N747SA

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 79,404 hrs · 47,293 cycles

LH HORIZONTAL UPPER FWD SLIDING SEAL CRACKED. REMOVED AND REPLACED LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM 53-31-31.

Part: SLIDE — UNSECURE (AFT SERVICE DOOR) · airframe 79,404 hrs · 47,293 cycles

-AFT SERVICE DOOR ESCAPE SLIDE GIRT FLAP NOT SECURED PROPERLY AND DRAGS THRESHOLD. REPACKED THE AFT SERVICE DOOR ESCAPE SLIDE REF AMM 25-66-01.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 79,404 hrs · 47,293 cycles

OVERHEAD BIN COVE PANEL EMERGENCY LIGHT LENS MISSING 19 RT. INSTALLED THE EMERGENCY LIGHT LENS COVER IAW AMM 33-51-03

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 79,404 hrs · 47,293 cycles

AFT RT EMERGENCY BATTERY FAILED. R & R THE BATTERY IAW AMM 33-51-06.

Part: SLIDE — UNSECURE (AFT PAX DOOR) · airframe 79,404 hrs · 47,293 cycles

-AFT ENTRY DOOR ESCAPE SLIDE GIRT FLAP NOT SECURED PROPERLY AND DRAGS THRESHOLD. REPACKED THE AFT ENTRY DOOR ESCAPE SLIDE IAW 25-66-01.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 79,404 hrs · 47,293 cycles

FWD CTR EMERGENCY BATTERY FAILED. R&R FWD CTR EMERGENCY BATTERY IAW AMM 33-51-06.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 79,404 hrs · 47,293 cycles

CENTER LT EMERGENCY BATTERY FAILED. R&R THE BATTERY IAW AMM 33-51-06.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 79,404 hrs · 47,293 cycles

FWD RT EMERGENCY BATTERY FAILED. R&R THE BATTERY IAW AMM 33-51-06.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 79,222 hrs · 47,153 cycles

FWD CARGO FLOOR PANEL CRACKED / [01] R&R FWD CARGO FLOOR PANEL 120 CF IN REF TO AMM 25-52-10.

Part: STRIP — BROKEN (AFT CABIN) · airframe 77,103 hrs · 45,724 cycles

AFT FLASHLIGHT STRIP BROKEN / [01] R&R AFT FLASHLIGHT STRIP PER AMM 25-64-00

Part: PANEL — ELONGATED · airframe 76,616 hrs · 45,449 cycles

PNL 194E HAS ELONGATED HOLES ; / [01] REMOVED AND REPLACED 194E PANEL PER AMM 53-51-21.

Part: PANEL — ELONGATED · airframe 76,616 hrs · 45,449 cycles

PNL 193D HAS ELONGATED HOLES ; / [01] REMOVED AND REPLACED 193D PANEL PER AMM 53-51-21.

Part: COVER — BROKEN (CABIN) · airframe 76,610 hrs · 45,446 cycles

?EXIT? SIGN IN EMERGENCY EXIT ROW RIGHT SIDE BROKEN ; / [01] R+R?D FWD LOWER RT WING EMERGENCY DOOR LIGHT COVER IAW MM 33-51-01

Part: NONE — CRACKED (FUSELAGE) · airframe 75,857 hrs · 44,997 cycles

SUPPLEMENTAL INFORMATION: FWD GROUND POWER DOOR CUTOUT HAS .700 IN CRACK ON LOWER EDGE; 2.5 IN FROM FWD EDGE OF CUTOUT ; / [01] ADDED TOOLS; [02] REPAIRED PER SRM 53-10-15-2R-4 REPAIR 4 ZONE 2.; [03] PERFORMED NDT PART 6; 51-00-00 PROCEDURE 23; NO DEFECTS NOTED. REPAIR GOOD PER SRM 53-10-15-2R-4 REPAIR 4 ZONE 2

Part: BATTERY PACK — FAILED (CABIN) · airframe 75,857 hrs · 44,997 cycles

SUPPLEMENTAL INFORMATION: RIGHT OVER WING EXIT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. ; / [01] REMOVED AND REPLACE BATTERY PACK AND CHARGE ASSY. PER AMM 33-51-06

Part: NONE — FAILED (CABIN) · airframe 75,857 hrs · 44,997 cycles

RIGHT OVER WING EXIT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. ; / [01] REMOVED AND REPLACE BATTERY PACK AND CHARGE ASSY. PER AMM 33-51-06

Part: HANDLE — LOOSE (L1 DOOR ASSIST) · airframe 74,617 hrs · 44,264 cycles

CUSTOMER WALK- L-1 DOOR AFT ASSIST HANDLE LOOSE / SECURED/ INSTALLED L-1 DOOR AFT ASSIST HANDLE PER B737-700 AMM 52-11-31-400-802

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 74,617 hrs · 44,264 cycles

L2 DOOR SLIDE PRESSURE IS LOW OUT OF GO BAND TO THE LEFT / REMOVAL AND REPLACEMENT OF L2 SLIDE PERFORMED PER MT 725-61-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,617 hrs · 44,264 cycles

EMERGENCY AISLE LIGHT ON SEAT ROW 24 L/H INOP. / RESEATED EMERGENCY AISLE (AREA) LIGHT LAMP ON SEAT ROW 24 L/H AS PE B737 AMM 33-51-03-960-801 AND PERFORMED LAMP TEST. TEST OK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,617 hrs · 44,264 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. / RESEATED R2 EXTERNAL EMERGENCY LIGHT LAMP AS PER B737 AMM 33-51-04-960-801. PERFORMED LAMP TEST OK

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 74,617 hrs · 44,264 cycles

AFT CARGO DOOR AFT SCUFF PLATE HAS A CRACK / RECEIVED AFT SCUFF PLATE. PORT CONTROL TAG # 359723.

Part: PANEL — CRACKED (LT RAM INLET) · airframe 74,617 hrs · 44,264 cycles

AT RAM AIR INLET LIP ASSEMBLY FOUND CRACK AT O/B SIDE AFT CORNER / RECEIVED SERVICEABLE PANEL LT RAM AIR INLET LIP ASSY 191HL APPLIED TOP COAT PER B737-700 AMM 51-21-73-370-803, PANEL WILL BE INSTALLED ON CUSTOMER CARD 5331-1-14524-NG.

