N401WN

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 76,507 hrs · 45,350 cycles

R/H OVERWING EXIT FWD EMERGENCY LIGHT INOP.<[01] RELAMPED PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 76,507 hrs · 45,350 cycles

L/H OVERWING EXIT FWD EMERGENCY LIGHT INOP.<[01] RELAMPED PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 76,507 hrs · 45,350 cycles

R/H OVERWING EXIT SIDEWALL LIGHT INOP<[01] RELAMPED PER AMM 33-51-01

Part: ENCLOSURE — CRACKED (DOOR SLIDE) · airframe 76,507 hrs · 45,350 cycles

FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT HAS 2 CRACKED ISOLATORS<[01] R&R FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATORS IAW AMM 52-41-00.

Part: STRINGER — CRACKED (LT WING) · airframe 76,427 hrs · 45,306 cycles

LEFT WING HAS CRACK INDICATION ON STRINGER 14 ON THE UPPER SKIN AT THE CHORDWISE SKIN SPLICE NEAR WS 579 FASTENERS NR 1 & 2 PER NDT PART 6 57-10-60 FIG 1SHEET 6. PERFORMED NDT INSPECTION OF FASTENERS 1 AND 2 AT WS 579; STRINGER 14 CHORD SPLICE PER 51-00-00 PROCEDURE 9 AND 51-00-00 PROCEDURE 23 PER BOEING NDT 57-10-60. NO FAULTS FOUND ON WING INTERNAL INSP. AT STRINGER 14; WS 579.;[03] EA 23-157-03471 C/W

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 76,282 hrs · 45,214 cycles

FRWD EMERGENCY LIGHT BATTERY PACK M1675 INOP / [01] R&R L/H FRWD EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD;[02] R&R L/H FRWD EMERGENCY LIGHT BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECK GOOD;[03] CW

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 75,547 hrs · 44,739 cycles

AFT GALLEY EMERGENCY EXIT LIGHT COVER SPRING BROKEN.<[01] R&R'D AFT GALLEY EMERGENCY EXIT LIGHT COVER PER SIP

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 75,547 hrs · 44,739 cycles

L1 DOOR CLOSE ASSIST HANDLE IS LOOSE.<[01] SECURED L1 DOOR CLOSE ASSIST HANDLE PER AMM 52-11-00.

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 75,547 hrs · 44,739 cycles

CABIN EMERGENCY LIGHT COVER NOT SECURE AT 13DEF AND 6DEF.<[01] INSTALLED NEW EMERGENCY LIGHT COVER LENSES AT 13DEF AND 6DEF PER AMM 33-51-03

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 75,349 hrs · 44,607 cycles

L-1 DOOR EMERGENCY EXIT SIGN LENS IS MISSING.<[01] INSTALLED EXIT SIGN LENS PER AMM 33-51-01.

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 74,469 hrs · 44,067 cycles

PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02;[02] C/W INSPECTIONS

Part: SIGN — BROKEN (ZN 200 FUS TOP) · airframe 74,361 hrs · 43,996 cycles

EMER OVER WING EXIT SIGN ON CEILING BROKEN<[01] REMOVED AND REPLACED EMER EXIT SIGN IAW AMM 33-51-01. OPS CHECK GOOD.

Part: SKIN — ELONGATED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

REJECT. ELONGATED HOLE LOWER SURFACE SKIN COUNTERSINK AT LEVEL ORSS 261 TRAILING EDGE AT LT WING (4 EA) 2022-688572<[01] PERFORMED OVERZISE COUNTERSINK ON 4 HOLES LOCATED LOWER SURFACE SKIN AT LEVEL ORSS 261 TRAILING EDGE AT LT WING (4 EA) IAW B737-700 SRM 51-40-08 TABLE A;[02] CERTIFIED RII WORK PERFORMED.

Part: CLAMP — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK ON CLIP LOCATED AT FWD CARGO COMPARTMENT AT BS400 AFT FACE AT LEVEL OF STRG26L 2022-688568<[01] REPLACED CLIP LOCATED AT FWD CARGO COMPARTMENT AT BS400 AFT FACE AT LEVEL OF STRG26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV B<BR>SEE INDIVIDUAL SING OFFS BELOW.;[02] REPLACED CLIP LOCATED AT FWD CARGO COMPARTMENT AT BS400 AFT FACE AT LEVEL OF STRG26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV B <BR>SEE INDIVIDUAL SING OFFS BELOW.<BR>RII

Part: CLAMP — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK ON CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS440 AFT FACE AT LEVEL OF STRG26L 2022-688569<[01] REPLACED CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS440 AFT FACE AT LEVEL OF STRG26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV B<BR>SEE INDIVIDUAL SING OFFS BELOW.;[02] REPLACED CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS440 AFT FACE AT LEVEL OF STRG26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV B <BR>SEE INDIVIDUAL SING OFFS BELOW.<BR>RII

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CORROSION ON SHIELD LOCATED BTW BS492 AND BS500A AT LEVEL OF STRG26R WL156.5 AND RBL21.8 IN FWD CARGO COMPARTMENT 2022-688566<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45 MG; S/ N: 130063701; DUE DATE: 16-JUN-23;[02] REPLACED SHIELD LOCATED BTW BS492 AND BS500A AT LEVEL OF STRG26R WL156.5 AND RBL21.8 IN FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080; SHEET 15; REV - SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SHIELD LOCATED BTW BS492 AND BS500A AT LEVEL OF STRG26R WL156.5 AND RBL21.8 IN FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080; SHEET 15; REV -<BR>RII ACCOMPLISHED <BR> SEE INDIVIDUAL SIGN OFFS BELOW.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 73,533 hrs · 43,472 cycles

CRACK INSPAR RIB LOC LE STA 120.30 AND 35 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER AT RT HORIZONTAL STABILIZER 2022-688563<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 13-MAY-23;[02] PERFORMED PERMANENT REPAIR LOC INSPAR RIB LOC LE STA 120.30 AND 35 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 55-10-09-2R-5 REPAIR 5; STEP 4; P; Q; R; S FIGURE 204; SHEET 1. MATERIAL USED: T-SECTION KIT: 55100003-01; ANGLE MATERIAL USED: BAC1490-2738; PO: 2022-127681; FILLER MATERIAL USED: 7075-T6 0.063? PO: 2020-203089 AND SHIM (2 E/A) MATERIAL USED: 7075-T6 0.020? PO: 2021-203786. CRACK LENGTH IS: 0.448 INCHES. TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21143495; DUE DATE: 29-JUN-23. SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] PERFORMED PERMANENT REPAIR LOC INSPAR RIB LOC LE STA 120.30 AND 35 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 55-10-09-2R-5 REPAIR 5; STEP 4; P; Q; R; S FIGURE 204; SHEET 1. MATERIAL USED: T-SECTION KIT: 55100003-01; ANGLE MATERIAL USED: BAC1490-2738; PO: 2022-127681; FILLER MATERIAL USED: 7075-T6 0.063? PO: 2020-203089 AND SHIM (2 E/A) MATERIAL USED: 7075-T6 0.020? PO: 2021-203786. CRACK LENGTH IS: 0.448 INCHES. TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21143495; DUE DATE: 29-JUN-23. SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>RII

Part: FASTENER — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK ON CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS500C AFT FACE AT LEVEL OF STRG26R 2022-688570<[01] REPLACED CLIP AND FASTENERS LOCATED AT FWD CARGO COMPARTMENT ON BS500C AFT FACE AT LEVEL OF STRG26R IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV A.<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED CLIP AND FASTENERS LOCATED AT FWD CARGO COMPARTMENT ON BS500C AFT FACE AT LEVEL OF STRG26R IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV A. <BR><BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SING OFF BELOW.

Part: SHIELD — ELONGATED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

ELONGATED HOLE OF SHIELD LOCATED ON AFT DOOR CUTOUT BTW BS847 AND BS867 AT LEVEL OF STRG25R WL156.4 AND RBL21 AT AFT CARGO COMPARTMENT 2022-688516<[01] REPLACED NEW SHIELD LOCATED ON AFT DOOR CUTOUT BTW BS847 AND BS867 AT LEVEL OF STRG25R WL156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET 13; REV A. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED SHIELD LOCATED ON AFT DOOR CUTOUT BTW BS847 AND BS867 AT LEVEL OF STRG25R WL156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET 13; REV A.<BR>RII ACCOMPLISHED <BR> SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: SPLICE STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOORBOARD SPLICE STRAP LOCATED ON BS727D PLUS 5IN ON WL156.4 AND BTW LBL21 AND RBL21 2022-688510<[01] REPLACED FLOORBOARD SPLICE STRAP LOCATED ON BS727D PLUS 5IN ON WL156.4 AND BTW LBL21 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;[02] REPLACED FLOORBOARD SPLICE STRAP LOCATED ON BS727D PLUS 5IN ON WL156.4 AND BTW LBL21 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9<BR>RII ACCOMPLISHED

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CORROSION ON SHIELD LOCATED FWD OF DOOR CUTOUT BTW BS767 AND BS794 AT LEVEL OF STRG25R WL156.4 AND RBL21 AT AFT CARGO COMPARTMENT 2022-688515<[01] REPLACED SHIELD WEB LOCATED FWD OF DOOR CUTOUT BTW BS767 AND BS794 AT LEVEL OF STR 25R WL156.4 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 SHEET 13 REV A.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS767 AT LEVEL OF STRG25R WL156.4 AND RBL21 IN AFT CARGO COMPARTMENT 2022-688509<[01] INSPECTION REJECT IN STEP 3<BR>SEE TTG8Q00GQ7R5;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS767 AT LEVEL OF STRG25R WL156.4 AND RBL21 IN AFT CARGO COMPARTMENT I.A.W. B737 SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 146A7500 REV. C;[03] CORRECTED STEP 2. REPLACED SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS767 AT LEVEL OF STRG25R WL156.4 AND RBL21 IN AFT CARGO COMPARTMENT I.A.W. B737 SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 146A7500 REV. C<BR>SEE INDIVIDUAL SING-OFFS BELOW;[04] CORRECTED STEP 3. REPLACED SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS767 AT LEVEL OF STRG25R WL156.4 AND RBL21 IN AFT CARGO COMPARTMENT I.A.W. B737 SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 146A7500 REV. C<BR>SEE INDIVIDUAL SIGN-OFFS BELOW;[05] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS847 AT LEVEL OF STRG25L WL156.4 AND LBL21 IN AFT CARGO COMPARTMENT 2022-688508<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 130060401 DUE DATE: 26-JAN-23;[02] INSPECTION REJECT IN STEP 5<BR>SEE TTG8Q00GQ6WE;[03] REPLACED SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS847 AT LEVEL OF STRG25L WL156.4 AND LBL21 IN AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING 146A7500 REV ?C?.<BR>SEE INDIVIDUAL SING-OFFS BELOW;[04] CORRECTED STEP 3. REPLACED SUPPORT ZEE LOCATED BTW BS727 PLUS 4 AND BS847 AT LEVEL OF STRG25L WL156.4 AND LBL21 IN AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING 146A7500 REV ?C?.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT LT WING 2022-688491<[01] REJECT. ELONGATED HOLE LOWER SURFACE SKIN COUNTERSINK AT LEVEL ORSS 261 TRAILING EDGE AT LT WING (4 EA). FAULT RAISED TTG8Q00GNDKE.;[02] FAULT TTG8Q00GNDKE HAS ALREADY BEEN CERTIFIED.;[03] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 115A2001 SHEET : 18 REV : ? SEE INDIVIDUAL SING-OFF BELOW.;[04] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 115A2001 SHEET : 18 REV : ? SEE INDIVIDUAL SING-OFF BELOW.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 73,533 hrs · 43,472 cycles

