N767SW

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 78,959 hrs · 46,849 cycles

EXTERNAL EMERGENCY LIGHT OUT JUST AFT OF L1 DOOR.<[01] R&R LIGHT BULB. OPS CHECK NORMAL. AMM 33-51-04.

Part: PANEL — CRACKED (ZN 300 STABILIZE) · airframe 78,354 hrs · 46,458 cycles

LEFT ELEVATOR HAS CRACKED FILLET FAIRING AT INBOARD FORWARD HINGE PANEL.<[01] REMOVED AND INSTALLED L/H ELEVATOR LOWER INBD FWD FILLET FAIRING PER SRM 51-40-02;[02] REPAIRED PANEL AS REQ. PER SRM 55-20-01-2R-4. NO CHANGE TO WT AND BALLANCE; WEIGHED PANEL BEFORE AND AFTER REPAIR NO WT CHANGE.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 77,799 hrs · 46,089 cycles

FWD ENTRY GIRT BAR LOOSE IN DISARM POSITION<[01] ADJUSTED FWD ENTRY GIRT BAR LOCKS IAW AMM 52-11-00

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 77,375 hrs · 45,813 cycles

LIGHTED LOWER EXIT SIGN COVER MISSING AT PILOT SIDE EXIT ROW<[01] INSTALLED EXIT COVER IAW 33-51-01

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 76,539 hrs · 45,300 cycles

R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK / [01] REMOVED AND REPLACED R/H AFT EMERGENCY LIGHTING BATTERY PACK PER M/M 33-51-06.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 76,539 hrs · 45,300 cycles

L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK / [01] REMOVED AND REPLACED L/H FWD EMERGENCY LIGHTING BATTERY PACK PER M/M 33-51-06.

Part: SLIDE — OUT OF POSITION (CABIN) · airframe 76,419 hrs · 45,218 cycles

FWD ENTRY DOOR ESCAPE SLIDE APPEARS TO BE PROTRUDING EXCESSIVELY (AT THE BOTTOM) FROM IT'S COVER. PERFORMED ESCAPE SLIDE PACK CHECK PER A.M.M. 25-66-01. NO DEFECTS NOTED.

Part: SENSOR — FAULTY (R/H WING) · airframe 76,050 hrs · 44,993 cycles

ON APPROACH; SELECTING FLAPS 30; LE FLAPS TRANSIT ANNUCIATOR REMAINED ILLUMINATED. ONLY ABNORMAL INDICATION IS LE SLAT NO. 8 HAS NO INDICATION. / [01] R&R #8 LE SLAT INBOARD PROX SENSOR REF 737 AMM 27-88-11 OPS CK GOOD

Part: LIGHT — BROKEN (PAX CABIN) · airframe 74,891 hrs · 44,251 cycles

EXIT SIGN LEFT SIDE MID CABIN DETACHED / [01] SECURED LENSE IAW AMM 33-51-01

Part: ENGINE — FAULTY (R/H WING) · airframe 74,459 hrs · 43,992 cycles

#2 ENG REPORTS OF SPARKS/FLAMES ON T/O. NO FIRE INDICATIONS. SUSPECTED COMPRESSOR STALL. WINDS 70 DEGREES OFF 20 KNOTS GUSTY. NO EGT SPIKE OR OVERHEAT. NO ABNORMAL ENGINE PARAMETERS OR INDICATIONS SEEN. / [01] PERFORMED BOROSCOPE INSPECTION PER MT 71-05-811 NO DEFECTS NOTED;[02] PERFORMED BOROSCOPE INSPECTION PER FIM 71-05 TASK 811 NO DEFECTS NOTED;[03] PERFORMED BORESCOPE INSPECTION PER FIM 71-05 TASK 811. NO DEFECTS NOTED;[04] PERFORMED BOROSCOPE INSPECTION PER FIM 71-05 TASK 811 NO DEFECTS NOTED;[05] PERFORMED BOROSCOPE INSPECTION PER FIM 71-05 TASK 811 NO DEFECTS NOTED LEAK CHECK GOOD

Part: WEB — CRACKED (AFT CARGO) · airframe 74,357 hrs · 43,930 cycles

CRACK ON LOWER SILL LOCATED BS 792 TO BS 847 AT LEVEL S-25R AFT CARGO COMPARTMENT 2022-95123 / [01] REPLACED LOWER SILL WEB AND FASTENERS LOCATED BS 792 TO BS 847 AT LEVEL S-25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING 146A8340 REV:A.;[02] CORRECTED STEP 1. REPLACED LOWER SILL WEB AND FASTENERS LOCATED BS 792 TO BS 847 AT LEVEL S-25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING 146A8340 REV:A. SEE INDIVIDUAL SIGNS OFF BELOW.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — CRACKED (R.H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK TRAILING EDGE HOLES ACCESS PANEL 661CB AT RT WING 2022-95082. / [01] TOOL USED: CALIPER P/N: 500-752-20; S/N:B16101362; DUE DATE: 05-NOV-22.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B S/N:15102320 DUE DATE:16-JAN-23;[03] TOOL USED: SCALE P/N:CL5000 S/N:AE-408751 DUE DATE:19-MAR-22.;[04] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18185781 DUE DATE:16-JAN-23;[05] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[06] REPAIRED ACCESS PANEL 661CB AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED.

Part: BRACKET — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK SUPPORT BRACKET LOCATED TRAILING EDGE AT ORSS278 AT LT WING 2022-95034 / [01] REPLACED SUPPORT BRACKET AND FASTENERS LOCATED TRAILING EDGE AT ORSS278 AT LT WING IAW B737-700 SRM 51-40-02.;[02] TASK CARD COMPLETED

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK TRAILING EDGE HOLES ACCESS PANEL 561AB AT LT WING 2022-95075. / [01] TOOL USED: CALIPER P/N: 500-752-20; S/N:B16101362; DUE DATE: 05-NOV-22.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B S/N:15102320 DUE DATE:16-JAN-23;[03] TOOL USED: SCALE P/N:CL5000 S/N:AE-408751 DUE DATE:19-MAR-22.;[04] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18185781 DUE DATE:16-JAN-23;[05] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22.;[06] REPAIRED ACCESS PANEL 561AB AT LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED.

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,357 hrs · 43,930 cycles

CRACK LEADING EDGE RIB STA 105.26 AT LT HORIZONTAL STABILIZER 2022-95022 / [01] REPLACED RIB LOC STA 105.26 AT LT HORIZONTAL STABILIZER AND FASTENERS I.A.W SRM B737-700 51-40-02 AND DRAWING #186A1001 REV:A;[02] CORRECTED STEP 1.REPLACED RIB LOC STA 105.26 AT LT HORIZONTAL STABILIZER AND FASTENERS I.A.W SRM B737-700 51-40-02 AND DRAWING #186A1001 REV:A; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS261 LT WING 2022-95033 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS261 LT WING SRM B737-700 51-40-02 AND 51-10-02 ITEM 9;[02] JOB CERTIFIED

Part: ANGLE — CRACKED (VERT. STAB.) · airframe 74,357 hrs · 43,930 cycles

CRACK BRACKET ANGLE LOCATED AT BS 1016 UPPER FUSELAGE AT LEVEL S-2R AND S-2L AT VERTICAL STABILIZER 2022-95043 / [01] REPLACED BRACKET ANGLE AND FASTENERS LOCATED AT BS 1016 UPPER FUSELAGE AT LEVEL S-2R AND S-2L AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DRAWING 176A3101 REV -: SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED BRACKET ANGLE AND FASTENERS LOCATED AT BS 1016 UPPER FUSELAGE AT LEVEL S-2R AND S-2L AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DRAWING 176A3101 REV; RII SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK TRAILING EDGE HOLES ACCESS PANEL 661BB AT RT WING 2022-95080. / [01] TOOL USED: CALIPER P/N: 500-752-20; S/N:B16101362; DUE DATE: 05-NOV-22.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B S/N:15102320 DUE DATE:16-JAN-23;[03] TOOL USED: SCALE P/N:CL5000 S/N:AE-408751 DUE DATE:19-MAR-22.;[04] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18185781 DUE DATE:16-JAN-23;[05] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[06] REPAIRED ACCESS PANEL 661BB AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED.

