107 LOT # AK9GP5303K-1 IAW SRM 53-00-50-2R-0 PARA 5.2(1); DWG 144A5810-21.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 62,884 hrs · 25,819 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. REMOVED THE DAMAGED PART AT RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STA 129.50; 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW. SRM 55-10-09-2R-4 55920U 11AUG20

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 62,884 hrs · 25,819 cycles

PASSENGER CABIN FLOOR PANEL 241BF HAS DAMAGE ON UPPER SURFACE 10' FROM FWD EDGE ; 2' FROM OUTBOARD EDGE. PASSENGER CABIN FLOOR PANEL 241BF WITH DAMAGE ON UPPER SURFACE 10' FROM FWD EDGE; 2' FROM OUTBOARD EDGE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY 2 LOT # 1437364-1; BMS 5-107 LOT # AK9GP5305K-1 DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0. PARA. 1.A. NOTE; 5.S.(1); DWG 144A5810-18.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 62,884 hrs · 25,819 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ACCOMPLISHED FLIGHT DECK FLOOR REPAIR FROM BS 255 TO 270; RBL10 TO LBL17 WL 207.54 IAW EA 1-A53-33179 REV 1 DATED 28MAY19.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 62,884 hrs · 25,819 cycles

CRACKED FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. REMOVED AND REPLACED FLOOR SUPPORT STA.540 BL-O TO RBL 24 PER SRM 51-40-02; SRM 51-40-05 AND DWG. 143A5240 91195U 8.9.20.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 62,884 hrs · 25,819 cycles

CRACK AT FASTENER ON #7 SLAT ON LOWER SURFACE SLAT NOSE SKIN AT ACTUATOR RIB ATTACH POINT. REMOVED THE DAMAGE PART AT #7 SLAT ON LWR SURFACE SLAT NOSE SKIN AT ACTUATOR RIB ATTACH POINT AND INSTALLED REPAIR PARTS IAW. SRM 5742012R8. 88920U 14AUG20

Part: SKIN — CHAFED (WING) · airframe 62,884 hrs · 25,819 cycles

FAIRING 542BB INNER SKIN I/B I-BEAM IS CHAFED. (MARKED) / REMOVED AND REPLACED WORN/CHAFFED INNER SKIN I/B I-BEAM COMMON TO 542BB AFT FLAP TRACK FAIRING IAW SRM 51-40-02-0G-0 REF DRAWING NUMBER 113A9550 REV. F 57053U 28AUG20

Part: FLOORBEAM — CRACKED (BS 540) · airframe 62,884 hrs · 25,819 cycles

CRACKED FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. REMOVED AND REPLACED FLOOR PANEL SUPPORT AT BS540; B.L0 - LBL24.5 WL.208.1 IAW SRM 51-40-02-0G-0 DWG 143A5240.

Part: BONDING JUMPER — CORRODED (RT WING) · airframe 62,884 hrs · 25,819 cycles

***CORROSION*** UNDER UPPER BONDING JUMPER ATTACH PO INT OF RIGHT FORWARD BOOST PUMP AT IFSS 120. REPAIRED CORROSION UNDER UPPER BONDING JUMPER ATTACH POINT OF RIGHT FWD BOOST PUMP AT IFSS 120 PER EA 2015701610 REV IR AND ER 2003053 REV. IR.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 62,612 hrs · 25,653 cycles

R/H INBOARD AFT FLAP DAMAGED. / R&R AFT FLAP PER AMM.

Part: SLIDING SLEEVE — CRACKED (RH HOR STAB) · airframe 61,989 hrs · 25,228 cycles

RIGHT HORIZONTAL L/E ;LOWER SLIDE DEFORMED AND CRACK. / REMOVED AND REPLACED LOWER SLIDER REF AMM 53-31-31.

Part: SLIDING SLEEVE — CRACKED (LH HOR STAB) · airframe 61,989 hrs · 25,228 cycles

LEFT HORIZONTAL L/E ;LOWER SLIDE DEFORMED AND CRACK. / REMOVED AND REPLACED LOWER SLIDER REF AMM 53-31-31.

Part: HOOK — BROKEN (L1 DOOR GIRT BAR) · airframe 61,666 hrs · 25,039 cycles

L1 DOOR SLIDE GIRT BAR SUPPORT HOOK BROKEN. / REPAIRED RETAINER CLIP PER EA.

Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 61,590 hrs · 24,989 cycles

L1 DOOR SLIDE BAR L/H SIDE FELL OUT WHILE OPENING FORWARD ENTRY DOOR. / SECURED GIRT BAR IAW AMM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 61,159 hrs · 24,699 cycles

L1 DOOR GIRT BAR "J" HOOK ON LOOSE. SECURED GAP ON GIRT BAR HOOK PER SIP.

Part: NUT PLATE — CRACKED (L2 DOOR) · airframe 59,945 hrs · 23,875 cycles

L2 DOOR FORWARD SLIDE ATTACHMENT STANDOFF'S LOWER ISOLATOR NUT PLATE CRACKED. R&R NUTPLATE PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,523 hrs · 23,006 cycles

L1 DOOR SLIDE GIRT BAR OUT OF POSITION. R&R SLIDE PER MM AND MT.

Part: HOLDER — DAMAGED (FLASHLIGHT) · airframe 58,512 hrs · 23,001 cycles

FORWARD WINDSCREEN LOWER EMERGENCY FLASHLIGHT DAMAGED HOLDER. R&R HOLDER IAW SOPM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 58,512 hrs · 23,001 cycles

GALLEY 1 EMERGENCY EXIT LIGHT WIRE BROKEN AT BS 293, RBL 51. R&R LIGHT PER AMM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

AFT CARGO BAY SHIELD FORWARD OF THE DOOR CORRODED BETWEEN BS 787 TO BS 794, RBL 23. R&R SHIELD PER SRM & DWG.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 58,512 hrs · 23,001 cycles

VERTICAL STIFFENER ON AFT SIDE OF BS 663 L/H VAPOR BARRIER LBL27 LOWER END IS CRACKED / REPLACED VERTICAL STIFFENER ON AFT SIDE OF BS 663 L/H VAPOR BARRIER LBL 27 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 111A1000; & DWG 149A7210

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500 TO BS 500D, LBL 23. R&R SUPPORT IAW SRM.

Part: SKIN — CRACKED (L/H WING) · airframe 58,512 hrs · 23,001 cycles

LT WING #3 SLAT MIDDLE FLEX SKIN IS CRACKED. / REMOVED #3 SLAT MIDDLE FLEX SKIN PER SRM 51-40-02-0G-0. 5318R 01NOV18 INSTALLED NEW MIDDLE FLEX SKIN PER SRM 51-40-02-0G-0 AND DWN # 114A5030

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 58,512 hrs · 23,001 cycles

LT LOWER VAPOR BARRIER CRACKED AT BS 663, LBL 25. REPAIRED BARRIER IAW SRM.

Part: ANGLE — CRACKED (ASD) · airframe 58,512 hrs · 23,001 cycles

AFT GALLEY DOOR LOWER PANEL 844DZ AFT SUPPORT ANGLE IS CRACKED. / REPLACED AFT GALLEY DOOR LOWER PANEL 844DZ AFT SUPPORT ANGLE IAW SRM 51-40-02-0G-0 57798U 14NOV18

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 58,512 hrs · 23,001 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE PER ER AND EA.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 58,512 hrs · 23,001 cycles

RT HORIZONTAL STIFFENER CRACKED AT BS 663, ON INBOARD END ON THE FORWARD SIDE OF THE LOWER VAPOR BARRIER. REPAIRED STIFFENER PER SRM AND DWG.

Part: PLATE — CRACKED (R/H WING) · airframe 58,512 hrs · 23,001 cycles

IB WIGGLE PLATE FOR PANEL 651GB IS CRACKED / REMOVED AND REPLACED I/B WIGGLE PLATE FOR PANEL 651GB IAW SRM 51-40-02-0G-0 AND SOPM 20-50-01

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 58,512 hrs · 23,001 cycles

AFT CABIN FLOOR PANEL 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE; REPLACED AFT CABIN FLOOR PANEL 242XF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 220. 57066U 10/29/18

Part: BRACKET — CRACKED (LEFT WING) · airframe 58,512 hrs · 23,001 cycles

LT WING TE SEAL RETAINER SUPPORT BRACKET ABOVE PYLON TIP IS CRACKED / REMOVED CRACKED LT WING T/E SEAL RETAINER SUPPORT BRACKET ABOVE #1 PYLON TIP. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-40-02-0G-0 PARA 4. AND IPC 57-50-00-25.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

FORWARD CARGO BAY BULKHEAD ANGLE CORRODED AT BS 500D, LBL 22. R&R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO BS 294, RBL 1. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R SUPPORT IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

FORWARD CARGO BAY BULKHEAD GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 492 TO BS 440, RBL 25. R&R WEB IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 58,512 hrs · 23,001 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS 727D HAS CORROSION / RECEIVED NEW ACB FLOOR SPLICE STRAP FOR B.S 727D ON PO #705890. FOR PART'S TRACKING ONLY.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 58,512 hrs · 23,001 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS 787 HAS CORROSION / RECEIVED NEW ACB FLOOR SPLICE STRAP FOR B.S 787 ON PO # 709587. FOR PART'S TRACKING ONLY.

