N778SW

Part: SIGN — MISSING (R/H OVERWING) · airframe 70,377 hrs · 41,681 cycles

EMERGENCY EXIT SIDE PANEL LIGHT COVER MISSING- F/O SIDE / [01] REPLACED RH OVERWING EXIT SIGN PER AMM 33-51-01

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,118 hrs · 41,516 cycles

ITEM R1 DOOR HAS EXCESSIVE GIRT MATERIAL HANGING LOW / [01] REMOVED R-1 DOOR (FS) SLIDE (P/N 63550-101; S/N 0358F) IN REF TO MT 725-61-06.;[02] OK TO INSTALL NEW SLIDE;[03] REPLACED R-1 DOOR (FS) SLIDE WITH NEW SLIDE (P/N 63550-101; S/N 0320F) IN REF TO MT 725-61-06.;[04] VERIFIED STEP 3.

Part: SUPPORT BEAM — BROKEN (L/H WING) · airframe 70,118 hrs · 41,516 cycles

LEFT WING TRAILING EDGE PANEL 561AB MOUNT SUPPORT ANGLE IS BROKEN AT INBOARD END / [01] REMOVED AND REPLACED L/W TRAILING EDGE PANEL 561AB MOUNT SUPPORT BEAM PER REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.

Part: BRACKET — BROKEN (R/H WING) · airframe 70,118 hrs · 41,516 cycles

RIGHT WING REAR SPAR I/B THROUGH ACCESS PANEL 651DB ATTACHED BRACKET TO SPAR IS BROKEN / [01] REMOVED DAMAGE BRACKET AT R/W REAR SPAR I/B THROUGH ACCESS PANEL 651DB PER REF B737-700 SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED DAMAGE BRACKET AT R/W REAR SPAR I/B THROUGH ACCESS PANEL 651DB PER REF B737-700 SRM 51-40-02-0G-0.;[03] VERIFIED 1 AND 2;COMPLETE

Part: PANEL — CRACKED (L/H WING) · airframe 70,118 hrs · 41,516 cycles

L/H CENTER WING-TO-B0DY FAIRING ACCESS PANEL 193CR UPPER SECTION HAS CRACK L/H CENTER WING-TO-B0DY FAIRING ACCESS PANEL 193CL UPPER SECTION HAS CRACK REMOVED PANEL 193CL FOR ACCESS TO REAPIR IRW B737-700 AMM 53-51-21-000-802; REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE FABRIC REPAIR PLIES; NO WATER NOTE; NO CORE DAMAGED AT ACCESS PANEL 193CR UPPER SURFACE. REF B737-700 SRM 53-40-70-2R-1 PARAGRAPH 4 C AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4 B & C.;INSTALLED THE FABRIC REPAIR PLIES AT ACCESS PANEL 193CR UPPER SURFACE. REF B737-700 SRM 53-40-70-2R-1 PARAGRAPH 4 C AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4 D;E & F. 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. APPLIED TOPCOAT AT REPAIR AREA. REF B737-700 AMM 51-21-99-300-802 PARAGRAPH 3 C. APPLIED THE FABRIC REPAIR PLIES AT DAMAGED AREA AT ACCESS PANEL 193CR UPPER SURFACE. REF B737-700 SRM 53-40-70-2R-1 PARAGRAPH 4 C AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4.

Part: STRAP — LOOSE · airframe 69,973 hrs · 41,418 cycles

PILOT SIDE OVERWING EXIT STRAP COVER LOOSE. / [01] RE-INSTALLED OVERWING EXIT STRAP COVER PER AMM 52-22-00.

Part: BUMPER — BROKEN (R2 SLIDE) · airframe 69,007 hrs · 40,823 cycles

AFT SERVICE DOOR SLIDE BOX BUMPER END CAP BROKEN. R & R AFT SERVICE DOOR SLIDE END CAP PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,976 hrs · 40,806 cycles

EXTERIOR AFT RT SVC DOOR EMERGENCY LIGHT INOP ; / [01] RELAMPED AFT RT DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: STRINGER — CRACKED (R/H WING) · airframe 68,867 hrs · 40,745 cycles

R/W L/E INB FRONT SPAR LOWER CHORD ATTACHED ANGLE BRACKET CRACKED I/B OF PYLON # 2. REMOVED ANGLE PER B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW STRINGER ANGLE IAW SRM 51-40-05-0G-0; [03] VERIFIED STEP 2; VERIFIED STEP 1; OK TO TREAT AND PRIME; [06] TREATED AND PRIME HOLES AT ANGLE REF B737-7 SRM 51-20-01-OG-0; VERIFIED STEP 6; OK TO INSTALL STRINGER ANGLE. INSTALLED RT WING L/E I/B FRONT SPAR LOWER STRINGER ANGLE IAW SRM 51-40-02-0G-0 AND DWG #116A4008. REMOVED AND REPLACED STRINGER ANGLE IAW SEM 51-40-02-0G-0 AND DWG 116A4008.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 688,672 hrs · 40,745 cycles

FWD CARGO BS 500B - 500C, WL 156, S25R BAFFLE CORRORED. REMOVED BAFFLE IAW SRM 51-40-02-0G-0, FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2, PARAGRAF 4.C.(2)(B), FIGURE 103, DETAIL 103. LOCATED AND DRILLED THE BAFFLE IAW SRM 51-40-05-0G-0. APPLIED ALODINE AND PRIMER AT ALL NEW HOLES ON THE BAFFLE IAW SRM 51-20-01-0G-0. INSTALLED THE NEW BAFFLE IAW SRM 51-40-02-0G-0.

