N720WN

Part: PLATE — CRACKED (L/H WING) · airframe 78,481 hrs · 46,766 cycles

LT WING LOWER T/E SHELF PANEL 551GB FWD SUPPORT BRACKET(WIGGLE PLATE) CRACKED. ; / [01] REMOVED AND REPLACED LT WING LOWER T/E SHELF PANEL 551GB FWD SUPPORT BRACKET(WIGGLE PLATE) PER SRM 51-40-02 AND 20-50-11; [02] REMOVED AND REPLACED LT WING LOWER T/E SHELF PANEL 551GB FWD SUPPORT BRACKET(WIGGLE PLATE) PER SRM 51-40-02 AND 20-50-11

Part: NONE — STUCK (L1 DOOR) · airframe 77,875 hrs · 46,388 cycles

FWD ENTRY DOOR SLIDE ACTIVATION HANDLE COVER IS STUCK UNDER BEZEL ; / [01] REPOSITIONED HANDLE COVER PER AMM 25-66-01

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 77,140 hrs · 45,972 cycles

FWD ENTRY SLIDE OUT OF ADJUSTMENT ; / [01] PERFORMED ADJUSTED OF THE FWD ENTRY SLIDE PER AMM 25-66-01; SLIDE DOESN'T REQUIRED REMOVED ASSEMBLY. OPS CHECK GOOD; NO DEFECT NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,351 hrs · 44,935 cycles

LT OVERWING EMERGENCY EXIT INSIDE + OUTSIDE LIGHTS ARE INOPERABLE. R & R LT OVERWING EMERGENCY EXIT LIGHT CHARGER ASSEMBLY & BATTERY PACK, IAW AMM 33-51-06.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,351 hrs · 44,935 cycles

LT OVERWING EMERGENCY EXIT INSIDE + OUTSIDE LIGHTS ARE INOPERABLE. R&R LT OVERWING EMERGENCY EXIT LIGHT CHARGER ASSEMBLY & BATTERY PACK, IAW AMM 33-51-06.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 75,351 hrs · 44,935 cycles

PANEL 193B HAS ELONGATED FASTENER HOLES. / REPLACED PANEL193B PER SRM 51-40-02 AND EO#14108

Part: SKIN — DEBONDED (VERTICAL STAB) · airframe 75,226 hrs · 44,854 cycles

WHILE PERFORMING TASK CARAD 712-00-21 POST DOCK INTERMEDIATE CHECK-GENERAL WALK AROUND SAFETY INSPECTION. FOUND AT VERTICAL FIN R/H MOST LOWERD FIN PANEL DEBONDED AND MISSING HARDWARE. (PANEL 324 ER) / FABRICATED NEW PANEL IAW BOEING DWG 175A1601 AND REINSTALLED 324ER

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,929 hrs · 44,674 cycles

LEFT OVER WING EMERGENCY EXIT SIGN HAS BURNED OUT BULBS. REPLACED THE BULB IN LEFT OVERWING EMERGENCY EXIT SIGN AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,929 hrs · 44,674 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT SIGN HAS BURNED OUT BULBS. REPLACED THE BULBS IN FOWARD SERVICE DOOR EMERGENCY EXIT SIGN AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-01-960-801.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 74,929 hrs · 44,674 cycles

FORWARD ENTRY LOCATOR SIGN HAS BURNED OUT BULBS. REPLACED THE BULBS IN FOWARD ENTRY LOCATOR SIGN AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-01-960-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,929 hrs · 44,674 cycles

EMERGENCY EXIT AISLE LIGHT AT ROW 17LEFT WAS INOPERATIVE. REPLACED THE LAMPS AND PERFORMED A GOOD FUNCTIONAL TEST IAW AMM 33-51-03-960-801.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,929 hrs · 44,674 cycles

EMERGENCY LIGHTS POWERED BY BATTERY PACK M1670 ARE INOPERATIVE. / REPLACED BATTERY PACK M1670 AND PERFORMED GOOD FUNCTIONAL TEST AS PER AMM 33-51-06-960-805.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 74,929 hrs · 44,674 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY AT CORNER SCUFF PLATE PER SRM #53-30-15-2B-1 TO BE INSTALLED ON CUSTOMER CARD #753-140-00-01Y. 37609U 22JUL20

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,929 hrs · 44,674 cycles

BS 927 - 947 INTERCOSTAL LOWER FLANGE FWD 2 HOLES COMMON TO SKIN ELONGATED / DRILLED (2EA) HOLES AT INTERCOSTAL FLANGE IAW SRM 51-40-05 FIG. 3+0 .228. 91195U 7-16-20. AT STA. 927-947 RBL3 WL175 91195U 7.16.20. 2EA HOLES WILL BE INSTALLED ON NRC U192866. 91195U 7.18.20.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 74,929 hrs · 44,674 cycles

RIGHT WING T/E PANEL 661AB AFT SUPPORT BEAM IS CRACKED / REMOVED RIGHT WING TE PANEL 661AB AFT SUPPORT BEAM IAW SOPM 20-50-01 6148C 20JUL20. RECIEVED NEW BEAM; INSTALLED NUT PLATES ONTO NEW BEAM IAW SRM 51-40-02-0G-0; REINSTALLED AFT SUPPORT BEAM IAW SOPM 20-50-01.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 74,929 hrs · 44,674 cycles

RH FIN-TO-BODY INTERFACE CLOSURE (SKATE) ANGLE CHAFED ALONG I/B SURFACE; BS 1016 TO 1066; APPROX. STR-3R / REMOVED AND REPLACED SKATE ANGLE BETWEEN BS 1016 TO BS 1121 APPROX STR 3R PER SRM 51-40-02 AND DWG 148A3590

Part: BAFFLE — CRACKED (BS 460-480) · airframe 74,929 hrs · 44,674 cycles

FWD CARGO BAY BAFFLE IS CRACKED AT BS 460-480 LBL21 / REMOVED AND REPLACED FCB BAFFLE BS460-480 LBL21 P/N 143A7510-13 IAW SRM 51-40-02 REF DWG 143A7505

Part: BAFFLE — CRACKED (BS 440-460) · airframe 74,929 hrs · 44,674 cycles

FWD CARGO BAY BAFFLE IS CRACKED AT BS 440-460 LBL21 / REMOVED AND REPLACED FCB BAFFLE BS440-460 LBL21 P/N 143A7510-9 PO #798079 IAW SRM 51-40-02 REF DWG 143A7505 89004U 16JUL20

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 74,929 hrs · 44,674 cycles

FWD CARGO BAY BAFFLE IS CRACKED AT BS 500A-500B LBL21 / REMOVED AND REPLACED FCB. BAFFLE BS500A-500B LBL21 P/N 143A7510-11; IAW SRM 51-40-02 REF DWG 143A7505 89004U 16JUL20

Part: BAFFLE — CRACKED (BS 400-420) · airframe 74,929 hrs · 44,674 cycles

FWD CARGO BAY BAFFLE IS CRACKED AT BS 400-420 LBL21 / REMOVED AND REPLACED F.C.B. BAFFLE BS400-420 LBL21 P/N 143A7510-33 IAW SRM 51-40-02 REF DWG 143A7505 89004U 16JUL20

Part: STRINGER CLIP — DAMAGED (BS 907) · airframe 74,929 hrs · 44,674 cycles

DAMAGED STRINGER CLIP AT BS 907, LBL 5, WL 168. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05, SRM 51-40-02, AND DWG 147A0040 91195U 7-18-20.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON STRINGER CLIP AT ACB BS 947. REMOVED AND REPLACED STRINGER CLIP AT ACB IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-10-02 AND BOEING DRAWING 147A7410.

