N763AS

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 71,420 hrs · 47,951 cycles

INTERIOR EMERGENCY LIGHTS INOPERATIVE RIGHT SIDE OF PASSENGER CABIN, INCLUDING R2 DOOR AREA. ACFT GROUNDED. REPLACED THE BATTERY PACK & POWER SUPPLY IAW AMM 33-51-51. OPS NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 71,133 hrs · 47,714 cycles

EMERGENCY EXIT LIGHTS OUT OVER R2 DOOR & SEVERAL RT AISLE LIGHTS. ACFT GROUNDED. REPLACED THE BATTERY PACK IAW AMM 33-51-51. OPS NORMAL.

Part: O-RING — DAMAGED (RT WING FUEL) · airframe 71,090 hrs · 47,676 cycles

DURING TAXI, NR 2 ENGINE SHUTDOWN ON ITS OWN. ENGINE PARAMETERS WERE ALL WITHIN LIMITS. ACFT GROUNDED. STARTED NR 2 ENGINE, INDICATIONS FLUCTUATING, N1 21.9 TO 21.2, EGT 460 TO 450, N2 59.6 TO 59.0, FF 85-75, APPROX 3 MIN AFTER INITIAL ENGINE START, ALL ENGINE PARAMETERS SETTLED TO NORMAL. ENGINE PARAMETERS MATCHED NR 1 ENG. MOVED FUEL PUMP SWITCHES TO OFF POSITION ENGINE PARAMETERS STAYED NORMAL. BOROSCOPE INSPECTION C/W, NO DEFECTS. SUMPED NR 2 FUEL TANK 3 GALLONS, NO WATER. FUEL PUMP IMPELLER ROTATION CHECKED IAW AMM 71-00-59-10, ROTATION OK. .

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,892 hrs · 47,515 cycles

R2 DOOR INTERIOR EMERGENCY EXIT LIGHT ABOVE DOOR ONLY ILLUMINATES FOR 5-10 SECONDS. ACFT GROUNDED. REPLACED R2 DOOR EMERGENCY LIGHT BATTERY PACK, REF AMM 33-51-51. OPS NORMAL.

Part: INTERCOSTAL — CRACKED (BS 500-500A) · airframe 70,518 hrs · 47,209 cycles

RIGHT INTERCOSTAL BETWEEN BS 500 - 500A, FOUND TO BE CRACKED. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0.

Part: TRANSITION PANEL — CRACKED (BS 500-500B) · airframe 70,518 hrs · 47,209 cycles

RIGHT TRANSITION PANEL BS 500 - 500B CRACKED. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW TRANSITION PANEL IAW SRM 51-40-05-0G-0

Part: BEAM — CRACKED (BS 727) · airframe 70,518 hrs · 47,209 cycles

BS 727 AUX BEAM AT STRINGER 18AL, FWD LOWER HOLE IS SHOWING CRACK INDICATION. ACFT GROUNDED. ACCOMPLISHED REPAIR IAW AD20122304-400-53-11L & AD20122304-400-53-7.

Part: BEAM — CRACKED (BS 727) · airframe 70,518 hrs · 47,209 cycles

BS 727 AUX BEAM AT STRINGER 18AL, SHOWING A CRACK INDICATION. ACFT GROUNDED. ACCOMPLISHED REPAIRS IAW T/C'S AD20122304-400-53-11L & AD20122304-400-53-7.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,518 hrs · 47,209 cycles

INTERCOSTAL CRACKED IN RADIUS STR 14R AT STA 277. REQUIRES REPLACEMENT IAW T/C AD20142206-400-53-2D. NOTE: REQ OPEN HOLE INSPECTION PRIOR TO INSTALLATION OF NEW PARTS IAW T/C. ACFT GROUNDED. R & R DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 70,518 hrs · 47,209 cycles

STRINGER CLIP IS CRACKED AT STA 277 AND STR 15R. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGLER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,518 hrs · 47,209 cycles

STRINGER CLIP IS CRACKED AT STA 277 AND STR 15R. ACFT GROUNDED. R & R CRACKED STR CLIP IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 70,518 hrs · 47,209 cycles

INTERCOSTAL CRACKED IN RADIUS STRINGER 14R AT BS 277. ACFT GROUNDED. REMOVED AND REPLACED THE DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,518 hrs · 47,209 cycles

FORWARD CARGO DOOR CUTOUT AFT FRAME IS CRACKED AT INBD STOP FITTING. ACFT GROUNDED. R & R DAMAGED FRAME IAW SRM 51-40-02-0G-0.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 70,518 hrs · 47,209 cycles

FORWARD CARGO DOOR CUTOUT AFT FRAME IS CRACKED AT INBOARD STOP FITTING. ACFT GROUNDED. REMOVED AND REPLACED DAMAGED FRAME IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 727E) · airframe 70,518 hrs · 47,209 cycles

FUSELAGE SKIN IS CRACKED AT CHEM-MILL BELOW STRINGER 23R, BS 727E +2. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01 REP 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,518 hrs · 47,209 cycles

FUSELAGE SKIN IS CRACKED AT CHEM-MILL BELOW STR 22L, STA 727E+3". REQUIRES INTERNAL NDT IAW FIGURE 4 OF GENERATING TASK CARD AFTER ACESSED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-2R-31 DET VII THIS IS A CATEGORY B REPAIR INITIAL THRESHOLD IS SET FOR 66,000 FLT CYCLES. REFER TO THE OPERATORS REPAIR ASSESSMENT PROGRAM FOR INTERVALS AND METHODS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,518 hrs · 47,209 cycles

FUSELAGE SKIN IS CRACKED AT CHEM-MILL, BELOW STR 23R, STA 727E +2". REQUIRES INTERNAL NDT IAW FIG 4 OF GENERATING TC AFTER ACCESSED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01, REP 31. THIS REPAIR IS A CAT B REPAIR WITH INSPECTION THRESHOLD OF 66,000 FLT CYCLES OR 12,000 FLT CYCLES AFTER REPAIR INSTALLATION. ACFT FLT CYCLES AT TIME OF REPAIR 47,209.

Part: SKIN — CRACKED (BS 727E) · airframe 70,518 hrs · 47,209 cycles

FUSELAGE SKIN IS CRACKED AT CHEM-MILL BELOW STRINGER 22L, BS 727E+3. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01-2R-31 DET VII.

Part: SUPPORT STRAP — CRACKED (FUSELAGE) · airframe 70,511 hrs · 47,205 cycles

FLOORBEAM SUPPORT STRAP IN ELECTRONIC EQUIPMENT BAY CRACKED AT FS 328 BL0. ACFT GROUNDED. R & R FLOORBEAM SUPPORT STRAP ON FS 328, BL0 IAW SRM 51-40-02-0E-0.

Part: SUPPORT STRAP — CRACKED (FUSELAGE) · airframe 70,511 hrs · 47,205 cycles

FLOORBEAM SUPPORT STRAP CRACKED IN ELECTRONICS EQUIPMENT BAY AT FS 328, RBL 33. ACFT GROUNDED. R & R FLOORBEAM SUPPORT STRAP ON FS 328, RBL 33 IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (BS 328) · airframe 70,511 hrs · 47,205 cycles

FLOORBEAM SUPPORT STRAP IN E&E BAY, CRACKED AT BS 328 BL 0. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT STRAP IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (BS 328) · airframe 70,511 hrs · 47,205 cycles

FLOORBEAM SUPPORT STRAP CRACKED IN E&E BAY AT BS 328 RBL 33. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT STRAP IAW SRM 51-40-02-0G-0.

Part: BOLT — CORRODED (MAIN CARGO DOOR) · airframe 70,372 hrs · 47,087 cycles

MAIN CARGO DOOR FITTING THAT HOLDS LOCK PINS, NR 6 POSITION MISSING HEAD, REMOVED 2 EA UPPER BOLTS AT NR 1 POSITION, 1 EA AT NR 6 POSITION FOUND HEAVY CORROSION TO HARDWARE. ACFT GROUNDED. ACCOMPLISHED RE-TORQUE ON BASE LATCH ASSEMBLIES IAW AMM 52-35-05, REQUIRED NEW HARDWARE ON BS 460-165, BS 400-24, BS 396-22. INSTALLED NEW HARDWARE ON LATCH BASES AT FUSELAGE BS 369, 2 AT 460, AND 400. REF AMM 52-35-05. ACFT RELEASED FOR THE FERRY FLIGHT, IAW FERRY PERMIT DATED 5-20-2016 TO ACCOMPLISH REPAIR TO MAIN CARGO DOOR. COMPLETED 400-52FCD-17144-1 MAIN CARGO DOOR LATCH BOLT INSPECTION.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 70,346 hrs · 47,063 cycles

F/A REPORTS THAT THE R1 SLIDE PRESSURE IS LOW. ACFT GROUNDED. REPLACED R1 SLIDE REF AMM 25-61-35.

Part: STIFFENER — CORRODED (BS 619) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

RIGHT LONGITUDINAL BEAM ANGLE ABOVE AFT HEAT EXCHANGER CUTOUT IS CORRODED AT BS 619. ACFT GROUNDED. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (DOOR FRAME) · airframe 68,143 hrs · 45,245 cycles

WHILE CLOSING FWD CARGO BAY, FOUND MAIN CARGO DOOR LOWER FRAME INNER SKIN STRAP AT BS 480 CRACKED. ACFT GROUNDED. R & R STRAP IAW SRM 51-40-02.

Part: WEB — CORRODED (BS 570-637) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFTER REMOVAL OF RT RAM AIR DUCT, FOUND CORROSION ON CENTER WING BOX RT SUPPORT BEAM WEB. ACFT GROUNDED. REPAIRED UNDERWING LONGITUDINAL BEAM, WEB BS 576-585 AND BS 637, RBL 40.875 IAW EA 400, 53EA 15279 AND 400, 53EA 15288, W 3, O .060, R .015, L 16.0, D .045.

Part: WEB — CORRODED (BS 570-637) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFTER REMOVAL OF RT RAM AIR DUCT FOUND CORROSION ON CENTER WING BOX RT SUPPORT BEAM WEB. ACFT GROUNDED. REPAIRED UNDERWING LONGITUDINAL BEAM WEB STA 576-585 AND 637, RBL 40.875 IAW EA'S 400, 53EA, 15279 AND 400, 53EA, 15288.

Part: LINK — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFTER REMOVING EXPANSION LINK TO REPLACE PIVOT FOUND EXFOLIATING CORROSION ON EXPANSION LINK AT LBL 24, BS 520. ACFT GROUNDED. REMOVED DAMAGED EXPANSION LINK AND REPLACED WITH NEW EXPANSION LINK IAW BSOPM 20-50-01 AND SRM 51-40-05-0G-0.

Part: LINK — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFTER REMOVING EXPANSION LINK TO REPLACE PIVOT, FOUND EXFOLIATING CORROSION ON EXPANSION LINK AT LBL 45, BS 520. ACFT GROUNDED. REMOVED DAMAGED EXPANSION LINK AND REPLACED WITH NEW EXPANSION LINK IAW BSOPM 20-50-01 AND SRM 51-40-05-0G-0.

