N784AS

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,631 hrs · 24,241 cycles

FOUND CRACKED INTERCOSTAL IN E RACK. REMOVED AND REPLACED INTERCOSTAL.

Part: SUPPORT — CRACKED (SPOILER) · airframe 43,631 hrs · 24,241 cycles

RIGHT WING FIX T/E INBOARD UPPER PANEL SUPPORT INBOARD OF NR 5 SPOILER CRACKED. REMOVED AND REPLACED RT FIXED T/E UPPER PANEL SUPPORT.

Part: PANEL — CHAFED (WING) · airframe 43,631 hrs · 24,241 cycles

PANEL 9220 LOWER SURFACE IS CHAFED. FABRICATED PANEL.

Part: PANEL — CRACKED (SPOILER) · airframe 43,631 hrs · 24,241 cycles

RIGHT WING T/E UPPER SURFACE PANEL O/B OF NR 5 SPOILER HAS A CRACK IN THE RADIUS. REPAIRED UPPER SURFACE OF PANEL.

Part: SKIN PANEL — CHAFED (FUSELAGE) · airframe 43,631 hrs · 24,241 cycles

PANEL 9503 HAS CHAFING DAMAGE ON THE INNER SURFACE. FABRICATED NEW PANEL.

Part: PANEL — CRACKED (SPOILER) · airframe 43,631 hrs · 24,241 cycles

RT WING T/E UPPER SURFACE PANEL O/B OF NR 5 SPOILER HAS A CRACK IN THE RADIUS. REPAIRED UPPER SURFACE PANEL.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,631 hrs · 24,241 cycles

RIGHT I/B AFT FLAP O/B END IS DELAMINATED. REMOVED EXISTING REPAIR AND ACCOMPLISHED LARGE REPAIR.

Part: SKIN — DELAMINATED (NR 1 NACELLE) · airframe 43,631 hrs · 24,241 cycles

NR NR 1 ENGINE COWL OUTER SURFACE IS DELAMINATED WITH DAMAGED FIBERS AT 1:00 POSITION. REPAIRED PER EA

Part: COWLING — DELAMINATED (NR 1 ENGINE) · airframe 43,631 hrs · 24,241 cycles

NR 1 ENGINE I/B FAN COWL LWR AFT CORNER IS DELAMINATED. REPAIRED NR 1 IB COWL.

Part: GUIDE ARM — STIFF (L1 DOOR) · airframe 40,887 hrs · 22,534 cycles

L1 DOOR HARD TO CLOSE FROM INSIDE FOUND WHILE REPOSITIONING JETWAY AFTER ARRIVAL. ADJUSTED L1 DOOR GUIDE ARM REF M/M 52-11-00-705-007-B00. OPERATED NORMALLY OK FOR SERVICE.

Part: TAB — GOUGED (LT AILERON) · airframe 40,125 hrs · 22,078 cycles

LT WING AILERON TRIM TAB T/E GOUGED. LT WING AILERON TRIM TAB T/E GOUGE REPAIRED IAW B737 400 SRM CH 51 70 06.

Part: SKIN — DENTED (TE FLAP) · airframe 40,125 hrs · 22,078 cycles

DENT 1 AND 2 (WBL 87.5 AND WBL 87.8) FOUND BEYOND ALLOWABLE LIMITS IAW B737 400 SRM 57 53 02. TRANSFERRED FROM MIG5 NR 5106400 LT INBOARD MID FLAP T/E WEDGE. LT INBOARD MID FLAP T/E WEDGE REPAIRED IAW B737 400 SRM CH 51 70 10.

Part: SKIN — DELAMINATED (LT WING AILERON) · airframe 40,125 hrs · 22,078 cycles

LT WING AILERON TRIM TAB HAS DELAM. LT WING AILERON TRIM TAB REPAIRED IAW B737 400 SRM CH 51 70 16.

Part: STRINGER CLIP — DAMAGED (BS 727F S26L) · airframe 40,125 hrs · 22,078 cycles

AFT CARGO PIT BS 727F STR 26L TIE CLIP DAMAGE. TIE CLIP REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 40 02 AND B DRAWG SPECS 69 35350.