Part: SUPPORT — CRACKED (RT WING SKIN) · airframe 74,617 hrs · 44,264 cycles

RIGHT WING APROX IRSS220 PANEL SUPPORT BRACKET CRACKED / REMOVED AND REPLACED CLIPAY, RIGHT WING APPROX IRSS220 PANEL SUPPORT CLIPPAY REF B737-700 SRM 51-40-02-0G-0

Part: CHANNEL — DAMAGED (BS 747-887) · airframe 74,617 hrs · 44,264 cycles

AFT CARGO COMPARTMENT R/H ZEE CHANNEL FROM ABOUT STA 887-747 WITH VARIOUS ELONGATED HOLES / FABRICATED NEW ZEE CHANNEL AS PER B737-700 SRM 51-40-05-0G-0 AND DWG# 146A7502.

Part: CHANNEL — CORRODED (BS 500D-505 S24L) · airframe 74,617 hrs · 44,264 cycles

CORROSION FWD CARGO COMPARTMENT Z-CHANNEL S24 ; LBL22 STA 505 TO 500D ALL O/B FASTENER'S HOLES WITH LIGHT CORROSION / FABRICATED NEW Z @ FWD CARGO COMPT, S24, LBL22, STA 505-500A AS PER B737-700 SRM 51-40-05-0G-0

Part: CHANNEL — CORRODED (BS 400-420 S24R) · airframe 74,617 hrs · 44,264 cycles

CORROSION ON FWD CARGO COMPARTMENT Z-CHANNEL S24R; RBL22; STA 400 TO 420 FEW FASTENERS'S HOLES WITH LIGHT CORROSION / CHECK ALLOWABLE DAMAGE LIMITS CORROSION FASTENERS HOLES L/H Z CHANNEL FWD DAMAGE IS NOT WITHIN LIMITS AS PER B737-700 SRM FIGURE 103 DETAIL D, LOCATED AND DRILLED NEW Z CHANNEL AS PER B737-700 (53-00-53-1A-2, 51-40-05-0G-0, TREATED AND PRIMED AS PER B737-700 SRM 51-20-01-0G-0 IT WILL BE INSTALL ON AD 90-25-01(C/C E16461).

Part: CHANNEL — CORRODED (BS 727-784) · airframe 74,617 hrs · 44,264 cycles

**CORROSION** FOUND SEVERAL SPOTS OF SURFACE CORROSION AT AFT CARGO COMPT ON ZEE CHANNEL LBL 21. BETWEEN STA 727+4 THROUGH 784. / REMOVED CORROSION ON ZEE CHANNEL. FOUND OUT OF LIMITS AS PER B737-700 SRM 51-10-02-0G-0 AND BAC 1496-377 AND SRM 53-00-53-1A-2. FABRICATED NEW ZEE CHANNEL AS PER B737-700 SRM 51-40-05-0G-0 AND DWG #146A7502.

Part: CHANNEL — CORRODED (BS 727-767) · airframe 74,617 hrs · 44,264 cycles

**CORROSION** FOUND SEVERAL SPOTS OF SURFACE CORROSION AT AFT CARGO COMPT ON ZEE CHANNEL RBL 21. BETWEEN STA 727+4 THROUGH 767. / REMOVED CORROSION ON ZEE CHANNEL. FOUND OUT OF LIMITS AS PER B737-700 SRM 51-10-02-0G-0. FABRICATED NEW ZEE CHANNEL AS PER B737-700 SRM 51-40-05-0G-0 AND DWG #146A7502.

Part: WEB — CORRODED (AFT CARGO) · airframe 74,617 hrs · 44,264 cycles

**CORROSION** FOUND SURFACE CORROSION ON FLOOR STRUCTURE WEB AT AFT CARGO COMPT RBL 6 BETWEEN STA 767 THROUGH STA 787. / REMOVED AND REPLACED AFT CARGO WEB BETWEEN STA 767 THROUGH STA 787 RBL 6. AS PER B737-700 SRM 51-40-02-0G-0

Part: SCUFF PLATE — CORRODED (AFT CARGO) · airframe 74,617 hrs · 44,264 cycles

**CORROSION** AFT CARGO DOOR CUTOUT SURROUND STRUCTURE UNDER SCUFF PLATE FWD SIDE; SPOT OF LIGHT SURFACE CORROSION. DOT # 208-31 / REFFERENCE TASK CARD W216843 FOR WORK ACCOMPLISHED. PER MPM 51.03.01

Part: RIB — CRACKED (RT WING) · airframe 74,617 hrs · 44,264 cycles

R/W DEFLECTION CONTROL RIB I/B BRACKET CRACKED ON FWD SIDE. / REMOVED AND REPLACED FITTING RH DEFLECTION CONTROL RIB REF B737-700 SRM 51-40-02-0G-0

Part: GCU — FAULTY (RT GENERATOR) · airframe 74,238 hrs · 44,046 cycles

#2 ENGINE SOURCE OFF LIGHT AT 40,000 FEET APU FAULT LIGHT ON ATTEMPTED START LANDING UNEVENTFUL. DID NOT START APU AFTER LANDING. / R&R #2 ENG GCU PER AMM 24-21-81 SPU FAULT 49-41010 CHECKS GOOD PER FIM 49-40 TASK 801._RAR# 90558 POS 2 PN OFF/ON 762185H SN OFF 3732 SN ON AAA6008973

Part: STRAP — BROKEN (AFT FLASHLIGHT) · airframe 74,177 hrs · 44,013 cycles

AFT OTBD EMERGENCY FLASHLIGHT STRAP BROKEN / R & R'D AFT OTBD EMERGENCY FLASHLIGHT SHIELD IAW MM 25-64-00

Part: SLIDE — DETACHED (LT FWD DOOR) · airframe 74,055 hrs · 43,936 cycles

LEFT FWD SLIDE VELCRO DETATCHED. SECURED VELCRO ON LT FWD DOOR, PER SIP.

Part: FIXTURE — BROKEN (EMERGENCY LIGHT) · airframe 73,052 hrs · 43,341 cycles

CENTER ISLE EXIT LIGHT FIXTURE BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-04.

Part: STRINGER SPLICE — CORRODED (BS 360) · airframe 71,804 hrs · 42,557 cycles

STRINGER SPLICE CORRODED AT BS. 360+5, STR. 25L. / REPAIRED SPLICE PER EA.

Part: STRINGER — CORRODED (BS 360) · airframe 71,804 hrs · 42,557 cycles

STRINGER CORRODED AT BS. 360+5, STR. 25L. / REPAIRED STRINGER PER ER AND EA.

