N7851A

Part: LOCK — LOOSE (ZN 200 FUS TOP) · airframe 63,808 hrs · 42,071 cycles

SEAT 11 E RECLINES -SHOULD NOT RECLINE DUE TO EXIT ROW ON 12 REQUIRES NEW HYDRLOCK SEAT SHOULD BE SECURED IN UPRIGHT POSITION AFTER INSTALLATION.<[01] OK TO CONTINUE PER MEL 25-6-02 SP1 B AUTHORIZATION # 172847;[02] REMOVED AND REPLACED SEAT 11E HYDROLOK ASSY; SECURED SEAT UPRIGHT & REATTACHED RECLINE CABLE OPS CHECK NORMAL. REF CMM 25-21-42 & AMM 25-22-00 <BR><BR>SP1B ACTIONS UNDONE (REATTACHED CABLE) & REMOVED PLACARD

Part: ACTUATOR — FAULTY (ZN 100 FUS LOWER) · airframe 63,802 hrs · 42,067 cycles

AUTOPILOT WOULD NOT ENGAGE; STAB OUT OF TRIM LIGHT ILLUMINATED MOMENTARILY. PLANE NOSED OVER SLIGHTLY; AUTOPILOT CONTINUED TO DISENGAGE AND WOULD NOT REMAIN ENGAGED. FLIGHT CONTROLS WERE LESS RESPONSIVE IN ROLL THAN USUAL. AUTOPILOT IS FAULTING THE LVDT ON THE ELEVATOR AUTOPILOT ACTUATOR.<[01] PERFORMED FIM 27-11 TASK 808; VISUALLY INSPECTED AILERON CABLES ABSA AND ABSB CABLES FOR BLOCKAGE/DAMAGE. NO DEFECTS NOTED TO CABLES. REF AMM 27-11-00 STEP I; ABSA LH WAS AT 175; ABSB LH 176. ABSA RH 180; ABSB RH 180. ALL CABLE TENSIONS WITHIN LIMITS. PERFORMED AILERON TRAVEL TEST REF AMM 27-11-00; AILERON DEFLECTION NORMAL AND WITHIN LIMITS.;[02] PER FIM 27-11 TASK 808; CONFORMATION AILERON OPS NORMAL. NO FAULTS FOUND AT THIS TIME.;[03] R&R 'B' AUTOPILOT ELEVATOR ACTUATOR IAW AMM 22-11-26

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,656 hrs · 41,970 cycles

RH OVER WING EMERGENCY LIGHT INOP<[01] RELAMPED RH SLIDE/OVERWING LIGHT PER AMM 33-51-04.

Part: SIGN — DETACHED (ZN 200 FUS TOP) · airframe 62,707 hrs · 41,368 cycles

AFT GALLEY EXIT SIGN OVERHEAD HANGING DOWN<[01] R/R'D AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN ASSY AS PER AMM 33-51-01

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 62,633 hrs · 41,319 cycles

R1 EMERGENCY SLIDE NOT ATTACHED TO THE DOOR.<[01] REINSTALLED FWD SERVICE DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06.

Part: LAMP — INOPERATIVE (ZN 200 FUS TOP) · airframe 62,071 hrs · 40,968 cycles

RH OVER WING EMERGENCY LIGHT<[01] REMOVED AND REPLACED RH OVER WING EMERGENCY LIGHT LAMP IN REFERENCE TO AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,001 hrs · 40,269 cycles

FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK AT LOC WO142 PER AMM 33-51-06. OPS CHECK GOOD.

Part: SENSOR — FAULTY (LE FLAPS) · airframe 60,791 hrs · 40,132 cycles

NUMBER 2 LEADING EDGE FLAP DID NOT RETRACT ON CLEANUP. QRH FOLLOWED, NO ROLL NOTED. DIVERT TO BWI. TROUBLESHOT IAW FIM 27-88, TASK 806. R & R THE NR 2 LE FLAP EXTEND PROXIMITY SENSOR (S171) IAW AMM 27-88-11. OPS TESTED GOOD.

Part: ACCESS PANEL — CRACKED (LT NACELLE) · airframe 60,531 hrs · 39,962 cycles

CRACK AFT STRUT FAIRING IB ACCESS PANEL AFT UPPER FASTENER HOLE AT LT PYLON. REPAIRED AFT STRUT FAIRING I/B ACCESS PANEL AT LT PYLON IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: STRAP — CORRODED (BS 767-787) · airframe 60,531 hrs · 39,962 cycles

CORRODED STRAP, BS 767-787, LBL21- RBL21, WL 155.5 IN THE AFT CARGO COMPARTMENT. REPLACED THE STRAP IAW SRM 51-40-02, AND SRM 51-10-02, STEP 9.

Part: SUPPORT ANGLE — ELONGATED (ZN 100 FUS LOWER) · airframe 60,531 hrs · 39,962 cycles

ELONGATED HOLE ON SUPPORT ANGLE, BS 727 BULKHEAD AREA BETWEEN S25-26L IN THE AFT CARGO. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 144A2600, SHEET 255, REV -.

Part: ANGLE — CRACKED (BS907-927) · airframe 60,531 hrs · 39,962 cycles

CRACKED ANGLE, BS 907-927, S25-27R IN THE AFT CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A7221, SHEET 17, REV D.

Part: ANGLE — CORRODED (BS 947 S25R-26L) · airframe 60,531 hrs · 39,962 cycles

CORROSION ANGLE, BS 947, S25R-26L IN THE AFT CARGO COMPARTMENT. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02, STEP 9, SRM 51-40-02, & DWG 149A8117, SHEET 4, REV C.

Part: FRAME — CRACKED (BS 907 S25-26R) · airframe 60,531 hrs · 39,962 cycles

CRACKED FRAME, BS 907, S25-26R IN THE AFT CARGO COMPARTMENT. REPAIRED THE FRAME IAW B737-700 SRM 51-40-02, EA 22-153-03263-WIP1, EA 22-153-03263-WIP2, & EA 22-153-03263.

Part: ANGLE — CRACKED (BS 867 S26-27L) · airframe 60,531 hrs · 39,962 cycles

CRACKED ANGLE, BS 867, S26L-27L IN THE AFT CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 60,531 hrs · 39,962 cycles

CRACK ON WEB MIDDLE POSITION O/B FAN COWL ON ENGINE 2 2022-584826 / [01] REPLACED WEB LOCATED MIDDLE POSITION O/B FAN COWL ON<BR>ENGINE 2 I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-<BR>02-0G-0 AND CMM-71-13-30 FIGURE 3. SEE INDIVIDUAL SIGN<BR>OFF BELLOW;[02] TASK CARD COMPLETED

Part: ACCESS PANEL — BROKEN (RT WING) · airframe 60,531 hrs · 39,962 cycles

BROKEN STRIP ON ACCESS PANEL 632NB, RT WING. INSTALLED ACCESS PANEL 632NB IAW AMM:28-11-11-400-801.