Part: CARGO TRACK — CORRODED (BS 727-727B) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON TRACK AROUND FASTENER HOLES AT ACB BS727 - BS727B RBL13 WL156. / TRACK TIE DOWN REMOVED AND REPLACED ACB AT BS727-BS727B RBL3 IAW NRC U192840

Part: SUPPORT — CORRODED (BS 807) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS807 LBL21 WL157. / REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT ACB BS 727 - BS 847 LBL 21 WL 157 PER SRM 51-40-02-0G-0; SRM 53-00-53-1A-2; 51-10-02; SRM 53-60-53-01-02 AND BOEING DRAWING 146A7500 ITEM # 7532037.

Part: STRINGER CLIP — CORRODED (BS 827) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON STRINGER CLIP AT ACB BS 827. REMOVED AND REPLACED STR CLIP STA. 827 PER SRM 51-40-02- SRM 50-40-05 AND DWG. 146A1280. 9115U 7-18-20 (NO SRM CORROSION ALLOWABLE LIMITS)

Part: ATTACH ANGLE — CORRODED (BS 766) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON STRINGER ATTACH ANGLE AT ACB BS766 RBL5 WL152. / REMOVED AND REPLACED STR. ATTACH ANGLE STA. 766 RBL5 WL152 PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A7810.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157. / REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT ACB B.S. 727 - BS 767 RBL 21 WL 157 ITEM # 7530898 IAW SRM 53-00-53-1A-2 AND SRM 51-10-02-0G-0; SRM 53-60-53-0I-2; SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG # 146A7502; DWG # 146A2500.

Part: SHIELD — CORRODED (BS 847-867) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** ON AFT SHIELD AT ACB BS847 - BS867 RBL21 WL164. / REMOVED AND INSTALLED NEW AFT SHIELD AT ACB BS. 847-867 RBL21 WL164 ITEM #7530336 IAW SRM 51-40-02-0G-0 AND DWG #146A0081

Part: FRAME SPLICE — CORRODED (AFT CARGO) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON FRAME AT ACB BS 787, RBL 26, WL 158. REMOVED AND REPLACED SPLICE ON ACB FRAME ITEM 146 A130003 IAW SRM 51-40-02-0G-0 AND DWG 146A1262.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON STRINGER CLIP AT ACB BS807 LBL14 WL156. / REMOVED AND REPLACED STR. CLIP STA. 807 LBL14 PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A1263. 91195U 7.18.20 (NO CORROSION SRM ALLOWABLE LIMITS)

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT ACB BS727D+6 LBL18 TO RBL18 WL156. / RECEIVED NEW/SERVICABLE FLOOR SUPPORT SPLICE AT ACB BS 727D+6 LBL18 TO RBL18 TO BC INSTALLED ON JPANEL-141-CLOSE; 57609U 21JUL20

Part: SHEAR TIE — CORRODED (BS 907) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON SHEAR TIE AT ACB BS 907 LBL 7 WL 165. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-40-05, AND DWG 147A0040.

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON STRINGER CLIP AT ACB BS 847, LBL 6 WL 160. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05; SRM 51-40-02 AND DWG. 146A1010.

Part: FLOOR SUPPORT — CORRODED (BS 727A-727B) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON INTERCOSTAL AT ACB BS 727A - 727B, LBL 3, WL 154. REMOVED CORROSION FROM ACB INTERCOSTAL, AREA OF 1' X 1' ORIGINAL MATERIAL THICKNESS, 0.036 REMAINING MATERIAL THICKNESS 0.099 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2, FIG 103. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 AND DWG 146A7505, AND INSTALLED IAW SRM 51-40-02-0G-0, DWG 146A7500, AND 146A7510.

Part: SPAR — CORRODED (RT WING) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** ON RIGHT WING REAR SPAR AROUND BOOST PUMP UPPER BONDING JUMPER IRSS145. MARKED / CORROSION ON RIGHT WING REAR SPAR AROUND BOOST PUMP UPPER BONDING JUMPER IRSS 145 WAS REPAIRED ON ATS ER 20-02904 REV IR AND SWA EA 20-157-01189 REV IR.

Part: ATTACH ANGLE — CRACKED (BS 865) · airframe 74,929 hrs · 44,674 cycles

CRACKED BULKHEAD ATTACH ANGLE AT ACB BS865 LBL10 WL 167. / REMOVED AND REPLACED B/H ATTACH ANGLE STA.865 LBL10 WL167 PER SRM 51-40-02; SRM 51-40-05 AND DWG. 149A8102 9118U 7.21.20

Part: CARGO TRACK — CORRODED (BS 764) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON TRACK AROUND FASTENER HOLE AT ACB BS764 RBL13 WL157. / REMOVED AND REPLACED TRACK TIE DOWN ACB AT BS727 TO BS887 IAW SRM 51-40-02-0G-0 DWG 146A7500 AND INSTALLED SPLICE REPAIR AT BS747+10 RBL13 WL157 IAW SRM 53-00-53-2R-3-REPAIR 3. 59205U 20JUL20

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** ON STRINGER CLIP AT ACB BS727C RBL15 WL154. / REMOVED AND REPLACED STR CLIP STA 727C RBL15 PER SRM 51-40-02; SRM 51-40-05 AND DWG 146A1702 91195U 7-18-20 (NO SRM CORROSION ALLOWABLE LIMITS)

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** FORWARD CARGO BAY AFT BULKHEAD RIGHT HAND PANEL LOWER SUPPORT AT B.S. 500D; R.B.L. 24; W.L. 154. / REMOVED AND INSTALLED NEW FCB AFT BULKHEAD R/H PANEL LOWER SUPPORT AT BS 500D RBL19-24 ITEM 7530202 PO #782418 IAW SRM 51-40-02 AND DWG 143A7902; DWG 143A9481 80648U 16JUL20

Part: SUPPORT — CORRODED (BS 494-500A) · airframe 74,929 hrs · 44,674 cycles

CORROSION FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 494 - 500A, RBL 23, WL 154. CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS PER SRM REPAIRABLE BY REPLACEMENT. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 143A0080.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 400 - 500D, LBL 23, WL 154. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, DWG 143A7500, AND SRM 53-00-53-2R-6.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 500D; L.B.L. 23 - R.B.L. 23; W.L. 154. / REMOVED AND REPLACED NEW FCB AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS500D LBL23-RBL23 ITEM 7530142 PO #795904 IAW SRM 51-40-02 AND DWG 143A9481 REV.A. 80641U 15JUL20

Part: SUPPORT — CORRODED (BS 420-440) · airframe 74,929 hrs · 44,674 cycles

CORROSION ON THE FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 420 - 440, RBL 23, WL 154. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT. LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A0080.

