N713AS

Part: DOUBLER — MISSING (TE FLAP) · airframe 52,415 hrs · 30,055 cycles

RT INBD FORE FLAP INBD BONDED DOUBLER MISSING ADJACENT TO INBD FOREFLAP TRACK. GROUNDED - YES. REPAIRED RT INBD FOREFLAP DAMAGE ADJACENT TO INBD FOREFLAP TRACK IAW SRM 51-70-10-2R-0 WITH PERMANENT REPAIR WITH NO FURTHER ACTION REQUIRED.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 52,415 hrs · 30,055 cycles

LEFT INBD AFT FLAP HAS SMALL AREA OF DELAMINATION ON TOP SURFACE INBD END. ACFT GROUNDED. REPAIRED LEFT INBD AFT FLAP REPAIRED IAW SRM 51-70-10-2R-0.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 52,415 hrs · 30,056 cycles

RIGHT INBD AFT FLAP OB END HAS AREA OF DELAMINATION. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-0, NO FURTHER ACTION REQUIRED.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 52,012 hrs · 29,770 cycles

AFT CARGO DOOR CROSSBEAM IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CORD IAW B737 400 SRM 51 40 02 0G 0.

Part: FRAME — CRACKED (BS 747) · airframe 52,012 hrs · 29,770 cycles

FRAME BS 747 CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 FIG 2 REV 00.

Part: FRAME — CRACKED (BS 907) · airframe 52,012 hrs · 29,770 cycles

FRAME BS 907 CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 FIGURE 2 REV 00.

Part: FRAME — CRACKED (BS 807) · airframe 52,012 hrs · 29,770 cycles

FRAME BS 807 CRACKED BETWEEN STRINGERS 8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 FIGURE 2 REV 00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,012 hrs · 29,770 cycles

CABIN FRAME STA 727D CRACKED BETWEEN STR 8L AND 9L. ACFT GROUNDED. REPAIRED CABIN FRAME AT STA 727D IAW T/C AD20067609-400-53-107, FIG 2, REV 00, DATED 11SEP15.

Part: FRAME — CRACKED (BS 827) · airframe 52,012 hrs · 29,770 cycles

FRAME BS 827 CRACKED BETWEEN STRINGERS 8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME7 IAW T/C AD20062609-400-53-107 FIGURE 2 REV 00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,012 hrs · 29,770 cycles

CABIN FRAME STA 867 CRACKED BETWEEN STR 8R AND STR 9R. ACFT GROUNDED. REPAIRED CABIN FRAME AT STA 867 IAW T/C AD20062609-400-53-107, FIG 2, REV 00, DATED 09/11/2015.

Part: FRAME — CRACKED (BS 827) · airframe 52,012 hrs · 29,770 cycles

FRAME BS 827 CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 FIGURE 2 REV 00.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 52,012 hrs · 29,770 cycles

DOOR SILL WEB CRACKED AT STA 294, RBL 56, SEEN FROM UNDERNEATH. ACFT GROUNDED. R & R SILL WEB IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,012 hrs · 29,770 cycles

INTERCOSTAL CRACKED BETWEEN STA 312 AND STA 328, LBL44. ACFT GROUNDED. R & R DAMAGED INTERCOSTAL IAW SRM 51-42-02-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,012 hrs · 29,770 cycles

INTERCOSTAL FROM STA 328 TO STA 344, LBL44 CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: CROSSBEAM — CRACKED (BS 840) · airframe 52,012 hrs · 29,770 cycles

AFT CARGO DOOR AFT END CROSSBEAM CRACKED. ACFT GROUNDED. REPAIRED IAW T/C AD20131312-400-52-16.

Part: STRINGER CLIP — CRACKED (BS 727) · airframe 52,012 hrs · 29,770 cycles

AFT CARGO STRINGER CLIP 20L, BS 727B IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: CROSSBEAM — CRACKED (BS 840) · airframe 52,012 hrs · 29,770 cycles

AFT CARGO DOOR AFT END CROSSBEAM CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO AFT CARGO DOOR E BEAM AFT END IAW T/C AD20131312-400-52-16.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 49,018 hrs · 27,686 cycles

RT WING OTBD FOREFLAP INBD L/E IS CHAFED ON PREVIOUS REPAIR. ACFT GROUNDED. REMOVED RT OTBD FOREFLAP INBD L/E SKIN AND INSTALLED NEW SKIN IAW SRM 51-40-04-0G-0-4 AND FIG 1.