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,357 hrs · 43,930 cycles

CRACK LEADING EDGE RIB STA 95.96 AT LT HORIZONTAL STABILIZER 2022-95021 / [01] REPLACED RIB LOC ON STA 95.96 AT LT HORIZONTAL STABILIZER AND FASTENERS. I.A.W SRM B737-700 51-40-02 AND DRAWING# 186A1001 REV :A ; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532FB AT LT WING 2022-95016 / [01] REPLACED FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532FB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11;[02] TASK COMPLETED

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,357 hrs · 43,930 cycles

CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2022-94942 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503 DUE DATE: 05-MAR-22<BR><BR>TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45MG S/N: 130061901 DUE DATE: 11-MAY-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED STRINGER 23R LOCATED BETWEEN BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1; SEE INDIVIDUAL SIGNOFFS BELOW.;[04] JOB CERTIFIED AS RII.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,357 hrs · 43,930 cycles

CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT 2022-94943 / [01] TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45MG S/N: 130061901 DUE DATE: 11-MAY-22;[02] ET TOOL USED PN: MIZ-21C; SN:769680; DUE DATE: 26-FEB-22;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[04] REPAIRED STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRN 53-00-03-2R-1 REPAIR 1 TABLE 101 AND DWG 143A3230 REV: - <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[05] REPAIRED STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRN 53-00-03-2R-1 REPAIR 1 TABLE 101 AND DWG 143A3230 REV: - <BR>SEE INDIVIDUAL SIGNOFFS BELOW.. RII ITEM;[06] CORRECTED REFERENCE

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,357 hrs · 43,930 cycles

CRACK STRINGER 23L AT BS 540 FWD CARGO COMPARTMENT 2022-94944 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503 DUE DATE: 05-MAR-22<BR><BR>TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45MG S/N: 130061901 DUE DATE: 11-MAY-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] PERFORMED PERMANENT REPAIR ON STRINGER 23L LOC. BTW BS500D TO BS 540 . I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3210 REV ?C?. SEE INDIVIDUAL SIGN OFF BELLOW.;[04] PERFORMED PERMANENT REPAIR ON STRINGER 23L LOC. BTW BS500D TO BS 540 . I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3210 REV ?C?. SEE INDIVIDUAL SIGN OFF BELLOW... RII ITEM

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,357 hrs · 43,930 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 500D AND BS 520 AT LEVEL S-28 R FWD CARGO COMPARTMENT 2022-94948 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOC. BETWEEN BS 500D AND BS 520 AT LEVEL STR 28R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV ?A? .;[03] REPLACED WEB-INTERCOSTAL AND FASTENERS LOC. BETWEEN BS 500D AND BS 520 AT LEVEL STR 28R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV ?A? ... RII ITEM

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,354 hrs · 43,929 cycles

CUSTOMER REQUEST-CRACK ON STRINGER 7L LOC BS 294.5 PASSENGER CABIN 2022-94941 / [01] CORRECTED STEP 1.REMOVED FITTING 1EA; ANGLE 1EA; STRAP 1EA AND FASTENERS LOCATED BTW BS 294.5 AND 303.9 AT LEVEL OF STR 7L PASSENGER CABIN. IAW SRM B737-700 51-40-02-0G-0. AND PERFORMED VISUAL INSPECTION ON REMOVED PARTS AND ADJACENT AREA AND NO FOUND MORE DAMAGE.;[02] STEP 1 ENTRY BY ERROR.;[03] TOOL USED: P/N: 45MG; S/N: 130060401; DUE DATE: 22-APR-22;[04] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 210138203; DUE DATE: 05-MAR-22;[05] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[06] PERFORMED PERMANENT ON STRINGER 7L LOC BTW BS 277 TO BS 294.5 I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[07] CORRECTED STEP 6. PERFORMED REPAIR ON STRINGER 7L LOC BTW BS 277 TO BS 294.5 I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[08] PERFORMED REPAIR CAT B ON STRINGER 7L LOC BTW BS 277 TO BS 294.5 I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: ANGLE — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX FORWARD BOOST PUMP AREA AT LT WING 2022-94919 / [01] CALIPER PN: 500-197-30; SN: B20189362; DUE DATE: 03-DEC-22.;[02] TOOL USED: POWER PACK P/N FMK0007096 S/N PE0414/70786 DUE DATE: 23-FEB-22. MULTIMETER P/N FLUKE-37 S/N 5335022 DUE DATE: 04-DEC-22. THERMOMETER P/N FLUKE 66 S/N AE-27240 DUE DATE: 24-MAR-22;[03] MACHINED SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX FORWARD BOOST PUMP AREA AT LT WING IAW B737-700 DWG 116A3939 REV B. SEE INDIVIDUAL SINGOFFS BELOW.;[04] CORRECTED STEP 3; MACHINED SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX FORWARD BOOST PUMP AREA AT LT WING IAW B737-700 DWG 116A3939 REV B. AND B737-700 SRM 57-20-10-0I-1 IDENTIFICATION 1. SEE INDIVIDUAL SINGOFFS BELOW.;[05] MACHINED SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX FORWARD BOOST PUMP AREA AT LT WING IAW B737-700 DWG 116A3939 REV B. AND B737-700 SRM 57-20-10-0I-1 IDENTIFICATION 1. SEE INDIVIDUAL SINGOFFS BELOW... RII ITEM;[06] INSTALLED ANGLE MUST BE COMPLETED ON TTG8Q00AU2EX.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[07] INSTALLED ANGLE MUST BE COMPLETED ON TTG8Q00AU2EX.SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 74,357 hrs · 43,930 cycles

CRACK LEADING EDGE RIB STA 95.96 RT HORIZONTAL STAB 2022-95018 / [01] REPLACED RIB STA 95.96 RT HORIZONTAL STAB LEADING EDGE IAW B737-700 SRM 51-40-02 AND DRAWING 186A1303 REV -: SEE INDIVIDUAL SINGOFFS BELOW.;[02] REPLACED RIB STA 95.96 RT HORIZONTAL STAB LEADING EDGE IAW B737-700 SRM 51-40-02 AND DRAWING 186A1303 REV -: SEE INDIVIDUAL SINGOFFS BELOW<BR>TASK COMPLETED

Part: ACCESS PANEL — BROKEN (L/H WING) · airframe 74,357 hrs · 43,930 cycles

BROKEN FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532NB AT LT WING 2022-95014 / [01] REPLACED FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532NB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11;[02] TASK COMPLETED

Part: ACCESS PANEL — BROKEN (L/H WING) · airframe 74,357 hrs · 43,930 cycles

BROKEN FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532QB AT LT WING 2022-95011 / [01] REPLACED FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532QB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11;[02] TASK COMPLETED

Part: BRACKET — CRACKED (R/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK ON SUPPORT BRACKET LOCATED ON REAR SPAR BTW WS 156.25 TO WS 331.00 LOWER SECTION ON RH WING 2022-94940 / [01] REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON REAR SPAR BTW WS 156.25 TO WS 331.00 LOWER SECTION ON RH WING IAW B737-700 SRM 51-40-02.;[02] TASK CARD COMPLETED

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532JB AT LT WING 2022-95015 / [01] REPLACED FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532JB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11 STEP 2.B.(1) PAG 302 AND STEP 2.B.(5) PAG 702. THE LEAK CHECK OF ACCESS PANEL 532JB WILL BE ACCOMPLISHED WITH TTG8Q0095N9Q. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED FUEL QUANTITY INDICATOR (FLOAT) ACCESS PANEL 532JB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11 STEP 2.B.(1) PAG 302 AND STEP 2.B.(5) PAG 702. THE LEAK CHECK OF ACCESS PANEL 532JB WILL BE ACCOMPLISHED WITH TTG8Q0095N9Q. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — ELONGATED (RH WING) · airframe 74,357 hrs · 43,930 cycles

