N7883A

Part: SUPPORT BRACKET — CRACKED (ZN 400 NACELLE/P) · airframe 56,321 hrs · 36,048 cycles

HYDRAULIC SYSTEM B PRESSURE LINE AND HYDRAULIC SYSTEM B RETURN HEAT EXCHANGER SUPPORT BRACKET FOUND CRACKED NEXT TO #2 ENGINE STRUT WING MOUNT<[01] REMOVED LOCATED DRILLED AND INSTALLED 2 EACH HILOK AND SUPPORT BRACKET PER SRM 51-40-02;[02] HI LOKS INSTALLED PER SRM 51-40-02<BR>COLLARS SEALED PER AMM 51-31-00;[03] REFERENCE VENDOR WO 12334R1364 FOR HILOCK COLLAR INSTALLATION AND CAP SEAL

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 56,229 hrs · 35,991 cycles

FORWARD PASSENGER DOOR L1 SLIDE GIRT HANGING TOO LOW.<[01] ADJUSTED FWD PASSENGER L1 DOOR SLIDE GIRT BAR REF AMM 25-66-01.

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 53,886 hrs · 34,495 cycles

RIGHT AFT SERVICE DOOR EMERGENCY SLIDE LIGHTS ARE INOP<[01] REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1672 BATTERY PACK IAW AMM 33-51-06 OPS CHECKS GOOD

Part: BALLAST — INOPERATIVE (EXIT LIGHT) · airframe 53,483 hrs · 34,237 cycles

LEFT OVERWING EXIT WINDOW LIGHT INOP. REPLACED BALLAST PER MM 33-26-02.

Part: BATTERY PACK — INOPERATIVE (L/H CABIN) · airframe 52,547 hrs · 33,631 cycles

INOP EMERGENCY LIGHT BATTERY PACKS FIN M1668 AT PASSENGER MIDDLE CABIN SIDE LT. 2022-427243 / [01] REPLACED EMERGENCY LIGHT BATTERY PACKS FIN M1668 AT PASSENGER MIDDLE CABIN SIDE LT. I.A.W B737-700 AMM 33-51-06-960-805.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED EMERGENCY LIGHT BATTERY PACKS FIN M1668 AT PASSENGER MIDDLE CABIN SIDE LT. I.A.W B737-700 AMM 33-51-06-960-805. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK ON INTERNAL SKIN OF EQUIPMENT ACCESS DOOR 2022-427230 / [01] REPLACED INTERNAL SKIN OF EQUIPMENT ACCESS DOOR AND FASTENERS IAW B737-700 SRM 51-10-02 AND DWG 141A6713 SHEET: 2 REV: - AND DWG 141A6710 SHEET: 7 REV: B;[02] REPLACED INTERNAL SKIN OF EQUIPMENT ACCESS DOOR AND FASTENERS IAW B737-700 SRM 51-10-02 AND DWG 141A6713 SHEET: 2 REV: - AND DWG 141A6710 SHEET: 7 REV: B RII;[03] REPLACED INTERNAL SKIN OF EQUIPMENT ACCESS DOOR AND FASTENERS IAW B737-700 SRM 51-10-02 AND DWG 141A6713 SHEET: 2 REV: - AND DWG 141A6710 SHEET: 7 REV: B SEE INDIVIDUAL SINGOFFS BELOW RII

Part: NONE — CORRODED (AFT CARGO) · airframe 52,547 hrs · 33,631 cycles

CORROSION ON SPLICE TEE STRAP LOC AT LEVEL OF BS 767 BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT 2022-427198 / [01] MADE SPLICE TEE STRAP LOC AT LEVEL BS 767 BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 DWG 146A9401 SHEET 2 REV C;[02] REPLACED SPLICE TEE STRAP LOC AT LEVEL BS 767 BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG 146A9401 SHEET 2 REV C;[03] CORRECT STEP 1AND 2: <BR>REPLACED SPLICE TEE STRAP LOC AT LEVEL BS 767 BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 DWG 146A9401 SHEET 2 REV C. SEE INDIVIDUAL STEP SING-OFF BELLOW;[04] REPLACED SPLICE TEE STRAP LOC AT LEVEL BS 767 BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 DWG 146A9401 SHEET 2 REV C. SEE INDIVIDUAL SING-OFF BELLOW .ITEM RII

Part: ANGLE — CRACKED (L/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK ANGLE LOCATED ON FRONT SPAR BOOST PUMP STA IFSS 115 AND WBL 94.24 AT LT WING. 2022-427199. / [01] REPLACED SUPPORT ANGLE LOCATED ON FRONT SPAR BOOST PUMP AT LEVEL OF STA IFSS 115 AND WBL 94.24 AT LT WING. IAW B737-700 SRM 51-40-02; SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3; DWG # 112A2004 SHEET 5; REV -; AND DWG # 116A3001 SHEET 22; REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED ON FRONT SPAR BOOST PUMP AT LEVEL OF STA IFSS 115 AND WBL 94.24 AT LT WING. IAW B737-700 SRM 51-40-02; SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3; DWG # 112A2004 SHEET 5; REV -; AND DWG # 116A3001 SHEET 22; REV - SEE INDIVIDUAL SIGNOFFS BELOW. <BR>CERTIFIED AS RII.

Part: NONE — CORRODED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CORROSION ON SPLICE TEE STRAP LOC AT LEVEL BS 727D BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT 2022-427197 / [01] MADE SPLICE TEE STRAP LOC AT LEVEL BS 727D BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 DWG 146A9401 SHEET 2 REV C;[02] REPLACED SPLICE TEE STRAP LOC AT LEVEL BS 727D BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 DWG 146A9401 SHEET 2 REV C;[03] CORRECT STEP 1 AND 2:<BR>REPLACED SPLICE TEE STRAP LOC AT LEVEL BS 727D BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 DWG 146A9401 SHEET 2 REV .SEE INDIVIDUAL STEP SIGN OFF BELOW.;[04] REPLACED SPLICE TEE STRAP LOC AT LEVEL BS 727D BTW STRINGER 25RH TO STRINGER 25LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 DWG 146A9401 SHEET 2 REV-C.SEE INDIVIDUAL SIGN OFF BELOW.

