N791AS

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 55,665 hrs · 31,248 cycles

EXIT SIGN AIRCRAFT LEFT BETWEEN ROW 16 & 17 BROKEN. ACFT GROUNDED. FOUND EXIT LIGHT COVER ABOVE OVERWING EXIT BETWEEN ROW 16 & 17 ON LT SIDE CAME OFF. INSTALLED COVER AND SECURED.

Part: HINGE FITTING — WORN (L1 DOOR) · airframe 55,140 hrs · 30,912 cycles

L1 DOOR UPPER HINGE FITTING, HAS ELONGATED MOUNTING HOLES FOR BOTH CAM PLATES. ACFT GROUNDED. UPPER HINGE FITTING REPLACED. REPLACED IAW SRM 51-40-02 AND DWG 65-17684.

Part: SHEAR TIE — CORRODED (BS 1006) · corrosion level 2 · airframe 55,136 hrs · 30,911 cycles

DURING CLEANING, AFT EQUPMENT FOUND SHEAR TIE AT S 1006, STR 27R-27L CORRODED ON THE AFT SIDE. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101, DETAIL II. R & R THE SHEAR TIE IAW SRM 51-40-02-0G-0, PARA 4 AND FIG 8.

Part: DOOR FRAME — CRACKED (BS 956) · airframe 55,136 hrs · 30,911 cycles

AFT GALLEY DOOR CUTOUT FWD LOWER INTERIOR CORNER 2ND OPEN HOLE FROM BOTTOM IS CRACKED .2500" LONG RADIATING FROM THE 7 O'CLOCK POSITION. ACFT GROUNDED. REPAIRED AFT GALLEY DOOR CUTOUT FWD FRAME LOWER AT STA 956 IAW EA 4700-53, EA-14041.

Part: FITTING — CORRODED (SEAL DEPRESSOR) · corrosion level 2 · airframe 55,136 hrs · 30,911 cycles

R2 DOOR CUTOUT LOWER FWD SEAL DEPRESSOR FITTING IS CORRODED AT FASTENER HOLE. ACFT GROUNDED. R & R DOOR CUTOUT LWR FWD SEAL FITTING IAW SRM 51-40-02-0G-0 FITTING MADE OUT OF MAGNESIUM, NO ALLOWABLE LIMITS PARTS REPLACEMENT REQ.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 55,136 hrs · 30,911 cycles

LT WING OTBD FOREFLAP INBD EDGE IS CHAFED. ACFT GROUNDED. REMOVED AND INSTALLED NEW SKIN IAW SRM 51-40-02-0G-0.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 55,136 hrs · 30,911 cycles

LEFT HORIZONTAL STABILIZER L/E HAS GOUGE APPROXIMATELY 5 FT FROM INBD EDGE. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-2, REPAIR 2.

Part: STRAP — CRACKED (BS 330) · airframe 54,739 hrs · 30,663 cycles

LOWER FLOOR STRAP AT BS 330, LBL 20 CRACKED. ACFT GROUNDED. FABRICATED REPAIR DOUBLER IAW SRM 53-10-51-2R-4 REPAIR. INSTALLED REPAIR IAW SRM 53-10-51-2R-4, REPAIR 4.

Part: SEAT TRACK — WORN (BS 413) · airframe 54,101 hrs · 30,339 cycles

BS 413, LEFT SLIDE OTBD SEAT TRACK IS WORN. ACFT GROUNDED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02 AND E/A 400-53A-12981.

Part: SEAT TRACK — WORN (BS 505G) · airframe 54,101 hrs · 30,339 cycles

BS 505G RT SIDE SECOND SEAT TRACK INBD WORN. ACFT GROUNDED. CUT OUT AND REMOVED BAD SECTION OF SEAT TRACK IAW SRM 53-00-52-2R-1. ACCOMPLISHED EA 400-53-EA12975. REPLACED SEAT TRACK IAW SRM 53-00-52-2R-1, REPAIR 1, PGS 1-4, NOTES 1-15.

Part: PUCK — WORN (CARGO BAY) · airframe 55,136 hrs · 30,911 cycles

FWD CARGO BAY LT AFT NET ANCHORS WORN, LOCATION LBL 18.2, AT BS 497. ACFT GROUNDED. REPAIRED IAW SRM 53-00-53-2R-2 REPAIR 2.

Part: HANDLE — BINDING (L1 DOOR) · airframe 51,972 hrs · 29,132 cycles

L1 DOOR HANDLE STIFF TO CLOSE AND SQUEAKS WHEN OPENED. ACFT GROUNDED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 50,780 hrs · 28,417 cycles

DURING SERVICE CHECK, FOUND RT AFT OVERWING EXIT EMERGENCY LIGHT DIM. R & R RT OVERWING EXIT EMERGENCY LIGHT BATTERY PACK REF MM 33-51-51. OPS CHECKED GOOD.

Part: NUT — LOOSE (L1 GUIDE ARM) · airframe 50,649 hrs · 28,338 cycles

FLIGHT CREW REPORTED L1 DOOR DIFFICULT TO OPEN ONCE PARKED AT GATE. ACFT GROUNDED. FOUND L1 DOOR GUIDE ARM JAM NUT LOOSE. MADE ADJUSTMENT TO L1 DOOR GUIDE ARM AND TIGHTENED GUIDE ARM JAM NUT. DOOR OPS CHECKED GOOD.

Part: GUIDE ARM — OUT OF RIG (R1 DOOR) · airframe 50,165 hrs · 28,055 cycles

R-1 DOOR OUT OF RIG. ACFT GROUNDED. FOUND AFT EDGE OF DOOR TRAILING BEHIND FWD EDGE WHEN CLOSING. BEGAN GUIDE ARM ADJUSTMENT. ROD END BEARING BOLT LOOSE REF AMM 52-41-21-404-004. ACCOMPLISHED FINAL GUIDE ARM ADJUSTMENT AND RESERCURED BEARING BOLT CHECK NUT. REF AMM 52-41-21. R & R R-1 DOOR SNUBBER AND OPS CHECKED NORMAL REF AMM 52-11-71. R-1 DOOR OPS / RIG CHECK GOOD.

Part: SNUBBER — DEFECTIVE (R2 DOOR) · airframe 47,521 hrs · 26,518 cycles

R2 DOOR HARD TO OPEN. REMOVED AND REPLACED R2 DOOR SNUBBER PER AMM.