ELONGATED HOLE ON SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX. FORWARD BOOST PUMP AREA AT RT WING 2022-95017 / [01] CALIPER PN: 500-197-30; SN: B20189362; DUE DATE: 03-DEC-22.;[02] POWER PACK P/N: FMK0007096; S/N: PE0414/70786 DUE DATE: 23-FEB-22. THERMOMETER P/N: FLUKE 37; S/N: 5335022 DUE DATE: 04-DEC-22. THERMOMETER P/N: FLUKE 66; S/N: AE-27240 DUE DATE: 24-MAR-22.;[03] MACHINED SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX. FORWARD BOOST PUMP AREA AT RT WING IAW B737-700 DWG 116A3939 REV B AND SRM 57-20-10-0I-1 IDENTIFICATION 1. SEE INDIVIDUAL SING-OFF BELOW.;[04] MACHINED SUPPORT ANGLE LOCATED FRONT SPAR IFSS 121 APPROX. FORWARD BOOST PUMP AREA AT RT WING IAW B737-700 DWG 116A3939 REV B AND SRM 57-20-10-0I-1 IDENTIFICATION 1. SEE INDIVIDUAL SING-OFF BELOW... RII ITEM

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,357 hrs · 43,930 cycles

CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT 2022-94946 / [01] TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45MG S/N: 130061901 DUE DATE: 11-MAY-22;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[04] REPAIRED STRINGER 26L BS 540 FWD CARGO I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[05] REPAIRED STRINGER 26L BS 540 FWD CARGO I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL STEP SIGN OFFS BELOW.. RII ITEM

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 74,357 hrs · 43,930 cycles

CRACK LEADING EDGE RIB STA 114.55 RT HORIZONTAL STAB 2022-95020 / [01] REPLACED RIB AND FASTENERS LOC STA 114.55 RT HORIZONTAL STAB I.A.W SRM B737-700 51-40-02 AND DRAWING# 186A1001 REV:A; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,357 hrs · 43,930 cycles

CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT 2022-94945 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503 DUE DATE: 05-MAR-22<BR><BR>TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45MG S/N: 130061901 DUE DATE: 11-MAY-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED STRINGER 25L LOC BTW BS520 I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] REPAIRED STRINGER 25L LOC BTW BS520 I.A.W SRM B737-700 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL STEP SIGN OFFS BELOW.. RII ITEM

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 74,357 hrs · 43,930 cycles

CRACK LEADING EDGE RIB STA 105.26 RT HORIZONTAL STAB 2022-95019 / [01] INSTALLED NEW RIB AND FASTENER LOC. LEADING EDGE STA 105.26 RT HORIZONTAL STAB I.A.W SRM B737-700 51-40-02 AND DRAWING 3 186A1001 REV:A. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] CORRECTED STEP 1. REPLACED NEW RIB AND FASTENER LOC. LEADING EDGE STA 105.26 RT HORIZONTAL STAB I.A.W SRM B737-700 51-40-02 AND DRAWING 3 186A1001 REV:A. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] ORRECTED STEP 2. REPLACED RIB AND FASTENER LOC. LEADING EDGE STA 105.26 RT HORIZONTAL STAB I.A.W SRM B737-700 51-40-02 AND DRAWING # 186A1001 REV:A. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (FWD CARGO) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE BS 500D AND S-28L FWD CARGO COMPARTMENT 2022-94947 / [01] REPLACED ANGLE AND FASTENERS LOC. AT BS 500D AND S-28L FWD CARGO COMPARTMENT. I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV ?A? .;[02] REPLACED ANGLE AND FASTENERS LOC. AT BS 500D AND S-28L FWD CARGO COMPARTMENT. I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV ?A? ... RII ITEM

Part: ANGLE — CRACKED (L/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 LT WING 2022-94826 / [01] REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 LT WING IAW. 737-700 SRM 51-40-02 AND DRAWING 115A2930. SEE INDIVIDUAL SINGOFFS BELOW.;[02] REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 LT WING IAW. 737-700 SRM 51-40-02 AND DRAWING 115A2930. SEE INDIVIDUAL SINGOFFS BELOW.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE LOCATED BS695 AND BL0 TO LBL1 AT CENTER WING BOX 2022-94818 / [01] REPLACED ANGLE LOCATED BS695 AND BL0 TO LBL1 AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 273A9110 REV:A; SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED ANGLE LOCATED BS695 AND BL0 TO LBL1 AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 273A9110 REV:A; SEE INDIVIDUAL SIGNOFFS BELOW. RII

Part: STRAP — CORRODED (AFT CARGO) · airframe 74,357 hrs · 43,930 cycles

CORROSION ON STRAP AFT CARGO COMPARTMENT FLOOR AREA LOCATED BTW STA 787 TO STA 794.3 SIDE RH. 2022-94911 / [01] REPLACED STRAP AFT CARGO COMP FLOOR AREA BTW STA 787 TO STA 94.3 RH SIDE I.A.W SRM B737-700 51-40-02;[02] TASK COMPLETED ; RII

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE LOCATED BS695 AND BL0 TO RBL1 AT CENTER WING BOX 2022-94819 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; SN: 142811019; DUE DATE: 02-FRB-23;;[02] REPLACED ANGLE LOCATED BS695 AND BL0 TO RBL1 AT CENTER WING BOX IAW SRM B737-700 51-40-02 Ï¿½TEM 9 AND DRAWING 273A9110; SHEET 5; REV: A; SEE INDIVIDUAL SIGNOFFS BELOW.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE LOCATED BS695 AT RBL24.5 AND WL208.1 LOWER POSITION AT CENTER WING BOX 2022-94821 / [01] REPLACED ANGLE LOCATED BS695 AT RBL24.5 AND WL208.1 LOWER POSITION AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 111A6000 REV: A. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED ANGLE LOCATED BS695 AT RBL24.5 AND WL208.1 LOWER POSITION AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 111A6000 REV: A. SEE INDIVIDUAL SIGNOFFS BELOW. RII

Part: ANGLE — CRACKED (R/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 AFT POSITION RT WING 2022-94829 / [01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING #115A29 30 REV;-; SEE INDIVIDUAL STEP SING OFFS BELOW;[02] CORRECTIVE STEP 1 REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 AFT POSITION RT WING I.A.W SRM B737-700 51-40-02 AND DRAWING #115A29 30 REV;-; SEE INDIVIDUAL STEP SING OFFS BELOW;[03] REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 AFT POSITION RT WING I.A.W SRM B737-700 51-40-02 AND DRAWING #115A29 30 REV;-; SEE INDIVIDUAL STEP SING OFFS BELOW

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 74,357 hrs · 43,930 cycles

CRACK SUPPORT BRACKET ASSY LOCATED BS540 AND BL0 TO LBL24.5 AT CENTER WING BOX 2022-94815 / [01] REPLACED SUPPORT BRACKET ASSY LOCATED BS540 AND BL0 TO LBL24.5 AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 143A0060 REV:B SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: STUB FRAME — CRACKED (FWD GALLEY) · airframe 74,357 hrs · 43,930 cycles

CRACK ON STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R FWD GALLEY AREA 2022-94790 / [01] REPLACED STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R FWD GALLEY AREA IAW B-737-700 SRM 51-40-02 AND DWG#141A8370 REV-D. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] REPLACED STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R FWD GALLEY AREA IAW B-737-700 SRM 51-40-02 AND DWG#141A8370 REV-D. SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR><BR>RII ACCOMPLISHED

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 74,357 hrs · 43,930 cycles

CRACK SUPPORT BRACKET ASSY LOCATED BS540 AND BL0 TO RBL24.5 AT CENTER WING BOX 2022-94816 / [01] REPLACED SUPPORT BRACKET ASSY LOCATED BS540 AND BL0 TO RBL24.5 AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 143A0060 REV:B; SEE INDIVIDUAL BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE LOCATED BS695 AT RBL24.5 AND WL208.1 UPPER POSITION AT CENTER WING BOX 2022-94820 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-SEP-23.;[02] REPLACED ANGLE LOCATED BS695 AT RBL24.5 AND WL208.1 UPPER POSITION AT CENTER WING BOX IAW SRM B737-700 51-10-02 Ï¿½TEM 9 AND DRAWING 273A9110; SHEET 5; REV: A; SEE INDIVIDUAL SIGNOFFS BELOW.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (R/H WING) · airframe 74,357 hrs · 43,930 cycles

CRACK ANGLE TRAILING EDGE LOCATED BETWEEN WS253 TO WS278 FORWARD POSITION RT WING 2022-94828 / [01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING #115A29 30 REV;-; SEE INDIVIDUAL STEP SING OFFS BELOW;[02] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING #115A29 30 REV;-; SEE INDIVIDUAL STEP SING OFFS BELOW

Part: BEAR STRAP — CRACKED (FWD FUSELAGE) · airframe 74,357 hrs · 43,930 cycles

CRACK INDICATION ON FWD SERVICE DOOR BEAR STRAP BETWEEN BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R AT PASSENGER CABIN 2022-94771 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 500D; S/N: N500X12101V022237; DUE DATE: 06-OCT-22;[02] EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[03] REPAIRED BEAR STRAP AREA OF FWD SERVICE DOOR; FUSELAGE SKIN BTW BS 277+8 INCH AND BS 312+4 INCH AND BTW STR 6R TO STR 11R IAW SRM B737-700 53-10-01-2R-6 AND EA 22-153-00577.;[04] CORRECTED STEP 3.REPAIRED BEAR STRAP AREA OF FWD SERVICE DOOR; FUSELAGE SKIN BTW BS 277+8 INCH AND BS 312+4 INCH AND BTW STR 6R TO STR 11R IAW SRM B737-700 53-10-01-2R-6 REPAIR 6 AND EA 22-153-00577.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[05] VERIFIED TASK COMPLETE. TASK RII.

