N793SA

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,058 hrs · 43,386 cycles

EMERGENCY LIGHT AT L/H OVERWING DOOR INT / EXT INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTRY PACK PER REF. AMM 33-51-06-960-801.PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER REF. AMM 33-51-00-720-801 FOUND NORMAL.;[02] VERIFIED REMOVED AND REPLACED EMERGENCY LIGHT BATTRY PACK. TEST NORMAL.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,058 hrs · 43,386 cycles

EMERGENCY LIGHT ON BULLNOSE AT BIN 6ABC INOP<[01] RELAMPED EMERGENCY LIGHT AT BIN 6 ABC AS PER REF. AMM 33-51-03-960-801.<BR>PERFORMED OPERACIONAL TEST FOUND NORMAL AS PER REF' AMM 33-51-03-960-801.;[02] VERIFIED RELAMPED EMERGENCY LIGHT AT BIN 6 ABC; AND PERFORMED OPERACIONAL TEST FOUND NORMAL.

Part: PRESSURE BLKHD — CANNING (ZN 100 FUS LOWER) · airframe 73,058 hrs · 43,386 cycles

REJECT-RII APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING REPAIR HAS TOP RIVET BUCKED AND CUT 50% AT SECOND ROW OUTBOARD TO INBOARD.<[01] REMOVE AND REPLACED FASTENER AT STA 1016 AFT PRESSURE BULKHEAD REPAIR JUST BELOW RH FITTING SECOND ROW OUTBOARD TO INBOARD REF B737-700 SRM 51-40-02-0G-0.;[02] RII-VERIFIED INSTALLATION

Part: PRESSURE BLKHD — CANNING (ZN 100 FUS LOWER) · airframe 73,058 hrs · 43,386 cycles

REJECT RII RIVET BUCKED INCORRECTLY AT APB OIL CANNING REPAIR STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING; NINE RIVETS FROM TOP TO BOTTOM HOLDING STIFFNER..<[01] REMOVED AND REPLACED ALL MARKED FASTENERS (9 RIVETS) THAT NEEDED REPLACEMENT REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.

Part: PRESSURE BLKHD — CANNING (ZN 100 FUS LOWER) · airframe 73,058 hrs · 43,386 cycles

REJECT- AS PER S/M SME REPLACE MARKED FASTENERS AT APB OIL CANNING REPAIR STA 1016 BETWEEN BL-0 AND S-3R JUST BELOW RIGHT FITTING 90% OF RIVETS MARKED ARE HOLDING STIFFNER.<[01] REMOVED ALL MARKED FASTENERS NEEDING REPLACEMENT REF SRM 51-40-02-0G-0.;[02] REMOVED 7EA MARKED FASTENERS NEEDING REPLACEMENT REF SRM 51-40-02-0G-0.;[03] VERIFIED FASTENERS REMOVAL (7EA)<BR>OK TO INSTALL NEW FASTENERS.;[04] INSTALLED ALL NEW FASTENERS (7 RIVETS) IN REF SRM 51-40-02-0G-0.;[05] VERIFIED STEP 4.

Part: BULKHEAD — OUT OF TOLERANCE (ZN 100 FUS LOWER) · airframe 73,058 hrs · 43,386 cycles

CUSTOMER REJECT- FOUND SEVERAL EXISTING HOLES OUT OF TOLERANCE AT STA 1016 BULKHEAD.<[01] OVERSIDE FASTENERS FOUND OUT OF TOLERANCE OF APB BETWEEN RBL-4 AND RBL-16 AS PER B737-700 SRM 51-40-05-0G-0 FIG 4 A TOTAL OF 10 FASTENERS WERE STEP UP TO 2ND OVERSIDE(.216') WITH NO CRACKS FOUND . TWO FASTENERS BOTTON SECTION OF RBL-15 AND RBL-16 FOUND BEYOND .216'.DAMAGES HOLES DIMENSIONS .230;[02] CORRECTIVE ACTION ENTRY #1 WAS ENTERED IN ERROR.;[03] ACCOMPLISHED APB OIL CANNING REPAIR AT STA 1016; BETWEEN BL-0 AND S-3R IN REF TO B737 SRM 53-80-08-2R-13; EA 23-153-03288-WIP1 (TTG8Q00PG488); EA 23-153-03288-WIP2 (TTG8Q00PKFYL); EA 23-153-03288-WIP3 (TTG8Q00PLRC6); EA 23-153-03288-WIP4 (TTG8Q00PNCJX); EA 23-153-03288-WIP5 (TTG8Q00PPV65); EA 23-153-03288-WIP6 (TTG8Q00PQ6JX); AND EA 23-153-03288-FINAL. (TTG8Q00PT2T9).;[04] RII VERIFIED STEP 3

Part: BULKHEAD — CANNING (ZN 100 FUS LOWER) · airframe 73,056 hrs · 43,385 cycles

APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING SEE TTG8Q00P9H5Q<[01] ACCOMPLISHED REPAIR AND PERFORMED EA 23-153-03288; REFERENCE FAULT 'TTG8Q00PF2MN & TTG8Q00PAJPT;[02] ACCOMPLISHED REPAIR AND PERFORMED EA 23-153-03288; REFERENCE FAULT 'TTG8Q00PF2MN & TTG8Q00PAJPT

Part: FITTING — UNKNOWN (AFT PRSS BLKHD) · airframe 73,058 hrs · 43,386 cycles

TRANSFERRED FROM LP 2479096: APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3L; JUST BELOW LEFT FITTING. SEE TTG8Q00P9JY8<[01] ACCOMPLISHED AFT PRESSURE BULKHEAD OIL CANNING REPAIR AT STA 1016 BETWEEN BL-0 AND S-3L IN REFERENCE TO B-737-700 SRM 53-80-08-2R-13.;[02] RII: VERIFIED ACCOMPLISHED OF AFT PRESSURE BULKHEAD OIL CANNING REPAIR AT STA 1016 BETWEEN BL-0 AND S-3L IN REFERENCE TO B-737-700 SRM 53-80-08-2R-13.

Part: BULKHEAD — CANNING (ZN 100 FUS LOWER) · airframe 73,058 hrs · 43,386 cycles

TRANSFERRED FROM LP 2479095: APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING SEE TTG8Q00P9H5Q<[01] ACCOMPLISHED APB OIL CANNING REPAIR AT STA 1016; BETWEEN BL-0 AND S-3R IN REF TO B737 SRM 53-80-08-2R-13; EA 23-153-03288-WIP1 (TTG8Q00PG488); EA 23-153-03288-WIP2 (TTG8Q00PKFYL); EA 23-153-03288-WIP3 (TTG8Q00PLRC6); EA 23-153-03288-WIP4 (TTG8Q00PNCJX); EA 23-153-03288-WIP5 (TTG8Q00PPV65); AND EA 23-153-03288-WIP6 (TTG8Q00PQ6JX).;[02] VERIFIED STEP # 1 NOTE RII;[03] PERFORMED EA 23-153-03288; REFERENCE FAULT 'TTG8Q00PF2MN'.;[04] RII- VERIFIED STEP 3- PERFORMED EA 23-153-03288; REFERENCE FAULT 'TTG8Q00PF2MN'.

Part: BULKHEAD — CANNING (ZN 100 FUS LOWER) · airframe 73,056 hrs · 43,385 cycles

APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3L; JUST BELOW LEFT FITTING. SEE TTG8Q00P9JY8<[01] ACCOMPLISHED REPAIR ON NR FAULT TTG8Q00PAHQ2.;[02] ACCOMPLISHED REPAIR ON NR FAULT TTG8Q00PAHQ2.

Part: BULKHEAD — CANNING (ZN 100 FUS LOWER) · airframe 73,056 hrs · 43,385 cycles

APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING<[01] FOUND MEASUREMENTS OUT OF LIMITS.;[02] NON ROUTINE TRANSFERED TO LOGBOOK SEE LP# 2479095;[03] FOUND MEASUREMENTS TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1; NON ROUTINE TRANSFERRED TO LOGBOOK SEE LP# 2479095

Part: BULKHEAD — CANNING (ZN 100 FUS LOWER) · airframe 73,056 hrs · 43,385 cycles

APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3L; JUST BELOW LEFT FITTING<[01] FOUND MEASUREMENTS TO BE OUT OF LIMITS;[02] EDIT MEASUREMENTS;[03] FOUND MEASUREMENTS TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1;[04] NON ROUTINE TRANSFERRED TO LOGBOOK SEE LP # 2479096

Part: FLAP — PEELING (ZN 500 LEFT WING) · airframe 72,576 hrs · 43,070 cycles

REF 23-157-02669-TLD LH OB AFT FLAP PREVIOUS REPAIR PEELING - PN 113A3700-7; SN 000054 - TIME LIMITED REQUIRES REPLACEMENT.<[01] REMOVED AND REPLACED L/H OUTBOARD AFT FLAP ASSEMBLY PER AMM. 27-51-22.

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 71,933 hrs · 42,658 cycles

EMERGENCY LIGHT BY FORWARD SERVICE DOOR INOP<[01] RELAMPED EMERGENCY LIGHT BY FORWARD SERVICE DOOR (ON FUSELAGE EXTERIOR) IAW AMM 33-51-04. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (LT OVERWING) · airframe 70,764 hrs · 41,915 cycles

CUSTOMER WALK: LT OVERWING EXIT INTERIOR EXIT MAKER HAS BULBS OUT.<[01] RE-LAMPED LT OVERWING INTERIOR EXIT SIGN AS PER REF AMM 33-51-01-960-801 LIGHT TEST OK;[02] VERIFIED STEP 1

Part: HANDLE — LOOSE (L1 DOOR) · airframe 70,764 hrs · 41,915 cycles

L1 DOOR LOWER ASSIST HANDLE LOOSE. SECURED FWD ENTRY DOOR LOWER ASSIST HANDLE PER B737 AMM 52-11-31-400-802-NG

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,764 hrs · 41,915 cycles

ASSOCIATED EMERGENCY LIGHTS WITH FWD ENTRY BATTERY PACK M1674 ARE INOP.<[01] REMOVED AND REPLACED (M1674) EMERGENCY BATTERY PACK IN REF WITH B737 AMM 33-51-06-960-805.;[02] EMERGENCY BATTERY PACK TEST NORMAL IN REF WITH B737 AMM 33-51-06-960-805.;[03] VERIFIED STEP 1; 2