Part: DOOR FRAME — CRACKED (BS 958-962) · airframe 49,018 hrs · 27,686 cycles

R2 DOOR FWD LOWER CORNER STUB FRAME IS CRACKED, FOUND USING B HEC INSPECTION. DURING BEAR STRAP INSPECTION. ACFT GROUNDED. R & R STUB B FRAME IAW SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CRACKED (BS 500F-540) · airframe 49,018 hrs · 27,686 cycles

RT RAM AIR DUCT INBD SUPPORT ANGLE CRACKED IN RADIUS AT AFT END. ACFT GROUNDED. R & R RT RAM AIR DUCT INBD SUPPORT ANGLE IAW SRM 51-40-02-0G-0.

Part: BEAR STRAP — CRACKED (BS 947-975) · airframe 49,018 hrs · 27,686 cycles

R2 DOOR FWD LOWER CORNER BEARSTRAP IS CRACKED. FOUND DURING LFEC INSPECTION AND VERIFIED USING BHEC. ACFT GROUNDED. REPAIRED BEAR STRAP IAW SRM 53-00-01-2R-32. THIS IS A CAT B REPAIR WITH A 24000 CYCLE INTERVAL AND 66000 CYCLE THRESHOLD CYCLES AT TIME OF REPAIR 27,686.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,574 hrs · 26,796 cycles

SKIN CRACKED, LT STABILIZER STA 125.00 AT LOWER REAR SPAR AND APPROXIMATELY 1.25" LONG. ACFT GROUNDED. SRM REPAIR 55-10-01-26-13 AND EA 400-55EA-13785.

Part: BEAM — GOUGED · airframe 46,003 hrs · 25,800 cycles

OVERHEAD BEAM GOUGED AND CHAFED AT THE FWD LAV FWD INBD ATTACH POINT. ACFT GROUNDED. REPAIRED FWD LAV INBD ATTACHED POINT WEB SECTION AND FABRICATE AND INSTALLED NEW BRACKET IAW SRM 57-70-11-09-0 AND SRM 51-40-02-0G-0.

Part: SIGN — DISLODGED (CABIN) · airframe 45,930 hrs · 25,753 cycles

EXIT ROW BETWEEN ROWS 16 AND 17, RT SIDE EXIT LIGHT IS FALLING OFF OF WALL. ACFT GROUNDED. SECURED SIGN IAW AMM 33-51-11.

Part: SKIN — CHAFED (BS 1140-1156) · airframe 42,645 hrs · 23,754 cycles

SKIN PANEL UNDER RT HORIZONTAL STAB AFT LWR ATTACH FITTING CHAFED (AT SLIDER SEAL OPENING). R & R SKIN IAW SRM 51-40-02.

Part: BRACKET — CRACKED (R1 DOOR) · airframe 42,645 hrs · 23,754 cycles

R1 DOOR ASSIST HANDLE BRACKET IS CRACKED. R & R BRACKET IAW SRM 51-40-02.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 42,645 hrs · 23,754 cycles

RT L/E HORIZONTAL STAB HAS A DEEP DENT MISPAN. REPAIRED L/E WITH PERMANENT REPAIR IAW SRM 55-10-01, REPAIR 2.

Part: FLOORBOARD — CRACKED (BS 727D-727F) · airframe 42,645 hrs · 23,754 cycles

AFT CARGO BAY FLOORBOARD 5 FT IWD CENTER HAS 3/4 HOLE. FABRICATED NEW FLOORBOARD IAW SRM 53-60-53, FIG 1 AND 51-40-05.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 42,645 hrs · 23,754 cycles

LEFT WING INBD FOREFLAP LOWER SURFACE IS DENTED AT CENTER OF FLAP REPAIRED LT WING INBD FOREFLAP LOWER SURFACE.

