N794AS

Part: WEB — CRACKED (LT WING) · airframe 57,168 hrs · 32,510 cycles

WHILE ACCOMPLISHING NDT OPEN HOLE INSPECTION ON LT WING WEB, UPPER ROW FASTENER HOLE AT APPROX. RSS 222.5 WAS FOUND TO BE CRACKED IN WEB. ACFT GROUNDED. REPAIRED THE CRACKED WEB IAW EA 400-57EA-17950.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 57,168 hrs · 32,510 cycles

RIGHT WING INBD FLAP UPPER SURFACE INBD END SKIN IS CHAFED. ACFT GROUNDED. BLENDED THE FLAP SKIN AND FOUND TO BE OUT OF LIMITS. INSTALLED A REPAIR IAW SRM 57-53-01-1A, 1 FIG 101, AND 57-53-01-2R-3, REPAIR 3.

Part: BEARING — MIGRATED (SPOILER HINGE) · airframe 57,168 hrs · 32,510 cycles

NR 4 SPOILER SECOND FROM OTBD HINGE HAS A MIGRATING BEARING. ACFT GROUNDED. REMOVED THE NR 4 SPOILER HINGE AND INSTALLED A NEW HINGE IAW SRM 51-40-04.

Part: SPAR — CRACKED (LT WING) · airframe 57,168 hrs · 32,510 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT APPROX RSS 216. ACFT GROUNDED. REPAIRED THE WING R & R THE SPAR UPPER ANGLE IAW SRM 57-20-10-2R-4 REPAIR 4

Part: ATTACH ANGLE — CRACKED (BS 291) · airframe 57,168 hrs · 32,510 cycles

INTERCOSTAL ATTACH ANGLE CRACKED BS 291 BETWEEN STRINGERS 13 AND 14R. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 55,640 hrs · 31,464 cycles

LEFT WING OVERWING, EXIT SIGN WILL NOT SECURE INTO PLACE. GROUNDED. REPLACED LT WING OVERWING EXIT SIGN IAW AMM 33-51-22.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 55,240 hrs · 31,210 cycles

EXIT SIGN OVER EXIT ROW A/C RT HAS DETACHED. ACFT GROUNDED. REATTACHED EMERGENCY EXIT SIGN OVER EXIT ROW A/C RT. NO DEFECTS NOTED.

Part: FRAME — CRACKED (BS 747) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 747 IS CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: FRAME — CRACKED (BS 827) · airframe 54,314 hrs · 30,574 cycles

CABIN FRAME AT BS 827 BETWEEN STR 8L AND 9L IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW DATED 14AUG15 WORKFRONT NOTIFICATION SENT TO STRUCTURES ENGINEERING TO ISSUE EC/TC TO ACCOMPLISH 1 TIME INSPECTION THIS IS A DT CATEGORY B REPAIR WITH 3RD STAGE APPROVAL. INSPECTION THRESHOLD: 66K TOTAL FC; INSPECTION INTERVAL: 24K FC. REFER TO DTI EC AD20062609, 400-53-4 FOR DT REQUIREMENTS. NOTE: ENTERED INTO FILMAKER PRO FOR DTI REINSPECTION REQUIREMENTS.

Part: FRAME — CRACKED (BS 787) · airframe 54,314 hrs · 30,574 cycles

FRAME BS 787 BETWEEN STRINGERS 8 - 9R FOUND CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: FRAME — CRACKED (BS 727D) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 727D BETWEEN STR 8 - 9R IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: FRAME — CRACKED (BS 480) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 480 CRACKED BETWEEN S 8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: FRAME — CRACKED (BS 440) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 440 CRACKED BETWEEN S8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: FRAME — CRACKED (BS 400) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 400 CRACKED BETWEEN S8 - 9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: CARGO TRACK — CORRODED (BS 764-877) · corrosion level 2 · airframe 54,314 hrs · 30,574 cycles

AFT CARGO TRACK, RBL 13 IS CORRODED AT BS 764-877. ACFT GROUNDED. REPAIRED AFT PIT CARGO TRACK BS 764-877, RBL 13.8 IAW EA 400, 53EA 15553 AND SRM 53-00-53-2R-2.

