N550WN

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 67,499 hrs · 41,963 cycles

L/H LOWER INBD FIXED TRAILING EDGE PANEL HAS 2 CRACKS AND 1 DENT FROM IMPACT<[01] REPLACED THE LEFT WING LOWER INBOARD FIXED TRAILING EDGE PANEL REF AMM 57-50-02.

Part: PANEL — CRACKED (LT WING) · airframe 67,499 hrs · 41,963 cycles

LH LOWER INBD TRAILING EDGE PANEL FWD OF MLG IS BENT AND CRACKED PANEL 551CB. REMOVED AND REPLACED LH LOWER INBD TRAILING EDGE PANEL FWD OF MLG PER SIP

Part: TIRE — FAILED (MLG) · airframe 67,499 hrs · 41,963 cycles

NR 2 TIRE TREAD LOSS ON TAKEOFF OUT OF TPA<[01] R&R #1 AND #2 TIRES MAIN TIRES PER AMM 32-45-11 & AMM 12-15-51 TIRE SERVICING.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 67,434 hrs · 41,926 cycles

EMEERGENCY LIGHT NEXT TO AFT SERVICE DOOR INOP<[01] RE-LAMPED PER AMM 33-51-04

Part: GIRT BAR — DISPLACED (ZN 800 DOOR) · airframe 66,864 hrs · 41,565 cycles

R1 DOOR ESCAPE SLIDE GIRT DISPLACED.<[01] SECURED R1 DOOR ESCAPE SLIDE GIRT PER AMM 25-66-01

Part: GIRT BAR — DISPLACED (ZN 800 DOOR) · airframe 66,864 hrs · 41,565 cycles

L1 DOOR ESCAPE SLIDE GIRT DISPLACED.<[01] SECURED L1 DOOR ESCAPE SLIDE GIRT PER AMM 25-66-01

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 66,547 hrs · 41,368 cycles

EMERGENCY CHARGER LEFT AFT C/B OUT; WILL NOT RESET<[01] FOUND EMERGENCY LIGHT BATTERY CHARGERS BAD. R & R CHARGER AND BATTERY PACK PER MM 33-51-06.

Part: LAMP — INOPERATIVE (ZN 200 FUS TOP) · airframe 65,675 hrs · 40,825 cycles

AFT MAIN ENTRY SLIDE EMERGENCY LIGHT INOP<[01] R/R AFT MAIN ENTRY SLIDE EMERGENCY LAMP I.A.W AMM 33-51-04 OPS CHECK GOOD.

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 65,420 hrs · 40,649 cycles

PROVO FWD INSIDE DOOR HANDLE SPRINGS UP 1/2 WHEN CLOSED. NO DOOR LIGHTS ILLUMINATED; PRESSURIZATION NORMAL.<[01] RESECURED FWD SERVICE DOOR HANDLE HARDWARE PER AMM 52-41-11. NO DISCREPENCIES NOTED AT THIS TIME

Part: HANDLE — LOOSE (SERVICE DOOR) · airframe 65,228 hrs · 40,522 cycles

FORWARD SERVICE DOOR HANDLE INSIDE AIRCRAFT IS LOOSE. TIGHTENED FWD SVC DOOR HANDLE REF AMM 52-11-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 64,956 hrs · 40,344 cycles

BURNED OUT BULB IN AN EXTERIOR EMERGENCY LIGHT LOCATED BEHIND AFT SERVICE DOOR. REPLACED THE BULB IAW AMM 33-51-04-960-801, TESTED OK.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 64,956 hrs · 40,344 cycles

CRACKED CENTER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. C.

Part: WEB — CORRODED (BS 787-807) · airframe 64,956 hrs · 40,344 cycles

CORROSION ON WEB LOCATED BETWEEN BS787 TO BS807 AT LEVEL STR 27R RBL6 WL 151 AFT CARGO COMPARTMENT 2022-636251 / [01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45MG; S/N: 130063701; DUE DATE: 16 JUN 23.;[02] REPLACED WEB LOCATED BETWEEN BS787 TO BS807 AT LEVEL STR 27R RBL6 WL 151 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 146A8130 SHEET 12 REV B SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED WEB LOCATED BETWEEN BS787 TO BS807 AT LEVEL STR 27R RBL6 WL 151 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 146A8130 SHEET 12 REV B SEE INDIVIDUAL SIGN OFFS BELOW<BR>RII

Part: SUPPORT — CORRODED (BS 727-847) · airframe 64,956 hrs · 40,344 cycles

CORROSION ON SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL 21 WL 156 AT LEVEL STR 25L AFT CARGO COMPARTMENT 2022-636250. REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL 21 WL 156 AT LEVEL STR 25L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0;SRM 51-40-02-0G-0 AND DWG 146A7500 REV -. SEE INDIVIDUAL SING-OFF BELOW.;[02] TASK CARD COMPLETED

Part: LIGHT — DETERIORATED (CABIN) · airframe 64,956 hrs · 40,344 cycles

DETERIORATED FLOOR PANEL PHOTOLUMINESCENT STRIP AT PASSENGER CABIN ( 3 EA) 2022-635784 / [01] REPLACED FLOOR PANEL PHOTOLUMINESCENT STRIP AT PASSENGER CABIN ( 3 EA) IAW AMM 33-51-15-400-802;[02] TASK CARD COMPLETED

Part: SUPPORT CHANNEL — CORRODED (BS 727-787 S25R) · airframe 64,956 hrs · 40,344 cycles

CORROSION SUPPORT CHANNEL SIDEPLATE LOCATED FROM BS 727 - 787, S25R, WL 156, IN THE AFT CARGO BAY. INSTALLED A NEW SUPPORT CHANNEL IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 146A7500, REV -.

Part: INTERCOSTAL — CRACKED (BS 440-460) · airframe 64,956 hrs · 40,344 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AND STR26L FWD CARGO COMPARTMENT 2022-636220 / [01] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A029157 ;DUE DATE 02-FEB-23;[02] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A21029157 ;DUE DATE 02-FEB-23;[03] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV:- SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (BS 460 S26L) · airframe 64,956 hrs · 40,344 cycles

CRACK ANGLE - CLIP LOCATED BETWEEN BS460 AND STR26L FWD CARGO COMPARTMENT 2022-636221 / [01] TOOL USED DIGITAL CALIPER : P/N 500-196-30; S/N A21029157 ;DUE DATE 02-FEB-23;[02] REPLACED ANGLE - CLIP LOCATED BETWEEN BS460 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED ANGLE - CLIP LOCATED BETWEEN BS460 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII

Part: INTERCOSTAL — CRACKED (BS 500B-500C) · airframe 64,956 hrs · 40,344 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26L FWD CARGO COMPARTMENT 2022-636218 / [01] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A029157 ;DUE DATE 02-FEB-23;[02] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A21029157 ;DUE DATE 02-FEB-23;[03] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26L FWD CARGO COMPARTMENT IAW B-737-700 SRM 51-40-02 AND DWG#143A7505 SHEET 6 REV D SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26L FWD CARGO COMPARTMENT IAW B-737-700 SRM 51-40-02 AND DWG#143A7505 SHEET 6 REV D; RII. SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 64,956 hrs · 40,344 cycles

CRACK ANGLE - CLIP LOCATED BETWEEN BS400 AND STR26L FWD CARGO COMPARTMENT 2022-636223 / [01] TOOL USED DIGITAL CALIPER P/N : 500-196-30; S/N A21029157; DUE DATE 02-FEB-22;[02] TOOL USED DIGITAL CALIPER P/N : 500-196-30; S/N A21029157; DUE DATE 02-FEB-23;[03] REPLACED ANGLE - CLIP LOCATED BETWEEN BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505. REV:- SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (BS 440 S26L) · airframe 64,956 hrs · 40,344 cycles

CRACK ANGLE - CLIP LOCATED BETWEEN BS440 AND STR26L FWD CARGO COMPARTMENT 2022-636222 / [01] TOOL USED DIGITAL CALIPER : P/N 500-196-30; S/N A21029157 ;DUE DATE 02-FEB-23;[02] REPLACED ANGLE - CLIP LOCATED BETWEEN BS440 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV:- SEE INDIVIDUAL SIGNOFFS<BR>BELOW;[03] REPLACED ANGLE - CLIP LOCATED BETWEEN BS440 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV:- SEE INDIVIDUAL SIGNOFFS BELOW ITEM RII

Part: INTERCOSTAL — CRACKED (BS 500-500A) · airframe 64,956 hrs · 40,344 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AND STR26L FWD CARGO COMPARTMENT 2022-636219 / [01] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A029157 ;DUE DATE 02-FEB-23;[02] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A021029157 ;DUE DATE 02-FEB-23;[03] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A021029157 ;DUE DATE 02-FEB-23;[04] REPLACED WEB -INTERCOSTAL LOC. BETWEEN BS500 TO BS500A AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 SHEET: 82 REV: - <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[05] CERTIFIED STEP 4 COMPLETED. ITEM RII

Part: ANGLE — CRACKED (BS 400 S26R) · airframe 64,956 hrs · 40,344 cycles

CRACK ANGLE - CLIP LOCATED BETWEEN BS400 AND STR26R FWD CARGO COMPARTMENT 2022-636224 / [01] TOOL USED DIGITAL CALIPER P/N : 500-196-30; S/N A21029157; DUE DATE 02-FEB-23;[02] REPLACED ANGLE - CLIP LOCATED BETWEEN BS400 AND STR26R FWD CARGO COMPARTMENT IAW B-737-700 SRM 51-40-02 AND DWG#143A7505 SHEET 81 REV- SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED ANGLE - CLIP LOCATED BETWEEN BS400 AND STR26R FWD CARGO COMPARTMENT IAW B-737-700 SRM 51-40-02 AND DWG#143A7505 SHEET 81 REV-RII; SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (BS 500D-520) · airframe 64,956 hrs · 40,344 cycles

CRACK WEB - INTERCOSTAL LOCATED BS500D TO BS520 AT LEVEL STR25R FWD CARGO COMPARTMENT 2022-636168 / [01] REPLACED WEB INTERCOSTAL LOCATED BS500D TO BS520 AT LEVEL STR25R FWD CARGO COMPARTMENT IAW B-737-700 SRM 51-40-02; B-737-700 SRM 51-10-02 ; DWG#143A7902 SHEET 127 REV A AND DWG#143A9801 SHEET 12 REV-;[02] STEP 1 ENTERED IN ERROR; CORRECT STEP IS:<BR>REPLACED WEB INTERCOSTAL LOCATED BS500D TO BS520 AT LEVEL STR25R FWD CARGO COMPARTMENT IAW B-737-700 SRM 51-40-02; B-737-700 SRM 51-10-02 ; DWG#143A7902 SHEET 127 REV A AND DWG#143A9801 SHEET 12 REV-<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — ELONGATED (BS 849-867 S25R) · airframe 64,956 hrs · 40,344 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOCATED BS849 TO BS867 AT LEVEL STR25R AFT CARGO COMPARTMENT 2022-636148 / [01] REPLACED WEB - INTERCOSTAL LOCATED BS849 TO BS867 AT LEVEL STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 REV: A SHEET:19.