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 70,764 hrs · 41,915 cycles

CRACK FOUND AT EXTERNAL LOWER SURFACE OF RH I/B AFT FLAP 19.5' FROM I/B EDGE AND 3.375' FROM T/E. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.393'. CUT OUT DAMAGED AERA AT R\H I\B AFT FLAP ON LOWER SURFACE SIZE 1.5'X0.5' NO CORE DAMAGE FOUND WATER IAW SRM 51-70-10-2R-0 PARAGRAPH(7.A). PERFORMED DRY OUT ON DAMAGE AREA; FOUND NO WATER; FABRICATE FILLER AND DOUBLER CLEANED PARTS AND APPLIED ADHESIVE PRIMER. NO CORE DAMAGE IAW SRM 51-70-10-2R-4. PERFORMED HFEC AT CUT OUT AS PER NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. REPAIRED DAMAGE AREA AT R/H LOWER SURFACE I/B AFT FLAP 19.5' FROM I/B EDGE AND 3.75' FROM T/E IAW SRM 51-70-10-2R-4. ACCOMPLISHED TAP TEST AT R/H I/B AFT FLAP LOWER SURFACE FOUND NO DELAMINATION IAW NTM 51-05-01.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,764 hrs · 41,915 cycles

AAFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED<[01] RECEIVED AFT CARGO DOOR FWD CORNER SCUFF PLATE IN SERVICEABLE CONDITION (REPAIRED BY OUTSIDE VENDOR J.L. WELDING INC. REF. BOEING 737-700 SRM 53-60-15-2R-1 UNDER AAR PO# 413820);[02] VERIFIED STEP 1

Part: DOOR — BROKEN (EXTERNAL POWER) · airframe 70,764 hrs · 41,915 cycles

EXTERNAL POWER DOOR GROUND BROKEN<[01] REMOVED AND REPLACED EXTERNAL POWER DOOR GROUND AS PER SWPM 28-20-00 AND SWPM 20-20-10.<BR>BONDING METER B/C 168697.;[02] VERIFIED REMOVAL AND REPLACEMENT OF EXTERNAL POWER DOOR GROUND.

Part: PUMP — LEAKING (#2 ENGINE) · airframe 69,659 hrs · 41,179 cycles

B LOW PRESSURE LIGHT ILLUMINATED; COMPLIED W/QRH; FOLLOW BY B ELEC LOW PRESSURE. B QTY SHOWED ZERO. LOSS OF SYS B @ 5 MINS AFTER THE LOW PRESSURE ENG 2 IS WHEN COMPLETE LOSS HAPPENED. / [01] REMOVED AND REPLACED SYS B EMDP PER AMM 29-11-21. PUMP LEAK CHECKED GOOD.;[02] REMOVED AND REPLACED #2 ENGINE DRIVEN HYDRAULIC PUMP; OPS AND LEAK CHECK GOOD IAW AMM 29-11-11.;[03] HIGH POWER RUN WAS ACCOMPLISHED ON TPGHQ00E9390. OK FOR SERVICE

Part: LIGHT — FAULTY (L/H WING) · airframe 69,637 hrs · 41,167 cycles

LEFT SLIDE/OVER WING EMERGENCY LIGHT EXTINGUISHED. / [01] RELAMPED LEFT SLIDE/OVER WING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (PAX CABIN) · airframe 69,084 hrs · 40,803 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; M1673; M1670 PER AMM 33-51-06 AND DRW 33500005

Part: BATTERY PACK — FAILED (PAX CABIN) · airframe 69,084 hrs · 40,803 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; M1673; M1670 PER AMM 33-51-06 AND DRW 33500005

Part: BATTERY PACK — FAILED (PAX CABIN) · airframe 69,084 hrs · 40,803 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; M1673; M1670 PER AMM 33-51-06 AND DRW 33500005

Part: BATTERY PACK — FAILED (PAX CABIN) · airframe 69,084 hrs · 40,803 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; M1673; M1670 PER AMM 33-51-06 AND DRW 33500005

Part: MEGAPHONE — BROKEN (CABIN) · airframe 67,533 hrs · 39,860 cycles

SUPPLEMENTAL INFORMATION: FA FWD MEGAPHONE; MEGAPHONE HANDLE IS BROKEN ; / [01] R&R'ED FWD FA MEGAPHONE IAW AMM 25-64-00. OK FOR SERVICE.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AFT CARGO SCUFF PATE HAS A CRACK .(AFT PLATE) ; / [01] SCUFF PLATE WAS SENT TO J.L WELDING FOR REPAIR AND RECEIVED SERVICEABLE. ITEM WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q0032CYS.; [02] VERIFIED 1.

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 67,300 hrs · 39,722 cycles

LT HORIZONTAL STAB RIB #5 STIFFENER #4 CRACKED ; / [01] 1.PERFORMED HFEC ON RIB #5 STIFFENER #4 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK FOUND AT LOWER AREA . CRACK LENGTH : 0.472'. <BR><BR>2.PERFORMED HFEC ROTO ON OPEN FASTENER HOLES IAW NDTM PART 6;51-00-00 PROCEDURE 16. NO CRACKS FOUND. <BR>[NORTEC 600; B/C 166317 ; CALIB.DUE-10/21]; [02] CUT OUT DAMAGE AREA AT LT. HORIZONTAL STAB RIB #5 STIFFENER #4 IAW. B-737-700 SRM. 55-10-09-2R-4 REPAIR 4 FIG.202 SHEET 1. SURFACE ROUGHNESS SMOOTHER THEN 63 MICROINCHES RA. IAW. B-737-700 SRM. 51-20-13-0G-0 TOOL USED 172331; [03] PERFORMED HFEC AT CUTOUT IAW NDTM PART 6;51-00-00 PROCEDURE 23. NO CRACKS.<BR>[NORTEC 600 ;B/C 166317 ; CALIB.DUE - 10/21]; [04] INSPECTED AREA PER55-10-09-2R-4 STEP 4E NO DEFECTS.; [05] LOCATED AND DRILLED REPAIR PARTS AS PER B737-700 SRM 55-10-09-2R-4; REPAIR 4.; [06] VERIFIED STEP # 5; [07] OK TO ALODINE AND PRIME REPAIR; [08] APPLIED ALODINE AND PRIMER AS PER B737-700 SRM 51020-01-0G-0.; [09] VERIFIED STEP # 8; [10] OK TO INSTALL REPAIR PARTS.; [11] INSTALLED REPAIR PARTS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4.; [12] REPAIRED CRACK AT LT HORIZONTAL STAB RIB #5 STIFFENER #4 AS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4.; [13] VERIFIED STEP 11 AND 12; [14] JOB IS COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

F/O SEAT TRACK HAS CORROSION ON LWR SURFACE FWD I/B. 8-79 ; / [01] REFER TO CUSTOMER CARD #(753-330-00-01Y) BARCODE# TTG8Q0032DAH FOR INSTALLATION.; [02] VERIFIED 1.

Part: STRAP — CRACKED (E&E BAY) · airframe 67,300 hrs · 39,722 cycles

AT ELECTRICAL AND ELECTRONICS COMPARTMENT(E/E) BS 312 TO BS 344;STABILIZER STRAP ON RBL 31.60 IS CRACKED. ; / [01] REMOVED DAMAGED STABILIZER STRAP AT E/E. COMPARTMENT BS. 312 TO BS. 344 RBL 31.60 IAW. B737-700 SRM. 51-40-02-0G-0; [02] MATCH DRILLED NEW STABILIZER STRAP IAW. B-737-700 SRM. 51-40-05-0G-0; [03] VERIFIED 1-2. OK TO INSTALL NEW STRAP.; [04] REMOVED AND REPLACED STABILIZER STRAP AT E/E COMPARTMENT BS 312 TO BS 344 RBL 31.60 IAW. B-737-700 SRM.51-40-02-0G-0 AND DWG #141A5400; [05] VERIFIED STEP 4

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FLOOR PANEL 221CF HAS LAMINATE DAMAGE AT FASTENER INSERT ; / [01] PREPARED FOR REPAIR FLOOR PANEL #221CF AS PER BOEING 737 SRM 53-00-50-2R-0; [02] REPARED FLOOR PANEL #221CF SMALL AREA AND REPLACED DAMAGE INSERTS AS PER BOEING 737 SRM53-00-50-2R-0 .MATERIAL USED EPOCAST 50-A/946 PLUS SLP5182A3 PO#1724790; [03] VERIFIED STEPS: 1 AND 2T

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AFT CARGO BUKLHEAD PNL 142NWB CRACKED. 8-78 ; / [01] RECEIVED A BRAND NEW AFT CARGO BULKHEAD PANEL 142NW. P/N: 453A2510-1. PANEL WILL BE INSTALLED ON TASK CARD# TTG8Q005ZBPS.; [02] VERIFIED 1

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CAPT SEAT TRACK HAS CORROSION ON LWR SURFACE AFT I/B. 8-57 ; / [01] RECEIVED NEW CAPT. SEAT TRACK POSITION AFT I/B REF B 737-700 IPC 25-11-01-55A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 67,300 hrs · 39,722 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE PANEL #341B; INTERNAL RIB LE STA 105.26 (RIB #4) BOTTOM EDGE RIVET HOLE CRACK NOTED. ; / [01] REMOVED DAMAGE INTERNAL RIB #4 AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA.105.26 IAW B-737-700 SRM 51-40-02-0G-0; [02] MATCH DRILLING INTERNAL RIB #4 IAW. B-737-700 SRM. 51-40-05-0G-0; [03] VERIFIED 1-2. OK TO INSTALL NEW RIB.; [04] REMOVED AND REPLACED DAMAGE INTERNAL RIB #4 AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA.86.66 IAW. B-737-700 SRM.51-40-05-0G-0 AND DWG #186A1304-2; [05] CORRECTION STEP #4. REMOVED AND REPLACED DAMAGE INTERNAL RIB#4 AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B SAT.105.26 IAW. B-737-700 SRM. 51-40-02-0G-0 AND DWG # 186A1001; [06] VERIFIED STEP 5.

