N728SW

Part: PANEL — ELONGATED (FUSELAGE)

FAIRING PANEL 194E HAS MULTIPLE ELONGATED FASTENER HOLES. ; / [01] TSR 2021007285 PNL REPLACEMENT; [02] INSTALLED NEW PANEL REF AMM 53-51-21

Part: PANEL — ELONGATED (FUSELAGE)

FAIRING PANEL 193D HAS MULTIPLE ELONGATED FASTENER HOLES. ; / [01] TSR 2021007285 PNL REPLACEMENT; [02] REPLACED PANEL PER AMM53-51-21.

Part: TRANSMITTER — OUT OF TOLERANCE (TE FLAPS) · airframe 76,503 hrs · 45,026 cycles

FLAPS WOULD NOT EXTEND DURING FLIGHT- USED ALT FLAP EXT AND LANDED FLAP 15 ; / [01] PERF FIM 27-51-849 WITH NO DEFECTS NOTED; PERF FLAP POSITION VERIFICATION TEST IAW AMM 27-50-00-820 AT FULL DOWN FOUND LH FLAP POSITION OUT OF LIMITS (MEASURED 275.5) R/R LH FLAP POSITION TRANSMITTER IAW AMM 27-58-01; PENDING OPS CHECK; [02] PERFORMED FLAP POSITION TRANSMITTER INSTALLATION TEST PER AMM 27-58-01-400-801 STEP 3 G THRU H; OPS CHECK GOOD.; [03] FOR PART INFORMATION REF MXI ID TTG8Q00707BN; [04] EDITE TO REF PART INFO.

Part: COVER — MISSING (EXIT SIGN) · airframe 74,808 hrs · 44,073 cycles

CTR O/W EXIT SIGN MISSING AFT COVER CREW REPORTS / INSTALLED O/W EXIT SIGN LIGHT COVER PER SIP

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 74,766 hrs · 44,047 cycles

LEFT & RIGHT LOWER EMER EXIT OVERWING LENS MISSING DIRECTIONAL ARROWS / REMOVED AND REPLACED LOWER EMER EXIT OVERWING LENS IAW AMM 33-51-01

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 74,766 hrs · 44,047 cycles

FWD ENTRY DOOR LOWER LENS NOT BILINGUAL / REMOVED & REPLACED FWD ENTRY DOOR LOWER EMERGENCIES EENS IAW AMM 33-51-01

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 74,024 hrs · 43,635 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / R&R RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: CLEVIS — DAMAGED (HORIZONTAL STAB) · airframe 74,024 hrs · 43,635 cycles

HORIZONTAL STABILIZER FORWARD LOWER SPAR CLEVIS DAMAGED AT AFT RADIUS. DAMAGE MEASURES L=.4 W=.25 D=.2 AT DEEPEST POINT. REPAIRED PER EA 20-155-02462 24647.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 74,024 hrs · 43,635 cycles

RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL CRACKED / R & R SLIDING SEAL PER AMM 53-31-31.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,319 hrs · 43,208 cycles

LEFT & RIGHT OVERWING EXIT SIGNS HAVE BURNED OUT BULBS. REPLACED THE LAMP AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,319 hrs · 43,208 cycles

LEFT OVERWING SLIDE LIGHT DOES NOT ILLUMINATE. REPLACED THE LAMPS AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-04-960-801.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,319 hrs · 43,208 cycles

LT & RT OVERWING EXIT SIGNS HAVE BURNED OUT BULBS. REPLACED THE LAMPS AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 73,319 hrs · 43,208 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-60-15-2R-1 PAGE 2. PAR. B.(4)(5);(6);(7); & (8). INSTALL WILL BE ACCOMPLISHED ON CUSTOMER CARD: 753-140-00-02Y

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 73,319 hrs · 43,208 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY AFT CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-60-15-2R-1 PAGE 2. PAR B.(4);(5);(6) (7); & (8). INSTALL WILL BE ACCOMPLISHED ON CUSTOMER CARD 753-140-00-02Y.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,319 hrs · 43,208 cycles

AFT EMERGENCY EXITS LIGHT BATTERY M1673 WILL NOT HOLD A CHARGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK M1673 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-805.

Part: SKIN — GOUGED (BS 1016) · airframe 73,319 hrs · 43,208 cycles

FUSELAGE SKIN HAS A GOUGE BS 1016+1; .6' BELOW STR 13L / FUSELAGE SKIN GOUGE @ BS 1016+1; .6' BELOW STR 13 LH DAMAGE REPAIRED AND EVALUATED PER EA 20-153-01365 REV IR. (ATS ER 20-03026 REV IR.

Part: SKIN — GOUGED (BS 1016) · airframe 73,319 hrs · 43,208 cycles

FUSELAGE SKIN HAS A GOUGE BS 1016+.3; 2' ABOVE STR 13L / FUSELAGE SKIN GOUGE BS 1016+.3; 2' ABOVE STR 13L WAS BLENDED INSPECTED & EVALUATED IAW EA 20-153-01365 REV IR DATED 08/09/2020 & ATS ER 20-03026 REV IR DATED 08/09/2020 DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITHOUT REPETATIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS. APPLIED DENT DOT REF MPM 52.03.01.02 PARA 2C(1)(B) & PARA 3

Part: SKIN — DENTED (BS 1016) · airframe 73,319 hrs · 43,208 cycles

FUSELAGE EXTERNAL SKIN HAS A DENT LOCATED AT BS 1016+6'; 1' BELOW STRINGER 14 L/H; DENT MEASURES L=0.9'; W=0.7'; Y=0.009' W/Y=77 / FUSELAGE EXTERNAL SKIN DENT @ BS 1016+6'; 1' BELOW STR 14L/H DAMAGE REPAIRED & EVALUATED PER EA 20-153-01365 REV IR DATED 08/09/2020 (ATS ER 20-03026 REV IR DATED 08/09/2020) REFER TO NRC U194468 FOR TRACKING

Part: SKIN — DENTED (BS 1016) · airframe 73,319 hrs · 43,208 cycles

DEFT TRANSFERRED FROM CARD 9841860=FUSELAGE EXTERNAL SKIN HAS A DENT LOCATED AT BS 1016+5'; 1' ABOVE STRINGER 14 L/H; DENT MEASURES L=2.7'; W=1.1'; Y=0.026' W/Y=42 / DENT TRANSFERD FROM CARD 9841860; FUSLAGE EXTERNAL SKIN HAS DENT LOCATED @ BS 1016+5'; 1' ABOVE STR14 LH WAS REPAIRED IAW EA 20-153-01365 REV.IR DATED 08/09/2020 & ATS ER 20-03026 REV IR DATED 08/09/2020 CATEGORY B REPAIR

Part: SKIN — DENTED (BS 420) · airframe 73,319 hrs · 43,208 cycles

FUSELAGE SKIN HAS A DENT BS 420+12; 2' BELOW STR 18L. DENT MEASURES L= 1; W= 1; Y= .026'; W/Y= 38 / REPAIRED SKIN DENT AT BS 420+12; 2' BELOW STR18L PER EA 20-153-01372 REV IR AND ER 20-03032 REV.IR.

