N784SW

Part: MEGAPHONE — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 71,211 hrs · 42,266 cycles

FA WRITE UP - FWD MEGAPHONE NEEDS BATTERY / [01] REMOVED AND REPLACED BATTERIES PER AMM SIP

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 71,041 hrs · 42,151 cycles

AFT A/C LEFT: EMERGENCY ESCAPE SLIDE HAS MANUAL PULL HANDLE EXPOSED / [01] ATTACHED PULLHANDLE COVER TO VELCRO PER SIP

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 69,904 hrs · 41,391 cycles

FWD ENTRY DOOR SLIDE PULLED OUT OF NORMAL / [01] SLIDE SKIRT DROOPING REFOLDED SLIDE SKIRT OK FOR SERVICE. SLIDE WAS NOT DEPLOYED IAW SIP

Part: COVER — LOOSE (L1 DOOR) · airframe 69,401 hrs · 41,038 cycles

SLIDE PULL HANDLE COVERS- FWD ENTRY & BOTH REAR DOORS NEED TO BE RESECURED / [01] RESECURED SLIDE PULL HANDLE COVERS ON FWD ENTRY AND BOTH DOORS PER SIP.;[02] RESECURED SLIDE PULL HANDLE COVERS ON FWD ENTRY AND BOTH REAR DOORS PER SIP.

Part: COVER — LOOSE (R/H CABIN) · airframe 69,338 hrs · 40,987 cycles

F/O OVER WING EXIT LIGHT FELL OFF / [01] RESECURE F/O OVERWING EXIT LIGHT COVER PER SIP

Part: LIGHT — LOOSE · airframe 69,140 hrs · 40,864 cycles

R/H OVERWING UPPER RIGHT EXIT/SALIDA SIGN COVER LOOSE. / [01] REPOSITION AND RE TIGHTEN SCREW ON R/H OVER WING UPPER RIGHT EXIT/SALIDA SIGN COVER; OPS CHECK GOOD REF AMM 33-51-01.

Part: LIGHT — INOPERATIVE · airframe 69,103 hrs · 40,843 cycles

LOWER EMERGENCY EXIT LIGHT INOP LOWER EMERGENCY EXIT LIGHT INOP (F/O) SIDE CENTER DOOR / [01] R&R LOWER EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01. OPS CHECK GOOD.

Part: NONE — NONE · airframe 69,093 hrs · 40,838 cycles

ON TAKEOFF ROLL TOWER OBSERVED FLAMES COMING OUT OF THE #2 ENGINE. ALL ENGINE PARAMETERS NORMAL. / [01] PERFORMED FIM TASK 71-05 TASK 811 WITH NO FAULTS FOUND. DETERMINED OIL PUDDLING IN OIL CENTER PLUG CAVITY CAUSED DUE TO BORESCOPE PRIOR TO FLIGHT AND DRY MOTOR OF ENGINE. CLEANED ALL RESIDUAL OIL. ENGINE WAS PREVIOUSLY SERVICED TO 99%. DRAINED TO 93%. PERFORMED ENGINE RUN WITH NO LEAKS.<BR>DRAINED ENGINE OIL TO 93%

Part: LIGHT — BROKEN · airframe 69,026 hrs · 40,793 cycles

AIRCRAFT RIGHT FO OVER WING FWD EXIT SIGN COVER BROKEN / [01] RESECURRED COVER PER SIP

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,617 hrs · 40,550 cycles

EMERGENCY LIGHT INOP AT OVERHEAD BIN SEAT 22 RH. ; EMERGENCY LIGHT INOP AT OVERHEAD IN SEAT 22 RH. / [01] RELAMPED EMERGENCY LIGHT AT OVERHEAD BIN SEAT 22 RH PERFORMED OPERATIONAL TEST; TEST OK AS PER REF B737 AMM 33-51-03-960-801; [02] VERIFIED

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: MAIN CABINE FLOOR SUPPORT CRACK AT STA.540 AND I/B OF SEAT TRACK RBL 24.75 ; / [01] LOCATED AND DRILLED NEW MAIN CABIN FLOOR SUPPORT PER B 737-700 SRM 51-40-05-0G-0; [02] VERIFIED 1.; [03] LATE ENTRY: REMOVED MAIN CABINE FLOOR SUPPORT BETWEEN STA.540 AND RBL 24.75 AS PER B737-700 SRM 51-40-02-0G-0; [04] OK TO INSTALL.; [05] INSTALLED FLOOR SUPPORT AS PER B737-700 SRM 51-40-02-0G-0; [06] VERIFIED ALL STEPS COMPLETED.

Part: ANGLE — CRACKED (FWD CARGO BAY) · airframe 68,617 hrs · 40,550 cycles

FWD CARGO BILGE BS500B AND S25R ANGLE CLIP CRACKED. ; / [01] REMOVED AND REPLACED CLIP AT STA 500B AND STR 25R PER SRM 51-40-02-0G-0; [02] VERIFIED 1

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 68,617 hrs · 40,550 cycles

FWD CARGO BILGE INTERCOSTAL CRACKED AT BS500B TO BS500C AND S25L. REMOVED INTERCOSTAL AT FWD CARGO BS 500B TO BS 500C IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED HOLES IAW SRM 51-40-05-0G-0. OK TO INSTALL INTERCOSTAL. INSTALLED INTERCOSTAL AT FWD CARGO IAW SRM 51-40-02-0G-0.

Part: CAP — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

AFT CARGO R/H CAP STRIPS WITH CORROSION ; / [01] RECIEVED NEW PARTS; [02] REMOVED DAMAGED AS PER B737-7 SRM 51-10-02-0G-0. CORROSION THROUGH MATERIAL FOUND OUT OF LIMITS; [03] FOR INSTALLATION REFERENCE TASK TTG8Q004ERCP; [04] VERIFIED STEPS 1; 2 AND 3

Part: CAP — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

AFT CARGO L/H CAP STRIPS WITH CORROSION ; / [01] ORDERED NEW PARTS; [02] REMOVED DAMAGED AS PER B737-7 SRM 51-10-02-0G-0. CORROSION THROUGH MATERIAL FOUND OUT OF LIMITS; [03] FOR INSTALLATION REFERENCE TASK TTG8Q004ERCP; [04] RECEIVED NEW CAP STRIPS 7EA TO REPLACE PARTS CORRODED REF SRM 51-10-02-0G-0; [05] VERIFIED STEPS 1; 2; 3 & 4.

