N765AS

Part: SNUBBER — OUT OF ADJUST (L2 DOOR) · airframe 71,585 hrs · 47,963 cycles

FA REPORTS L2 DOOR HARD TO OPEN, ALMOST LIKE HINGES NEED TO BE LUBRICATED. GROUNDED - YES. FOUND L2 DOOR SNUBBER BOTTOMING OUT WITH DOOR CLOSED. ADJUSTED SNUBBER LENGTH AS REQUIRED PER AMM 52-13-11. OPS CHECK OF DOOR GOOD.

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · airframe 71,527 hrs · 47,913 cycles

AFT CARGO DOOR THRESHOLD AFT CORNER CRACKED. ACCOMPLISHED TEMP REPAIR PER EA 5310-01251. ACFT GROUNDED.

Part: SNUBBER — FAILED (L2 DOOR) · airframe 71,477 hrs · 47,874 cycles

FA'S REPORTS L2 DOOR STIFF AND HARD TO OPEN/CLOSE. GROUNDED, YES. REMOVED & REPLACED SNUBBER REF AMM 52-13-71. OPS CK'S GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,740 hrs · 47,249 cycles

R1 DOOR CUTOUT AFT FRAME IS CRACKED AT FASTENER HOLE BENEATH LOWER AFT CORNER REVEAL. ACFT GROUNDED. REPAIRED DAMAGE TO FRAME STA 332.1 IAW EA 400-53EA-17552. THIS IS A CAT-B REPAIR WITH 1ST AND 2ND STAGE APPROVAL, DTE 3RD STAGE APPROVAL IS REQUIRED PRIOR TO THE INSPECTION THRESHOLD OF 66,000 TOTAL A/C CYCLES.

Part: SKIN — CRACKED (BS 332) · airframe 70,740 hrs · 47,249 cycles

R1 DOOR CUTOUT LOWER AFT CORNER CRACKED. ACFT GROUNDED. REPAIRED IAW SRM 53-10-01-2R-19.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,740 hrs · 47,249 cycles

VHF NR 2 INTERNAL PAN CRACKED. ACFT GROUNDED. ACCOMPLISHED REPAIRS TO INTERNAL SUPPORT PAN AND FUSELAGE SKIN IAW T/C AD2016-1004-53-3 AND EA AD20161004-400-53-102. THIS IS A CATEGORY B REPAIR WITH 1ST AND 2ND STAGE APPROVAL DTE. STAGE 3 APPROVAL IS REQUIRED PRIOR TO THE INSPECTION THRESHOLD OF 75,000 TOTAL FLT CYCLES.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 70,740 hrs · 47,249 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN AFT SIDE BETWEEN HSS 136 AND 146 IS CRACKED. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-4.

Part: SKIN — CRACKED (BS 727D) · airframe 70,740 hrs · 47,249 cycles

CHEM MILL HAS A CRACK IN THE RT FUSELAGE SKIN, BS 727D+2. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01-2R-31 DET VII.

Part: SKIN — CRACKED (BS 291) · airframe 70,740 hrs · 47,249 cycles

RIGHT FUSELAGE AT R1 DOOR LOWER HINGE CUTOUT IS CRACKED. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-10-01-2R-15.

Part: TRACK — DIRTY (PAX DOOR) · airframe 70,249 hrs · 46,838 cycles

F/A REPORTS L2 DOOR DIFFICULT TO OPERATE. ACFT GROUNDED. INSPECTED L2 DOOR, IAW AMM 52-13-00-206-001. FOUND NO OBVIOUS DEFECTS. OPERATED L2 DOOR THROUGH MULTIPLE CYCLES, DOOR OPERATES SMOOTHLY. IAW AMM 52-13-00/501. CLEANED DOOR TRACKS AS PRECAUTION. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (BS 945) · airframe 69,108 hrs · 45,873 cycles

SKIN IS CRACKED AT BS 945 AT 24L. ACFT GROUNDED. REPAIRED SKIN IAW EA AD20131808-400-53-118 CAT B, STAGE 2 TRACKING UNDER AD20131808-400-53-119.

Part: SKIN — CRACKED (BS 727E-727F) · airframe 69,108 hrs · 45,873 cycles

SKIN IS CRACKED AT BS 727F +1 AT S21R. ACFT GROUNDED. CUTOUT AND REPAIRED DAMAGE TO FUSELAGE SKIN AT BS 727F+1 AND STR 21R IAW SRM 53-00-01, REP 31. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 FLT CYCLES REFER TO OPERATORS REPAIR ASSESSMENT PROGRAM FOR METHODS AND INTERVALS.

Part: SHEAR TIE — CRACKED (BS 500B) · airframe 68,410 hrs · 45,294 cycles

SKIN ATTACH FRAME, P/N 007-00420-10 AT FS 500B BETWEEN STRS 2 AND 3 LT IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. R & R SHEAR TIE IAW SRM 51-40-02-0G-0 PARA 4.

Part: RIB — CRACKED · airframe 68,410 hrs · 45,294 cycles

RIGHT WBL 135, RIB CHORD FOUND CRACKED WHILE ACCESSING FASTENERS ON NR-00021 UPPER WING AFT PYLON FAIRING. ACFT GROUNDED. REPAIRED RT WING RIB CHORD AT WBL 135 IAW EA 400, 57 EA 15473.

Part: RIB — CRACKED (LT WING) · airframe 68,410 hrs · 45,294 cycles

LT WBL 135 RIB CHORD FOUND CRACKED WHILE ACCESSING FASTENERS ON NR 00021, UPPER WING AFT PYLON FAIRING. ACFT GROUNDED. REPAIRED LT WING RIB CHORD AT WBL 135 IAW EA 400, 57 EA 15473.

Part: SKIN — CRACKED (BS 951-972) · airframe 68,410 hrs · 45,294 cycles

L2 DOOR CUTOUT FWD LOWER CORNER HAS CRACK INDICATION. REMOVAL OF MARKED FASTENER IS REQUIRED TO VERIFY USING BHEC INSPECTION. GROUNDED - YES. REPAIRED L2 DOOR CUTOUT FWD LWER SKIN IAW SRM 53 00 01 2R 32 REPAIR 32.

Part: SKIN — CRACKED (BS 951-972) · airframe 68,410 hrs · 45,294 cycles

L2 DOOR CUTOUT FWD LOWER CORNER HAS CRACK INDICATION. REMOVAL OF MARKED FASTENER IS REQUIRED TO VERIFY USING BHEC INSPECTION. ACFT GROUNDED. REPAIRED L2 DOOR CUTOUT FWD LOWER SKIN IAW SRM 53-00-01-2R-32, REPAIR 32. THIS IS A CATEGORY B REPAIR WITH A THRESHOLD OF 66,000 CYCLES AND AN INTERVAL OF 24,000 CYCLES AT TIME OF REPAIR IS 45,294.

Part: SKIN — CRACKED (BS 947-967) · airframe 68,410 hrs · 45,294 cycles

AFT GALLEY R2 SERVICE DOOR, CUT OUT LOWER FORWARD CORNER IS CRACKED FROM CORNER EXTENDING THROUGH 3 FASTENERS AND IS APPROXIMATELY 3" LONG. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01-2R-32.

Part: FRAME — CRACKED (BS 500F) · airframe 68,410 hrs · 45,294 cycles

FRAME 500F LT HAS A CRACK .25" LONG EXTENDING INBD AT 9:00 POSITION FROM 1" WIRE PENETRATION HOLE. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 68,410 hrs · 45,294 cycles

RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER SKIN BETWEEN RIBS 5 AND 6 STAB STA 120.30-129.50 HAS .2500" CRACK IN LENGTH. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER LWR SKIN BETWEEN RIB 5 AND 6, STABILIZER BS 120.30- BS 129 .50, CRACKED IAW SRM 55-10-01-2R-13. THIS IS A CATEGORY B REPAIR REQ ALL OF LWR SKIN INSPECTION IN SRM 55-10-01-2R13, REPAIR 13 PARA 5.A AT INTERVALS EQUALS TO OR LESS THAN 12 MOS AFTER YOU INSTALL THE REPAIR.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 68,410 hrs · 45,294 cycles

AFT CARGO DOOR CROSSBEAM E ON AFT END IS CRACKED. ACFT GROUNDED. REPAIRED AFT CARGO DOOR AFT END IAW ATTACHED WO 300444, AD 20131312-400-52-6.

Part: WEB — CRACKED (BS 796-844) · airframe 68,410 hrs · 45,294 cycles

AFT CARGO DOOR CROSSBEAM AND WEB ARE CRACKED AT FWD END. ACFT GROUNDED. REPAIRED AFT CARGO DOOR CROSSBEAM AND WEB IAW ATTACHED WO 300444, AD20131312-400-52-5.

Part: WEB — CRACKED (BS 796-844) · airframe 68,410 hrs · 45,294 cycles

AFT CARGO DOOR CROSSBEAM AND WEB ARE CRACKED AT FWD END. ACFT GROUNDED. REPAIRED AFT CARGO DOOR CROSSBEAM AND WEB IAW ATTACHED WO 300444, AD20131312-400-52-5.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 67,899 hrs · 44,869 cycles

L-1 DOOR EMERGENCY EXIT LIGHT LENS ADJACENT TO JUMP SEAT, FELL OFF. ACFT GROUNDED. RE-INSTALLED LENS. OK FOR SERVICE.

Part: SKIN — CRACKED (BS 727F) · airframe 67,848 hrs · 44,836 cycles

FOUND POSSIBLE CRACK APPROXIMATELY 24" AFT OF LOWER LT WING TO BODY FAIRING ON 3RD LONGERON UP FROM PRODUCTION SEAM. ACFT GROUNDED. REPAIRED SKIN CRACK IAW SRM 53-00 01-2R-31 DETAIL IX.

Part: SKIN — CRACKED (BS 727E-727F) · airframe 67,313 hrs · 44,406 cycles

CRACK IN FUSELAGE SKIN FOUND 10 INCHES ABOVE S-25R LOCATION 727F+ 18 TO 727F + 20 RIGHT ABOVE EDGE OF SR- 24R VERIFIED CRACK WITH HFEC PART 6. CHUBBARD 57797. GROUNDED - YES. (RESOLVED ON W/O: 289152 TASKCARD: N/R-00001 ) REPAIRED CRACK IN FUSELAGE SKIN @ S25R, 727F IAW B737 400 SRM 53 00 01 2R 31 DETAIL VII CATEGORY B REPAIR 60,000 CYCLES THRESHOLD FOR METHODS AND INTERVALS REFER TO THE OPERATORS REPAIR ASSESSMENT PROGRAM.

Part: DOOR — OUT OF ADJUST (L1) · airframe 66,649 hrs · 43,848 cycles

FLEET SERVICE REPORTS UNABLE TO CLOSE THE L1 DOOR. ACFT GROUNDED. PERFORMED L1 DOOR FORCE CHECK, EXCEEDED LIMITS TO CLOSE THE DOOR. REF 52-11-00-755-051 STEP ED 5, E). ADJUSTED L1 DOOR IAW MM 52-11-00-705-007. ENTRY DOOR TEST GOOD IAW MM 52-11-00-755-051. OPS TEST GOOD.

Part: SEAL DEPRESSOR — CRACKED (BS 329) · airframe 66,646 hrs · 43,847 cycles

R1 DOOR A CRACK WAS FOUND ON THE UPPER SEAL DEPRESSOR AT THE AFT END. ACFT GROUNDED. R & R UPPER AFT CORNER SEAL DEPRESSOR, CORNER REVEAL, ON R1 DOOR CUTOUT IAW SRM 51-40-02-0G-0, PARA 4.

Part: SEAL DEPRESSOR — CRACKED (R1 DOORWAY) · airframe 66,646 hrs · 43,847 cycles

R1 DOOR UPPER FWD CORNER SEAL DEPRESSOR CRACKED. ACFT GROUNDED. R & R R1 DOOR FWD UPPER SEAL DEPRESSOR IAW SRM 51-40-02-0G-0.

Part: SEAL DEPRESSOR — CRACKED (BS 299) · airframe 66,646 hrs · 43,847 cycles

FOUND R1 DOOR SEAL DEPRESSOR JUST ABOVE UPPER HINGE CUT OUT CRACKED. ACFT GROUNDED. R & R R1 DOOR SEAL DEPRESSOR JUST ABOVE UPPER HINGE CUTOUT IAW SRM 51-40-02-0G-0.

Part: HANDLE — OUT OF ADJUST (L1 DOOR) · airframe 65,440 hrs · 42,808 cycles

L1 DOOR HANDLE DIFFICULT TO PUSH DOWN AND CLOSE DOOR. ACFT GROUNDED. ADJUSTED CONTROL RODS UPPER AND LOWER AT CONTROL ROD ONE FLAT OUT IAW AMM 52-11-00. ADJUSTED TORQUE TUBE NUTS ONE FLAT EACH FOR UP MOVEMENT IAW AMM 52-11-0. ADJUSTED HANDLE CONTROL PUSH ROD TO TORQUE TUBE 180 PERCENT OUTWARD IAW 52-110. LIGHT INDICATION AGREED WITH DOOR POSITION. ACCOMPLISHED FORWARD ENTRY DOOR TEST IAW AMM 52-11-00-755-051, ALL TESTS PASSED. OK FOR SERVICE.

Part: SEAL — OUT OF POSITION (L1 DOOR) · airframe 64,887 hrs · 42,318 cycles

L1 DOOR IS BINDING AND HARD TO CLOSE. ACFT GROUNDED. REPOSITIONED L1 DOOR BULB SEAL, NO BINDING NOTED AFTER SEAL REPOSITION IAW 52-11-31.

Part: CARGO TRACK — CRACKED (BS 727) · airframe 64,887 hrs · 42,318 cycles

WHILE PREPPING FOR CIC APPLICATION, FOUND AFT CARGO TRACK, RBL 13.8 CRACKED AT BS 727G. ACFT GROUNDED. REPAIRED CARGO TRACK IAW SRM IAW SRM 53-00-53-2R-2.

Part: STRINGER CLIP — CRACKED (BS 500) · airframe 64,887 hrs · 42,318 cycles

IN CARGO BAY STRINGER CLIP 25R BS 500E IS CRACKED, ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 500C) · airframe 64,887 hrs · 42,318 cycles

IN FWD CARGO BAY STRINGER CLIP 25R BS 500C IS CRACKED, ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 500F) · airframe 64,887 hrs · 42,318 cycles

FWD CARGO BAY FRAME BS 500F SHEAR TIE IS CRACKED BETWEEN STRINGERS 25-2LL. ACFT GROUNDED. REPAIRED SHEAR TIE IAW EA 400-53EA-12411, REV NEW.