Part: BOOT — DAMAGED (RADOME) · airframe 73,319 hrs · 43,208 cycles

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

Part: GUSSET — CRACKED (FWD CARGO) · airframe 73,319 hrs · 43,208 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS 500D S-19L WL193. PER SRM 51-40-02 REF DWG 143A7902

Part: SHIELD — CORRODED (AFT CARGO) · airframe 73,319 hrs · 43,208 cycles

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS494 - BS500A RBL24 WL157. / REMOVED AND REPLACED FCB AFT SHIELD PER SRM S140102; SRM 51-40-05 AND DWG. 143A0080; 91195U 8/1/20

Part: SUPPORT — CORRODED (BS 727-767) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157. CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727-BS767 RBL21 WL157 FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 50% MATERIAL LOSS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. REMOVED AND REPLACED FLOOR TO SIDEWALL FROM BS727+4 TO BS767 RBL21 IAW SRM 51-40-02 AND IAW DWG #146A7500 AND IAW DWG #146A7502

Part: WEB — CORRODED (BS 767) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON WEB AT ACB BS767+6 RBL20 WL157. / REMOVED AND REPLACED WEB AT ACB BS767 787 RBL 20 WL157 PER SRM 51-40-02-0G-0; SRM 53-60-15-01-01; SRM 53-60-15-1A-1 AND BOEING DRAWING 146A0081. 57006U 03AUG20

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS500A - BS500D RBL22 WL157. REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS500A BS400D RBL22 IAW SRM 51-40-02; SRM 51-40-05 SRM 51-20-01; DWG 143A7501 AND DWG 143A7500; SRM 53-00-53-1A-2.

Part: SUPPORT — CORRODED (BS 727-807) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS807 LBL21 WL157. / CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727-BS807 LBL21 WL157 FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 20% MATERIAL LOSS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. REMOVED AND REPLACED FLOOR TO SIDEWALL FROM 727+4-BS847 LBL21 IAW SRM 51-40-02 AND IAW DWG #146A7500 AND IAW DWG #146A7502.

Part: TRACK — CORRODED (BS 766) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON TRACK AT ACB BS766 RBL13 WL156. / REMOVED CORROSION ON ACB TRACK BS 766 RBL 13 WL156 MAX. MAT. LOSS 2.' X .5' X .04' TOP SIDE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ACB TRACK BS 727-BS 887 RBL13 WL156 I.A.W SRM 53-00-53-1A-2; SRM 53-00-53-2R-3 AND DWG #146A7500 & 147A7500

Part: ATTACH ANGLE — CORRODED (BS 767) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON STRINGER ATTACH ANGLE BS767 RBL5 WL150. MARKED / REMOVED AND REPLACED STRINGER ATTACH ANGLE P/N 146A1320-14 PO #799088; BS767 RBL5 WL150 IAW SRM 51-40-02-OG-0 STEP 7.D. REF DWG 146A7810 89004U 04AUG20

Part: FLOORBEAM — CORRODED (BS 947) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL20 WL181. MARKED / REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL20 TO LBL10 WL181 IAW SRM 51-40-02 REF DWG 149A8117.

Part: SUPPORT — CORRODED (BS 400-420) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 WL157. REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS400-BS420 RBL23. REMAINING THICKNESS IS 0.034' OUT OF LIMITS PER SRM 53-00-53-1A-2. FABRICATED NEW FLOOR TO SIDEWALL SUPPORT FROM BAC1496-444#7075T62 LOT #1437451-1. LOCATED AND DRILLED AND CHEMICAL CONVERSION COATING AND PRIMER AND INSTALLED ON FLOOR TO SIDEWALL SUPPORT AT FCB BS 400-420 RBL23 IAW SRM 51-40-02; SRM 51-40-05; SRM 51-20-01 AND DWG 143A7501; DWG 143A7500.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 73,319 hrs · 43,208 cycles

***CORROSION*** ON TRACK AT ACB BS787 - BS867 RBL13 WL160. / ACB CARGO TRACK AT BS787-BS867 RBL13 WL160 WILL BE REPLACED ON CUSTOMER CARD U194211.

Part: WEB — CORRODED (BS 794-847) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON SUBTHRESHOLD WEB AT ACB BS794 - BS847 RBL26 WL157. / REMOVED AND REPLACED ACB SUB THRESHOLD WEB PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A8340; 91195U 8.2.20

Part: WEB — CORRODED (BS 440-490) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS490 RBL27 WL157. / REMOVED CORROSION AT FCB SUB THRESHOLD WEB BS440-490 RBL27 L=3' W=2.4' ORIGINAL THICKNESS 0.045'; MATERIAL LOSS MORE THAN 50% FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED FCB SUB THRESHOLD WEB BS440-492.4 P/N 7530597 PO #799108 IAW SRM 51-40-02 REF DWG 143A8330 89004U 29JUL20

Part: STRINGER — CRACKED (BS 540) · airframe 73,319 hrs · 43,208 cycles

CRACKED STRINGER 25R AFT OF BS 540.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 73,319 hrs · 43,208 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS 500D S-19R WL193. PER SRM 51-40-02 REF DWG 143A7902

Part: FLOORBEAM — CRACKED (BS 540) · airframe 73,319 hrs · 43,208 cycles

CRACKED FLOORBEAM AT BS 540, BL 0 - LBL 24.5, WL 208.1. REMOVED AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02-0G-0.