Part: SUPPORT BEAM — ELONGATED (R/H WING) · airframe 68,617 hrs · 40,550 cycles

RIGHT WING ACCESS PANEL 651GB UPPER SUPPORT BEAN FASTENER HOLE ELONGATED ( MARKED) ; / [01] PERFORMED HFEC INSP. IAW B737 NDT<BR>PART 6; 51-00-00; PROCEDURE 23. NO CRACKS <BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/08/22; [22] REPAIR ACCOMPLISHED PER EA-22-157-00011; [23] JOB IS COMPLETE

Part: SHIELD — CRACKED (FWD CARGO) · airframe 68,617 hrs · 40,550 cycles

FWD CARGO AFT SHIELD IS CRACK ; / [01] RECEIVED NEW SHIELD LOCATED AND DRILL HOLES NEW SHIELD INSTALLED NUTPLATES AS PER SRM 51-40-05 AND 51-40-02; [02] VERIFIED 1

Part: SKIN — DELAMINATED (LT NR 6 SPOILER) · airframe 68,617 hrs · 40,550 cycles

L/H WING SPOILER #6 HAS A DELAMINATED DENT LOCATED AT 9.75' FROM I/B EDGE AND 6.5' FROM AFT EDGE MEASURES L=0.5';W=O.5';Y=0.004';W/Y=125 ; / [01] PREPARED THE DAMAGED AREA TO EXAMINE THE DAMAGE IN THE REPAIR AREA. REF B737-700 SRM 57-70-01-2R-2 AND SRM 51-70-10-2R-0 PARAGRAPH 6.; [02] PERFORMED HFEC INSP ON DAMAGE AREA. IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166316. CRACK INDICATION FOUND.; [03] PERFORMED CUT OUT OF 0.750'' DIAMETER AND PREPARED AREA TO APPLY REPAIR AT L/H WING SPOILER #6 LOCATED AT 9.75'' FROM I/B EDGE AND 6.5'' FROM AFT EDGE. REF B737-700 SRM 57-70-01-2R-2 AND B737-700 SRM 51-70-10-2R-2 PARAGRAPH 4 D.; [04] FABRICATED FILLER (0.750'' DIAMETER) AND DOUBLER (3'' DIAMETER) B737-700 SRM 51-70-10-2R-2 PARAGRAPH 4 D AND B737-700 SRM 51-70-10-2R-0 PARAGRAPH 8. APPLIED BOEGEL AC 130 AND ADHESIVE PRIMER BMS 5-137 REPAIR PARTS REF B737-700 SRM 51-70-10-2R-2 PARAGRAPH 4 D AND B737-700 SRM 51-70-10-2R-0 PARAGRAPH 14 AND 15.; [05] PERFORMED DRY OUT FOR 1 HOUR AT REPAIR AREA; NO CORE DAMAGED. REF B737-700 SRM 51-70-10-2R-2 PARAGRAPH 4 D AND B737-700 SRM 51-70-10-2R-0 PARAGRAPH 7 A (3); 08] INSTALLED REPAIR PARTS AT DAMAGED AREA . REF B737-700 SRM 51-70-10-2R-2 AND B737-700 SRM 51-70-10-2R-0 PARAGRAPH 18 AND 20.; [09] VERIFIED 8; [10] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AROUND THE REPAIR AREA; NO DELAMINATION FOUND; NO DAMAGED NOTE. REF B737-700 NDT PART 1 51-05-01 PARAGRAPH 5 TAP TEST TOOL USED ST8842.;

Part: RIB — CRACKED (VERT. STAB.) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: VERTICAL DORSAL FIN FWD RIB CRACKED ; / [01] REMOVED AND REPLACED VERTICAL DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 174A0103; [02] VERIFIED STEP 1

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: R/H STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.50 STIFFENER NO.4 CRACKED ; / [01] TRIMMED OUT DAMAGED AREA ON RH STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.5 STIFFENER 4 AS PER B737-700 SRM 55-10-09-2R-4; [06] FABRICATED REPAIR PARTS (SHIM; FILLER AND ANGLE (BAC1490-2793)) AS PER B737-700 SRM 55-10-09-2R-5. FIG 204.; [15] INSTALLED REPAIR PARTS (SHIM; FILLERS; ANGLE (BAC1490-2793) AND REPAIR STIFFENER) AS PER B737-700 SRM 51-40-02-0G-0 AND 55-10-09-2R-5. FIG 204.; [16] VERIFIED STEP 15; [17] APPLIED FILLET SEALANT ON REPAIR EDGES AS PER SOPM 20-50-19; [18] TRIMMED OUT DAMAGED AREA ON RH STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.5 STIFFENER 4 AS PER B737-700 SRM 55-10-09-2R-5. PERFORMED HFEC INSP; NO CRACKS. PERFORMED A FASTENER HOLE INSPECTION (ROTARY SCANNER); NO CRACKS. ACCOMPLISHED A GVI OF ALL AREAS WITHIN THE REPAIR AREA. NO OTHER DEFECTS NOTE. FABRICATED REPAIR PARTS (SHIM; FILLERS; ANGLE (BAC1490-2793) AND REPAIR STIFFENER) AS PER B737-700 SRM 55-10-09-2R-5. FIG 204. TREATED AND PRIMED REWORKED AREAS AND REPAIR PARTS AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804. INSTALLED REPAIR PARTS (SHIM; FILLERS; ANGLE (BAC1490-2793) AND REPAIR STIFFENER) AS PER B737-700 SRM 51-40-02-0G-0 AND 55-10-09-2R-5. FIG 204.;

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: PAX CABIN FLOOR PANEL 222AF AFT O/B CORNER DELAMINATED ; / [01] MEASUREMENTS; [02] PREPARED DAMAGED AREA FOR REPAIR AT CABIN FLOOR PANEL 222AF PER B737 SRM 53-00-50-2R-0; [03] VERIFIED STEPS 1 AND 2.; [04] REPAIRED DAMAGED AREA AT CABIN FLOOR PANEL 222AF PER B737<BR>SRM 53-00-50-2R-0 MATERIAL USED RESIN 50-A PO#1714421; [05] VERIFIED REPAIR; [06] LATE ENTRY: RII<BR>RII OK TO INSTALL REPAIR.<BR>RII VERIFIED REPAIR.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

PAX CABIN FLOOR PANEL 221BF AFT O/B CORNER CRACKED ; / [01] PREPARED DAMAGED AREA AT FLOOR PANEL 221BF PER B737 SRN<BR>53-00-50-2R-0; [02] REPAIRED DAMAGED AREA AT FLOOR PANEL #221BF PER B737<BR>53-00-50-2R-0 MATERIAL USED RESIN 50-A PO# 1714421; [03] VERIFIED STEP # 1 AND # 2

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

PAX CABIN FLOOR PANEL 221GF UPPER LAMINATE WITH SOME DELAMINATION ; / [01] RECEIVED FLOOR PANEL 221GF P/N:141A5810-181 REF. TASK CARD TTG8Q006QHXA FOR PANEL INSTALLATION; [02] VERIFIED STEP 1