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 64,956 hrs · 40,344 cycles

CRACK STRINGER 25R AT BS540 FWD CARGO COMPARTMENT 2022-636140 / [01] TOOL USED : P/N 45MG S/N :130066701 DUE DATE : 08-APR-23.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200053402 DUE DATE: 13-MAY-23.;[04] REPAIRED STR 25R BTW BS 500C TO BS 540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGN OFFS BELOW;[05] REPAIRED STR 25R BTW BS 500C TO BS 540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: STRAP — CORRODED (ZONE 100) · airframe 64,956 hrs · 40,344 cycles

CORROSION STRAP LOCATED BS787 TO BS794 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT 2022-636150 / [01] REPLACED STRAP LOCATED BS787 TO BS794 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND ITEM 9. DWG 143A8340 REV B.;[02] CORRECTED STEP 1 REPLACED STRAP LOCATED BS787 TO BS794 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND ITEM 9. DWG 143A8340 REV B. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 REPLACED STRAP LOCATED BS787 TO BS794 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND ITEM 9. DWG 143A8340 REV B. RII; SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 64,956 hrs · 40,344 cycles

CRACK STRINGER 25L AT BS540 FWD CARGO COMPARTMENT 2022-636141 / [01] TOOL USED : P/N 45MG S/N :130066701 DUE DATE : 08-APR-23.;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; DUE DATE: 11-APR-23;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23.;[04] REPAIRED STRINGER 25L BTW BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGN OFFS BELOW;[05] REPAIRED STRINGER 25L BTW BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGN OFFS BELOW

Part: ACCESS PANEL — BROKEN (LT WING) · airframe 64,956 hrs · 40,344 cycles

BROKEN ACCESS PANEL 532NB FUEL TANK FLOAT ON THE LT WING. REPLACED THE ACCESS PANEL IAW CMM 28-40-11, DISASSEMBLY STEP 2, B, H, 1. AND ASSEMBLY STEP 2, B, 5.

Part: SUPPORT BRACKET — CORRODED (LT WING) · airframe 64,956 hrs · 40,344 cycles

CORRODED SUPPORT BRACKET AT BOOST PUMP TANK 1 AFT IRSS145, LT WING. REPLACED THE SUPPORT BRACKET IAW AMM 28-22-41-000-801, STEP 2.H. 8, 9, 10, AND AMM 28-22-41-400-801, STEP 3, H, 18, 20, 21, 23, E, F. ELECTRICAL BONDING RESISTANCE OK.

Part: INTERCOSTAL — CORRODED (BS 492-500) · airframe 64,956 hrs · 40,344 cycles

CORROSION WEB - INTERCOSTAL LOCATED BS492 TO BS500 AT LEVEL STR 26R AND WL156 FWD CARGO COMPARTMENT 2022-636120 / [01] REPLACED WEB INTERCOSTAL LOCATED BS492 TO BS500 AT LEVEL STR 26R AND WL156 FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DRAWING 143A0080 SHEET 19 REV -<BR>SEE INDIVIDUAL SINGOFF BELOW;[02] JOB COMPLETED AND CERTIFIED AS RII.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 64,956 hrs · 40,344 cycles

CRACK ON ACCESS PANEL 661BB ON THE RT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ACCESS PANEL — DELAMINATED (BODY FAIRING) · airframe 64,956 hrs · 40,344 cycles

DELAMINATED ACCESS PANEL 192HL BODY FAIRING. REPAIRED THE ACCESS PANEL 192HL IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ACCESS PANEL — DELAMINATED (BODY FAIRING) · airframe 64,956 hrs · 40,344 cycles

DELAMINATED ACCESS PANEL 192HR BODY FAIRING. REPAIRED THE ACCESS PANEL 193HR IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: BALANCE WEIGHT — CORRODED (RT WING AILERON) · airframe 64,956 hrs · 40,344 cycles

CORROSION ON BALANCE WEIGHTS POSITION NR 3, UPPER AILERON, IN THE BALANCE BAY NR 5, RT WING. REPLACED THE AILERON BALANCE WEIGHT IAW SRM 51-60-01-0G-0, STEP 5.A. 5 . D.

Part: BALANCE WEIGHT — CORRODED (LT WING AILERON) · airframe 64,956 hrs · 40,344 cycles

CORROSION ON BALANCE WEIGHTS POSITION NR 3, UPPER AND LOWER AILERON, BALANCE BAY NR 5, LT WING. REPLACED THE AILERON BALANCE WEIGHTS IAW SRM 51-60-01-0G-0 STEP 5, A, 5, D.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 64,956 hrs · 40,344 cycles

BROKEN AFT LAVATORY B EMERGENCY LIGHT COVER. REPLACED THE EMERGENCY LIGHT COVER IAW AMM 33-51-01-960-802.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 64,956 hrs · 40,344 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.000 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.300 INCH 2022-636045 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N:NORTEC600D; S/N 60009161631; DUE DATE: 03-DEC-22;[02] REPAIRED RH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STAB STA 193.90; 16 INCH FROM FRONT SPAR I.A.W B737-700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK CARD COMPLETED <BR>REPAIRED RH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STAB STA 193.90; 16 INCH FROM FRONT SPAR I.A.W B737-700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: SEAT TRACK — CORRODED (BS 827-847) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED BETWEEN BS 827 AND BS 847 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN 2022-635966 / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:A21146537; DUE DATE: 29-OCT-23.;[02] REMOVED CORROSION ON SEAT TRACK LOCATED BETWEEN BS 827 AND BS 847 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN AND EVALUATED REWORK AREA AND FOUND WITHIN LIMITS IAW B737-700 B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A(2) FIGURE 103; DETAIL A. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CORRECTED CORRECTIVE ACTION.<BR>REMOVED CORROSION ON SEAT TRACK LOCATED BETWEEN BS 827 AND BS 847 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND EVALUATED REWORK AREA AND FOUND WITHIN LIMITS IAW B737-700 B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A(2) FIGURE 103; DETAIL A. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REMOVED CORROSION ON SEAT TRACK LOCATED BETWEEN BS 827 AND BS 847 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND EVALUATED REWORK AREA AND FOUND WITHIN LIMITS IAW B737-700 B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A(2) FIGURE 103; DETAIL A. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SEAT TRACK — CORRODED (BS 727A-727B) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED BETWEEN BS 727A AND BS 727B RBL 45 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN 2022-635963 / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N: 15319560; DUE DATE: 30-JUN-23.;[02] REMOVED CORROSION AND EVALUATED REWORKED AREA LOCATED BETWEEN BS 727A AND BS 727B RBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[03] CORRECTED CORRECTIVE ACTION.<BR>REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 727A AND BS 727B RBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW.;[04] CORRECTED CORRECTIVE ACTION STEP 3<BR>REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 727A AND BS 727B RBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,956 hrs · 40,344 cycles

INOP BATTERY PACK LOWER SIDEWALL PANEL EMERGENCY EXIT LT SIDE AT PASSENGER CABIN. BATTERY PACK LOWER SIDEWALL PANEL EMERGENCY EXIT LT SIDE AT PASSENGER CABIN AND PERFORMED OPERATIONAL TEST IS GOOD IAW B737-700 AMM-33-51-06-960-806. TEST FOUND ON SATISFACTORY CONDITION.

Part: SEAT TRACK — CORRODED (BS 847-867) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED BETWEEN BS 847 AND BS 867 RBL 45 BOTTOM SURFACE AT PASSENGER CABIN 2022-635965 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N:15319560; DUE DATE: 30-JUN-23.;[02] REMOVED CORROSION AND EVALUATED REWORKED AREA LOCATED BETWEEN BS 847 AND BS 867 RBL 45 BOTTOM SURFACE AW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[03] CORRECTED CORRECTIVE ACTION.<BR>REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 847 AND BS 867 RBL 45 BOTTOM SURFACE AW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW;[04] REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 847 AND BS 867 RBL 45 BOTTOM SURFACE AW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW

Part: SEAT TRACK — CORRODED (BS 663) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED AT BS 663.75 RBL 45 BOTTOM SURFACE WL 208.1 AT PASSENGER CABIN 2022-635962 / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N: 15319560; DUE DATE: 30-JUN-23.;[02] REMOVED CORROSION AND EVALUATED REWORKED AREA LOCATED AT BS 663.75 RBL 45 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[03] REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED AT BS 663.75 RBL 45 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS .SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: SEAT TRACK — CORRODED (BS 827) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK AT BS 827 RBL 45 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN 2022-635964 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N:15319560; DUE DATE: 30-JUN-23.;[02] REMOVED CORROSION AND EVALUATED REWORKED AREA LOCATED AT BS 827 RBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[03] CORRECTED CORRECTIVE ACTION.<BR>REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED AT BS 827 RBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW;[04] REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED AT BS 827 RBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW

Part: SEAT TRACK — CORRODED (BS 727D-727E) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED BETWEEN BS 727D AND BS 727E LBL 45 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN 2022-635970 / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N: 15319560; DUE DATE: 30-JUN-23.;[02] REMOVED CORROSION AND EVALUATED REWORKED AREA LOCATED BETWEEN BS 727D AND BS 727E LBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[03] CORRECTED CORRECTIVE ACTION.<BR>REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 727D AND BS 727E LBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW.;[04] CORRECTED CORRECTIVE ACTION STEP 3<BR>REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 727D AND BS 727E LBL 45 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS. SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: SEAT TRACK — CORRODED (BS 827) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED AT BS 827 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN 2022-635967 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21146537; DUE DATE: 29-OCT-23.;[02] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:A21041924; DUE DATE: 24-SEP-23.;[03] REMOVED CORROSION LOCATED ON SEAT TRACK AT BS 827 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND EVALUATED AND FOUND WITHIN LIMITS SRM 53-00-52-1A-1 PARAGRAPH 4.A(2) FIGURE 103; DETAIL A. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] CORRECTED CORRECTIVE ACTION.<BR>REMOVED CORROSION LOCATED ON SEAT TRACK AT BS 827 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND EVALUATED AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A(2) FIGURE 103; DETAIL A. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REMOVED CORROSION LOCATED ON SEAT TRACK AT BS 827 RBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND EVALUATED AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A(2) FIGURE 103; DETAIL A. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SEAT TRACK — CORRODED (BS 685-706) · airframe 64,956 hrs · 40,344 cycles

CORROSION SEAT TRACK LOCATED BETWEEN BS 685 AND BS 706 LBL 24.5 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN 2022-635968CORRECTED LOCATION: CORROSION SEAT TRACK LOCATED BETWEEN BS 685 AND BS 706 LBL 24.75 WL 208.1 BOTTOM SURFACE AT PASSENGER CABIN / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N: 15319560; DUE DATE: 30-JUN-23.;[02] REMOVED CORROSION AND EVALUATED REWORKED AREA LOCATED BETWEEN BS 685 AND BS 706 LBL 24.5 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITH LIMITS<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[03] REMOVED CORROSION AND EVALUATED REWORK AREA LOCATED BETWEEN BS 685 AND BS 706 LBL 24.5 WL 208.1 BOTTOM SURFACE IAW B737-700 SRM 53-00-52-1A-1 PARAGRAPH 4.A.(2) FIG 103; DETAIL A; AND FOUND WITHIN LIMITS .SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 690) · airframe 64,956 hrs · 40,344 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 690 LBL24.5 WL 208 CENTER SECTION 2022-635800 / [01] TOOLS USED: TEMPERATURE CONTROLLER: PN: P3015GOES00000; S/N: 112820025 DUE DATE 01-FEB-23 AND TEMPERATURE CONTROLLER PN: P3015GOES00000; S/N: 112031023 DUE DATE 01-FEB-23.;[02] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED AT BS 690 LBL24.5 WL 208 CENTER SECTION I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING #273A9110; SHEET 5; REV ?A?<BR>SEE INDIVIDUAL SING-OFFS BELOW;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FITTING — CRACKED (LT WING) · airframe 64,956 hrs · 40,344 cycles

CRACK SLAT ACTUATOR FITTING LOCATED SLAT STATION 202.45 AT LT WING 2022-635919EXACTLY LOCATION OF CRACK: CRACK IS LOCATED ON LOWER SKIN OF SLAT 3 AT SLAT STATION 202.45 (COMMON TO THE ACTUATOR RIB). PERFORMED REPAIR ON LOWER SKIN LOCATED ON SLAT #3 STATION 192.45 TO 212.45 AT LT WING IAW B737-700 SRM 57-42-01-2R-8;REPAIR 8;FIGURE 202;ALTERNATIVE 1;SHEET 3.

Part: FITTING — CRACKED (LT WING) · airframe 64,956 hrs · 40,344 cycles

CRACK ON SLAT 1 NOSE SKIN SS 451.97 AT FASTENERS HOLE LOCATED AT ACTUATOR RIB LEVEL LT WING 2022-635918EXACTLY LOCATION OF CRACK: CRACK IS LOCATED ON LOWER SKIN OF SLAT 1 AT SLAT STATION 451.97 (COMMON TO THE ACTUATOR RIB). REPAIRED LOWER SKIN OF SLAT 1 BTW SS 446.45 & SS 457.49 (COMMON TO THE ACTUATOR RIB) IAW EA 22-157-03486-WIP1, EA 22-157-03486-WIP2 AND EA 22-157-03486.

Part: FLOOR SUPPORT — CRACKED (BS 690) · airframe 64,956 hrs · 40,344 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 690 RBL24.5 WL208 CENTER SECTION 2022-635799 / [01] TOOLS USED: TEMPERATURE CONTROLLER: PN: P3015GOES00000; S/N: 112820025 DUE DATE 01-FEB-23 AND TEMPERATURE CONTROLLER PN: P3015GOES00000; S/N: 112031023 DUE DATE 01-FEB-23.;[02] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED AT BS 690 RBL24.5 WL208 CENTER SECTION I.A.W 737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING #273A9110; SHEET 5; REV ?A?.<BR>SEE INDIVIDUAL SING-OFFS BELOW;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: NONE — INOPERATIVE (PAX CABIN) · airframe 64,586 hrs · 40,093 cycles

L1 DOOR EMERGENCY EXIT SIGN INOP. / [01] RELAMPED L1 DOOR EMERGENCY EXIT SIGN & OPS CHECK GOOD REF AMM 33-51-01.

Part: NONE — INOPERATIVE (PAX CABIN) · airframe 64,586 hrs · 40,093 cycles

EMERGENCY LIGHT OUT @ 7C. / [01] RELAMPED EMERGENCY LIGHT @ 7C & OPS CHECK GOOD REF AMM 33-51-03.

Part: SUPPORT BRACKET — MISSING (LH WING) · airframe 64,373 hrs · 39,959 cycles

LEFT WING #3 SLAT O/B AUX TRACK; SKIN TAB O/B SUPPORT BRACKET IS MISSING. / [01] INSTALLED SKIN TAB O/B SUPPORT BRACKET ON LEFT WING # 3 SLAT PER SRM 51-40-02

Part: NONE — FAILED (PAX CABIN) · airframe 64,373 hrs · 39,959 cycles

EMERGENCY LIGHT BATTERY M01675 FAILED CAPACITANCE CHECK / [01] REMOVED AND REPLACED BATTERY PACK AT LOCATION M01675 PER AMM 33-51-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,593 hrs · 37,112 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERABLE. DISCONNECTED RUDDER PEDALS FOR ACCESS AND RECONNECTED PEDALS AFTER WORK WAS COMPLETED, IAW B737 AMM 27-21-31-400-801. ACCOMPLISHED RUDDER PEDAL ADJUSTMENT AND LIMIT TRAVEL TEST. PEDALS WITHIN LIMITS, IAW B737 AMM 27-21-00-700-813-002.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 59,593 hrs · 37,112 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR UPPER EMERGENCY LIGHT INOPERABLE. RESECURED CONNECTOR D12464, AS PER REFERENCE B737 SWPM 20-60-06. PERFORMED OPERATIONAL TEST, AS PER REFERENCE B737 AMM 33-51-00-710-801 NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,593 hrs · 37,112 cycles

R1 DOOR OUTSIDE EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED R1 DOOR OUTSIDE EMERGENCY LIGHT LAMP, AS PER REF B737 AMM 33-51-04-960-801. PERFORMED OPERATIONS CHECK AND FOUND NORMAL.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 59,593 hrs · 37,112 cycles

DORSAL FIN FWD RIB STA 877 SEVERAL CRACKS NOTED (MKD DOT 016). REMOVED AND REPLACED DORSAL FIN RIB AT STA 877, IAW B737-700 SRM 51-40-02-0G-0 AND DWG 174A1103.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 59,593 hrs · 37,112 cycles

**CORROSION** AFT OF FWD CARGO COMP AT END OF S-26L STA 540. / ACCOMPLISHED PERMANENT STRINGER S-26L REPAIR AT FWD CARGO BETWEEN STA 500D+12-5' AND STA 540 LBL 23.5 REF B 737-700 SRM 51-40-02-0G-0 AND DWG# 143A3230

Part: FITTING — CRACKED (BS 1016) · airframe 59,593 hrs · 37,112 cycles

LOWE FUSELAGE AT STA 1016 DRAIN FITTING CRACKED. / REMOVED AND REPLACED 2 DRAIN FITTINGS AT LOWER FUSELAGE STA 1016. IAW B737-700 SRM 51-40-02-0G-0 AND DWG# 148A3320

Part: FLOOR PANEL — CRACKED (AFT CABIN) · airframe 59,593 hrs · 37,112 cycles

AFT CABIN WET AREA FLOOR PANEL NR 241ADF CRACKED, MARKED DOT 60-058. CLEANED AND REPAIRED DAMAGE CRACK AREAS, AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241 ADF, AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO 1480720 AND PO 1692653.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 59,593 hrs · 37,112 cycles

** CORROSION ** AFT OF FWD CARGO COMPARTMENT AT END OF S-27L STA 540 MKD DOT 60-055 / ACCOMPLISHED PERMANENT REPAIR AT S-27L ON FWD CARGO BETWEEN STA 500D +11.5' AND STA 540 LBL 15.5' REF B737-700 SRM 53-00-03-2R-1 AND DWG #143A3230

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 59,593 hrs · 37,112 cycles

CORROSION, MAIN CABIN SEAT TRACK LBL 24.75 CORRODED FROM BS 380 TO BS 370 MKD 126-028. REMOVED, REPLACED, AND INSTALLED MAIN CABIN SEAT TRACK (PO 1696448) AT LBL 24.75 FROM BS 380 TO BS 480, IAW B737-700 SRM 5140-02-00G-0 SRM 51-4005-0G-0 SRM 51-20-01-0G-0 SOPM 20-41*04;AND BOEING DWG DOC 143A5300. EVALUATION OF SEAT TRACK CORROSION WAS FOUND OUT OF LIMITS, IAW B737-700 SRM 53-00-52-1A-1 FIG 103 DETAIL A.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 59,593 hrs · 37,112 cycles

MAIN CABIN CENTER WING BOX FLOOR PANEL 241EF UPPER SURFACE LAYERS DELAMINATED, MARKED. RECEIVED NEW PANEL 241EF. THIS PANEL WILL BE INSTALL ON CUSTOMER CARD JPANEL-231-CLOSE.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 59,593 hrs · 37,112 cycles

MAIN CABIN CENTER WING BOX FLOOR PANEL 241BF UPPER SURFACE LAYERS DELAMINATED, MARKED. RECEIVED NEW PANEL 241BF, THIS PANEL WILL BE INSTALLED ON CUSTOMER CARD JPANEL-231-CLOSE.

