N7818L

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,811 hrs · 40,445 cycles

EMERGENCY LIGHTING BATTERY PACK M1670 NOT HOLDING CHARGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1670, SEATS 17ABC, IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: SLIDE — OUT OF POSITION (AFT SERVICE DOOR) · airframe 67,206 hrs · 40,021 cycles

LH AFT SERVICE DOOR SLIDE FELL OUT / [01] REPACKED LH AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01. NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE.

Part: INLET — PULLED (#2 ENGINE) · airframe 66,818 hrs · 39,762 cycles

#2 ENGINE INLET O/B SKIN MULTIPLE FASTENERS PULLED THROUGH / [01] R&R #2 ENGINE INLET AS PER AMM 71-11-01. OPS CHECK OK.

Part: COVER — MISSING (L1 DOOR) · airframe 66,158 hrs · 39,345 cycles

WHITE EXIT LIGHT COVER FORWARD ENTRY DOOR IS MISSING / [01] OK TO CONTINUE PER MEL 25-10-01<BR>SP 1 B<BR>67148;[02] INSTALLED NEW FWD ENTRY DOOR EXIT LIGHT COVER PER AMM 33-51-01 OPS CHECK GOOD MEL CLEARED.

Part: PUMP — FAULTY (#1 ENGINE) · airframe 65,545 hrs · 38,963 cycles

#1 ENGINE WILL NOT ACCELERATE TO COMMANDED SETTING; THIS OCCURS DURING TAKE OFF AND CLIMB; THE N1 REMAINS 5% BELOW THE N2 ENGINE REGARDLESS OF THROTTLE POSITION; HAPPENS WITH A/T ON OR OFF; DIFFERENCE GOES AWAY SLOWLY UNTIL THE N1'S ARE MATCHED IN THE HIGH 20S. / [01] COMPLIED WITH FUEL PUMP INSPECTION 73-11-01; FOUND FUEL PUMP IMPELLER SHEERED; R & R FUEL PUMP PER MT 773-11-00.

Part: NONE — CRACKED (FUSELAGE) · airframe 65,272 hrs · 38,770 cycles

T-CLIP IS CRACK IN 193 PANEL LEFT SIDE APPROX. .75' ; / [01] INSTALLED FABRICATED T CLIP REF B737 SRM 51-40-02 USED I.P.C. 53-14-00 FOR FASTENER CALLOUT REF E.A.22-453-00329 REF P.O. COC (P.O.# P2345342)

Part: SKIN — DENTED (BS 219-224 S24L) · airframe 63,312 hrs · 37,556 cycles

DENT EXTERNAL SKIN LOCATED BETWEEN STA 219.5 TO STA 224.8 AND ABOVE S-24L FUSELAGE EXTERIOR ; 2021-217461 / EA # 21-153-01510 COMPLETED; EA # 21-153-01510 COMPLETED RII; EA # 21-153-01510 COMPLETED RII

Part: SKIN — DENTED (BS 219-224 S24L) · airframe 63,312 hrs · 37,556 cycles

DENT EXTERNAL SKIN LOCATED BETWEEN STA 219.5 TO STA 224.8 AND ABOVE S-24L FUSELAGE EXTERIOR ; 2021-217461 / PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510; PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510 RII; PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510 RII

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,312 hrs · 37,556 cycles

CRACK ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 6 AT RT WING (1 EA) ; / REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 6 AT RT WING (1E/A) IAW B737-700 SRM 51-40-02-0G-0; REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 6 AT RT WING (1E/A) IAW B737-700 SRM 51-40-02-0G-0

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,312 hrs · 37,556 cycles

CRACK ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 3 AT LT WING (1 EA) ; 2021-217453 / REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 3 AT LT WING (1 EA) IAW B737-700. SRM 51-40-02.; REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 3 AT LT WING (1 EA) IAW B737-700. SRM 51-40-02.

Part: WEB — CRACKED (BS 400-420 S26L) · airframe 63,312 hrs · 37,556 cycles

CRACK ON WEB LOCATED BETWEEN BS 400 TO BS 420 AND STRINGER 26L FWD CARGO COMPARTMENT ; 2021-217403 / REPLACED WEB LOCATED BETWEEN BS 400 TO BS 420 AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7505 REV: B; REPLACED WEB LOCATED BETWEEN BS 400 TO BS 420 AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7505 REV: B

Part: ANGLE — CRACKED (BS 420 S26L) · airframe 63,312 hrs · 37,556 cycles

CRACK ANGLE LOCATED ON BS 420 AND STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-217404 / REPLACED ANGLE LOCATED ON BS 420 AND STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 143A7505 REV :B; REPLACED ANGLE LOCATED ON BS 420 AND STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 143A7505 REV :B

Part: STIFFENER — CORRODED (BS 1088) · airframe 63,312 hrs · 37,556 cycles

CORROSION SUPPORT BRACKET (STIFFENER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL217 APPROX ON APU COMPARTMENT ; 2021-217348 / TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22.; REPLACED STIFFENER LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL 217 ON APU COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING # 148A2410 REV :-; REPLACED STIFFENER LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL 217 ON APU COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING # 148A2410 REV :-

Part: SUPPORT BRACKET — CORRODED (BS 1088) · airframe 63,312 hrs · 37,556 cycles

CORROSION SUPPORT BRACKET (STIFFENER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL224 APPROX. ON APU COMPARTMENT ; 2021-217349 / TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22.; REPLACED SUPPORT BRACKET (STIFFENER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL224 APPROX. ON APU COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING # 148A0924 REV :-; REPLACED SUPPORT BRACKET (STIFFENER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL224 APPROX. ON APU COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING # 148A0924 REV :-

Part: BEARING — CRACKED (LT WING TE FLAP) · airframe 63,312 hrs · 37,556 cycles

CRACK OB FLAP BEARING ROLLER TRACK #1 AT LT WING (2 EA) ; 2021-217318 / REPLACED BEARING ROLLER ON O/B FLAP TRACK CARRIAGE #1 AT LT WING (2 EA) IAW AMM 27-51-23-400-803 STEP 7.C.(2)(A) TOOL USED TORQUE PN:QD2R1000A. SN:0319122619. D/D:04 MAR 22.; COMPLETED

Part: PLATE — CRACKED (RT WING) · airframe 63,312 hrs · 37,556 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS 204.25 TO WS 228.25 AT RT WING ; 2021-217256 / REPLACED REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS 204.25 TO WS 228.25 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING #115A2001 REV:B; REPLACED REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS 204.25 TO WS 228.25 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING #115A2001 REV:B

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 63,312 hrs · 37,556 cycles

CRACK EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) ; 2021-217269 / REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA IAW AMM 33-51-01-960-802; REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA IAW AMM 33-51-01-960-802

Part: PLATE — CRACKED (RT WING) · airframe 63,312 hrs · 37,556 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS 228.25 TO WS 253.00 AT RT WING ; 2021-217259 / REPLACED REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS 228.25 TO WS 253.00 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #115A2001 REV:-; TASK CARD COMPLETE.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 63,312 hrs · 37,556 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-217206 / TOOL USED DIGITAL CALIPER PN:500-197-30;SN:15120588;DUE DATE:12-JUL-21.; REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW 737-700 SRM 53-30-15-2R-1 REPAIR 1. TOOL USED DIGITAL CALIPER PN:500-197-30;SN:15120588;DUE DATE:12-JUL-21.; REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW 737-700 SRM 53-30-15-2R-1 REPAIR 1.

