N709SW

Part: HOUSING — LOOSE (CABIN) · airframe 78,363 hrs · 46,604 cycles

MID CABIN CEILING EMERGENCY EXIT LIGHT SIGN HANGING LOOSE ; / [01] REMOVED AND REPLACED CEILING EMERGENCY LIGHT HOUSING AS PER AMM 33-51-02.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 78,210 hrs · 46,521 cycles

194E PANEL ; THE 194E PANEL HAS 2 AREAS OF DELAMINATION ON SKIN FACE. / [01] REPLACE

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,210 hrs · 46,521 cycles

FUSELAGE SUBSURFACE CRACK INDICATION AT BS 500D+9 ABOVE STR4R ; FSELAGE SSRFACE CRACK INDICATION AT BS 500D+9 AOVE STR4R SING 737NDT PART 6; 53-30-25. VERIFIED FSELAGE SSRFACE CRACK INDICATION SING 737NDT PART 6; 53-30-18 AND 737NDT PART 4; 53-30-07. (CRACK INDICATION MEASRES APPROXIMATELY 1.5? IN LENGTH) SEE ATTACHED FILES FOR MORE INFORMATION. / [01] ADDED EA 21-153-03591-WIP2

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,671 hrs · 45,037 cycles

R1 DOOR SERVICE EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED OPS GOOD REF B737 AMM 33-51-04.

Part: COVER — MISSING (L2 DOOR SLIDE) · airframe 75,097 hrs · 44,704 cycles

AFT ENTRY DOOR SLIDE MANUAL INFLATION HANDLE COVER MISSING. REMOVED AND REPACKED SLIDE INTO CASE, IAW MT 725-61-06.

Part: LAMP — INOPERATIVE (EMERGENCY SIGN) · airframe 74,940 hrs · 44,603 cycles

FWD SERVICE DOOR EMERGENCY EXIT LOCATOR SIGN HAS INOP LAMPS. RELAMPED FWD SERVICE DOOR EMERGENCY EXIT LOCATOR SIGN AND PERFORMED GOOD INSTALLATION TEST, AS PER AMM 33-51-01-960-801 STEP 2.B1(1;3)2;4. 59132U 19SEP20.

Part: LAMP — INOPERATIVE (EMERGENCY SIGN) · airframe 74,940 hrs · 44,603 cycles

AFT SERVICE DOOR EMERGENCY EXIT SIGN HAS LAMPS INOP. RELAMPED AFT SERVICE DOOR EMERGENCY EXIT SIGN AND PERFORMED GOOD INSTALLATION TEST, AS PER AMM 33-51-01-960-801 STEP 2B1(A;C)2;4 59132U 19SEP20.

Part: STRIP — DAMAGED (FWD CARGO) · airframe 74,940 hrs · 44,603 cycles

FORWARD CARGO BAY AFT BULKHEAD FLOOR CAP STRIP IS DAMAGED / RECEIVED NEW FCB AFT BLKHD FLOOR CAP STRIP ON PO # 754287 NEW CAP STRIP TO BE INSTALLED ON CUST CARD # JPANEL-121-CLOSE

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 74,940 hrs · 44,603 cycles

AFT RT DOORWAY HEADER PANEL EMERGENCY DOWNLIGHT LENS IS CRACKED. REMOVED AND REPLACED AFT RT DOORWAY HEADER PANEL EMERGENCY DOWNLIGHT LENS, PER AMM 33-51-01-960-801 STEP 2B(1)(A) AND 2B(4).

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 74,940 hrs · 44,603 cycles

CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208. REMOVED OLD INTERCOSTAL STA 277-294 RBL 1 WL 208, IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW INTERCOSTAL, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG NR 141A5400. OK TO INSTALL. 8464R 14SEP20. INSP 21 14SEP20 INSTALLED, IAW SRM 51-40-02-0G-0 DWG NR 141A5400.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 74,940 hrs · 44,603 cycles

FWD LOWERED CEILING CLOSE OUT PANEL EXIT SIGN ASSY IS DAMAGED. REMOVED AND REPLACED FWD LOWERED CEILING CLOSEOUT PANEL EXIT SIGN ASSY, IAW AMM 33-51-01-960-802 STEP 3 C (5) (6). 57887U 11SEP20 5279C 11SEP20 INSP 267 9-11-20. OPS CHECK REQUIRED 5279C 11SEP20. PERFORMED OP'S CHECK OF FWD CLOSEOUT PANEL EXIT SIGN ASSY CHECKS GOOD, PER AMM 33-51-01-960-802 STEP 3C(7).

Part: ISOLATOR — BROKEN (L1 DOOR) · airframe 77,226 hrs · 45,946 cycles

ON TOP FRAME OF FED; FOUND AFT INBD ISOLATOR FOR FED PANEL 831EZ BROKEN / REMOVED AND REPLACED TOP FRAME AFT INBOARD ISOLATOR FOR PANEL 831EZ IAW SRM 51-40-02-0G-0 AND IPC 52-11-00-05. 59796C 9SEP20

Part: BULKHEAD — CRACKED (BS 663) · airframe 74,940 hrs · 44,603 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 14 WL 154. REPAIRED CRACK AT BS 663 LOWER COMPOSITE BULKHEAD AT LBL 14 WL 154, IAW SRM 51-70-04-2R-10.

Part: STRINGER — DAMAGED (BS 500D) · airframe 74,940 hrs · 44,603 cycles

STRINGER 25R BETWEEN BS 500D TO BS500D+10 HAS OVERSIZED HOLES COMMON THE INTERCOSTAL WEB. REPAIRED DAMAGED STRINGER 25R BETWEEN BS 500D TO 5000D + 10' COMMON TO THE INTERCOSTAL WEB, PER ER 20-03198 REV IR AND EA 20-153-01611 REV IR.

Part: SEAT TRACK — CORRODED (BS 500-520) · airframe 74,940 hrs · 44,603 cycles

CORROSION ON SEAT TRACK BS 500+10-520 LBL 45 WL 208 VARIOUS SPOTS. REMOVED CORROSION ON SEAT TRACK CROWN STA 500+10- 520 LBL 45 WL 208 VARIOUS SPOTS. MAX MATERIAL REMOVED WAS .038' X 1' X 1' ON TOP. OUT OF LIMITS, IAW SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. REMOVED AND REPLACED SEAT TRACK, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; SEAT TRACK WAS FABRICATED, PER NR ATSHFAB-100-303 REV C BOEING DWG NR 453A1610 JOB NR 533873.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 74,940 hrs · 44,603 cycles

FWD ENTRY DOOR BOTH ASSIST HANDLES ARE LOOSE. TIGHTENED FWD ENTRY DOOR BOTH ASSIST HANDLES, IAW AMM 52-11-31-400-802 STEP 3 G (3) 57887U 13SEP20.