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 74,929 hrs · 44,674 cycles

CORROSION FORWARD CARGO BAY DOOR CUTOUT THRESHOLD SUB WEB AT BS 440 - 494, WL 154, RBL 25. REMOVED FCB SUB THRESHOLD WEB IAW SRM 51-40-02. OUT OF LIMITS IAW SRM 53-30-15-1A-1. ORIG; MAT'L THICKNESS .045. REMAINING THICKNESS .033 AFTER CORROSION REMOVAL IAW SRM 51-10-02. LOCATED, DRILLED, AND INSTALLED A NEW WEB IAW SRM 51-40-02, DWG. 143A8330, AND DWG 143A8120.

Part: BOOT — DAMAGED (RADOME) · airframe 74,929 hrs · 44,674 cycles

NOSE RADOME BOOT IS DAMAGED / REMOVED NOSE RADOME BOOT AND INSTALLED NEW NOSE RADOME BOOT IAW AMM 53-52-00-000-802; AMM 53-52-00-400-802

Part: WINDOW FRAME — CORRODED (BS 220) · airframe 74,929 hrs · 44,674 cycles

***CORROSION*** CORROSION ON CAPTAIN SIDE #4 WINDOW PLUG SURROUND STRUCTURE APPROXIMA TELY BS 220; LBL 26 ; WL 273 (MARKED) / CORROSION ON CAPTAIN SIDE # WINDOW PLUG SURROUND STRUCTURE APPROX. BS 220 LBL 26 WL273 WAS REPAIRED IAW EA 20-153-01224 REV IR DATED 07/28/2020 & ATS ER 20-02865 REV IR DATED 07/28/2020

Part: FLOORBEAM — CRACKED (BS 540) · airframe 74,929 hrs · 44,674 cycles

CRACKED FLOORBEAM, BS 540, BL 0 - LBL 24.5, WL 208.1. REMOVED THE CABIN FLOORBEAM IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW FLOORBEAM ANGLE IAW SRM 51-40-05-0G-0, AND DWG 143A5240, REV-B. AND INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060, REV-B.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 74,929 hrs · 44,674 cycles

L/W #2 SLAT NOSE SKIN IS CRACKED AT FASTENER HOLE AT ACTUATOR RIB (MARKED) / REMOVED #2 SLAT; #2 SLAT WAS REPAIRED ON ATS WORK ORDER #533969; INSTALLED SERVICEABLE #2 SLAT AND ADJUSTED AND FUNCTIONAL TEST IAW MM 27-81-21-000-801 AND MM 27-81-21-400-801 ADJUSTMENT/TEST CHECK GOOD (POS:2; TAG NO:721858; P/N OFF:114A5020-3; S/N OFF:000120; P/N ON:14A5020-3; S/N ON:000120)

Part: COVER — OUT OF POSITION (R2 DOOR) · airframe 73,610 hrs · 43,858 cycles

SUPPLEMENTAL INFORMATION, COVER FOR MANUAL RELEASE AFT SERVICE DOOR SLIDE OFF. REINSTALLED COVER OVER MANUAL SLIDE RELEASE ON AFT SERVICE PER MT 725-62-01.

Part: WEB — CORRODED (BS 260) · airframe 73,426 hrs · 43,746 cycles

UPPER SURFACE OF VERTICAL WEB CORRODED AT BS. 260, BETWEEN LBL 10 TO BL 0. / REPAIRED WEB PER EA AND ER.

Part: FLOOR SUPPORT — CORRODED (BS 260) · airframe 73,426 hrs · 43,746 cycles

FLOOR SUPPORT CHANNEL CORRODED AT BS. 260, BL 0. / R&R FLOOR SUPPORT CHANNEL IAW DWG & SRM.

Part: FAILSAFE — CORRODED (BS 260) · airframe 73,426 hrs · 43,746 cycles

UPPER SURFACE UPPER FAIL SAFE CHORD CORRODED AT BS. 260, BETWEEN LBL 33 TO RBL 33. / R&R "FAIL SAFE" CHORD IAW SRM AND DWG.

Part: WEB — CORRODED (BS 260) · airframe 73,426 hrs · 43,746 cycles

UPPER SURFACE VERTICAL WEB CORRODED AT BS. 260, BETWEEN BL 0 TO RBL 10. / REPAIRED WEB PER EA & ER.

Part: FLOORBEAM — CORRODED (BS 260) · airframe 73,426 hrs · 43,746 cycles

SUBSTRUCTURE CORRODED AT BS. 260, BETWEEN LBL 4 TO RBL 10 ON UPPER SURFACE OF AFT CHORD. / REPAIRED AFT CHORD IAW ER AND EA.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 72,671 hrs · 43,241 cycles

RIGHT FWD O/B LWR WHEEL WELL PANEL HAS A CRACK @ APPROX 13' 5/8 FROM OUTTER EDGE & 9' 3/4 FROM AFT EDGE MEASURING AT APPROX .406' L X .031' W ONE FACE SHEET ONLY. (BAG SIDE-INNER SURFACE).PANEL 193 AR MOD / REMOVED WING TO BODY FAIRING PANEL 193AR PER AMM 53-51-21-000-802 STEPS 4E3(B)2) 57006U 09JUL20 LEAD 216 09JUL20 REPAIRED CRACK ON INNER SURFACE OF PANEL 193AR; 13 5/8' FROM OUTER EDGE; 9 3/4' FROM AFT EDGE IAW SRM 53-40-70; SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11 LEAD 236 07/15/20 INSP 14 15JUL20 REINSTALLED BODY FAIRING PANEL 193AR IAW AMM 53-51-400-802 59781U 15JUL20

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 72,033 hrs · 42,838 cycles

L2 DOOR SLIDE PRESSURE GAUGE INDICATION OUT OF LIMITS. / R&R SLIDE PER MT.

Part: FLOOR SKIN — DAMAGED (COCKPIT) · airframe 71,994 hrs · 42,819 cycles

FOUND COCKPIT FLOOR SKIN CREASED ALONG CHANNEL AT BS. 258, LBL 15.33. / REPAIRED SKIN IAW EA.