CRACK IN SPAR RIB LOCATED LE STA120.30 AND 27 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-688410<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00X12101V022235; CAL DUE DATE: 03-AUG-23 AND ELECTRONIC CALIPER P/N: 500-196-30; S/N: A20231610; CAL DUE DATE: 12-SEP-23[04] PERFORMED PERMANENT REPAIR LOC INSPAR RIB LE STA120.30 AND 27 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 55-10-09-2R-5 REPAIR 5; STEP 4; P; Q; R; S FIGURE 204; SHEET 1. <BR>MATERIAL USED: T-SECTION KIT: 55100003-01; ANGLE MATERIAL USED: BAC1490-2738; PO: 2022-127681; FILLER MATERIAL USED: 7075-T6 0.063? PO: 2020-203089 AND SHIM (2 E/A) MATERIAL USED: 7075-T6 0.020? PO: 2021-203786. CRACK LENGTH IS: 0.448 INCHES. TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21143495; DUE DATE: 29-JUN-23. SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>RII

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 229 AT LT WING 2022-688437<[01] REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED AT LEVEL IRSS 229 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9.SEE STEP SIGNOFF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 73,533 hrs · 43,472 cycles

CRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 269 TRAILING EDGE AT RT WING 2022-688466<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 115A2001 SHEET : 18 REV :? SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 115A2001 SHEET : 18 REV :? SEE INDIVIDUAL SIGN-OFF BELOW

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 73,533 hrs · 43,472 cycles

CRACK STRINGER 25R BS 540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 25R BS 540 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1;REPAIR 1;STEP K; SRM 51-40-02-0G-0. DWG 143A1215 REV - AND DWG 143A3230 REV A. AND DRAWING 143A7902 REV A. PERFORMED PERMANENT REPAIR ON STRINGER 25R BS 540 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1;REPAIR 1;STEP K; SRM 51-40-02-0G-0. DWG 143A1215 REV - AND DWG 143A3230 REV A. AND DRAWING 143A7902 REV A.

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 73,533 hrs · 43,472 cycles

CRACKED STRINGER 25L, BS 540, FWD CARGO COMPARTMENT. REPAIRED STRINGER 25L BTW BS520 TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 73,533 hrs · 43,472 cycles

CRACKED STRINGER 26R, BS 540, FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 26R BS 540 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1;REPAIR 1; DWG 143A1215 REV - AND DWG 143A3230 REV A.

Part: STRINGER — CRACKED (BS 540 S27R) · airframe 73,533 hrs · 43,472 cycles

CORRODED STRINGER 27R BS 540 AND WL 156, FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED ON STRINGER 27R BS 540 AND WL 156 FWD COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.

Part: PLATE — CRACKED (LT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 229 AT LT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE IRSS 229 LT WING IAW SRM 51-10-02 ITEM 9.

Part: STRINGER — CRACKED (BS 540 S27L) · airframe 73,533 hrs · 43,472 cycles

CRACKED STRINGER 27L, BS 540, FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 27L BS 540 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1;REPAIR 1; SRM 51-40-02-0G-0. DWG 143A1215 REV - AND DWG 143A3230 REV A.

Part: FASTENER — CRACKED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING 2022-688318<[01] REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SING OFF BELOW;[02] CORRECTED STEP 1 REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[03] TASK COMPLETED

Part: FASTENER — CRACKED (ZN 600 RIGHT WIN) · airframe 73,533 hrs · 43,472 cycles

CRACK ON ANGLE LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT RT WING 2022-688297<[01] REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SING OFF BELOW

Part: FITTING — CRACKED (ZN 600 RIGHT WIN) · airframe 73,533 hrs · 43,472 cycles

CRACK ON FITTING LOCATED AL LEVEL ORSS 271 TRAILING EDGE AT RT WING 2022-688300<[01] REPLACED FITTING LOCATED AL LEVEL ORSS 271 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CERTIFIED WORK PERFORMED.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING 2022-688318<[01] REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SING OFF BELOW;[02] CORRECTED STEP 1 REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[03] TASK COMPLETED

Part: SUPPORT BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK ON SUPPORT BRACKET LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING 2022-688311<[01] REPLACED SUPPORT BRACKET LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND DGW 115A2900; SHEET 1; REV-E.<BR><BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED SUPPORT BRACKET LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND DGW 115A2900; SHEET 1; REV-E. RII;SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 73,533 hrs · 43,472 cycles

CRACK ON ANGLE LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT RT WING 2022-688297<[01] REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL ORSS 271 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SING OFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 695 LBL0 WL 208.1 CENTER SECTION 2022-688143<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30; S/N:A21033538; DUE DATE: 25-SEP-23.;[02] REPLACED ANGLE AND FASTENERS ON FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 273A9110; SHEET 3; REV - DRAWING 273A9112-45;[03] CORRECTED STEP 2. REPLACED ANGLE AND FASTENERS ON FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 273A9110; SHEET 3; REV - DRAWING 273A9112 SHEET 30 REV. -;[04] CORRECTED STEP 2. REPLACED ANGLE AND FASTENERS ON FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 273A9110; SHEET 3; REV - DRAWING 273A9112 SHEET 30 REV. -

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK STIFFENER FLOOR STRUCTURE PLATE LOCATED AT BS 540 BETWEEN LBL 24.5 AND LBL 45 WL 208.1 CENTER SECTION 2022-688200<[01] REPLACED STIFFENER FLOOR STRUCTURE PLATE LOCATED AT BS 540 BETWEEN LBL 24.5 AND LBL 45 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-10-02; ITEM 9; SRM 51-40-02 AND DWG NO. 143A0060; SHEET 2; REV. B<BR>SEE INDIVIDUAL SING OFFS BELOW.;[02] TASK CARD COMPLETED RII CERTIFIED;[03] CORRECTED STEP 1. <BR>REPLACED STIFFENER FLOOR STRUCTURE PLATE LOCATED AT BS 540 BETWEEN LBL 24.5 AND LBL 45 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-10-02; ITEM 9; SRM 51-40-02 AND DWG NO. 143A0060; SHEET 2; REV. B <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] TASK CARD COMPLETED RII CERTIFIED

Part: FASTENER — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 695 LBL0 WL 208.1 CENTER SECTION 2022-688143<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30; S/N:A21033538; DUE DATE: 25-SEP-23.;[02] REPLACED ANGLE AND FASTENERS ON FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 273A9110; SHEET 3; REV - DRAWING 273A9112-45;[03] CORRECTED STEP 2. REPLACED ANGLE AND FASTENERS ON FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 273A9110; SHEET 3; REV - DRAWING 273A9112 SHEET 30 REV. -;[04] CORRECTED STEP 2. REPLACED ANGLE AND FASTENERS ON FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 273A9110; SHEET 3; REV - DRAWING 273A9112 SHEET 30 REV. -

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.5 WL 208.1. CENTER SECTION 2022-688188<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.5 WL 208.1. CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 REV B.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.5 WL 208.1. CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 REV B. RII;<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: TABLE — BROKEN (SEAT) · airframe 73,533 hrs · 43,472 cycles

BROKEN PASSENGER SEAT TABLE ROW 12 CB ROW 13 C ROW 14 CB ROW 15 CB 16 AB ROW 18 B AT PASSENGER CABIN (10 EA) REPLACED PASSENGER SEAT TABLE ROW 12 B ROW 13 C ROW 14 B ROW 15 CB 16 AB ROW 18 B AT PASSENGER CABIN (10 EA) IAW CMM 25-21-45 REV 5 IPL FIGURE 4 ITEM 60 PAGE 10088.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK LOCATED ON AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2022-688237<[01] TOOL USED DIGITAL CALIPER P/N 500-464; S/N B17030933; DUE DATE 17-OCT-23;[02] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB TASK COMPLETED.

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND RBL 24.5 WL 208.1 CENTER SECTION 2022-688184<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL 0 AND RBL 24.5 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 REV B.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL 0 AND RBL 24.5 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 REV B. RII;<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ACCESS PANEL — CRACKED (THRESHOLD) · airframe 73,533 hrs · 43,472 cycles

CRACK THRESHOLD ACCESS PANEL AT FWD CARGO COMPARTMENT 2022-688049<[01] TOOL USED: DIGITAL CALIPER P/N 500-464; S/N B17030933; DUE DATE 17-OCT-23.;[02] REPAIRED MIDDLE SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] TASK COMPLETED

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 73,533 hrs · 43,472 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED AT STA663 LH SIDE 2022-688027<[01] TOOL USED. CALIPER: PN: 500-752-20; SN: B21038255; DUE DATE: 14-SEP-23.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196127 DUE DATE 16-JAN-23.;[03] TOOL USED: SCALE P/N: CL5000 S/N:AE-408751 DUE DATE:01-APR-23.;[04] TOOL USED: SCALE P/N: CL5000; S/N: AE-409558; DUE DATE: 09-JUN-23;[05] REPAIRED VAPOR BARRIER LOCATED AT STA663 LH SIDE IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED VAPOR BARRIER LOCATED AT STA663 LH SIDE IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 RII COMPLETED

Part: SLAT — CRACKED (ZN 500 LEFT WING) · airframe 73,533 hrs · 43,472 cycles

CRACK LOWER SURFACE SLAT 2 LEADING EDGE EXTERNAL SKIN SS 322.26 LT WING 2022-688025<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138103; CAL DUE DATE: 11-APR-23;[02] REPLACED LEADING EDGE SLAT 2 ON LT WING IAW B737-700 AMM 27-81-21-400-801 AND 27-81-21-000-801.ADJUSTMENT IS OK ;TEST IS OK <BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,245 hrs · 43,284 cycles

AFT SERVICE DOOR EMERGENCY LIGHT INOP / [01] RELAMPED EMERGENCY LIGHT REF 33-51-04.

Part: HANDLE — MISSING (L/H OVERWING DOO) · airframe 69,938 hrs · 41,181 cycles

L/H OVER WING EXIT ASSIST HANDLE FRAME IS MISSING THE AFT FASTENER. ; / [01] REPLACED L/H OVER WING EXIT ASSIST HANDLE FRAME AFT FASTENER REF AMM 52-22-51; [02] INSPECTED.

Part: HANDLE — BROKEN (L2 DOOR ASSIST) · airframe 69,394 hrs · 40,859 cycles

LEFT SIDE AFT GALLEY SERVICE DOOR GUIDE (ASSIST) HANDLE IS BROKEN AT BASE/BOTTOM. ; / [01] SWAPPED AFT ENTRY ASSIST HANDLE WITH AFT LAV ASSIST HANDLE REF AMM 52-13-31. OK TO CONTINUE ON MEL 25-10-01; SP1B.; [02] R+R GUIDE HANDLE PER SIP

Part: LIGHT — LOOSE (CABIN) · airframe 69,018 hrs · 40,632 cycles

PHOTO LUMINESCENT STRIP LOOSE FROM FLOOR IN REAR OR AIRCRAFT. / RE-SECURED FLOOR PATH LIGHT STRIP PER AMM 25-27-31.