Part: JACKSCREW — NOISY (STABILIZER) · airframe 45,563 hrs · 25,355 cycles

A LOUD CLUNKING NOISE IN PEDESTAL WHILE RUNNING STAB TRIM WHEEL EITHER DIRECTION. REPLACED STABILIZER JACK SCREW IAW ASA TASK CARD NR 48727000. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (STABILIZER) · airframe 45,563 hrs · 25,355 cycles

DURING TROUBLESHOOTING OF AUTOPILOT TRIM DURING NORMAL OPS STAB TRIM ROLLS BACK ON ITS OWN. REPLACED STAB TRIM ACTUATOR IAW B737 400 AMM 27 41 71. OPS NORMAL.

Part: SKIN — DENTED (HORIZ STAB) · airframe 45,112 hrs · 25,077 cycles

REF SAD NUMBER 6787318 2 DENT ON LT HORIZ STAB L/E AT STA 178 AND 197. REMOVED DAMAGED SECTION FABBED REPAIR PARTS & INSTALLED REPAIR IAW B737 400 SRM 55 10 01 FIG 204.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

BAFFLE CLIP AT STA 500F AT LBL 21 CRACKED. REMOVED CLIP FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 30 01.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

BS 1006 FRAME CORRODED UNDER R2 DOOR MOP SILL. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 07.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

UPON REMOVAL OF LT SHEAR WEB FOUND CORROSION ON WEB FS 1006 1016 LBL 45. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 15 FIG 101. REMOVED AND REPLACED LT SHEAR WEB HS 1006 1016 IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

FRAME STA 1006 CORRODED UNDER L2 MOP SILL. REMOVED DAMAGED SECTION. FABRICATED HEAT TREATED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED FRAME REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

R2 DOOR WAY SHEAR WEB AT BS 986 TO BS 992 RBL 45 CORRODED. REMOVED WEB FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

LOWER SILL WEB AT L 2 DOOR MOP SILL IS CORRODED BETWEEN BS 986 AND BS 992 LBL 45. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

L2 DOOR WAY LOWER SILL WEB CORRODED AT BS 967 TO BS 986 LBL 45. REMOVED CORRODED WEB AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

SHEAR WEB IS CORRODED BETWEEN BS 967 AND BS 986 RBL 45. REMOVED CORRODED WEB AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

E&E BAY DOOR CUTOUT AFT WEB PUNCTURED ABOVE LATCH FITTING. REMOVED DAMAGED WEB. FABRICATED TREATED PRIMED TOPCOATED AND INSTALLED WEB REPAIR IAW EA 400 53EA 1439.

Part: WEB — GOUGED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

E&E BAY DOOR CUTOUT LEFT WEB GOUGED ABOVE LATCH FITTING. REMOVED DAMAGE IAW B737 400 SRM 53 10 15 FIG 101 AND INSTALLED FASTENERS.

Part: PANEL — CHAFED (NR 2 PYLON) · airframe 35,855 hrs · 21,974 cycles

NR 2 STRUT OUTBOARD FUSE PIN PANEL CHAFED. FABRICATED REPLACEMENT PANEL AND INSTALLED IAW BOEING DWG 313A1200 AND B737 400 SRM 51 30 01.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

R1 DOOR CREASE BEAM WEB CRACKED. REMOVED AND REPLACED SILL WEB IAW B737 400 SRM 51 40 02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

LT SHEAR WEB CORRODED STA 986 LBL 44. REMOVED CORRODED WEB. FABRICATED TREATED PRIMED TOPCOATED AND INSTALLED NEW SHEAR WEB IAW B737 400 SRM 51 40 02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

STRINGER 22L IS CORRODED JUST FORWARD OF BS 1016. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 03 FIG 201 DETAIL VII.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 45,112 hrs · 25,077 cycles

RT HORIZONTAL L/E PANEL HAS TOOL MARK APPROX 12 INCHES FROM INBD END. REMOVED DAMAGED SKIN FORMED TREATED PRIMED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 55 10 01 FIG 202 REPAIR 12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN FRAME CRACKED AT BS 867 BETWEEN STR 8R AND 9R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW ASA EA AD20062609 400 53 118 REV NEW DATED 12 APR 2011.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

RT SHEAR WEB HAS CORROSION AT FS 986. REMOVED AND REPLACED SHEAR WEB IAW B737 400 SRM 51 40 02.

Part: PAN — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

AFT LAV SB QUICK PAN CORRODED ON INNER SURFACE. REMOVED CORRODED DOUBLER. RECEIVED LOCATED & DRILLED AND INSTALLED (2) NEW DOUBLERS IAW B737 400 SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

FLOOR SUPPORT STA 967-986 LBL 16 CORRODED. REMOVED CORRODED SUPPORT AND INSTALLED NEW FLOOR SUPPORT IAW B737 400 SRM 51 30 01 FIG 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN FRAME CRACKED AT BS 747 BETWEEN STR 8R AND 9R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW ASA EA AD20062609 400 53 118 REV NEW DATED 12 APR 2011.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

CABIN FLOOR WEB AT BS 944 RBL 10 IS CORRODED. FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 51 70 13 FIG 1 STEP I.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

IN MAIN CABIN BELOW FLOOR BULKHEAD STIFFENER STA 1017 BL 0 CORRODED. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED NEW STIFFENER AND SPLICE ANGLES IAW EA 400 53EA 05365.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN FRAME AT BS 727F CRACKED BETWEEN STR 8R AND 9R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW ASA EA AD20062609 400 53 118 REV NEW DATED 12 APR 2011.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

MAIN CABIN FLOORBEAM CORRODED AT STA 986 RBL 30 AT FASTENER HOLE. REMOVED DAMAGED FLOORBEAM LOCATED DRILLED TREATED PRIMED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05335.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

SHEAR TIE ON FWD SIDE OF FRAME AT BS 986 HAS CORROSION AT STR 26R. REMOVED SHEAR TIE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

IN MAIN CABIN BELOW FLOOR BULKHEAD WEB CORRODED STA 1017 LBL 2. CUT OUT DAMAGED WEB. FABRICATED TREATED PRIMED AND INSTALLER DOUBLER & FILLER WEB REPAIR IAW EA 400 53EA 05365.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

LEFT FLOOR SUPPORT ANGLE AT BS 616 CORRODED. REPAIRED ANGLE IAW B737 400 SRM 51 70 12.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

INTERCOSTAL AT BS 996 LBL 35 IS CORRODED. REMOVED CORRODED INTERCOSTAL FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

INTERCOSTAL CORRODED AT BS 989 RBL 33. REMOVED CORRODED INTERCOSTAL, FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

BULKHEAD ATTACH ANGLE CORRODED AT BS 945 BETWEEN STR 25R AND 26R. REMOVED AND REPLACED ATTACH ANGLE IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN LT FRAME STA 992 CORRODED BETWEEN 16L 17L. REMOVED DAMAGED SECTION. RECEIVED HEAT TREATED LOCATED PRIMED TOPCOATED AND INSTALLED FRAME REPAIR IAW EA 400 53EA 05333.