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR ANGLE AT STA 540 LBL 64 IS CRACK (228-007) ; CAIN FLOOR ANGLE AT STA 540 LBL 64 IS CRACK (228-007) / [01] INSTALLED PARCIAL PROTECTION OF THE EWIS IN THE AREA AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 AMM 20-60--07-913-801; [02] REMOVED FLOOR ANGLE CRACK AT MAIN CABIN STA. 540 LBL 64' IAW B737-700 SRM 51-40-02-0G-0; [03] PARTIAL LOCATED AND DRILLED HOLES AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 SRM 51-40-05-0G-0 AND 51-40-02-0G-0; [04] COMPLETED LOCATED AND DILLED HOLES AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0; [06] OK TO ALODINE AND PRIME NEW ANGLE; [07] APPLIED ALODINE AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 SRM 51-20-01-0G-0; [08] APPLIED PRIMER AT CABIN FLOOR ANGLE SAT 540 LBL 64'' AS PER B737-700 AMM 51-21-72-370-801; [09] VERIFIED STEPS 7 AND 8; OK TO INSTALL NEW ANGLE; [10] COMPLETED INSTALLED FASTENERS AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 SRM 51-40-02-0G-0; [11] REMOVED IWIS PROTECTION AND CLEANED AREA AT CABIN FLOOR STA. 540 LBL. 64' IAW B737-700 AMM 20-60-07-913-801; [12] COMPLETED INSTALLED AT MAIN CABIN FLOOR SUPPORT ANGLE STA.540 LBL 64' WAS ACCOMPLISHED IAW B737-700 SRM 5W-40-02-0G-0 AND DWG.# 144A5901; [13] INSTALLED( COMPLETE) PROTECTION OF THE EWIS IN THE AREA AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 AMM 20-60--07-913-801; [15] VERIFIED CORRECTION STEP 13

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 68,617 hrs · 40,550 cycles

CABIN FLOORBEAM AT BS 986.5, RBL 30, AND RBL 34 HAS SURFACE CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4 51-00-00 PROCEDURE 3. PERFORMED A HFEC INSPECTION IAW NDT PART 06 51-00-00 PROC 23, NO CRACKS. PERFORMED A OPEN HOLE HFEC INSPECTION IAW NDT PART 06 51-00-00 PROC 16, NO CRACKS. REPAIR ACCOMPLISHED IAW ADD-M-21-153-00612, REPAIR ACCOMPLISHED TTG8Q009K1WR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

AFT CARGO, BS 727 TO 847 LBL 21, S25L SIDEPLATE SUPPORT ZEE CORROUDED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. REMOVED CORROSION ON LT Z-CHANNEL BS 727-847 LBL 21 IAW SRM 51-10-02-0G-0. REMOVED THREE NUTPLATES AND ONE FASTENER TO REMOVE CORROSION ON LT Z-CHANNEL IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

CABIN FLOOR BEAM AT STA 986.5 LBL 32 AND LBL 35 HAS SURFACE CORROSION ON THE UPPER AND LOWER SURFACES OF THE FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02-0G-0. NDT PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS 0.124'. PERFORMED A HFEC INSPECTION IAW NDT PART 06 51-00-00 PROC 23 NO CRACKS. PERFORMED A OPEN HOLE HFEC INSPECTION IAW NDT PART 06 51-00-00 PROC 23, NO CRACKS.. ROUGHNESS TEST DONE MATERIAL LOSS .026', FOUND OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIG 103 DETAIL C. REPAIR ACCOMPLISHED PER ADD-M-21-153-00612 REPAIR FUSELAGE B-S 986.5.

Part: TRACK — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

CABIN L/H SEAT TRACK I/B TRACK AT ABOUT STA 500A +6' WITH CORROSION. REMOVED LIGHT CORROSION AT CABIN L/H SEAT TRACK I/B TRACK STA 500A +6' CORRECTION TO STEP 1: REMOVED LIGHT CORROSION AT CABIN L/H SEAT TRACK I/B TRACK STA 500A +6' AS PER B737-700 SRM 51-10-02-0G-0 VERIFIED STEP 2. MAXIMUM CLEANUP DEPTH 0.012'. FOUND WITHIN LIMITS AS PER B737-700 SRM 53-00-52-1A-1. TOOL ID: 410019 DUE DATE: 4/13/2022 VERIFIED STEP 4. OK TO TREAT AND PRIME. TREATED AND PRIMED REWORKED AREA AS PER B737-700 SRM 53-00-52-1A-1 VERIFIED STEP#6

Part: TRACK — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

CABIN L/H SEAT TRACK O/B TRACK AT ABOUT STA 559+14' WITH CORROSION. REMOVED CORROSION ON SEAT TRACK STA 559B+14' LBL 45 AS PER B737-700 SRM 51-10-02-0G-0 VERIFIED STEP 1. MAXIMUM CLEANUP DEPTH 0.014'. FOUND WITHIN LIMITS AS PER B737-700 SRM 53-00-52-1A-1. TOOL ID: 410019 DUE DATE: 4/13/2022 VERIFIED STEP 3. OK TO TREAT AND PRIME. TRATED AND PRIMED REWORKED AREA AS PER B737-700 SRM 53-00-52-1A-1. VERIFIED STEP#5

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

CABIN L/H SEAT TRACK AT ABOUT STA 500D +14' WITH CORROSION. FAULT FOUND AT OB TRACK. REMOVED SURFACE CORROSION ON L/H I/B TRACK STA 500D+14 PER B737-700 SRM 51-10-02-0G-0 VERIFIED 1 ORIGINAL MMATERIAL 0.230' MATERIAL LOSS 0.011' AND MATERIAL REMAINING 0.219' FOUND TO BE IN LIMITS PER SRM 53-00-52-1A-1 STEP 4 NOTE(C) FIGURE 103 DETAIL E. TOOL USED DEPTH GAUGE ID#WN0006 CAL DUE:5/17/2022 VERIFIED STEP # 3. OK TO TREAT AND PRIME. TREATED AND PRIMED AREA PER B737-700 SRM 51-20-01-0G-0 AND SOPM 20-41-04 VERIFIED 6.