Part: HANDLE — OUT OF ADJUST (AFT CARGO DOOR) · airframe 68,079 hrs · 40,102 cycles

AFT CARGO DOOR HANDLE NEED ADJUSTING. / EVALATED; REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE ASSY. OP CHECK GOOD IAW SRM 51-40-02; SRM 51-40-05 SRM 51-40-08; DWG 149A6134 CMM 52-36-15; AMM 52-31-00-700-801

Part: THRESHOLD — CRACKED (R1 DOOR) · airframe 68,079 hrs · 40,102 cycles

FWD SERVICE DOOR THRESHOLD IS CRACKED AT FWD O/B FLANGE AT 2ND RELIEF CUT / REMOVED; REPAIRED AND REINSTALLED FSD THRESHOLD PER AMM 53-11-01; AND SRM 53-10-15-2R-2 92929U 09FEB21

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,079 hrs · 40,102 cycles

RH OVERWING EXIT HATCH EMERGENCY AREA LIGHT IS OUT (FWD) / REPLACED LAMP FOR RH OVERWING EXIT HATCH EMERGENCY AREA LIGHT (FWD) AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-01-960-801.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,079 hrs · 40,102 cycles

L/H SIDE OVERWING EXIT; EMERG. EXIT SIDEWALL LIGHT INOP / WHILE TROUBLE SHOOTING SWAPPED BATTERY PACK WITH GOOD WORKING BATTERY PACK AND LIGHT WAS FULLY OPERATIONAL. PART ON ORDER AND OPS CHECK WILL BE PERFORMED ON DEFECT #U267901 AVIO-5024 PER AMM 33-51-06-960-805

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,079 hrs · 40,102 cycles

R/H SIDE ABOVE OVERWING EXIT; EMERG. EXIT LIGHT INOP / REMOVED AND REPLACED FUSE F1 IN POWER SUPPLY AND PERFORMED GOOD OPERATIONAL TEST OF R/H SIDE ABOVE OVERWING EMERGENCY EXIT LIGHT AMM 33-51-06-960-804; WDM 33-51-11; AMM 33-51-00-720-801. 81136U 31JAN21

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,079 hrs · 40,102 cycles

R/H SIDE OVERWING EXIT; EMERG. EXIT SIDEWALL LIGHT INOP / REMOVED AND REPLACED SIDEWALL EMERGENCY EXIT LIGHT AND F1 POWER SUPPLY FUSE AND PERFORMED GOOD OPERATIONAL TEST OF SIDEWALL EMERGENCY EXIT LIGHT PER WDM 33-51-11 WDM 33-51-13; WDM 33-51-21; AMM 33-51-06-960-804; AMM 33-51-01-960-802; AMM 33-51-00-720-801. 81136U 31JAN21 56576R 31JAN21

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,079 hrs · 40,102 cycles

L/H SIDE ABOVE OVERWING EXIT ; EMERG. EXIT LIGHT INOP / REMOVED AND REPLACED EMERG. EXIT BATTERY M1668 AT SWA 603 WL 212 LBL 67 AND PERFORMED GOOD OP CHECK AS PER AMM 33-51-06-960-805

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,079 hrs · 40,102 cycles

R/H SIDE OVERWING EXIT; EMERG. EXIT SIDEWALL LIGHT INOP / REMOVED AND REPLACED SIDEWALL EMERGENCY EXIT LIGHT AND F1 POWER SUPPLY FUSE AND PERFORMED GOOD OPERATIONAL TEST OF SIDEWALL EMERGENCY EXIT LIGHT PER WDM 33-51-11 WDM 33-51-13; WDM 33-51-21; AMM 33-51-06-960-804; AMM 33-51-01-960-802; AMM 33-51-00-720-801. 81136U 31JAN21 56576R 31JAN21

Part: SUPPORT — CORRODED (NR 2 NACELLE) · airframe 68,079 hrs · 40,102 cycles

#2 ENGINE PYLON LOWER CHORD SUPPORT FOR PANEL 441DR IS CORRODED IN SEVERAL AREAS. / REMOVED AND RESTORED #2 ENG PYLON LOWER CHORD SUPPORT FOR PANEL 441DR ACCOMPLISHED ON SAM 326 A1289457; A1289778 PER AMM 54-51-01 SRM 54-50-71-1A-2 56225U 29JAN21

Part: NUT PLATE — DAMAGED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

AFT CARGO BAY HAS SEVERAL DAMAGED NUTPLATES COMMON TO SIDEWALL; BULKHEAD PANELS / REMOVED AND REPLACED AFT CARGO BAY HAS; SEVERAL NUT PLATES COMMON TO SIDEWALL; BULKHEAD IAW SRM 51-40-02 59899U 26JAN21

Part: GUSSET — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY GUSSET IS CRACKED BS 500D; STR 19L / REMOVED AND INSTALLED NEW FWD CARGO BAY GUSSET BS500D; STR19L PER DWG 143A7902; AND SRM 51-40-02-0G-0 87713U 19JAN21

Part: GUSSET — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY GUSSET IS CRACKED BS 500D; STR 19R / REMOVED FCB GUSSET AT BS500D; STR19R PER SRM 51-40-02-0G-0; INSTALLED NEW GUSSET AT BS500D; STR19R PER SRM 51-40-02-0G-0 AND DWG 143A7902 93114U 19JAN21

Part: INTERCOSTAL — DAMAGED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

AFT CARGO BAY INTERCOSTAL IS DAMAGED BS 727A LBL 23; W/L 156 / REMOVED AND REPLACED ACB INTERCOSTAL B/S 727A-727B; LBL23 IAW SRM 51-40-02-0G-0; DWG# 146A7500.

Part: FLOOR SUPPORT — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY INTERCOSTAL BS 500C- 500D RBL 21 WL 154 IS CRACKED ON UPPER FLANGE AT AFT END / REMOVED AND REPLACED FCB INTERCOSTAL B/S 500C-500D; RBL21; WL154 IAW SRM 51-40-02-0G-0; DWG #143A7505.

Part: ATTACH ANGLE — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED AT BS 500C LBL 22 / REMOVED & REPLACED CLIP AT FCB BWS 500C LBL22 IAW SRM 51-40-02-2G-0 & DWG 143A7505 REV B 59191U 15JAN21

Part: BAFFLE — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500B - BS 500C LBL 22 / REMOVED & REPLACED BAFFLE AT FCB BS500-B - BS-500C LBL22 IAW SRM 51-40-02-0G-01 & DWG 143A7505 REV.B 59191U 15JAN21

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

CRACK NOTED IN FWD SERVICE DOOR BEAR STRAP BETWEEN STR 8R AND STR 9R FWD OF DOOR CUTOUT. / REPAIRED FWD SERVICE DOOR BEAR STRAP BETWEEN STR 8R AND STR 9R FWD OF DOOR CUTOUT IAW SRM 53-10-01-2R-6

Part: DEPRESSOR — CRACKED (R1 DOOR) · airframe 68,079 hrs · 40,102 cycles

FSD UPPER HINGE CUTOUT SEAL DEPRESSOR IS CRACKED BS 2945 / REMOVED AND REPLACED FSD UPPER HINGE CUTOUT SEAL DEPRESSOR AT BS 294.5 PER SRM 51-40-02; SRM 51-40-05; AND DWG 141A8370.

Part: BAFFLE — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500 - BS 500A LBL 22 / REMOVED & REPLACED BAFFLE AT FCB BS-500 TO BS 500A LBL 22 IAW SRM 51-40-02-0G-01 & DWG 143A7505 REV A 59191U 15JAN21

Part: ATTACH ANGLE — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500B LBL 22 / REMOVED & REPLACED CLIP AT FCB BS500B LBL22 IAW SRM 51-40-02-0G-01 & DWG 143A7505 REV B 59191U 15JAN21

Part: ATTACH ANGLE — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500 LBL 22 / REMOVED & REPLACED CLIP AT FCB BS500C LBL22 IAW SRM 51-40-02-0G-01 & DWG 143A7505 REV A 59191U 21JAN21

Part: STRAP — CORRODED (ZONE 200) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN CTR SECTION BS692 LBL63 WL203. MARKED / REPAIRED DAMAGED AREA AT B.S.692; LBL63; WL203 IAW ER 21-01086 & EA 21-153-00218 REV IR.

Part: STRAP — CORRODED (PAX CABIN) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN CTR SECTION BS713 RBL66 WL203. MARKED / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 21-153-00218 REV IR (ATS EA 21-01086 REV IR) REFER TO NRC U267791 FOR TRACKING AT B.S. 713; RBL66; WL203.

Part: STRAP — CORRODED (PAX CABIN) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN CTR SECTION BS704 RBL63 WL203. MARKED / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 21-153-00218 REV IR (ATS ER 21-01086 REV IR). REFER TO NRC U267791 FOR TRACKING. AT B.S. 704; RBL63; WL203

Part: ATTACH ANGLE — CRACKED (PAX CABIN) · airframe 68,079 hrs · 40,102 cycles

PASSENGER CABIN INTERCOSTAL ATTACH TAB IS CRACKED (273A9112-45) BS692 RBL24 WL204. / REMOVED AND REPLACED INTERCOSTAL ATTACH TAB P/N 273A9112-45; BS692; RBL24 WL204 PER B737 SRM 51-40-02-OG-0 AND BOEING DWG 273A9110. FABRICATED FROM BAC1490-2782-7075-0 PER BOEING DWG 273A9112; RECEIVED PART HEAT TREATED TO T73 CONDITION FROM OSS P.O. #812834-SWA

Part: STRAP — CORRODED (CENTER CABIN) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN CTR SECTION BS696 LBL63 WL203. MARKED / DAMAGE REPAIRED/INSPECTED AND EVALULATED PER EA #21-153-00218 REV IR (ATS EA 21-01086 REV IR) REFER TO NRC U267791 FOR TRACKING AT B.S. 696; LBL63; WL203.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 68,079 hrs · 40,102 cycles

PASSENGER CABIN FLOOR PANEL 241AF LOWER SURFACE CENTER INSERTS ARE DAMAGED. / FOUND DAMAGE AROUND INSERT LOCATIONS; DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241AF USING BMS 4-23TY2 LOT#1443771-1; INSTALLED INSERTS USING BMS 5-107 LOT#AKOHP5746K AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND DWG 144A5810-8. 57066U 1/14/21

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 68,079 hrs · 40,102 cycles

PASSENGER CABIN FLOOR PANEL 242CF AFT CORNERS HAVE DAMAGE. MARKED / DUE TO EXTENT OF DAMAGE; FABRICATED NEW PASSENGER CABIN FLOOR PANEL 242CF USING BMS 4-23 TY2 LOT# 1443771-1; INSTALLED INSERTS USING BMS 5-107 LOT# AK0HP5746K AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND DWG 144A5810-6. 57066U 1/15/21

Part: ROLLER — DAMAGED (R1 DOOR) · airframe 68,079 hrs · 40,102 cycles

PASSENGER CABIN FWD SERVICE DOOR FWD LOWER LATCH ROLLER HAS DAMAGE. / REMOVED AND REPLACED DAMAGED LOWER FWD LATCH ROLLER ON PASSENGER CABIN SERVICE DOOR IAW SOPM 20-50-01; SOPM 20-50-02; AND IPC 52-41-41-05 LUBED IAW AMM 12-25-13-640-801

Part: STRAP — CORRODED (PAX CABIN) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN CTR SECTION BS693 RBL64 WL203. MARKED / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 21-153-00218 REV IR (ATS EA 21-01086 REV IR) REFER TO NRC U267791 FOR TRACKING. AT B.S. 693; RBL64 WL203.