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 67,300 hrs · 39,722 cycles

LEFT HORIZONTAL STABILIZER (LE STA 105.26); INTERNAL RIB #4 BOTTOM EDGE RIVET HOLE CRACK NOTED. ; LEFT HORIZONTAL STAILIZER LEADING EDGE PANEL #331B; INTERNAL RI LE STA 105.26 (RI #4) OTTOM EDGE RIVET HOLE CRACK NOTED. / [01] REMOVED CRACKED INTERNAL RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW B737-700 SRM 51-40-02-0G-0; [02] (RII) VERIFIED STEP #1.; [03] OK TO INSTALL NEW #4 RIB.; [04] STEP #3 ENTER IN ERROR.; [05] LOCATED AND DRILLED NEW INTERNAL RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW B737-700 SRM 51-40-05-0G-0; [06] (RII) TREAT AND PRIME NEW DRILLED HOLES.; [07] TREATED AND PRIMED NEW HOLES AT INTERNAL RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW B737-700 AMM 51-21-72-370-804 AND AMM 51-21-41-370-802.; [08] (RII) VERIFIED STEP #7; [09] (RII) OK TO INSTALL NEW RIB #4.; [10] INSTALLED NEW RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW SRM 51-40-02-0G-0 AND BOEING DWG #186A1001.; [11] (FINAL) REMOVED CRACKED INTERNAL RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW B737-700 SRM 51-40-02-0G-0. INSTALLED NEW RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW SRM 51-40-02-0G-0 AND BOEING DWG #186A1001.; [12] REMOVED AND REPLACED RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW B737-700 SRM 51-40-02-0G-0. INSTALLED NEW RIB #4 AT LEFT HORIZONTAL STABILIZER (LE STA 105.26) IAW SRM 51-40-02-0G-0 AND BOEING DWG #186A1001.; [13] FINAL INSPECTION; RIB #4 REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

F/O SEAT TRACK HAS CORROSION ON LWR SURFACE FWD O/B. 8-54 ; / [01] RECEIVED NEW F/O. SEAT TRACK POSITION FWD O/B REF B 737-700 IPC 25-11-51-09A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CAPT SEAT TRACK HAS CORROSION ON LWR SURFACE FWD O/B. 8-55 ; / [01] RECEIVED NEW CAPT. SEAT TRACK POSITION FWD O/B REF B 737-700 IPC 25-11-51-09A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 67,300 hrs · 39,722 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE PANEL #341B; INTERNAL RIB LE STA 95.96 (RIB #3) BOTTOM EDGE RIVET HOLE CRACK NOTED. ; / [01] MATCH DRILLING NEW INTERNAL RIB L/E AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA. 95.96 [RIB #3] IAW. B-737-700 SRM.51-40-05-0G-0; [02] LATE ENTRY REMOVED DAMAGE INTERNAL RIB #3 AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA. 95.96 IAW. B-737-700 SRM. 51-40-02-0G-0; [03] VERIFIED 1-2. OK TO INSTALL NEW RIB.; [04] INSTALLED NEW INTERNAL RIB #3 AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA.95.96 IAW. B-737-700 SRM 51-40-02-0G-0 AND DWG #186A1001; [05] VERIFIED STEP 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

F/O SEAT TRACK HAS CORROSION ON LWR SURFACE AFT I/B. 8-52 ; / [01] RECEIVED NEW F/O. SEAT TRACK POSITION AFT I/B REF B 737-700 IPC 25-11-01-55A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CAPT SEAT TRACK HAS CORROSION ON LWR SURFACE FWD I/B. 8-56 ; / [01] RECEIVED NEW CAPT. SEAT TRACK POSITION FWD I/B REF B 737-700 IPC 25-11-01-55A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FOUND CRACK AT R1 DOOR CUT OUT FWD UPPER STUB FRAME. ; / [01] REMOVED R1 DOOR FWD CUTOUT UPPER STUB FRAME RE B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW STUB FRAME AT R1 DOOR UPPER FWD CUTOUT REF B737-700 SRM 51-40-05-0G-0 AND DWG# 141A8370.; [03] VERIFIED 1-2.; [04] OK TO INSTALL R-1 DOOR STUB FRAME.; [05] INSTALLED 95% OF FASTENERS AT R1 DOOR FWD UPPER STUB FRAME REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A8370.; [06] COMPLETED INSTALLATION R1 DOOR FWD UPPER STUB FRAME REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A8370; [07] VERIFIED STEP 5 & 6; [08] REMOVED AND REPLACED R1 DOOR FWD UPPER STUB FRAME RE B737-700 SRM 51-40-02-0G-0 AND DWG#141A8370.; [09] VERIFIED STEP 8

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AFT OF FWD CARGO INTERCOSTAL CRACKED BS 520 S-25R. 8-90 ; / [01] REMOVED INTERCOSTAL AT AFT OF FWD CARGO ;STA 520 STGR - 25R AS PER B737-700 SRM 51-40-02-0G-0; [02] FABRICATED INTERCOSTAL FOR AFT OF FWD. CARGO BS. 520 S-25R IAW. DWG#143A9803-58; HEAT TREATED FABRICATED PART FROM 7075-0 TO 7075-T62 PER BAC5602. HEAT TREATMENT PAPER WORK ATTACHED.; [03] VERIFIED FABRICATION PER BOEING DRAWING 143A9803-58 AND HEAT TREAT FORM OP 84; [04] OK TO ALODINE AND PRIME FABRICATED PART.; [05] TREATED AND PRIME NEW INTERCOSTAL IAW. B-737-700 SRM. 51-20 01-0G-0; [06] VERIFIED STEP 5<BR>OK TO INSTALL FABRICATED INTERCOSTAL AT AFT OF FWD CARGO STA 520;S-25R; [07] INSTALLED NEW INTERCOSTAL A FWD CARGO STR 25R BETWEEN BS 500D AND 520 PER REF B737 SRM 51-40-02-0G-0 AND DWG 143A7902; [08] REMOVED AND REPLACED INTERCOSTAL A FWD CARGO STR 25R BETWEEN BS 500D AND 520 PER REF B737 SRM 51-40-02-0G-0 AND DWG 143A7902; [09] VERIFIED STEP # 7 AND 8; [10] JOB IS COMPLETE

Part: BULKHEAD — CRACKED (CENTER WING) · airframe 67,300 hrs · 39,722 cycles

LEFT A/C COMPT BS 663 BULKHEAD HAS 1.5' CRACK FROM LWR EDGE LBL 13. 8-19 ; / [01] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT LEFT HAND VAPOR BARRIER; FOUND CRACK 1.5''; WATER NOTE REF B737 NDT PART 1 51-05-01. MADE STOP-DRILLING OF CRACK REF B737-700 SRM51-10-02-0G-0 PARAGRAPH 12 PAGE 9 AND PREPARED DAMAGED AREA TO APPLY DRY OUT REF B737-700 SRM 51-70-04-2R-0 PARAGRAPH 4D.; [02] VERIFIED 1. OK TO DRY OUT AREA.; [03] APPLIED DRY OUT PROCESS AT THE LEFT HAND VAPOR BARRIER AS PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4D. AND PREPARED AREA TO APPLY REPAIR.; [04] VERIFIED 3. OK TO INSTALL REPAIR.; [05] REPAIRED AT PANEL LEFT A/C BS 663 BULKHEAD AS PER B 737-700 SRM 57-10-10-2R-2 PARAGRAPH 6 MATERIAL USED PO.1150387 AND PO. 1731757; [06] VERIFIED STEP 5

Part: NONE — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO COMPARTMENT BILGE R/H FLOOR SUPPORT Z CHANNEL CRACKED AT STA 5OO ; S-26R ; / [01] RECEIVED NEW Z CHANNEL (SHIELD); FOR FWD CARGO COMP LOWER BILGE STR 26R BETWEEN STA 500AND 500A; LOCATED AND DRILLED PER B737 SRM 51-40-05-0G-0 AND DWG 143A0080 INSTALLATION WILL BE ACCOMPLISHED ON CUSTOMER CARD 5330-E-16461-NG (TTG8Q004E8R8).; [02] VERIFIED STEP 1

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION ON FLIGHT DECK ENTRY CEILING INTERCOSTAL SUPPORT AT STA 270 LBL 5. CLEANED AREA AND INSPECTED, NO CORROSION FOUND IAW SRM 51-10-040G-0 AND SOPM 20-30-03. APPLIED PRIMER ON AREAS IAW AMM 51-21-72-370-804.

Part: NONE — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO COMPARTMENT BILGE R/H FLOOR SUPPORT Z CHANNEL CRACKED AT STA 5OO ; S-26R ; /

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION AT FASTENERS HOLES FWD CARGO BILGE L/H FLOOR SUPPORT Z CHANNEL FROM STA 500 TO 500D. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSPECTION ON REWORKED AREAS IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS 0.038'. ORIGINAL MAT 0.04 MATERIAL REMAINING 0.038, MATERIAL REMOVED 0.002, MAT ALLOWED TO BE REMOVED 0.004 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. TREATED AND PRIMED AREA IAW AMM 51-21-72-370-804.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

SURFACE CORROSION AT FLIGHT DECK FLOOR SKIN PANEL BETWEEN STA 259.5 AND STA 270 ;S-17L ;WL 208.1. REMOVED THE CORROSION IAW SRM. 51-10-02-0G-0. PERFORMED UT THICKNESS INSPECTION ON REWORKED AREA IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS IS 0.059'. ORIGINAL MAT 0.063' MATERIAL REMAINING 0.059' MATERIAL REMOVED 0.004', FOUND TO BE WITHIN LIMITS IAW SRM 53-10-51-1A-1 FIG 105 DETAIL C. TREATED AND PRIMED AREA IAW AMM51-21-72-370-804.

Part: NONE — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION AT FASTENERS HOLES FWD CARGO BILGE R/H FLOOR SUPPORT Z CHANNEL S-26R BETWEEN STA 480 AND 500A ; /

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION AT FASTENER HOLES FWD CARGO BILGE L/H Z CHANNEL BETWEEN STA 460 AND 480. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT PART 4 51-00-00 PROCE 3. ORIGINAL MATERIAL 0.040' MATERIAL LOSS 0.001 MATERIAL REMAINING 0.039' FOUND TO BE WITHIN LIMITS IAW SRM 53-30-53-01-2. FIGURE 103 DETAIL D. APPLIED ALODINE AND PRIMER ON AREAS IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804.

Part: NONE — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION AT FASTENERS HOLES FWD CARGO BILGE R/H FLOOR SUPPORT Z CHANNEL S-26R BETWEEN STA 480 AND 500A ; / [01] REMOVED CORRECTION ON AREAS AT S-26R BTW STA 480-500A AS PER B737-700 SRM 51-10-02-0G-0; [02] THIS FAULT WILL BE RESOLVE ON FAULT TTG8Q006LM5N.<BR>NOTE: SUPPORT Z CHANNEL STAR AT STA 500; [03] VERIFIED 2.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 67,300 hrs · 39,722 cycles

RHS # 4 RIB SUSPECT CRACK AT STIFFENER #3 LWR AREA. ; /

Part: PANEL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AFT WET AREA STA. 986.5 LBL 45.50 HAS CORROSION AROUND BOTTOM OF BOLT HOLE. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSPECTION, IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS 0.099'. ORIGINAL MAT. 0.100', MAT REMOVED 0.001' MAT REMAINING 0.099', FOUND WITHIN LIMITS IAW SRM 53-70-15-1A-1 AND FIG. 103. TREATED AND PRIMED IAW AMM 51-21-72-370-804 & AMM 51-21-41-370-802.