Part: NONE — CORRODED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CORROSION ON SUPPORT ZEE LOC BS 727B TO BS807 AT LEVEL STRINGER 25LH AFT CARGO COMPARTMENT 2022-427195 / [01] REPLACED SUPPORT ZEE AND FASTENERS LOC BTW BS 727 TO BS 847 AT LEVEL OF STR 25L AT AFT CARGO COMPARTMENT IAW SRM B737-700-51-10-02 ITEM 9. AND DRAWINGS # 146A7502 REV. A AND 146A7500 REV. - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1.<BR>REPAIRED SUPPORT ZEE LOC BTW BS 727 TO BS 847 AT LEVEL OF STR 25L AT AFT CARGO COMPARTMENT IAW B737-700-SRM 51-10-02 ITEM 9; SRM 53-00-53-2R-6 REPAIR 6; FIGURE 203 SHEET 1 AND DRAWINGS # 146A7502 REV. A AND 146A7500 REV. - SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPAIRED SUPPORT ZEE LOC BTW BS 727 TO BS 847 AT LEVEL OF STR 25L AT AFT CARGO COMPARTMENT IAW B737-700-SRM 51-10-02 ITEM 9; SRM 53-00-53-2R-6 REPAIR 6; FIGURE 203 SHEET 1 AND DRAWINGS # 146A7502 REV. A AND 146A7500 REV. - SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: FASTENER — LOOSE (R1 DOOR) · airframe 52,547 hrs · 33,631 cycles

LOOSE FASTENER ENTRY DOOR ESCAPE SLIDE AT FWD GALLEY AREA (1 EA) 2022 427136 / [01] REPLACED FASTENER ENTRY DOOR ESCAPE SLIDE AT FWD GALLEY AREA (1 EA) IAW B737-700 DWG 416A2204 SHEET 5 REV B; AND B737-700 SRM 51-40-02.;[02] REPLACED FASTENER ENTRY DOOR ESCAPE SLIDE AT FWD GALLEY AREA (1 EA) IAW B737-700 DWG 416A2204 SHEET 5 REV B; AND B737-700 SRM 51-40-02.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 52,547 hrs · 33,631 cycles

CRACK INDICATIONS FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.965 INCH 2022-427118 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN/ NORTEC 600D ; SN/ 190023010; DUE DATE/ 14-FEB-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 11-APR-23;[03] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCH FROM FRONT SPAR; INBD SIDE OF RIB. IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 PARAGRAPH 4 SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCH FROM FRONT SPAR; INBD SIDE OF RIB. IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 PARAGRAPH 4 SEE INDIVIDUAL SIGNOFFS BELOW.. RII ITEM

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 52,547 hrs · 33,631 cycles

CRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.100 INCH 2022-427117 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210136503; DUE DATE: 11-APR-23.;[02] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N : A21147752 DUE DATE: 06-OCT-22;[03] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC600D S/N 190023010 DUE DATE 14-FEB-23.;[04] PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER INSPAR SKIN BTW SSTA 184.70 & SSTA 193.90 IAW EA 22-155-02653; SEE INDIVIDUAL SIGN OFF BELOW;[05] PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER INSPAR SKIN BTW SSTA 184.70 & SSTA 193.90 IAW EA 22-155-02653; SEE INDIVIDUAL SIGN OFF BELOW<BR><BR>CERTIFIED AS RII

Part: PLATE — CRACKED (R/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2022-427104 / [01] REPLACED NEW CORRUGATED PLATE AND NEW FASTENERS IAW SRM B737-700 51-10-02 ITEM 9 ;51-40-02 AND DRAWING 115A2001 REV - LOCATED TRAILING EDGE AT LEVEL ORSS 261 AT RT WING;[02] REPLACED NEW CORRUGATED PLATE AND NEW FASTENERS IAW SRM B737-700 51-10-02 ITEM 9 ;51-40-02 AND DRAWING 115A2001 REV - LOCATED TRAILING EDGE AT LEVEL ORSS 261 AT RT WING

Part: ANGLE — CRACKED (R/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK ON SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING 2022-427109 / [01] REPLACED SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-40-02;[02] CERTIFIED WORK PERFORMED.

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 52,547 hrs · 33,631 cycles

CRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 25.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.010 INCH 2022-427116 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N : A21147752 DUE DATE: 06-OCT-22;[02] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC600D S/N 190023010 DUE DATE 14-FEB-23.;[03] REFER TO FAULT TTG8Q00E71N5 WHERE EA 22-155-02653 HAS BEEN ATTACHED AS A SUBTASK.;[04] CORRECTED STEP 3<BR>REFER TO FAULT TTG8Q00E71N5 WHERE EA 22-155-02653 HAS BEEN ATTACHED AS A SUBTASK. SEE INDIVIDUAL SIGN OFF BELOW;[05] REFER TO FAULT TTG8Q00E71N5 WHERE EA 22-155-02653 HAS BEEN ATTACHED AS A SUBTASK. SEE INDIVIDUAL SIGN OFF BELOW<BR><BR>CERTIFIED AS RII

Part: ANGLE — CRACKED (R/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK SUPPORT ANGLE AT LEVEL ORSS 282 TRAILING EDGE AT RT WING 2022-427080 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOC. AT LEVEL ORSS 282 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND B737-700 DWG 115A3700 SHEET 27 REV -.SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOC. AT LEVEL ORSS 282 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND B737-700 DWG 115A3700 SHEET 27 REV -.SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: ANGLE — CRACKED (L/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK SUPPORT ANGLE AT LEVEL ORSS 282 TRAILING EDGE AT LT WING 2022-427079 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON ORSS 280 ON TRAILING EDGE AT LT WING. IAW B737-700 SRM 51-40-02 AND DWG 115A3758 SHEET 4 AND REV -.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON ORSS 280 ON TRAILING EDGE AT LT WING. IAW B737-700 SRM 51-40-02 AND DWG 115A3758 SHEET 4 AND REV -. 'SEE INDIVIDUAL SIGNOFFS BELOW'.;[03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON ORSS 280 ON TRAILING EDGE AT LT WING. IAW B737-700 SRM 51-40-02 AND DWG 115A3758 SHEET 4 AND REV -. 'SEE INDIVIDUAL SIGNOFFS BELOW'.

Part: BRACKET — CRACKED (R/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK SUPPORT BRACKET TRAILING EDGE AT LEVEL ORSS 274 RT WING 2022-427081 / [01] REPLACED SUPPORT BRACKET ON TRAILING EDGE AT LEVEL ORSS 274 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG #115A2930 SHEET 8 AND REV -. MEASURE OF CRACK IS 0.470'. TOOL USED IS CALIPER P/N:700-113-10; S/N:0033158; DUE DATE: 01-OCT-22.;[02] REPLACED SUPPORT BRACKET ON TRAILING EDGE AT LEVEL ORSS 274 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG #115A2930 SHEET 8 AND REV -. MEASURE OF CRACK IS 0.470'. TOOL USED IS CALIPER P/N:700-113-10; S/N:0033158; DUE DATE: 01-OCT-22.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 52,547 hrs · 33,631 cycles