Part: FLOOR SKIN — DAMAGED (COCKPIT) · airframe 71,994 hrs · 42,819 cycles

FOUND COCKPIT FLOOR SKIN CREASED ALONG CHANNEL AT BS. 258, LBL 4. / REPAIRED SKIN IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 71,685 hrs · 42,627 cycles

L1 DOOR ESCAPE SLIDE DROPPED, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLEEVE — DELAMINATED (LH NACELLE) · airframe 71,532 hrs · 42,529 cycles

#1 T/R OUTBOARD SLEEVE TRAILING EDGE HAS AREA OF DELAMINATION MOD / ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-05 CL #40579

Part: SLEEVE — DELAMINATED (LH NACELLE) · airframe 71,532 hrs · 42,529 cycles

#1 ENGINE O/B T/R SLEEVE HAS AREA OF DELAMINATION / ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-05. CL #40579

Part: CABLE — CORRODED (LT MLG) · airframe 70,471 hrs · 41,840 cycles

LT MAIN LANDING GEAR MANUAL EXTENSION CABLE MAIN LANDING GEAR-L CABLE D CORRODED AT CABLE DRUM. R&R CABLE PER AMM AND EA.

Part: BATTERY — FAILED (CABIN) · airframe 70,471 hrs · 41,840 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER MM.

Part: CABLE — CORRODED (RT MLG) · airframe 70,471 hrs · 41,840 cycles

RT MAIN LANDING GEAR MANUAL EXTENSION CABLE MAIN LANDING GEARED-R CABLE B CORRODED AT CABLE DRUM. R&R CABLE IAW EA AND AMM.

Part: BATTERY — FAILED (CABIN) · airframe 70,471 hrs · 41,840 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,430 hrs · 41,810 cycles

LT AFT OVERHEAD BIN EMERGENCY LIGHT INOP. R&R COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,430 hrs · 41,810 cycles

LT AFT OVERHEAD BIN EMERGENCY LIGHT INOP. R&R BULB IAW AMM.

Part: PLATE — CRACKED (R/H WING) · airframe 70,430 hrs · 41,810 cycles

RH WING TRAILING EDGE MLG STRUT WELL LOWER PANEL WIGGLE PLATE IS CRACKED RSS 229. / REMOVED & REPLACED R/H WING TRAILING EDGE MLG STRUT WELL LOWER PANEL WIGGLE PLATE P/N 115A2781-4 ATAG LD 1555 IAW SRM 51-40-02-0G-0 & DWG 115A2001 SHT 1 REV B.

Part: PLATE — BROKEN (R/H WING) · airframe 70,430 hrs · 41,810 cycles

RH WING TRAILING EDGE MLG STRUT WELL LOWER PANEL WIGGLE PLATE HAS BROKEN FASTENERS / CRACKS RSS 212-219. / REMOVED & REPACED R/H WING TRAILING EDGE MLG STRUT WELL LOWER PANEL WIGGLE PLATE P/N 115A2781-202 ATAG LD1561 IAW SRM 51-40-02-0G-0& DWG 115A2001 SHT 1 REV B.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 70,430 hrs · 41,810 cycles

RIGHT WING LOWER TRAILING EDGE STIFFENER BETWEEN PANELS 651FB AND 651EB FORWARD ATTACH FITTING CRACKED / REMOVED & REINSTALLED #6 FORWARD FAIRING & PANEL 651 EB TO REPAIR FORWARD ATTACH FITTING IAW AMM 27-51-18-000-801; AMM 27-51-18-400-801 SRM 51-40-02 A68563

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

THIRD TIER- FOUND LOWER SILL MIDDLE SUPPORT CRACKED UNDER SILL WEB AT BS 817. R&R WEB IAW SRM & DWG.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 70,430 hrs · 41,810 cycles

RT AC BAY VAPOR BARRIER WEB UPPER CHORD CRACKED AT BS 663, RBL 6. REPAIRED CHORD IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

FORWARD SIDE OF BULKHEAD VAPOR BARRIER VERTICAL STIFFENER T ANGLE CRACKED AT BS 663, LBL 6. R&R STIFFENER IAW DWG & SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

LOWER E&E COMPARTMENT STRINGER END FITTING SHIM CORRODED AT BS 362, STR 28L. R&R FITTING IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

INTERCOSTAL CORRODED AT BS 343, STR 23L. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO BAY INTERCOSTAL STA.907 TO STA.927 LBL 21 HAS CORROSION AT 2 EACH FASTNERS / MARKED / REMOVED CORROSION AT STA 907 TO 927 LBL 21 IAW SRM 53-00-53-1A-2 FIG 12 SHEET 1. VERIFIED MATERIAL LIMITS. REMOVED .016' REMAINING .055' ORIG. MAT. .071'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED INTERCOSTAL AT STA 907 TO 927 LBL21 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 & DWG 147A7401 REV C. APPLIED CIC IAW 737-700 AMM 51-21-91-620-802

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

FORWARD CARGO BAY RT Z ANGLE CORRODED BETWEEN BS 500 TO BS 500D. R&R Z ANGLE IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO BAY STRINGER CORRODED BETWEEN BS 928 TO BS 967, STR 25L. R&R STRINGER IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 492.5 TO BS 500A. REPAIRED SHIELD PER SRM.

Part: BRACKET — CRACKED (LEFT WING) · airframe 70,430 hrs · 41,810 cycles

LH WING DEFLECTOR RIB TO TOP WING PANEL L-BRACKET CRACKED BETWEEN FASTNERS / REMOVED AND REPLACED BRAKET ON L/H WING ON DEFLECTOR RIB IAW BOEING 737 SRM 51-40-02

Part: SUPPORT — CORRODED (FWD CARGO LH) · airframe 70,430 hrs · 41,810 cycles

FWD CARGO BAY STA 500D BETWEEN STR 25L AND 21L SIDEWALL SUPPORT STRUCTURE IS CORRODED IN SEVERAL AREAS TOP SURFACE AS MARKED / REMOVED CORROSION L/H SIDEWALL SUPPORT @500D 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SIDEWALL SUPPORT P/N 7530854 ATAG WN8816 IAW BOEING 737-700 SRM 53-00-53-1A-2 FIG 103 DETAIL C SHEET 2. BOEING DWG 143A9485 REV D. #AAR 36307 DUE 10-17-18

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

FORWARD CARGO BAY BETWEEN LT Z ANGLE CORRODED BETWEEN BS 400 TO BS 500B. R&R Z ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO BAY STA 986.5 AND 1006.5 BETWEEN STR 25L AND 24L GREY WATER/ DRAIN MAST SUPPORT STRUCTURE ON INSIDE AS MARKED HAS (INTERGRANULAR CORROSION) / REMOVED AND REPLACED GREY/WATER DRAIN MAST SUPPORT STRUCTURE IN AFT CARGO BAY AT STA 9865-1006.5 DUE TO FOUND TO BE OUT OF LIMITS WITH 100% MATERIAL LOSS WITH A TAG DC1516 IAW BOEING DWG 147A7443 REVB