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 42,645 hrs · 23,754 cycles

RT W6 OTBD FOREFLAP INBD L/E IS CHAFED. REMOVED, FABRICATED AND INSTALLED NEW L/E SECTION IAW SRM 51-40-05 AND 51-40-02.

Part: HANDLE — LACK OF LUBE (L2 DOOR) · airframe 41,956 hrs · 23,339 cycles

L2 DOOR HANDLE IS VERY STIFF / HARD TO MOVE. CLEANED AND LUBED DOOR HANDLE ASSY, L2 OPS NORMAL. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,739 hrs · 22,011 cycles

EMERGENCY EXIT LIGHT AT ROW 9 DEF INOP. IN REPAIR.

Part: LINK — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

UPON REMOVING THE 65 45410 396 TO FOM FOUND LINK TO BE CRACKED ON FWD END. REPLACED PIVOT LINK BEAM IAW B737 400 SRM 51 40 02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

LT RAM AIR DUCT O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED LT RAM AIR DUCT O/B ATTACH ANGLE IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,739 hrs · 22,011 cycles

STR 19 LT AFT OF 986.5 STRINGER CLIP HAS CORROSION. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,739 hrs · 22,011 cycles

UPON REMOVAL OF L2 MOPSILL FOUND FWD DOOR WEB FOUND TO HAVE SEVERAL AREAS OF CORROSION. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 15. REPLACED IAW B737 400 SRM 51 40 05 SRM 51 40 02 W 2" O .056 R .049 L 5" D .007.

Part: RIB — CRACKED (RT WING) · airframe 39,739 hrs · 22,011 cycles

RT WING RIB LOWER CHORD CRACKED BETWEEN STR 2 AND 3 AND WBL 135.5. REPAIRED CHORD IAW EA 400 57EA 07164.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

PASSENGER CABIN LT FRAME STA 440 CRACKED BETWEEN STR 8L & 9L. REPAIRED STA 440 LT FRAME IAW EA AD 20062609 400 53 128.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,739 hrs · 22,011 cycles

R1 MOPSILL HAS AREAS OF CORROSION FWD OF DOOR OPENING AND AT AFT END OF DOOR OPENING. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 15 W 2.0 O .080 R .068 L 4.0 D .012. REPLACED MOPSILL IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 380 RT BETWEEN STRINGER 8R 9R IS CRACKED. REPAIRED STA 380 RT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 907 RT FRAME BETWEEN STRINGER 8R 9R IS CRACKED. REPAIRED STA 907 RT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 440 RT BETWEEN STRINGER 8R 9R IS CRACKED. REPAIRED STA 440 RT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 867 LT FRAME BETWEEN STRINGER 8L 9L IS CRACKED. REPAIRED STA 867 LT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 787 LT FRAME BETWEEN STRINGER 8L 9L IS CRACKED. REPAIRED STA 787 LT FRAME IAW EA AD 20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 747 RT FRAME BETWEEN STRINGER 8R 9R IS CRACKED. REPAIRED STA 747 RT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 480 FRAME LT BETWEEN STRINGER 8L 9L IS CRACKED. REPAIRED STA 480 LT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 360 LT FRAME BETWEEN STRINGER 8L 9L IS CRACKED. REPAIRED STA 360 LT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 400 RT FRAME BETWEEN STRINGER 8R 9R IS CRACKED. REPAIRED STA 400 RT FRAME IAW EA AD20062609 400 53 128.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,739 hrs · 22,011 cycles

STA 480 RT FRAME BETWEEN STRINGER 8R 9R IS CRACKED. REPAIRED STA 480 RT FRAME IAW EA AD20062609 400 53 128.

Part: SKIN — PUNCTURED (AILERON TAB) · airframe 36,324 hrs · 19,999 cycles

RT AILERON TAB PUNCTURED AT TAB MAST FAIRING. REMOVED DAMAGED PLYS BONDED REPAIR.