Part: MEGAPHONE — FAULTY (CABIN) · airframe 73,903 hrs · 43,658 cycles

SUPPLEMENTAL INFORMATION: FWD GALLEY MEGAPHONE INTERMITTENT ; / [01] R&R FWD GALLEY MEGAPHONE PER AMM REF 25-94-00

Part: LIGHT — INOPERATIVE · airframe 73,610 hrs · 43,475 cycles

PAX CABIN R AFT EMER CHGR (LIGHT) CB WAS OUT ON PREFLIGHT; RESET ONCE & POPPED OUT AGAIN. ; / [01] R & RD EMERGENCY LIGHTING CHARGING ASSY M1669 & M1674 PER MM 33-51-06

Part: FAIRING — DAMAGED (WNG-BDY) · airframe 73,117 hrs · 43,159 cycles

WING TO BODY FAIRING PANEL 193B FASTENER HOLES ENLARGED AT LOCATIONS 1 - 36 AND 38 / [01] C/W REMOVED AND REPLACED PANEL 193B REF SRM 51-40-02; [02] REMOVED AND REPLACED PNL 193B REF SRM 51-40-02; [03] C/W

Part: HANDLE — BROKEN (MEGAPHONE) · airframe 72,699 hrs · 42,925 cycles

FWD MEGAPHONE BROKEN HANDLE ; / [01] R AND R FWD MEGAPHONE PER AMM 25-64-00.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 72,591 hrs · 42,857 cycles

EXTERIOR EMERGENCY LIGHT AFT OF L4 DOOR INOP ; / [01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF L4 DOOR REF. AMM 33-51-04 OPS CHECKS NORMAL

Part: FLASHLIGHT — OUT OF POSITION (FWD CABIN) · airframe 71,411 hrs · 42,169 cycles

FLIGHT ATTENDANTS REPORT A FOREIGN OBJECT ROLLING IN CEILING ABOVE FLIGHT ATT. FORWARD JUMPSEAT WHEN AIRCRAFT ROLLS. LOUD SOUND. POSSIBLY LARGE OBJECT. / REMOVED FLASH LIGHT FROM CEILING AREA ABOVE FORWARD ENTRY AREA. REFERENCE AMM 25-21-45. AIRCRAFT OK FOR SERVICE

Part: BALANCE WEIGHT — CORRODED (TAIL) · airframe 71,402 hrs · 42,162 cycles

RUDDER BALANCE WEIGHT HAS EVIDENCE OF CORROSION. / REMOVED AND REPLACED PER CMM 55-40-09.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 71,402 hrs · 42,162 cycles

LEFT HORIZONTAL FWD LOWER SLIDER SEAL HAS A CRACK AT UPPER AFT EDGE. / REMOVED AND REPLACED LEFT FWD LOWER SLIDER SEAL IAW AMM 53-31-31.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,728 hrs · 41,764 cycles

FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW. REPLACED LIGHT LENS COVER, REF AMM 33-51-01. OPERATIONS GOOD.

Part: FITTING — BROKEN (R1 ASSIST HANDL) · airframe 70,295 hrs · 41,483 cycles

FWD SERVICE DOOR ASSIST HANDLE BROKEN / R&R ASSIST HANDLE FITTING REF MM CH 52-11-00

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 69,753 hrs · 41,135 cycles

AFT LAV SMOKE DETECTOR ACTIVATED / RESET AFT LAV SMOKE DETECTOR OPS CHECK OK PER AMM 26-14-00

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 69,382 hrs · 40,900 cycles

AFT WING TO BODY FUSELAGE SIDE EMERGENCY LIGHT INOPERATIVE. / FOUND LOOSE GROUND. RECONNECTED AND TIED GROUND IAW WDM AND AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,382 hrs · 40,900 cycles

EMERGENCY LIGHTS INOP FROM ROW 6 LH TO 11 LH. / REMOVED AND REPLACED BATTERY POWER SUPPLY ON M1668 AND M1670 AS PER B737 AMM 33-51-06-960-806 TEST OK.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,382 hrs · 40,900 cycles

R2 DOOR SLIDE GIRT EXTENDED OUT TOO FAR AND RUBBING ON DOOR CUTOUT. / REPOSITIONED SLIDE PER MT & AMM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 69,382 hrs · 40,900 cycles

INTERNAL CABIN L/H WING EMERGENCY EXIT UPPER LIGHT COVER LOOSE. / SECURED COVER PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 69,382 hrs · 40,900 cycles

AFT CARGO DOOR LOWER SILL FWD SCUFF PLATE FOUND CRACKED / RECEIVED WELDED SCUFF PLATE BY OUTSIDE VENDOR W/O 412612 ; SCUFF PLATE WILL BE INSTALL ON CUSTOMER CARD J753-140-00-02Y

Part: SCUFF PLATE — CRACKED (CABIN) · airframe 69,382 hrs · 40,900 cycles

R1 DOOR SCUFF PLATE HAS 2 EACH CRACKS AT BEND RADIUS. / RECEIVED NEW SCUFF PLATE FOR R1 DOOR; SCUFF PLATE WILL BE INSTALLED ON WORK CARD #J725-025-00-01Y 2015609 2000/0002.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,382 hrs · 40,900 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 10 STIFFENER 1 HAD A CRACK. REPAIRED STIFFENER NR 1 IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,382 hrs · 40,900 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 STIFFENER 2 HAD A CRACK. REPAIRED STIFFENER NR 2 IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,382 hrs · 40,900 cycles

RIGHT HORIZONTAL STABILIZER INSPAR STIFFENER RIB #4 P/N 182A2405-14 CRACK NOTED / RECEIVED NEW STIFFENER LOCATED AND DRILLED. APPLIED TREAT AND PRIME AND INSTALLED AT R/H HORIZ STABILIZER RIB #4 AS PER REF B737-700 SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 AND AMM 51-21-72-370-804

Part: BRACKET — CORRODED (R2 DOOR SLIDE) · airframe 69,382 hrs · 40,900 cycles

*** CORROSION *** R-2 DOOR AFT SLIDE BRAKET PLATE HAS CORROSION. / RECEIVED NEW R-2 DOOR BRACKET PLATE IN SERVICEABLE CONDITION. INSTALLATION WILL BE ACCOMPLISH ON T/C 725-025-00-02Y

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 69,382 hrs · 40,900 cycles

HORIZ STAB CENTER BOX REAR SPAR RIGHT UPPER CLEVIS FITTING FWD LUG HAS FRETTING AT BUSHING FACE. / REMOVED AND REPLACED R HORIZONTAL CENTER BOX REAR RIGHT UPPER FITTING FWD LUG BUSHING AS PER RES-WI2015612-4 AND EA-1-755-4629

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 69,382 hrs · 40,900 cycles

CUSTOMER REQUEST - RT HORIZ STAB REAR SPAR UPPER TERMINAL FITTING HAS FRETTING AT BUSHING FACE. / REMOVED AND REPLACED RT HORIZONTAL STAB REAR SPAR UPPER TERMINAL LUG AFT FLANGE BUSHING AS PER RES-WI2015612-4 AND EA 1-7554629