Part: MOUNT — CORRODED (TAIL) · airframe 67,300 hrs · 39,722 cycles

DORSAL FIN AFT RIGHT MOUNT HAS CORROSION ON FASTENERS. REMOVED AND REPLACED FASTENERS AT DORSAL FIN AFT RIGHT MOUNT REF B-737-700 SRM-51-40-02-0G-0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,300 hrs · 39,722 cycles

LHS # 5 RIB SUSPECT CRACK AT STIFFENER #3 LWR AREA. PERFORMED HFEC INSPECTION ON RIB AREA IAW NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. PERFORMED HFEC AT CUTOUT IAW NDTM PART 651-00-00 PROCEDURE 23. NO CRACKS. INSPECTED. AREA PER 55-10-09-2R-4 4E NO DEFECTS. LOCATED AND DRILLED REPAIR IAW SRM 55-10-09-2R-4, REPAIR 4. APPLIED ALODINE AND PRIMER IAW SRM 51-20-01-0G-0. INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4.

Part: NONE — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CABIN FLOOR BEAM 380 TOP CAP HAS LIGHT CORROSION 20' RIGHT OF CENTERLINE ; / [01] CLEANED AREA NO CORROSION FOUND AT CABIN FLOOR BEAM 380 TOP CAP 20' RIGHT OF CENTER LINE; [02] SOPM 20-30-03; [03] VERIFIED STEP # 1 AND # 2; [04] OK TO TREAT AND PRIME; [05] TREATED AND PRIMED AREA AS PER B737 SRM 51-20-01-0G-0; [06] VERIFIED STEP # 5

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

L-1 DOOR FWD GIRT BAR FITTING MOUNT IS CORRODED. REMOVED AND REPLACED GIRT BAR FITTING MOUNT AT L-1 DOOR FWD IAW SRM 51-40-02-0G-0.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 67,300 hrs · 39,722 cycles

RHS # 4 RIB SUSPECT CRACK AT STIFFENER #3 LWR AREA. ; / [11] INSTALLED REPAIR PARTS ON RHS #4 RIB AT STIFFENER #3 LWR AREA PER B737-700 SRM 55-10-09-2R-4 FIG. 202; [12] CUT OUT DAMAGE AREA AT RHS. #4 RIB STIFFENER #3 IAW. B-737-700 SRM.55-10-09-2R-4 REPAIR 4 FIG.202 SHEET 1. SURFACE SMOOTHER THEN 63 MICROINCHES RA. TOOL USED 172331 LOCATED AND DRILLED REPAIR PARTS ON RHS #4 RIB AT STIFFENER #3 LWR AREA PER B737-700 SRM 55-10-09-2R-4 FIG. 202 AND SRM 51-40-05-0G-0 AND INSTALLED REPAIR PARTS ON RHS #4 RIB AT STIFFENER #3 LWR AREA PER B737-700 SRM 55-10-09-2R-4 FIG. 202; [13] LATE ENTRY INSPECTED REPAIR AREA PER 55-10-09-2R-4 STEP 4 E.; [14] VERIFIED STEP # 11 AND 12; [15] JOB IS COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR LEFT O/B SEAT TRACK B.S. 827+15 - 887. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MAT. REMOVED 0.015 MAXIMUM ALLOWABLE CLEANUP DEPTH AT BOTTOM TRACK 0.040 FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO DOOR LOWER FWD CUT-OUT EXTERNAL SKIN EVIDENCE OF SURFACE CORROSION AROUND FASTENER HOLES. CLEANED AND RE-INSPECTED AREA AT FWD CARGO COMP DOOR LOWER FWD CUTOUT EXTERNAL SKIN AND RE-INSPECTED NO CORROSION FOUND ONLY REST OF SEALANT AND PRIMER DAMAGED AS PER REF B737-700 SOPM 20-30-03 AND SRM 51-10-040G-0 TO CORRECT SRM 51-10-04-0G-0 ON STEP 1 APPLIED PRIMER ON AREAS AS PER REF B737-700 SRM 51-21-72-370-804 VERIFIED 1-3.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO COMP SIDEWALL STRUCTURE GUSSET CRACKED AT BS 500D STGR 19-R ; / [01] REMOVED GUSSET AT FWD CARGO COMP SIDEWALL STRUCTURE AT STA 500D ; STGR 19- R AS PER B737-700 SRM 51-40-02-0G-0; [02] RECEIVED ;LOCATED AND DRILLED NEW GUSSET AT STA 500D STGR 19-R AS PER B737-700 SRM 51-40-05-0G-0 .; [03] VERIFIED 1-2. OK TO INSTALL.; [04] INSTALL NEW GUSSET PER REF B737 SRM 51-40-02-0G-0; [05] REMOVED AND REPLACED GUSSET AT FWD CARGO COMP SIDEWALL STRUCTURE AT STA 500D ; STGR 19- R AS PER B737-700 SRM 51-40-02-0G-0 AND DWG 143A7902; [06] VERIFIED 4-5

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR LEFT I/B SEAT TRACK B.S. 360+10 - 380. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MAT. REMOVED 0.008' MAXIMUM ALLOWABLE CLEANUP DEPTH BOTTOM TRACK 0.040' FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOT ON CABIN FLOOR LEFT O/B SEAT TRACK B.S. 727A+10. REMOVED CORROSION SPOT ON CABIN FLOOR LEFT O/B SEAT TRACK IAW SRM 51-10-02-0G-0. REMOVED 0.013 MAXIMUM ALLOWABLE CLEANUP DEPTH AT BOTTOM TRACK 0.040, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOT ON CABIN FLOOR LEFT O/B SEAT TRACK B.S. 805+5. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MATERIAL REMOVED 0.015 MAXIMUM ALLOWABLE CLEANUP DEPTH AT BOTTOM TRACK 0.040 FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOT ON CABIN FLOOR RIGHT O/B SEAT TRACK B.S. 500A+6. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MAT. REMOVED 0.020' MAXIMUM ALLOWABLE DAMAGE AT BOTTOM OF THE TRACK 0.04, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED CABIN FLOOR RIGHT O/B SEAT TRACK IAW 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR LEFT O/B SEAT TRACK B.S. 360+10 - 380. REMOVED CORROSION SPOTS ON CABIN FLOOR LEFT O/B SEAT TRACK IAW SRM 51-10-02-0G-0. REMOVED 0.009' MAXIMUM ALLOWABLE, CLEANUP DEPTH ON THE TOP TRACK 0.02' FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG A-A. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR RIGHT O/B SEAT TRACK BETWEEN B.S. 616-667.75. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MATERIAL REMOVED 0.006' MAXIMUM ALLOWABLE DAMAGE AT BOTTOM OF THE TRACK 0.04, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR LEFT I/B SEAT TRACK B.S 500-500A. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MAT. REMOVED 0.005' MAXIMUM ALLOWABLE CLEANUP DEPTH ON THE TOP TRACK 0.02' FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR RIGHT O/B SEAT TRACK BETWEEN B.S. 667.75+15 - 727. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MATERIAL REMOVED 0.012' MAXIMUM ALLOWABLE DAMAGE AT BOTTOM OF THE TRACK 0.04, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED IAW SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOT ON CABIN FLOOR RIGHT I/B SEAT TRACK B.S. 578+13. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MATERIAL REMOVED 0.007' MAXIMUM ALLOWABLE DAMAGE AT BOTTOM OF THE TRACK 0.04, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED IAW 51-20-01-0G-0.

Part: PANEL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

PANEL 211AF HAS CORROSION ALONG EDGES. 8-4 ; / [01] RECEIVED NEW PANEL 211AF; DRILLED NEW HOLES PER REF B737 SRM 51-40-05-0G-0. INSTALLATION WILL BE ACCOMPLISHED ON FAULT TTG8Q005ZC6T; [02] VERIFIED 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO DOOR LOWER AFT CUT-OUT EXTERNAL SKIN EVIDENCE OF SURFACE CORROSION AROUND FASTENER HOLES. CLEANED AND RE-INSPECTED AREA AT FWD CARGO COMP DOOR LOWER AFT CUTOUT EXTERNAL SKIN AND RE-INSPECTED NO CORROSION FOUND ONLY REST OF SEALANT AND PRIMER DAMAGED AS PER REF B737-700 SOPM 20-30-03 AND SRM 51-10-040G-0 APPLIED PRIMER ON AREAS AS PER REF B737-700 AMM 51-21-72-370-804 TO CORRECT SRM 51-10-04-0G-0 ON STEP 1 VERIFIED 1-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AFT WET AREA AT STA. 1006 UNDER PANEL 242VF HAS CORROSION ON FRAME. REMOVED CORROSION IAW SRM 51-10-02-0G-0. UT THICKNESS INSP. IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS 0.079'. ORIGINAL MAT. 0.080''. MAT REMOVED 0.001' MAT REMAINING 0.079' FOUND WITHIN LIMITS IAW SRM 53-70-51-1A-1, & DWG 147A5733. TREATED AND PRIMED AREA IAW AMM 51-21-72-37-804 AND AMM 51-21-41-370-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN LEFT O/B SEAT TRACK B.S. 727C -727D. REMOVED CORROSION IAW SRM 51-10-02-0G-0. EVALUATED AREA. MAT. REMOVED 0.016 MAXIMUM ALLOWABLE, CLEANUP DEPTH AT BOTTOM TRACK 0.040 FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED REWORKED AREA IAW SRM 51-20-01-0G-0.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO COMP SIDEWALL STRUCTURE GUSSET CRACKED AT BS 500D STGR 19-L. ; / [01] REMOVED GUSSET AT FWD CARGO COMP SIDEWALL STRUCTURE ;STA 500D STGR 19-L AS PER B737-700 SRM 51-40-02-0G-0; [02] RECEIVED; LOCATED AND DRILLED NEW GUSSET AS PER B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP 1 AND 2; [04] OK TO INSTALL NEW GUSSET AT FWD CARGO STA 500D STGD 19-L; [05] INSTALLED NEW GUSSET AT FWD CARGO SIDEWALL STRUCTURE STA 500D ;STGR 19-L AS PER B737-700 SRM 51-40-02-0G-0 DWG # 143A9481; [06] REMOVED AND REPLACED GUSSET AT FWD CARGO SIDEWALL STRUCTURE STA 500D ;STGR 19-L AS PER B737-700 SRM 51-40-02-0G-0 DWG # 143A9481; [07] VERIFIED 5-6.

Part: PANEL — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

PANEL 211AF HAS CORROSION ALONG EDGES. 8-4 ; /

Part: ACCESS PANEL — DETERIORATED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AROUND THE SCREW DOOR HINGE OF THE BONDING WIRE OF PANEL 191D COMPOSITE IS DETERIORATED (228-004) ; / [01] PERFORMED VISUAL INSPECTION AT ACCESS PANEL 191D FOUND FASTENER HOLES DAMAGED; NO WATER NOTE. PREPARED DAMAGED AREA TO APPLY REPAIR. REF B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARAGRAPH 4 A;B AND C; [02] VERIFIED 1. OK TO CONTINUE REPAIR.; [03] APPLIED REPAIR ON DAMAGED FASTENERS HOLES AT ACCESS PANEL 192D REF B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARAGRAPH 4 D - O.