Part: ATTACH ANGLE — CRACKED (BS 694) · airframe 74,940 hrs · 44,603 cycles

CRACKED ATTACH CLIP ON CABLE GUARD INTERCOSTAL STA 694; RBL 24; WL 204. / REMOVED DAMAGED ATTACH CLIP ON CABLE GUARD INTERCOSTAL BS.694 RBL24 WL204; AND INSTALLED NEW CLIP PER SRM 51-40-02; DWG 273A9112 SH.8; AND DWG 273A9110 SH.2; SRM 51-40-05.

Part: FLOORBEAM — CRACKED (BS 540 LBL 1) · airframe 74,940 hrs · 44,603 cycles

CRACKED BREAK PANEL STA 540; LBL 1; WL 208. / REMOVED AND REPLACED BREAK PANEL STA540; LBL1 WL208 PER DWG# 143A0060 REV A; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0

Part: SIDEWALL SUPPORT — CORRODED (BS 727-847) · airframe 74,940 hrs · 44,603 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUT PLATES HOLES BS727 TO BS847 WL156 LBL23 / REMOVED ACB L/H FLOOR TO SIDEWALL SUPPORT BS 727-847; LOCATED; DRILLED AND INSTALLED NEW L/H FLOOR TO SIDEWALL SUPPORT; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; AND DWG 146A7500.

Part: PRESSURE BLKHD — CORRODED (BS 1016) · airframe 74,940 hrs · 44,603 cycles

CORROSION ON INNER SURFACE OF BS 1016 PRESSURE DOME ON FWD SIDE RBL 2 TO LBL 1 WL 191. EVALUATED CORROSION ON INNER SURFCE OF BS 1016 PRESSURE DOME FWD SIDE. RBL 2-LBL 1 FOUND TO BE OUT OF LIMITS. REPAIRED BS 1016 PRESSURE BLKHD WEB, PER ER 20-03169 REV A EA 20-153-01658 REV 1.

Part: STRINGER — CORRODED (BS 536) · airframe 74,940 hrs · 44,603 cycles

CORROSION COMMON TO END OF STR 26R IN SNAKE PIT BS 536 WL 152. CORROSION COMMON TO END OF STR 26R BS 536 WL 152 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-03-1A-1. CUTOUT DAMAGED SECTION OF STRINGER AND REPAIRED, PER SRM 53-00-03-2R-1 SRM 51-40-02-0G-0.

Part: CARGO TRACK — CRACKED (BS 767) · airframe 74,940 hrs · 44,603 cycles

AFT CARGO BAY RT CARGO TIEDOWN TRACK IS CRACKED IN THE SADDLE AT BS 767 RBL 13.84 WL 155. REMOVED AND REPLACED AFT CARGO BAY RT CARGO TIEDOWN TRACK BS 747+8.5-BS 887 RBL 13.84 WL 155, IAW SRM 53-00-53-2R-3 PARA 4 STEPS C-P.

Part: STRINGER — CORRODED (BS 536) · airframe 74,940 hrs · 44,603 cycles

CORROSION COMMON TO END OF STR 26L IN SNAKE PIT BS 536 WL 152. CORROSION COMMON TO END OF STR 26L BS 536 WL 152 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-03-1A-1. CUTOUT DAMAGED SECTION OF STRINGER AND REPAIRED, PER SRM 53-00-03-2R-1 SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CRACKED (BS 694) · airframe 74,940 hrs · 44,603 cycles

CRACKED ATTACH CLIP ON FWD END OF CABLE GUARD INTERCOSTAL STA 694; RBL 1; WL 204-208. / REMOVED DAMAGED ATTACH CLIP ON FWD END OF CABLE GUARD INTERCOSTAL AT B.S.694 RBL1 WL204-208; AND INSTALLED NEW CLIP PER SRM 51-40-05; SRM 51-40-02; DWG 273A9112 SH.16; AND DWG 273A9111 SH.2.

Part: SUPPORT PLATE — CORRODED (AFT CARGO) · airframe 74,940 hrs · 44,603 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUT PLATES HOLES BS727 TO BS767 WL156 RBL23 / REMOVED CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE IN NUMEROUS 1' X 1' AREAS; ORIGINAL THICKNESS 0.040; MATERIAL REMOVED 0.015 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED AND REPLACED AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727 TO BS 767 WL 156 RBL 23 IAW SRM 51-40-02-0G-0; DWG 146A7500 AND DWG 146A0061

Part: SKIN — CORRODED (BS 677-707 S2R) · airframe 74,940 hrs · 44,603 cycles

***CORROSION*** ON EXTERNAL FUSELAGE SKIN BS677 - BS707 S-1 - TO S-2R WL306. MARKED / REPAIRED EXTERNAL FUSELAGE SKIN BS 677 - BS 707 STR S-1 TO S-2R WL 306 IAW SWA EA 20-153-01779 REV IR AND ATS ER 20-03207 REV IR

Part: STRINGER — CORRODED (BS 536) · airframe 74,940 hrs · 44,603 cycles

CORROSION COMMON TO END OF STR 25R IN SNAKE PIT BS 536 WL 154. REPAIRED CORROSION DAMAGED STR 25R IN SNAKE PIT BS 536 WL 154 COMMON TO END, PER ER 20-03198 REV 1R AND EA 20-153-01611 REV IR.

Part: WEB — CORRODED (BS 259.5) · airframe 74,940 hrs · 44,603 cycles

CORROSION ON BS 259.5 VERTICAL WEB LBL 5 WL 207. DAMAGE REPAIRED, PER EA 20-153-01732 REV IR ATS ER 20-03179 REV IR. REFER TO NRC U209733 FOR TRACKING.

Part: STRUCTURE — CORRODED (BS 259.5) · airframe 74,940 hrs · 44,603 cycles

CORROSION AT BS 259.5 AFT CHORD LBL 5 WL 208. DAMAGE REPAIRED, PER EA 20-153-01732 REV IR & ATS ER 20-03179 REV IR.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 74,940 hrs · 44,603 cycles

CORROSION AT BS 270 LBL 6 TO RBL 10 WL 208. DAMAGE REPAIRED, PER EA 1-A53-13812 REV 2.

Part: STRUCTURE — CORRODED (BS 259.5) · airframe 74,940 hrs · 44,603 cycles

CORROSION AT BS 259.5 FWD CHORD LBL 5 WL 208. REMOVED AND REPLACED BS 259 FWD CHORD WL 208, IAW BOEING DWG 141A7430 AND SRM 51-40-02-0G-0.