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

POSSIBLE CRACK AT CABIN R-1 DOOR FUSELAGE CUTOUT FWD EDGE BETWEEN S-8R AND S-9R. REMOVED SEALANT TO GAIN ACCESS FOR NDT INSPECTIONS TO CHECK FOR CRACK REF SRM 51-31-00-100-801. PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23.CRACK CONFIRMED. CRACK LENGTH : 1.339'. REMOVED UPPER STUB FRAME AT R1 DOOR CUT OUT IAW SRM 51-40-02-0G-0. LOCATED & DRILL NEW STUB FRAME IAW SRM 51-40-05-0G-0. TREATED & PRIMER HOLES STUB FRAME IAW SRM 51-20-01-0G-0 & AMM 51-21-72--370-804. TOP COAT STUB FRAME IAW AMM 51-21-73. INSTALLED NEW STUB FRAME AT CABIN R-1 DOOR FUSELAGE CUT OUT IAW SRM 51-40-02-0G-0 & DWG 141A8370.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

FLOOR PANEL 241DF UPPER SURFACE DELAMINATED ; / [01] RECEIVED NEW FLOOR PANEL 241DF P/N 144A5810-128 P/O:1728471 REF. TASK CARD TTG8Q006QHHG FOR PANEL INSTALLATION; [02] VERIFIED STEP 1

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

FLOOR PANEL 241DF UPPER SURFACE DELAMINATED ; / [01] RECEIVED NEW FLOOR PANEL 241DF P/N 144A5810-128 P/O:1728471 REF. TASK CARD TTG8Q006QHHG FOR PANEL INSTALLATION; [02] VERIFIED STEP 1

Part: FITTING — CRACKED (L/H WING) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: L/H WING T/E AT LWR DEFLECTOR RIB SEAL BRACKET INNER SIDE CRACKED ; / [01] REMOVED LWR DEFLECTOR RIB; FITTING AND SEAL; L/H WING T/E LOWER DEFLECTOR RIB REF B737-700 SRM 51-40-02-OG-0.. LOCATED AND DRILLED NEW FITTING PER. REF.B737-700 SRM 51-40-05-OG-0; [02] . VERIFIED STEP 1 . OK TO INSTALL NEW FITTING AND NEW SEAL; [03] INSTALLED SEAL AND FITTING; L/H WING T/E LOWER DEFLECTOR RIB PER. REF B-737-700 SRM 51-40-02-OG-0; [04] VERIFIED 3

Part: FITTING — CRACKED (L/H WING) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: L/H WING T/E AT LWR DEFLECTOR RIB SEAL BRACKET INNER SIDE CRACKED ; / [01] REMOVED LWR DEFLECTOR RIB; FITTING AND SEAL; L/H WING T/E LOWER DEFLECTOR RIB REF B737-700 SRM 51-40-02-OG-0.. LOCATED AND DRILLED NEW FITTING PER. REF.B737-700 SRM 51-40-05-OG-0; [02] . VERIFIED STEP 1 . OK TO INSTALL NEW FITTING AND NEW SEAL; [03] INSTALLED SEAL AND FITTING; L/H WING T/E LOWER DEFLECTOR RIB PER. REF B-737-700 SRM 51-40-02-OG-0; [04] VERIFIED 3

Part: FLOOR PANEL — DETERIORATED (FUSELAGE) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT;FLOOR PANEL 140AF IS DETERIORATED ; / [01] FABRICATED AFT CARGO FLOOR PANEL 140AF AS PER B737-700 AMM 25-52-01-201-801; [02] STEP 1 VERIFIED

Part: RETAINER CUP — OUT OF TOLERANCE (L1 DOOR) · airframe 68,617 hrs · 40,550 cycles

L1 DOOR EMERGENCY ESCAPE SYSTEM; RETAINER CLIPS (BOTH); MEASUREMENTS OUT OF LIMITS ; / [01] REMOVED AND REPLACED BOTH FLOOR-MOUNTED ESCAPE SLIDE BRACKET/CLIP ON THE L1 ENTRANCE FLOOR IN REF. TO B737 AMM 25-66-02-000-801; 25-66-02-400-801. PENDING INSTALLATION TEST; [02] ACCOMPLISHED L-1 DOOR EMERGENCY ESCAPE SLIDE PACK GIRT BAR RETAINER CLIPS CHECK. ALL MEASUREMENTS AT GIRT BARS RETAINING CLIPS ARE WITHIN LIMITS IN REF WITH B737-7 AMM 25-66-01-200-802.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: FOUND EMERGENCY LIGHT POWER SUPPLY M1673 INOP ;(AFT GALLEY CEILING). ; / [01] REMOVED AND REPLACED BATTERY PACK AT AFT GALLEY CEILING PANEL M1693 POSITION.; [02] PERFORMED OPS OF BATTERY PACK M1693 CHECK FOUND PASS AS PER B737 AMM 33-51-06-960-006; [03] VERIFIED 1 AND 2. <BR>SERIAL NUMBER BATTERY PACK M1693: 32185

Part: NONE — OUT OF TOLERANCE (L2 DOOR) · airframe 68,617 hrs · 40,550 cycles

SUPPLEMENTAL INFORMATION: L2 DOOR EMERGENCY ESCAPE SYSTEM; RETAINER CLIPS (BOTH); MEASUREMENTS OUT OF LIMITS ; / [01] DUPLICATE. REF TASK CARD# TTG8Q009B258.; [02] VERIFIED

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 68,144 hrs · 40,255 cycles

R1 DOOR SLIDE DISLODGED. / RESECURED SLIDE PER AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER W/O SSR1208.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER WO SSR1207.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG INBOARD FACE HAD CORROSION. REPAIRED FACE PER W/O SSR1208.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER W/O SSR1208.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER WO SSR1207.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED PER WO SSR1207.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INBOARD FACE HAD CORROSION. REPAIRED FACE PER W/O SSR1208.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER W/O SSR1208.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG INBOARD FACE HAD CORROSION. REPAIRED FACE PER WO SSR1207.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INBOARD FACE HAD CORROSION. REPAIRED FACE PER WO 1207.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER WO SSR1207.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,117 hrs · 40,234 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER W/O SSR1208.

Part: PANEL — DELAMINATED · airframe 67,711 hrs · 39,967 cycles

193B PANEL HAS DELAMINATION AND ELONGATED FASTENER HOLES. / REPLACED PANEL 193B PER EO #14108 AND SRM 51-40-02

Part: FLAP — CRACKED (R/H WING) · airframe 67,604 hrs · 39,903 cycles

RH INBD AFT FLAP HAS DENT WITH CRACK IN CENTER. LENGTH .653 WIDTH .623 DEPTH .055. APPROX 21' FROM INBD EDGE; 6' FROM TE / R&R I/B AFT FLAP AS PER M/M 27-51-12 POS RH PN OFF 113A2700-2 SN OFF 00014 PN ON 113A2700-22 SN ON D-1400

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 66,770 hrs · 39,372 cycles

FORWARD CARGO BAY CENTER BULL NOSE SCUFF PLATE IS CRACKED. / REMOVED AND REPLACED PER AMM 53-11-02.

Part: BATTERY — FAILED (CABIN) · airframe 65,681 hrs · 38,673 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 65,681 hrs · 38,673 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 65,681 hrs · 38,673 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 65,681 hrs · 38,673 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER MM.

