N798SW

Part: COVER — MISSING (CABIN) · airframe 73,249 hrs · 43,720 cycles

EMERGENCY LIGHT COVER MISSING OVER PAX SEATS 2D. EMERGENCY LIGHT COVER WAS FOUND TO BE CABIN TEMP SCREEN. OK TO CONTINUE PER MEL 25-10-01. SP1

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 72,902 hrs · 43,529 cycles

AFT SERVICE DOOR ESCAPE SLIDE SAGS ; / [01] ACCOMPLISHED MT 725-61-06 TO REPOSITION AFT SERVICE DOOR SLIDE AS REQUIRED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 72,181 hrs · 43,139 cycles

NUMEROUS EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. 6 LEFT AND LEFT OVERWING; LEFT 14;17;20;23. L2 DOOR SMALL SIGN; R2 DOOR BIG SIGN ; / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS @ CONNECTORS; M1674; M1675;M1669;M1668;M1670;M1672; AND M1673 PER DWG NO. 33500005

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 72,116 hrs · 43,105 cycles

RIGHT WING I/B MAIN FLAP O/B L/E RIB CRACKED O/B OF AFT FLAP DRIVE ARM. REMOVED CRACKED RIB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW RIB IAW SRM 51-40-05-0G-0 AND DWG 113A2213 REV- AND 113A2100 REV E. TREATED AND PRIMED NEW RIB IAW AMM 51-21-41 51-21-99 & EO 21-157-01920-WIP1. LOCATED AND DRILLED NEW RIB IAW SRM 51-40-05-0G-0 AND DWG 113A2213 REV- AND 113A2100 REV E . ACCOMPLISHED EA 21-157-01920-WIP1 AND 21-157-01920. INSTALLED NEW RIB IAW SRM 51-40-02-G-0 DWG 113A2100 REV C. APPLIED TOP COAT IAW AMM 51-21-73-370-804.

Part: COVER — OUT OF POSITION (R2 DOOR) · airframe 71,853 hrs · 42,957 cycles

MANUAL PULL HANDLE AFT GALLEY DOOR (FO SIDE) EXPOSED ; / REPOSITION AFT GALLEY (R-2) DOOR SLIDE MANUAL HANDLE COVER IAW SIP

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 70,652 hrs · 42,302 cycles

AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK, PER M/M 33-51-06.

Part: SIGN — BROKEN (CABIN) · airframe 70,600 hrs · 42,271 cycles

EMERGENCY EXIT SIGN AT R1 DOOR IS CRACKED & BROKEN. REPLACED R1 DOOR EMERGENCY EXIT SIGN, REF AMM 33-51-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,627 hrs · 41,652 cycles

AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW AMM 33-51-04.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,588 hrs · 41,626 cycles

FORWARD RT CABIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD RT BATTERY PACK IAW AMM 33-51-09. OPS CHECK GOOD.

Part: HYDRAULIC LINE — CRACKED (RT WING) · airframe 69,508 hrs · 41,569 cycles

WHILE CONFIGURING FOR LANDING; LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH TRAILING EDGE FLAPS AT 30. LE DEVICE PANEL ON OVERHEAD SHOWED ALL GREEN WITH LE FLAPS EXTENDED AND LE SLATS IN EXT. AFTER LANDING HYD SYSTEM B SHOWED RF AND 60%. ON INSPECTION; RIGHT WING LE HAS A LEAK. / FOUND #7 SLAT ACTUATOR OTBD PRESSURE HYDRAULIC LINE LEAKING. REMOVED & REPLACED HYDRAULIC LINE IAW AMM 20-10-51. OPS & LEAK CHECK GOOD. SERVICED 'B' SYS HYDRAULICS IAW AMM 12-12-00

Part: HYDRAULIC LINE — LEAKING (LE SLAT) · airframe 69,508 hrs · 41,569 cycles

REF LOG PAGE # 1391847. L/E IND / HYD LEAK / HYD QTY / SERVICED B SYSTEM HYD PER AMM 12-12-00. FOUND LINE LEAKING @ #7 SLAT ACTUATOR. REF AMM 29-00-00. REF LOG PAGE # 1391847 FOR CORRECTIVE ACTION

Part: PAD — CRACKED (AFT CARGO DOOR) · airframe 69,468 hrs · 41,544 cycles

AFT CARGO DOOR STOP FITTING PAD CRACKED; AFT SIDE 2ND FROM BOTTOM / REMOVED AND REPLACED AFT CARGO DOOR STOP FITTING PAD AFT SIDE 2ND FROM BOTTOM IAW AMM 52-31-01

Part: NUT PLATE — BROKEN (BS 360) · airframe 69,451 hrs · 41,534 cycles

BROKEN FLOOR PANEL NUT PLATE AT BS360 RBL25 WL208. / REMOVED FLOOR PANEL NUT PLATE; BS 360; RBL 25; WL 208; REPLACED WITH NEW PER AMM 53-21-00-400-801

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

AFT CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED AND INSTALLED SCUFF PLATE ACB AFT CORNER IAW EA 1-A53-2076 R11

Part: SPLICE — CORRODED (AFT CARGO FLOOR) · airframe 69,451 hrs · 41,534 cycles

AFT CARGO BAY FLOOR PNL SPLICE TEE IS CRACKED BS 727D WL 156 RBL10 / NO ALLOWABLE DAMAGE GIVEN FOR SPLICE STRIP ASSY IN AFT CARGO BAY AT BS 727D; WL 156; RBL 10 PER SRM 53-00-53-1A-2; REPAIR BY REPLACEMENT PER SRM 51-10-02-0G-0. RECEIVED A NEW SPLICE STRIP ASSY FROM STORES. REF: PO 788431. SPLICE STRIP TO BE INSTALLED ON JPANEL-141-CLOSE. REF: ATTACHED COPY.

Part: STUD — DAMAGED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

RH EMERGENCY DOOR EXIT CUT OUT FWD MID AND LOWER STUD COMMON TO SURROUND PANEL INSTALL DAMAGED / REMOVED AND REPLACED RH EMERGENCY DOOR EXIT CUT OUT FWD MID AND LOWER STUDS IAW SOPM 20-50-01. 59908U 28MAR20.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

APU POWER CABLE SUPPORT ANGLE CRACKED BS 867 BETWEEN STR 2 AND 3 R/H. / REMOVED AND REPLACED APU POWER CABLE SUPPORT ANGLE BS 867 BETWEEN STR 2-3 R/H PER SRM 51-40-02; MM 25-80-00 AND DWG# 146A7901 REV A

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

CABIN FLOOR PANEL 222AF HAS UPPER SURFACE FIBER DAMAGE. / UPPER SURFACE FIBER DAMAGE TO CABIN FLOOR PANEL 222AF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1; AND SRM 53-00-50-2R-4. 59198U 3.20.20.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

INTERCOSTAL STRAP IS CRACKED AT BS 302 STR 4L REMOVED AND REPLACMENT INTERCOSTAL. STRAP. FROM STR 4L AT B.S. 300-318 IAW. SRM. 51-40-05- AND SRM 51-40-02-0G-0 AND DWG NO: 141A0742 ID: 0004 REV:- & DWG NO: 141A8130 ID: 0008 REV: B 59826U MAR.10.2020

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

FCB GUSSET CRACKED BS 500D STR 19L WL 195 FCB GUSSET AT BS 500D STR 19L REMOVED AND REPLACED IAW SRM 51-40-02.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

FCB GUSSET CRACKED BS 500D STR 19R WL 195 FCB GUSSET AT BS 500D STR 19R REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 143A7902.

Part: WEB — DAMAGED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

INSTALLED REPAIR AT BS 336; STRINGER 5R; FASTENERS DO NOT MEET SRM CRITERIA FOR SPACING AND PROPER INSTALLATION. / REMOVED AND REPLACED WEB ASSY AT BS 328-344 R/H STR 5R IAW SRM CH 51-40-02 AND DRAWING # 141A8330.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** MULTIPLE POINTS OF CORROSION ON ACB FLOOR RAIL UPPER, LOWER SURFACES, BS 727+8 TO 727C, RBL 3, WL 156 REPAIRED FLOOR RAIL, B/S 727 TO B/S 727B+16" RBL 3 WL 156 IAW SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 1 AND DWG 146A7500 REV: B 59900U 17MAR20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727D+5, LBL 12.5 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL B/S 727D+5 LBL 12.5 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2, REPAIR 2, ALTERNATIVE 5. 59900U 12MAR20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727D+5, RBL 3 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL, B/S 727D+5 RBL 3 WL 156 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5 59900U 11MAR20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, RBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL, B/S 767+5, RBL 8 AND WL 156 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, 727D+5, RBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL, B/S 727D+5 RBL 8 WL 156 IAW SRM 51-40-02-0G-0, PARAGRAPH 7D AND SRM 53-00-53-2R-2, REPAIR 2, ALTERNATIVE 5. 59900U 12MAR20