Part: PLATE — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL PLATE CORRODED BETWEEN BS 727 TO BS 767, RBL 23. R&R PLATE PER SRM & DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL PLATE CORRODED BETWEEN BS 727 TO BS 847, LBL 23. R&R PLATE PER SRM AND DWG.

Part: STANCHION — CRACKED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

AFT CARGO BAY LOWER LAV BULKHEAD STANCHION CLIP CRACKED AT BS 847. R&R STANCHION CLIP PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,512 hrs · 23,001 cycles

SUB THRESHOLD WEB CORRODED BETWEEN BS 787 TO BS 827, RBL 25. R&R WEB IAW SRM & DWG.

Part: STIFFENER — CRACKED (WHEEL WELL LH) · airframe 58,512 hrs · 23,001 cycles

L/H HORIZONTAL STIFFNER IS CRACKED ON INBOARD END ON THE FWD SIDE OF THE LOWER 663 VAPOR BARRIER / LOCATED; DRILLED; DEBURRED L/H HORIZONTAL STIFFNER; PER SRM 51-40-05-0G-0 DWG 111A1001; PART REMOVED AND INSTALLED ON CUSTOMER CARD T861052.

Part: FORMER — CRACKED (LOWER EXT FUSELA) · airframe 58,512 hrs · 23,001 cycles

BS500D FAIRING FORMER JUST ABOVE STR19L IS CRACKED / REMOVED AND REPLACED FRAME (FAIRING FORMER) AT BS 500D STA 19L PER SRM 51-40-02 & DWGS 116A3010; 116A3110

Part: SKIN — CRACKED (SLAT) · airframe 58,512 hrs · 23,001 cycles

CRACK ARROUND (MARKED) FASTENERS AT SLAT #3 ACTUATOR ATTACH POINT / REPAIRED #3 SLAT LOWER BULL NOSE SKIN COMMON TO ACTUATOR RIBS ATTACHED POINT PER SRM 57-42-01-28-8.

Part: BEAM — CRACKED (FSD) · airframe 58,512 hrs · 23,001 cycles

DURING INSPECTION OF CUSTOMER CARD #14079 FOUND #4 LOWER BEAM CRACKED AT INBOARD RADIUS MOST FORWARD ATTACH POINT OF HANDLE BOX. / CRACKED #4 LOWER BEAM AT INBOARD RADIUS MOST FWD ATTACH POINT OF HANDLE BOX WAS REPAIRED ON CUSTOMER RO NO 05200 55-CRR

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 58,512 hrs · 23,001 cycles

LT LOWER VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 5 TO LBL 15. REPAIRED BARRIER IAW SRM.

Part: SLAT — CRACKED (R/H WING) · airframe 58,512 hrs · 23,001 cycles

CRACK ARROUND (MARKED) FASTENERS AT SLAT #8 ACTUATOR ATTACH POINT / REPAIRED #8 SLAT LOWER BULL NOSE SKIN COMMON TO ACTUATOR RIBS ATTACHED POINT PER SRM 57-42-01-2R-8.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 57,960 hrs · 22,650 cycles

R1 DOOR SLIDE GIRT BAR INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 57,647 hrs · 22,439 cycles

FWD CARGO BIN FLOOR CRACKED (OUT OF SERVICE). / REMOVED AND REPLACED THE FWD CARGO BIN FLOOR PER AMM 25-52-10.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 57,370 hrs · 22,272 cycles

L2 DOOR ESCAPE SLIDE HOUSING NEAR GIRT BAR STRAP OUT OF POSITION. REPOSITION SLIDE IAW MT.

Part: HOOK AND LOOP — MISSING (EMERGENCY EXIT) · airframe 57,329 hrs · 22,248 cycles

LT OVERWING EMERGENCY EXIT ASSIST ROPE COVER VELCRO MISSING. R&R ROPE COVER IAW SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,855 hrs · 21,947 cycles

R1 DOOR SLIDE OUT OF POSITION. R & R THE SLIDE ASSY IAW MM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 56,341 hrs · 21,640 cycles

AFT CARGO AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO AFT CORNER SCUFF PLAE IAW EA #1-A53-2076 REV 11.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 56,341 hrs · 21,640 cycles

AFT CARGO FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO FWD CORNER SCUFF PLATE IAW EA #1-A53-2076 REV 11.