Part: SKIN — DENTED (BS 727F) · airframe 40,125 hrs · 22,078 cycles

DENT FOUND AT A C, SKIN AT BS 727F BETWEEN STR 25L AND 26L. REPAIRED IAW ERO 8620 AND EA 5330 02385.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 40,125 hrs · 22,078 cycles

LEFT HORIZONTAL STAB LEADING EDGE PREVIOUS BLEND OUT AT APPROX STAB STA 98.70 HAS NICK IN THE BLEND OUT. NICK BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACE LEADING EDGE IAW SRM 55 10 01.

Part: FRAME — CRACKED (BS 616) · airframe 40,125 hrs · 22,078 cycles

FRAME INNER CHORD BS 616 RT BELOW FLOOR IS CRACKED FROM BOTTOM TIP TO THE LWR HOLE. REPAIRED IAW ERO 8605 AND EA 5310 028114

Part: SKIN — DAMAGED (BS 178) · airframe 40,125 hrs · 22,078 cycles

LOWER FUSELAGE SKIN DAMAGED AT BS 178 BETWEEN STR 27R AND 28R. REPAIRED IAW CASCADE ERO 8610 AND ASA EA 5330 02383.

Part: SKIN — DENTED (BS 331 S20-21R) · airframe 40,125 hrs · 22,078 cycles

DENT IN EXTERIOR SKIN OF FUSELAGE AT BS 331.5 BETWEEN STR 20R AND 21R. REPAIRED IAW CASCADE ERO 8620 AND EA 5330 02384.

Part: SKIN — DAMAGED (BS 178) · airframe 40,125 hrs · 22,078 cycles

LWR FUSELAGE SKIN DAMAGED AT FS 178 BETWEEN STR 27R AND 28R. REPAIRED IAW ERO 8610 AND EA 5330 02383.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 40,125 hrs · 22,078 cycles

RT ENGINE INLET COWL LIP SKIN AT 6 O'CLOCK POSITION MULTIPLE SCRATCHES. REPAIRED IAW GRO8617 AND EA.

Part: SKIN — DEFORMED (PAX DOO) · airframe 38,431 hrs · 21,122 cycles

L1 DOOR UPPER AFT CORNER DEFORMED. INSTALLED REPAIR DOUBLER IAW SRM 52 00 01 REPAIR 2. PAINTED PER MM 51 20 99.

Part: LENS — CRACKED (CABIN) · airframe 37,227 hrs · 20,471 cycles

EXIT INDICATOR AT EMERGENCY EXIT DOOR ROW 13 LEFT LENS FELL OFF. FOUND LENS CRACKED DUE OVER TORQUED. REPLACED LENS.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 37,094 hrs · 20,379 cycles

DAMAGE TO LEFT HORIZONTAL STABILIZER TIP DUE TO CONTACT FROM AC PUSHING BACK. REFERENCE SDR ASAA0742008. TEMPORARY REPAIR TO LEFT HAND HORIZONAL STAB TIP REPAIRED IAW CASCADE ERO 7152 AND EA 5510 01304. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 6 MONTHS.

Part: SKIN — DAMAGED (HORIZ STAB)

DAMAGE TO LEFT HORIZONAL STABILIZER TIP DUE TO CONTACT FROM AIRCRAFT PUSHING BACK INTO ALLEY. INTERM REPAIR PER EA 5510 01303 AIRCRAFT RELEASED FOR FERRY FLIGHT TO YXX.

Part: SKIN — DENTED (BS 820-832) · airframe 36,220 hrs · 19,921 cycles

FUSELAGE SKIN SCRATCHED AND DENTED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW ASA EA 5330 02212.

Part: SKIN — DENTED (BS 793-818) · airframe 36,220 hrs · 19,921 cycles

DENT IN FUSELAGE SKIN. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLERS DOUBLERS AND TRIPLER IAW ASA EA 5330 02211.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,220 hrs · 19,921 cycles

LEFT WING O/B TRAILING EDGE FLAP IS DELAMINATED AT I/B AFT CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: ATTACH FITTING — CRACKED (NR 4 SPOILER) · airframe 36,220 hrs · 19,921 cycles

NR 4 GROUND SPOILER O/B ACTUATOR ATTACH FITTING IS BROKEN IN TWO PIECES. NR 4 GROUND SPOILER REMOVED AND REPLACED IAW AMM 27-62-12.