Part: STRAP — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

AFT CARGO COMPARTMENT ;CORROSION AT T STRAP STA 727 D +5 ; / [01] FOUND EXFOLIATION CORROSION ON T STRAP AT STA. 727 +5; OUT OF LIMITS PER SRM 53-00-53-1A-2; AND ORDERED AND RECEIVED NEW T STRAP P/N 146A9401-8; NEW T TO BE INSTALLED ON T/C 5360-E-16462-NG; [02] VERIFIED STEP 1.

Part: SUPPORT — CORRODED (FUSLEAGE) · airframe 68,867 hrs · 40,745 cycles

CORROSION.....FWD CARGO COMPARTMENT FLOOR @ STA 500D STR25L - STR25R WL155.5 ACCESS PANEL ANGLE SUPPORT HAS CORROSION IN SEVERAL AREAS. (18-033) ; / [01] RECEIVED NEW ANGLE SUPPORT P/N 143A9485-35 AAR ISSUE TAG WN4490 P.O 1684224 FOR FWD CARGO COMPARTMENT FLOOR FS 500D;BETWEEN STR'S 25R-25L WL 155.5; [02] ANGLE SUPPORT REMOVAL AND INSTALLATION BEING ACCOMPLISHED ON TASK CARD TTG8Q004DXN5; [03] VERIFIED STEP 1 AND 2

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

CORROSION.....R/H FWD CARGO COMPARTMENT FLOOR @ STA 420 - STA 440 STR 25R WL 155.5 FWD SHIELD HAS CORROSION. (18-039) ; / [01] RECEIVED NEW SHIELD P/N 143A8126U21 AAR ISSUE TAG WN9098 P.O 1684224 FOR FWD CARGO COMPARTMENT FLOOR FS 420 TO FS 440 STR 25R WL 155.5; [02] LOCATED AND DRILLED SHIELD AT FWD CARGO COMPARTMENT FLOOR FS 420 TO 440 STR 25R IN REF B737-700 SRM 51-40-05-0G-0;APPLIED ALODINE AND PRIMER AT ALL NEW HOLES IN REF B737-700 SRM 51-20-01-0G-0; [03] SHIELD REMOVAL AND INSTALLATION BEING ACCOMPLISHED ON TASK CARD TTG8Q004DXN5; [04] VERIFIED STEP #2; [05] VERIFIED STEP #3

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

RT FWD CARGO FLOOR BS 500A - 500D, S25R, WL 155.5 Z CHANNEL HAS CORROSION IN SEVERAL AREAS. LOCATED AND DRILLED A NEW Z CHANNEL IAW SRM 51-40-05-0G-0. VERIFIED STEP 1. TREATED AND APPLIED PRIMER TO Z CHANNEL IAW SRM 51-20-01-0G-0. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED THE NEW Z CHANNEL IAW SRM 51-40-05-0G-0.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

CORROSION ON RT FWD CARGO FLOOR, BS 492.4 - 500A, S25R, WL 155.5. AFT SHIELD HAS CORROSION. LOCATED AND DRILLED A NEW SHIELD IAW SRM 51-40-05-0G-0, APPLIED ALODINE AND PRIMER AT ALL NEW HOLES IAW SRM 51-20-01-0G-0. SHIELD REMOVAL AND INSTALLATION BEING ACCOMPLISHED ON TASK CARD TTG8Q004DXN5.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

CORROSION ON L/H FWD CARGO FLOOR, BS 480 - 500D, S25L, WL155.5, Z CHANNEL HAS CORROSION IN SEVERAL AREAS. REMOVED THE ZEE CHANNEL IAW AD CARD 5330-E-16461-NG, TASK CARD TTG8Q004DXN5 STEP 11, LOCATED AND DRILLED THE NEW ZEE CHANNEL IAW SRM 51-40-05-0G-0. TREATED AND APPLIED PRIMER TO THE ZEE CHANNEL IAW SRM 51-20-01-0G-0. ] FOUND ZEE-CHANNEL CORROSION OUT OF LIMITS IAW SRM 53-00-53-1A-2, STEP 4 .A. (2), FIGURE 103, DETAIL D. FABRICATED ZEE-CHANNEL, AND LOCATED IAW SRM 51-40-05-0G-0.

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 68,867 hrs · 40,745 cycles

SUPPLEMENTAL INFORMATION: CORROSION.....R/H FWD CARGO COMPARTMENT FLOOR @ STA 440 - STA 492.4 STR 25R WL 155.5 WEB HAS CORROSION IN SEVERAL AREAS. (18-038) ; / [01] WEB REMOVAL AND INSTALLATION BEING ACCOMPLISHED ON CARD #TTG8Q004DXN5; [02] LOCATED AND DRILLED WEB REF. B737-7 SRM 51-40-05-0G-0; [03] OK TO TREAT AN DPRIME HOLES; [04] TREATED AND PRIMED HOLES ON WEB REF.B737-7 SRM 51-20-01-0G-0; [05] INSTALLED NUT PLATES AND COMPLETED FWD CARGO COMPARTMENT DOOR CUTOUT WEB STA.492.4; STR25R; WL155 REF. USED; B737-7 SRM 51-40-02-0G-0; 51-20-01-0G-0; & 51-40-05-0G-0; [06] VERIFIED STEP 4 & 5

Part: NONE — CRACKED (R1 DOOR) · airframe 68,867 hrs · 40,745 cycles

R1 DOOR FWD CORNER CUTOUT FRAME CRACKED. REMOVED FASTENERS ON FRAME IAW SRM 51-40-02-0G-0 REMOVED THE CORNER CUTOUT FRAME IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW UPPER FWD FRAME IAW SRM 51-40-05-0G-0. TREATED AND PRIME FRAME HOLES IAW SRM 51-20-01-0G-0. COMPLETED R1 DOOR FWD CORNER CUTOUT FRAME DRILLING AND PREPARATION. INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q007258V.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

