N793AS

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 55,566 hrs · 31,533 cycles

R-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. RELAMPED R-1 DOOR EXTERIOR EMERGENCY LIGHT, OPS CHECK GOOD, REF AMM 33-51-22.

Part: LIGHT — INOPERATIVE (NAV) · airframe 54,646 hrs · 30,900 cycles

V NAV LIGHT DOES NOT LIGHT UP. ACFT GROUNDED. DFCS LIBRARY TEST NR 50 SHOWED ALL MCP SWITCH LIGHTS TO BE INOPERATIVE. SUSPECT INTERNAL MCP FAULT. R & R AND TESTED DFCS MODE CONTROL PANEL IAW MM 22-11-34-004-004, MM 22-11-34-404-003. PERFORMED DFCS GROUP NR 10, CURRENT STATUS, NR 15, ALTITUDE ALERT AND NR 32, MCP LRU INTERFACE, TESTS IAW MM 22-11-34-745-001 AND HGS SENSOR TEST FOR FCC IAW HGS SMM 34-36-00. ALL TESTS PASS. ACFT REMAINS QUALIFIED FOR CAT IIIA AUTOLAND AND HGS OPS AND STATUS PLACARD.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 52,789 hrs · 29,712 cycles

AFT CARGO DOOR HANDLE HAS MISSING BUMPER AND HOUSING DAMAGE, GOUGE. ACFT GROUNDED. STARTED MIG 2C 220443,84881 02/03/2015, REINSTALLED HOUSING AND SEAL WITH SEALANT, ATTACHED WITH FASTENERS IAW SRM 51-40-02.84881. INSTALLED INTERIOR HANDLE IAW MM 52-31-14-004-054. ALL MIG-2C ITEMS ON NR 220443, CLEARED.

Part: SKIN — CHAFED (RUDDER) · airframe 51,490 hrs · 28,957 cycles

RUDDER RT SIDE L/E CAP CHAFED BETWEEN NR 5 & 6 HINGES. ACFT GROUNDED. REPAIRED RIGHT L/E CAP ON RUDDER IAW EA 400-55EA-12816.

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

FLOOR SUPPORT BS 312-328 RBL 11 IS CORRODED, ACFT GROUNDED. CORROSION FOUND TO BE 100 PERCENT MATERIAL LOSS. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 277-291) · airframe 51,490 hrs · 28,957 cycles

ANGLE FWD OF R1 DOOR BS 277-291 WL 249 ABOVE STR 12 IS CRACKED. ACFT GROUNDED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE AT STA 277-291 ABOVE STR 12 IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 227-291) · airframe 51,490 hrs · 28,957 cycles

ANGLE FWD OF R1 DOOR STA 277-291, WL 259 ABOVE STR 10 IS CRACKED. ACFT GROUNDED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE AT STA 277-291 ABOVE STR 10 IAW SRM 51-40-02-0G.

Part: ANGLE — CRACKED (BS 277-279) · airframe 51,490 hrs · 28,957 cycles

ANGLE FWD OF R1 DOOR BS 277-291, WL 241 ABOVE STR 13 IS CRACKED. ACFT GROUNDED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE AT STA 277-291 ABOVE STR 13 IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 616) · airframe 51,490 hrs · 28,957 cycles

STRINGER CLIP CRACKED AT BS 616, S5L REQ REPLACEMENT IAW FIG 32 OF T/C 5310-02658-3, STEP 341. ACFT GROUNDED. R & R STRINGER CLIP IAW ASA T/C 5310 02658 3, REV: 0.

Part: STRINGER CLIP — CRACKED · airframe 51,490 hrs · 28,957 cycles

STR CLIP CRACKED AT STA 500F AT STR 6 LT REQ. REPLACEMENT IAW FIG 16 OF T/C 5310 02658 3 REF STEP 251. ACFT GROUNDED. REMOVED DAMAGED STRINGER CLIP AND INSTALLED NEW STR CLIP AT STA 500F, STR 6 LT IAW ASA T/C 5310 02658 3.

Part: FRAME — CRACKED (BS 867) · airframe 51,490 hrs · 28,957 cycles

CABIN FRAME BS 867, LT IS CRACKED AT ACFT RAIL ATTACH LOCATION. ACFT GROUNDED. CUT OUT DAMAGE AND REPAIRED FRAME IAW EA 400-53EA-12733.

Part: FRAME — CRACKED (BS 827) · airframe 51,490 hrs · 28,957 cycles

CABIN FRAME 827, RT IS CRACKED AT ACFT RAIL ATTACH LOCATION. ACFT GROUNDED. CUT OUT DAMAGE AND REPAIRED FRAME IAW EA 400-53EA-12733.

Part: FRAME — CRACKED (BS 727B) · airframe 51,490 hrs · 28,957 cycles

CABIN FRAME BS 727B, RT IS CRACKED AT ACFT RAIL ATTACH LOCATION. ACFT GROUNDED. CUTOUT DAMAGE AND REPAIRED FRAME IAW EA 400-53EA-12733.

Part: FRAME — CRACKED (BS 907) · airframe 51,490 hrs · 28,957 cycles

CABIN FRAME BS 907, LT IS CRACKED AT ACFT RAIL ATTACH LOCATION. ACFT GROUNDED. CUTOUT DAMAGE AND REPAIRED FRAME IAW EA 400-53EA-12733.

Part: ANGLE — CRACKED (BS 348) · airframe 51,490 hrs · 28,957 cycles

REINFORCEMENT ANGLE CRACKED AT STA 348 AND STR 15L. ACFT GROUNDED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE AT STA 348 AND STR 15L IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 360) · airframe 51,490 hrs · 28,957 cycles

FWD PASSENGER CABIN AT FRAME, BS 360 BETWEEN STRINGER 8L AND 7L CRACK LOCATED ON AFT FACE OF FRAME AT RIVET HEAD ABOVE STRINGER CLIP 8L. ACFT GROUNDED. CUTOUT DAMAGE AND REPAIRED FRAME IAW EA 400-53EA-12733.

Part: FLOOR SUPPORT — CORRODED (BS 259-270) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

FLOOR SUPPORT BS 259 - 270 LBL 11 HAS CORROSION. ACFT GROUNDED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CRACKED (BS 1116) · airframe 51,490 hrs · 28,957 cycles

VERTICAL ATTACH ANGLE CRACKED INSIDE APU RT TORQUE BOX BELOW FWD LWR CORNER OF AIR INLET. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 400) · airframe 51,490 hrs · 28,957 cycles

FWD CABIN AT FRAME BS 400, BETWEEN STRINGER 8R AND 9R RIVET BUCKTAIL ON AFT SIDE OF FRAME IS CRACKED. LOOK FOR 2EA SMALL CRACKS LOCATED BELOW STRINGER CLIP. ACFT GROUNDED. CUT OUT DAMAGE AND REPAIRED FRAME IAW EA 400-53EA-12733.