Part: ANGLE — CORRODED (APU BAY) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

APU COMPARTMENT RIGHT L-ANGLE CORRODED. REPLACED ANGLE IAW BOEING DWG 65 46579 AND B747 400 SRM 51 40 02.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

LONGERON CORRODED AROUND NUT PLATES STA 945 STR 26L. REMOVED CORRODED SECTION. RECEIVED MACHINED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED LONGERON REPAIR IAW B737 400 SRM 53 00 53 FIG 201.

Part: FRAME — DENTED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FRAME AT STA 727G HAS 2 EA DENTS ON UPPER SURFACE BETWEEN STR 20L & 22L. REMOVED DAMAGED AREAS FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ASA EA 400 43EA 05352 AND AAR EA 14369.

Part: FRAME — DENTED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FRAME AT STA 767 HAS A DENT BETWEEN STR 24R & 25R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS & INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05350 & AAR EA 14360.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

AFT PIT Z-ANGLE HAS CORROSION AT FASTENER HOLES ON LOWER SURFACE AT STA 949 LBL 20. REMOVED DAMAGED AREA, FABBED REPLACEMENT AND REPAIR PARTS AND INSTALLED PART IAW B737 400 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

BS 767 FRAME STIFFENER CORRODED FROM STR 26R TO 27R. REPLACED FRAME STIFFENER IAW B737 400 SRM 51 40 02 AND 53 00 01.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

AFT PIT LOWER SIDE WALL SUPPORT ANGLE AT BS 727 HAS SEVERAL BROKE OUT SCREW HOLES. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

L2 DOOR MOP SILL IS CORRODED. REMOVED CORRODED MOP SILL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

BULKHEAD ATTACH ANGLE STA 945 BETWEEN STA 25L 26L CORRODED. REMOVED CORRODED ANGLE. RECEIVED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02.

Part: FRAME — DENTED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FRAME STA 827.0 HAS 2 DENTS UPPER SURFACE BETWEEN STR 24L 25L. CUT OUT DAMAGED SECTION. FABRICATED HEAT TREATED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED FRAME REPAIR IAW EA 400 53EA 05338.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

AFT CARGO COMPT SHEAR TIE CORRODED ON FWD SIDE FRAME STA 747 BETWEEN STR 25R TO 26R. REPAIRED IAW B737 SRM 53 00 07 FIG 201 REPAIR 7 (SHEAR TIE) W 1IN. O .063 R .000 L 3IN. D 100 PERCENT.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

R2 DOOR MOP SILL CORRODED. REMOVED MOP SILL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

AFT PIT SHEAR TIE STA 727D CORRODED OUTBOARD OF STR 26R. REMOVED CORRODED SHEAR TIE. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 7.

Part: FRAME — DENTED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

AFT PIT LT FRAME STA 767 DENTED ON UPPER SURFACE ABOVE STR 25L. CUT OUT DAMAGED AREA FORMED HEAT TREATED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED FRAME REPAIR IAW ASA EA 400 53EA 05363.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

STA 947 FRAME IS CORRODED BETWEEN STR 25L & 26L. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05359.

Part: TRACK — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FLOOR SUPPORT CORRODED & DENTED STA 807 STR 27R (TIE DOWN TRACK). REMOVED DAMAGED TRACK: RECEIVED MACHINED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED TIE DOWN TRACK REPAIR IAW EA 400 53EA 05361.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FLOOR SUPPORT ANGLE STA 400 STR 25R DAMAGED. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW B737 400 SRM 51 70 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN FRAME AT BS 360 IS CRACKED AT STR 8L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW ASA EA AD20062609 400 53 118 REV NEW DATED 12 APR 2011.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FWD GALLEY DOOR CUTOUT INTERCOSTAL FORMED ANGLE HAS A CRACK APPROX .6" IN LENGTH BS 290.5 2.5" ABOVE STR 9R. REMOVED AND REPLACED ANGLE IAW ASA EA 400 53EA 05318 AND AAR EA 14349.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FORWARD GALLEY DOOR CUTOUT INTERCOSTAL WEB HAS A CRACK AT THE INBOARD BEND RADIUS BS 277 STR 13R. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW ASA EA 400 53EA 05318 AND AAR 14349.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FWD GALLEY DOOR CUTOUT INTERCOSTAL FORMED ANGLE HAS A CRACK APPROX. .5" IN LENGTH BS 290 BETWEEN STR 10R AND 9R. REMOVED AND REPLACED ANGLE IAW ASA EA 400 53EA 05318 AND AAR EA 14349.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN FRAME CRACKED AT BS 440 BETWEEN STR 8L AND 9L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW ASA EA AD20062609 400 53 118 REV NEW DATED 12 APR 2011.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FWD GALLEY DOOR CUTOUT INTERCOSTAL FORMED ANGLE HAS A CRACK AT THE JOGGLE APPROX .25" IN LENGTH BS 290 BETWEEN STR 11R AND 10R. REMOVED AND REPLACED ANGLE IAW ASA EA 400 53EA 05318 AND AAR EA 14349.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

WEB AT STA 294.5 STR 7R IS CRACKED AT UPPER RADIUS (STUB FRAME). REMOVED DAMAGED STUB FRAME AND REPLACED DAMAGED PARTS IAW ASA EA 400 53EA 05318.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FWD GALLEY DOOR CUTOUT INTERCOSTAL FORMED ANGLE HAS A CRACK AT THE JOGGLE APPROX .4" IN LENGTH BS 290 4" BELOW STR 11R. REMOVED AND REPLACED ANGLE IAW ASA EA 400 53EA 05318 AND AAR EA 14349.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

PASSENGER CABIN FRAME CRACKED AT BS 400 BETWEEN STR 8L AND 9L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW ASA EA AD20062609 400 53 118 REV NEW DATED 12 APR 2011.