AFT CARGO LEFT SIDE 'Z' CHANNEL IS CORRODED 727-847; ; / [01] FOUND EXFOLIATION CORROSION ON L/H SIDE Z CHANNEL BETWEEN STA. 272 AND STA. 847 ; OUT OF LIMITS PER 737 SRM 53-00-53-1A-2; [02] CORRECTION ; FOUND EXFOLIATION CORROSION ON L/H SIDE Z CHANNEL BETWEEN STA. 727 TO STA. 847; OUT OF LIMITS PER REF 737 SRM 53-00-53-1A-2; [03] VERIFIED CORRECTED STEP 2.; [04] RECEIVED NEW L/H Z CHANNEL; P/N 146A7502-27; NEW CHANNEL TO BE INSTALLED ON T/C 5360-E-16462-NG; [05] STEP 4 VERIFIED; [06] STEP 4 VERIFIED

Part: FRAME — CRACKED · airframe 68,867 hrs · 40,745 cycles

FWD CABIN LT FUSELAGE SUPPORT FRAME FLANGE HAS SMALL CRACK ABOVE L-1 DOOR CUTOUT, BS 312. TRIMMED DAMAGED AREA IAW SRM 53-10-07-2R-1, FIGURE 202. REMOVED FASTENERS AT REPAIR LOCATION IAW SRM 51-40-02-0G-0. PERFORMED HFEC ROTO ON OPEN FASTENER HOLES WITHIN REPAIR AREA IAW NDTM PART 6, 51-00-00 PROCEDURE 16. NO CRACKS. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6, 51-00-00 PROCEDURE 23. NO CRACKS. PERFORMED INSURANCE CUT IAW SRM 53-10-07-2R-1. FABRICATED DOUBLER IAW SRM 53-10-07-2R-1. INSPECTED STEP 7 AND 8. REPAIR DOUBLER HEAT TREATED TO 7075-T6. APPLIED ALODINE AND PRIMER TO REPAIR AND AREA IAW SRM 51-20-01-0G-0. INSTALLED REPAIR IAW SRM 53-10-07-2R-1.

Part: CHANNEL — CORRODED (FUSLEAGE) · airframe 68,867 hrs · 40,745 cycles

AFT CARGO RIGHT SIDE Z CHANNEL IS CORRODED BS 727-767. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED A NEW Z CHANNEL IAW SRM 51-40-05-0G-0. TREATED AND PRIMERED, AND FABRICATED RT Z CHANNEL IAW AMM 51-21-41-370-802, AND 51-21-72-370--804. INSTALLED NUT PLATES ON NEW Z CHANNEL IAW SRM 51-40-02-0G-0, AND DRAWING 146A7502.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

AFT CARGO RIGHT 'Z' CHANNEL HAS LIGHT CORROSION AND MISSING PAINT FROM 847-964 AFT CARGO CHANNEL CORRECT STATION IS FROM 847 TO 947. REMOVED CORROSION ON AFT CARGO RIGHT ' Z' CHANNEL FROM STA847 TO STA 964 IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN. THICKNESS 0.048'. ORIGINAL MATERIAL 0.050' MATERIAL REMOVED 0.002' MATERIAL REMAINING 0.048'. FOUND WITH IN LIMITS IAW SRM 53-00-53-1A-2 FIG 103. TREATED AND PRIMER IAW SRM 51-21-41-370-802 & 51-21 72-370-804.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

L/H FWD CARGO COMPARTMENT SIDEWALL @ STA500D STR 18L HAS (1 EACH) SUPPORT BRACKET CRACKED. (18-030) ; LH FWD CARGO COMPARTMENT SIDEWALL @ STA 500D STR19 HAS (1 EACH) GUSSET CRACKED. (18-030) / [01] REMOVED LT FWD SUPPORT BRACKET AT FWD CARGO COMP.SIDE WALL STA 500D STR 19L REF B737-7 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW SUPPORT BRACKET REF B737-7 SRM 51-40-05-0G-0; [03] VERIFIED STEPS 1 AND 2; [04] OK TO PRIME AND INSTALL BRACKET; [05] APPLIED PRIMER AT GUSSET AND INSTALLED IN FWD CARGO COMPARTMENT FS 540 STR 19L IN REF B737-700 SRM 51-40-02-0-G-0; [06] RII VERIFIED STEP 5

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

FWD CARGO SIDEWALL, BS 500D S19R HAS ONE GUSSET CRACKED. REMOVED GUSSET IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED GUSSET IAW SRM 51-20-01-0G-0. TREATED AND PRIMED GUSSET IAW SRM 51-20-01-0G-0. LOCATED AND DRILLED GUSSET IAW SRM 51-40-05-0G-0. INSTALLED THE GUSSET IAW SRM 51-40-02-0G-0.

Part: SUPPORT — CRACKED (CABIN FLOOR) · airframe 68,867 hrs · 40,745 cycles

MAIN CABIN FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL24 MKD DOT ; / [01] REMOVED FLOOR SUPPORT BREAK REF B737-7 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW PANEL BREAK REF. B737-7 SRM 51-40-05-0G-0; TREATED AND PRIMED HOLES REF. SRM 51-20-01-0G-0; [03] VERIFIED STEP 1 AND 2; [04] OK TO INSTALL FLOOR SUPPORT BREAK; [05] REMOVED AND REPLACED FLOOR PANEL BREAK AT STA.540 BL'0' TO LBL24; REF USED B737-7 SRM 51-40-05-0G-0; 51-40-02-0G-0; 51-20-01-0G-0; & DRW#143A0060; [06] INSPECTED INSTALLATION

Part: SUPPORT — CRACKED (CABIN FLOOR) · airframe 68,867 hrs · 40,745 cycles

MAIN CABIN FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1 MKD DOT ; / [01] REMOVED MAIN CABIN FLOOR SUPPORT AT FS 540 RBL 1 IN REF B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] OK TO INSTALL PART; [04] INSTALLED NEW FLOOR SUPPORT AT FS 540 BETWEEN RBL 1 TO RBL 24;IN REF B737-700 SRM 51-40-02-0G-0; [05] VERIFIED STEP 4