Part: PLATE — CRACKED (RT WING) · airframe 63,312 hrs · 37,556 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATED BETWEEN WS 278.50 TO WS 302.50 AT RT WING ; 2021-217262 / INSTALLED NEW REAR SPAR CORRUGATED PLATE AND FASTENERS LOCATED BETWEEN WS278.50 TO WS302.50 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 REV. C; INSTALLED NEW REAR SPAR CORRUGATED PLATE AND FASTENERS LOCATED BETWEEN WS278.50 TO WS302.50 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 REV. C IS OK

Part: SUPPORT ANGLE — CRACKED (BS 690 BL0) · airframe 63,312 hrs · 37,556 cycles

CRACK SUPPORT ANGLE LOCATED AT BS 690 AT BL 0 CENTER SECTION ; 2021-217197 / RECORD INSPECTION WAS SELECTED IN ERROR. NOT REQUIRED FOR THIS TASK. AEMP DOES NOT HAVE ABILITY TO ACCESS THE SIGN OFF ONCE CREATED; REPLACED SUPPORT ANGLE LOCATED AT BS 690 AT BL 0 CENTER SECTION IAW DWG D273A9110 REV:- AND SRM B737-700 51-40-02; REPLACED SUPPORT ANGLE LOCATED AT BS 690 AT BL 0 CENTER SECTION IAW DWG D273A9110 REV:- AND SRM B737-700 51-40-02

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,312 hrs · 37,556 cycles

CRACK INSPAR RIB LOCATED STAB STA 120 .30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-217187 / PERFORMED REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5. PART USED: KIT T-SECTION P/N 55100003-1.; PERFORMED REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5. PART USED: KIT T-SECTION P/N 55100003-1.; COMPLETED

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,312 hrs · 37,556 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 20 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-217186 / TOOL USED CALIPER P/N 700-113-10 S/N 0013356 DUE DATE 01-APR-22 RADIUS GAUGE P/N S167C S/N AE-28450 DUE DATE 17-JUN-21; PERFORMED REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 20 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5 PART USED: KIT T-SECTION P/N:55100003-01.; COMPLETED

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,312 hrs · 37,556 cycles

CRACK ACCESS PANEL 542BB ON RETAINER SEAL AT LT WING. REPLACED ACCESS PANEL 542BB RETAINER SEAL AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #113A9375 REV:A; REPLACED ACCESS PANEL 542BB RETAINER SEAL AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #113A9375 REV:A

Part: SUPPORT ANGLE — CRACKED (BS 690 RBL 24.5) · airframe 63,312 hrs · 37,556 cycles

CRACK SUPPORT ANGLE LOCATED AT BS 690 AT RBBL 24.5 CENTER SECTION ; 2021-217196 / TOOL USED P/N: NORTEC 600D S/N 210138503 CAL DUE DATE: 05- MAR- 22; REPLACED SUPPORT ANGLE LOCATED AT BS 690 AT RBBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-02 DRAWING # 111A6000 REV:A AND 273A9110; REPLACED SUPPORT ANGLE LOCATED AT BS 690 AT RBBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-02 DRAWING # 111A6000 REV:A AND 273A9110

Part: STRUT — CRACKED (RT WING FUEL STA) · airframe 63,312 hrs · 37,556 cycles

CRACK FUEL STATION PANEL STRUT ASSY AT RT WING ; 2021-217199 / REMOVED AND REPLACED FUEL STATION PANEL STRUT AT RT WING IAW AMM 52-49-21-400-801-NG SUBTASK 52-49-21-420-004; REMOVED AND REPLACED FUEL STATION PANEL STRUT AT RT WING IAW AMM 52-49-21-400-801-NG SUBTASK 52-49-21-420-004

Part: SKIN — CRACKED (RT NR 6 SLAT) · airframe 63,312 hrs · 37,556 cycles

CRACK LOWER SURFACE SLAT 6 NOSE SKIN ACTUATOR FITTING RT WING ; 2021-217143 / TOOL USED PN/ NORTEC 600D; SN/ 2000053402; DUE DATE/ 23APR22.; RAISED NEW FAULT TTG8Q0058LX7 TO REMOVE AND REPLACE SLAT #6; RAISED NEW FAULT TTG8Q0058LX7 TO REMOVE AND REPLACE SLAT #6

Part: SKIN — CRACKED (RT K FLAP) · airframe 63,312 hrs · 37,556 cycles

CRACK KRUEGER FLAP LOCATED AT 6 INCH AFT EDGE AND 15 INCH O/B EDGE AT RT WING ; 2021-217167 / PERFORMED REPAIR IAW EA #21-157-01349-WIP1 AND EA #21-157-0134-9; PERFORMED REPAIR IAW EA #21-157-01349-WIP1 AND EA #21-157-0134-9 RII; PERFORMED REPAIR IAW EA #21-157-01349-WIP1 AND EA #21-157-0134-9 RII

Part: LIGHT — CRACKED (CABIN) · airframe 63,312 hrs · 37,556 cycles

CRACK PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (9 EA) ; 2021-217152 / REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (9 EA) I.A.W AMM 33-51-15-400-802; COMPLETE; REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (9 EA) I.A.W AMM 33-51-15-400-802

Part: VAPOR BARRIER — CRACKED (L/H MLG W/W) · airframe 62,696 hrs · 37,212 cycles

LEFT MAIN WHEEL WELL FORWARD LOWER VAPOR BARRIER CRACKED. / FACT AS A RESULT OF POST REPAIR INSPECTION

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,935 hrs · 36,151 cycles

EXTERNAL EMERGENCY LIGHT AFT OF R2 DOOR INOP / RE-LAMPED EXT. EMERGENCY LIGHT AFT OF R2 DOOR; OPS CHECK GOOD IAW AMM 33-51-04-960-801

Part: LATCH — LOOSE (R1 DOOR SLIDE) · airframe 60,569 hrs · 35,903 cycles

R1 DOOR ESCAPE SLIDE COVER LATCH NOT SECURED. / RESECURED COVER LATCH PER AMM & MT.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 58,323 hrs · 34,449 cycles

R/H AFT LOWERED CEILING PANEL EMERGENCY BATTERY PACK FAILED TO CHARGE (M1672). R&R BATTERY PACK IAW AMM.