Part: SUPPORT ANGLE — CRACKED (BS 663) · airframe 60,531 hrs · 39,962 cycles

CRACKED SUPPORT ANGLE, BS 663 LT SIDE. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 111A1000 REV-.

Part: WEB — BROKEN (NR 1 NACELLE) · airframe 60,531 hrs · 39,962 cycles

BROKEN WEB CENTER POSITION I/B FAN COWL ON ENGINE 1 2022-584817 / [01] REPLACED WEB CENTER POSITION I/B FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] TASK CARD COMPLETED

Part: SUPPORT BRACKET — BROKEN (RT WING) · airframe 60,531 hrs · 39,962 cycles

BROKEN SUPPORT BRACKET ON ACCESS PANEL 651FB, RT WING. REPLACED THE SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 60,531 hrs · 39,962 cycles

CRACK TRAILING EDGE BRAKET SUPPORT LOCATED IRSS 142, LT WING. REPLACED TRAILING EDGE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9.

Part: SUPPORT CHANNEL — CORRODED (BS727D-727E S25L) · airframe 60,531 hrs · 39,962 cycles

CORRODED CHANNEL SUPPORT ZEE, BS 727D & 727E, S25L IN THE AFT CARGO COMPARTMENT. REPLACED THE CHANNEL SUPPORT ZEE IAW SRM 51-10-02, ITEM 9, AND DWG 146A7500, SHEET 37, REV C.

Part: ANGLE — CRACKED (BS 500D S28L) · airframe 60,531 hrs · 39,962 cycles

CRACKED ANGLE, BS 500D,S28L IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 60,531 hrs · 39,962 cycles

CRACKED STRINGER 26R, BS 540, IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1. THIS REPAIR IS CATEGORY A.

Part: INTERCOSTAL — CRACKED (BS 500D-520 S28L) · airframe 60,531 hrs · 39,962 cycles

CRACKED INTERCOSTAL, BS 500D-520, S28L, IN THE FWD CARGO COMPARTMENT. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND DWG 143A9803, SHEET 8, REV B.

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 60,531 hrs · 39,962 cycles

CRACKED STRINGER 26L, BS 540, IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1 REPAIR 1 .

Part: SUPPORT CHANNEL — CORRODED (BS727D-727E S25R) · airframe 60,531 hrs · 39,962 cycles

CORRODED CHANNEL SUPPORT ZEE, BS 727D & 727E, S25R IN THE AFT CARGO COMPARTMENT. REPLACED THE CHANNEL SUPPORT ZEE IAW SRM 51-10-02, ITEM 9, & DWG 146A7502, SHEET 2, REV A.

Part: WEB — CRACKED (BS 540) · airframe 60,531 hrs · 39,962 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BTW LBL 0.07 TO LBL 24.82 AND BS 540 CENTER SECTION. REPLACED THE WEB IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A0060 SHEET 35; REV A.

Part: CHANNEL — CORRODED (BS 767-787 RBL 8) · airframe 60,531 hrs · 39,962 cycles

CORROSION ON RAIL CHANNEL LOC BTW BS 767 AND BS 787 RBL 8.10 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CHANNEL IAW SRM 53-00-53-2R-2, REPAIR 2.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 60,531 hrs · 39,962 cycles

CRACKED STRINGER 23R, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED STRINGER 23R LOCATED AT BS 540 FWD CARGO COMPARTMENT IAW 53-00-03-2R-1, REPAIR 1, THIS REPAIR IS CATEGORY A.

Part: WEB — CORRODED (BS 737-787 S25R) · airframe 60,531 hrs · 39,962 cycles

CORROSION ON SHIELD WEB LOC BTW BS 767 AND BS 787 AND STR 25R RBL 21 IN AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOC BTW BS 767 AND BS 787 AND STR 25R RBL 21 IAW SRM 51-10-02-0G-0 ITEM 9.

Part: LIGHT — DETERIORATED (CABIN) · airframe 60,531 hrs · 39,962 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN IAW AMM-33-51-15-400-802.

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 60,531 hrs · 39,962 cycles

CRACKED STRINGER 23L, BS 540, IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: WEB — CORRODED (BS 847-867 S25R) · airframe 60,531 hrs · 39,962 cycles

CORRODED SHIELD WEB, BS 847 & 867, S25R RBL 21 IN AFT CARGO COMPARTMENT. REPLACED THE SHIELD WEB IAW SRM 51-10-02, ITEM 9.

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 60,531 hrs · 39,962 cycles

CRACK SUPPORT ANGLE LOCATED AT LBL 0.07 AND BS 695 CENTER SECTION 2022-584736. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT LBL 0.07 AND BS 695 CENTER SECTION IAW SRM B737-700-51-40-02; 51-10-02 ITEM 9 AND DRAWING 273A9111 REV F;[03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT LBL 0.07 AND BS 695 CENTER SECTION IAW SRM B737-700-51-40-02; 51-10-02 ITEM 9 AND DRAWING 273A9111 REV F ITEM RII

Part: CHANNEL — CORRODED (BS 500-500A S25R) · airframe 60,531 hrs · 39,962 cycles

CORROSION ON CHANNEL SUPPORT SHIELD, BTW BS 500 AND BS 500A, S25R IN THE FWD CARGO COMPARTMENT. REPLACED WEB-CHANNEL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A8126 SHEET 10 REV A.

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 60,531 hrs · 39,962 cycles

CRACK SUPPORT ANGLE LOCATED ON BS 695 RBL 24.82 FLOOR STRUCTURE AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED ON BS 695 RBL 24.82 FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 111A6000 REV A.

Part: PLATE — CRACKED (RT WING) · airframe 60,531 hrs · 39,962 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING 2022-584665. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT RT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2001 SHEET 18 REV -.

Part: ANGLE — CORRODED (RT WING TE) · airframe 60,531 hrs · 39,962 cycles

CORRODED ANGLE, TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA WS 270 AND ORSS 273. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 8, REV C.