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 69,382 hrs · 40,900 cycles

CUSTOMER REQUEST - HORIZ STAB CENTER BOX RIGHT REAR SPAR UPPER CLEVIS FITTING AFT LUG HAS FRETTING AT BUSHING FACE. / REMOVED AND REPLACED R HORIZONTAL STAB CENTER BOX REAR SPAR UPPER CLEVIS FITTING AFT LUG BUSHING AS PER RES-WI2015612-4IR AND EA-1-755-4629 REV IR

Part: SHIELD — CRACKED (HORIZONTAL STAB) · airframe 69,382 hrs · 40,900 cycles

HORIZONTAL STAB FWD CONTROL STABILIZER TRIM MECHANISM DRIP SHIELD CRACKED. MARKED 29-47 / RECEIVED NEW DRIP SHIELD. REPLACED ON THE RACK

Part: ATTACH BRACKET — BROKEN (BS 727) · airframe 69,382 hrs · 40,900 cycles

AFT CARGO COMPT STA 727 BULK HEAD BRACKET ATTACH ANGEL BROKEN LOWER CENTER LINE / REMOVED DAMAGE BRACKET AND INSTALLED NEW BRACKET AT BULKHEAD STA 727 IN REF B737 SRM 51-40-02-0G-0 AND DWG 144A9401.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,382 hrs · 40,900 cycles

FORWARD CARGO COMPARTMENT Z-CHANNEL CORRODED BETWEEN BS 500 TO BS 500A, STR 25R. R&R Z CHANNEL PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,382 hrs · 40,900 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 18R. / R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,382 hrs · 40,900 cycles

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

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,382 hrs · 40,900 cycles

R1 DOOR LOWER BEAM NR 4 CRACKED AT FILLET REGION OPPOSITE MOST INBOARD HOLE. R&R LOWER BEAM NR 4 IAW DWG.

Part: SUPPORT ANGLE — CRACKED (R/H MLG W/W) · airframe 69,382 hrs · 40,900 cycles

RIGHT WHEEL WELL; SUPPORT ANGLE APPEARS TO BE CRACK AT RLB 9' WL 172; MARKED 29-39 / ACCOMPLISHED INSTALLATION NEW REPAIR ANGLE STA 663 RIGHT WHEEL WELL RBL 9' WL 172 ; AS PER B737-700 SRM 57-10-10-2R-5

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,382 hrs · 40,900 cycles

LT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 STAB STA 120.30 STIFFENER 3 HAD A CRACK. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,382 hrs · 40,900 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 STAB STA 120.30 STIFFENER 3 HAD A CRACK. REPAIRED RIB ASSEMBLY IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,382 hrs · 40,900 cycles

LT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 3 STAB STA 111.10 STIFFENER 3 HAD A CRACK. INSTALLED STIFFENER IAW SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,382 hrs · 40,900 cycles

RT VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 67,540 hrs · 39,707 cycles

L1 DOOR EXIT SIGN COVER MISSING FROM MOUNT. R&R LIGHT ASSEMBLY IAW AMM.

Part: SUPPORT BEAM — CRACKED (RHMLG) · airframe 67,376 hrs · 39,600 cycles

R/H MLG UPPER INBD PANEL SUPPORT BEAM FWD ATTACH BRACKET CRACKED (PANEL 651AT) / REMOVED & REPLACED FWD ATTACHMENT BRACKET ON R\H MLG UPPER I\B PANEL SUPPORT BEAM REF SRM 51-40-*01

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 67,376 hrs · 39,600 cycles

R\H MLG FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 67,376 hrs · 39,600 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD CORRODED. REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 67,376 hrs · 39,600 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,376 hrs · 39,600 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD BORE CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD CORRODED. / REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 67,376 hrs · 39,600 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD CORRODED. / REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 67,376 hrs · 39,600 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 67,376 hrs · 39,600 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 66,533 hrs · 39,060 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO CENTER SCUFF PLATE DENTED AND CRACKED AT CARGO DOOR LOWER STOP CONTACT POINTS / REMOVED AND REPLACED CTR SCUFF PLATE PER SRM 51-40- 02. AND AMM 53-11-02

Part: FAIRING — DELAMINATED (L/H FUSELAGE) · airframe 66,320 hrs · 38,927 cycles

LEFT SIDE WING TO BODY FAIRING PANEL 193AL DELAMINATED AT LEADING EDGE OF PANEL. / REMOVED AND REPLACED LEFT SIDE WING TO BODY FAIRING PANEL 193AL PER AMM 53-51-21.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,320 hrs · 38,927 cycles

ONE BATTERY PACK FAILED EMERGENCY LIGHT CAPACITY CHECK AT POSITION M01668. R&R BATTERY PACK PER AMM AND DWG.

Part: BRACKET — CRACKED (L/H WING) · airframe 66,320 hrs · 38,927 cycles

LEFT WING UPPER I/B FIXED TRAILING EDGE PANEL AFT SEAL BRACKET CRACKED / REMOVED AND REPLACED LEFT WING UPPER I/B FIXED TRAILING EDGE PANEL AFT SEAL PER AMM 20-50-11 AND SRM 51-40-02

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 66,320 hrs · 38,927 cycles

FLOOR PANEL SUPPORT CRACKED 2' @ BS540 BL 20 RIGHT / REMOVED AND REPLACED FLOOR PANEL SUPPORT @ BS540 BL 20 RIGHT IAW SRM 51-40-02 AND AMM 53-21-00

Part: LENS — UNSECURE (CABIN) · airframe 64,973 hrs · 38,024 cycles

EXIT LIGHT COVER FELL OFF. INSTALLED LENS PER SIP.

Part: COVER — UNSECURE (CABIN) · airframe 64,780 hrs · 37,902 cycles

L1 DOOR FORWARD BUCKHEAD EXIT SIGN LIGHT COVER FELL OFF. REINSTALLED COVER PER AMM.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 64,258 hrs · 37,543 cycles

LT VERTICAL STABILIZER AFT SKATE ANGLE CHAFED. R&R SKATE ANGLE PER SRM.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 64,258 hrs · 37,543 cycles

LT VERTICAL STABILIZER FORWARD SKATE ANGLE CHAFED. R&R SKATE ANGLE PER SRM.

Part: BRACKET — BROKEN (LOWER EXT FUSELA) · airframe 64,258 hrs · 37,543 cycles

FWD L/H ATTACH BRACKET FOR ACCESS PANEL 192E IS BROKEN. / REMOVED AND REPLACED ACCESS PANEL 192E FWD L/H ATTACH BRACKET REF. SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,134 hrs · 36,830 cycles

LOWER EMERGENCY EXIT LIGHTS JUST FORWARD OF LEFT AND RIGHT OVERWING EXITS INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,134 hrs · 36,830 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: DOUBLER — CRACKED (LT WHEEL WELL) · airframe 63,134 hrs · 36,830 cycles

REAR SPAR SEAL DOUBLER CRACKED/BROKEN B.S. 663 LT W/W / REMOVED AND REPLACED REAR SPAR SEAL DOUBLER B.S 663 LT W/W I.A.W SRM 51-40-02-0G-0 AND BOEING DWG # 111A1000

Part: CONNECTOR — BROKEN (CABIN) · airframe 63,134 hrs · 36,830 cycles

FOR EMERGENCY EXIT LIGHT CONNECTOR BROKEN AT BS 712, STR 4L. REPAIRED CONNECTER PER WDM.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT FLOORBOARD 241AEF IS DELAMINATED / REPAIRED DELAMINATION DAMAGE ON AFT FLOOR BOARD 241AEF IAW SRM 53-00-50-2R-9 56749U 08FEB18

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,134 hrs · 36,830 cycles

AFT SERVICE DOOR LOWER MOP SILL ANGLE CORRODED. R&R ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 63,134 hrs · 36,830 cycles

BULKHEAD STIFFENER CRACKED AT BS 663, LBL 8. R & R THE BULKHEAD STIFFENER IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, RBL 3. R & R THE FLOORBEAM IAW SRM.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 63,134 hrs · 36,830 cycles