CRACK STRINGER 23L LOCATED BS540 AND WL164 FWD CARGO COMPARTMENT 2022-427027 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N:A21147756 DUE DATE: 25-OCT-22;[02] TOOL USED ULTRASONIC THICKNESS INSTRUMENT P/N 38DLPLUS S/N 120398603 DUE DATE 18-OCT-22.;[03] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE: 08-SEP-22 WAS USED.;[04] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-23.;[05] PERFORMED PERMANENT REPAIR ON STR 23L LOCATED BS540 AND WL164 FWD CARGO COMPARTMENT IAR. B737-700 SRM 53-00-03-2R-1 REPAIR 1 TABLE 201; 202 ;203 FIGURE 205. SEE INDIVIDUAL SIGN-OFF BELOW.;[06] CORRECTED STEP 5.<BR>PERFORMED PERMANENT REPAIR ON STR 23L LOCATED BS540 AND WL164 FWD CARGO COMPARTMENT IAW. B737-700 SRM 53-00-03-2R-1 REPAIR 1 TABLE 201; 202 ;203 FIGURE 205. SEE INDIVIDUAL SIGN-OFF BELOW.;[07] PERFORMED PERMANENT REPAIR ON STR 23L LOCATED BS540 AND WL164 FWD CARGO COMPARTMENT IAW. B737-700 SRM 53-00-03-2R-1 REPAIR 1 TABLE 201; 202 ;203 FIGURE 205 RII ACCOMPLISHED. SEE INDIVIDUAL SIGN-OFF BELOW.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK STRINGER 26L LOCATED BS540 AND WL152 FWD CARGO COMPARTMENT 2022-427029 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N:A21147756 DUE DATE: 25-OCT-22;[02] TOOL USED ULTRASONIC THICKNESS INSTRUMENT P/N 38DLPLUS S/N 120398603 DUE DATE 18-OCT-22.;[03] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[04] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 26L LOCATED BS540 AND WL152 FWD CARGO COMPARTMENT IAW. B737-700 SRM 53-00-03-2R-1 REPAIR 1 TABLE 201; 202 ;203 FIGURE 205. SEE INDIVIDUAL SIGN-OFF BELOW.;[06] PERFORMED PERMANENT REPAIR ON STRINGER 26L LOCATED BS540 AND WL152 FWD CARGO COMPARTMENT IAW. B737-700 SRM 53-00-03-2R-1 REPAIR 1 TABLE 201; 202 ;203 FIGURE 205 RII ACCOMPLISHED . SEE INDIVIDUAL SIGN-OFF BELOW.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK STRINGER 24L LOCATED BS540 AND WL159 AT FWD CARGO COMPARTMENT 2022-427028 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N:A21147756 DUE DATE: 25-OCT-22;[02] TOOL USED ULTRASONIC THICKNESS INSTRUMENT P/N 38DLPLUS S/N 120398603 DUE DATE 18-OCT-22.;[03] TOOL USED EDDY CURRENT P/N: NORTEC 500D; S/N: N500X12101V022237; DUE DATE: 06-OCT-22.;[04] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-23.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 24L LOCATED BS540 AND WL159 AT FWD CARGO COMPARTMENT IAW. B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIG 206 AND TABLE 203. SEE INDIVIDUAL SIGN-OFF BELOW.;[06] PERFORMED PERMANENT REPAIR ON STRINGER 24L LOCATED BS540 AND WL159 AT FWD CARGO COMPARTMENT IAW. B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIG 206 AND TABLE 203. RII ACCOMPLISHED SEE INDIVIDUAL SIGN-OFF BELOW

Part: COVER — BROKEN (L1 DOOR) · airframe 52,547 hrs · 33,631 cycles

BROKEN ENTRY DOORWAY LINNING COVER EMERGENCY EXIT AT FWD GALLEY AREA (1 EA) 2022-427005 / [01] REPLACED ENTRY DOORWAY LINNING COVER EMERGENCY EXIT AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802;[02] REPLACED ENTRY DOORWAY LINNING COVER EMERGENCY EXIT AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 52,547 hrs · 33,631 cycles

CRACK INSPAR RIB STAB STA 120.30 AT 36 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-426955 / [01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] EDDY CURRENT EQUIPMENT USED: P/N: NORTEC 600D; S/N: 60009161631<BR>DUE DATE: 03-DEC-22;[03] PERFORMED PERMANENT ON INSPAR RIB 120.30 AT 36 INCHES FROM FRONT SPAR IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIGURE 2 SHEET 1;[04] CORRECTED STEP 3.<BR>REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4; REPAIR 4 FIGURE 2 SHEET 1. SEE INDIVIDUAL SIGN OFF BELLOW;[05] CORRECTED STEP 3. <BR>REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4; REPAIR 4 FIGURE 2 SHEET 1. RII ;SEE INDIVIDUAL SIGN OFF BELLOW.

Part: LENS — BROKEN (AFT CABIN) · airframe 52,547 hrs · 33,631 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA 2022-426959 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802;[02] CORRECTED STEP 1 <BR>REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 STEP 3.C.(5).(D) AND 3.C.(10);[03] TASK CARD COMPLTED

Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK SUPPORT BRACKET BODY STATION 540 AT LBL 6.01 KEEL BEAM 2022-426969 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 AT LBL 6.01 KEEL BEAM IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED SUPPORT BRACKET BODY STATION 540 AT LBL 6.01 KEEL BEAM IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9

Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK SUPPORT BRACKET BODY STATION 540 AT RBL 6.01 KEEL BEAM 2022-426968 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 AT RBL 6.01 KEEL BEAM IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED SUPPORT BRACKET BODY STATION 540 AT RBL 6.01 KEEL BEAM IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 52,547 hrs · 33,631 cycles

CRACK ON SCUFF PLATE AT FWD POSITION OF FWD CARGO COMPARTMENT DOOR 2022-426965 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: B20189516 ; DUE DATE: 03-DEC-22.;[02] REPAIRED SCUFF PLATE AT FWD POSITION OF FWD CARGO COMPARTMENT DOOR I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 PARAGRAPH 4.B. AND BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW;[03] REPAIRED SCUFF PLATE AT FWD POSITION OF FWD CARGO COMPARTMENT DOOR I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 PARAGRAPH 4.B. AND BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 52,547 hrs · 33,631 cycles

CRACK ACCESS PANEL 661BB AROUND FASTENERS HOLES AT RT WING 2022-426980 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 16-JAN-23.;[03] TOOL USED SCALE P/N: 91847; S/N: AE-409320; DUE DATE: 06-JUN-23.;[04] TOOL USED SCALE P/N CL5000 S/N AE-409559 DUE DATE 06/JUN/23.;[05] TOOL USED MULTIMETER P/N: FLUKE 87-5 ; S/N: 32040125; DUE DATE 21-SEP-22.;[06] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.COMPLETED

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 52,547 hrs · 33,631 cycles

CRACK INSPAR RIB STAB STA 120.30 AT 19 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-426954 / [01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] EDDY CURRENT EQUIPMENT USED: P/N: NORTEC 600D; S/N: 60009161631<BR>DUE DATE: 03-DEC-22;[03] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 19 INCHES FROM FRONT SPAR IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIGURE 2 SHEET 1;[04] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4; REPAIR 4. SEE INDIVIDUAL SIGN OFF BELLOW;[05] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4; REPAIR 4. RII ;SEE INDIVIDUAL SIGN OFF BELLOW.

