N795AS

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 55,228 hrs · 30,987 cycles

THE FLIGHT DECK EMERGENCY LIGHT (DOME LIGHT ABOVE SECOND JUMPSEAT) SEEMS TO HAVE A LOOSE CONNECTION AS IT DOES NOT ILLUMINATE EVERY TIME BUT WILL ILLUMINATE IF THE PLASTIC COVER IS TAPPED. GROUNDED - YES. EXAMINED WIRING AT FLIGHT DECK EMERGENCY LIGHT MOUNTING AND FOUND NO DAMAGE. RE-LAMPED FLIGHT DECK EMERGENCY LIGHT AND OPS CHECK IS NORMAL. REF AMM 33-51-42.

Part: CARGO TRACK — CORRODED (BS 794) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

CARGO TRACK BS 794, LBL 17.20 CORRODED. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: STIFFENER — CORRODED · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFTER REMOVAL OF THE BS 1088, BULKHEAD APU AIR INLET RT STIFFENER FOUND CORRECT ON BULKHEAD WEB. ACFT GROUNDED. BLENDED STA 1088 BULKHEAD AT RBL 22, OUT OF LIMITS, REPAIRED AREA IAW EA 400, 53EA 14565, SRM 53-80-08-2R 8, REPAIR 8, 53 8008 1A 1, W 1.00, O .032, R .028, L 1.00, D .004.

Part: BULKHEAD WEB — CORRODED (BS 1088) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFTER REMOVAL OF THE BS 1088, BULKHEAD APU AIR INLET LT STIFFENER THE BULKHEAD WEB WAS FOUND CORRODED UNDER IT. ACFT GROUNDED. BLENDED STA 1088, BULKHEAD AT RBL 34, OUT OF LIMITS REPAIRED AREA IAW EA 400-53EA 14565, SRM 53-80-08-2R-8, REPAIR 8-53-80-08, 1A, 1W 1.00, O .032, R .028, L 1.00, D .004.

Part: SKIN — CORRODED · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

WHILE CLEANING THE CENTER WING BOX AT STA 663.5 AT, APPROXIMATELY RBL 64 NOTICED THAT WHAT APPEARED TO BE ANOTHER HIGH LOCK IN THE AREA WOULD FLEX WHILE CLEANING. UPON FURTHER INVESTIGATION FOUND THAT IT WAS A POCKET THAT WAS CORRODED UNDER THE FUEL VAPOR BARRIER. ACFT GROUNDED. REMOVED CENTER WING, SECTION UPPER SKIN CORRODED AT BS663, RBL 64 AND ACCOMPLISHED CORROSION BLEND REPAIR IAW EA NR 400, 57EA 14573. THIS IS A CAT A REPAIR. HOWEVER MFG RECOMMENDS THAT PERFORMS REPEAT VISUAL INSPECTIONS EVERY 24 MOS. TO AVOID POTENTIAL CORROSION DEVELOPMENT IN THE FUTURE REFER TO T/C 400 57 EA 14574 FOR INSPECTIONS W 2.07, O .180, R .097, L 1.19, D .083.

Part: SKIN — CORRODED (BS 1088) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

TAIL COMPARTMENT, BS 1088 BULKHEAD APU AIR INLET CUTOUT RT LANDING HAS CORRECTED ON FWD SIDE. ACFT GROUNDED. R & R APU INLET RT LANDING IAW SRM 51-40-02-0G-0 AND SRM 51-30-01 0G-0, W .75 N, O .070, R .061, L 2.0, D .009.

Part: SKIN — CORRODED (BS 1088) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

FS 1088, BULKHEAD RT APU AIR INLET CUTOUT LT LANDING HAS CORROSION ON FWD SURFACE. ACFT GROUNDED. R & R APU INLET LT LANDING IAW SRM 51-40-02-0G-0 AND SRM 51-30-01-0G-0 W .75", O .070", R .052", L 3.0", D .018".

Part: ANGLE — CORRODED (BS 400-420) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

L1 DOOR CUTOUT LOWER SCUFF PLATE SUPPORT IS CORRODED. ACFT GROUNDED. BLENDED L1 DOOR SCUFF PLATE SUPPORT FOUND TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW SUPPORT IAW SRM 53-30-51-1A-1 AND SRM 51-40-02-0G-0, W 1, O .050, R .044, L 1, D .006.

Part: FRAME — CRACKED (BS 827) · airframe 53,072 hrs · 29,632 cycles

FRAME AT BS 827 HAS EVIDENCE OF A CRACK AT THE INBD FASTENER HOLE FOR BRACKET BETWEEN STRINGERS 8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW DWG A5310025688.

Part: ANGLE — CRACKED (BS 294) · airframe 53,072 hrs · 29,632 cycles

BS 294, STRINGER 12R ANGLE CRACKED. ACFT GROUNDED. R & R CRACKED ANGLE IAW SRM 51 40-02-0G-0.

Part: ATTACH BRACKET — CORRODED (BS 312) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

L1 DOOR EMERGENCY FLOOR FITTING ATTACHMENT BRACKET CORRODED. ACFT GROUNDED. REMOVED CORROSION CHECK OUT OF LIMITS IAW SRM 5-30-51-1A-1 R & R ATTACH BRACKET ASSY IAW SOPM 20-50-01, W 2", O .071, R .062, L 2', D .009.