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

DAMAGE TO UPPER SURFACE OF FLOOR PANEL 231YF. / DUE TO EXTENT OF DAMAGE; OPTED TO FABRICATE NEW PANEL PER SRM 53-00-50-2R-0 PARA 1A USING BMS 4-23 TY2 LOT# 1399953-1 FLOORBOARD MATERIAL. INSTALLED ALL THRU INSERTS USING BMS5-107 CLASS 1 LOT# AK9FP3008K ADHESIVE PER DWG 144A5810-124 AND SRM 53-00-50-2R-0 PARA 5S. 59654U 3-8-2020 20021C 8MAR20 PART MARKED AND APPLIED SKYFLEX TAPE PER DWG 144A5810-124 59654U 3-9-2020 20021C 9MAR20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, RBL 3 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL B/S 767+5 RBL 3 WL 156 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5 59900U 11MAR20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727D+5, LBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED ACB FLOOR RAIL B/S 727D+5 LBL 8 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2- REPAIR 2. 59900U 12MAR20.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, LBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED ACB FLOOR RAIL, B/S 767+5 LBL 8 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5. 59900U 11MAR20.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

DAMAGE TO UPPER SURFACE OF FLOOR PANEL 241BF. / FLOOR PANEL 241BF WITH DAMAGE TO UPPER SURFACE HAS BEEN REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A. (1). 59812U 03/06/2020

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727+8 AND 727B, LBL 3, WL 156 (MARKED) REPAIRED FLOOR RAIL, B/S 727 TO B/S 727C+6" LBL 3 WL 156 IAW SRM 53-00-53-2R-2. REPAIR 2 ALTERNATIVE 1 AND DWG 146A7500 REV: B 59900U 17MAR20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, LBL 3 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL ON ACB B/S 767+5" LBL 3 IAW SRM 51-40-02 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5. 59900U 11MAR20

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

AFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE SKIN PLIES / DUE TO THE EXTENT OF DAMAGE TO FLOOR PANEL 241AAF; OPTED TO FABRICATE A NEW FLOOR PANEL USING BMS4-17 TYV1 LOT#1420733-1 IAW SRM 53-00-50-2R-0 PARA 1A 'NOTE' & DWG 147A5810-8-M. INSTALLED INSERTS USING BMS 5-107 LOT#AK9FP3008K IAW SRM 53-00-50-2R-0 PARA 5S. 59401U 4MAR20 10529C 3/4/20

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

DURING DTIP INSPECTION, FOUND INTERCOSTAL WEB AT BS 303, STRINGER 4L CRACKED. REMOVED. AND. REPLACMENT. INTERCOSTAL. WEB. AT B.S 303. STR.4L. PART NO: 7530155 IAW. SRM. 51-40-05. AND SRM 51-40-02-0G 0 AND DWG. 141A8130 ID: 0001 REV: - & DWG NO: 141A0742 ID: 0004 REV: - 59826U MAR.10.20

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

AFT CABIN FLOOR PANEL 241ACF HAS DAMAGED INSERTS / REPLACED DAMAGED INSERTS AND FIXED ADDITIONAL DAMAGE TO AFT CABIN FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-4; AND SRM 53-00-50-2R-6. 59198U 3.20.20.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

(SKYLINE DTIP) L/H HORIZ. STAB. CRACK ON SECOND STIFFENER, LWR I/B SIDE STA. 92.70. CUTOUT DAMAGE AREA. DIM: (1.630" X .175") AT L/H HORIZ STAB ON SECOND STIFFENER STA 92.70. RABRICATED LOCATED, DRILLED & INSTALLED T-ANGLE, ANGLE, SHIM. IAW B737 SRM 55-10-09. (Y000422) NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1151

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

(SKYLINE DTIP) L/H HORIZ. STAB. CRACK AT FIRST STIFFENER, LWR. I/B SIDE STA. 92.70. CUTOUT DAMAGE AREA. DIM: (1.650" X .175") AT L/H HORIZ STAB FIRT STIFFENER. STA 92.70. REPAIR INSTALLED IAW B737 SRM 55-10-09. (Y000421) NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1151

Part: WEB — DAMAGED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

FLOOR WEB AT BS 986-1016 RBL 38 IS CREASED. WL 208 REMOVED AND REPLACED FLOOR WEB AT B.S 986-1016 RBL 38 PER SRM 51-40-02-0G-0, DWG 147A0000, REV A.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

DURING COMPLETION OF CCN: 14539 FOUND BS 1016 BULKHEAD S-23L WEB SPLICE TO BE CRACKED ON AFT SIDE FROM EDGE TERMINATING AT FASTENER NEAREST APEX IN OTBD ROW; AREA MARKED. ENGINEERING DISPOSITION REQUIRED. / CUT OUT DAMAGED SECTION OF 1016 BULKHEAD STR 23L AND ACCOMPLISHED REPAIR IAW EA 20-153-00135 REV IR AND ER 20-02115 REV IR

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CORROSION FOUND ON AED THRESHOLD WEB UPON MOPSILL REMOVAL AT BS 983 LBL45 WL 208 / AED THRESHOLD WEB AT BS 983 LBL 45 FOUND TO BE OUT OF LIMITS AT BS 984 RBL 46 2' X 2' X .012' ORIGINAL THICKNESS .071' REMAINING .059' PER SRM 53-70-15-1A-1. REPLACED THRESHOLD WEB BS 992 - LBL 50-45 PER SRM 51-40-02 & DWG 147A8501. 59641U; 26MAR20.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

(SKYLINE DTIP) RH HORIZONTAL STAB, CRACK AT FIRST STIFFENER, LWR. I/B SIDE STA. 92.70 CUT OUT DAMAGE AREA. DIM: (.800"X.153"). AT. R/H HORIZ. STAB. FIRST STIFFENER. STA. 92.70. FABRICATED , LOCATED, DRILLED AND INSTALLED. T-ANGLE, AUGLE, SHIM. IAW B737SRM 55-10-09. (Y000419) NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1151

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

AFT CABIN FLOOR PANEL 241ABF HAS DAMAGED INSERTS / REPLACED ALL DAMAGED INSERTS; & REPAIRED DAMAGE TO PANEL IAW SRM 53-00-50-2R-1 & SRM 53-00-50-2R-6. 57885U 03-23-2020

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CORROSION ON FLOOR INTERCOASTAL AT BS 989 RBL 38 . WL 208 REMOVED CORROSION ON FLOOR INTERCOSTAL B.S 989 RBL 38 WL 208 2" X 1.5" X .015"D REMAINING THICKNESS 065", ORIGINAL THICKNESS .080" FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 PAR 4A(2) FIG 103. REMOVED AND REPLACED FLOOR INTERCOSTAL B.S 986-1006 RBL 38 PER SRM 51-40-02-0G-0, DWG 147A5730, REV C.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

AFT CABIN FLOOR PANEL 242UF HAS DAMAGED INSERTS / REPLACED DAMAGED INSERTS & REPAIRED ALL DAMAGE TO FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1 & SRM 53-00-50-2R-6. 57885U; 03-25-2020.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

AFT CABIN FLOOR PANEL 241ZF HAS DAMAGED UPPER SURFACE SKIN PLIES AFT EDGE UPPER SURFACE SKIN DAMAGE ON FLOOR PANEL 241ZF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1, SRM 53-00-50-2R-4 AND DWG 200-048. 59198U 3.10.20.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,451 hrs · 41,534 cycles

AFT CABIN FLOOR PANEL 241ADF HAS DAMAGED INSERTS / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL; FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0 PARA 1A NOTE & BFG DWG 2000-048-2. 57885U 03-26-2020

Part: WEB — CANNING (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

FLOOR WEB AT BS 986-1016 LBL 38 IS OIL CANNED. / REMOVED AND REPLACED FLOOR WEB AT BS 986-1016 LBL 38 PER SRM 51-40-02; SRM 51-04-05; DWG 147A0004; AND DWG 147A5600.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

(SKYLINE DTIP) RH HORIZONTAL STAB, CRACK ON SECOND STIFFENER, LWR. I/B SIDE STA. 92.70 CUTOUT DAMAGE AREA.DIM: (.900" X .167") AT R/H HORIZ. STAB SECOND STIFFENER STA. 92.70. FABRICATED LOCATED, DRILLED & INSTALLED T-ANGLE, ANGLE, SHIM. IAW B737 SRM 55-10-09. (Y000420) NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1151

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

(SKYLINE DTIP) L/H HORIZ. STAB. CRACK ON THIRD STIFFENER, LWR. I/B SIDE STA. 92.70. CUTOUT DAMAGE AREA. DIM: (1.300" X .175") AT L/H HORIZ STAB THIRD STIFFENER STA 92.70 FABRICATED, LOCATED, DRILLED & INSTALLED T-ANGLE, ANGLE, SHIM IAW B737 SRM SRM 55-10-09. (Y000497) NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1151

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** E/E BAY INTERNAL SKIN AT BILGE VENT BELOW MAIN BATTERY, STA 380+2, BL 0 CORROSION ON E&E BAY INTERNAL DOUBLER IN BILGE BS-380+2. BL-0 FOUND TO BE OUT OF LIMITS PER SRM - 53-30-01-1A-1. FABRICATED NEW DOUBLER FROM 2024-T3 .050" LOT # 1425168-1 IAW DWG - 143A3230, SRM 51-40-05. INSTALLED PER DWG - 143A3230 & SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