Part: ANGLE — CRACKED (VERT. STAB.) · airframe 52,547 hrs · 33,631 cycles

CRACK ANGLE LOCATED AT BS 1016 BETWEEN S-3R AND S-3L WL 308.5 AT VERTICAL STABILIZER 2022-426896 / [01] REPLACED ANGLE AND FASTENERS LOCATED AT BS 1016 BETWEEN S-3R AND S-3L WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 176A3001 SHEET 17 REV = ? SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOCATED AT BS 1016 BETWEEN S-3R AND S-3L WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 176A3001 SHEET 17 REV = ? SEE INDIVIDUAL SIGN-OFF BELOW.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK FLOOR STRUCTURE INTERCOSTAL LOCATED BS 540 AND BTW BL 0 TO LBL 24.82 AT PASSENGER CABIN 2022-426874 / [01] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BS 540 AND BTW BL 0 TO LBL 24.82 AT PASSENGER CABIN IAW B737-700 51-10-02. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BS 540 AND BTW BL 0 TO LBL 24.82 AT PASSENGER CABIN IAW B737-700 51-10-02. SEE INDIVIDUAL SIGNOFFS BELOW AS RII

Part: STRIP — DETERIORATED (CABIN) · airframe 52,547 hrs · 33,631 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (6 EA) 2022-426866 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-15-400-802;[02] TASK COMPLETED

Part: BRACKET — CRACKED (NLG) · airframe 52,547 hrs · 33,631 cycles

CRACK SUPPORT BRACKET AFT POSITION ON NOSE LANDING GEAR 2022-426894 / [01] REPLACED SUPPORT BRACKET AFT POSITION ON NOSE LANDING GEAR IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED SUPPORT BRACKET AFT POSITION ON NOSE LANDING GEAR IAW B737-700 SRM 51-40-02-0G-0

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,547 hrs · 33,631 cycles

CRACK FLOOR STRUCTURE INTERCOSTAL LOCATED BS 540 AND BTW BL 0 TO RBL 24.82 AT PASSENGER CABIN 2022-426873 / [01] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BS 540 AND BTW BL 0 TO RBL 24.82 AT PASSENGER CABIN IAW B737-700 51-10-02. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BS 540 AND BTW BL 0 TO RBL 24.82 AT PASSENGER CABIN IAW B737-700 51-10-02. SEE INDIVIDUAL SIGNOFFS BELOW. AS RII

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,547 hrs · 33,631 cycles

INOP POWER SUPPLY LT SIDE M1673 ON LOWERED CEILING ENTRY AT AFT GALLEY AREA 2022-426829 / [01] REPLACED EMERGENCY LIGHT POWER SUPPLY LT SIDE M1673 ON LOWERED CEILING ENTRY AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-06-960-805. <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — DEBONDED (R/H WING) · airframe 52,547 hrs · 33,631 cycles

CUSTOMER REQUEST - DEBONDED EXISTING REPAIR ON OB AFT FLAP UPPER SURFACE I/B EDGE AT RT WING 2022-426805 / [01] TOOL USED: CALIPER P/N:500-193-30 S/N:0000285 DUE DATE: 10-DEC-22;[02] TOOL USED BOND TESTER P/N: S-3; S/N: 064; DUE DATE: 19-JUL-23.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24-FEB-23.;[04] TOOL USED BOND TESTER P/N: S-3; S/N: 064; DUE DATE: 19-JUL-23.;[05] REPAIRED OB AFT FLAP UPPER SURFACE I/B EDGE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. TOOL USED: HOT BONDER PN:HCS9200B-AV SN: 18196021 DUE DATE 16/JAN/23. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] CORRECTIVE ACTIONS 5 ENTERED IN ERROR. <BR>THE CORRECT IS: PERFORMED PERMANENT REPAIR ON OB AFT FLAP UPPER SURFACE I/B EDGE AT RT WING DUE TO NO EXCEED 200 SI. IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. TOOL USED: HOT BONDER PN:HCS9200B-AV SN: 18196021 DUE DATE 16/JAN/23. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED

Part: SLIDE — LOOSE (L1 DOOR) · airframe 52,433 hrs · 33,561 cycles

FWD ENTRY SLIDE FELL OUT OF CONTAINER UPON DOOR OPENING ; SLIDE DID NOT DEPLOY / [01] INSPECT SLIDE AND REMOVE FORM DOOR TO REPACK PER MM 25-66-01-400-804 OK FOR SERVICE

Part: LIGHT — INOPERATIVE · airframe 51,981 hrs · 33,270 cycles

SEVERAL EMERGENCY LIGHTS IN FWD CABIN INOP / [01] R&R EMERGENCY LIGHTS BATTERY PACK M1674 PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (L/H OVERWING) · airframe 51,881 hrs · 33,202 cycles

L/H OVERWING EXIT LOCATOR; ESCAPE HACTH AND ESCAPE LIGHT INOP / [01] R&R POWER SUPPLY BATTERY PACK (M1668); OPS NORMAL AT THIS TIME. 737 AMM 33-51-06.

Part: LAMP — INOPERATIVE (EXIT SIGN) · airframe 51,881 hrs · 33,202 cycles

FWD EMERGENCY EXIT SIGN HAS MULTIPLE BULBS OUT / [01] RELAMPED FWD EXIT SIGN; OPS NORMAL AT THIS TIME. 737 AMM 33-51-00.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 50,630 hrs · 32,418 cycles

SUPPLEMENTAL INFORMATION: L2 SLIDE FELL OUT ; L2 DOOR SLIDE FELL OT OF SSEL / [01] RESECURED L2 DOOR SLIDE IAW AMM 25-66-01. A/C OK FOR SVC.