Part: SKIN — PUNCTURED (AILERON TAB) · airframe 36,324 hrs · 19,999 cycles

RT AILERON TAB HAS PUNCTURED SKIN AT TAB MAST FAIRING. REPAIRED SKIN.

Part: REPAIR — DELAMINATED (TE FLAP) · airframe 36,324 hrs · 19,999 cycles

LEFT WING O/B AFT FLAP LOWER SKIN PREVIOUS REPAIR IS DELAMINATED JUST ABOVE THE I/B EDGE OF NR 1 FAIRING. REPAIRED SKIN.

Part: FLAP — DELAMINATED (LT WING) · airframe 36,324 hrs · 19,999 cycles

LEFT O/B AFT FLAP O/B AFT EDGE DELAMINATED. REMOVED DAMAGED AREA AND BONDED REPAIR DOUBLER AND FILLER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 36,324 hrs · 19,999 cycles

RT LEADING EDGE NR 4 SLAT HAS DELAM ON IB UPPER SURFACE. REPAIRED THE DAMAGED AREA AND REPAIRED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 36,324 hrs · 19,999 cycles

RT LEADING EDGE NR 5 SLAT HAS DELAM JUST I/B OF THE O/B END LOWER SURFACE. REPAIRED SLAT.

Part: SKIN — DELAMINATED (SPOILER) · airframe 36,324 hrs · 19,999 cycles

RT WING NR 7 SPOILER UPPER SURFACE HAS DELAMINATION NEXT TO EXISTING REPAIR. REPAIRED WING.

Part: SPRING — DEFECTIVE (L1 DOOR) · airframe 34,788 hrs · 19,063 cycles

FSA REPORTS L1 DOOR DIFFICULT TO OPEN AND CLOSE FOUND HOLD OPEN MECHANISM CAME APART ON UPPER HINGE. REPLACED PIN WASHERS AND RETAINING SPRING ON HOLD OPEN MECHANISM FOR FORWARD ENTRY DOOR. OPERATED DOOR. OPERATED NORMAL REF AMM 52 11 21 404 002 2.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 33,209 hrs · 18,090 cycles

L1 DOOR LOWER HINGE FITTING IS CRACKED. REPAIRED LOWER HINGE FITTING.

Part: SKIN — GOUGED (FUSELAGE) · airframe 33,210 hrs · 18,090 cycles

WHILE WORKING CUSTOMER CARD N/R 00013 WHEN PAINT WAS STRIPPED FOR REPAINT FOUND DAMAGE TO SKIN. REPAIRED SKIN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,209 hrs · 18,090 cycles

WHILE WORKING REPAIR AT L2 DOOR CUTOUT FOUND FWD CORNER REVEAL FITTING TO BE CRACKED. REPLACED FITTING.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 33,209 hrs · 18,090 cycles

L1 DOOR LOWER HINGE FITTING IS CRACKED. REPAIRED LOWER HINGE FITTING.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 33,209 hrs · 18,090 cycles

LEFT I/B FORE FLAP LOWER SKIN PUNCTURED 16 INCHES FROM I/B EDGE AND 6 INCHES FROM TRAILING EDGE. REPAIRED PUNCTURE ON LEFT I/B FORE FLAP LOWER SKIN PUNCTURED 16 INCHES FROM I/B EDGE AND 6 INCHES FROM TRAILING EDGE.

Part: SKIN PANEL — CHAFED (TE FLAP) · airframe 33,209 hrs · 18,090 cycles

RT, OB MID FLAP LOWER AFT PANEL UPPER SKIN IS CHAFED AT NR4 AFT FLAP TRACK. RT OB MID FLAP LOWER AFT PANEL UPPER SKIN IS CHAFFED AT NR 4 AFT FLAP TRACK WAS REPAIRED.

Part: SKIN — CHAFED (FORE FLAP) · airframe 33,209 hrs · 18,090 cycles

LEFT O/B FORE FLAP LLE IS CHAFED AT O/B EDGE. REPAIRED LEFT O/B FORE FLAP LEADING EDGE O/B EDGE.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,209 hrs · 18,090 cycles

RIGHT O/B FORE FLAP LLE IS CHAFED AT O/B EDGE. REPAIRED RIGHT O/B FORE FLAP LEADING EDGE O/B END.