Part: CHANNEL — CORRODED (BS 986-1006) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT DRAIN MAST SUPPORT CHANNEL CORROSION DAMAGE. ACFT GROUNDED. REPLACED DRAIN MAST SUPPORT CHANNEL IAW EA AD20122314-400-53-102 REV NEW ISSUED 20FEB15. THIS IS A CAT A REPAIR.

Part: CHANNEL — CORRODED (BS 290-344) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

RT MOP SILL HAS MULTIPLE CORRODED AREAS FROM BS 290 - 344. ACFT GROUNDED. REMOVED AND REPLACED THE MOP SILL IAW SRM 51 40-02-0G-0 , 53-10-15-1A-1.

Part: CHANNEL — CORRODED (BS 294-332) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

RT MOP SILL STRAP CORRODED AT BS 294. ACFT GROUNDED. R & R THE MOP SILL IAW SRM 51-40-02-0G-0.

Part: RIB — CRACKED (WING) · airframe 53,072 hrs · 29,632 cycles

RIGHT WBL 135.5 WING RIB LOWER CHORD IS CRACKED BETWEEN LOWER STRINGERS 2 AND 3. ACFT GROUNDED. REPAIRED LOWER CHORD RIB AT WBL 135.5. BETWEEN STR 2R AND STR 3R IAW EA 400 57 EA 14548.

Part: FRAME — DENTED (BS 500D) · airframe 53,072 hrs · 29,632 cycles

FWD CARGO BAY FRAME 500D, LBL 40, DAMAGED AND DENTED. ACFT GROUNDED. REPAIRED THE FRAME IAW EA 53EA14531, THIS REPAIR IS A CAT B REPAIR WITH STAGE II DTI.

Part: FLOOR SUPPORT — CORRODED (BS 767) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0-W-1.00.

Part: SUPPORT — CORRODED (BS 294-332) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

R1 DOOR CUTOUT THRESHOLD SUPPORT HAS MULTIPLE CORROSION SPOTS. ACFT GROUNDED. R & R THRESHOLD SUPPORT IAW SRM 51-40-02-0G-0, W 1, O .090, R .073, L 2", D .017.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 53,072 hrs · 29,632 cycles

LEFT INBD MIDFLAP UPPER INBD OUTER SKIN CHAFED. ACFT GROUNDED. REMOVED LT MIDFLAP UPPER INBD OUTER SKIN SECTION FABRICATED AND INSTALLED NEW SKIN IAW SRM 57-53-01-2R-3 FIG 201, REPAIR 3.

Part: FRAME — CORRODED (BS 992) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT WET AREA BS 992.8, RT FRAME CORRODED WL 196 - 214. ACFT GROUNDED. REPAIRED FRAME IAW EA 400, 53EA, 14535 REV NEW ISSUED 19FEB15 THIS REPAIR HAS STAGE II DTI APPROVAL AND REQUIRES STAGE III DTI APPROVAL ON OR BEFORE 66000 TOTAL FLIGHT CYCLES AT TIME OF REPAIR 29,631, W .75, O .063, R .052, L 2.0, D .019.

Part: SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT WET AREA LT OTBD LAVATORY SUPPORT BS 954, LBL 50 HAS AREA OF CORROSION. ACFT GROUNDED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. R & R THE LAVATORY SUPPORT IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 927-947) · airframe 53,072 hrs · 29,632 cycles

AFT WET AREA INTERCOSTAL BS 927-947.5, LBL 25 IS CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT WET AREA BS 986 FLOORBEAM CORRODED AT LBL 44, LBL 4 AND RBL 44 ON UPPER CAP. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 400, 53EA 14519, REV NEW ISSUED 18FEB15, W 1.00, O .150, R .119, L 6.00, D .031.

Part: SKIN — CRACKED (AIR DOOR) · airframe 53,072 hrs · 29,632 cycles

GROUND AIR DOOR RT LAND AREA IS DAMAGED. ACFT GROUNDED. REPAIRED GROUND AIR DOOR LANDING IAW SRM 53-30-01-2R-2, REPAIR 2.

Part: DOOR SILL — CORRODED (BS 887-1006) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT WET AREA R2 DOOR SILL CORRODED. ACFT GROUNDED. R & R DOOR SILL IAW SRM 51-40-02-0G-0 AND DWG 65 45855.

Part: FRAME — CORRODED (BS 992) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT WET AREA BS 994 LT FRAME CORRODED ABOVE WL 208. ACFT GROUNDED. REPAIRED 994 LT FRAME IAW EA 400, 5 EA 14523. THIS REPAIR IS PROVIDED WITH STAGE II DTI AND REQUIRES STAGE III DTI ON OR BEFORE 60000 TOTAL ACFT FLT CYCLES. CURRENT ACFT CYCLES AT TIME OF REPAIR 29, 631.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 53,072 hrs · 29,632 cycles

LEFT OTBD FORE FLAP INBD L/E CHAFED. ACFT GROUNDED. REPAIRED LT OTBD FOREFLAP INBD L/E IAW SRM 57-53-01-2R-1. REPAIR 1, IAW SRM.