Part: SCUFF PLATE — CRACKED (R1 DOOR) · airframe 68,867 hrs · 40,745 cycles

R1 DOOR CENTER SCUFF PLATE HAS A CRACK ; / [01] CRACK AT R1 DOOR CENTER SCUFF PLATE REPAIRED AS PER B737-700 SRM 53-10-15-2R REPAIR 2 BY J.L.WELDING INC.; FAA REPAIR STATION JLWR146K. ROUTING TAG #397622.; [02] VERIFIED WORK PERFORMED

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 68,867 hrs · 40,745 cycles

TYPICAL CRACK FOUND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR BEAR STRAP BETWEEN STA.291.5 AND STA.294.5 BETWEEN S-8R AND S-9R. APPROXIMATE LENGTH OF CRACK : 1.457' ; TYPICAL CRACK FOND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR BEAR STRAP ETWEEN STA.291.5 AND STA.294.5 ETWEEN S-8R AND S-9R. APPROXIMATE LENGTH OF CRACK : 1.457'.FASTENER HOLE FWD OF AOVE STATED FASTENER IS ALSO CRACKED.TYPICAL CRACK FOND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR / [01] INSTALLED EWIS PROTECTION AT RT FUSELAGE INTERNALLY REPAIR AREA REF B737-7 AMM 20-60-07-913-801;INSTALLED REPAIR AT R1 DOOR BEAR STRAP BETWEEN STA.291.5 AND STA.294.5 BETWEEN S-8R AND S-9R AREA, REF.USED B737-7 SRM 51

Part: PLATE — ELONGATED (AFT CARGO BAY) · airframe 68,867 hrs · 40,745 cycles

AFT CARGO FWD CAP STRIP PLATE SCREWS PASS THRU ; HOLES ELONGATED ; / [01] INSTALLED NEW AFT CARGO CAP STRIP; FWD PLATE PER REF. 737 AMM 25-52-10-400-801; [02] VERIFIED STEP 1.

Part: ANGLE — CORRODED (RH WING) · airframe 68,867 hrs · 40,745 cycles

RT WING I/B FRONT SPAR BOOST PUMP 2 FWD UPPER BONDING STRAP SURROUNDING STRUCTURE CORRODED. REMOVED BONDING STRAP IAW SRM 51-40-02-0G-0. INSTALLED EWIS PROTECTION IAW AMM 20-60-07-913-801. DISCONNECT CONNECTOR (D00076) AND CAPPED IAW AMM 28-22-41-000-801. REMOVED ANGLE AT RT WING ABOVE BOOST PUMP IAW SRM 51-40-02-0G-0, INSTALLED RT WING I/B FROM SPAR BOOST PUMP FWD UPPER ANGLE IAW SRM 57-20-10-1A-3 STEP 2.C. INSTALLED BONDING STRAP IAW AMM 20-50-11-910-80.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 68,721 hrs · 40,656 cycles

RH SERVICE DOOR GUIRT BAR LATCH LOOSE ADJUSTED FWD SVC DOOR GIRT BAR STOW CLIP ON DOOR LINER PER SIP OK FOR SVC

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,379 hrs · 40,435 cycles

5 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST. / R&R BATTERY PACKS PER AMM AND DWG.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 68,099 hrs · 40,250 cycles

CAPTAIN EMERGENCY EXIT LIGHT INOP. / RELAMPED LIGHT PER MM.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

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

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG BORE EVIDENCE OF CORRODED. / REPAIRED LUG BORE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD HAT SIDE CORRODED. / REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

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

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,405 hrs · 39,811 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.

Part: PANEL — CRACKED (ELEVATOR RH) · airframe 66,347 hrs · 39,124 cycles

RIGHT ELEVATOR CENTER BALANCE BAY IDLER HINGE PANEL CRACKED / REMOVED AND REPLACED RIGHT ELEVATOR CENTER BALANCE BAY IDLER HINGE PANEL PER AMM. 27-31-41 AND SRM 51-40-02

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 66,347 hrs · 39,124 cycles

LEFT VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER CRACKED / R&R LEFT VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER PER SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 66,347 hrs · 39,124 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER AMM. 53-31-31

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 65,957 hrs · 38,855 cycles

L1 DOOR CAPTAIN SIDE PROTECTIVE FLAP THAT COVERS MANUAL DEPLOY HANDLE STUCK IN HOUSING. REPOSITIONED COVER PER MT.

Part: LENS — DISLODGED (CABIN) · airframe 65,203 hrs · 38,393 cycles

LT OVERHEAD EMERGENCY EXIT LIGHT LENS COVER DISLODGED AT ROW 14. REINSTALLED LENS IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,208 hrs · 37,781 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED AFT FLAP PER SRM.

Part: DETECTOR — FAULTY (LT WING) · airframe 63,996 hrs · 37,645 cycles

DIVERSION, LT WING TO BODY OVERHEAT AT 39K AT CRUISE. R&R OVERHEAT DETECTOR PER AMM.

Part: PANEL — DELAMINATED (LT WING) · airframe 63,755 hrs · 37,491 cycles

(QC) #1 ENG PYLON PANEL 431ER DISBONDED AT FWD LOWER CORNER (MARKED) / REMOVED AND REPLACED #1 ENG PNL 431ER PER AMM 24-53-01

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,755 hrs · 37,491 cycles

AFT ENTRY RT AREA EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 63,755 hrs · 37,491 cycles

AFT LOWERED CEILING PANEL CENTER EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

INTERCOSTAL CORRODED AT BS 270, LBL 40. R&R INTERCOSTAL IAW SRM & DWG.