Part: SKIN — CORRODED (ZONE 200) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB; BS 1040 TO 1072; STR 2LT TO 3' BELOW / REMOVED CORROSION ON FUSELAGE SKIN UNDER VERTICAL STAB BS1040-1072 STR 2L/H TO 3' BELOW W/L308 REPAIRED PER ATS ER 21-01081 REV IR AND SWA EA 21-153-00179 REV IR

Part: SKIN — CORRODED (UPPER FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB; BS 1024 TO 1036; STR 1 TO 2 RT; WL 308 / REMOVED CORROSION ON FUSELAGE SKIN UNDER VERTICAL STAB BS1024-1036 STR 1-2 R/H W/L 308. REPAIRED PER ATS ER 21-01081 REV IR AND SWA EA 21-153-00179 REV IR

Part: SKIN — CORRODED (ZONE 200) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB; BS 1040 TO 1045; STR 2 RT TO 3' ABOVE / REMOVED CORROSION ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB BS 1040 TO 1045 STR 2 R/H TO 3' ABOVE. REPAIRED PER EA 21-153-00179 REV IR AND ER 21-01081 REV IR

Part: SKIN — CORRODED (ZONE 200) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB; BS 1024 TO 1036; STR 1 TO 2 LT; WL 308 / REMOVED CORROSION ON FUSELAGE SKIN UNDER VERTICAL STAB B/S 1024-1036 STR 1-2 L/H W/L 308. REPAIRED PER ATS ER 21-01081 REV IR AND SWA EA 21-153-00179 REV IR

Part: SKIN — CORRODED (UPPER FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB; BS 1040; STR 2 RT TO 3' BELOW / REMOVED CORROSION ON FUSELAGE SKIN UNDER VERTICAL STAB BS 1040-1080 STR 2 R/H TO 3' BELOW. REPAIRED PER ATS ER 21-01081 REV IR AND SWA EA 21-153-00179 REV IR

Part: SUPPORT — BENT (E/E BAY) · airframe 68,079 hrs · 40,102 cycles

MAIN EBAY DOOR 117A AFT ROLLER SUPPORT TAB IS BENT. MARKED / REPLACED MAIN EBAY DOOR 117A AFT ROLLER SUPPORT TAB IAW SRM 51-40-02 AND BOEING DWG 141A6710. 59807U 1/16/21. FIT CHECK GOOD. 59807U 1/16/21

Part: ANGLE — CORRODED (FWD CARGO BLKHD) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** FWD CARGO BAY AFT L/H BULKHEAD LOWER ANGLE BS 500D; WL 154; LBL 21 / REMOVED AND REPLACED BULKHEAD ANGLE B/S 500D; LBL21 WL154 IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 143A9481 REV:A AND DWG 143A7902 REV:E 59900U 20JAN21

Part: ANGLE — CORRODED (FWD CARGO BLKHD) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** FWD CARGO BAY AFT R/H BULKHEAD LOWER ANGLE BS 500D; WL 154; RBL 21 / REMOVED AND REPLACED BULKHEAD ANGLE B/S 500D; WL154 RBL21 IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 DWG 143A9481 REV:A AND DWG 143A7902 REV:E 59900U 20JAN21

Part: ATTACH ANGLE — CORRODED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** FWD CARGO BAY AFT CENTER BULKHEAD LOWER ATTACH ANGLE BS 500D; WL 154; LBL 21 - RBL 21 / REMOVED AND REPLACED BULKHEAD ANGLE B/S 500D WL154 LBL21-RBL21 IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 DWG 143A9481 REV:A AND DWG 143A7902 REV:E 59900U 20JAN21

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 490-500D; WL 154; LBL 22 / REMOVED AND REPLACED FWD CARGO BAY L/H NEW FLOOR TO SIDEWALL SUPPORT B/S 490-500D WL 154; LBL22 IAW SRM 51-40-02 AND DWG 143A7500 REV:A AND DWG 143A7501 REV:B 59899U 19JAN21 SIDEWALL SUPPORT REPAIR SPLICE LOCATED BETWEEN BS480-500 LBL22 WL154 PER SRM 53-00-53-2R-6.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 68,079 hrs · 40,102 cycles

FWD CARGO BAY S-26L CRACKED AT BS 540 / REPAIRED STRINGER 26L AT BS540 PER B737-700 SRM 53-00-03-2R-1 REPAIR 1.

Part: STUB FRAME — CRACKED (R1 DOORWAY) · airframe 68,079 hrs · 40,102 cycles

CRACK NOTED ON FWD SVC DOOR CUTOUT FWD INNER SURFACE; BS 294.5 BETWEEN STR 6R AND 7R (MARKED) / REPLACED STUB FRAME FWD SERVICE DOOR FWD SIDE BS 294.5 BETWEEN STR 5R AND STR 7R IAW SRM 51-40-02 AND DWG 141A8370 REV D

Part: NUT PLATE — BROKEN (SIDEWALL) · airframe 68,079 hrs · 40,102 cycles

CABIN SIDEWALL ISOLATOR NUT PLATES ARE BROKEN; 2 EA AT BS 727; BETWEEN STR 13R AND STR 15R; MARKED / REMOVED AND REPLACED 2EA CABIN SIDEWALL ISOLATORS NUT PLATES AT BS727 BETWEEN STR13R AND STR15R IAW SRM 51-40-02 SECTION 4

Part: NUT PLATE — BROKEN (SIDEWALL) · airframe 68,079 hrs · 40,102 cycles

CABIN SIDEWALL ISOLATOR NUT PLATES ARE BROKEN; 2 EA AT BS 685; BETWEEN STR 13R AND STR 15R; MARKED / REMOVED AND REPLACED 2EA CABIN SIDEWALL ISOLATOR NUT PLATES AT BS685 BETWEEN STR 13R AND STR 15R IAW SRM 51-40-02 SECTION 4

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 68,079 hrs · 40,102 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED; BS 294-312; RBL 15; WL 207. / REMOVED AND REPLACED INTERCOSTAL AT B.S294-312; RBL15; WL207 IAW SRM 51-40-02-0G-0; DWG 141A5400 SH92

Part: FLOOR SUPPORT — ELONGATED (CABIN) · airframe 68,079 hrs · 40,102 cycles

INTERCOSTAL FLOOR SUPPORT HAS ELONGATED FASTENER HOLES; BS 312-328; RBL 31; WL 207. / REMOVED AND REPLACED FLOOR SUPPORT BS312-328 RBL31 WL207 PER SRM 51-40-02; SRM 51-40-05 AND DWG# 141A5400 REV-

Part: NUT PLATE — BROKEN (SIDEWALL) · airframe 68,079 hrs · 40,102 cycles

CABIN SIDEWALL ISOLATOR NUT PLATES ARE BROKEN; 3 EA AT BS 685; BETWEEN STR 13L AND STR 15L; MARKED / REMOVED AND REPLACED 3EA CABIN SIDEWALL ISOLATOR NUT PLATES AT BS685 BETWEEN STR 13L AND STR 15L IAW SRM 51-40-02 SECTION 4.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR SUPPORT; BS 294-312; RBL 11; WL 207. / REMOVED AND REPLACED FLOOR SUPPORT AT BS 294-312; RBL11; WL 207 PER DWG NO. 141A5400 AND SRM 51-40-02-OG-0. CIC WILL BE APPLIED PER CUSTOMER CARD NBR 16397.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 68,079 hrs · 40,102 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED; BS 328-344; LBL 44; WL 207. / REMOVED AND REPLACED CRACKED INTERCOSTAL FLOOR SUPPORT BS328-344; LBL44; WL207 IAW SRM 51-40-02 AND DWG 141A5400 56693U 17JAN21

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 68,079 hrs · 40,102 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED; BS 312-328; LBL 44; WL 207. / REMOVED AND REPLACED CRACKED INTERCOSTAL FLOOR SUPPORT BS 312-328; LBL44; WL207 IAW SRM 51-40-02 AND DWG 141A5400 56693U 17JAN21

Part: NUT PLATE — BROKEN (SIDEWALL) · airframe 68,079 hrs · 40,102 cycles

CABIN SIDEWALL ISOLATOR NUT PLATES ARE BROKEN; 3 EA AT BS 727; BETWEEN STR 12L AND STR 15L; MARKED / REMOVED AND REPLACED 3EA CABIN SIDEWALL ISOLATOR NUT PLATES AT BS727 BETWEEN STR12L AND STR15L IAW SRM 51-40-02-SECTION 4.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 68,079 hrs · 40,102 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED; BS 277-294; BL 0; WL 207. / REMOVED AND INSTALLED A NEW INTERCOSTAL AT B.S 277-294; BL0; WL207 IAW SRM 51-40-02-0G-0; DWG 141A5400

Part: SEAT TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS945 RBL3 WL179. / REMOVED AND REPLACED ACB RAIL B/S887-947; RBL3 IAW SRM 51-40-02-0G-0; DWG# 147A7500.

Part: CARGO TRACK — CORRODED (AFT CARGO FLOOR) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON TRACK TIEDOWN AT AFT CARGO BAY BS787 LBL17 WL158. / AFT BAY CARGO TIEDOWN TRACK IS REPAIRED BY REPLACEMENT OF TRACK BS727-867 LBL17; ACCOMPLISHED ON CUSTOMER CARD# U267683

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AT AFT CARGO BAY BS767+6 RBL3 WL157. / REPAIRED RAIL AT AFT CARGO BAY B/S 767+6 RBL3 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2 59900U 14JAN21

Part: ANGLE — CORRODED (AFT) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT AFT CARGO BAY BS947 RBL22 WL180. / REMOVED AND REPLACED ACB AFT RH BULKHEAD SUPPORT ANGLE B/S 947; IAW SRM 51-40-02-G-0. DWG # 149A8117.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON AFT SHIELD AT AFT CARGO BAY BS865 RBL22 WL165. / REMOVED AND REPLACED ACB AFT SHIELD ASSY BS865 RBL22 WL165 PER SRM 51-40-02 AND DWG# 146A0081 REV:A.