E/E BAY STRINGER; LAYER OF METAL SPLIT/LIFTED AT BOTTOM OF CHANNEL - STA 380+1; S-28L (POSSIBLE JOGGLE POINT FOR BILGE VENT DOUBLER) / CRACK ON STR-28L; BS - 380+1 FOUND TO BE OUT OF LIMITS PER 53-00-03-1A-1. CUT OUT; FABRICATED NEW STR SECTION BS-388-360 AND REPAIR SPLICE CAP AT BS- 355; STR-28L. PER SRM-53-40-05; PO# 785308-SWA; PO# 785309-SWA. AND INSTALLED PER SRM-53-40-02 SRM-53-00-03-2R-1 FIG 202

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB AFT ANTENNA SUPPORT BASE BS 727D +10 RBL 5; WL 150 / REMOVED ACB AFT ANTENNA SUPPORT BASE BS 727D+10 RBL 5 WL 150 I.A.W SRM 54-40-02-0G-0. AND INSTALLED NEW ACB AFT ANTENNA SUPPORT BASE I.A.W SRM 51-40-02-0G-0 AND DWG 146A7730 ID: 0001 REV:B

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY SUB WEB THRESHOLD AT B .S. 440-494, R.B.L. 28, W.L. 155 REMOVED.AND. REPLACMENT SUB WEB THRESHOLD PART NO: 7530597 FROM FORWARD CARGO BAY AT B.S 440 494 - R.B.L. 28. W.L-155 IAW 737-700 SRM. 51-40-02 0G 0 AND DWG NO: 143A8330 I.D 0010 REV: A 59826U MAR 4-2020

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CRACKED FLOOR SUPPORT AT B.S 540, B.L. 0 - L.B.L. 24.5, W.L. 208.1. REMOVED AND REPLACED NEW FLOOR SUPPORT AT BS 540- B.L-0 - L.B.L 24.5, W.L. 208.1 PER DWG # 143A0060 REV:B AND SRM 51-40-02 88911U 03MAR20

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB RIB ATTACH ANGLE, BS 747 RBL 15 , WL 150 REMOVED AND REPLACED A.C.B CLIP ANGLE BS 747 RBL 15, WL 150, IAW SRM 51-40-02, PARA 4.B, AND DWG 146A1260 REV A. 59899U, 13 MA 20.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD LEFT HAND PANEL LOWER SUPPORT AT B.S. 500D, L.B.L. 24, W.L. 155 REMOVED AND REPLACED FORWARD CARGO BAY AFT BULKHEAD LEFT HAND PANEL LOWER SUPPORT AT BS 500D, L.B.L 24, W.L 155 IAW SRM 51-40-02 PARA 4.B AND DW 143A7902 REV: D 59899U 12MA20

Part: SUPPORT — PUNCTURED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

FWD CARGO BAY; RIGHT FLOOR TO SIDEWALL SUPPORT STA 500A TO STA 500D; WL 156; RBL 24 HAS A PUNCTURE (MARKED) / FWD CARGO BAY; RIGHT FLOOR TO SIDEWALL SUPPORT STA 500A - 500D; WL 156 TO BE REPLACED ON NON ROUTINE CARD U131684.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B .S. 400-500D, L.B.L. 22, W.L. 155 REMOVED AND REPLACED IN F.C.B FLOOR TO SIDEWALL SUPPORT AT BS 440-500D L.B.L 22, W.L 155 IAW SRM 51-40-02 PARA. 4-B AND DWG 143A7501 REV: B 59899U, 6 MARCH 20. AND SPLICE SIDEPLATE INSTALLED BTW BS 480+10 - 500D IAW SRM 53-00-53-2R-6, REPAIR 6.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B .S. 400-420, R.B.L. 22, W.L. 155 REMOVED FCB FLOOR TO SIDEWALL SUPPORT AT BS 400-420 RBL 22 WL 155 I.A.W SRM 51-40-02-0G-0. INSTALLED NEW FLOOR TO SIDEWALL SUPPORT I.A.W. SRM 51-40-02-0G-0 AND DWG 143A7500 ID: 0001 REV: -

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB ANCHOR SUPPORT BASE BS 787 +5 STNGR L23 / REMOVED AND REPLACED ACB ANCHOR SUPPORT BASE AT BS 787+5 STR 23L IAW DWG 146A9403-13; DWG 146A9401-8 & SRM 51-40-02-0G-0.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY SHIELD AT B.S. 494-500A, R.B.L. 22, W.L. 155 REMOVED AND REPLACED SHIELD AT FCB BS. 494-500A RBL. 22 WL 155 IAW SRM 51-40-02 & DWG 143A0080 REV.- 59191U 05MAR20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

FWD CARGO BAY, RIGHT FLOOR TO SIDEWALL SUPPORT STA 420 TO STA 440, WL 156, RBL 24 IS CORRODED (MARKED) REMOVED FWD CARGO BAY, RIGHT FLOOR TO SIDEWALL SUPPORT STA 420 TO STA 440 WL 156 RBL 24 I.A.W SRM 51-40-02-0G-0. INSTALLED NEW FLOOR TO SIDEWALL SUPPORT I.A.W SRM 51-40-02-0G-0 AND DWG 143A0080 ID: 0006 REV: -

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** FLOOR TO SIDEWALL SUPPORT BS 727- 767 RBL 24, WL 156 REMOVED FLOOR TO SIDEWALL SUPPORT BS 727-767 - RBL 24, WL 156 IN ACB AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0, SRM 53-00-53-1A-2, DWG 146A7502 REV -, SRM 51-40-0G-0, SRM 51-40-02-0G-0, 4B (1-3), AMM 51-21-72-370-804 92954U 03/10/20

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CRACKED FLOOR SUPPORT AT B.S 540, B.L. 0 - R.B.L. 24.5, W.L. 208.1. REMOVED AND REPLACED NEW FLOOR SUPPORT AT BS. 540, B.L-0 - RBL, 24.5, WL. 208.1 PER DWG # 143A0060 REV: B AND SRM 51-40-02 88911U 03MAR20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B .S. 500A-500D, R.B.L. 22, W.L. 155 REMOVED CORRODED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500A-500D RBL 22 WL 155 AND REPLACED WITH NEW IAW SRM 51-40-05, SRM 51-40-02, DWG 143A7902, DWG 143A7500, SRM 53-00-53-1A-2, SOPM 20-41-02, SRM 51-20-01-0G-0. 92954U 03/14/20.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB; INTERCOSTAL BOTTOM O/B SIDE; BS 770 RBL 7 / REMOVED CORRODED AFT CARGO BAY INTERCOSTAL AT BS 770 RBL 7 AND REPLACED WITH NEW IAW SRM 51-40-02; DWG 146A8130 REV. C; SRM 53-00-53-1A-2; FIG 103; SRM 51-40-05; SRM 51-20-01 92954U 03/28/20

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB AFT ANTENNA SUPPORT BASE AFT OUTER ATTACH ANGLE BS 727D +11 RBL 5; WL 150(MARKED) / REMOVED ACB AFT ANTENNA SUPPORT BASE AFT OUTER ATTACH ANGLE BS 727D+11 RBL 5 WL 150. INSTALLED NEW ACB AFT ANTENNA SUPPORT BASE AFT OUTER ATTACH ANGLE I.A.W SRM 51-40-02-0G-0 AND DWG 146A7730 ID: 0001 REV: B

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB ANCHOR SUPPORT BASE BS 787 +5 STNGR L24 / REMOVED AND REPLACED ACB ANCHOR SUPPORT BASE AND FILLER AT BS787+5 STR 24L IAW DWG 146A9401; DWG 146A9405 & SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** FLOOR TO SIDEWALL SUPPORT BS 727D- 787 LBL 24 WL 156 REMOVED AND REPLACED FLOOR TO SIDE WALL SUPPORT AT ACB BS 727 TO BS 847 LBL 24 WL 156 IAW SRM 51-40-02 AND DWG 146A7500 REV. B

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 500D, R.B.L. 22 - L.B.L. 22, W.L. 155 REMOVED AND REPLACED ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 500D, RBL 22. W.L 155 IAW SRM 51-40-02 PARA 4.B AND DWG 143A9481 REV:A. 59899U 12MA20

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB FWD ANTENNA SUPPORT BASE AFT OUTER ATTACH ANGLE BS 727D +11 RBL 5; WL 150 (MARKED) / REMOVED ACB FWD ANTENNA SUPPORT BASE AFT OUTER ATTACH ANGLE BS 727D+11 RBL 5 WL 150 I.A.W SRM 51-40-02-0G-0. INSTALLED NEW ACB FWD ANTENNA SUPPORT BASE AFT OUTER ANGLE I.A.W SRM 51-40-02-0G-0 AND DWG 146A7730 ID: 0001 REV: B