***CORROSION*** AFT CARGO BAY FLOOR PANEL SPLICE STRIP AT BS 772 HAS AREAS OF CORROSION BETWEEN LBL 21 AND RBL 21 WL 156. / UPON INVESTIGATION AFT CARGO BAY FLOOR SPLICE; TEE STRAP AT BS 772. BETWEEN; LBL 21 TO RBL 21; WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE ON SRM. PART WILL BE REPAIR BY REPLACEMENT. IAW SRM 51-10-02-0G-0. FABRICATED NEW TEE STRAP ITEM # BAC1505-100581 # 7075T6; LOT # 1294347. APPLIED CHEMICAL CONVERSION AND PRIMER. IAW DWG # 146A9401 SOPM 20-43-03 AND AMM 51-21-72-370-804. 80002U 07FEB18

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT WET AREA FLOOR BOARD 242WF IS DELAMINATED / AFT WET AREA FLOOR BOARD 242WF WITH DELAMINATIONS OVER ENTIRE BOARD WAS REPLACED WITH A SERVICEABLE FLOOR BOARD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT WET AREA FLOOR BOARD 242VF IS DELAMINATED / AFT WET AREA FLOOR BOARD 242VF WITH DELAMINATIONS OVER ENTIRE UPPER SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR BOARD AND WILL BE INSTALLED ON SA-M 565E JPANEL-241-CLOSE

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

FWD WET AREA FLOOR BOARD 221BF IS DELAMINATED / FWD WET AREA FLOOR BOARD 221BF WITH DELAMINATIONS OVER ENTIRE BOARD WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 3. R & R THE FLOORBEAM IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,134 hrs · 36,830 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, RBL 12. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 63,134 hrs · 36,830 cycles

FWD CARGO BAY FLOOR PANEL 120BF HAS ***CORROSION*** AROUND FASTENER HOLES / FABRICATED FWD CARGO BAY FLOOR PANEL 120BF. MAT'L USED 2024-T3 .080' LOT # 1319626-1. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW DWG 453A1610; SRM 51-2141-370-802 AND SRM 51-21-72-370-804.

Part: ATTACH ANGLE — CRACKED (BS 866) · airframe 63,134 hrs · 36,830 cycles

STANCHION ATTACH ANGLE CRACKED AT BS 866, LBL 10. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY PANEL 140CF HAS ***CORROSION*** AROUND FASTENER HOLES / FABRICATED AFT CARGO BAY PANEL 140CF - MAT'L USED 2024T3 .080' LOT 1319626-1. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW DWG 453A2610; SRM 51-21-41-370-802 AND SRM 51-21-72-370-804

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,134 hrs · 36,830 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 1. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 63,134 hrs · 36,830 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, RBL 1. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

FWD WET AREA FLOOR BOARD 221AF IS DELAMINATED / FWD WET AREA FLOOR BOARD 221AF WITH DELAMINATIONS OVER ENTIRE BOARD WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 8. R & R THE FLOORBEAM IAW SRM & EA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT WET AREA FLOOR BOARD 242UF IS DELAMINATED AND BROKEN / AFT WET AREA FLOOR BOARD 242UF WITH DELAMINATIONS OVER ENTIRE UPPER SURFACE AND BROKEN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL AND WILL BE INSTALLED ON SA-M 565E JPANEL-241-CLOSE

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

FWD WET AREA FLOOR BOARD 221GF IS DELAMINATED / REPAIRED DELAMINATION ON FWD FLOOR BOARD 221GF IAW SRM 53-00-50-2R-7. 56749U 07FEB18

Part: SUPPORT — CRACKED (LT WING) · airframe 63,134 hrs · 36,830 cycles

LEFT WING UPPER ANGLE ATTACHED TO THE UPPER PANEL SUPPORT, JUST OUTBOARD OF THE UPPER INBD REAR SPAR BATH TUB FITTING FOUND CRACKED. R & R THE SUPPORT IAW SRM.

Part: BULKHEAD — DELAMINATED (FUSELAGE) · airframe 63,134 hrs · 36,830 cycles

BULKHEAD DELAMINATED AT BS 663, LBL 12. REPAIRED BULKHEAD IAW SRM.

Part: DOUBLER — CORRODED (LOWER INT FUSELA) · airframe 63,134 hrs · 36,830 cycles

***CORROSION*** ON UPPER SURFACE OF ANTENNA DOUBLER IN FCB BILGE; BL-0; BS-510 / F.C.B BILGE ANTENNA DOUBLER BS 510; BL 0. REMOVED AND REPLACED DOUBLER SI # 7530980 PO# 670672 IAW SRM 51-10-02. PARA.9

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,134 hrs · 36,830 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, LBL 11. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT WET AREA FLOOR BOARD 242RF IS DELAMINATED / AFT WET AREA FLOOR BOARD 242RF WITH DELAMINATIONS OVER ENTIRE UPPER SURFACE WAS REPLACED WITH A SERVICEABLE FLOOR BOARD AND WILL BE INSTALLED ON SA-M 565E JPANEL-241-CLOSE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT WET AREA FLOOR BOARD 241ABF IS DELAMINATED / DAMAGED FLOOR PANEL 241ABF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR.9.

Part: DOUBLER — CORRODED (LOWER INT FUSELA) · airframe 63,134 hrs · 36,830 cycles

***CORROSION*** ON UPPER SURFACE OF ANTENNA DOUBLER IN FCB BILGE; BL-0; BS-500A+14. / F.C.B BILGE; ANTENNA DOUBLER BS 500A + 14 BL 0. REMOVED AND REPLACED DOUBLER P/N 7530980. PO# 610806 IAW SRM 51-10-02 PARA. 9.

Part: CHANNEL — CORRODED (BS 960-990) · airframe 63,134 hrs · 36,830 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 960 TO 990. R & R THE MOP SILL IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 500) · airframe 63,134 hrs · 36,830 cycles

FORWARD CARGO BAY, FORWARD SURFACE OF LOWER AFT BULKHEAD ANGLE CORRODED AT BS. 500D. R & R THE ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,134 hrs · 36,830 cycles

AFT WET AREA FLOOR BOARD 242TF IS DELAMINATED / DAMAGED FLOOR PANEL 242 TF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,134 hrs · 36,830 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 300 TO BS 344. R&R MOPSILL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 12.5. R & R THE FLOORBEAM IAW SRM & EA.

Part: SIDEWALL SUPPORT — CORRODED (BS 847-867) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO 867, RBL 15.5. R & R THE SUPPORT IAW SRM & DWG.

Part: STRIP — CORRODED (AFT CARGO THRESH) · airframe 63,134 hrs · 36,830 cycles

**CORROSION** REINFORCING CAP STRIP AT AFT CARGO DOORWAY THRESHOLD HAS CORROSION AT FASTENER HOLE; BS800; RBL 19.5 / REIFORCING CAP STRIP AT AFT CARGO BAY REPLACEMENT WILL BE ACCOMPLISHED ON COSTOMER CARD T754714

Part: SIDEWALL SUPPORT — CORRODED (BS 500A-500D) · airframe 63,134 hrs · 36,830 cycles

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

Part: WEB — CRACKED (BS 665) · airframe 63,134 hrs · 36,830 cycles

PRESSURE DECK WEB CRACKED AT BS 665, RBL 43. REPAIRED THE BULKHEAD WEB IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 63,134 hrs · 36,830 cycles

LEFT WING TRAILING EDGE UPPER PANEL BULB SEAL SUPPORT BRACKET ABOVE INBOARD DEFLECTION CONTROL RIB CRACKED. R & R THE BRACKET IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 943.5) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY, NUT PLATE HOLE IN THE FLOOR SUPPORT CHANNEL CORRODED AT BS 943.5, RBL 3. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: WEB — CRACKED (RT WING) · airframe 63,134 hrs · 36,830 cycles

RIGHT WING TRAILING EDGE UPPER PANEL TRANSVERSE WEB ABOVE NR 2 PYLON CRACKED AT OTBD UPPER ATTACH FASTENER HOLE. R & R THE WEB IAW SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,134 hrs · 36,830 cycles

**CORROSION** AFT CARGO BAY; CORROSION ON FWD END UPPER SURFACE OF LOWER FLOOR/ BULKHEAD SUPPORT ANGLE; BS867; LBL14.5 / BS 867 LOWER BULKHEAD SUPPORT ANGLE WAS REPAIRED IAW ATS ER 18-01529 REV IR DATED 19FEB18 AND EA 1-753-32278 REV IR