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 70,430 hrs · 41,810 cycles

RT MAIN WHEEL WELL VAPOR BARRIER BULKHEAD CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO; RH SPLASH SHIELD JUST AFT OF CARGO DOOR HAS CORROSION FROM STA 847 TO 867; UPPER AND LOWER SURFACE. / REMOVED AND EVALUATED CORROSION FOUND 100% MATERIAL LOSS; BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT CARGO DOOR AFT SHIELD PER DWG 146A0081 REV C AND SRM 51-40-02-0G-0

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

RIGHT HAND SPLASH SHIELD;. JUST FWD OF AFT CARGO DOOR HAS CORROSION ON UPPER AND LOWER SURFACE / REMOVED & REPLACED R/H SPLASH SHIELD FWD OF AFT CARGO DOOR DUE TO BEING OUT OF LIMITS WITH 100% MATERIAL LOSS USING ATAG ANN5340 IAW SRM 51-40-02

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

LH SIDE WALL SUPPORT STRUCTURE HAS CORROSION AROUND NUT PLATE HOLE; STA 727D; JUST O/B OF Z-ANGLE / REMOVED CORROSION AT AFT CARGO LH WALL SUPPORT STA 727D IAW SRM 51-10-02 VERIFIED WITH 10X MAG. VERIFIED LIMITS. ORIG T = .063 LOSS .015 REM T .048. FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1FIG 102 DET C SHEET 1. RECEIVED AND VERIFIED NEW PART P/N 7531776 ATAG WN3270. LOCATED AND DRILLED PER SRM 51-40-05 & DWG 146A9403 RE AE INSTALLED NEW LH SIDEWALL SUPPORT AT STA 727D PER SRM 51-40-02 & DWG 146A9403 REV AE

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO COMPARTMENT SIDEWALL TO FLOOR TRANSITION STRIP R/H/S AFT; IS CORRODED IN SEVERAL AREAS TOP AND BOTTOM SURFACES AS MARKED / REMOVED CORROSION AND FOUND AFT CARGO COMPART SIDEWALL TO FLOOR STRANSITION STRIP R/H/S AFT TO BE OUT OF LIMITS. DRILLED AND LOCATED NEW STRIP WITH P/N 453A2611-3 AND A TAG WN0697 IAW AIPC 25-52-10-02 AND SRM 51-10-02 AND SRM 51-40-05.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO DOOR CUTOUT EXTERNAL SKIN CORRODED BETWEEN BS 794 TO BS 847, STR 25R. REPAIRED SKIN IAW SRM & EA.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO COMPARTMENT SPLICE ON BOTH SIDES SEVERAL AREAS OF CORROSION PART # 463A241-1 / REMOVED CORROSION AND FOUND AFT CARGO COMP SPLICE P/N 453A2411-1 TO BE OUT OF LIMITS IAW SRM 51-00-53-1A-2 AND VERIFIED NEW SPLICE WITH ATAG A14635 IAW BOEING DWG 453A2411 REV C.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO RT Z-ANGLE CORRODED BETWEEN BS 727B TO BS 767. R&R Z ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

STRINGER CLIP CORRODED AT BS 747, STR 26L. R&R CLIP PER SRM & DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

RH SIDE WALL SUPPORT STRUCTURE HAS CORROSION AROUND NUT PLATE HOLE; STA 727D; JUST O/B OF Z-ANGLE / REMOVED AND REPLACED R/H SIDEWALL SUPPORT STRUCTURE AT STA STA 727D AND FOUND TO BE OUT OF LIMITS WITH ORIG .063 LOSS OF .019 REMAINING .044 WITH BACKSHOP W/O 38120-1600-0001 IAW SRM 51-40-02; BOEING DWG 146A1220 REV - AND BOEING DWG 146A9403 REV AE.

Part: WEB — DEBONDED (CABIN) · airframe 70,430 hrs · 41,810 cycles

PASSENGER CABIN BETWEEN STA 663.5 AND 685 STR 5R METAL GLUE ON WEB DISBONBED FROM STR AS MARKED / REBONDED METAL GLUE ON WEB A+ STR 5; FROM STA 663.5 AND 685 IAW SOPM 20-50-12 PARA (AR) STEPS (2B&D) AND BOEING ENGINEERING DRAWING 144 A1906 REV LETTER (A)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 767+3, STR 27R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO COMPARTMENT AFT CARGO DOOR CUTOUT THRESHOLD PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO COMPARTMENT FWD CARGO DOOR CUTOUT; TRESHOLD PLATE IS CRACKED / RECIEVED AND LOCATED AND DRILLED NEW AFT CARGO COMP FWD CARGO DOOR CUTOUT THRESHOLD PLATE WITH ATAG WN0355 PN 146A8341-5 IAW SRM 51-40-05 AND BOEING DWG 146A8341 REV B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

FLOOR SUPPORT RAIL CORRODED AT BS 767+6, RBL 8. REPAIRED SUPPORT PER SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

LT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 727E+12. R&R Z ANGLE IAW DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO LT Z-ANGLE CORRODED BETWEEN BS 727E TO BS 787+3. R&R Z ANGLE IAW DWG AND SRM.

Part: BAFFLE — CORRODED (AFT CARGO COMPT) · airframe 70,430 hrs · 41,810 cycles

AFT CARGO; RH BAFFLE BELOW Z-ANGLE IS CORRODED AT NUT PLATE HOLES; STA 747-767 / REMOVED CORROSION AT RH BAFFLE ON NUTPLATE HOLES AT STA 747-767. UPON FURTHER INVESTIGATION FOUND PUNCTURE. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-14-2 PAR. C. RECEIVED AND VERIFIED NEW BAFFLE INTERCOSTAL P/N 7531031 ATAG LD1501. LOCATED AND DRILLED INTERCOSTAL P/N 753103 AT STA 747-767 RH STR25R INSTALLED NEW BAFFLE INTERCOSTAL AT STA 747-767 STR25R PER SRM 51-40-02. DRILLED PER DWG 146A7505_REV. -

Part: ANGLE — BROKEN (LOWER EXT FUSELA) · airframe 70,430 hrs · 41,810 cycles

LOWER KEEL BEAM FAIRING SUPPORT ANGLE BROKEN OFF AT STA. 540 + 11' / REMOVED & REPLACED LOWER KEEL BEAM FAIRING SUPPORT ANGLE AT STA 540 + 11' IAW SRM 51-40-02-09-0 & DWG 149A7701 SHT 1 REV - A12190.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,430 hrs · 41,810 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.