Part: SEAT TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AT AFT CARGO BAY BS767+6 LBL8 WL157. / REPAIRED RAIL AT AFT CARGO BAY B/S 767+6 LBL8 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2. 59900U 14JAN21

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** RIGHT OWE LOWER SILL INTERCOSTAL; BS 657; S-15R. / REPAIRED RIGHT OWE LOWER SILL INTERCOSTAL CORROSION AT B.S. 657; STR - 15R IAW SOUTHWEST EA 21-153-00195 REV IR AND ATS ER NUMBER 21-01047 REV IR

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 68,079 hrs · 40,102 cycles

RH INTERFACE CLOSURE (SKATE ANGLE) MATING SURFACE CHAFED; BS 1120 TO BS 1132 / REMOVED AND REMPLACED SKATE ANGLE AT STR 3R BS1016 TO BS1132 IAW SRM 51-40-02 AND DWG 148A8300 REV C 57049U 13JAN21

Part: ATTACH BRACKET — CHAFED (TIE ROD) · airframe 68,079 hrs · 40,102 cycles

TIE ROD ATTACH BRACKET CHAFED; BS 364; S-4L. / REMOVED AND REPLACED THE TIRE ROD ATTACH BRACKET AT B.S 364 S4L IAW SRM 51-40-02-0G-0; DWG 413A3210

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 RBL20 TO LBL7 WL168. / PROCURE & REPLACE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 & DWG 147A7500 REV.B AND SRM 51-10-02-0G-0 PARAG 9 59191U 13JAN21

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS887- BS947 RBL21 WL-156. / FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY; BS 887- BS 947; RBL 21; WL 156 FOUND TO BE DAMAGED BEYOND ALLOWABLE DAMAGE LIMITS. REPAIR BY REPLACEMENT IAW SRM 51-10-02; PARA 9A(1). RECEIVED A NEW FLOOR TO SIDEWALL SUPPORT FROM STORES. REF: PO 805518. REMOVED DAMAGED SUPPORT; LOCATED; DRILLED AND INSTALLED THE NEW SUPPORT IAW SRM 51-40-02; SRM 51-40-08 AND DWG 147A7500

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS787 LBL21 WL157. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB B/S 727-847 LH. IAW SRM 51-40-02-0G-0 DWG# 146A7500.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AT AFT CARGO BAY BS767+6 RBL8 WL157. / REPAIRED RAIL AT AFT CARGO BAY B/S 767+6 RBL8 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2 59900U 14JAN21

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS914 RBL11 WL171. / REMOVED AND REPLACED SUPPORT ANGLE OF WATER SERVICE PANEL AT AFT CARGO BAY B/S 914 RBL11 WL171 P/N 147A7221-32 LOT:7531385 PO:808742-1 IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 147A7221 REV:D 59900U 17JAN21

Part: CARGO TRACK — CHAFED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

CHAFING DAMAGE ON RAIL AT AFT CARGO BAY BS806 LBL3 WL159. / REPAIRED RAIL AT AFT CARGO BAY BTW B/S 787 - B/S 847 LBL3 WL159 IAW SRM 53-00-53-2R-2 REPAIR 2 AND DWG 146A7500 REV AND DWG 146A7503 REV: 5900U 16JAN21

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS947 RBL19 TO LBL8 WL179. / REMOVED AND REPLACED AFT LOWER BULKHEAD SUPPORT ANGLE B/S 947. RBL19 TO LBL08; IAW SRM 51-40-02-0G-0; DWG # 149A8117; AIPC 53-11-51-01.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FWD SHIELD AT AFT CARGO BAY BS767 RBL22 WL158. / REMOVED AND REPLACED SHIELD AT AFT CARGO BAY B/S 767 RBL 22 WL158 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A0081 REV:A

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727E+3 RBL8 WL156. / REPAIRED RAIL AT AFT CARGO BAY BTW B/S 727D TO B/S 747 RBL8 WL156 IAW SRM 51-40-02 SRM 53-00-53-2R-2 REPAIR 2 AND DWG 146A7500 REV: C 59900U 16JAN21

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS927 LBL3 WL176. / REMOVED AND REPLACED RAIL IN ACB FROM BS887-947 LBL3 WL176 IAW SRM 51-40-02; DWG# 147A7500 REV -; SRM 53-00-53-1A-2 59042U 15JAN21

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON TRACK IN MULTIPLE AREAS AT AFT CARGO BAY BS727 - BS767 LBL17 WL157. / REMOVED AND INSTALLED NEW TRACK AT AFT CARGO BAY B/S 727-867 LBL17 WL157 FROM P/N ITEM 7531208 PO# 809392/2 IAW SRM 51-40-02 AND DWG 146A7500 REV:C 59899U 14JAN21

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON RAIL AT AFT CARGO BAY BS767+6 LBL12 WL157. / REPAIRED RAIL AT AFT CARGO BAY B/S 767+6 LBL12 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2 59900U 14JAN21

Part: SUPPORT ANGLE — CRACKED (WATER SERVICE) · airframe 68,079 hrs · 40,102 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL11 WL171. / REMOVED AND REPLACED SUPPORT ANGLE OF WATER SERVICE PANEL AT AFT CARGO BAY B/S 918 RBL 11 WL 171 LOT: 7531385; PO: 808742-1 P/N 147A7221-32 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 147A7221 REV: D 59900U 17JAN21

Part: FRAME — DENTED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

DENT ON FRAME AT AFT CARGO BAY BS807 S-24L WL162. / REPAIRED FRAME AT AFT CARGO BAY B/S 807 S-24L WL 162 IAW ATS ER-21-01049 REV IR AND SWA EA-21-153-00167 REV IR

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS767 RBL21 WL157. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 TO BS767 RBL L21 WL 157 IAW SRM 51-40-02; DWG 146A7502 AND DWG 146A7500 REV. C

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 68,079 hrs · 40,102 cycles

LH INTERFACE CLOSURE (SKATE ANGLE) MATING SURFACE CHAFED; BS 1010 TO BS 1016 / REMOVED & REPLACED L/H INTERFACE CLOSURE (SKATE ANGLE) AT BS1006 TO BS1016 IAW SRM 51-40-02-0G-0 & DWG 147A0030 REV.B 59191U 01-12-2021 & DWG 147A0070 REV- 59191U 01-12-2021

Part: RETAINER — CRACKED (RT WING) · airframe 68,079 hrs · 40,102 cycles

R/W T/E UPPER SURFACE PANEL AT ORSS 275 LOWER SEAL RETAINER IS CRACKED / REMOVED AND REPLACED R/W T/E UPPER SURFACE PANEL @ ORSS 275 LOWER SEAL RETAINER IAW SRM 51-40-02 SECTION 9 49570U 10JAN21

Part: RETAINER — CRACKED (LT WING) · airframe 68,079 hrs · 40,102 cycles

LEFT WING T/E UPPER SURFACE PANEL AT ORSS 275 LOWER SEAL RETAINER IS CRACKED / REMOVED AND REPLACED LEFT WING T/E UPPER SURFACE PANEL @ ORSS 275 LOWER SEAL RETAINER IAW SRM 51-40-02 SECTION 9 49510U 10JAN21

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,079 hrs · 40,102 cycles

RT HORIZONTAL STAB REMOVABLE LEADING EDGE 341B NR 3 RIB IS CRACKED. REMOVED & REPLACED THE (CRACK) R/H HORIZONTAL STAB REMOVABLE L/E 341B # 3 RIB IAW SRM 51-40-02-0G-0 PAR 4 (B)(C)(1-3)

Part: RETAINER — CRACKED (LT WING) · airframe 68,079 hrs · 40,102 cycles

LEFT WING T/E VERTICAL BULB SEAL RETAINER AT ORSS 275 JUST AFT OF AFT PYLON TIN IS CRACKED / REMOVED & REPLACED THE DAMAGED LEFT WING T/E VERTICAL BULB SEAL RETAINER AT ORSS 275 JUST AFT OF AFT PYLON TIN IAW SRM 51-40-02-0G0- PAR 4 (B)(C) (2-3) & PAR 9B

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 68,079 hrs · 40,102 cycles

CORROSION, INTERCOSTAL INNER FLANGE BS 270-291 S-5R. UPON FURTHER INVESTIGATION DAMAGE TO BE ON PAINT SURFACE NO DAMAGE TO STRUCTURE. TREATED & PRIMED PER SRM 51-00-58-201 STEP 2. E. (6) (7) & (8)

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 68,079 hrs · 40,102 cycles

LT HORIZONTAL STAB INSPAR RIB AT STAB STA 111.10 3RD STIFFENER FROM FWD END IS CRACKED.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 68,079 hrs · 40,102 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221BF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,079 hrs · 40,102 cycles

RT HORIZONTAL STABILIZER STA 138.70 RIB CRACKED AT 4TH STIFFENER.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 68,079 hrs · 40,102 cycles

LEFT HORIZONTAL STAB INSPAR RIB AT STAB STA 129.5 3RD STIFFENER FROM FWD END IS CRACKED.

Part: FLOOR PANEL — PULLED · airframe 68,079 hrs · 40,102 cycles

FWD FLOOR PANEL 221EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 68,079 hrs · 40,102 cycles

FWD FLOOR PANEL 221FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221FF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).

Part: FLOORBEAM — CORRODED (BS 947) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR SUPPORT LOWER SIDE OF AFT FLANGE AT BS 947.5+3; RBL 32- RBL 39; WL 207 / CORROSION ON FLOOR SUPPORT BS947.5+3'; RBL32-RBL39 WL207 FOUND TO BE OUT OF LIMITS 1' X 2' X .018' ORIGINAL THICKNESS .071' PER SRM 53-70-51-1A-1; REMOVED AND REPLACED PER SRM 51-40-02; SRM 51-40-05 AND DWG# 147A5760 REV-

Part: FLOORBEAM — CORRODED (BS 947) · airframe 68,079 hrs · 40,102 cycles

***CORROSION*** ON FLOOR SUPPORT LOWER SIDE OF AFT FLANGE AT BS 947.5+3; RBL 46- RBL 48; WL 207 / CORROSION ON FLOOR SUPPORT BS947.5+3 RBL46-RBL48; WL207 REMOVED IN A 1' X 1' X .015' ORIGINAL THICKNESS .072' FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02; SRM 51-40-05 AND DWG# 147A5760 REV - 88911U JAN12-21

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

CORROSION, ON FUSELAGE SKIN EXTERNAL SURFACE AROUND FASTENER HOLES BS 669.75+15-BS 685+13, STR 1-STR 2R.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

FWD FLOOR PANEL 222DF HAS A DAMAGED INSERT WITH LOWER SKIN DAMAGE. / REPAIRED DAMAGED LOWER SKIN AND REPLACED DAMAGED INSERT ON FWD FLOOR PANEL 222DF IAW SRM 53-00-50-2R-4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

FWD FLOOR PANEL 222DF HAS A DAMAGED INSERT WITH LOWER SKIN DAMAGE. / REPAIRED DAMAGED LOWER SKIN AND REPLACED DAMAGED INSERT ON FWD FLOOR PANEL 222DF IAW SRM 53-00-50-2R-4.

Part: FLOOR PANEL — PULLED · airframe 68,079 hrs · 40,102 cycles

FWD FLOOR PANEL 222BF UPPER SKIN HAS 2 AREAS OF PULLED STRANDS.

Part: SHEAR TIE — CORRODED (SECTION 48) · airframe 68,079 hrs · 40,102 cycles

CORROSION ON SHEAR TIE IN 48 SECTION JUST AFT OF STAB TRIM ACCESS COMPARTMENT DOOR BS 1064; LBL 19; WL 205 / REMOVED CORROSION ON SHEAR TIE JUST AFT OF STAB TRIM ACCESS COMPARTMENT DOOR BS 1064; LBL 19; WL 205; BLEND WAS 1' X .8' X .003'. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-07-1A-1 DWG# 148A0933 59042U 07JAN2021. TREATED AND PRIMED IAW SRM 53-00-07-1A-1 59042U 07JAN2021

Part: FLOOR PANEL — DAMAGED · airframe 68,079 hrs · 40,102 cycles

AFT FLOOR PANEL 241ADF OUTBOARD AFT CORNER IS DAMAGED, MARKED.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

AFT FLOOR PANEL 242VF I/B EDGE HAS MULTIPLE AREAS OF DAMAGE. (MARKED) / AFT FLOOR PANEL 242VF WITH I/B EDGE HAVING MULTIPLE AREAS OF DAMAGE AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 68,079 hrs · 40,102 cycles

AFT FLOOR PANEL 242SF I/B EDGE OF UPPER SKIN IS DAMAGED. (MARKED) REPAIRED DAMAGE TO FLOOR BOARD 242SF I/B EDGE IAW SRM 53-00-50-2R-1.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 68,079 hrs · 40,102 cycles

AFT FLOOR PANEL 241ACF O/B FWD CORNER IS DAMAGED. (MARKED) REPAIRED DAMAGE TO FLOOR PANEL 241ACF FWD CORNER IAW SRM 53-00-50-2R-1.