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB CARGO TRACK BS 797-817 RBL 15 WL 156 / CORROSION ON ACB CARGO TRACK BS-797-817 RBL-15; WL-156 FOUND TO BE OUT OF LIMITS PER SRM-53-00-53-1A-2. CUT OUT CARGO TRACK SECTION BS-727-887; RBL-13.84 WL-156. LOCATED AND INSTALLED REPLACEMENT TRACK SECTION AND REPAIR SPLICE MADE FROM BAC1509-100688 7050-T76511 LOT #1353710-1 & TRACK SECTION654A0004-617 ALL IAW EA 1-753-36747 REV IR (ATS ER 20-02130 REV IR); SRM-55- 654A0004-617 ALL IAW EA -1753-36747 REV IR (ATS ER 20-02130 REV IR) SRM-53-00-53-2R-3 REPAIR-3

Part: CHANNEL — CORRODED (BS 967-986) · airframe 69,451 hrs · 41,534 cycles

CORROSION ON AED MOPSILL BS 967-986 LBL45 WL 208 / REMOVED CORROSION FROM MOPSILL AT BS984; LBL 45; WL 208 IN AN AREA OF L= 1.0' X W= 0.5' X D= .030' PER SRM 51-10-02-0G-0; FOUND TO BE OUT OF LIMITS PER B737 SRM 53-70-15-1A-1; PAR. 4.D. FIG; 103; DETAIL D. REMOVED AND REPLACED AED MOPSILL LBL 45 PER B737 SRM 51-40-02-0G-0; AND BOEING DWG. # 147A8501; REV. B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CORROSION 986 FLOORBEAM LBL 44- RBL 44 WL 208 AT NUTPLATE HOLE LOCATIONS / REMOVED & REPLACED 986.5 TRANSVERSE FLOOR BEAM IAW ER 20-02132; DWG 719926-100-311 REV B. DWG 147A5506 REV G. SR; 51-40-02-0G-0; EA 1-753-36712 REV IR

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,451 hrs · 41,534 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / RECIEVED SERVICABLE DOOR; TO BE INSTALLED ON CUSTOMER CARD # 14079 (POS:FSD;TAG NO.:685056;P/N OFF:146A6516-18;S/N OFF:001523;P/N ON:141A6516-5M;S/N ON:BN000006)

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CHAFFING DAMAGE ON INTERCOSTAL AT BL 0 WL 207 BS 265 REMOVED DAMAGED INTERCOSTAL AT BL.0 WL 207 BS 265, AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5210 SH1.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** ACB DOOR THRESHOLD UPPER WEB BS 797-847, RBL 25, WL 156 REMOVED. AND REPLACEMENT ODB DOOR THRESHOLD UPPER WEB FROM R.B.L 25, W.L 156 - B.S. 797-847 IAW. 737-700 SRM 51-40-02-0G-0 AND. DWG. NO: 146A8340 ID: 0009 59826U 05MAR-20

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

CHAFFING DAMAGE ON INTERCOSTAL AT LBL 11 WL 207 BS 265 REMOVED DAMAGE INTERCOSTAL AT BS LBL 11 WL 207 BS 265 AND REPLACED WITH NEW INTERCOSTAL IAW SRM 51-40-02 AND DWG # 141A5210, AND DWG # 141A5600, 59042U, 16MAR20.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,451 hrs · 41,534 cycles

***CORROSION*** PERFORMING GVI IAW EA 1-A53-33197 FOUND CORROSION ON TOP RIB FLANGE BS 260 LBL 5-RBL 5 WL 208 / REPAIRED THE B.S. 259.5 BULKHEAD AFT CHORD AT WL 208 IAW SOUTHWEST EA 1-753-36768 REV IR AND ATS ER 20-01936 REV IR

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

L/H HORIZONTAL STAB RIB AT STAB STA. 120.30 3RD STIFFENER FROM FWD END IS CRACKED REPAIR L/H. HORIZONTAL STAB RIB AT STAB STA. 120.30 3RD STIFFNER FROM FWD END PER SRM 55-10-09-2R-5

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

R/H HORIZONTAL STAB RIB AT STAB STA. 120.30 3RD STIFFENER FROM FWD END IS CRACKED REPAIRED R/H HORIZONTAL STAB RIB AT STAB STA. 120.30 3RD STIFFNER FROM FWD END PER SRM 55-10-09-2R-5

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,451 hrs · 41,534 cycles

L/H HORIZONTAL STAB RIB AT STAB STA. 92.70 4TH STIFFENER FROM FWD END IS CRACKED REPAIRED L/H HORIZONTAL STAB RIB AT STAB STA 92.70 4TH STIFFNER FROM FWD END PER SRM 55-10-09-2R-4

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 69,451 hrs · 41,534 cycles

FWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED / REPAIRED CRACKED FWD CARGO COMPARTMENT AFT LOWER SCUFF PLATE PER EA 1-A53-2076; REV 11. SEE ATTACHED EA

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 69,451 hrs · 41,534 cycles

AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY. FWD SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 69,451 hrs · 41,534 cycles

FLIGHT DECK FLOOR PANE IS DENTED AT B.S. 260 - 270; R.B.L. 11 - L.B.L. 11; W.L. 207.54. / REMOVED FLIGHT DECK FLOOR PANEL AT BS 260-270 RBL 11 - LBL 11 AND FABRICATED NEW ONE AND INSTALLED IAW SRM 51-40-02 AND DWG # 141A5133; REV. C.; 59042U; 16MAR20.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 69,451 hrs · 41,534 cycles

FLIGHT DECK FLOOR PANE IS DENTED AT B.S. 260 - 270, R.B.L. 11 - L.B.L. 11, W.L. 207.54. REMOVED FLIGHT DECK FLOOR PANEL AT BS 260-270 RBL 11 - LBL 11 AND FABRICATED NEW ONE AND INSTALLED IAW SRM 51-40-02 AND DWG # 141A5133, REV. C., 59042U, 16MAR20.

Part: STRUCTURE — DENTED (COCKPIT) · airframe 69,451 hrs · 41,534 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255, R.B.L. 4 - L.B.L. 14, W.L. 207.54. REMOVED DAMAGED AREA ON FLIGHT DECK FLOOR AT BS 255, RBL 4 - LBL 14, WL 207.54 AND REPLACED IAW EA 1-A53-33179, REV IR, 59042U, 16MAR20.

Part: LENS — INCORRECT (CABIN) · airframe 68,670 hrs · 41,087 cycles

L2 DOOR EMERGENCY LIGHT LENS ON EXTERIOR OF LAV WALL HAD WRONG ARROW. / R&R LENS IAW SIP.

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 67,713 hrs · 40,512 cycles

R1 DOOR GIRT BAR HOLDER LOOSE. ADJUSTED THE GRIP TENSION ON BRACKET PER SIP.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 67,584 hrs · 40,427 cycles

GROUND POWER RECEPTACLE DOOR DOUBLER AND SKIN ALONG THE LOWER FORWARD EDGE DAMAGED. / REPAIRED DOUBLER PER SRM.

Part: BATTERY PACK — LOW VOLTAGE (CABIN) · airframe 67,505 hrs · 40,376 cycles

EMERGENCY BATTERY PACK LOW CAPACITY AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 67,505 hrs · 40,376 cycles

RIGHT WING T/E FIXED LOWER PANEL SEAL RETAINER IS CRACKED. JUST AFT OF #2 PYLON / R&R'D RIGHT WING T/E FIXED LOWER PANEL SEAL RETAINER AFT OF #2 PYLON REF SRM 51-40-02

Part: SIGN — BROKEN (R2 DOOR) · airframe 66,847 hrs · 39,952 cycles

R2 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: SWITCH — MISSING (EMERGENCY LIGHT) · airframe 66,467 hrs · 39,735 cycles

EMERGENCY EXIT LIGHT "NOT ARMED" SWITCH LIGHT MISSING. / R&R SWITCH PER SWPM.