Part: RIVET — LOOSE (R1 DOOR) · airframe 64,543 hrs · 37,957 cycles

R1 DOOR EMERGENCY SLIDE GIRT BAR BRACKET LOOSE. R&R RIVET IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 64,368 hrs · 37,836 cycles

CENTER OVERWING EXIT SIGN BROKEN. R&R SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,449 hrs · 37,224 cycles

R2 DOOR SLIDE PRESSURE GAUGE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FITTING — MISSING (L1 DOOR) · airframe 63,351 hrs · 37,158 cycles

L1 DOORWAY FORWARD GIRT BAR BRACKET FITTING MISSING. INSTALLED FITTING PER DWG AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FUSELAGE LAP LOWER SKIN CRACKED BETWEEN BS 749.5 TO BS 751.5, STR 14R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

(QC) EXTERNAL SKIN BULGE BELOW STR 14R LAP BETWEEN BS 767 AND BS 787. / REPAIRED PER: ER 18-03879 REV IR AND SWA EA 1-753-33180 REV 1

Part: PANEL — DELAMINATED (RT WING) · airframe 63,351 hrs · 37,158 cycles

RIGHT WING L/E PANEL 621NB DELAMINATED AT I/B AFT CORNER / REPAIRED DELAMINATION AT I/B AFT CORNER OF RIGHT WING L/E PANEL 621NB IAW SRM 57-41-01-2R-6.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FLOOR SUPPORT CRACKED AT BS 663, BETWEEN LBL 45 TO LBL 50. R&R SUPPORT PER SRM AND DWG.

Part: INTERCOSTAL — ELONGATED (FWD CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

FWD CARGO BAY INTERCOSTAL CLIP HAS OBLONG HOLES BS500B; LBL24 FWD SIDE OF FRAME. / REMOVED AND INSTALLED NEW FCB INTERCOSTAL CLIP ON FWD SIDE OF BS 500B LBL 24 PER DWG 143A7505; AND SRM 51-40-02 87713U 08AUG18

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,351 hrs · 37,158 cycles

VAPOR BARRIER LOWER STIFFENER CRACKED AT BS 663, RBL 27. R&R STIFFENER PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

ANGLE CRACKED BETWEEN BS 291 TO BS 294, RBL 52. R&R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 63,351 hrs · 37,158 cycles

STIFFENER AT BS 663 LOWER LEFT MWW LBL27 CRACKED / REMOVED AND REPLACED STIFFENER AT B.S. 663 LBL 27 7531206/NEW PER SRM 51-40-02-0G-0 AND DWG 111A1000

Part: INTERCOSTAL — ELONGATED (FWD CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

FWD CARGO BAY INTERCOSTAL HAS OBLONG HOLES BS500B-500C; LBL25. / REMOVED AND INSTALLED NEW FCB INTERCOSTAL AT BS 500B-500C LBL 25 PER DWG 143A7505 AND SRM 51-40-02-0G-0 87713U 08AUG18

Part: INTERCOSTAL — ELONGATED (FWD CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

FWD CARGO BAY INTERCOSTAL HAS OBLONG HOLES BS500C-500D; LBL25. / REMOVED AND INSTALLED NEW FCB INTERCOSTAL BS 500C-500D LBL 25 PER DWG 143A7505 AND SRM 51-40-02 87713U 08AUG18

Part: INTERCOSTAL — ELONGATED (FWD CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

FWD CARGO BAY INTERCOSTAL HAS OBLONG HOLES BS500A-500B; LBL25. / REMOVED AND INSTALLED NEW FCB INTERCOSTAL BS 500A-500B LBL 25 PER DWG 143A7505; AND SRM 51-40-02 87713U 08AUG18

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 63,351 hrs · 37,158 cycles

RT WHEEL WELL VAPOR BARRIER BULKHEAD CRACKED AT BS 663, RBL 25. REPAIRED BULKHEAD IAW SRM.

Part: RADOME — DEBONDED (FWD FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

ROW 44 RADOME AFT STIFFENER DISBONDED 6' AT FASTENER / REPAIRED STIFFENER ON RADOME PER SAINT GOBAIN SRM 5214 STEP 4.E.2; REMOVED AND REINSTALLED RADOME PER AMM SUPPLEMENT 23-36-12.

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 63,351 hrs · 37,158 cycles

DOUBLER CRACKED ON VAPOR BARRIER AT BS663 RBL 22 WL 142 / REMOVED AND REPLACED VAPOR BARRIER DOUBLER 7570349/NEW AT B.S. 663 RBL 22 LL142 PER SRM 51-40-02-0G-0 AND IPC 57-11-00-02

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,351 hrs · 37,158 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3 3RD VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

R2 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS 967 TO BS 986, RBL 52. R&R MOPSILL PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

L1 DOOR THRESHOLD ANGLE CORRODED BETWEEN BS 312 TO BS 328, LBL 52. R&R ANGLE IAW DWG & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,351 hrs · 37,158 cycles

FLOOR PANEL 222DF 3 OF 4 CORNERS ARE DELAMINATED. (MARKED) / FLOOR PANEL 222DF DELAMINATED CORNERS WERE REPAIRED IAW SRM 53-00-50-2R-10. 56144U 07/31/2018.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

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

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

WHILE WORKING CUSTOMER CARD # 7447124 FOUND DENT AT BS 380 BETWEEN STR 16L AND 17L TO BE OUT OF LIMITS PER THE SRM REQUIRES REPAIR / REPAIRED SKIN DENT AT BS 380 STR 16L - 17L PER ER 18-03571 REV IR AND EA 1-753-33114 REV IR.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD MOPSILL ATTACH ANGLE CORRODED BETWEEN BS 314 TO BS 320, RBL 53. R&R ANGLE IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 22. R&R SUPPORT PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 490, RBL 28. R&R WEB PER SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY LT FLOOR RAIL CORRODED AT BS 767+4, LBL 12. R&R RAIL PER SRM AND EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 792 TO BS 847. R&R WEB PER DWG & SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY SUB THRESHOLD STRAP CORRODED BETWEEN BS 792 TO BS 847, RBL 22. R&R STRAP PER SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS 787 TO BS 807, RBL 6. R&R WEB IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 460 TO BS 480, LBL 25. R&R INTERCOSTAL PER SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY FRAME TO INTERCOSTAL CLIP CRACKED AT BS 500C, STR 26L. R&R CLIP PER DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY FLOOR TO BULKHEAD SUPPORT CORRODED AT BS 947. R&R SUPPORT ANGLE PER SRM & DWG.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 63,351 hrs · 37,158 cycles