Part: FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

RT INBD FLAP, EB RIB TORQUE TUBE FITTING HAS PITTING , DISCOVERED AFTER REMOVING TORQUE TUBE. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE ACCEPTABLE FOR CONTINUED SERVICE IAW SAS EA 400, 57EA, 15179, REV. NEW DATED 04JUN15. THIS IS A CATEGORY B REPAIR STAGE 1 REF, CMPT 57DTI, 15180, W 1", O .250, R .247, L .003, D 3".

Part: FLOORBEAM — CORRODED (BS 500C) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

BS 500C FLOORBEAM LOWER FLANGE IS CORRODED AT LBL 10. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-51-1A-1, REPAIRED IAW 53EA-15206.

Part: FLOORBEAM — CRACKED (BS 661) · airframe 68,143 hrs · 45,245 cycles

FLOORBEAM BS 661 BL 0 UPPER TEE IS CRACKED OUT OF FLOOR PANEL ATTACH HOLE AT . ACFT GROUNDED. REPAIRED THE FLOORBEAM IAW T/C AD20080421, 400-57-5, REV 0.

Part: SHEAR TIE — CORRODED (BS 887) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFT CARGO FRAME AT BS 887 BETWEEN STR 25 AND 26 RT HAS CORROSION. ACFT GROUNDED. CORROSION BEYOND LIMITS.

Part: FLOOR SUPPORT — CORRODED (BS 747) · airframe 68,143 hrs · 45,245 cycles

AFT CARGO FLOOR SUPPORT ANGLE JUST INBD OF STR 27LT IS CORRODED AT FS 747. ACFT GROUNDED. REPAIRED AFT CARGO FLOOR SUPPORT IAW SRM 53-00-53-2 R 1, REPAIR 1.

Part: RIB — CRACKED (RT WING) · airframe 68,143 hrs · 45,245 cycles

RIGHT WING RIB AT WBL 135 LOWER RIB CHORD BETWEEN STR 2 AND 3 IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO RT WING LWR RIB CHORD, WBL 135 IAW EA 400, 57EA 15246.

Part: RIB — CRACKED (LT WING) · airframe 68,143 hrs · 45,245 cycles

LT WING RIB AT WBL 135, LOWER RIB CHORD BETWEEN STR 2 AND 3 IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO LT WING LWR RIB CHORD, WBL 135 IAW EA 400, 57EA 15246.

Part: STRINGER — CORRODED (BS 1088-1138) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

APU TORQUE BOX INLET, LOWER STRINGER IS CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02-0G-0, W 1", O .065", R .055", L 12", D .010".

Part: FILLER — CORRODED (APU) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

APU TORQUE BOX INLET AFT FILLER IS CORRODED. ACFT GROUNDED. R & R FILLER IAW SRM 51-40-02, 0G 0.

Part: FILLER — CORRODED (APU) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

APU TORQUE BOX INLET FWD FILLER IS CORRODED. ACFT GROUNDED. R & R FILLER IAW SRM 51-40-02-0G.

Part: STRINGER — CORRODED (BS 1088-1156) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

APU TORQUE BOX INLET UPPER STRINGER IS CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02-0G-0-1 1.0, O .065, R .045, L 12, D .020.

Part: STIFFENER — CORRODED (BS 1112-1116) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

APU TORQUE BOX INLET FWD STIFFENER IS CORRODED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0, W 1.P, O .060, R .044, L 16.0, D .010.

Part: PIVOT — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

PIVOT LINK AT BS 520, RBL 45 IS CORRODED. ACFT GROUNDED. R & R PIVOT LINK IAW SRM 51-40-02-0G-0.

Part: PIVOT ASSY — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

PIVOT LINK AT BS 520, RBL 24 IS CORRODED. ACFT GROUNDED. R & R PIVOT LINK IAW SRM 51-40-02-0G-0.

Part: STIFFENER — CORRODED (BS 1122-1128) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

APU TORQUE BOX INLET AFT STIFFENER IS CORRODED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0.

Part: LINK — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

RBL 45 LONGITUDINAL FLOORBEAM EXPANSION LINK AT FS 520 IS EXFOLIATED. ACFT GROUNDED. R & R EXPANSION LINK IAW SOPM 20-50-01, W 1", O .110, R 0, L 1", D .110.

Part: TRANSITION PANEL — CORRODED (BS 727-727B) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFT CARGO BAY RT SIDE FROM BS 727 TO APPROXIMATELY BS 727C TRANSITION PANEL IS CORRODED SEVERAL AREAS. ACFT GROUNDED. R & R RT SIDE TRANSITION PANEL STA 727- BS 727B+10 IAW SRM 51-40-02-0G-0, W 2, O .040, R .030, L 23, D .010.

Part: FLOOR SUPPORT — CORRODED (BS 520-540) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

RBL 24, LONGITUDINAL FLOORBEAM EXPANSION LINK AT STA 520 IS EXFOLIATED. ACFT GROUNDED. R & R EXPANSION LINK IAW SOPM 20-50-01, W 1". O .110, R 0, L 1", D .110.

Part: TRANSITION PANEL — CORRODED (BS 727C-787) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFT CARGO PIT RT SIDE TRANSITION PANEL FROM APPROXIMATELY BS 727C - 787 IS CORRODED. ACFT GROUNDED. R & R RT SIDE TRANSITION PANEL IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 727-727A) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFT CARGO BAY BETWEEN BS 727 - 727A FLOOR SUPPORT CORRODED. ACFT GROUNDED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53-2R-1 REPAIR 1.

Part: TRANSITION PANEL — CORRODED (BS 727-727E) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

AFT CARGO BAY FROM BS 727 TO 727E, LEFT TRANSITION PANEL IS CORRODED. ACFT GROUNDED. R & R THE TRANSITION PANEL IAW SRM 51-40-02-0G-0.

Part: PIVOT — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

PIVOT LINK AT STA 520, LBL 45 IS EXFOLIATED. ACFT GROUNDED. REMOVED DAMAGED PIVOT LINK AND REPLACED WITH NEW PIVOT LINK IAW SRM 51-40-02-0G-0, W 1", O .100, R .000, L 3", D .100.

Part: PIVOT — CORRODED (BS 520) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

PIVOT LINK AT BS 520, LBL 24 IS EXFOLIATED. ACFT GROUNDED. REMOVED DAMAGED PIVOT LINK AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0.

Part: SEAT TRACK — CORRODED (BS 520-540) · corrosion level 2 · airframe 68,143 hrs · 45,245 cycles

SEAT TRACK RBL 24, BS 520 - 540 IS EXFOLIATED. ACFT GROUNDED. R & R SEAT TRACK IAW AMM 20-50-11-912-002.

Part: ATTACH FITTING — CRACKED (RT MLG SUPPORT) · airframe 68,143 hrs · 45,245 cycles

RIGHT MLG SUPPORT BEAM ATTACH FITTING IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. R & R ATTACH FITTING AND ACCOMPLISHED REPAIRS TO AFT SPAR IAW EA 400, 57EA 15257. THIS IS A CAT B REPAIR, REQUIRES DETAIL VISUAL INSPECTION AND HFEC AT NEXT C-CHECK OR 4,500 FLT. CYCLES, REPEAT INTERVAL AT EVERY C-CHECK OR 4,500 FLIGHT CYCLES WHICHEVER COMES FIRST. REFER TO DTI/EC 400 57DTI-15259. NOTE: ENTERED INTO AT TASK FOR CAT. B REPAIR.

Part: ATTACH FITTING — CRACKED (LT MLG) · airframe 68,143 hrs · 45,245 cycles

LEFT MLG SUPPORT BEAM ATTACH FITTING IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. INSPECTED LT MLG BEAM AFT SUPPORT FITTING IAW EA 400, 57EA 15116. CATEGORY C, REPAIR LT MLG BEAM AFT SUPPORT FITTING MUST BE R & R BEFORE ACFT 57,245 TOTAL FLIGHT CYCLES REFER TO EA 400, 57EA, 15117 AND T/C 400, 57EA, 15117-1 FOR FITTING REMOVAL AND REPLACEMENT.

Part: ANGLE — CRACKED (BS 440) · airframe 68,143 hrs · 45,245 cycles

FWD CARGO DOOR CUTOUT FWD FRAME REINFORCEMENT ANGLE IS CRACKED AT STR 25R. ACFT GROUNDED. R & R SHEAR WEB IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 947) · airframe 68,143 hrs · 45,245 cycles

SKIN HAS A 1.25" CRACK ON THE LT SIDE AT BS 943, DIRECTLY ABOVE S24L AT CHEM MILL. ACFT GROUNDED. REPAIRED IAW EA AD20092101 400-53-104.

Part: STRAP — CRACKED (BS 305) · airframe 68,143 hrs · 45,245 cycles

FLOORBEAM SUPPORT STRAP AT RBL 45 IS CRACKED. ACFT GROUNDED. R & R STRAP IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 951-974) · airframe 67,259 hrs · 44,527 cycles

A CRACK FOUND PROTRUDING FROM THE R2 DOOR THRESHOLD BELOW THE LOWER FWD CORNER OF THE DOOR CUTOUT. ACFT GROUNDED. REPAIRED SKIN IAW EA 400-53, EA-14073. CATEGORY B REPAIR.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 66,715 hrs · 44,079 cycles

STRINGER CLIP AT S4R BS 727C IS CRACKED. ACFT GROUNDED. R & R THE STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 460) · airframe 66,715 hrs · 44,079 cycles

STRINGER CLIP CRACKED AT BS 480 S10R. ACFT GROUNDED. R & R THE STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 500E) · airframe 66,715 hrs · 44,079 cycles

STRINGER CLIP 10R CRACKED AT BS 500E. ACFT GROUNDED. R & R DAMAGED STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 950) · airframe 65,376 hrs · 42,909 cycles

FOUND FUSELAGE SKIN CRACKED FWD OF L2 DOOR AT LOWER CORNER FUSELAGE BS 950 AT S17L. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-1-2R-32, DETAIL IV.

Part: STIFFENER — CORRODED (BS 277.5) · corrosion level 2 · airframe 64,895 hrs · 42,511 cycles

LOWER NOSE COMPARTMENT VERTICAL STIFFENER CORRODED AT BS 227.5 FWD SIDE OF BULKHEAD BL 0. ACFT GROUNDED. REMOVED CORRODED STIFFENER, FABRICATED, AND INSTALLED NEW STIFFNER IAW DWG 65-45801 AND SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 925-927) · corrosion level 2 · airframe 64,895 hrs · 42,511 cycles

AFTER REMOVAL OF THE AFT CARGO BALLAST, THE AFT CARGO TRACK AT RBL 17.2 FOUND CORRODED. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 64,895 hrs · 42,511 cycles

CRACK AT LOWER LIGHTNING HOLE ON BOTTOM EDGE. BLENDED CRACK ON R2 DOOR LOWER LIGHTNING HOLE, FOUND TO BE OUT OF LIMITS, REPAIRED LIGHTNING HOLE IAW SRM 51-70-13-0G-0.