Part: FRAME — CRACKED (BS 827) · airframe 36,220 hrs · 19,921 cycles

FRAME SKIN ATTACHMENT ANGLE IS CRACKED AT ATTACHMENT HOLE. REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR SHEAR TIE FILLER AND ANGLE IAW SRM 53-00-07 REPAIR 3.

Part: SHEAR TIE — CRACKED (BS 807) · airframe 36,220 hrs · 19,921 cycles

SHEAR TIE IS CRACKED. REMOVED DAMAGED SECTION OF FRAME SHEAR TIE, FABRICATED AND INSTALLED REPAIR SHEAR TIE FILLER AND ANGLE IAW SRM 53-00-07 REPAIR 3.

Part: FITTING — GOUGED (SPOILER) · airframe 36,220 hrs · 19,921 cycles

NR 9 FLIGHT SPOILER FITTING IS GOUGED AT ACTUATOR ATTACH POINT. REMOVED AND REPLACED SPOILER ASSY IAW AMM 27-62-71.

Part: CARGO TRACK — GOUGED (BS 470-512) · airframe 36,220 hrs · 19,921 cycles

CARGO TIE DOWN IS GOUGED. REMOVED DAMAGED SECTION OF TRACK, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW ASA EA 5310 02722.

Part: FRAME — CORRODED (BS 727E) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

FRAME IS CORRODED. REMOVED CORRODED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR SECTION OF FRAME IAW SRM 53-00-07 REPAIR 3.

Part: FITTING — CORRODED (NR 4 SPOILER) · airframe 36,220 hrs · 19,921 cycles

NR 4 SPOILER INBOARD ACTUATOR MOUNT FITTING HAS FRETTING CORROSION. REMOVED FITTING, INSTALLED NEW FITTING IAW SRM 51-40-02.

Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 36,220 hrs · 19,921 cycles

NR 3 SLAT INBOARD TRAILING EDGE HAS COMPOSITE LAYERS SHOWING. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

FLOORBEAM UPPER CHORD IS CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAP AND TAPERED SHIMS IAW ASA EA 5310 02721.

Part: STIFFENER — CORRODED (BS 1125) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

APU AIR INLET TORQUE BOX OPENING AFT VERTICAL STIFFENER CORRODED AT FASTENER HOLES. REMOVED CORRODED STIFFENER, FABRICATED AND INSTALLED STIFFENER IAW SRM 51-30-01 AND 51-40-02.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 36,220 hrs · 19,921 cycles

NR 4 SLAT IS CHAFED AT INBOARD CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (T/E FLAP) · airframe 36,220 hrs · 19,921 cycles

LEFT WING O/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

WEB BELOW R1 DOOR CUTOUT IS CORRODED ON LOWER SURFACE. REMOVED CORRODED WEB, FABRICATED AND INSTALLED NEW WEB IAW SRM 51-40-02.

Part: TAB — CRACKED (ELEVATOR) · airframe 36,220 hrs · 19,921 cycles

RIGHT ELEVATOR TAB NR 3 HINGE CUTOUT IS CRACKED. PREPPED DAMAGED AREA, FABRICATED AND BONDED REPAIR IAW SRM 51-70-17 REPAIR 7.

Part: SILL — CORRODED · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

R1 DOOR SILL (INNER CHORD) IS CORRODED. REMOVED CORRODED SILL, REPLACED WITH NEW PART IAW SRM 51-40-02.

Part: TAB — DELAMINATED (AILERON) · airframe 36,220 hrs · 19,921 cycles

LEFT AILERON TAB IS DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERION TAB IAW AMM 27-11-21 PG 401.

Part: SILL — CORRODED (BS 915-1006) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

LEFT AFT MOP SILL CORRODED (INNER CHORD). REMOVED CORRODED SILL, REPLACED SILL WITH NEW PART IAW SRM 51-40-02.

Part: SILL — CORRODED (BS 915-1006) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

AR AFT MOPSILL CORRODED (INNER CHORD). REMOVED CORRODED SILL, REPLACED SILL WITH NEW PART IAW SRM 51-40-02.