Part: NONE — MISSING (RH OVERWING) · airframe 50,202 hrs · 32,158 cycles

RIGHT OVER WING EXIT LOWER FORWARD EMERGENCY EXIT LIGHT LENS MISSING. ; / [01] INSTALLED LENS PER AMM 33-51-01

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 49,300 hrs · 31,643 cycles

AFT L2 DOOR SLIDE GAUGE COVER IS LOOSE ; / [01] SECURED FT L2 DOOR SLIDE GAUGE COVER REF MM25-66-01

Part: SUPPORT BRACKET — CRACKED (AFT GALLEY) · airframe 48,987 hrs · 31,460 cycles

AFT GALLEY SERVICE DOOR LINER PAN CRACKED ON FWD ATTACH SUPPORT ; / REMOVED AND REPLACED CRACKED PAN SUPPORT BRACKET I.A.W. SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 48,257 hrs · 31,048 cycles

EMERGENCY AREA LIGHTS AT ROW 6;9;14 ABC INOP / REMOVED AND REPLACED BATTERY PACK M2335 PER AMM 33-51-06 OPS CHECK GOOD

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 48,206 hrs · 31,017 cycles

THE LIGHT COVER (LENS) FOR THE LIGHT UNDER THE OVERHEAD BIN ABOVE SEAT 9C HAS FALLEN OUT. (EMERGENCY LIGHT) / REINSTALLED EMERGENCY LIGHT LENS COVER PER 33-51-21; LITE OPS CHECK GOOD;

Part: ESCAPE ROPE — CORRODED (EMERGENCY EXIT) · airframe 47,393 hrs · 30,527 cycles

LT EMERGENCY EXIT DOOR ESCAPE STRAP HOOK HAS EVIDENCE OF SURFACE CORROSION. / REMOVED AND REPLACED LT EMERGENCY EXIT DOOR ESCAPE STRAP AS PER B737-7 AMM 25-61-10-000-802 AND AMM 25-61-10-400-802.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 47,982 hrs · 30,879 cycles

FWD ENTRY DOOR EMERGENCY SLIDE GIRT BAR DIFFICULT TO ENGAGE IN FLOOR BRACKET. ADJUSTED SLIP PER SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 47,705 hrs · 30,717 cycles

FWD ENTRY DOOR ESCAPE SLIDE PERTRUDING FROM COVER. RE-INSTALLED FWD ENTRY ESCAPE SLIDE, PER AMM 25-6-01. OK FOR SERVICE STSLM Q6TR841X.

Part: FRAME — DAMAGED (FWD CARGO) · airframe 47,393 hrs · 30,527 cycles

R/H FWD CARGO FRAME AT STA 420 BETWEEN STR22R - STR23R UPPER FLANGE WITH (2 EACH) ELONGATED HOLES AT FASTENER LOCATION. PREVIOUS REWORK NOT APPLICABLE PER SRM; REFERENCE N/R W50072 / CUTOUT DAMAGE AREAS AT FWD CARGO FRAME STA.420; BETWEEN STR21R - 24R; AND INSTALLED REPAIR REF. AAR RES-WI # 2016199-13 REV IR AND EA NO. 20-153-01771 REV IR.

Part: SKIN — DENTED (BS 251 S17L) · airframe 47,393 hrs · 30,527 cycles

DENT ON FUSELAGE SKIN BS 251+5; 5' ABOVE STR 17L (EXISTING DENT T874699 WITH EVIDENCE OF FURTHER DAMAGE) / CUT OUT DAMAGE AREA AND INSTALLED REPAIR AT FUSELAGE SKIN STA. 251.6 TO 259.5 AND BETWEEN STR15L AND STR.18L REF. AAR RES-WI # 2016200-8 REV IR AND EA. NO. 20-153-01686 REV IR.

Part: WASHER — CORRODED (VERTICAL STAB) · airframe 47,393 hrs · 30,527 cycles

VERTICAL STABILIZER R/H AFT O/B SPAR NUT WASHERS CORRODED( 2EA) / RECEIVED TWO (2EA) WASHERS FOR VERTICAL STAB. R/H AFT O/B SPAR (NUT SIDE) TO BE INSTALLEDON CUSTOMER CARD J753-480-00-00

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 221CF FACESHEET DAMAGED. CLEANED & REPAIRED DAMAGED AT FLOOR PANEL NR 221CF PER B737 SRM 53-00-50-2R-1 MATERIAL USED RESIN 50-A PO NR 1688495 AND FIBERGLASS PO 1480720.

Part: WASHER — CORRODED (VERTICAL STAB) · airframe 47,393 hrs · 30,527 cycles

VERTICAL STABILIZER R/H AFT I/B SPAR NUT WASHERS CORRODED( 2EA) / RECEIVED TWO (2EA) WASHERS FOR VERTICAL STAB. R/H AFT I/B SPAR (NUT SIDE) TO BE INSTALLED ON CUSTOMER CARD J753-480-00-00

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 222CF FACESHEET DAMAGED. CLEANED & REPAIRED DAMAGED AT FLOOR PANEL NR 222CF PER B737 SRM 53-00-50-2R-1 MATERIAL USED RESIN 50-A PO NR 1688445 & FIBERGLASS PO NR 1480720.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 221AF FACESHEET DAMAGED. CLEANED & REPAIRED DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221AF UPPER SURFACE AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO NR 1480720 AND PO NR 1688495.

Part: WASHER — CORRODED (VERTICAL STAB) · airframe 47,393 hrs · 30,527 cycles

VERTICAL STABILIZER L/H AFT O/B SPAR NUT WASHERS CORRODED( 2EA) / RECEIVED TWO (2EA) WASHERS FOR VERTICAL STAB. L/H AFT O/B SPAR (NUT SIDE) TO BE INSTALLED ON CUSTOMER CARD J753-480-00-00

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 221BF FACESHEET DAMAGED. CLEANED AND REPAIRED DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221BF UPPER SURFACE AS PER B737 SRM 53-00-50-2R-1. MATERIAL USED PO NR 1480720 AND PO 1688495.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 221DF FACESHEET DAMAGED. CLEANED & REPAIRED DAMAGED AREA AT FLOOR PANEL NR 221DF PER B737 SRM 53-00-50-2R-1 MATERIAL USED RESIN 50-A PO NR 1688495 FIBERGLASS PO NR 1480720.

Part: FLOOR SKIN — DENTED (BS 255) · airframe 47,393 hrs · 30,527 cycles

COCKPIT FLOOR DENTED AT STA 255.6. REPAIRED DENTED COCKPIT FLOOR AT STA 255.6, AS PER SWA EA NR: 1-A53-33179.

Part: FLOOR PANEL — DAMAGED (FWD WET AREA) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 222DF FACESHEET DAMAGED. CLEANED & REPAIRED DAMAGED AT FLOOR PANEL NR 222DF PER B737 SRM 53-00-50-2R-1. MATERIAL USED RESIN 50-A PO 1688495 & FIBERGLASS PO 1480720.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,393 hrs · 30,527 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 221EF FACESHEET DAMAGED. CLEANED AND REPAIRED DAMAGED AREA AT FLOOR PANEL NR 221EF PER B737 SRM 53-00-500-2R-1. MATERIAL USED RESIN 50-A PO NR 1688495.

Part: FRAME — PUNCTURED (BS 500C) · airframe 47,393 hrs · 30,527 cycles

FRAME AT STA 500C PUNCTURED BETWEEN S-11L AND S-13L. REPAIRED PUNCTURE AT FRAME AT STA 500C BETWEEN S-11L AND S-13L, AS PER B737-700 SRM 53-00-07-2R-1.