Part: FRAME — CRACKED (BS 400) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 400 CRACKED BETWEEN S7 - 8L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: ATTACH ANGLE — CRACKED (BS 348) · airframe 54,314 hrs · 30,574 cycles

INTERCOSTAL TO FRAME ATTACH ANGLE CRACKED AT STA 348 AND S-14L. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 360) · airframe 54,314 hrs · 30,574 cycles

FRAME AT BS 360 CRACKED BETWEEN S8 - 9L. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.

Part: CARGO TRACK — CORRODED (BS 764-877) · corrosion level 2 · airframe 54,314 hrs · 30,574 cycles

CARGO TRACK RBL 13 IS CORRODED AT BS 764-877. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW EA AND SRM.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 54,314 hrs · 30,574 cycles

FWD FLOORBEAM, BS 312 CORRODED AT LBL 11 AND RBL 10 ON UPPER CAP. ACFT GROUNDED. CORROSION WAS FOUND TO BE OUT OF LIMITS, REMOVED DAMAGE AND REPAIRED IAW SRM 51-10-51-2R, REPAIR 5.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 54,314 hrs · 30,574 cycles

FLOORBEAM BS 344 IS CORRODED AT LBL 11.1 AROUND FASTENER. ACFT GROUNDED. REPAIRED THE FLOORBEAM IAW EA 400 53EA 15489.

Part: FITTING — CORRODED (BS 344) · corrosion level 2 · airframe 54,314 hrs · 30,574 cycles

L1 DOOR AFT GIRT BAR FITTING FLOOR BRACKET BS 344 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1. R & R GIRT BAR FITTING FLOOR BRACKET IAW SRM 51-40-02-0G-0, W 1", O .071", R .020", L 1", D .051.

Part: FRAME — CORRODED (BS 992) · corrosion level 2 · airframe 54,314 hrs · 30,574 cycles

BS 992, FRAME CORRODED, WL 208 - 212. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. , REPAIRED IAW EA 400, 53EA-15509.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 50,912 hrs · 28,479 cycles

L1 DOOR UPPER AFT STOP PIN FITTING CRACKED, NDT VERIFIED, FOUND DURING LINER INSTALL. ACFT GROUNDED. R & R L1 DOOR UPPER AFT STOP IN FITTING IAW EA 400-52, EA-124 32.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 50,912 hrs · 28,479 cycles

RIGHT WING NR 5 SLAT OTBD UPPER CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CHAFED (EXHAUST GATE) · airframe 50,912 hrs · 28,479 cycles

LEFT INBD EXHAUST GATE OTBD UPPER SKIN IS CHAFED. ACFT GROUNDED. REPAIRED EXHAUST GATE UPPER SKIN IAW SRM 57-53-01-2R-10, PARA 7.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 50,912 hrs · 28,479 cycles

RT WING NR 5 SLAT INBD UPPER AFT CORNER EXISTING REPAIR IS DELAMINATED. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SUPPORT ANGLE — CORRODED (TRANS PANEL) · corrosion level 2 · airframe 50,912 hrs · 28,479 cycles

AFT CARGO EQUIPMENT BAY LT AFT BS 947, L28L TRANSITION ANGLE END BACKSIDE HAS HEAVY CORROSION. ACFT GROUNDED. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF THE AFT PIT LT AFT TRANSITION PANEL FROM STA 947 TO STA 917 IAW SRM 53-60-53-2R-4, FIG 201, W 2", O .040", R .034", L 2.00", D .006.

Part: FRAME — CRACKED (BS 348) · airframe 50,912 hrs · 28,479 cycles

LT FRAME AT BS 348 HAS A CRACKED ANGLE BELOW S15L. ACFT GROUNDED. FABRICATED NEW ANGLE IAW DWG 65-17685 AND INSTALLED IAW SRM 51-40-02-0G-0.