Part: WEB — CRACKED (BS 950-986) · airframe 36,220 hrs · 19,921 cycles

FLOOR WEB BELOW L2 DOOR CRACKED (UNDER MOPSILL). REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 36,220 hrs · 19,921 cycles

FLOORBEAM CORRODED UPPER CHORD. REMOVED CORRODED SECTION OF UPPER CHORD FABRICATED AND INSTALLED REPLACEMENT CHORD ANGLES AND SHIMS IAW SRM 53-10-51.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 36,220 hrs · 19,921 cycles

AFT CABIN FLOOR WEB PUNCTURED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-70-13 FIG 1.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 35,478 hrs · 19,516 cycles

EVAC SLIDE NEW FROM STOCK INFLATION CABLE MISROUTED AT GIRT FROM MANUFACTURES OVERAHUL. REROUTED INFLATION CABLE PRIOR TO INSTALLATION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,546 hrs · 17,888 cycles

FOUND CORROSION ON FRAME. REPLACED FRAME PER SRM 51 40 02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,546 hrs · 17,888 cycles

AFT CARGO DOOR CUTOUT FRAME HAS CORROSION ON UPPER FLANGE AND VERICAL FLANGE FWD SIDE. CUT OUT DAMAGED ON FLANGE AND REPAIRED PER SRM 51 70 11 REMOVED CORROSION FROM REFIT SIDE OF FRAME 6IN BY 3IN BY .006. IN LIMITS PER SRM 51 20 01 AND 53 00 07.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO BAY OBLONG HOLE IN FRAME. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51 70 11.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO BAY OBLONG HOLE IN FRAME. REMOVED DAMAGED SECTION OF FRAME FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51 70 11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO BAY CORROSION FOUND ON FRAME SHEAR TIE. REMOVED DAMAGED SECTION OF SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 07.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO COMPARTMENT CORROSION ON BACK SIDE OF FRAME. REMOVED CORROSION ON FRAME FOUND TO BE OUT OF LIMITS REPLACED FRAME PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO COMPARTMENT CORROSION ON SHEAR TIE. REMOVED DAMAGE FABRICATED AND INSTALLED NEW SHEAR TIE PR SRM 53 00 07.

Part: FRAME — DENTED (BS 727C) · airframe 32,546 hrs · 17,888 cycles

FOUND AFT CARGO FRAME DENTED. REPAIRED FRAME IAW SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

FOUND AFT CARGO BAY CORROSION ON FRAME SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727F S26-27R) · airframe 32,546 hrs · 17,888 cycles

FOUND AFT CARGO BAY CORROSION ON FRAME SHEAR TIE. REMOVED DAMAGED PARTS OF FRAME FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 747 S29-27R) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO COMPARTMENT FRAME CORRODED. REMOVED DAMAGED PORTION OF FRAME FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — CORRODED (BS 747) · airframe 32,546 hrs · 17,888 cycles

FOUND CORROSION ON FRAME. REMOVED CORRDED AREA OF FRAME SHEARTIE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 07.

Part: SHEAR TIE — DAMAGED (BS 767) · airframe 32,546 hrs · 17,888 cycles

AFT CARGO COMPARTMENT ON SHEAR TIE. REMOVED DAMAGED SECTION OF SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 7.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,546 hrs · 17,888 cycles

FOUND FRAME CORRODED ON FWD SIDE. REMOVED CORRODED SHEAR TIE FABRICATED AND INSTALLED SHEAR TIE PER SRM 53 00 17 PG 201.

Part: SHEAR TIE — CORRODED (BS 500B S27-28R) · airframe 32,546 hrs · 17,888 cycles

FOUND FRAME CORRODED ON FWD SIDE. REMOVED SHEAR TIE FABRICATED AND INSTALLED SHEAR TIE PER SRM 53 00 07 PG 201.

Part: SKIN — CHAFED (L/E SLAT) · airframe 32,546 hrs · 17,888 cycles

NR 1 SLAT LOWER TRAILING EDGE SKIN CHAFED. REPAIRED NR 1 SLAT IAW SRM 57 43. 01.