Part: FLOOR SUPPORT — BROKEN · airframe 58,323 hrs · 34,449 cycles

FLOORBOARD SUPPORT AT STA. 540 BL0-24R BROKEN / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 BL-0 - RBL 24 IAW B737-700 SRM. 51-40-02-0G-0 AND DWG 143A0060 REV. B

Part: VAPOR BARRIER — UNRELIABLE (WHEEL WELL LH) · airframe 58,323 hrs · 34,449 cycles

DURING DTIP REPAIR SURVEY; DOUBLER REPAIR COMMON TO THE WING CENTER SECTION REAR SPAR VAPOR BARRIER; LOWER LH WEB (GFRP) BETWEEN LBL 6 TO LBL 31.83 WAS FOUND TO BE UNDOCUMENTED. REPLACEMENT REQUIRED. / VAPOR BARRIER @ STA 663 L/H SIDE REMOVED & REINSTALLED ON NRC X941106; REPAIRED ON BACKSHOP W/O 39281-1900-0002. PER SA-M 735 DTD 17FEB20 THE REPAIR WAS CONSISTENT WITH 737-700 SRM 57-10-10 -2R-2 PARAGRAPH 4. THE REPAIR WAS REMOVED AND A NEW CATEGORY A WET LAYUP REPAIR INSSTALLED PER 737-700 SRM 51-70-04-2R-10. (S CHIRAYIL E 104352)

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 58,323 hrs · 34,449 cycles

MAIN LANDING GEAR FORWARD PRESSURE BULKHEAD CRACKED AT BS. 663, RBL 34. REPAIRED BULKHEAD IAW EA.

Part: STRINGER — DAMAGED (FWD CARGO BAY) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT STR 19R STA 500D REQUIRES REPAIR DUE TO FREEZE PLUG. / REMOVED DAMAGED STR SECTION; FABRICATED REPAIR PARTS FROM BAC1493-249 7075T6 ATAG A88270; BAC1493-574 7075T6 ATAG A08345; INSTALLED AT STR 19R STA 500C TO 500D + 6' IAW SRM 53-00-03-2R-1 FIG 206; SRM 51-40-02-01-0G; SOPM 20-41-05

Part: SKIN — OUT OF TOLERANCE (EXT FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

DTIP - DOUBLER REPAIR FOUND ON LOWER EXTERNAL FUSELAGE SKIN AT BODY STATION 185; LBL 5; REPAIR DEVIATIONS REGARDING FASTENER TYPE; SPACING; AND REPAIR DOUBLER LOCATION REQUIRE INSTALLATION OF NEW REPAIR PER AAR EA 190305. / REMOVED EXISTING REPAIR ON EXTERNAL FUSELAGE SKIN AT STA 185; LBL 5 AND REPAIRED IAW AAR EA 190305 P1-P6; AND IR AND SWA EA 1-753-34785 REV IR.

Part: SKIN — DAMAGED (BS 380-400) · airframe 58,323 hrs · 34,449 cycles

SKIN CREASED BETWEEN BS. 380 TO BS. 400, BETWEEN 1" ABOVE STR. 24L TO 1" BELOW STR. 23L. / REPAIRED SKIN IAW EA.

Part: PANEL — DELAMINATED (LT WING) · airframe 58,323 hrs · 34,449 cycles

LH WING LEADING EDGE PANEL 521PB IS WARPED / DELAMINATED AT FWD INBD CORNER. / REPAIRED AND APPLIED DECORATIVE RESTORATIVE FINISH TO L/H WING LEADING EDGE PANEL #521PB OF DISBONDING OF EROSION STRIP (AS MARKED) IAW B737-700 SRM 52-41-01-2R-6 REV 67 AND B737 AMM 51-21-99-300-801 REV 68. A63650; A50544

Part: SKIN — CRACKED (BS 180-188) · airframe 58,323 hrs · 34,449 cycles

FASTENER HOLE OF T CORD CRACKED BETWEEN BS. 180 TO BS. 188, BETWEEN LBL 1 TO LBL 8. / REPAIRED SKIN PER EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

WEB SUPPORT CLIP CRACKED AT AFT END BS. 294, RBL 53. R&R CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 24. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: FUEL CELL — CORRODED (LT WING) · airframe 58,323 hrs · 34,449 cycles

LEFT WING FUEL PANEL 532KB HAS CORROSION AROUND INNER LIP OF PANEL - MARKED / EVALUATED CORROSION AROUND INNER LIP OF LH WING FUEL 532KB. CORROSION DAMAGE OUTSIDE OF SRM REPAIR LIMITS. UNABLE TO ENSURE WIDTH AND WILL REMAIN FLAT TO WITHIN 0.005' IAW B737 SRM 57-20-01-2R-1 FIGURE 203 SHEET 1 CIRCLE NOTE A. ORDERED AND RECEIVED SERVICABLE PANEL FOR LEFT WING FUEL PANEL 532KB IAW B737 SRM 51-10-02-0G-0 STEP 9A AND IPC 28-11-11-02. ATAG#FY1462

Part: BEAM — CRACKED (R1 DOOR) · airframe 58,323 hrs · 34,449 cycles

R1 DOOR BEAM #4 CRACKED IN RADIUS UPPER INBOARD. / R&R R1 DOOR # 4 BEAM IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

CABIN FLOOR PANEL 232DF DISBONDED AND TORN ON LWR SKIN AT FWD INBD CORNER. / REPAIRED PASSENGER CABIN FLOOR PANEL 232DF DISBONDED ON LWR SKIN AT FWD INBD IAW B737-700 SRM 53-00-50-2R-1 REV 67 REPAIR 1 TAB 201 AND 53-00-50-2R-0 (A20045; A13436; 42408)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

CABIN FLOOR PANEL 231ZF DISBONDED AND TORN ON LWR SKIN AT AFT INBD CORNER. / REPAIRED PASSENGER CABIN FLOOR BAORD 231ZF DISBONDED ON LWR SKIN AT AFT IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 67 TAB 201 AND SRM 53-00-50-2R-0 (A20045; A13436; A42408)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