Part: ROLLER — OUT OF LIMITS (SLIDING WINDOW) · airframe 49,696 hrs · 27,718 cycles

F/O WINDOW WILL NOT OPEN WHEN WINDOW LATCH IS ACTIVATED. ACFT GROUNDED. CHECKED FORCE TO OPEN AND CLOSE R2 WINDOW, FOUND TO BE OUT OF LIMITS ON HIGH SIDE IAW AMM 56-12-11-825-001. FOUND FWD LWR ROLLER FELL OUT OF WINDOW- REINSTALLED ROLLER AND SHIMED AS REQ IAW 56-12-11. OPS NORMAL. NO OTHER RIGGING AFFECTED OR ADJUSTED.

Part: LENS — MISSING (EXIT SIGN) · airframe 49,463 hrs · 27,555 cycles

AFT GALLEY L2 EXIT SIGN LENS MISSING. ACFT GROUNDED. INSTALLED EXIT LENS.

Part: SCREW — LOOSE (R2 WINDOW) · airframe 49,293 hrs · 27,440 cycles

F/O R2 SLIDING WINDOW WOULD NOT SHUT. FOUND NUT AND WASHER IN WINDOW TRACK. ACFT GROUNDED. FOUND SCREW LOOSE UNDER HANDLE, R2 WINDOW. REINSTALLED HARDWARE- NO ADJUSTMENTS MADE, WINDOW OPENS AND CLOSES NORMAL. PERFORMED TASK 56-12-11-715-018. OK FOR SERVICE.

Part: STRUCTURE — GOUGED (CARGO DOOR) · airframe 48,165 hrs · 26,730 cycles

AFT CARGO DOOR HANDLE MISSING RUBBER BUMPER AND DOOR STRUCTURE GOUGED. GOUGE IN DOOR HANDLE HOUSING IS OUT OF LIMITS REF AMM 52-31-15-801. REMOVED INTERIOR AND EXTERIOR AFT PIT DOOR HANDLE IAW AMM 52-31-14. REMOVED DOOR HANDLE HOUSING REF SRM 51-40-02. COMPLETED CARGO DOOR FLUSH HANDLE HSG REPLACED REF SRM 51-40-02. REINSTALLED THE AFT CARGO DOOR HANDLE REF AMM 52-31-14-004-054, STEPS 12-24, DOOR AND HANDLE OPS CH GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,895 hrs · 26,573 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT RT FWD OVERWING EXIT HAS BROKEN LENS AND MULTIPLE LAMPS INOPERATIVE. REPLACED LAMP & LENS, AND TESTED IAW MM 33-51-81-962-044. OPS NORMAL.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 47,628 hrs · 26,415 cycles

PAX CABIN FLOOR SUPPORT CRACKED BETWEEN STA 312 AND 328. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 778-880) · airframe 47,628 hrs · 26,415 cycles

AFT CARGO TRACK, RBL 13.8 IS CORRODED BS 807 TO 837. REPAIRED CORRODED CARGO TRACK IAW EA -09534 .

Part: TRANSITION PANEL — CORRODED (BS 727D-727F) · airframe 47,628 hrs · 26,415 cycles

AFT CARGO RT TRANSITION PANEL IS CORRODED, BS 727D, REMOVED CORROSION STA 727D, FOUND TO BE WITHIN LIMITS IAW SRM 53 60 53 1A 1, REMOVED AND INSTALLED SECTION OF TRANSITION PANEL, 727F, DUE TO 100 BEYOND LIMITS IAW SRM 53-60-53.