Part: SKIN — GOUGED (TE FLAP) · airframe 33,209 hrs · 18,090 cycles

LT OB MID FLAP LOWER AFT PANEL UPPER SKIN IS GOUGED AT NR 4 AFT FLAP TRACK. LT OB MID FLAP LOWER AFT PANEL UPPER SKIN IS GOUGED AT NR 4 AFT FLAP TRACK WAS REAPIRED.

Part: HINGE FITTING — CRACKED (PAX DOOR) · airframe 33,209 hrs · 18,090 cycles

DOOR HINGE FITTING IS CRACKED. REPAIRED HINGE FITTING.

Part: DOOR FRAME — DAMAGED (BS 792-797) · airframe 33,209 hrs · 18,090 cycles

AFT CARGO FWD DOORWAY FRAME DAMAGED REPLACED WEB.

Part: SUPPORT BEAM — GOUGED (RT MLG) · airframe 33,209 hrs · 18,090 cycles

FWD WEB OF RIGHT MAIN GEAR SUPPORT BEAM GOUGED OTBD OF RETRACT ACTUATOR OTBD BOLT. REPAIRED GEAR SUPPORT BEAM.

Part: SUPPORT BRACKET — CHAFED (LT MLG WW) · airframe 33,209 hrs · 18,090 cycles

SUPPORT BRACKET LT WHEEL WELL CHAFED BY FWD I/B END OF NR 4 FLAP TRACK FAIRING. REPLACED SUPPORT BEAM.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,209 hrs · 18,090 cycles

FUSELAGE SKIN DENT AT L2 DOOR CUTOUT 8 INCH ABOVE LOWER FWD CORNER ALONG SKIN EDGE. REPAIRED DAMAGED AREA IAW SRM.

Part: SLIDE — CONTAMINATED (R2 DOOR) · airframe 29,417 hrs · 16,021 cycles

RIGHT FORWARD (R 2) SERVICE DOOR EMERGENCY SLIDE FAILED TO DEPLOY DURING DURING TEST. DETERMINE THAT SLIDE WAS TIED WITH A CHORD WHICH PREVENTED IT FROM DEPLOYING. REMOVED SLIDE AND SHIPPED WITH A VIDEO OF THE FAILED DEPLOYMENT TEST. DETERMINED NO SYSTEM FAULT. NON SYSTEM STRAP LEFT IN SLIDE DURING REPACKING AT THE AIR CRUISER FACILITY CAUSED FAILURE TO DEPLOY.

Part: GUIDE ARM — WORN (L2 DOOR) · airframe 27,914 hrs · 15,217 cycles

L2 DOOR HITTING LEFT TOP OF DOOR FRAME. REPLACED ENTRY DOOR GUIDE ARM.

Part: FITTING — OUT OF ADJUST (L1 DOOR) · airframe 26,383 hrs · 14,377 cycles

L1 DOOR HARD TO CLOSE AND LOCK. ADJUSTED L1 DOOR UPPER AFT CAM FITTING. OPS CHECK GOOD.

Part: SKIN — PUNCTURED (E/E BAY DOOR) · airframe 26,150 hrs · 14,243 cycles

E&E COMPARTMENT DOOR PUNCTURED AT EXTERNAL SKIN REPAIRED PER SRM 52-00-01 FIG 201.

Part: FRAME — CRACKED (BS 2945) · airframe 26,150 hrs · 14,243 cycles

FUSELAGE FRAME CRACKED ON LWR FLANGE. REPAIRED WITH REPAIR PART PER SRM 51-40-02.

Part: SKIN — GOUGED · airframe 26,150 hrs · 14,243 cycles

FUSELAGE SKIN GOUGED WHERE DORSAL FIN SITS. REPAIRED PER EA 5330 02178.