Part: SERVICE PANEL — CORRODED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

TOILET SERVICE PANEL 145AL INNER SURFACE PREVIOUS REPAIR BETWEEN HINGES HAS MISSING PAINT AND POSSIBLE CORROSION. / REMOVED TOILET SERVICE PANEL 145AL AND REPLACED WITH NEW PANEL IAW SRM 51-40-02; AMM 52-49-07-000-801; AMM 52-49-07-400-801. OHMS CHECK GOOD. 59042U 09JAN21 PRIOR TO PNL145AL REPLACEMENT CORROSION NOTED COMMON TO EXISTING REPAIR NO SRM LIMITS FOR CORROSION ON REPAIR. OUT OF LIMITS REPAIR BY REPLACEMENT IAW SRM 52-40-01-1A-4

Part: ISOLATOR — BROKEN (LT OVERWING) · airframe 68,079 hrs · 40,102 cycles

L/H OVER WING SURROUND STRUCTURE THE FWD TOP ISOLATOR FOR UPPER PANEL IS BROKE; / REMOVED AND REPLACED L/H OVERWING SURROUND STRUCTURE FWD TOP ISOLATOR FOR UPPER PANEL PER SRM 51-10-02-0G-0 STEP 9.C.; SRM 51-40-02; AND AIPC 53-13-00-61.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 68,079 hrs · 40,102 cycles

PANEL 195CR IS CRACKED AT AFT LOWER CORNER / PANEL 195CR WITH CRACK AT AFT LOWER CORNER WAS REPLACED WITH A SERVICEABLE PANEL PER SRM 51-10-02-0G-0 PARA 9.A.(1) DUE TO EXTENT OF DAMAGE.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 68,079 hrs · 40,102 cycles

AFT FLOOR PANEL 241ZF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / AFT FLOOR PANEL 241ZF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).

Part: PRESSURE DECK — CRACKED (BS 664) · airframe 68,079 hrs · 40,102 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 664.5; LBL 30.5 WL 202. MARKED IN RED INK UNDER WASTE TUBE. / REPAIRED THE HORIZONTAL PRESSURE DECK AT B.S 664.5 LBL 30.5; WL 202 IAW SRM 53-40-51-2R-2

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PANEL #140CF. / FABRICATED NEW ACB FLOOR PANEL 140CF FROM 080 2024T-3; LOT# 1445686-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PANEL #140AF. / FABRICATED NEW ACB FLOOR PANEL 140AF FROM 090 CONOLITE; LOT# 1446619-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 68,079 hrs · 40,102 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PANEL #140BF. / FABRICATED NEW ACB FLOO PANEL 140BF FROM 090 CONOLITE; LOT# 1446619-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 68,079 hrs · 40,102 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / COMPLETED REPAIR FLIGHT DECK FLOOR AT B.S 255 RBL4-LBL14 WL207.54 PER EA #1-A53-33179 REV 1

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,920 hrs · 40,009 cycles

FWD CARGO AFT FLOOR PANEL DAMAGED / REMOVED AND REPLACED FWD CARGO CARGO PANEL 120 CG PER AMM 25-52-10

Part: COVER — OUT OF POSITION (R1 DOOR SLIDE) · airframe 67,856 hrs · 39,969 cycles

F/A NOTED PROTECTIVE FABRIC FLAP FOR MANUAL PULL/DEPLOYMENT HANDLE ON THE FWD SERVICE DOOR SLIDE WAS MISSING. REPOSITIONED HANDLE COVER FLAP, IAW MT 725-61-06.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 66,741 hrs · 39,272 cycles

FA SAYS 'THE RT REAR SERVICE DOOR SLIDE HAS TO MUCH HANGING OUT OF THE COVER. RESECURED AFT SERVICE SLIDE PER AMM 25-66-01.

Part: MOUNT — LOOSE (L2 DOOR SLIDE) · airframe 65,959 hrs · 38,784 cycles

L2 DOOR ESCAPE SLIDE SHROUD MOUNT LOOSE. / TIGHTENED MOUNT PER AMM.

Part: TRIM PANEL — UNSECURE (EMERGENCY EXIT) · airframe 65,712 hrs · 38,621 cycles

L/H OVERWING EMERGENCY EXIT DOOR LOWER HAND-HOLD ASSEMBLY CAME OUT. / SECURED HAND HOLD TRIM ASSEMBLY PER SIP.

Part: HOLDER — LOOSE (R2 DOOR) · airframe 64,150 hrs · 37,627 cycles

R2 DOOR SLIDE GIRT BAR HOLDER LOOSE. SECURED GIRT BAR PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,982 hrs · 37,519 cycles

OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,593 hrs · 37,278 cycles

L1 DOOR SLIDE OUT OF POSITION. / REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 63,593 hrs · 37,278 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 63,234 hrs · 37,065 cycles

L/H W/W ON THE STA 633 BULKHEAD VERTICAL STIFFINER AT LBL 24.92 CRACKED. R&R THE STIFFINER PER SRM

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 63,234 hrs · 37,065 cycles

R/H MAIN LANDING GEAR W/W ON THE BS 633 BULKHEAD_VERTICAL STIFFINER AT RBL 25 HAS A 1.75" CRACK AT LOWER EDGE OF STIFFINER. R&R THE STIFFINER PER SRM

Part: DOUBLER — CRACKED (FWD FUSELAGE) · airframe 63,234 hrs · 37,065 cycles

EGPR HAS AN APPROX. 1' LONG CRACK THROUGH FASTENER AT LOWER EDGE OF EGPR CUTOUT. CRACK IS LOCATED AT BS.231. / REPAIRED EGPR DOUBLER IAW SRM 53-10-15 ZONE 2 REPAIR ; FIG 204

Part: GIRT BAR — OUT OF POSITION (R2 DOOR SLIDE) · airframe 63,087 hrs · 36,974 cycles

R2 DOOR GIRT BAR CAUGHT OUTSIDE DOOR, UNABLE TO ARM SLIDE. / SECURED GIRT BAR PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,676 hrs · 36,716 cycles

LT OVERWING ESCAPE GROUND ILLUMINATION LIGHTS L547 & L548 INOP. R&R EMERGENCY BATTERY PACK M1670 PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,676 hrs · 36,716 cycles

LT EMERGENCY EXIT BIN LIGHTS INOP BETWEEN ROW 9 TO ROW 12. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,676 hrs · 36,716 cycles

RT OVERWING ESCAPE GROUND ILLUMINATION LIGHTS L547 & L548 INOP. R&R EMERGENCY BATTERY PACK M1670 PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

BS 312-328 RBL 11 INTERCOSTAL IS CRACKED / REMOVED AND REPLACED INTERCOSTAL BS 312 - 328 ON C.C. T884803

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

HORIZONTAL PRESSURE DECK BEADED STIFFENER CRACKED AT BS 672, RBL 42. REPAIRED STIFFENER IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 5. R&R INTERCOSTAL PER DWG & SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY THRESHOLD SUPPORT STRAP CORRODED BETWEEN BS 787+4 TO BS 847+6, RBL 20. R&R STRAP PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY OUTBOARD FACE INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 807, RBL 5. R&R INTERCOSTAL PER SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY FLOOR TRACK CRACKED AT BS 727C, LBL 8. R&R FLOOR TRACK PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

INTERCOSTAL CORRODED BETWEEN BS 328 TO BS 344, LBL 11. R&R PANEL BREAK PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 500 TO BS 500A, RBL 22. R&R SHIELD PER SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

L1 DOOR THRESHOLD SUPPORT ANGLE CORRODED AT BS 328, LBL 63. R&R ANGLE PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

INTERCOSTAL CORRODED AT BS 312+13, RBL 11. R&R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD PASSENGER COMPARTMENT WET AREA INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL PER SRM & DWG.

Part: FRAME — CORRODED (CABIN) · airframe 62,676 hrs · 36,716 cycles

***CORROSION*** ON FRAME AT FWD PASSENGER COMPARTMENT BS294.5 S-3L WL288.1. (MARKED) / AFTER DAMAGE REMOVAL; THE BLEND MEASURES 1.6' X 1.0'; MINIMUM REMAINING THICKNESS OF 0.043'. ORIGINAL THICKNESS 0.051' THE AREA WAS REWORKED AS PER EA 1-753-34250 REV IR AND ATS ER 19-01714 REV IR

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD PASSENGER COMPARTMENT WET AREA INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL PER SRM & DWG.

Part: SCUFF PLATE — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY DOOR SCUFF PLATE CORRODED BETWEEN BS 787+8 TO BS 847, RBL 27. R&R THRESHOLD WEB PER SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FLOORBEAM CORRODED AT BS 344, LBL 3. REPAIRED FLOOR BEAM PER SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,676 hrs · 36,716 cycles

R1 DOOR NR 4 (LOWER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R NR 4 (LOWER) BEAM PER WO.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BS 727C+9 TO BS 767, RBL 21. R&R SUPPORT PER DWG & SRM.

Part: BEAM — CORRODED (CABIN) · airframe 62,676 hrs · 36,716 cycles

***CORROSION*** ON FLOOR BEAM BS294 RBL46 WL208.1. / REMOVED CORROSION FROM BS 294 FLOOR BEAM RBL 46 WL 208.1 2' X 2' X .002' FROM ORIGINAL .094' AND FOUND TO BE IN LIMITS TREATED AND PRIMED AREA ALL IAW ER 19-01479 REV IR AND EA 1-753-34123 REV IR

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

L1 DOOR MOP SILL CORRODED BETWEEN BS 304 TO BS 346, LBL 59. R&R MOPSILL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 787+6, RBL 21. R&R SUPPORT PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

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

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,676 hrs · 36,716 cycles

R1 DOOR NR 5 (UPPER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R NR 5 (UPPER) BEAM PER WO.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727E+9 TO BS 787+9, LBL 21. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

L1 DOOR THRESHOLD SUPPORT ANGLE CORRODED AT BS 328, LBL 60. R&R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD PASSENGER COMPARTMENT WET AREA INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL PER DWG AND SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD PASSENGER COMPARTMENT WET AREA INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, RBL 1. R&R INTERCOSTAL PER SRM DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

INTERCOSTAL CORRODED AT BS 312+5, LBL 11. R&R PANEL BREAKS PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 727E+9, LBL 21. R&R SUPPORT PER SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 500, RBL 26. R&R WEB PER SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 62,676 hrs · 36,716 cycles

AFT CABIN FLOOR PANEL 241AEF TRAILING EDGE IS DELAMINATED / REPAIRED AFT CABIN PANEL 241 AEF DELAMINATED TRAILING EDGE IAW SRM 53-00-50-2R-1 57278U 1/29/19

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

SHEAR WEB UPPER SURFACE CORRODED AT BS 1015, LBL 40. R&R SHEAR WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

FRAME UPPER SURFACE CORRODED AT BS 986.5, BETWEEN LBL 45 TO RBL 45. REPAIRED FLOORBEAM IAW ATS ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

R2 DOOR MOP SILL UPPER SURFACE CORRODED BETWEEN BS 957 TO BS 995, RBL 50. R&R MOPSILL IAW SRM AND DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,676 hrs · 36,716 cycles

SHEAR WEB UPPER SURFACE CORRODED AT BS 988, RBL 39. R&R SHEAR WEB IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 62,676 hrs · 36,716 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT RSS 261. R&R WIGGLE PLATE IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 62,676 hrs · 36,716 cycles

RT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT RSS 261. R&R WIGGLE PLATE ASSEMBLY IAW SRM.