Part: CHANNEL — CRACKED (NLG WW)

PAE - LT CHANNEL BELOW WXR UNIT IN NOSE BAY CRACKED. REMOVED, FABRICATED AND INSTALLED LT CHANNEL BELOW WXR UNIT IN NOSE BAY. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - CORROSION ON FLOORBEAM AT FASTENER HOLE STA B344, LBL 25, WL 208. REPAIRED IAW SRM 53-00-51, FIG 203. (K)

Part: SKIN — LIGHTNING STRIKE (NOSE COMPT DOOR)

PAE - LIGHTING STRIKE ON NOSE COMPARTMENT DOOR SKIN. REPAIRED LIGHTING STRIKE. (K)

Part: WIRE — LOOSE (CABIN)

DEN - FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE AT SEAT POSITION 22C. RECONNECTED LOOSE WIRE AND SECURED. OPS CHECK GOOD. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT LEFT Z-ANGLE HAS CORROSION BETWEEN STATION 727G AND 770, MARKED. REPAIRED IAW SRM 53-60-53 PAGE 209. (M)

Part: LIGHT — INOPERATIVE (ROW 13-15)

SAN PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FOUND INOPERATIVE AT ROW 13-15. REATTACHED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

PDX - DURING LINE CHECK, FOUND FLOOR TRACK IGHTING INOPERATIVE AT ROW 13-15. RECONNECTED WIRES, OPS CHECKED GOOD. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS 480 AND STRINGER 22L. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (LT WING)

DURING SI CHECK, FOUND ANGLE CRACKED ON LEFT WING TRAILING EDGE. REPAIRED IAW EA. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING SI CHECKED, FOUND FRAME CRACKED AT BS 400 BETWEEN STRINGER 7R AND 8R AT FORWARD FASTENER HOLES. REPAIRED IAW SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D AND STRINGER 18. REPAIRED IAW SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING SI CHECK, FOUND DENTED FRAME AT BS 787 BETWEEN STRINGER 24 AND 25. REPAIRED IAW SRM. (M)

Part: SUPPORT — CHAFED (RT WING)

PAE - DURING SI CHECKED, FOUND RIGHT WING TRAILING EDGE PANEL SUPPORT IS CHAFED ABOVE PYLON CUTOUT. REPAIRED IAW SRM. (M)

Part: SUPPORT — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT DAMAGED AT BS 500D-G. REPAIRED IAW SRM. (M)

Part: WEB — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CLOSE OUT WEB IS DAMAGED, AT BS 492.4, RBL 27 AND WL 156. REPAIRED IAW SRM. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT ATTACH ANGLE CRACKED AT BS 500 AND RBL 25. REPAIRED IAW SRM. (M)

Part: ANGLE — WORN (FUSELAGE)

DURING SI CHECKED, FOUND VERTICAL STABILIZER SKATE ANGLE WORN. REPAIRED IAW SRM. (M)

Part: FLANGE — CORRODED (CARGO DOOR)

PAE - DURING SI CHECK, FOUND CORROSION ON UPPER FLANGE AT BS 492, RBL 24 AND WL 156 FWD CARGO DOOR. REPAIRED IAW SRM. (M)

Part: SUPPORT — DAMAGED (RT WING)

PAE - DURING SI CHECKED, FOUND RIGHT WING UPPER TRAILING EDGE PANEL SUPPORT HAS FASTENER HOLE ELONGATED AT WBL 70 AT BS 729. REPAIRED IAW SRM. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

DURING SI CHECKED, FOUND FORWARD CARGO COMPARTMENT ATTACH ANGLE CRACKED AT BS 500F AND LBL 25. REPAIRED IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING SI CHECK, FOUND CRACKED FRAME AT BS 360 FROM STRINGER 7 TO STRINGER 8. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORTS AT BS 727E TO 818 AND 727 TO 767 AND 927 TO 947, AND LEFT/RIGHT BL 20 AND FROM WL 156 TO 175. REPAIRED IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING SI CHECK, FOUND CRACKED FRAME AT BS 400 AT STRINGER 7R AND 8R. REPAIRED IAW SRM. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

DURING SI CHECK, FOUND CRACKED SKIN STIFFENERS AT BS 291 AND STRINGERS 9R, 10R AND 12R. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING SI CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPAIRED IAW SRM. (M)