Part: BALLAST — FAULTY (CABIN) · airframe 70,558 hrs · 41,782 cycles

CREW REPORTED BURNING PLASTIC SMELL IN CABIN THROUGHOUT FLIGHT. R&R FORWARD ENTRY LIGHTS BALLASTS PER AMM.

Part: BALLAST — FAULTY (CABIN) · airframe 70,558 hrs · 41,782 cycles

CREW REPORTED BURNING PLASTIC SMELL IN CABIN THROUGHOUT FLIGHT. R&R AFT ENTRY LIGHTS BALLASTS PER AMM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 70,376 hrs · 41,653 cycles

PANEL 193 B HAS DELAMINATION ON THE CORNER AT FASTENER LOCATION 7 MEASURING 1.5'X1.25'. / REMOVED AND REPLACED 193B PANEL PER AMM 53-81-21.

Part: PANEL — CORRODED (LOWER EXT FUSELA) · airframe 70,376 hrs · 41,653 cycles

PANEL 193 B HAS EDGE CORROSION ON CORNERS AT FASTENER LOCATIONS 1;26; AND 33. MEASURMENTS AT LOCATION 1 IS 1.0'; LOCATION 26 (CORNER) .75'X.5' AND LOCATION 33 IS .75'. / REMOVED AND REPLACED 193B PANEL PER 53-51-21

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 70,376 hrs · 41,653 cycles

PANEL 193B HAS DELAMINATION ON THE LOCATE AT FASTENER CORNER AT FASTENER LOCATION 20 MEASURING 1'X 1' / REMOVED AND REPLACED 193B PANEL PER AMM 53-51-21.

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 70,122 hrs · 41,490 cycles

FORWARD ENTRY SLIDE VELCRO COVER LOOSE. REPOSITIONED SLIDE DEPLOY HANDLE COVER IAW AMM.

Part: ESCAPE ROPE — DISCONNECTED (COCKPIT) · airframe 70,066 hrs · 41,458 cycles

FIRST OFFICERS ESCAPE ROPE DISCONNECTED. REATTACHED ROPE PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1674. R&R BATTER PACK PER AMM.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1674. / R&R POWER SUPPLY PER AMM.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1674. R&R POWER SUPPLY PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1670. R&R BATTERY PACK PER AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS L7 AND L1188 INOPERATIVE DURING EMERGENCY LIGHT TEST AT M1669. R&R BAD FUSE IN BATTERY PACK M1669 PER AMM.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1670. / R&R POWER SUPPLY PER AMM.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1668. R&R POWER SUPPLY PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,708 hrs · 41,221 cycles

EMERGENCY LIGHTS FAILED OPERATIONAL TEST AT UNIT M1668. R&R BATTER PACK PER AMM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 69,708 hrs · 41,221 cycles

PANEL 193AR HAS DELAMINATION ON THE INNER SURFACE CORE AREA / PANEL 193AR WITH DELAMINATION ON THE INNER SURFACE CORE AREA WAS REPAIRED IAW SRM 51-70-05-2R-2

Part: FLOOR SUPPORT — CORRODED (BS 787-794) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS.787 TO BS. 794, RBL 23. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: PANEL — ELONGATED (VERTICAL STABILI) · airframe 69,708 hrs · 41,221 cycles

VERTICAL FIN L/E PANEL 322B HAS ELONGATED FASTENER HOLE ON L/H SIDE AT L/E STA 314.2 / VERTICAL FIN L/E PANEL FASTENER HOLE ON L/H SIDE AT L/E STA 314.2 WAS REPAIRED ON ATS COMPONENTS JOB#523817; CUSTOMER RO# 0550028-D8R.

Part: DOOR SILL — CORRODED (R1 AREA) · airframe 69,708 hrs · 41,221 cycles

R1 DOOR CUTOUT UPPER AUXILIARY SILL INNER CHORD CORRODED OUTBOARD SURFACE BETWEEN BS. 277+3 TO BS. 277+9, STR. 5R. / REPAIRED CHORD PER ER AND EA.

Part: SKIN — DAMAGED (BS 207) · airframe 69,708 hrs · 41,221 cycles

PRESSURIZED SKIN DAMAGED AT BS. 207, R/H SIDE 9 IN ABOVE FORWARD ELECTRONIC AND EQUIPMENT BAY CUTOUT. / REPAIRED SKIN PER EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,708 hrs · 41,221 cycles

L/H HORIZONTAL STABILIZER RIB AT STAB. STA. 120.30, CRACKED AT 3RD VERTICAL STIFFENER LOWER RADIUS. / REPAIRED RIB IAW SRM.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 21. / R&R SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 69,708 hrs · 41,221 cycles

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

Part: CLEVIS — CORRODED (RT WING) · airframe 69,708 hrs · 41,221 cycles

***CORROSION*** RT WING O/B NO STEP PANEL FWD ATTACH ROD CLEVISES CORRODED AND ROD WORN / REMOVED AND REPLACED NEW RT WING O/B NO STEP PANEL FWD ATTACH ROD IAW SOPM #20-50-01 AND AIPC #57-50-00-36 51609U 26MAY19

Part: RETAINER — CRACKED (RT WING) · airframe 69,708 hrs · 41,221 cycles

RT WING VERTICAL SEAL RETAINER AT TRANS WEB CRACKED / REMOVED AND REPLACED NEW RT WING VERTICAL SEAL RETAINER AT TRANS WEB IAW SRM # 51-40-02-0G-0 AND AIPC # 57-50-00-25. 57609U 24MAY19

Part: SUPPORT — CORRODED (BS 727-847) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 21. / R&R PANEL IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,708 hrs · 41,221 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET PER SRM AND DWG.

Part: CHANNEL — CORRODED (BS 360) · airframe 69,708 hrs · 41,221 cycles

STRINGER TIE CORRODED AT BS. 360, STR. 28L. / R&R "U" CHANNEL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887 TO BS. 947, RBL 21. R&R SUPPORT PER DWG & SRM.