Part: INTERCOSTAL — CRACKED (R1 DOOR) · airframe 70,430 hrs · 41,810 cycles

R1 DOOR INTERCOSTAL CRACKED BELOW NR 4 WEB BEAM. R&R INTERCOSTAL IAW SRM AND DWG.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 70,430 hrs · 41,810 cycles

LEFT WING ACCESS PANEL 521DB; L/E IS DELAMINATED 2 PLACES. / REPAIRED LT WING ACCESS PANEL 521DB IAW SRM 57-41-01-2R-6 REV. 65 RESTORED FINISH TO PANEL IAW AMM 51-21-99-300-801 REV.66

Part: BEAM — CRACKED (FSD) · airframe 70,430 hrs · 41,810 cycles

CARD #I14079 CRACK FOUND ON 141A6536-15 BEAM / REMOVED AND REPLACED R1 DOOR #5 BEAM IAW SRM 51-4-02-0G-0 AND BOEING DWG 141A6516 REV F ATAG: WN3808

Part: BEAM — CRACKED (FSD) · airframe 70,430 hrs · 41,810 cycles

CARD # I14079 CRACK FOUND ON 141A6536-14 BEAM / REMOVED AND REPLACED R1 DOOR #4 BEAM IAW SRM 51-40-02-0G-0 AND BOEING DWG 14A6516 REV F. ATAG: WN2226

Part: PANEL — DELAMINATED (LH PYLON) · airframe 70,154 hrs · 41,631 cycles

#1 ENGINE INBOARD PANEL 431 ER DAMAGED & DELAMINATED DELAMINATED APPROXIMATELY 5 LAYERS DAMAGE EXTENDS 8 1/2' FROM FWD EDGE TO AFT EDGE OF PANEL. 10 INCHES WIDE DIAGONALLY 3 1/4' WIDE & 6' WIDE FORMING ON 'L' SHAPE THRUST REVERSER SEAL JUST FORWARD OF PANEL HAS DAMAGED AND MISSING A SECTION / RPLED PANEL PER AMM 54-53-01 AND SEAL PER SIP

Part: BALLAST — INOPERATIVE (CABIN) · airframe 70,143 hrs · 41,624 cycles

LT OVERWING EXIT LIGHT INOP. R&R LIGHT BALLAST IAW MM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 69,843 hrs · 41,437 cycles

FORWARD CABIN PHOTOLUMINESCENT LIGHTING INOP BETWEEN BS 342 TO BS 360, LT SIDE. R&R STRIP PER AMM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 69,843 hrs · 41,437 cycles

FORWARD CABIN PHOTOLUMINESCENT LIGHTING INOP BETWEEN BS 328 TO BS 354, RT SIDE. R&R STRIP PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 69,661 hrs · 41,314 cycles

L1 DOOR SLIDE LOOSE. SECURED SLIDE PER MM.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,811 hrs · 40,110 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,811 hrs · 40,110 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: BALANCE WEIGHT — CRACKED (RUDDER) · airframe 54,720 hrs · 31,787 cycles

CORROSION ON RUDER MID COUNTER BALANCE WEIGHT / REMOVED AND REPLACED RUDDER MIDCOUNTER WEIGHT IAW CMM 55-40-09

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 66,843 hrs · 39,492 cycles

VERTICAL FIN RH SIDE PANEL 323CR LOWER SKATE ANGLE RETAINER BRACKET IS CRACKED / R&R VERTICAL FIN RH SIDE PANEL 323CR LOWER SKATE ANGLE RETAINER BRACKET PER SRM 51-40-02

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 66,843 hrs · 39,492 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. ADJUSTED GIRT PER MT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,995 hrs · 37,754 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK M1668 INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

CHANNEL CORRODED AT BS 348, LBL 68. R & R CHANNEL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

L1 DOOR MOPSIL SUPPORT WEB CORRODED BETWEEN BS 312 TO BS 347. R & R WEB ASSEMBLY IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 63,995 hrs · 37,754 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 344, LBL 47. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

FLOORBEAM CORRODED AT BS 328, RBL 42. REPAIRED FLOORBEAM IAW EA.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 63,995 hrs · 37,754 cycles

L1 DOOR FORWARD GIRT BAR SUPPORT FITTING CORRODED AT BS 312, WL 208.1. R & R THE FITTING IAW AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

L1 DOOR OTBD THRESHOLD SUPPORT CORRODED BETWEEN BS 312 TO BS 336. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R & R INTERCOSTAL IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

R1 DOOR FORWARD LOWER STUB BEAM FRAME CRACKED BETWEEN BS 294-BS 295, WL 209. REPAIRED FRAME IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

L1 DOOR INBD THRESHOLD SUPPORT CORRODED BETWEEN BS 309 TO BS 340. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 63,995 hrs · 37,754 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294 TO 312, RBL 15. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,995 hrs · 37,754 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, WL 208. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,995 hrs · 37,754 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 47. R & R THE FLOOR SUPPORT IAW SRM.

Part: SHEAR WEB — CORRODED (BS 1016) · airframe 63,995 hrs · 37,754 cycles

SHEAR WEB UPPER SURFACE CORRODED AT BS 1016, BETWEEN BL 0 TO LBL 36. R & R THE SHEAR WEB IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

R2 DOOR MOP SILL SPLICE CORRODED BETWEEN BS 1000 TO BS 1016, RBL 45. R & R SPLICE IAW SRM.

Part: STRAP — CORRODED (BS 1019-1023) · airframe 63,995 hrs · 37,754 cycles

SHEAR WEB STRAP UPPER SURFACE CORRODED BETWEEN BS 1019 TO 1023, RBL 3. R & R THE STRAP IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

FLOORBEAM UPPER SURFACE CHORD CORRODED AT BS 986.5, BETWEEN LBL 50 TO RBL 50. REPAIRED CHORD IAW EA & ER.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,995 hrs · 37,754 cycles

RIGHT HORIZONTAL PRESSURE DECK CRACKED AT BS 672, RBL 42. REPAIRED DECK IAW ER AND EA.

Part: PRESSURE DECK — CRACKED (BS 665) · airframe 63,995 hrs · 37,754 cycles

LEFT HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665, LBL 33. REPAIRED PRESSURE WEB PER EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 770. R & R SPLICE IAW SOPM.

Part: CREASE BEAM — CORRODED (BS 706-727) · airframe 63,995 hrs · 37,754 cycles

CREASE BEAM CORRODED BETWEEN BS 706 TO 727, RBL 64. REPAIRED THE CREASE BEAM IAW EA AND ER.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R WEB IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 767 TO 787, RBL 22. R & R THE SHIELD IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,995 hrs · 37,754 cycles

LEFT WING TRAILING EDGE RSS 280 UPPER PANEL SUPPORT CRACKED AT THE PROGRAM TRACK ROLLER FITTING. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

FORWARD CARGO BAY CORRODED ON LOWER BULKHEAD SUPPORT CHANNEL, CORRODED AT BS 500D, BETWEEN STR 26R TO STR 26L. R & R CHANNEL IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 495 TO BS 500A, STR 26R. R & R SHIELD IAW SRM & DWG.