Part: ANGLE — CRACKED (LT WING) · airframe 60,531 hrs · 39,962 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 271 APROX AT LT WING. REPLACED THE ANGLE TRAILING EDGE LOCATED ORSS 271 APROX AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 60,531 hrs · 39,962 cycles

CRACK SUPPORT ANGLE LOCATED ON BS 695 LBL 24.82 FLOOR STRUCTURE AT PASSENGER CABIN 2022-584667. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON BS 695 LBL 24.82 FLOOR STRUCTURE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DRAWING 273A9110 SHEET 2 REV A.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 60,531 hrs · 39,962 cycles

CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT. FABRICATED A NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND DWG 453A2610 SHEET 18 REV B, SRM 51-10-02 ITEM 9. REPLACED THE FLOOR PANEL 140CF IAW AMM 25-52-01-201-801 AND DWG 453A2610 SHEET 18 REV B, SRM 51-10-02 ITEM 9

Part: WEDGE — DEBONDED (RT WING TE FLAP) · airframe 60,531 hrs · 39,962 cycles

DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING. REPAIRED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING IAW SRM 57-53-01-2R-7, REPAIR 7.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,531 hrs · 39,962 cycles

CRACK STIFFENER INSPAR RIB 147.90 TO 25 INCH FRONT SPAR AT LT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB 147.90 TO 25 INCH FRONT SPAR AT LT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-4 REPAIR 4 THIS REPAIR IS CATEGORY A.

Part: PRESSURE PANEL — CRACKED (BS 663 RBL 41) · airframe 60,531 hrs · 39,962 cycles

CRACK INDICATION ON PRESSURE WEB PANEL, RBL 41, BS 663. CRACK LENGTH 1 INCH. REPAIRED THE PRESSURE PANEL IAW SRM 53-40-51-2R-2, REPAIR 2.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 60,531 hrs · 39,962 cycles

CRACK ON FWD CORNER SCUFF PLATE IN THE AFT CARGO COMPARTMENT. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, STEPS 2 & 4 - 7 BAC 5975.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,531 hrs · 39,962 cycles

INOP LOWER SIDEWALL PANEL BATTERY PACK BTW STATION 597 AND 616 LT SIDE IN PASSENGER CABIN. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-806 TESTED OK.

Part: SKIN — CRACKED (LT NR 3 SLAT) · airframe 60,531 hrs · 39,962 cycles

CRACK SLAT 3 LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR RIBS AT LT WING 2022-584338 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 190023010;CAL DUE DATE: 14-FEB-23;[02] REMOVED AND REPLACED LEADING EDGE SLAT 3 IAW B737-700 AMM 27-81-21.STEPS ARE DOCUMENTED ON NRC TTG8Q00FJ87E.;[03] JOB COMPLETED AND CERTIFIED AS RII.

Part: BATTERY — INOPERATIVE (BULLHORN) · airframe 60,461 hrs · 39,915 cycles

FORWARD BULLHORN IS INOP / REPLACED BATTERIES IN A BULL HORN PER AMM 25-64-00

Part: NONE — INOPERATIVE (OVERWING EXIT) · airframe 60,329 hrs · 39,824 cycles

OVER WING EXIT LEFT-HAND SIDE EMERGENCY LIGHTS ON CEILING ;OVER DOOR ;AND NEXT TO DOOR ARE INOPERATIVE / [01] R/R BATERY PACK IAW AMM 33-51-06 OPS CHK OK.;[02] R/R BATTERY PACK IAW AMM 33-51-06 OPS CHK GOOD

Part: FUSE — INOPERATIVE (R/H CABIN) · airframe 59,979 hrs · 39,576 cycles

RIGHT EMERGENCY EXIT SIDEWALL LIGHT INOP / [01] REMOVED AND REPLACED RIGHT EMERGENCY EXIT SIDEWALL LIGHT FUSE IAW AMM 33-21-00. OPS CHECK GOOD.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 59,654 hrs · 39,348 cycles

193B PANEL FASTENER HOLES 1; 2; 3; 5; 8; 10; 16; 21; 26; 29; 30 AND 31 ARE ELONGATED. 193B PANEL FASTENER HOLES 1 2 3 5 8 10 16 21 26 29 30 AND 31 ARE ELONGATED. / [01] COMPLIED WITH EA 22-153-01854;[02] PERFORMED TIME LIMITED REPAIR PER TSR: 2022004838 AND EA 22-153-01854

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 59,575 hrs · 39,295 cycles

FWD SERVICE DOOR GIRT BAR LOOSE. / [01] RESECURED FWD SERVICE DOOR SLIDE GIRT BAR CLIP IAW WITH S.I.P. OPS CHECK NORMAL.

Part: GIRT BAR — DISLODGED (R1 DOOR) · airframe 59,570 hrs · 39,293 cycles

FWD SERVICE DOOR GIRT BAR DISLODGED / [01] REPOSITION FWD SERVICE DOOR GIRT BAR. VERIFIED SMOOTH OPERATION REF MM 25-66-00

Part: LIGHT — INOPERATIVE · airframe 59,106 hrs · 39,006 cycles

12 ABC BULLNOSE EMERGENCY LIGHT LENS NOT SECURE / [01] REMOVED AND REPLACED EMERGENCY LIGHT LENS AT 12 ABC REF AMM 33-51-03;[02] INSP

Part: LIGHT — FAILED (FWD GALLEY)

EMARGENCY EXIT LIGHT COVER FELL OFF ; / [01] REINSTALLED AND SECURED EMERGENCY EXIT SIGN AT FWD GALLEY I/A/W AMM 33-51-01.

Part: COVER — CRACKED (RT OVRWG ASSIST) · airframe 57,356 hrs · 37,928 cycles

R/H OVER WING DOOR ASSIST HANDLE COVER IS CRACKED. ; / [01] REPLACED RT OVER WING EMERGENCY EXIT DOOR ASSIST HANDLE COVER PER 52-22-00; [02] INSPECTED.

Part: MEGAPHONE — WEAK (AFT CABIN) · airframe 57,339 hrs · 37,916 cycles

AFT MEGAPHONE BATTERY WEAK ; / [01] CONDITION OF MEGAPHONE UNKNOWN. REPLACED MEGAPHONE IN AFT POSITION. NOW CHECKS GOOD. REF AMM 25-64-00.