Part: SUPPORT FITTING — CORRODED (AFT CARGO BAY) · airframe 69,708 hrs · 41,221 cycles

***CORROSION*** ON GRAY WATER DRAIN DOUBLER IN AREA AFT OF ACB STA 986+7 LBL 19 WL 183 / REMOVED & REPLACED GRAY WATER DRAIN SUPPORT FITTING IN AFT OF ACB STA 986+7 LBL 19 WL183 IAW SRM 51-40-02-0G-0

Part: FLOOR SUPPORT — CRACKED (BS 500D) · airframe 69,708 hrs · 41,221 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE AT CRACKED BS. 500B, LBL 25. / R&R ANGLE PER DWG & SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,708 hrs · 41,221 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM AND DWG.

Part: SUPPORT — CORRODED (BS 947) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS. 947, BETWEEN RBL 6 TO RBL 20. / R&R SUPPORT IAW DWG & SRM.

Part: NUT PLATE — CORRODED (BS 795) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY INTERCOSTAL, NUT PLATE STRAP CORRODED AT BS. 795, RBL 20. R&R PLATE STRAP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 400) · airframe 69,708 hrs · 41,221 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS. 400, LBL 25. / R&R ANGLE PER DWG & SRM.

Part: CARGO TRACK — CORRODED (BS 790) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY CARGO TRACK TIE DOWN CORRODED AT BS. 790, LBL 17. / R&R TRACK TIE DOWN IAW SRM & DWG.

Part: SUPPORT BRACKET — CORRODED (AFT CARGO BAY) · airframe 69,708 hrs · 41,221 cycles

***CORROSION*** ON WATER TANK DRAIN VALVE SUPPORT BRACKET LOCATED AT 947+1 WL 177 BL 0 / REMOVED AND REPLACED DRAIN VALVE SUPPORT BRACKET PN HFAB53-BR-01 AT STA 947+1 WL 177 BL0 IAW DWG 147A9100; SRM 51-40-02

Part: CLEVIS — CORRODED (RT WING) · airframe 69,708 hrs · 41,221 cycles

***CORROSION*** RT WING O/B NO STEP PANEL AFT ATTACH ROD CLEVISES CORRODED AND ROD WORN / REMOVED AND REPLACED RT WING O/B NO STEP PANEL AFT ATTACH ROD PER SOPM 20-50-01 57006U 24MAY19

Part: SUPPORT — CORRODED (BS 767-794) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 794, RBL 21. / R&R SHIELD IAW SRM AND DWG.

Part: WEB — CORRODED (BS 794-847) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 794 TO BS. 847, RBL 25. / R&R THRESHOLD WEB IAW SRM AND DWG.

Part: SUPPORT ROD — CORRODED (RT WING) · airframe 69,708 hrs · 41,221 cycles

RT WING AFT ATTACH SUPPORT ROD JUST OUTBOARD OF MAIN LANDING GEAR BEAM FITTING CLEVISES CORRODED. R&R SUPPORT ROD IAW SOPM.

Part: STRINGER CLIP — CORRODED (BS 360) · airframe 69,708 hrs · 41,221 cycles

STRINGER TIE CORRODED AT BS. 360, STR. 28L. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,708 hrs · 41,221 cycles

FORWARD CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE CORRODED AT BS. 500D, BETWEEN BL 0 TO LBL 23. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (BS 867-947) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY BULKHEAD AFT LOWER PANEL SUPPORT CORRODED BETWEEN BS. 867 TO BS. 947, LBL 10. / R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. R&R SUPPORT PER DWG & SRM.

Part: STRAP — CORRODED (BS 794-827) · airframe 69,708 hrs · 41,221 cycles

AFT CARGO BAY TENSION STRAP CORRODED BETWEEN BS. 794 TO BS. 827, RBL 20. / R&R STRAP IAW SRM AND DWG.

Part: SUPPORT ROD — CORRODED (RT WING) · airframe 69,708 hrs · 41,221 cycles

RT WING FORWARD ATTACH SUPPORT ROD JUST OUTBOARD OF MAIN LANDING GEAR BEAM FITTING CLEVISES CORRODED. R&R SUPPORT ROD IAW SOPM.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 69,708 hrs · 41,221 cycles

PANEL 195CR HAS AN ELONGATED FASTENER HOLE / PANEL 195CR WITH AN ELONGATED FASTNER HOLE WAS REPAIRED IAW SRM 51-70-04-2R-9 57545U 5-31-19

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 69,708 hrs · 41,221 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 30 TO LBL 60. / REPAIRED DECK PER SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 69,708 hrs · 41,221 cycles

ACB FWD AND AFT SCUFF PLATE ARE CRACKED / RECIVED FWD AND AFT SCUFF PLATE; ACB AND LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 WILL BE INSTALL WITH CARD# 753-721-00-01 59205U 27MAY19

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,708 hrs · 41,221 cycles

FCB FWD AND AFT SCUFF PLATES ARE CRACKED / RECEIVED NEWS PARTS WITH P/N 654A0004-337 FWD SIDE P/N 654A0004-338 AFT SIDE LOCATED AND DRILLED CORNER SCUFF PLATES IAW SRM 51-40-05; FWD AND AFT CORNER SCUFF PLATE WILL BE ISNTALLED WITH CARD #753-646-62-01. 59202U 21MAY19.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,708 hrs · 41,221 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN RBL 30 TO RBL 60. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (BS 312) · airframe 69,708 hrs · 41,221 cycles

FRAME CRACKED JUST ABOVE L1 DOOR AT BS. 312, APPROX. WL 283. / REPAIRED FRAME IAW EA AND ER.

Part: WEB — CORRODED (BS 441-492) · airframe 69,708 hrs · 41,221 cycles

FORWARD CARGO DOORWAY LOWER THRESHOLD SUB WEB CORRODED BETWEEN BS. 441 TO BS. 492, BETWEEN RBL 23 TO RBL 30. / R&R THRESHOLD WEB IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,708 hrs · 41,221 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 24.5. R&R FLOOR SUPPORT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,708 hrs · 41,221 cycles

LT WING LEADING EDGE #4 SLAT NOSE SKIN CRACKED AROUND FASTENER AT LOWER SURFACE OF THE AT ACTUATOR RIBS. REPAIRED SKIN IAW SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,646 hrs · 41,173 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION AND AC POWER BEING SUPPLIED. REMOVED AND REPLACED A/C BATTERY PER AMM 24-31-11

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHTS) · airframe 69,646 hrs · 41,173 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION AND AC POWER SUPPLIED / FOUND DEFECTIVE AFT F/A PANEL REMOVED AND REPLACED AFT F/A PANEL PER AMM

Part: HANDLE — CRACKED (R2 DOOR) · airframe 69,531 hrs · 41,097 cycles

R2 DOOR HANDLE CRACKED. R&R ASSIST HANDLE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 68,750 hrs · 40,574 cycles

LT OVERWING EMERGENCY EXIT LIGHT ADJACENT EXIT DOOR LENS LOOSE. R&R LIGHT ASSEMBLY PER AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 68,404 hrs · 40,365 cycles

RT PHOTOLUMINESCENT LIGHT STRIP DAMAGED AT SECTION 1. R&R LIGHT STRIP PER AMM.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,497 hrs · 39,800 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,497 hrs · 39,800 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 67,468 hrs · 39,785 cycles

AIR TURNBACK, DURING CLIMB OUT AT APPROXIMATELY 21,000 CABIN WARNING HORN CAME ON-CABIN APPROXIMATELY 10-11000FT. DESCENDED AND RETURNED TO PHX. R&R NR 2 ENGINE HIGH STAGE REGULATOR PER MM.