Part: SKIN — CRACKED (BS 827) · airframe 56,342 hrs · 21,640 cycles

AFT CARGO DOOR CUTOUT CRACKED AT BS 827, STRINGER 25R. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,341 hrs · 21,640 cycles

***LOG BOOK ENTRY*** PG 0631368 TRANSFERRED FROM NRWC 0263112. WHILE PERFORMING HFEC IAW EA 1-753-32343 REV 1 FOUND CRACK INDICATION 3' LONG BELOW AFT CARGO DOOR @ STA827 STR25R. HFEC DONE PER 737 NDT PT6 51-00-00 PROC 23. VERIFIED WITH 10X MGNIFYING GLASS AND PENETRANT INSPECTION. / BLENDED AND REMOVED DAMAGE ON FUSELAGE SKIN BELOW AFT CARGO DOOR AT STA 827 STR 25R. ACCOMPLISHED HFEC OF BLENDED AREA NO DEFECTS NOTED FABRICATED REPAIR DOUBLER AND INSTALLED IAW EA 180116 REV IR AND S/W EA 1-753-32351 REV IR. PRIOR TO BLENDOUT OF SUSPECTED CRACKED AREA ACCOMPLISHED FPI AND HFEC OF FUSELAGE SKIN NO CRACK NOTED IAW SOPM 20-20-02 AND B737 NDT PT6 51-00-00 P23. ORG 'T' AT BLENDED AREA 080' WITH .016' MATERIAL LOSS AN

Part: ENGINE — DAMAGED (NR 1) · airframe 55,848 hrs · 21,327 cycles

AIR TURNBACK, LEFT ENGINE VIBRATION 4.1. PULLING BACK WILL REDUCE. R&R NR 1 ENGINE FAN BLADE PLATFORM PER MT.

Part: LENS — LOOSE (CABIN) · airframe 55,200 hrs · 20,912 cycles

LT OVERHEAD BULL NOSE EMERGENCY LIGHT LENS LOOSE AT ROW 6. R&R LENS IAW AMM.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 53,612 hrs · 19,944 cycles

AFT CARGO FLOOR DECK MATERIAL DELAMEATED CENTER FLOOR IN FRONT OF DOOR THRESHOLD APPROX 4.0' BY 2.0' / R & R AFT CARGO FLOOR PANEL IAW M/M 25-52-10

Part: FUSE — INOPERATIVE (CABIN) · airframe 52,059 hrs · 18,998 cycles

LT OVERWING EXIT SIGN INOP. R&R FUSE PER AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 52,059 hrs · 18,998 cycles

LT OVERWING ESCAPE HATCH LIGHT INOP. R&R FUSE PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,059 hrs · 18,998 cycles

R1 EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,059 hrs · 18,998 cycles

L1 EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,059 hrs · 18,998 cycles

RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

STRINGER CORRODED BETWEEN BS 344 TO BS 400, STR 25L. R&R STRINGER IAW SRM.

Part: SUPPORT — CORRODED (BS 294-300) · airframe 52,059 hrs · 18,998 cycles

INTERCOSTAL SUPPORT CORRODED BETWEEN BS 294 TO 300, STRINGER 23L. R & R THE INTERCOSTAL SUPPORT IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

STRINGER CORRODED AT BS 380, STR 23L. R&R STRINGER IAW SRM.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

FORWARD BULKHEAD PANEL SUPPORT CORRODED AT BS 727, LBL 45. R&R SUPPORT IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

ELECTRONIC AND EQUIPMENT COMPARTMENT ATTACH FITTING CORRODED AT BS 330.62, STR 23L. REPAIRED FITTING IAW ER AND EA.

Part: ATTACH FITTING — CORRODED (BS 320) · airframe 52,059 hrs · 18,998 cycles

ELECTRONICS AND EQUIPMENT COMPARTMENT ATTACH FITTING CORRODED AT BS 320, STRINGER 23L. R & R THE ATTACH FITTING IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

ELECTRONIC AND EQUIPMENT COMPARTMENT OUTER CHORD CORRODED AT BS 336, BETWEEN STR 22L TO STR 23L. R&R CHORD PER ER AND EA.