Part: FLOOR PANEL — CORRODED (BS 767-772) · corrosion level 2 · airframe 47,628 hrs · 26,415 cycles

AFT CARGO BAY FLOOR PANEL FS 767 CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, FAB NEW FLOOR PANEL SPLICE IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (BS 767) · corrosion level 2 · airframe 47,628 hrs · 26,415 cycles

AFT CARGO BAY FLOOR PANEL, FS 767 CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 FAB NEW FLOOR PANEL SPLICE IAW SRM 51-40-02, W 1, O .070, R .055, L .2, D .015.

Part: TIE DOWN — CORRODED (BS 492) · corrosion level 2 · airframe 47,628 hrs · 26,415 cycles

FWD CARGO SCUFF AFT TIE DOWN PLATE CORRODED ON LOWER SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,233 hrs · 25,560 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY & RELAMPED, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,971 hrs · 24,289 cycles

LT FORWARD OVERWING EMERGENCY EXIT IDENTIFIER HAS BULBS INOP. RELAMPED & PERFORMED GOOD OPS TEST IAW AMM 33 51 22 962 001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,971 hrs · 24,289 cycles

BS 601 RT FRAME INNER CHORD CRACKED AT 1 EA LOWEST FASTENER HOLE WL 200. FOUND DURING NDI HEEC BOTTOM SIDE OF HOLE MARKED. CUT OUT CRACKED FASTENER HOLE AND REPAIRED IAW ASA EA 400 53EA 06258 AND ATS ER 11 04186.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,971 hrs · 24,289 cycles

BS 601 L FRAME INNER CHORD CRACKED AT LOWEST 2 EA FASTENER HOLES WL 200 MARKED. CUT OUT DAMAGE AT LOWEST 2 FASTENER HOLES AND REPAIRED CHORD IAW ASA EA 400 53EA 06253 AND ATS ER 11 04185.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,971 hrs · 24,289 cycles

BS 616 RT FRAME INNER CHORD CRACKED AT LOWEST FASTENER HOLE WL 200. FOUND DURING NDI HFEC BOTTOM POSITION OF HOLE MARKED. REPAIRED BS 616 RT FRAME INNER CHORD WL 200 PER T/C AD20102506 400 53 8 AND EA 400 53EA 06250.

Part: ANGLE — CRACKED (RT WING TE FLAP) · airframe 43,971 hrs · 24,289 cycles

RIGHT WING DOG HOUSE PANEL I/B ATTACH ANGLE COMMON TO NR 6 FLAP TRACK FAIRING CRACKED ON LOWER END. ACFT GROUNDED. REMOVED FABRICATED AND INSTALLED PANEL I/B ANGLE IAW DWG 65-69646 SRM 51-40-05 & 51-40-02.

Part: PANEL — CRACKED (TE FLAP) · airframe 43,971 hrs · 24,289 cycles

NR 6 FLAP TRACK FAIRING I/B PANEL CRACKED ABOVE UPPER FORWARD SCREW (NR 2 PYLON). REPLACED NR 2 PYLON PANEL.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,241 hrs · 22,131 cycles

RIGHT I/B MID FLAP DELAMINATED IN SEVERAL AREAS. REPAIRED MID FLAP.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 40,241 hrs · 22,131 cycles

RIGHT I/B MID FLAP LOWER T/E WEDGE IS DAMAGED. REPAIRED MID FLAP.

Part: WEB — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

AFT PIT ENTRY WEB IS CORRODED. REMOVED AND REPLACED WEB.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

AFT CARGO PIT INTERCOSTAL CORRODED STA 847. REMOVED DAMAGED INTERCOSTAL AND INSTALLED REPLACEMENT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

SHEAR TIE AFT SIDE CORRODED ON FWD SIDE OF FRAME AT STA 747 BETWEEN STR 26R 27R. REMOVED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

AFT PIT STRINGER 27L SPLICE DOUBLER BETWEEN FRAMES 867 847 CORRODED UPPER SURFACE. REMOVED CORRODED SPLICE DOUBLER AND INSTALLED NEW SPLICE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