Part: NONE — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO DOOR LOWER MAIN SILL WEB BS 455 TO BS 480 STGR 25-R; SEVERAL FASTENER HOLES WITH EVIDENCE OF SURFACE CORROSION. REMOVED CORROSION ON AREAS AT FWD CARGO DOOR LOWER MAIN SILL WEB IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA. IAW NDT PART 4 51-00-00 PROCE 3. MIN THICK 0.039'. CORROSION MIN THICKNESS 0.044'. AFTER PERFORMED UT THICKNESS ON REWORKED AREAS .ORIGINAL MATERIAL 0.045' MATERIAL LOSS 0.001 MATERIAL REMAINING 0.044', FOUND TO BE WITHIN LIMITS IAW SRM 53-30-53-15-0L-1, FIGURE 103, DETAIL D. DIMENSION FOUND WITHIN LIMITS. APPLIED ALODINE AND PRIMER ON AREAS IAW SRM 51-20-01-0G-0 & AMM 51-21-72-370-804.

Part: ANGLE — CRACKED (CENTER WING) · airframe 67,300 hrs · 39,722 cycles

VAPOR BARRIER ANGLE CRACKED AT L/H WHEEL WELL ON AFT SIDE OF STA 663 AND ABOUT LBL-8 ; / [24] ACCOMPLISHED REPAIR AT VAPOR BARRIER ANGLE AT L/H WHEEL WELL ON AFT SIDE I/B STA 663 LBL 8 IAW SRM 51-10-10-2R-5 FIG 202 SHEET 4; [25] VERIFIED 24.

Part: ANGLE — CRACKED (CENTER WING) · airframe 67,300 hrs · 39,722 cycles

VAPOR BARRIER ANGLE CRACKED AT L/H WHEEL WELL ON AFT SIDE OF STA 663 AND ABOUT LBL-8 ; /

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

CORROSION SPOTS ON CABIN FLOOR RIGHT O/B SEAT TRACK BETWEEN B.S. 578 - 597.9. REMOVED CORROSION IAW SRM 51-10-02-0G-0. MATERIAL REMOVED 0.012' MAXIMUM ALLOWABLE DAMAGE AT BOTTOM OF THE TRACK 0.04, FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG. 103. TREATED AND PRIMED IAW SRM 51-20-01-0G-0.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FWD CARGO COMP SIDEWALL STRUCTURE GUSSET CRACKED AT BS 500D STGR 19-R ; /

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

AFT CARGO DOOR LOWER SILL AFT CORNER SCUFF PLATE FOUND CRACKED. ; / [01] RECEIVED NEW AFT CORNER SCUFF PLATE. AFT CORNER SCUFF PLATE WILL BE INSTALLED ON CUSTOMER CARD # TTG8Q0032F54.; [02] VERIFIED STEP 1

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FORWARD GALLY DOOR (R1) BEAR STRAP BS290 TO 296 BETWEEN S-8R AND S-9R HAS A 1.625' CRACK EMINATING FROM STRAP T/E THROUGH THE 2ND FASTENER FROM THE TOP (TYPICAL LOCATION) / [01] BEAR STRAP - CRACK #1 = 1.078'; CRACK #2 = 0.281'; [02] INSTALLED EWIS PROTECTION AT MAIN CABIN R1 DOOR REPAIR AREA REF B737-700 AMM 20-60-07-913-801.; [03] REMOVED RAIN GUTTERS AT R1 DOOR FUSELAGE SKIN TO GAIN ACCESS REF B737-700 SRM 51-40-02-0G-0.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

FORWARD GALLY DOOR (R1) BEAR STRAP BS290 TO 296 BETWEEN S-8R AND S-9R HAS A 1.625' CRACK EMINATING FROM STRAP T/E THROUGH THE 2ND FASTENER FROM THE TOP (TYPICAL LOCATION) ; FORWARD GALLY DOOR (R1) BEAR STRAP BS290 TO 296 BETWEEN S-8R AND S-9R HAS A 1.625' CRACK EMINATING FROM STRAP TE THROUGH THE 2ND FASTENER FROM THE TOP (TYPICAL LOCATION) / [39] ACCOMPLISHED PERMANENT REPAIR AT R1 DOOR BEAR STRAP BS290 TO BS296 BETWEEN S-8R,NG,NRC,2021-10-25 15:20:32,20Y,Y,MX,0,0,,FORWARD GALLY DOOR (R1) BEAR STRAP BS290 TO 296 BETWEEN S-8R AND S-9R HAS A 1.625' CRACK EMINATING FROM STRAP T/E THROUGH THE 2ND FASTENER FROM THE TOP (TYPICAL LOCATION) ; FORWARD GALLY DOOR (R1) BEAR STRAP BS290 TO 296 BETWEEN S-8R AND S-9R HAS A 1.625' CRACK EMINATING FROM STRAP TE THROUGH THE 2ND FASTENER FROM THE TOP (TYPICAL LOCATION)"

Part: DOOR — CORRODED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

TOILET SERVICE DOOR 145AL HAS CORROSION SPOTS ON INNER AND OUTER SURFACES.(51-004) ; / [01] STARTED REMOVING CORROSION AT SERVICE DOOR 145AL ON INNER SURFACE AROUND GROUND HOLE PER B737 SRM 51-10-02-0G-0; FOUND EXFOLIATION THROUGHOUT MORE THAN 50% OF MATERIAL THICKNESS; FOUND TO BE OUT OF LIMITS PER B737 SRM 52-40-01-1A-4; [02] REMOVED DAMEGE TOILET SERVICE DOOR 145AL AS PER SRM 737 51-40-02-0G-0; [03] VERIFIED STEP:1 AND 3<BR>OK TO INSTALL NEW DOOR PANEL 145 AL; [04] INSTALLED TOILET SERVICE DOOR 145AL AS PER SRM 737 51-40-02-0G-0; [05] VERIFIED 4. PENDING PAINT AND DECAL; [06] TOUCHED UP PAINT AS REQUIRED REF B-737-AMM 51-21-73-370-803; [07] CORRECTING STEP 6: TOUCHED UP PAINT AS REQUIRED AND APPLIED STENCIL REF B-737-AMM 51-21-73-370-803; [08] CORRECTION STEP 3:VERIFIED STEPS:1 AND 2; [09] VERIFIED STEP 7; [10] INSTALL NEW PLACARDS PER REF B737 AMM 11-00-00-201; [11] REMOVED AND REPLACED TOILET SERVICE DOOR 145AL PER REF B737 SRM 51-40-02-0G-0

Part: PANEL — CRACKED (FUSELAGE) · airframe 67,300 hrs · 39,722 cycles

PANEL 194E AFT EDGE RT SCREW HOLE AREA BULGING INWARD AND APPEARS CRACKED. 8 ; / [01] PREPARED PANEL #193E FOR REPAIR AS PER B737 SRM 51-70-06-2R-9; [02] VERIFIED STEP # 1; [03] REPAIRED AT PANEL 193 E AS PER B 737 SRM. 51-70-06-2R-9 MATERIAL USED PO.1731939 AND PO. 1690463; [04] VERIFIED STEP #3; [05] CORRECTION TO STEP 1: PREPARED PANEL #194E FOR REPAIR AS PER B737 SRM 53-60-70-2R-1 AND SRM 51-70-04-2R-9; [06] CORRECTION TO STEP 3: REPAIRED PANEL 194E AS PER B737 53-60-70-2R-1 AND SRM 51-70-04-2R-9 . MATERIALS USED P/O #1731939 AND P/O #1690463; [07] FINISHED REPAIR; [08] CORRECTION TO STEP 6: REPAIRED PANEL 194E AS PER B737 53-60-70-2R-1 AND SRM 51-70-04-2R-9. PAINTED PANEL AS PER B737 AMM 51-21-99-300-802. MATERIALS USED P/O# 1731939 AND P/O# 1690463 AND P/O#1686310; [09] VERIFIED 5-8.

Part: STIFFENER — CRACKED (BS 250) · airframe 66,849 hrs · 39,442 cycles

STIFFENER CRACKED AT BS. 250, BETWEEN LBL 5 TO LBL 15. / R&R STIFFENER IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 260-270) · airframe 66,849 hrs · 39,442 cycles

FLIGHT DECK FLOOR STRUCTURE INTERCOSTAL CORRODED BETWEEN BS. 260 TO BS. 270, BL 0. / R&R INTERCOSTAL IAW SRM & DWG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,727 hrs · 39,358 cycles

EMERGENCY INTERIOR LIGHT INOP AT ROW 20. RELAMPED LIGHT IAW AMM.

Part: COVER — OUT OF POSITION (R2 DOOR SLIDE) · airframe 66,112 hrs · 38,980 cycles

R2 DOOR, EMERGENCY ESCAPE SLIDES, PULL HANDLE ACCESS HANDLE COVER MISSING. / FOUND HANDLE COVER OUT OF POSITION PER MT.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 65,793 hrs · 38,791 cycles

193B PANEL HAS EROSION AND ELONGATED HOLES AT HOLE POSITIONS 13 THRU 20. / REMOVED AND INSTALLED NEW PANEL IAW SRM 51-40-02.

Part: SKIN — CRACKED (R/H WING) · airframe 65,793 hrs · 38,791 cycles

NUMBER EIGHT SLAT COVE SKIN PANEL 625DAB HAS THREE CRACKS COMMON TO ONE FASTENER HOLE. / ACCOMPLISHED A PERMANENT REPAIR REF EA NO:1-757-16616.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 63,670 hrs · 37,415 cycles

R/H HORIZONTAL STAB. UPPER FWD. SLIDING SEAL IS CRACKED / R&R R/H HORIZONTAL STAB. UPPER FWD. SLIDING SEAL REF AMM 53-31-31.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 63,392 hrs · 37,243 cycles

LT OVERWING LOWER EMERGENCY EXIT SIGN BULBS INOP. R&R LAMP PER AMM.

Part: FUSE — BLOWN (CABIN) · airframe 63,392 hrs · 37,243 cycles

EMERGENCY EXIT LIGHT IN COCKPIT INOP. R&R FUSE PER AMM.

Part: WIRE — BROKEN (CABIN) · airframe 63,392 hrs · 37,243 cycles

FORWARD LAV EMERGENCY EXIT LIGHT WIRE CONNECTOR BROKEN. R&R WIRE PER WDM AND AMM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 63,392 hrs · 37,243 cycles

R2 DOOR SLIDE LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

STRINGER CLIP CRACKED AT BS 787, STR 26R. R&R CLIP PER SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

CLIP CRACKED AT BS 787, STR 26R. R&R CLIP PER SRM AND DWG.