Part: NUT PLATE — BROKEN (ADF ANTENNA) · airframe 59,593 hrs · 37,112 cycles

UPPER FUSELAGE SKIN WHERE FWD ADF ANTENNIA ATTACHES HAS FWD RT NUTPLATE BROKEN, REF SRM 53-40-01-2R-1. REPAIRED DAMAGE NUT PLATE AT UPPER FUSELAGE SKIN BS 676 STR 1-STR 2R, IAW B737-700 SRM 53-40-01-2R-1.

Part: BRACKET — CRACKED (LT WING TE) · airframe 59,593 hrs · 37,112 cycles

LEFT WING UPPER TRAILING EDGE PNL AFT OF PYLON HAS SEAL RETAINER BRACKET CRACKED AT FASTENER HOLE. / REMOVED AND REPLACED BRACKET AT L/WING UPPER TRAILING EDGE PANEL AFT OF PYLON IN REF B737-700 SRM 51-40-02-0G-0

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 59,593 hrs · 37,112 cycles

FWD CABIN FLOOR PANEL 222B 2 EA UPPER SURFACE LAYERS DELAMINATED, MARKED. CLEANED AND REPAIRED SMALL LOOSE FIBERS ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 222B, AS PER B737 SRM 53-00-50-2R-11 REPAIR 11 MATERIAL USED PO 1692653.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,593 hrs · 37,112 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE FAIRING INT RIB NR 7 CRACKED AT EDGE, MARKED DOT 60-031. FABRICATED AND INSTALLED RIB NR 8 CHORD AT RT HOTL. STABILIZER LEADING EDGE FAIRING MAT USED BAC 1490-2655 2024-0 CLAD PO 17016 55 AND TREATED PART WITH ALODINE & PRIME AND LOCATED & DRILLED PARTS, IN REF B737-700 SRM 51-40-05-0G-0; 51-20-01 AND DWG 186A1308.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 59,593 hrs · 37,112 cycles

FWD CABIN FLOOR PANELS 222CF UPPER SURFACE LAYERS DELAMINATED, MARKED. CLEANED AND REPAIRED SMALL LOOSE FIBERS ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 222CF, AS PER B737 SRM 53-00-50-2R-11 REPAIR 11 MATERIAL USED PO 1692653.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,593 hrs · 37,112 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE FAIRING INT RIB NR 4 CRACKED AT FASTENER TAIL MARKED DOT 60-030. REMOVED AND REPLACED RIB NR 4 AT LT HORIZONTAL STABILIZER LEADING EDGE FAIRING, IN REF B737-700 DWG 186A1001 AND APPLIED PRIME TO ALL FASTENERS HOLES, IN REF SRM 51-20-01-0G-0.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 59,593 hrs · 37,112 cycles

AFT CABIN FLOOR PANEL NR 241ZF UPPER SURFACE AFT LAYERS DELAMINATED, MARKED. CLEANED AND REPAIRED DAMAGE TOP LAYERS OF MAIN CABIN FLOOR PANEL 2412F UPPER SURFACE, AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO 1480720 AND PO 1692653.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,593 hrs · 37,112 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE FAIRING INT RIB NR 3 CRACKED AT FASTENER TAIL, MARKED DOT 60-029. REMOVED AND REPLACED RIB NR 3 AT LT HORIZONTAL STABILIZER LEADING EDGE FAIRING, IN REF B737-700 DWG 186A1001 AND APPLIED PRIME TO ALL FASTENERS HOLES IN REF SRM 51-20-01-0G-0.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 59,593 hrs · 37,112 cycles

CRACK INDICATION FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663+10', RBL 43 WITH LENGTH APPROXIMATELY 0.394'. ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR AT MAIN CABIN RT SIDE BETWEEN STA 663.75 AND STA 675 FROM RBL 38 TO RBL 60 FIG 202 TABLE 201, REF B737-700 SRM 53-40-51-2R-2.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 59,593 hrs · 37,112 cycles

LH WING; NO 2 SLAT NOSE SKIN; LWR SKIN AT ACTUATOR ATTACHEMNT HAS CRACK PROTRUDING FROM THE SECOND INBD FASTENER FROM THE AFT EDG. / ACCOMPLISHED PERMANENT REPAIR OF DAMAGE FOUND AT #2 SLAT NOSE SKIN AT ACTUATOR ATTACHMENT AREA PER B737-700 SRM 57-42-01-ZR-2 FIG 202 AND APB SRM 57-42-01 REPAIR 8

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,873 hrs · 36,649 cycles

EXIT SIGN PLACARD NEAR FORWARD ENTRY FELL OFF THE BULKHEAD. / REPLACED LENS PER MM 33-51-01

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,535 hrs · 36,430 cycles

AFT GALLEY SECTION OF EMERGENCY LIGHTS INOP. / REMOVED AND REPLACED AFT GALLEY EMERGENCY LIGHTS BATTERY BACK OPS CHECK GOOD REFERENCE AMM 33-51-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,439 hrs · 36,373 cycles

EMERGENCY AISLE LIGHT AT ROW 4ABC INOP. / REPLACED LAMP FOR EMERGENCY AISLE LIGHT AT ROW 4ABC AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-03-960-801.

Part: FUSE — INOPERATIVE (CABIN) · airframe 58,439 hrs · 36,373 cycles

RIGHT AND LEFT OVERWING EMERGENCY EXIT WINDOW LIGHTS INOP. / REMOVED AND REPLACED INOP FUSE IN M1669 AND M1668 EMERGENCY LIGHTS BATTERY CHARGER (POWER SUPPLY). PER AMM 33-51-06-960-804 STEP.3.D. (1 THRU 3). PERFORMED GOOD OPS TEST PER AMM 33-51-06-960-804 STEP. 3.D.(4.). RIGHT AND LEFT OVERWING EMERGENCY EXIT WINDOW LIGHT NOW FULLY OPERATIONAL.

Part: GROUND WIRE — DAMAGED (CABIN) · airframe 58,439 hrs · 36,373 cycles

EXIT LOCATOR LIGHTS AD FWD SERVICE DOOR AND LEFT OVERWING EXIT DOOR ARE INOP. / REPLACED FUSE IN M1668 PER AMM 33-51-06-960-804. RETERMINATED GROUND WIRE W 4142-0052-20 AT GD 10086 DC PER WDM 33-51-21 AND SWPM 20-90-15 OPS CHECKED EMERGENCY EXIT LIGHTS PER AMM 33-51-00-710-801 CHECKED GOOD

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,439 hrs · 36,373 cycles

M1675 EMERGENCY EXIT LIGHT BATTERY PACK FAILS CAPACITY TEST. / REMOVED; REPLACED; AND OPS CHECKED M1675 EMERGENCY EXIT LIGHT BATTERY PACK PER AMM 33-51-06-960-805 CHECKS GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,439 hrs · 36,373 cycles

FWD SERVICE DOOR SLIDE LIGHT INOP. / REPLACED LAMP FOR FWD SERVICE DOOR SLIDE LIGHT AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-04-960-801.

Part: SPAR — CORRODED (LT WING) · airframe 58,439 hrs · 36,373 cycles

**CORROSION*** EVIDENCE OF CORROSION AT LEFT WING FRONT SPAR WEB AT IFSS 119 COMMON TO BOOST PUMP UPPER AND LOWER BONDING JUMPER FASTENER HOLES / REPAIRED LEFT WING SPARE WEB AT IFSS 119 AT BOOST PUMP BONDING JUMPERS IAW SOUTHWEST EA 20-157-00208 REV IR AND ATS ER 20-02287 REV IR

Part: SPAR — CORRODED (RT WING) · airframe 58,439 hrs · 36,373 cycles

**CORROSION*** EVIDENCE OF CORROSION AT RIGHT WING FRONT SPAR WEB AT IFSS 119 COMMON TO BOOST PUMP UPPER AND LOWER BONDING JUMPER FASTENER HOLES / REPAIRED R/W FRON SPAR WEB AT IFSS 119 COMMON TO BOOST PUMP UPPER AND LOWER BONDING JUMPER FASTENER HOLES IAW ATS ER # 20-02274 REV IR AND CUSTOMER ACCEPTANCE SWA EA 20-157-00207 REV IR

Part: BLOCK — CORRODED (ENTRY DOOR) · airframe 58,439 hrs · 36,373 cycles

CORROSION ON AFT ENTRY DOOR BOTH FWD AND AFT GIRT BAR BLOCKS. / REMOVED AND INSTALLED NEW FWD AND AFT GIRT BAR BLOCKS AT AFT ENTRY DOOR AND PERFORMED INSTALLATION TEST; TEST GOOD PER AMM 25-66-02-000-801; 25-66-02-400-801.

Part: BLOCK — CORRODED (R1 DOOR) · airframe 58,439 hrs · 36,373 cycles

CORROSION ON FWD SEVICE DOOR BOTH FWD AND AFT GIRT BAR BLOCKS. / REMOVED BOTH FWD AND AFT GIRT BAR BLOCKS; FWD SERVICE DOOR AND REPLACED WITH NEW PER AMM 25-66-02-400-801

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 58,439 hrs · 36,373 cycles

REPAIR TWO OPEN HOLES IN FLOOR PANEL 241ABF. / REPAIRED OPEN HOLES IN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-6

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 58,439 hrs · 36,373 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY-FWD CORNER SCUFF PLATE PER EA #1-A53-2076 REV: 11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,439 hrs · 36,373 cycles

FUSELAGE EXTERIOR SKIN REPAIR AT BS 302-310; STRINGER 17R-18R DOES NOT MEET SRM CRITERIA FOR FASTENER INSTALLATION AND ADEQUATE DAMAGE REMOVAL. / REMOVED FUSELAGE EXTERNAL SKIN REPAIR BS. 302-310 STR 17R/H-18R/H. REPAIRED PER ATS ER #20-02206 REV IR AND SWA EA #20-153-00213 REV IR

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 58,439 hrs · 36,373 cycles

(SKYLINE DTIP) FOUND PREVIOUS REPAIR ANGLE DOUBLER CRACKED; STA 294; ABOVE S-17R; LWR INBOARD FLANGE AT FASTENER HOLE. / REMOVED AND REPLACED STUB FRAME; STA 294; RBL 65 WL APPROX 230 TO 208. PER DWG 141A8370 AND SRM 54-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,439 hrs · 36,373 cycles