Part: SKIN — DENTED (SPOILER) · airframe 45,112 hrs · 25,077 cycles

NR 2 SPOILER HAS PROTRUDING DENTS ON UPPER SURFACE 25 IN FROM OUTBOARD EDGE AND 5.5 IN FROM LEADING EDGE. REMOVED DAMAGE AND REPAIRED UPPER SKIN IAW B737 400 SRM 57 70 01 FIG 201.

Part: ANGLE — CHAFED (RT WING) · airframe 45,112 hrs · 25,077 cycles

RIGHT WING TRAILING EDGE UPPER ANGLE I/B OF AILERON IS CHAFED. REMOVED AND REPLACED ANGLE IAW B737 400 SRM 57 51 90 AND SRM 51 40 02.

Part: STRUCTURE — CHAFED (NR 1 PYLON) · airframe 45,112 hrs · 25,077 cycles

NR 1 ENGINE INBOARD FORWARD UPPER PYLON CHORD CHAFED SEVERAL AREAS LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5296 REV NEW DATED 21 APR 2011.

Part: SKIN — DENTED (SPOILER) · airframe 45,112 hrs · 25,077 cycles

NR 2 SPOILER HAS CLUSTER OF DENTS 9 INCHES FROM LEADING EDGE AND 4.8 INCHES FROM O/B EDGE. REMOVED DAMAGED SKIN, FABRICATED DOUBLER SKIN REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: STRUCTURE — CHAFED (NR 1 PYLON) · airframe 45,112 hrs · 25,077 cycles

NR 1 ENGINE OUTBOARD UPPER FORWARD PYLON CHORD CHAFED LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5296 REV NEW DATED 21 APR 2011.

Part: STRUCTURE — CHAFED (NR 2 PYLON) · airframe 45,112 hrs · 25,077 cycles

NR 2 ENGINE PYLON UPPER FORWARD CHORD CHAFED SEVERAL AREAS OUTBOARD LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5297 REV NEW DATED 21 APR 2011.

Part: STRUCTURE — CHAFED (NR 2 PYLON) · airframe 45,112 hrs · 25,077 cycles

NR 2 ENGINE PYLON UPPER FORWARD CHORD CHAFED SEVERAL AREAS INBOARD LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5297 REV NEW DATED 21 APR 2011.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

REINFORCEMENT ANGLE STA 500G CORRODED BETWEEN STR 27R 28R. REMOVED ANGLE AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

BAFFLE ATTACH CLIP AT STA 600F AND RBL 21 CRACKED. REMOVED CLIP FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 30 01.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 45,112 hrs · 25,077 cycles

FORWARD PIT RIGHT TRANSITION PANEL IS CORRODED FROM BS 500A TO BS 500G. REMOVED DAMAGED AREA, FABRICATED REPLACEMENT AND REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 30 53.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

BAFFLE ATTACH CLIP CRACKED STA 380 LBL 21.8 . REMOVED CRACKED CLIP. FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (SPOILER) · airframe 45,112 hrs · 25,077 cycles

NR 4 SPOILER LOWER SURFACE DENTED 38 IN FROM OUTBOARD END 2 IN FROM TRAILING EDGE. REPAIRED DENT DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: FITTING — CHAFED (FOREFLAP) · airframe 45,112 hrs · 25,077 cycles

LEFT O/B TRAILING EDGE ABOVE O/B END OF FORE FLAP ROLLER GUIDE FITTING CHAFED. REMOVED AND REPLACED FORE FLAP ROLLER GUIDE FITTING IAW B737 400 SRM 57 51 90 AND SRM 51 40 02.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 45,112 hrs · 25,077 cycles

NR 5 LEADING EDGE SLAT UPPER INBOARD TRAILING EDGE SURFACE DELAMINATED. REPAIRED SLAT UPPER INBOARD TRAILING EDGE SURFACE IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,112 hrs · 25,077 cycles

SHEAR TIE ON FRAME AT BS 500 IS CORRODED. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

SHEAR TIE STA 500A CORRODED BETWEEN STR 27R 28R. REMOVED CORRODED SHEAR TIE. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 07.

Part: STRAP — BROKEN (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FLOORBEAM CENTER STRAP BROKEN STA 312. REMOVED BROKEN STRAP FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (HORIZ STAB) · airframe 45,112 hrs · 25,077 cycles

REF SAD NUMBER 6787318 3 DENTS IN LT HORIZ STAB L/E APPROX MID SPAN APPROX STATION IS 162.5. REMOVED DAMAGED SECTION FABBED DOUBLERS & FILLER & INSTALLED REPAIR IAW B737 400 SRM 55 10 01 FIG 201.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

FUSELAGE SKIN DENT AT BS 938 JUST BELOW STR 17R IS WITHIN 10 INCHES OF NEGATIVE PRESSURE RELIEF VALVE. CUT OUT DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05325.

Part: STRIP — CORRODED (FUSELAGE) · airframe 45,112 hrs · 25,077 cycles

AFT CARGO COMPT NR 5 DECK PANEL LEFT CAP STRIP HAS SEVERAL AREAS OF CORROSION. FABRICATED NEW CAP STRIP AND INSTALLED IAW B737 400 SRM 53 60 53 AND 51 40 05.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 43,136 hrs · 23,916 cycles

DURING APPROACH, FLAPS SELECTED NO LE OR TE FLAP INDICATED. ACCOMPLISHED QRH FOR INDICATION & ALTERNATE FLAP EXTENSION. FULL EXTENSION ON LE BUT NO INDICATION ON TE FLAPS CONFIRMED VISUALLY. LANDED WITH FLAP HANDLE IN 1 DEGREE POSITION. AFTER LANDING, SELECTED FLAP UP POSITION & NOTICED LE FLAP TRANSIT LIGHT OUT. VISUALLY CONFIRMED THAT LE HAD RETRACTED. CHECKED LUBE ON FLAP DRIVE UNIT. NO MOISTURE OR DEBRIS IN GREASE. REPLACED FLAP PRIORITY VALVE & FLOW LIMITING VALVE IAW MM 27-51-84-404-004 OPS CHECK GOOD. ACCOMPLISHED LEAK & FUNCTIONAL TEST OF FLAP PRIORITY VALVE IAW MM 27-51-84-724-012. OPS & LEAK CHECKED GOOD. REPLACED T/E FLAP BYPASS VALVE, OPS CHECK GOOD PER MM 27-51-82. REPLACED NR 5 FLAP TRANSMISSION BALLSCREW REF MM 27-51-73. REPLACED THE NR 7 FLAP TRANSMISSION & BALLSCREW PER MM 27-51-71. REPLACED NR 3 FLAP BALLSCREW PER MM 27-51-73-404-023. ORIGINAL SUBMISSION DATE: 7/21/2010

Part: SKIN — DELAMINATED (SPOILER) · airframe 41,802 hrs · 23,099 cycles

LEFT WING NUMBER 1 SPOILER UPPER SURFACE DELAMINATED NEXT TO O/B REPAIR. REPAIRED DELAMINATED UPPER SURFACE OF SPOILER NR 1.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,802 hrs · 23,099 cycles

NR 4 SLAT SKIN DISBONDED AT O/B EDGE UNDER WEDGE SEAL. REPAIRED SKIN.