Part: ATTACH FITTING — CORRODED (BS 300) · airframe 52,059 hrs · 18,998 cycles

ELECTRONICS EQUIPMENT COMPARTMENT ATTACH FITTING CORRODED AT BS 300, STRINGER 23L. R & R THE ATTACH FITTING IAW SRM.

Part: ATTACH FITTING — CORRODED (BS 336) · airframe 52,059 hrs · 18,998 cycles

ELECTRONICS AND EQUIPMENT COMPARTMENT ATTACH FITTING CORRODED AT BS 336, STRINGER 23L. R & R THE ATTACH FITTING IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

FRAME CORRODED AT BS 336, BETWEEN STR 22L TO STR 23L. R&R FRAME IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

ELECTRONIC AND EQUIPMENT COMPARTMENT OUTER CHORD CORRODED AT BS 320, BETWEEN STR 22L TO STR 23L. R&R CHORD PER ER AND EA.

Part: FRAME — CORRODED (BS 320) · airframe 52,059 hrs · 18,998 cycles

ELECTRONICS AND EQUIPMENT COMPARTMENT FRAME CORRODED AT BS 320, BETWEEN STRINGERS 22 - 23L. R & R FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

CENTER WING BOX UPPER SKIN PANEL CRACKED AT BS 540+7, RBL 15.04. REPAIRED SKIN IAW ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

STRINGER CORRODED AT BS 380, STR 24L. R&R STRINGER IAW SRM.

Part: SKATE ANGLE — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

VERTICAL FIN RT SKATE ANGLE CORRODED AT BS 1121. R&R SKATE ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AIR STAIR LOWER AUXILIARY SILL WEB CORRODED BETWEEN BS 294.5 TO BS 351.2, BETWEEN STR 23L TO STR 24L. R&R WEB IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

R1 DOOR FORWARD STUB FRAME LOWER HOLE CRACKED AT BS 295. REPAIRED FRAME IAW ER AND EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 52,059 hrs · 18,998 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70, SECOND FROM FORWARD VERTICAL STIFFENER AT LOWER END. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 52,059 hrs · 18,998 cycles

RT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STA 92.70, 3RD VERTICAL STIFFENER AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 52,059 hrs · 18,998 cycles

RT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STA 92.70, 2ND FROM FORWARD SPAR AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

PRESSURE DOME WEB CRACKED AT BS 1016, RBL 10. REPAIRED WEB IAW ER AND EA.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT PRESSURE BULKHEAD SKIN OIL CANNING AT BS 1016, BETWEEN STR 2R TO STR 3R. REPAIRED SKIN IAW ER AND EA.

Part: TAB — CORRODED (RT AILERON) · airframe 52,059 hrs · 18,998 cycles

RT WING AILERON BALANCE TAB HINGE NR 2 ROD END CORRODED. R&R TAB IAW CMM.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

FRAME SPLICE CORRODED AT BS 727D, STR 25R. REPAIRED FRAME SPLICE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, LBL 8. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, LBL 3. REPAIRED FLOORBEAM PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

LAV TANK PANEL SUPPORT CORRODED AT BS 847, STR 25L. REPAIRED SUPPORT IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 727D+5, RBL 3. REPAIRED FLOORBEAM PER SRM AND EA.

Part: FRAME — CRACKED (BS 500B) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGERS 21 & 22L. REPAIRED THE FRAME IAW ER AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT CARGO DOOR CUTOUT INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 794, STR 25R. R&R INTERCOSTAL IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT CARGO DOOR CUTOUT SHIELD CORRODED BETWEEN BS 847 TO BS 867, STR 25R. R&R SHIELD PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

AFT CARGO DOOR CUTOUT INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 856, STR 25R. R&R INTERCOSTAL PER SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 52,059 hrs · 18,998 cycles

LT NR 1 FLIGHT DECK WINDOW FRAME CRACKED AT UPPER AFT CORNER. REPAIRED FRAME PER ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

LT NR 3 WINDOW FRAME E-F POST SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST PER CUSTOMER CARD.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 52,059 hrs · 18,998 cycles

RT NR 1 FLIGHT DECK WINDOW FRAME CRACKED AT UPPER AFT CORNER. REPAIRED FRAME PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 827) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 500A) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500A) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 500A STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,059 hrs · 18,998 cycles

RT CREASEBEAM WEB CORRODED AT BS 337. REPAIRED WEB PER ER AND EA.

Part: FRAME — CRACKED (BS 827) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 440) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 440 STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 480) · airframe 52,059 hrs · 18,998 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 52,059 hrs · 18,998 cycles

RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB PER SRM.