Part: SKIN — CHAFED (BS 1104) · airframe 53,072 hrs · 29,632 cycles

LT HORIZONTAL STABILIZER TO FUSELAGE AT AFT ATTACH FITTING LOWER SIDE SKIN PLATE DIRECTLY BELOW THE FITTING CHAFED/KNIFE EDGED. ACFT GROUNDED. REMOVED DAMAGE AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1, FIG 101. R & R LWR SIDE SCREW PLATE IAW SRM 51-40-02-0G-0, PARA 4B AND AMM 20-50-11-912-002.

Part: DOOR FRAME — CRACKED (BS 348) · airframe 53,072 hrs · 29,632 cycles

L1 DOOR CUTOUT FRAME 348.2 INNER CHORD IS CRACKED IN LOWER HOLE AT FLOOR LINE. ACFT GROUNDED. R & R CRACKED L1 DOOR CUTOUT FRAME AT 348.2 IAW SRM 51-40-02-0G-0 AND IN CONJUNCTION WITH TASK CARD AD20121205 400-53-2.

Part: FRAME — CORRODED · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT FWD END LIGHT SWITCH, CUTOUT STA 794, VIEWED FROM BACKSIDE OF FRAME, CORRODED BELOW RETAINING NUT. ACFT GROUNDED. REPAIRED FRAME AND REPLACED DOUBLER IAW EA 400, 53EA, 14576 REV NEW ISSUED 24FEB15. THIS IS A CAT B REPAIR WITH FIRST, SECOND AND THIRD STAGE APPROVAL. SUBJECT REPAIR HAS BEEN FOUND IN COMPLIANCE WITH 14 CFR PART 26, SECTION 26.43.D WITHOUT ANY ADDITIONAL SUPPLEMENTAL INSPECTIONS BEYOND WHAT IS REQUIRED IAW AD 2005 07-19 AND SB 53A 1228, REV O, W2 .071, O 1.18, R 1.196, L 1.0, D .016.

Part: DOOR FRAME — CHAFED (BS 486-490) · airframe 53,072 hrs · 29,632 cycles

FWD CARGO DOOR BOTTOM EDGE FRAME AFT CORNER HAS A CHAFED AREA. ACFT GROUNDED. REMOVED CHAFED ANGLE AT AFT CORNER AND REPLACED WITH NEW ANGLE IAW SRM 51-40-02-0G-0.

Part: SKIN — CORRODED (SERVICE PANEL) · corrosion level 2 · airframe 53,072 hrs · 29,632 cycles

POTABLE WATER SERVICE PANEL CUTOUT INNER SKIN IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, CK OUT OF LIMITS IAW SRM 53-00-01-1A. R & R POTABLE WATER SERVICE PAN IAW SRM 5-40-02-0G-0, W 2", O .06, R .053, L 2', D .010.

Part: SKIN — GOUGED (BS 947-967) · airframe 53,072 hrs · 29,632 cycles

POTABLE WATER SERVICE PANEL DOOR LANDING IS GOUGED UNDER AFT DOOR HINGE. ACFT GROUNDED. REPAIRED POTABLE WATER SERVICE DOOR LANDING IAW EA 400, 53EA 14533.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 53,072 hrs · 29,632 cycles

AFT CARGO BAY FLOOR PANEL IS CRACKED. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW SRM 51-40-05, SRM 51-20-01 AND SOPM 20-41-02.

Part: RIB — CRACKED (LT WING) · airframe 53,033 hrs · 29,602 cycles

LEFT WBL 135.5 WING RIB LOWER CHORD IS CRACKED BETWEEN LOWER STRINGERS 2 AND 3. ACFT GROUNDED. REPAIRED LOWER CHORD RIB AT LT WBL 135.5 BETWEEN STR 2L - STR 3L IAW EA 400 57 EA 14548.

Part: DOOR — OUT OF ADJUST (L1) · airframe 50,225 hrs · 27,914 cycles

L1 DOOR VERY HARD TO CLOSE ON LAST DETENT. ACFT GROUNDED. ADJUSTED L1 DOOR IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: HOUSING — GOUGED (DOOR HANDLE) · airframe 50,080 hrs · 27,842 cycles

AFT CARGO BAY DOOR HANDLE STOW CASTING APPEARS GOUGED. ACFT GROUNDED. REMOVED INTERIOR & EXTERIOR AFT CARGO PIT DOOR HANDLES, REF MM 52-31-14-004. R & R AFT PIT CARGO DOOR HANDLE HOUSING REF SRM 51-40-02. NOTE- PERFORMED HFEC OF FASTNER HOLES IAW NDT PART 6 51-00-00 PROCEDURE 16 NO DISCONTINUITIES NOTED. INSTALLED INTERIOR & EXTERIOR DOOR HANDLES, REF MM 52-31-14-004-054.

Part: HOUSING — GOUGED (DOOR HANDLE) · airframe 47,977 hrs · 26,594 cycles

FWD CARGO DOOR HANDLE HOUSING IS GOUGED .065 DEEP ON UPPER LANDING AREA. LOWER AREA IS ALSO GOUGED. DAMAGE IS OUT OF LIMITS AF AMM 52-31-15-801. REMOVED FWD CARGO DOOR HANDLE ASSY REF AMM 52-31-14-004-035. REMOVED OLD HOUSING & DRILLED NEW ONE REF SRM 51-40-02. INSTALLED NEW HANDLE HOUSING IAW SRM 51-40-02. INSTALLED NEW FWD CARGO DOOR HANDLE ASSY IAW AMM 52-31-14-004-054, OPS CHECKED GOOD.