Part: STRINGER — CRACKED (BS 540) · airframe 73,319 hrs · 43,208 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-24L WL165. MARKED / REPAIRED STR AT STA;540 STR 24L WL 165 PER SRM 53-00-03-2R-1; EA 20-153-01391 REV IR AND ER 20-02989 REV IR

Part: TAB — DELAMINATED (RIGHT ELEVATOR) · airframe 73,319 hrs · 43,208 cycles

RT ELEVATOR TAB HAS SMALL DELAMINATION ON O/B EDGE ON BULLNOSE. REMOVED FINISH FROM DAMAGE AREA IAW AMM 51-21-99-300-802, PARA 3C, (3)(A)-(D). RT ELEVATOR TAB WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR 9 AND WILL BE REINSTALLED.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON INTERCOSTAL AT ACB BS767 - BS787 RBL6 WL154. / REMOVED AND REPLACED NEW INTERCOATAL AT ACB BS767-BS787 RBL 6 ITEM 7532036 PO#794694 IAW SRM 51-40-02; 51-40-03; SRM 53-60-15-01-1 AND DWG 146A8131; DWG 146A8130. 80641U 03AUG20

Part: FLOORBEAM — CORRODED (BS 500D) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON AFT BULKHEAD LOWER SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL157. CORROSION FOUND ON FCB AFT BULKHEAD LOWER SUPPORT ANGLE BS-500D LBL-23 TO RBL-23 WL-157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLACEMENT IAW SRM 51-10-02-09-0 PAR-9C. LOCATED AND DRILLED NEW SUPPORT P/N 143A9485-35 IAW SRM 51-40-05-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG #143A9481 REV-A

Part: SHIELD — CORRODED (FWD CARGO) · airframe 73,319 hrs · 43,208 cycles

***CORROSION*** ON FWD SHIELD AT ACB BS767 - BS787 RBL22 WL157. / REMOVED AND REPLACED FWD SHIELD AT ACB BS767 - BS787 RBL22 WL157 PER SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DRAWING 146A8127 BOEING DRAWING 146A0081. 57006U 03AUG20

Part: STRINGER CLIP — CORRODED (BS 747) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON STRINGER CLIP AT ACB BS747 LBL14 WL153. REMOVED AND REPLACED ON STRINGER CLIP AT ACB BS 747 LBL 14 IAW SRM 51-40-02 AND DWG 146A1260 80641U 03AUG20

Part: ANGLE — CORRODED (BS 914) · airframe 73,319 hrs · 43,208 cycles

CORROSION ON SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11 WL171. REMOVED AND INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11 WL171 ITEM #7531385 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; DWG #147A7221

Part: SHIELD — CORRODED (FWD CARGO) · airframe 73,319 hrs · 43,208 cycles

***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL157. / REMOVED AND REPLACED FWD SHIELD AT F.C.B. BS420-440 RBL23 WL157 SRM 51-40-02 REF DWG 143A0080 890040 31JUL20

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 73,319 hrs · 43,208 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS500D LBL23 WL157. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB BS400-BS500D LBL23 ITEM 7530869 PO #797129 IAW SRM 53-00-53-1A-2; SRM 51-40-02; SRM 51-40-05 AND DWG 143A7501; DWG 143A7500. 80641U 30JUL20

Part: SUPPORT ANGLE — CRACKED (BS 918) · airframe 73,319 hrs · 43,208 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11 WL171. REMOVED AND INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11 WL171 ITEM #7531385 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DWG #147A7221.

Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 73,319 hrs · 43,208 cycles

FAIRING 193B HAS NUMEROUS AREAS OF DELAMINATION ON OUTER SURFACE (MARKED). / REPLACED FAIRING 193B WITH NEW SERVICEABLE UNIT IAW SRM 51-10-02-0G-0 PAR 9.A.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 73,319 hrs · 43,208 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 2ND VERTICAL STIFFENER IS CRACKED. / REPAIRED LH HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR 4.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 73,319 hrs · 43,208 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. FLIGHT DECK FLOOR DENT AT BS 255 RBL 4 TO LBL 14 REPAIRED EA NO: 1-A53-33179 REV 1.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,232 hrs · 43,152 cycles

EMERGENCY LIGHTS ARE INOP AT 1ABC; 4ABC; 9ABC; 12ABC; 16DEF; 18DEF; AFT ENTRY DOOR AND AFT CENTER LIGHT. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES; ALL LIGHTS NOW FUNCTIONAL AT 1ABC; 4ABC; 9ABC; 12ABC; 16DEF; 18DEF; AFT ENTRY DOOR AND AFT CENTER LIGHT PER AMM 33-51-06.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,232 hrs · 43,152 cycles

7 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY BATTERIES PACKS AT LOCATIONS M1669; M1674; M1675; M1668; M1670; M1673; M1672 AND REMOVED AND REPLACED EMERGENCY BATTERY CHARGERS AT M1668 AND M1673 PER AMM 33-51-06.

Part: CONTROL CARD — FAULTY (CABIN LIGHT) · airframe 71,645 hrs · 42,173 cycles

SMOKE AT ROW 22F OVERHEAD PASSENGER READING LIGHT. REPLACED CONTROL CARD AT 22DEF IAW AMM. DECLARED EMERGENCY, SMOKE AT ROW 22F OVERHEAD PASSENGER READING LIGHT. REPLACED CONTROL CARD AT "22DEF" IAW AMM.

Part: HANDLE — EXPOSED (R2 DOOR SLIDE) · airframe 70,483 hrs · 41,437 cycles

R2 DOOR SLIDE HANDLE EXPOSED. / REINSTALLED SLIDE IAW AMM.