Part: BEAM — CRACKED (RT WING) · airframe 66,217 hrs · 39,592 cycles

BEAM PANEL ABOVE PANEL 661AB BROKEN / R&R BEAM COMMON TO PANEL 661AB ON RT WING REF. SRM 51-40-02.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 66,044 hrs · 39,490 cycles

PANEL CAP STRIP LH SIDE OF PANEL 140 DF BETWEEN 887-947 IS CORRODED / FABRICATED NEW CAP STRIP FROM 2024-T3 .063' DRILLED TREATED AND PRIMED REF SRM 53-70-53 AND SRM 51-20-01

Part: SCUFF PLATE — CORRODED · airframe 66,044 hrs · 39,490 cycles

SUPPLEMENTAL INFORMATION: FWD SCUFF PLATE @ STA 793 HAS CORROSION ON AFT SIDE. / REMOVED AND REPLACED FWD SCUFF PLATE REF SRM 51-40-05 AND AMM 20-60-11

Part: ANGLE — CORRODED · airframe 66,044 hrs · 39,490 cycles

TRANSITION ANGLE (TEE ASSY) AT STATION 887 P/N 146A9401-39 CORRODED / REMOVED AND REPLACED TEE ASSY (TRANSITION ANGEL AT STA 887 PER SRM 51-40-02 REF SA-M 326 - A1133975

Part: SCUFF PLATE — CORRODED · airframe 66,044 hrs · 39,490 cycles

AFT SCUFF PLATE @ STA 847 HAS CORROSION ON FASTENER HOLES / REMOVED AND REPLACED AFT SCUFF PLATE REF SRM 51-40-05 AND AMM 20-60-11

Part: TRACK — CORRODED · airframe 66,044 hrs · 39,490 cycles

RBL 13.8 FLOOR TRACK NUT PLATE HOLES HAS DEEP PITTED CORROSION / REMOVED AND REPLACED FLOOR TRACK PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 66,044 hrs · 39,490 cycles

LOWER SURFACE OF TRANITION ANGLE AT BELT FROM 947; AFT BULK HEAD CORRODED AT NUT PLATE HOLES. / REMOVED AND REPLACED TRANSITION ANGLE AT BELT FRAME STA 947 PER SRM 51-40-02 REF SA-M 326 - A1133986

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 66,044 hrs · 39,490 cycles

LBL 3 FLOOR TRACK; VERY AFT NUT PLATE HOLE CORRODED / REMOVED AND REPLACED FLOOR TRACK PER SRM 51-40-02

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 66,044 hrs · 39,490 cycles

R BL 13.8 FLOOR TRACK HAS CORRODED NUT PLATE HOLES FROM 947 TO 887 / REMOVED AND REPLAED FLOOR TRACK PER SRM 51-40-02 REF SA-M 326 - A1133985

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 66,044 hrs · 39,490 cycles

LBL 3 FLOOR TRACK HAS DEEP PITTING CORROSION ON NUT PLATE HOLES FROM STA 947 TO STA 887 / REMOVED AND REPLACED FLOOR TRACK PER SRM 51-40-02 REF SA-M 326 - A1133984

Part: ANGLE — CORRODED · airframe 66,044 hrs · 39,490 cycles

UPPER SURFACE OF TRANSITION ANGLE AT BELT FRAME 947; AFT BUKHEAD CORRODED AT NUT PLATE HOLES / RMEOVED AND REPLACED TRANSITION ANGLE AT BELT FRAME 947 STA PER SRM 51-40-02

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 66,044 hrs · 39,490 cycles

CORROSION AT RBL 13.8 SPLICE AT BELT FRAME 887. CORROSION IS ON INSIDE OF 'U' CHANNEL OF SPLICE. / REMOVED AND REPLACED 'U' CHANNEL AT RBL 13.8 AT STA 887. PER SRM 51-40-02 REF SA-M 326 - A1133988

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 66,044 hrs · 39,490 cycles

AFT CARGO; AFT FLOOR PANEL; LOWER SIDE HAS SERVERAL AREAS OF CORROSION AROUND CUT OUTS / FABRICATED AFT FLOOR PANEL 2024 T-3 .808 PER SRM 51-30-01 REMOVED CORROSION AROUND CUT-OUTS IAW SRM 51-10-02. INSTALLED AFT FLOOR PANEL IAW AMM 25-52-10 REF SA-M 326 - A1133978

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 66,044 hrs · 39,490 cycles

AFT CARGO; AFT FLOOR PANEL; LOWER SIDE HAS SEVERAL AREAS OF CORROSION AROUND PERIMETER FASTENER HOLES / REPLACEMENT OF PANEL TO BE COMPLETED ON SAM 112 N/R 0365861 REF SA-M 326 - A1133979

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 66,044 hrs · 39,490 cycles

RBL 13.8 FLOOR TRACK HAS PITTING CORROSION AT NUT PLATE; APPROXIMATLEY 13' FWD OF BELT FRAME 947 / REMOVED AND REPLACED FLOOR TRACK PER SRM 51-40-02

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 65,855 hrs · 39,384 cycles

EMERGENCY EXIT SIGN CONNECTOR DISCONNECTED AT BS 727A. REPAIRED SIGN PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,479 hrs · 39,167 cycles

EMERGENCY LIGHTS AT LOCATION M1672 FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: COVER — ABNORMAL (EXIT SIGN) · airframe 64,748 hrs · 38,710 cycles

L1 EMERGENCY EXIT SIGN FELL OFF. SECURED COVER PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,390 hrs · 38,479 cycles

LT OVERWING EXIT LIGHT INOP. R&R LIGHT IAW WPM & AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,390 hrs · 38,479 cycles

LT EMERGENCY EXIT LIGHTS AFT WING TO BODY PANELS INOP. R&R LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,390 hrs · 38,479 cycles

LT STOWBIN EMERGENCY EXIT LIGHT INOP BETWEEN ROW 9 TO ROW 12. R&R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,390 hrs · 38,479 cycles

RT EMERGENCY EXIT LIGHTS AFT WING TO BODY PANELS INOP. R&R LIGHT IAW AMM.

Part: STRAP — BROKEN (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

E&E COMPARTMENT SUPPORT STRAP BROKEN BETWEEN BS 360 TO BS 380, RBL 1. REPAIRED STRAP IAW EA.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 64,390 hrs · 38,479 cycles

PASSENGER CABIN FLOOR PANEL 221GF FACE SHEET HAS PEELED STRANDS REPAIRED PASSENGER CABIN FWD BOARD 221GF ON UPPER FACE SHEET IAW B737 SRM 53-00-50-2R-1. CURED IN OVEN FOR 1 HR. IN AT 8:00 A.M. - OUT AT 9:00 AM. A80435 A80195

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

L1 DOOR CREASE BEAM CHORD CORRODED AT BS 340. R&R CREASE BEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

INTERCOSTAL CORRODED AT BS 360+2, STR 28L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 64,390 hrs · 38,479 cycles

PASSENGER CABIN FLOOR PANEL 222AF HAS FIBER DAMAGE ON TOP OF PANEL / REPAIRED PASSENGER CABIN FLOOR PANEL 222AF ON TOP OF PANEL IN MULTIPLE AREAS IAW B737 SRM 53-00-50-2R-1. CURED IN OVEN FOR 1 HR. IN AT 11:00AM - OUT AT 12:00 PM. A30990 A11393

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 64,390 hrs · 38,479 cycles

CABIN FWD WET AREA FLOORBOARD 222BF UPPER SURFACE HAS FRAYED FIBERS. / REPAIRED AREA'S OF FRAMING ON UPPER SURFACE OF PANEL 222BF. IAW B737-700 SRM 53-00-00-2R-1 REPAIR 1; SRM 53-00-50-2R-0 REPAIR GENERAL

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 64,390 hrs · 38,479 cycles

CABIN FWD WET AREA FLOORBOARD 222DF UPPER SURFACE HAS FRAYED FIBERS. / REPAIRED CABIN FWD WET AREA FLOORBOARD 222DF UPPER SURAFCE I/A/W SRM 53-00-50-2R-1 REV 65; SRM 53-00-50-2R-0 GENERAL REV 65.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 64,390 hrs · 38,479 cycles

CABIN FWD WET AREA FLOORBOARD 222BF LOWER SURFACE OTBD EDGE DELAMED. REPAIRED AREA OF DELAMN ON LOWER SURFACE OF PANEL 222BF. IAW B737-700 SRM 53-00-50-2R-9 REPAIR 9, SRM 53.00.50.2R.0 REPAIR GENERAL

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

R1 DOOR CREASE BEAM CHORD CORRODED BETWEEN BS 300 TO BS 335. R&R CREASE BEAM IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

E&E COMPARTMENT STUB FRAME WEB CORRODED AT BS 328+6, BETWEEN STR 19L TO 19R. REPAIRED FRAME IAW EA.

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

LOWER INTERNAL FUSELAGE E&E COMPARTMENT BILGE FRAME BUTT SPLICE STRAP CORRODED AT BS 360, BETWEEN BL 0 TO RBL 6. REPAIRED BUTT SPLICE STRAP IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

STRINGER CORRODED AT BS 362, STR 28L. R&R STRINGER IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

SHEAR TIE CORRODED AT BS 360, BL 0. R&R SHEAR TIE IAW DWG AND SRM.

Part: STRINGER — CORRODED (E&E BAY) · airframe 64,390 hrs · 38,479 cycles

TRANSFERRED FROM LOG PAGE (0094339) TRANSFERRED FROM NRC# D213027 AT BS 362; STR 28L CORROSION IN STRINGER AND INTERCOSTAL JOINT. / REMOVED & REPLACED STA 360 STR 28L I/B & O/B STRINGER END SPLICES IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; & DWG 140A9101 SHT 4 REV C

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,390 hrs · 38,479 cycles

SHEAR TIE CORRODED AT BS 360, BL 0. R&R SHEAR TIE IAW DWG AND SRM.