Part: WEB — CORRODED (BS 685-697) · airframe 63,995 hrs · 37,754 cycles

WEB CORRODED BETWEEN BS 685 - 697, LBL 67. R & R THE WEB IAW DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 715 TO BS 727, LBL 67. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (BS 706-727) · airframe 63,995 hrs · 37,754 cycles

CREASE BEAM CORRODED BETWEEN BS 706 TO 727, LBL 64. REPAIRED CREASE BEAM IAW ER AND EA.

Part: SUPPORT CHANNEL — CORRODED (BS 500A) · airframe 63,995 hrs · 37,754 cycles

FORWARD CARGO BAY SUPPORT CHANNEL CORRODED AT BS 500A+10, BL 0. R & R THE SUPPORT CHANNEL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO BAY INTERCOSTAL WEB CORRODED BETWEEN BS 727A TO BS 727B, RBL 3. R & R INTERCOSTAL IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 767, RBL 22. R & R SIDEWALL SUPPORT IAW SRM.

Part: CARGO TRACK — CRACKED (BS 767) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO TRACK CRACKED BS 767, RBL 14. R & R THE CARGO TRACK IAW SRM.

Part: SUPPORT ANGLE — CRACKED (BS 867) · airframe 63,995 hrs · 37,754 cycles

AFT CARGO BAY EQUIPMENT BAY SUPPORT ANGLE CRACKED AT BS 867, LBL 13. R & R THE SUPPORT ANGLE IAW SRM.

Part: SHIELD — CORRODED (BS 420-440) · airframe 63,995 hrs · 37,754 cycles

FORWARD CARGO BAY CORRODED ON SIDE SHIELD CORRODED BETWEEN BS 420 - 440, STRINGER 26R. R & R THE SHIELD IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 490-500A) · airframe 63,995 hrs · 37,754 cycles

FORWARD CARGO BAY CORRODED ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 490 TO 500A, STRINGER 26L. R & R THE SIDWALL SUPPORT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,995 hrs · 37,754 cycles

RIGHT WING NR 5 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 5 SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,995 hrs · 37,754 cycles

RIGHT WING NR 6 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 6 SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,995 hrs · 37,754 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 3 SLAT SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,995 hrs · 37,754 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 62,789 hrs · 37,026 cycles

VERTICAL STABILIZER PANEL 324AL SKATE ANGLE CHAFED. REPAIRED ANGLE IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 62,464 hrs · 36,840 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,728 hrs · 36,423 cycles

RIGHT OVERHEAD BIN BULLNOSE EMER LIGHT INOPERATIVE AT ROW 8. R & R LIGHT IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 61,728 hrs · 36,423 cycles

RIGHT OVERWING AFT EMER EXIT SIGN INOPERATIVE. R & R BATTERY SUPPLY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 60,708 hrs · 35,820 cycles

RIGHT LOWER EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 60,708 hrs · 35,820 cycles

LEFT FWD UPPER EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 60,708 hrs · 35,820 cycles

RIGHT AFT EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 59,629 hrs · 35,192 cycles

R1 DOOR EMER EVAC SLIDE REPOSITIONED. REPOSITIONED SLIDE IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,049 hrs · 34,339 cycles

L1 DOOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 57,624 hrs · 34,093 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CASE. R & R SLIDE IAW AMM & MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,624 hrs · 34,093 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 400 BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 787 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 360 BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 400 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 440 BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 500A BETWEEN STRINGER TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 440 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 747 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

FRAME CRACKED AT BS 747 BETWEEN STRINGER 8R TO 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

STRINGER CLIP CRACKED AT BS 360 STRINGER 8R. R & R STRINGER CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B LBL 45. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B LBL 24. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B RBL 45. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,624 hrs · 34,093 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B RBL 24. REPAIRED BEAM IAW EA.

Part: SUPPORT — CRACKED (VERTICAL STAB) · airframe 57,624 hrs · 34,093 cycles

VERTICAL STAB INTERNAL FWD SUPPORT WEB STRINGER 8L FRAME CRACKED. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,416 hrs · 33,975 cycles

RIGHT EMER EXIT LIGHT INOPERATIVE AT ROW 7. R & R BULB IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,276 hrs · 33,890 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 57,254 hrs · 33,879 cycles

L2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,982 hrs · 33,141 cycles

CEILING AFT ENTRY CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,982 hrs · 33,141 cycles

FORWARD ENTRY CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,982 hrs · 33,141 cycles

MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK, RT NR 3 WINDOW CUT OUT FWD WINDOW FRAME CRACKED AT UPPER FASTENER. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK, LT NR 3 WINDOW CUT OUT FWD WINDOW FRAME CRACKED AT UPPER FASTENER. R & R PLACED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

RIGHT NR 1 WINDOW FRAME UPPER AFT CORNER CRACKED. R & R FRAME IAW ACO.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,924 hrs · 33,107 cycles

RT HORIZONTAL STABILIZER, RIB STATION 92.7, FIRST VERTICAL STIFFENER AFT OF FWD SPAR CRACKED NEAR LOWER FLANGE. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,924 hrs · 33,107 cycles

RT HORIZONTAL STABILIZER RIB STATION 92.7, 2ND VERTICAL STIFFENER AFT OF FWD SPAR CRACKED NEAR LOWER FLANGE. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,924 hrs · 33,107 cycles

RT HORIZONTAL STABILIZER RIB STATION 92.7, 3RD VERTICAL STIFFENER AFT OF FWD SPAR CRACKED NEAR LOWER FLANGE. REPAIRED STIFFENER IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK LT NR 3 FIXED WINDOW FRAME FWD SIDE PANE ATTACH FASTENER HOLES, 1ST HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK LT NR 3 FIXED WINDOW FRAME FWD SIDE PANE ATTACH FASTENER HOLES 2ND HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK RT NR 3 FIXED WINDOW FRAME FWD SIDE PANE ATTACH FASTENER HOLES 3RD HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK RT NR 3 FIXED WINDOW FRAME FWD SIDE PANE ATTACH FASTENER HOLES, 2ND HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,924 hrs · 33,107 cycles

FLIGHT DECK RT NR 3 FIXED WINDOW FRAME FWD SIDE PANE ATTACH FASTENER HOLES 5TH HOLE FROM BOTTOM CRACKED. R & R FRAME IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 55,614 hrs · 32,916 cycles

OVERHEAD EMERGENCY EXIT LIGHT AT CRACKED BETWEEN ROW 11 TO ROW 12. R & R LIGHT ASSEMBLY IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,530 hrs · 32,865 cycles

NR 1 RT WINDOW FRAME CRACKED AT THE UPPER OTBD CORNER. REPAIRED FRAME IAW EA & ACO.