AFT WET AREA LT WEB STATION 1006 TO 1016 IS CORRODED. REMOVED, FABRICATED AND INSTALLED NEW WEB.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

AFT WET AREA SHEAR WEB AREA 986 TO 1016 LT SIDE IS CORRODED. REMOVED, FABRICATED AND INSTALLED NEW WEB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

FRAME CRACKED BETWEEN STRINGERS 8 & 9. CUT OUT DAMAGE, FABRICATED DOUBLERS AND INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

FRAME AT STA 827 CRACKED BETWEEN STR 8 & 9. CUT OUT DAMAGE, FABRICATED DOUBLERS AND INSTALLED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

INTERCOSTAL TO SKIN ATTACH ANGLE CRACKED AT STA 291. REMOVED DAMAGED INTERCOSTAL AND INSTALLED REPLACEMENT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

AC GROUND CONNECTION DOOR LANDING CRACKED ALONG THE RIGHT EDGE OF THE CUTOUT. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

STRINGER CLIP CORRODED BS 907 STR 8R. INSTALLED NEW CLIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

FRAME AT STA 787 CRACKED BETWEEN STR 8 & 9. CUT OUT DAMAGE, FABRICATED DOUBLERS AND INSTALLED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

INTERCOSTAL TO SKIN ATTACH ANGLE CRACKED AT STA 291. REMOVED DAMAGED INTERCOSTAL AND INSTALLED REPLACEMENT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

FRAME AT STA 380 CRACKED BETWEEN STR 8 & 9. CUT OUT DAMAGE, FABRICATED DOUBLERS AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

AFT CABIN FLOORBEAM AT STA 947 LBL 6 IS CORRODED. REPAIRED FLOORBEAM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

AFT PIT SHEAR TIE FWD SIDE OF FRAME CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED SHEAR TIE REPAIR.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

INTERCOSTAL TO SKIN ATTACH ANGLE CRACKED AT STA 291. REMOVED DAMAGED INTERCOSTAL AND INSTALLED REPLACEMENT.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

R2 DOOR MOP SILL CORRODED. REMOVED CORRODED MOP SILL, INSTALLED NEW MOP SILL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

FWD CABIN STA 440 ABOVE STR 9L FRAME CRACKED. CUT OUT DAMAGE, FABRICATED DOUBLERS AND INSTALLED.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

AFT GALLEY DOOR CUTOUT THRESHOLD WEB CORRODED. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB.

Part: STRUCTURE — CRACKED (LT WING) · airframe 40,241 hrs · 22,131 cycles

LEFT WING LOWER CHORD IS CRACKED BETWEEN STRINGER 2 & 3 WBL 135.5. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR TEE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

AFT PIT SHEAR TIE IS CORRODED BETWEEN STR 26R AND 27R BOTH SIDES OF THE SHEAR TIE. REPAIRED SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

AFT PIT SHEAR TIE AT STA 727F IS CORRODED BETWEEN STR 26R AND 27R BOTH SIDES OF THE SHEAR TIE. REPAIRED SHEAR TIE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,241 hrs · 22,131 cycles

AFT PIT FRAME IS CORRODED ON UNDERSIDE OF UPPER FLANGE AT HI-LOK Z-ANGLE ATTACH POINT. CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR ANGLE AND 2 EACH FILLERS AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,241 hrs · 22,131 cycles

FWD CARGO PIT FRAME STA 500B CORRODED BETWEEN 28L AND 28R. CUT OUT DAMAGED SHEAR TIE ON FRAME, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE.

Part: SKIN — CHAFED (LE SLAT) · airframe 40,241 hrs · 22,131 cycles

NR 4 SLAT I/B END LWR SURFACE CHAFED AT PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR BONDED NEW REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 36,928 hrs · 20,171 cycles

RT IB AFT FLAP IS DENTED ON UPPER SURFACE 1.5" AFT OF FWD SPAR AND 51" IB OF OB END. REPAIRED DENT DAMAGE ON UPPER SURFACE OF RT IB AFT FLAP 1.5" AFT OF FWD SPAR AND 51" IB OF OB END IAW SRM 51 70 10 REPAIR 4 PG 201.