Part: DOME NUT — DAMAGED (ANTENNA MOUNT) · airframe 47,393 hrs · 30,527 cycles

DAMAGED DOMENUT AT #1 ADF ANTENNA MOUNTING AREA REPAIR PER SRM / ACCOMPLISHED ADF ANTENNA MOUNTING REPAIR STRAP REF B737-700 SRM 53-40-01-2R-1 STEP 4 FIG 203 DETAIL 'A'

Part: CHANNEL — CORRODED (BS 727B-767) · airframe 47,393 hrs · 30,527 cycles

CORROSION AFT CARGO RT Z CHANNEL FROM STA 727B TO STA. 767 RBL 21' AND WL 153.8. REMOVED AND REPLACED RT ZEE CHANNEL ON AFT CARGO COMP FROM STA 727' TO 767', PER REF B737 SRM 51-40-02-0G-0 AND DRAWING 146A7500.

Part: INTERCOSTAL — BENT (BS 787-807 S21L) · airframe 47,393 hrs · 30,527 cycles

AFT CARGO COMPARTMENT INTERCOSTAL BETWEEN STA 787 AND STA 807 AT S-21L UPPER FWD CORNER BENT / STRAIGHTENED BENT AREA ON INTERCOASTAL TO ORIGINAL CONTOUR; UPPER FWD CORNER PER BAC 5300-2 AND PERFORMED HFEC INSPECTION AT REWORKED ARE; NO CRACK PER NDT 51-00-00 PROC 23

Part: CHANNEL — CORRODED (BS 727B-807) · airframe 47,393 hrs · 30,527 cycles

CORROSION AFT CARGO LT Z CHANNEL FROM STA 727B TO STA 807 LBL 21' AND WL 153.8. REMOVED AND REPLACED Z CHANNEL AT AFT CARGO COMP LT FROM STA 727 TO STA 847. USED SAME SPLICE BETWEEN STA 727E TO STA 747, AS PER REF B737-700 SRM 53-00-53-2R-6.

Part: PLATE — CORRODED (FWD CARGO) · airframe 47,393 hrs · 30,527 cycles

**CORROSION** FWD CARGO COMPARTMENT R/H SIDEPLATE SECTION BETWEEN STA-492 TO STA-500A UPPER SURFACE WITH CORROSION AT S-26R; WL 155 / REMOVED AND REPLACED SIDEPLATE AT FWD CARGO COMPARTMENT R/H BETWEEN STA 492-STA500A REF B737-7 SRM 51-40-02-0G-0

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 47,393 hrs · 30,527 cycles

CRACK RT HORIZONTAL STAB RIB NR 4 AT STIFFENER NR 3. INSTALLED HORIZONTAL STABILIZER MACHINE INSPAR RIB LOWER CHORD AND VERTICAL STIFFENER CRACK REPAIR AT RIB NR 4 STIFFENER NR 3, RT HORIZONTAL, PER REF B737 SRM 55-10-09-2R-5 REP 5.

Part: CHANNEL — CORRODED (BS 500A-500B) · airframe 47,393 hrs · 30,527 cycles

CORROSION, FWD CARGO RT SIDE PLATE UPPER SURFACE FROM STA-500A TO STA-500B SEVERAL SPOTS WITH CORROSION AT S-26R; WL 155. REMOVED AND REPLACED Z-CHANNEL (SIDEPLATE) AT FWD CARGO RT FROM STA500A-STA500D, REF B737-7 SRM 51-40-02-0G-0.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 47,393 hrs · 30,527 cycles

CABIN CENTER SECTION FLOOR PANEL 241DF HAS PEELED UPPER SURFACE FIBERS. DOT 124-003. CLEANED AND REPAIRED DAMAGE AREA AT CABIN CENTER SECTION FLOOR PANEL 241DF, REF B737-7 SRM 53-00-50-2R-1 REPAIR 1. MATERIAL USED RESIN PO 1688495 AND FABRIC PO: 148720.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 47,393 hrs · 30,527 cycles

CABIN CENTER SECTION FLOOR PANEL 241AF IS DAMAGED. DOT 124-001. CLEANED AND REPAIRED DAMAGE AREA AT CABIN CENTER SECTION FLOOR PANEL 241AF, REF B737-7 SRM 53-00-500-2R-1 REPAIR 1. MATERIAL USED RESIN PO: 168495 AND FABRIC PO: 1480720.

Part: OUTLET — DAMAGED (R1 DOOR) · airframe 47,393 hrs · 30,527 cycles

R1 DOOR POWER OUTLET BOX IS DAMAGED. / REPLACED R-1 DOOR POWER OUTLET BOX AS PER B737-700 SRM 51-40-02-0G-0

Part: SKIN — DENTED (BS 907) · airframe 47,393 hrs · 30,527 cycles

5 DENT ON FUSELAGE SKIN COMMON TO BS 907, 4" ABOVE STR20 L. INSTALLED DOUBLER REPAIR ON FUSELAGE SKIN AT STA 907, 4" ABOVE STRINGER 20L, PER REF RES 2016200-1, REV-IR AND EA NR 20-153-01549 REV-1.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,141 hrs · 28,441 cycles

L/H EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 6. / R&R LENS IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,141 hrs · 28,441 cycles

L/H EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 6. R&R LENS IAW MM.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 43,307 hrs · 27,894 cycles

RT WING UPPER INBOARD STABILIZER LINK FORWARD ATTACHMENT BRACKET CRACKED ACCESS PANEL 651AT. R&R BRACKET PER SRM.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 43,307 hrs · 27,894 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,875 hrs · 27,608 cycles

CABIN EMERGENCY LIGHTS INOP AT LOCATION M1674. R&R LIGHTS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,875 hrs · 27,608 cycles

CABIN EMERGENCY LIGHTS INOP AT LOCATION M1672. R&R LIGHTS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,875 hrs · 27,608 cycles

CABIN EMERGENCY LIGHTS INOP AT LOCATION M1673. R&R LIGHTS PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 42,875 hrs · 27,608 cycles

RT HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED RT HORIZ STAB FWD UPPER SLIDE SEAL IAW MM 53-31-31-000-802 STEPS 2.D.;2.E. AND MM 52-31-31-400-802 STEPS 3.D.;3.E.

Part: ANGLE — CRACKED (ASD) · airframe 42,875 hrs · 27,608 cycles

AFT SERVICE DOOR FWD ATTACH ANGLE ON LOWER HINGE ACCESS PANEL 844DZ IS CRACKED. / REMOVED AND REPLACED CRACK LOWER HINGE ON ACCESS PANEL 844DZ IAW SRM 51-40-02-0G-0. 59419U 01/09/19. 53838C 09JAN19 SRM 51-40-05-0G-0; AND IPC 52-41-31-10.