Part: PRESSURE DECK — CRACKED (BS 665) · airframe 74,940 hrs · 44,603 cycles

DURING COMPLETION OF CCN 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK TO BE CRACKED AT BS 665 LBL 31 WL 201, AREA MARKED. REPAIRED HORIZONTAL PRESSURE DECK DAMAGE AT BS 665 LBL31 WL201, PER SRM 53-40-51-2R-2.

Part: PRESSURE DECK — CRACKED (BS 673) · airframe 74,940 hrs · 44,603 cycles

DURING COMPLETION OF CCN 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK TO BE CRACKED AT BS 673 RBL 42 WL 201, AREA MARKED. REPAIRED HORIZONTAL PRESSURE DECK AT BS 673 RBL 42 WL 201, PER SRM 53-40-51-2R-2.

Part: FLOOR SKIN — DENTED (BS 255) · airframe 74,940 hrs · 44,603 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4-LBL 14 WL 207.54. DAMAGE REPAIRED, PER EA 1-A53-33179 REV 1.

Part: BULKHEAD — CRACKED (BS 663) · airframe 74,940 hrs · 44,603 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 14 WL 154. REMOVED CRACKED BS 663 LOWER COMPOSITE BULKHEAD LBL 6-LBL 70 WL 154. INSTALLED REPAIRED BULKHEAD, PER SRM 51-40-02-0G-0 DWG 111A1000 DWG 111A1001 DWG 144A7100.

Part: ATTACH BOLT — UNSECURE (R2 DOOR) · airframe 73,187 hrs · 43,486 cycles

R2 DOOR SLIDE BEZEL ATTACH BOLT FELL OUT. / SECURED SLIDE PER AMM.

Part: LIGHT — INOPERATIVE (ROW 24) · airframe 71,967 hrs · 42,666 cycles

PHOTOLUMINESCENT STRIP AT ROW 24 INOP. / R&R PHOTO STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,389 hrs · 42,283 cycles

EXTERNAL POWER PANEL FUSELAGE CUTOUT FORWARD LOWER CORNER DOUBLER SKIN CRACKED. / REPAIRED SKIN PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,293 hrs · 42,220 cycles

R/H OVERWING DOOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT IAW AMM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

BEAR STRAP CORRODED AT BS 310, STR 28L. REPAIRED BEAR STRAP IAW ER & EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

ANTENNA RING DOUBLER CORRODED AT BS 310, STR 28L. REPAIRED DOUBLER IAW ER & EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

BASE PLATE CORRODED AT BS 310, STR 28L. REPAIRED DOUBLER IAW ER & EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

SPLICE CORRODED BETWEEN BS 350 TO BS 366, STR 28R. REPAIRED SPLICE PER ER AND EA.

Part: RETAINER — BROKEN (RIGHT WING) · airframe 70,244 hrs · 41,548 cycles

_R/H WING CANOE FAIRING 642BB O/B SEAL RETAINER BROKEN / REPLACED R/H WING CANOE FAIRING 642BB O/B SEAL RETAINER PER SRM 51-40-02-0G-0 PARA 10; 11 AND PER BOEING DRAWING #113A9350 REV: F; RIVETS: 5 (EA.) BACR15GA-11. SEAL RETAINER P/N 113A9380-1. IDENIFIED PART IAW SRM 57-53-70-01-3 FIG. 4 SH 1 TABLE 3 FIG. 8 SH TABLE 6

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 70,244 hrs · 41,548 cycles

REPAIR; FWD CARGO; AFT CORNER SCUFF PLATE AS REQUIRED DUE TO CRACK AT FWD UPPER EDGE. / WELDED CRACK ON FWD CARGO AFT CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 STEPS 3 AND 4

Part: STRINGER — CRACKED (RT WING) · airframe 70,244 hrs · 41,548 cycles

RT WING FIXED LEADING EDGE UPPER SKIN STRINGER CRACKED AT IFSS 227. R&R STRINGER PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

AFT CARGO BAY FORWARD R/H FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 767 TO BS 787. R&R SHIELD IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO BAY INTERCOSTAL BAFFLE AFT ATTACHING CLIP CRACKED BETWEEN BS 500 TO BS 500A. R&R CLIP PER SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO BAY INTERCOSTAL BAFFLE AFT ATTACHING CLIP CRACKED BETWEEN BS 500A TO BS 500B. R&R CLIP PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO DOOR CUTOUT EDGE CRACKED BETWEEN BS 491.5 TO BS 500, STR 24R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

SKIN CORRODED AT BS 952, LBL 12. REPAIRED SKIN PER ER AND EA.

Part: SIGN — CRACKED (CABIN) · airframe 70,244 hrs · 41,548 cycles

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

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

L1 DOOR FORWARD CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW AMM.

Part: TRACK — CORRODED · airframe 70,244 hrs · 41,548 cycles

***CORROSION*** L/H SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 540 TO BS 600; LBL45 / REMOVAL AND INSTALLATION OF NEW SEAT TRACK FROM STA 540-727 LBL 45 ON CUSTOMER CARD N165740 800983 INTER-5096. 57575U 10/26/18

Part: SEAT TRACK — CORRODED (CABIN) · airframe 70,244 hrs · 41,548 cycles

***CORROSION*** L/H SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 653 TO BS 727; LBL45 / REMOVAL AND INSTALLATION OF NEW SEAT TRACK FROM STA 540-727 LBL 45 ON CUSTOMER CARD N165740 800983 INTER-5096. 57575U 10/26/18

Part: TRACK — CORRODED (CABIN) · airframe 70,244 hrs · 41,548 cycles

***CORROSION*** L/H SEAT TRACK HAS CORROSION AT BS 570; LBL 24 / REMOVAL AND INSTALLATION OF NEW SEAT TRACK FROM STA 540-727 LBL 24 ON CUSTOMER CARD N165736 800983 INTER-5092. 57575U 10/26/18

Part: TRACK — CORRODED (CABIN) · airframe 70,244 hrs · 41,548 cycles

***CORROSION*** L/H SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 663 TO BS 727; LBL 24 / REMOVAL AND INSTALLATION OF NEW SEAT TRACK FROM STA 540-727 LBL 24 ON CUSTOMER CARD N165736 800983 INTER-5092. 57575U 10/26/18

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

SEAT TRACK CORRODED BETWEEN BS 600 TO BS 663, RBL 45. REPAIRED SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

RT SEAT TRACK CHANNEL CORRODED AT BS 581, RBL 24. R&R SEAT TRACK IAW SRM & DWG.