Part: CARGO TRACK — WORN (BS 787) · airframe 26,150 hrs · 14,243 cycles

AFT CARGO PIT TIE DOWN TRACK WORN. REPAIRED WITH REPAIR PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,150 hrs · 14,243 cycles

FLOORBEAM CAP HAS CORROSION AROUND A NUT HOLES. FLOORBEAM REPAIRED IAW SRM 53-60-51 FIG 201 REPAIR 3.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 26,150 hrs · 14,243 cycles

RIGHT WING NR 5 SLAT DELAMINATED AT I/B CORNER (UPPER SKIN). RIGHT WING NR 5 SLAT DELAMINATION REPAIRED IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 26,150 hrs · 14,243 cycles

RIGHT NR 5 SLAT DELAMINATION AT THE O/B CORNER. RIGHT NR 5 SLAT DELAMINATION AT THE O/B CORNER REPAIRED IAW SRM 51-70-10 REPAIR 4.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,150 hrs · 14,243 cycles

R2 DOOR SILL CHORD CORRODED. SILL CHORD REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,150 hrs · 14,243 cycles

AFT CARGO PIT BODY FRAME FAIL SAFE ANGLE CORRODED. AFT CARGO BODY FRAME FAILSAFE REINFORCEMENT ANGLE REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05.

Part: CARGO TRACK — WORN (BS 847) · airframe 26,150 hrs · 14,243 cycles

AFT CARGO PIT TIE DOWN TRACK WORN. REPAIRED WITH REPAIR PART PER SRM 53-00-53 REPAIR 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,150 hrs · 14,243 cycles

FLOORBEAM CAP CORRODED AROUND NUT HOLES. FLOORBEAM REPAIRED PER SRM 53-60-51 FIG 201 REPAIR 3.

Part: SEAT TRACK — WORN (BS 520) · airframe 26,150 hrs · 14,243 cycles

SEAT TRACK WORN. REPAIRED WITH REPAIR PART PER SRM 53-00-02 FIG 201.

Part: SEAT TRACK — WORN (BS 520-500G) · airframe 26,150 hrs · 14,243 cycles

SEAT TRACK WORN. SEAT TRACK REPAIRED PER SRM 53-00-50 FIG 201.

Part: CARGO TRACK — CORRODED (BS 480) · corrosion level 2 · airframe 26,150 hrs · 14,243 cycles

FWD CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED WITH REPAIR PART PER SRM 53-00-53.

Part: SILL — CORRODED (BS 947-986) · airframe 26,150 hrs · 14,243 cycles

L2 DOOR SILL CHORD CORRODED. SILL CHORD REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 23,429 hrs · 12,774 cycles

NR 2 PYLON AFT FAIRING 5843R SUPPORT CROSS ANGLE CRACKED AT FASTENER HOLE 14 INCHES BELOW WING SKIN. REPAIRED PER EA 51 40 01168.

Part: SEAL DEPRESSOR — CRACKED (FWD GALLEY DOOR) · airframe 19,834 hrs · 10,879 cycles

PAE - FWD GALLEY DOOR CUTOUT FWD SIDE SEAL DEPRESSOR CRACKED ABOVE UPPER HINGE CUTOUT. REMOVED AND REPLACED. (K)

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 19,834 hrs · 10,879 cycles

PAE - AFT CARGO DOOR, EXTERNAL SKIN HAS 2EA DENTS AT O/B AFT CORNER AREA. REMOVED AND REPLACED AFT CARGO DOOR SKIN. (K)

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 19,834 hrs · 10,879 cycles

PAE - VERTICAL STABILIZER SKATE STA 1001-1016, STA 2R-3R IS CHAFED. CHAFED OUT OF LIMITS, FABRICATED AND INSTALLED NEW SKATE. (K)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 19,834 hrs · 10,879 cycles

PAE - FLOOR SUPPORT DAMAGED FROM PREVIOUS PANEL REPAIR. SPLICED IN REPAIR. (K)

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 19,834 hrs · 10,879 cycles

PAE - VERTICAL STAB SKATE STA 1001-1016, STA 21-31 IS CHAFFED. VERTICAL SKATE CHAFED OUT OF LIMITS, FABRICATED AND INSTALLED NEW SKATE. (K)