Part: LIGHT — LOOSE (SEAT 8A) · airframe 56,570 hrs · 37,469 cycles

EMERGENCY EXIT LIGHT STRIP NEAR SEAT 8A STICKING UP IN FLIGHT ONLY ; / RESECURED LIGHT STRIP IAW MM 33-51-15 (PHOTOLUMINESCENT STRIP)

Part: LIGHT — LOOSE (SEAT 8A) · airframe 56,570 hrs · 37,469 cycles

EMERGENCY EXIT LIGHT STRIP AT SEAT 8A STICKING UP FROM FLOOR. RESECURED

Part: ATTACH ANGLE — CORRODED (RT WING TE) · airframe 55,315 hrs · 36,725 cycles

CORROSION RT WING UPPER AFT TRAILING EDGE PANEL AFT ATTACH ANGLE HAS CORROSON AT ORSS 404. / REMOVED AND REPLACED RT WING T/E PANEL ATTACH RETAINER ANGLE AT ORSS A04 PER REF B737 SRM 51-45-02-0G-0

Part: ATTACH ANGLE — CORRODED (RT WING TE) · airframe 55,315 hrs · 36,725 cycles

CORROSION *** RT WING UPPER AFT TRAILING EDGE PANEL AFT ATTACH ANGLE HAS CORROSON AT ORSS 345. / REMOVED AND REPLACED RT WING UPPER AFT T/E ANGLE RETAINER AT ORSS 345 PER REF B737 SRM 51-40-02-0G-0

Part: SKIRT — OUT OF POSITION (L2 DOOR SLIDE) · airframe 55,315 hrs · 36,725 cycles

QA CABIN WALK R-2 AND L-2 DOORS ESCAPE SLIDE SKIRT TOUCHING SCUFF PLATE WHEN CLOSING. REPOSITION R2 AND L2 DOOR SLIDE SKIRT,AS PER MNT 725-61-0 AND AMM 25-66-01-400-801, WITHOUT DISTUBE THE SLIDE COMPARTMENT.

Part: FITTING — CRACKED (BS 1016) · airframe 55,315 hrs · 36,725 cycles

CRACK DRAINS AT AFT FUSELAGE LOWER SKIN AREA SAT 1016 / REMOVED AND REPLACED 3EA. DRAINS FITTING AT STA 1016 LOWER SKIN AREA IAW DWG #148A3320 AND B-737-700 SRM 51-40-02-0G-0

Part: SCUFF PLATE — OUT OF POSITION (R2 DOOR) · airframe 55,315 hrs · 36,725 cycles

QA CABIN WALK R-2 AND L-2 DOORS ESCAPE SLIDE SKIRT TOUCHING SCUFF PLATE WHEN CLOSING. REPOSITION R2 AND L2 DOOR SLIDE SKIRT, AS PER MNT 725-61-0 AND AMM 25-66-01-400-801 WITHOUT DISTUBE THE SLIDE COMPARTMENT.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 55,315 hrs · 36,725 cycles

FWD CLOSET 2 EACH FLASHLIGHTS DEAD. REPLACED FWD CLOSET 2 EACH FLASH LIGHTS, IAW B737-700 DWG NR 25600001.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,315 hrs · 36,725 cycles

EMERGENCY EXIT LIGHT (L1223) AT AFT GALLEY CEILING INOPERABLE. FOUND LOOSE CONNECTOR D10180 OF EMERGENCY LIGHT (L1223). RESECURED CONNECTOR, AS PER B737 WDM 33-51-14. PERFORMED SELF ILLUMINATED EXIT SIGN, AS PER B737 AMM 33-51-02-720-801. TEST FOUND NORMAL.

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 55,315 hrs · 36,725 cycles

VERTICAL STAB AFT SPAR RIGHT OUTBOARD FIN ATTACH POINT HAS FWD DRAG BRACE FITTING WITH PITTING IN UPPER INBOARD AREA OF BOLT HOLE. / REMOVED AND REPLACED VERTICAL STAB AFT SPAR RIGHT O/B FIN ATTACH POINT FWD DRAG BRACE FITTING REF B737-700 SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 AND DWG #148A8200

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 55,315 hrs · 36,725 cycles

VERTICAL STAB AFT SPAR LEFT OUTBOARD FIN ATTACH POINT HAS FWD DRAG BRACE FITTING WITH PITTING IN UPPER OB AREA OF BOLT HOLE. / REMOVED AND REPLACED VERTICAL STAB AFT SPAR LEFT O/B FIN ATTACH POINT FWD DRAG BRACE FITTING REF B737-700 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG #148A8200

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 55,315 hrs · 36,725 cycles

VERTICAL STAB AFT SPAR RIGHT OUTBOARD FIN ATTACH POINT HAS AFT DRAG BRACE FITTING WITH PITTING IN LWR OB AREA OF BOLT HOLE. / REMOVED AND REPLACED VERTICAL STAB AFT RIGHT O/B FIN ATTACH POINT AFT DRAG BRACE FITTING REF B737-700 SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 AND DWG #148A8200

Part: SEAL — MISSING (HORIZONTAL STAB) · airframe 55,315 hrs · 36,725 cycles

HORIZ STAB UPPER SLIDING SEAL HAS WORN AREAS AND MISSING CHAFE PAD. / REMOVED AND REPLACED HORIZONAL STABLIZER UPPER SLIDING SEAL IAW B737-70 SRM 51-40-02-OG-0 .

Part: STAND OFF — BROKEN (BS 259) · airframe 55,315 hrs · 36,725 cycles

COCKPIT FRAME BS 259.5 LBL 13 HAS BROKEN METAL STANDOFF. / REMOVED AND REPLACED STANDOFF AT COCKPIT FRAME BS 259.5 LBL 13 REF B-737-700 SRM 51-40-02

Part: PLATE — CORRODED (AFT CARGO) · airframe 55,315 hrs · 36,725 cycles

***CORROSION*** AFT CARGO COMPARTMENT R/H SIDE PLATE HAS SPOTS OF CORROSION FROM STA.767 TO 727 +4' RBL 21 / REMOVED AND REPLACED SIDE PLATE( INTERCOASTAL TRACK) AT AFT CAFGO COMPARTMENT R/H FROM STA 767 TO STA 727 PER B737-700 SRM 51-40-02-0G-0 AND DWG#146A7502

Part: FLOOR SUPPORT — DAMAGED (BS 865-887) · airframe 55,315 hrs · 36,725 cycles

AFT CARGO FLOOR SUPPORT HAS TWO ELONGATED HOLES BETWEEN STA.865 AND STA.887. APPROX LBL 9'. / REMOVED AND INSTALLED AFT CARGO FLOOR SUPPORT BET STA 865 AND STA 887 IAW B737-700 SRM 51-40-02-0G-0; BOEING DWG DOC #146A7503