Part: SKIN — DENTED (TE FLAP) · airframe 36,928 hrs · 20,171 cycles

RT IB AFT FLAP IS DENTED ON UPPER SURFACE 1" AFT OF FWD SPAR AND 7" IB OF OB END. REPAIRED DENT DAMAGE ON UPPER SURFACE OF RT IB AFT FLAP 1" AFT OF FWD SPAR AND 7" IB OF OB END IAW SRM 51 70 10 REPAIR 4 PG 201.

Part: SKIN — GOUGED (MID FLAP) · airframe 36,928 hrs · 20,171 cycles

RT OB MID FLAP LOWER SURFACE SKIN GOUGED. REMOVED DAMAGE FABBED FILLERS AND DOUBLERS INSTALLED REPAIR IAW EA 13093 AND SRM 57 53 01 FIG 201.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 36,928 hrs · 20,171 cycles

RT OTBD MID FLAP LOWER SURFACE GOUGED. REMOVED DAMAGED AREA FABRICATED FILLERS AND DOUBLER INSTALLED REPAIR IAW SRM 57-53-01 FIG 201 EA 13093.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 36,928 hrs · 20,171 cycles

NR 1 FLAP TRACK CRACKED ON IB UPPER FLANGE. REMOVED CRACKED FLAP TRACK INSTALLED REPLACEMENT TRACK IAW B737 400 MM 27 51 49.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 36,928 hrs · 20,171 cycles

LT WING NR 1 SLAT CRACK ON LOWER TE AT RIVET 19" FROM OB OF ACTUATOR MARKED. REPAIRED LT WING NR 1 SLAT IAW B737 400 SRM 57 43 01 FIG 201.

Part: FITTING — GOUGED (RT AILERON) · airframe 36,928 hrs · 20,171 cycles

RT AILERON O/B CORNER FWD EDGE FITTING IS GOUGED. REMOVED GOUGED FITTING INSTALLED REPLACEMENT FITTING IAW B737 SRM 51 40 02.

Part: SKIN — DAMAGED (LT MID FLAP) · airframe 29,552 hrs · 16,157 cycles

LEFT OUTBOARD MIDFLAP UPPER SURFACE CHAFED AT OUTBOARD END. LEFT OUTBOARD MIDFLAP UPPER SURFACE REPAIRED IAW SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (LT MID FLAP) · airframe 29,552 hrs · 16,157 cycles

LEFT OUTBOARD MIDFLAP L/E CHAFED AT INBOARD END. LEFT OUTBOARD MIDFLAP L/E CHAFED AREAS AT INBOARD END REPAIRED AND MADE SERVICEABLE ON WING AND ADJUSTMENT CHECK CARRIED OUT AND FOUND SERVICEABLE IAW SRM 57 53 01 AND AMM 27 51 34 501.

Part: SKIN — CHAFED (LT MID FLAP) · airframe 29,552 hrs · 16,157 cycles

LEFT INBOARD MIDFLAP UPPER SURFACE INBOARD EDGE SKIN CHAFED. LT INBOARD MIDFLAP UPPER SKIN CHAFED AREAS REPAIRED ON WING AND MADE SERVICEABLE AND GAP CHECK CARRIED OUT FOUND SERVICEABLE IAW SRM 57 53 01 AND AMM 27 51 04 401.

Part: STRINGER CLIP — CRACKED (BS 500G) · airframe 29,552 hrs · 16,157 cycles

TIE CLIP CRACKED. CRACKED TIE CLIP REPLACED WITH FABRICATED REPAIR PART IAW SRM 51 04 02.