Part: SHUTOFF VALVE — LEAKING (BLEED AIR SYS) · airframe 67,468 hrs · 39,785 cycles

AIR TURNBACK, DURING CLIMB OUT AT APPROXIMATELY 21,000 CABIN WARNING HORN CAME ON-CABIN APPROXIMATELY 10-11000FT. DESCENDED AND RETURNED TO PHX. R&R NR 2 PRESSURE REGULATORY SHUTOFF VALVE PER MM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 67,468 hrs · 39,785 cycles

AIR TURNBACK, DURING CLIMB OUT AT APPROXIMATELY 21,000 CABIN WARNING HORN CAME ON-CABIN APPROXIMATELY 10-11000FT. DESCENDED AND RETURNED TO PHX. R&R NR 1 ENGINE HIGH STAGE REGULATOR PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,391 hrs · 39,729 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1670. R&R BATTERY PACK PER AMM.

Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 67,391 hrs · 39,729 cycles

FUSELAGE MAIN GEAR WHEEL WELL LOWER ATTACH BRACKET CRACKED AT BS 663.75, RBL 28.73. INSTALLED BRACKET PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,391 hrs · 39,729 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,391 hrs · 39,729 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1673. R&R BATTERY PACK PER AMM.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 67,391 hrs · 39,729 cycles

FUSELAGE MAIN GEAR WHEEL WELL LOWER ATTACH BRACKET CRACKED AT BS 663.75, LBL 28.73. R&R BRACKET PER SRM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 67,391 hrs · 39,729 cycles

RIGHT HORIZONTAL STAB FWD LOWER SLIDER CRACKED. / R&R RIGHT HORIZONTAL STAB FWD LOWER SLIDER PER AMM 53-31-31.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,391 hrs · 39,729 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1672. R&R BATTERY PACK PER AMM.

Part: RETAINER — CRACKED (LEFT WING) · airframe 65,209 hrs · 38,306 cycles

LEFT WING FIXED UPPER TRAILING EDGE PANEL AFT SEAL RETAINER INBD OF DEFLECTION RIB CRACKED / REMOVED AND REPLACED PER SRM 51-40-02

Part: BEAM — BROKEN (RT WING) · airframe 65,142 hrs · 38,263 cycles

SUPPLEMENTAL INFORMATION: RIGHT WING AFT OUTBOARD FLAP I/B SEAL BEAM BROKEN / R&R'D SEAL BEAM PER IPC 57-50-00; SRM 57-51-02

Part: SIGN — MISSING (CABIN) · airframe 64,460 hrs · 37,816 cycles

RT EMERGENCY OVERWING EXIT SIGN MISSING. INSTALLED SIGN IAW AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 63,284 hrs · 37,070 cycles

L/H STAB. LOWER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED PER AMM 53-31-31.

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 63,284 hrs · 37,070 cycles

VERTICAL STAB PANEL 324AR LOWER RETAINER; WHICH SECURES PANEL TO STRUCTURE IS CRACKED. / REMOVED AND REPLACED LOWER RETAINER REF SRM 51-40-02.

Part: PAN — CRACKED (ASD) · airframe 63,284 hrs · 37,070 cycles

AFT GALLEY SERVICE DOOR LOWER PAN ASSEMBLY CRACKED. / R&R'D PAN ASSY PER SIP

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,282 hrs · 37,069 cycles

CENTER SECTION OF AFT CARGO SCUFF PLATE CRACKED. / REMOVED AND REPLACED SCUFF PLATE REF AMM 53-11-02.

Part: BUSHING — BROKEN (RT MLG) · airframe 63,212 hrs · 37,028 cycles

RIGHT MAIN LANDING GEAR HANGER LINK FORWARD LOWER BUSHING BROKEN. R & R THE BUSHING IAW EA AND AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 63,212 hrs · 37,028 cycles

AFT GALLEY AREA LT FLASHLIGHT STRAP BROKEN. R & R STRAP IAW CMM.

Part: WEB — CRACKED (LT WING) · airframe 63,212 hrs · 37,028 cycles

LEFT WING TRAILING EDGE WEB ASSEMBLY CRACKED AT WBL 201.90. R & R WEB IAW DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 63,212 hrs · 37,028 cycles

RT WING FLAP TRACK FAIRING 644BB CRACKED AT INTERNAL AREA. REPAIRED FAIRING IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

FORWARD CARGO COMPARTMENT CHANNEL SIDE PLATE CORRODED BETWEEN BS 480 TO BS 500D, LBL 21.8. R&R CHANNEL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

FORWARD CARGO COMPARTMENT CHANNEL SIDE PLATE CORRODED BETWEEN BS 500A TO BS 500D, RBL 21.8. R&R CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,212 hrs · 37,028 cycles

RIGHT WING TRAILING EDGE ANGLE CRACKED ON WBL 201.90. R & R THE ANGLE IAW SRM.

Part: ANGLE — CRACKED (BS 344-360) · airframe 63,212 hrs · 37,028 cycles

WEB ANGLE CRACKED BETWEEN BS 344 TO 360, BL 0. R & R THE WEB ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN LBL 43 AND RBL 43. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (BS 312-328) · airframe 63,212 hrs · 37,028 cycles

FUSELAGE WEB CRACKED AT BS 312 TO 328, RBL 31. R & R THE WEB IAW SRM.

Part: ATTACH ANGLE — CRACKED (BS 277) · airframe 63,212 hrs · 37,028 cycles

STRINGER 10R ATTACH ANGLE CRACKED AT BS. 277. R & R THE ATTACH ANGLE IAW SRM & DWG.