Part: TRUNNION — CORRODED (LT WING MLG) · airframe 63,465 hrs · 37,905 cycles

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

Part: TRUNNION — CORRODED (RT WING MLG) · airframe 63,465 hrs · 37,905 cycles

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

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,387 hrs · 37,854 cycles

PASSENGER CABIN EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 8 TO 13. R & R THE CHARGER IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,387 hrs · 37,854 cycles

PASSENGER CABIN EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 8 TO 13. R & R THE BATTERY PACK IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

FWD CARGO FWD SCUFF PLATE IS CRACKED / REPAIRED SCUFF PLATE AT FWD CARGO FWD CARGO FWD SCUFF PLATE IN SW EA 1-A53-2076 REV II

Part: SEAL — BROKEN (LT HORIZ STAB) · airframe 63,387 hrs · 37,854 cycles

LEFT HORIZONTAL STAB; AFT UPPER SLIDER SEAL FORWARD TRACK IS MISSING A CHUNK OUT OF THE EDGE. / LEFT HORIZONTAL STAB; REMOVED AND REPLACED SEAL FORWARD TRACK MPN 181A8060-15 SI 7550179 A. TAG KV1285 IAW AIPC 53-31-31-05 PAGE 10 OF 14 AND SRM 51-40-02-0G-0 AND DWG 181A8050

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 63,387 hrs · 37,854 cycles

G4 GALLEY EMERGENCY EXIT LIGHT COVER BROKEN AT ATTACH POINT. R & R THE COVER ASSEMBLY IAW AMM.

Part: SHIELD — CRACKED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO PIT; RIGHT SIDE FLOOR STRUCTURE STATION 767 TO 787; RBL 21; FORWARD FLOOR SHIELD IS PUNCTURED AND CRACKED AS MARKED. / REPLACED AFT PIT; RIGHT SIDE FLOOR STA. 767 - 787; RBL 21 SHIELD FLOOR IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0 AND APPLIED CIC AMM 51-21-91-620-802 DWG: 146A0081 REV: C TAG: WN8366

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 63,387 hrs · 37,854 cycles

SAM494/X700239/AFT CARGO AFT SHIELD IS CORRODED / REMOVED AND REPLACED SHIELD IAW B737-700 DWG 146A0081 SHEET 7 REVC AND SRM 51-40-02-0-0G

Part: SPAR — OUT OF TOLERANCE (RIGHT WING) · airframe 63,387 hrs · 37,854 cycles

SUPPLEMENTAL INFORMATION: RIGHT WING STA 450 REAR SPAR UPPER FASTENER HOLE OUT OF ROUND. / REMOVED FASTENERS AT STA 450 R/H AFT SPAR OVERSIZE UPPER HOLE REAMED TO 261 VISUALLY INSPECTED HOLE FOUND HOLE TRUE ROUND IAW SRM 51-40-05-0G-00 AND BOEING DWG 115A6100 INSTALLED NEW FASTENERS IAW SRM 51-40-02-0G-00 AND BOEING DWG 115A6100 CAP SEALED FASTENER IAW MM 51-31-00-390-805 LEAKED CHECKED AREA IAW MM 28-11-00-400-801 NO LEAKS NO LEAKS NOTED

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,387 hrs · 37,854 cycles

FLIGHT DECK SUPPORT BRACKET FOR P18 CRACKED AT BS 260, STR 10. R&R BRACKET IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,387 hrs · 37,854 cycles

LEFT HORIZONTAL STAB LEADING EDGE RIB CRACKED AT HSS 105.26. R & R THE RIB IAW DWG AND SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO COMPT; PNL 142KW IS CORRODED ALONG LWR EDGE ON BOTH SIDES. / REPLACED PNL 142KW WITH NEW PANEL P/N 146A7403-237 AND APPLIED TOPCOAT IAW DWG 146A9403 REV - AND AMM 51-21-99. A TAG WN9494.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,387 hrs · 37,854 cycles

FLIGHT DECK P18 SUPPORT BRACKET CRACKED AT BS 260, STR 8L. R&R CLIP IAW DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,387 hrs · 37,854 cycles

LEFT HORIZONTAL STAB LEADING EDGE RIB CRACKED AT BS 95.96. R & R THE RIB IAW DWG AND SRM.

Part: FRAME — CRACKED (RT WING) · airframe 63,387 hrs · 37,854 cycles

RH WING INBD LE BODY FAIRING SUPPORT STRUCTURE; INBD OF LANDING LILGHT ASSY; ANGLE CRACKED ON AFT SIDE. / REMOVED CRACKED FRAME IAW B737 SRM 51-40-02-0G-0. FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-30-71-1A-1; FIG 105. IDENTIFIED NEW PART AS FRAME P/N 116A3118V10 PER BOEING ENG DWG.NO. 116A3110 REV:-. INSTALLED FRAME IAW B737-SRM 51-40-02-0G-0; BOEING ENG DWG NO. 116A3010 REV :C; AND BOEING ENG DWG NO. 116A3110 REV:-. ATAG#A17075

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,387 hrs · 37,854 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 151.75. R & R THE RIB IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,387 hrs · 37,854 cycles

FUSELAGE INTERCOSTAL CRACKED AT BS 303.9, STR 4L. REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,387 hrs · 37,854 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 114.55. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,387 hrs · 37,854 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 86.66. R & R THE RIB ASSEMBLY IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (BS 663) · airframe 63,387 hrs · 37,854 cycles

RIGHT LOWER FUSELAGE VAPOR BARRIER CRACKED AT BS 663 INBOARD EDGE. REPAIRED THE BARRIER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LWR FUSELAGE) · airframe 63,387 hrs · 37,854 cycles

LEFT HAND; LWR FUSELAGE; SUPPORT ANGLE COMMOND TO GSE EXHAUST SEAL IS CRACKED / REMOVED AND REPLACED DAMAGED SUPPORT ANGLE AT LEFT HAND LWR FUSELAGE COMMON TO GSE EXHAUST SEAL IAW SRM 51-40-02-0G-0 AND DWG 111A1515 REV- RESTORED CIC IAW AMM 51-71-91-620-802

Part: ANGLE — CRACKED (LWR FUSELAGE) · airframe 63,387 hrs · 37,854 cycles

RIGHT HAND LWR FUSELAGE; UPPER ANGLE; COMMOND TO GSE EXHAUST SEAL; INBRD SIDE IS CRACKED / REMOVED AND REPLACED DAMAGED SUPPORT ANGLE AT RIGHT HAND LWR FUSELAGE COMMON TO GSE EXHAUST SEAL IAW SRM 51-40-02-0G-0 AND DWG 111A1515 REV-. RESTORED CIC IAW AMM 51-21-91-620-802

Part: SUPPORT ANGLE — CRACKED (LT WHEEL WELL) · airframe 63,387 hrs · 37,854 cycles

LEFT HAND VAPOR BARRIER; 45 DEGREE SUPPORT ANGLE; HAS CRACK / REMOVED L/H VAPOR BARRIER 45 DEGREE SUPPORT ANGLE I.A.W SRM 51-40-02-0G-00. DRILLED NEW SUPPORT ANGLE I.A.W SRM 51-40-05-0G-00 AND BOEING DWG 1111A1000. INSTALLED NEW SUPPORT ANGLE I.A.W SRM 51-40-02-0G-00 AND BOEING DWG 111A1000

Part: SEAL — CRACKED (LT WING) · airframe 63,387 hrs · 37,854 cycles

LEFT WING; FIXED TRAILING EDGE; MIDDLE SUPPORT RIB; CURVED SEAL RETAINER IS CRACKED AT UPPER FASTENER / REMOVED AND REPLACED L/H WING FIXED TRAILNIG EDGE MIDDLE SUPPORT RIB; CURVED SEAL RETAINER IAW SRM 51-40-02 AND DWG 115A2930 REV- ATAG A94753

Part: BULKHEAD — CRACKED (BS 663) · airframe 63,387 hrs · 37,854 cycles

LEFT MAIN WHEEL WELL VAPOR BARRIER CRACKED AT BS 663, INBOARD EDGE. REPAIRED THE BARRIER IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 63,387 hrs · 37,854 cycles

RIGHT WING; OTBRD FIXED T/E PANEL; ATTACH ANGLE COMMOND TO SEAL RETAINER; OTBRD END IS CRACKED / REMOVED AND REPLACED RIGHT WING OTBD FIXED T/E PANEL ATTACH ANGLE COMMOND TO SEAL RETAINER. I/A/W 737-700 SRM 51-40-02-0G-0 AND BOEING DWG 115A6200 REV. A

Part: GUSSET — CRACKED (BS 500D) · airframe 63,387 hrs · 37,854 cycles

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

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 63,387 hrs · 37,854 cycles

RIGHT WING; OTBRD FIXED T/E PANEL; ATTACH ANGLE COMMOND TO CENTER FWD CURVED SEAL RETAINER; IS CRACKED / REMOVED AND INSTALLED NEW R/H WING OTBRD FIXED T/E PANEL ATTACH ANGLE COMMOND TO CENTER FWD CURVED SEAL RETAINER IAW SRM 51-0-02-0G-0 AND BOEING DWG 115A2930