Part: SKIN — DENTED (TE FLAP) · airframe 41,802 hrs · 23,099 cycles

LEFT O/B AFT FLAP LOWER SURFACE HAS A CLUSTER OF DENTS AT REPAIR. INSTALLED FILLER AND DOUBLER AFTER DAMAGED WAS REMOVED.

Part: SKIN — DAMAGED (SPOILER) · airframe 41,802 hrs · 23,099 cycles

NR 5 SPOILERS UPPER SURFACE HAS A SMALL DENT WITH A CREASE 6 INCHES AFT OF FORWARD EDGE 15 INCHES FROM O/B EDGE. INSTALLED DOUBLER.

Part: SKIN — CHAFED (TE FLAP) · airframe 41,802 hrs · 23,099 cycles

LEFT I/B FORE FLAP HAS WORN THROUGH DOUBLER INTO SKIN. INSTALLED CORE AND DOUBLER.

Part: SLAT — DEBONDED (NR 2) · airframe 41,802 hrs · 23,099 cycles

NR 2 SLAT I/B UPPER TRAILING EDGE DISBONDED. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 41,802 hrs · 23,099 cycles

RIGHT I/B FORE FLAP UPPER SURFACE REPAIR 36 INCHES FROM O/B END IS DELAMINATED. INSTALLED DOUBLER.

Part: SKIN — DELAMINATED (SPOILER) · airframe 41,802 hrs · 23,099 cycles

NR 7 SPOILER UPPER SURFACE DELAMINATED. INSTALLED DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,802 hrs · 23,099 cycles

FUSELAGE DENT ON FRAME AT STA 986 & STR 19R. REMOVED DAMAGE, INSTALLED DOUBLER.

Part: SKIN — DELAMINATED (SPOILER) · airframe 41,802 hrs · 23,099 cycles

NR 1 SPOILER UPPER SURFACE IS DELAMINATED IN TWO SPOTS OF PREVIOUS REPAIR. INSTALLED FILLER AND DOUBLER AT BOTH AREAS OF DELAMINATION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,802 hrs · 23,099 cycles

AFT PIT FRAME AT STA 794 UPPER FLANGE CORRODED BETWEEN STR 25R & 26R. REMOVED AND REPLACED FRAME.

Part: RIB — CRACKED (RT WING) · airframe 41,802 hrs · 23,099 cycles

RIGHT WING RIB WBL 135.5 LOWER CHORD CRACKED AFT OF STRINGER 2. REPAIRED CHORD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,802 hrs · 23,099 cycles

RT INTERCOSTAL STA 747 - 767 STA 25L 26L CORRODED AND CRACKED. REMOVED AND INSTALLED NEW INTERCOSTAL.

Part: SKIN — DELAMINATED (SPOILER) · airframe 41,802 hrs · 23,099 cycles

NR 1 SPOILER UPPER SURFACE DELAM ADJACENT TO O/B PREVIOUS REPAIR. REMOVED DELAMINATED AREA, PREPPED AREA, FABBED FILLER AND DOUBLER AND BONDED.

Part: SKIN — CHAFED (LE SLAT) · airframe 41,802 hrs · 23,099 cycles

LT WING NR 3 SLAT LOWER SURFACE ALONG UPPER PORTION IS CHAFED THROUGH TEFLON. BLENDED OUT DAMAGE, PREPPED AREA, FABBED REPAIR AND BONDED REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 41,802 hrs · 23,099 cycles

LEFT O/B AFT FLAP TRAILING EDGE DENTED APPROX 3.75 INCHES FROM I/B EDGE. REPAIRED LEFT O/B AFT FLAP BY FABRICATING REPAIR PARTS.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 41,802 hrs · 23,099 cycles

LEFT SHEAR WEB IS CRACKED AT A FASTENER HOLE FS 1016 AND LBL 38. REPAIRED WEB.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,802 hrs · 23,099 cycles

LT WING NR 3 SLAT O/B UPPER T/E IS DELAMINATED. REMOVED DAMAGED, PREPPED AREA, FABBED REPAIR AND BONDED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,802 hrs · 23,099 cycles

LEFT WING NR 3 SLAT INBOARD UPPER TRAILING EDGE IS DELAMINATED. REPAIRED WING.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,802 hrs · 23,099 cycles

NR 5 SLAT UPPER SURFACE O/B AFT CORNER DELAMINATED. REPAIRED SLAT.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 38,954 hrs · 21,433 cycles

NR 1 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 38,954 hrs · 21,433 cycles

NR 2 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 38,954 hrs · 21,433 cycles

NR 8 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 38,954 hrs · 21,433 cycles

NR 7 FLAP TRACK HAS EVIDENCE OF CORROSION.

Part: SKIN — DENTED (BS 1010) · airframe 38,310 hrs · 21,012 cycles

BS 1010 UPPER SIDE OF STR 15 RT SKIN HAS DENTS 2 EA. REPAIR SKIN STA 1010 BETWEEN STR 14R AND 15R IAW ASA EA 5330 02387.