Part: STRUCTURE — CORRODED (BS 312-328) · airframe 63,212 hrs · 37,028 cycles

INNER STRUCTURE CORRODED BETWEEN BS 312 TO 328, RBL 55. R & R THE STRUCTURE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (BS 328) · airframe 63,212 hrs · 37,028 cycles

FORWARD GALLEY AREA FLOORBEAM UPPER TEE CRACKED AT BS 328, RBL 22. REPAIRED THE FLOORBEAM TEE IAW EA.

Part: ANGLE — CRACKED (BS 344-360) · airframe 63,212 hrs · 37,028 cycles

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

Part: ANGLE — CRACKED (BS 277-294) · airframe 63,212 hrs · 37,028 cycles

WEB ANGLE CRACKED BETWEEN BS 277 TO 294.5, BL 0. R & R THE WEB ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

FLOORBEAM CHORD CRACKED AT BS 294.5, RBL 51. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

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

Part: WEB — CRACKED (BS 312-328) · airframe 63,212 hrs · 37,028 cycles

FUSELAGE WEB CRACKED AT BS 312 TO 328, LBL 45. R & R THE WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED BETWEEN BS 907 TO BS 927, BETWEEN STR 25R TO STR 27R. R&R ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (BS 947.5) · airframe 63,212 hrs · 37,028 cycles

AFT CARGO BAY FITTING CRACKED AT BS 947.5, STRINGER 25L. R & R THE FITTING IAW SRM AND DWG.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 63,212 hrs · 37,028 cycles

AFT GALLEY AREA LAVATORY B WALL EXIT SIGN BROKEN. R & R THE SIGN IAW AMM.

Part: CARGO TRACK — CRACKED (BS 747-767) · airframe 63,212 hrs · 37,028 cycles

AFT CARGO BAY CARGO TRACK CRACKED BETWEEN BS 747 TO 767. REPAIRED THE CARGO TRACK IAW SRM.

Part: CARGO TRACK — CORRODED (BS 787-867) · airframe 63,212 hrs · 37,028 cycles

AFT CARGO BAY TRACK CORRODED BETWEEN BS 787 TO 867, BETWEEN RBL 13 TO 80. R & R THE CARGO TRACK IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727E-767) · airframe 63,212 hrs · 37,028 cycles

AFT CARGO BAY SUPPORT ZEE CORRODED BETWEEN BS 727E TO 767, STRINGER 25R. R & R THE SUPPORT ZEE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,212 hrs · 37,028 cycles

FUSELAGE INTERCOSTAL CRACKED AT STA 927 TO STA 948, STR 25R. REPAIRED INTERCOSTAL PER SRM.

Part: SUPPORT — CORRODED (BS 727D-807) · airframe 63,212 hrs · 37,028 cycles

AFT CARGO BAY SUPPORT ZEE CORRODED BETWEEN BS 727D TO 807, STRINGER 25L. R & R THE SUPPORT ZEE IAW SRM.

Part: SKIN — CRACKED (BS 235) · airframe 63,212 hrs · 37,028 cycles

EXTERNAL GROUND ELECTRICAL POWER ACCESS DOOR LOWER FUSELAGE CUTOUT CRACKED AT BS 235.8. REPAIRED THE SKIN IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 63,210 hrs · 37,027 cycles

RT WING REAR SPAR LOWER VAPOR WEB BAY CRACKED VERTICAL. / REPAIRED WEB PER SRM.

Part: STIFFENER — FAILED (BS 663) · airframe 63,210 hrs · 37,027 cycles

BULKHEAD WEB CROSS BRACE SEVERED BETWEEN RBL 6.15 AND RBL 31.83. R & R STIFFENER IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,873 hrs · 36,820 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R&R SLIDE PER MT.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,763 hrs · 36,155 cycles

R1 DOOR NR 5 BEAM CRACKED. R&R DOOR PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 61,631 hrs · 36,081 cycles

FORWARD EMERGENCY BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: CONTROL HANDLE — DIRTY (COCKPIT) · airframe 59,928 hrs · 35,058 cycles

ALL LANDING GEAR INDICATED BOTH GREEN & RED LIGHTS ON FIRST APPROACH, WENT AROUND, CYCLED GEAR. CLEANED GEAR HANDLE IAW MM.

Part: LENS — MISSING (CABIN) · airframe 58,249 hrs · 34,105 cycles

RIGHT OVERWING EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 57,873 hrs · 33,858 cycles

AFT MOUNTED CTR AISLE EMER SIGN LIGHT LENS COVER FELL OFF. R & R SIGN ASSEMBLY IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,421 hrs · 33,609 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,112 hrs · 33,439 cycles

FOUND AN EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 11 ABC. REPLACED THE LAMP IAW MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

WEB CRACKED AT STATION 235 TO 260, STRINGER 7L. R & R WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SUPPORT ANGLE CRACKED AT STATION 500D, RT SIDE, WBL 76. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

WEB CRACKED AT STATION 794.3, STRINGER 25R. R & R WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

LOWER WEB CRACKED AT LT ACFT BAY AREA, STATION 661. REPAIRED WEB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,112 hrs · 33,439 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON LOWER SIDE AT STAB STATION 92.70, 29" AFT TO FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,112 hrs · 33,439 cycles

LEFT HORIZONTAL STABILIZER LOWER SIDE OF RIB CRACKED AT STAB STATION 92.70, 11" AFT TO FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,112 hrs · 33,439 cycles

FOUND THE LEFT HORIZONTAL STAB RIB CRACKED AT HSS 120.30 FRONT SPAR. REPAIRED THE RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,112 hrs · 33,439 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON LOWER SIDE AT STAB STATION 92.70, 39" AFT TO FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,112 hrs · 33,439 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON LOWER SIDE AT STAB STATION 92.70, 20" AFT TO FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,112 hrs · 33,439 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 101.90, BETWEEN 9.5" TO 37. REPAIRED RIB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 867, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 500C, STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 867, STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FUSELAGE FRAME CRACKED AT STATION 500C, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EO & EA.