Part: RETAINER — CRACKED (LEFT WING) · airframe 62,676 hrs · 36,716 cycles

LT WING T/E BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED LT WING T/E BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP P/N 115A2953-1 IAW. SRM 51-40-02 AND - AIPC 57-50-00-25 88920U 04FEB19

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 62,676 hrs · 36,716 cycles

RT WING LOWER L/E PANEL 621DB HAS AN AREA OF DELAMINATION IN THE L/E / RT WING LOWER L/E PANEL 621DB WITH AN AREA OF DELAMINATION IN THE L/E WAS REPAIRED IAW SRM 51-70-05-2R-6. 57543U 06.FEB.19.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,676 hrs · 36,716 cycles

RT WING NR 6 SLAT AT LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AROUND FASTENER CRACKED AT ACTUATOR RIBS. REPAIRED NR 6 SLAT IAW SRM.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 62,676 hrs · 36,716 cycles

RT WING LOWER L/E PANEL 621QB HAS AN AREA OF DELAMINATION IN THE L/E / RT WING LOWER L/E PANEL 621QB WITH AN AREA OF DELAMINATION IN THE L/E WAS REPAIRED IAW SRM 51-70-05-2R-6. 57543U 06.FEB.19.

Part: WINDOW — CRACKED (COCKPIT) · airframe 62,360 hrs · 36,511 cycles

R2 WINDOW OUTER PANE CRACKED. R&R R2 WINDOW HEAT CONTROLLER PER MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 62,360 hrs · 36,511 cycles

R2 WINDOW OUTER PANE ARCED. R&R R2 WINDOW PER MT.

Part: DOOR — BROKEN (LWR FUSELAGE) · airframe 62,137 hrs · 36,355 cycles

GROUND A/C DOOR LATCH IS BROKEN. / REMOVED AND REPLACED GROUND A/C DOOR PANEL ASSY IN REF TO SOPM 20-50-01. OPS TEST NORMAL AT THIS TIME

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,437 hrs · 35,906 cycles

L2 DOOR SLIDE GIRT BAR STRAP OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,675 hrs · 34,757 cycles

RT OVER WING EXIT FORWARD LOWER EMERGENCY EXIT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 59,675 hrs · 34,757 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 46. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (L1 DOOR AREA) · airframe 59,675 hrs · 34,757 cycles

L1 DOOR AFT GIRT BAR FITTING ATTACH CHANNEL CORRODED. R & R THE CHANNEL IAW DWG AND SRM.

Part: CHANNEL — CORRODED (BS 332) · airframe 59,675 hrs · 34,757 cycles

R1 DOOR INBOARD OF THRESHOLD WEB, CHANNEL LOWER MAIN SILL STRUCTURE CORRODED AT BS 332.10. R & R THE CHANNEL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,675 hrs · 34,757 cycles

R1 DOOR INBOARD OF THRESHOLD WEB CHANNEL LOWER MAIN SILL STRUCTURE CORRODED AT BS 332.10. R&R STRAP IAW DWG AND SRM.

Part: COVER — LOOSE (R1 DOOR SLIDE) · airframe 59,619 hrs · 34,724 cycles

R1 DOOR SLIDE MANUAL RELEASE HANDLE COVER LOOSE. SECURED THE COVER IAW MT.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 59,619 hrs · 34,724 cycles

L2 DOOR SLIDE MANUAL RELEASE HANDLE COVER LOOSE. SECURED COVER IAW MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 59,197 hrs · 34,462 cycles

L1 DOOR SLIDE LOOSE. SECURED THE SLIDE ASSY IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 58,229 hrs · 33,845 cycles

FORWARD UPPER EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,567 hrs · 33,438 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 56,344 hrs · 32,705 cycles

LEFT EMERGENCY EXIT HATCH, EMERGENCY LIGHT LENS BROKEN. R & R THE LIGHT ASSY IAW MM.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 56,178 hrs · 32,602 cycles

RIGHT AFT OVERWING EMERGENCY EXIT WINDOW LIGHT ELECTRICAL CONNECTOR BROKEN. R & R THE LIGHT ASSEMBLY PER AMM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 56,178 hrs · 32,602 cycles

LT MAIN LANDING GEAR WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 45.64 TO LBL 31.83. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 56,178 hrs · 32,602 cycles

RIGHT WING NR 7 SLAT LOWER SURFACE CRACKED IN SKIN AROUND ACTUATOR RIBS. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,178 hrs · 32,602 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE 4TH INTERNAL RIB CRACKED AT FASTENER. R & R RIB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 56,178 hrs · 32,602 cycles

LEFT HORIZONTAL STAB HSS 138.70 RIB VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: KEELBEAM — CRACKED (BS 663) · airframe 56,178 hrs · 32,602 cycles

KEEL BEAM CRACKED AT FORWARD SIDE OF BS 663, LBL 8, AT SECOND FASTENER OUTBOARD. REPAIRED THE KEELBEAM IAW EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 56,178 hrs · 32,602 cycles

LEFT HORIZONTAL STABILIZER RIB FLANGE CRACKED AT BS 92.70. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CRACKED (BS 540) · airframe 56,178 hrs · 32,602 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CRACKED (BS 540) · airframe 56,178 hrs · 32,602 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,178 hrs · 32,602 cycles

EXTERNAL POWER RECEPTACLE DOOR CUTOUT STRUCTURE CRACKED. REPAIRED CUTOUT IAW ER AND EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,178 hrs · 32,602 cycles

BATTERY PACK M1675 FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,332 hrs · 31,481 cycles

FORWARD RT BATTERY PACK FAILED TIME CHECK ON CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLAT — DAMAGED (RT WING) · airframe 54,332 hrs · 31,481 cycles

RT WING NR 5 L/E SLAT OTBD UPPER T/E DAMAGED. R & R SLAT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,332 hrs · 31,481 cycles

AFT RT BATTERY PACK FAILED TIME CHECK ON CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,332 hrs · 31,481 cycles

AFT LT BATTERY PACK FAILED TIME CHECK ON CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLAT — DAMAGED (RT WING) · airframe 54,332 hrs · 31,481 cycles

RIGHT WING NR 5 L/E SLAT OTBD UPPER T/E DAMAGED. REPAIRED SLAT IAW EA.

Part: PUMP — LOW PRESSURE (HYDRAULIC SYS) · airframe 51,713 hrs · 29,936 cycles

DIVERSION, ENG DRIVEN HYD A SYS PUMP LOW PRESS LIGHT ILLUMINATED A SYS TO 17%. R & R NR 1 ENG DRIVEN PUMP IAW MM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 50,578 hrs · 29,303 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP IAW MT.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,066 hrs · 29,028 cycles

MAIN CABIN INTERIOR SIDE OF LT MAIN WW CHORD CRACKED AT BS 663, LBL 37 AT BALL DRAIN CUT OUT. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 50,066 hrs · 29,028 cycles

VERTICAL PRESS DECK LOWER CHORD CRACKED AT BS 663, LBL 34.5. REPAIRED CHORD IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,066 hrs · 29,028 cycles

LEFT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED AT LOWER PART OF RADIUS. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN REAR SPAR CRACKED AT STAB STATION 98.90. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,066 hrs · 29,028 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, APPROX 30 INCHES AFT OF LE SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, APPROX 11 INCHES AFT OF LE SPAR. REPAIRED RIB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,066 hrs · 29,028 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, RBL 39. REPAIRED WEB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, APPROX 30 INCHES AFT OF LE SPAR. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,066 hrs · 29,028 cycles

RIGHT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED AT LOWER PART OF RADIUS. REPAIRED FRAME IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,066 hrs · 29,028 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST THIRD HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,066 hrs · 29,028 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST SECOND HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, APPROX 20 INCHES AFT OF LE SPAR. REPAIRED RIB IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,066 hrs · 29,028 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST SECOND HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 101, APPROX 10 INCHES FROM FWD SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 147.90, 16 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,066 hrs · 29,028 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR LOWER IN SPAR SKIN CRACKED AT STAB STATION 97. REPAIRED SKIN IAW SRM.

Part: SIGN — DETACHED (CABIN) · airframe 49,465 hrs · 28,690 cycles

MID CABIN OVERWING EXIT SIGN DETACHED. R & R SIGN ASSEMBLY IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 48,287 hrs · 27,975 cycles

CENTER OVERWING EXIT SIGN LENS LOOSE. SECURED LENS IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 47,890 hrs · 27,752 cycles

R2 DOOR EXIT LIGHT SIGN BROKEN. R & R SIGN IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 47,831 hrs · 27,719 cycles

L2 DOOR EMER EXIT LIGHT ASSEMBLY LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,698 hrs · 27,641 cycles

MID CABIN EMER LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 50,066 hrs · 29,028 cycles

LEFT OVERHEAD EMER LIGHT ASSEMBLY BROKEN AT ROW 4. R & R LIGHT IAW MMM.

Part: LENS — LOOSE (CABIN) · airframe 45,497 hrs · 26,347 cycles

LT BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 11. SECURED LIGHT IAW AMM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 45,444 hrs · 26,313 cycles

RT WING UPPER SHELF PANEL AFT SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 45,201 hrs · 26,172 cycles

MID CABIN EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,433 hrs · 25,706 cycles

LT AFT EMERGENCY AREA LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 44,433 hrs · 25,706 cycles

RT FWD OVERWING EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

AFT GALLEY FLOOR STRUCTURE, STA 1016 LBL 36, LEFT FLOOR WEB CRACKED AT AFT O/B CORNER FASTENER. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FRAME CORRODED AT BS 540, STR 9L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FRAME CORRODED AT BS 540, STR 10R. REPAIRED SPLICE IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

STRINGER CLIP DAMAGED AT BS 380, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

L1 DOOR UPPER AFT CORNER EXTERIOR SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FUSELAGE INTERNAL STA 907 BELOW STR 8L CRACK INDICATION ON FRAME INBD FASTENER FOR DISTRIBUTION DUCT ATTACH BRACKET. REPAIRED BRACKET PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FUSELAGE FRAME BRACKET CRACKED AT BS 400, STR 8R. REPAIRED BRACKET PER EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 43,217 hrs · 24,988 cycles

NR 6 CANOE FAIRING AT AFT END HAS A CRACK THAT RUNS THROUGH A NUT PLATE FOR AFT FAIRING. REPAIRED FAIRING PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,217 hrs · 24,988 cycles

AFT CARGO PIT FLOOR TRACK HEAVILY CORRODED FROM STA 787-807, RBL 14. REMOVED AND REPLACED FLOOR TRACK PER SRM.