Part: BRACKET — CRACKED (LEFT WING) · airframe 42,875 hrs · 27,608 cycles

BULB SEAL RETAINER BRACKET IS CRACKED AT LOWER FASTENER HOLE AT LEFT WING FIXED TE PANEL JUST AFT OF THE PYLON. MARKED / REMOVED AND REPLACED BULB SEAL RETAINER BRACKET AT LWR LEFT WING FIXED T/E PANEL AFT OF PYLON. IAW SOPM 20-50-01 AND SRM 51-40-02-0G-0 84036U 31DEC18

Part: RETAINER — CRACKED (RIGHT WING) · airframe 42,875 hrs · 27,608 cycles

BULB SEAL RETAINER IS CRACKED AT LOWER FASTENER HOLE AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON. MARKED / REMOVED AND REPLACED BULB SEAL RETAINER AT RIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON I.A.W SRM 51-40-02-0G-0 AND SOPM 20-50-01

Part: STRAP — CORRODED (LT MLG WW) · airframe 42,875 hrs · 27,608 cycles

PRESSURE DECK REINFORCING STRAP CORRODED AT BS 687, LBL 62, ABOVE MAIN WHEEL WELL. R&R STRAP PER SRM AND DWG.

Part: SPAR — CORRODED (RIGHT WING) · airframe 42,875 hrs · 27,608 cycles

***CORROSION*** ON AFT SPAR AROUND LOWER BONDING JUMPER AT RIGHT WING BOOST PUMP TANK2 AFT. MARKED / ACESSED HYDRAULIC LINES AS REQUIRED TO BLEND CORROSION ON RT WING AFT SEAL AT BOOST PUMP TANK 2 AFT; IAW AMM 20-10-51-000-801. BLENDED CORROSION; FINAL DIMENSION IS 3.8' X 2.6' X .068' DEEP; REMAINING THICKNESS IS .607' WHICH IS WITHIN ALLOWABLE LIMITS PER BOEING DWG 112A1101 AND SRM 57-20-10-1A-3; FIAR PEENED BLENDED AREA AND RESTORED FINISH PER SOPM 20-10-03; REINSTALLED HYDRAULIC LINES AND PERFORMED SATISFACTORY LEAK CHECK. NO LEAKS NOTED IAW AMM 20-10-51-400-804

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 42,875 hrs · 27,608 cycles

PANEL 193AR HAS A BULGE IN THE EXTERNAL SKIN; 8' FROM FORWARD EDGE; 12.5' FROM O/B EDGE / PANEL 193AR BULGE IN EXTERNAL SKIN 8' FROM FWD EDGE 12.5' FROM O/B EDGE WAS REPAIRED IAW SRM 51-70-05-2R-1

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

SEAT TRACK, CORRODED BETWEEN BS 727B TO BS 887, RBL 45. R&R SEAT TRACK PER SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

SHEAR TIE CORRODED AT BS 667, RBL 69. REPAIRED SHEAR TIE IAW EA & ER.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 42,875 hrs · 27,608 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE PER ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294 TO BS 312, RBL 16. R&R FLOOR SUPPORT PER SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, RBL 32. R&R FLOOR SUPPORT PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 315 TO BS 344, RBL 54. R&R MOPSILL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

CLIP ANGLE CRACKED AT BS 293, RBL 53. R&R CLIP ANGLE PER SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FLOOR SUPPORT CRACKED AT STA 328 TO STA 344, LBL 46, WL 208. R&R SUPPORT PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FLOOR SUPPORT CRACKED AT STA 277 TO STA 294, RBL 1, WL 208. R&R SUPPORT PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO BS 360, LBL 12. R&R SUPPORT IAW SRM AND DWG 141A5230.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FLOOR SUPPORT CRACKED AT STA 312 TO STA 328, LBL 46, WL 208. R&R SUPPORT PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 42,875 hrs · 27,608 cycles

AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER BROKEN. R&R COVER PER CMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FUSELAGE SKIN DENT AT BS 1016+15, STR 15L. REPAIRED SKIN PER ER & EA.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FUSELAGE SKIN DENT AT BS 1016+3, STR 13L. REPAIRED SKIN ER & EA.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,875 hrs · 27,608 cycles

FUSELAGE SKIN DENT AT BS 1016+10, STR 16L. REPAIRED SKIN PER EA.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 42,875 hrs · 27,608 cycles

LOWER VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 29.83 TO LBL 46.64. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 42,875 hrs · 27,608 cycles

LOWER VAPOR BARRIER CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 35. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 42,597 hrs · 27,436 cycles

LT WING AFT SPAR VAPOR BARRIER CRACKED BETWEEN LBL 29.83 TO LBL 46.64. REPAIRED BARRIER IAW EA.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 42,597 hrs · 27,436 cycles

LEFT WING LEADING EDGE LOWER PANEL 521GB HAS DELAMINATION ON THE LEADING EDGE OF THE PANEL. / REMOVED AND REPLACED PER AMM. 57-41-02

Part: CONTAINER — DETACHED (L1 DOOR) · airframe 41,749 hrs · 26,879 cycles

L1 DOOR ESCAPE SLIDE CONTAINER DETACHED. STOWED SLIDE IAW TC.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 41,646 hrs · 26,817 cycles

L1 DOOR EVAC SLIDE PRESS INDICATOR BELOW LIMITS. R&R SLIDE ASSY PER MM.

Part: PROXIMITY SENSOR — INOPERATIVE (LE SLAT) · airframe 41,596 hrs · 26,785 cycles

DECLARED EMERGENCY, LEADING EDGE FLAPS TRANSIT LIGHT INDICATION WITH LOW AIRS PEED ALERT. R&R NR 1 LE SLAT INBD PROX POSITION SENSOR.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 41,520 hrs · 26,739 cycles

CRACK INDICATION AT DENT ON LEADING EDGE OF AFT CARGO BIN DOOR SCUFF PLATE PER NDT MANUEL PART 6; 51-00-00 PRO.14 / REMOVED AND REPLACED AFT CARGO BIN DOOR SCUFF PLATE PER SRM 53-60-15

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,898 hrs · 26,344 cycles

R2 DOOR EXRTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,898 hrs · 26,344 cycles

L1 DOOR EXTERNALEMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,898 hrs · 26,344 cycles

LEFT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: SKIN — CORRODED (BS 972) · airframe 40,898 hrs · 26,344 cycles

FUSELAGE SKIN AROUND AFT POTABLE WATER DRAIN PORT CORRODED AT BS 972, LBL 7.8. REPAIRED THE SKIN IAW SRM AND EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,575 hrs · 26,131 cycles

LT EXTERIOR OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 38,774 hrs · 24,998 cycles