CABIN FLOOR PANEL 241BF UPR AND LWR SKINS DISBONDED AT FWD OTBD CORNER. / REPLACED PASENGER CABIN FLOOR PANEL 241 BF IAW B737-700 SRM 53-00-50-2R-0 GENERAL STEP 1 (A) BAC 5085 PAG 20 8.4.2.1; BOEING DOC PANEL NO INSTALLED ON THIS DOCUMENT (A40776; A49691; MP1341)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOOR PANEL 242 UF; UPPER SURFACE HAS AREAS OF MISSING FIBERS IN FACE SHEET. / REPAIRED AFT CABIN FLOOR PANEL 242VF I/A/W SRM 53-00-50-2R-1 REV 67 PARA 3 STEPS N; L; M AND I/A/W SRM 53-00-50-2R-0 REV 67.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOOR PANEL 241 AAF; UPPER SURFACE HAS AREAS OF MISSING FIBERS IN FACE SHEET. / REPAIRED AFT CABIN FLOOR PANEL 241 AAF I/A/W SRM 53-00-50-2R-1 REV 67 PARA 3 STEPS N .L; M AND I/A/W SRM 53-00-50-2R-0 REV 67

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOOR PANEL 241 ACF; UPPER SURFACE HAS AREAS OF MISSING FIBERS IN FACE SHEET. / REPAIRED AFT CABIN FLOOR PANEL 241ACF I/A/W SRM 53-00-50-2R-1 REV 67 PARA 3 STEPS N; L; M; AND I/A/W SRM 53-00-50-2R-0 REV 67 A13426; A10124

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOOR PANEL 241 ABF; UPPER SURFACE HAS AREAS OF MISSING FIBERS IN FACE SHEET. / REPAIRED AFT CABIN FLOOR PANEL 241ABF I/A/W SRM 53-00-50-2R-1 REV 67 PARA STEPS N; L; M AND I/A/W SRM 53-00-50-2R-0 REV 67

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

CABIN FLOOR PANEL 231FF DISBONDED AND CRACKED ON LWR SKIN AT FWD INBD CORNER. / REPAIRED PASSENEGR CABIN FLOOR PANEL 231FF DISBONDED IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 67 AND SRM 53-00-50-2R-0 GENERAL (A20045; A13436; A42408)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

CABIN FLOOR PANEL 232DF DISBONDED AND TORN ON LWR SKIN AT AFT INBD CORNER. / REPAIRED PASSENGER CABIN FLOOR PANEL 232DF DISBONDED ON LWR SKIN AFT IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 67 TAB 201 AND 53-00-50-2R-0 (A20045; A13436; A42408)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOOR PANEL 241 ADF; UPPER SURFACE HAS AREAS OF MISSING FIBERS IN FACE SHEET. / REPAIRED AFT CABIIN FLOOR PANEL 241DF I/A/W SRM 53-00-50-2R-1 REV 67 PARA 3 STEPS U ;L; AND M AND I/A/W SRM 53-00-50-2R-0 REV 67. A13436; A101L4

Part: FLOOR PANEL — TORN (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

CABIN FLOOR PANEL 232JF LWR SKIN TORN AND CRUSHED AT FWD EDGE 7' OTBD OF INBD EDGE. / REPAIRED PASSENGER CABIN FLOOR PANEL 232JF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 67 AND SRM 53-00-50-2R-0 GENERAL (A20045; A13936; A42408)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOOR PANEL 242 VF; UPPER SURFACE HAS AREAS OF MISSING FIBERS IN FACE SHEET. / REPAIRED AFT CABIN FLOOR PANEL 242VF I/A/W SRM 53-00-50-2R-1 REV 67 PARA 3. STEPS N; L; M; AND SRM 53-00-50-2R-0 REV 6).

Part: SUPPORT BRACKET — CRACKED (AFT ENTRY DOOR () · airframe 58,323 hrs · 34,449 cycles

AFT ENTRY DOOR LOWER HINGE ACCESS 834DZ HAS CRACKED SUPPORT BRACKET. / REPAIRED CRACKED SUPPRT BRACKET OUT AFT ENTRY DOOR LOWER HINGE ACCESS 834DZ. I.A.W B737-700 SRM 51-40-02-0G & BOEING DWG #411A2119 TY:DWG; ID:0072; REV:-

Part: STRINGER — CORRODED (BS 376-380) · airframe 58,323 hrs · 34,449 cycles

EQUIPMENT AND ELECTRONICS COMPARTMENT STRINGER CORRODED BETWEEN BS. 376 TO BS. 380, STR. 23L. / R&R STRINGER IAW SRM.

Part: SUPPORT BRACKET — CORRODED (E&E BAY) · airframe 58,323 hrs · 34,449 cycles

E & E COMPARTMENT STA 380 STR 23L; P91 SUPPORT BRACKET IS CORRODED. / REMOVED CORRODED SUPPORT ANGLE AND REPLACED WITH NREW SUPPORT ANGLE P/N 143A9173-25 IAW B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 143A9173 LEV.-

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

EQUIPMENT AND ELECTRONIC COMPARTMENT CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 663 BULKHEAD) · airframe 58,323 hrs · 34,449 cycles

VAPOR BARRIER CRACKED AT BS. 663, BETWEEN LBL 45 TO LBL 48, AFT UPPER CHORD OF WING BOX. REPAIRED UPPER CHORD IAW EA.

Part: FRAME — CRACKED (BS 663 BULKHEAD) · airframe 58,323 hrs · 34,449 cycles

VAPOR BARRIER AFT UPPER CHORD OF WING BOX CRACKED AT BS. 663, BETWEEN RBL 45 TO RBL 48. / REPAIRED UPPER CHORD IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 58,323 hrs · 34,449 cycles

RT HORIZONTAL STAB LEADING EDGE PANEL 341B AT LEADING EDGE STA 86.66 RIB CHORD CRACKED. R&R CHORD ASSEMBLY IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPT; FLOOR PANEL 140DF CORROSION ON PANEL. MARKED. / REPLACED FLOOR PANEL 140DF 'ON BENCH' W/ P/N 453A2610-20 SI# 7253767 ATAG# WN4460 IAW DWG 453A2600 SHEET 43 REV A BEGAN REMOVING CORROSION FROM AFT CARGO COMPT FLOOR PANEL 140DF IAW SRM 51-10-02. TOTAL ACCUMULATED DAMAGE LENGTH EXCEEDED 20 INCHES AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 SHEET 1

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPT; FLOOR PANEL 140BF CORROSION ON EDGES. / REPLACED FLOOR PANEL 140BF 'ON BENCH' W/ PN 453A2610-32 SI# 725313 ATAG# WN7863 IAW DWG 453A2600 REV A SHEET 43 REMOVED CORROSION FROM FLOOR PANEL 140BF IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS; EXCEEDING 20' MAX.; IAW SRM 53-00-53-1A-1 FIG. 102.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 58,323 hrs · 34,449 cycles

RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341B AT LEADING EDGE STA. 78.29 RIB CHORD CRACKED. R&R CHORD ASSEMBLY IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

FRAME AFT SIDE INTERCOSTAL TO FRAME CLIP CORRODED BS. 277, STR. 5R. R&R CLIP IAW SRM & DWG.

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 58,323 hrs · 34,449 cycles

LT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. R&R HATCH HOOK IAW MT.