Part: SUPPORT FRAME — CRACKED (LWR FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

RH ECS BAY FAIRING SUPPORT FRAME IS CRACKED AT BS 650 RBL 26 / REMOVED R/H ECS BAY SUPPORT FRAME AT STA 663 RBL 26 PER SRM 51-40-02; FABRICATED SUPPORT FRAME OUT OF BAC 150 6-4475 7075T73511 LOT # 1311004-1 PER SRM 51-40-05 AND DWG. 149A7214. RECEIVED SUPPORT FRAME IN ANODIZED CONDITION HFAB53-FR-012 P.O.#727402-SWA. INSTALLED SUPPORT FRAME PER SRM 51-40-02; DWG. 149A7210 AND DWG. 111A1000. 91195U 1-22-19

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,392 hrs · 37,243 cycles

VAPOR BARRIER SUPPORT STIFFENER CRACKED AT BS 663, RBL 7. R&R STIFFENER PER SRM AND DWG.

Part: SKIN — CHAFED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

EXTERNAL SKIN CHAFED AT BS 850, BL 0. REPAIRED SKIN IAW ER AND EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

OUTBOARD LT SHEAR WEB CRACKED BETWEEN BS 986.5 TO BS 1016. R&R WEB PER SRM AND DWG.

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 63,392 hrs · 37,243 cycles

FILLET FAIRING PANEL 191D HAS A CRACK LOCATED AT BL0; 39' FROM THE LEADING EDGE / REPAIRED FILLET FAIRING PANEL 191D CRACK LOCATED AT BL; 0 39' FROM THE LEADING EDGE IAW SRM 51-70-05-2R-11; AND SRM 51-70-14-2R-4

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,392 hrs · 37,243 cycles

***CORROSION*** ON AFT CARGO BAY PANEL; 140CF; AROUND PERIPHERY OF PANEL. / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .071 2024T3; LOT #137373B-1 PER AMM 25-52-01-201-801 AND DWG 4532610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN FOR THIS PART IN SRM

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

SCUFF PLATE INNER SUPPORT CORRODED AT BS 312, RBL 57. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FLOORBEAM AT FORWARD CAB CORRODED AT BS 328 RBL 48. R&R UPPER CHORD PER SRM & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

L1 DOOR SCUFF PLATE INNER SUPPORT CORRODED AT BS 312, LBL 59. R&R SUPPORT IAW SRM & DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,392 hrs · 37,243 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 DOOR PER AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

L1 DOOR SCUFF PLATE INNER SUPPORT CORRODED AT BS 312, LBL 62. R&R SUPPORT IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

R1 DOOR LOWER STUB FRAME CRACKED AT BS 294, RBL 54. R&R STUB FRAME IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT SHIELD AT FORWARD CARGO BAY CORRODED BETWEEN BS 492 TO BS 500A, RBL 25. R&R SHIELD PER SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500A+19, LBL 24. R&R SUPPORT ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C TO BS 767, RBL 21. R&R SUPPORT PER SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO DOORWAY FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 21. REPAIRED SUPPORT PER SRM AND DWG.

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY FORWARD BULKHEAD PANEL SUPPORT BROKEN AT BS 727, RBL 4. R&R SUPPORT PER SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R THRESHOLD WEB PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 440, LBL 24. REPAIRED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

HORIZONTAL PRESSURE DECK WEB CORRODED AT BS 667, LBL 67. R&R SHEAR TIE PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 887 TO BS 947, LBL 3. R&R FLOOR TRACK PER SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY BILGE AREA CORRODED AT BS 500+8, BL 0. R&R BILGE AREA IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO DOORWAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SUPPORT — CORRODED (LT MLG WW) · airframe 63,392 hrs · 37,243 cycles

HORIZONTAL PRESSURE DECK WEB L ANGLE SUPPORT CORRODED AT BS 687, LBL 69. REPAIRED SUPPORT PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500B+1, LBL 24. R&R SUPPORT ANGLE IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 887 TO BS 947, RBL 13. R&R FLOOR TRACK IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

INTERCOSTAL CORRODED AT BS 850, RBL 18. R&R INTERCOSTAL PER SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 24 TO LBL 24. R&R RAIL IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 787 TO BS 847, STR 25R. R&R WEB IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY FLOOR TRACK CORRODED AT BS 767+5, RBL14. R&R FLOOR TRACK IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 21. R&R SHIELD PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 400, LBL 24. R&R ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

HORIZONTAL PRESSURE DECK WEB CORRODED AT BS 705, LBL 67. REPAIRED WEB IAW ER AND EA.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 63,392 hrs · 37,243 cycles

PANEL 193B HAS DELAMINATION DAMAGE ON OUTER SKIN / PANEL 193B WITH DELAMINATION DAMAGE ON OUTER SKIN WAS REPAIRED PER SRM 51-70-05-2R-2 57545U 1-17-19

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500A+1, LBL 24. R&R ANGLE IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 787 TO BS 887, RBL 14. R&R FLOOR TRACK IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FLOORBEAM CORRODED AT BS 987, LBL 43. REPAIRED FLOORBEAM IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 17 TO RBL 44. REPAIRED FLOORBEAM IAW ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

L2 DOOR MOPSILL CORRODED. R&R MOPSILL IAW DWG

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

R2 DOOR MOPSILL CORRODED. R&R MOPSILL IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,392 hrs · 37,243 cycles

INTERCOSTAL CRACKED AT BS 927+17, LBL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 63,392 hrs · 37,243 cycles

FWD CABIN FLOOR PANEL 221GF HAS BROKEN TANG ON FWD O/B CORNER / DAMAGED FLOOR PANEL 221GF WAS REPLACED WITH A SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR 9.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,392 hrs · 37,243 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW ER AND EA.

Part: PLATE — CRACKED (R/H WING) · airframe 63,392 hrs · 37,243 cycles

RT WING LOWER SURFACE WIGGLE PLATE AT RSS 261 IS CRACKED / REMOVED AND REPLACED RT WING LOWER SURFACE WIGGLE PLATE AT R55 261; P/N. 115A2781-14 IAW. 51-40-02 AND AIPC 57-50-00-30. 889204 28DEC18

Part: WEB — CRACKED (LT WING) · airframe 63,392 hrs · 37,243 cycles

LT WING TRANSVERSE WEB ABOVE NR 1 PYLON AFT TIP CRACKED ON THE OUTBOARD END. R&R WEB IAW SRM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 63,392 hrs · 37,243 cycles

RT WING BULB SEAL RETAINER ABOVE #2 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED RT WING BULB SEAL RETAINER ABOVE #2 PYLON P/N 115A2953-2 IDW SRM 51-40-02 AND AIPC 57-50-00-25 88920U 29DEC18

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 63,392 hrs · 37,243 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS 663, RBL 12. REPAIRED BULKHEAD IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,392 hrs · 37,243 cycles

RT WING SLAT NR 7 LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB ATTACHMENT FASTENER CRACKED. REPAIRED SLAT SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,773 hrs · 36,833 cycles

L2 DOOR ESCAPE SLIDE PULL TAB AND CHAIN OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 62,167 hrs · 36,445 cycles

R1 DOOR SLIDE PARTIALLY DEPLOYED. R&R SLIDE IAW MT.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 61,657 hrs · 36,136 cycles

LT FLOOR PHOTOLUMINESCENT STRIP DAMAGED AT 1ST SECTION. R&R STRIP PER AMM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,102 hrs · 35,778 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,525 hrs · 35,426 cycles

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

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,306 hrs · 35,286 cycles

EMERGENCY EXIT LIGHT SWITCH GUARD INOPERATIVE. R & R THE SWITCH GUARD SYSTEM IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,861 hrs · 34,999 cycles

RT OVERWING EMERGENCY LIGHT INOP. RE-LAMPED LIGHT PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,861 hrs · 34,999 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. REPAIRED INTERCOSTAL IAW EA.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 59,861 hrs · 34,999 cycles

TWO EACH CRACKS NOTED IN THE UPPER BEAM OF THE INTERCASTER AT LBL 12; BETWEEN STA'S 344-360. THE FED CRACK MEASURES .55' AND DOES NOT INTERSECT A FASTENER HOLE. THE AFT CRACK MEASURES .67' AND ENDS AT A FASTENER HOLE / TRANSFERRED TO NRC N113456

Part: INTERCOSTAL — CRACKED (E & E COMPT) · airframe 59,860 hrs · 34,998 cycles

INTERCOSTAL (-24) TO THE RIGHT OF CENTER BETWEEN STAS 344-360 HAS A CRACK NOTED IN THE UPPER BEAM. / REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02 AND SIP.

Part: INTERCOSTAL — CRACKED (E & E COMPT) · airframe 59,860 hrs · 34,998 cycles

CENTER INTERCOSTAL (-23) BETWEEN STAS 344-360 HAS TWO CRACKS NOTED IN THE UPPER BEAM. / REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02 AND SIP.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 59,452 hrs · 34,731 cycles

FORWARD GALLEY UPPER EMERGENCY FLASH LIGHT STRAP BROKEN. R&R STRAP PER MM.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO SMOKE NR 3 DETECTOR PER AMM.

Part: CONTROL PANEL — ABNORMAL (FIRE PROTECTION) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO FIRE PROTECTION CONTROL PANEL PER AMM.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO SMOKE NR 6 DETECTOR PER AMM.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO SMOKE NR 4 DETECTOR PER AMM.

Part: ELECTRONIC UNIT — FAULTY (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO FIRE PROTECTION ELECTRONIC UNIT PER AMM.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO SMOKE NR 5 DETECTOR PER AMM.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO SMOKE NR 2 DETECTOR PER AMM.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 59,218 hrs · 34,583 cycles

DECLARED EMERGENCY, AFT CARGO FIRE LIGHT CAME ON DURING APPROACH THEN WENT OFF. R&R CARGO SMOKE NR 1 DETECTOR PER AMM.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 58,930 hrs · 34,400 cycles

CRACK IN AFT CARGO FLOOR / PLACED PATCH ON CRACK IAW SRM 53-30-01

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 58,097 hrs · 33,877 cycles

LEFT EMERGENCY EXIT SIGN COVER LOOSE. SECURED THE SIGN COVER IAW SIP.

Part: FITTING — LOOSE (R1 DOOR GIRT BAR) · airframe 57,885 hrs · 33,747 cycles

R1 DOOR SLIDE GIRT BAR STOWAGE CLIP LOOSE. SECURED THE FITTING IAW MT.

Part: SEAL — CRACKED (BS 663) · airframe 56,928 hrs · 33,196 cycles

VAPOR BARRIER SEAL CRACKED AT BS 663, RBL 9. REPAIRED VAPOR BARRIER IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 56,928 hrs · 33,196 cycles

FORWARD EMERGENCY EXIT LIGHT LENS LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,928 hrs · 33,196 cycles

RT WING NR 8 SLAT LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR FITTING AREA CRACKED. REPAIRED SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,928 hrs · 33,196 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,928 hrs · 33,196 cycles

RT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.