Part: WEB — CORRODED (THRESHOLD) · airframe 63,134 hrs · 36,830 cycles

CORROSION ON THE UPPER SURFACE ON FORWARD CARGO BAY THRESHOLD SUB WEB. R & R THE WEB IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 400-500D) · airframe 63,134 hrs · 36,830 cycles

FORWARD CARGO BAY, FLOOR TO SIDEWALL SUPPORT FOUND CORRODED BETWEEN BS 400 TO 500D, LBL 24. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,134 hrs · 36,830 cycles

**CORROSION** AFT CARGO BAY; AFT FLOOR PANEL SPLICE STRAP IS CORRODED ALONG ENTIRE UPPER SURFACE; BS887; RBL15 TO LBL15 REJECT: PER ATTACHED SA-M 326 A1196050 ITEM #3 PANEL SPLICE STRAP BS 887 HAS NOT BEEN INSTALLED. / REJECT INSP # 379 12FEB18 INSTALLED PANEL SPLICE STRAP AT BS 887 ON SA-M 326 A1196050 ITEM 3

Part: SUPPORT ANGLE — CORRODED (BS 947 BULKHEAD) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY, AFT BULKHEAD SUPPORT ANGLE FOUND CORRODED AT BS 947, RBL 6.5 TO LBL 14. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 462) · airframe 63,134 hrs · 36,830 cycles

FORWARD CARGO BAY, CARGO TRACK CORRODED AT BS 462, RBL 15. R & R THE CARGO TRACK IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,134 hrs · 36,830 cycles

FORWARD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. R & R THE SCUFF PLATE IAW SRM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 63,134 hrs · 36,830 cycles

RT WING T/E BULB SEAL RETAINER ABOVE #2 PYLON AFT TIP IS CRACKED / REMOVED THE CRACKED; RT. WING T/E BULB SEAL RETAINER AND WORN BULB SEAL ABOVE THE #2 PYLON; REPLACED THE CRACK BULB SEAL RETAINER. AND WORN BULB SEAL WITH NEW AND INSTALLED THE NEW BULB SEAL RETAINER AND BULB SEAL IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0; AND AIPC 57-50-00-25.

Part: ANGLE — CORRODED (BS 943.5) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY, FLOOR SUPPORT REINFORCING ANGLE CORRODED AT BS 943.5, RBL 9. R & R THE ANGLE IAW DWG AND SRM.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 63,134 hrs · 36,830 cycles

UPPER SURFACE OF THE AFT CARGO DOORWAY LOWER SILL CORRODED BETWEEN BS 795 TO 847, RBL 26. R & R THE DOOR SILL IAW DWG AND SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO 767. R & R SUPPORT IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 63,134 hrs · 36,830 cycles

***CORROSION*** AFT CARGO BAY FLOOR SPLICE AT BS 727D +6 CORRODED / UPON INVESTIGATION AFT GARBO BAY FLOOR SPLICE; TEE STRAP AT BS 727D+6; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE ON SRM. PART WILL BE REPAIR BY REPLACEMENT. IAW SRM 51-10-02-0G-0. FABRICATED NEW TEE STRAP; ITEM# BAC1505-100581#7075T6; LOT# 1294347 APPLIED CHEMICAL CONVERSION AND PRIMER. IAW DWG# 146A9401; SOPM 20-43-03 AND AMM 51-21-72-370-804. 80002U 07FEB18.

Part: SUPPORT — CORRODED (BS 867-887) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO 887, RBL 15. R & R THE SUPPORT IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 420-440) · airframe 63,134 hrs · 36,830 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL CORRODED BETWEEN BS 420 TO 440, RBL 24. R & R THE SUPPORT PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 727) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727+13, LBL 3. REPAIRED THE FLOOR SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (BS 767-787) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY, RIGHT FLOOR TO SIDEWALL CORRODED BETWEEN BS 767 TO 787. R & R SHIELD WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 63,134 hrs · 36,830 cycles

FORWARD AND AFT REINFORCING ANGLES ON THE WATER SERVICE PAN IN THE AFT CARGO BAY, CRACKED. R & R THE ANGLE IAW DWG AND SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727B-847) · airframe 63,134 hrs · 36,830 cycles

AFT CARGO BAY, LEFT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727B TO 847. R & R THE SUPPORT IAW SRM & DWG.

Part: DOUBLER — CRACKED (LT WING SLAT) · airframe 63,134 hrs · 36,830 cycles

LEFT WING, NR 2 SLAT NOSE SKIN REPAIR DOUBLER CRACKED ON THE LOWER SURFACE AT ACTUATOR RIB. REPAIRED THE SKIN REPAIR DOUBLER IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,134 hrs · 36,830 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,001 hrs · 36,740 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. R & R THE SIGN IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,440 hrs · 36,390 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1675 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,440 hrs · 36,390 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1672 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 62,440 hrs · 36,390 cycles

RIGHT FLOOR EMERGENCY LIGHT STRIP DELAMINATED AT ROW 1. R & R THE LIGHT IAW DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,440 hrs · 36,390 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1673 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 61,992 hrs · 36,084 cycles

L1 DOOR EXIT SIGN PLACARD FELL OFF. SECURED LENS COVER PER MM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 61,964 hrs · 36,065 cycles

RT OVERWING EMERGENCY EXIT SIDEWALL EXIT SIGN COVER FELL OFF. R&R COVER PER MM

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,603 hrs · 35,832 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,603 hrs · 35,832 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,530 hrs · 35,200 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. R & R THE LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 59,348 hrs · 34,471 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING ARROW. R&R COVER PER AMM.

Part: COVER — DEFECTIVE (CABIN) · airframe 59,348 hrs · 34,471 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING ARROW. R&R COVER PER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 59,294 hrs · 34,437 cycles

LT OVERWING EXIT SIGN LENS MISSING. R&R LENS PER SIP.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R AT LOWER FUSELAGE. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

WING TO BODY FAIRING SUPPORT STRUCTURE CHORD CRACKED AT BS 500D, BETWEEN STRINGER 18R - 19R. REPAIRED CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 727B, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FAIRING — CRACKED (LT WING) · airframe 57,118 hrs · 33,155 cycles

LEFT WING AFT FAIRING 544BB CRACKED. REPAIRED AFT FAIRING IAW SRM & EA.

Part: FAIRING — CRACKED (RT WING) · airframe 57,118 hrs · 33,155 cycles

RIGHT WING AFT FAIRING 643BB CRACKED. REPAIRED FAIRING IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FAIRING — CRACKED (RT WING) · airframe 57,118 hrs · 33,155 cycles

RIGHT WING AFT FAIRING 644BB CRACKED. REPAIRED AFT FAIRING IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 7R - 15R. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,118 hrs · 33,155 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, RBL 2.5. REPAIRED WEB IAW EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 56,304 hrs · 32,698 cycles

FORWARD CABIN LT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 56,304 hrs · 32,698 cycles

MIDDLE CABIN RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 56,304 hrs · 32,698 cycles

MIDDLE CABIN LT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 56,304 hrs · 32,698 cycles

FORWARD EMERGENCY LIGHT STRIP CRACKED AT 1 ABC. R & R LIGHT IAW MM.

Part: LIGHT — CRACKED (ROW 4 ABC) · airframe 56,304 hrs · 32,698 cycles

FORWARD EMERGENCY LIGHT STRIP CRACKED AT 4 ABC. R & R STRIP IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 53,647 hrs · 31,180 cycles

L1 DOOR FLOOR LEVEL EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: ACTUATOR — LEAKING (LE SLAT) · airframe 52,167 hrs · 30,319 cycles

LEADING EDGE FLAPS TRANSIT LIGHT ON WHEN SELECTED FLAPS 5 NR 5, 6 & 8. BLACK NR 7 GREEN HYD LEAK FROM SLATS. R & R NR 7 SLAT ACTUATOR IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 51,431 hrs · 29,905 cycles

R2 DOOR ENTRANCE EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,780 hrs · 29,540 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.7 VERTICAL STIFFENER CRACKED 19.5 INCHES FROM FRONT SPAR AT BOTTOM OF RIB. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,780 hrs · 29,540 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.7 VERTICAL STIFFENER CRACKED 10 INCHES FROM FRONT SPAR BOTTOM OF RIB. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,780 hrs · 29,540 cycles

RIGHT HORIZONTAL STABILIZER STATION 129.5 VERTICAL STIFFENER CRACKED 17 INCHES FROM FRONT SPAR AT BOTTOM OF RIB. REPAIRED STIFFENER IAW SRM.