Part: RETAINER — CRACKED (LEFT WING) · airframe 58,323 hrs · 34,449 cycles

LEFT WING #2 FLAP TRACK FORWARD FAIRING 543AB INBOARD SEAL RETAINER IS CRACKED / REMOVED AND REPLACED #2 FLAP TRACK FWD FAIRING 543AB INBD SEAL RETAINER IAW BOEING SRM 51-40-02-0G-0 FOR 737 LEFT WING A63565

Part: STRINGER CLIP — DEFORMED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT CLIP DEFORMED AT BS. 727C, STR. 21L. R&R STRINGER CLIP IAW SRM & DWG.

Part: RETAINER — CRACKED (LEFT WING) · airframe 58,323 hrs · 34,449 cycles

LEFT WING #3 FLAP TRACK FORWARD FAIRING 542AB OUTBOARD SEAL RETAINER IS CRACKED / R/R LW #3FLAP TRACK FWD FAIRING O/B SEAL RETAINER IAW SRM 51-40-02-0G-0 (STEP 91;B1) ATAG:A53229

Part: GUSSET — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

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

Part: RETAINER — CRACKED (LEFT WING) · airframe 58,323 hrs · 34,449 cycles

LEFT WING #2 FLAP TRACK FORWARD FAIRING 543AB OUTBOARD SEAL RETAINER IS CRACKED / REMOVED AND REPLACED LEFT WING #2 FLAP TRACK FWD FAIRING 543AB OTBD SEAL RETAINIER IAW BOEING 737 SRM 51-40-02-0G-0 A63565

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 58,323 hrs · 34,449 cycles

RT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. CLEANED STRAP IAW AMM.

Part: STRINGER CLIP — DEFORMED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT CLIP DEFORMED AT BS. 767, STR. 21R. R&R STRINGER CLIP IAW SRM & DWG.

Part: STRINGER CLIP — DEFORMED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT CLIP DEFORMED AT BS. 727B, STR. 22R. R&R STRINGER CLIP IAW SRM & DWG.

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO STA 947; ABOVE STR 25R; SPLICE PLATE FOR AFT BULKHEAD ATTACH ANGLE HAS CORROSION / REMOVED CORROSION ON SPLICE PLATE IAW SRM 51-10-02-0G-0. ORIGINAL MAT THICKNESS .064'; LOSS OF .008'; WITH .056 REMAINING. FOUND TO BE OUT OF LIMITS IAW 51-10-02-0G-0 PARA 9C. . FABRICATED NEW SPLICE PLATE FROM 7075-0 .063' IAW DWG 149A8118 REV A ATAG # A32454. REMOVED DAMAGED SPLICE PLATE IAW SRM 51-40-02-0G-0 FIG 8. DRILLED AND LOCATED IAW DWG 149A8118 REV A SHEET 11. TREATED AND PRIMED IAW SRM 51-20-01-0G-0. TOP COATED SPLICE IAW AMM 51-21-99-300-801. INSTALLED NEW SPLICE PLATE IAW AFT CARGO STA 947 ABOVE STR 25R AT AFT BULKHEAD P/N 149A8118-13 IAW DWG 149A8118 REV A SHEET 6; SRM 51-40-02-0G-0.

Part: STRINGER CLIP — BENT (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT CLIP BENT AT BS. 727E, STR. 24L. R&R STRINGER CLIP IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

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

Part: STRINGER CLIP — DEFORMED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT CLIP DEFORMED AT BS. 727B, STR. 24L. R&R STRINGER CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

FRAME FORWARD SIDE STRINGER CLIP CRACKED AT BS. 294.5, STR. 13L. R&R STRINGER CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

FORWARD CARGO COMPARTMENT BULKHEAD SUPPORT ANGLE CORRODED AT BS. 500D, BETWEEN STR. 26L TO STR. 26R. R&R ANGLE IAW SRM & DWG.

Part: FAILSAFE — CORRODED (BS 986.5) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FAIL SAFE CHORD SPLICE CORRODED AT BS. 986.5, BETWEEN STR. 3R TO STR. 4R. / R&R CHORD SPLICE IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL CRACKED BETWEEN BS. 500A TO BS. 500B, STR. 26L FORWARD FASTENERS. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

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

Part: PANEL — DEBONDED (RIGHT WING) · airframe 58,323 hrs · 34,449 cycles

RIGHT WING LE PANEL 621UB DISBONDED IN CORNER. / REPAIRED RIGHT WING L/E PANEL 621UB CORNER AS MARKED IAW SRM 51-70-04-2R-13 REV 67.

Part: PANEL — DEBONDED (RIGHT WING) · airframe 58,323 hrs · 34,449 cycles

RIGHT WING LE PANEL 621TB DISBONDED AND CRACKED IN CORNER. / REPAIRED AND APPLIED DECORATIVE FINISH TO RIGHT WING L/E PANEL 621TB OF A DISBOND ON CORNER (AS MARKED) IAW B737-700 SRM 51-70-04-2R-13 REV 67 AND B737 AMM 51-21-99-300-801 REV 68 A38760; AA50544

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 58,323 hrs · 34,449 cycles

R\H HORIZONTAL STAB FWD SPAR FITTNG UPPER SLIDING SEAL CRACKED. / REMOVED AND INSTALLED R/H HORIZONTAL STAB FWD. SPAR FITTING UPPER SLIDING SEAL IAW BOEING 737 AMM 51-31-31-000-802 AND 51-31-31-400-802 A44532; A84335; A71376 ATAGS-A01192; A06826; ATAG-A51933

Part: PANEL — DEBONDED (RIGHT WING) · airframe 58,323 hrs · 34,449 cycles

RIGHT WING LE PANEL 621DB IS DISBONDED AT CUTOUT. / REPAIRED R/H WING L/E PANEL 621DB AT I/B AND O/B CORNERS AT CUTOUT AREA IAW B737 SRM 51-70-04-2R-13 REV 67. A38760

Part: PANEL — CRACKED (RIGHT WING) · airframe 58,323 hrs · 34,449 cycles

RIGHT WING LE PANEL 621ZB IS DISBONDED AND CRACKED IN CORNER. / REPAIRED RIGHT WING L/E PANEL 321ZB CORNER AS MARKED IAW SRM 51-70-04-2R-13 REV 67.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

EXTERNAL FUSELAGE SKIN CORRODED BETWEEN BS. 907+4 TO BS. 927, BETWEEN STR. 27R TO STR. 26R. REPAIRED SKIN IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT RT "Z" ANGLE UPPER SURFACE CORRODED BETWEEN BS. 727B+6 TO BS. 767. R&R ZEE ANGLE DWG AND SRM.

Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 58,323 hrs · 34,449 cycles

AFT CARGO COMPARTMENT STA 867 LBL 11 STANCHION LOWER ATTACH ANGLE CRACKED. / REMOVED AFT CARGO STA 867; LBL 11 STANCHION ATTACH ANGLE AND REPLACED WITH NEW; PN# 149A8109U114 IAW SRM 51-40-02-0G-0 PARA 4 AND DWG 149A8109 REV: -; DWG 149A8102 REV:-

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

FORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS. 500D, STR. 26L. R&R STRINGER CLIP IAW DWG.

Part: MOUNT — CRACKED (CARGO BAY) · airframe 58,323 hrs · 34,449 cycles

FORWARD CARGO COMPARTMENT NUT PLATE MOUNT CRACKED AT BS. 500B, BETWEEN STR. 24L TO STR. 25L. R&R NUTPLATE MOUNT IAW SRM & DWG.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT AFT SHIELD HAS 2 EA. AREAS OF CORROSION AT FASTENER HOLES AS MARKED. STA; 497 TO 500A; RBL 25 / REMOVED CORROSION FROM FWD CARGO AFT SHILED; VERIFIED WITH 10X MAGNIFYING GLASS IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS .032' WITH A LOSS OF .015'; .017' REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-01-1. TOOL # 36309 CAL DUE 04/19/20. FABRICATED IN BACK SHOP ON W/O 392181-1400-0002. HEAT TREATED TO T62 ON BACKSHOP WO # 39281-1400-0002. LOCATED AND DRILLED IAW DWG 143A0080 SHEET 9 REV - AND SRM 51-40-05-0G. TREATED AND PRIMED IAW SRM 51-20-01-0G. INSTALLED FWD CARGO AFT SHIELD IAW SRM 51-40-02-0G- PARA 4 AND DWG 143A0080 SHEET 9 REV - P/N 143A8126-19

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,323 hrs · 34,449 cycles

AFT CABIN FLOORBEAM STANCHION SUPPORT INTERCOSTAL CRACKED AT BS. 850, LBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: MOUNT — CRACKED (FWD CARGO LH) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT STA 500A BETWEEN S24L AND S25L NUT PLATE MOUNT IS CRACKED. / REMOVED + REPLACED NUTPLATE MOUNT AT STA 500A 524L-525L P/N 417A2106-26 AAR-AJJ IAW SRM 51-40-02-01-0G; SRM 51-40-05; DWG 417A2106 REV AF SOPM 20-41-05

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 58,323 hrs · 34,449 cycles

WING TO BODY PANEL 193CL INBD EDGE HAS HOLE THAT IS ELONGATED. / REPAIRED WING TO BODY PANEL 193CL I/B EDGE FASTNER HOLE AS MARKED IAW 737-700 SRM 51-70-04-2R-01 REV 67.

Part: MOUNT — CORRODED (FWD CARGO LH) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT STA 500C BETWEEN S24L TO S25L NUT PLATE MOUNT HAS CORROSION ON THE UNDERSIDE. / BEGAN REMOVING CORROSION ON NUTPLATE MOUNT AT STA 500C ; S24L S25L. ORIG 'T' .040; REMAINING .020' LOSS AT 020 NO LIMITS GIVEN ' REPAIRABLE BY REPLACEMENT; REMOVED AND REPALCED P/N 417A2106-32 AAR AJJ IAW SRM 51-10-02-0G; SRM 51-40-02-06; SRM 51-40-05 DWG 417A2106 REV-; SOPM 20-41-05

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT PANEL 120AF HAS CORROSION AT THE OUTER EDGES AS MARKED. / REMOVED CORROSION FROM FWD CARGO PANEL 120AF. MAX MAT. LOSS .066' ORIGINAL MAT .071'; WITH VERIFICATION OF CORROSION REMOVAL WITH 10X MAGNIFING GLASS. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0 AND SRM 53-00-53-1A; 53-30-53-01-1 SRM; CAL DUE 11/01/19 TOOL# 31794. REPLACED PANEL 120AF 'ON THE BENCH' W/ PN# 453A1610-14 SI# 7253765 ATAG# WN4101 IAW DWG 453A1600 REV A SHEET 3 INFO ONLY: P/N 453A1610-14

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT AFT SCUFF PLATE IS CRACKED IN TWO PLACES. / RECIEVED WELDED SCUFF PLATE FROM BACKSHOP ON BACKSHOP W/O 39281/1400/0001 REPAIR COMPLETED IAW EA NO 1-A53-2076 REV 11

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 58,323 hrs · 34,449 cycles

FWD CARGO COMPARTMENT PANEL 120CF HAS CORROSION AT THE OUTER EDGES AS MARKED. / REMOVED CORROSION FROM FWD COMP FLOOR PANEL 120CF. MAX MATERIAL REMOVED .006' WITH TOTAL COMBINED LENGTH 70.5' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G SRM 51-00-53-1A-1. TOOL# 31794 CAL DUE# 11/0119. REPLACED FLOOR PANEL 120CF ON THE BENCH WITH PN# 453A1610-32 SI# 7253766 IAW DWG 453A1600 REV A SHEET 43

Part: FITTING — CRACKED (LT WING) · airframe 58,152 hrs · 34,351 cycles

LEFT WING TE HAS FITTING CRACKED IN FIXED TRAILING EDGE FLAP WELL; APPROXIMATE WS 278 LEFT / REMOVED AND REPLACED FITTING PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,987 hrs · 34,252 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE APPEARED LOOSE. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,910 hrs · 34,209 cycles

RT AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LAMP PER AMM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 57,890 hrs · 34,199 cycles

R2 DOOR EVAC SLIDE WAS NOT IN GREEN BAND. R&R SLIDE PER MT.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,765 hrs · 34,107 cycles

AFT CARGO PIT FLOOR CORRODED ON FLOOR PAN RAIL BETWEEN BS 767 TO BS 747 ON A/C LT 12 PLACES WHERE NUT PLATES WHERE LOCATED ON TRANSITION ANGLE UNDER PANEL 141DW. R&R ANGLE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,155 hrs · 33,713 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED ON UPPER AND LOWER SKINS AT INBOARD AFT CORNER. REPAIRED AFT FLAP IAW EA.