Part: ENGINE — POWER LOSS (NR 2)

NR 2 ENGINE COULD NOT ACHIEVE FULL CLIMB THRUST. COMPLIED WITH FAN TRIM BALANCE IAW TC.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,164 hrs · 32,745 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,164 hrs · 32,745 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,164 hrs · 32,745 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 56,164 hrs · 32,745 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,164 hrs · 32,745 cycles

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

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 56,164 hrs · 32,745 cycles

CABIN FORWARD LT ENTRY GLOWSTRIP DAMAGED. R&R THE GLOWSTRIP IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,164 hrs · 32,745 cycles

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

Part: ACTUATOR — LEAKING (RT WING SPOILIER) · airframe 56,164 hrs · 32,745 cycles

RIGHT WING NR 8 FLIGHT SPOILER ACTUATOR LEAKED. R & R THE ACTUATOR IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,164 hrs · 32,745 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,024 hrs · 30,913 cycles

LEFT WING OTBD FLAP LOWER INBD SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, FASTENER HOLE NR 19. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, FASTENER HOLE NR 5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75, BETWEEN FASTENER HOLE NR 7 - 10. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, BETWEEN FASTENER HOLE NR 7 - 9. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, AT HOLE NR 19. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5, BETWEEN FASTENER HOLE NR 7 - 10. REPAIRED SEAT TRACK IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

LEFT FLIGHT DECK NR 3 WINDOW POST, SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

FLIGHT DECK NR 1 RT OTBD WINDOW FRAME CRACKED AT UPPER OTBD CORNER, ON INTERIOR SIDE OF FRAME. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 53,024 hrs · 30,913 cycles

RIGHT FLIGHT DECK NR 3 WINDOW POST, SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,514 hrs · 30,609 cycles

LEFT OVERHEAD EMER LIGHT INOPERATIVE AT ROW 4. RELAMPED LIGHT IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,214 hrs · 29,884 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 50,538 hrs · 29,504 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,456 hrs · 29,456 cycles

LEFT NR 1 FLIGHT DECK WINDOW FRAME CRACKED AT THE UPPER OTBD CORNER. REPAIRED FRAME IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 49,562 hrs · 28,920 cycles

LEFT EMER LIGHT FAILED CAPACITY CHECK BETWEEN ROW 1 TO ROW 6. R & R BATTERY IAW AMM.

Part: FAN — FAILED (AC BAY) · airframe 49,541 hrs · 28,909 cycles

DECLARED EMER ON DOWNWIND APPROACH TO AIRPORT FLIGHT ATTENDANTS & PAXS SMELLED SMOKE IN REAR & MID CABIN. FOUND RECIRCULATION FAN POPPING CB, FAN INOPERATIVE. R & R RECIRCULATION FAN IAW MM.

Part: BEARING — FAULTY (AILERON) · airframe 46,266 hrs · 26,984 cycles

AIR TURN BACK, DECLARED EMERGENCY, AILERON RESTRICTED MOVEMENT DURING CLIMB. R & R CAM BEARING IAW MM.

Part: COVER — CRACKED (LT AILERON) · airframe 45,114 hrs · 26,288 cycles

LT WING AILERON LOWER HINGE COVER/SEAL CRACKED THROUGH A FASTENER HOLE. REPAIRED COVER IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 45,114 hrs · 26,288 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED AT ACTUATOR MOUNT FITTING. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,959 hrs · 25,586 cycles

R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 43,959 hrs · 25,586 cycles

FLOOR TRACK LIGHT COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

RIGHT CARGO Z-ANGLE CORRODED BETWEEN BS 727 TO BS 727C. REPAIRED ZEE ANGLE IAW SRM.

Part: LIGHT — DETERIORATED (CABIN) · airframe 43,557 hrs · 25,320 cycles

EMERGENCY FLOOR LIGHTING FROM STA 500B TO 639 HAS NUMEROUS COMPONENTS DETERIORATED. INSTALLED NEW TRACK LIGHT LENS AND TRACK COVERS FROM STA 500B TO 639 IAW AMM 25-27-31-400-801-001, OPS CHECK GOOD IAW AMM 33-51-00-710-801.

Part: LIGHT — CORRODED (CABIN) · airframe 43,557 hrs · 25,320 cycles

EMERGENCY FLOOR LIGHTING BETWEEN BS 360 TO BS 500B CORRODED. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: LIGHT — DETERIORATED (CABIN) · airframe 43,557 hrs · 25,320 cycles

EMERGENCY FLOOR LIGHTING FROM STA 639 TO 747 HAS NUMEROUS COMPONENTS DETERIORATED. INSTALLED NEW TRACK LIGHT LENS AND TRACK COVERS FROM STA 639 TO 747 IAW AMM 25-27-31-400-801-001, OPS CHECK GOOD IAW AMM 33-51-00-710-801.

Part: PIN — CORRODED (LT HORIZ STAB) · airframe 43,557 hrs · 25,320 cycles

LEFT HORIZONTAL STABILIZER LWR REAR SPAR ATTACHMENT PIN IS PITTED IN SEVERAL AREAS. REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER, LWR REAR SPAR ATTACHMENT PIN, IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

AFT CARGO INTERCOSTAL WEB STA 767 TO 787 RBL 6 CORRODED ON FORWARD O/B SIDE. REMOVED CORROSION, HAD .008 MAT LOSS OF .036 ORIGINAL MAT WITH .028 REMAINING, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 DETAIL D AND SRM 51-10-02-0G-0 REMO

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 43,557 hrs · 25,320 cycles

LEFT MAIN W/W FWD BULKHEAD STA-663, LBL-27, LOWER CORD VERT STIFFENER CRACKED AT LOWER RADIUS. REMOVED AND REPLACED DAMAGE VERTICAL STIFFENER AT BS 663 LBL 27 IAW SRM 51-40-02 & BOEING DOCUMENT 111A100.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-480 BELOW STR-8R AT PSU RAIL. REPAIRED MAIN CABIN FRAME AT STA 480 BELOW STR 8R AT PSU RAIL BY INSTALLING RESTED ANGLE IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

FORWARD CARGO COMPARTMENT, INTERCOSTAL ATTACH ANGLE CRACKED, STATION 500C, LBL 25, AFT SIDE OF FRAME. REMOVED AND REPLACED ATTACH ANGLE WITH NEW AT STA 500C LBL 25 AFT SIDE IAW SRM 5

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-727D BELOW STR-8R AT PSU RAIL. REPAIRED MAIN CABIN FRAME AT STA 727D BELOW STRINGER 8R BY INSTALLING NESTED ANGLE IAW EA 1-A53-12114 REV 2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,557 hrs · 25,320 cycles

AFT CARGO TRACK CORRODED BETWEEN BS 792 TO BS 820, RBL 12. REMOVED AND REPLACED TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-440 BELOW STR 8R AT PSU RAIL. REPAIRED FRAME IAW EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

PASSENGER CABIN STA 787 FRAME CRACKED AT INBOARD FASTENER NEAR STRINGER 8L. REPAIRED FRAME IN PASSENGER CABIN AT STA 787 BELOW STRINGER 8 WITH A RIVETED NESTED ANGLE REPAIR PER EA 1-A53-12114 REV 2. ALL WORK PERFORMED ON EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-400 BELOW STR-8L AT PSU RAIL. REPAIRED FRAME IN MAIN CABIN AT SAT 400 BELOW STR 8L AT THE PSU RAIL WITH A RIVETED NESTED ANGLE REPAIR PER EA 1-A53-12114 REV 2 ALL WORK ACCOMPLISHED ON EA 1-A53-12114 REV 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN, INTERCOSTAL BL-0 STA-277 TO STA-294.5 IS CRACKED. REMOVED AND REPLACED INTERCOSTAL BL-0 STA 277 - STA 294.5 IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0. RESTORED CORROSION INHIBITING COMPOUND TO AREA IAW AMM 51-21-91-620-802.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-727D BELOW STR-8L AT PSU RAIL. INSTALLED FRAME REPAIR AT STA 727 "D" BETWEEN STRINGER 8L AND 9L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

PASSENGER CABIN STA 747 FRAME CRACKED AT INBOARD FASTENER NEAR STRINGER 8L. REPAIRED FRAME IN PASSENGER CABIN AT STA 747 NEAR STRINGER 8L WITH A RIVETED NESTED ANGLE REPAIR AS PER EA 1-A53-12114 REV 2 ALL WORK PERFORMED ON EA 1-A53-12114 REV 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN INTERCOSTAL AT STA-332 STR-5R IS CRACKED. REMOVED AND REPLACED INTERCOSTAL AT STA 332 STR 5R IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

RIGHT SIDE FLOOR STRUCTURE, Z-ANGLE CORRODED BETWEEN BS 727D TO 767. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-867 BELOW STR-8L AT PSU RAIL. REPAIRED FRAME IN MAIN CABIN AT STA 867 BELOW STR 8L AT THE PSU RAIL WITH A RIVETED NESTED ANGLE REPAIR PER EA 1 A-53-12114 REV 2. ALL WORK ACCOMPLISHED ON EA 1-A53-12114 REV 2.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

FLOOR STRUCTURE STA 887 SUPPORT STRAP CORRODED. REMOVED AND REPLACED STRAP IAW SRM AND BOEING DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-500A BELOW STR-8L AT PSU RAIL. INSTALLED FRAME REPAIR AT FSTA 500A BETWEEN STRINGER 8L AND STRINGER 9L IAW EA 1-A53-12114 REV 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

FRAME STRUCTURE STA 947 LBL 6 TO 8, FLANGE BELOW BULKHEAD CORRODED. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-440 BELOW STR-8L AT PSU RAIL. REPAIRED FRAME IN MAIN CABIN AT STA 440 BELOW STR 8L AT THE PSU RAIL WITH A RIVETED NESTED ANGLE REPAIR PER EA 1-A53-12114 REV 2. ALL WORK ACCOMPLISHED ON EA 1 A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

MAIN CABIN FRAME CRACKED AT STA-787 BELOW STR-8R AT PSU RAIL. REPAIRED MAIN CABIN FRAME AT STA 787 BELOW STRINGER 8L BY INSTALLING NESTED ANGLES IAW EA 1-A53-12114 REV 2.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

WEB SURFACE UNDER SCUFF PLATE HAS BARE METAL WITH SURFACE CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 43,557 hrs · 25,320 cycles

NR 1 LEFT GIRT BAR FLOOR MOUNT BRACKET HOLES CORRODED. REMOVED AND REPLACED MOUNT IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

FWD PASSENGER CABIN DOOR NR 1 LEFT FLOOR CRESE BEAM STA 332 LBL 58 HAS CORROSION. REMOVED AND REPLACED L-1 CREASE BEAM FROM STA 271 TO 360 IAW SRM 1-40-02 AND DWG

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

SEAT TRACK SUPPORT STRUCTURE CRACKED AT LEFT AND RIGHT SIDES BS 727B, BETWEEN RBL 22 TO 27. REMOVED AND REPLACED TRACK IAW SRM AND BOEING DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

PASSENGER CABIN STA 540, LBL 1, SEAT TRACK SUPPORT STRUCTURE IS CRACKED AT FASTENER ON LOWER SIDE. REMOVED & REPLACED SEAT TRACK STRUCTURE AT BS 540 LBL 1 IAW SRM 51-40-02 (EXPANSION JOINT).