Part: SPLICE — CORRODED (FWD FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

**CORROSION** ON BS 360; STR 28L INBD AND OUTBD END SPLICES / REMOVED AND REPLACED I/B AND O/B END SPLICES AT STR 28L BS 360 PER SRM 51-40-02-0G-0 AND BOEING DWG # 140A9101 92385U 12/05/18

Part: WEB — CORRODED (E & E COMPT) · airframe 70,244 hrs · 41,548 cycles

**CORROSION** WEB AT STR 28L BETWEEN BS 350-BS 360 / CORROSION ON WEB AT STR 28L BETWEEN STA 350-360 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS FOUND AND IS ONLY REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-09C. FABRICATED REPLACEMENT WEB OUT OF 7075 T6 0.032' LOT #5064425-1. REPLACEMENT WEB WILL BE INSTALLED ON CUSTOMER DEFECT #N165705 SA-M 326 A1228361 ITEM #2

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. R&R SHEAR TIE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

CHANNEL CORRODED AT BS 360, STR 28L. R&R CHANNEL IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27R TO STR 28R. R&R SHEAR TIE IAW SRM AND DWG.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

ANTENNA SUPPORT CHANNEL CORRODED AT BS 360, BL 0. R&R CHANNEL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

ANGLE CORRODED AT BS 360, STR 28L. R&R ANGLE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

INBOARD AND OUTBOARD END SPLICES CORRODED AT BS 360, STR 27R. R&R SPLICE IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

"T" CHORD CORRODED BETWEEN BS 358 TO BS 365, STR 28L. REPAIRED "T" CHORD IAW ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

STRINGER CLIP CORRODED AT BS 360, STR 28R. R&R CLIP IAW SRM AND DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

E&E EXHAUST DUCT DOUBLER CORRODED BETWEEN BS 360 TO BS 380, BETWEEN STR 28R TO STR 28L. R&R DOUBLER IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

BUTT SPLICE CORRODED AT BS 360, STR 28R. R&R BUTT SPLICE STRAP IAW SRM AND DWG.

Part: STIFFENER — CRACKED · airframe 70,244 hrs · 41,548 cycles

STIFFENER CRACKED AT BS 663 WL 145 LBL 27 P/N 111A1308-7 / RECIEVED NEW PART#111A1308-7 PO#711890 LOCATED & DRILLED IAW DWG 111A1000; SRM 51-40-05-0G-0 TO BE INSTALLED ON DEFECT CARD #N165689 COPY ATTACHED. 81146U 10/17/18

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

COCKPIT FLOOR PANEL INTERCOSTAL CORRODED BETWEEN BS 259.5 TO BS 277. R&R SUPPORT CHANNEL IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 70,244 hrs · 41,548 cycles

RT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED AT STAB STA 120.3, 3RD STIFFENER FROM FORWARD END. REPAIRED STIFFENER IAW SRM.

Part: PANEL — DELAMINATED (L/H VERT. STAB.) · airframe 70,244 hrs · 41,548 cycles

LEFT HAND VERTICAL STABILIZER PANEL 324 AL EDGE OF PANEL IS DELAMINATED / REPAIRED DELAMINATED EDGE OF L/H VERTICAL STAB PANEL 324 AL IAW 737-700 SRM 55-30-01-2R-9 AND 51-70-05-2R-6 LEAD 191 10-24-18

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 70,244 hrs · 41,548 cycles

RT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED AT STAB STA 120.3, 4TH STIFFENER FROM FORWARD END. REPAIRED STIFFENER IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

LT FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500A TO BS 500B. REPAIRED INTERCOSTAL IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

LT FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 400 TO BS 420. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

RT BAFFLE CRACKED BETWEEN BS 500A TO BS 500B. REPAIRED BAFFLE IAW ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

AFT CARGO REAR BULKHEAD SUPPORT ANGLE CORRODED AT BS 947.5, BETWEEN STR 25R TO STR 26L. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO AFT LT BULKHEAD SUPPORT CORRODED. R&R SUPPORT IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

STRINGER CORRODED BETWEEN BS 360 TO BS 380, STR 27R. R&R STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

STRINGER, CLIP CORRODED BETWEEN BS 360 TO BS 380, STR 28L. REPAIRED STRINGER IAW ER AND EA.

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 70,244 hrs · 41,548 cycles

***CORROSION*** AFT CARGO REAR BULKHEAD SUPPORT ANGLE STA 947.5; S21R TO S25R / REMOVED AND REPLACED AFT CARGO REAR BULKHEAD SUPPORT ANGLE @ STA 947.5 STR 21R TO 25R IAW SRM 51-40-02-0G-0 AND DWG 149A8117

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

LOWER FLANGE OF INTERCOSTAL CORRODED BETWEEN BS 927 TO BS 947, LBL 25. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 70,244 hrs · 41,548 cycles

RT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON INBOARD AT STAB STA 129.5, 2ND STIFFENER FROM FORWARD END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 70,244 hrs · 41,548 cycles

RT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED AT STAB STA 120.3, 2ND STIFFENER FROM FORWARD END. REPAIRED STIFFENER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

UPPER SURFACE OF AFT CARGO FLOOR RAIL CORRODED AT BS 927, LBL 2.5. REPAIRED RAIL IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

STRINGER CORRODED AT BS 365, STR 27L. REPAIRED STRINGER PER ER AND EA.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 70,244 hrs · 41,548 cycles

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

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

STRINGER SPLICE CORRODED AT BS 365, STR 27L. REPAIRED STRINGER SPLICE PER ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

STRINGER CORRODED BETWEEN BS 360 TO BS 380, STR 28R. REPAIRED STRINGER IAW ER AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO AFT RT BULKHEAD SUPPORT CORRODED. R&R SUPPORT PER SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 70,244 hrs · 41,548 cycles

AFT CARGO FLOOR RAIL CORRODED AT BS 934, RBL 13. R&R FLOOR RAIL IAW AMM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

LT HORIZONTAL PRESSURE DECK SHEAR TIE CORRODED AT BS 665, LBL 67. R&R SHEAR TIE IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO COMPARTMENT R/H SIDEWALL TO FLOOR SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO COMPARTMENT RT AFT SHIELD STRIP CORRODED BETWEEN BS 492 TO BS 500A, RBL 23. R&R SHIELD IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

FORWARD CARGO COMPARTMENT LT SIDEWALL TO FLOOR SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

LT HORIZONTAL PRESSURE DECK SHEAR TIE ANGLE CORRODED AT BS 665, LBL 67. R&R ANGLE IAW DWG & SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,244 hrs · 41,548 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3, THIRD VERTICAL STIFFENER. REPAIRED RIB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

AFT CARGO RT SIDEWALL TO FLOOR SUPPORT CORRODED BETWEEN BS 747 TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

LT FAIRING SUPPORT STRUCTURE CRACKED AT BS 663, LBL 25. R&R SUPPORT IAW SRM & DWG.

Part: CHANNEL — CORRODED (LT HORIZ STAB) · airframe 70,244 hrs · 41,548 cycles

LT HORIZONTAL STABILIZER AFT SPAR BAY 2 BALANCE BAY PANEL SUPPORT CORRODED. REPAIRED CHANNEL PER SRM & DWG.