Part: SKIN — CHAFED (NR 2 SLAT) · airframe 64,895 hrs · 42,511 cycles

NR 2 SLAT INNER SURFACE CHAFED AT INBD END. ACFT GROUNDED. REPAIRED NR 2 SLAT IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CRACKED (BS 520-540) · airframe 64,895 hrs · 42,511 cycles

LEFT LOWER FUSELAGE EXTERNAL FWD A/C BAY GROUND SERVICE ACCESS DOOR CUTOUT FAIRING INBD SIDE SKIN IS BENT. ACFT GROUNDED. REMOVED DAMAGE IAW SRM 53-00-01-1A-1. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1. FABRICATED -1, DOUBLER, -4 FILLERS, -5 TAPERED SHIMS AND INSTALLED REPAIR PARTS IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH AN INTERVAL OF 4,500 CYCLES THRESHOLD OF 60,000 CYCLES. CURRENT CYCLES AT TIME OF REPAIR 42,511.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 64,895 hrs · 42,511 cycles

NR 4 SLAT UPPER SURFACE HAS EVIDENCE OF DELAMINATION. REPAIRED SLAT IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: DOOR FRAME — CRACKED (BS 440) · airframe 64,895 hrs · 42,511 cycles

FWD CARGO DOOR FORWARD FRAME IS CRACKED AT LOWER STOP FITTING, ACFT GROUNDED. R & R FWD CARGO DOOR CUT OUT FWD FRAME IAW SRM 51-40-02-0G-0-PAR-7D.

Part: DOUBLER — GOUGED (BS 230-232) · airframe 64,895 hrs · 42,511 cycles

RIGHT FUSELAGE EXTERNAL POWER DOOR CUTOUT IS GOUGED AT LOWER LAND. AREA REPAIRED IAW EA 400-53EA.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 64,895 hrs · 42,511 cycles

NR 4 SLAT OTBD LOWER CORNER HAS EVIDENCE OF DELAMINATION. REPAIRED NR 4 SLAT OTBD LOWER CORNER IAW SRM 51-70-10-2R 2 PARA. D

Part: TEE FITTING — CORRODED (BS 540-663) · corrosion level 2 · airframe 64,895 hrs · 42,511 cycles

LEFT ACFT BAY DOOR INBD LANDING TEE FITTING IS CORRODED SEVERAL PLACES FRONT TO BACK. R & R TEE FITTING IAW SRM 51-40-02-0G-0.

Part: SLIDE — NO TEST (L2 DOOR) · airframe 64,895 hrs · 42,511 cycles

L2 DOOR SLIDE FAILED DEPLOYMENT TEST. TWO INTEGRAL LIGHTS FAILED TO ILLUMINATE. ACFT GROUNDED. SLIDE REPLACED ON T/C 61621-469 PNC.

Part: DOOR — OUT OF ADJUST (L2) · airframe 64,515 hrs · 42,212 cycles

L2 DOOR STICKS WHILE OPENING AND CLOSING. ACFT GROUNDED. ADJUSTED DOOR IAW 52-13-00. OPS CHECKED GOOD.

Part: SNUBBER — FAILED (L2 DOOR) · airframe 62,269 hrs · 40,235 cycles

F/A REPORTS THAT THE L2 DOOR IS DIFFICULT TO OPEN FROM THE INSIDE. REPLACED DOOR L-2 SNUBBER, OPS CHECKED GOOD 52-13-71-004-020, PGS 1 AND 2, 52-13-71-404-022, PGS 1-3.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 61,927 hrs · 39,953 cycles

R2 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK ON POWER SUPPLY M01137 R2 DOOR OVERHEAD EMERGENCY LIGHT OPS CHECKS GOOD IAW MM 33-51-51-962-015.

Part: SKIN — DELAMINATED (NR 4 SPOILER) · airframe 61,927 hrs · 39,953 cycles

NR 4 SPOILER DELAMINATED ON UPPER SIDE. REPAIRED SPOILER IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 61,927 hrs · 39,953 cycles

NR 1 SLAT OTBD LOWER SURFACE DELAMINATED. REPAIRED IAW SRM 51-70-10.

Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 61,927 hrs · 39,953 cycles

NR 1 SLAT OTBD UPPER AFT CORNER DELAMINATED. REPAIRED NR1 SLAT OTBD UPPER SURFACE IAW SRM 51 20 10, REP 4.

Part: SKIN — DELAMINATED (NR 4 SPOILER) · airframe 61,927 hrs · 39,953 cycles

NR 4 SPOILER DELAMINATION ON UPPER SIDE. ACFT GROUNDED. REPAIRED NR 4 SPOILER IAW SRM 51 70 10, REP 4.

Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 61,927 hrs · 39,953 cycles

NR 1 SLAT INBD UPPER AFT CORNER DELAMINATED. REPAIRED NR 1 SLAT IAW SRM 51 70 10, REPAIR 4 PARA 20, PG 254.

Part: FRAME — CRACKED (BS 520) · airframe 61,927 hrs · 39,953 cycles

RIGHT FRAME BS 520 HAS A CRACK AT THE ONE WIRE FEED THRU HOLE APPROXIMATELY .3750 LONG, REPAIRED RT FRAME IAW SRM 53 00 07, REPAIR 13 DETAIL.

Part: SKIN — CRACKED (BS 727D) · airframe 61,927 hrs · 39,953 cycles

AFT FUSELAGE SKIN HAS A CRACK AT THE CHEM MILL AREA AFT SIDE. NOT OPEN TO THE OUTSIDE SURFACE, DETECTED WITH MFEC .2500 BELOW STRINGER 23R BS 727D APPROX .5 LONG. REPAIRED SKIN IAW SRM 53 00 01, FIG 201, REP 31.

Part: REVEAL — CORRODED (BS 787-794.4) · corrosion level 2 · airframe 61,927 hrs · 39,953 cycles

AFT CARGO BAY LOWER FWD REVEAL HAS CORROSION. FABRICATED NEW REVEAL IAW SRM 51 30 01, FIG 7.

Part: SKIN — CRACKED (L1 DOOR) · airframe 68,775 hrs · 37,196 cycles

L1 DOOR ASSEMBLY FOUND THE FORWARD LOWER TORQUE TUBE ACCESS HOLE CRACKED. REPAIRED L1 DOOR INNER SKIN IAW EA 400 52EA 06146 REV NEW ISSUED 8/23/2011.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,775 hrs · 37,196 cycles

AFT PRESSURE BULKHEAD FWD SIDE LOWER WEB CORRODED STA 1016 LBL 4.0. REPAIRED APB LOWER WEB IAW ASA EA 400 53EA 06114.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

CRACK INDICATION AT FUS STATION 727D STR 23L ON MFEC. INSPECTION OF SKIN SUBSURFACE EDGES REF NDTM PART 6 53 30 09. REPAIRED CRACKED SKIN IAW B737 400 SRM 53 00 01 REPAIR 31 DETAIL 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

FRAME 440 CRACKED AT FORMER AC BRACKET ATTACHMENT HOLE. REPAIRED FRAM IAW ASA EA 14486 AND ASA DWG A5310025688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

RT FRAME 500A CRACKED AT FORMER AC BRACKET ATTACHMENT HOLE. REPAIRED FRAM IAW ASA EA AD 2006 2609 400 52 122 AND ASA DWG A5310025688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

RT FRAME 400 CRACKED AT FORMER ATTACHMENT HOLE FOR AC BRACKET. REPAIRED FRAME IAW ASA EA AD 2006 2609 400 53 122 AND ASA DWG 5310025688.

Part: SKIN — CHAFED (TE FLAP) · airframe 58,775 hrs · 37,196 cycles

RT WING OUTBD FORE FLAP INBD END L/E CHAFED.REMOVED DAMAGED DOUBLER FABRICATED AND INSTALLED NEW DOUBLER IAW B737 400 SRM 57 53 01 FIG 201 SRM REQUIRED BLIND FASTENER INSPECTION AT EVERY "C" CHECK INTERVALS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

LT FRAME 500D CRACKED AT FORMER AC BRACKET ATTACHMENT HOLE. REPAIRED FRAME IAW ASA EA AD 2006 2609 400 53 122 AND ASA DWG A5310025688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

LT FRAME 520 CRACKED AT FORMER A/C BRACKET ATTACHMENT HOLE. REPAIRED FRAME IAW ASA EA 20062609 400 53 122 AND ASA DWG A5310052688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

FRAME 500C CRACKED AT LT FORMER AC BRACKET ATTACHEMENT HOLE. REPAIRED FRAME IAW ASA EA AD 2006 2609 400 53 122 AND ASA DWG A531025688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,775 hrs · 37,196 cycles

RT FRAME 480 CRACKED AT FORMER AC BRACKET ATTACHMENT HOLE. REPAIRED FRAME IAW ASA EA AD 2006 2609 400 53 122 AND ASA DWG A5310025688.

Part: SHUTOFF VALVE — OUT OF POSITION (FUEL SYSTEM) · airframe 58,363 hrs · 36,831 cycles

CLIMBING OUT THRU 14 000 NR 2 ENG EXPERIENCED A PARTIAL POWER LOSS N1'S 94 / 79 EGT 820 / 644 N2'S 95.4 / 78.0 FFS 6.50 / 3.7. ON APPROACH WHEN POWER LEVERS ADVANCED NR 2 ONLY ACHIEVED 25 TO 30 PERCENT OF NORMAL POWER. NO SURGING. NO THRUST LEVER MOVEMENTS WHILE AUTO THROTTLE STILL ENGAGED. P63 D3 SHUTOFF VALVE NR 2 WAS FOUND OUT. IN WORK.

Part: SKIN — DENTED (HORIZ STAB) · airframe 57,298 hrs · 35,888 cycles

DENT ON RT FIXED STAB LE APPROX 12.5 INCHES FROM FUSELAGE. DENT IS OUT OF LIMITS PER SRM 55 10 01. DENT REPAIRED AS PER ASA EA 400 55EA 04576 STEPS 1 & 2.

Part: SNUBBER — WORN (ENTRY DOOR) · airframe 57,278 hrs · 35,874 cycles

AFT ENTRY DOOR (L2) VERY DIFFICULT TO CLOSE, REPORT BY F/A. REPLACED WORN SNUBBER IAW B737 400 MM 52 13 71.

Part: REVEAL — CORRODED (BS 787-794.4) · corrosion level 2 · airframe 61,927 hrs · 39,953 cycles

AFT CARGO BAY LOWER FWD REVEAL HAS CORROSION. FABRICATED NEW REVEAL IAW SRM 51 30 01, FIG 7, W1O .032 L 1 REMAINING .028 DEPTH .004.

Part: BRACKET — BENT (ELEVATOR TAB) · airframe 56,283 hrs · 34,974 cycles

RT ELEVATOR TAB MECHANISM I/B ATTACH POINT BRACKET BENT. REMOVED AND REPLACED BRACKET.