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

RI DOOR THRESHOLD HAS SPOTS OF LIGHT CORROSION. REPAIRED PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

FWD PASSENGER CABIN FLOOR STRUCTURE AREA STA 344, LBL 45, INTERCOSTAL CRACKED. REPLACED CRACKED INTERCOSTAL FWD CABIN FLOOR WET AREA STA 344 LBL 45 IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

FWD CARGO COMPARTMENT STA 500C, LBL 25, INTERCOSTAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE WITH NEW AT STA 500C LBL 25 IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

SKIN CORRODED AT BS 500, BL 0. REPAIRED SKIN IAW SWA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

AFT PASSENGER CABIN AREA CORROSION AT STA 967, RBL 24 TOP CORD NUT PLATE HOLE. REPAIRED DAMAGED AREA AT STA 967 RBL 24 IAW SRM 53-00-51-2R-1 SRM 51-10-02 SRM 53-70-51-1A-1 SRM 51-40-02 SRM 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

AFT PASSENGER CABIN FLOOR STRUCTURE WET AREA STA 986.5 RBL 36 TO RBL 45 NUT PLATE HOLES HAS CORROSION. REPAIRED AFT CABIN STA 986.5 RBL 36 TO RBL 45 FLOORBEAM BY INSTALLING A "T" CAP SPLICE REPAIR IAW SRM 53-70-51-2R-4 AND EA 1-753-21388 REV

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

SUP: NUT PLATE HOLES CORRODED AT BS 986.5, BETWEEN RBL 36 TO RBL 45. REPAIRED SPLICE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

LOWER FUSELAGE FWD SIDE OF STA 663 RBL 19, BULKHEAD CRACKED AROUND PACK EXHAUST CUTOUT. WORK ACCOMPLISHED ON EA 1-A53-3376.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

NR 2 RIGHT STA 967 TO 986.5 CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,557 hrs · 25,320 cycles

LOWER FUSELAGE, FWD SIDE OF STA 663 RBL 27 ANGLE CRACKED JUST O/B OF PACK EXAUST DUCT OUTLET. REMOVED, FABBED AND INSTALLED ANGLE IN LOWER FUSELAGE FWD SIDE OF STA 663 RBL 27 PACK EXHAUST OUTLET IAW EA 130030 IR AND EA 1-753-21439.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,557 hrs · 25,320 cycles

LEFT WING NR 1 SLAT CRACKED ON LOWER SKIN AT ACTUATOR FITTING. REMOVED AND REPLACED SKIN IAW SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 43,557 hrs · 25,320 cycles

LEFT ELEVATOR TAB UPPER SURFACE AT NR 6 HINGE EXPOSED COMPOSITE. REMOVED AND REPLACED TAB IAW AMM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 43,557 hrs · 25,320 cycles

RIGHT ELEVATOR TAB TRAILING EDGE EXPOSED COMPOSITE. REMOVED AND REPLACED TAB IAW AMM.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 43,557 hrs · 25,320 cycles

LEFT HORIZ STAB, STAB STA 129.50, RIB VERTICAL STIFFENER CRACKED AFT OF FRONT SPAR. REPAIRED STIFFENER PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 43,213 hrs · 25,110 cycles

EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 43,213 hrs · 25,110 cycles

EEPLS COVER CRACKED BETWEEN ROW 14 TO ROW 21. REMOVED AND REPLACED COVER PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 41,173 hrs · 23,896 cycles

EMERGENCY LIGHT TRACK LENS BROKEN ROW 1. REPLACED EMERGENCY LIGHT LENS PER MM.

Part: RETAINER — LOOSE (L1 DOOR) · airframe 40,973 hrs · 23,782 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER LOOSE. SECURED RETAINER PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 40,973 hrs · 23,782 cycles

EMERGENCY LIGHT TRACK COVERS CRACKED AT ROWS 1 AND ROW 3. REMOVED AND REPLACED COVERS IAW M/M.

Part: RETAINER — LOOSE (R1 DOOR) · airframe 40,973 hrs · 23,782 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FORWARD RETAINER LOOSE. SECURED RETAINER PER SRM.

Part: LENS — MISSING (CABIN) · airframe 40,777 hrs · 23,675 cycles

EMERGENCY EXIT FLOOR LIGHT LENS MISSING AT ROW 11. INSTALLED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 39,947 hrs · 23,168 cycles

DURING SCHEDULED CV CHECK FOUND, LT AFT EEPLS COVER BROKEN AT ROW 14. REMOVED AND REPLACED COVER PER MM.

Part: CAP — MISSING (CABIN) · airframe 38,861 hrs · 22,541 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 38,861 hrs · 22,541 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 38,677 hrs · 22,434 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINTER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B END NR 5 SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN PUNCTURED. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 6.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 6.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,813 hrs · 21,398 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 36,555 hrs · 21,246 cycles

DURING SCHEDULED HC2 CHECK, FWD LT BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 36,555 hrs · 21,246 cycles

DURING SCHEDULED HC2 CHECK, AFT RT BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,430 hrs · 20,574 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,359 hrs · 20,527 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,359 hrs · 20,527 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 33,303 hrs · 19,287 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: COVER — CRACKED (CABIN) · airframe 33,198 hrs · 19,233 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 10 TO ROW 17. REMOVED AND REPLACED COVER PER MM.

Part: CAP — MISSING (CABIN) · airframe 32,061 hrs · 18,548 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS END CAP MISSING AT ROW 1. INSTALLED END CAP PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 31,873 hrs · 18,423 cycles

AFT EMERGENCY EXIT LIGHT COVER FELL OFF. RE-INSTALLED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,020 hrs · 17,293 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CAP — LOOSE (EMERGENCY LIGHT) · airframe 28,668 hrs · 16,481 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,450 hrs · 16,340 cycles

EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,357 hrs · 16,287 cycles

EEPL INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 28,357 hrs · 16,287 cycles

EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 26,124 hrs · 14,904 cycles

EEPLS COVER LOOSE AT ROW 11. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,116 hrs · 14,301 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLIGHT DECK EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,102 hrs · 14,294 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,009 hrs · 14,233 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,009 hrs · 14,233 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,009 hrs · 14,233 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 24,850 hrs · 14,138 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 24,194 hrs · 13,760 cycles

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

Part: ENGINE — FAILED (NR 2) · airframe 23,216 hrs · 13,186 cycles

IN FLT SHUT DOWN / DIVERSION / DECLARED EMERGENCY. NR 2 ENG FAILED, ENGINE SHUTTERED BANGED (FLAME OUT BACK) AND RED ARC LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,130 hrs · 13,139 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT 11 ABC. RELAMPED PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 22,683 hrs · 12,890 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS AT FWD CABIN INOP. REPAIRED BROKEN WIRE AT FWD CABIN PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 22,683 hrs · 12,890 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS AT MID CABIN INOP. REPAIRED BROKEN WIRE AT FWD CABIN PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 22,714 hrs · 12,912 cycles

EEPLS COVER LOOSE AT ROW 17 ABC. REMOVED AND REPLACED COVER PER MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 22,662 hrs · 12,877 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP BETWEEN ROW 11 ABC AND ROW 16 ABC. FOUND LIGHT ASSY WIRE BROKEN AT ROW 15 ABC. REPAIRED WIRE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 22,601 hrs · 12,839 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 22,601 hrs · 12,839 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 22,601 hrs · 12,839 cycles

DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,314 hrs · 12,655 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 22,218 hrs · 12,599 cycles

EEPLS COVER LOOSE AT ROW 2 ABC. SECURED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 21,319 hrs · 12,104 cycles

EEPLS LIGHT COVER LOOSE AT ROW 4 ABC. SECURED LIGHT COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 21,113 hrs · 11,985 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 2 DEF. REMOVED AND REPLACED EEPLS LIGHT COVER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 20,994 hrs · 11,914 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 19,784 hrs · 11,215 cycles

AFT ENTRY EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 19,678 hrs · 11,154 cycles

EEPLS TRACK COVER LOOSE. SECURED COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 19,279 hrs · 10,931 cycles

EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED COVER PER MM.

Part: MODULE — INOPERATIVE (EXTERIOR LIGHTS) · airframe 18,722 hrs · 10,636 cycles

FWD LEFT EXTERIOR EXIT LIGHT MODULE INOP. REMOVED & REPLACED LIGHT MODULE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,080 hrs · 9,680 cycles

DURING SCHEDULED MV3 CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 16,655 hrs · 9,420 cycles

R2 COCKPIT WINDOW ARCING WITH WINDOW HEAT SWITCH TURNED ON. REMOVED AND REPLACED R2 WINDOW & HEAT CONTROLLER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 16,219 hrs · 9,182 cycles

DURING SCHEDULED MV2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED AT ROWS 1 TO ROW 17. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 15,164 hrs · 8,586 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN RT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 15,164 hrs · 8,586 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,621 hrs · 8,249 cycles

FWD EEPLS FLOOR TRACK LOOSE. REMOVED AND REPLACED EEPLS LIGHT ASSEMBLY PER MM.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 14,610 hrs · 8,243 cycles

FWD EMERGENCY EXIT LIGHT AND WIRING LOOSE. SECURED LIGHT AND WIRING PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 14,441 hrs · 8,136 cycles

EEPLS COVER AT ROW 1 ABC, LOOSE. SECURED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 & L2 DOORS) · airframe 12,829 hrs · 7,271 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 & L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 & L2 DOOR EVAC SLIDES PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 9,191 hrs · 5,307 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS BROKEN AT ROWS NR 1, NR 17 AND NR 19. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: LIGHT — INOPERATIVE (ROW 2) · airframe 8,420 hrs · 4,873 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 2. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,429 hrs · 2,588 cycles

ONE EEPLS INOP. RELAMPED EEPLS PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 4,259 hrs · 2,496 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP LOOSE. SECURED SLIDE PER MM.

Part: WEB — CRACKED (MLG W/W'S) · airframe 4,025 hrs · 2,354 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT OTBD WEBS CRACKED IN BOTH LT AND RT MLG W/W, IN THE MID SECTION OF THE WEBS. REMOVED AND REPLACED WEBS PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 3,401 hrs · 1,994 cycles

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

Part: COVER — MISSING (CABIN) · airframe 3,327 hrs · 1,942 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS MISSING AT ROWS 1 AND 17. INSTALLED COVERS PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 3,055 hrs · 1,785 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BRACKET — BROKEN (AFT SVC DOOR) · airframe 1,478 hrs · 854 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH BROKEN. R&R AFT SVC DOOR GIRT BAR LATCH PER MM.