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5. REMOVED UPPER CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 5310-02512. (M)

Part: REPAIR — UNKNOWN (FUSELAGE)

OKC - FOUND INTERIM EXTERNAL DOUBLER REPAIR PREVIOUSLY INSTALLED AT BS 279, STRINGER 17-18 LEFT. REMOVED INTERIM REPAIR, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ASA EA 5310-02513. (M)

Part: STIFFENER — DAMAGED (WING)

OKC - FOUND DURING ACCOMPLISHMENT OF EO 5710-01108, 1 FASTENER HOLE COMMON TO LBL 6.15 STIFFENER WAS OVERSIZED BEYOND ALLOWABLE DIAMETER TO REMOVED DAMAGE. REAMED HOLE TO .388/.391 DIAMETER, INSTALLED FASTENER IAW ASA EA 5710-01123. (M)

Part: FRAME — DAMAGED (FUSELAGE)

OKC - FOUND BS 277 FRAME WEB DAMAGED AT BS 17-18 LEFT DOUBLER REPAIR. REMOVED DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED REPAIR ANGLE IAW ASA EA 5310-02511. (M)

Part: SKIN — GOUGED (FS 792-824)

OKC - MULTIPLE SKIN GOUGES BELOW AFT PIT DOOR SCUFF PLATE LOWER FORWARD AREA. SKIN REPAIR PER B737-400 SRM 53-00-01 FIG 201 REPAIR IS CATEGORY "B", HOLES HAVE BEEN ZERO TIMED. (M)

Part: SKIN — CHAFED (NR 1 SLAT)

OKC - NR 1 SLAT T/E LOWER SURFACE IS CHAFED AND CRACKED AT O/B CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737-400 SRM 51-70-10. (M)

Part: TAB — BENT (RT ELEVATOR)

OKC - FOUND RIGHT ELEVATOR TAB BENT AT T/E. PREPPED AREA, BONDED REPAIR PER B737-400 SRM 51-70-05 FIGURE 8. (M)

Part: CREASE BEAM — CORRODED (FS 312-343)

PAE - FOUND FORWARD CABIN CREASE BEAM CORRODED AT INNER CHORD, SEVERAL AREAS AT L1 DOOR. REMOVED AND REPLACED CREASE BEAM INNER CHORD IAW B737-400 SRM 51-40-02 PAGE 2. (M)

Part: SHEAR TIE — CORRODED (BS 787)

PAE - AFT CARGO COMPARTMENT CORRODED SHEAR TIE AT BS 787 BETWEEN STRINGER 26 RIGHT AND 27 RIGHT. REMOVED CORRODED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED IAW 737-400 SRM 53-00-07 FIGURE 201. (M)

Part: SKIN — CHAFED (NR 1 SLAT)

OKC - FOUND NR 1 SLAT LOWER T/E IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: WEB — CORRODED (FS 344-348)

OKC - FOUND WEB AROUND L1 DOOR CUTOUT CORRODED AT BS 344, WL 208.5. REMOVED WEB, FABRICATED AND INSTALLED REPLACEMENT WEB IAW 737-400 SRM 51-30-01 FIGURE 7 AND DWG 6517685. (M)

Part: SKIN — DELAMINATED (NR 5 SLAT)

OKC - NR 5 SLAT INBOARD TRAILING EDGE IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — PUNCTURED (TE FLAP)

OKC - FOUND DURING RIGHT WING INBOARD MID FLAP T/E PANEL LOWER SKIN IS PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES PER B737-200 SRM 51-70-10. (M)

Part: SKIN — DAMAGED (TE FLAP)

OKC - FOUND RIGHT OUTBOARD AFT FLAP IS DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED CORE AND DOUBLER PER B737-200 SRM 51-70-10. (M)

Part: CREASE BEAM — CORRODED (FS 947-987)

OKC - FOUND CORROSION ON CREASE BEAM AT L-2 DOOR, BS 947-987. REMOVED CORRODED PART AND REPLACED WITH NEW PART PER B737-200 SRM 51-40-2. (M)