Part: SUPPORT — DAMAGED (LT WING)

DURING SI CHECKED, FOUND LEFT WING UPPER TRAILING EDGE PANEL SUPPORT HAS FASTENER HOLE ELONGATED AT WBL 70 RIGHT AND BS 729. REPAIRED IAW SRM. (M)

Part: FRAME — DAMAGED (FUSELAGE)

DURING SI CHECK, FOUND FRAME WEB DAMAGED AT BS 793 BETWEEN STRINGER 27R AND 25R. REPAIRED IAW SRM. (M)

Part: ANGLE — GOUGED (FUSELAGE)

PAE - DURING SI CHECKED, FOUND VERTICAL STABILIZER RIGHT SKATE ANGLE GOUGED. REPAIRED IAW SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION AND DENT ON SIDEWALL SUPPORT ANGLE AT BS 727B AND STR 25R. REPAIRED IAW SRM. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - DURING CHECKED, FOUND SEAT TRACKS IS DAMAGED AT BS 540 LEFT AND RIGHT BL 25, LEFT AND RIGHT BL 45 AND WL 208. REPAIRED IAW SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - DURING C-CHECKED, FOUND FORWARD CARGO COMPARTMENT STRINGER CLIP IS CRACKED .25 INCH AT BS 480 AND STRINGER 22L. REPAIRED IAW SRM. (M)

Part: ACM — LEAKING (A/C BAY)

PDX - DURING CLIMB-OUT AT ABOUT 15,000 FEET FLIGHT ATTENDANT REPORTED ODOR IN THE CABIN. DIVERTED TO PDX. NO SMOKE OR FIRE WAS NOTED. LANDED WITHOUT INCIDENT, INSPECTED AND FOUND LEFT AIR CYCLE MACHINE LEAKING OIL. REMOVED AND REPLACE ACM, OPS NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 15-18. RECONNECTED LIGHTS OPS NORMAL. (M)

Part: WIRE — LOOSE (CABIN)

PSP - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 10, LOOSE WIRING. INSPECTED AND FOUND LOOSE WIRING, RECONNECTED WIRING. OPS CHECK NORMAL. (M)

Part: SLIDE — DAMAGED (CABIN)

YVR - DURING PREFLIGHT FOR FLIGHT 654, CREW REPORTED THAT THE R1, R2, AND L2 DOOR EVACUATION SLIDE MANUAL INFLATION HANDLES WERE MISSING. REPLACED THE R1, R2, AND L2 DOOR EVACUATION SLIDES. (M)

Part: FITTING — FRETTING (ELEV HINGE)

SEA - DURING C-CHECK, THE LEFT AND RT HORIZONTAL STAB OUTBOARD HINGE FITTINGS WERE FOUND TO BE FRETTING. REPAIRED PER EA 5520-01055. (M)

Part: SKIN — DAMAGED (BS 1138)

SEA - DURING C-CHECK, FOUND DAMAGE ON THE FUSELAGE CUTOUTS FOR THE APU ACCESS DOOR HINGE. REPAIRED PER EA 5380-01006 AND BOEING TELEX ASA-SEA-98-0069RR. (M)

Part: SKIN — DENTED (RT TE MIDFLAP)

SEA - DURING C-CHECK, RIGHT INBOARD MID FLAP WEDGE LOWER SURFACE WAS FOUND TO BE DENTED. REPAIRED PER EA 5750-01272 AND BOEING TELEX ASA-SEA-98-0062RR. (M)

Part: SPAR — DELAMINATED (RT AILERON)

SEA - DURING C-CHECK, FOUND DELAMINATION IN THE LOWER INBOARD EDGE OF THE RT AILERON FRONT SPAR. REPAIRED PER EA 5760-01008 AND BOEING TELEX ASA-SEA-98-0063RR. (M)

Part: DOOR — DAMAGED (NR 2 ENG TR)

SEA - DURING C-CHECK, THE NR 2 ENGINE INBOARD T/R MID ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO BE DAMAGED. REPAIRED PER EA 7110-01064 AND BOEING TELEX ASA-SEA-98-0061RR. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENNCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15 THROUGH 17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)