(SKYLINE DTIP) PREVIOUS REPAIR NOTED FUSELAGE FRAME, STA 294, ABOVE S-17R CRACK REPAIRED PER SRM 51-70-11-2R-1 FOUND PREVIOUS REPAIR DOUBLER CRACKED AT FRAME STA 294 ABOVE S-17R, PER SRM 51-70-11-2R-1, GENERATED NRC U154242 TO REPLACE REPAIR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,439 hrs · 36,373 cycles

***CORROSION*** ACB RH FLOOR-TO-SIDEWALL SUPPORT HAS MULTIPLE POINTS OF CORROSION; BS 727D TO 767; RBL 20; WL 156 / REMOVED AND REPLACED ACB RH FLOOR TO SIDEWALL SUPPORT B/S 727 TO 767; RBL 20; WL 156 IAW SRM 51-40-02 AND DWG 146A7500 REV:- 59899U; 17MAR20.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 58,439 hrs · 36,373 cycles

AFT CABIN FLOOR PANEL 242WF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242WF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1)

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 58,439 hrs · 36,373 cycles

AFT CABIN FLOOR PANEL 241ABF HAS DAMAGED UPPER SURFACE SKIN / DAMAGED FLOOR PANEL 241ABF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-22-0G-0 PAR. 9

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 58,439 hrs · 36,373 cycles

AFT CABIN FLOOR PANEL 242VF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242VF DAMAGED UPPER SURFACE SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1. 56144U; 03/12/2020.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 58,439 hrs · 36,373 cycles

AFT CABIN FLOOR PANEL 242UF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242UF WITH DAMAGED UPPER SURFACE SKIN 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 58,439 hrs · 36,373 cycles

AFT CABIN FLOOR PANEL 241XF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 241XF WITH DAMAGED UPPER SURFACE SKIN 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 58,439 hrs · 36,373 cycles

AFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 241AAF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1) 59812U 03/10/2020

Part: RUDDER — PUNCTURED (TAIL) · airframe 58,439 hrs · 36,373 cycles

RUDDER L/H SIDE IS PUNCTURED 35' FROM BOTTOM / REPAIRED RUDDER L/H SIDE 35' FROM BOTTOM ON WORK ORDER #532072; FORM TRACKING #N137283. FUNCTIONAL TESTS PASSED. (POS: ONLY; TAGNO: 686535; P/N OFF/ON: 173A0103-8; S/N OFF: CASA-0069; S/N ON: CASA-0069)

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,439 hrs · 36,373 cycles

CRACKED VERTICAL STIFFENER AT B.S.663 LOWER COMPOSITE BULKHEAD; ON AFT SIDE; L.B.L 25; W.L. 150. / REMOVED & REPLACED VERTICAL STIFFNER AT BS663 LBL-25 IAW SRM 51-40-02 & DWGS 111A1000 REV.-; 149A7210 REV.B. 59191U;17MAR2020.

Part: STRUCTURE — DENTED (COCKPIT) · airframe 58,439 hrs · 36,373 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; L.B.L. 3 - L.B.L. 12; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR BS 255 LBL 3-LBL12 WL 207.54 PER ATS ER #20-02160 REV IR AND EA 1-753-36792 REV IR.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,345 hrs · 35,672 cycles

FORWARD SERVICE DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS BROKEN. / REMOVED AND REPLACED LENS IAW AMM 33-51-01.

Part: LENS — LOOSE (SERVICE DOOR) · airframe 56,203 hrs · 34,942 cycles

FORWARD GALLEY SERVICE DOOR SLIDE COMPARTMENT GAUGE LENS IS LOOSE. SECURED LENS IAW AMM.

Part: POSITION SENSOR — FAULTY (LE SLAT) · airframe 56,130 hrs · 34,898 cycles

DECLARED EMERGENCY, ON FINAL APPROACH INDICATIONS NORMAL "AIRSPEED LOW" AURAL WARNING SOUNDED. DURING 2ND APPROACH LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED WHEN FLAPS EXTENDED TO 15. #2 SLAT SHOWED AMBER ON LEADING EDGE DEVICES OVERHEAD PANEL. R&R #2 SLAT OUTBOARD POSITION SENSOR S0966 IAW AMM.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 56,111 hrs · 34,887 cycles

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

Part: BRACKET — CRACKED (RIGHT WING) · airframe 56,111 hrs · 34,887 cycles

R/H WING GEAR ACCESS PANEL 'Z' SUPPOT BRACKET CRACKED / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: COVER — LOOSE (EXIT SIGN) · airframe 55,230 hrs · 34,321 cycles

AFT ENTRY "EXIT" SIGN LOOSE. SECURED COVER PER SIP.

Part: CASTING — CRACKED (ENTRY DOOR) · airframe 55,213 hrs · 34,313 cycles

DOOR HANDLE MECHANISM CASTING CRACKED AT THE HORIZONTAL CONTROL ROD PASS THROUGH ON THE FORWARD ENTRY DOOR. R&R FORWARD ENTRY DOOR IAW AMM.

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 55,213 hrs · 34,313 cycles

L2 DOOR AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR IAW AMM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 55,213 hrs · 34,313 cycles

R2 DOOR AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,213 hrs · 34,313 cycles

RT EMERGENCY LIGHT INOP AT SEAT 6. R&R LAMP IAW AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 55,213 hrs · 34,313 cycles

EMERGENCY BATTERY PACK (M1670) WILL NOT CHARGE AT BS 727C+13, LBL 68. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 55,213 hrs · 34,313 cycles

EMERGENCY BATTERY PACK (M2335) WILL NOT CHARGE AT BS 500C+7.5, LBL 67. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 55,213 hrs · 34,313 cycles

RT SIDE AFT OF COCKPIT DOOR EMERGENCY BATTERY PACK M1674 WILL NOT CHARGE. R&R BATTERY PACK PER AMM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FLIGHT DECK FLOOR DAMAGED AT BS 256, LBL 16. REPAIRED FLIGHT DECK FLOOR IAW SRM AND AMM.

Part: FAIRING — DELAMINATED (RIGHT WING) · airframe 55,213 hrs · 34,313 cycles

RH FWD FAIRING 643AB HAS DELAMINATION ON BAGSIDE / RH FWD FAIRING 643AB DELAMINATION ON BAGSIDE REPAIRED IAW SRM 57-53-70-2R-3 TABLE 201 AND IAW SRM 51-70-05-2R-1. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1 PARA 4A(5)(A). DELAMINATION GREATER THAN 2.0' DIA.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 55,213 hrs · 34,313 cycles

FWD. CARGO DOOR SCUFF PLATE HAS CRACK. (MARKED) / RECEIVED NEW PART FWD CARGO DOOR SCUFF PLATE; INSTALLATION PERFORMED ON CUSTOMER CARD NBR 753-140-00-01Y PO# 733324

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 55,213 hrs · 34,313 cycles

FWD. CARGO DOOR AFT THRESHOLD CORNER PLATE HAS CRACK. (MARKED) / RECEIVED NEW PART FWD CARGO DOOR AFT THRESHOLD CORNER PLATE PO# 710370; INSTALLATION PERFORMED ON CUSTOMER CARD NBR 753-140-00-01Y

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** CARGO FLOOR SPLICE PLATE STA 775 RBL 2 TO RBL 21 WL156 / CARGO FLOOR PLATE / SUPPORT STA 775 FOUND DAMAGED OUT OF LIMITS DUE TO NO LIMITS 82032C 2/22/19 AND REPLACED WITH NEW SUPPORT PN 146A9401-4 PO# 732179 ON STORAGE SHELF IAW SRM 51-10-02-0G-0 AND DWG# 146A7500. SUPPORT LOCATED BS775 L13 L21 - RBL 2 RBL 21 WL156. NO LIMITS IN SRM FOUUDN; REPLACEMENT OF PART REQ IAW SRM 51-10-02-0G-0 ST 9. 20325C 2/22/19

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO INTERCOSTAL DAMAGED LT SIDE BETWEEN BS 500A TO BS 500B. R&R INTERCOSTAL IAW SRM & EA.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

RT SIDE FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN BS 500A TO BS 500B. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

STRINGER CLIP CRACKED AT BS 847, STR 25L. R&R CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AROUND FASTENER HOLES ON INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 855, RBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** FOUND ON AFT CARGO BAY FWD SHIELD SUPPORT ANGLE BS 767-787 RBL 20 WL 156. / AFT CARGO BAY FWD SHEILD SUPPORT ANGLE BS 767-787 RBL 20 WL 156 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM. REMOVED SUPPORT ANGLE I.A.W. SRM. 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE P/O# 688813 I.A.W. SRM 51-40-05-0G-0 AND BOEING DWG 146A8R3 REV:-. INSTALLED NEW SUPPORT ANGLE I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 146A8123 REV: -.

Part: DOUBLER — CRACKED (LT WHEEL WELL) · airframe 55,213 hrs · 34,313 cycles

SEAL ASSY. DOUBLER CRACKED AT BS 663 LBL 24 / REMOVED AND REPLACED CRACKED SEAL ASSY DOUBLER IAW SRM 51-40-02-0G-0 AND DWG 111A1000. NEW PART # 7570583 AT BS663 LBL24.

Part: TRACK — CRACKED (HORIZONTAL STAB) · airframe 55,213 hrs · 34,313 cycles

LT HORIZONTAL STABILIZER 333AT ACCESS PANEL FWD TRACK HAVE CRACK / REPLACED LT HORZ STAB. 333AT PANEL FWD TRACK IAW SOPM 20-50-01

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 55,213 hrs · 34,313 cycles

PASSENGER CABIN FLOORBOARD 221EF HAS TWO AREAS OF DISBAND. / REPAIRED PASSENGER CABIN FLOORBOARD 221EG TWO AREAS OF DISBOND IAW SRM 737 53-00-50-2R-0 AND IAW SRM 737 53-00-50-2R-1

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 55,213 hrs · 34,313 cycles

FWD CABIN PASS FLOORBOARD 222DF HAS AREA OF DELAMINATION 7' FWD OF AFT EDGE / FWD CABIN PASS FLOORBOARD 22DF AREA OF DELAMINATION 7' FWD OF AFT EDGE REPAIRED IAW SRM 53-00-50-2R-1. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. DELAMINATION NOT PERMITTED.