Part: NONE — CORRODED (L/H FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

***CORROSION*** LH ENGINE UPPER NOSE COWL SKIN CORRODED AFT EDGE FROM 4 OCLOCK TO 8 OCLOCK POSITIONS (UPPER) / REMOVED + REPLACED #1 ENG NOSE (INLET) COWL IAW AMMS 73-21-05; 71-11-00; 71-11-01; + 71-00-00. (POS:#1; TAG NO:475165; P/N OFF:314-2100-2; S/N OFF:5806001; P/N ON:314-2100-2; S/N ON:0066001)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

RT WING TO BODY SUPPORT CRACKED AT BS 500D, STR 19R. R&R SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

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

Part: BARRIER — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

R/H BS663 LOWER VAPOR BARRIER CRACK AT LOWER I/B END OF EXHAUST DUCT CUTOUT / R/H BD663 LOWER VAPOR BARRIER CRACK AT LOWER I/B END OF EXAUST DUCT CUTOUT WAS REPAIRED ON DEFECT NO. 165461 (DOCUMENT INCLUDED). REMOVED AND REINSTALLED VERTICAL STIFFENER AT BS663 RBL14. BULB SEAL RETAINER AT BS663 RBL 14 TO 26; WING TO BODY SUPPORT AT BS652 TO 670 RBL14 F.O.M. IAW SRM 51-40-02-0G-0 AND DWG 111A1000. 92058U 10/15/18

Part: SKIN — CRACKED (LE SLAT) · airframe 70,244 hrs · 41,548 cycles

RT WING NR 6 SLAT STA 202.45 LOWER SURFACE OF THE LEADING EDGE NOSE SKIN AT ACTUATOR FITTING CRACKED. R&R NR 6 SLAT IAW MM & SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 70,244 hrs · 41,548 cycles

AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 70,207 hrs · 41,529 cycles

RT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: FLAP — DELAMINATED (RH OUTBD AFT FLA) · airframe 69,874 hrs · 41,311 cycles

SUPPLEMENTAL INFORMATION: WHILE PERFORMING PHASE I INSPECTION; FOUND ENVIRONMENTAL DELAMINATION OF THE RIGHT OUTBOARD AFT FLAP TRAILING EDGE WEDGE INBOARD BOTTOM CORNER; APPROXIMATELY 1' VERTICAL PLANE AND 2' HORIZONTAL PLANE. / PERMANENTLY REPAIRED DELAMINATION AT INBOARD BOTTOM CORNER OD AFT OUTBOARD RIGHT HAND FLAP TRAILING EDGE WEDGE PER SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-4

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 68,056 hrs · 40,171 cycles

RIGHT EMERGENCY EXIT DOOR LOWER HANDLE COVER LOOSE. INSTALLED THE COVER IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 67,791 hrs · 39,990 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 67,791 hrs · 39,990 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER DWG.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 67,791 hrs · 39,990 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY IAW DWG.

Part: BATTERY — FAILED (CABIN) · airframe 67,791 hrs · 39,990 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER DWG.

Part: BATTERY — FAILED (CABIN) · airframe 67,791 hrs · 39,990 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,229 hrs · 39,631 cycles

AFT EMERGENCY EXIT LIGHTS FAULTY. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,229 hrs · 39,631 cycles

FORWARD EMERGENCY EXIT LIGHTS FAULTY. R&R BATTERY PACK PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 66,880 hrs · 39,410 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 66,880 hrs · 39,410 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 65,862 hrs · 38,775 cycles

LT WING TRAILING EDGE RIB CRACKED IN RADIUS JUST OUTBOARD OF OUTBOARD FLAP WS 512. REPAIRED RIB PER EA.

Part: PANEL — DELAMINATED (RT WING) · airframe 65,862 hrs · 38,775 cycles

R/H WING FIXED TRAILING EDGE PANEL 551BB HAS A BURN MARK 1.5' X 0.25' WITH DELAMINATION ON THE INBD CENTER SIDE OF THE PANEL. / CORRECTION RH PANEL 651BB IS PANEL IN QUESTION NOT 551BB. REPLACED RH LOWER WING ACCESS PANEL 651BB REF AMM. 32-11-00.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 63,860 hrs · 37,595 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. REPAIRED BRACKET PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,645 hrs · 37,453 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,645 hrs · 37,453 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW AMM.

Part: WEB — CRACKED (LT WING) · airframe 63,645 hrs · 37,453 cycles

LEFT WING LANDING LIGHT COVE WEB CRACKED AT UPPER OUTBOARD CORNER BETWEEN KRAS 106.3 TO KRAS 125.3. R & R WEB IAW DWG.

Part: COVER — CRACKED (LT WING) · airframe 63,645 hrs · 37,453 cycles

LEFT WING ROOT UPPER STIFFENER AT LANDING LIGHT COVER CRACKED AT OUTBOARD END. REPAIRED COVER IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 63,645 hrs · 37,453 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE AT INBOARD EDGE OF PANEL 551EB CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,645 hrs · 37,453 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 45. R & R THE FLOOR SUPPORT IAW SRM.

Part: SPAR — CORRODED (LT WING) · airframe 63,645 hrs · 37,453 cycles

LT WING FRONT SPAR WEB CORRODED ON BONDING STRAP FOR BOOST PUMP. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CORRODED (BS 1016-1023) · airframe 63,645 hrs · 37,453 cycles

INTERCOSTAL CORRODED BETWEEN BS 1016 TO 1023, LBL 17. R & R THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 1016) · airframe 63,645 hrs · 37,453 cycles

RIGHT BULKHEAD INTERCOSTAL CORRODED AT BS 1016. R & R THE BULKHEAD INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 1006-1016) · airframe 63,645 hrs · 37,453 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS. 1006 TO BS. 1016, RBL 50. R & R THE CREASE BEAM IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

RT LOWER SILL WEB CORRODED BETWEEN BS 95 TO BS 990, RBL 53. R&R WEB IAW SRM AND DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

LT SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1016, LBL 50. R&R SHEAR WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

TEE SUPPORT ANGLE BELOW RT SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1000, RBL 49. R&R ANGLE IAW DWG AND SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

LT LOWER SILL WEB CORRODED BETWEEN BS 947 TO BS 994, LBL 53. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-759) · airframe 63,645 hrs · 37,453 cycles

LEFT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO 759, LBL 21. R & R THE SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 63,645 hrs · 37,453 cycles

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

Part: FLOORBEAM — CORRODED (BS 312) · airframe 63,645 hrs · 37,453 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 312, LBL 13. REPAIRED THE FLOORBEAM IAW ER & EA.