Part: FAILSAFE — CRACKED (BS 480) · airframe 64,887 hrs · 42,318 cycles

FAILSAFE AT RT BS 480 IS CRACKED IN RADIUS JUST BELOW CABIN FLOOR LEVEL. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW FAILSAFE IAW SRM 51-40-05-0G-0. R & R NEW FAILSAFE IAW SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 500F) · airframe 64,887 hrs · 42,318 cycles

BS 500F, FRAME SHEAR TIE IS CRACKED BETWEEN STRINGERS 25&26R. FOUND DURING DISPLACEMENT OF FRAME. ACFT GROUNDED. REPAIRED SHEAR TIE IAW EA 400, 53EA 124113 REV.

Part: STRINGER — CORRODED (BS 1088) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

BS 1088 BULKHEAD APU AIR INLET CUTOUT UPPER STRINGER IS CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02.

Part: STIFFENER — CORRODED (BS 1088) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

STA 1088, BULKHEAD APU AIR INLET CUTOUT LT VERTICAL STIFFENER IS CORRODED. ACFT GROUNDED. R & R VERTICAL STIFFENER, STA 1088 BULKHEAD LT SDIE OF APU AIR INLET CUTOUT IAW SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CORRODED (BS 1088) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

BS 1088, BULKHEAD APU AIR INLET CUTOUT LOWER TORQUE BOX LINER DRAIN SUPPORT ANGLE IS CORRODED. ACFT GROUNDED. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0.

Part: STIFFENER — CORRODED (BS 1088) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

BS 1088, BULKHEAD APU AIR INLET CUTOUT RT VERTICAL STIFFENER IS CORRODED. ACFT GROUNDED. R & R RT VERTICAL STIFFENER IAW SRM 51-40-02-0.

Part: STRINGER — CORRODED (BS 1088-1139) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

APU INLET CUTOUT IN APU BAY STRINGER IS CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02-0G-0.

Part: STIFFENER — CORRODED (BS 1117) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

APU INLET CUTOUT IN APU COMPARTMENT FWD STIFFENER IS CORRODED. ACFT GROUNDED. R & R FWD STIFFENER IAW SRM 51-40-02-0G-0.

Part: STIFFENER — CORRODED (BS 1129) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

APU INLET CUTOUT IN APU COMPARTMENT AFT STIFFENER IS CORRODED. ACFT GROUNDED. R & R AFT STIFFENER IAW SRM 51-40-02-0G-0, W 1", O .060", R .052", L 1", D .008".

Part: FLOOR SUPPORT — CORRODED (BS 787-847) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO FLOOR SUPPORT RBL 8 IS CORRODED AROUND NUTPLATES BS 787-847. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW SRM 53-00-53-2R-1 REPAIR 1, FIG 101.

Part: CARGO TRACK — CORRODED (BS 787-847) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO TRACK LBL 3 IS CORRODED AROUND NUTPLATES, BS 787-847. ACFT GROUNDED. REPAIRED CARGO TRACK IAW SRM 55-00-53-2R-1.

Part: SKIN — CRACKED (BS 520) · airframe 64,887 hrs · 42,318 cycles

FUSELAGE SKIN HAS TWO MFEC CRACK INDICATIONS, UNDER BS 520, BELOW S14L. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-30.

Part: STRINGER CLIP — CRACKED (BS 727E) · airframe 64,887 hrs · 42,318 cycles

CRACKED STRINGER CLIP AT STR4L BS 727E. ACFT GROUNDED. R & R NEW STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 500F) · airframe 64,887 hrs · 42,318 cycles

FUSELAGE SKIN HAS CRACK INDICATION FWD OF BS 500F, JUST BELOW S10R, IN CABIN. ACFT GROUNDED. REPAIRED SKIN IAW EA AD20130901-400-53-101.

Part: CUSP WEB — CRACKED (BS 500) · airframe 64,887 hrs · 42,318 cycles

PASSENGER-CARGO FWD CABIN AREA AT FRAME BS 500 ON LT CUSP WEB FWD OTBD CORNER IS CRACKED. ACFT GROUNDED. R & R LT CUSP WEB IAW SRM 51-40-020-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 727) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO BAY RBL 6, FLOOR SUPPORT FRAME HAS CORROSION IN FWD END. ACFT GROUNDED. REPAIRED AFT FLOOR SUPPORT IAW SRM 53-00-53-2R1.

Part: FLOOR SUPPORT — CORRODED (BS 773-860) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO COMPARTMENT, RBL 20, FLOOR CAP STRIP STA 773-860 HAS MULTIPLE CORROSION SPOTS ON UPPER SIDE. ACFT GROUNDED. REMOVED CORRODED FLOOR CAP STRIP. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REPLACED NEW FLOOR CAPSTRIP IAW SRM 51-40-02-0G-0.

Part: FLOOR PANEL — CORRODED (BS 727-947) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO BAY LT FLOOR PANEL FROM BS 727 - 947 HAS MULTIPLE CORRODED AREAS. ACFT GROUNDED. R & R FLOOR PANEL IAW SRM 51-40-02-0G-0.

Part: TRANSITION PANEL — CORRODED (BS 767-793) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO BAY RT FLOOR TRANSITION PANEL, BS 767-793 HAS MULTIPLE CORROSION SPOTS. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A1. REPLACED WITH NEW IAW SRM 51-40-02-0G.

Part: SHEAR TIE — CRACKED (BS 927) · airframe 64,887 hrs · 42,318 cycles

AFT CARGO BAY AT BS 927 AND S25R FWD STRINGER CLIP IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP AFT CARGO AT STA 927 S-25R IAW SRM 51-40-02-0G-0.

Part: FRAME — CORRODED (BS 807) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO COMPARTMENT BS 807, INBD S27L, CORROSION EXIST ON FWD SIDE OF FRAME. ACFT GROUNDED. REMOVED DOUBLER FABRICATED NEW AND INSTALLED DOUBLER IAW SRM 51-40-07-0G-0 AND 53-00-07-2R-8, REPAIR 8.

Part: FLOOR SUPPORT — CORRODED (BS 787-947) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO BAY FROM BS 787 - 947.5 RT FLOOR SUPPORT CORRODED. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 727-767) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT CARGO BAY RT FLOOR SUPPORT FROM BS 727-767 HAS MULTIPLE CORRODED AREAS. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: STRINGER — CORRODED (BS 500G) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

FWD CARGO BAY AFTER S27R AND BS 500G, STRINGER CORRODED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED IAW SRM IAW SRM 53-0-03-2R-1, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 380-500) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

FWD CARGO COMPARTMENT RT FLOOR SUPPORT FROM BS 380 TO 500D SEVERAL SCREW HOLES CORRODED. ACFT GROUNDED. R & R RT FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: ANGLE — CORRODED (BS 535) · airframe 64,887 hrs · 42,318 cycles

FLOOR SUPPORT ANGLE AT BS 535 LT OTBD HAS CORROSION. ACFT GROUNDED. REPAIRED FLOOR SUPPORT ANGLE IAW SRM 51-70-12-0G-0.

Part: STRINGER CLIP — CRACKED (BS 500B) · airframe 64,887 hrs · 42,318 cycles

LT FUSELAGE STA 500B, STRINGER S-16L CLIP IS CRACKED. ACFT GROUNDED. REMOVED STRINGER CLIP, LOCATED AND DRILLED NEW, INSTALLED STRINGER CLIP AT 500R STR 16L IAW SRM 51-40-02-0G-0, STEP 4B.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 64,887 hrs · 42,318 cycles

RT FUSELAGE BS 360, BETWEEN S24-25R HAS FRAME SHEAR TIE IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-7.

Part: CREASE BEAM — CORRODED (BS 500C) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

CREASE BEAM INBD ANGLE AT BS 500C, LT OTBD HAS CORROSION. ACFT GROUNDED. REMOVED ANGLE, FABRICATED NEW, AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 380-500G) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

FWD CARGO BAY AFT LT FLOOR SUPPORT FROM BS 380-500G SEVERAL SCREW HOLES CORRODED. ACFT GROUNDED. REPAIREDFLOOR SUPPORT IAW SRM 53-30-53-2R-3.

Part: SILL — CORRODED (BS 907-1006) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT WET AREA R2 DOOR MOP SILL CORRODED. ACFT GROUNDED. R & R R2 MOP SILL IAW SRM 51-40 02-0.

Part: CHANNEL — CORRODED (BS 967-1006) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

AFT WET AREA L2 DOOR MOP SILL CORRODED. ACFT GROUNDED.. REMOVED CORROSION, CHECKED OUT OF LIMITS IAW SRM 53 60-15-1A-1, FIG 101. R & R L2 DOOR MOP SILL IAW IAW SRM 51-40-02-0G-0, W 2", O .071, R .062, L 8FT, D .009.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 64,887 hrs · 42,318 cycles

RT FWD BOTTOM HORIZONTAL STABILIZER THRUST BEAM CORNER FITTING IS CRACKED. ACFT GROUNDED. FITTING REPLACED ON SB737-55-1091-400-2 IAW EA 400, 55EA, 12366.

Part: TRACK — CORRODED (BS 540) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

LT LATERAL TRACK AT BS 540 IS CORRODED. ACFT GROUNDED. R & R LATERAL TRACK IAW AMM 20-50-11-912-002.

Part: SKIN — PUNCTURED (NR 3 SPOILER) · airframe 64,887 hrs · 42,318 cycles

LEFT WING, NR 3 SPOILER LOWER SURFACE INBD OF ACTUATOR SKIN HAS A PUNCTURE AND PRODUCTION DOUBLER. ACFT GROUNDED. REPAIRED LT WING NR 3 SPOILER LOWER SURFACE IAW EA 400, 57EA, 12286.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,887 hrs · 42,318 cycles

RT HORIZONTAL STABILIZER L/E HAS A CRACKED RIB THIRD FROM INBD. ACFT GROUNDED. REPAIRED RIB IAW EA 400, 55 & EA 12393, REV.

Part: SKIN — DENTED (TE FLAP) · airframe 64,887 hrs · 42,318 cycles

LEFT OTBD FOREFLAP HAS A DENT & DELAMINATED AREA ON UPPER SIDE APPROXIMATELY 40" FROM INBD END. ACFT GROUNDED. REPAIRED LEFT OTBD FOREFLAP DENT & DELAMINATED AREA ON UPPER SIDE APPROXIMATELY 40" FROM INBD END IAW SRM 51-70-10, R & R.

Part: SKIN — DAMAGED (SPOILER) · airframe 64,887 hrs · 42,318 cycles

LEFT WING NR 3 SPOILER LOWER SURFACE OTBD OF ACTUATOR SKIN HAS A CREASE. ACFT GROUNDED. REPAIRED LT WING NR 3 SPOILER LOWER SURFACE OTBD OF ACTUATOR IAW EA 400, 57EA 12286.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 64,887 hrs · 42,318 cycles

LT WING INBD FLAP HAS DENT IN LOWER SECTION. ACFT GROUNDED. REPAIRED LT WING INBD FLAP DENT IN LOWER T/E SECTION OF FOREFLAP IAW SRM 51-70-2R-4, REPAIR 4.

Part: HINGE FITTING — LACK OF LUBE (L2 DOOR) · airframe 64,520 hrs · 42,011 cycles

L2 DOOR DIFFICULT TO OPEN. ACFT GROUNDED. LUBRICATED HINGE GUIDE PLATES IAW AMM 12-25-11-603-001, DOOR OPERATES NORMALLY.

Part: FLOOR PANEL — SCRATCHED (PAX CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2377 TOP SURFACE HAS SCRATCHES. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 3C, PGS 1 AND 2.

Part: RETAINER — CORRODED (BS 698-671) · airframe 65,323 hrs · 37,698 cycles

RT MLG W/W NR 4 LOWER SEAL RETAINER CORRODED, LOCATED AND DRILLED NEW SEAL RETAINER IAW SRM 51-40-05-0G-0.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 65,323 hrs · 37,698 cycles

PAX CABIN FLOOR PANEL 2468Y TOPSIDE HAS NUMEROUS DENTS AND CRUSHED, MISSING CRACKED HONEYCOMB CORE. ACFT GROUNDED. REPAIRED FLOOR PANEL IAW SRM 53-00-50, PAR 36, PGS 1 AND 2.

Part: SKIN — CHAFED (LT WING) · airframe 62,504 hrs · 40,216 cycles

LT WING OTBD MIDFLAP LOWER SURFACE SKIN IS CHAFED INBD OF NR 1 FLAP TRACK FAIRING. REPAIRED IAW EA CMPT-57EA-09933.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

WEAR MARK ON THE LT OTBD MIDFLAP T/E AT THE CONTACT AREA WITH THE NR 1 FAIRING. REPAIRED THE LT OTBD MIDFLAP T/E AT THE CONTACT AREA WITH THE NR 1 FAIRING IAW EA CMPT-57EA-09933.

Part: COVER — CRACKED (L1 DOOR SLIDE) · airframe 62,504 hrs · 40,216 cycles

L1 DOOR ESCAPE SLIDE HAS CRACK AT GRIT BAR RETAINER RIVETS. ACFT GROUNDED. REPAIRED L1 DOOR ESCAPE SLIDE COVER IAW EA 400-25EA-09929, REV NEW.

Part: CARGO TRACK — DAMAGED (BS 800) · airframe 62,504 hrs · 40,216 cycles

CARGO TRACK DAMAGED. REMOVED DAMAGED SECTION OF CARGO TRACK AT BS 800 LBL 17 AND SPLICED IN NEW SECTION IAW SRM 53-00-53, FIG 201, REPAIR 2.

Part: CARGO TRACK — CORRODED (BS 887-927.5) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

AFT PIT CARGO TRACK IS CORRODED RBL 13.8, STA 907. REMOVED CORRODED ON CARGO TRACK AT STA 907, RBL 13.8, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53 60 53, FIG 101, DETAIL IX. R & R CARGO TRACK SECTION IAW SRM 53 00 53, FIG 201, REPAIR 2W 1.90 O .140 R .113 L 1.5 D .027.

Part: FLOOR PANEL — CHAFED (BS 787-847) · airframe 62,504 hrs · 40,216 cycles

AFT CARGO NR 4 FLOOR PANEL EDGE DAMAGED. FABRICATED FLOOR PANEL AND REPLACED.

Part: SKIN — DENTED (BS 992-1016) · airframe 62,504 hrs · 40,216 cycles

THREE DENTS ON FUSELAGE AFT OF L2 DOOR & FWD OF BS 1016. NR 1 DENT AT BS 1011, 9.0 BELOW S-10L LAP, NR 2 DENT AT BS 1011.5, 2.0 BELOW S-11L AND NR 3 DENT AT BS 1007, 3.5 BELOW S11L. R & R SKIN IAW SRM 51-40-02.