Part: FITTING — CRACKED (FED) · airframe 70,387 hrs · 41,377 cycles

CABIN 1L DOOR LOWER HINGE RADIOUS LINK FITTING LOWER LUG IS CRACKED. / REMOVED L1 DOOR IAW 52-11-00-000-802 STEP 2.F. AND REPLACED DAMAGED LOWER HINGE RADIOUS LINK FITTING IAW 52-11-400-802 STEP 3.F; REINSTALLED L1 DOOR IAW 52-11-00-400-802 STEP 3.F(1-10). L1 DOOR RIG/ADJUSTMENT GOOD ATAG: WN1046 POS: L TAG/GRB NO.: 559957 P/N OFF & ON: 50150-1 S/N OFF: TAS-V01739 S/N ON: TAS-V07125

Part: SKIN — CRACKED (L1 DOOR) · airframe 70,387 hrs · 41,377 cycles

L1 DOOR EXTERIOR SKIN AFT CORNER OF SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,387 hrs · 41,377 cycles

AFT PRESSURE BULKHEAD WEB OUTER SKIN CRACKED INDICATION AT STR. 23R INNER MOST FASTENERS ADJACENT TO CENTER PLUG. REPAIRED AFT PRESSURE BULKHEAD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,387 hrs · 41,377 cycles

AFT PRESSURE BULKHEAD WEB OUTER SKIN CRACKED AT BS. 1016, STR. 7R INNER MOST FASTENER ADJACENT TO CENTER PLUG. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,388 hrs · 40,750 cycles

R2 EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 69,175 hrs · 40,615 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER SIP.

Part: O-RING — BLOWN (HYDRAULIC SYS) · airframe 69,013 hrs · 40,506 cycles

AIR TURNBACK, ON TAKE OFF ROLL GOT MOMENTARY MASTER CAUTION (HYD). AT GEAR UP, GOT FLIGHT CONT A LOW PRESSURE FOR 15SEC THEN OUT. NOTICED FLUID QUANTITY DECREASING. R&R O RING PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,489 hrs · 40,166 cycles

RT LOWER EXTERIOR EMERGENCY LIGHT INOP. R&R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,489 hrs · 40,166 cycles

LT AISLE LIGHT INOP AT SEAT ROW 20. R&R HOUSING LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,489 hrs · 40,166 cycles

LT LOWER OVERWING EXIT INDICATOR LIGHT INOP. R&R LAMPS IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

SHEAR TIE CORRODED AT BS 1121 AT INNER CHORD ANGLE VIEWED THRU CENTER ACCESS ON LT SIDE APU COMPARTMENT. R&R SHEAR TIE IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 68,489 hrs · 40,166 cycles

LT UPPER BARRIER TO REAR LOWER SPAR ATTACH ANGLE CRACKED AT BS 663, LBL 7. REPAIRED ANGLE IAW ER & EA.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 68,489 hrs · 40,166 cycles

CABIN FLOOR PANEL 242UF HAS O/B FWD CORNER IS DISBONDED / REPAIRED DISBONDED O/B FWD CORNER ON CABIN FLOOR PANEL 242UF IAW SRM 53-00-50-2R-9 80733U 01SEP18

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 68,489 hrs · 40,166 cycles

FLOORBOARD 242UF HAS HEEL STRIKE DAMAGE IN CENTER OF PANEL / REPAIRED HEEL STRIKE DAMAGE IN CENTER OF PANEL ON FLOORBOARD 242UF IAW SRM 53-00-50-2R-1 80753U 01SEP18

Part: DOUBLER — CRACKED (WHEEL WELL LH) · airframe 68,489 hrs · 40,166 cycles

SEAL DOUBLER CRACKED ON BS 663 LOWER VAPOR BARRIER LBL 25 WL 149 / REPLACED SEAL DOUBLER ON 663 LOWER VAPOR BARRIER LBL 25 WL149 WITH NEW PO# 704655 LOCATED AND DRILLED P3R SRM 51-40-05 WILL BE INSTALLED ON NRC N155629 DWG 111A1512

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

RT LOWER MAIN SILL WEB CORRODED BETWEEN BS 947.4 TO BS 986. R&R WEB IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

FUEL TANK TO VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 7. REPAIRED ANGLE IAW ER AND EA.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 68,489 hrs · 40,166 cycles

STIFFENER CRACKED ON BS 663 LOWER VAPOR BARRIER RBL 20 WL 155 / REPLACED CRACKED STIFFENER ON 663 RBL 20 WL 155 WITH NEW PO#693255 LOCATED AND DRILLED PSR SRM 51-40-05 AND DWG 111A1301 WILL BE INSTALLED ON NRC N155630

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 68,489 hrs · 40,166 cycles

SEAL DOUBLER CRACKED ON BS 663 LOWER VAPOR BARRIER RBL 25 WL 149 / REPLACED CRACKED SEAL DOUBLER ON 663 VAPOR BARRIER RBL 25 WL 149 WITH NEW PO# 704655 LOCATED AND DRILLED P3R SRM 51-40-05 AND DWG 111A1512 WILL BE INSTALLED ON NRC N155630

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

LONGITUDINAL FLOORBEAM DAMAGED BETWEEN BS 540 TO BS 727, LBL 24.75. REPAIRED BEAM PER ER AND EA.

Part: SIGN — CRACKED (CABIN) · airframe 68,489 hrs · 40,166 cycles

AFT LOWERED CEILING PANEL EMERGENCY EXIT SIGN HOUSING ASSEMBLY CRACKED. R&R SIGN IAW AMM.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

***CORROSION*** ON EXTERNAL SKIN UNDER VERTICAL STAB STA 1016-1131 BETWEEN STR 3 R/H AND 3L/H / REPAIR VERTICAL STAB STAR 1016-1131 BETWEEN STR 3R-3L IAW ATS ER 18-04071 IR AND SWA EA 1-753-33314 IR

Part: STIFFENER — CORRODED (AFT FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

***CORROSION*** ON STIFFER UNDER VERTICAL STAB STA 1037 BETWEEN STR 2L AND 2R / REMOVED CORROSION ON STIFFENER BY MECHANICAL MEANS IN AN AREA OF L5.30'X W.800'X D.005' I.A.W. 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM 51-10-02-0G-0 PAGE 7 STEP 9(C); REMOVED STIFFENER UNDER VERTICAL STAB STA 1037 BETWEEN STR 2L AND 2R I.A.W. SRM 51-40-02-0G-0. REMOVED WIRING BRACKET AT BS 1036 BL'O'. I.A.W. SRM 51-40-02-0G-0. INSTALLED FABRICATED BRACKET I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 148A3110 REV:-. INSTALLED WIRING BRACKET I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 148A0931 REV:A.