Part: SIGN — MISSING (CABIN) · airframe 57,155 hrs · 33,713 cycles

R1 DOOR EMERGENCY EXIT LIGHTED SIGN DIRECTIONAL ARROW MISSING. INSTALLED SIGN PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,155 hrs · 33,713 cycles

LT WING OUTBOARD AFT TRAILING EDGE FLAP DELAMINATED OF UPPER AND LOWER AT INBOARD AFT CORNER. R&R AFT FLAP PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 56,805 hrs · 33,490 cycles

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

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 56,805 hrs · 33,490 cycles

SUPPLEMENTAL INFORMATION: R/H CENTER LOWER REAR SPAR SEAL ASSY DOUBLER FOR RAM AIR EXHAUST LOWER LOBE CRACKED (PART NUMBER 111A1512-2 ). REQUIRES REPLACEMENT / REMOVED AND INSTALLED NEW R/H CTR LOWER REAR SPAR SEAL ASSY DOUBLER FOR RAM AIR EXHAUST (PN 111A1512-2) IAW SRM 51-40-02-0G-0. REFERENCE IPC 57-11-00-02 FOR FASTENER CALL OUT. PERFORMED LEAK CHECK GOOD IAW AMM 21-51-24-400-801 STEP 3.J.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,447 hrs · 33,255 cycles

L2 DOOR SLIDE OUT OF POSITION. R&R SLIDE PER MT.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 56,172 hrs · 33,079 cycles

RIGHT HORIZONTAL STAB FWD LOWER SLIDING SEAL CRACKED. / R&R RIGHT HORIZONTAL STAB FWD LOWER SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 56,172 hrs · 33,079 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 56,148 hrs · 33,063 cycles

L/H HORIZ STAB #4 INSPAR RIB STAB STA. 120.30 HAS CRACKS ON #3 AND #4 VERTICAL STIFFENRES. (2 CRACKS TOTAL) VERIFIED VIA HFEC NDT PART 6 51-00-00 PROCEDURE 23. / L/H HORIZONTAL STAB #4 IN SPAR RIB; STAB STA 120.30 REMOVED RIB REPAIRED #3 AND #4 VERTICAL STIFFENERS; AND REINSTALLED RIB I/A/W SRM 55-10-09-2R-4; AND BOEING DWG 182A5304 REV B.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 55,086 hrs · 32,396 cycles

R1 DOOR EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW MM.

Part: SLIDE — DAMAGED (R1 DOOR) · airframe 54,997 hrs · 32,340 cycles

R1 DOOR SLIDE, FLOOR LEVEL RT SIDE BY GIRT BAR, HAD EXPOSED JAGGED METAL. R & R THE SLIDE IAW MT.

Part: HOUSING — LOOSE (EXIT SIGN) · airframe 54,401 hrs · 31,974 cycles

AFT OVERHEAD EMERGENCY EXIT SIGN HOUSING ASSEMBLY LOOSE. R&R SIGN ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,146 hrs · 31,165 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW AMM.

Part: STRAP — LOOSE (EMERGENCY EXIT) · airframe 53,146 hrs · 31,165 cycles

RIGHT EMERGENCY EXIT DOOR STORAGE HANDLE STRAP LOOSE AT ROW 12. SECURED THE STRAP ASSEMBLY IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,650 hrs · 30,858 cycles

FORWARD UPPER FLASHLIGHT INOP. R&R BATTERY IAW MM.

Part: STIFFENER — CRACKED (LEFT WING) · airframe 52,106 hrs · 30,524 cycles

UPPER OUTBOARD STIFFENER ON STRAKELET PANEL CRACKED. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02.

Part: HOUSING — CRACKED (OVERWING EXIT) · airframe 52,087 hrs · 30,512 cycles

LT OVERWING EXIT LOWER STRAP HOUSING CRACKED. R&R STRAP HOUSING IAW AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 52,087 hrs · 30,512 cycles

RT CREASE BEAM CRACKED AT BS 294, AFT OUTBOARD ATTACH FASTENER. R&R CREASE BEAM IAW DWG AND SRM.

Part: FRAME — CRACKED (LT WING) · airframe 52,087 hrs · 30,512 cycles

LT WING LEADING EDGE INBOARD BULLNOSE CURVED WING TO BODY ATTACH BRACKET CRACKED AT STA 500D. R&R FRAME ASSEMBLY IAW DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,087 hrs · 30,512 cycles

R2 DOOR SLIDE OUT OF POSITION. R & R THE SLIDE ASSEMBLY IAW MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,087 hrs · 30,512 cycles

FLOOR STRUCTURE UPPER ''T'' CAP CRACKED AT BS 294, RBL 52. REPAIRED T CAP PER IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,087 hrs · 30,512 cycles

CABIN FLOOR INTERCOSTAL CRACKED AT STA 312 TO STA 328, LBL 46. R&R INTERCOSTAL SECTION PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 278-294) · airframe 52,087 hrs · 30,512 cycles

FLOOR SUPPORT UPPER SURFACE FLANGE CRACKED BETWEEN BS 278 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: WIRE — MISSING (EXTERIOR LIGHT) · airframe 52,087 hrs · 30,512 cycles

AFT LAV EXTERIOR EXIT LIGHT QUICK DISCONNECT WIRE MISSING. R&R LIGHT IAW AMM.

Part: ANGLE — CORRODED (BS 727A-727D) · airframe 52,087 hrs · 30,512 cycles

AFT CARGO LT ZEE ANGLE CORRODED BETWEEN BS 727A TO 727D. R & R THE ZEE ANGLE IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,087 hrs · 30,512 cycles

BULKHEAD WEB CRACKED AT BS 663, LBL 26. REPAIRED THE BULKHEAD WEB IAW EA.

Part: ANGLE — CORRODED (BS 727-727C) · airframe 52,087 hrs · 30,512 cycles

AFT CARGO RT ZEE ANGLE CORRODED BETWEEN BS 727 TO 727C. R & R THE ANGLE IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,087 hrs · 30,512 cycles

BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 52,087 hrs · 30,512 cycles

RIGHT WING SLAT NR 7 ALL 6 FASTENERS FOR THE ACTUATOR ON THE NOSE SKIN CRACKED. R & R THE SKIN IAW SRM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,011 hrs · 29,248 cycles

OVERWING EXIT LIGHT INOPERATIVE. R & R THE FUSE IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,733 hrs · 29,087 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MAINTENANCE.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,189 hrs · 28,770 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,973 hrs · 28,095 cycles

RIGHT EMER EXIT MID CABIN EMER LIGHT BATTERY PACK FAILED CAPACITY TEST AT MO1669. R & R BATTERY PACK IAW AMM.

Part: CAP — MISSING (L2 DOOR) · airframe 47,973 hrs · 28,095 cycles

L2 DOOR EMER EVAC SLIDE COVER, BUMPER BAR ENDCAP MISSING. INSTALLED ENDCAP IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 46,114 hrs · 27,030 cycles

R1 DOOR EMER EVAC SLIDE BATTERY FAST LOAD OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: SLAT — CRACKED (RT WING) · airframe 45,846 hrs · 26,889 cycles

RIGHT WING NR 5 SLAT CRACKED. REPAIRED NR 5 SLAT IAW SRM.