Part: SEAT TRACK — CRACKED (BS 727A) · airframe 57,112 hrs · 33,439 cycles

FOUND THE SEAT TRACK CRACKED AT BS 727A+18, RBL 45.5. REPAIRED THE SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK OTBD FLANGE CRACKED AT BS 727A+18, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK INBD FLANGE FLOOR BEAM UPPER CHORD CRACKED AT BS 727A+17, LBL 24.5. REPAIRED CHORD IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK INBD & OTBD FLANGE FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FLOORBEAM WEB CRACKED AT BS 727B, RBL 24.5. REPAIRED WEB IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK INBD & OTBD FLANGE FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 727A+17 TO 727A+18, LBL 24.5. REPAIRED CHORD IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK OTBD & INBD FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

FLOORBEAM WEB CRACKED AT BS 727B, LBL 45.5. REPAIRED WEB IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK INBD & OTBD FLANGE FLOORBEAM UPPER CHORD CRACKED AT BS 727+18, RBL 24.5. REPAIRED CHORD IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK INBD & OTBD FLANGE CRACKED AT BS 727B, RBL 24.5. REPAIRED SEAT TRACK IAW EO & EA.

Part: SEAT TRACK — CRACKED (BS 727A) · airframe 57,112 hrs · 33,439 cycles

FOUND THE SEAT TRACK CRACKED AT BS 727A+18, RBL 45.5. REPAIRED THE SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (BS 727A) · airframe 57,112 hrs · 33,439 cycles

FOUND THE SEAT TRACK CRACKED AT BS 727A+17, RBL 45.5. REPAIRED THE SEAT TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,112 hrs · 33,439 cycles

SEAT TRACK INBD & OTBD FLANGE FLOORBEAM UPPER CHORD CRACKED AT BS 727A+18, LBL 45.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,112 hrs · 33,439 cycles

LEFT WING LE SLAT SKIN CRACKED AT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,112 hrs · 33,439 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 13 TO 50. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,112 hrs · 33,439 cycles

LEFT WING LE SLAT SKIN CRACKED AT STATION 451.97. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,112 hrs · 33,439 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 13 TO 50. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,112 hrs · 33,439 cycles

RIGHT WING, LT SLAT SKIN CRACKED AT STATION 202.45. REPAIRED SKIN IAW SUM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,112 hrs · 33,439 cycles

RIGHT WING LE SLAT SKIN CRACKED AT STATION 332.71. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,112 hrs · 33,439 cycles

RIGHT WING LE SLAT SKIN CRACKED AT STATION 85.1. REPAIRED SKIN IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,344 hrs · 33,009 cycles

OVERWING EXIT CEILING LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 55,499 hrs · 32,508 cycles

LEFT CTR EMER BATTERY PACK FAILED THE CAPACITY TEST. R & R BATTERY IAW AMM.

Part: RIB — BROKEN (RT WING) · airframe 55,499 hrs · 32,508 cycles

RIGHT WING TRAILING FIXED FAIRING SUPPORT CASTING BROKEN. R & R RIB IAW DWG.

Part: BATTERY — FAILED (CABIN) · airframe 55,499 hrs · 32,508 cycles

AFT RT EMER BATTERY PACK FAILED THE CAPACITY TEST. R & R BATTERY IAW AMM.

Part: FLAP — LOOSE (RT WING) · airframe 55,235 hrs · 32,355 cycles

RIGHT WING OTBD AFT FLAP LOOSE. R & R AFT FLAP IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,683 cycles

LEFT BULKHEAD CHORDS SKIN DOUBLER CRACKED AT BS 540, STRINGER 22L. REPAIRED DOUBLER IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,683 cycles

LEFT BULKHEAD CHORDS CRACKED AT BS 540, STRINGER 22L. REPAIRED CHORD IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,683 cycles

RIGHT LOWER CHORD SKIN DOUBLER CRACKED AT BS 540. REPAIRED DOUBLER IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,683 cycles

RIGHT LOWER CHORD SKIN DOUBLER CRACKED AT BS 540, STRINGER 22R. REPAIRED DOUBLER IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 53,316 hrs · 31,248 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 53,084 hrs · 31,118 cycles

L1 DOOR SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: SENSOR — FAULTY (TE FLAP) · airframe 52,307 hrs · 30,659 cycles

DECLARED EMERGENCY SELECTED FLAPS 15 & NOTICED TE FLAPS SPLIT & STOPPED WITH RT FLAP AT 2 DEGREE. LT FLAP AT 3 DEGREE. R & R NR 8 FLAP SKIN SENSOR T532 IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 50,862 hrs · 29,797 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 50,618 hrs · 29,660 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSY IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,520 hrs · 29,606 cycles

LT WING OTBD AFT FLAP, INBD CORNER EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,520 hrs · 29,606 cycles

LEFT WING OTBD AFT FLAP INBD CORNER EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,520 hrs · 29,606 cycles

LEFT FLIGHT DECK WINDOW FRAME FASTENER HOLE CRACKED AT NR 8 FASTENER BETWEEN E-F POST. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,520 hrs · 29,606 cycles

NR 3 CO-PILOT WINDOW, FWD FRAME CRACKED IN NR 7 HOLE. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,520 hrs · 29,606 cycles

NR 3 CO-PILOT WINDOW, FWD FRAME CRACKED IN #5 HOLE. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,520 hrs · 29,606 cycles

RIGHT FLIGHT DECK WINDOW FRAME FASTENER HOLE CRACKED AT NR 8 FASTENER BETWEEN E-F POST. REPAIRED FRAME IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 50,520 hrs · 29,606 cycles

LEFT OVERHEAD BIN BULLNOSE LIGHT LENS LOOSE AT ROW 17. SECURED LENS IAW MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 49,041 hrs · 28,733 cycles

FWD ENTRY DOOR EMERGENCY SLIDE SHOWS LOW PRESSURE. REPLACED FWD ENT SLIDE ASSY PER AMM AND MT 325-61-06 ICT 657406 POS:F/E P/N OFF/ON:63550-101 S/N OFF:0205F S/N ON:0216F.

Part: BATTERY — FAILED (CABIN) · airframe 48,958 hrs · 28,686 cycles

THREE EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. CTR RT, ROW 16 LT, AFT LT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES CTR RT-M01669, ROW 16 LT-M01670 AND AFT LT-M01673, PER M/M AND SSM.