Part: PLATE — CRACKED (RT WING) · airframe 52,002 hrs · 30,779 cycles

WIGGLE PLATE CRACKED AT RIGHT WING PANEL 651GB. REMOVED AND REPLACED REF AMM, AND SRM 51-40-02.

Part: LENS — LOOSE (CABIN) · airframe 52,002 hrs · 30,779 cycles

EMERGENCY LIGHT LENS LOOSE AT BIN 16CBA. SECURED EMERGENCY LIGHT LENS AT BIN 16CBA. REF M/M

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,845 hrs · 30,029 cycles

LEFT WING OUTBOARD AFT FLAP INBOARD CONNER UPPER SURFACE DELAMINATED. REPAIRED DOUBLER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,845 hrs · 30,029 cycles

LEFT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS IAW AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,897 hrs · 29,463 cycles

STRINGER CORRODED AT BS 847+10, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,897 hrs · 29,463 cycles

STRINGER CRACKED AT BS 847+10, STR 27L. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,635 hrs · 28,723 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 9. REMOVED AND REPLACED BULB PER MM.

Part: LENS — BROKEN (CABIN) · airframe 48,304 hrs · 28,535 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 45,280 hrs · 26,820 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 17 TO ROW 18. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,820 hrs · 25,973 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM ANGLE CORRODED BETWEEN BS 291+19 TO BS 312+14. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,820 hrs · 25,973 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 34 TO RBL 46. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,820 hrs · 25,973 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 43,820 hrs · 25,973 cycles

DURING SCHEDULED 12Y CHECK, FOUND PASSENGER CABIN GALLEY EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,820 hrs · 25,973 cycles

DURING SCHEDULED 12Y CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT R2 DOOR. RELAMPED LIGHT PER MM.

Part: FLOORBEAM — PUNCTURED (FUSELAGE) · airframe 43,820 hrs · 25,973 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM PUNCTURED AT BS 1028, BETWEEN RBL 17R TO RBL 27R. REPAIRED BEAM PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,541 hrs · 9,283 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1010, LBL 39. REPAIRED WEB PER SRM.

Part: COVER — MISSING (CABIN) · airframe 43,774 hrs · 25,945 cycles

L1 DOOR EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 43,271 hrs · 25,660 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS MISSING COVER AT ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — PUNCTURED (RT WING) · airframe 42,026 hrs · 24,912 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,049 hrs · 24,308 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD GALLEY EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 39,505 hrs · 23,370 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.

Part: FITTING — CORRODED (LT WING) · airframe 34,843 hrs · 20,557 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 34,843 hrs · 20,557 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,122 hrs · 20,098 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 9 ABC AND ROW 11 ABC. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,055 hrs · 20,052 cycles

DURING SCHEDULED HC2 CHECK, FOUND CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 32,512 hrs · 19,168 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 31,501 hrs · 318,567 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,010 hrs · 17,684 cycles

DURING SCHEDULED 8Y CHECK, FOUND BS 986 FLOORBEAM UPPER CAP CORRODED BETWEEN LBL 19 TO LBL 45. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER — CRACKED (BS 337) · airframe 28,074 hrs · 16,112 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER 5R CRACKED AT BS 337. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (BS 508) · airframe 30,010 hrs · 17,684 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIRFONE ANTENNA CUTOUT BS 508, BL 0. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 512A) · airframe 30,010 hrs · 17,684 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIRFONE ANTENNA CUTOUT BS 512A, BL 0. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,130 hrs · 17,140 cycles

DURING SCHEDULED MV2 CHECK, FOUND INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT AFT ENTRY DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,935 hrs · 17,039 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,935 hrs · 17,039 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,316 hrs · 16,690 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 2 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,850 hrs · 16,422 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 8 TO ROW 11. REMOVED AND REPLACED STRIP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,423 hrs · 16,178 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 25,340 hrs · 15,035 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,851 hrs · 14,748 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (LT WING SKIN) · airframe 21,976 hrs · 13,070 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED T/E FLAP PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 21,494 hrs · 12,793 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 21,139 hrs · 12,609 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,431 hrs · 12,224 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — DEPLOYED (R2 DOOR.) · airframe 20,058 hrs · 12,029 cycles

R2 DOOR EVAC SLIDE DEPLOYED WHEN DOOR WAS OPENED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 18,711 hrs · 11,282 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJUST (SLIDE) · airframe 18,512 hrs · 11,176 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — WORN (LT/RT ELEV) · airframe 16,412 hrs · 10,019 cycles

DURING SCHEDULED 5Y CHECK, FOUND EXCESSIVE PLAY AT BOTH LT AND RT ELEVATOR NR 4 ATTACH HINGE POINTS. REMOVED AND REPLACED BOTH NR 4 ELEV HINGE FITTINGS PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 15,469 hrs · 9,493 cycles

DURING SCHEDULED C3 CHECK, FOUND LOOSE FASTENER AT FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET. REMOVED AND REPLACED FASTENER PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 9,683 hrs · 6,031 cycles

DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS TRACK COVERS CRACKED. REPLACED COVERS PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 9,579 hrs · 5,963 cycles

DURING RON,AD 11052-55 FOUND LT ELEVATOR TRIM TAB CONTROL ROD ENDS WORN. R&R TAB CONTROL ROD ENDS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 9,136 hrs · 5,720 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 6,658 hrs · 4,209 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE AND ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. RE-INSTALLED SLIDE ASSY PER MM.

Part: COVER — TORN (ESCAPE LIGHT) · airframe 6,658 hrs · 4,209 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER TORN BETWEEN ROW 1 THRU 20. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,658 hrs · 4,209 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 6,599 hrs · 4,174 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT EVACUATION SLIDE PRESSURE INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSY''S PER MM.

Part: MODULE — ERRATIC (MLG WW)

HYD LOW PRESS LIGHT ILLUMINATED ON BOTH ENG DRIVEN PUMPS. REMOVED AND REPLACED BOTH ENG DRIVEN HYD PUMP FILTERS AND REMOVED AND REPLACED HYD PRESS MODULE PER MM.

Part: COVER — CRACKED (ROW 1)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW I. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT)

AIR TURNBACK, GEAR LEVER WOULD NOT RAISE ON TAKEOFF, RETRACTED FLAPS AND NO TAKEOFF WARNING HORN. FOUND LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BRAKER TRIPPED. RESET CIRCUIT BRAKER, PERFORMED GEAR HANDLE OPS CHECK, SYSTEM WORKS GOOD PER MM.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULE C3 CHECK, FOUND EMERGENCY EVACUATION FLOOR LIGHTING MISSING SECTION AT OVERWING EXIT. INSTALLED LIGHTING STRIP PER MM.

Part: PUMP — FAILED (NR 1 ENGINE)

AIR TURNBACK - NR 1 ENG 'A' HYD SYSTEM LOW PRESS LIGHT ILLUMINATED DURING CLIMB-OUT. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENG HYD PUMP AND FILTERS.