Part: RETAINING RING — LOOSE (EMERGENCY LIGHT) · airframe 45,846 hrs · 26,889 cycles

FOUND THE AFT RIGHT FUSELAGE EXTERNAL EMERGENCY EXIT LIGHT LOOSE. SECURED THE EMERGENCY LIGHT RETAINING RING IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 45,846 hrs · 26,889 cycles

LEFT FWD BULLNOSE EMER LIGHT INOPERATIVE. REPAIRED ELEC WIRE IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 45,846 hrs · 26,889 cycles

EMERGENCY EXIT LIGHT AFT OF LT OVERWING DOOR INOPERATIVE. REPAIRED ELEC WIRE IAW MM.

Part: PAN — CORRODED (NR 1 PYLON) · airframe 45,846 hrs · 26,889 cycles

NUMBER 1 ENG PYLON AFT PAN FARING NR 3 CORRODED. REPAIRED PAN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 45,846 hrs · 26,889 cycles

LEFT WING NR 1 SLAT ON LOWER SURFACE OF NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

BULKHEAD LOWER FRAME WEB CRACKED AT BS 727, WL 200 INBD FASTENER HOLE. REPAIRED WEB IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

R1 DOOR CUT OUT FWD LOWER STUB BEAM CRACKED AT BS 294.5, WL. 209 AT INBD FASTENER HOLE. REPAIRED STUB BEAM IAW EA & ER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

INTERCOSTAL CRACKED AT STATION 312 - 328, RBL 31, WL 208. REPAIRED INTERCOSTAL IAW EA.

Part: RETAINING CLIP — LOOSE (L2 DOOR) · airframe 45,846 hrs · 26,889 cycles

L2 DOOR EMER EVAC SLIDE COVER FWD GIRT BAR RETAINER CLIP LOOSE. R & R CLIP IAW SRM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 45,846 hrs · 26,889 cycles

L1 DOOR EMER EVAC SLIDE COVER AFT GIRT BAR RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 45,846 hrs · 26,889 cycles

R1 DOOR EMER EVAC SLIDE COVER FWD GIRT BAR RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: COVER — DAMAGED (R1 DOOR) · airframe 45,846 hrs · 26,889 cycles

R1 DOOR EMER EVAC SLIDE COVER DAMAGED AT LOWER AFT CORNER. REPAIRED COVER IAW CMM.

Part: SLIDE — WORN (L1 DOOR) · airframe 45,846 hrs · 26,889 cycles

L1 DOOR ESCAPE SLIDE GIRT WORN ON LOWER SURFACE. R & R SLIDE ASSEMBLY IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

LEFT CREASE BEAM WEB LOWER SURFACE CORRODED BETWEEN BS 650 - 659, LBL 64. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CENTER WING UPPER FRONT SPAR SHEAR FITTING CRACKED AT AFT FASTENER HOLE, RBL 14.5. R & R FITTING IAW ACO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CENTER WING UPPER FRONT SPAR SHEAR FITTING CRACKED AT AFT FASTENER HOLE, LBL 6.5. R & R FITTING IAW ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

LEFT CREASE BEAM WEB LOWER SURFACE CORRODED BETWEEN BS 580 - 588, LBL 64. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CENTER WING UPPER FRONT SPAR SHEAR FITTING CRACKED AT FASTENER HOLE, RBL 40.5. R & R FITTING IAW ACO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CENTER WING UPPER FRONT SPAR SHEAR FITTING CRACKED AT AFT FASTENER HOLE, RBL 31.5. R & R FITTING IAW ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

LEFT CREASE BEAM WEB LOWER SURFACE CORRODED BETWEEN BS 616 - 639, LBL 64. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

LEFT CREASE BEAM WEB LOWER SURFACE CORRODED BETWEEN BS 563 - 572, LBL 64. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

LEFT CREASE BEAM CORRODED AT STATION 540 TO 559. REPAIRED CREASE BEAM IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,846 hrs · 26,889 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STATION 92.70 AT FOUR VERTICAL STIFFENERS ON LOWER END. REPAIRED RIB IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

STRINGER CLIP CORRODED AT BS 967, STRINGER 27L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CREASE BEAM INNER CHORD CORRODED ON UPPER SURFACE BETWEEN BS 695+6 - 706+1, LBL 63. REPAIRED CHORD IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY INTERCOSTAL AFT ATTACH ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY CARGO TIE DOWN TRACK CORRODED AT BS 500C+16, RBL 14. R & R TRACK IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500B - 500D, LBL 24. REPAIRED PLATE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY ON BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY LT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN STRINGER 24L - 26L. R & R ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CREASE BEAM WEB LOWER SURFACE CORRODED AT BS 706+6, LBL 63. R & R WEB IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY ON THRESHOLD INBD STRAP, CORRODED BETWEEN BS 440 - 492, RBL 22. R & R STRAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

RIGHT CREASE BEAM CORRODED AT STATION 706 + 1.5. REPAIRED CREASE BEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CREASE BEAM WEB LOWER SURFACE CORRODED AT BS 685+4, LBL 63. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

CREASE BEAM INNER CHORD CORRODED ON UPPER SURFACE AT BS 716.3+6, RBL 63. REPAIRED CHORD IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A - 500D, RBL 24. R & R SUPPORT IAW SRM.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FRAME SPLICE CORRODED AT STATION 967, STRINGER 24R - 25R. R & R SPLICE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FRAME CRACKED AT BS 727A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 773, RBL 9. REPAIRED SUPPORT IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

AFT CARGO LOWER SILL INNER CHORD CORRODED AT BS 772, RBL 25. R & R CHORD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

BULKHEAD TO SIDEWALL SUPPORT CORRODED AT BS 727+6, LBL 13. R & R SUPPORT IAW SRM & DWG.

Part: POST — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

NUMBER 3 COCKPIT WINDOW POST LOWER CORNER CRACKED. REPAIRED POST IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

INTERIOR SEAT TRACK FLANGE FWD CRACKED AT BS 727B, LBL 45, INBD AFT HOLE. REPAIRED FLANGE IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FRAME INNER CHORD CORRODED AT BS 727D, BETWEEN STRINGER 23L - 25L. R & R CHORD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 933 - 937, RBL 20. REPAIRED SUPPORT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

INTERIOR SEAT TRACK FLANGE FWD CRACKED AT BS 727B, LBL 24, INBD AFT & OTBD FWD HOLE. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL. REPAIRED CHORD IAW ER & EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

AFT PRESS BULKHEAD INTERCOSTAL CORRODED AT BS 1016, RBL 25. R & R INTERCOSTAL IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

INTERIOR SEAT TRACK FLANGE FWD CRACKED AT BS 727B, RBL 24, OTBD FWD & AFT HOLES. REPAIRED FLANGE IAW ER & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

NUMBER 1 COCKPIT WINDOW POST UPPER AFT CORNER CRACKED. REPAIRED POST IAW ACO.

Part: WEB — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

COCKPIT FLOOR CORRODED AT STATION 251, BL 0. REPAIRED FLOOR WEB IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,846 hrs · 26,889 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 773, LBL 3. REPAIRED SUPPORT IAW EA.