Part: WEB — CRACKED (LT MLG WW) · airframe 43,217 hrs · 24,988 cycles

LEFT W/W FIBERGLASS WEB 16" CRACKED STA 663 LBL 32"-37". REPAIRED WEB PER EA 1-A53-3376.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,217 hrs · 24,988 cycles

AFT CARGO PIT FLOOR TRACK STA 794 RBL 13.8 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FLOOR TRACK PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FLOOR SUPPORT ANGLE CORRODED AT FS 270, BETWEEN RBL RBL 10 TO LBL 10. REPAIRED ANGLE PER EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

LEFT A/C BAY AFT WEB AT STA 663, LBL 60, 10 INCHES DOWN FROM CENTER TANK SKIN, DOUBLER FOR HYDRAULIC LINES IS CRACKED. REMOVED AND REPLACED DOUBLERS IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,217 hrs · 24,988 cycles

LEFT W/W FWD BULKHEAD STA 663 CRACKED APPROX 6" LONG BEHIND FILLER ASSY LBL 29 APPROX, 6" FROM BOTTOM OF W/W CUTOUT. REPAIRED PER EA 1-A53-3376.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FORWARD ENTRY DOOR THRESHOLD "Z" ANGLE CRACKED AT FLOOR LEVEL STA 294.5. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

INTERCOSTAL CRACKED TWO PLACES STA 312-328 RBL 33. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 43,217 hrs · 24,988 cycles

RIGHT WING UPPER SURFACE, SUPPORT BRACKET CRACKED UNDER PANEL 651AT AT THE FORWARD INBOARD CORNER. REMOVED AND REPLACED SUPPORT BRACKET PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

Z-ANGLE CORRODED IN FWD ENTRY DOOR THRESHOLD AREA STA 294-328 IN NUMEROUS AREAS. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

INBOARD AFT HOLE AND OUTBOARD FWD HOLE CRACKED AT STA 727B AT RBL 24.75. REPAIRED BEAM PER EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 43,217 hrs · 24,988 cycles

LEFT W/W ANGLE CRACKED AT BS 663, LBL 27. REMOVED AND REPLACED ANGLE PER SRM.

Part: TAIL CONE — DELAMINATED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

TAIL CONE IS DELAMINATED ON TOP UPPER LEFT SIDE. REPAIRED TAIL CONE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

INTERCOSTAL CRACKED IN TWO LOCATIONS STA 270-294 BL 0. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,217 hrs · 24,988 cycles

LEFT W/W FWD BULKHEAD STA 663 CRACKED APPROX 8" LONG BEHIND FILLER ASSY LBL 32 APPROX, 20" FROM BOTTOM OF W/W CUTOUT. REPAIRED PER EA 1-A53-3376.

Part: ACCESS PANEL — DELAMINATED (NR 2 NACELLE) · airframe 43,217 hrs · 24,988 cycles

NR 2 ENGINE ACCESS PANEL 441AL, IS DELAMINATED. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,217 hrs · 24,988 cycles

LEFT W/W FWD BULKHEAD STA 663 CRACKED APPROX 12" LONG BEHIND HYD FUSE LBL 38 APPROX, 8" FROM BOTTOM OF W/W CUTOUT. REPAIRED PER EA 1-A53-3376.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

FLOOR PANEL STRAP AT STA 772 HAS LIGHT CORROSION. REMOVED AND REPLACED FLOOR STRAP IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

AFT CARGO FLOOR TEE STRAP AT BS 771 HAS CORROSION. REMOVED AND REPLACED T-STRAP PER SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,217 hrs · 24,988 cycles

STA 727B AT LBL 45.5, INBOARD FORWARD SEAT TRACK HOLE IS CRACKED (HOLE SIZE IS .247). REPAIRED PER EA1-757-7897.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 43,217 hrs · 24,988 cycles

R1 DOOR SLIDE COVER APPEARS TO BE COMING OFF SLIDE PACK INSIDE SLIDE COMPARTMENT. REPOSITIONED SLIDE IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,217 hrs · 24,988 cycles

RIGHT HORIZ STAB LOWER INSPAR SKIN 3/8" CRACKED AT STA 101.90, 9" FROM REAR SPAR. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 43,217 hrs · 24,988 cycles

EGRESS LIGHTING - FLOOR STRIP COVER CRACKED AT 1ABC, 4ABC, 5ABC, 6ABC, 7ABC, 8ABC AND 17ABC. REMOVED AND REPLACED EEPLS PER MM.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 41,460 hrs · 23,883 cycles

DIVERSION - NR 1 ENGINE DRIVEN PUMP FAILED. LOST A SYSTEM QUANTITY. REMOVED AND REPLACED NR 1 ENGNE DRIVEN PUMP, CASE DRAIN FILTER, SYSTEM A HYDRAULIC EMPD, AND A HYDRAULIC EMDP ACOUSITC FILTER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,454 hrs · 23,880 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 41,231 hrs · 23,752 cycles

FLOOR TRACK LIGHTING COVER CRACKED AT 20C. REMOVED AND REPLACED COVER PER MM

Part: ISOLATOR — CRACKED (CABIN) · airframe 41,231 hrs · 23,752 cycles

R1 DOOR ESCAPE SLIDE COVER AFT MOUNTING BRACKET ATTACH ISOLATOR CRACKED. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE COVER AFT MOUNTING BRACKET ATTACH ISOLATOR PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 41,231 hrs · 23,752 cycles

L1 DOOR ESCAPE SLIDE COVER AFT GIRT BAR STOW HOOK IS LOOSE. REMOVED AND REPLACED FASTENERS IN L1 DOOR ESCAPE SLIDE COVER AFT GIRT BAR STOW HOOK PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 40,818 hrs · 23,528 cycles

LEFT EEPLS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: FITTING — LOOSE (GIRT BAR) · airframe 4,037 hrs · 23,085 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,037 hrs · 23,085 cycles

EMERGENCY EXIT LIGHTS INOP BETWEEN ROWS 1 AND ROW 16. REMOVED AND REPLACED LIGHTS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 39,699 hrs · 22,870 cycles

LT EEPLS LENS MISSING AT ROW 16. INSTALLED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 39,012 hrs · 22,470 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT FWD CABIN EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,012 hrs · 22,470 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT AFT CABIN EEPLS INOP AT ROW 18. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,012 hrs · 22,470 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT AFT CABIN EEPLS INOP AT ROW 13. RELAMPED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,580 hrs · 21,041 cycles

DURING SCHEDULED HC2 CHECK, FOUND CENTER EMERGENCY EXIT LIGHTS LOOSE. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 36,580 hrs · 21,041 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 36,580 hrs · 21,041 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,371 hrs · 20,922 cycles

FWD EEPLS INOP. RELAMPED PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR L-ANGLE CORRODED AT BS 270, BL 0. REMOVED AND REPLACED L-ANGLE PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 270, BL 0. REMOVED AND REPLACED WEB PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 546, LBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 546, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 546, RBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 546, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 546, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,280 hrs · 20,879 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 546, LBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,212 hrs · 20,834 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 35,530 hrs · 20,440 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,165 hrs · 20,214 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTNG PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,165 hrs · 20,214 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTNG PER EA.

Part: COVER — CRACKED (CABIN) · airframe 34,453 hrs · 19,820 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT BS 13. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,132 hrs · 19,625 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,614 hrs · 19,319 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD BIN EMERGENCY EXIT LIGHT INOP AT ROW 21. RELAMPED LIGHT ASSY PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 32,801 hrs · 18,864 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED BRACKET PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 32,801 hrs · 18,864 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED. REPAIRED SLAT PER AAR EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 32,193 hrs · 18,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120.3. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 31,287 hrs · 17,928 cycles

L1 COCKPIT WINDOW ARCED AND SHATTERED. REMOVED AND REPLACED WINDOW PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 986, RBL 45. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 44. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT CREASE BEAM CORRODED AT R2 DOOR LOWER SILL. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CABIN FLOORBEAM CORRODED AT BS 295, RBL 10. REPAIRED BEAM PER AAR EA.

Part: SKIN — WORN (VERTICAL STAB) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND L/E DORSAL FIN SKIN WORN BETWEEN BS 850 TO BS 853. REPAIRED DOUBLER PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 120. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,684 hrs · 16,940 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CABIN CREASE BEAM CORRODED BETWEEN BS 295 TO BS 328, RBL 56. REPAIRED BEAM PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 29,645 hrs · 16,913 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,566 hrs · 16,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND OVERHEAD BIN EXIT LIGHT INOP AT ROW 15. REMOVED AND REPLACED LAMP ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 29,127 hrs · 16,618 cycles

FWD FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,815 hrs · 16,428 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 1. REPAIRED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,816 hrs · 16,428 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP INOP AT ROW 1. REPAIRED STRIP PER MM.

Part: SIGN — MISSING (CABIN) · airframe 28,495 hrs · 16,255 cycles

FOUND FWD MID CABIN EMERGENCY EXIT SIGN MISSING. REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,425 hrs · 16,220 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT STRIP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 27,710 hrs · 15,778 cycles

EEPLS LENS LOOSE AT ROW 5 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 27,466 hrs · 15,640 cycles

EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,288 hrs · 15,534 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,099 hrs · 15,408 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,091 hrs · 14,204 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (CABIN) · airframe 25,083 hrs · 14,198 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,996 hrs · 13,544 cycles

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

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 23,924 hrs · 13,503 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,917 hrs · 12,912 cycles

DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,917 hrs · 12,912 cycles

DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 20,529 hrs · 11,557 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 20,529 hrs · 11,557 cycles

DURING SCHEDULED HC1 CHECK, FOUND MID CABIN EEPLS LIGHT COVERS CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 20,529 hrs · 11,557 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 20,529 hrs · 11,557 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 20,529 hrs · 11,557 cycles

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

Part: ACM — ODOR (AC BAY) · airframe 20,004 hrs · 11,255 cycles

DIVERSION - DURING FLIGHT AIRCRAFT DEVELOPED A STRONG OILY SMELL IN THE MAIN CABIN. ALL ENGINE AND HYDRAULIC INDICATIONS NORMAL. INSPECTED AND CLEANED AIR CONDITIONER DUCTS IN THE A/C BAY PER MM. REMOVED AND REPLACED LT PRIMARY AND SECONDARY HEAT EXCHANGERS PER MM. REMOVED AND REPLACED LT ACM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,991 hrs · 10,668 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK INOP AT FWD END. RELAMPED LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,749 hrs · 10,529 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 17,886 hrs · 10,038 cycles

EEPLS TRACK COVER MISSING AT ROW 1. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,497 hrs · 9,294 cycles

EEPLS TRACK COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 15,687 hrs · 8,836 cycles

EEPLS COVER DAMAGED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,092 hrs · 8,507 cycles

R1 COCKPIT WINDOW ARCED & OUTER PANE SHATTERED. REMOVED AND REPLACED R1 WINDOW & HEAT CONTROLLER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,404 hrs · 8,151 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 14,228 hrs · 8,044 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 14,170 hrs · 8,012 cycles

EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,881 hrs · 7,840 cycles

FWD MOST LT EEPLS INOP. RELAMPED PER MM.

Part: LIGHT — LOOSE (GALLEY) · airframe 13,582 hrs · 7,660 cycles

FWD EEPLS STRIP NEAR FWD GALLEY LOOSE. SECURED EEPLS STRIP PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 9,475 hrs · 5,355 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 10. REMOVED AND REPLACED COVER PER MM.

Part: BULB — INOPERATIVE (EXIT LIGHT) · airframe 9,449 hrs · 5,338 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 8,404 hrs · 4,769 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 8,269 hrs · 4,683 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT OVERWING EXIT. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 7,057 hrs · 4,012 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT ILLUMINATE FROM COCKPIT SWITCH. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 10,063 hrs · 622 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EMERGENCY EVAC SLIDE PER MM.

Part: LATCH — UNSECURE (COCKPIT) · airframe 755 hrs · 443 cycles

COCKPIT DOOR EMERGENCY EXIT HATCH NOT SECURED. RESEATED EMERGENCY EXIT LATCHES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 472 hrs · 278 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 18 DEF. RELAMPED BULLNOSE LIGHT PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 93 hrs · 69 cycles

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