Part: SKIN — DEFORMED (RT HORIZ STAB) · airframe 50,780 hrs · 29,540 cycles

RIGHT HORIZONTAL STABILIZER STATION 111.1 SKIN DEFORMED AT BOTTOM OF RIB. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA & SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

CABIN FLOOR BEAM SEAT TRACK CRACKED FWD OF BS 727B, LBL 45.50. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

CABIN FLOORBEAM SEAT TRACK CRACKED FWD OF BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

FLOOR SEAT TRACK CRACKED AT BS 727B, RBL 45.50. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

CABIN FLOOR SEAT TRACK CRACKED FWD OF BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

FLIGHT COMPARTMENT FIRST OFFICER`S NR 1 WINDOW FRAME CRACKED JUST BELOW THE UPPER OTBD. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

COCKPIT RT NR 3 WINDOW FRAME E-F POST CRACKED IN 2ND HOLE FROM BOTTOM. REPAIRED FRAME IAW ACO.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,780 hrs · 29,540 cycles

FLIGHT COMPARTMENT CAPTAIN`S NR 1 WINDOW FRAME CRACKED JUST BELOW THE UPPER OTBD. REPAIRED FRAME IAW ACO.

Part: LENS — LOOSE (L2 DOOR) · airframe 49,482 hrs · 28,764 cycles

L2 DOOR EXIT LIGHT COVER LOOSE. SECURED EMERGENCY EXIT LIGHT LENS COVER IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 49,299 hrs · 28,648 cycles

OVERWING EMERGENCY EXIT LIGHT BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,341 hrs · 28,060 cycles

RT AFT EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,341 hrs · 28,060 cycles

RT AFT EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY CHARGER ASSEMBLY IAW MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 47,475 hrs · 27,564 cycles

LT MLG WHEEL WELL FWD BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 540, LBL 42.80. REPAIRED WEB IAW SRM.

Part: VALVE — FAULTED (FUEL SYSTEM) · airframe 46,642 hrs · 27,058 cycles

DURING CLIMB GOT FUEL IMBALANCE ALERT RIGHT TANK 1,000LBS LOW-TOTAL FUEL ABOUT RIGHT. CROSS FEED VALVE C/B FOUND POPPED. RESET C/B, CROSSFEED TO REGAIN BALANCE. (NOTE-CROSSFEED VALVE LIGHT INIP, REPLACED BULBS, STILL NOT ILLUMINATING) REMOVED AND REPLACED CROSSFEED VALVE PER MM. OK CHECK GOOD. P/N OFF/ON MA30A1001, S/N OFF AA217063C S/N ON AA210248D

Part: COVER — LOOSE (EXIT SIGN) · airframe 44,972 hrs · 25,968 cycles

R2 DOOR EMERGENCY EXIT SIGN LIGHT COVER LOOSE. REMOVED AND REPLACED SIGN PER M/M.

Part: LENS — LOOSE (CABIN) · airframe 44,415 hrs · 25,634 cycles

R2 DOOR LOWER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER EA.

Part: SENSOR — FAULTY (TE FLAP) · airframe 43,607 hrs · 25,167 cycles

DECLARED EMERGENCY - FLAPS WOULD NOT EXTEND USING NORMAL PROCEDURES. EXTENDED FLAPS USING ALT METHOD TO POS 15 AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 6 AND NR 8 FLAP SKEW DETECTION SENSORS PER M/M.

Part: LIGHT — LOOSE (CABIN) · airframe 43,236 hrs · 24,962 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 43,134 hrs · 24,905 cycles

OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: COVER — BROKEN (CABIN) · airframe 43,134 hrs · 24,905 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,970 hrs · 24,793 cycles

EEPLS STRIP LOOSE ROW 1 DEF. SECURE LIGHT STRIP PER MM.

Part: DOOR — CRACKED (RT MLG) · airframe 42,721 hrs · 24,657 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MLG INNER DOOR CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 42,702 hrs · 24,644 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS DAMAGED AT ROW 7. REMOVED AND REPLACED EEPLS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,116 hrs · 23,706 cycles

DURING SCHEDULE HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,116 hrs · 23,706 cycles

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

Part: LIGHT — CRACKED (CABIN) · airframe 37,258 hrs · 21,496 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT EEPLS CRACKED BETWEEN ROW 1 TO ROW 3. REMOVED AND REPLACED EEPLS PER MM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND LATERAL INTERCOSTAL CORRODED AT BS 270, LBL 6. REPAIRED INTERCOSTAL PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO FLOOR SUPPORT CORRODED AT BS 503, LBL 14. REPAIRED SUPPORT PER EA.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, LBL 7. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, RBL 32. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, LBL 32. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, LBL 14. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, RBL 14. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 548, LBL 54. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 2 SLAT PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, RBL 7. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (CENTER WING) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING STIFFENER ANGLE CRACKED AT BS 547, LBL 42. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,142 hrs · 21,430 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO FLOOR SUPPORT BEAM CORRODED AT BS 503, RBL 9. REPAIRED BEAM PER EA.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 36,554 hrs · 21,075 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RECONNECTED CONNECTOR PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,218 hrs · 20,239 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING ATTACH LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,218 hrs · 20,239 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING ATTACH LUGS CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,990 hrs · 20,094 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,290 hrs · 19,668 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. RELAMPED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 33,841 hrs · 19,395 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,009 hrs · 18,913 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,762 hrs · 18,774 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP BETWEEN ROW 10 TO ROW 13. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,508 hrs · 17,379 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 45. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,508 hrs · 17,379 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 733D, LBL 12 TO RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,508 hrs · 17,379 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER 5R CRACKED AT BS 332. REPAIRED STRINGER PER SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 30,508 hrs · 17,379 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 9 ABC. INSTALLED STRIP PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,685 hrs · 16,877 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 27,087 hrs · 15,370 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: COFFEEMAKER — FAULTY (REAR GALLEY) · airframe 26,936 hrs · 15,300 cycles

DIVERSION, AT ALTITUDE F/A REPORTED ELECTRICAL ODOR IN REAR GALLEY, TURNED POWER OFF ODOR WENT AWAY. REMOVED AND REPLACED AFT COFFEEMAKER PER MM.

Part: O-RING — BLOWN (A/C PACK) · airframe 25,032 hrs · 14,206 cycles

AIR TURNBACK, ALTITUDE WARNING HORN SOUNDED. FOUND LEFT A/C PACK COMPRESSOR DISCHARGE TO ACM DUCT SEGMENT O-RINGS BLOWN. REMOVED AND REPLACED O-RINGS PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,649 hrs · 13,984 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT LEFT CABIN BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 24,649 hrs · 13,984 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 23,641 hrs · 13,386 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 22,193 hrs · 12,546 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP COVER MISSING BETWEEN ROW 6 TO ROW 9. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,944 hrs · 12,405 cycles

EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15 DEF. RELAMPED LIGHT PER MM.

Part: GLOWSTRIP — LOOSE (ROW 8-10) · airframe 20,386 hrs · 11,532 cycles

PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 TO ROW 10. SECURED STRIP PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 19,663 hrs · 11,138 cycles

DURING SCHEDULED RON CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,651 hrs · 11,130 cycles

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

Part: BLADE — TORN (NR 2 COMPRESSOR) · airframe 17,436 hrs · 9,818 cycles

DURING SCHEDULED HC2 CHECK, FOUND NR 2 ENGINE 8TH STAGE HPC ROTOR HAS 1 EACH BLADE TORN. REMOVED AND REPLACED NR 2 ENGINE PER MT 771-00-01.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 17,436 hrs · 9,818 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,166 hrs · 7,998 cycles

EEPLS FLOOR TRACK LIGHTING LENS MISSING. INSTALLED EEPLS LENS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 8,865 hrs · 5,116 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,630 hrs · 4,395 cycles

EEPLS INOP AT ROW 4. RELAMPED EEPLS AT ROW 4 PER MM.