Part: CONTROL ROD — OUT OF ADJUST (L1 DOOR) · airframe 55,838 hrs · 34,580 cycles

L1 DOOR HARD TO CLOSE. ADJUSTED UPPER AND LOWER LATCH ROLLER CONTROL RODS AND LOWER GATE CONTROL ROD. REF AMM 52 11 00 705 007.

Part: ROD END — OUT OF ADJUST (L2 DOOR) · airframe 55,838 hrs · 34,580 cycles

L2 DOOR DOES NOT CLOSE PROPERLY UPPER FWD LATCH ROLLER DOES NOT ENGAGE PLATE UNLESS DOOR IS PUSHED UP. ADJUSTED L2 DOOR HANDLE MECHANISM ROD END REF AMM 52 13 00 705 001, OPERATIONAL CHECKED NORMAL REF AMM 52 13 00 705 034.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

A CLUSTER OF 3 DENTS AND 6 PROTRUDING DENTS AT 913 JUST ABOVE REPAIR DOUBLER. REPAIRED FUSELAGE SKIN.

Part: SKIN — DENTED (TE FLAP) · airframe 55,828 hrs · 34,576 cycles

LT INBOARD FORE FLAP LOWER SURFACE HAS MULTIPLE MINOR DENTS BETWEEN INBOARD AND CNT TRACKS. REMOVED DAMAGED AREA AND BONDED REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

LEFT I/B TRAILING EDGE AFT FLAP CLUSTER OF DENTS ON UPPER SURFACE. REMOVED DAMAGED SKIN SECTION, FABRICATED FILLER AND DOUBLER AND BONDED.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FUSE LT EXTERIOR SKIN DENTED OUT OF LIMITS. REMOVED DAMAGED SKIN SECTION, FABRICATED SKIN BONDED DOUBLER AND INSTALLED.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 55,828 hrs · 34,576 cycles

LT INBOARD AFT FLAP LOWER SURFACE HAS AREAS OF DELAMINATION. REMOVED DAMAGE AND BONDED REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

LT FUSELAGE EXTERNAL SKIN DENTED APPROX STA 490 BELOW STR L16. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, FILLER AND INSTALLED.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT LT SHEAR TIE HAS 2 CREASES. REMOVED WEB FABRICATED AND INSTALLED NEW WEB.

Part: WEB — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

WEB AT LBL 55 AT STA 966 CORRODED. REMOVED WEB FABRICATED AND INSTALLED NEW WEB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

A .900 INCH CRACK EMANATING FROM LOWER HINGE CUTOUT ON FWD GALLEY SERVICE DOOR. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER.

Part: SPAR — DELAMINATED (RUDDER) · airframe 55,828 hrs · 34,576 cycles

RUDDER FRONT IS DELAMINATED AT RUDDER STA 17.25. CUT OUT DAMAGED AREA AND BONDED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FRAME CRACKED AT STA 500C. REMOVED DAMAGE AND INSTALLED NEW FRAME REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FRAME CRACKED AT STA 500C BETWEEN 8L & 9L. REMOVED RIVET PLUGS AND CUTOUT DAMAGE INSTALLED FRAME REPAIR.

Part: WEB — DAMAGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

CABIN FLOOR WEB DAMAGED FASTENER HOLES AFT OF FLOORBEAM. REMOVED DAMAGE AREA, INSTALLED NEW WEB.

Part: WEB — DAMAGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

CABIN FLOOR WEB DAMAGED FASTENER HOLES AFT OF FLOORBEAM. REMOVED DAMAGE AREA, INSTALLED NEW WEB.

Part: SILL — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

R2 THRESHOLD MOP SEAL HAS SEVERAL AREAS OF CORROSION. REMOVED MOP SILL AND INSTALLED NEW MOP SILL.

Part: SILL — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

CABIN FLOOR STR RT STA 500 ON MOP SILL. REMOVED AND INSTALLED NEW MOP SILL.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,828 hrs · 34,576 cycles

AFT PIT SHEAR TIE STA 727G CORRODED. REMOVED SHEAR TIE FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CABIN FLOORBEAM STA 967 HAS AREA OF CORROSION. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FLOORBEAM REPAIR.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 55,828 hrs · 34,576 cycles

AFT PIT FLOOR SUPPORT CORRODED AT JOGGLE RBL 3 STA 727. CUTOUT DAMAGED AREA FABRICATED AND INSTALLED JOGGLE REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT PIT FLOOR SUPPORT CORRODED STA 860 CUTOUT DAMAGED AREA FABRICATED AND INSTALLED JOGGLE REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FLOOR SUPPORT CORRODED AT RBL 3 STA 727 O. CUTOUT DAMAGED AREA FABRICATED AND INSTALLED JOGGLE REPAIR.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 55,828 hrs · 34,576 cycles

AFT PIT FLOOR SUPPORT CORRODED AT JOGGLE BETWEEN STA 727D CUTOUT DAMAGED AREA FABRICATED AND INSTALLED JOGGLE REPAIR.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 55,828 hrs · 34,576 cycles

AFT PIT FLOOR SUPPORT CORRODED AT LBL 8 JOGGLE. CUTOUT DAMAGED AREA FABRICATED A AND INSTALLED JOGGLE REPAIR.

Part: SKIN — GOUGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

GOUGE IN FUSELAGE SKIN. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED FWD SIDE OF FS 807. INSTALLED REPAIR ANGLE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,828 hrs · 34,576 cycles

APU COMPARTMENT RT STRINGER ABOVE AIRNET CUTOUT IS CORRODED. REMOVED AND REPLACED STRINGER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,828 hrs · 34,576 cycles

CABIN FLOORBEAM CORRODED AROUND FASTENER HOLES AT PREVIOUS REPAIR. REMOVED EXISTING UPPER T-CHORD REPAIR, INSTALLED NEW CHORD AND REPAIR PARTS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

CABIN FLOOR T-CHORD UNDER O/B LEFT SEAT TRACK CRACKED AT FASTENER HOLE. CUT OUT DAMAGED AREA, INSTALLED REPAIR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CARGO PIT INTERCOSTAL SUPPORT BRACKET CORRODED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW.

Part: SKIN — DENTED (TE FLAP) · airframe 55,828 hrs · 34,576 cycles

LEFT I/B AFT FLAP L/E IS DENTED 24 INCHES IN O/B OF I/B END. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CARGO PIT FRAME CORRODED. REMOVED DAMAGE AREA INSTALLED REPAIR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT PIT INTERCOSTAL CORRODED STA 767. REMOVED DAMAGE INTERCOSTAL INSTALLED NEW.

Part: SILL — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

L2 ENTRY DOOR MOP SILL HAS CORROSION. INSTALLED NEW MOP SILL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

INTERCOSTAL STA 288 IS CRACKED. REMOVED INTERCOSTAL FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: FRAME — GOUGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

CABIN FRAME GOUGED. REMOVED DAMAGE AREA, INSTALLED REPAIR.

Part: FRAME — CHAFED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FRAME AT STA 559 IS CHAFED. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,828 hrs · 34,576 cycles

FWD CARGO COMPARTMENT SHEAR TIE IS CORRODED O/B OF STR 26R. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED.

Part: SKIN — CHAFED (FOREFLAP) · airframe 55,828 hrs · 34,576 cycles

RIGHT O/B FOREFLAP LOWER LEADING SKIN IS CHAFED 6 IN FROM I/B END. REMOVED EXISTING REPAIR DOUBLER, FABRICATED NEW DOUBLER AND INSTALLED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

CABIN FRAME GOUGED. REMOVED DAMAGE AREA, INSTALLED REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

SCRIBE LINE AT STR 20L. FABRICATED REPAIR PARTS AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 727D FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CABIN RT CUSP WEB IS CORRODED. REMOVED AND REPLACED CUSP WEB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

STA 747 FRAME IS CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

STA 787 FRAME IS CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

STA 727F FRAME IS CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 867 FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FWD CARGO COMPARTMENT STRINGER 22L IS GOUGED. REPAIRED STRINGER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 747 FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FRAME AT STA 907 IS CRACKED. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 727B FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FRAME AT STA 867 IS CRACKED. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 907 FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CABIN FLOORBEAMS HAS CORROSION IN SEVERAL PLACES. REMOVED DAMAGED AREA INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

STA 727D FRAME IS CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FRAME AT STA 727B IS CRACKED. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 727F FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 827 FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

FS 787 FRAME IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

AFT CARGO COMPT FAIL SAFE ON FRAME FS 747 CORRODED. INSTALLED REPAIR ANGLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,828 hrs · 34,576 cycles

STA 827 FRAME IS CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIR.

Part: SKIN — DENTED (HORIZ STAB) · airframe 55,828 hrs · 34,576 cycles

LEFT HORIZ STAB L/E DENTED OUT OF LIMITS. REMOVED DAMAGED AREA, INSTALLED NEW SECTION.

Part: SKIN — CHAFED (MIDFLAP) · airframe 55,828 hrs · 34,576 cycles

LEFT O/B MIDFLAP RUB STRIP WORN THROUGH JUST O/B OF I/B CARRIAGE FITTING. REMOVED DAMAGED SKIN AND INSTALLED REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 55,828 hrs · 34,576 cycles

NR 4 SLAT T/E WEDGE I/B END IS DAMAGED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS FILLER AND DOUBLER AND BONDED.

Part: SKIN PANEL — DAMAGED (SPOILER) · airframe 55,828 hrs · 34,576 cycles

RT WING NR 7 SPOILER PANEL LOWER SURFACE HAS CREASE AT I/B CORNER. REMOVED DAMAGED AREA, INSTALLED REPAIR PARTS.

Part: SKIN — DENTED (FOREFLAP) · airframe 55,828 hrs · 34,576 cycles

LEFT I/B AFT FORE FLAP LOWER SURFACE REPAIR DOUBLER DENTED. REMOVED DAMAGED DOUBLER, INSTALLED NEW.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 54,842 hrs · 33,699 cycles

L1 DOOR EXTREMELY DIFFICULT TO LATCH CLOSED. ADJUSTED GUIDE ARM AND PERFORMED FWD ENTRY DOOR OPS TEST FOUND TO BE WITHIN LIMITS REF MM 52 11 00 705 060 AND MM 52 11 00 705 007.

Part: FASTENER — LOOSE (CARGO BAY) · airframe 52,967 hrs · 32,029 cycles

FWD CARGO PIT BLOW OUT PANEL NOT SECURED. REPLACED BUTTON HEAD FASTENERS WITH FLUSH RIVETS AND STRAP PER ASA EA 400 53EA 00501 AND ASA EA 400 53A 00973.

Part: STRAP — DAMAGED (CARGO BAY) · airframe 52,967 hrs · 32,029 cycles

AFT CARGO STRAP HAS ELONGATED HOLES. INSTALLED NEW STRAP PER SRM 51 40 02.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 52,967 hrs · 32,029 cycles

CARGO DOOR THRESHOLD STRAP FRAME BS 767+15 TO BS 794+9 RBL 20 WL 156 THAT GOES UNDER BOTH WEBS HAS EXISTING ELONGATED HOLE. REMOVED AND REPLACED STRAP PER SRM 51 40 02 AND 51 40 05.