Part: SHEAR WEB — CORRODED (BS 348) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

L1 DOOR AFT LOWER DOOR FRAME SHEAR WEB IS CORRODED AROUND LOWER NUTPLATE. ACFT GROUNDED. BLENDED CORRODED AREA FOUND TO BE OUT OF LIMITS, FABRICATED LOCATED AND DRILLED NEW SHEAR WEB AFT OF L1 DOOR IAW SRM 53-15-1A-1 AND SRM 51-30-01-0G-0. W=.500, O=.040, R=.034, L= .500, D=.006.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

BS 328, FLOORBEAM HAS AREAS OF CORROSION ON UPPER TEE CAP. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 400-53EA-12778.

Part: DOOR SILL — CORRODED (BS 270-360) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

L1 DOOR MOPSILL HAS AREAS OF CORROSION. ACFT GROUNDED. REMOVED, DRILLED, LOCATED AND INSTALLED NEW INNER CHORD IAW SRM 51-40-02-0G-0, W 1", O .090", R .073", L 3". D .017.

Part: FAILSAFE — CORRODED (BS 986) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

FAILSAFE BS 986 S25 -27L IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, CHECKED OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101. R & R FAILSAFE IAW SRM 51-40-02-OG-0.

Part: FAILSAFE — CORRODED (BS 986) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

FAILSAFE BS 986 S25 - 27L IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, CHECKED OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101. R & R FAILSAFE IAW SRM 51-40-02-OG-0.

Part: FRAME — CORRODED (BS 992) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

LEFT FRAME BS 992 IS CORRODED ON INNER FLANGE ABOVE L2 MOP SILL. ACFT GROUNDED. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED FRAME IAW EA 400-53EA-12793.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 51,490 hrs · 28,957 cycles

RT WING OTBD AFT FLAP LOWER SKIN HAS A CREASE JUST OTBD OF NR 7 FLAP TRACK. ACFT GROUNDED. REPAIRED RT WING OTBD AFT FLAP LOWER SKIN JUST OTBD OF NR 7 FLAP TRACK IAW SRM 51-70-10-2R-0, REPAIR 4.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 51,490 hrs · 28,957 cycles

FWD CARGO BAY NR 3 FLOORBOARD IS CRACKED. ACFT GROUNDED. FABRICATED, TREATED AND PRIMED NEW NR 3 FLOORBOARD IAW SRM 51-40-05-0G-0, SRM 51-20-01-0G-0 AND BSOPM 20-41-02, PARA 6.

Part: TRANSITION PANEL — CORRODED (BS 727E-767) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

AFT CARGO BAY RT TRANSITION PANEL IS CORRODED STA 727E-767. ACFT GROUNDED. BLENDED CORROSION ON TRANSITION PANEL, REMAINING MAT FOUND TO BE OUT OPF LIMITS, REPAIRED TRANSITION PANEL AT AFT CARGO, COMP B, STA 727E-767 RT, IAW SRM 53-60-53-2R-4, REPAIR 4, FIG 201, PAGE 2. W=3", O=.040, R=.033, L=80", D=.007.

Part: STRINGER CLIP — CRACKED (BS 727) · airframe 51,490 hrs · 28,957 cycles

AFT CARGO BAY STRINGER CLIP BS 727F, S21L IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: SHEAR TIE — CORRODED (BS 520) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

SHEAR TIE CORRODED AT BS 520 BETWEEN S28L-S28R. ACFT GROUNDED. R & R THE SHEAR TIE IAW SRM 51-40-02-0G-0.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 51,490 hrs · 28,957 cycles

AFT CARGO NR 3 FLOOR PANEL IS CRACKED. ACFT GROUNDED. FABRICATED, TREATED AND PRIMED NEW NR 3 AFT CARGO FLOOR PANEL IAW SRM 51-40-05-0G-0, SRM 51-20-01-0G-0 AND BSOPM 20-41-02.

Part: SKIN — CHAFED (LT WING SPOILER) · airframe 51,490 hrs · 28,957 cycles

LEFT WING NR 4 SPOILER LOWER SKIN IS CHAFED ON PREVIOUS REPAIR. ACFT GROUNDED. REPAIRED NR 4 SPOILER LOWER SKIN IAW EA 400-57EA-12749.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 51,490 hrs · 28,957 cycles

LEFT WING NR 2 SLAT T/E WEDGE OTBD CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED LT NR 2 SLAT T/E WEDGE OTBD CORNER IAW SRM 51-70-10-2R-0, REPAIR 4.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 51,490 hrs · 28,957 cycles

RIGHT INBD MID FLAP CHAFED ON UPPER SURFACE. ACFT GROUNDED. REPAIRED SKIN IAW SRM 57-53-01-2R-3, REPAIR 3.

Part: CARGO TRACK — CORRODED (BS 780-847) · corrosion level 2 · airframe 51,490 hrs · 28,957 cycles

AFT CARGO BAY RT CARGO TRACK STA 780 TO 847 IS CORRODED. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGEED SECTION OF CARGO TRACK AND REPAIRED IAW SRM 53-00-53-2R-2, REPAIR 2 & ASA EA 400-53EA-12742.

Part: BEARING — FROZEN (R1 DOOR) · airframe 50,835 hrs · 28,576 cycles

R1 DOOR WILL NOT FULLY OPEN, FOUND JIGGLING THE DOOR HANDLE RELEASES THE DOOR TO FULL OPEN POSITION. GROUNDED. FOUND TORQUE BOX SEQUENCING BEARINGS ROUGH IN MOVEMENT, R & R BOTH ROLLERS DOOR NOW OPERATES SMOOTHLY REF CMM 52-46-06, STEPS D (5) AND D (21). LUBRICATED OUTER DOOR HANDLE REF AMM 12-25-41. GALLEY DOOR TEST GOOD REF AMM 52-41-00-705-041-001.