Part: HOUSING — GOUGED (DOOR HANDLE) · airframe 47,977 hrs · 26,594 cycles

FWD CARGO DOOR HANDLE HOUSING IS GOUGED .065 DEEP ON UPPER LANDING AREA. LOWER AREA IS ALSO GOUGED. DAMAGE IS OUT OF LIMITS AF AMM 52-31-15-801. REMOVED FWD CARGO DOOR HANDLE ASSY REF AMM 52-31-14-004-035. REMOVED OLD HOUSING, ALSO DRILLED UP NEW 1 REF SRM 51-40-02. INSTALLED NEW HANDLE HOUSING REF SRM 51-40-02. INSTALLED NEW FWD CARGO DOOR HANDLE ASSY IAW AMM 52-31-14-004-054, OPS CHECKED GOOD.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 47,932 hrs · 26,559 cycles

EMERGENCY LIGHT PHOTOLUMINESCENT ESCAPE PATH STRIP ON LT SIDE OF AISLE ADJACENT TO ROW 19 A,B,C IS CRACKED, BROKEN, AND LOOSE. R & R GLOWSTRIP IAW MM 33-51-91-960-801C1.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 47,312 hrs · 26,202 cycles

LT OTBD FORE FLAP INBD L/E HAS A HOLE. REMOVED AND INSTALLED A NEW SKIN IAW AMM 20-50-11-912-002, FIG 202.

Part: STRINGER — DENTED (BS 312) · airframe 47,312 hrs · 26,202 cycles

BS 312, STRINGER 24R IS BENT ALONG BOTTOM OF VERTICAL FLANGE, APPROX 2 INCHES LONG. REPAIRED IAW EA 400-53EA-09424.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 47,312 hrs · 26,202 cycles

LEFT WING OTBD FORE FLAP LWR SURFACE AT INBD END HAS A CREASE AND SEVERAL DENTS JUST OTBD OF A PREVIOUS REPAIR. REPAIRED SKIN DAMAGE IAW SRM 51-70-10, REPAIR 4 PG 201 PAINT T/U ON WO 1009234-500-0002, AP-16-28127, AP-17 ITEM 3.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,312 hrs · 26,202 cycles

LT WING INBD MIDFLAP INBD END UPPER SURFACE IS CHAFED. CHAFE FOUND TO BE 100 PERCENT OUT OF LIMITS IAW SRM 57 53 01. R & R SKIN IAW SRM 51-40-02.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,312 hrs · 26,202 cycles

LEFT WING OTBD FORE FLAP OTBD L/E IS CHAFED ON A PREVIOUS REPAIR. REMOVED CHAFED DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 51-40-02 AND 57-53-01, FIG 201.

Part: SKIN — DENTED (BS 332-333) · airframe 46,271 hrs · 25,574 cycles

SHARP DENT AND GOUGE JUST AFT OF R1 DOOR AT S13R APPROXIMATELY SIX INCHES AFT OF DOOR CUTOUT AFT EDGE. CONDITION IS OUT OF LIMITS IAW SRM 53-00-01, AD-1. BLENDED OUT GOUGE IAW SRM 53-00-01. PERFORMED HFEC OF BLENDED AREA IAW MANUAL PART 6 51-00-00, FIG 23. NO CRACKS NOTED. ACCOMPLISHED EXTERNAL REPAIR IAW EA 400-53, EA-08354, REV NEW.

Part: GUIDE ARM — OUT OF ADJUST (R1 DOOR) · airframe 44,682 hrs · 24,709 cycles

R1 DOOR HITS OVEN ENCLOSURE WHEN OPENING. FOUND GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM. REF AMM 52 41 21 404 004 STEP C.6. 1. & 2. FOUND TWO FWD CENTER STOP PINS FROZEN. REPLACED FROZEN STOP PIN BUSHINGS ON FWD CENTER OF R 1 DOOR & ADJUSTED ALL STOP PINS REF AMM 52 41 00 705 041 001 1 FIG 508 & COMPONENT MAINT MANUAL 52 46 06 STEP E (2). ACCOMPLISHED R1 DOOR OPERATIONAL TESTS & GALLEY SERVICE DOOR TEST. TESTED GOOD REF AMM 52 41 00 705 001 001 1 & 52 41 00 705 041 001 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,382 hrs · 24,557 cycles

CRACKED FRAME STA 616 ABOVE STR 18R. REPAIRED FRAME IAW AD 20102506 400 53 12 AND ASA EA 400 53EA 06916.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 44,382 hrs · 24,557 cycles

WIRE ATTACH BRACKET CRACKED. REPLACED BRACKET.

Part: ANGLE — CRACKED (RT WING) · airframe 44,382 hrs · 24,557 cycles

RIGHT WING LOWER FIXED L/E ANGLE CRACKED AT LES 198. REPLACED ANGLE AND CLIP.

Part: FITTING — CRACKED (RT WING) · airframe 44,382 hrs · 24,557 cycles

WHILE REMOVING CRACKED ANGLE ON CUST CARD 5351122 FOUND CRACKED CLIP FOR THE ANGLE (CHANNEL). REPLACED CLIP.