Part: BRACKET — CORRODED (MAIN CABIN) · airframe 63,755 hrs · 37,491 cycles

***CORROSION*** LOWERED CEILING SUPPORT TIE-ROD BRACKET AT 927 STR 4L (MARKED) / REPLACED LOWERED CEILING SUPPORT TIE-ROD BRACKET STA 927; STR 4L IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; DWG # 147A9019; REV C.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 63,755 hrs · 37,491 cycles

FWD CABIN FLOOR PANEL 221BF HAS BROKEN O/B AFT CORNER / FWD CABIN FLOOR PANEL 221BF BROKEN O/B AFT CORNER REPAIRED IAW SRM 53-00-50-2R-6 AND DWG 141A5810 ID- 0056 57824U 08-11-2018

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 698 TO BS 701, RBL 45. R&R SEAT TRACK CROWN IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

INTERCOSTAL CRACKED BETWEEN BS 270 TO BS 294, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 25 TO RBL 42. REPAIRED FLOORBEAM IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

FRAME ATTACH ANGLE CRACKED BETWEEN BS 290 TO BS 294, RT WL 208. R&R ANGLE IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

FORWARD ENTRY DOOR MOPSILL CORRODED BETWEEN BS 300 TO BS 356, WL 208. R&R MOPSILL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 1. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986, BETWEEN RBL 43 TO LBL 43. REPAIRED CHORD IAW EA & ER.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

L2 DOOR MOPSILL CORRODED BETWEEN BS 952 TO BS 992, WL 208. R&R MOPSILL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

STRAP CORRODED BETWEEN BS 1016 TO BS 1030, LBL 3. R&R STRAP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

INTERCOSTAL CRACKED AT BS 308, RBL 15. R&R INTERCOSTAL PER SRM AND DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

WEB CORRODED BETWEEN BS 986 TO BS 1016, BETWEEN LBL 34 TO LBL 44. R&R SHEAR WEB IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

AFT SERVICE MOPSILL CORRODED BETWEEN BS 947 TO BS 994, WL 208. R&R MOPSILL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

FLOOR SUPPORT CORRODED AT BS 955, BETWEEN RBL 11 TO RBL 27. R&R SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

WEB CORRODED BETWEEN BS 986 TO BS 1016, BETWEEN RBL 37 TO RBL 42. R&R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

FLOOR SUPPORT CORRODED AT BS 950.5, BETWEEN RBL 32 TO RBL 33. R&R SUPPORT IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 294 TO BS 363, WL 208. R&R MOPSILL IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

STRAP CORRODED BETWEEN BS 1016 TO BS 1030, RBL 3. R&R STRAP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 63,755 hrs · 37,491 cycles

***CORROSION*** ON FLOOR SUPPORT STA 325; RBL 10; WL 208. (MARKED) / REPLACED FLOOR SUPPORT STA 325; RBL 10; WL 208 IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 141A5400 57449U 15AUG18

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

STRAP CORRODED BETWEEN BS 1016 TO BS 1028, RBL 17. R&R STRAP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

INTERCOSTAL CRACKED AT BS 349, RBL 32. R&R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT — CORRODED (L1 DOOR) · airframe 63,755 hrs · 37,491 cycles

L1 DOOR GIRT BAR FITTING SUPPORTS CORRODED BETWEEN BS 312 TO BS 344. R&R SUPPORTS IAW SOPM.

Part: RETAINER — CRACKED (RT WING) · airframe 63,755 hrs · 37,491 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 ENGINE; HORIZ. SEAL RETAINER IS CRACKED. / REMOVED CRACKED SEAL RETAINER AND INSTALLED NEW HORIZONTAL SEAL RETAINER ON R/H UPPER T/E PANEL JUST AFT OF #2 ENGINE IAW SRM 51-40-02-0G-0 4. FASTENER IDENTIFICATION WAS FROM IPC 57-50-00-25 ITEM 35 53916C 05AUG18

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

PANEL 192K HAS A DELAMINATED DENT ON THE EXTERIOR SKIN / PANEL 192K WITH A DELAMINATED DENT ON THE EXTERIOR SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY LT CARGO TIE DOWN TRACK CRACKED AT BS 792, LBL 17. R&R TIE DOWN TRACK PER SRM AND DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 63,755 hrs · 37,491 cycles

LT WING UPPER T/E PANEL AFT OF #1 ENGINE; VERT SEAL RETAINER IS CRACKED. / REMOVED OLD AND INSTALLED NEW L/W UPPER T/E PANEL VERTICAL SEAL RETAINER AFT OF #1 ENGINE IAW SRM 51-40-02-0G-0 4. FASTENER IDENTIFICATION WAS FROM IPC 57-50-00-25 ITEM 199 AND 200 55916U 05AUG18

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 23. R&R SHIELD PER SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

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

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,755 hrs · 37,491 cycles

LT HORIZONTAL PRESSURE DECK TO BE CRACKED BETWEEN BS 663 TO BS 675, BETWEEN LBL 31 TO LBL 33. REPAIRED WEB IAW EA & ER.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 63,755 hrs · 37,491 cycles

RT MAIN LANDING GEAR BAY FIBERGLASS VAPOR BARRIER BULKHEAD CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

APU DUCT SHROUD BRACKET CRACKED AT BS 727, RBL 6. R&R BRACKET IAW SRM AND DWG.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY CARGO TIE DOWN TRACK CRACKED AT BS 767, RBL 13. R&R TRACK PER SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS AREAS OF CORROSION AT BS 772 LBL10 TO RBL10 / RECEIVED NEW ACB FLOOR SPLICE STRAP AT B.S 772 ON PO# 699391

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY TENSION STRAP IN DOORWAY CORRODED BETWEEN BS 792 TO BS 847, RBL 18. R&R STRAP PER SRM DWG.