Part: TAIL CONE — DELAMINATED (AFT FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

2 AREAS OF DELAMINATION ON THE TAIL CONE. BOTH ARE ABOUT 9 INCHES AFT OF THE 1156 BULKHEAD; ONE IS 3 INCHES BELOW ACCESS PANEL 318BR AND THE OTHER IS 5 INCHES BELOW ACCESS PANEL 318BR. **AREAS MARKED** / REPAIRED (2) AREAS OF DELAMINATION ON THE TAILCONE 9' AFT OF 1156 BULKHEAD 3' & 5' BELOW ACCESS PANEL 318BR I.A.W 737 SRM 53-80-70-2R-1 PARA 4D TABLE 201 AND TABLE 202; 200 OF CURE PER 737 SRM 51-70-04 REPAIR 11; REPAIR 2

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: PANEL — CRACKED (AFT FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

INBD INLET PANEL OF 8 PIECE APU INLET HAS CRACKED CORNER ON ATTACHED ANGEL / REMOVED AND REPLACED ATTACH ANGLE ON I/B APU INLET PANEL OF 8 PIECE INLET IAW SRM 51-40-02-0G-0 REF 49-15-00-01

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

R2 DOOR LOWER SILL INNER CHORD CORRODED. R&R CHORD IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

STRINGER TIE CRACKED AT BS 294, STR 13L. R&R ANGLE PER SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

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

Part: RIB — BENT (HORIZONTAL STAB) · airframe 68,489 hrs · 40,166 cycles

L/H HORIZONTAL STABILIZER #7 RIB AT APPROX. STAB STATION 147.9 SUPPORT LOWER FOOT 3RD BACK FRONT SPAR IS BENT / REMOVED DAMAGE; INSTALLED REPAIR AT L/H STAB STA 147.9 3RD STIFFENER FROM FRONT SPAR IAW SRM 55-10-09-2R-5

Part: STRAP — DAMAGED (CABIN) · airframe 68,489 hrs · 40,166 cycles

LT EMERGENCY EXIT HATCH ESCAPE STRAP DAMAGED. R&R STRAP IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL PER DWG AND SRM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 68,489 hrs · 40,166 cycles

PASS CABIN FLOORBOARD 222AF BROKEN AFT RH CORNER / PASS CABINFLOORBOARD 222 AF BROKEN AFT RH CORNER REPAIRED IAW SRM 53-00-50-2R-01 AND IAW SRM 53-00-50-2R-5; REMOVED AND INSTALLED INSERTS IN REPAIR AREA IAW SRM 53-00-50-2R-0 PARA. 1. 5. I.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 68,489 hrs · 40,166 cycles

LT VAPOR BARRIER CRACKED AT BS 663.75. REPAIRED BARRIER PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,489 hrs · 40,166 cycles

R/H HORIZONTAL LEADING EDGE 5TH RIB OUTBOARD OF INBOARD END CRACKED / REMOVED AND REPLACED R/H HORIZONTAL LEADING EDGE 5TH RIB OUTBOARD OF INBOARD END IAW B737 51-40-02 FIG 8; FIG 4 AND BOEING DWG #186A1001 REV A

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 68,489 hrs · 40,166 cycles

RT VAPOR BARRIER CRACKED AT BS 663.75. REPAIRED BARRIER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 68,489 hrs · 40,166 cycles

RT HORIZONTAL LEADING EDGE 4TH RIB OUTBOARD OF INBOARD END CRACKED. R&R RIB IAW SRM AND DWG.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 68,489 hrs · 40,166 cycles

PASS CABIN FLOORBOARD 221GF BROKEN FORWARD LT CORNER. REPAIRED FLOOR BOARD IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 68,489 hrs · 40,166 cycles

RT HORIZONTAL LEADING EDGE 9TH RIB OUTBOARD OF INBOARD SPLICE CRACKED. R&R RIB IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL12. R&R INTERCOSTAL IAW SRM AND AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 68,489 hrs · 40,166 cycles

LT HORIZONTAL STABILIZER LEADING EDGE 2ND RIB OUTBOARD OF INBOARD END CRACKED. R&R RIB IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

FORWARD CARGO GUSSETS CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM AND DWG.

Part: BEAM — CRACKED (FSD) · airframe 68,489 hrs · 40,166 cycles

REF: FWD SERVICE DOOR #4 AND #5 BEAMS INSP; LOWER BEAM; 141A6536-14 BEAM CRACKED / FWD SERVICE DOOR TO BE REPLACED ON CUSTOMER CARD N155201

Part: WIRE — EXPOSED (CABIN) · airframe 68,489 hrs · 40,166 cycles

AFT LAV EXIT SIGN CONNECTOR WIRE EXPOSED. TERMINATED CONNECTORS PER WDM & AMM.

Part: PANEL — DELAMINATED (RH PYLON) · airframe 68,489 hrs · 40,166 cycles

POSSIBLE COMPOSITE DELAMINATION ON PANEL 441BL / POSSIBLE COMPOSITE DELAMINATION ON PANEL 441BL REPAIRED IAW SRM 54-50-70-2R-1 TABLE 201 AND IAW SRM 51-70-05-2R-2

Part: WIRE — EXPOSED (CABIN) · airframe 68,489 hrs · 40,166 cycles

AFT LAV EXIT SIGN CONNECTOR WIRE EXPOSED. TERMINATED CONNECTORS PER WDM & AMM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

AFT CARGO COMPARTMENT RT SIDE ON FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727C TO BS 767. R&R ANGLE IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED BETWEEN BS 727B TO BS 807, LT SIDE. R&R ANGLE IAW SRM & DWG.

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 68,489 hrs · 40,166 cycles

***CORROSION*** CORROSION AROUND MULTIPLE FASTENER HOLES ON AFT SHIELD AT STA.847 TO 867 R/H SIDE IN AFT CARGO COMPARTMENT / REMOVED AND REPLACED AFT SHIELD IN AFT CARGO COMPARTMENT IAW B737 NG SRM 51-40-02 AND DWG 146A0081.