Part: SKIN — CRACKED (LT ELEVATOR TAB) · airframe 44,382 hrs · 24,557 cycles

LT ELEVATOR TAB UPPER SURFACE SKIN IS CRACKED AT FORWARD HINGE CUTOUT O/B RADIUS O/B NR 1 HINGE FITTING. REPLACED TAB ON CUST CARD 5351211 AND T/C 5520 01234 2 REF AD 2006 12 23.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,382 hrs · 24,557 cycles

AFT BULKHEAD BS 947 BILGE AREA INTERCOSTAL ATTACH ANGLE CRACKED RBL 19. GROUNDED YES. REMOVED FABRICATED INSTALLED BS 947 INTERCOSTAL ATTACH ANGLE AT RBL 19 PER SRM 51 40 02 DWG 65 49680

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,382 hrs · 24,557 cycles

AFT BULKHEAD BS 947 BILGE AREA STRINGER CLIP CRACKED RBL 16. GROUNDED YES. FOUND BS 947 RBL 16 STR CLIP TO BE OUT OF LIMITS. REPLACED IAW SRM 53 00 03 FIG 101. ALLOWABLE DAMAGE 2 CRACKS NOT PERMITTED 51 40 02 STEPS 4. SRM 51 40 05 FIG 2 TABLE I SRM 51 20 01 STEP 4G (1) (4) AND SOPM 20 11 02 STEO 2G.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 43,045 hrs · 23,699 cycles

F/A'S REPORT FUMES FROM ROW 10 22. OCCURRED TWICE FOR 10 20 SECONDS. SMELLED LIKE WOOD BURNING OR ELECTRICAL FUMES. NO SMOKE REPORTED. PER CHECKLIST RECIRC FAN BOTH OFF BUS TIE OFF GALLEY POWER OFF. GALLEY POWER TURNED BACK ON LATER PER PILOT DISCRETION CHECKLIST NO FURTHER FUMES FOR DURATION OF FLIGHT (LAST APROX 1+ 30 HOURS). REMOVED AND REPLACED LT RECIRCULATION FAN AND PERFORMED OPERATIONAL CHECK IAW B737 400 AMM 21 21 22.

Part: SEAL — OUT OF ADJUST (ENTRY DOOR) · airframe 41,855 hrs · 23,033 cycles

F/A REPORTS L2 DOOR HARD TO CLOSE & HITS TOP OF FRAME. ADJUSTED DOOR LINER SEAL AND DOOR OPERATION CHECKED IAW B737 400 MM 52 13 00 705 034.

Part: WEB — DAMAGED (FUSELAGE) · airframe 4,112 hrs · 22,573 cycles

PREVIOUS BLEND OUTS OUT OF LIMITS ON AFT CARGO DOOR CUTOUT LOWER SILL VERTICAL WEB. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.

Part: SKIN — CHAFED (TE FLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT O/B MID FLAP SKIN CHAFED NR 2 AFT FLAP TRACK CUTOUT. REMOVED DAMAGED AREA AND BONDED DOUBLER.

Part: SKIN — ACTIVATED (TE FLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT O/B MID FLAP LOWER SKIN CHAFED AT NR 1 AFT FLAP TRACK CUTOUT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

STRINGER CLIP STA 500G STR 25A CRACKED AT RIVET. REMOVED STRINGER CLIP AND INSTALLED NEW CLIP.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

FRAME STA 847 STR CORRODED. REMOVED CORRODED FRAME AND INSTALLED NEW FRAME.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

INTERCOSTAL CORRODED BETWEEN FRAME STA 847 - 867 AT STR 26R. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW ONE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT TRANSITION Z-ANGLE BETWEEN STA 847 - 867 CORRODED. REMOVED CORRODED ANGLE AND INSTALLED NEW Z-ANGLE.

Part: SKIN — CHAFED (LE SLAT) · airframe 41,102 hrs · 22,573 cycles

NR 2 SLAT AFT LOWER SURFACE CHAFED SEVERAL AREAS. REMOVED DAMAGED SKIN AND BONDED REPAIR DOUBLERS.

Part: SKIN — CHAFED (LE SLAT) · airframe 41,102 hrs · 22,573 cycles

NR 3 SLAT AFT LOWER SURFACE CHAFED SEVERAL AREAS. REMOVED DAMAGED SKIN AND BONDED REPAIR DOUBLERS.

Part: SKIN — CHAFED (TE FLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT O/B FOREFLAP I/B END LEADING EDGE IS CHAFED. REMOVED LEADING EDGE SKIN AND INSTALLED NEW SKIN.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

STRINGER CLIP STA 847 - STR 27R CRACKED. REMOVED CLIP AND INSTALLED NEW.

Part: SKIN — CHAFED (LE SLAT) · airframe 41,102 hrs · 22,573 cycles

NR 1 SLAT AFT LOWER SURFACE CHAFED SEVERAL AREAS. REMOVED DAMAGED SKIN AND BONDED REPAIR DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 787L HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

CRACKS ON FRAME AT BS 500G. ONE CRACK IS AT RBL 13.8 THE OTHER AT RBL 21. REPAIRED FRAME.