Part: INTERCOSTAL — CORRODED (BS 849) · airframe 63,645 hrs · 37,453 cycles

INTERCOSTAL CORRODED AT BS 849, RBL 6. R & R THE INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 63,645 hrs · 37,453 cycles

FLOORBEAM UPPER TEE CORRODED AT BS 967, RBL 27, UPPER AND LOWER SURFACES. REPAIRED THE FLOORBEAM IAW EA & ER.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 63,645 hrs · 37,453 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO 500D. R & R THE SUPPORT IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

RT HORIZONTAL WEB CRACKED AT 1016, RBL 30. R&R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 63,645 hrs · 37,453 cycles

FLOORBEAM UPPER TEE CORRODED AT BS 947, BETWEEN RBL 6 TO LBL 12. REPAIRED THE FLOORBEAM IAW EA & ER.

Part: STRINGER CLIP — CORRODED (BS 727D) · airframe 63,645 hrs · 37,453 cycles

STRINGER CLIP CORRODED AT BS. 727D, LBL 14. R & R THE STRINGER CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

FLOORBEAM UPPER FLANGE FORWARD EDGE CORRODED AT BS 328, RBL 48. REPAIRED CHORD PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · airframe 63,645 hrs · 37,453 cycles

FORWARD PASSENGER CABIN FLOOR SUPPORT CORRODED BETWEEN BS 328 TO 344, LBL 13. R & R THE FLOOR SUPPORT IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

G4 FLOOR SUPPORT OUTBOARD SHEAR WEB CORRODED BETWEEN BS 987 TO BS 1016, RBL 40. R&R SHEAR WEB IAW SRM AND DWG.

Part: BULKHEAD WEB — CORRODED (BS 1016) · airframe 63,645 hrs · 37,453 cycles

LEFT BULKHEAD WEB CORRODED AT BS 1016, LBL 10. R & R THE BULKHEAD WEB IAW SRM AND DWG.

Part: WEB — CORRODED (THRESHOLD) · airframe 63,645 hrs · 37,453 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R & R WEB IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 63,645 hrs · 37,453 cycles

FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO 767, RBL 20. R & R SIDEWALL SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 63,645 hrs · 37,453 cycles

CARGO TRACK CORRODED AT BS 727D, LBL 17. R & R CARGO TRACK SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D. R&R LOWER RAIL IAW SRM.

Part: STRAP — CORRODED (BS 1008-1016) · airframe 63,645 hrs · 37,453 cycles

AT AFT LAVATORY SHEAR STRAP CORRODED BETWEEN BS 1008 TO 1016, LBL 3. R & R THE STRAP IAW SRM.

Part: DOOR FRAME — CRACKED (R1 DOORWAY) · airframe 63,645 hrs · 37,453 cycles

R1 DOOR DOOR FRAME INTERIOR CRACKED AT WL 266. R & R THE DOOR FRAME IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,645 hrs · 37,453 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (BS 767-794) · airframe 63,645 hrs · 37,453 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO 794, RBL 21. R & R SHIELD IAW SRM.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 63,645 hrs · 37,453 cycles

FLOORBEAM UPPER TEE CORRODED AT BS 987, BETWEEN STRINGERS 17L TO 17R. REPAIRED FLOORBEAM IAW EA & ER.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,645 hrs · 37,453 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, RBL 31. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 63,645 hrs · 37,453 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R FLOOR SUPPORT IAW SRM.

Part: DOOR — CRACKED (RT MLG) · airframe 61,914 hrs · 36,427 cycles

RIGHT MLG CTR OF DOOR CRACKED. R & R DOOR IAW AMM.

Part: RIB — CRACKED (RT WING) · airframe 61,914 hrs · 36,427 cycles

RIGHT WING RIB AT WBL 413 CRACKED, AT UPPER BEAM. REPAIRED RIB IAW EA.

Part: ACTUATOR — CRACKED (RT MLG) · airframe 61,636 hrs · 36,271 cycles

RIGHT MLG ACTUATOR CRACKED. R & R RT MLG ACTUATOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,469 hrs · 36,171 cycles

LEFT OVERWING SIDEWALL EMER EXIT LOWER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 60,214 hrs · 35,473 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,747 hrs · 35,203 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M01675. R & R BATTERY PACK IAW AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,747 hrs · 35,203 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M01673. R & R BATTERY PACK IAW AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,747 hrs · 35,203 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M01672. R & R BATTERY PACK IAW AMM & DWG.

Part: LENS — BROKEN (EXIT SIGN) · airframe 59,502 hrs · 35,070 cycles

RIGHT WING EMER EXIT SIGN LENS COVER BROKEN AT LOWER SIDEWALL. R & R COVER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 58,703 hrs · 34,641 cycles

L1 DOOR EGRESS LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,669 hrs · 34,050 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 22. RE LAMPED LIGHT IAW AMM.

Part: STRINGER — CRACKED (LT WING) · airframe 57,656 hrs · 34,039 cycles

LEFT WING INBD FIXED LE STRINGER CRACKED. R & R STRINGER IAW SRM & DWG.

Part: FRAME — BUCKLED (FUSELAGE) · airframe 57,656 hrs · 34,039 cycles

FRAME BUCKLED AT BS 198, BETWEEN LBL 1 TO RBL 14. REPAIRED FRAME IAW SRM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 57,439 hrs · 33,921 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 18. CONNECTED CONNECTOR IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,439 hrs · 33,921 cycles

INTERCOSTAL CRACKED AT BS 520 STRINGER 19L. R & R INTERCOSTAL IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,439 hrs · 33,921 cycles

STUB BEAM CRACKED AT BS 616 RBL 70. REPAIRED STUB BEAM IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,439 hrs · 33,921 cycles

STRINGER CRACKED AT BS 540 STRINGER 22L. REPAIRED STRINGER IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,439 hrs · 33,921 cycles

LEFT WING OTBD FLAP UPPER SURFACE AT INBD TE CORNER DELAMINATED. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,439 hrs · 33,921 cycles

WHEEL WELL SPAR VERTICAL PRESS WEB CRACKED AT BS 663 LBL 41. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 57,439 hrs · 33,921 cycles

FIRST OFFICERS LT AFT SEAT TRACK CRACKED. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 57,439 hrs · 33,921 cycles

CAPTAIN`S LT FRONT SEAT TRACK CRACKED AT AFT LOWER RADIUS. R & R SEAT TRACK IAW AMM.