PANEL 193AR INNER SKIN IS DISBONDED NEAR I/B EDGE. (MARKED) / PANEL 193AR INNER SKIN DISBOND NEAR I/B EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2 56144U. 08/01/2018.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 25. R&R WEB PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 847, RBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947, RBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS 807 TO BS 827, RBL 6. R&R WEB IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY FLOOR TRACK INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, RBL 15. R&R INTERCOSTAL PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500B, RBL 25. R&R SUPPORT IAW DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY RT FLOOR RAIL CORRODED AT BS 767+4, RBL 8. R&R RAIL PER SRM AND EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY LT FLOOR RAIL CORRODED AT BS 767+4, LBL 8. R&R RAIL PER SRM AND EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 792 TO BS 847, RBL 13. R&R FLOOR TRACK ASSEMBLY IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

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

Part: WEB — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 6. R&R WEB IAW DWG AND SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY RT SHIELD CORRODED BETWEEN BS 767 TO BS 792, RBL 25. R&R SHIELD PER SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY LT FLOOR RAIL CORRODED AT BS 767+4, LBL 3. R&R RAIL PER SRM AND EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY RT FLOOR RAIL CORRODED AT BS 767+4, RBL 3. R&R RAIL PER SRM AND EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 420, RBL 25. R&R SIDE PLATE PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 396 TO BS 500D, LBL 25. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY FLOOR TO BULKHEAD CORRODED AT BS 500D, BETWEEN LBL 25 TO RBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,351 hrs · 37,158 cycles

ACB FLOOR STRAP BS 887 RBL 20 TO LBL 11 HAS CORROSION / NO ESTABLISHED LIMITS IN SRM FOR CORROSION ON ACB FLOOR STRAP AT BS 887. REMOVED AND REPLACED ACB FLOOR STRAP AT BS 887 WITH NEW FLOOR STRAP ASSEMBLY- SI# 7530863 PER SRM 51-10-02 STEP 9.C.; SRM 51-40-02; SRM 51-40-05 AND AIPC 53-42-11-30. 57546U 09AUG18

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,351 hrs · 37,158 cycles

ACB ACB FLOOR STRAP BS 727D+4 RBL 22 TO LBL 22 HAS CORROSION / ACB FLOOR STRAP BS 727D+4 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN FOR IT IN THE SRM. RECEIVED NEW STRAP FOR TRACKING ONLY

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,351 hrs · 37,158 cycles

ACB ACB FLOOR STRAP BS 767D+4 RBL 22 TO LBL 22 HAS CORROSION / ACB FLOOR STRAP BS 767+4 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN FOR IT IN THE SRM. RECEIVED NEW STRAP FOR TRACKING ONLY

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT CORRODED AT BS 500, LBL 25. R&R SUPPORT PER SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY LT FLOOR TRACK CORRODED AT BS 767+4, LBL 17.24. REPAIRED FLOOR TRACK PER EA.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 63,351 hrs · 37,158 cycles

FCB SHIELD BS 492 TO 500A RBL 25 HAS CORROSION / REPLACED FCB SHIELD B.S. 492-500A RBL 25 AND NO ALLOWABLE LIMITS - REPAIR BY REPLACEMENT PER SRM 51-10-02 STEP 9(C); 51-40-02 AND DWG. 143A0080.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 63,351 hrs · 37,158 cycles

FCB SHIELD BS 420 TO 440 RBL 25 HAS CORROSION FASTENER NOT INSTALLED PER SRM; STA 420 + 9 IN; THROUGH VERTICAL TAB; RBL 25. / REPLACED FCB SHIELD B.S. 420-440 RBL 25 PER SRM 51-40-02 AND DWG # 143A0080. NO ALLOWABLE LIMITS GIVEN IN SRM - REPAIRABLE BY REPLACEMENT PER SRM 51-10-02.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 25. R&R INTERCOSTAL PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 20. R&R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 767, RBL 25. R&R SUPPORT PER DWG & SRM.

Part: FLAP — DELAMINATED (RH OUTBD AFT FLA) · airframe 63,351 hrs · 37,158 cycles

RT WING O/B AFT FLAP I/B END AT T/E IS DISBANDED. / RIGHT WING O/B AFT FLAP I/B END DELAMINATION WAS REPAIRED ON ATS WORK ORDER 508604. FLAP WAS REMOVED AND REINSTALLED ON AIRCRAFT ON CARD # T822371

Part: PANEL — BROKEN (LOWER EXT FUSELA) · airframe 63,351 hrs · 37,158 cycles

FAIRING PANEL 195AR HAS A PIECE BROKEN OFF AFT END MARKED / REPAIRED DAMAGE TO FAIRING PANEL 195AR IAW SRM 51-70-05-2R-6. 56749U 30JUL18

Part: RETAINER — CRACKED (LEFT WING) · airframe 63,351 hrs · 37,158 cycles

LT WING T/E UPPER PANEL JUST AFT IF #1 ENGINE VERT SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED THE LT WING T/E UPPER PANEL; JUST AFT OF #1 ENGINE; VERTICAL SEAL RETAINER IAW SRM 51-40-02-0G-0 AND SOPM 20-50-01.

Part: FLAP — DELAMINATED (LH OUTBD AFT FLA) · airframe 63,351 hrs · 37,158 cycles

LT WING O/B AFT FLAP I/B LWR END T/E IS DISBANDED. / LT WING O/B AFT FLAP WAS REPLACED AND NEW UNIT WAS INSTALLED ON A/C ON CARD # T822335

Part: ANGLE — CRACKED (RT MLG WW) · airframe 63,351 hrs · 37,158 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE PER ER AND EA.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 63,351 hrs · 37,158 cycles

FORWARD SIDE OF BULKHEAD LOWER WEB CRACKED AT BS 663, LBL 16. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,351 hrs · 37,158 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 672, LBL 37. REPAIRED DECK IAW EA.

Part: SUPPORT — CRACKED (LT MLG WW) · airframe 63,351 hrs · 37,158 cycles

LT MAIN LANDING GEAR WHEEL WELL RAM AIR EXHAUST CUTOUT SUPPORT CRACKED AT BS 663, LBL 21. R&R CUTOUT IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,351 hrs · 37,158 cycles

RT MAIN LANDING GEAR WHEEL WELL WEB CRACKED AT BS 663, BETWEEN RBL 9 TO RBL 14. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,351 hrs · 37,158 cycles

LT WING NR 2 SLAT LOWER SURFACE LEADING EDGE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 63,262 hrs · 37,102 cycles

FWD. CARGO ALUNINUM FLOOR PANEL HAS 1/2' CRACK 2.5' FROM R/H SIDE & 34' FROM AFT EDGE. / CLOSING # 84852 PERFORMED INTERIUM REPAIR REF SRM 53-00-53-1A-1 SEE LOG PAGE #0778668 INSPECT 400 CYCLES REINSPECT EVERY 400 CYCLES PERMANENT REPAIR 4000 CYCLES

Part: GLOWSTRIP — WORN (CABIN) · airframe 62,879 hrs · 36,847 cycles

RT CABIN PHOTO LUMINESCENT STRIP WORN AT ROW 1. R&R PHOTO LUMINESCENT STRIP PER SIP.