Part: RETAINER — CRACKED (LEFT WING) · airframe 68,489 hrs · 40,166 cycles

L/H WING HAS CRACK ON SEAL RETAINER WHERE ATTACHES AT REAR SPAR APPROX ORSS 278.50.( MARKED) / REMOVED AND REPLACED CRACKED SEAL RETAINER ON LH WING AT APPROX. ORSS 278.5 IAW SRM 51-40-02-0G-0 AND DRAWING 115A2930

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,489 hrs · 40,166 cycles

AFT CARGO COMPARTMENT FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 800, RT SIDE. R&R SHIELD IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,489 hrs · 40,166 cycles

LT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663+1, LBL 36. R&R WEB PER EA AND ER.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 68,489 hrs · 40,166 cycles

RT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663+1, RBL 41. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (SLAT) · airframe 68,489 hrs · 40,166 cycles

RT WING; #8 L/E SLAT SS 451.97; HAS SIGNS OF CRACK; AND SMOKING FASTENERS. / FOUND 1 EA. HOLE CRACKED IN SKIN ONLY. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-02-0G-0 AND SRM 57-42-01-2R-8 AND DWG 114A5010

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 68,489 hrs · 40,166 cycles

RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB PER SRM.

Part: PANEL — CRACKED (RIGHT WING) · airframe 68,489 hrs · 40,166 cycles

PANEL 651BT HAS FASTENER HOLE CRACKED; AT LEADING EDGE INBOARD SIDE; MARKED WITH TAPE. / REPAIRED PANEL 651BT CRACK IN FASTENER HOLE; AT LEADING EDGE I/B SIDE I-A-W 737 SRM 57-51-01-2R-1 PARA 1;4 C TABLE 202; 200 DEGREE F CURE; PER 737 SRM 51-70-04 REPAIR 6

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,215 hrs · 39,983 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,215 hrs · 39,983 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED FITTING PER EA.

Part: ENGINE — FLUID LOSS (LEFT) · airframe 67,662 hrs · 39,613 cycles

AIR TURNBACK/INFLIGHT SHUTDOWN/DECLARED EMERGENCY, NR 1 ENGINE LOST OIL PRESSURE. R&R NR 1 ENGINE PER MT.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 67,433 hrs · 39,470 cycles

RIGHT MAIN WHEEL WELL STA 663 RBL 26 STIFFENER CRACKED OUTBD OF EXHAUST DUCT / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02.

Part: STIFFENER — CRACKED (WHEEL WELL LH) · airframe 67,433 hrs · 39,470 cycles

LEFT MAIN WHEEL WELL STA 663 LBL 26 STIFFENER CRACKED OUTBD OF EXHAUST DUCT / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02

Part: RADOME — DELAMINATED (FWD FUSELAGE) · airframe 67,433 hrs · 39,470 cycles

NOSE RADOME DELAMINATED IN NUMEROUS INNUMEROUS AREAS / REPLACED NOSE RADOME REF MM 53-52-00 TAG NO: 395001 PN ON: 1001002-1 SN ON: 9801062C PN OFF: SN OFF: 0207102

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 67,171 hrs · 39,315 cycles

L2 DOOR EXIT LIGHT LENS BROKEN. R & R THE LENS PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,151 hrs · 39,301 cycles

L1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,151 hrs · 39,301 cycles

R1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,151 hrs · 39,301 cycles

RIGHT AISLE EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: HOOK — LOOSE (R2 DOOR) · airframe 67,047 hrs · 39,232 cycles

R2 DOOR EMERGENCY SLIDE HOLDER GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SHROUD — LOOSE (L1 DOOR SLIDE) · airframe 66,443 hrs · 38,850 cycles

L1 DOOR SLIDE SHROUD LOOSE. SECURED THE SLIDE ASSEMBLY IAW AMM.

Part: HOUSING — CRACKED (FWD CARGO BAY) · airframe 65,854 hrs · 38,475 cycles

FWD CARGO DOOR FLUSH DOOR LATCH HANDLE HOUSING CRACKED / R/R'D FWD CARGO HANDLE HOUSING REF CMM 52-36-15 & SRM 51-40-02

Part: INTERCOSTAL — CRACKED (AIR COND BAY) · airframe 65,436 hrs · 38,223 cycles

CENTER RIGHT FLOOR SUPPORT INTERCOSTAL A STA 540 IS CRACKED / REMOVED AND REPLACED CENTER RIGHT FLOOR SUPPORT INTERCOSTAL A STA 540; REFERENCE SRM 51-40-05 AND SRM 51-40-02.

Part: INTERCOSTAL — CRACKED · airframe 65,436 hrs · 38,223 cycles

CENTER LEFT FLOOR SUPPORT INTERCOSTAL A STA 540 IS CRACKED / REMOVED AND REPLACED CENTER LEFT FLOOR SUPPORT INTERCOSTAL A STA 540; REFERENCE SRM 51-40-05 AND SRM 51-40-02.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 62,919 hrs · 36,689 cycles

R2 DOOR SLIDE COMING OUT OF CONTAINER. SECURED THE SLIDE IAW MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 62,581 hrs · 36,500 cycles

AFT ENTRY DOOR SLIDE LOOSE AND COMING OUT OF CONTAINER. REPOSITIONED SLIDE AT GIRT BAR ANGLES IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 62,217 hrs · 36,254 cycles

L1 DOOR LOWER EXIT SIGN AT DIRECTIONAL ARROW MISSING. REPLACED THE SIGN IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 62,217 hrs · 36,254 cycles

R1 DOOR LOWER EXIT SIGN AT DIRECTIONAL ARROW MISSING. REPLACED THE SIGN IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,934 hrs · 36,080 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R THE BULB IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,934 hrs · 36,080 cycles

L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R THE BULB IAW AMM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 61,934 hrs · 36,080 cycles

AFT LAVATORY OTBD EMERGENCY LIGHT INOPERATIVE, CONNECTED LIGHT ASSY IAW AMM.

Part: GUSSET — CRACKED (BS 500D) · airframe 61,934 hrs · 36,080 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW DWG AND SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 61,934 hrs · 36,080 cycles

FLOORBEAM UPPER TOP CAP CORRODED AT BS 986, BETWEEN RBL 20 - 49. R & R THE FLOORBEAM TEE CAP IAW EA.