Part: PIN — LACK OF LUBE (COCKPIT DOOR) · airframe 57,439 hrs · 33,921 cycles

FLIGHT DECK DOOR UPPER EMER EXIT RT SIDE SLIDE PIN STUCK. LUBRICATED PIN IAW SOPM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,439 hrs · 33,921 cycles

WHEEL WELL SPAR VERTICAL PRESS WEB CRACKED AT BS 663 RBL 40. REPAIRED WEB IAW SRM & EA.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 57,439 hrs · 33,921 cycles

FIRST OFFICERS LT FWD SEAT TRACK CRACKED. R & R SEAT TRACK IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,439 hrs · 33,921 cycles

SKIN CRACKED AT SKIN BS 540 STRINGER 22L. REPAIRED SKIN IAW EA.

Part: DOUBLER — CRACKED (LE SLAT) · airframe 57,439 hrs · 33,921 cycles

LEFT WING NR 3 SLAT SKIN DOUBLER LOWER SURFACE OF THE LE AT ACTUATOR RIB CRACKED. REPAIRED DOUBLER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,439 hrs · 33,921 cycles

LEFT WING LOWER SURFACE OF THE LE SLAT NR 1 NOSE SKIN AT ACTUATOR RIBS CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,439 hrs · 33,921 cycles

RIGHT WING NR 8 SLAT SKIN CRACKED AT LOWER SURFACE OF THE LE ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,316 hrs · 33,854 cycles

FORWARD EMER LIGHTS BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 56,824 hrs · 33,563 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS LOOSE. R & R LENS IAW AMM.

Part: HOOK — OUT OF ADJUST (R1 DOOR) · airframe 55,991 hrs · 33,090 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOKS OUT OF ADJUSTMENT. ADJUSTED HOOKS IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 55,848 hrs · 33,005 cycles

AFT RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED THE FUNCTIONAL TEST. R & R BATTERY IAW AMM.

Part: PANEL — LOOSE (LT WING) · airframe 55,848 hrs · 33,005 cycles

LEFT WING INBD FIXED LE PANEL LOOSE. SECURED PANEL IAW EA.

Part: PANEL — LOOSE (RT WING) · airframe 55,848 hrs · 33,005 cycles

RIGHT WING INBD FIXED LE PANEL LOOSE. SECURED PANEL IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,350 hrs · 32,137 cycles

RT AFT SLIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

LT NR 1 COCKPIT WINDOW CRACKED IN UPPER OTBD CORNER. R &R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

RT NR 1 WINDOW FRAME OTBD UPPER AFT FASTENER HOLE CRACKED. R & R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

FRAME CRACKED AT BS 400, STINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

FRAME CRACKED AT STATION 727B STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

FRAME CRACKED AT STATION 747 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

FRAME CRACKED AT STATION 727D STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

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

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 54,099 hrs · 31,980 cycles

LT HORIZONTAL STABILIZER WING STA 92.7, 10" AFT OF FRONT SPAR RIB CRACKED IN STIFFENER ANGLE. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 54,099 hrs · 31,980 cycles

LT HORIZONTAL STABILIZER WING STA 92.7 20" AFT OF FWD SPAR RIB CRACKED IN STIFFENER ANGLE. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,099 hrs · 31,980 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME E-F POST SECOND LOWER CORNER FASTENER HOLE CRACKED AT FWD & AFT SIDES OF FASTENER HOLE. R & R FRAME IAW EA & DRAWING.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,850 hrs · 31,831 cycles

FWD EMERGENCY LIGHTS FAILED CAPACITY CHECK. R&R BATTERY PACK IAW MM.

Part: BLOCK — MISSING (FUSELAGE) · airframe 53,085 hrs · 31,380 cycles

EXTERNAL POWER DOOR CUTOUT AFT SIDE MISSING PHENOLIC LATCH BLOCK. REPAIRED CUTOUT IAW ER AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,085 hrs · 31,380 cycles

RIGHT FWD LAV EMERGENCY EXIT LIGHT BULBS INOP. R & R BULBS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,085 hrs · 31,380 cycles

EXTERNAL POWER DOOR CUTOUT CRACKED. REPAIRED CUTOUT IAW ER AND EA.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 53,085 hrs · 31,380 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT BULB INOP. R & R BULBS IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,085 hrs · 31,380 cycles

SEAT TRACK CRACKED AT STA 727B, RBL 24.75. REPAIRED SEAT TRACK IAW ER AND EA.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 53,085 hrs · 31,380 cycles

SEAT TRACK SPLICE PLATE CRACKED AT BS 727A+18, LBL 45.5. REMOVED AND REPLACED PLATE PER ACO.

Part: STRAP — CRACKED (FUSELAGE) · airframe 53,085 hrs · 31,380 cycles

STRAP CRACKED AT BS 807, RBL 26. R & R STRAP IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,085 hrs · 31,380 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED AT AFT CORNER. R & R WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,028 hrs · 31,350 cycles

RIGHT FWD EMERGENCY LIGHT IN PASS CABIN INOP. RELAMPED LIGHT IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,233 hrs · 30,859 cycles

R2 DOOR GIRT BAR CATCHES DOOR FRAME WHEN DOOR IS OPENED. REPOSITIONED SLIDE IN CASE PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,682 hrs · 30,506 cycles

MID RIGHT CABIN EMERGENCY LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M1669 PER M/M. OPS CHECK GOOD.

Part: SLIDE — CRACKED (RT HORIZ STAB) · airframe 51,682 hrs · 30,506 cycles

RIGHT HORIZONTAL STAB FWD LOWER SLIDE IS CRACK. REMOVED AND REPLACED PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,873 hrs · 29,999 cycles

SKIN CORRODED AT BS 500A+3, BL 0. REPAIRED SKIN IAW SRM & EA.

Part: BEAM — WORN (THRUST REVERSER)

REF: CMM 78-31-37, REV 024, 01JUL2012, FIGURE 21 AND RELATED BOEING SERVICE BULLETIN 737-78-1071. THE 315A2403-5 BEAM (ITEM 370A), COMPONENT OF THE 315A2402-3 LATCH BEAM ASSY (ITEM 305A) HAS MATERIAL WEAR ON IT`S OUTBOARD SURFACE LOCATED 14.0 FWD FROM AFT END AND .50 UP FROM LWR EDGE. MATERIAL WEAR AREA MEASURES APPROXIMATELY .85 LONG X .045 WIDE X .013 DEEP. WEAR APPEARS TO BE THE RESULT OF CONTACT WITH THE 315A2585 SEAL RETAINER.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 50,432 hrs · 29,715 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE PER M/M & MT.

Part: BATTERY — NO TEST (CABIN) · airframe 49,640 hrs · 29,249 cycles

FWD LEFT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,640 hrs · 29,249 cycles

AFT LEFT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER M/M.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,640 hrs · 29,249 cycles

AFT RIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER M/M.