Part: PLATE — CORRODED (BS 727D) · airframe 55,315 hrs · 36,725 cycles

***CORROSION*** AFT CARGO R/H SIDE PLATE HAS SPOTS OF CORROSION FROM STA.727D TO FWD BULKHEAD. / WORK TO BE ACCOMPLISED ON N/R W179547

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 55,315 hrs · 36,725 cycles

FWD CARGO HAS GUSSET CRACKED AT BS 500D & STR 19R. / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP BS 500D STR 19R IN REF B737-700 SRM 51-40-02-0G-0 AND DWG 143A7902

Part: GUSSET — CRACKED (BS 500D S21L) · airframe 55,315 hrs · 36,725 cycles

FWD CARGO GUSSET APPEARS TO BE CRACKED AT BS 500D STR 21L. / REMOVED; LOCATED AND DRILLED ; INSTALLED GUSSET AT FWD CARGO COMPARTMENT BS 500D STR 21L AS PER REF B737-700 SRM 51-40-02-0G-0 ; DWG # 143A7902 AND SRM 51-40-05-0G-0

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 55,315 hrs · 36,725 cycles

FWD CARGO HAS GUSSET CRACKED AT BS 500D $ STR 19L. / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP AT BS 500D AT STR 19L IN REF B737-700 SRM 51-40-02-0G-0 AND DWG 143A7902

Part: SKIN — CHAFED (LT WING SLAT) · airframe 55,315 hrs · 36,725 cycles

LW #1 ; 2; 3 & 4 SLATS TE LWR SURFACE SHOWS EVIDENCE OF CHAFING WITH VISIBLE BARE METAL IN ISOLATED AREAS. PREPARED; TREATED APPLIED PRIMER AND PAINT TELFON AT LW #1;2;3; AND 4 SLAT TE LOWER SYRFACE IN AREAS REF B737 SRM 5120010G0; AMM 512172370804; AMM 51281370802.

Part: WEB — DAMAGED (FUSELAGE) · airframe 55,315 hrs · 36,725 cycles

FLIGHT DECK FLOOR WEB DAMAGE AT APPROXIMATELY STA 260. ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR, REF EA 1-A53-33170 REV 1.

Part: SKIN — CHAFED (RT WING SLAT) · airframe 55,315 hrs · 36,725 cycles

R/W #5; 6; 7 & 8 SLATS TE LWR SURFACE SHOWS EVIDENCE OF CHAFING WITH VISIBLE BARE METAL IN ISOLATED AREAS. PREPARED TREATED APPLIED PRIMER AND PAINT TELFON AT RW #5;6;7; AND 8 SLATS TE LOWER SURFACE IN AREAS REF B737 SRM 5120010G0 ; AMM 512172-370-804; AMM 512181370802

Part: PANEL — CRACKED (AFT CARGO) · airframe 55,315 hrs · 36,725 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD PANEL # 141LW; EDGE AREAS WITH TEARS; CRACKS AND/OR DELAMINATED. / RECEIVED NEW AFT CARGO COMPARTMENT FWD BULKHEAD PANEL #141LW. NEW PANEL WILL BE INSTALLED ON REFERENCE CUSTOMER CARD # JPANEL-141-CLOSE

Part: PANEL — CRACKED (AFT CARGO) · airframe 55,315 hrs · 36,725 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD PANEL # 142NW; UPPER AND LOWER EDGES WITH TEARS; CRACKS AND/OR DELAMINATED. / RECEIVED PANEL #142 NW. TO BE INSTALLED ON T/C-JPANEL -141-CLOSE.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 55,315 hrs · 36,725 cycles

CABIN FLOOR SUPPORT CRACKED AT BEND RADIUS BS 540 LBL 1' (51-001). REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN BS 540 LBL AND TREATED & PRIME, IN REF B737-700 SRM 51-40-02-0G-0 AND DWG NR 143A0060.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 55,315 hrs · 36,725 cycles

CABIN FLOOR SUPPORT CRACKED AT BEND RADIUS BS 540 RBL 1' (51-002). REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN BS 540 RBL AND TREATED AND PRIMED, IN REF B737-700 SRM 51-40-02-0G-0 AND DWG NR 143A0060.

Part: STRAP — DAMAGED (LT CABIN) · airframe 55,315 hrs · 36,725 cycles

LH EMERGENCY EXIT HATCH CUT-OFF VELCRO SUPPORT ESCAPE STRAP IS DAMAGED / REMOVED AND REPLACED VELCRO SUPPORT ESCAPE STAP AT LH EMERGENCY EXIT CUT-OUT PER REF B737-700 AMM 20-10-06-000-801

Part: STRAP — DAMAGED (RT CABIN) · airframe 55,315 hrs · 36,725 cycles

RH EMERGENCY EXIT CUT-OUT VELCRO SUPPORT ESCAPE STRAP IS DAMAGE. / REMOVED AND REPLACED VELCRO SUPPORT ESCAPE STRAP AT R/H EMERGENCY EXIT CUT-OUT PER REF B737-700 AMM 20-10-06-000-801

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,623 hrs · 36,287 cycles

SEVERAL INTERIOR EMERGENCY EGRESS LIGHTS INOP. REMOVED AND INSTALLED EMERGENCY LIGHT BOTTOM PACK ON M1670 AT STA 727C+13; WL 212; LBL 68 727C PER AMM 333-51-06-960-805. TESTED EMERGENCY LIGHTS PER AMM 53-51-06-960-805 4D(5). PASS.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 54,099 hrs · 35,963 cycles

L1 DOOR SLIDE GIRT TOO LONG, NEEDS REINSTALLED. RESECURED GIRT PER MT.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 54,099 hrs · 35,963 cycles

L2 DOOR SLIDE GIRT TOO LONGS NEEDS REINSTALLED. RESECURED GRIT PER MT.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 54,099 hrs · 35,963 cycles

R2 DOOR SLIDE GIRT TOO LONGS, NEEDS REINSTALLED. RESECURED GRIT PER MT.

Part: LENS — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,413 hrs · 35,522 cycles

L/H OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. / R&R LENS PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,421 hrs · 34,899 cycles

AFT LT EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: LENS — MISSING (CABIN) · airframe 51,857 hrs · 34,549 cycles

RT OVERWING EMERGENCY LIGHT FLOOR SIDE WALL EXIT LENS MISSING. R&R BATTERY PACK PER MM.

Part: LENS — MISSING (CABIN) · airframe 51,857 hrs · 34,549 cycles

RT OVERWING EMERGENCY LIGHT FLOOR SIDE WALL EXIT LENS MISSING. R&R CHARGER PER MM.