Part: GATE — CRACKED (L2 DOOR) · airframe 48,958 hrs · 28,686 cycles

FUSELAGE AFT ENTRY DOOR LOWER GATE IS CRACKED AT AFT FASTENER VERTICAL TO EDGE. INSTALLED AFT ENTRY DOOR LOWER GATE ASSY PER MM, NO LEAKS NOTED.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 48,958 hrs · 28,686 cycles

CRACKED AT I/B FASTENER AND BEAM RADIUS. REMOVED AND REPLACED DOOR PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,704 hrs · 27,333 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CHECK AT 16L. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,704 hrs · 27,333 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CHECK AT AFT LEFT CABIN. REMOVED AND REPLACED LEFT AFT EMERGENCY LIGHT BATTERY PACK PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,704 hrs · 27,333 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CHECK AT FWD LEFT CABIN. REMOVED AND REPLACED BATTERY & CHARGER PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,704 hrs · 27,333 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CHECK AT CENTER RIGHT CABIN. REMOVED AND REPLACED RIGHT AFT EMERGENCY LIGHT BATTERY PACK PER AMM.

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 46,481 hrs · 27,192 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED HOOKS PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 43,749 hrs · 25,613 cycles

MID CABIN EMERGENCY EXIT COVER LOOSE. INSTALLED COVER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, FLOORBEAM CRACKED AT BS 540, BETWEEN RBL 0 TO RBL 24. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME PER SRM.

Part: SKIN — CANNING (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN OIL CANNED AT BS 480+10, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, LT HORIZONTAL STABILZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 40.87. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 6.17. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 32.40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 32.40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 40.87. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, LT HORIZ STAB LOWER SKIN CRACKED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, FLOORBEAM CORRODED AT BS 344, RBL 3. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, FLOORBEAM CORRODED AT BS 328, LBL 22. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK FOUND, FRAME CRACKED AT BS 787, BETWEEN STR 7L TO STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,739 hrs · 25,607 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT FRAME CRACKED AT BS 500A, BETWEEN STR 7R TO STR 8R. REPAIRED FRAME PER SRM.

Part: SIGN — CRACKED (CABIN) · airframe 43,545 hrs · 25,499 cycles

RT WING EMERGENCY EXIT DOOR LOWER SIGN CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 42,610 hrs · 24,960 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,513 hrs · 24,908 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 178, STR 4R. REPAIRED SKIN PER EA.

Part: BATTERY — FAILED (CABIN) · airframe 42,512 hrs · 24,907 cycles

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

Part: CHARGER — FAILED (CABIN) · airframe 42,512 hrs · 24,907 cycles

DURING SCHEDULED HC1 CHECK, AFT RT EMERGENCY EXIT BATTERY PACK FAILED. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 40,330 hrs · 23,619 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EVAC SLIDE FWD GIRT BAR FITTING LOOSE. TIGHTENED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 40,330 hrs · 23,619 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR FITTING LOOSE. TIGHTENED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 40,330 hrs · 23,619 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EVAC SLIDE FWD GIRT BAR FITTING LOOSE. TIGHTENED FITTING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,943 hrs · 22,120 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT DOOR WINDOW LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LUG — CORRODED (LT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B LOWER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING O/B LOWER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B UPPER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING I/B LOWER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING LOWER I/B LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING O/B UPPER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING UPPER I/B LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,495 hrs · 20,612 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING I/B UPPER LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,115 hrs · 19,111 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,806 hrs · 18,938 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,773 hrs · 18,910 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,404 hrs · 18,102 cycles

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

Part: SLIDE — LOOSE (L1 DOOR) · airframe 30,301 hrs · 17,447 cycles

L1 DOOR EVAC SLIDE LOOSE. SECURED SLIDE ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,217 hrs · 17,394 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 27. REPAIRED FLOORBEAM PER ER.

Part: FITTING — CORRODED (L1 DOOR) · airframe 30,217 hrs · 17,394 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. R&R GIRT BAR FITTING PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 29,958 hrs · 17,240 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,615 hrs · 16,452 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 26,244 hrs · 15,089 cycles

DURING SCHEDULED HC2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS FAIL LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LATCH — BROKEN (L2 DOOR SLIDE) · airframe 26,142 hrs · 15,030 cycles

FOUND L2 DOOR EMERGENCY EVAC SLIDE LOWER RELEASE LATCH BROKEN. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,673 hrs · 13,599 cycles

DURING SCHEDULED RON CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — DELAMINATED (AFT CABIN) · airframe 21,868 hrs · 12,569 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EEPLS STRIP DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 20,329 hrs · 11,691 cycles

DURING SPV, FOUND 2 EACH BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 10 DEF AND ROW 19 ABC, LOOSE. SECURED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 18,135 hrs · 10,457 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 16,437 hrs · 9,571 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT LENS OUT IN OVERHEAD NEAR SEAT ROW 13 ABC. REINSTALLED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 11,398 hrs · 6,742 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 15,379 hrs · 8,980 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: PIN — BENT (CONNECTOR) · airframe 9,566 hrs · 5,733 cycles

WITH LANDING GEAR HANDLE IN UP OR OFF POSITION, GOT RED NOSE GEAR LIGHT. WITH LANDING GEAR HANDLE IN DOWN POSITION, GOT THREE GREEN LIGHTS ON OVERHEAD PANEL AND FORWARD PANEL, PLUS THREE RED LIGHTS ON FWD PANEL. FOUND DAMAGED PINS IN CONNECTOR D 10982. REMOVED AND REPLACED PINS PER MM.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 5,401 hrs · 3,315 cycles

DURING SCHEDULED A1 CHECK, FOUND .5 EXTERNAL SKIN CRACK ON L/H VERTICAL STAB PITOT CUTOUT. REPAIRED VERTICAL STAB SKIN PER RA 1-755-0382.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,204 hrs · 3,193 cycles

AIR TURNBACK. AFTER TAKEOFF, HOT OIL SMELL IN COCKPIT. PERFORMED ENGINE RUN, BLEED OPS CHECK, COOLING FAN OPS CHECKS, WINDOW HEAT OPS CHECK, CONTROL CABIN LIGHTING OPS CHECK, APU BLEED OPS CHECK PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 4,434 hrs · 2,709 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: DOOR — UNSECURED (PAX DOOR)

AIRCRAFT WOULD NOT PRESSURIZE PROPERLY AFTER TAKEOFF. PRESS LEAK AROUND FWD ENTRY DOOR, DOOR INDICATION LIGHTS NORMAL. FOUND FWD ENTRY DOOR NOT PROPERLY CLOSED AROUND AFT EDGE. OPERATED DOOR, OPS CK GOOD PER MM.