Part: STIFFENER — CRACKED (LT M LG WW) · airframe 63,755 hrs · 37,491 cycles

VERTICAL STIFFENER CRACKED IN RADIUS ON AFT SIDE OF BS 663, LBL 25. R&R STIFFENER IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO BS 767, RBL 23. R&R SUPPORT IAW DWG & SRM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,755 hrs · 37,491 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS AREAS OF CORROSION AT BS.887 LBL10 TO RBL10 / DUE TO NO LIMITS IN SRM. FOR ACB FLOOR SPLIE STRAP WAS REMOVED AND REPLACED I.A.W. SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0. 88919U 22AUG18 AT BS 887 88919U 22AUG18

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,755 hrs · 37,491 cycles

R1 DOOR NR 4 LOWER BEAM CRACKED. R&R BEAM PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,755 hrs · 37,491 cycles

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

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 63,755 hrs · 37,491 cycles

LT MAIN LANDING GEAR BAY FIBERGLASS VAPOR BARRIER BULKHEAD CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: COVER — DAMAGED (CABIN) · airframe 63,755 hrs · 37,491 cycles

R2 DOOR EMERGENCY LIGHT COVER DAMAGED. R&R COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,848 hrs · 36,926 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,848 hrs · 36,926 cycles

EXTERNAL POWER DOOR CUTOUT CRACKED. REPAIRED THE SKIN IAW EA.

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 62,633 hrs · 36,795 cycles

A SYSTEM HYDRAULIC QUANTITY DECREASED DURING FLIGHT TO 54%. ALL A SYSTEM HYDRAULIC FLIGHT CONTROLS REMAINED NORMAL. R & R THE A/P ACTUATOR PRESSURE LINE PACKING IN THE ELEVATOR SERVO IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,355 hrs · 36,611 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT M1674. R & R THE BATTERY IAW MM.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 62,355 hrs · 36,611 cycles

FLOOR SUPPORT WEB CRACKED BETWEEN BS 328 TO 344, LBL 48. R & R THE FLOOR SUPPORT WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 62,355 hrs · 36,611 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, LBL 12. R & R THE FLOOR SUPPORT IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 62,355 hrs · 36,611 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT M1675. R & R THE BATTERY IAW MM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 62,355 hrs · 36,611 cycles

FLOOR SUPPORT WEB CRACKED BETWEEN BS 312 TO 328, LBL 48. R & R THE FLOOR SUPPORT WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 62,355 hrs · 36,611 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, RBL 12. R & R THE FLOOR SUPPORT IAW SRM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 62,276 hrs · 36,563 cycles

L1 DOOR EMERGENCY SLIDE PACKAGE GIRT BAR LOOSE. SECURED THE GRIT BAR IAW AMM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,302 hrs · 35,953 cycles

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

Part: BRACKET — CRACKED (AED) · airframe 60,309 hrs · 35,316 cycles

AFT PASSENGER DOOR LOWER GATE SUPPORT BRACKET IS CRACKED / REMOVED AND REPAIRED MOUNTING BRACKETS PER SRM 51-40-02

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 60,203 hrs · 35,256 cycles

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

Part: SIGN — WRONG PART (EMERGENCY LIGHTS) · airframe 59,122 hrs · 34,611 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. R & R THE SIGN IAW AMM.

Part: LIGHT — LOOSE (ROW 9) · airframe 59,122 hrs · 34,611 cycles

LEFT OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LOOSE AT ROW 9. SECURED THE LIGHT IAW AMM.

Part: SIGN — WRONG PART (EMERGENCY LIGHTS) · airframe 59,122 hrs · 34,611 cycles

L2 DOOR EMERGENCY EXIT LIGHT SIGN MISSING RED ARROW. R & R THE SIGN IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 59,019 hrs · 34,549 cycles

L1 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 58,582 hrs · 34,287 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 57,849 hrs · 33,859 cycles

FORWARD UPPER ALLEY FLASHLIGHT INOP. R&R FLASHLIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,079 hrs · 33,386 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1670 INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 57,079 hrs · 33,386 cycles

OVERHEAD EMERGENCY EXIT SIGN ASSEMBLY BROKEN AT BS 627.5. R & R THE SIGN IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,079 hrs · 33,386 cycles

RIGHT ACFT BAY UPPER CHORD ON FORWARD SIDE OF BS 663, BULKHEAD CRACKED. REPAIRED BULKHEAD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,079 hrs · 33,386 cycles

RT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665, RBL 41. REPAIRED WEB IAW ER AND EA.

Part: FRAME — CRACKED (BS 827) · airframe 57,079 hrs · 33,386 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 57,079 hrs · 33,386 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 747) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 663) · airframe 57,079 hrs · 33,386 cycles

LEFT A/C BAY BULKHEAD UPPER FRAME CRACKED AT BS 663, LBL 8, ON FORWARD SIDE. REPAIRED IAW ER AND EA.

Part: FRAME — CRACKED (BS 727D) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 500C) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 727) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 57,079 hrs · 33,386 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 440) · airframe 57,079 hrs · 33,386 cycles

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

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 57,079 hrs · 33,386 cycles

BULKHEAD STIFFENER CRACKED AT BS 663, LBL 8. REPAIRED THE STIFFENER IAW SRM.

Part: FRAME — CRACKED (BS 480) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 727D) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 57,079 hrs · 33,386 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,079 hrs · 33,386 cycles

FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,079 hrs · 33,386 cycles

FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 727B) · airframe 57,079 hrs · 33,386 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 57,079 hrs · 33,386 cycles

G-1 GALLEY EMERGENCY LIGHT LENS CRACKED. R & R THE LENS IAW AMM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 57,079 hrs · 33,386 cycles

LEFT WING NR 1 SLAT LEADING EDGE LOWER SKIN CRACKED AT ACTUATOR RIB FASTENER HOLES. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,079 hrs · 33,386 cycles

LEFT WING NR 4 SLAT L/E LOWER SKIN CRACKED AT ACTUATOR RIB FASTENER HOLE. R & R NR 4 SLAT SKIN IAW SRM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 56,991 hrs · 33,327 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. R & R THE SLIDE IAW MT.