Part: STRAP — LOOSE (L1 DOOR) · airframe 62,582 hrs · 36,671 cycles

L1 EMERGENCY EXIT DOOR ASSIST STRAP COVER LOOSE. SECURED THE STRAP IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 61,869 hrs · 36,230 cycles

CENTER AISLE EMERGENCY EXIT SIGN BROKEN FROM CEILING MOUNT. R&R SIGN PER MM.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 60,567 hrs · 35,373 cycles

RT OVERWING EMERGENCY EXIT CLOSING STRAP COVER LOOSE. R&R VELCRO PER MM.

Part: LIGHT — UNSECURE (CABIN) · airframe 60,315 hrs · 35,219 cycles

R1 DOOR EMERGENCY EXIT PLACARD FELL OFF. R&R LIGHT ASSEMBLY PER MM.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 602,214 hrs · 35,167 cycles

L1 DOOR SLIDE GIRT BAR LOOSE. INSTALLED THE BRACKET IAW SRM AND MT.

Part: BATTERY — FAILED (CABIN) · airframe 57,879 hrs · 33,774 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 57,879 hrs · 33,774 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 57,879 hrs · 33,774 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1670. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 57,879 hrs · 33,774 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R&R BATTERY PER AMM.

Part: SIGN — LOOSE (R2 DOOR) · airframe 56,960 hrs · 33,228 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 56,624 hrs · 33,031 cycles

RIGHT WING NR 7 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (EXT POWER DOOR) · airframe 56,624 hrs · 33,031 cycles

EXTERNAL POWER DOOR SKIN CUTOUT DOUBLER CRACKED IN THE AFT LOWER CORNER. REPAIRED THE SKIN IAW ER AND EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 56,624 hrs · 33,031 cycles

RIGHT MLG WHEEL WELL PRESSURE DECK CRACKED AT BS 663, RBL 41. REPAIRED THE PRESSURE DECK IAW ER AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,375 hrs · 32,882 cycles

RIGHT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,423 hrs · 32,333 cycles

LEFT WING NR 1 OTBD AFT FLAP DELAMINATED AT INBD CORNER. R & R AFT FLAP IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 54,704 hrs · 31,905 cycles

RIGHT WING SIDEWALL EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 53,698 hrs · 31,286 cycles

R2 DOOR EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,315 hrs · 31,076 cycles

FORWARD EMER EXIT LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 53,315 hrs · 31,076 cycles

FORWARD EMER EXIT LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

RIGHT SIDE 727 BULKHEAD FRAME INNER CHORD 5TH FASTENER FROM OTBD END. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

AFT CARGO COMPARTMENT WEB INNER CHORD CRACKED AT BS 727B BULKHEAD WL 201 AROUND FRAME FASTENER ON LT SIDE, 5TH FASTENER FROM OTBD END. REPAIRED CHORD IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

AFT HOLE OF INBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

AFT HOLE OF OTBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

FORWARD HOLE OF INBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

FORWARD HOLE OF OTBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

LEFT NR 3 WINDOW FRAME E - F POST FASTENER HOLE NR 7 CRACKED. REPAIRED POST IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

RIGHT NR 3 WINDOW FRAME E - F POST FASTENER HOLE NR 8 CRACKED. REPAIRED POST IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

AFT HOLE OF OTBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

AFT HOLE INBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

FORWARD HOLE OF INBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

RIGHT NR 3 WINDOW FRAME E - F POST FASTENER HOLE NR 7 CRACKED. REPAIRED POST IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

LEFT NR 3 WINDOW FRAME E - F POST FASTENER HOLE NR 8 CRACKED. REPAIRED POST IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

FORWARD HOLE OF OTBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: STRUCTURE — DELAMINATED (VERTICAL STAB) · airframe 50,285 hrs · 29,311 cycles

DORSAL FIN DELAMINATED RT SIDE AT STATION 961, 23 INCHES FROM LOWER LIP. REPAIRED FIN IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

RIGHT NR 3 WINDOW FRAME E - F POST FASTENER HOLE NR 7 CRACKED. REPAIRED POST IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

FORWARD HOLE OF OTBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW ACO.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,285 hrs · 29,311 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME CRACKED ON INTERNAL SIDE OF UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 50,285 hrs · 29,311 cycles

RIGHT HORIZONTAL STABILIZER CRACKED AT STATION 101.90, 9.5 INCHES FROM REAR SPAR. REPAIRED STABILIZER IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,285 hrs · 29,311 cycles

FORWARD HOLE OTBD FLANGE OF FWD SEAT TRACK CRACKED AT BS 727B LBL 24. REPAIRED SEAT TRACK IAW ACO.

Part: CABLE — MISROUTED (L1 DOOR) · airframe 49,640 hrs · 28,947 cycles

L1 DOOR EMER EVAC SLIDE CABLE MISROUTED. ROUTED CABLE IAW MT.

Part: LIGHT — CRACKED (CABIN) · airframe 48,570 hrs · 28,315 cycles

MID CABIN CEILING EMERGENCY EXIT LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 48,377 hrs · 28,189 cycles

INFLIGHT SHUTDOWN, DECLARED EMERGENCY, AT APPROXIMATELY 5,000 FEET IMC CREW FELT AN EXCESSIVE AIRFRAME VIBRATION. AFTER A FEW SECONDS NR 2 ENG N1 BEGAN TO DECREASE WITH NO CORRESPONDING MOVEMENT OF THE THRUST LEVER. CREW SHUT DOWN THE NR 2 ENG. R & R NR 2 ENG IAW MT.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 47,196 hrs · 27,485 cycles

RT MAIN WW FWD BULKHEAD VAPOR BARRIER CRACKED FWD OF B SYSTEM HYD PUMP. REPAIRED BARRIER IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 47,196 hrs · 27,485 cycles

RT WING CENTER SECTION REAR SPAR LOWER CHORD CRACKED AT BS 663 RBL 8. REPAIRED CHORD IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 45,694 hrs · 26,607 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT AFT OF DOOR INOP. RELAMPED SIGN PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 45,308 hrs · 26,374 cycles

RIGHT EMERGENCY EXIT LENS CRACKED. REMOVED AND REPLACED RIGHT EMERGENCY EXIT LENS PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 45,225 hrs · 26,322 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 45,224 hrs · 26,322 cycles

FORWARD EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: ESCAPE ROPE — LOOSE (CABIN) · airframe 44,820 hrs · 26,061 cycles

LEFT OVERWING EMERGENCY EXIT ESCAPE ROPE IS NOT STOWED PROPERLY. RESTOWED LEFT OVERWING EMERGENCY EXIT ESCAPE ROPE PER M/M.