Part: WEB — CRACKED (BS 294) · airframe 61,934 hrs · 36,080 cycles

R1 DOOR CUTOUT FORWARD FRAME WEB CRACKED AT BS 294, STRINGER 17R. REPAIRED WEB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 964) · airframe 61,934 hrs · 36,080 cycles

FLOOR SUPPORT CORRODED AT BS 964, LBL 34. R & R THE FLOOR SUPPORT IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 61,934 hrs · 36,080 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 - 312, RBL 31. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,934 hrs · 36,080 cycles

L2 DOOR CREASE BEAM INNER CHORD ANGLE CORRODED BETWEEN BS 947 TO BS 986, LBL 48. R & R CREASE BEAM IAW SRM AND DWG.

Part: PANEL — CRACKED (LT WING) · airframe 61,934 hrs · 36,080 cycles

LEFT WING TRAILING EDGE INBOARD OF THE DEFLECTOR BEAM AROUND REAR SPAR STA 261, THE FIXED UPPER PANEL CENTER AFT TRIANGLE SHAPED STIFFENER CRACKED AT THE LOWER ATTACH. R & R PANEL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 296-340) · airframe 61,934 hrs · 36,080 cycles

R1 DOOR CREASE BEAM INNER ANGLE CORRODED BETWEEN BS 296 - 340, STRINGER 17R. R & R CREASE BEAM IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 61,934 hrs · 36,080 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 45.5. R&R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 312-360) · airframe 61,934 hrs · 36,080 cycles

L1 DOOR CREASE BEAM CORRODED BETWEEN BS 312 - 360. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,934 hrs · 36,080 cycles

CREASE BEAM ANGLE CORRODED AT BS 984, LBL 46. R & R ANGLE IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (BS 787-847) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 787 - 847, RBL 13. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 61,934 hrs · 36,080 cycles

STRINGER CLIP 27L CORRODED AT BS 847. R & R THE STRINGER CLIP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 727) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO BAY FLOOR SUPPORT UPPER SURFACE CORRODED AT BS 727+10, RBL 3. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 773) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 773, RBL 5. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 773) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 773, RBL 10. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 773) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 773, LBL 10. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 61,934 hrs · 36,080 cycles

RIGHT WING TRAILING EDGE SEAL RETAINER BRACKET CRACKED AT WS 278. R & R BRACKET IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 773) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS. 773, LBL 5. REPAIRED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 773) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 773, RBL 15. REPAIRED THE FLOOR SUPPORT IAW SRM AND EA.

Part: PLATE — CORRODED (FWD CARGO DOOR) · airframe 61,934 hrs · 36,080 cycles

FORWARD CARGO DOOR ENTRY PLATE CORRODED. R & R THE PLATE IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,934 hrs · 36,080 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 827. R & R Z-ANGLE IAW SRM.

Part: PANEL — CRACKED (LT MLG WW) · airframe 61,934 hrs · 36,080 cycles

LOWER BULKHEAD GIL-LINER CRACKED AT BS 663, LBL 10. REPAIRED BULKHEAD IAW EA.

Part: STRUCTURE — CRACKED (LT ELEVATOR) · airframe 61,693 hrs · 35,940 cycles

LEFT ELEVATOR CRACKED. R & R ELEVATOR IAW MM.

Part: BRACKET — CRACKED (RT WING) · airframe 61,473 hrs · 35,819 cycles

RIGHT WING T/E FIXED PANEL BRACKET CRACKED ON INBD SIDE OF DEFLECTION CONTROL BEAM. R & R BRACKET IAW SRM.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 61,072 hrs · 35,587 cycles

INFLIGHT SHUTDOWN & DECLARED EMER. NR 1 ENG OIL FILTER BYPASS, ENG SHUTDOWN IAW QRH. R & R NR 1 ENG IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,376 hrs · 34,026 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 13. R & R LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,995 hrs · 33,249 cycles

FORWARD GALLEY RT EMER LIGHT BATTERY FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,656 hrs · 33,048 cycles

R1 DOOR EMER EXIT SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,656 hrs · 33,048 cycles

RIGHT PANEL 232YHW EMER EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

RIGHT AFT WW RING WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 56,656 hrs · 33,048 cycles

LEFT OVERWING EMER EXIT PULL HANDLE BROKEN. R & R HANDLE IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,656 hrs · 33,048 cycles

LEFT MLG WW VERTICAL PRESS DECK WEB CUT OUT CRACKED AT BS 663, LBL 33. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 56,656 hrs · 33,048 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED AT TE. REPAIRED FLAP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,656 hrs · 33,048 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,656 hrs · 33,048 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,656 hrs · 33,048 cycles

WEB CRACKED AT BS 663, BETWEEN LBL 40 TO LBL 45. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,656 hrs · 33,048 cycles

RIGHT WING NR 5 LE SLAT LOWER SURFACE CRACKED AT OTBD ACTUATOR CUT OUT. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,656 hrs · 33,048 cycles

RIGHT WING NR 6 LE SLAT LOWER SURFACE CRACKED AT OTBD ACTUATOR CUT OUT. REPAIRED SLAT IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 54,312 hrs · 31,682 cycles

AFT GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,151 hrs · 31,012 cycles

FUSELAGE SKIN CRACKED AT BS 540 STRINGER 22R. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,151 hrs · 31,012 cycles

FLIGHT COMPARTMENT, PILOT'S 3 FIXED WINDOW FRAME, FWD SIDE WINDOW ATTACH FASTENER HOLES, 2ND HOLE FROM BOTTOM, CRACKED IN FASTENER HOLE. REPAIRED FRAME IAW ACO.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 53,151 hrs · 31,012 cycles

LT HORIZONTAL STABILIZER RIB STATION 92.7, 1ST VERTICAL STIFFENER, 11.5" AFT OF FWD SPAR CRACKED THROUGH TO OTBD SIDE OF RIB. REPAIRED STIFFENER IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 53,151 hrs · 31,012 cycles

LT HORIZONTAL STABILIZER RIB STATION 92.7, 2ND VERTICAL STIFFENER, 21" AFT OF FWD SPAR CRACKED THROUGH TO OTBD SIDE OF RIB. REPAIRED STIFFENER IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 53,151 hrs · 31,012 cycles

LT HORIZONTAL STABILIZER RIB STATION 92.7, 3RD VERTICAL STIFFENER, 30" AFT OF FWD SPAR CRACKED THROUGH TO OTBD SIDE OF RIB. REPAIRED STIFFENER IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 53,151 hrs · 31,012 cycles

LT HORIZONTAL STABILIZER RIB STATION 129.5, 3RD VERTICAL STIFFENER, 27" AFT OF FWD SPAR CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 53,151 hrs · 31,012 cycles

LT HORIZONTAL STABILIZER RIB STATION 92.7, 4TH VERTICAL STIFFENER, 39.5" AFT OF FWD SPAR CRACKED. REPAIRED STIFFENER IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,151 hrs · 31,012 cycles

FLIGHT COMPARTMENT PILOT'S NR 3 FIXED WINDOW FRAME, FWD SIDE WINDOW ATTACH FASTENER HOLES, 3RD HOLE FROM BOTTOM, CRACKED IN FASTENER HOLE. REPAIRED FRAME IAW ACO.