Part: SKIN — DENTED (LE SLAT) · airframe 41,102 hrs · 22,573 cycles

NR 5 SLAT HAS PROTRUDING DENT 38 INCHES FORM O/B EDGE. REMOVED DAMAGED SKIN, FABRICATED AND BONDED REPAIR DOUBLER.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

FWD PIT SHEAR TIE AT STA 500 IS CRACKED AND CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED SHEAR TIE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 827L HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,102 hrs · 22,573 cycles

NR 5 SLAT I/B AFT CORNER DELAMINATED. REMOVED DAMAGED SKIN, FABRICATED AND BONDED REPAIR DOUBLER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FWD CARGO PIT STRINGER CLIP IS CRACKED AT STA 500G. REMOVED DAMAGED STRINGER CLIP AND REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 400L HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 440L HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 747L HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

FWD CARGO PIT SHEAR TIE CORRODED AT 500E. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED SHEAR TIE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 727F HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STATION 727D HAS CRACK BETWEEN STRINGERS 8 & 9 AT OH BIN MOUNT FASTENERS. REMOVED DAMAGED AREA INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

FRAME AT STA 500G CRACKED BETWEEN STR 27L AND 26L. CUT OUT DAMAGE AND INSTALLED REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT LT STA 727F FRAME HAS 2 DENTS ON UPPER SURFACE. REMOVED DAMAGED AREA AND INSTALLED REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT RT 727F FRAME HAS DENT ON UPPER SURFACE ABOVE STR 24R. REMOVED DAMAGED AREA AND INSTALLED REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT RT 727C FRAME DENTED UPPER SURFACE BETWEEN STR 24 & 25. REMOVED DAMAGED AREA AND INSTALLED REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT RT 747 FRAME DENTED UPPER SURFACE BETWEEN STR 24 & 25. REMOVED DAMAGED AREA AND INSTALLED REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT SHEAR TIE FRAME AT STA 727E BETWEEN STR 27R & 26R CORRODED. REMOVED AND REPLACED SHEAR TIE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

L1 DOOR SILL INNER CHORD ANGLE CORRODED STA 312. REMOVED CORRODED CHORD ANGLE AND REPLACED WITH NEW.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

FLOORBEAM AT STATION 986 HAS CORROSION AT FIRST FASTENER HOLE NEXT TO L2 DOOR SILL. REPAIRED FLOORBEAM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

AFT PIT SHEAR TIE CORRODED AT STA 867 BETWEEN STR 26L AND 27L ON EXISTING REPAIR. REMOVED EXISTING REPAIR DOUBLER AND ANGLES AND INSTALLED NEW.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,102 hrs · 22,573 cycles

L2 DOOR SILL HAS CORROSION FROM STA 946 TO 986.5. REMOVED DAMAGED DOOR SILL AND INSTALLED NEW.

Part: SKIN — CHAFED (TE FLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT WING I/B AFT MID FLAP UPPER I/B SKIN CHAFED AT PREVIOUS REPAIR. REMOVED DAMAGED SKIN AND INSTALLED NEW REPAIR.

Part: SKIN — CHAFED (FOREFLAP) · airframe 41,102 hrs · 22,573 cycles

RIGHT I/B FORE FLAP UPPER SURFACE PREVIOUS REPAIR CHAFED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.

Part: SKIN — GOUGED (FOREFLAP) · airframe 41,102 hrs · 22,573 cycles

RIGHT WING O/B FORE FLAP IS GOUGED ON THE O/B END LOWER SURFACE. CUT OUT DAMAGE AND INSTALLED DOUBLER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT O/B FLAP AFT FLAP I/B UPPER SURFACE DELAMINATED. REPAIRED FLAP.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 41,102 hrs · 22,573 cycles

RIGHT I/B FORE FLAP UPPER SURFACE HAS DELAMINATION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT I/B FOREFLAP UPPER SURFACE HAS DELAMINATION ON EXISTING REPAIR. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 41,102 hrs · 22,573 cycles

LEFT I/B FORE FLAP UPPER SURFACE HAS DELAMINATION ON EXISTING REPAIR. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,102 hrs · 22,573 cycles

NR 5 SLAT O/B CORNER AFT END DELAMINATED. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.

Part: SKIN — BULGED (FUSELAGE) · airframe 41,102 hrs · 22,573 cycles

EXTERNAL FUSELAGE SKIN AT STA 186, 4 INCHES BELOW STR 24L IS BULGED OUT. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 41,102 hrs · 22,573 cycles

RIGHT O/B AFT FLAP AT APPROX 12 INCHES FROM I/B EDGE DENTED. REMOVED DAMAGED AREA, INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (RT WING) · airframe 41,102 hrs · 22,573 cycles

DENT ON RT WING OUTBOARD AFT JUST O/B OF NR 7 CANOE. REMOVED DAMAGED AREA, INSTALLED DOUBLER REPAIR.

Part: SKIN — CHAFED (SPOILER) · airframe 30,400 hrs · 11,919 cycles

NR 4 SPOILER IS CHAFED ON LOWER SURFACE. REPAIRED DAMAGE ON LOWER SURFACE IAW SRM.

Part: SKIN — DENTED (FOREFLAP) · airframe 30,400 hrs · 11,919 cycles

RIGHT I/B FORE FLAP LOWER SURFACE PREVIOUS REPAIR HAS DENTS. REPAIRED DAMAGE IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,400 hrs · 11,919 cycles

AFT PIT CARGO TRACK CORRODED STA 847 RBL 13.8. REPAIRED TRACK BY SPLICING IN NEW SECTION.