Part: WEDGE — DEBONDED (NR 3 SLAT) · airframe 62,504 hrs · 40,216 cycles

NR 3 SLAT T/E WEDGE UPPER SKIN HAS PREVIOUS REPAIR DOUBLER THAT IS DISBONDED. REPAIRED NR 3 SLAT UPPER SKIN T/E WEDGE IAW SRM 51 70 10, REP 4.

Part: BUTTSTRAP — DAMAGED (BS 908) · airframe 62,504 hrs · 40,216 cycles

SCRIBE LINE AT BS 908 BUTT STRAP FROM STR 7L TO STR 8L. REMOVED, FABRICATED AND INSTALLED NEW BUTT JOINT STRAP IAW SRM 51 40 05 AND 51 40 02.

Part: FRAME — CORRODED (BS 867) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

UPON REMOVAL OF AFT PIT FLOOR PANEL FOR CARGO TRACK REPAIR FOUND FRAME SHEAR TIE AT STA 867 BETWEEN STR 27L AND 27R CORRODED. REMOVED CORROSION BY BLENDING, FOUND TO BE OUT OF LIMITS REPAIRED AREA IAW SRM 53-00-07, FIG 101 AND 53-60-07, FIG 201.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 62,504 hrs · 40,216 cycles

NR 3 SLAT LOWER INBD CORNER IS CHAFED ON SKIN FILLER. REPAIRED NR 3 SLAT LOWER INBD CORNER IAW SRM 51-70-10, REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 520) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

RT LATERAL SEAT TRACK AT BS 520, CORRODED. ACFT GROUNDED. R & R SEAT TRACK IAW SRM 51-40-02.

Part: SKIN — CHAFED (BS 1138-1156) · airframe 62,504 hrs · 40,216 cycles

SKIN PANEL BELOW LT HORIZONTAL STAB AFT ATTACH FITTING IS CHAFED. R & R SKIN PANEL IAW SRM 51 40 02.

Part: SEAT TRACK — CORRODED (BS 500G) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

RT LATERAL SEAT TRACK AT BS 500G IS CORRODED. R & R SEAT TRACK IAW SRM-51-40-02.

Part: STRAP — CORRODED (BS 727D FLOOR) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

AFT CARGO FLOOR PANEL SPLICE STRAP AT BS 727D+5.6 IS CORRODED. FABRICATED NEW SPLICE STRAP IAW 51-40-05 SRM.

Part: SEAT TRACK — CORRODED (BS 520) · corrosion level 2 · airframe 62,504 hrs · 40,213 cycles

LEFT LATERAL SEAT TRACK, BS 520 CORRODED. R & R SEAT TRACK IAW SRM 51-40-02.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 62,504 hrs · 40,216 cycles

AFT CARGO BAY FORWARD FLOOR PANEL HAS SMALL CRACK REMOVED, FABRICATED AND INSTALLED NEW FLOOR PANEL IAW AMM 25-52-51-004-001, SRM 51-40-05, AND MM 25-52-51-404-011.

Part: TAB — GOUGED (ELEVATOR) · airframe 62,504 hrs · 40,216 cycles

RIGHT ELEVATOR TAB INBD HINGE CUTOUT HAS DAMAGE ON INBD EDGE. REPAIRED RT ELEVATOR TAB INBD HINGE CUTOUT ON INBD EDGE IAW SRM 51 70 04, REPAIR 10.

Part: SKIN — DENTED (BS 1016-1040) · airframe 62,504 hrs · 40,216 cycles

FOUND A DENT OUT OF LIMITS AT BS 1022, BL 0. REPAIRED DAMAGED AREA IAW EA 400-53EA-09950.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

RIGHT WING OTBD FOREFLAP INBD L/E SKIN IS CHAFED. REPAIRED IAW SRM 57-53-01, FIG 201.

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 62,504 hrs · 40,216 cycles

AFT CARGO DOOR INNER SKIN HAS TOOLING DAMAGE LOWER CENTER RIVET LINE REPAIRED INNER SKIN IAW SRM 51-70-13.

Part: FLOOR PANEL — PUNCTURED (BS 578) · airframe 62,504 hrs · 40,216 cycles

FLOOR PANEL JUST LEFT OF BL 0 IS PUNCTURED AT BS 578 REPAIRED FLOOR PANEL USING FIBERGLASS CLOTH AND RESIN.

Part: SKIN — CHAFED (NR 7 FLAP) · airframe 62,504 hrs · 40,216 cycles

RIGHT WING OTBD FLAP LOWER SURFACE INBD OF NR 7 FLAP TRACK IS CHAFED. REPAIRED RT WING OTBD FLAP LOWER SURFACE IAW SRM 51-70-10, REPAIR 4.

Part: CAP — CORRODED (THRESHOLD) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

FWD CARGO FWD THRESHOLD CAP CORRODED, CORRODED THROUGH HOLES, 100 MATL LOSS OUT OF LIMITS IAW SRM 53 30 53, FIG 101. FABRICATED NEW THRESHOLD CAP IAW SRM 51- 40-05.

Part: THRESHOLD — CORRODED (BS 476-480) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

FWD CARGO AFT THRESHOLD CAP CORRODED. ON FURTHER INVESTIGATION CAP FOUND TO BE BROKEN AND OUT OF LIMITS IAW SRM 53-30-53, FIG 101. FABRICATED NEW THRESHOLD CAP IAW SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (BS 727D-727F) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

AFT PIT NR 2 FLOOR PANEL IS CORRODED. REMOVED CORRODED MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53. FABRICATED FLOOR PANEL IAW SRM 51-40-05, TREATED NEW FLOOR PANEL IAW AMM 51-21-41-377-032, STEP D 1-6 AND PRIMED NEW FLOOR PANEL IAW SOPM 20 44 01, STEP D 1.C W 1.0 O .071 R 0 L 36 D .071.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

RIGHT WING OTBD FLAP LOWER SURFACE OTBD OF NR 7 FLAP TRACK IS CHAFED ON EXISTING REPAIR. REPAIRED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (BS 233) · airframe 62,504 hrs · 40,216 cycles

RT FUSELAGE SKIN BS 233 AND S22R IS DENTED. DENT WITHIN 3" OF LAP SEAM. REPAIRED SKIN, REPAIR IS A CATEGORY B REPAIR.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 65,204 hrs · 40,216 cycles

RIGHT WING OTBD FLAP LOWER SURFACE OTBD OF FLAP JACKSCREW SKIN DAMAGED. REPAIRED IAW SRM 51 70 10, REPAIR 4.

Part: CARGO TRACK — CORRODED (BS 945) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

AFT CARGO TRACK BS 945 LBL 17.2 IS CORRODED. REMOVED CORRODED ON CARGO TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53 60 53, FIG 101. SPLICED IN NEW SECTION IAW SRM 53 00 53, FIG 201.

Part: ATTACH ANGLE — CRACKED (DOOR FRAME) · airframe 62,504 hrs · 40,216 cycles

FWD CARGO DOORWAY FWD FRAME ATTACHMENT TO STR 22R CRACKED ON INNER RADIUS. R & R FRAME ATTACH ANGLE IAW SRM 51 40 02.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 65,204 hrs · 40,216 cycles

LEFT WING OTBD MIDFLAP LOWER SKIN IS CHAFED. REPAIRED IAW SRM 51 70 10, REPAIR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 65,204 hrs · 40,216 cycles

LEFT WING OTBD MIDFLAP LOWER SURFACE SKIN IS CHAFED ON A PREVIOUS REPAIR INBD OF THE NR 2 FLAP TRACK FAIRING. REPAIRED LT WING OTBD MIDFLAP LOWER SURFACE SKIN IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 65,204 hrs · 40,216 cycles

LEFT WING NR 3 SLAT T/E WEDGE IS CHAFED ON THE LOWER SURFACE BEHIND ACTUATOR. REPAIRED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

LT WING OTBD FOREFLAP INBD L/E IS CHAFED REPAIRED L/E SKIN IAW SRM 57 53 01, FIG 201, REPAIR 1.

Part: SKIN — CHAFED (LT WING) · airframe 62,504 hrs · 40,216 cycles

LEFT WING INBD EXHAUST GATE IS CHAFED ON UPPER OTBD SURFACE. REPAIRED LT WING INBD EXHAUST GATE IAW SRM 57-53-01, REPAIR 10.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

LEFT WING INBD MIDFLAP UPPER SURFACE IS CHAFED ON INBD END. REPAIRED MIDFLAP UPPER SURFACE IAW SRM 57-53-01, FIG 201, REPAIR 3.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

LEFT WING OTBD AFT FLAP LOWER SURFACE IS DENTED. LT WING OTBD AFT FLAP LOWER SURFACE REPAIRED IAW SRM 51-70-10, REP 4.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 62,504 hrs · 40,216 cycles

LT WING INBD FOREFLAP IS GOUGED. REPAIRED IAW SRM 51-70-10, REPAIR 4.

Part: BULKHEAD — DENTED (BS 616) · airframe 62,504 hrs · 40,216 cycles

MAIN CARGO DECK AFT BULKHEAD DOOR HAS SEVERAL DENTS (PARTITION) ON FWD FACE. REPAIRED MAIN CARGO AREA AFT PARTITION DOOR DENTS ON FWD SURFACE IAW EA 15023 AND ASA EA NR 400 53EA 09926, REV IR.

Part: BULKHEAD — DENTED (BS 616) · airframe 62,504 hrs · 40,216 cycles

MAIN CARGO AREA AFT PARTITION DOOR IS GOUGED ON FWD SIDE REPAIRED MAIN CARGO AREA AFT PARTITION DOOR FWD SIDE GOUGE IAW EA 15023 AND EA 400-53EA-09926, REV IR.

Part: BULKHEAD — DENTED (BS 616) · airframe 62,504 hrs · 40,216 cycles

MAIN CARGO AREA AFT PARTITION IS DENTED ON DOOR BELOW LATCH MAIN CARGO AREA AFT PARTITION DENT ON EDGE OF DOOR BELOW LATCH IS ACCEPTABLE TO LEAVE AS IS NO FURTHER ACTION REQUIRED IAW EA 15023, AND ASA EA 400 53EA 09926, REV IR.

Part: BULKHEAD — GOUGED (BS 616) · airframe 62,504 hrs · 40,216 cycles

MAIN CARGO AREA AFT PARTITION DOOR IS GOUGED ON FWD SIDE REPAIRED MAIN CARGO AREA AFT PARTITION DOOR FWD SIDE GOUGE IAW EA 15023 AND EA 400-53EA-09926, REV IR

Part: BULKHEAD — DENTED (BS 616) · airframe 62,504 hrs · 40,216 cycles

MAIN CARGO AREA AFT PARTITION RT BULKHEAD HAS SEVERAL DENTS ON SURFACE. REPAIRED MAIN CARGO AREA AFT PARTITION RT BULKHEAD DENTS ON FWD SURFACE IAW EA 15023 AND ASA EA 400-53EA-09926, REV IR.

Part: THRESHOLD — CORRODED (BS 398-403) · corrosion level 2 · airframe 62,504 hrs · 40,216 cycles

FWD CARGO FWD THRESHOLD CAP CORRODED. CORRODED THROUGH HOLES, 100 PERCENT MATERIAL LOSS. OUT OF LIMITS IAW SRM 53 30 53, FIG 101. FABRICATED NEW THRESHOLD CAP IAW SRM 51-40-05.

Part: BEARING — INOPERATIVE (L2 DOOR) · airframe 62,401 hrs · 40,125 cycles

F/A REPORTS AFT LT DOOR IS DIFFICULT TO OPEN. ACFT GROUNDED. REMOVED DOOR, REPLACED UPPER FORWARD HINGE BEARING REINSTALLED DOOR ASSY, REF MM 52-13 42 AND REPLACED WORN DOOR SNUBBER REF MM 52-13-71. OPS CHECK GOOD.

Part: STRAP — CORRODED (BS 492) · airframe 61,276 hrs · 39,134 cycles

CORROSION FOUND IN FWD CARGO BAY ON STRAP COMMON TO FRAME AT FS 492 AFT SIDE OF DOOR OPENING. ACFT GROUNDED. CORROSION BLENDED OUT AND REMOVED REF SRM 53-30-15, AD-1, PG 105. DEPTH OF DAMAGE WAS .037 OUT OF LIMITS IAW SAID REF REMOVED STRAP. SEVERAL HOLES FOUND TO BE ELONGATED IN TURTLE STRAP. REMOVED TURTLE STRAP. STARTING FABRICATION IAW DWG 65-59659. INSPECTION VERIFIED MATERIAL ID 7075-T6, .080 THICK. REMOVED WEB FOR S/M ACCESS. ACCOMPLISHED HFEC TO FASTENER HOLES REF. BNDT 51-00-00 PART 6, FIG 16, NO CRACKS NOTED. REMOVED RT SIDEWALL LINER AFT OF CARGO DOOR FOR ACCESS WITH REF TO AMM 25-52-73-004-018. CUT FILLER STRAP UNDER FRAME AND REMOVED IAW ENGINEERING REQUEST. REAMED ELONGATED HOLES IN FRAME IAW ENG REQUEST. INSTALLED OF REPAIR COMPLETED, REF EA 400-53EA-08690. ACCOMP PERM REPAIR AT NEXT HMV ON DEFERRAL.

Part: DOOR FRAME — CORRODED (500) · corrosion level 2 · airframe 61,276 hrs · 39,134 cycles

FRAME CORRODED. INSTALLED FORWARD CARGO DOOR AFT CORRODED REINFORCEMENT STRAP. ACFT GROUNDED. R & R REINFORCEMENT STRAP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,225 hrs · 37,303 cycles

FRAME 500B RIGHT SIDE CRACKED AT WIRE PENETRATION HOLE. C/W ASA EA 400 53EA 06699 REV NEW ISSUED 03 NOV 2011.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,225 hrs · 37,303 cycles

FRAME 520 RIGHT SIDE CRACKED AT WIRE PENETRATION HOLE. REPAIRED STA 520 RT FRAME IAW B737 400 SRM 53 00 07 REPAIR 13.

Part: GUIDE ARM — WORN (L2 DOOR) · airframe 57,979 hrs · 36,196 cycles

L2 DOOR DOES NOT CLOSE PROPERLY. REMOVED AND REPLACED L2 DOOR SNUBBER PER AMM 52 13 17. DOOR STILL CHECKS BAD. L2 DOOR UPPER GUIDE ARM WORN REPLACED GUIDE ARM REF AMM 52 13 13.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

DEEP BLEND MARK AT BS 455 STR 21L. CUT OUT DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW PEMCO 737 400 SRM SUPPLEMENT 53 30 81 FIG 204.