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 55,213 hrs · 34,313 cycles

FWD CABIN FLOOR BOARD 221DF HAS FRAYED PLY ON TOP SURFACE. / REPAIRED FRAYED PLY ON TOP SURFACE OF FWD CABIN FLOOR BOARD SRM 53-00-50-2R-1 DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-00-50-1A-1 PARA 4B

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO COMPARTMENT INTERCOSTAL BAFFLE CORRODED BETWEEN BS 747 TO BS 767, RBL 21. R&R BAFFLE IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** INTERCOSTAL BAFFLE IN AFT CARGO COMPARTMENT L/H SIDE AT STA 827-847 LBL 21 WL156 HAS CORROSION / AFTER EVALUATION OF THE INTERCOSTAL BAFFLE FOUND TO BE OUT OF LIMITS I.A.W. S.R.M. 53-00-53-1A-2 STEP 4- C DETAIL D REMOVED AND REPLACED INTERCOSTAL BAFFLE IN AFT CARGO COMPARTMENT L/H SIDE AT STA 827-847 LBL 21 WL 156 I.A.W. S.R.M. 51-40-02-0G-0 PARA 4-B DWG# 146A7500 AND S.R.M 51-40-03-0G-0 (2-E)

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO COMPARTMENT INTERCOSTAL BAFFLE CORRODED BETWEEN BS 727A TO BS 727B, LBL 21. R&R BAFFLE IAW SRM AND DWG.

Part: FLAP — DEBONDED (R/H WING) · airframe 55,213 hrs · 34,313 cycles

RT. WING OUTBD AFT FLAP IS DISBONDED ON INBD LOWER CORNER. / REPAIRED DISBOND OF RT WING OUTBD. AFT FLAP AT INBD. LOWER CORNER PER SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-4. DETERMINED DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 57-53-01-1A-4 PARA 4A(5)(7).

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO AREA RT Z CHANNEL CORRODED BETWEEN BS 887 TO BS 947, RBL 20. R&R RT Z CHANNEL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO LT Z CHANNEL CORRODED BETWEEN BS 727 TO BS 847, LBL 20. R&R Z CHANNEL IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD ENTRY DOOR CUTOUT STRINGER CRACKED AT BS 294.5+1, STR 15L. REPAIRED CUTOUT IAW ER AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO COMPARTMENT RT Z CHANNEL CORRODED BETWEEN BS 500A TO BS 500D, RBL 21. R&R Z CHANNEL IAW SRM AND DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

L1 DOOR FRAME CUTOUT CORRODED AT BS 303.9, BETWEEN STR 9L TO STR 8L. REPAIRED FRAME IAW ER AND EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

L1 DOOR CUTOUT INNER CHORD CORRODED BETWEEN BS 312 +3 TO BS 344 +8, STR 17L. R&R LOWER INNER CHORD PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO RT Z CHANNEL CORRODED BETWEEN BS 727 TO BS 767, RBL 20. R&R ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO AREA RT Z CHANNEL CORRODED BETWEEN BS 867 TO BS 887, RBL 20. R&R ANGLE IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

L1 DOOR CUT OUT INNER CHORD ATTACHED ANGLE CORRODED BETWEEN BS 312 TO BS 344, STR 17L. R&R ANGLE IAW SRM AND DWG.

Part: NUT PLATE — CORRODED (LWR FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

PANEL 192HL NUT PLATE RETAINER STRIP ON INTERIOR SIDE OF PANEL HAS CORROSION / 192 HL NUT PLATE RETAINER STRIP FOUND TO BE OUT OF LIMITS DUE TO NO STATEMENT IN SRM IAW SRM 51-10-02-0G-0 PAR 9. REMOVED DAMGED RETAINER FABRICATED NEW REATAINER MAT ID 2024-T3 .032 LOT# 5054775 AND INSTALLED ON PANEL 192HL IAW SRM 51-40-02-0G-0; DWG 149A7263 81146U 1/28/19

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** FWD CARGO COMPARTMENT FLOOR SHIELD AFT OF DOOR CUT OUT HAS CORROSION IN 3 SPOTS FROM STATION 497 TO 500A RBL 21 WL 156 / AFTE EVALUATION OF CORROSION DAMAGE ON THE FWD CARGO AFT FLOOR SHIELD FOUND TO BE OUT OF ALLOWABLE LIMITS. IAW SRM 53-00-53-1A-2. FIGURE C. REMOVED AND REPLACED FLOOR SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080. 59600U 11FEB19

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO DOOR AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD GALLEY DOOR CUTOUT INNER CHORD CORRODED BETWEEN BS 294+7 TO BS 312+13, STR 17R. R&R CUTOUT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO COMPARTMENT LT AFT BULKHEAD SUPPORT CORRODED AT BS 500D, LBL 27. R&R SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO COMPARTMENT LT 'Z' CHANNEL CORRODED BETWEEN BS 500A TO BS 500D, LBL 21. R&R ANGLE IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

L1 DOOR CUTOUT INNER CHORD CRACKED AT BS 303.9, STR 17L. REPAIRED CHORD IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO COMPARTMENT FLOOR SHIELD FORWARD OF DOOR CUTOUT CORRODED AT BS 426, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO COMPARTMENT SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 497, RBL 28. R&R WEB IAW SRM AND DWG.

Part: THRESHOLD WEB — CORRODED (AFT CARGO BAY) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** AFT CARGO DOOR LOWER THRESHOLD BS 787+7 TO BS 847 RBL 26 WL 159 / AFTER EVALUATION OF AFT CARGO DOOR LOWER THRESHOLD WEB BS 787+7 TO BS 847 RBL 26 WL 159 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103 DETAIL 'D' REMOVED AND REPLACED THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 146A8340

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

AFT CARGO DOOR FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 787+5, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FRAME CLIP CRACKED AT BS 277, STR 10R. R&R CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FWD ENTRY DOOR () · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** FWD ENTRY DOOR CUT OUT; STA 312 +7 TO STA 344 MIDDLE SCUFF PLATE SUPPORT ANGLE HAS CORROSION ( 9 LOCATIONS) / CORROSION AT FWD ENTRY DOOR CUT OUT STA 312 + 7 TO STA 344 MIDDLE SCUFF PLATE SUPPORT ANGLE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1. REMOVED SUPPORT ANGLE IAW SRM 51-40-02-0G-0. LOCATED; DRILLED AND INSTALLED NEW SUPPORT ANGLE P.O.# 721902 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0. AND DWG 141A8110. 92058 02/05/19

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

PANEL 194CR CRACKED ON EXTERIOR SIDE OF PANEL (MARKED) / REPAIRED CRACKED EXTERIOR SKIN OF PANEL 194CR IAW 737-700 SRM 53-60-70-2R-1 AND 51-70-05-2R-1; CRACK WAS BEYOND 1-PLY SO DAMAGE WAS OUT OF LIMITS IAW 737-700 SRM 53-60-70-1A-1 PARA 4A1

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

PANEL 194AR HAS MULTIPLE AREAS OF DELAMINATION AT UPPER EDGE OF PANEL / REPAIRED MULTIPLE AREAS OF DELAMINATION AT UPPER EDGE OF PANEL 194AR PER SRM 53-60-70-2R-1 TABLE 202 AND SRM 51-70-05-2R-6. DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-60-70-1A-1 PARA 4B(6)

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FORWARD CARGO COMPARTMENT LOWER AFT BULKHEAD SUPPORT CORRODED AT BS 500D, BETWEEN RBL 15 TO LBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 55,213 hrs · 34,313 cycles

LT WING; I/B OF DEFLECTION ARM; CENTER SUPPORT __BRACKET PANEL CRACK. / REMOVED & REPLACED CENTER SUPPORT BRACKET (LH WING; ADJACENT IB OF FLAP DEFLECTION CONTROL ARM) IAW B737 SRM 51-40-02 & BOEING DRAWING DOCUMENT 115A2512

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,213 hrs · 34,313 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 4. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FLOOR INTERCOSTAL CRACKED FORWARD OF BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 55,213 hrs · 34,313 cycles

LT WING ORSS 261 LOWER WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM AND DWG.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 55,213 hrs · 34,313 cycles

VAPOR BARRIER WEB CRACKED AT BS 663, LBL 9. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 48 TO LBL 48. REPAIRED FLOORBEAM IAW ER AND EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

L2 DOOR LOWER INNER CHORD CORRODED AT BS 968-3, LBL 52. R&R CHORD PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

PASSENGER CABIN FLOOR INTERCOSTAL CRACKED AFT AT BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** CORROSION FLOOR BEAM BS 1006 LBL 32 WL 208 / REPAIRED FLOOR BEAM BS 1006 LBL 32 WL 208 PER ATS ER 19-01480 REV IR AND SWA EA 1-753-34223 REV IR.

Part: NONE — CORRODED (MAIN CABIN) · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** CORROSION FLOOR BEAM 3 PLACES BS 968 LBL 28 TO LBL 41 WL 208 (MARKED) / CORROSION ON 986 (BS) LBL 28 TO 41 WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIG 103 'C'. DEEPEST OF 3EA .9' X .7' X .112'. REPAIRED DAMAGE AREA IAW ATS ER 19-01479 IR & SWA EA 1-753-34204 REV IR

Part: SHEAR TIE — CORRODED (MAIN CABIN) · airframe 55,213 hrs · 34,313 cycles

FUSELAGE; PASSENGER CABIN; STA 727 S17R; WL 203 APPROX. UPPER PLATE HAS SIGNS OF CORROSION. / UPPER PLATE/SHEAR TIE BS 727 STR 17R WL 203 FOUND OUT OF LIMITS DUE TO NO LIMITS IN AN AREA OF 3' X 2' X .069'. REPAIRED DAMAGE IAW ATS ER 19-01497 IR & SWA EA 1-753-34142 IR

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

LT OUTBOARD SEAT TRACK CORRODED BETWEEN BS 480 TO BS 520+1, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: NONE — CRACKED (RT WHEEL WELL) · airframe 55,213 hrs · 34,313 cycles

CUSTOMER REQUEST. CRACKED LOWER CORD COMMON TO FUEL __ TANK STA 663 ;LBL9; WL165 / REPAIRED CRACKED LOWER CHORD COMMON TO FUEL TANK BS 663 LBL 8 WL 165 PER ER 19-01358 REV IR AND EA 1-757-1587 REV IR

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

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

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 55,213 hrs · 34,313 cycles

FWD CARGO COMPARTMENT AFT CORNER SCUFFPLATE IS CRACK / RECEIVED NEW PART FWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE PO# 710370; INSTALLATION PERFORMED ON CUSTOMER CARD NBR. 753-140-00-01Y