R/H WHEEL WELL BAY 7 RIGHT HAS 14 INCH CRACK VAPOR BARRIER / APPLIED INTERIM PATCH REPAIR PER SRM 57-10-10-2R-2.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 36,824 hrs · 23,743 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,714 hrs · 23,676 cycles

EMERGENCY OVERWING ESCAPE GROUND ILLUMINATION LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,714 hrs · 23,676 cycles

AFT OF FORWARD GALLEY EMERGENCY BATTERY INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 36,714 hrs · 23,676 cycles

LT EMERGENCY LIGHT LENS MISSING AT ROW 4. INSTALLED LENS PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

INTERCOSTAL CRACKED BETWEEN BS 400 TO BS 420, LBL 22. R&R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

ANGLE CORRODED AT BS 847+3, STR 25L. REPAIRED ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

LONGITUDINAL FLOOR BEAM FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, RBL 22. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 22. R&R INTERCOSTAL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FRAME CRACKED AT BS 400 STR 8R. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 36,714 hrs · 23,676 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STATION 120.3, 3RD VERTICAL STIFFENER FROM LEADING EDGE. REPAIRED RIB IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 36,714 hrs · 23,676 cycles

LT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED JUST INBOARD OF NR 1 PYLON AFT TIP. R&R WAFFLE PLATE PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

SEAT TRACK CORRODED BETWEEN BS 480 TO BS 520, RBL 24.5. R&R SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

INTERCOSTAL CRACKED AT BS 335, LBL 45. R&R INTERCOSTAL PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

SEAT TRACK CORRODED BETWEEN BS 520 TO BS 540, RBL 24.5. R&R SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

INTERCOSTAL CRACKED AT BS 321, LBL 45. R&R INTERCOSTAL PER SRM.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FRAME SPLICE CORRODED AT BS 727D, BETWEEN STR 24R TO STR 25R. R&R SPLICE IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, RBL 24.5. REPAIRED SEAT TRACK IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

R1 DOOR FORWARD STUB FRAME SKIN CRACKED AT BS 296, WL 208. R&R STUB FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FUSELAGE SKIN CORRODED BETWEEN BS 294 TO BS 328, WL 209. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FLOORBEAM CORRODED AT BS 312 BL 0. REPAIRED FLOORBEAM IAW ER AND EA.

Part: TIE DOWN — CORRODED (L1 DOOR) · airframe 36,714 hrs · 23,676 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING TIE DOWN CORRODED. R&R TIE DOWN PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 312 TO BS 328, LBL 10. R&R SUPPORT PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

THRESHOLD SUPPORT Z ANGLE CRACKED BETWEEN BS 310 TO BS 345, LBL 63. R&R Z ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FLOORBEAM CORRODED AT BS 328, LBL 22. REPAIRED FLOORBEAM IAW EA.

Part: TIE DOWN — CORRODED (L1 DOOR) · airframe 36,714 hrs · 23,676 cycles

L1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR FITTING TIE DOWN CORRODED. R&R TIE DOWN PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FUSELAGE SKIN Z ANGLE CORRODED BETWEEN BS 310 TO BS 340, LBL 60. R&R Z ANGLE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 312 TO BS 328, RBL 11. R&R SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 328 TO BS 344, LBL 10. R&R SUPPORT PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

INTERCOSTAL CORRODED AT BS 363, LBL 21. R&R INTERCOSTAL IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,714 hrs · 23,676 cycles

R/H HORIZONTAL STABILIZER 4TH FROM FORWARD RIB CRACKED AT STAB STA 92.70. REPAIRED RIB IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY LOWER BULKHEAD STANCHION SUPPORT CLIP CRACKED AT BS 867, LBL 16. R&R CLIP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY RBL22 FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727D+3, LBL 3. R&R SUPPORT IAW EA AND SRM.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 492 TO 500A, RBL 22. R & R SHIELD IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY SUPPORT CLIP CRACKED AT BS 500D, STR 19R. R&R CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR SUPPORT JOGGLE CORRODED AT BS 727D+3, LBL 12. REPAIRED JOGGLE IAW SRM & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727D+3, LBL 7. REPAIRED SUPPORT IAW EA AND SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 867 TO BS 887, RBL 22. R&R PLATE IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR SPLICE STRAP CORRODED AT BS 772, BETWEEN RBL 22 TO LBL 22. R&R STRAP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY SIDEWALL FRAME SUPPORT CORRODED AT BS 727D, LBL 25. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 396 TO BS 500, LBL 22. R&R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

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

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 22 TO LBL 22. R&R ANGLE IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY AFT OF CARGO DOOR SHIELD CORRODED AT BS 847, RBL 20. R&R SHIELD PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, LBL 8. REPAIRED SUPPORT IAW EA AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY BULKHEAD SUPPORT ANGLE FITTING CRACKED AT BS 947, LBL 10. R&R FITTING PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 22. R&R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, LBL 17. REPAIRED SUPPORT IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 396 BS 420, RBL 22. R&R SUPPORT IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

FORWARD CARGO BAY SUPPORT CLIP CRACKED AT BS 500D, STR 19L. R&R CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 36,714 hrs · 23,676 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847. R&R WEB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,714 hrs · 23,676 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 92.70, 3RD FROM FORWARD. REPAIRED RIB IAW SRM.

Part: FASTENER — LOOSE (L2 DOOR) · airframe 36,714 hrs · 23,676 cycles

L2 DOOR ESCAPE SLIDE PACK GIRT BAR RETAINER FASTENERS LOOSE. R&R RETAINER ASSEMBLY IAW SRM.

Part: RETAINING CLIP — OUT OF LIMITS (R2 DOOR) · airframe 36,714 hrs · 23,676 cycles

R2 DOOR ESCAPE SLIDE PACK GIRT BAR RETAINER CLIPS RETAINER OUT OF LIMIT. R&R CLIPS PER SRM.

Part: RETAINING CLIP — OUT OF LIMITS (L2 DOOR) · airframe 36,714 hrs · 23,676 cycles

L2 DOOR ESCAPE SLIDE PACK GIRT BAR RETAINER CLIPS RETAINER OUT OF LIMIT. R&R CLIPS PER SRM.

Part: RETAINING CLIP — OUT OF LIMITS (R1 DOOR) · airframe 36,714 hrs · 23,676 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE PACK GIRT BAR RETAINER CLIPS OUT OF LIMIT. R&R CLIPS PER SRM.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 36,714 hrs · 23,676 cycles

R1 DOOR ESCAPE SLIDE PACK GIRT BAR RETAINER FASTENERS LOOSE. R&R RETAINERS PER SRM.

Part: RETAINING CLIP — OUT OF LIMITS (L1 DOOR) · airframe 36,714 hrs · 23,676 cycles

L1 DOOR ESCAPE SLIDE PACK GIRT BAR RETAINER CLIPS RETAINER OUT OF LIMIT. R&R CLIPS PER SRM.