Part: BRACKET — CORRODED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO COMPARTMENT; L/H STA.727D; STR 23L-25L; GILL LINER ATTACH BRACKET HAVE CORROSION AROUND THE FASTENER HOLES. / REMOVED CORROSION IN AFT CARGO COMPARTMENT AROUND FASTNERS HOLES AT STA 727D GILL LINER ATTACH BRACKET BETWEEN STR 23L AND 25L. VERIFIED MATERIAL LOSS. ORIG'.063. REMAINING .052. LOSS OF .011. THERE ARE NO SRM LIMITS IN THIS AREA. REPAIRED IAW AAR EA 180102IR AND SWA EA 1-753-32317 REV IR

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO PIT FWD CORNER SCUFF PLATE CRACKED / RECEIVED FROM BACK SHOP ON W/O 37006-100-0001 AFT CARGO PIT FWD CORNER SCUFF PLATE

Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO COMPARTMENT; R/H STA. 947; AN ATTACH BRACKET UNDER THE Z-ANGLE HAVE EVIDENCE OF A CRACK AT THE LOWER FASTNER. / REMOVED ATTACH BRACKET IN AFT CARGO PIT AT STA 947 UNDER Z ANGLE. FABRICATED ATTACH BRACKET FROM BAC1509-100298 7075-T6511 AND INSTALLED ATTACH ANGLE IAW EA 180094 REV IR AND S/W EA 1-753-32292

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO COMPARTMENT; R/H STA. 867-887; R/H Z-ANGLE HAVE CORROSION AROUND THE FASTENER HOLES. / REMOVED CORROSION ON AFT R/H Z-ANGLE STA 867-887 100% MAT LOSS IAWB737-700 SRM 53-00-53-1A-2 FIG 103; REMOVED & REPLACE Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,387 hrs · 37,854 cycles

AFT CARGO COMPARTMENT; L/H STA.735-817; L/H Z-ANGLE HAVE CORROSION AROUND THE FASTENER HOLES. / VERIFIED MATERIAL LOSS AND LIMITS ORIG '7'. .040' 'LOSS OF 025' WITH .004' ALLOWED IS OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 FIG 109 DETAIL D. REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5; STA 727 C + 18 TO 847 LBL 25. TAG: A95297

Part: LINK — FAILED (LT MLG) · airframe 63,387 hrs · 37,854 cycles

LT MAIN LANDING GEAR BEAM HANGER LINK FAILED FREE PLAY CHECK. R&R LINK IAW AMM.

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 63,387 hrs · 37,854 cycles

PANEL 191FL UPPER AFT CORNER CRACKED / BROKEN / REPAIRED PANEL 191FL UPPER AFT CORNER IAW 737-700 SRM 51-70-04-2R-6 REV 63: 737-700 SRM 51-70-04-2R-0 REV 63 PER 737-700 SRM 53-30-70-2R-1 TABLE 202 REV 63.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,387 hrs · 37,854 cycles

RT WING NR 6 LEADING EDGE SLAT NOSE SKIN CRACKED AT SLAT STA 202.45. REPAIRED THE SKIN IAW AMM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 63,387 hrs · 37,854 cycles

LEFT WING NR 3 LEADING EDGE SLAT LOWER SURFACE OF NOSE SKIN CRACKED AT SLAT STA 202.45. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,387 hrs · 37,854 cycles

RIGHT WING NR 7 LEADING EDGE SLAT NOSE SKIN CRACKED AT SLAT STA 322.71. REPAIRED THE SKIN IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,387 hrs · 37,854 cycles

LEFT EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 1 TO 17. R & R THE POWER SUPPLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 62,855 hrs · 37,553 cycles

MID CABIN OVERWING EXIT SIGN BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 61,952 hrs · 37,020 cycles

SUPPLEMENTAL INFORMATION: RIGHT MAIN GEAR WHEEL WELL STA 663 STIFFENER CRACKED OUTBD OF RAM AIR EXHAUST DUCT / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02

Part: NONE — CORRODED (RUDDER) · airframe 61,952 hrs · 37,020 cycles

SUPPLEMENTAL INFORMATION: THE RUDDER BALANCE ARM WEIGHT IS CORRODED. / REMOVED AND REPLACED PER CMM 55-40-09.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 60,905 hrs · 36,454 cycles

R1 DOOR LOWER EXIT SIGN LENS INCORRECT. R & R LENS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,826 hrs · 36,402 cycles

LT EMERGENCY EXIT CEILING LIGHT INOP. R&R LIGHT ASSEMBLY PER MM.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 60,727 hrs · 36,336 cycles

RIGHT OVERWING EXIT LIGHT COVER FELL OFF. R & R THE COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,278 hrs · 35,519 cycles

LT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 57,859 hrs · 34,690 cycles

RIGHT CENTER EMERGENCY BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,422 hrs · 34,452 cycles

EMERGENCY LIGHT CHARGER M1674 INOPERATIVE. R & R CHARGER IAW AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

FRAME CRACKED AT BS 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

RIGHT DOOR STUB FRAME CRACKED SURROUND STRINGER 17R. R & R STAB FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

LEFT LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

LEFT FWD FRAME WEB STRAP CRACKED AT BS 303.9. R & R WEB STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

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

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 57,422 hrs · 34,452 cycles

R2 DOOR ENTRY CHORD CORRODED. R & R CHORD IAW SRM & DWG.

Part: FITTING — CORRODED (L1 DOOR) · airframe 57,422 hrs · 34,452 cycles

L1 DOOR EMER EVAC SLIDE FWD GIRT BAR FITTING CORRODED. R & R FITTING IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, LBL 10. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 57,422 hrs · 34,452 cycles

L1 DOOR AFT GIRT BAR FITTING CORRODED ON TOP SIDE. R & R FITTING IAW SRM.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 57,422 hrs · 34,452 cycles

RIGHT HORIZONTAL STABILIZER CRACKED ON SECOND STIFFENER, LOWER INBD SIDE STATION 92.70. REPAIRED T ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 57,422 hrs · 34,452 cycles

LEFT HORIZONTAL STABILIZER CRACKED AT FIRST STIFFENER.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 57,422 hrs · 34,452 cycles

LEFT HORIZONTAL STABILIZER CRACKED ON THIRD STIFFENER, LOWER INBD SIDE STATION 92.70. REPAIRED T ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 57,422 hrs · 34,452 cycles

RIGHT HORIZONTAL STABILIZER CRACKED AT FIRST STIFFENER LOWER INBD SIDE STATION 92.70. REPAIRED STABILIZER IAW SRM.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 57,422 hrs · 34,452 cycles

LEFT HORIZONTAL STABILIZER CRACKED ON SECOND STIFFENER, LOWER INBD SIDE STATION 92.70. REPAIRED T ANGLE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,422 hrs · 34,452 cycles

RIGHT WING NR 4 SLAT LE SKIN CRACKED AT ACTUATOR. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

LEFT HORIZONTAL WEB CRACKED AT BS 663, BETWEEN LBL 25 - 45. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,422 hrs · 34,452 cycles

RIGHT HORIZONTAL WEB CRACKED AT BS 673, BETWEEN RBL 25 - 45. REPAIRED WEB IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 55,275 hrs · 33,211 cycles

FORWARD ENTRY DOOR WALL EXIT SIGN LIGHT BROKEN. R & R SIGN IAW MM.

Part: SWITCH — LOOSE (CABIN) · airframe 52,716 hrs · 31,810 cycles

EMERGENCY EXIT LIGHT SWITCH LOOSE. R & R SWITCH ASSEMBLY IAW SIP.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,607 hrs · 31,168 cycles

FORWARD CARGO COMPARTMENT AIR CONDITIONING DISTRIBUTION BAY UPPER FLOORBOARD SUPPORT BRACKET CRACKED AT BS 540 LT OF CTR. R & R BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,607 hrs · 31,168 cycles

FORWARD CARGO COMPARTMENT AIR CONDITIONING DISTRIBUTION BAY UPPER FLOORBOARD SUPPORT BRACKET CRACKED AT BS 540 RT OF CTR. R & R BRACKET IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,607 hrs · 31,168 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,607 hrs · 31,168 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT ROW 16. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,607 hrs · 31,168 cycles

LEFT EMER LIGHT BATTERY PACKS FAILED CAPACITY CHECK. R & R PAX BATTERY PACKS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,607 hrs · 31,168 cycles

RIGHT EMER LIGHT BATTERY PACKS FAILED CAPACITY CHECK. R & R PAX BATTERY PACKS IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

RIGHT NR 3 WINDOW FRAME E - F POST 2ND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

RIGHT NR 3 WINDOW FRAME E - F POST 3RD FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,415 hrs · 31,062 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

RIGHT NR 3 WINDOW FRAME E - F POST 4TH FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

LEFT NR 3 WINDOW FRAME E - F POST 3RD FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

LEFT NR 3 WINDOW FRAME E - F POST 2ND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 51,415 hrs · 31,062 cycles

BULKHEAD VERTICAL WEB CRACKED AT BS 663, BETWEEN RBL 40.6 TO RBL 41. REPAIRED WEB IAW SRM.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

LEFT UPPER WING TO BODY FAIRING 195CL CRACKED. REPAIRED FAIRING IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,415 hrs · 31,062 cycles

VERTICAL WEB CRACKED AT BS 663 BETWEEN LBL 33 TO LBL 34. REPAIRED WEB IAW SRM.