Part: SKIN — DENTED (BS 388) · airframe 38,310 hrs · 21,012 cycles

DENT 2 INCHES AFT OF D2 BLOWOUT DISC. DENT WITHIN 10 INCHES OF CUTOUT. REPAIRED SKIN DENT STA 388.5 AND STR 21R IAW ASA EA 5330 02388.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

RIGHT I/B FOREFLAP LOWER SURFACE ABOVE NR 3 TIRE IS DENTED ON A REPAIR DOUBLER. REPAIRED THE DAMAGED AREA OF THE LOWER SURFACE OF I/B FORE FLAP IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING NR 3 SPOILER UPPER SURFACE HAS 2 EA INVERTED DENTS. REPAIRED NR 3 SPOILER UPPER SURFACE IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

RIGHT I/B MID FLAP LOWER SURFACE T/E WEDGE HAS MULTIPLE SMALL DENTS BETWEEN MIDDLE TRACKS. REPAIRED RIGHT I/B MID FLAP WEDGE LOWER SURFACE DENTS IAW B737 400 SRM 51-30-01 PG 13.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING I/B FOR FLAP REPAIR ON UPPER SURFACE 34 INCHES FROM O/B AND CHAFED AND DELAMINATED. REPAIRED DAMAGE TO LT WING I/B FORE FLAP UPPER SURFACE IAW B737 400 SRM 51-70-10 PARA 96 PG 217 REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING I/B UPPER TRAILING EDGE PANEL HAS A SMALL DENT 85 INCHES O/B OF I/B END 9 INCHES FWD OF TRAILING EDGE. REPAIRED LT WING I/B UPPER TRAILING EDGE PANEL IAW B737 400 SRM 51-70-10 REPAIR.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING I/B MID FLAP TRAILING EDGE WEDGE HAS 3 EA SHARP DENTS ON LOWER SURFACE 46 INCHES FROM I/B END. REPAIRED LT WING TRAILING EDGE WEDGE MID FLAP IAW B737 400 SPM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (NR 6 SPOILER) · airframe 38,310 hrs · 21,012 cycles

NR 6 SPOILER IS DENTED ON UPPER SURFACE FROM SEAL SCREWS ON LOWER SURFACE. REPAIRED NR 6 SPOILER IAW B737 400 SRM 51-70-10 REPAIR 4 PG 201.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

RIGHT I/B FORE FLAP LOWER SURFACE ABOVE NR 4 TIRE IS PUNCTURED AT ONE DENT IN THE MIDDLE OF A GROUP OF DENTS. REPAIR RIGHT I/B FORE FLAP LOWER SURFACE IAW B737 400 SRM 51-70-10.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING I/B FORE FLAP UPPER SURFACE HAS A SMALL DENT 53 INCHES O/B FROM I/B END AND .75 INCHES UP FROM TRAILING EDGE. REPAIRED LT WING I/B FORE FLAP UPPER SUFRACE IAW B737 400 SRM 51-70-10 REP 2 PG 201.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING I/B UPPER TRAILING EDGE PANEL DELAMINATED 2 EA PLACES AS MARKED 53 AND 70 INCHES O/B OF I/B END. REPAIRED LT WING I/B UPPER TRAILING EDGE PNL IAW B737 400 SRM 51 70 10 REPAIR 2 PG 201.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 38,310 hrs · 21,012 cycles

DENT IN LOWER SURFACE OF NR 3 SPOILER. PREPPED AREA, FABBED DOUBLER AND BONDED IAW B737 400 SRM 51-70-10.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 38,310 hrs · 21,012 cycles

LEFT WING NR 3 SLAT LOWER T/E WEDGE CHAFED ON I/B SIDE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LEFT WING I/B FORE FLAP UPPER SURFACE DENTED AND CHAFED 47 INCHES FROM I/B END AND 9 INCHES FROM T/E. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 38,310 hrs · 21,012 cycles

RIGHT WING NR 5 SPOILER CLUSTER OF DENTS ON UPPER SURFACE 12 INCHES FROM O/B END. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 38,310 hrs · 21,012 cycles

UPPER SURFACE OF NR 2 SPOILER DENTED. PREPPED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW SRM 51-70-10.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 38,310 hrs · 21,012 cycles

RT WING NR 8 SPOILER DENTED ON UPPER SURFACE MIDDLE NEAR T/E. PREPARED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 38,310 hrs · 21,012 cycles

DENT IN UPPER INBOARD SURFACE OF NR 1 SPOILER. PREPPED AREA, FABRICATED DOUBLER BONDED REPAIR IAW B737 400 SRM 51-70-10.

Part: SKIN — DENTED (NR 7 SPOILER) · airframe 38,310 hrs · 21,012 cycles

RT WING NR 7 SPOILER UPPER SURFACE MULTIPLE PROTRUDING DENTS. REMOVED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER BONDED IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 38,310 hrs · 21,012 cycles

RIGHT WING NR 5 SPOILER LOWER SURFACE SEVERAL DENTS WITH PUNCTURES 24 INCHES FROM I/B END AND 6 INCHES FROM L/E. REMOVED DAMAGED AREA, FABRICATED TWO FILLER SKINS AND ONE EXTERNAL DOUBLER PREPARED AREA AND BONDED IAW B737 400 SRM REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 38,310 hrs · 21,012 cycles

RIGHT I/B SPOILER LOWER SURFACE MULTIPLE SMALL DENTS. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (SPOILER) · airframe 38,310 hrs · 21,012 cycles

LT WING NR 0 SPOILER UPPER SURFACE PROTRUDING DENT 6 INCHES FROM O/B AND 7 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED FILLER AND EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 38,310 hrs · 21,012 cycles

RIGHT WING NR 5 SPOILER UPPER SURFACE DENTED 5 INCHES FWD OF T/E AND 24 FROM O/B EDGE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BOUNDED IAW B737 4 SRM 51 70 10 REPAIR 2.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 38,310 hrs · 21,012 cycles

INBOARD TRAILING EDGE OF NR 4 SLAT CHAFED. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51-70-10.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 38,310 hrs · 21,012 cycles

DENT IN UPPER OUTBOARD SURFACE OF NR 1 SPOILER. PREPPED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51-70-10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

RIGHT WING O/B FOREFLAP DENTED 24 INCHES FROM I/B END 4 INCHES FROM T/E. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 38,310 hrs · 21,012 cycles

LT WING I/B AFT FLAP DENTED ON LOWER LEADING EDGE SURFACE 46 INCHES FROM I/B END. REMOVED DAMAGED SECTION OF FLAP LEADING EDGE FABRICATED, LOCATED, DRILLED AND INSTALLED NEW LEADING EDGE SECTION IAW B737 400 SRM 57 53 01 DETAIL IV PG 4 AND B DWG 65 4634.