Part: PLATE — CRACKED (LT WING) · airframe 52,842 hrs · 30,831 cycles

LT WING LOWER FIXED TE PANEL AFT OF ENGINE CRACKED WIGGLE PLATE. R & R WIGGLE PLATE IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 49,733 hrs · 28,982 cycles

RIGHT EMERGENCY EXIT SIGN LENS (LOWER FWD) LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 49,733 hrs · 28,982 cycles

LEFT EMERGENCY EXIT SIGN LENS (LOWER FWD) LOOSE. SECURED LENS PER MM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 48,922 hrs · 28,462 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED SIGN ASSY PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 48,380 hrs · 28,128 cycles

L1 DOOR LOWER EMERGENCY LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 47,805 hrs · 27,777 cycles

FWD ENTRY DOOR EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW M/M.

Part: SIGN — BROKEN (CABIN) · airframe 47,039 hrs · 27,327 cycles

OVERWING CEILING EMERGENCY EXIT SIGN LIGHT BROKEN. SECURED SIGN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 46,321 hrs · 26,925 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,014 hrs · 26,743 cycles

RT AFT EMERGENCY FLASHLIGHT INDICATOR LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,903 hrs · 26,668 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: RELAY — FAULTY (COCKPIT) · airframe 45,634 hrs · 26,519 cycles

DIVERSION - ON APPROACH, OVERHEAD PANEL P-5 PANEL ANNUNCIATOR WARNING LIGHTS ILLUMINATED ALL WITH NR 1 COM+2/NAV CONTROL PANELS FLASHING IN TEST MODE. REMOVED AND REPLACED R33 MASTER TEST RELAY PER MM.

Part: WIRE — DAMAGED (COCKPIT) · airframe 45,632 hrs · 26,518 cycles

AIR TURNBACK - LIGHT, WINDOW LIGHTS, PROBE LIGHTS, DOOR LIGHTS, LANDING GEAR LIGHTS ILLUMINATED. RADIO NR 1, NAV NR 2 INOP. REPAIRED WIRE TO TB502 ON P-5 OVERHEAD PANEL PER SWPM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,297 hrs · 26,333 cycles

LT EEPLS BROKEN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,803 hrs · 25,493 cycles

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

Part: CABLE — LOOSE (EVAC SLIDE) · airframe 430,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PACK CABLE LOOSE. SECURED CABLE PER MT.

Part: FITTING — OUT OF POSITION (GIRT BAR) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING OUT OF POSITION. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT CREASE BEAM CORRODED AT BS 360-4, LBL 61, WL 208. REPAIRED BEAM PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FLOOR ANGLE CORRODED UNDER THE AFT GIRT BAR FITTING. REPAIRED PLATE ASSY PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK ENTRY WAY FLOOR SUPPORT AFT ANGLE CORRODED. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 316 TO BS 336. REPAIRED BEAM PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK ENTRY WAY FLOOR PANEL SUPPORT WEB CORRODED. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 6R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,803 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR CREASE BEAM I/B ATTACH ANGLE CORRODED BETWEEN BS 316 TO BS 336. REPAIRED BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,967 hrs · 25,013 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 13. REMOVED AND REPLACED BULB PER MM.

Part: LENS — BROKEN (CABIN) · airframe 38,962 hrs · 22,583 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 37,165 hrs · 21,506 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 34,822 hrs · 20,084 cycles

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

Part: LIGHT — CRACKED (CABIN) · airframe 34,606 hrs · 19,946 cycles

R2 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SENSOR — FAULTY (FWD CARGO BAY) · airframe 34,544 hrs · 19,899 cycles

AIR TURBACK / DECLARED EMERGENCY. FWD CARGO COMPT FIRE WARN INDICATION. FOUND FWD CARGO COMPT B2 SENSOR FAULTY. REMOVED AND REPLACED FWD CEU AND B2 SENSOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,279 hrs · 17,413 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 27.50. REPAIRED FLOORBEAM PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER CLIP — CRACKED (BS 420 S4R) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 27.50. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, BETWEEN LBL 12.5 AND RBL 8.1. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 345, RBL 1. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 26. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,251 hrs · 17,390 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 343, RBL 1. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,183 hrs · 17,344 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,529 hrs · 12,753 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,367 hrs · 15,150 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,255 hrs · 12,288 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 16 ABC. RELAMPED LIGHT PER MM.

Part: COVER — LOOSE (L1 DOOR SLIDE) · airframe 23,510 hrs · 13,541 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 20,468 hrs · 11,833 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN UNDER AIRPHONE ANTENNA AT BS 500 + 8, CORRODED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 20,373 hrs · 11,778 cycles

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

Part: ACTUATOR — LEAKING (NLG) · airframe 20,168 hrs · 11,648 cycles

AFTER RETRACTING LANDING GEAR, NOSE WHEEL EXTENDED WHEN HANDLE PLACED TO OFF. CYCLED GEAR, WORKED NORMAL. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (ENTRY DOOR) · airframe 15,808 hrs · 9,233 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 12,131 hrs · 7,149 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: BUSHING — WORN (LT ELEVATOR.) · airframe 12,131 hrs · 7,149 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,552 hrs · 6,232 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 5, 11, 15 AND 20. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 9,388 hrs · 5,584 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 17. R&R COVER PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 9,350 hrs · 5,557 cycles

DURING SCHEDULED A2 CHECK (SI 11157-53), FOUND OIL CANNING AT AFT PRESS BULKHEAD WEB, BS 1016, STR 3L. REPAIRED WEB PER SWA RA.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 7,568 hrs · 4,586 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 3 & 4 TAB HINGE BUSHINGS PER MM.