Part: FUSE — BLOWN (CABIN) · airframe 56,874 hrs · 33,254 cycles

AFT EMERGENCY AISLE LIGHT INOP. R&R FUSE PER AMM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 56,864 hrs · 33,248 cycles

AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, STR 1L. REPAIRED BULKHEAD PER SRM AND EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,939 hrs · 31,528 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M1775. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,939 hrs · 31,528 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M1669. R & R BATTERY PACK IAW MM.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 52,686 hrs · 30,812 cycles

FUEL CROSS FEED VLV INOPERATIVE IN FLIGHT. FUEL CROSS FEED CB TRIPPED. FUEL WOULD NOT FEED FROM LT SIDE. R & R CROSS FEED VLV IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 50,916 hrs · 29,801 cycles

L1 DOOR LOWER EMER EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

FLOORBEAM TRACK CORRODED BETWEEN BS 800 TO 820 RBL 13. REPAIRED TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

FRAME CRACKED AT BS 747 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,497 hrs · 29,550 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663 BETWEEN RBL 25 TO RBL 45. REPAIRED WEB IAW ACO.

Part: BRACKET — CRACKED (RT WING) · airframe 50,497 hrs · 29,550 cycles

RIGHT WING TE UPPER SHELF PANEL SUPPORT ANGLE CRACKED. R & R BRACKET ASSEMBLY IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

NUMBER 2 SEAT TRACK LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B LBL 24.75 OTBD AFT FASTENER HOLE. REPAIRED BEAM IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 50,497 hrs · 29,550 cycles

LEFT WING UPPER TE SHELF PANEL SUPPORT RIB BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

NUMBER 2 SEAT TRACK LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B LBL 24.75 INBD FWD FASTENER HOLE REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

NUMBER 3 SEAT TRACK LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B, RBL 24.75 INBD FWD FASTENER HOLE. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

NR 4 SEAT TRACK LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B RBL 45.5 OTBD AFT FASTENER HOLE. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,497 hrs · 29,550 cycles

NUMBER 3 SEAT TRACK LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B, RBL 24.75 OTBD FWD FASTENER HOLE. REPAIRED BEAM IAW EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 49,493 hrs · 28,980 cycles

L2 DOOR EVAC SLIDE GIRT LOOSE. ADJUSTED SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,493 hrs · 28,980 cycles

R2 DOOR EVAC SLIDE GIRT LOOSE. ADJUSTED SLIDE IAW MT.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 49,212 hrs · 28,822 cycles

DURING CRUISE AFT LAVATORY SMOKE DETECTOR ACTIVATED. NO OTHER INDICATIONS OF SMOKE OR FIRE. DIVERTED AND DECLARED EMERGENCY. R & R AFT LAVATORY SMOKE DETECTOR IAW AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 49,179 hrs · 28,806 cycles

LEFT HORIZONTAL STABILIZER RIB AT STATION 129.5 CRACKED AT 1ST VERTICAL STIFFENER FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,179 hrs · 28,806 cycles

RIGHT NR 3 WINDOW FRAME E F POST CRACKED. REPAIRED FRAME IAW ACO.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 49,179 hrs · 28,806 cycles

LEFT WINDOW NR 3 WINDOW FRAME E F POST DOUBLER CRACKED. REPAIRED DOUBLER IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,179 hrs · 28,806 cycles

NR 1 RT COCKPIT WINDOW FRAME CRACKED IN UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,179 hrs · 28,806 cycles

NR 1 LT COCKPIT WINDOW FRAME CRACKED IN UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: COVER — BROKEN (CABIN) · airframe 47,198 hrs · 27,634 cycles

EMERGENCY EXIT LIGHT COVER BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: FAN — DEFECTIVE (AC BAY) · airframe 43,817 hrs · 25,578 cycles

DIVERSION/DECLARED EMERGENCY -- DURING CRUISE FLT ATTENDANT REPORTED ELEC SMOKE SMELL, SMELL DISSIPATED AFTER 8-10 MIN. FOUND CABIN AIR RECIRCULATION FAN BREAKER POPPED. REMOVED & REPLACED RECIRC FAN PER MM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT LOWER END AT STA 92.70. REMOVED & REPAIRED RIB IAW SRM AND ER.

Part: CAP — WORN (FUSELAGE) · airframe 43,769 hrs · 25,546 cycles

WEB CAP WORN AT BS 336, STR 5R. REMOVED AND REPLACED WEB CAP IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,769 hrs · 25,546 cycles

FRAME CRACKED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,769 hrs · 25,546 cycles

SUB FRAME CRACKED AT BS 296.5, RBL 53. REPAIRED SUB FRAME IAW ATS ER AND EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120.30 18. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

LEFT HORIZ STAB LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: LENS — DAMAGED (CABIN) · airframe 43,769 hrs · 25,546 cycles

FORWARD EMERGENCY EXIT LIGHT DAMAGED AT BS 303.5. REMOVED AND REPLACED LENS IAW M/M.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 43,769 hrs · 25,546 cycles

PRESSURE WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW ER AND EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 203.1. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,769 hrs · 25,546 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 43,369 hrs · 25,298 cycles

EMERGENCY EXIT LENS COVER MISSING. INSTALLED COVER PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 43,232 hrs · 25,213 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK ASSY PER SRM.