Part: SKIN — DENTED (SPOILER) · airframe 38,310 hrs · 21,012 cycles

RIGHT I/B GROUND SPOILER LOWER SURFACE 12 EA SMALL DENTS AT I/B AREA. REMOVED DAMAGED AREA, FABRICATED FILLER AND EXTERNAL DOUBLER PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4

Part: UNKNOWN — BINDING (L1 DOOR) · airframe 36,429 hrs · 19,973 cycles

L1 DOOR RELEASES INWARD OK VERY DIFFICULT TO PUSH OPEN. CHECKED DOOR FOR LOOSE OR DAMAGED PARTS, NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF L1 DOOR. DOOR OP CHECKS NORMAL.

Part: SKIN — CHAFED (TE FLAP) · airframe 34,522 hrs · 18,945 cycles

LEFT I/B FORE FLAP UPPER SIDE 82 INCHES FROM I/B HAS CHAFING DAMAGE. LEFT I/B FORE FLAP UPPER SIDE 82 INCHES FROM I/B DAMAGE REPAIRED IAW SRM 51-70-10 REPAIR 4.

Part: STRINGER — DENTED (BS 1081) · airframe 34,522 hrs · 18,945 cycles

DENT ON TOP OF STRINGER. REPAIRED DENT IAW SRM 53-00-53 FIG 201 REPAIR 1.

Part: SKIN — DENTED (TE FLAP) · airframe 34,522 hrs · 18,945 cycles

LEFT WING I/B FORE FLAP UPPER CAMBER HAS 2 EACH DENTS. RECORDED AND DOUBLER OVER LAY PER SRM 51-70-10.

Part: SKIN — DELAMINATED · airframe 34,522 hrs · 18,945 cycles

LEFT I/B FORE FLAP UPPER SIDE 77 INCHES FROM INBOARD END DELAMINATED. RECORDED AND DOUBLER OVERLAY PER SRM 51-70-10.

Part: SKIN — CHAFED (FORE FLAP) · airframe 30,887 hrs · 16,898 cycles

LT OB FORE FLAP HAS 2 AREAS CHAFED AT IB LE. BLENDED CHAFED AREA INSTALLED RIVET IAW ASA EA 5750 02249.

Part: WEDGE — DELAMINATED (NR 2 SLAT) · airframe 30,887 hrs · 16,898 cycles

NR 2 SLAT OB TE DELAMINATED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.

Part: SKIN — GOUGED (BS 1024 S14L) · airframe 30,887 hrs · 16,897 cycles

FOUND DENT GOUGE ON EXTERIOR SKIN. REMOVED DAMAGED SECTION OD SKIN FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW ASA EA 5330 02088.

Part: WEDGE — DENTED (NR 2 SLAT) · airframe 30,887 hrs · 16,897 cycles

FOUND LT WING NR 2 SLAT IS DENTED AT OB AUX TRACK. REPAIRED DAMAGED AREA OF THE LT WING NR 2 SLAT PER SRM 51 70 10 PG 211 PARA 7 PG 213 PARA 8 PG 221 PARA 238 PARA 15 AND PAGE 249 PARA 20.

Part: SKIN — DENTED (CARGO DOOR)

PAE - AFT CARGO DOOR REQUIRES RE-SKIN DO TO NUMEROUS DENTS. REPLACED SKIN. (M)

Part: SKIN — CORRODED (CARGO DOOR)

PAE - AFT CARGO DOOR HAS AREAS OF CORROSION ON INTERNAL SKIN. REPAIRED INTERNAL SKIN. (M)

Part: CASTING — GOUGED (CARGO DOOR)

PAE - FOUND AFT CARGO DOOR EXTERNAL DOOR HANDLE HOUSING IS GOUGED. REMOVED AND REPLACED HOUSING. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - PASSENGER CABIN, BS 601 FRAME CHORD IS CRACKED AT RBL 64, WL 204. REPAIRED FRAME CHORD PR EA 5310-02449. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - FOUND DENT AT BS 385 STRINGER 24R. REPAIRED DENT PER EA. (M)

Part: SEAL DEPRESSOR — CRACKED (GALLEY DOOR)

PAE - FORWARD GALLEY DOOR CUTOUT UPPER SEAL DEPRESSOR IS CRACKED. REPLACED SEAL DEPRESSOR. (M)

Part: SEAL DEPRESSOR — CORRODED (GALLEY DOOR)

PAE - FOUND CORROSION ON AFT GALLEY DOOR SEAL DEPRESSOR UPPER FORWARD STATION 959. REPLACED SEAL DEPRESSOR. (M)

Part: SEAL DEPRESSOR — CRACKED (FWD GALLEY DOOR) · airframe 26,983 hrs · 14,795 cycles

PAE - FWD GALLEY DOOR CUTOUT UPPER AFT SEAL DEPRESSOR CRACKED AT 2 PLACES, STA 328, RBL 52, WL 274. REMOVED AND INSTALLED NEW FWD GALLEY DOOR CUTOUT UPPER SEAL DEPRESSOR. (K)

Part: SUPPORT — DENTED (FUSELAGE) · airframe 26,983 hrs · 14,795 cycles

PASSENGER CABIN, FWD GALLEY SUPPORT IS DENTED BS 354, RBL 10, WL 208. REMOVED AND REPLACED SUPPORT. (K)

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,983 hrs · 14,795 cycles

PAE - CORROSION ON SHEAR WEB. BLENDED ON CORROSION, FUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHEAR WEB. (K)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON AFT ENTRY DOOR MOPSILL. REPLACED MOPSILL. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SIDEWALL SUPPORT. REPLACED WITH NEW SIDEWALL SUPPORT. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

PAE - FRAME SHEAR TIE CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHEAR TIE. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SIDEWALL SUPPORT PLATE, BS 837-947, LBL 22, WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LT ENTRY DOOR CUTOUT MOPSILL BS 303 TO 360, LBL 60, WL 208. REPLACED MOPSILL. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727-727E PLUS 10 INCHES, LBL 22, WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LT ENTRY DOOR CUTOUT BS 312-344, LBL 62, SL 208 LOWER FRAME THRESHOLD SUPPORT. REPLACED SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SIDEWALL SUPPORT PLATE, BS 500 PLUS 6 INCHES, WL 156, RBL 25. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 847-867. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON INTERCOSTAL AT BS 858 RBL 20 WL 163. REMOVED AND REPLACED INTERCOSTAL. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AFT CARGO BAY ON FRAME BS 767 STRINGER 25R AND 27R FORWARD SIDE OF FRAME. REMOVED AND REPLACED FRAME. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON RIGHT ENTRY DOOR CUTOUT, BS 297-328 RBL 62, WL 208 LOWER FRAME INBOARD THRESHOLD SUPPORT HAS CORROSION. REMOVED AND REPLACED. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON TIE DOWN TRACK. REMOVED AND REPLACED. (M)

