N9420D

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,742 hrs · 34,473 cycles

CRACK IN LEFT SKATE ANGLE BETWEEN VERTICAL STABILIZER AND FUSELAGE, AT CANT FRAME 1463. ROUTED OUT CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,270 hrs · 33,656 cycles

FIRST CLASS GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN FIRST CLASS.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,878 hrs · 33,437 cycles

AFT VENTRAL STAIRWAY LOWER BULKHEAD WEB LEFT AND RIGHT SIDES AT STATION 1338 CORRODED. REMOVED AND REPLACED LEFT AND RIGHT BULKHEAD WEBS UNDER SRM.

Part: BULB — INOPERATIVE (OIL SYSTEM) · airframe 52,158 hrs · 33,053 cycles

DURING CLIMBOUT AT CLIMB POWER, LEFT ENGINE OIL TEMP REACHED 166 DEGREES. OIL QUANTITY & OIL PRESS NORMAL. SHUT LEFT ENGINE DOWN AND WAS SHUT DOWN FOR 18 MINS FLIGHT DURATION. ACCOMPLISHED CARDS 71-92-11 AND 71-91-11. REPLACED LEFT ENGINE OIL TEMP BULB, OPS CHECKED, LEAK CHECK GOOD, REPLACED P1-182 CONNECTOR AT LEFT ENGINE. RAN ENGINE FOUND ALL PARAMETERS TO BE NORMAL AT DIFFERENT POWER SETTINGS.

Part: ATTACH BRACKET — CRACKED (ZONE 500) · airframe 30,565 hrs · 3,238 cycles

NUMBER 5 SLAT OUTBOARD TRACK ATTACH BRACKET CRACKED. REPLACED OUTBOARD ATTACH FITTING PER ESO 80117.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 50,891 hrs · 32,355 cycles

NUMBER 5 SLAT SECOND FROM OUTBOARD TRACK ATTACH BRACKET CRACKED. REPLACED ATTACH FITTING PER ESO 80117.

Part: ATTACH BRACKET — CRACKED (NR 5 SLAT TRACK) · airframe 50,891 hrs · 32,355 cycles

NUMBER 5 SLAT OUTBOARD TRACK ATTACH BRACKET CRACKED. REPAIRED OUTBOARD ATTACH BRACKET PER ESO 80117.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON LEFT TIE DOWN TRACK OUTBOARD AT STATION 674 TO 676. REPLACED SHEAR TIE DOWN TRACK FROM STATION 522 TO 731 PER AARD 51-00-00-012.

Part: FRAME — DENTED (ZONE 200) · airframe 50,891 hrs · 32,355 cycles

DENT ON FUSELAGE AT CANT FRAME AT STATION 1497 LONGERON 15 LEFT. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH WITH A DEPTH OF .043 INCH. DYE CHECKED DENT AND NO CRACKS. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 5.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON LONGERON 30 BETWEEN STATION 1178 AND STATION 1193 AT AFT CARGO BAY UNDER FLOOR. AREA OF DISCREPANCY IS .24 INCH BY 4 INCHES WITH A DEPTH OF .049 INCH. INSTALLED REPAIR STRAP DOUBLER PER ENGINEERING AUTHORIZATION MD80 53-005338 DATED 28 JAN 09

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON SHEAR TIE AT STATION 1250 BETWEEN LONGERON 28 LEFT AND LONGERON 29 LEFT. REPLACED SHEAR TIE FROM LONGERON 28 RIGHT TO LONGERON 28 LEFT AT STATION 1250 IN ACCORDANCE WITH SRM 53 03 00.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON LEFT TIE DOWN TRACK CENTER MOUNT LUG AT STATION 670 TO 731. REPLACED LEFT TIE DOWN TRACK FROM STATION 522 TO 731 PER AARD 51-00-00-12.

Part: SKIN — DAMAGED (ZONE 600) · airframe 50,891 hrs · 32,355 cycles

RIGHT WING INBOARD SIDE OF OUTBOARD TRAILING EDGE FORWARD OF AILERON HAS SEVERAL FASTENER HOLES DAMAGED IN STRAP. INSTALLED RT WING TE PANEL IAW EA 57-005347 DATED 26 JANUARY 2009.

Part: FRAME — DAMAGED (ZONE 100) · airframe 50,891 hrs · 32,355 cycles

OVERSIZED AND ELONGATED HOLES ON FRAME 1287 BETWEEN LONGERON 29 RIGHT AND LONGERON 29 LEFT. INSTALLED J ANGLE REPAIR WITH OVERSIZED FASTENERS PER AARD 53-10-00-14.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

ANGLE BRACKET CORRODED AT LONGERON 26 LEFT STATION 1022. REPLACED ANGLE BRACKET PER SRM 51-02-00.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

TIE DOWN TRACK CORRODED STATION 1212 TO 1322 RIGHT. INSTALLED NEW TIE DOWN TRACK PER SRM 51-32-02

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION IN CENTER OF LONGERON 30 AT STATION 1200 TO 1240. DAMAGE REPAIRED PER ENGINEERING AUTHORITY 53-005339 DATED 1/27/09.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,891 hrs · 32,355 cycles

WHEEL WELL PRESSURE DECK CRACKED JUST AFT AND OUTBOARD UNDER CLIP ABOVE FUEL SHROUD LINE. INSTALLED DOUBLER ON PRESSURE DECK PER AARD 53-30-00-13.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