Part: SKIN — DENTED (FOREFLAP) · airframe 30,400 hrs · 11,919 cycles

RIGHT I/B FORE FLAP UPPER SURFACE HAS CHAFED REPAIRS. REPAIRED DAMAGED AREAS IAW SRM.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 38,233 hrs · 20,906 cycles

AFT PIT LOWER SPLICE STRAP STA 787 794 RBL 20 WL 156 CORRODED. REMOVED CORRODED STRAP RECEIVED LOCATED DRILLED AND INSTALLED NEW SPLICE STRAP

Part: SKIN — CHAFED (TE FLAP) · airframe 38,233 hrs · 20,906 cycles

LT INBD MID FLAP UPPER IB SURFACE CHAFED. CUT OUT DAMAGED AREA FABRICATED TREATED PRIMED AND BONDED SKIN DOUBLER AND FILLER REPAIR IAW SRM 57 30 01.

Part: SKIN — CRACKED (LE SLAT) · airframe 38,233 hrs · 20,906 cycles

NR 1 SLAT CRACKED AROUND RIVET AT MIDDLE AUX TRACK. REMOVED DAMAGED SECTION OF SKIN FABRICATED TREATED PRIMED AND INSTALLED SKIN DOUBLER AND FILLER REPAIR IAW SRM 57 43 01.

Part: SKIN — CHAFED (TE FLAP) · airframe 38,233 hrs · 20,906 cycles

LT INBD FLAP UPPER SURFACE CHAFED AT PREVIOUS REPAIR. REMOVED PREVIOUS REPAIRS, FABRICATED TREATED, PRIMED AND INSTALLED SKIN DOUBLER REPAIR IAW SRM 51 70 10.

Part: SKIN — CHAFED (FOREFLAP) · airframe 38,233 hrs · 20,906 cycles

LT INBD FORE FLAP UPPER SURFACE IB EDGE CHAFED. REMOVED DAMAGED SKIN FABRICATED TREATED PRIMED AND BONDED DOUBLER REPAIR IAW SRM 51 70 10.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 38,233 hrs · 20,906 cycles

L1 DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING IAW SRM 51 40 02.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,233 hrs · 20,906 cycles

SKIN DENTED STA 1020 BETWEEN STR 25R 26R DENT IS WITHIN 3 INCH FROM SPLICE. REMOVED DAMAGED AREA FABRICATED TREATED PRIMED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53 80 01.

Part: SKIN — DENTED (HORIZ STAB) · airframe 35,288 hrs · 19,300 cycles

DENT FOUND IN RIGHTHAND HORIZONTAL STABILIZER LEADING EDGE. INSTALLED EXTERNAL DOULBER PER ALK EA 5510 01322.

Part: DOOR — BINDS (L1 DOOR) · airframe 34,247 hrs · 18,721 cycles

FLT ATTENDANT HAS TROUBLE OPENING L1 DOOR. CARRIED OUT GENERAL VISUAL INSPECTION OF L1 DOOR. NO DEFECTS NOTED. OPERATIONAL CHECK COMPLETED, NO FAULTS FOUND. OP CHECKS GOOD PER MM 52-11-00.

Part: SKIN — DENTED · airframe 29,982 hrs · 16,365 cycles

SCRATCH AND DENT IN AFT CARGO DOOR APPROX 7" FROM LE OF DOOR 14" FROM BOTTOM. SCRATCHES 8" LONG ENDING IN A DENT 3.1" BY 1.4" BY .3" DEEP WITH GOUGE APPROX 1 2" LONG BY 1 4" WIDE. CUT OUT SKIN AT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53 00 01 REPAIR 2.

Part: THRESHOLD — CORRODED (FS 794-847)

FOUND CORROSION AT AFT CARGO BAY DOOR CUTOUT LOWER THRESHOLD. REMOVED AND REPLACED LOWER THRESHOLD IAW B737-400 SRM 51-40-02. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,103 hrs · 22,534 cycles

PAE- CORROSION ON FWD CARGO FRAME SHEAR TIE AT BSTA 500B BL 0, STR 28 LT. FOUND CORROSION TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR TO FRAME SHEAR TIE IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FS 867)

FOUND CORROSION AFT CARGO BAY SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 53-00-07.

Part: SKIN — CHAFED (FS 907-908)

PAE - FOUND UPPER FUSELAGE SKIN CHAFED. REPAIRED DAMAGED SKIN BY ADDING DOUBLERS AND REPAIR STRAPS PER ASA EA 5330-02033. (M)

Part: SHEAR TIE — CORRODED (FS 500D)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED CORROSION, CUT OUT FRAME SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW B737-400 SRM 53-00-07 FIG 201, REPAIR 3. (M)

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,244 hrs · 14,937 cycles

PAE: CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED DAMAGED SUPPORT, FABRICATED AND NEW SUPPORT PIECE AND INSTALLED IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FS 500C)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW ASA EA 5310-02545. (M)

Part: SHEAR TIE — CORRODED (FS 500B)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR TO FRAME SHEAR TIE IAW B737-400 SRM 53-00-07. (M)

Part: SHEAR TIE — CORRODED (FS 440-500A)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. FOUND CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR TO FRAME SHEAR TIE IAW B737-400 SRM 53-00-07. (M)