Part: DOOR — CRACKED (LT MLG) · airframe 49,603 hrs · 29,962 cycles

LT MLG INNER DOOR CRACKED AT AFT HINGE, FWD SIDE. R & R DOOR IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 48,466 hrs · 29,290 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,407 hrs · 29,251 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,407 hrs · 29,251 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,407 hrs · 29,251 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,407 hrs · 29,251 cycles

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

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 48,282 hrs · 29,169 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,786 hrs · 28,865 cycles

RIGHT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT PER M/M.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,625 hrs · 28,747 cycles

RIGHT OUTBD AFT FLAP T/E SHOWS SIGNS OF DELAMINATION JUST ABOVE NR 5 FLAP FAIRING. REPAIRED AFT FLAP IAW SRM AND AMM.

Part: SIGN — LOOSE (CABIN) · airframe 47,128 hrs · 28,425 cycles

MID CABIN OVERHEAD EXIT SIGN IS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER M/M. OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 47,096 hrs · 28,403 cycles

AFT WALL OF THE FWD LAV EMERGENCY EXIT SIGN LIGHT LENS MISSING. INSTALLED LENS ASSY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,242 hrs · 27,869 cycles

R1 COCKPIT NR 5 WINDOW UPPER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,242 hrs · 27,869 cycles

R1 WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND BOEING DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,242 hrs · 27,869 cycles

L1 WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND BOEING DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 45,849 hrs · 27,649 cycles

LEFT WING NR 1 SLAT LOWER SURFACE SKIN CRACKED AT ACTUATOR MOUNT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 45,849 hrs · 27,649 cycles

LEFT HORIZONTAL STABILIZER SKIN CRACKED AT STA 129.50. REPAIRED SKIN IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 45,826 hrs · 27,640 cycles

OVERWING EMERGENCY EXIT SIGN PLASTIC COVER MISSING. REMOVED AND REPLACED COVER PER M/M.

Part: LIGHT — LOOSE (CABIN) · airframe 45,720 hrs · 27,579 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER AMM.

Part: SIGN — MISSING (CABIN) · airframe 45,712 hrs · 27,573 cycles

AFT CEILING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 45,345 hrs · 27,357 cycles

FORWARD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,090 hrs · 27,200 cycles

CENTER AISLE EEPLS ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: LENS — DEFECTIVE (CABIN) · airframe 44,660 hrs · 26,945 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 15 INOP. REMOVED AND REPLACED LENS PER MM.

Part: LENS — UNKNOWN (CABIN) · airframe 44,660 hrs · 26,945 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 15.

Part: SIGN — BROKEN (CABIN) · airframe 42,811 hrs · 25,858 cycles

EMERGENCY EXIT SIGN ATTACH CLIP BROKEN. REPAIRED SIGN ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 41,522 hrs · 25,137 cycles

CENTER OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 41,377 hrs · 25,047 cycles

MID CABIN EMERGENCY EXIT LIGHT LENS LOOSE. RE-SECURED EMERGENCY EXIT LIGHT LENS PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 39,374 hrs · 23,876 cycles

AFT OVERHEAD EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, BL 0. REPAIRED FLOORBEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,614 hrs · 23,445 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,614 hrs · 23,445 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD GALLEY FLOOR BEAM UPPER T-CAP CORRODED AT BS 328 BETWEEN LBL 34 TO RBL 56. REMOVED AND REPLACED T-CAP PER SRM AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,268 hrs · 23,217 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,268 hrs · 23,217 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,268 hrs · 23,217 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,268 hrs · 23,217 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,614 hrs · 23,445 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH BRACKET — LOOSE (EVAC SLIDE) · airframe 37,248 hrs · 22,597 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE ATTACH BRACKETS LOOSE. SECURED BRACKET PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,248 hrs · 22,597 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 37,248 hrs · 22,597 cycles

DURING SCHEDULED HC1 CHECK, L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LENS — MISSING (CABIN) · airframe 37,088 hrs · 22,491 cycles

MID CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 35,600 hrs · 21,584 cycles

EMERGENCY EXIT SIGN ON LIFE RAFT BOX LOOSE. SECURED SIGN PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 34,947 hrs · 21,205 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,159 hrs · 20,734 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32.40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRUCTURE — CRACKED (NR 5 SLAT) · airframe 32,919 hrs · 19,973 cycles

DURING SCHEDULED 6Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 32,919 hrs · 19,973 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,421 hrs · 19,678 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FITTING — CORRODED (RT WING) · airframe 31,569 hrs · 19,171 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 31,569 hrs · 19,171 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 31,349 hrs · 19,037 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,280 hrs · 18,903 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 29,254 hrs · 17,761 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 29,214 hrs · 17,734 cycles

MID CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,076 hrs · 14,132 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 9 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,846 hrs · 16,931 cycles

DURING SCHEDULED HC1 CHECK, RIGHT AFT CABIN EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 27,846 hrs · 16,931 cycles

DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,846 hrs · 16,931 cycles

DURING SCHEDULED HC1 CHECK, RIGHT OVERWING EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — WEAK (EMERGENCY LIGHT) · airframe 26,286 hrs · 16,016 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS WEAK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,596 hrs · 15,619 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,596 hrs · 15,629 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 25,365 hrs · 15,485 cycles

DURING SCHEDULED HC2 CHECK, RT ELEVATOR FAILED OUTPUT TORQUE TUBE CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE BEARING PER MM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 25,218 hrs · 15,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 43 TO RBL 50. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,218 hrs · 15,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 7. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,218 hrs · 15,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 32.5 TO RBL 43. REMOVED AND REPLACED FLOORBEAM SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,218 hrs · 15,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,933 hrs · 15,249 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 22,351 hrs · 13,795 cycles

DURING SCHEDULED RON, FOUND CABIN CEILING NR 3 EMERGENCY EXIT SIGN FWD LENS MISSING. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SKIN — CRACKED (BS 235) · airframe 22,259 hrs · 13,743 cycles

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

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 22,053 hrs · 13,626 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: RETAINER — BROKEN (R2 DOOR) · airframe 20,190 hrs · 12,530 cycles

R2 DOOR WILL NOT OPEN OR CLOSE, STUCK IN MID-POSITION. INSTALLED R2 DOOR HANDLE INNER BEARING RETAINER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,140 hrs · 12,499 cycles

OVERWING CENTER AISLE EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 18,948 hrs · 11,818 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,046 hrs · 10,209 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 16,046 hrs · 10,209 cycles

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

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 14,616 hrs · 9,443 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,200 hrs · 8,074 cycles

DURING SCHEDULED RON, FOUND FWD RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FUSE — DEFECTIVE (HYD SYSTEM) · airframe 9,124 hrs · 6,340 cycles

AIR TURNBACK, DURING CLIMB L/E DEVICES WOULD NOT RETRACT. UPON LANDING DEVICES WOULD NOT FULLY EXTEND. REMOVED AND REPLACED EXTEND AND RETRACT HYD FUSES PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 8,975 hrs · 6,241 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP BETWEEN ROWS 16 AND 20. SEATED EEPLS CONNECTOR AND OPS CK GOOD PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,703 hrs · 5,508 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED IN FWD CABIN. REMOVED AND REPLACED COVER PER MM.

Part: CONTROL UNIT — INOPERATIVE (ELEVATOR) · airframe 7,543 hrs · 5,398 cycles

DURING DESCENT, STAB TRIM LIGHT ILLUMINATED, DISCONNECTED AUTOPILOT SYS, AND CONTROL COLUMN FORE/AFT OPERATION WAS UNAVAILABLE FROM APPROX 15,000 FEET TO 4,000 FEET. C/W AUTOPILOT BITE CK. REMOVED AND REPLACED STAB TRIM RELAY AND ACTUATOR. ALL OPS CK GOOD. MX FERRY TO DAL, WHERE ENTIRE ELEV CONTROL SYS WAS INSP AND NO DISCREPANCIES NOTED. C/W DFCS BITE CK. ALL OPS CK GOOD. REMOVED AND REPLACED FDR FOR MX CONVENIENCE. LATER MX FERRY FROM JAX BACK TO DAL PER MX CONTROL REQUEST FOR BOEING EVALUATION. REMOVED AND REPLACED ELEVATOR FEEL / CENTERING UNIT, AND LOWER ELEVATOR TORQUE TUBE PER BOEING REQUEST AND EVALUATION OF THESE COMPONENTS. ALL MX C/W AND OPS CK GOOD PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,111 hrs · 5,129 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 6,343 hrs · 4,678 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED ON GROUND. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 6,222 hrs · 4,610 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER LOOSE. Removed and replaced EXIT LIGHT ASSY PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 6,095 hrs · 4,538 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,174 hrs · 3,404 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 4,004 hrs · 3,315 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.