Part: STRAP — CRACKED (BS 312-344) · airframe 50,128 hrs · 28,114 cycles

FLOOR STRAP ABOVE FWD E/E RACK BROKEN. ACFT GROUNDED. REMOVED AND INSTALLED FLOOR STRAP IAW SRM 51-40-02.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 47,933 hrs · 26,735 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 1 GALLEY ADJACENT TO R-1 DOOR IS BROKEN. ACFT GROUNDED. REF WDM SUPPLEMENT 33-51-41. R & R L1186 LIGHT ASSY AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: FITTING — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 47,871 hrs · 26,700 cycles

AFT CARGO FWD DOOR STOP NR 2 HAS CORROSION AROUND STOP PAD. LOCATED AND DRILLED NEW STOP FITTING IAW SRM 51-40-05.

Part: FITTING — CORRODED (BS 847) · corrosion level 2 · airframe 47,871 hrs · 26,700 cycles

AFT PIT/AFT DOOR STOP FITTING NR 5 HAS CORROSION AROUND STOP PAD. ACFT GROUNDED. LOCATED AND DRILLED NEW STOP FITTING IAW SRM 51-40-05.

Part: FITTING — CORRODED (CARGO DOORWAY) · airframe 47,871 hrs · 26,700 cycles

AFT CARGO BAY FWD DOOR STOP NR 1 HAS CORROSION AROUND STOP PAD. NEW STOP FITTING, LOCATED, DRILLED AND TOPCOATED IAW SRM 51-40-05 AND MM 51-21-41-377-0320.

Part: FITTING — CORRODED · corrosion level 2 · airframe 47,871 hrs · 26,700 cycles

AFT CARGO BAY AFT DOOR STOP FITTING NR 4 CORROSION AROUND STOP PAD. NEW STOP FITTING LOCATED, DRILLED AND TOPCOATED IAW SRM 51-40-05 AND MM 51-21-41-377-032.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 47,871 hrs · 26,700 cycles

LT WING INBD FOREFLAP UPPER SURFACE IS DENTED. NOTE WAS LISTED ON PLT BUT HAS PROGRESSED IN LENGTH AND DEPTH. ACFT GROUNDED. REPAIRED DENT ON LT WING INBD FOREFLAP UPPER SURFACE IAW SRM 51-70-10, REPAIR 3 AND 4.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 47,871 hrs · 26,700 cycles

OTBD UPPER EDGE OF NR 2 SLAT DELAMINATED. REPAIRED OTBD UPPER EDGE OF NR 2 SLAT IAW SRM 51-70-10, PG 201M, REPAIR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,871 hrs · 26,700 cycles

LT WING INBD MIDFLAP UPPER SURFACE INBD END IS CHAFED. REPAIRED MIDFLAP SKIN IAW SRM 57-53-01, REP 3, FIG 201.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 47,871 hrs · 26,700 cycles

OTBD UPPER EDGE OF NR 2 SLAT DELAMINATED. REPAIRED OTBD UPPER EDGE OF NR 2 SLAT IAW SRM 51-70-10, PG 201, REPAIR 4.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,143 hrs · 26,275 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGNS AT L-1 DOOR, L-2 DOOR, RT FWD OVERWING EXIT, AND LT FWD OVERWING EXIT HAVE MULTIPLE LAMPS INOPATIVE. RELAMPED AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: SKIN — DENTED (BS 400) · airframe 46,038 hrs · 25,570 cycles

DENT ON FUSELAGE AFT OF L1 DOOR AT APPROXIMATELY BS 400 AND THREE FEET FROM TOP OF WINDOWS. REMOVED PAINT FROM DAMAGED AREA IAW AMM 51-21-11. INSPECTED DAMAGE WITHIN L = .085 W=.060 D=.011 AT BS 402 S7L IAW SRM 53-00-00. COMPLETED MEASUREMENT OF REMAINING SKIN THICKNESS ORIGINAL THICKNESS .035 MEASURED .030 DEEPEST BLEND AREA. COMPLETED HFEC OF BLENDED IAW MANUAL 51-00-00 PART 5 FIG 28, NO CRACKS NOTED. ON FURTHER INVESTIGATION, DEEP BURN PIT FOUND IN CENTER OF BLENDED AREA. REMOVED DAMAGE TO A DEPTH OF ENTIRE SKIN THICKNESS PENATRATING TO STRINGER IAW 400-53A. REPAIRED PER EA 400-53 & EA 08141.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,397 hrs · 24,625 cycles

RIGHT BULLNOSE EMERGENCY LIGHT INOP. RELAMPED RIGHT BULLNOSE EMERGENCY LIGHT, OPS CHECK GOOD PER AMM 33 51 21 962 001.

Part: SKIN — CRACKED (RT WING) · airframe 44,397 hrs · 24,625 cycles

RIGHT WING FIXED L/E SKIN IS CRACKED AND DELAMINATED UPPER SIDE AT SLAT ACTUATOR AREA. REPAIRED CRACKED AND DELAMINATED AREA PER ASA EA 400 57EA 06545.

Part: SUPPORT ANGLE — CRACKED (NR 2 PYLON) · airframe 44,397 hrs · 24,625 cycles

RIGHT WING NR 2 AFT PYLON O/B SUPPORT ANGLE L3 CRACKED AT AFT FASTENER. REPLACED RIGHT WING NR 2 AFT PYLON O/B SUPPORT ANGLE.

Part: WEB — CRACKED (HORIZ STAB) · airframe 44,397 hrs · 24,625 cycles

RT HORIZONTAL STAB O/B END CLOSER WEB AFT HOLES/UPPER AND LOWER FOR STAB TIP PANEL ARE ELONGATED AND CRACKED. REPLACED CLOSURE WEB FLANGE PLATE IAW SRM 51 40 02 AND BOEING DRAWING 65C25162.

Part: STRAP — CRACKED (FUSELAGE) · airframe 44,397 hrs · 24,625 cycles

FLOOR STRUCTURE STABILIZATION STRAP CRACKED. NO LIMITS ALLOWED, BS 312 WL 200 LBL 11. REMOVED CRACKED STRAP, INSTALLED NEW STABILIZATION STRAP PER DWG 65 45834 AND SRM 51 40 02.

Part: SKATE ANGLE — CRACKED (NR 1 PYLON) · airframe 44,397 hrs · 24,625 cycles

POSSIBLE CRACK ON NR 1 PYLON AFT O/B SKATE ANGLE AFT FASTENER HOLE. REPLACED NR 1 PYLON AFT O/B SKATE ANGLE PER SRM 51 40 02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 44,397 hrs · 24,625 cycles

FOUND LEFT WING I/B TRAILING EDGE (NO STEP PNL) I/B ANGLE AFT ATTACH FASTENER HOLE OVERSIZE AND WORN. ALSO POSSIBLE CRACK ABOVE THE FASTENER IN THE ANGLE. REPLACED IAW SRM 51 40 02 SEC 4 (B).

Part: SKIN — CRACKED (NR 1 SLAT)

NR 1 SLAT L/E BULLNOSE SKIN LOWER SURFACE CRACKED AT CENTER AUX TRACK ATTACH AREA 1.5FT FROM AFT EDGE. REPAIRED PER SRM 57-43-01.

Part: STRAP — CRACKED (FUSELAGE) · airframe 44,397 hrs · 24,625 cycles

E & E BAY STRAP CRACKED. REPLACED STRAP PER SRM 51 40 02.

Part: SKIN — DENTED (SPOILER) · airframe 57,368 hrs · 35,406 cycles

LEFT NR 3 FLIGHT PANEL HAS A DENT ON LOWER SKIN. REPAIRED DAMAGED AREA, FABRICATED FILLER AND DOUBLER.

Part: SKIN — DENTED (TE FLAP) · airframe 40,830 hrs · 22,499 cycles

RIGHT INBOARD AFT FLAP IS DENTED ON LWR SURFACE 9.5 INCHES FROM INBOARD EDGE 4.5 INCHES FROM T/E WITH EXPOSED COMPOSITE. REPAIRED RIGHT INBOARD FLAP IAW B737 400 SRM 51 70 06 REPAIR 2.

Part: FLAP — CHAFED (RT WING) · airframe 40,830 hrs · 22,499 cycles

RIGHT OUTBOARD FORE FLAP OUTBOARD END IS CHAFING ON FIXED TRAILING EDGE PANEL. REMOVED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW B747 400 SRM 57 53 01.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,830 hrs · 22,499 cycles

LEFT INBOARD AFT FLAP DELAM OUTBOARD TRAILING EDGE CORNER UPPER SIDE. REPAIRED LEFT INBOARD AFT FLAP UPPER SIDE IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,830 hrs · 22,499 cycles

LEFT INBOARD AFT FLAP DELAMINATED TRAILING EDGE OUTBOARD SIDE LOWER. REPAIRED LEFT INBOARD AFT FLAP LOWER SIDES IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFTER REMOVAL OF TRANSITION PANEL FOUND FRAME CRACKED AT STA 460 ABOVE STR 25L. REMOVED DAMAGED AREA, FABRICATED, LOCATED, DRILLED DOUBLER, FABRICATED FREEZE PLUG AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — BENT (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

DURING CORROSION REMOVAL FOUND SHEAR TIE BENT AND CREASED AT 747 STRINGER 27 TO 26R AFT PIT. REMOVED SHEAR TIE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER IAW B737 400 SRM 53 00 07.

Part: SKIN — MISREPAIRED (HORIZ STAB) · airframe 37,804 hrs · 20,710 cycles

PREVIOUS REPAIR LT HORIZONTAL L/E IMPROPER STA 220 226. REMOVE EXISTING REPAIR, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR IAW B737 400 SRM 55 10 01.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 37,804 hrs · 20,710 cycles

RIGHT CARGO TIEDOWN TRACK CRACKED AT STA 727F ON LOWER FLANGE. REMOVED DAMAGED TRACK, FABRICATED NEW CARGO TIE DOWN TRACK, DRILLED FITTED TRACK, PRIMED AND INSTALLED REPLACEMENT REPAIR IAW B737 400 SRM 51 20 01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT PIT INTERCOSTAL AFT CLIP STR 25L BETWEEN STA 727A 727B CRACKED. REMOVED DAMAGED CLIP, FABRICATED, LOCATED, TREATED, PRIMED, INSTALLED NEW CLIP IAW BOEING DWG 66 13842 AND B737 400 SRM 51 40 02.

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

L2 DOOR LOWER PRESSURE RETAINER CORRODED AT STA 954. REMOVED LOWER SEAL DEPRESSOR RETAINER NEW PART LOCATED, DRILLED AND INSTALLED RETAINER IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

L2 DOOR STUB FRAME CRACKED AT STA 954 FOUND DURING OPEN UP FOR SKIN REPAIR. REMOVED DAMAGED SECTION OF FRAME, FABRICATED, LOCATED, DRILLED, INSTALLED REPAIR ANGLE IAW B737 400 SRM 51 40 02.

Part: WEB — GOUGED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT CARGO PIT SILL WEB LOWER SILL BEAM VERTICAL WEB GOUGED BETWEEN STA 800 807 ON O/B SIDE. REMOVED SILL BEAM, RECEIVED NEW PART, LOCATED AND DRILLED HOLES ON NEW PART, INSTALLED LOWER SILL BEAM VERTICAL WEB IAW B737 400 SRM 51 40 05.

Part: SKIN — BENT (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

FUSELAGE SKIN BENT BELOW L2 DOOR LOWER HINGE. REMOVED ORDERED AND RECEIVED NEW STOP FITTING, DRILLED AND INSTALLED FITTING IAW B737 400 SRM 51 40 02 CAUSING SKIN TO BE BROUGHT BACK TO ORIGINAL CONTOUR.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 37,804 hrs · 20,710 cycles

LT HORIZONTAL STAB L/E GOUGED STA 190.34. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED PLATE AND FILLER IAW B737 400 SRM 55 10 01.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 37,804 hrs · 20,710 cycles

LEFT HORIZONTAL L/E GOUGED STA 139.55. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737 400 SRM 55 10 01.

Part: FRAME — DENTED (FUSELAGE) · airframe 32,592 hrs · 14,359 cycles

FRAME DENTED STA 727C BETWEEN STR 24 25R. CUT OUT DAMAGE, FABRICATED AND INSTALLED ANGLE IAW B737 400 SRM 51 70 11.

Part: SHEAR WEB — DAMAGED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

L1 DOOR SHEAR WEB MISDRILLED STA 342 WL 208.1. REMOVED SHEAR WEB, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW WEB AND DOUBLER IAW B737 400 SRM 51 40 02.

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

FWD FRAME STA 500A CORRODED BETWEEN STR 28L 28L. REMOVED DAMAGED SECTION OF FRAME, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED DOUBLER AND TRIPLER IAW ASA EA 400 53 EA 01205.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 37,804 hrs · 20,710 cycles

LT HORIZONTAL STAB L/E GOUGED STA 229.13. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737 400 SRM 55 10 01.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 37,804 hrs · 20,710 cycles

LT HORIZONTAL STAB L/E GOUGED STA 218.43. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR FILLER IAW B737 400 SRM 55 10 01.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 32,592 hrs · 14,359 cycles

LT HORIZONTAL STAB L/E IS GOUGED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PLATE AND FILLER IAW B737 400 SRM 55 10 01.

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

AFT PIT FRAME 787 CORRODED BETWEEN STR 26R 27R. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED SHEAR TIE FRAME REPAIR IAW B737 400 SRM 53 00 07.

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

FWD PIT SHEAR TIE CORRODED STA 500B STR 27L 28L. REMOVED CORRODED SHEAR TIE, FABRICATED, TREATED, PRIMED AND INSTALLED NEW SHEAR TIE IAW B737 400 SRM 53 30 53.

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

LT AFT WEB OF STA 986 FLOORBEAM LBL 32 CORRODED. REMOVED CORRODED WEB, FABRICATED, TREATED, LOCATED, PRIMED, TOP COATED AND INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

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

LT AFT WEB OF STA 986 FLOORBEAM LBL 32 CORRODED. REMOVED CORRODED WEB, FABRICATED, TREATED, LOCATED, PRIMED, TOP COATED AND INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Part: AILERON — DELAMINATED (LT WING) · airframe 37,804 hrs · 20,710 cycles

LT AILERON LWR BOTTOM I/B EDGE DISBONDED. PREPPED DELAMINATED AREA, BONDED REPAIR IAW B737 400 SRM 51 70 03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

FRAME CRACKED AT RIVET 1 INCH LONG. REMOVED FRAME, FABRICATED, CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR ANGLES AND FRAME IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

FRAME CRACKED AT RIVET STA 867 STR 8R AND 9R. REMOVED FRAME, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR ANGLES IAW B737 400 SRM 53 60 07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

CABIN SUPPORT RT FRAME ANGLE CRACKED AT STA 601. REMOVED DAMAGED AREA, FABRICATED, LOCATED, DRILLED, PRIMED AND INSTALLED ANGLE IAW B737 400 SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT CABIN APB LOWER MEMBRANE WEB CRACKED STA 1032 STR 17 LBL 15. REMOVED CRACKED WEB, RECEIVED NEW WEB, LOCATED, DRILLED, INSTALLED IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

FRAME CRACKED FROM LOWER FASTENER TO BOTTOM EDGE OF FRAME FWD SIDE STA 616 JUST BELOW STR 17R. REMOVED DAMAGED AREA, FABRICATED, LOCATED, DRILLED, PRIMED AND INSTALLED REPAIR IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT PIT FRAME FWD LOWER FLANGE CORRODED STA 272F BETWEEN STR 27R 26R. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED SHEAR TIE AND FILLER REPAIR IAW B737 400 SRM 53 00 07.

Part: FRAME — BENT (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT PIT FRAME UPPER FLANGE STA 907 DENTED BETWEEN 23L AND 22L BENT. REMOVED FACTORY FRAME AND CUT OUT DAMAGED AREA, FABRICATE, TREATED, PRIMED TOP COATED AND INSTALLED DOUBLER 2 FILLERS AND NEW SPLICE IAW B737 400 SRM 51 70 11.

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

AFT PIT FRAME STA 727C CORRODED BETWEEN STR 26R 27R. REMOVED DAMAGED SECTION OF FRAME SHEAR TIE, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07.

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

AFT PIT STRINGER TIE CORRODED STA 747 STR 25R. REMOVED CORRODED STRINGER TIE, RECEIVED NEW TIE, LOCATED, DRILLED, INSTALLED TIE IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — BENT (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT PIT STRINGER TIE BENT STA 727B STR 25L. REMOVED STRINGER TIE, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED SHEAR TIE IAW B737 400 SRM 51 30 1.

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

AFT PIT FRAME LWR FLANGE STA 787 CORRODED BETWEEN STR 25R 26R. REMOVED CORRODED SHEAR TIE, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT PIT FRAME UPPER FLANGE STA 727E ABOVE STR 22L. REMOVED DAMAGED ARE, FABRICATED, LOCATED, TREATED, PRIMED, TOP COATED AND INSTALLED IAW B737 400 SRM 51 70 11.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

AFT PIT FRAME UPPER FLANGE STA 727C DENTED BETWEEN 24L AND 25L. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED TOP COATED AND INSTALLED REPAIR PART IAW B737 400 SRM 51 70 11.

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

AFT CABIN FLOORBEAM CORRODED STA 986 RBL 42 44. CUT OUT DAMAGED SECTION, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED FLOOR BEAM REPAIR IAW EA 400 53EA 01199.

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

FWD PIT STA 500E STR 28L 28R FRAME CORRODED ON SKIN SIDE. CUT OUT DAMAGED AREA, FABRICATED INSTALLED FRAME REPAIR IAW B737 400 SRM 53 00 07.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

R2 DOOR MOP SILL CORRODED STA 954 992 RBL 54. REMOVED CORRODED MOP SILL, REVIEWED, LOCATED, DRILLED AND INSTALLED NEW MOP SILL IAW B737 400 SRM 51 40 02.

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

AFT CABIN FLOORBEAM CORRODED STA 986 RBL 42 44. CUT OUT DAMAGED SECTION, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED FRAME REPAIR IAW EA 400 53EA 01199.

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

FWD PIT STA 500B STR 28L 28R FRAME CORRODED FWD SIDE. CUT OUT DAMAGED AREA, FABRICATED, INSTALLED FRAME REPAIR IAW B737 400 SRM 53 00 07.

Part: MOUNT FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 37,804 hrs · 20,710 cycles

L1 DOOR AFT GIRT BAR FITTING MOUNT CORRODED. REMOVED CORRODED MOUNT FITTING. RECEIVED AND INSTALLED NEW FITTING IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

L1 DOOR OPENING INNER CHORD STA 344 CORRODED. REMOVED CORRODED CHORD, RECEIVED NEW MOP SILL CHORD, LOCATED, DRILLED, TREATED AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

RT AFT EMERGENCY EXIT HATCH CUTOUT LWR SILL PLATE CORRODED. REMOVED CORRODED SEAL PLATE. FORMED HEAT TREATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW SILL PLATE IAW B737 400 SRM 53 60 15.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

LT FWD EMERGENCY EXIT HATCH CUTOUT LWR SILL PLATE IS CORRODED. REMOVED CORRODED SEAL PLATE. FORMED HEAT TREATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW SILL PLATE IAW B737 400 SRM 53 60 15.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

RT FWD EMERGENCY EXIT HATCH CUTOUT LWR LATCH FITTING HAS CORROSION AROUND IT. REMOVED CORRODED SEAL PLATE. FORMED HEAT TREATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW SILL PLATE IAW B737 400 SRM 53 60 15.

Part: SKIN — GOUGED (FUSELAGE) · airframe 37,804 hrs · 20,710 cycles

FUSELAGE SKIN GOUGED AFT OF L2 DOOR STA 1000 BETWEEN STR 13R 14R. REMOVED DAMAGED SKIN, RECEIVED, LOCATED AND DRILLED, TREATED PRIMED AND INSTALLED NEW REPLACEMENT SKIN IAW B737 400 SRM 51 40 02.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 37,804 hrs · 20,710 cycles

C1 DOOR SKIN HAS 5 EA/ DENTS THAT ARE GOUGED OR CREASED OUT OF LIMITS IAW B 737 400 SRM 52 00 01. REMOVED DAMAGED SKIN, FABRICATED, INSTALLED NEW SKIN IAW B737 400 SRM 51 40 02.

Part: GUIDE ARM — WORN (L1 DOOR) · airframe 36,632 hrs · 20,021 cycles

L1 DOOR GUIDE ARM BINDING AND POPPING UPPER HINGE LOWER CAM PLATE WORN. INITIATED MIG2C 227000. REPLACED UPPER HINGE LOWER GUIDE PLATE GUIDE ARM ASSY, OPS CHECK GOOD REF MM 52 11 41 AND MM 52 11 00.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 34,113 hrs · 18,654 cycles

RIGHT I/B TRAILING EDGE FLAP LOWER SKIN HAS A 2" X 1" HOLE TEAR 9.5" FWD OF TRAILING EDGE 16" I/B OF O/B EDGE (TEMPORARY REPAIR). PREPARED DAMAGED AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, PREPARED AREA AND BONDED IAW B737 SRM 51 70 10. PREPARED AND INSTALLED GLASS OVERLAY IAW B737 51 70 70.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 34,113 hrs · 18,654 cycles

LT WING INBOARD GROUND SPOILER LOWER SURFACE DELAMINATED. REMOVED DAMAGED AREA OF SKIN. FABRICATED FILLER AND EXTERNAL DOUBLER, PREPARED AREA AND BONDED IAW B737 400 PAR 7 8 11 12 AND 20.

Part: SKIN — DENTED (RT WING SPOILER) · airframe 34,113 hrs · 18,654 cycles

RT WING INBOARD GROUND SPOILER LOWER SURFACE HAS MULTIPLE DENTS PREPARED AREA OF DAMAGE FOR REPAIR 4 IAW SRM 57-70-01 PGS 201-202. FABRICATED DOUBLERS AND BONDED IAW SRM 57-70-01 REPAIR 2.

Part: SKIN — CHAFED (T/E FLAP) · airframe 34,113 hrs · 18,654 cycles

RIGHT WING NR 4 L/E SLAT LOWER SURFACE OF T/E WEDGE CHAFED IN CENTER AREA. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER, PREPARED AREA AND BONDED IAW B737 SRM 51 70 10 PAR 7 8 11 15 AND 20.

Part: SKIN — CHAFED (FOREFLAP) · airframe 34,113 hrs · 18,654 cycles

RIGHT WING O/B AFT FORE FLAP UPPER SURFACE CHAFED IN CENTER AREA. REMOVED DAMAGED AREA OF SKIN, FABRICATED FILLER AND REPAIR DOUBLER, PREPARED AREA AND BONDED IAW BOEING SRM 51 70 10 PAR 7 8 11 12 AND 20.

Part: SKIN — CHAFED (RT WING FLAP) · airframe 34,113 hrs · 18,654 cycles

RT WING O/B FOREFLAP LEADING EDGE IS CHAFED AT O/B CORNER REMOVED DAMAGE FROM SKIN ON L/E. FABRICATED DRILLED AND INSTALLED A REPAIR DOUBLER IAW SRM 57-53-01 FIG 201.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 34,113 hrs · 18,654 cycles

LT WING NR 1 SPOILER DENTED ON UPPER SURFACE PREPARED AREA OF DAMAGE FOR REPAIR 4 IAW SRM 57-70-01 PGS 201-202. FABRICATED DOUBLER AND BONDED IAW SRM 57-70-01 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAPS) · airframe 34,113 hrs · 18,654 cycles

LT INBOARD AFT FLAP HAS MULTIPLE DENTS ON INBOARD UPPER SURFACE SMALL AREA PREPARED DAMAGED AREA IAW B737 400 SRM 51 70 10. REPAIR 2 FABRICATED REPAIR DOUBLER PREPARED AND BONDED IAW B737 400 SRM 51 70 10 PAR 11 12 AND 20.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 34,113 hrs · 18,654 cycles

LT WING NR 3 SPOILER DENTED ON UPPER SURFACE PREPARED AREA OF DAMAGE FOR REPAIR 4 IAW SRM 57-70-01 PGS 201 202. FABRICATED DOUBLER AND BONDED IAW SRM 57-70-01 REPAIR 2.

Part: SKIN — DENTED (TE FLAPS) · airframe 34,113 hrs · 18,654 cycles

LT INBOARD FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA,FABRICATED FILLER AND DOUBLER, PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 PER 7 8 11 12 AND 20.

Part: SKIN — DENTED (FORE FLAP) · airframe 30,624 hrs · 16,752 cycles

RT WING OB FORE FLAP IS DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57 53 01 FIG 201.

Part: SKIN — DENTED (FORE FLAP) · airframe 30,625 hrs · 16,752 cycles

LEFT WING I/B FORE FLAP HAS SMALL DENT ON LWR SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (FORE FLAP) · airframe 30,625 hrs · 16,752 cycles

LEFT WING I/B FORE FLAP HAS CLUSTER OF DENTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (FORE FLAP) · airframe 30,625 hrs · 16,752 cycles

LEFT WING I/B FORE FLAP HAS A DENT ON LWR SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (FORE FLAP) · airframe 30,625 hrs · 16,752 cycles

LEFT I/B FORE FLAP HAS CLUSTERS OF DENTS ON LWR SURFACE. REMOVED DAMAGED SKIN, FABRICATED AND REPLACED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (SPOILER) · airframe 30,625 hrs · 16,752 cycles

LEFT WING I/B SPOILER HAS SEVERAL CLUSTERS OF SMALL DENTS ON LWR SURFACE. PREPPED LWR SKIN AREAS FOR REPAIR FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51-70-10 REPAIR 4.

Part: FLOOR SUPPORT — CRACKED (FS 727E)

PAE - FLOOR SUPPORT CRACKED AT FRAME FASTENERS. REPAIRED CRACKED FLOOR SUPPORT PER B737-200 SRM 53-00-53. (M)

Part: SHEAR TIE — BENT (FS 460)

PAE - FOUND FRAME SHEAR TIE BENT. REPAIRED FRAME SHEAR TIE AT BS 460, RBL 8 PER EA 5330-02006. (M)

Part: CARGO TRACK — CORRODED (FS 945-915)

PAE - FOUND CORROSION AT LEFT CARGO TIE DOWN TRACK AT NUT PLATE LOCATIONS. REMOVED CORROSION ON LEFT CARGO TIE DOWN NUT PLATE LOCATIONS, FABRICATED REPAIR PARTS AND INSTALLED PER B737-200 SRM 53-62-53. (M)

Part: FRAME — NICKED (FS 794)

PAE - FOUND AFT CARGO BAY DOORWAY FORWARD FRAME IS NICKED. REPLACED FRAME AND DOUBLER PER B737-200 SRM 51-40-02. (M)

Part: SILL — CORRODED (FS 987)

PAE - FOUND CORROSION ON RIGHT MOPSILL. REMOVED AND REPLACED MOPSILL PER B737-200 SRM 53-60-15. (M)

Part: FRAME — CRACKED (FS 440)

PAE - FRAME CRACKED AT BIN RAIL SUPPORT BETWEEN STRINGER 8 LEFT AND 9 LEFT AT INBOARD FASTENER. REPAIRED DAMAGED FRAME AT BIN RAIL SUPPORT PER B737-200 SRM 53-00-07. (M)

Part: SKIN — DENTED (FS 460)

PAE - FOUND EXTERNAL SKIN DENT. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED PER EA 5330-02006. (M)

Part: SKIN — CHAFED (FS 860-887)

PAE - FUSELAGE SKIN IS CHAFED LT AND RT SIDES, BS 860 TO 887 STRINGER 2 LEFT TO STRINGER 2 RT. REPAIRED SKIN PER EA 5360-01043, ER 05-4273. (M)

Part: SEAT TRACK — GOUGED (FS 320-540)

PAE - FOUND SEAT TRACK AT WL 208, RBL 45 HAS MECHANICAL DAMAGE AT BS 520 AND 540. SEAT TRACK AT WL 208, RBL 45 GOUGED 1 INCH BY 1 INCH BY 40 INCH OUT OF LIMITS. REPAIRED TRACK PER SRM 53-00-52 PAGE 201 FIGURE 21. (M)

Part: INTERCOSTAL — CRACKED (FS 767)

PAE - WHILE WORKING CARD NR 4953433, FOUND INTERCOSTAL WEB DENTED. REMOVED AND REPLACED INTERCOSTAL WEB IN AFT CARGO BAY PER SRM 53-00-04. (M)

Part: FRAME — CRACKED (FS 987)

PAE - FOUND FRAME CRACKED AT BIN RAIL SUPPORT. REPAIRED FRAME CRACK PER B737-200 SRM 53-00-07. (M)

Part: PAN — CORRODED (FS 950)

PAE - FOUND CORROSION, FORWARD LAVATORY DUP SERVICE PAN DOUBLER. REMOVED AND REPLACED DOUBLER PER B737-200 SRM 51-40-02. (M)

Part: FRAME — CRACKED (FS 940)

PAE - FOUND FRAME CRACKED AT BIN RAIL SUPPORT. REPAIRED FRAME CRACK PER B737-200 SRM 53-00-07. (M)

Part: SKIN — DENTED (FS 795-846)

PAE - AFT CARGO DOOR HAD 4 SMALL DENTS AND CREASES AT BOTTOM AFT CORNER. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW B737-400 SRM 52-30-01. (M)

Part: SKIN — DENTED (FS 795-846)

PAE - FOUND AFT CARGO DOOR OUTER SKIN HAS 4 SMALL DENTS AND CREASE AT BOTTOM AFT CORNER. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW B737-400 SRM 53-30-01. (M)

Part: SPLICE — CORRODED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

FUSELAGE SKIN BUTT SPLICE HAS CORROSION AT EXISTING REPAIR. REMOVED EXISTING BUTT SPLICE, FABRICATED AND INSTALLED NEW SPLICE IAW SRM. (K)

Part: CARGO TRACK — CORRODED (FS 945-915)

PAE - CORROSION AT LEFT CARGO TIE DOWN TRACK AN NUT PLATE LOCATIONS. REMOVED CORROSION ON LEFT CARGO TIE DOWN NUT PLATE LOCATIONS. REMOVED CORROSION ON LEFT CARGO TIE DOWN NUT-PLATE LOCATIONS, FABRICATED AND INSTALLED REPAIR PARTS B737-200 SRM 53-60-53.

Part: SEAT TRACK — DAMAGED (BS 520-540)

PAE - FOUND SEAT TRACK AT WL 208, RBL 45 HAS MECHANICAL DAMAGE AT BS 520 AND 540. SEAT TRACK AT WL 208, RBL 45 GOUGED 1 INCH BY 1 INCH BY .040 OUT OF LIMITS REPAIRED TRACK PER B737-200 SRM 53-00-52 PAGE 201 FIG 20. (M)

Part: SEAT TRACK — GOUGED (BS 536)

PAE - FOUND SEAT TRACK SUPPORT ANGLE GOUGED ON OUTBOARD SIDE. REMOVED AND REPLACED SEAT TRACK SUPPORT ANGLE AT BS 536, RBL 45 WL 206, PER B737-200 SRM 51-40-02. (M)

Part: INTERCOSTAL — CRACKED (FS 767-787)

PAE - WHILE WORKING CARD NUMBER 4953433, FOUND INTERCOSTAL WEB DENTED. REMOVED AND REPLACED INTERCOSTAL WEB IN AFT CARGO BAY PER B737-200 SRM 53-00-04. (M)

Part: SHEAR TIE — BENT (BS 460) · airframe 26,880 hrs · 14,747 cycles

FWD CARGO BAY SHEAR TIE BENT. REMOVED BENT SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM. (K)

Part: CLIP — DAMAGED (BS 500C) · airframe 26,880 hrs · 14,747 cycles

DAMAGED STRINGER CLIP AT FWD CARGO BAY. REMOVED AND REPLACED STRINGER CLIP IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

PAE FRAME CRACKED BIN RAIL SUPPORT BETWEEN STR 8 AND 9 LT AT IB FASTENER. REPAIRED DAMAGED FRAME AT BIN RAIL SUPPORT IAW SRM. (K)

Part: FRAME — CRACKED (APU BAY) · airframe 26,880 hrs · 14,747 cycles

RT APU CHORD AT FWD HINGE CUTOUT CRACKED. REMOVED AND REPLACED CHORD IAW SRM. (K)

Part: FLOOR SUPPORT — CRACKED (BS 727E) · airframe 26,880 hrs · 14,747 cycles

PAE - FLOOR SUPPORT CRACKED AT FRAME FASTENERS. REPAIRED CRACKED FLOOR SUPPORT IAW SRM. (K)

Part: SILL — CORRODED (BS 987) · corrosion level 2 · airframe 26,880 hrs · 14,747 cycles

CORROSION ON RT MOPSILL AT BS 987+ 10 INCHES, RBL 48. REMOVED AND REPLACED RT MOPSILL AT BS 987 + 10 INCHES, RBL 48 IAW SRM. (K)

Part: SHEAR WEB — CRACKED (BS 998) · airframe 26,880 hrs · 14,747 cycles

SHEAR WEB CRACKED AT BSTA 998, RBL 41, WL 208. REMOVED AND REPLACED SHEAR WEB AT BSTA 986.5 - 1016, RBL 29-41, WL 208 IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,880 hrs · 14,747 cycles

CORROSION ON LT MOPSILL. REMOVED AND REPLACED LT MOPSILL AT BSTA 987+ 10 INCHES, LBL 48. (K)

Part: FRAME — CORRODED (BS 995) · airframe 26,880 hrs · 14,747 cycles

CORROSION ON FRAME AT BS 995, RBL 46, WL 209. REPAIRED FRAME AT BSTA 995, RBL 46, WL 209 IAW SRM. (K)

Part: CLIP — GOUGED (BS 460) · airframe 26,880 hrs · 14,747 cycles

FWD CARGO BAY STRINGER CLIP GROUGED. REMOVED AND REPLACED STRINGER CLIP IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 14,747 hrs

PAE - FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

BSTA 380, FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

BSTA 480, FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

BSTA 787 FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K)

Part: SKIN — CHAFED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

RT EMPENNAGE SKIN CHAFED AT RT HORIZONTAL STABILIZER AFT SPAR LOWER CUTOUT. FOUND RT EMPENNAGE SKIN CHAFED AT RT HORIZONTAL STABILIZER AFT SPAR CUTOUT OUT OF LIMITS. REMOVED AND REPLACED SKIN SECTION AND TRACK FILLER. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

BSTA 480 FRAME IS CRACKED AT BIN RAIL SUPPORT BETWEEN STR 8 LT AND 9 LT AT IB FASTENER. CUTOUT DAMAGE AT BSTA 480 FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR. (K)

Part: STIFFENER — CHAFED (BS 1091) · airframe 26,880 hrs · 14,747 cycles

APU BAY STIFFENER CHAFED ON FWD END. REMOVED AND REPLACED IAW SRM. (K)

Part: ANGLE — BENT (FUSELAGE) · airframe 26,880 hrs · 14,747 cycles

LT L-ANGLE BENT AT BSTA 178, WL 207, LBL 24. REMOVED AND REPLACED BENT ANGLE IAW SRM. (K)

Part: FRAME — DENTED (BS 500E) · airframe 26,880 hrs · 14,747 cycles

FWD CARGO BAY FRAME IS DENTED. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,880 hrs · 14,747 cycles

CORROSION ON FLOORBEAM AFT FLANGE. REMOVED CORROSION ON FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,880 hrs · 14,747 cycles

CORROSION ON FWD GALLEY MOPSILL. REPLACED MOPSILL. (K)

Part: SKIN — DENTED (LT HORIZ STAB)

OAK - DURING C-CHECK, FOUND LEFT HORIZONTAL STAB LE INBOARD SIDE DENTED. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SIDE WALL SUPPORT AT BS 727G AND WL 156. REPAIRED IAW SRM. (M)

Part: SPLICE PLATE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SPLICE PLATE STATION 727F PLUS 6 AND WL 156. REPAIRED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON 947 BULKHEAD L-ANGLE. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND DENT ON FLOOR SUPPORT AT BS 794 AND WL 156. REPAIRED IAW EA. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT AT BS 757-797 AND WL 156. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND DAMAGED FLOOR SUPPORTS AT BS 747 TO 817 WL 156 AND LEFT/RIGHT BL 8-12. REPAIRED IAW SRM AND EA. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON BULKHEAD SUPPORT ANGLE AT BS 500G WL 156 AND LBL 24. REPAIRED IAW SRM. (M)

Part: SPLICE PLATE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SPLICE PLATE AT STATION 727F PLUS 6 AND WL 156. REPAIRED IAW SRM. (M)

Part: SWITCH — DIRTY (RT MLG DOOR)

AFTER GEAR RETRACTION-GEAR DOOR LIGHT ILLUMINATED. RECYCLED GEAR ONCE. GEAR DOOR LT. EXTINGUISHED. CLEANED RT MAIN GEAR DOOR SWITCH. OPS CHECK GOOD IAW 727 MM CH 32-61-01.

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE AT ROW 10-12. REMOVED AND REPLACED LIGHT ASSEMBLY OPERATIONAL CHECK GOOD. (M)

Part: PCU — FAULTY (RUDDER)

SEA - DURING TEST FLIGHT, LEFT RUDDER RESTRICTION IN FLIGHT. LEFT RUDDER COULD BE MOVED APPROX 2 INCH AND STOPPED, STANDBY HAD MORE AUTHORITY BUT HAS RESTRICTIONS. REMOVED AND REPLACED PCU, OPS NORMAL. (M)

Part: ROD — OUT OF ADJUST (RT COCKPIT)

ANC - PRIOR TO FLT 92, THE CREW REPORTED THAT THEY WERE UNABLE TO CLOSE THE FIRST OFFICERS SLIDING WINDOW. INSPECTED AND FOUND THE PIN GUIDE ROD OUT OF ADJUSTMENT. REPOSITIONED PIN GUIDE ROD AND THE WINDOW SLIDING WINDOW OPERATED NORMALLY. (M)

Part: BEARING — SEIZED (L1 DOOR)

SEA - PRIOR TO FLT 322, THE L1 DOOR WAS FOUND TO BE HARD TO OPEN. REPLACED CRANK ARM BEARING AND DOOR OPERATED NORMALLY.