Part: FRAME — CRACKED (FS 380)

PAE - FOUND FRAME CRACKED AT BIN RAIL ATTACH CLIP. REMOVED CRACK IN FRAME, FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 53-00-07. (M)

Part: FRAME — CRACKED (FS 907)

PAE - REJECTED ITEM FROM CARD 4963163. FRAME CRACKED AT BIN RAIL SUPPORT STATION 907 BETWEEN STRINGER 8R AND 9R. DAMAGE REMOVED EXCEEDS ALLOWABLE LIMITS IN B737-400 SRM 53-00-07 REPAIR 2, DETAIL 1. INSTALLED FRAME REPAIR AT BS 907 FRAME BETWEEN STRINGER 8R AND 9R PER B737-400 SRM 53-00-07 PAGE 201 FIG 2014, REPAIR 1. (M)

Part: FRAME — CRACKED (FS 360)

PAE - FOUND CRACKED FRAME AT BIN RAIL SUPPORT BRACKET LEFT SIDE. REPAIRED FRAME AT BIN RAIL SUPPORT BRACKET PER SRM 53-00-07, REPAIR 1. (M)

Part: SHEAR TIE — CORRODED (FS 500C)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. FABRICATED AND INSTALLED REPAIR TO FRAME PER SRM 53-00-07. (M)

Part: SHEAR TIE — CORRODED (FS 500)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. CORRODED OUT OF LIMITS FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-00-07. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW B737-400 SRM 53-00-07. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON AFT ENTRY DOOR MOPSILL. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 53-60-15. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED AT BIN RAIL ATTACH CLIP. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED IAW B737-400 SRM 53-00-07. (M)

Part: THRESHOLD — CORRODED (FS 794-847)

PAE - FOUND CORROSION AFT CARGO BAY DOOR CUTOUT LOWER THRESHOLD. REMOVED AND REPLACED LOWER THRESHOLD IAW B737-400 SRM 51-40-02. (M)

Part: STRINGER CLIP — GOUGED (FUSELAGE)

PAE - FOUND AFT CARGO BAY STRINGER CLIP GOUGED. REMOVED AND REPLACED STRINGER CLIP IAW B737-400 SRM 51-40-02. (M)

Part: SKIN — CHAFED (FUSELAGE)

PAE - FOUND RIGHT SKIN CHAFED AT LOWER AFT HORIZONTAL STAB FITTING. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED IAW B737-400 SRM 51-40-02. (M)

Part: SEAT TRACK — GOUGED (BS 540-727)

PAE - FOUND MECHANICAL DAMAGE ON MAIN CABIN SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW B737-400 SRM 53-00-52. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - MECHANICAL DAMAGE ON MAIN CABIN SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW B737-400 SRM 53-00-52. (M)

Part: STRINGER CLIP — GOUGED (FUSELAGE)

AFT CARGO BAY STRINGER CLIP GOUGED. REMOVED AND REPLACED STRINGER CLIP IAW B737-400 SRM 51-40-02. (M)

Part: SKIN — DENTED (TE FLAP) · airframe 25,102 hrs · 13,751 cycles

IB FORE FLAP HAS NUMEROUS DENTS IN LOWER SKIN SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)

Part: SKIN — CHAFED (FUSELAGE) · airframe 25,102 hrs · 13,751 cycles

LT FUSELAGE EXTERNAL SKIN CHAFED AT LT STAB AFT OF BOTTOM LUG CUTOUT STA 1150-1140. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM. (K)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 25,102 hrs · 13,751 cycles

LIGHTING STRIKE AT FRAME 211.8 ON CREASE BEAM. REMOVED DAMAGED, COMPLIED WITH A HFEC INSPECTION IAW MFG NDT MANUAL, NO DEFECTS NOTED. FABRICATED AND INSTALLED A REPAIR FILLER, DOUBLER, AND TRIPLER IAW SRM. (K)

Part: WEDGE — DENTED (TE FLAP) · airframe 25,102 hrs · 13,751 cycles

LT WING IB MID FLAP WEDGE IS DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)

Part: SKIN — DELAMINATED (RUDDER) · airframe 25,102 hrs · 13,751 cycles

RUDDER IS DAMAGED AT LT SIDE LOWER EDGE. COMPLIED WITH A BOND REPAIR IAW SRM. (K)

Part: SKIN — PUNCTURED (RUDDER) · airframe 25,102 hrs · 13,751 cycles

BOTTOM OF RUDDER IS PUNCTURED. COMPLIED WITH A BOND REPAIR IAW SRM. (K)

Part: ACCESSORY UNIT — INOPERATIVE (TE FLAPS)

ANC - FOUND THE TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES ADVANCED TO TAKEOFF POWER. ABORTED TAKEOFF AT LESS THAN 50 KTS. REPLACED FLAP/SLAT ACCY UNIT. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - TRACK LIGHTS INOPERATIVE AT ROWS 21-24. RECONNECTED WIRES, OPS CHECKED NORMAL. (M)

Part: SNUBBER — INOPERATIVE (PAX DOOR) · airframe 25,678 hrs · 15,403 cycles

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR SNUBBER WAS FOUND TO BE INOPERATIVE ALLOWING DOOR TO SLAM SHUT. REPLACED THE L1 DOOR SNUBBER AND THE DOOR OPERATED NORMALLY. (M)