Part: SUPPORT ANGLE — CRACKED (E&E BAY) · airframe 52,967 hrs · 32,029 cycles

E1 2 EQUIPMENT SHELF RT SUPPORT ANGLE CRACKED. REMOVED AND REPLACED PER ER 09 2053 ASA EA 400 25EA 00939.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,967 hrs · 3,029 cycles

AFT CARGO VERTICAL WEB BS 847 867 STR 25R HAS CORROSION. REPLACED WEB PER SRM 53 60 15 AND SRM 51 40 02.

Part: FUSE — BLOWN (CABIN) · airframe 52,967 hrs · 32,029 cycles

L1 EMERGENCY EXIT SIGN OVER THE DOOR IS INOP. REMOVED AND REPLACED FUSE IN EMERGENCY BATTERY PACK POWER SUPPLY.

Part: SKIN — CHAFED (LE SLAT) · airframe 52,967 hrs · 32,029 cycles

NR 4 SLAT CHAFED ON THE INNER UPPER SURFACE T/E WEDGE. REMOVED PREVIOUS REPAIR AT I/B END. INSTALLED NEW DOUBLER AND REPAIRED PER ER 09 2016 ASA EA 400 57EA 0096.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,967 hrs · 32,029 cycles

FLOOR SUPPORT IS CORRODED STA 847 867. REMOVED AND REPLACED SUPPORT PER SRM 51 40 02.

Part: RIB — DAMAGED (LE SLAT) · airframe 52,967 hrs · 32,029 cycles

INBOARD AND OUTBOARD ACTUATOR ATTACH RIBS DAMAGED AT NR 4 SLAT AND LOWER T-CHORD DAMAGED. REPAIRED INBOARD AND OUTBOARD NR 4 SLAT ACTUATOR RIBS AND REPLACED LOWER T-CHORD PER SRM 57 43 03 PG 106 SRM 51 20 00 AND DWG 65C26603.

Part: TEE FITTING — DAMAGED (LE SLAT) · airframe 52,967 hrs · 32,029 cycles

NR 4 SLAT LOWER T-CHORD DAMAGED AT PCU ATTACH POINT. REPLACED T-CHORD PER SRM 51 40 05, SRM 51 30 01 AND DWG 65C26603.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 52,967 hrs · 32,029 cycles

CHANNEL CRACKED BS 794 STR 17 RT. REPLACED CHANNEL PER SRM 51 30 01 & SRM 51 40 02.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 52,967 hrs · 32,029 cycles

FRAME STRAP BS 794 STR 16 26R HAS ELONGATED HOLES. REPLACED FRAME STRAP PER SRM 51 40 02.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 52,967 hrs · 32,029 cycles

DURING BS 794 RT FRAME REPLACEMENT FOUND WEB MECHANICAL DAMAGE BS 794 STR 16R. REPLACED WEB PER SRM 53 60 15 DETAIL VI SRM 51 40 05 AND DWG 65 47962.

Part: DOOR FRAME — CHAFED (ENTRY DOOR) · airframe 52,966 hrs · 32,029 cycles

FWD ENTRY DOOR UPPER AFT CORNER OF DOOR SIDE FRAME CHAFED BY UPPER AFT DOOR STOP FTG. REPAIRED PER ER 09 1862 AND EA NUMBER 400 52EA 00931.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

CLOSE OUT WEB CRACKED. REPAIRED WEB IAW SRM 51-70-13.

Part: SKIN PANEL — GOUGED (RT PYLON) · airframe 52,966 hrs · 32,029 cycles

RT ENGINE PYLON PANEL 5827B CUTOUT INNER SURFACE ON MOUNTING FLANGE GOUGED. REPAIRED PER EA 400 54EA 00912.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION AFT CARGO DOOR CUTOUT ON INNER SURFACE OF BEAR STRAP. REMOVED EXISTING DOUBLER AND TRIPLER, FABRICATED NEW REPAIR PARTS AND INSTALLED PER EA-400-53EA-00980.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FWD ENTRY DOOR AFT LOWER WEB ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE.

Part: SKIN — DENTED (HORIZ STAB) · airframe 52,966 hrs · 32,029 cycles

LT HORIZONTAL STAB L/E DENTED OUT OF LIMITS. REPAIRED LT HORIZONTAL STAB L/E PANEL AT THE 10TH RIB FROM THE O/B END.

Part: SKIN — CHAFED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FUSELAGE SKIN WORN WHERE DORSAL FIN CONTACTS. REPAIRED PER SRM 53-60-01.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FAIRING SUPPORT ANGLE CRACKED STA 540 LBL 20. REMOVED AND REPLACED FAIRING SUPPORT ANGLE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 767 787 RBL 20. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SKIN — WORN (TE FLAP) · airframe 52,966 hrs · 32,029 cycles

LEFT I/B EXHAUST GATE UPPER SKIN IS WORN BEYOND REPAIR. REMOVED AND REPLACED LEFT I/B EXHAUST GATE UPPER SKIN PER SRM 51 40 02.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 52,966 hrs · 32,029 cycles

NR 5 SLAT DISBONDED AT I/B UPPER OUTER CORNER. REPAIRED DISBOND AT I/B UPPER OUTER CORNER OF NR 5 SLAT.

Part: WEDGE — CHAFED (LE SLAT) · airframe 52,966 hrs · 32,029 cycles

NR 5 SLAT CHAFED ON THE INNER UPPER I/B CORNER I/B MAIN TRACK AND O/B MAIN TRACK. REPAIRED CHAFING ON INNER UPPER I/B CORNER I/B MAIN TRACK AND O/B MAIN TRACK ON T/E WEDGE OF NR 5 SLAT.

Part: SKIN — CHAFED (FOREFLAP) · airframe 52,966 hrs · 32,029 cycles

RIGHT O/B FORE FLAP LWD LEADING EDGE SKIN IS CHAFED 6 INCHES FROM I/B END. REPAIRED FORE FLAP.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 52,966 hrs · 32,029 cycles

NR 5 SLAT DISBONDED AT O/B UPPER OUTER CORNER. REPAIRED DISBOND AT UPPER OUTER CORNER OF NR 5 SLAT.

Part: SKIN — CHAFED (RT WING) · airframe 52,966 hrs · 32,029 cycles

RIGHT O/B WING L/E IS CHAFED AT NR 4 SLAT I/B TRACK CUTOUT O/B SIDE. REPAIRED CHAFING DAMAGE ON RT WING FIXED L/E NR 4 SLAT I/B TRACK CUTOUT O/B SIDE.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,966 hrs · 32,029 cycles

NR 6 SLAT UPPER SURFACE I/B END HAS AREA OF DELAMINATION. REPAIRED DELAMINATION ON UPPER SURFACE ON I/ END OF THE NR 6 SLAT.

Part: WEDGE — CHAFED (LE SLAT) · airframe 52,966 hrs · 32,029 cycles

NR 2 SLAT CHAFED AT T/E WEDGE I/B END. REPAIRED CHAFE ON I/B END OF T/E WEDGE ON NR 2 SLAT IAW B737 400 SRM 51 70 10.

Part: SUPPORT BRACKET — GOUGED (FUSELAGE) · airframe 52,967 hrs · 32,029 cycles

AFT CARGO BAY THRESHOLD SUPPORT BRACKET LOCATED AT BS 817 WL 159 RBL 25 IS GOUGED. REMOVED AND REPLACED PER SRM 51 30 01 AND 51 40 02.

Part: SKIN — CHAFED (RT WING) · airframe 52,966 hrs · 32,029 cycles

RIGHT O/B WING LEADING EDGE IS CHAFED AT NR 4 SLAT I/B TRACK CUTOUT O/B SIDE. REPAIRED CHAFING DAMAGE ON RIGHT O/B WING LEADING EDGE AT NR 4 SLAT I/B TRACK CUTOUT O/B SIDE.

Part: SKIN — CHAFED (RT WING) · airframe 52,966 hrs · 32,029 cycles

RIGHT O/B WING LEADING EDGE O/B OF PYLON HAS CHAFE MARKS. REPAIRED SKIN.

Part: SKIN — DENTED (STABILIZER) · airframe 52,966 hrs · 32,029 cycles

RT STABILIZER LEADING EDGE HAS DENT. REPAIRED RT STABILIZER LEADING EDGE DENT.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

MISDRILLED HOLE IN UPPER WEB ANGLE ONLY THAT ATTACHES TO SEAT TRACK AT BS 500G 520 LBL 45 WL 208. REMOVED AND REPLACED ANGLE.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

BS 520 FLOORBEAM FWD VERTICAL STIFFENER IS GOUGED LBL 45 WL 207 201. REMOVED AND REPLACED TEE STIFFENER BS 520 LBL 45 WL 207 201.

Part: SKIN — CHAFED (RT WING) · airframe 52,966 hrs · 32,029 cycles

RIGHT O/B WING L/E JUST O/B OF PYLON HAS CHAFE MARKS. REPAIRED RT WING.

Part: INTERCOSTAL — CRACKED (BS 301) · airframe 52,966 hrs · 32,029 cycles

CRACK IN INTERCOSTAL ANGLE. REMOVED AND REPLACED INTERCOSTAL ANGLE.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FOUND FLOOR STABILIZER CRACKED STA 314 LBL 13. REPAIRED FLOOR STABILIZER STA 314 LBL 13.

Part: SKIN PANEL — GOUGED (LT PYLON) · airframe 52,966 hrs · 32,029 cycles

LT PYLON PANEL 5729L CUTOUT AFT EDGE HAS MECH DAMAGE. REPAIRED PER EA 400-54EA-00913.

Part: STOP FITTING — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FWD CARGO DOOR 2ND STOP FITTING FROM TOP DOWN FWD SIDE IS GOUGED. REMOVED AND REPLACED STOP FITTING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FOUND FLOOR STABILIZER CRACKED STA 314 RBL 30 WL 200. REPAIRED FLOOR STABILIZER STRAP STA 314 RBL 30 WL 200 IAW SRM 53 10 51.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

FOUND FLOOR STABILIZER CRACKED STA 314 BL 0 WL 200. REPAIRED FLOOR STABILIZER STRAP STA 314 BL 0 WL 200 IAW SRM 53 10 51.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

AFT CARGO BAY FWD BULKHEAD CENTER LWR SUPPORT ANGLE CORRODED. REPLACED ANGLE AT AFT CARGO BAY FWD BULKHEAD CENTER LWR SUPPORT.

Part: SKIN — GOUGED (FOREFLAP) · airframe 52,966 hrs · 32,029 cycles

LEFT O/B FORE FLAP CENTER OF LEADING EDGE SKIN IS GOUGED 6 INCHES FROM I/B. LEFT O/B FORE FLAP REPAIRED GOUGE 6 INCHES FROM I/B ON LEADING EDGE.

Part: PANEL — CRACKED (LT PYLON) · airframe 52,966 hrs · 32,029 cycles

LT PYLON PANEL 5727L CUTOUT CRACKED. REPAIRED PER ER 09-1861 AND ASA EA 400-54EA-00915.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

OVERSIZED HOLES IN INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL.