Part: SCUFF PLATE — CORRODED · airframe 55,213 hrs · 34,313 cycles

***CORROSION*** CORROSION SCUFF PLATE ANGLE BRACKETS 3 PLACES BS 968+5 TO 968+15 LBL 54 WL 208 (MARKED) / REMOVED CORRODED SCUFF PLATE ANGLES (3EA) BETWEEN BS 968+5 TO 968+15 + REPLACED WITH NEW SCUFF PLATE ANGLES IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 + BOEING DWG 147A8530 THEY'RE FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G #9; OUT DUE TO NO LIMITS

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

LT OUTBOARD SEAT TRACK CORRODED BETWEEN BS 727B TO BS 887, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

HORIZONTAL PRESSURE WEB UPPER SURFACE CRACKED AT EDGE OF STIFFENING BEAD BS 664, LBL 32. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

LT OUTBOARD SEAT TRACK CORRODED AT BS 433, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: SUPPORT — CRACKED (LH WING) · airframe 55,213 hrs · 34,313 cycles

__LT WING; I/B OF DEFLECTION ARM; WEB SUPPORT PANEL CRACK. / REMOVED & REPLACED WEB SUPPORT PANEL IAW B737 SRM 51-40-02 ON LT WING

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 55,213 hrs · 34,313 cycles

R2 DOOR LOWER INNER CHORD CORRODED BETWEEN BS 968 TO BS 988, RBL 48. R&R CHORD IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LH WING) · airframe 55,213 hrs · 34,313 cycles

CUSTOMER REQUEST. CRACKED STIFFENER L/H663 ;LBL9; WL 152 / REPLACED CRACKED STIFFENER WITH NEW STIFFENER; PART# 7530146 IAW SRM 51-40-05 AND DWG 111A1000. REFERENCE NRC# N182531 FOR INSTALLATION.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 55,213 hrs · 34,313 cycles

FWD CABIN PASS FLOOR BOARD 221BF AFT LH CORNER BROKEN / REPAIRED BROKEN AFT LH CORNER ON FWD CABIN PASS FLOOR BOARD 221BF IAW SRM 53-00-50-2R-6 & SRM 53-00-50-2R-0. DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F. DELAM IS NOT PERMITTED. 80733U 31JAN19

Part: SKIN — CRACKED (LE SLAT) · airframe 55,213 hrs · 34,313 cycles

RT WING NR 8 SLAT AT ACTUATOR RIBS AND ONE CRACKED IN SKIN. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,213 hrs · 34,313 cycles

OVERHEAD BIN NR 6 EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: LENS — MISSING (CABIN) · airframe 55,169 hrs · 34,293 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT 12F. INSTALLED LENS PER MM.

Part: RETAINER — CRACKED (RT WING) · airframe 54,741 hrs · 33,994 cycles

R/H WING FIXED TRAILING EDGE BULKHEAD SEAL BRACKET LOCATED AFT OF ENGINE PYLON IS CRACKED. / REMOVED AND REPLACED PER SRM 51-40-02

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 54,739 hrs · 33,993 cycles

FORWARD LEFT CORNER ON PANEL 193B HAS AREA OF DELAMINATION. / REPAIRED AREA OF DELANINATION ON FORWARD LEFT CORNER OF PANEL 193B IAW SRM 53-40-70-2R-1 & SRM 51-70-05-2R-6. DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA. 4. B. (6)(A) DAMAGE WAS GREATER THAN .625' ARROSS LARGEST DIMENSION

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 54,739 hrs · 33,993 cycles

PANEL 192BL HAS AN AREA OF DELAMINATION ON FORWARD EDGE. / DAMAGE WAS REPAIRED ON NRC #N182403.

Part: DOUBLER — CRACKED (WHEEL WELL LH) · airframe 54,027 hrs · 33,532 cycles

LEFT MAIN W/W FWD BULKHEAD DOUBLER ABOVE L/H RAM AIR EXHAUST DUCT BROKEN. / REPAIRED PER SRM 51-70-11-2R-0

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,692 hrs · 33,297 cycles

LT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,537 hrs · 32,535 cycles

LEFT MAIN LANDING GEAR WHEEL WELL, FORWARD BULKHEAD FIBERGLASS VAPOR BARRIER CRACKED AT BS 663, LBL 9. REPAIRED BARRIER PER EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 52,537 hrs · 32,535 cycles

FWD CARGO DOOR ENTRY SCUFF PLATE CRACKED. / REMOVED AND REPLACED PER AMM 53-11-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,537 hrs · 32,535 cycles

EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST AT M01669. R & R THE BATTERY PACK IAW AMM.

Part: BRACKET — CRACKED (WTB FAIRING) · airframe 52,537 hrs · 32,535 cycles

LT FWD UPPER WING TO BODY FAIRING 191AL AFT MIDDLE SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED L/H FWD UPPER WING TO BODY FAIRING 191AL AFT MIDDLE SUPPORT BRACKET PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,537 hrs · 32,535 cycles

R2 DOOR SLIDE OUT OF POSITION. R & R THE SLIDE IAW MT.

Part: COVER — LOOSE (CABIN) · airframe 51,780 hrs · 32,066 cycles

LT EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,879 hrs · 31,482 cycles

RT EMERGENCY LIGHT INOP AT ROW 19. R&R LIGHT PER AMM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 50,607 hrs · 31,304 cycles

R1 DOOR BEAM UNDER CAM HOUSING BOX CRACKED. R & R THE DOOR ASSEMBLY IAW MM.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 50,528 hrs · 31,257 cycles

L1 DOOR SLIDE GIRT BAR LOOSE. SECURED SLIDE ASSY IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,385 hrs · 31,169 cycles

LT WING OUTBOARD AFT FLAP TRAILING EDGE INBOARD CORNER DELAMINATED. R&R AFT FLAP PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,922 hrs · 30,898 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 18 DEF. REPLACED THE LAMP IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,922 hrs · 30,898 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 23 ABC. REPLACED THE LAMPS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,922 hrs · 30,898 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 8 ABC. REPLACED THE LAMP IAW MM.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 48,721 hrs · 30,192 cycles

BULKHEAD PANEL STIFFENER CRACKED AT BS 663, RBL 12. R & R THE STIFFENER IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 48,721 hrs · 30,192 cycles

RT WING LEADING EDGE SKIN AFT STIFFENER CRACKED AT STA 226.32. R&R SKIN IAW SRM.

Part: BULKHEAD — DELAMINATED (MLG WW) · airframe 48,721 hrs · 30,192 cycles

FORWARD INBOARD WHEEL WELL PANEL 193B EXTERIOR SKIN DELAMINATED FORWARD FROM AFT END AT CENTER AREA. REPAIRED PANEL IAW SRM & EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 48,721 hrs · 30,192 cycles

LT HORIZONTAL STABILIZER RIB FORWARD STIFFENER CRACKED AT STA 101.9, NEAR THE LOWER END. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (BS 727) · airframe 48,721 hrs · 30,192 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,721 hrs · 30,192 cycles

LT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 6. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,721 hrs · 30,192 cycles

RT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 8. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,721 hrs · 30,192 cycles

RT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 7. RELAMPED LIGHT PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 48,721 hrs · 30,192 cycles

RIGHT SIDEWALL PANEL 232YHW, EMERGENCY LIGHT LENS LOOSE. R & R THE LENS IAW AMM.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 48,584 hrs · 30,106 cycles

R/H WHEEL WELL VAPOR WEB CRACKED AT BS. 663, BETWEEN RBL 6.15 TO RBL 15.54. / REPAIRED WEB IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 46,562 hrs · 28,912 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R & R BATTERY IAW AMM.

Part: FITTING — OUT OF ADJUST (R1 DOOR) · airframe 45,857 hrs · 28,492 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR CLIP OUT OF ADJUSTMENT. ADJUSTED CLIP IAW SIP.

Part: LENS — MISSING (EXIT SIGN) · airframe 45,543 hrs · 28,319 cycles

R2 DOOR "EXIT-SALIDA" SIGN COVER LENS MISSING. INSTALLED LENS PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 44,663 hrs · 27,813 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER LENS LOOSE. REPAIRED LENS IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 44,336 hrs · 27,611 cycles

CABIN EMER BATTERY PACKS FAILED CAPACITY CHECK AT M1675. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,336 hrs · 27,611 cycles

CABIN EMER BATTERY PACKS FAILED CAPACITY CHECK AT M1672. R & R BATTERY IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

AFT SEAT TRACK CRACKED AT BS 727B, RBL 24.75 BETWEEN INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 24.75 FWD & AFT HOLE ON INBD FLANGE. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 45.5, FWD & AFT HOLE ON OTBD FLANGE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 45.5, AFT HOLE ON INBD FLANGE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 24.75 FWD & AFT HOLE ON OTBD FLANGE. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 45.5 BETWEEN INBD & OTBD FLANGES. REPAIRED SEAT TRACK IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

RIGHT NR 3 WINDOW FRAME E - F POST NR 6 FASTENER HOLE CRACKED, AFT SIDE OF HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

RIGHT NR 3 WINDOW FRAME E - F POST NR 8 FASTENER HOLE CRACKED, FWD & AFT SIDE OF HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

LEFT NR 3 WINDOW FRAME E - F POST NR 8 FASTENER HOLE CRACKED, FWD & AFT SIDE OF HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

RIGHT NR 3 WINDOW FRAME E - F POST NR 5 FASTENER HOLE CRACKED, AFT SIDE OF HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,534 hrs · 26,592 cycles

RIGHT NR 3 WINDOW FRAME E - F POST NR 7 FASTENER HOLE CRACKED, AFT SIDE OF HOLE. REPAIRED POST IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,534 hrs · 26,592 cycles

LEFT HORIZONTAL STABILIZER OF LOWER IN SPAR SKIN CRACKED AT STAB STATION 157.10 RIB, APPROX 9" FROM REAR SPAR. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,534 hrs · 26,592 cycles

LEFT HORIZONTAL STABILIZER OF LOWER IN SPAR SKIN CRACKED AT STAB STATION 138.7 RIB, APPROX 15 INCHES FROM REAR SPAR. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,534 hrs · 26,592 cycles

RIGHT WING NR 7 SLAT LOWER SURFACE OF WING LE SLAT NOSE SKIN CRACKED AT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: LENS — UNSECURE (CABIN) · airframe 39,851 hrs · 25,050 cycles

FORWARD ENTRY EMER EXIT LIGHT LENS COVER FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 39,408 hrs · 24,786 cycles

FIRST OFFICER'S UPPER OTBD WINDSHIELD POST CRACKED BELOW MIDDLE OF CORNER RADIUS. REPAIRED POST IAW EA.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 36,356 hrs · 22,958 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,256 hrs · 22,888 cycles

LT LOWER OVERWING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 35,814 hrs · 22,640 cycles

LENS MISSING FROM EMERGENCY LIGHT LOCATED AT FWD AISLE CEILING. INSTALLED LENS IAW AMM.

Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

WING TO BODY FAIRING 191FL DELAMINATED AT UPPER FWD CORNER. REPAIRED FAIRING IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

LEFT SUPPORT CRACKED BETWEEN BS 500B TO BS 500C, BETWEEN STR 25L TO STR 26L. REMOVED & REPLACED SUPPORT PER SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

LEFT SUPPORT CRACKED BETWEEN BS 440 TO BS 460. REMOVED & REPLACED SUPPORT PER SRM AND DRAWING.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FWD CARGO BAY INTERCOSTAL UNDER FLOOR TO SIDEWALL SUPPORT CRACKED BETWEEN BS 500A TO BS 500B, RBL 20. REPAIRED SUPPORT IAW ER AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL CORRODED BETWEEN BS 500B TO BS 500C, RBL 20. REMOVED & REPLACED INTERCOSTAL PER SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

SUPPORT INTERCOSTAL CRACKED BETWEEN BS 727A TO BS 727B, RBL 22. REMOVED & REPLACED SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL CRACKED BETWEEN BS 500A TO BS 500B, LBL 20. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FLOOR TO SIDEWALL SUPPORT CRACKED BETWEEN BS 727A TO BS 727B. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

CRACKED AT AFT EDGE OF EXT POWER DOOR CUTOUT. REPAIRED SKIN IAW EA.

Part: PANEL — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

AFT CARGO BAY PANEL 140CF CORRODED. REMOVED AND REPLACED PANEL IAW SRM AND DWG.

Part: PANEL — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

AFT CARGO BAY PANEL 140DF CORRODED. REMOVED AND REPLACED PANEL IAW SRM AND DWG.

Part: PANEL — DELAMINATED (LT WING) · airframe 35,814 hrs · 22,640 cycles

LEFT WING PANEL 521EB LOWER SURFACE DELAMINATED AT CORNER. REPAIRED PANEL PER SRM.

Part: PANEL — DELAMINATED (LT WING) · airframe 35,814 hrs · 22,640 cycles

LEFT WING PANEL 521SB LOWER SURFACE DELAMINATED AT CORNER. REPAIRED PANEL PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 400 FRAME, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500B, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

SUPPORT CORRODED BETWEEN BS 500A - BS 500D, RBL 22. REMOVED AND REPLACED SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

SUPPORT CORRODED BETWEEN BS 400 - BS 500D, LBL 22. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500B, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

SUPPORT CORRODED BETWEEN BS 405 TO BS 420, RBL 22. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,814 hrs · 22,640 cycles

LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 147.9. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D+6 - 767, RBL 20. REPAIRED SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 771 TO BS 797, LBL 21. REMOVED, AND REPLACED SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,814 hrs · 22,640 cycles

LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED BETWEEN STAB STA 92.7 AND 101.9 RIBS. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 787, RBL 22. REMOVED AND REPLACED SUPPORT PER SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW ATS ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 797 TO BS 820, RBL 14. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

INTERCOSTAL WEB CRACKED AT BS 420, STR 19R. REMOVED AND REPLACED WEB IAW DWG.

Part: SUPPORT — CRACKED (RT WING) · airframe 35,814 hrs · 22,640 cycles

RIGHT WING UPPER T/E PANEL AFT SUPPORT INTERCOSTAL CRACKED. REMOVED AND REPLACED SUPPORT IAW SOPM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

STRINGER CORRODED AT BS 727D, BETWEEN STR 23L TO STR 25L. REPAIRED STRINGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,814 hrs · 22,640 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED BETWEEN STAB STA 92.7 AND 101.9 RIBS. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

NR 1 LEFT FLIGHT DECK WINDOW FRAME CRACKED AT UPPER O/B CORNER. REPAIRED FRAME IAW ATS ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

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

Part: FLOORBOARD — BROKEN (CABIN) · airframe 35,814 hrs · 22,640 cycles

PASSENGER CABIN FLOORBOARD 222C UPPER SURFACE FWD CORNER BROKEN. REPAIRED FLOORBOARD IAW SRM.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 35,814 hrs · 22,640 cycles

PASSENGER CABIN FLOORBOARD 221B FORWARD LEFT CORNER BROKEN. REPAIRED FLOORBOARD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,814 hrs · 22,640 cycles

FLOORBEAM CORRODED AT BS 312, BETWEEN RBL 13 AND RBL 28. REPAIRED BEAM IAW ATS ER.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 35,814 hrs · 22,640 cycles

PASSENGER CABIN FLOORBOARD 222DF FWD EDGE BROKEN. REPAIRED FLOORBOARD IAW SRM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 35,027 hrs · 22,163 cycles

SMOKE & FUMES IN GALLEY. REMOVED AND REPLACED COFFEEMAKER PER M/M.

Part: LIGHT — BROKEN (CABIN) · airframe 34,611 hrs · 21,929 cycles

CENTER O/H EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: FILTER — FAULTY (AC BAY) · airframe 34,033 hrs · 21,538 cycles

AIR TURNBACK -- SMOKE DETECTED IN PASSENGER CABIN AIR. REMOVED AND REPLACED RECIRCULATION HEPA FILTER PER AMM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 33,812 hrs · 21,399 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (L2 DOOR) · airframe 33,472 hrs · 21,200 cycles

L2 DOOR OUTER FUSELAGE SKIN CRACKED AT THE UPPER FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 33,472 hrs · 21,200 cycles

RIGHT EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 33,472 hrs · 21,200 cycles

LEFT EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 33,315 hrs · 21,103 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE IAW MM AND MT.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 31,047 hrs · 19,743 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, RBL 33. REMOVED AND REPLACED STIFFENER PER ACO.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 31,047 hrs · 19,743 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, LBL 32. REMOVED AND REPLACED STIFFENER PER ACO.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 31,047 hrs · 19,743 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, RBL 41. REMOVED AND REPLACED STIFFENER PER ACO.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 31,047 hrs · 19,743 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, LBL 7. REMOVED AND REPLACED STIFFENER PER ACO.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 31,047 hrs · 19,743 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, LBL 42. REMOVED AND REPLACED STIFFENER PER ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 28,908 hrs · 18,506 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN CRACKED. REPAIRED NR 2 SLAT PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,779 hrs · 17,241 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 25,929 hrs · 16,708 cycles

DURING SCHEDULED MV2 CHECK FOUND, OVERHEAD CENTER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,929 hrs · 16,708 cycles

DURING SCHEDULED MV2 CHECK FOUND, RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,527 hrs · 15,858 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,332 hrs · 15,736 cycles

RT EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,208 hrs · 15,664 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LIGHT INOP AT ROW 6. RELAMPED PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 23,945 hrs · 15,500 cycles

DIVERSION / INFLIGHT SHUTDOWN. CLIMBING THROUGH 32,000 FT IN CLIMB, NR 1 ENGINE LOST MOST OF ITS POWER, AND PLANE SHUTTERED WITH YAW LEFT. STILL PRODUCED SOME POWER, ENGINE INDICATIONS WERE NORMAL EXCEPT FOR VIBRATION LEVEL AROUND 5. PULLED BACK THRUST LEVER NR 1. STILL HAD HIGH VIBRATION AND SHUT DOWN. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947.5, BETWEEN RBL 16 TO LBL 16. REPAIRED CHORD PER ER.

Part: SIGN — MISSING (CABIN) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT AFT LAV "B" EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER ER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT WING O/B AFT FLAP I/B AFT TRAILING EDGE CORNER LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND FRAME CRACKED AT BS 294, STR 17R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 7. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,623 hrs · 15,277 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, RBL 12. REPAIRED BEAM PER SRM.

Part: LENS — MISSING (CABIN) · airframe 23,131 hrs · 14,985 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS MISSING AT ROW 15. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 23,131 hrs · 14,985 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 23,131 hrs · 14,985 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER OUT OF POSITION AT ROW 21. REPOSITIONED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 22,743 hrs · 14,750 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,436 hrs · 14,564 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP BETWEEN ROW 12 TO ROW 13. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 22,235 hrs · 14,445 cycles

EEPLS COVER OUT OF POSITION AT ROW 15. REMOVED AND REPLACED COVER PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 22,090 hrs · 14,362 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP BETWEEN ROW 12 TO ROW 18. REPAIRED WIRE PER WDM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,016 hrs · 14,312 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TRACK — MISSING (CABIN) · airframe 21,944 hrs · 14,262 cycles

EEPLS TRACK MISSING AT ROW 18. INSTALLED EEPLS PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 21,685 hrs · 14,084 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 21,685 hrs · 14,084 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: BEARING — CORRODED (RT MLG) · airframe 21,051 hrs · 13,683 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG AFT TRUNNION BEARING RACE INNER SURFACE CORRODED. REMOVED AND REPLACED BEARING PER MM.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 21,051 hrs · 13,683 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING ATTACH FITTING LUG FACE CORRODED. REPAIRED FITTING PER SWA EA.

Part: BEARING — CORRODED (LT MLG) · airframe 21,051 hrs · 13,683 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG AFT TRUNNION BEARING INNER RACE SURFACE CORRODED. REMOVED AND REPLACED BEARING PER MM.

Part: LENS — MISSING (CABIN) · airframe 18,741 hrs · 12,339 cycles

EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 18,049 hrs · 11,914 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CAP — LOOSE (EMERGENCY LIGHT) · airframe 17,662 hrs · 11,727 cycles

EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,351 hrs · 10,976 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP BETWEEN ROW 4 ABC AND ROW 7 ABC. FOUND LOOSE CONNECTOR, RECONNECTED PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 16,014 hrs · 10,779 cycles

FLIGHT DECK L2 WINDOW ARCING DURING FLIGHT. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,887 hrs · 10,687 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,887 hrs · 10,687 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.