Part: FLAP — CRACKED (RT WING) · airframe 48,759 hrs · 28,718 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT I/B AFT FLAP CRACKED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 46,808 hrs · 27,554 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT CRACKED AT LOWER L/E SKIN. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CRACKED AT BS 967, RBL 46. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT FWD EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, BETWEEN LBL 5 TO LBL 26. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED SKIN PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 967 TO BS 986.5, RBL 22. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 950, BETWEEN RBL 30 TO RBL 50. REPAIRED SUPPORT PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 294 TO BS 328, RBL 54. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED AT BS 947.5, RBL 52. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 500A, STR 8R. REPAIRED STRINGER PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBOARD SUPPORT WEB CRACKED BETWEEN BS 312 TO BS 328, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR WEB CRACKED AT 2ND STOP FITTING FROM FLOOR. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,114 hrs · 26,030 cycles

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

Part: STRAP — MISSING (LE SLAT) · airframe 44,092 hrs · 26,017 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 8 SLAT UPPER SURFACE O/B TRAILING EDGE STRAP MISSING. REMOVED AND REPLACED NR 8 SLAT PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 43,058 hrs · 25,434 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS DAMAGED BETWEEN ROW 13 TO ROW 14. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 41,494 hrs · 24,497 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 40,787 hrs · 24,077 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 40,787 hrs · 24,077 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,748 hrs · 24,048 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 40,589 hrs · 23,949 cycles

L1 DOOR EGRESS LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 39,915 hrs · 23,548 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,445 hrs · 22,627 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,445 hrs · 22,627 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,445 hrs · 22,627 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,249 hrs · 21,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 36,249 hrs · 21,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,275 hrs · 20,734 cycles

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

Part: FITTING — CORRODED (RT WING) · airframe 34,778 hrs · 20,448 cycles

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

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 34,029 hrs · 20,017 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,853 hrs · 19,922 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 33,853 hrs · 19,922 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.50. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,791 hrs · 19,888 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 3 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 30,369 hrs · 17,887 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 11 TO RBL 47. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 30,369 hrs · 17,887 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 20 TO RBL 48. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,369 hrs · 17,887 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 2 TO RBL 44. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 30,369 hrs · 17,887 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 30,369 hrs · 17,887 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 TO BS 787, RBL 7.5 TO LBL 17.5. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 731D) · airframe 30,369 hrs · 17,887 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 731D, RBL 7.5 TO LBL 7.5. REPAIRED FLOORBEAM PER SWA EA.

Part: HMU — FAULTY (NR 1 ENGINE) · airframe 29,629 hrs · 17,443 cycles

INFLIGHT SHUTDOWN, NR 1 ENGINE ROLLED BACK AT FL 390 AND FLAMED OUT. REMOVED AND REPLACED HMU, FUEL PUMP AND EEC PER MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 29,388 hrs · 17,299 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE IN RETAINING HOOKS. ADJUSTED EVAC SLIDE RETAINING HOOKS PER MM.

Part: BELLCRANK — BROKEN (TE FLAP ACT) · airframe 27,751 hrs · 16,366 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E FLAP INBOARD ACTUATOR BELLCRANK BROKEN. REMOVED AND REPLACED BELLCRANK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,066 hrs · 15,958 cycles

EEPLS STRIP COVER LOOSE BETWEEN ROW 6 DEF TO ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,482 hrs · 15,618 cycles

FUSELAGE SKIN CRACKED AT BS 235.8, EXTERNAL GROUND POWER DOOR CUTOUT. REPAIRED SKIN IAW EA.

Part: DRIVE ASSY — BROKEN (FLAP TRACK) · airframe 24,936 hrs · 14,776 cycles

DIVERSION/DECLARED EMERGENCY, FLIGHT ATTENDANT NOTIFIED COCKPIT THAT PIECE OF LT WING WAS FALLING OFF. VISUAL INSPECTION CONFIRMED THAT NR 2 OUTBOARD T/E FLAP TRACK FAIRING CANOE EXTENDED BELOW WING. REMOVED AND REPLACED NR 2 OUTBOARD T/E FLAP TRACK FAIRING CANOE DRIVE ROD PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 24,844 hrs · 14,729 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOYED. INSTALLED SLIDE ASSY PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,520 hrs · 14,541 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT R2 DOORWAY. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,740 hrs · 14,115 cycles

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

Part: ENGINE — FAILED (NR 1) · airframe 18,855 hrs · 11,393 cycles

ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURN BACK, NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 12,751 hrs · 7,871 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB AND BALLAST PER MM.

Part: CONTROL VALVE — FAILED (L/E SLAT) · airframe 12,720 hrs · 7,847 cycles

AIR TURNBACK, L/E SLATS WOULD NOT RETRACT AFTER T/O. REMOVED AND REPLACED AUTO SLAT CONTROL VALVE PER MM.

Part: CLIP — LOOSE (FWD ENTRY DOOR) · airframe 12,631 hrs · 7,781 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER CLIP LOOSE. SECURED CLIP PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 11,820 hrs · 7,317 cycles

DURING SCHEDULED A2 CHECK, SI 11157-53 FOUND AFT PRESSURE BULKHEAD OIL CANNED BETWEEN STR 5L & 11L AND BETWEEN STR 9R & 11R. REPAIRED BULKHEAD PER SWA RA.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 10,407 hrs · 6,502 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11052-55,FOUND RH ELEVATOR TRIM TAB ATTACH BUSHINGS WORN AT # 2 & #3 HINGES. R&R TRIM TAB BUSHINGS PER MM.

Part: BUSHING — WORN (LH ELEVATOR) · airframe 10,216 hrs · 6,392 cycles

DURING SCHEDULED C2 CHECK, FOUND VERTICAL PLAY AT LH ELEVATOR TAB # 3 HINGE. R&R # 3 HINGE BUSHINGS PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 10,216 hrs · 6,392 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. R&R EEPLS COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 9,405 hrs · 5,881 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS LENS MISSING AT FWD ENTRY. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 9,199 hrs · 5,772 cycles

EEPLS RED LENS LOOSE AT FWD SECTION. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 8,301 hrs · 5,251 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (PAX DOORWAY)

FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY SAGGING. REPOSITIONED SLIDE ASSY PER MM.

Part: TAB — CRACKED (LT & RT ELEV)

DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT ELEVATOR TABS WITH NUMEROUS CRACKS AROUND ATTACH POINT CUTOUTS. REMOVED AND REPLACED ELEVATOR TABS PER MM.

Part: CONTROLLER — INOP (LT/RT WINDSHIELD)

FLIGHT DIVERTED TPA DUE TO KNOWN ICING CONDITIONS IN BWI. COCKPIT L1 AND R2 WINDOW HEAT WERE INOP. REPLACED 2 WINDOW HEAT CONTROLLERS AND REPAIRED WIRING AT R2 TERMINAL.