Part: LIMIT SWITCH — FAULTY (HORIZ STAB) · airframe 50,677 hrs · 33,822 cycles

AIR TURNBACK/DECLARED EMERGENCY, ON CLIMBOUT THE NOSE STARTED TO PITCH UP WITHOUT A/P ENGAGED, TRIED NOSE DOWN TRIM AND WOULD NOT WORK. MANUALLY TRIMMED A/C - NO C/B'S POPPED. R&R NOSE DOWN LIMIT SWITCH IAW AMM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 50,639 hrs · 33,796 cycles

R2 DOOR AFT GIRT BAR LATCH LOOSE. R&R FITTING PER AMM.

Part: SUPPORT ANGLE — CRACKED (LT WHEEL WELL) · airframe 50,639 hrs · 33,796 cycles

QC - VERTICAL SUPPORT ANGLE IN LH MLG BAY CRACKED AT LOWER END; BS 663; LBL 28; WL 152. / REMOVED & REPLACED VERTICAL SUPPORT ANGLE FROM L/H MLG BAY BS. 663; LBL 28 WL 152 IAW DWG 111A1000 REV. F 59191U 12JAN19

Part: GUSSET — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

GUSSET CORRODED BETWEEN BS 847 TO BS 855, RBL 25. R&R GUSSET PER SRM AND DWG.

Part: LENS — LOOSE (CABIN) · airframe 50,639 hrs · 33,796 cycles

RT EMERGENCY LIGHT ASSEMBLY LENS LOOSE BETWEEN AT ROW. SECURED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 50,639 hrs · 33,796 cycles

RT EMERGENCY LIGHT ASSEMBLY LENS LOOSE AT ROW 8. SECURED LENS IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

STRINGER CLIP CRACKED AT BS 500C, LBL 21. R&R CLIP PER DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

FLOOR SUPPORT CRACKED AT BS 318, LBL 47. R&R SUPPORT PER SRM AND DWG.

Part: VAPOR BARRIER — DETERIORATED (LT MLG WW) · airframe 50,639 hrs · 33,796 cycles

LT WHEEL WELL VAPOR BARRIER DETERIORATED AT BS 663, LBL 25. REPAIRED BARRIER IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,639 hrs · 33,796 cycles

MAIN CABIN FLOOR PANEL 241AF UPPER SURFACE DELAMINATED. / DUE TO EXTENT OF DAMAGE; OPTED TO FABRICATED A NEW PANEL; AND ROUGH-CUT NEW PANEL PER DWG 144A5810-8 IAW SRM 53-00-50-2R-0 PARA 1A-NOTE'. 59198U 12.14.18 10524C 12/14/18 FINISHED FABRICATION IAW SRM 53-00-50-2R-0 PARA 1A 'NOTE'; INSTALLED AND CURED ALL THROUGH INSERTS USING BMS 5-107 LOT #AK8EP4363K IAW SRM 53-00-50-2R-0 PARA 5S. PART MARKED AND LABELED PER DWG 144A5810-8 59198U 12.15.18.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,639 hrs · 33,796 cycles

MAIN CABIN FLOOR PANEL 231XF UPPER SURFACE DELAMINATED. / DUE TO EXTENT OF DAMAGE; FABRICATED A REPLACEMENT PANEL FOR MAIN CABIN FLOOR PANEL 231XF FROM BMS 4-23 TYPE II LOT# 1368331-1; INSTALLED ALL INSERTS WITH RESIN BMS5-107 LOT# AK8EP4363K; AND PART MARKED PANEL IAW SRM 53-00-30-2R-0 PARA 1A 'NOTE'. PARA 4; DWG #144A58107 AND BAC 5088 59278U 12/17/18

Part: VAPOR BARRIER — DETERIORATED (RT MLG WW) · airframe 50,639 hrs · 33,796 cycles

VAPOR BARRIER DETERIORATED AT BS 663, RBL 10.845. REPAIRED BARRIER IAW SRM.

Part: TAIL CONE — DEBONDED (AFT FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

TAILCONE DISBONDED AT STA 1163.5; LBL 12. / REPAIRED DAMAGE ON TAILCONE AT STA 1163.5; LBL 12 IAW SRM 51-70-04-2R-2. 56749U 31DEC18

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

FORWARD CARGO BAY INTERCOSTAL CLIP CRACKED AT BS 500C, LBL 21. R&R CLIP PER DWG & AND SRM.

Part: NONE — CRACKED (FWD CARGO) · airframe 50,639 hrs · 33,796 cycles

FWD CARGO BAY INTERCOSTAL CLIP AT BS 400 LBL 21 W/L 156 IS CRACKED / REMOVED & REPLACED FWD CARGO BAY INSTERCOSTAL CLIP AT BS400; LBL21; WL156 IAW SRM 51-40-02-0G-0 STEP 4 AND 7.D. 56790U 07JAN19

Part: PLATE — BROKEN (L/H WING) · airframe 50,639 hrs · 33,796 cycles

L/W T/E WIGGLE PLATE JUST I/B OF #1 PYLON IS BROKEN / REMOVED BROKEN WIGGLE PLATE FROM L/W T/E JUST I/B OF #1 PYLON. INSTALLED NEW WIGGLE PLATE IAW SRM 51-40-02-0G-0 PARA 4. & IPC 57-50-00-30.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,639 hrs · 33,796 cycles

LT HORIZONTAL STABILIZER REMOVABLE LEADING EDGE 5TH RIB FROM INBOARD END CRACKED. REPAIRED RIB IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,639 hrs · 33,796 cycles

RT HORIZONTAL STABILIZER REMOVABLE LEADING EDGE 3RD RIB FROM INBOARD END CRACKED. R&R RIB IAW SRM & DWG.

Part: PANEL — ELONGATED (RT WING) · airframe 50,639 hrs · 33,796 cycles

R/W T/E PANEL 671BB HAS A ELONGATED HOLE. ( MARKED ) / REPAIRED ELONGATED HOLE ON R/W T/E PANEL 671BB IAW SRM 51-70-05-2R-6 59278U 12/17/18

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

VAPOR BARRIER FOUND A TEE STIFFENER CRACKED AT BS 663, LBL 25. R&R STIFFENER IAW DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 50,639 hrs · 33,796 cycles

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

Part: STRAP — CORRODED (MAIN CABIN) · airframe 50,639 hrs · 33,796 cycles

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016+2 LBL3 WL208.1.MARKED / REPAIRED THE TENSION STRAP AT AFT CABIN B.S 1016+2 LBL 3; WL 208.1 IAW ER 18-05986 REV IR AND SWA EA 1-753-33918 REV IR

Part: STRAP — CORRODED (MAIN CABIN) · airframe 50,639 hrs · 33,796 cycles

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016+10 RBL17 WL208.1. MARKED / REPAIRED THE TENSION STRAP AT BS 1016-110 RBL 17 WL 208.1 IAW ER 18-05986 REV IR AND SWA EA 1-753-33918 REV IR.