Part: ENGINE — FLAMED OUT (NR 1) · airframe 15,824 hrs · 8,725 cycles

DURING CRUISE NR 1 ENGINE EXPERIENCE ELECTRICAL POWER DISCREPANCIES AND SUBSEQUENT FLAME OUT. AIRCRAFT DIVERTED AND LANDED WITH OUT INCIDENT. WHILE PERFORMING ENGINE FUEL FEED LINES/COUPLING VACUUM TEST IAW TECH SERVICE REQUEST AND IAW AMM, FOUND THE THERMAL RELIEF VALVE ON PORT ADAPTER ASSY ON ENGINE FUEL SHUT OFF VALVE LEAKING AIR. REMOVED AND REPLACED ENGINE FUEL SHUT OFF VALVE. OPERATIONAL CHECKED GOOD.

Part: CARGO TRACK — DAMAGED (FUSELAGE)

OAK - DURING C-CHECK, FOUND AFT CARGO LEFT CARGO TRACK IS DAMAGE BEYOND LIMITS. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (STAB LE)

OAK - DURING C-CHECK, FOUND DENT IN RIGHT STABILIZER LEADING EDGE. REPAIRED IAW SRM. (M)

Part: MEMBRANE — CORRODED (FUSELAGE)

OAK - DUIRNG C-CHECK, FOUND BILGE DOOR MEMBRANE CORRODED ON TOP SIDE IN MULTIPLE LOCATIONS. REPAIRED IAW SRM. (M)

Part: SHUTOFF VALVE — LEAKING (ENGINE FUEL)

DURING CRUISE, NR 1 ENGINE EXPERIENCE ELECTRICAL POWER DISREPANCIES AND SUBSEQUENT FLAME OUT. AIRCRAFT DIVERTED TO EUG AND LANDED WITHOUT INCIDENT. SEA - WHILE PERFORMING ENGINE FUEL FEED LINES/COUPLING VACUUM TEST AS PER TECH SERVICE REQUEST AND IAW BOEING AMM 28-22-00. FOUND THE THERMAL RELIEF VALVE ON PORT ADAPTER ASSEMBLY ON ENGINE FUEL SHUTOFF VALVE LEAKING AIR. REMOVED AND REPLACED ENGINE FUEL SHUTOFF VALVE. OPS CHECKED GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 14 INOPERATIVE, WIRE DISCONNECTED. RECONNECTED WIRE, OPS CHECK NORMAL. (M)

Part: WIRE — DISCONNECTED (MID CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROWS 12 AND 13 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/STRIP AT ROWS 12 AND 13, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE RIGHT FORWARD EMERGENCY EXIT LIGHT AND THE EMERGENCY TRACK LIGHTS AT ROWS 8-12 WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY AND BATTERY CHARGER AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: CHARGER — INOPERATIVE (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE RIGHT FORWARD EMERGENCY EXIT LIGHT AND THE EMERGENCY TRACK LIGHTS AT ROWS 8-12 WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY AND BATTERY CHARGER AND ALL LIGHTS OPERATED NORMALLY. REF ASAA0040107. (M)

Part: WIRE — DISCONNECTED (MID CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 12 AND 13. RECONNECTED WIRING TO LIGHT TERMINAL AND LIGHTS OPERATED NORMALLY. (M)

Part: CABLE — DISCONNECTED (SLIDE)

SEA - DURING SCHEDULED C-CHECK, THE L2 DOOR EMERGENCY ESCAPE SLIDE RELEASE CABLE HAD COME LOOSE FROM ATTACH SCREW. REPLACED CABLE. (M)

Part: WIRE — DISCONNECTED (ROWS 12 - 13)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12-13 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 15)

OAK - PRIOR TO FLT 381, THE EMERGENCY EXIT FLOOR TRACKS LIGHTS WERE FOUND INOPERABLE IN THE CENTER CABIN AREA. RECONNECTED WIRE AT ROW 15 AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (ROW 14)

SFO - PRIOR TO FLT 357, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 14. RECONNECTED WIRING AT ROW 14, AND LIGHTS OPERATED NORMALLY. (X)