Part: SHEAR TIE — DENTED (FS 500C)

OKC - FOUND SHEAR TIE AT BS 500C STRINGER 28 LEFT-28-RT IS CORRODED. REMOVED CORRODED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-02 FIG 201. (M)

Part: SKIN — DELAMINATED (RT AILERON)

OKC - FOUND RIGHT AILERON LOWER SKIN DELAMINATED ON FORWARD INBOARD CORNER. PREPPED AREA, APPLIED BONDED GRAPHITE LAYUP IAW B737-400 SRM 51-70-17. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY, DOOR THRESHOLD CORRODED UPPER SURFACE BS 794-834, RBL 25 TO 34, WL 156. REPLACED AFT CARGO BAY DOOR THRESHOLD UPPER SURFACE BS 794-834, RBL 25-34, WL 156. (M)

Part: STRINGER — GOUGED (FUSELAGE)

PAE - FOUND STRINGER IS GOUGED AT AFT CARGO BAY. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: STRINGER — GOUGED (FUSELAGE)

PAE - FOUND STRINGER IS GOUGED AT AFT CARGO BAY. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND AFT CARGO BAY, FLOOR SUPPORT CORRODED AT BS 794 TO 847. REMOVED AND REPLACED FLOOR SUPPORT. (M)

Part: SUPPORT — CORRODED (FS)

PAE - FOUND AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT AT BS 930-947, RBL 23 HAS CORROSION AT NUTPLATE LOCATIONS. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT BS 930-947, RBL 23. (M)

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE)

PAE - FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED FLOOR TO SIDEWALL SUPPORT. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED FLOOR TO SIDEWALL SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,983 hrs · 14,795 cycles

PAE - AFT CARGO BAY, AT PREVIOUS REPAIR, FLOOR SUPPORT CORRODED AND MISSING NUTPLATES UNDER FLOOR SPLICE AT B-STA 771, WL 156, LBL 3. REMOVED CORRODED FLOOR SUPPORT AT PREVIOUS REPAIR, FABRICATED AND INSTALLED REPAIR PARTS. (K)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,561 hrs · 12,946 cycles

LT AFT OUTSIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK.

Part: SKIN — DENTED (FUSELAGE)

GYR - FOUND TEMP REPAIR TO DENT IN EXTERIOR SKIN. REPAIRED DENT IN FUSELAGE SKIN AT STATION 279 BETWEEN STRINGER 18L-19L IAW SRM. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

PAE - DURING C-CHECKED, FOUND SHELF SUPPORT ABOVE AUTOGYROS IN E/E BAY IS CRACKED. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION ON UPPER SURFACE RIGHT BS 847. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORTS HAVE CORROSION ON UPPER SURFACES AT BS 727 TO BS 877. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT AT LEFT BL 24 TO RT BL 24. REPAIRED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 AND 15 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: DOOR MECHANISM — LACK OF LUBE (L1 DOOR)

SEA - FLIGHT 429 - L1 DOOR DIFFICULT TO OPEN AND WAS MAKING A POPPING SOUND WHEN OPENING AND CLOSING. INSPECTED DOOR AND FOUND CAM PLATE DRY. LUBRICATED DOOR HINGES AND SNUBBER. DOOR OPERATED NORMALLY. (M)

Part: MECHANISM — LUBE (L1 DOOR)

SEA - PRIOR TO FLT 681 - THE L1 DOOR WAS VERY DIFFICULT TO OPEN. LUBRICATED THE L1 DOOR CAM PLATES AND THE DOOR OPERATED NORMALLY. (M)

Part: GUIDE ARM — OUT OF ADJUST (PASSENGER DOOR)

SEA - PRIOR TO FLT 446, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. ADJUSTED UPPER GUIDE ARM AND DOOR OPERATED NORMALLY. (M)

Part: DOOR — LACK OF LUBE (LT DOOR)

SFO - FLT 291 - PRIOR TO FLIGHT, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (X)