Part: WEB — CORRODED (MAIN CABIN) · airframe 50,639 hrs · 33,796 cycles

***CORROSION*** ON 1016 WEB STA1016 LBL28 WL208.1. MARKED / REPAIRED THE WEB AT STA 1016 LBL 28; WL 208.1 IAW ER 18-05986 REV IR AND SWA EA 1-753-33918 REV IR.

Part: WEB — CORRODED (MAIN CABIN) · airframe 50,639 hrs · 33,796 cycles

***CORROSION*** ON 1016 WEB STA1016 LBL13 WL208.1. MARKED / REPAIRED THE WEB AT BS 1016 LBL 13; WL 208.1 IAW ER 18-05986 REV IR AND SWA 1-753-33918 REV IR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR TRACK CORRODED AT BS 787+16, RBL 14. R&R TRACK PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

R2 DOORWAY FRAME ANGLE CORRODED AT BS 993, STR 14R. R&R ANGLE PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 295, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 22. R&R SHIELD ASSEMBLY IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 50,639 hrs · 33,796 cycles

AFT CABIN FLOOR PANEL 241AEF HAS DAMAGED INSERT AND DELAMINATED UPPER SURFACE PLIES / REPAIRED DAMAGE TO UPPER SURFACE & INSERTS ON AFT CABIN FLOOR PANEL 241 AEF IAW SRM 53-00-50-2R-9 & SRM 53-00-50-2R-4. 57885U 12-12-18

Part: SUPPORT — CORRODED (AFT ENTRY DOOR () · airframe 50,639 hrs · 33,796 cycles

***CORROSION*** ON AFT ENTRY DOORWAY SURROUND SUPPORT STRUCTURE AT UPPER FWD CORNER; INBD SURFACE BS957; STR7; LBL46 / REMOVED AND REPLACED AFT ENTRY DOORWAY SURROUND STRUCTURE UPPER ASSY -167 PER DWG 411A2229-167 13457C JAN3 19 INSP 24 3JAN19 SURROUND STRUCTURE AFT ENTRY DOORWAY UPPER FWD CORNER BS 957; STR 7; LBL 46

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 767 TO BS 787+7, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 312 TO BS 344, LBL 65. R&R MOPSILL IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727E+12 TO BS 847, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 22. R&R SUPPORT IAW SRM.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 50,639 hrs · 33,796 cycles

FWD CABIN FLOOR PANEL 221GF FWD O/B CORNER (TANG) BROKEN / DUT TO THE EXTENT OF DAMAGE TO FWD O/B CORNER; REPLACED FWD CABIN FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-32A ITEM 720. 57066U 12/7/18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

FORWARD CARGO BAY AFT RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 21. R&R SUPPORT BAY IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

FORWARD CARGO BAY RT AFT FLOOR SUPPORT SHIELD CORRODED. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,639 hrs · 33,796 cycles

FORWARD CARGO BAY LT FLOOR-TO-SIDEWALL SUPPORT CORRODED. REPAIRED SUPPORT IAW SRM.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 50,639 hrs · 33,796 cycles

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

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / REMOVED CRACK DAMAGED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW SOPM 20-50-01 LOCATED AND DRILLED NEW SCUFF PLATE IAW SRM 51-40-05-0G-0 OK TO INSTALL 13656R 12JAN19 INSP 358 01/12/19 INSTALLED NEW SCUFF PLATE AT AFT CARGO FWD CORNER IAW AMM 53-11-02-420-801 13656U 12JAN19

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

FWD CARGO BAY FLOOR PNL 120CF HAS CORROSION AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120CF FROM .090 CONOLITE; LOT # 1369104-2 PER AMM 25-52-01-201-801 AND DWG 453A1610

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR PNL 140AF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140AF FROM .090 CONOLITE; LOT # 1369104-2 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,639 hrs · 33,796 cycles

RT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW NR 3. R&R BULB PER AMM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR PNL 140CF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .071 2024T3; LOT # 1371389-1 PER AMM 25-52-01-201-801 AND EA 1-A53-2446 REV 1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,639 hrs · 33,796 cycles

LT INBOARD OVERWING EMERGENCY EXIT LIGHT INBOARD UPPER LIGHTS INOP. R&R BULB PER MM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR PNL 140BF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140BF FROM .090 CONOLITE; LOT # 1369104-2 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,639 hrs · 33,796 cycles

R1 DOOR EMERGENCY EXIT LIGHT FORWARD LOWER LIGHT PACK INOP. R&R BATTERY PACK PER AMM.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

FWD CARGO BAY FLOOR PNL 120AF HAS CORROSION AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120AF FROM .090 CONOLITE; LOT # 1369104-2 PER AMM 25-52-01-201-801 AND DWG 453A1610

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

FWD CARGO BAY FLOOR PNL 120BF HAS CORROSION AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120BF FROM .071 2024T3; LOT # 1371389-1 PER AMM 25-52-01-201-801 AND EA 1-A53-2446 REV 1

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 50,639 hrs · 33,796 cycles

AFT CARGO BAY FLOOR PNL 140DF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140DF FROM .090 CONOLITE; LOT # 1369104-2 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: SKIN — CRACKED (LE SLAT) · airframe 50,639 hrs · 33,796 cycles

LT WING LEADING EDGE SLAT NOSE SKIN AT NR 1 SLAT ACTUATOR CRACKED AT FASTENER HOLE. REPAIRED NR 1 SLAT SKIN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 48,940 hrs · 32,719 cycles

FORWARD GALLEY LOWER EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: NONE — NONE · airframe 48,739 hrs · 32,588 cycles

VAPOR BARRIER IN R/H WHEEL WELL HAS A 15' LONG CRACK IN BAY 1R AT STA 663.75 AT APPROX. RBL 10.845 / APPLIED INTERIM REPAIR TO CRACK PER EA 1-757-15126 ON FWD SIDE OF VAPOR BARRIER

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 48,190 hrs · 32,241 cycles

RH W/W LOWER WEB IS CRACKED VERTICALLY APPROX. 10' LONG AT STA 663.75 AT RBL 10.845 / PERFORMED PERMANAANT REPAIR ON CRACK PORTION LOCATED IN VAPOR BARRIER BAY 2R SRM 51-70-04. REPAIR 10 SEE NRC# D294008 FOR REMAINDER OF CRACK LOCATED IN BAY 1R.