Part: SKIN — GOUGED (MAIN CARGO DOOR) · airframe 52,966 hrs · 32,029 cycles

MAIN CARGO DOOR EXTERIOR SURFACE GOUGED ABOVE LATCH RELEASE LEVER. REPAIRED PER EA 400-52EA-00882.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

CORROSION OF BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE BS 947 LBL 17.

Part: SKIN — WORN (TE FLAP) · airframe 52,966 hrs · 32,029 cycles

RIGHT I/B EXHAUST GATE UPPER SKIN IS WORN BEYOND REPAIRABLE LIMITS. REPLACED RIGHT I/B EXHAUST GATE PER AMM 27 51 05.

Part: PANEL — GOUGED (RT WING) · airframe 52,966 hrs · 32,029 cycles

RIGHT WING O/B OF PYLON FAIRING T/E DOGHOUSE HAS DEEP GOUGE AND CHAFING. FABRICATED A REPLACEMENT PANEL AND INSTALLED PER SRM 51 10 02.

Part: SEAL — CRACKED (MIDFLAP) · airframe 52,966 hrs · 32,029 cycles

RIGHT I/B MID FLAP SEAL PLATE ADAPTER PLATE ATTACH FASTENERS ARE LOOSE. REMOVED RIGHT I/B MID FLAP SEAL PLATE ADAPTER FOUND TO BE CRACKED, REPLACED WITH NEW PER SRM 51 40 02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL WITH NEW PER SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

BS 794 RT FRAME HAS CORROSION AT RBL 18.23 AFT CARGO DOORWAY FWD FRAME. REPLACED FRAME PER SRM 51-40-02 AND 53-60-15.

Part: SUPPORT ANGLE — DAMAGED (BS 727-727G) · airframe 52,966 hrs · 32,029 cycles

MISDRILLED HOLE IN SUPPORT ZEE. REPAIRED FROM BS 727 TO BS 727G.

Part: FLOOR PANEL — DENTED (FWD CARGO BAY) · airframe 52,966 hrs · 32,029 cycles

NR 4 FLOOR PANEL IS DENTED FWD CARGO BAY. REMOVED AND REPLACED FLOOR PANEL.

Part: SUPPORT ANGLE — CORRODED (BS BS 727B-807) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION ON SUPPORT ZEE BS 727B+8 TO BS 807. REPAIRED FROM BS 727 TO BS 798.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

CORROSION ON ZEE ANGLE BS 727 727C RBL 20. REPLACED FLOOR TO SIDEWALL SUPPORT ZEE ANGLE BS 727-727C RBL 20.

Part: SUPPORT ANGLE — CORRODED (BS 807-847) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION ON SUPPORT ZEE BS 807-847 LBL 20. REPAIRED FROM BS 798 TO BS 876.

Part: RETAINER — GOUGED (KRUEGER FLAP) · airframe 52,966 hrs · 32,029 cycles

GOUGES ON RIGHT I/B LEADING EDGE NR 4 KRUEGER FLAP AFT SIDE AROUND THE THIRD FASTENER NUT FOR BLADE SEAL IS OUT OF LIMITS. REMOVED AND REPLACED SEAL RETAINER.

Part: ATTACH ANGLE — CRACKED (TE FLAP) · airframe 52,966 hrs · 32,029 cycles

SEAL RIB ATTACH ANGLE O/B OF NR 3 FLAP TRACK FAIRING COMMON TO LOWER T/E COVE PANEL IS CRACKED. REMOVED AND REPLACED ANGLE.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION ON ZEE SUPPORT (FLOOR TO SIDEWALL SUPPORT) AFT CARGO BAY BS 727F 747 LT. REMOVED AND REPLACED SUPPORT ZEE PER SRM 53 60 53.

Part: STIFFENER — CRACKED (RT WING) · airframe 52,966 hrs · 32,029 cycles

STIFFENER CRACKED AT RT WING IFOT I/B SIDE. REMOVED AND REPLACED STIFFENER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

BS 747 RT FRAME RBL 18 23 HAS OBLONG HOLES. REMOVED DAMAGE ON FRAME BS 747 RBL 18 23 AND INSTALLED REPAIR DOUBLER.

Part: STIFFENER — CRACKED (LT WING) · airframe 52,966 hrs · 32,029 cycles

LT WING AFT INBOARD NO STEP PANEL LWR SURFACE OUTBOARD STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER SRM 51 40 02.

Part: DOUBLER — CRACKED (AC BAY DOOR) · airframe 52,966 hrs · 32,029 cycles

GROUND CONDITIONING AIR PANEL INTERNAL DOUBLER IS CRACKED. REMOVED AND REPLACED WITH NEW.

Part: SKIN — CHAFED (MIDFLAP) · airframe 52,966 hrs · 32,029 cycles

LEFT O/B MID FLAP O/B LOWER AFT PANEL CHAFED ON PREVIOUS REPAIR 14 INCHES I/B OF NR 1 FLAP TRACK. LEFT O/B MID FLAP O/B LOWER AFT PANEL 14.5 INCHES O/B OF NR 1 TRACK CHAFE MEASURES .018 ORIGINAL THICKNESS .064 OUT OF LIMITS. AREA WAS REPAIRED AND REFINISHED.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 52,966 hrs · 32,029 cycles

RIGHT O/B MID FLAP O/B LOWER AFT SKIN PANEL INNER SURFACE AT NR 3 AND NR 4 FLAP TRACKS. RIGHT O/B MID FLAP O/B LOWER AFT SKIN OUT OF LIMITS AT NR 3 AND NR 4 TRACK PER SRM. DAMAGE WAS REMOVED AT NR 3 TRACK 1 INCH DIAMETER .032 DEEP AT NR 4 TRACK 1 INCH DIA .032 DEEP AND REPAIRED PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,966 hrs · 32,029 cycles

FWD ENTRY DOORWAY AFT GIRT BAR FITTING ASSY IS CORRODED. REMOVED AND REPLACED CORRODED FWD ENTRY DOORWAY AFT GIRT BAR FITTING ASSY PER SRM 51 40 02.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

FWD ENTRY DOORWAY GIRT BAR FITTING BRACKET ASSY IS CORRODED. REPLACED FWD ENTRY DOORWAY GIRT BAR FITTING BRACKET ASSY.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 52,966 hrs · 32,029 cycles

LEFT O/B MID FLAP O/B LOWER AFT PANEL CHAFED ON INNER SURFACE AT NR 3 AND NR 4 FLAP TRACK. LEFT O/B MID FLAP O/B LWR PANEL AT NR 3 AND 4 TRACK DAMAGE OUT OF LIMIT. REMOVED DAMAGE AT NR 3 TRACK 1" X 2", .032 DEEP AT NR 4 TRACK 1 INCH DIAMETER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

HOLE CRACKED IN BEAR STRAP AT FWD ENTRY DOOR CUTOUT UPPER HINGE CUTOUT. REPAIRED BEAR STRAP.

Part: CARGO TRACK — CORRODED (BS 727-945) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

AFT PIT FWD LT ANCHOR FITTING LOCKING LUGS DAMAGED ADDITION DAMAGE NOTED/CORROSION.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

HOLE CRACKED IN BEAR STRAP AT FWD ENTRY DOOR CUTOUT LOWER HINGE CUTOUT. REPAIRED PER EA 400-53EA-0093.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 52,966 hrs · 32,029 cycles

NR 7 FLAP TRACK CORRODED. REMOVED AND REPLACED WITH SERVICEABLE UNIT ON DEFECT.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

NR 7 FLAP TRACK CORRODED. NR 7 FLAP TRACK REMOVED AND REPLACED WITH SERVICEABLE UNIT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

CORROSION AT STA 747+5 RBL 3 ON FLOOR SUPPORT. CORROSION OUT OF LIMITS. REMOVED FLOOR SUPPORT BS 740 793.5 PER SRM 53-60-53. NEW FLOOR SUPPORT TO BE INSTALLED ON CUST CARD.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

BS 794 FRAME VERTICAL WEB CORRODED. CORROSION OUT OF LIMITS. REMOVED AND REPLACED WEB PER SRM 51-40-02 AND 53-60-15.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

STRAP CORRODED AT AFT CARGO DOOR CUTOUT THRESHOLD. CORROSION OUT OF LIMITS. REMOVED AND REPLACED STRAP WITH FABRICATED PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

STA 859 RBL 3 FLOOR SUPPORT IS CORRODED AROUND NUT PLATE HOLES. REPLACED DAMAGED SECTION OF RBL 3 FLOOR SUPPORT BS 740-873.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

BS 794 FRAME CORRODED VERT WEB DOOR SURROUND. REMOVED AND REPLACED WEB PER SRM 51-40-02 & 51-40-05 AND DWG 65-47957.

Part: REVEAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

AFT CARGO BAY DOOR CUTOUT FWD REVEAL (COVER PLATE) CORRODED. REMOVED AND REPLACED FRAME UPPER COVER PLATE PER SRM 51-20-01 & 51-40-02 AND DWG 65-56655.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

GOUGES IN SEAT TRACK UPPER FLANGE BS 500E+15 TO 500E+18. REMOVED AND REPLACED SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

CORROSION AT STA 927G+17 RBL 3 FLOOR SUPPORT. REPLACED RBL 3 FLOOR SUPPORT BS 873 TO 947.

Part: SPLICE — CORRODED (FLOOR PANEL) · airframe 52,966 hrs · 32,029 cycles

FLOOR PANEL NR 3 TO NR 4 SPLICE STRIP STA 787 STR 25 25 CORRODED. REMOVED AND REPLACED SPLICE STRAP.

Part: FLOOR SUPPORT — CORRODED (BS 787-807) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION AT STA 787-807 RBL 20 FLOOR SUPPORT. CORROSION OUT OF LIMITS. REMOVED AND REPLACED SUPPORT STRAP PER SRM 53-60-15 AND 51-40-05.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

GOUGES IN SEAT TRACK UPPER FLANGE BS 570 TO BS 575 RBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — GOUGED (BS 608-612) · airframe 52,966 hrs · 32,029 cycles

GOUGES IN SEAT TRACK UPPER FLANGE BS 608 TO BS 612 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK WITH NEW SEAT TRACK.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

GOUGES IN SEAT TRACK UPPER FLANGE BS 541 RBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION ON SUPPORT ZEE (FLOOR TO SIDEWALL SUPPORT) BS 727C +10 TO BS 767. REPLACED FLOOR TO SIDEWALL SUPPORT BS 727C +10 TO BS 767 PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,966 hrs · 32,029 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY. REPAIRED ON MIG 5.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

GOUGE IN SEAT TRACK UPPER FLANGE. REMOVED AND REPLACED SEAT TRACK.

Part: FRAME — CHAFED (BS 601) · airframe 52,966 hrs · 32,029 cycles

FRAME AT BS 601, 3 INCHES ABOVE STR 5 IS CHAFED. REPAIRED FRAME PER SRM.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

GOUGE IN SEAT TRACK UPPER FLANGE. REMOVED AND REPLACED SEAT TRACK.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

LOWER RT SPLICE ANGLE AT BODY STATION 727+3 MISDRILLED HOLE. REMOVED AND REPLACED SUPPORT ANGLE.