Part: FUSE — BLOWN (CABIN) · airframe 44,038 hrs · 25,567 cycles

LEFT LOWER FLAP EMERGENCY EXIT SLIDE LIGHT INOP AT BS 727C+13, LBL 68. REMOVED AND REPLACED CHARGER FUSE CHARGER PER AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

R1 DOOR STUB FRAME CRACKED AT BS 295, RBL 53. REPAIRED ANGLE PER ER & SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 44,038 hrs · 25,567 cycles

RIGHT HORIZONTAL STABILIZER L/E PANEL 341B 3RD RIB FROM I/B END ATTACH ANGLE TO SKIN CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 44,038 hrs · 25,567 cycles

RIGHT HORIZONTAL STABILIZER L/E PANEL 341B 4TH RIB FROM I/B END ATTACH ANGLE TO SKIN CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 44,038 hrs · 25,567 cycles

LEFT HORIZONTAL STAB LEADING EDGE PANEL 331B 3RD RIB FROM I/B END ATTACH ANGLE TO SKIN CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 44,038 hrs · 25,567 cycles

RIGHT HORIZONTAL STABILIZER L/E PANEL 2ND RIB FROM I/B END ATTACH ANGLE TO SKIN CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

STRINGER CLIP CORRODED AT BS 540, STR 2R. REMOVED AND REPLACED CLIP IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

CREASE BEAM I/B CHORD CORRODED BETWEEN BS 700 TO BS 727, STR 17L. REPAIRED CHORD PER ER AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 719 TO BS 725, STR 17L. REPAIRED WEB PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 708 TO BS 715, STR 17L. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 44,038 hrs · 25,567 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. REPAIRED RIB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

RIGHT FLOORBEAM CORRODED AT BS 986, RBL 38.36. REPAIRED BEAM PER ER AND EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 44,038 hrs · 25,567 cycles

(LEFT WING) UPPER T/E PANEL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP ON AFT SIDE OF TRANSVERSE BEAM. REMOVED AND REPLACED ANGLE IAW SOPM.

Part: SILL — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

MOPSILL CORRODED BETWEEN BS 294 TO BS 344, RBL 57. REMOVED AND REPLACED MOPSILL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP IAW SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 44,038 hrs · 25,567 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED BETWEEN BS 344 TO BS 351, LBL 59. REMOVED AND REPLACED GIRT BAR IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 44,038 hrs · 25,567 cycles

LEFT WING NR 1 SLAT LEADING EDGE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 44,038 hrs · 25,567 cycles

RIGHT WING NR 8 SLAT LEADING EDGE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,038 hrs · 25,567 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED BETWEEN STA 92.7 AND STA 101.9. REPAIRED SKIN IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

FORWARD CARGO DOOR CUTOUT SUB THRESOLD WEB CORRODED BETWEEN BS 440 TO BS 480, RBL 28. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,038 hrs · 25,567 cycles

ZEE ANGLE CORRODED BETWEEN BS 727D+6 TO BS 767, LBL 20. REMOVED AND REPLACED ZEE ANGLE IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,811 hrs · 25,407 cycles

FORWARD GALLEY LOWER FLASHLIGHT INDICATOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,769 hrs · 25,377 cycles

L1 WINDOW POST CRACKED IN TOP LEFT CORNER. REPAIRED FRAME PER EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 43,729 hrs · 25,352 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 41,560 hrs · 24,066 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — DIRTY (GIRT BAR) · airframe 39,407 hrs · 22,808 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO UNARM. CLEANED AND LUBED GIRT BAR CLIPS PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 39,211 hrs · 22,697 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 38,362 hrs · 22,227 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT LOWER SURFACE CRACKED AT ACTUATOR. REPAIRED SLAT PER EA.

Part: HOOK — LOOSE (R1 DOOR) · airframe 38,362 hrs · 22,227 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR RETAINER HOOK FASTENERS LOOSE. REMOVED AND REPLACED HOOK ASSY PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 38,362 hrs · 22,227 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 38,362 hrs · 22,227 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,824 hrs · 21,332 cycles

ELECTRICAL SMELL AFTER GASPER FAN SWITCHED ON. SMELL WENT AWAY AFTER LANDING. CHECKED CABIN EQUIP, RECIRC & GASPER FAN, FOUND LT OVERHEAD CEILING LIGHT INOP AT ROW 6. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX FITTING CRACKED AT BS 547, RBL 41. R&R FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

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

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

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

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

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

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

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

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,792 hrs · 21,313 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 54. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 36,792 hrs · 21,313 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,608 hrs · 21,197 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 35,306 hrs · 20,435 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,260 hrs · 20,404 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,260 hrs · 20,404 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 33,631 hrs · 19,379 cycles

NR 2 L/E SLAT SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,502 hrs · 18,104 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT 1 ABC. RELAMPED EMERGENCY LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 30,838 hrs · 17,699 cycles

EEPLS LIGHT STRIP LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,379 hrs · 17,435 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 39 TO LBL 42. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,379 hrs · 17,435 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 30. REPAIRED BEAM PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 30,379 hrs · 17,435 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 28,773 hrs · 16,469 cycles

EEPLS LENS LOOSE AT ROW 9 ABC. SECURED LENS PER MM.

Part: SLIDE — READS LOW (L2 DOOR) · airframe 27,119 hrs · 15,477 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 26,973 hrs · 15,389 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 ABC. SECURED STRIP PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,973 hrs · 15,389 cycles

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

Part: LENS — MISSING (CABIN) · airframe 25,793 hrs · 14,686 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: SLIDE — FAILED (R2 DOOR) · airframe 22,032 hrs · 12,488 cycles

DURING SCHEDULED MV2 CHECK, R2 DOOR EMERGENCY EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 21,889 hrs · 12,416 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,724 hrs · 11,755 cycles

DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. RELAMPED LIGHT PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 19,504 hrs · 11,068 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: LIGHT — WORN (CABIN) · airframe 19,504 hrs · 11,068 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 18,507 hrs · 10,499 cycles

DURING SCHEDULED 5Y CHECK, FOUND RIGHT MLG W/W FWD WEB CRACKED AT BS 663, RBL 14. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 12,803 hrs · 7,256 cycles

R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE R2 DOOR EVAC SLIDE INTO CONTAINER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 10,397 hrs · 5,943 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (7 EA) AT ROWS NR 1, 3, 5, 19, 20, 22 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 7,708 hrs · 4,467 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11038-55, BOTH LT/RT ELEVATOR TAB HINGE BUSHINGS WORN AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED HINGE BUSHINGS PER MM.

Part: HINGE — WORN (LT/RT ELEVATOR) · airframe 7,708 hrs · 4,467 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11038-55, BOTH LT/RT ELEVATOR NR 4 HINGES WORN. REMOVED AND REPLACED NR 4 LT/RT ELEVATOR TAB HINGES PER MM.