Part: RETAINER — CRACKED (LT WING) · airframe 48,190 hrs · 32,241 cycles

LEFT WING INBOARD FLAP OUTBOARD LEADING EDGE SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED LEFT WING INBOARD FLAP OUTBOARD LEADING EDGE SEAL RETAINER IAW SRM 51-40-02

Part: BEAM — CRACKED (R1 DOOR) · airframe 48,190 hrs · 32,241 cycles

R1 DOOR BEAM FORWARD INBOARD FASTENER CRACKED AT THE RADIUS. R & R THE DOOR IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 46,294 hrs · 31,044 cycles

EMERGENCY LIGHT BATTERY M1669 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 46,294 hrs · 31,044 cycles

EMERGENCY LIGHT BATTERY M1672 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 46,294 hrs · 31,044 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 45,230 hrs · 30,393 cycles

RIGHT OVERWING EMERGENCY EXIT SMALL SIGN COVER MISSING. REINSTALLED THE COVER IAW AMM.

Part: SIGN — WRONG PART (EMERGENCY LIGHT) · airframe 45,123 hrs · 30,337 cycles

R2 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROWS. R & R THE SIGN IAW AMM.

Part: SIGN — WRONG PART (EMERGENCY LIGHT) · airframe 45,123 hrs · 30,337 cycles

R1 DOOR EMERGENCY EXIT SIGN MISSING RED ARROW. R & R THE SIGN IAW AMM.

Part: COVER — DISCOLORED (EMERGENCY LIGHT) · airframe 45,123 hrs · 30,337 cycles

RIGHT EMERGENCY LIGHT COVER DISCOLORED. R & R THE COVER IAW AMM.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 45,123 hrs · 30,337 cycles

LEFT EMERGENCY LIGHT LENS DIRTY. R & R THE LENS IAW AMM.

Part: SIGN — WRONG PART (EMERGENCY LIGHT) · airframe 45,123 hrs · 30,337 cycles

L2 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROWS. R & R THE SIGN IAW AMM.

Part: SIGN — WRONG PART (EMERGENCY LIGHT) · airframe 45,123 hrs · 30,337 cycles

L1 DOOR EMERGENCY EXIT SIGN MISSING RED ARROW. R & R THE SIGN IAW AMM.

Part: LATCH — DIRTY (L1 DOOR) · airframe 44,177 hrs · 29,743 cycles

L1 DOOR EMERGENCY EVAC SLIDE LATCHES DIRTY. CLEANED LATCHES PER SIP.

Part: WIRE — BROKEN (CABIN) · airframe 44,177 hrs · 29,743 cycles

EMERGENCY EXIT LIGHT WIRE BROKEN AT BS 747, RBL 25. REPAIRED WIRE PER AMM.

Part: SUPPORT ANGLE — CRACKED (BS 727 BULKHEAD) · airframe 44,177 hrs · 29,743 cycles

BULKHEAD SUPPORT ANGLE CRACKED AT BS 727. R & R THE SUPPORT ANGLE IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 44,177 hrs · 29,743 cycles

LT HORIZONTAL STABILIZER VERT STIFFENER CRACKED AT STA 157.10, 3RD FROM FORWARD AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (BS 440) · airframe 44,177 hrs · 29,743 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

L1 DOOR CUTOUT LOWER CENTER THRESHOLD ZEE CHANNEL SUPPORT CORRODED AT LBL 63. R&R SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSEAGE) · airframe 44,177 hrs · 29,743 cycles

R1 DOOR LOWER SUPPORT ANGLE CORRODED AT WL 208, RBL 59. R & R THE SUPPORT ANGLE IAW SRM.

Part: FRAME — CRACKED (BS 500A) · airframe 44,177 hrs · 29,743 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 44,177 hrs · 29,743 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER EA.

Part: SUPPORT ANGLE — CRACKED (BS 726) · airframe 44,177 hrs · 29,743 cycles

RIGHT MAIN WHEEL WELL KEEL BEAM UPPER WEB SUPPORT ANGLE CRACKED AT BS 726, BETWEEN RBL 4.3 TO LBL 4.3. REPAIRED THE SUPPORT ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 44,177 hrs · 29,743 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294.5, RBL 1. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 44,177 hrs · 29,743 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

STUB BEAM CRACKED AT BS 295, WL 207. R&R STUB FRAME PER SRM AND AMM.

Part: HOOK — CORRODED (ESCAPE ROPE) · airframe 44,177 hrs · 29,743 cycles

LEFT OVERWING EMERGENCY EXIT ESCAPE ROPE HAS A CORRODED HOOK END. R & R HOOK END IAW MM.

Part: HOOK — CORRODED (ESCAPE ROPE) · airframe 44,177 hrs · 29,743 cycles

RIGHT OVERWING EMERGENCY EXIT ESCAPE ROPE HAS A CORRODED HOOK END. R & R HOOK END IAW MM.

Part: PLATE — CRACKED (RT WING) · airframe 44,177 hrs · 29,743 cycles

RT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED JUST INBOARD OF NR 2 PYLON AFT TIP. R&R WAFFLE PLATE IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 44,177 hrs · 29,743 cycles

THE LEFT WING LOWER TRAILING EDGE WAFFLE PLATE JUST INBOARD OF THE NR 1 PYLON AFT TIP CRACKED R & R THE PLATE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

SIDEWALL SUPPORT ANGLE CORRODED AT BS 500, BETWEEN STR 18L TO STR 26L. REPAIRED SUPPORT IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

CENTER AFT LOWER BULKHEAD PANEL SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 23 TO LBL 23. R&R ANGLE PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FORWARD CARGO BAY, CORRODED ON SHIELD CORRODED BETWEEN BS 430 TO BS 440, RBL 24. R&R SHIELD IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FORWARD CARGO BAY LOWER MAIN SILL SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 490, RBL 32. R&R WEB IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FUSELAGE SKIN COMMON TO BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STR 22L TO STR 23L. REPAIRED CHORD IAW EA & ER.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 44,177 hrs · 29,743 cycles

FUSELAGE SKIN COMMON TO BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STR 22R TO STR 23R. REPAIRED CHORD IAW ER AND EA.