Part: SEAT TRACK — GOUGED (BS 500G) · airframe 52,966 hrs · 32,029 cycles

GOUGE IN SEAT TRACK UPPER FLANGE. REPLACED SEAT TRACK BS 480-520 LBL 45 WL 208.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

SUB THRESHOLD WEB AFT CARGO CORRODED. REMOVED, FABRICATED & INSTALLED NEW SUB THRESHOLD WEB PER SRM 51-40-05 & 51-20-01 AND DWG S330018186.

Part: SNUBBER — DEFECTIVE (L1 DOOR) · airframe 52,911 hrs · 31,975 cycles

L1 DOOR WILL NOT SHUT PROPERLY. REPLACED L1 DOOR SNUBBER REF ASMM 52 11 71 004 023 52 11 71 404 009. ADJUSTED DOOR GUIDE ARM REF ASMM 52 11 21 404 007 002, OPS CHECK OK.

Part: FLAP SYSTEM — MALFUNCTIONED (RT WING) · airframe 52,421 hrs · 31,558 cycles

DURING ARRIVAL INTO OTZ FLAPS EXTENDED TO JUST SHORT OF 10 WITH A GREEN LIGHT ON THE LEADING EDGE. FLAPS COULD NOT BE EXTENDED PAST 10 WITH NORMAL OR ALTERNATE FLAP EXTENSION. RAN APPROPRIATE CHECK LIST AND LANDED IN OTZ. RELEASED PER CDL 57 53 1 PLACARD INSTALLED & DOOR REMOVED MIDFLAP TORQUE SHAFT CLEARANCE RT. OPS CHECK FLAP CHECKS NORMAL ED NOTIFIED CN 1217001 RH

Part: PUMP — FAILED (HYD SYSTEM) · airframe 51,027 hrs · 30,267 cycles

DURING CLIMB-OUT RIGHT HYDRAULIC QTY SHOWED 44 PERCENT DURING LANDING ROLLOUT NR 2 ENG LOW PRESSURE LIGHT ILLUMINATED AND REMAINED ON LOUD METAL GRINDING NOISE NOTED BY PILOT RIDING IN BACK DURING TAXI IN SERVICED RT HYD SYSTEM TO FULL REF MM 12-12-00 (91541). OPERATED NR 2 ENG W NO ENG HYD PRESSURE NOTED (91541). REPLACED NR 2 ENG HYD PUMP REF ASA 29 15 11(13287). STILL REQ FILTERS CHANGED. OPS CK AND LEAK CHECK. FLUSH B HYD SYSTEM NO FILTERS CONTAINED. LEAK CHECK GOOD. OPS NORMAL REF AMM 29-15-00-172-037.

Part: WARNING LIGHT — FALSE INDICATION (CARGO FIRE) · airframe 50,072 hrs · 29,385 cycles

ON CLIMB-OUT, BOTH CARGO FIRE SUPPRESSION BOTTLE LIGHTS ILLUMINATED. REPLACED BOTH BOTTLES AND MODULE FOR CARGO FIRE SUPPRESSION SYSTEM.

Part: SKIN — DENTED (BS 490-510) · airframe 47,269 hrs · 26,917 cycles

FUSELAGE SKIN PANEL DENTED 2.5 INCHES FROM EXISTING REPAIR. REMOVED EXISTING REPAIR INSTALLED NEW REPAIR IAW PEMCO EA PD37 53 693C AND ASA EA 5330 02514.

Part: SKIN — DENTED (BS 460-480) · airframe 47,269 hrs · 26,917 cycles

FUSELAGE EXTERIOR DENTS. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-00-01 FIG 201 DETAIL X.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 47,269 hrs · 26,917 cycles

REF AD 2005 20 03 L1 DOOR S16 INTERCOSTAL WEB CRACKED. REPLACED S16L INTERCOSTAL WEB IAW PEMCO EA PD 37 53 552 AND ASA EA 5310 02650.

Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 47,269 hrs · 26,917 cycles

REF AD 2005 20 03 L1 DOOR S7L INTERCOSTAL WEB CRACKED FWD INBOARD IN RADIUS. REPLACED S7L INTERCOSTAL WEB IAW PEMCO EA PD 37 53 552 AND ASA EA 5310 02650.

Part: BEAM — CRACKED (HORIZONTAL STAB) · airframe 47,269 hrs · 26,917 cycles

LT HORIZONAL STAB NR 2 BALANCE BAY BEAM SPAN WEB CRACKED APPROX 1 INCH AT STAB STA 165. ACCOMPLISHED INTERIM REPAIR IAW PEMCO EA PD37 55 012 AND ASA EA 5510 01246 PER BOEING MESSAGE NUMBER 1 210047303.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,269 hrs · 26,917 cycles

LT HORIZ STAB LWR SKIN CRACKED APPROX 1" LONG AT REAR SPAR. ACCOMPLISHED TEMP REPAIR IAW PEMCO EA PD37 55 0111 AND ASA EA 5510 01245 AND PER BOEING MESSAGE 1 209186222 8 DATED 19 JUL 06.

Part: SKIN — DAMAGED (FUSELAGE)

KTN - FOUND BAGGAGE CART IMPACTED FUSELAGE SKIN. REPAIRED FRAME AT BS 907, STRINGERS 22 RT, BS 897, STRINGER 23RT, BS 847-907, STRINGER 24 RT, BS 847-907 AND FUSELAGE SKIN AT S22-24RT AND BS 887-927. ALL WORK PERFORMED IAW B737-400 SRM 53-00-03 REPAIR 1. (M)

Part: HOUSING — WORN (NR 1 PYLON)

NR 1 ENGINE PYLON SPHERICAL BEARING OUTER RACE IS LOOSE IN HOUSING UPPER SPAR ATTACHMENT FITTING FOR UPPER LINK. REMOVED AND REPLACED NR 1 ENGINE PYLON SPHERICAL BEARING, PYLON CROWN BEAM, IAW ASA EA 5440-01011, TYPICAL REPAIR. (M)

Part: FRAME — CORRODED (FUSELAGE)

AFT PIT STUB FRAME HAS CORROSION AROUND NUT PLATE BS 792 BL 18R. REPAIRED IAW SRM 51-40-02. (M)

Part: STRUCTURE — DENTED (FUSELAGE)

AIRCRAFT DENTED AT TAIL JACK PAD AREA STATION 1088. REPAIRED IAW EA 9330-01741. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND BS 986 FLOORBEAM HAS CORROSON AROUND CLIPNUT HOLES AT NUMEROUS PLACES FROM LBL 46 TO RBL 46, TOP AND BOTTOM SURFACES. REPAIRED IAW EA 5310-02303. (M)

Part: MODULE — MALFUNCTIONED (APU FIRE DETECT)

GYR - AFTER TAKEOFF APU FIRE DETECTION FAULT LIGHTS ON FIRE WARNING PANEL ILLUMINATED. AIRCRAFT RETURNED TO GYR AND LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. REPLACED FIRE DETECTION ELECTRONICS RACK MODULE. OPERATIONS CHECKED GOOD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - DURING SCHEDULED MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT BS 967. REPAIR IAW EA. (M)

Part: SKIN — CHAFED (NR 1 PYLON)

GYR - DURING MAINTENANCE CHECK, NR 1 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257. REPAIR IAW EA. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - DURING MAINTENANCE CHECK, FOUND R-2 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 947-997. REPAIR IAW SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - DURING MAINTENANCE CHECK, FOUND L1 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 306 TO 342. REPAIR IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 967. REPAIR IAW EA. (M)

Part: SKIN — DAMAGED (FUSELAGE)

GYR - DURING MAINTENANCE CHECK, FOUND SKIN CREASE AT STATION 792 TO 803 AND STRINGER 25R TO 27L. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - DURING MAINTENANCE CHECK, FOUND L2 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 947 TO 986. REPAIR IAW SRM. (M)

Part: SKIN — WORN (NR 2 PYLON)

GYR - DURING MAINTENANCE CHECK, NR 2 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257 RIGHT. REPAIR IAW EA. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - DURING MAINTENANCE CHECK, FOUND R-1 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 306-350. REPAIR IAW SRM. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SEA - DURING LINE CHECK, FOUND NEAR ROW 23 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 1-6 INOPERATIVE. RECONNECTED WIRES, OPERATIONAL CHECKED GOOD. (M)

Part: DOOR FRAME — DAMAGED (FUSELAGE)

DURING C-CHECK, FOUND FORWARD CARGO BAY FORWARD DOOR FRAME CLOSURE WEB DAMAGED. REPAIRED IAW SRM. (M)

Part: SKIN — CRACKED (RT WING)

DURING C-CHECK, FOUND RIGHT WING LE CRACKED AT SLAT ACTUATOR CUT OUT. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SKIN IS DENTED AT BS 807 STRINGER 27R TO 27L. REPAIRED IAW SRM. (M)

Part: RETAINER — CHAFED (APU DOOR)

DURING C-CHECK, FOUND APU ACCESS DOOR SEAL RETAINER ANGLE IS CHAFED ON LEFT SIDE. REPAIR IAW SRM. (M)

Part: COTTER PIN — OUT OF POSITION (PAX DOOR)

DURING C-CHECK, FOUND FORWARD ENTRY DOOR SNUBBER COTTER PINS CHAFING FUSELAGE STRUCTURE INBOARD LOWER CAM PLATE. REPAIR IAW SRM. (M)

Part: SKIN — DENTED (APU DOOR)

DURING C-CHECK, FOUND APU ACCESS DOOR SKIN DENTED AND CHAFED OUT OF LIMITS. REPAIR IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 727-762, RBL 20 WL 150 IS CORRODED. REMOVED AND REPLACED SIDE WALL PLATE IAW SRM. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY RIGHT FLOOR TRACK BS 747 TO 947 RBL 14 WL 150 CORRODED. REMOVED AND REPLACED PER SRM. (M)

Part: WEB — GOUGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FORWARD ENTRY DOOR WEB GOUGED OUTBOARD OF AFT STOP FITTING. REPAIRED PER EA. (M)

Part: SKIN — DENTED (CARGO DOOR)

PAE - DURING C-CHECK, FOUND AFT CARGO DOOR SKIN DENTED. REPLACES SKIN IAW SRM. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY BS 792, RBL 24-28 WL 160 DOOR FRAME PLATE IS CORRODED. REMOVED AND REPLACED PLATE IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY LEFT FLOOR SIDEWALL SUPPORT PLATE FROM BS 727-947 AND LBL 20, WL 150 CORRODED. REPLACED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SUB THRESHOLD WEB CORRODED OUT OF LIMITS AT BS 794-847, RBL 21, WL 150. REMOVED AND REPLACED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SUB THRESHOLD TIE STRAP CORRODED OUT OF LIMITS AT BS 775-847, WL 150. REMOVED AND REPLACED PER SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY SUB THRESHOLD STRAP CORRODED OUT OF LIMITS AT BS 782-800, RBL 20, WL 149. REMOVED AND REPLACED PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION OUT OF LIMITS AT AFT CARGO BAY AT BS 847-867, RBL 24, WL 160 SIDEWALL SUPPORT PLATE. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND LOWER BULKHEAD SUPPORT ANGLE CORRODED OUT OF LIMITS AT BS 947, LBL 19, WL 178. REMOVED AND REPLACED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION OUT OF LIMITS ON FORWARD CARGO DOOR SUB THRESHOLD WEB AT NUT PLATE HOLES AT STATION 441-492, RBL 25, WL 157. REMOVED AND REPLACED PER SRM. (M)

Part: POWER SUPPLY — INOPERATIVE

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 21-24. REMOVED AND REPLACED POWER SUPPLY (BALLAST), OPS NORMAL. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

PDX - DURING LINE CHECK,FOUND EMERGENCY EGRESS LIGHT AT L2 DOOR INOPERATIVE. RESTORED TENSIONING TO POSITIVE CONTACT AND RELAMPED. OPS CHECK GOOD. (M)

Part: LIGHT — DISCONNECTED (AFT MID CABIN)

FAI - BEFORE FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS AT AFT MID CABIN INOPERATIVE. RECONNECTED WIRES, OPS CHECKS GOOD. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - PRIOR TO DEPARTURE OF FLIGHT 63, CREW REPORTED L-1 DOOR DIFFICULT TO CLOSE. ADUSTED DOOR MECHANISM AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (R-2 DOOR)

SEA - DURING MAINTENANCE CHECK, THE R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND BROKEN. REPLACED R-2 DOOR EXIT IDENTIFIER LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: FLOORBEAM — CORRODED (BS 294.5)

PHX - DURING SI CHECK, FOUND THE FLOORBEAM AT STATION 294.5, BL 0 - RBL 5 UPPER CAP CORRODED. REPAIRED PER EA 53-10-08. (M)

Part: BEAM — CORRODED (BS 280-344)

PHX - DURING SI CHECK, FOUND THE R1 DOOR TRANSVERSE BEAM CORRODED AT STATION 280-344. (M)

Part: FLOORBEAM — CORRODED (BS 312)

PHX - DURING SI CHECK, FOUND THE FLOORBEAM UPPER HORIZONTAL CAP, TO SURFACE, CORRODED AT STATION 312 LBL 2 - RLB 7. REPAIRED PER SRM 53-10-51 AND DRAWING 65C33941. (M)

Part: SKIN — DENTED (BS 440)

PHX - DURING SI CHECK, FOUND THE FORWARD CARGO DOOR CUTOUT, FORWARD SIDE DENTED BETWEEN S23R AND S24R. REPAIRED PER EA 5330-01369. (M)

Part: FRAME — CRACKED (R1 DOORWAY)

PHX - DURING SI CHECK, FOUND THE R1 DOOR CUTOUT FORWARD FRAME AT STATION 296 WL 209 CRACKED. REPAIRED PER EA 5310-01664. (M)

Part: SKIN — DAMAGED (BS 490-500)

PHX - DURING SI CHECK, FOUND THE RIGHT FUSELAGE SKIN AT STATION 490-500, STRINGER 22R-24R NICKED. REPAIRED PER SRM 53-00-01. (M)

Part: FLOORBEAM — CORRODED (BS 967)

PHX - DURING SI CHECK, FOUND THE FLOORBEAM UPPER HORIZONTAL CAP CORRODED AT STAITON 967, LBL 18. REPAIRED PER SRM 53-00-51. (M)

Part: FLOORBEAM — CORRODED (BS 986.5)

PHX - DURING SI CHECK, FOUND THE UPPER HORIZONTAL CAP OF THE FLOORBEAM AT STATION 986.5 CORRODED IN NUMEROUS AREAS FROM LBL 45 TO RBL 31. REPAIRED PER EA 5310-01667. (M)

Part: BEAM — CORRODED (BS 949-997)

PHX - DURING SI CHECK, FOUND THE L-2 DOOR LOWER SEAL TRANSVERSE BEAM CORRODED FROM STATION 949 TO 997. REPAIRED PER SRM 51-40-02. (M)

Part: WEB — CORRODED (BS 991)

PHX - DURING SI CHECK, FOUND THE SHEAR WEB UNDER LEFT TRANSVERSE BEAM AT L-2 DOOR THRESHOLD CORRODED AT STATION 991, LBL 37. REPAIRED PER SRM 51-40-02 AND SRM 53-60-51. (M)

Part: FLOORBEAM — CORRODED (BS 947.5)

PHX - DURING SI CHECK, FOUND THE UPPER HORIZONTAL CAP OF THE FLOORBEAM AT STATION 947.5 CORRODED FROM RBL 13 TO LBL 13. REPAIRED PER EA 5310-01665. (M)

Part: FLOORBEAM — CORRODED (BS 360)

PHX - DURING SI CHECK, FOUND THE UPPER HORIZONTAL CAP OF THE FLOORBEAM AT STATION 360 CORRODED FROM RBL 14 TO RBL 28. REPAIRED PER EA 5310-01666. (M)

Part: LIGHT — LOOSE (CABIN)

SEA - PRIOR TO FLT 468, TWO EACH RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE FIRST CLASS SECTION. CLEANED AND RESECURED TRACK AND THE LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, TWO FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: FAIRINGS — WORN (NR 1/2)

SEA - DURING C-CHECK, WEAR WAS FOUND AT VARIOUS LOCATINS ON ALL FOUR BULLNOSE FAIRINGS ON NR 1 AND NR 2 ENGINES AS A RESULT OF THE BLOCKER DOOR HINGE FITTINGS RUBBING AGAINST THE FAIRING SURFACES. REPAIRED PER EA 5430-01029 AND BOEING TELEX ASA-SEA-98-0049RR. (M)

Part: SKIN — LIGHTNING STRIKE (RT WING)

SEA - DURING C-CHECK, PREVIOUS INTERIM REPAIRED LIGHTNING STRIKE DAMAGE WAS FOUND ON THE CONDUCTIVE STRIP OF THE RT WING FIXED T/E. REPAIRED PER EA 5740-01270 AND BOEING TELEX ASA-SEA-98-0045RR. (M)

Part: SKIN — DENTED (CARGO DOOR)

SEA - DURING C-CHECK, A SERIES OF DENTS AND SCRATCHES WERE FOUND IN THE SKIN OF THE FORWARD CARGO DOOR IN THE VICINITY OF THE DOOR HANDLE. REPAIRED PER EA 5230-01079. (M)

Part: SKIN — WORN (LT TE MID FLAP)

SEA - DURING C-CHECK, THE LEFT WING OUTBOARD MID FLAP LOWER SURFACE NR 1 TRACK AFT FAIRING NYLON PADS WORN INTO WING SURFACE. REPAIRED PER EA 5750-01185 AND BOEING TELEX ASA-SEA-95-0634RR. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 6-10. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 79 - PRIOR TO FLIGHT THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD 2 AND AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: SEAL RETAINER — BENT (L1 DOOR)

SEA - FLT 553 - PRIOR TO DEPARTURE, THE L1 DOOR HANDLE WAS FOUND TO BE EXTREMELY DIFFICULT TO CLOSE. MAINTENANCE INSPECTED AND FOUND THAT THE SEAL RETAINER WAS BENT ON THE LOWER AFT CORNER. THE SEAL RETAINER WAS REPOSITIONED AND THE DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SNA - FLT 445 - PRIOR TO DEPARTURE, CREW REPORTED THE TWO FORWARD AND THE SECOND FROM AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED THE FORWARD LIGHTS, RELAMPED AND REPLACED LENS ON THE AFT LIGHT. ALL LIGHTS OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L-1 DOOR)

PDX - FLT 437 - CREW REPORTED L1 DOOR DIFFICULT TO CLOSE. LUBED CAM ROLLER/CAM PLATE AND ADJUSTED TOP AFT LATCH CAM FITTING, DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE AFT RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-27. REPLACED BROKEN WIRE AND LIGHT ASSEMBLY, P/N 5417N5048, AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

LAS - FLIGHT 621 - DURING CREW PREFLIGHT, THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED TRACK LIGHT WIRES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: MEC — MALFUNCTIONED (NR 1 ENGINE)

PVR - FLT 110 - ON ARRIVAL, CREW REPORTED THE NR 1 ENGINE FLAMED OUT DURING DESCENT AT 15,000 FEET. ACCOMPLISHED ENGINE FAILURE/SHUTDOWN AND INFLIGHT START CHECK LIST. ENGINE RESTARTED NORMALLY AND LANDED WITHOUT INCIDENT. AT THE TIME OF FLAME OUT, THE AIRCRAFT HAD BEEN AT IDLE THRUST FOR 10 MINUTES DURING THE DESCENT. ACCOMPLISHED EXTENSIVE TROUBLE SHOOTING PER TSR 0900041, PERFORMED GROUND RUN UP AND NO TROUBLE WAS FOUND. FERRIED AIRCRAFT TO SEA AND REPLACED NR 1 ENGINE MAIN ENGINE CONTROL AS PRECAUTIONARY, ENGINE OPERATED NORMALLY. (M)

Part: LAMP — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FIRST TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPINNED LAMP ASSY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRE HARNESSES AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (FWD CABIN)

JNU - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

JNU - DURING MAINTENANCE CHECK, FOUND TWO SECTIONS OF EMERGENCY EXIT TRACK LIGHTS INOPERATIVE FORWARD CABIN AREA. RECONNECTED LOOSE WIRES AT ROW 1C AND REPAIRED BROKEN WIRES AT FORWARD COAT CLOSET. EMERGNCY EXIT LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PVR - FLT NR 255 - CREW REPORTED, THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE AT ROW 17. RESECURED AND RESPLICED WIRING AT ROW 17 AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT NR 54 - EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 15 AND 16. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, TWO SECTIONS OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 1-2 AND 14-15. RECONNECTED LOOSE TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS, IN AREA OF ROW 15, WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 14 TO 15 WERE FOUND INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON THE AFT TRACK AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTORS — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 12 THROUGH 16 AND ROW 27 AFT. SPLICED BROKEN WIRES AT ROWS 14-15, AND RECONNECTED LOOSE CONNECTORS AT ROWS 13, 27 AND AT THE AFT LAVATORY DOOR. REFERENCE ASAA9540050.

Part: EEL WIRING — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 12 THROUGH 16 AND ROW 27 AFT. SPLICED BROKEN WIRES AT ROWS 14-15, AND RECONNECTED LOOSE CONNECTORS AT ROWS 13, 27 AND AT THE AFT LAVATORY DOOR. (M)

Part: EEL BATT CHARGER — INOPERATIVE (CABIN)

SEA - L1 DOOR EMERGENCY EXIT IDENTIFIER INOP. MAINTENANCE REPLACED M1132 POWER SUPPLY. (M)

Part: EEL LAMP — INOP (CABIN)

SEA - CHECK, ROW 25ABC OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. (Z)