Part: FLAP — DAMAGED (RT WING) · airframe 57,665 hrs · 35,926 cycles

RIGHT INBOARD AFT FLAP DAMAGED. TRAILING EDGE REMOVED DAMAGED FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 57,665 hrs · 35,926 cycles

VERTICAL STABILIZER TRAILING EDGE BEAM CRACKED LEFT SIDE. REMOVED AND REPLACED BEAM IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

BS 908 BUTT SPLICE FROM 4R TO 10R STRINGER SPLICE HAS TOOLING MARKS ON INSIDE AND IN RADIUS. REMOVED AND REPLACED STRINGER SPLICE IAW B737 400 SRM 51 40 02.

Part: SKIN — PUNCTURED (RUDDER) · airframe 57,665 hrs · 35,926 cycles

LEFT RUDDER SKIN PUNCTURED BONDED DAMAGED AREA IAW B737 400 SRM 51 70 17 REPAIR 1.

Part: FLAP — DAMAGED (LT WING) · airframe 57,665 hrs · 35,926 cycles

LT OUTBOARD FLAP OUTBOARD END DAMAGED. REPAIRED IAW B737 400 SRM 51 70 10.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

SCRIBE AT BS 727G BUTT JOINT. REMOVED AND REPLACED BUTT SPLICE IAW B737 400 SRM 51 40 02.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

SCRIBE AT BS 908 BUTT JOINT. REMOVED AND REPLACED BUTT SPLICE IAW B737 400 SRM 51 40 02.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

SCRIBE AT BS 727G SCRIBE LENGTH 1.25 INCH UPPER STR X 11L DISTANCE FROM SCRIBE UPPER END TO STR X 10 INCH LOWER STR Y 13L DISTANCE FROM SCRIBE END TO STR Y 6 INCH DEPTH .002. REMOVED AND REPLACED BUTT SPLICE STRAP IAW B737 400 SRM 51 40 02.

Part: SPLICE — SCRATCHED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

SCRIBE AT BS 908 SCRIBE LENGTH 3.5 INCH UPPER STR X 3R DISTANCE FROM SCRIBE UPPER END TO STR X 5.5 IN. LOWER STR Y 4R DISTANCE FROM SCRIBE END TO STR Y 2.250 IN. SCRIBE DEPTH 0.002 IN REMOVED AND REPLACED BUTT SPLICE AT BS 908 STR 4L TO STR 4R IAW B737 400 SRM 51 40 02.

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 57,665 hrs · 35,926 cycles

SCRIBE AT BS 727G SCRIBE LENGTH 20 INCHES UPPER STR X1 DISTANCE FROM SCRIBE UPPER END TO STR X 6.250 IN. LOWER STR Y 4L DISTANCE FROM SCRIBE END TO STR Y 3.750 IN. DEPTH .003. REMOVED AND REPLACED BUTT SPLICE PLATE IAW B737 400 SRM 51 40 02.

Part: SNUBBER — BINDING (ENTRY DOOR) · airframe 57,628 hrs · 35,892 cycles

L2 (AFT ENTRY) DOOR HARD TO CLOSE (BINDS ABOUT 3/4 CLOSED). REMOVED AND REPLACED AFT ENTRY DOOR SNUBBER PER B737 400 AMM 52 13 71.

Part: SNUBBER — DEFECTIVE (ENTRY DOOR) · airframe 57,453 hrs · 35,742 cycles

L2 DOOR (AFT ENTRY) DIFFICULT TO LOCK. REPLACED DOOR SNUBBER IAW B737 400 MM 52 13 71.

Part: SKIN — DENTED (HORIZ STAB) · airframe 57,359 hrs · 35,669 cycles

DENT ON LOWER STABILIZER SKIN APPROX L/E STA 155 18 INCHES AFT OF LEADING EDGE STAB 147.9. CONDITIONAL INSPECTION ACCOMPLISHED IAW AMM 05 51 59, NO ADDITIONAL DAMAGE NOTED. DENT LOCATION IS STA 150.25 1.5L X 1.25W X .142D INCHES OUT OF SRM LIMITS. COMPLETED REPAIR PER EA 400 55EA 04561.

Part: SKIN — DENTED (HORIZ STAB) · airframe 57,359 hrs · 35,669 cycles

GOLF BALL SIZE DENT LOCATED ON LEADING EDGE OF LEFT HORIZONTAL STABILIZER. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER USING .063" 2024 T3 MATERIAL LAYED OUT & DRILLED FASTENER HOLES & COUNTERSUNK DOUBLER ALODINED & PRIMED INNER SURFACE OF DOUBLER REF SRM 55 10 01 REPAIR 3. INSTALLED DOUBLER SRM 55 10 01 REPAIR 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,910 hrs · 35,284 cycles

FUSELAGE SKIN CRACKED AND STRINGER 22L HAS BAD FASTENER HOLES. REMOVED DAMAGED AREA INSTALLED DOUBLER AND TRIPLER AND SPLICED IN NEW SECTION OF STRINGER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,444 hrs · 34,877 cycles

CRACK IN AFT UPPER END OF STRINGER 24R AT BS 1013. INSTALLED NEW STRINGER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,444 hrs · 34,877 cycles

CRACK IN AFT UPPER END OF STRINGER 23R AT BS 1013. INSTALLED NEW STRINGER.

Part: SKIN — CHAFED (TE FLAP) · airframe 56,444 hrs · 34,877 cycles

RT WING O/B MID FLAP HAS A CHAFE JUST O/B OF THE NR 7 FLAP TRACK FAIRING. REMOVED DAMAGED AREA AND BONDED REPAIR.

Part: SKIN — DAMAGED (MIDFLAP) · airframe 56,444 hrs · 34,877 cycles

LEFT O/B MID FLAP LOWER SURFACE SKIN PANEL INTERNAL DAMAGE TO INNER SKIN. REPAIRED LEFT O/B MID FLAP LOWER SURFACE SKIN PANEL.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 56,444 hrs · 34,877 cycles

RT WING I/B FOREFLAP UPPER SURFACE REPAIR DELAMINATED. REPAIRED THE DAMAGED AREA OF THE I/B FORE FLAP.

Part: SKIN — DENTED (SPOILER) · airframe 56,444 hrs · 34,877 cycles

RIGHT WING NR 7 SPOILER DENT AT SLOPE 4 INCHES FROM O/B EDGE. REPAIRED NR 7 SPOILER.

Part: SKIN — DENTED (TE FLAP) · airframe 56,444 hrs · 34,877 cycles

LEFT WING O/B AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED DAMAGED AREAS.

Part: SKIN — DENTED (SPOILER) · airframe 56,444 hrs · 34,877 cycles

RT WING NR 8 SPOILER DENT 5 INCHES PAST INBOARD HINGE POINT. REPAIRED NR 8 SPOILER.

Part: SKIN — DENTED (SPOILER) · airframe 56,444 hrs · 34,877 cycles

NR 1 SPOILER HAS MULTIPLE DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA AND BONDED REPAIR.

Part: DOUBLER — DAMAGED (LE SLAT) · airframe 56,444 hrs · 34,877 cycles

NR 2 LEADING EDGE SLAT OUTBOARD UPPER SURFACE HAS PREVIOUS REPAIR DENTED AND IS SEPARATING AT O/B END. REMOVED AND REPLACED EXTERNAL DOUBLER.

Part: SKIN — DENTED (FOREFLAP) · airframe 56,444 hrs · 34,877 cycles

LT WING O/B FOREFLAP DENTED ABOVE NR 1 FLAP TRANSMISSION. REPAIRED O/B FOREFLAP.

Part: SKIN — DENTED (TE FLAP) · airframe 56,444 hrs · 34,877 cycles

LT WING I/B FOREFLAP HAS TWO DENTS ON LOWER SURFACE. REPAIRED LT WING INBOARD FORE FLAP.

Part: SKIN — DENTED (ELEVATOR) · airframe 56,444 hrs · 34,877 cycles

LEFT ELEVATOR LOWER SURFACE HAS DENT WITH DELAMINATION. REPAIRED DENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,444 hrs · 34,877 cycles

EXTERNAL FUSELAGE SKIN IS DENTED AND GOUGED AT STA 1013 STR 13L. REMOVED DAMAGE AND INSTALLED NEW SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,444 hrs · 34,877 cycles

STA 500C + 15 ABOVE STR 26L FASTENER ROW DENTED. REPAIRED DENTED AREA.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,444 hrs · 34,877 cycles

EXTERNAL FUSELAGE SKIN IS DENTED AND GOUGED AT STA 1013 STR 13L. REMOVED SKIN AND REPLACED WITH NEW SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,444 hrs · 34,877 cycles

DENT AT STA 1020 FOUND WITHIN 3 INCHES OF SKIN SPLICE FASTENER ROW. REPAIRED DENT.

Part: GUIDE ARM — LACK OF LUBE (L2 DOOR) · airframe 55,649 hrs · 34,188 cycles

L2 DOOR DIFFICULT TO OPEN/CLOSE CATCHES. LUBRICATED GUIDE ARM ATTACH POINTS AND OPERATED DOOR. OBSERVED NORMAL OP'S DOOR FIT AND LIGHTS AGREED WITH HANDLE POSITION. OK FOR SERVICE. REF M/M 52 13 00 705 003.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME STA 907 STR 8L HAS PREVIOUS REPAIR WITH DEVIATIONS. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: WEB — DAMAGED (CARGO BAY) · airframe 53,358 hrs · 29,064 cycles

AFT CARGO DOOR CUTOUT LOWER CLOSEOUT WEB SCRATCHED HAS ELONGATED HOLES. REMOVED AND REPLACED WEB.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME AT STA 867 STR 8R HAS PREVIOUS REPAIR WITH DEVIATIONS. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

ACB FWD BULKHEAD WL 179 BS 727+3 LBL 46 54 CHANNEL ASSY IS BROKEN. REMOVED AND REPLACED CHANNEL.

Part: STRINGER CLIP — DAMAGED (BS 440 S4R) · airframe 53,358 hrs · 32,175 cycles

ELONGATED HOLE IN STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP.

Part: INTERCOSTAL — CORRODED (BS 747-767) · airframe 53,358 hrs · 32,175 cycles

FOUND INTERCOSTAL STA 747-767 RBL 22, WL 154 CORRODED AT UPPER AND LOWER FLANGES. REMOVED AND INSTALLED NEW INTERCOSTAL.

Part: WEB — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

VERTICAL WEB HAS OVERSIZE FASTENER HOLE AFT CARGO BAY. REMOVED AND INSTALLED NEW VERTICAL WEB.

Part: FRAME — DENTED (BS 500E) · airframe 53,358 hrs · 32,175 cycles

FRAME DENTED ON INBD CROWN FLANGE. REMOVED DENT FROM FRAME FABRICATED REPAIR PARTS AND INSTALLED.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 53,358 hrs · 32,175 cycles

RT WING NR 2 PYLON SUPPORT ANGLE IS CRACKED AT UPPER INBD SIDE OF AFT FRAME. REMOVED AND REPLACED.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

ELONGATED HOLE IN STR CLIP STA 400 STR 8R. REMOVED AND REPLACED STR CLIP WITH NEW.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO DOOR CUTOUT FLOOR TO SIDEWALL SUPPORT PLATE IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE.

Part: SUPPORT ANGLE — CRACKED (NACELLE) · airframe 53,358 hrs · 32,175 cycles

NR 2 SUPPORT ANGLE CRACKED REMOVED AND REPLACED NR 2 SUPPORT ANGLE.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

PUNCTURE IN WEB AT BS 1025 LBL 1 WL 208. REMOVED AND REPLACED PUNCTURED WEB PER SRM.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

INTERCOSTAL BS 927 947 BL 0 IS DAMAGED. REMOVED AND REPLACED INTERCOSTAL WITH FABRICATED PART.

Part: WEB — CORRODED (BS 1006-1036) · corrosion level 2 · airframe 53,358 hrs · 29,064 cycles

RT SHEAR WEB CORRODED. REPLACED ON MIG 5.

Part: BRACKET — GOUGED · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY GOUGES AT SCREW HOLE BRACKET. REMOVED AND REPLACED.

Part: SKIN — DENTED (CARGO DOOR) · airframe 53,358 hrs · 32,175 cycles

MAIN CARGO DOOR SKIN LOWER LIP DAMAGED DENTED. REPAIRED MAIN CARGO DOOR.

Part: FRAME — GOUGED (NR 2 PYLON) · airframe 53,358 hrs · 32,175 cycles

NR 2 PYLON TE FAIRING UPPER FWD ACCESS PANEL AFT ATTACHMENT AFT APERTURE FRAME GOUGED REMOVED AND REPLACED NR 2 PYLON AFT APERTURE FRAME.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FORK LIFT LOADER CONTACTED LOWER MAIN CARGO OPENING DENTED. REPAIRED LOWER MAIN CARGO DOOR OPENING.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY DRILL MARKS AT SCREW HOLES. REMOVED AND REPLACED.

Part: BRACKET — DAMAGED (BS 500F) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY DRILL MARKS AT SCREW HOLES BRACKET. REMOVED AND REPLACED.

Part: BRACKET — SCRATCHED (BS 398) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY OXYGEN BOTTLE SUPPORT BRACKET SCRATCHED. REMOVED FABRICATED NEW AND REPLACED.

Part: SHROUD — CRACKED (APU) · airframe 53,358 hrs · 32,175 cycles

APU SHROUD UPPER LT EDGE HAS AREAS BENT AND CRACKED. REPAIRED APU LOWER SHROUD UPPER LT EDGE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME AT 727D STR 8R CRACKED AT FASTENER HOLE. REPAIRED FRAME.

Part: DOUBLER — CHAFED (LE SLAT) · airframe 53,358 hrs · 32,175 cycles

LT WING NR 3 SLAT T/E LWR SURFACE PREVIOUS DOUBLER HAS CHAFING DAMAGE AT IB END. REPAIRED CHAFING DAMAGE AT IB END ON 33 SLAT T/E LWR SURFACE IAW SRM 51 10 02.

Part: SKIN — CHAFED (LE SLAT) · airframe 53,358 hrs · 32,175 cycles

LT WING NR 3 SLAT T/E LWR SURFACE HAS CHAFING DAMAGE AT OB END. REPAIRED CHAFING DAMAGE ON NR 3 SLAT T/E AT OB END IAW SRM 51 10 02.

Part: SKIN — CHAFED (LE SLAT) · airframe 53,358 hrs · 32,175 cycles

LT WING NR 3 SLAT T/E LOWER SURFACE PREVIOUS REPAIR HAS CHAFING DAMAGE 56 INCHES FROM IB END. REPAIRED CHAFING DAMAGE 56 INCHES FROM IB END ON NR 3 SLAT LWR SURFACE T/E IAW SRM 57 43 02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

SKIN DIMPLED BS 500 BETWEEN STR 24-27L. REPAIRED PER EA 400-53EA-01485.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME BS 727F STR 8R PREVIOUS REPAIR HAS DEVIATION. REMOVED PREVIOUS REPAIR PARTS AND INSTALLED.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME AT 727D STR 8L HAS PREVIOUS REPAIR WITH DEVIATIONS. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 29,064 cycles

FOUND SUB THRESHOLD WEB IB VERTICAL SUPPORT WEB ASSY CORRODED AT FWD END STA 795 RBL 20 WL 158. REMOVED AND REPLACED THRESHOLD WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME CRACKED AT INBD FASTENER HOLE STA 400 BETWEEN STR 8R AND 9R. REPAIRED PER SRM.

Part: HOUSING — CORRODED (GALLEY DOOR) · corrosion level 2 · airframe 53,358 hrs · 29,064 cycles

FWD GALLEY DOOR HANDLE MECHANISM HOUSING CORRODED. REMOVED AND REPLACED HOUSING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

SUPPORT ANGLE CRACKED BS 520 WL 200 LBL 25 REMOVED AND REPLACED SUPPORT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME STA 747, STR 8L CRACK NOTED AT IB FASTENER HOLE REQUIRES REPAIR IAW EA NR 400-53EA-01028. REPAIRED.

Part: SILL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

CORROSION ON L2 DOOR CUTOUT MOPSILL. REMOVED AND REPLACED MOPSILL.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

PREVIOUS REPAIR ON FRAME WITH DEVIATIONS IAW EA 5310-02439. REMOVED PREVIOUS REPAIR, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME CRACKED AT IB FASTENER HOLE FOR AIR CONDITIONING BRACKET. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FOUND STA 500 FRAME CRACKED AT NUTPLATE HOLES WL 156 RBL 24.5. REMOVED DAMAGE FROME FRAME FABRICATED REPAIR PARTS AND INSTALLED.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 53,358 hrs · 29,064 cycles

LT TAB HAS CRACK AT NR 1 HINGE CUTOUT ON LOWER SURFACE AT FWD EDGE. REPAIRED LT TAB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME CRACKED AT AIR CONDITIONING BRACKET. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED.

Part: SKIN PANEL — CHAFED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

PANEL 9504R HAS INNER SURFACE CHAFING DAMAGE. REPAIRED PANEL 9504R INNER SURFACE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME AT BS 827, STR 8R CRACKED. REPAIRED FRAME AT BS 827 STR 8R.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

OPEN HOLE IN VERTICAL WEB OF LONGITUDINAL BEAM. REMOVED OPEN HOLE BY EXTENDING SLOT IN WEB HFEC INSPECTED TREATED AND PRIMED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FRAME AT STR 8L BS 727F CRACKED AT FASTENER HOLE. REPAIRED.

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT SPLICE PLATE HAS DRILL STARTS. REMOVED SUPPORT SPLICE FABRICATED NEW SPLICE AND INSTALLED.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FWD ENTRY DOOR UPPER FUSELAGE HINGE FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE FITTING ON FWD ENTRY DOOR.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON AFT PRESSURE BULKHEAD CHANNEL STIFFENER RT SIDE. REPAIRED AFT PRESSURE BULKHEAD CHANNEL STIFFENER PER EA.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION AFT PRESSURE CHANNEL STIFFENER LT SIDE. REPAIRED AFT PRESSURE BULKHEAD CHANNEL STIFFENER LT SIDE PER EA400 53EA 01476.

Part: SUPPORT BRACKET — DENTED (ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

SUPPORT BRACKET DENTED FWD SIDE OF RT ELEV STA 123. REPLACED SUPPORT BRACKET DENTED FWD SIDE OF RT ELEV STA 123.

Part: SUPPORT BRACKET — DENTED (ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

SUPPORT BRACKET DENTED FWD SIDE OF RT ELEV STA 119. REPLACED SUPPORT BRACKET AT STA 119.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FRAME AT 907 STR 8R HAS PREVIOUS REPAIR ACCOMPLISHED WITH DEVIATION. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: SUPPORT BRACKET — DENTED (ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

SUPPORT BRACKET DENTED FWD SIDE OF RT ELEV STA 123. REPLACED SUPPORT BRACKET ON FWD SIDE OF RT SIDE ELEV STA 123.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FRAME AT 747 CRACKED AT FASTENER HOLE STR 8R. REPAIRED.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FRAME 787 S8R HAS PREVIOUS REPAIR WITH DEVIATIONS. REMOVED PREVIOUS, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: SUPPORT BRACKET — DENTED (ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

SUPPORT BRACKET DENTED FWD SIDE OF RT ELEV STA 174. REPLACED SUPPORT BRACKET ON FWD SIDE OF RT SIDE ELEV STA 174.

Part: SUPPORT BRACKET — DENTED (ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

SUPPORT BRACKET DENTED FWD SIDE ELEV STA 41. REPLACED SUPPORT BRACKET ON FWD SIDE OF RT SIDE ELEV STA 41.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

BS 540 LBL 25 LBL 45 WL 208 SUPPORT CHANNEL UPPER COVER IS BENT AND PUNCTURED. REMOVED AND REPLACED SUPPORT CHANNEL IAW SRM 51 40 02 AND SRM 51 40 05.

Part: SUPPORT CHANNEL — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

BS 540 BL 0 RBL 25 WL 208 SUPPORT CHANNEL UPPER COVER IS TORN AND BENT. REMOVED AND REPLACED SUPPORT CHANNEL IAW SRM 51 40 02 AND SRM 51 40 05.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

PRESSURE BULKHEAD IS CORRODED. REPAIRED PRESSURE BULKHEAD PER EA 400-53EA-01476.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

BS 540 BL 0 LBL 25 WL 208 SUPPORT CHANNEL UPPER COVER IS BENT AND PUNCTURED. REMOVED AND REPLACED SUPPORT CHANNEL IAW SRM 51 40 02 AND SRM 51 40 05.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

APU RT UPPER TORQUE BOX LOWER STRINGER CORRODED. REMOVED AND REPLACED LOWER STRINGER ON APU RT TORQUE BOX.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON 32 FLAP TRACK. REPAIRED TRACK PER OHM.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

APU RT UPPER STRINGER CORRODED AT AIR INLET DUCT OPENING. REMOVED AND REPLACED STRINGER AT APU AIR INLET DUCT OPENING IAW SRM 51 40 02.

Part: FRAME — MISREPAIRED (BS 847) · airframe 53,358 hrs · 32,175 cycles

EXISTING REPAIRS ON 847 FRAME NOT PER DWG A 5330018185 FIG 5. REMOVED AND REPLACED FRAME.

Part: SUPPORT BRACKET — CRACKED (RT ELEVATOR) · airframe 53,358 hrs · 32,175 cycles

SUPPORT BRACKET CRACKED ON FWD SIDE OF RT ELEV STA 123. REPLACED SUPPORT BRACKET ON FWD SIDE OF RT ELEVATOR STA 123.

Part: FRAME — CRACKED (BS 767) · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED AT FASTENER HOLE FOR OVERHEAD CENTER LINE DUCT SUPPORT STA 767 2 INCHES LT SIDE OF STR 1. TRIMMED OUT DAMAGE AND REPAIRED PER SRM.

Part: BRACKET — CRACKED (PAX DOOR PAN) · airframe 53,358 hrs · 32,175 cycles

AFT ENTRY DOOR LOWER PAN BRACKETS ARE CRACKED. REPLACED PAN BRACKETS.

Part: FRAME — CRACKED (BS 767) · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED AT FASTENER HOLE FOR OVERHEAD CENTER LINE DUCT SUPPORT STA 767 2IN LT SIDE OF STR 1. REPAIRED IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD ENTRY DOOR LOWER LINER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR AFT LINER SUPPORT ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD ENTRY DOOR FWD LINER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR FWD LINER SUPPORT

Part: INTERCOSTAL — CORRODED (BS 853) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON INTERCOSTAL IN AFT CARGO BAY. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED.

Part: FRAME — CRACKED (BS 480) · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED STA 480 BETWEEN STR 8R AND 9R OUT OF LIMITS SRM 53-00-07. REPAIRED FRAME IAW SRM 53-00-07.

Part: STRAP — CRACKED (FLOORBEAM) · airframe 53,358 hrs · 32,175 cycles

FLOORBEAM STABILIZATION STRAP CRACKED STA 328 RBL 0 WL 200. REPAIRED STABILIZATION STRAP STA 328 RBL 0 WL 200.

Part: CREASE BEAM — CORRODED (BS 500D-520) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CREASE BEAM HAS AREAS OF CORROSION REMOVED AND REPLACED CORRODED SECTION OF CREASE BEAM WITH NEW FABRICATED SECTION.

Part: WEB — DAMAGED (BS 437) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY DOOR CUTOUT FWD FRAME CLOSE OUT WEB DAMAGED HOLES. REPLACED WITH NEW CLOSE OUT WEB PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED STA 440 BETWEEN STR 8R AND 9R OUT OF LIMITS SRM 53-00-07. REPAIRED PER SRM.

Part: FRAME — DAMAGED (FAIRING) · airframe 53,358 hrs · 32,175 cycles

RT FAIRING FORMER HAS ELONGATED HOLES FAIRING FORMER REPLACED.

Part: STRAP — CRACKED (FLOORBEAM) · airframe 53,358 hrs · 32,175 cycles

FLOORBEAM STABILIZATION STRAP CRACKED STA 328 RBL 46 WL 200. REPAIRED STABILIZATION STRAP STA 328 RBL 46 WL 200.

Part: FRAME — CRACKED (BS 867) · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED AT FASTENER HOLE FOR OVERHEAD CENTERLINE NUT. REMOVED AND REPLACED CRACKED SECTION OF FRAME PER REPAIR.

Part: FRAME — CRACKED (BS 867 L1R) · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED AT FASTENER HOLE FOR OVERHEAD CENTERLINE NUT. TRIMMED CRACKED SECTION AND REPAIRED PER SRM.

Part: ATTACH BRACKET — CRACKED (BS 500-500A) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL WEB ATTACH BRACKET CRACKED. REMOVED AND REPLACED ATTACH BRACKET.

Part: ATTACH BRACKET — CRACKED (BS 500F) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL ATTACH BRACKET CRACKED. FABRICATED REPLACEMENT BRACKET AND INSTALLED.

Part: BRACKET — CRACKED (BS 1110) · airframe 53,358 hrs · 32,175 cycles

LT HORIZONTAL STAB NR 5 GAP PANEL BRACKET ASSY CRACKED AT LOWER INBD SPT. REMOVED AND REPLACED.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 53,358 hrs · 32,175 cycles

RT OTBD FORE FLAP LE CHAFED 6 INCH FROM INBD END. REPAIRED PER SRM. BLIND REPAIR FASTENERS INSPECTION REQUIRED AT EVERY C-CHECK.

Part: SUPPORT — GOUGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO DOOR CUTOUT CARGO TIE DOWN SUPPORT PLATE. FABRICATED NEW SUPPORT PLATE PER SRM/DRAWING.

Part: INTERCOSTAL — DAMAGED (BS 463) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY INTERCOSTAL DAMAGED AT LIGHTNING HOLE. REMOVED AND REPLACED INTERCOSTAL.

Part: ATTACH BRACKET — CRACKED (BS 500F) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET.

Part: SUPPORT ANGLE — DAMAGED (BS 500D) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY SIDEWALL SUPPORT ANGLE HAS DAMAGE AT NUTPLATE. REMOVED SIDEWALL SUPPORT BY REMOVING DAMAGE FABRICATING REPAIR PARTS AND INSTALLED.

Part: FRAME — CRACKED · airframe 53,358 hrs · 32,175 cycles

FRAME CRACKED AT FASTENER HOLE FOR OVERHEAD CENTERLINE DENT. CUT OUT CRACKED FRAME SECTION AND REPAIRED FRAME IAW SRM 53-00-07.

Part: WEB — CORRODED (BS 851) · airframe 53,358 hrs · 32,175 cycles

CORROSION AFT CARGO DOOR CUTOUT MID CLOSEOUT WEB. REMOVED AND REPLACED.

Part: MECHANISM — CORRODED (GALLEY DOOR) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT GALLEY DOOR MECHANISM HOUSING CORRODED. REPLACED GALLEY DOOR MECHANISM.

Part: SUPPORT — GOUGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP SIDEWALL SUPPORT IS GOUGED. REMOVED SIDEWALL SUPPORT FABRICATED NEW SUPPORT AND INSTALLED.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY SIDEWALL SUPPORT DAMAGED. REMOVED AND REPLACED SUPPORT.

Part: SUPPORT — GOUGED (CARGO BAY) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT GOUGED AT SEVERAL FASTENER HOLES. REMOVED DAMAGED SUPPORT FABRICATED NEW PART AND INSTALLED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO BAY INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO DOOR SURROUND WEB OVER FWD FRAME. REMOVED AND REPLACED WEB.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 53,358 hrs · 32,175 cycles

RT OTBD AFT FLAP PANEL BETWEEN NR 1 CARRIAGE ARMS UPPER SURFACE IS CHAFED BY AFT TWO FASTENER. REMOVED FABRICATED AND INSTALLED PANEL.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FRAME TO SIDEWALL SUPPORT HAS DAMAGE ON I/B FACE AT NUT PLATE LOCATIONS. INSTALLED NEW FRAME.

Part: PIN — GOUGED (GALLEY DOOR) · airframe 53,358 hrs · 32,175 cycles

AFT GALLEY DOOR OUTER HANDLE PIN GOUGED. REMOVED AND REPLACED THE PIN PER SRM 51 40 02.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

R1DOOR CUTOUT I/B CREASE BEAM SPLICE HAS DAMAGED HOLE. REPLACED CREASE BEAM SPLICE PER SRM.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

HOLD DOWN LIP ON SEAT TRACK BROKEN OFF. REMOVED AND REPLACED SEAT TRACK.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

WHILE WORKING 5173671 FOUND WEB WITH DAMAGED FASTENER HOLE. REMOVED AND REPLACED DAMAGED WEB.

Part: SUPPORT CHANNEL — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY SIDEWALL SUPPORT CHANNEL HAS DAMAGE AT NUT PLATES. REMOVED SUPPORT CHANNEL FABRICATED NEW CHANNEL AND INSTALLED.

Part: CHANNEL — DAMAGED (CARGO BAY) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY CHANNEL HAS ELONGATED HOLES. REMOVED AND REPLACED CHANNEL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

TOP FLANGE OF FRAME IS DAMAGED. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY THRESHOLD SUPPORT HAS ELONGATED HOLE. REMOVED SUPPORT FABRICATED NEW SUPPORT AND INSTALLED.

Part: ANGLE — CHAFED (LT WING) · airframe 53,358 hrs · 32,175 cycles

LEFT WING TRAILING EDGE PANEL ANGLE IS CHAFED. REMOVED AND REPLACED ANGLE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

CREASE BEAM HAS AREAS OF CORROSION BS 380 440 WL 208 RBL 65. REPLACED CREASE BEAM IAW SRM.

Part: FRAME — DAMAGED (BS 500D S22-25R) · airframe 53,358 hrs · 32,175 cycles

FCB FRAME HAS DAMAGE AT NUTPLATES BS 500D S22-25R. REMOVED AND REPLACED SPLICE CHANNEL PER SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FCB FRAME HAS DAMAGE AT NUTPLATES BS 500D STR 22R 25R. REMOVED AND REPLACED SPLICE CHANNEL PER SRM.

Part: MECHANISM — CORRODED (ENTRY DOOR) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION AFT ENTRY DOOR HANDLE HOUSING MECHANISM IS CORRODED. REPLACED CORRODED AFT ENTRY DOOR HANDLE HOUSING MECHANISM WITH SERVICEABLE HANDLE HOUSING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CREASE BEAM HAS AREAS OF CORROSION BS 380-440 WL 208 RBL 65. REPLACED CREASE BEAM PER SRM 51-70-12.

Part: WEB — PUNCTURED (RUDDER) · airframe 53,358 hrs · 32,175 cycles

WEB BELOW RUDDER PCU PUNCTURED. REMOVED REPAIRED AND RE-INSTALLED PAN ASSY.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FLOOR SPLICE STRAP HAS DOUBLE HOLE. REMOVED AND REPLACED STRAP.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FWD GALLEY DOOR AFT FRAME CRACKED AT NR 3 AND 4 STOP FRAME CUTOUTS. BLENDED ON AFT NR 3 AND 4 CUTOUTS BOTH FOUND TO BE OUT OF LIMITS FABRICATED REPAIR DOUBLES TREATED AND INSTALLED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

CORROSION ON FLOOR SUPPORT AT FASTENER HOLE AND PREVIOUS BLENDOUT. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SKIN PANEL — WORN (TE FLAP) · airframe 53,358 hrs · 29,064 cycles

TRAILING EDGE PANEL I/B SUPPORT IS WORN ON LT WING. REMOVED AND REPLACED

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 53,358 hrs · 29,064 cycles

FWD ENTRY GATE BEAM CRACKED AT FWD I/B EDGE. REPAIRED IAW SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 29,064 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED. WORK ACCOMPLISHED ON WO 5179280.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FWD GALLEY DOOR AFT FRAME AND DOUBLER CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED.

Part: PANEL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO BAY DOOR CUTOUT TEE CHORD CORRODED. REMOVED CORRODED TEE CHORD, FABRICATED NEW TEE CHORD AND INSTALLED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

FWD ENTRY DOOR AFT FRAME CRACKED AT NR 6 STOP PIN FITTING. REPAIRED IAW SRM 51-70-11.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FASTENER HOLE. REPAIRED PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 53,358 hrs · 29,064 cycles

CREASE BEAM UPPER SPHERE IS CRACKED. REMOVED FABRICATED AND INSTALLED NEW CREASE BEAM SPLICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTERLINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT BRACKET — DAMAGED (RAM AIR INLET) · airframe 53,358 hrs · 32,175 cycles

LT RAM AIR INLET DUCT UPPER AFT O/B SUPPORT BRACKET HAS ELONGATED HOLES. REMOVED AND REPLACED SUPPORT BRACKET.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTERLINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT — DENTED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT IS DENTED. REMOVED AND REPLACED SUPPORT.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP FLOOR TO SIDEWALL SUPPORT HAS CORROSION. REMOVED AND REPLACED ACB FLOOR SIDEWALL SUPPORT PER SRM.

Part: SUPPORT — GOUGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT GOUGED. REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT CORROSION ON INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL ASSY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD FRAME OF AFT CARGO COMPT. CUT OUT HAS A CRACK IN FRAME AT STOP FITTING HOLE BETWEEN STR 21 22 APPROX .375 INCH LONG (BS 794 FRAME). REMOVED AND REPLACED FRAME.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

SUPPORT ANGLE CRACKED FOR OVERHEAD CENTER LINE DUCT. REMOVED AND REPLACED ANGLE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION FCB AFT BULKHEAD LWR ANGLE IS CORRODED BS 500G LBL 24-RBL 24 WL 156. REMOVED AND REPLACED ANGLE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FORWARD CARGO BAY BS 440 FRAME UPPER SURFACE HAS DAMAGE IN RADIUS. REMOVED AND REPLACED FRAME PER DWG 65-20727.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

DAMAGED EDGE OF FRAME FLANGE. REMOVED DAMAGED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED BS 706 STR 11R. REMOVED AND REPLACED STRINGER CLIP.

Part: TORQUE BOX — CORRODED (APU BAY) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

APU RT TORQUE BOX HAS CORROSION AROUND THE INLET DUCT MOUNTING AREA I/B AND O/B SIDES. REMOVED AND REPLACED VERTICAL STIFFNER ON THE APU RT TORQUE BOX IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CRACK AT AFT FASTENER HOLE FOR RAM AIR ATTACH ANGLE. REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO DOOR CUTOUT STRAP CORRODED ON UPPER SURFACE. REMOVED, FABRICATED AND REPLACED TO CD CUTOUT STRAP PER SRM.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY DRILL STARTS ON STRAP. REPLACED 121 STRAP WITH FABRICATED STRAP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED BS 706 STR 11L. REMOVED AND REPLACED STRINGER CLIP.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

DRILL START ON FRAME DOUBLER. REMOVED DRILL START ON BS 500A DOUBLER FWD FACE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

5 DRILL STARTS ON EDGE OF FLOOR SUPPORT. REMOVED FLOOR SUPPORT FABRICATED NEW SUPPORT AND INSTALLED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED STRINGER CLIP.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT BS 727D+11 LBL 1 TO RBL 1 WL 148 CORROSION ON ANTENNA SUPPORT CHANNEL. REMOVED AND REPLACED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 794 STR 24L CARGO TIE DOWN IS CORRODED. REPLACED TIE DOWN PLATES PER SRM.

Part: SKIN — GOUGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FCB FUSE SKIN GOUGED BS 500+8 BETWEEN STR 24-25R. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND INSTALLED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT BS 727G+6 TO 827+6 LBL 20 WL 154 FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT ZEE.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 799-804 RBL 8 WL 154 3 DRILLED HOLES IN FLOOR SUPPORT. REPAIRED IN ACCORDANCE WITH SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED.

Part: STRINGER — DENTED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY STR 22R BENT BS 394 ON UPPER I/B FLANGE. REMOVED DAMAGED STRINGER, FABRICATED REPAIR PARTS.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT BS 827 FRAME DENTED 2 INCHES ABOVE STR 24L.

Part: FRAME — DENTED (BS 747) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMPARTMENT BS 747 FRAME DENTED 2 INCHES ABOVE STR 25L. REMOVED DAMAGED SECTION OF FRAME FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — DENTED (BS 767) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 767 FRAME DENTED 1 INCH ABOVE STR 24R. REMOVED DAMAGED SECTION OF FRAME FABRICATED REPAIR PARTS AND INSTALLED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CREASE BEAM WEB CORRODED. REPLACED WEB WITH FABRICATED CREASE BEAM WEB.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION FCB FLOOR TO SIDEWALL SUPPORT BS 500B+5-500D+10 WL 156 LBL 23-25. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT ANGLE — CHAFED (TE FLAP) · airframe 53,358 hrs · 32,175 cycles

LEFT PYLON I/B MID FLAP SPRING DOOR CUTOUT LOWER EDGE SUPPORT ANGLE AT AFT END HAS CHAFING DAMAGE. REMOVED DAMAGED STIFFENER AND INSTALLED NEW STIFFENER.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION FCB FLOOR TO SIDEWALL SUPPORT AT NUT PLATE HOLES BS 380-420 WL 156 LBL 23-25. REMOVED AND REPLACED SUPPORT ZEE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION FCB FLOOR TO SIDEWALL SUPPORT BS 500G-500D+10 WL 156 LBL 23-25. REMOVED AND REPLACED SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION FCB FLOOR TO SIDEWALL SUPPORT CORRODED AT NUT PLATE HOLES BS 380-500B+5 LBL 24 WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 727E STR 23R 25R SIDEWALL SUPPORT HAS AREAS OF CORROSION AT FASTENER HOLES. REMOVED DAMAGED SUPPORT FABRICATED NEW PART AND INSTALLED.

Part: INTERCOSTAL — CRACKED (BS 278) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL IS CRACKED AT 278 STR 14R. REMOVED AND REPLACED DAMAGED FRAME SECTION PER REPAIR.

Part: WEB — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO BAY DOOR CUTOUT WEB DAMAGED. REMOVED AND REPLACED WEB.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO BAY FLOOR PANEL IS PUNCTURED. REMOVED AND REPLACED FLOOR PANEL.

Part: BRACKET — CRACKED (TE FLAP) · airframe 53,358 hrs · 32,175 cycles

NR 6 FLAP TRANSMISSION O/B TORQUE TUBE DOGHOUSE LOWER I/B BRACKET. REPLACED CRACKED BRACKET.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 727O+10 727G+6 LBL20 WL 154 FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION. REMOVED AND REPLACED SUPPORT ZEE.

Part: STRINGER CLIP — CRACKED (BS 907 S8L) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP.

Part: REINFORCEMENT — GOUGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

DRILL MARKS ON FRAME REINFORCEMENT CHORD. FAB NEW FRAME MATERIAL TREATED DRILLED AND LOCATED ALODINE AND PRIME.

Part: SKIN PANEL — CHAFED (MIDFLAP) · airframe 53,358 hrs · 32,175 cycles

RIGHT O/B MID FLAP LOWER AFT I/B SKIN PANEL IS CHAFED ON LOWER SURFACE 48 INCHES FROM I/B END OF PANEL ON PREVIOUS REPAIR DOUBLER. RIGHT I/B MID FLAP LOWER AFT SKIN WAS REPAIRED PER SRM 51-70-10.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 727 727D+10 LBL 20 WL 154 FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION. REMOVED AND REPLACED SUPPORT ZEE.

Part: STRINGER CLIP — CRACKED (BS 727C S4L) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP.

Part: SKIN PANEL — CHAFED (TE FLAP) · airframe 53,358 hrs · 32,175 cycles

RIGHT O/B MID FLAP LOWER AFT I/B SKIN PANEL IS CHAFED ON LOWER SURFACE 33 INCHES FROM I/B END OF PANEL ON PREVIOUS REPAIR DOUBLER. RIGHT O/B MID FLAP LWR AFT SKIN WAS REPAIRED PER SRM 51-70-10.

Part: STRINGER CLIP — CRACKED (BS 887 S4L) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED STA 907 STR 8R. REMOVED AND REPLACED STR CLIP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

AFT CARGO COMP BS 727E+10 767 RBL 20 WL 154 FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT.

Part: SKIN PANEL — CHAFED (MIDFLAP) · airframe 53,358 hrs · 32,175 cycles

RIGHT O/B MID FLAP LOWER AFT I/B SKIN PANEL IS CHAFED ON LOWER SURFACE 48 INCHES FROM I/B END OF PANEL ON PREVIOUS REPAIR DOUBLER. RIGHT I/B MID FLAP LOWER AFT SKIN WAS REPAIRED PER SRM 51-70-10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON SURFACE OF FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON SEAT TRACK STA 685 RBL 45. REMOVED AND REPLACED SEAT TRACK.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,358 hrs · 32,175 cycles

LT HORZ STAB LWR SKIN CRACKED (NDI VERIFIED 2 INCH CRACK) STAB STA 125 REAR SPAR AREA. REPAIRED IAW EA 400-55EA-01247.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL DAMAGED. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED.

Part: STRINGER — DENTED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

STRINGER DENTED. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON AFT CARGO DOOR CUTOUT AFT FRAME CLOSEOUT WEB. REMOVED WE FABRICATED NEW WEB WEB TO BE INSTALLED ON MIG 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON FCB FLOORBEAM RBL 13 WL 156 BS 500F+14 AND BS 500E AT NUT PLATES. REMOVED AND REPLACED WITH NEW FLOORBEAM SECTION.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON WEB BOTTOM SURFACE. REMOVED AND REPLACED WEB.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 53,358 hrs · 32,175 cycles

L1 DOOR AFT GIRT BAR FITTING ATTACH BRACKET HAS CORROSION. REMOVED AND REPLACED GIRT BAR FITTING ATTACH BRACKET.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL CRACKED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

INTERCOSTAL CRACKED. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED.

Part: STRINGER CLIP — CRACKED (BS 727B S4L) · airframe 53,358 hrs · 32,175 cycles

CRACKED STRINGER CLIP STA 727B STR 4L. REMOVED AND REPLACED STRINGER CLIP.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON ZEE CHANNEL. REMOVED AND REPLACED ZEE CHANNEL.

Part: SILL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

R2 MOPSILL SUB THRESHOLD WEB IS CORRODED BS 952-986.5 RBL 53. REMOVED AND REPLACED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

DRILL START IN TOP OF STR 16L BS 603 NEXT TO HI-LOK FASTENER. REPAIRED PER EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CRACK IN BEAR STRAP AT FASTENER HOLES AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REMOVED CRACKS REPAIRED PER ASA EA 400-53EA-01453.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON GALLEY MOUNT BS 998.5 LBL 32 WL 208. REMOVED AND REPLACED.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON GALLEY MOUNT BS 1016 RBL 32 WL 208. REMOVED AND REPLACED.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON ZEE CHANNEL BS 992.5 LBL 33-43 WL 208. REMOVED CORROSION FOUND TO BE 100% MATERIAL LOSS PER SRM 51-10-02 REMOVED AND REPLACED ZEE CHANNEL PER SRM 51-40-02.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION ON GALLEY MOUNT BS 998.5 RBL 32 WL 208. MOUNT TO BE REPLACED ON NRC.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON ZEE CHANNEL BS 992.5 LBL 33-43 WL 208. REMOVED AND REPLACED ZEE CHANNEL.

Part: WEB — GOUGED (CARGO DOOR) · airframe 53,358 hrs · 32,175 cycles

FWD CARGO DOOR SURROUND WEB DAMAGED GOUGED. REPLACED WEB SURROUND WEB.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON R2 MOPSILL SUB THRESHOLD WEB BS 952 986 AT FASTENER HOLE. REMOVED MOPSILL FABRICATED NEW MOPSILL AND INSTALLED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON WEB BS 986. REPLACED SHEAR WEB WITH FABRICATED WEB.

Part: SKIN — DAMAGED (BS 951) · airframe 53,358 hrs · 32,175 cycles

DENT/BULGE ON FUSELAGE EXTERNAL SKIN. CUT OUT DAMAGED SKIN ACCOMPLISHED FUSELAGE SKIN REPAIR BS 951 STR 22L TO STR 23L. SRM 53-00-01

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION AFT WET AREA ON 986 FLOORBEAM SKIN TO SKIN. REPAIRED FLOORBEAM UPPER TEE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON R1 DOOR MOPSILL. REMOVED AND REPLACED MOPSILL.

Part: SILL — DAMAGED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

AFT CARGO DOOR SURROUND LOWER SILL TOP I/B EDGE HAS MECHANICAL DAMAGE AND SHARP EDGES. REMOVED AND REPLACED AFT CARGO DOOR LOWER SILL CENTER SCUFF PLATE ASSY.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION ON WEB AT BS 1000-1003 RBL 36-39 WL 208. WEB REPLACED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

CORROSION WEB BULGING AT BS 987 LBL 34-42 WL 208. REPLACED SHEAR WEB WITH FABRICATED WEB.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

L1 DOOR I/B THRESHOLD SUPPORT C-CHANNEL HAS CORROSION BS 312-340 WL 208 LBL 67. REMOVED AND REPLACED C-CHANNEL.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

BEAR STRAP CRACKED AT FASTENER HOLE BS 304.5 WL 238. REMOVED CRACKS REPAIRED PER ASA EA 400-53EA-01453.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,358 hrs · 32,175 cycles

L1 DOOR O/B THRESHOLD SUPPORT Z-CHANNEL HAS CORROSION BS 320 340 WL 208 LBL 65. REPLACED WITH NEW ZEE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,804 hrs · 20,710 cycles

CORROSION AFT WET AREA BS 986 FLOORBEAM UPPER CHORD HAS EXTENSIVE CORROSION SKIN TO SKIN.

Part: SILL — CORRODED (FUSELAGE) · airframe 53,358 hrs · 32,175 cycles

CORROSION AFT WET AREA R2 MOPSILL HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED PER SRM.

Part: GUIDE ARM — WORN (L2 DOOR) · airframe 53,315 hrs · 32,140 cycles

F/A REPORTED L2 DOOR DIFFICULT TO CLOSE AND SEEMS TO HANG UP. REMOVED AND REPLACED L2 DOOR GUIDE ARM AND GUIDE ARM ROLLER PER MM 52 13 31. OPS CHECK GOOD.

Part: GUIDE ARM — WORN (L2 DOOR) · airframe 52,866 hrs · 31,744 cycles

L2 ENTRY DOOR HARD TO CLOSE. R&R L2 DOOR GUIDE ARM PER AMM 52 13 31.

Part: GUIDE ARM — OUT OF ADJUST (L2 DOOR) · airframe 52,616 hrs · 31,540 cycles

L2 DOOR STICKS OPENING AND CLOSING ADJUSTED L2 DOOR GUIDE ARM REF MM 52-13-31 404 004 STEP C (6). OPS CK GOOD. LUBRICATED L2 DOOR HINGES AND GUIDE ARM ONLY. REF 12-25-11. DOOR OPERATES SMOOTH THRU OPEN AND CLOSE CYCLE.

Part: NUT — LACK OF LUBE (TE FLAPS) · airframe 52,205 hrs · 31,171 cycles

FLAPS WOULD NOT EXTEND PAST 15 DEG, NO SPLIT OBSERVED. CREW REPORTS NO "NEEDLE SPLIT" & NO ABNORMAL ROLL CONTROL INPUTS REQUIRED. CONDUCTED VISUAL INSPECTION OF FLAP TRACK & DRIVE MECHANISM. FOUND SEVERAL DRY JACK SCREWS. LUBED SCREWS & BALL NUTS REF MM 12 22 51. ACCOMPLISHED ASYMMETRY TEST PER MM 27 51 00. CYCLED FLAPS MANY TIMES NO ABNORMAL FUNCTION OR INDICATION NOTED.

Part: HINGE — LACK OF LUBE (L2 DOOR) · airframe 51,994 hrs · 30,994 cycles

F/A'S REPORT L2 HARD TO OPEN. LUBRICATED L2 DOOR GUIDE PLATES & DOOR HINGES AS REQUIRED. L2 DOOR CHECKS NORMAL, REFERENCE MM 12 25 11.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 51,973 hrs · 30,977 cycles

LOWER LEFT CORNER OF MAIN CARGO DOOR BENT OUT APPROXIMATELY 2 1 2" 3". DOOR WAS CLOSED ON A CORNER OF THE AIRSTAIRS WHICH APPARENTLY WERE MOVED AFTER CARGO DOOR WAS OPENED. REPAIRED MAIN CARGO DOOR IAW SRM 52-90-01 FIG 203 SHTS 1 3 AND EA 0500-01337.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 51,853 hrs · 30,872 cycles

AT CRUISE 350 CABIN ALT HORN SOUNDED. CABIN PRESSURE VERIFIED TO BE BETWEEN 10,000 - 11,000 FT, 2 PSI DIFFERENTIAL. RAN CHECK. LIST NO AUTOFAIL LIGHT. MOVED SWITCH TO STBY AND SET CRUISE ALT OF 7000 FT IN WINDOW. CABIN STARTED DOWN AT 700 FPM. BEGAN DESCENT INTO ARC AND SLOWLY REGAINED THE CABIN ALT. REMOVED & REPLACED CABIN PRESS CONT REF AMM 21 31 21, OPS CHECK GOOD REF AMM 21 31 00 702 001.

Part: SEAL — FAILED (CARGO DOOR) · airframe 51,828 hrs · 30,853 cycles

AT CRUISE FL340 CABIN ALT WARNING HORN CAME ON CABIN ALT WAS 10.5 11.0, RAN CABIN ALT WARN HORN RAPID DEPRESS CK LIST. CONTROLLED CABIN AT ABOUT 11 12 THOUSAND BEGAN NORMAL DESCENT AND DECLARED EMERGENCY DEVIATE YVR. ABOUT FL190 CABIN PRESS FELT LIKE IT WAS EXCESSIVE. CRACKED OUTFLOW OPEN AND GOT 4K FT MIN INCREASE CLOSED OUTFLOW + CAUGHT CABIN AGAIN. CABIN GOT COLD, PRESSURIZED AIRCRAFT PER MM 05 51 91 702 001 AND FOUND THE FOLLOWING. UNABLE TO PRESSURIZE USING ONE AIR COND PACK REQUIRED RT ENG AND APU AS BLEED SOURCE AND BOTH PACKS OPERATING TO REACH 4 PSID. DECAY RATE FROM 4 PSID TO 2.5 PSID WAS 50 SECS. OUT OF LIMITS. FOUND AIR LEAKS AT NOSE GEAR DOWNLOCK VIEWER IN NOSE W/W AND FROM MAIN CARGO DOOR.

Part: DOOR — STIFF (L1) · airframe 50,957 hrs · 30,031 cycles

FLIGHT ATTENDANT REPORTS THAT THE L1 DOOR HANDLE IS DIFFICULT TO MOVE TOWARDS THE CLOSED POSITION THE LAST FEW INCHES OF TRAVEL. ADJ FWD ENTRY DOOR GUIDE ARM REF MM 52 11 00, NO HELP. 76732. ADJ GUIDE ARM 1 FLAT IN76732. CONT WITH FWD ENTRY DOOR ADJ MIG 2 C 211789 INIT. SEE MIG 2C 211789 FOR WORK ACCP. RIGGED L1 DOOR REF MM 52 11 00 705 007 B00. PERFORMED FWD DOOR ENTRY DOOR TEST. REF MM 52 11 00 755 051 B00. MIG 2C 211789 CLOSED.

Part: DOOR — STUCK (FORWARD ENTRY) · airframe 50,915 hrs · 29,991 cycles

FLIGHT ATTENDANT REPORTS L1 DOOR HARD TO CLOSE. OPENS EASILY NO SQUEALING DURING FLIGHT. LIGHT INDICATION NORMAL. INSPECTED L1 DOOR FOR PROPER OPERATION. FOUND OK REF 52 11 00, LUBED DOOR HINGES.

Part: HINGE — LACK OF LUBE (L2 DOOR) · airframe 50,414 hrs · 29,532 cycles

L2 DOOR GRINDING STIFF & DIFFICULT TO CLOSE & OPEN. LUBRICATED UPPER HINGE, L2 DOOR OP CHECKS GOOD.

Part: FITTING — DEFECTIVE (L2 DOOR) · airframe 49,974 hrs · 29,137 cycles

FLIGHT ATTENDANT REPORTS L2 DOOR DIFFICULT TO OPEN & MAKES A SQUEAKING SOUND ON OPENING. REPLACED LOWER TORQUE TUBE SPROCKET UPPER DOOR FITTING AND UPPER GUIDE ARM & PIN. DOOR OP CHECKS GOOD & NO SQUEAKING NOISES ON DOOR.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 49,717 hrs · 28,892 cycles

CANNOT CLOSE L1 DOOR. ADJUSTED UPPER GUIDE ARM (REF 52 11 00). DOOR OPS NORMAL.

Part: LUBRICATION — ODOR (NR 2 ENGINE) · airframe 48,896 hrs · 28,186 cycles

ODOR IN COCKPIT, FLT ATTENDANTS REPORTED ODOR AND HAZE IN FWD GALLEY PAX PORTION AND IN AFT GALLEY. FAN LUB ACCOMPLISHED ON NR 2 ENG JUST PRIOR TO THIS FLIGHT. FOUND RESIDUAL LUBE MATERIAL ON FAN BLADES BOOSTER COMP AND IGV'S. CLEANED OFF EXCESS LUBRICANT. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING PER ASA MM 05-60-00 AND BURN OUT PROCEDURE PER AMM 21 00 01.

Part: ACTUATOR — BYPASSING (LT MLG) · airframe 45,154 hrs · 25,826 cycles

AFTER T/O GEAR HANDLE IN UP THEN OFF POSITION, LEFT GEAR DOOR AND LEFT GREEN GEAR LIGHT ILLUMINATED. DEFINITE YAW NOTICED. GEAR HANDLE PUT TO DOWN POSITION, ALL GEAR DOWN AND GREEN. REMOVED AND REPLACED LEFT MLG ACTUATOR AND LEFT MLG UPLOCK ACTUATOR.

Part: SKIN — GOUGED (RT WING FOREFLAP) · airframe 44,847 hrs · 25,677 cycles

RT WING OB FOREFLAP IS GOUGED AT THE UPPER SURFACE AT THE IB END. REMOVED DAMAGED AREA OF FORE FLAP UPPER SKIN, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER PER SRM 51-70-10 REPAIR 4.

Part: SKIN — GOUGED (BS 1121-1138) · airframe 44,847 hrs · 25,677 cycles

FOUND FUSELAGE SKIN PANEL IS CHAFED AND GOUGED JUST BELOW THE LT HORIZ STAB. BLENDED DAMAGED AREA OF SKIN, PERFORMED HFEC INSPECTION OF BLEND AREA TO ENSURE NO OTHER DEFECTS EXIST. FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW ASA EA 5380-01016 AND AAR EA 11314.

Part: TAB — CHIPPED (AILERONS) · airframe 44,847 hrs · 25,677 cycles

THE RIGHT AILERON TAB IS CHIPPED ON THE TE AT THE IB END. SMOOTHED DAMAGED AREA, PREPPED AND APPLIED ONE REPAIR AND TWO FILLER FIBERGLASS PLIES AND HOT BONDED IAW SRM 51-70-16 PG 4,10,20 AND 26.

Part: SKIN — DENTED (T/E FLAP)

OKC - FOUND RIGHT WING INBOARD T/E FLAP WEDGE NR 7420 LOWER SURFACE HAS DENTS. REMOVED DENTED AREAS OF ALL 6 DENTS, FABRICATED ALL 6 FILLERS AND DOUBLERS AND INSTALLED IAW B737-400 SRM 51-70-10 PAGE 211 PARAGRAPH 7, PAGE 213 PARAGRAPH 8, PAGE 221, PARAGRAPH 12, PAGE 238 PARAGRAPH 156 AND PAGE 249 PARAGRAPH 20. (M)

Part: TORQUE TUBE — WORN (FLAP DRIVE)

TORQUE TUBE JUST IB OF NR 1 ENGINE PYLON WORN, FLAP DRIVE TORQUE TUBE AT FLOATING SEAL ASSEMBLY WBL 182. REMOVED AND REPLACED TORQUE TUBE JUST IB IF NR 1 ENGINE PYLON PER AMM. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - SEAT TRACK, MECHANICAL DAMAGE STA 360 TO 480, RBL 45, WL208. REPLACED SEAT TRACK. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - CORROSION ON FLOORBEAM, STA 360. REPAIRED FLOORBEAM IAW EA. (K)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

PAE - CORROSION ON SIDEWALL SUPPORT. REPLACED IAW SRM. (K)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

PAE - CORROSION ON UPPER FUSELAGE SKIN AROUND ANTENNA CUTOUT STA 620 BETWEEN STRINGER 1 AND 2R. REPAIRED IAW EA. (K)

Part: ANGLE — CRACKED (LT WING)

PAE - LT WING T/E LWR ANGLE CRACK ON UPPER T/E PANEL. REMOVED, FABRICATED AND REPLACED ANGLE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

PAE - CORROSION ON FLOORBEAM, STA 967 LBL 14-48, WL 208. REPAIRED 967 FLOORBEAM UPPER FLANGE IAW EA. (K)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FUSELAGE EXTERNAL LONGITUDINAL LAP REPAIR AT STA 927, STR 20R NOT IAW SRM, ENGINEERING INSTRUCTIONS REQUIRED. REPAIRED IAW EA. (K)

Part: SCUFF PLATE — GOUGED (CARGO DOOR) · airframe 41,104 hrs · 23,691 cycles

PAE - AFT LOWER CARGO DOOR CTR SCUFF PLATE GOUGED. REPLACED SCUFF PLATE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET STA 867 LT. REPAIRED FRAME IAW EA. (K)

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - VERTICAL STIFFENER CRACKED AT BS 947. REPLACED STIFFENER ANGLE. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - UPPER LOBE INTERIOR FRAME CRACKED FWD SIDE UNDER STOP FITTING SUPPORT. REPAIRED FRAME WEB. (K)

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - SHEAR WEB UPPER ANGLE DAMAGED AT THE EDGE AT BS 946, WL 208. REPLACED ANGLE. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FRAME CRACKED. REPAIRED FRAME IAW EA. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FRAME CRACKED. REPAIRED FRAME IAW EA. (K)

Part: FRAME — DENTED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - DENT IN TOP OF FRAME FLANGE. REPAIRED IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - STRINGER 20R CRACKED. REPLACED STRINGER. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET. REPAIRED CRACKED FRAME. (K)

Part: SEAT TRACK — MISMANUFACTURED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - OB FLANGE OF SEAT TRACK IS MISSING FLOOR PANEL ATTACHMENT HOLES AT BS 360-480. LOCATED AND DRILLED HOLES. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - SEAT TRACK CORRODED AT STA 370. REPAIRED SEAT TRACK. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION ON FLOORBEAM. REPAIRED CORRODED FLOORBEAM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K)

Part: SKIN — CORRODED (LT WING) · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION ON LT UPPER WING PANEL 8117 CUTOUT UPPER FLANGE. BLENDED CORROSION AND REPAIRED. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - MECHANICAL DAMAGE SEAT TRACK AT BS 727B TO 927. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET. REPAIRED CRACKED FRAME. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FRAME CRACKED AT PSU SUPPORT BRACKET. REPAIRED FRAME IAW EA. (K)

Part: STRINGER — IMPROPER (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - STR 19R HAS SHORT EDGE DISTANCE AT FACTORY TERMINATION BS 927. REPLACED STRINGER. (K)

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - DAMAGED SEAT TRACK AT BS 727B. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - DAMAGED SEAT TRACK AT BS 927. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - DAMAGED SEAT TRACK AT BS 480. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,104 hrs · 23,691 cycles

PAE- CORROSION ON GALLEY FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION FOUND ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION ON GALLEY FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION FOUND ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,104 hrs · 23,691 cycles

PAE - CORROSION ON GALLEY FLOOR SUPPORT. REPAIRED FLOOR SUPPORT. (K)

Part: WEB — CANNING (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - OIL CANNED WEB. REMOVED FABRICATION AND INSTALLED NEW WEB. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K)

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - FWD SERVICE DOOR, DAMAGE ON WEB. REMOVED DAMAGE ON CREASE BEAM WEB, FABRICATED REPAIR PARTS AND INSTALLED. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K)

Part: SEAT TRACK — TORN (FUSELAGE) · airframe 41,104 hrs · 23,691 cycles

PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K)

Part: CREASE BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON CREASE BEAM CHORD, MOPSILL. REPLACED PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - FOUND INTERCOSTAL IS CRACKED. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CORROSION ON FLOOR SUPPORT. REPLACED PER AMM. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - FOUND FRAME DAMAGED. REPAIRED PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - FOUND DENT ON TOP OF FRAME FLANGE. REPLACED FLANGE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE - INTERCOSTAL ANGLE IS CRACKED. REPLACED PER SRM. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON INBOARD CHORD OF RT CREASE BEAM, MOPSILL. REPLACED MOPSILL, CREASE BEAM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SIDEWALL SUPPORT. REPLACED PER SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - FOUND DOUBLE HOLE IN FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - LT VERTICAL STAB SKATE (FWD) ANGLE IS CHAFFED. REPLACED LEFT VERTICAL STAB FORWARD SKATE ANGLE. (M)

Part: ANGLE — CRACKED (INTERCOSTAL)

PAE - INTERCOSTAL ANGLE IS CRACKED. REPLACED PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DENT AFT CARGO BAY FRAME. REPAIRED FRAME PER SRM. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - FOUND FRAME DAMAGED. REPAIRED PER SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE - FOUND CRACKED ANGLE. REPLACED PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - FOUND DENT ON TOP OF FRAME. REPAIRED FRAME PER SRM. (M)

Part: CREASE BEAM — DENTED (FUSELAGE)

PAE - FOUND CORROSION ON INBOARD CREASE BEAM CHORD, MOPSILL. REPLACED CREASE BEAM CHORD. (M)

Part: ATTACH FITTING — CORRODED (GIRT BAR)

PAE - FOUND CORROSION ON GIRT BAR MOUNT. REPLACED GIRT BAR MOUNT. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM UPPER CHORD PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - FOUND DENT ON TOP OF FRAME FLANGES. REPAIRED PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - FOUND DENT ON TOP OF FRAME FLANGES. REPAIRED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON U-ANGLE. REPLACED U-ANGLE. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON UPPER LOBE INTERIOR CORROSION ON CREASE BEAM WEB. REPLACED CREASE BEAM WEB. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON Z-ANGLE. REPLACED Z-ANGLE. REPLACED Z-ANGLE PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED. REPLACED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED PER SRM. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

PAE - FOUND CREASE BEAM CHORD CORRODED. REPLACED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED. REPLACED FRAME PER EA. (M)

Part: WEB — DENTED (CARGO DOOR)

PAE - FOUND DENT AT LIGHTING HOLE FORWARD CARGO DOOR INNER WEB. REMOVED DAMAGED AREA, FABRICATED TWO REPAIR PARTS, AND REPAIRED PER SRM. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

PAE - FOUND CREASE BEAM CHORD CORRODED. REPAIRED PER SRM. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON L-ANGLE OF RIGHT CREASE BEAM. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND AFT LOWER CARGO COMPARTMENT LEFT SIDEWALL/FLOOR SUPPORT CORRODED. REPAIRED FLOOR TO SIDEWALL SUPPORT PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - FOUND DENT ON TOP OF FRAME. FABRICATED REPAIR PART AND INSTALLED. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORRODED FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: SUPPORT — GOUGED (FUSELAGE)

PAE - FOUND FORWARD CARGO SIDEWALL SUPPORT IS GOUGED. INSTALLED NEW SIDEWALL SUPPORT. (M)

Part: WEB — DENTED (FUSELAGE)

PAE - FOUND FORWARD CARGO DOOR CUTOUT, LOWER FORWARD CLOSE OUT WEB DENTED. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND AFT CARGO FLOOR SUPPORT CORRODED. REPAIRED PER EA. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND FLOOR SUPPORT CORRODED. REPAIRED PER EA. (M)

Part: WEB — DENTED (FUSELAGE)

PAE - FOUND DENT IN FORWARD CARGO INNER WEB. FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: STRUCTURE — DENTED (CARGO DOOR)

PAE - FOUND DENT IN EDGE OF LIGHTING HOLE, FORWARD CARGO DOOR INNER SURFACE AT UPPER FORWARD CORNER. CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - FOUND INTERCOSTAL CRACKED. REPAIRED PER SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - FOUND STRINGER CLIP CRACKED. REPAIRED PER SRM. (M)

Part: FITTING — GOUGED (FUSELAGE)

PAE - FOUND LOWER AFT LATCH FITTING FOR ASD GOUGED. REPLACED PER SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - FOUND CRACKED STRINGER CLIP. REPLACED PER SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - FOUND CRACKED STRINGER CLIP. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REPAIRED AND REPLACED PART PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND LOWRE FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE Z-ANGLE AFT OF DOOR CUTOUT FS 867 TO AFT BULKHEAD IS CORRODED, ALONG ENTIRE LENGTH. INSTALLED NEW Z-ANGLE ON RT AFT SIDE FROM STATION 867 TO AFT BULKHEAD, PER SRM 51-40-02 PAGES 3 AND 4 PAR B. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE REINFORCEMENT DOUBLER FORWARD SIDE CARGO DOOR FORWARD FRAME CORRODED BETWEEN STRINGER 26R AND 24R. REMOVED AND REPLACED DOUBLER PER SRM 51-70-11 PAGES 1-6. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT, BILGE Z-ANGLE FROM STATION 727 RT TO CARGO DOOR HAS CORROSION, STATION 767. REMOVED AND REPLACED AFT CARGO Z-ANGLE FROM STATION 727 TO RT CARGO DOOR STATION 767 RT SIDE. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT MID CABIN INOPERATIVE. RECONNECTED WIRE AND OPERATIONAL CHECKED GOOD. (M)

Part: SKIN — DAMAGED (ELEVATOR)

PAE - DURING C-CHECK, FOUND AREA OF EXPOSED FIBER ON UPPER SKIN OF LEFT ELEVATOR UNDER TAB DRIVE ROD FAIRING OUTBOARD OF AFT FASTENER. REPAIRED IAW EA. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON OUTBOARD C-CHANNEL IN AFT CARGO BAY THRESHOLD AT BS 794 TO 847, RBL 24 AND WL 150. REMOVED AND REPLACED IAW SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND GOUGE ON OUTER SKIN AT STATION 385, 4 INCHES BELOW STRINGER 17L. REPAIRED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY SUB-THRESHOLD WEB IS CORRODED AT BS 793-847 AND RBL 20-28. REPAIR VIA REMOVED AND REPLACED IAW SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND GOUGE ON OUTER SKIN AT STATION 369, 2 INCHES BELOW STRINGER 17L. REPAIRED IAW SRM. (M)

Part: WIRE — DISCONNECTED (ROW 12-15)

PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 12-15 INOPERATIVE. RECONNECTED WIRES, OPERATIONS CHECKED GOOD. (M)

Part: WIRE — DAMAGED (CABIN)

YVR - BEFORE FLIGHT FOUND EMERGENCY TRACK LIGHTS AT ROW 16 DAMAGED WIRE. REPAIR WIRE, OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JNU - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 25. REPLACED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 13 TO 15. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

GEG - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 21. RECONNECTED LOOSE WIRE, OPS CHECK GOOD. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

PDX - BEFORE FLIGHT FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 14/15, DISCONNECTED. RECONNECTED FLOOR TRACK LIGHTS. OPERATIONAL CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, FOUND 2 FORWARD RED EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SAN - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 12-15. RECONNECTED LIGHTS OPS NORMAL. (M)

Part: LIGHT — DISCONNECTED (ROW 22 - 24)

PDX DURING SERVICE INSPECTION FOUND EMERGENCY TRACK LIGHTS INOP AT ROW 22-24, DISCONNECTED. RECONNECTED TRACK LIGHTS, OPERATION CHECKED NORMAL. NO DEFECTS NOTED.

Part: WIRE — DISCONNECTED (ROW 16)

ANC - FLT 140 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14-16 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 21 - 25)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 21-25 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO FLIGHT 97, THE EMERGENCY EXIT TRACK LIGHT AT ROW 1 WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: ARM — INOPERATIVE (PAX DOOR)

SEA - PRIOR TO FLT 444, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO OPEN. REPLACED THE L1 DOOR GUIDE ARM AND THE DOOR OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: ACTUATOR — INOPERATIVE (RT MLG)

SAN - FLT 501 - ON DEPARTURE FROM SAN, RAISED LANDING GEAR NORMALLY BUT WHEN SELECTED GEAR HANDLE TO OFF, THE RIGHT GEAR EXTENDED UNCOMMANDED. PLACED GEAR HANDLE BACK TO UP, THEN RETURNED GEAR HANDLE TO OFF POSITION AND THE RIGHT GEAR REMAINED UP. CONTINUED TO SEA WHERE EXTENDED NORMALLY AND ACFT LANDED WITHOUT INCIDENT. SEA MAINTENANCE REPLACED THE RIGHT MLG LOCK ACTUATOR. COMPLETED GEAR SWING AND EMERGENCY EXTENSION CHECK, AND THE GEAR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: LIGHT — CORRODED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED R1 EMERGENCY LIGHT REFLECTOR ASSY AND LIGHT OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED 3 LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: RELEASE ASSY — INOPERATIVE (R1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE THE R1 DOOR HOLD OPEN RELEASE ASSEMBLY WOULD NOT HOLD DOOR OPEN. REPLACED DOOR HOLD OPEN RELEASE ASSY, OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, TEH AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 26 AFT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — CHAFED (APU AREA)

OAK - FLT 438 - THE APU FIRE WARNING ACTUATED AT CRUISE ALTITUDE, WITH THE APU HAVING BEEN OFF FOR 20 MINUTES. CREW PULLED APU FIRE HANDLE AND DISCHARGED BOTTLE. BOTH THE APU DETECTION INOPERATIVE LIGHT AND THE APU FIRE WARNING CAME ON INTERMITTENTLY THEREAFTER. AIRCRAFT LANDED IN OAK WITHOUT INCIDENT. MAINTENANCE OPENED APU COWL AND INSPECTED AREA. NO EVIDENCE OF FIRE NOTED, SUSPECT FALSE FIRE INDICATION. RELEASED PER MEL 26-7, APU FIRE EXTINGUISHING SYSTEM INOPERATIVE. SUBSEQUENTLY FOUND WIRES FROM D4816P DAMAGED BY SHROUD. REPAIRED INSULATION AND REPOSITIONED WIRE BUNDLE. REMOVED AND REPLACED APU FIRE BOTTLE AND INDICATION DISK. SYSTEM OPERATES NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R-2 ESCAPE SLIDE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPAIRED CONTACT AND LIGHT OPERATED NORMALLY.

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 27 AFT. RECONNECTED LOOSE WIRE AND LIGHTS OPERATED NORMALLY. (X)

Part: SWITCH — DEFECTIVE (LANDING GEAR)

LAS - FLT NR 621 - DURING DEPARTURE THE GEAR HANDLE WOULD NOT MOVE UP. RAN 'GEAR WILL NOT GO UP' CHECKLIST AND THE TAKEOFF WARNING CONTINUED TO SOUND AFTER FLAPS WERE FULLY RETRACTED, RETURNED TO LAS. REPLACED LANDING GEAR SAFETY SWITCH. PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST AND GEAR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: TRACK LIGHT — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 2 LIGHT ASSEMBLY BASES AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL ASSY — DAMAGED (CABIN)

EMERGENCY FLOOR TRACK LIGHTS INOP AFT OF ROW 27. MAINTENANCE REPLACED ROW 27 LIGHT ASSY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W)