Part: SILL — CORRODED (FUSELAGE) · airframe 26,983 hrs · 14,795 cycles

PAE - CORROSION ON LT ENTRY DOOR CUTOUT MOPSILL HAS CORROSION FROM BS 303 TO 360, LBL 60, WL 208. REPLACED MOPSILL. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LT ENTRY DOOR CUTOUT BS 312, LBL 62, WL 208. LOWR FRAME INBOARD THRESHOLD SUPPORT HAS CORROSION. REPLACED SUPPORT. (M)

Part: SUPPORT — CORRODED (CARGO BAY)

PAE - FOUND CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, BLENDED OUT OF LIMITS. REPLACED WITH NEW PART. (M)

Part: BULKHEAD — DENTED (FUSELAGE)

PAE - FOUND DENT ON 1016 BULKHEAD. INSTALLED REPAIR DOUBLER. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,983 hrs · 14,795 cycles

PAE - AFT CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 727 TO BS 727E +10 INCHES, RBL 21, WL 156. REMOVED OUT OF LIMITS CORRODED FLOOR TO SIDEWALL SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT. (K)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,983 hrs · 14,795 cycles

PAE - AFTER ACCESSED LT AFT ENTRY MOPSILL WEB FOUND CORRODED. BLENDED OUT OF LIMITS, FABRICATED AND INSTALLED NEW WEB BELOW MOPSILL LT AFT ENTRY. (K)

Part: SKIN — DENTED (FUSLAGE)

SEA - FOUND BAGGAGE CART STRUCK AIRCRAFT AFT DRAIN MAST AND FUSELAGE SKIN. THREE SCRATCHES JUST ABOVE POTABLE WATER SERVICE DOOR. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA .004 DEEP, 1 INCH LONG. BLENDED DAMAGED AREA AND ALODINED PER EA 5330-10789. (M)

Part: WIRE — BROKEN (CABIN)

FOUND FLOOR TRACK LIGHT INOPERATIVE AT AFT LEFT BIFFY. REPAIRED BROKEN WIRE, TRACK LIGHT CHECKS GOOD. (M)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT)

YUR - ON DEPARTURE FROM YUR, GEAR WAS IN TRANSIT UP AND THE FIRE WARNING BELL AND FIRE WARNING LIGHTS ILLUMINATED. BOTH CARGO SMOKE FAULT LIGHTS ILLUMINATED. PRESSED FIRE WARNING AND ALL LIGHTS WENT OFF, AND BELL SILENCED. PERFORMED FIRE TEST ON ENGINES, APU AND CARGO SMOKE SYSTEM ALL OPS NORMAL. REFORMED FORWARD AND AFT CARGO FIRE SYSTEM TEST, VISUALLY INSPECTED SMOKE DETECTORS IN CARGO PITS, NO DEFECTS NOTED. AT NO TIME WAS THERE ANY EVIDENCE OF FIRE OR SMOKE. NO DEFECTS NOTED ON INSPECTION. ALL OPS NORMAL. (M)

Part: MODULE — BURNED (FUEL SYSTEM)

SEA - AFTER TAKEOFF AT SEVERAL HUNDRED FEET, NR 1 FUEL TANK FORWARD PUMP LIGHT ILLUMINATED IN CONJUNCTION WITH A 'POP' FOLLOWED BY SMOKE IN THE COCKPIT AND AN ELECTRICAL SMELL. RETURNED TO FIELD AND LANDED UNEVENTFULLY. FOUND SHORT CIRCUIT BETWEEN OPEN AND CLOSED WIRE OF NR 1 ENGINE SHUTOFF VALVE AND THE 115 VOLT AC RETRACT WIRE FOR THE OUTBOARD LANDING LIGHT. REMOVED AND REPLACED FUEL SYSTEM MODULE ASSEMBLY. OPERATIONAL CHECKED NORMAL IAW MM. (M)

Part: SLEEVE — WORN (FAIRING)

SEA - DURING SCHEDULED C-CHECK, THE NR 2 ENGINE INBOARD AND OUTBOARD SLEEVE TO STRUT FAIRING WERE FOUND TO HAVE WEAR MARKS. REPAIRED PER EA 5450-01044 AND BOEING TELEX ASA-SEA-00-00070H. (M)

Part: STRUT — WORN (FAIRING)

SEA - DURING SCHEDULED C-CHECK, THE NR 1 ENGINE INBOARD AND OUTBOARD SLEEVE TO STRUT FAIRING WERE FOUND TO HAVE WEAR MARKS. REPAIRED PER EA 5450-01044 AND BOEING TELEX ASA-SEA-00-00070H. (M)

Part: SKIN — GOUGED (LE FLAP)

SEA - DURING SCHEDULED C-CHECK, THE LEFT WING OUTBOARD FOREFLAP INBOARD END L/E SKIN WAS FOUND TO BE GOUGED. REPAIRED PER EA 5750-01374. (M)

Part: CARGO TRACK — CORRODED (BS 827)

SEA - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT TIE DOWN TRACK WAS FOUND TO BE CORRODED AT STATION 827. REPAIRED PER EA 5320-01402. (M)

Part: BOLT — LOOSE (LT COCKPIT)

SEA - PRIOR TO FLIGHT 426 - CREW REPORTED THAT THE CAPTAINS WINDOW WAS BINDING. INSPECTED AND FOUND THAT THE LOWER ROLLER BEARING ATTACH BOLT WAS LOOSE. TIGHTENED BOLT. CLEANED AND LUBRICATED TRACK. WINDOW OPERATED NORMALLY. (M)

Part: FUSE — FAILED (R-2 DOOR)

YVR - FLT 688 - THE R-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. FERRIED AIRCRAFT TO LAX. REPLACED FUSE AND EXIT LIGHT OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

SEA - PRIOR TO FLIGHT 76, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO OPEN OR CLOSE. INSPECTED DOOR, NO DEFECTS NOTED. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M)

Part: WINDOW — LACK OF LUBE (LT COCKPIT)

LAX - FLT 418 - PRIOR TO FLIGHT, THE CAPTAIN'S SLIDING WINDOW WAS FOUND DIFFICULT TO OPEN AND LATCH. REMOVED DEBRIS FROM TRACK AND LUBRICATED. WINDOW OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 6 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)