Part: FLANGE — CRACKED (VERTICAL STAB.) · airframe 40,323 hrs · 23,509 cycles

DURING SCHEDULED OTS CHECK, FOUND VERTICAL STABILIZER L/E FLANGE CRACKED AT LT SIDE BELOW TOP OF L/E. REPAIRED FLANGE IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 39,390 hrs · 22,972 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 39,014 hrs · 22,745 cycles

L2 DOOR EMERGENCY EVAC SLIDE ASSY LOOSE. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,745 hrs · 22,583 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 38,745 hrs · 22,583 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 38,745 hrs · 22,583 cycles

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

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,977 hrs · 21,550 cycles

DURING SCHEDULED MV2 CHECK, FOUND COCKPIT OVERHEAD PANEL EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT ASSY PER MM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,586 hrs · 21,321 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,586 hrs · 21,321 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,586 hrs · 21,321 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,586 hrs · 21,321 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,586 hrs · 21,321 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,586 hrs · 21,321 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 23. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,197 hrs · 21,120 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,473 hrs · 20,696 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT AFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,025 hrs · 20,428 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,025 hrs · 20,428 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,023 hrs · 19,784 cycles

DURING SCHEDULED MV2, FOUND RT OVERWING EMERGENCY EXIT LIGHT BURNED OUT. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,881 hrs · 19,690 cycles

RIGHT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8. RELAMPED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,332 hrs · 19,353 cycles

EEPLS STRIP LOOSE NEAR ROW 8. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,230 hrs · 18,709 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,031 hrs · 18,589 cycles

DURING SCHEDULED MV1 CHECK, FOUND BS 663.75 BULKHEAD VERTICAL PRESSURE WEB CRACKED AT RBL 42.5. REPAIRED PER SWA EA.

Part: GLOWSTRIP — LOOSE (ROW 8 ABC) · airframe 30,423 hrs · 17,589 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 ABC. SECURED STRIP PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 30,033 hrs · 17,328 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 27,885 hrs · 16,052 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: CONTROL VALVE — FAULTY (NR 2 ENGINE) · airframe 23,872 hrs · 13,724 cycles

DIVERSION, RT BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB, RESET, ILLUMINATED AGAIN. DURING CRUISE AT FL 390 CABIN WAS CLIMBING 200 FT PER MINUTE, DURING DESCENT CABIN CLIMBED AT 400 FT PER MINUTE, AUTO DID NOT APPEAR TO MAINTAIN CABIN ALT. FERRY FLIGHT TO TPA FOR TROUBLESHOOTING. SECURED PNEUMATIC BOOT ASSY AT AFT PRESSURE BULKHEAD PER MM. REMOVED AND REPLACED NR 2 ENG PRECOOLER CONTROL VALVE PER MM.

Part: FITTING — LOOSE (R2 DOOR GIRT BAR) · airframe 23,174 hrs · 13,344 cycles

R2 DOOR EMEREGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED EVAC SLIDE FITTING PER MM.

Part: PUMP — MAKING METAL (NR 1 ENGINE) · airframe 19,620 hrs · 11,255 cycles

AIR TURBACK, LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION AFTER T/O. FOUND METAL DEBRIS AT HYD A-SYS NR 1 ENG HYD PUMP CASE DRAIN FILTER. REMOVED AND REPLACED BOTH NR 1 ENG HYD PUMP CASE DRAIN FILTERS. REMOVED AND REPLACED HYD RESTRICTOR CHECK VALVE. REMOVED AND REPLACED LANDING GEAR BYPASS VALVE PER MM. OPS CK GOOD.

Part: PUSH-PULL CABLE — FAULTY (MLG) · airframe 18,316 hrs · 10,516 cycles

DECLARED EMERGENCY, LANDING GEAR LEVER STUCK IN THE OFF POSITION, WOULD NOT MOVE UP OR DOWN. REMOVED AND REPLACED LANDING GEAR PUSH/PULL CABLE & LEVER GEARBOX PER MM.

Part: LEVER — FAULTY (MLG) · airframe 18,297 hrs · 10,505 cycles

DECLARED EMERGENCY, LANDING GEAR LEVER STUCK IN THE OFF POSITION, WOULD NOT MOVE UP OR DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER ASSY PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 15,391 hrs · 8,822 cycles

DURING SCHEDULED HC2-CHECK, FOUND AFT PRESSURE BULKHEAD ABS 1016, BETWEEN STR 11R AND STR 12L, OIL CANNING. REPAIRED BULKHEAD SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 15,386 hrs · 8,819 cycles

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

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 15,386 hrs · 8,819 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 15,195 hrs · 8,711 cycles

EEPLS FWD COVER MISSING. REPLACED EEPLS COVER PER MM.

Part: LENS — MISSING (ROW 1 ABC) · airframe 14,956 hrs · 8,569 cycles

DURING SCHEDULED RON, FOUND EEPLS LENS AT ROW 1 ABC, MISSING. INSTALLED EEPLS LENS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,020 hrs · 8,033 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS AT ROWS 1 TO 4, INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 12,918 hrs · 7,431 cycles

DURING MS CHECK, FOUND EMERGENCY EXIT FLOOR LIGHT INOP AT L1 DOOR. RELAMPED PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 11,391 hrs · 6,570 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED (5 EA) IN CABIN. REMOVED AND REPLCED EEPLS COVERS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 10,361 hrs · 5,998 cycles

FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 8,090 hrs · 4,706 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS LENS MISSING AT ROW NR 1. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,016 hrs · 4,668 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 7,885 hrs · 4,580 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 7,474 hrs · 4,351 cycles

AFT SVC DOOR EMERGENCY EXIT EVAC SLIDE INADVERTENTLY WAS PULLED FROM CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 6,719 hrs · 3,924 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,719 hrs · 3,924 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED THROUGHTOUT CABIN. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 3,847 hrs · 2,309 cycles

EEPLS COVER DAMAGED AT OVERWING EXIT ROW. R&R EEPLS COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 2,034 hrs · 1,231 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER.