N788AS

Part: STRUCTURE — CRACKED (BS 1040) · airframe 57,254 hrs · 32,310 cycles

LIGHTNING HOLE AT AFT TAIL COMPARTMENT ENTRANCE BELOW LEFT CABLE PULLEY BRACKET IS CRACKED. ACFT GROUNDED. REPAIRED LIGHTNING HOLE IN WEB SUPPORT ASSY AT BS 1040 IN AFT TAIL COMPARTMENT IAW EA 400-53EA-15819.

Part: SOCKET — DEFECTIVE (EMERGENCY LIGHT) · airframe 54,308 hrs · 30,448 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. TAGGED EMERGENCY LIGHTS SWITCH TO OFF. REPLACED DEFECTIVE LAMP SOCKET TO L730 REF W/D 33-51-12 AND EQUIP LIST. REMOVED TAD, OPS TEST GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 54,074 hrs · 30,325 cycles

L1 DOOR OVERHEAD EXIT SIGN AND R1 DOOR LWR EXIT SIGN BOTH INOPERATIVE. ACFT GROUNDED. R & R BATTERY PACK FOR L1 DOOR OVERHEAD EXIT SIGN AND R1 DOOR LWR EXIT SIGN IAW MM 33-51-51-962-015.

Part: FRAME — CORRODED (BS 727F) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

AFT CARGO BAY RT SIDE AT BS 727F BETWEEN S26-27R AFT SIDE OF FRAME CORRODED. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-4.

Part: FRAME — CORRODED (BS 727F) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

AFT CARGO BAYBS 727F BETWEEN S26-27R AFT SIDE OF FRAME CORRODED. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-4.

Part: SHEAR TIE — CORRODED (BS 500F) · airframe 54,074 hrs · 30,325 cycles

FWD CARGO BAY AT BS 500F JUST INBD OF S26L FWD SIDE OF SHEAR TIE HAS CORROSION. ACFT GROUNDED. REPAIRED IAW SRM 53-00-07-2R-17.

Part: ATTACH ANGLE — BROKEN (HORIZONTAL STAB) · airframe 54,074 hrs · 30,325 cycles

RIGHT HORIZONTAL STABILIZER UPPER FWD ATTACH ANGLE BROKEN AT 9219 ACCESS PANEL. ACFT GROUNDED. REPAIRED RT HORZIZONTAL STABILIZER INBD UPPER ATTACH ANGLE IAW EA CMPT-55EA-12914. THIS IS A CATERGORY B REPAIR WITH FIRST AND SECOND STAGE APPROVAL. THIRD STAGE APPROVAL IS REQUIRED BEFORE 66,000 FLIGHT CYCLES AIR FRAME AGE. A TASK NOTIFICATION SENT. CURRENT CYCLES ON ACFT AT TIME OF REPAIR IS 3,325.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,074 hrs · 30,325 cycles

FUSELAGE SKIN IS CRACKED 0.156 INCHES LONG AT THE R1 DOOR CUTOUT FWD EDGE OF LWR HINGE CUTOUT. ACFT GROUNDED. REPAIRED SKIN AT R1 DOOR CUTOUT AT LOWER HINGE CUTOUT IAW EA AD20140521-400-53-104.

Part: STRINGER CLIP — CRACKED (BS 947) · airframe 54,074 hrs · 30,325 cycles

AFT CARGO BAY STRINGER CLIP BS 947 S25R IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0, PAR 7.

Part: STRINGER CLIP — CRACKED (BS 907) · airframe 54,074 hrs · 30,325 cycles

STRINGER CLIP AT BS 907, S8L IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 54,074 hrs · 30,325 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727) · airframe 54,074 hrs · 30,325 cycles

STRINGER CLIP AT BS 727C, S6R IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 54,074 hrs · 30,325 cycles

STRINGER CLIP AT BS 380, S4R IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 54,074 hrs · 30,325 cycles

STRINGER CLIP BS 727C S7R CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: CHANNEL — CORRODED (BS 947-986) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

MOP SILL IN FRONT OF LT AFT ENTRY DOOR FROM BS 947.5 - 986.5 SEVERAL AREA CORRODED. ACFT GROUNDED. REMOVED CORROSION ON MOP SILL, FOUND OUT OF LIMITS, REMOVED DAMAGED MOP SILL AND INSTALLED NEW MOP SILL IAW SRMS 53-60-15-1A-1, 51-40-02-0G-0W.

Part: ATTACH ANGLE — CORRODED (BS 967) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

ATTACH ANGLE CORRODED BS 967 S23L. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0.

Part: CHANNEL — CORRODED (BS 947-986) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

MOP SILL IN FRONT OF RT AFT ENTRY DOOR FROM S 947.5-986.5 SEVERAL AREAS CORRODED. ACFT GROUNDED. REPLACED MOP SILL IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 54,074 hrs · 30,325 cycles

STRINGER CLIP BS 727C S5R CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: BRACKET — CORRODED (BS 947) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

AFT CARGO BAY LOWER FRAME BRACKET CORRODED BS BS 947, S25R . ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101. R & R BRACKET IAW SRM 51-40-02-06.

Part: ATTACH ANGLE — CORRODED (BS 967) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

ATTACH ANGLE CORRODED BS 967 S23L. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0 PAR DW-1.0.

Part: BAFFLE — CRACKED (BS 500F-500G) · airframe 54,074 hrs · 30,325 cycles

FORWARD CARGO BAY BS 500G, S26R, OTBD SIDE OF INTERCOSTAL, BAFFLE, UPPER END HAS A ONE INCH CRACK. ACFT GROUNDED. R & R BAFFLE IAW SRM 51-40-02-0G-0.

Part: CUSP WEB — CORRODED (BS 827-847) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

AFT CABIN LT SIDE CUSP WEB CORRODED AT BETWEEN BS 827 - 847. ACFT GROUNDED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-60-13-1A-1, FIG 101. R & R CUSP WEB IAW SRM 51-40-02-0.

Part: CARGO TRACK — CRACKED (BS 767-827) · airframe 54,074 hrs · 30,325 cycles

AFT CARGO BAY LT SIDE CARGO TRACK CRACKED. ACFT GROUNDED. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: SEAT TRACK — GOUGED (BS 480-520) · airframe 54,074 hrs · 30,325 cycles

CABIN SEAT TRACK FROM BS 480-520, LBL 45 GOUGED. ACFT GROUNDED. BLENDED GOUGES, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1, REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-2.

Part: CHANNEL — CORRODED (BS 270-370) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

FWD WET AREA, L1 DOOR MOP SILL CORRODED. ACFT GROUNDED. REMOVED MOP SILL AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 54,074 hrs · 30,325 cycles

FWD WET AREA BS 312 FLOORBEAM CORRODED LBL 10 - RBL 10. ACFT GROUNDED. REPAIRED FLOORBEAM UPPER TEE IAW SRM 53-10-51.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 54,074 hrs · 30,325 cycles

LEFT WING L/E NR 2 SLAT UPPER INBD CORNER SURFACE REPAIR DOUBLER IS DELAMINATED. ACFT GROUNDED. REPAIRED LT WING L/E NR 2 SLAT LOWER & UPPER INBD SKIN CORNER IAW SRM 51-70-10-2R-0, REP 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 54,074 hrs · 30,325 cycles

LEFT WING INBD FORE FLAP OTBD EDGE IS CHAFED. ACFT GROUNDED. REPAIRED LT WING INBD FORE FLAP OTBD EDGE IAW SRM 51-70-10, REP 4.

Part: FITTING — CORRODED (NLG) · airframe 52,800 hrs · 29,567 cycles

NLG RETRACT ACTUATOR UPPER ATTACH BEARING IS STIFF & RUSTED. ACFT GROUNDED. REMOVED BEARING FROM NLG RETRACT ACTUATOR UPPER FITTING. FOUND PITTING IN BORE OF FITTING. FITTING BORE AT MAXIMUM DESIGN DIMENSION, REF DWG 65C10300. REMOVED FITTING REF SRM 51-40-02. CLEANED AND REFINISHED FITTING SUPPORT STRUCTURE MATING SURFACE REF AMM 51-21. DRILLED 10EA HOLES IN VERTICAL LEG OF NEW FITTING .247 DIA. REF SRM 51-40-02. DRILLED 14 EA HOLES IN HORIZONTAL LEG OF FITTING AND TOUCHED UP COUNTERBORES IAW DWG. 65C10300. INSTALLED NEW FITTING AND FASTENERS WET WITH SEALANT IAW SRM 51-40-02.

Part: GUIDE ARM — OUT OF ADJUST (R1 DOOR) · airframe 51,321 hrs · 28,644 cycles

R1 DOOR NOT COMING INTO CUT OUT CORRECTLY. ACFT GROUNDED. ADJUSTED DOOR GUIDE ARM REF AMM 52-41-00.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 50,510 hrs · 28,166 cycles

LEFT WING NR 3 SLAT INBD L/E IS DAMAGED. REPAIRED SLAT IAW EA 400-57EA-09803, REV.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 50,510 hrs · 28,166 cycles

RT INBD AFT FLAP DENT WITH EVIDENCE OF A CRACK, 35 INCHES FROM OTBD EDGE 1/2 INCH UP FROM T/E UPPER SKIN. REPAIRED IAW SRM 51 70 10, REP 2, PG 201.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 50,510 hrs · 28,166 cycles

LEFT WING INBD AFT FLAP IS DENTED ON LOWER SURFACE 22 INCHES FROM INBD END. REPAIRED DENT IAW SRM 51-70-05, PG 16, PARA 42, REPAIR 1.

Part: PANEL — DAMAGED (LT WING) · airframe 50,510 hrs · 28,166 cycles

LEFT WING PIE PANEL AFT LANDING HAS TWO MISDRILLED HOLES. REPAIRED PIE PANEL LANDING IAW ASA EA 400-57EA-09832, REV.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 50,510 hrs · 28,166 cycles

LEFT INBD T/E AFT FLAP HAS THREE DENTS ON THE LOWER SURFACE. REPAIRED IAW SRM 51-70-10, REPAIR 4 AND SRM 51-70-05, REPAIR 1.

Part: TRANSITION PANEL — CORRODED (BS 727D-767) · airframe 50,510 hrs · 28,166 cycles

AFT CARGO BAY RT TRANSITION PANEL CORRODED AT FASTENER HOLES. BLENDED TRANSITION PANEL FOUND TO BE OUT OF LIMITS REMOVED, FABRICATED NEW PART AND INSTALLED NEW PART IAW SRM 53-60-53.

Part: SPLICE — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 50,510 hrs · 28,166 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SPLICE BETWEEN NR 1 AND NR 2 FLOOR PANELS HAS EXFOLIATION CORROSION FABRICATED, LOCATED AND DRILLED A NEW AFT CARGO COMPARTMENT FLOOR PANEL SPLICE PLATE BETWEEN NR 1 AND NR 2 FLOOR PANELS IAW SRM 51 40 05.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 50,510 hrs · 28,166 cycles

RT OTBD FOREFLAP INBD L/E IS CHAFED. REPAIRED RT OTBD FOREFLAP INBD L/E IAW SRM 57-53-01, REPAIR 1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 50,510 hrs · 28,166 cycles

RT INBD AFT FLAP HAS DENT 22" FROM OTBD EDGE AND 1" UP FROM T/E UPPER SKIN. REPAIRED RT INBD AFT FLAP DAMAGE 22 FROM OTBD EDGE IAW SRM 51 70 10, REP 2, PG 201. (PERMANENT REPAIR).

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 50,510 hrs · 28,166 cycles

NR 4 SLAT UPPER T/E INBD CORNER DELAMINATED. ACFT GROUNDED. BONDED REPAIR OF NR 4 SLAT UPPER T/E INBD CORNER IAW SRM 51 70 10, REPAIR NR 4.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 50,510 hrs · 28,166 cycles

RT INBD UPPER FIXED T/E SUPPORT ANGLE CRACKED. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 50,510 hrs · 28,166 cycles

LT WING L/E SLAT NR 3 UPPER SURFACE T/E INBD CORNER DELAMINATED. REPAIRED DELAMINATION ON LT WING L/E SLAT NR 3 IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — CHAFED (BS 1138-1156) · airframe 50,510 hrs · 28,166 cycles

LT HORIZ STAB TO FUSELAGE SKIN PLATE CHAFED BELOW AND JUST AFT OF AFT LWR ATTACH FITTING. ACFT GROUNDED. R & R WITH A NEW LT HORIZ STAB TO FUSE SKIN PLATE IAW DWG 65-48240 AND 737-400, SRM 51 40 02.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 50,510 hrs · 28,166 cycles

LT OTBD FOREFLAP INBD L/E CHAFING ON REAR SPAR ACCESS PANEL. REMOVED, FABRICATED AND INSTALLED NEW L/E SKIN SECTION IAW SRM 51-40-05 AND 51-40-02.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 50,510 hrs · 28,166 cycles

LT WING L/E SLAT NR 3 LWR SURFACE INBD T/E PREVIOUS REPAIR CHAFED. REPAIRED CHAFING ON LT WING L/E SLAT NR 3 LWR SURFACE IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (BS 942) · airframe 50,510 hrs · 28,166 cycles

RT FUSELAGE SKIN IS DENTED 5 INCHES AFT OF THE NEG PRESSURE RELIEF DOOR. REPAIRED DENT AFT OF NEG PRESSURE RELIEF DOOR AT BS 942 IAW EA NR 400 53 EA, 09804 REV NEW.

Part: STRAP — CRACKED (FLOOR SUPPORT) · airframe 50,510 hrs · 28,166 cycles

FLOOR SUPPORT LOWER SUPPORT STRAP AT BL 0 IN E & E BAY CRACKED. REMOVED AND INSTALLED NEW FLOOR SUPPORT LOWER SUPPORT STRAP IAW SRM 51-40-02.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 50,290 hrs · 28,042 cycles

EMERGENCY LIGHTING ABOVE EXIT ROW WINDOWS INTERMITTENT. TURNED ON EMERGENCY LIGHTS, ALL LIGHTS ABOVE EXIT ROW WINDOWS ILLUMINATE STEADY. OPS NORMAL. EMERGENCY LIGHTS SWITCHED OFF.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 49,286 hrs · 27,424 cycles

F/A REPORTS FWD EXIT LIGHT COVER NOT STAYING ATTACHED. REPLACED EXIT LIGHT COVER REF MM 33-51-51.

Part: HINGE — INOPERATIVE (L1 DOOR) · airframe 48,514 hrs · 26,963 cycles

L1 DOOR WILL NOT CLOSE PROPERLY. ACFT GROUNDED. REINSTALLED DOOR HINGE COVER. OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 47,707 hrs · 26,482 cycles

FWD LT EMERGENCY OVERWING EXIT DOOR EMERGENCY LIGHT LENS BROKEN OFF. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY L1208 PER MM 33-51-81. OPS CHECKED NORMAL PER 33-51-02-715-001.

Part: SKIN — DENTED (SPOILER) · airframe 44,061 hrs · 24,413 cycles

RT WING NR 6 SPOILER HAS DENT. REPAIRED RT WING NR 6 SPOILER.

Part: WEDGE — DENTED (LE SLAT) · airframe 44,055 hrs · 24,405 cycles

NR 6 SLAT T/E WEDGE UPPER SURFACE DENTED 28 INCHES OUTBOARD OF INBOARD END A=2 Y=.007 A/Y=28. REMOVED DAMAGE, FABRICATED REPAIR PARTS, REMOVED MOISTURE TREATED PRIMED AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: WEDGE — DENTED (LE SLAT) · airframe 44,055 hrs · 24,405 cycles

NR 5 SLAT T/E WEDGE LOWER SURFACE DENTED 46 INCHES INBOARD OF OUTBOARD END A=3 Y=.012 A/Y=25. REMOVED DAMAGE FABRICATED REPAIR PARTS, REMOVED MOISTURE TREATED PRIMED AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: FITTING — LACK OF LUBE (L1 DOOR)

F/A'S REPORTS L1 ENTRY DOOR HARD TO CLOSE AND MAKE CREAKING SOUNDS. LUBED L1 DOOR FITTINGS AND PERFORM OPS CHECK REF AMM 52 11 00 705 060, OPS CHECK GOOD.

Part: SKIN — DENTED (HORIZ STAB)

LARGE DENT IN RT HORIZONTAL STABILIZER FIXED LEADING EDGE. REPLACED SKIN.

Part: FRAME — CRACKED (BS 907) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 907 BETWEEN STR 8 AND 9 RT. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 747) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 747 BETWEEN STR 8L AND 9L. REPAIRED FRAME AT STA 747 LT.

Part: FRAME — CRACKED (BS 827) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 827 BETWEEN STR 8 AND 9 LT. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 747) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 747 BETWEEN STR 8R AND 9R. REPAIRED FRAME AT STA 747 RT.

Part: FRAME — CRACKED (BS 787) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 787 BETWEEN STR 8 AND 9 LT. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 907 BETWEEN STR 8 AND 9 LT. REPAIRED FRAME AT STA 907 IAW EA.

Part: FRAME — CRACKED · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 400 BETWEEN STR 8L AND 9L. REPAIRED FRAME AT STA 400 LT.

Part: SKIN — PUNCTURED (NR 9 SPOILER) · airframe 40,693 hrs · 22,422 cycles

NR 9 SPOILER IS PUNCTURED ON UPPER SURFACE OB END. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW SRM.

Part: FRAME — CRACKED (BS 827) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 827 BETWEEN STR 8R AND 9R. REPAIRED FRAME AT STA 827 RT.

Part: INTERCOSTAL — MISINSTALLED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

INTERCOSTAL AT STR 26R STA 747 767 IMPROPERLY INSTALLED. REMOVED INTERCOSTAL, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW INTERCOSTAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

STR 21L CRACKED .300 LONG BETWEEN STA 986 AND 1006. REPAIRED STRINGER IAW SRM.

Part: WEDGE — DENTED (TE FLAP) · airframe 40,693 hrs · 22,422 cycles

RIGHT I/B MIDFLAP T/E WEDGE LOWER SURFACE DENTED IN SEVERAL LOCATIONS. REMOVED DAMAGED AREAS, FABRICATED, TREATED, PRIMED AND BONDED FILLER AND DOUBLER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FUSELAGE STRINGER TO FRAME SHEAR CLIP CRACKED FS 727F STR 9L. REMOVED DAMAGED CLIP AND INSTALL NEW CLIP IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

MAIN CABIN R1 MOPSILL CORRODED STA 294.5 344. REMOVED AND REPLACED MOP SILL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

MAIN CABIN RT SIDE OF I/B SIDEWALL STA 294.5 TOP OF BEAM CORRODED. SPLICED IN NEW T-CAP SECTION IAW SRM.

Part: SPOILER — DENTED (LT WING) · airframe 40,693 hrs · 22,422 cycles

LT WING NR 1 SPOILER PANEL LOWER SURFACE HAS A SHARP DENT. REPAIRED LT WING NR 1 SPOILER IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FRAME TO INTERCOSTAL ATTACH CLIP AT FS 500F STR 26L IS CRACKED. REMOVED DAMAGED CLIP, FABBED NEW CLIP AND INSTALLED PARTS IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — CRACKED · airframe 40,693 hrs · 22,422 cycles

STR CLIP AT STA 500D STR26R CRACKED. REMOVED CLIP FABRICATED LOCATED DRILLED TREATED PRIMED TOP COATED AND INSTALLED NEW CLIP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

SHEAR WEB FOR APB AT STA 1018 RBL 37 CRACKED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND INSTALLED REPAIR IAW B737 400 SRM 51 70 13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FRAME CLIP ON THE AFT SIDE OF THE FRAME AT STA 500E STR 26L CRACKED AT THE BOTTOM HOLE. REMOVED DAMAGED CLIP AND INSTALLED NEW CLIP IAW B737 400 SRM 51 40 02.

Part: SILL — DAMAGED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

AFT PIT LOWER DOOR SILL WEB BETWEEN STA 794 807 HAS TOOLING MARKS. REMOVED DAMAGED WEB, FABBED REPLACEMENT WEB AND INSTALLED REPLACEMENT PARTS IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

AFT PIT LWR DOOR SILL WEB CORRODED. ,FOUND ON PARTS AFTER REMOVAL. REMOVED CORROSION, RECEIVED NEW WEB, LOCATED, DRILLED, TREATED, PRIMED, TOP COATED REPLACEMENT WEB.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

WEB CLIP AT STA 500E STR 26R IS CRACKED. REMOVED DAMAGED CLIP, FABBED AND INSTALLED REPLACEMENT CLIP IAW B737 400 SRM 51 40 02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

WEB TO FRAME CLIP CRACKED AT STA 500F STR 26L. REMOVED DAMAGED CLIP FABBED REPLACEMENT CLIP AND INSTALLED CLIP IAW B737 400 SRM 51 40 02.

Part: WEDGE — DENTED (TE FLAP) · airframe 40,693 hrs · 22,422 cycles

LEFT I/B TRAILING EDGE WEDGE LOWER SURFACE HAS CLUSTERS OF DENTS. PREPPED DAMAGED AREAS, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,693 hrs · 22,422 cycles

LEFT O/B AFT FLAP LOWER SURFACE HAS DELAMINATION ON I/B END. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REF 4.

Part: STRINGER CLIP — BENT (BS 520 S27L) · airframe 40,693 hrs · 22,422 cycles

STRINGER CLIP BENT STA 520 STR 27L. REMOVED BENT CLIP FABRICATED LOCATED DRILLED TREATED PRIMED TOP COATED AND INSTALLED NEW STRINGER CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FRAME STA 727C UPPER FLANGE IS DENTED BETWEEN STR 24L - 25L. CUT OUT DAMAGED SECTION. FABRICATED, LOCATED AND DRILLED, HEAT TREATED, PRIMED, TOP COATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 11 FIG 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FRAME AT STA 986 CORRODED ON FWD UPPER FLANGE ABOVE STR 20L. REMOVED CORRODED FRAME SECTION, RECEIVED MAT FROM HEAT TREAT, FABRICATED, LOCATED, TREATED, PRIMED, INSTALLED NEW ANGLE.

Part: SHEAR TIE — CORRODED (BS 520) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

SHEAR TIE LOWER FLANGE AT STA 520 BETWEEN STR 28L AND 27R IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED REPAIR.

Part: SKIN — DENTED (SPOILER) · airframe 40,693 hrs · 22,422 cycles

NR 4 SPOILER LOWER SURFACE I/B END HAS SEVERAL SHARP DENTS SREF SAD 5080535. PREPPED DAMAGED AREA, FABBED DOUBLERS AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REP 2.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

L2 DOOR CUTOUT FRAME STA 994 CORRODED I/B AND FWD SIDES JUST ABOVE FLOOR LEVEL LBL 47 LBL 49 WL 208.5 210.5. REMOVED DAMAGED AREA, FABBED DOUBLER AND FILLER AND INSTALLED REPAIR IAW B737 400 SRM 51 70 11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

FWD PIT BETWEEN STA 500C 500D STR 27R CORRODED AROUND FASTENERS. REMOVED DAMAGED SECTION OF STR 27R. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 03 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FRAME STA 500B CORRODED BETWEEN STR 26L 26R. REMOVED DAMAGED AREA, RECEIVED NEW PART FROM HEAT TREAT, LOCATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED PART AND FILLER.

Part: STRINGER — CORRODED (BS 500E-500F) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

FWD PIT STA 500E-500F, STRINGER 28 R, CORRODED AROUND RIVETS. REMOVED CORROSION REMOVED DAMAGED PORTION OF STRINGER FABRICATED LOCATED DRILLED TREATED PRIMED TOP COATED AND INSTALLED REPAIR PARTS.

Part: STRINGER CLIP — DAMAGED (BS 1006 S16R) · airframe 40,693 hrs · 22,422 cycles

STR CLIP, STA 1006, STR 16R IS DAMAGED. REMOVED DAMAGED CLIP DRILLED NEW CLIP AND INSTALLED THE NEW CLIP.

Part: FRAME — CRACKED (BS 727F S8-9L) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 727F BETWEEN STR 8L AND 9L. REPAIRED FRAME AT 727F IAW EA.

Part: FRAME — CRACKED (BS 440) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 440 BETWEEN STR 8L AND 9L. REPAIRED FRAME AT 440 LT IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 440 BETWEEN STR 8R & 9R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED.

Part: STRINGER CLIP — BENT (BS 420 S22R) · airframe 40,693 hrs · 22,422 cycles

STR CLIP, STA 420, STR 22R IS BENT. REMOVED DAMAGED CLIP, FABRICATED REPLACEMENT PARTS AND INSTALLED REPLACEMENT PARTS.

Part: FRAME — CRACKED (BS 867) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 867 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FLAP — CHAFED (LT WING) · airframe 40,693 hrs · 22,422 cycles

LT WING O/B FORE FLAP CHAFED O/B CORNER. REMOVED EXISTING DOUBLER, FABRICATED, TREATED, PRIMED AND INSTALLED NEW REPAIR DOUBLER IAW B737 400 SRM 57 53 01 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FUSELAGE FRAME AT STA 480 BETWEEN STR 8R AND 9R IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

AFT PIT FRAME, STA 747, DENTED UPPER FLANGE BETWEEN STR 22R 23R. REMOVED DAMAGED FLANGE FABRICATED LOCATED AND DRILLED TREATED PRIMED TOP COATED AND INSTALLED REPAIR IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

INTERCOSTAL (AFT PIT) STA 747 767 STR 25R 26R CORRODED AROUND FASTENER HOLES. REMOVED CORRODED INTERCOSTAL. FABRICATED, LOCATED, TREATED, PRIMED, TOPCOATED AND INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 05 FIG 2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

SHEAR TIE CORRODED STA 787 STR 27L 25L. REMOVED CORRODED SHEAR TIE, RECEIVED NEW PARTS FROM HEAT TREAT, LOCATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW SHEAR TIE.

Part: FRAME — CRACKED (BS 480) · airframe 40,693 hrs · 22,422 cycles

FRAME CRACKED AT STA 480 BETWEEN STR 8 AND 9 LT. REMOVED DAMAGED AREA FABBED REPAIR PARTS AND FILLER AND INSTALLED REPAIR IAW EA.

Part: FRAME — CORRODED (BS 847) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

AFT PIT FRAME AT STA 847 IS CORRODED ON UNDERSIDE OF LOWER BETWEEN STR 26R AND INTERCOSTAL OB OF STR 26. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

SHEAR TIE CORRODED ON FWD SIDE OF FRAME AT STA 767 BETWEEN STR 25L AND 26L. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: STRINGER CLIP — CORRODED · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

STR CLIP AT STA 807 STR 27L CORRODED. REMOVED CORRODED STR CLIP RECEIVED PART FROM HEAT TREAT FABRICATED LOCATED DRILLED TREATED PRIMED TOP COATED AND INSTALLED NEW CLIP.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

SHEAR TIE CORRODED FWD FRAME STA 407 BETWEEN STR 27L 25L. REMOVED SHEAR TIE, HEAT TREATED, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED DOUBLER AND FILLER.

Part: CARGO TRACK — CORRODED (BS 947-787) · airframe 40,693 hrs · 22,422 cycles

AFT PIT LT CARGO TRACK TIE DOWNS HAVE LIGHT CORROSION STA 947 TO 787. REMOVED CORROSION, TREATED, PRIMED AREAS WITHIN LIMITS FABRICATED LOCATED DRILLED AND INSTALLED NEW ANGLE.

Part: SUPPORT — GOUGED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

AFT PIT SIDEWALL SUPPORT GOUGED BETWEEN STR 22R AND 21R AND BETWEEN STA 867 AND 887. INSTALLED NEW STUB FRAME IAW SRM.

Part: ATTACH ANGLE — CRACKED (BS 747A) · airframe 40,693 hrs · 22,422 cycles

STA 727A FRAME TO INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN 25L AND 26L. REMOVED ANGLE, FABRICATED, LOCATED, DRILLED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW ANGLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,693 hrs · 22,422 cycles

AFT PIT INTERCOSTAL CORRODED BETWEEN STA 947 927 OF STR 24L. REMOVED CORRODED INTERCOSTAL, FABRICATED, LOCATED, TREATED, PRIMED, TOPCOATED AND INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 05 FIG 2.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,693 hrs · 22,422 cycles

LEFT I/B AFT FLAP LOWER SURFACE DELAMINATED. REMOVED DAMAGED SKIN & CORE. FABRICATED, TREATED, PRIMED AND BONDED NEW REPAIR DOUBLER AND CORE IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

SHEAR WEB STA 986 1016 CRACKED, FOUND AFTER REMOVAL. FABRICATED, LOCATED & DRILLED, PRIMED AND TOPCOATED NEW SHEAR WEB IAW B737 400 SRM 51 40 05.

Part: DOUBLER — CHAFED (TE FLAP) · airframe 40,693 hrs · 22,422 cycles

LEFT I/B FOREFLAP UPPER SURFACE REPAIR DOUBLER CHAFED JUST ABOVE CENTER TRACK. REMOVED DAMAGED DOUBLER, FABRICATED, TREATED, PRIMED AND BONDED NEW REPAIR IAW SRM.

Part: FLAP — CHAFED (RT WING) · airframe 40,693 hrs · 22,422 cycles

RIGHT O/B FLAP I/B LEADING EDGE CHAPPED. REMOVED DAMAGED DOUBLER, FABRICATED, TREATED, PRIMED AND INSTALLED NEW REPAIR DOUBLER IAW B737 400 SRM 52 53 01 FIG 201.

Part: FLAP — DENTED (RT WING) · airframe 40,693 hrs · 22,422 cycles

RT WING INBOARD AFT FLAP DENTED 1.5 INCHES FROM T/E 34 INCHES FROM INBOARD END. PREPPED DENTED AREA. BONDED REPAIR IAW SRM 51 07 FAR 4.

Part: FLAP — DENTED (RT WING) · airframe 40,693 hrs · 22,422 cycles

RIGHT I/B FORE FLAP DENTED SEVERAL LOCATIONS. PREPPED DAMAGED AREA. FABRICATED, TREATED AND BONDED (3) DOUBLER REPAIRS IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: STRINGER CLIP — CRACKED (BS 867 S27R) · airframe 37,178 hrs · 20,381 cycles

AFT CARGO PIT STR 27R TIE CLIP AT STA 867 CRACKED FOUND DURING FLOOR PANEL CLOSING AFT CARGO PIT STR 27R CRACKED TIE CLIP AT STA 867. REPLACED WITH MADE REPAIR PART IAW B737 400 SRM CH 51 40 02.

Part: SKIN — DENTED (T/E FLAP) · airframe 37,178 hrs · 20,381 cycles

LT OUTBOARD AFT FLAP LWR SURFACE AT WBL 255 IS DENTED. DENT REPAIRED IAW B737 400 SRM CH 51 70 10.

Part: SKIN — DENTED (RT FORE FLAP) · airframe 37,178 hrs · 20,381 cycles

DENTS FOUND ON INBD RT FOREFLAP UPPER SURFACE. DENTS ON UPPER SURFACE OF RT INBOARD FOREFLAP 8" FROM T/E APPROX 48" AND 77" FROM 18 END REPAIRED IAW B737 400 SRM 51 70 10 REPAIR 3.

Part: SKIN — DENTED (HORIZ STAB) · airframe 37,178 hrs · 20,381 cycles

ON PRE FLIGHT, FOUND NICKEL SIZE ON HORIZONTAL STAB RT SIDE LEADING EDGE DENT AT HORIZ STAB L/E SKIN AT STAB STA 102. REPAIRED IAW B737 400 SRM 55 10 01 REPAIR 2.

Part: WEB — DAMAGED (BS 986-1016) · airframe 37,178 hrs · 20,381 cycles

AFT CABIN WEB 2 STA 986 5 1016 RBL 32 47 WL 207.5 DAMAGED, REPAIRED WITH REPAIR PART.

Part: WEB — CORRODED (BS 986-992) · airframe 37,178 hrs · 20,381 cycles

AFT CABIN WEB AT STA 986.5 992 RBL 47 52 WL 207.5 HAS CORROSION, REPLACED WITH MADE REPAIR PART.

Part: FLOOR SUPPORT — GOUGED (BS 1006-1016) · airframe 37,178 hrs · 20,381 cycles

FLOOR SUPPORT AT STA 1006 1016 RBL 37 WL 207.5 GOUGED, REPAIRED WITH REPAIR PART.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 37,178 hrs · 20,381 cycles

WHILE PERFORMING FLAP RIGGING LT O/B MIDFLAP CONTACTED WITH NR 2 SPOILER LOCK ON LEADING EDGE DAMAGE ON LT O/B MIDFLAP LEADING EDGE WAS REPAIRED IAW B737 400 SRM CH 57 53 01 FIG 201 REPAIR 7.

Part: BRACKET — CORRODED (BS 787) · airframe 37,178 hrs · 20,381 cycles

AFT CARGO PIT RT FLOOR SHIELD FWD GUSSET BRACKET CORREODED AT BS 787 RBL 23, REPLACED WITH MADE REPAIR PART.

Part: FLOORBEAM — DAMAGED (BS 913) · airframe 37,178 hrs · 20,381 cycles

AFT CABIN FLOOR INTERCOSTAL AT BS 913.74 RBL 51 TO RBL 56 HAS EXISTING DOUBLE DRILLED FASTENER HOLE AT O B END (SUPPORT) INTERCOSTAL AT BS 913.74 RBL 56. REPLACED IAW B737 400 SRM CH. 51 40 05 USING BAC 1506 43 7075773511 PO NR 166385 AND INSTALLED IAW B737 400 SRM CH 51 40 02.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CABIN FLOORBEAM AT STA 986.5 RBL 27 WL 207.5 CORRODED ON UNDERSIDE AT CLIPNUT ATTACH POINT. REPAIRED IAW EA NR 5320 01832.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CABIN UPPER SIDE OF FLOOR SUPPORT AT BS STA 960 RB 46 WL 207.5 HAS CORRODED. REPLACED WITH MADE REPAIR PART.

Part: BRACKET — CORRODED (BS 787) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CARGO PIT RT FLOOR SHIELD FWD GUSSET BRACKET CORRODED AT BS 787 RBL 23, REPLACED WITH MADE REPAIR PART.

Part: SKIN — DENTED (T/E FLAP) · airframe 37,178 hrs · 20,381 cycles

RT OUTBOARD AFT FLAP UPPER SKIN HAS DENTS AT SECOND TO INBD FITTING (68 INCHES FROM INBOARD END AND 6 INCHES FROM T/E) AND 113 INCHES FROM INBOARD END AND 3 INCHES FROM T/E DENTS. REPAIRED IAW B737 400 SRM CH 51 70 10 REP 2.

Part: SKIN — GOUGED (BS 1021) · airframe 37,178 hrs · 20,381 cycles

FUSELAGE SKIN AT BS 1016 + 52" BELOW STR 16L DENTED AND GOUGED FROM CONTACTS WITH SCISSOR LIFT. REPAIRED AREA WITH REPAIR PART.

Part: WEB — CORRODED (BS 951-986) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CABIN UNDERSIDE OF WEB 2 STA 975 986.5 RBL 48 WL 207.5 CORRODED. REPLACED WITH MADE REPAIR PART.

Part: SKIN — DENTED (T/E FLAP) · airframe 37,178 hrs · 20,381 cycles

LT INBD FORE FLAP UPPER SURFACE HAS IRREGULARITY DENT ON UPPER SURFACE OF THE LT INBD FOREFLAP AT WBL 134. REPAIRED IAW B 737 400 SRM 51 70 10 REPAIR 3 PARA 7.

Part: SKIN — DENTED (L/E SLAT) · airframe 37,178 hrs · 20,381 cycles

NR 3 SLAT LWR SURFACE DENTED. DENT REPAIR IAW SRM 51 70 10, REPAIR NR 4.

Part: SKIN — DENTED (FORE FLAP) · airframe 37,178 hrs · 20,381 cycles

LT OUTBOARD FORE FLAP UPPER SURFACE DENTED. DENTS REPAIRED IAW SRM 51-70-10, REPAIR 3.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 37,178 hrs · 20,381 cycles

NR 5 SLAT INBD AND OUTBD END DELAMINATED NR 5 SLAT DELAMINATIONS. REPAIRED IAW B737 400 SRM CH 51 70 10 REPAIR 4.

Part: SILL — CORRODED (BS 947-986) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

R2 CABIN DOORWAY LOWER SILL CORROSION FOUND FROM BS 947 TO 986.50 CORROSION ON R2 CABIN DOORWAY LOWER SILL CHORD WAS BLENDED OUT AND FOUND TO BE BEYOND LIMITS IAW 53-60-15 FIG 101. REMOVED DAMAGE PART IAW SRM 51-40-02 AND INSTALLED A NEW SILL CHORD IAW SRM 51-40-05 AND 51-40-02.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CABIN STA 986.50 FLOORBEAM UPPER CAP TOP SURFACE CORROSION FOUND BETWEEN RBL35 AND 40. REPAIRED WITH MADE REPAIRED PART.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 37,178 hrs · 20,381 cycles

NR 2 SPOILER LWR SURFACE 4 INCHES FROM INBOARD EDGE 7 INCHES FROM L/E IS DENTED. NR 2 SPOILER LWR SURFACE DENT REPAIRED IAW B737 400 SRM 51 70 10, REPAIR NR 2.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 37,178 hrs · 20,381 cycles

NR 2 SLAT OUTBD UPPER CORNER DELAMINATED NR 2 SLAT O/B UPPER CORNER DELAMINATION. REPAIRED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: ATTACH FITTING — CORRODED (BS 795) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

CORROSION ON ATTACH CLIP BS 795 TO VERTICAL WEB OF KEELBEAM STR 27R (RBL 6 ) AFT CARGO PIT, CORRODED CHIP AT BS 795 FRAME TO VERTICAL WEB OF KEEL BEAM STR 27R. REPLACED WITH MADE REPAIR PART IAW BAC DWG 65 47958 AND B737 400 SRM CH 51 30 01 AND 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

CORROSION ON FRAME IN AFT CARGO PIT AT BS 747 STR 26L TO STR 26R, REPAIRED WITH REPAIR PART.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CARGO PIT BS 794 TO BS 767 RBL 21 SHIELD IS CORRODED, REPAIRED WITH REPAIR PART.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

TIE CLIP FWD SIDE OF BS 787 OUTBD OF THE RT TIE DOWN TRACK RBL 13.80 CORRODED. AFT CARGO PIT REPAIRED WITH REPAIR PART.

Part: WEDGE — DENTED (T/E FLAP) · airframe 37,178 hrs · 20,381 cycles

RN IB FLAP TRAILINES EDGE WEDGE 27 INCHES OUTBD OF INBD END AND 3.5 INCHES FWD OF TRAILING EDGE HAS DENT R N IB FLAP TRAILING EDGE WEDGE WEDGE 27" OB OF IB END AND 3.5 INCHES FWD OF T/E DENT REPAIRED IAW B 737 400 SRM CH 51 70 10 REPAIR 2.

Part: SHEAR TIE — CORRODED (BS 807) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

CORROSION ON ATTACH CLIP AT BS 807 OUTBD OF RT CARGO TIE DOWN TRACK RBL 13.80 ON FWD SIDE AFT CARGO PIT CORROSION ON ATTACH CLIP IN AFT CARGO AT BS 807 OUTBOARD OF RT CARGO TIE DOWN TRACK RBL 13.80 FOUND BEYOND LIMITS. REPLACED WITH NEW PART IAW B737 400 SRM LT 51 40 02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,178 hrs · 20,381 cycles

DRILL MARKS ON FRAME IN CARGO PIT AT BS 747 RBL3 TO LBL3, REPAIRED WITH REPAIR PART.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT ENTRY AREA RT FLOORBEAM AT STA 986 RBL 43.5 WL 207.5 DOUBLER STRAP, UNDER FWD FLOORBEAM CAP CORRODED. PREVIOUS REPAIR REPAIRED IAW EA 5320 01832.

Part: CHANNEL — CORRODED (BS 867-887) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

AFT CARGO PIT BS 867 TO BS 887 RBL 21 SHIELD IS CORRODED. REPAIRED WITH REPAIR PART.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

FOUND CORROSION ON FRAME IN AFT CARGO PIT AT BS 767 STR 26R TO STR 27R. REPAIRED WITH REPAIR PART.

Part: ATTACH FITTING — CORRODED (BS 795) · corrosion level 2 · airframe 37,178 hrs · 20,381 cycles

TIE CLIP AFT SIDE OF FRAME AT BS 795 OUTBD OF RT TIE DOWN TRACK RBL 13.80 CORRODED AFT CARGO PIT. REPAIRED WITH REPAIR PART.

Part: SKIN — DENTED (BS 1070) · airframe 37,178 hrs · 20,381 cycles

FUSELAGE SKIN APPROX BS 1070 AT STR 14L DENTED FUSELAGE SKIN BS 1070 STR 14L. REPAIRED IAW B737 400 SRM 53 80 01.

Part: STRINGER — DENTED (FUSELAGE) · airframe 37,178 hrs · 20,381 cycles

STR 14L AT BS 1070 DENTED STR 14L BS 1070, REPARIED IAW B737 400 SRM 53 00 03.

Part: SKIN — DENTED (TE FLAP) · airframe 37,178 hrs · 20,381 cycles

LEFT INBOARD T/E AFT FLAP HAS A DENT IN THE LEADING EDGE 26 INCHES OUTBOARD OF THE INBOARD EDGE. DENT REPAIRED IAW B737 400 SRM CH 57 53 01 REPAIR 4.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,178 hrs · 20,381 cycles

FUSELAGE SKIN APPROX BS 1070 AT STR 146 DENTED FROM CONTACT WITH WORK SCAFFOLD FUSELAGE SKIN APPROX BS 1070 STR 14L DENT REPAIRED IAW B737 400 SRM CH 53 80 01.

Part: SKIN — DENTED (HORIZ STAB) · airframe 37,178 hrs · 20,381 cycles

R N HORIZ STAB L/E SKIN DENTED AT STAB STA 249.10 AND 1.5, REPAIRED IAW B737 400 SRM 55 10 01 FIG 201.

Part: SKIN — DENTED (HORIZ STAB) · airframe 37,178 hrs · 20,381 cycles

R N HORIZ STABILIZER E SKIN DENTED AT STAB STA 147.90 AND 8 DENT AT RT HORIZ STAB L/E SKIN AT STAB STA 147.90 AND 8. REPAIRED IAW B737 400 SRM 55 10 01 REPAIR 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,693 hrs · 22,422 cycles

FUSELAGE DENTED FWD OF L2 DOOR CUTOUT DENT. HFEC CUT OUT FABRICATED TREATED. PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737 400 SRM 53 00 01 FIG 201.

Part: DOOR — OBSTRUCTED (PSU) · airframe 35,515 hrs · 19,456 cycles

O2 MASK AT SEAT 7ABC DID NOT DEPLOY. O2 MASK IN RIGHT AFT LAV DID NOT DEPLOY. FOUND MASK HOSES CAUGHT ON PSU DOOR. REPACKED MASK, REMOVED AND REPLACED RIGHT AFT LAV OXY GEN REF MM 35-22-11. COMPLETED ACTIVATION PROCEDURE REF MM 35-22-11 STEPS 3D(4). OPS CK GOOD. REF MM 35-22-00 PG 506, 507.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 35,515 hrs · 19,456 cycles

AT CRUSE ALTITUDE HORN CAME ON (FLT LVL 330). CABIN CLIMBING TO 11000 FT. FOLLOWED QRH. NO OTHER INDICATIONS BESIDES ALTITUDE WARNING HORN AND CABIN CLIMBING. LANDED AT KTN, REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER AMM.

Part: SKIN — DENTED (BS 986-1006) · airframe 33,672 hrs · 18,430 cycles

FOUND DENT IN FUSELAGE SKIN. REMOVED DAMAGED SECTION OF SKIN FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW ASA EA 5330 02175.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,672 hrs · 18,430 cycles

FOUND DAMAGE TO EXISTING REPAIR DOUBLER. REMOVED EXISTING REPAIR PIECES TRIMMED OUT UPPER SKIN AREA WITH SHORT ED. FABRICATED AND INSTALLED FILLERS DOUBLERS AND TRIPLER IAW ASA EA 5330 02176.

Part: SKIN — CHAFED (FORE FLAP) · airframe 33,672 hrs · 18,430 cycles

RIGHT O/B FORE FLAP L EADING EDGE CHAFED. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-53-01 FIG 201 REPAIR 1.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 33,672 hrs · 18,430 cycles

RIGHT I/B AFT FLAP IS DELAMINATED ON O/B EDGE LOWER SURFACE. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 33,672 hrs · 18,430 cycles

LEFT STABLIZER I/B LEADING EDGE PANEL IS CREASED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PLATE AND FILLER IAW SRM 55-10-01 FIGURE 201 REPAIR 2.

Part: SKIN — DENTED (T/E FLAP) · airframe 33,672 hrs · 18,430 cycles

RIGHT I/B AFT FLAP UPPER SKIN DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.

Part: STRUCTURE — DENTED (FORE FLAP) · airframe 33,672 hrs · 18,430 cycles

LT IB FORE FLAP HAS SEVERAL DENTS ON THE LOWER SURFACE. PREPPED DENTED AREAS FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51 70 10.

Part: FLAP — DELAMINATED (LT WING) · airframe 33,672 hrs · 18,430 cycles

LEFT OUTBOARD T/E FLAP IS SPLIT (DELAMINATED) AT INBOARD EDGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 33,672 hrs · 18,430 cycles

NR 4 GROUND SPOILER HAS SEVERAL DENTS ON LWR SURFACE. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-70-10.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 33,672 hrs · 18,430 cycles

NR 2 SLAT INBOARD END TRAILING EDGE WEDGE IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PAE - FOUND LIGHTNING STRIKE AT BS 249 STRINGER 4L. REMOVED BLIND FASTENER AND INSTALLED SOLID FASTENER IAW B737-400 SRM 51-40-02. (M)

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

FRAME CRACKED BELOW STRINGER FOR BIN RAIL. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

FRAME CRACKED BELOW STRINGER FOR BIN RAIL. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

CRACK IN FRAME AT FASTENER FOR BIN HANGAR. REMOVED CRACK, FABRICATED REPAIR PARTS AND INSTALLED.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

STRINGER IS GOUGED. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,971 hrs · 14,219 cycles

CORROSION ON FRAME. REPAIRED CORRODED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

CRACKED FRAME. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,971 hrs · 14,219 cycles

CORROSION FRAME BS 907 BETWEEN STR 27R-27L. REPAIRED CORRODED FRAME IAW SRM.

Part: SKIN — CORRODED (LT MLG CUTOUT) · corrosion level 2 · airframe 25,971 hrs · 14,219 cycles

CORROSION ON LOWER INNER CHORD OF LT MLG CUTOUT. REMOVED AND REPLACED LOWER CHORD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

PAE - CORROSION ON FLOORBEAM. REPLACED EXISTING REPAIR STRAP.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,971 hrs · 14,219 cycles

PAE - CORROSION ON SHEAR TIE. REPAIRED SHEAR TIE.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 25,971 hrs · 14,219 cycles

PAE - CORROSION AFT CARGO BAY ON SHEAR TIE. REMOVED CORRODED SHEAR-TIE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 25,971 hrs · 14,219 cycles

PAE - CORROSION AFT CARGO BAY ON SHEAR TIE. REMOVED CORRODED SHEAR-TIE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: TERMINAL — LOOSE (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 16-18 INOPERATIVE AT TEST. RESECURED LOOSE TERMINALS AT ROW 16, OPERATIONAL CHECKED GOOD. (M)

Part: LIGHT — BROKEN (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS BROKEN AND DISCONNECTED AT ROW 16. REPLACED SECTION AND RECONNECTED WIRES. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS FOR ROWS 25 AND AFT, THE L2 OVERHEAD EXIT LIGHT AND R2 LOWER EXIT LIGHT WERE FOUND INOPERATIVE. SECURED LOOSE GROUND TERMINAL FOR THE AFT LEFT EMERGENCY BATTERY PACK AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

LAX - PRIOR TO FLT 103, THE L-1 DOOR WAS FOUND EXTREMELY HARD TO MOVE. LUBRICATED L-1 DOOR AND THE DOOR OPERATED NORMALLY. (X)