RIGHT TIE DOWN TRACK CORRODED AT SCREW HOLES STATION 1022 TO 1146. INSTALLED NEW TIE DOWN TRACK PER AARD 51-00-00-012.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON LONGERON 23 LEFT AT STATION 1254 TO 1257 LONGERON STIFFENER. REPLACED LONGERON STIFFENER STRAP IN ACCORDANCE WITH SRM 53 14 03.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

RIGHT TIE DOWN TRACK CORRODED AT SCREW HEADS AT STATION 1022 TO 1146 AT AFT CARGO. INSTALLED NEW TIE DOWN TRACK PER AARD 51-00-00-012.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

FUSELAGE FRAME AFT SIDE HAS CORROSION FROM LONGERON 29 RIGHT TO LONGERON 28 LEFT AT STATION 1231. REMOVED CORROSION AND INSTALLED J ANGLE DOUBLER PER AARD 53-10-00-14.

Part: FRAME — CRACKED (ZONE 100) · airframe 50,891 hrs · 3,236 cycles

CRACK IN CANT FRAME AT STATION 1485 BELOW STAIR CONTROL ACTUATOR RIGHT SIDE. INSTALLED REPAIR DOUBLER ON RIGHT CANT FRAME AT STATION 1485 PER AARD 53-10-00-33 FIG 2 SHEET 7.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,981 hrs · 32,355 cycles

CORROSION ON LONGERON 21 RIGHT. INSTALLED EXTRUSION AND LONGERON SPLICE BETWEEN STATION 1271 AND 1309 PER SRM 53-02-00 FIG 18 SHEET 1.

Part: LONGERON — CRACKED (ZONE 200) · airframe 50,891 hrs · 32,355 cycles

LONGERON 3 LEFT IS CRACKED AT STATION 160. INSTALLED SPLICE PER SRM 53-02-00.

Part: SKIN — CRACKED (ZONE 100) · airframe 50,891 hrs · 32,355 cycles

CRACK IN FUSELAGE SKIN AT STATION 1474. INSTALLED DOUBLER PER SRM 53-01-00.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

BOTTOM SIDE OF LEFT CUSP CORRODED STATION 1032. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16. AREA OF DISCREPANCY IS 4 INCHES BY 10 INCHES.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON TOP OF CABIN FLOORBEAM UNDER RIGHT AFT LAVATORY PAN STATION 1338. INSTALLED REPAIR ANGLE PER SRM 53-05.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

AFT CARGO DOOR LOWER DOOR BEAM VERTICAL FACE HAS CHIPPED PAINT AND LIGHT CORROSION. AREA OF DISCREPANCY IS THREE INCHES BY THREE INCHES. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

RIGHT CUSP AT CABIN FLOOR HAS CORROSION AT STATION 503 TO 522. AREA OF DISCREPANCY IS 4 INCHES BY 19 INCHES. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON BELLY SKIN AT STATION 750 TO 760 LONGERON 30 TO LONGERON 29 RIGHT INCLUDING REPAIR DOUBLER AND SKIN LAP. CUT OUT CORROSION. INSTALLED DOUBLER PER EA MD80-53-005317 DATED 21 JAN 09.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON RIGHT CUSP AT STATION 611 TO 614. CUT OUT CORRODED AREA AND INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 20 16.

Part: LONGERON — CRACKED (ZONE 200) · airframe 50,891 hrs · 32,355 cycles

LONGERON CRACKED AT FRAME 200 LONGERON 4 LEFT. REPLACED LONGERON 4 LEFT FROM STATION 170 TO 230 IN ACCORDANCE WITH SRM 53-02-00.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 50,891 hrs · 32,355 cycles

SHEAR TIE CRACKED AT STATION 1437 LONGERON ONE RIGHT. INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH SRM 51-02-00.

Part: PAN — CRACKED (ZONE 100) · airframe 50,891 hrs · 32,355 cycles

PAN CRACKED AT LOWER HINGE ON FORWARD SERVICE DOOR. DYE CHECKED AND STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER PER ESO 80177.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 50,891 hrs · 32,355 cycles

CRACK AT LIGHTENING HOLE ON LEFT CUSP MEMBRANE AT STATION 227. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON FITTING AT AFT END OF GALLEY NR 1 INBOARD FLOOR MOUNT STA 168. INSTALLED SERVICEABLE F/B MOUNT PER SRM 51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

NUMBER FOUR SEAT TRACK CORROSION REMOVAL OUT OF LIMITS AT STATION 237. INSTALLED SEAT TRACK PLUG AND CHANNEL IN ACCORDANCE WITH AARD 53 20 00 10.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 50,891 hrs · 32,355 cycles

TWO PUNCTURES IN SUBFLOOR 6 INCHES TO THE RIGHT OF AIRCRAFT CENTERLINE AT STATION 170. PLUG HOLES WITH LOCK FASTENERS PER SRM 53-01-00, 51-01-00, 53-04-00.

Part: SKIN — DENTED (ZONE 100) · airframe 50,891 hrs · 32,355 cycles

FUSELAGE DENT STA 233, 238, 247, BETWEEN LONGERON 17 LEFT AND 18 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIG 17B SHEET 34. AREA OF DISCREPANCY IS 3.5 INCHES BY 5 INCHES WITH A DEPTH OF .125 INCH.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,891 hrs · 32,355 cycles

CRACKED ANGLE TOP OF STIFFENER ON UPPER END OF STATION 1338 BULKHEAD AT LONGERON 4 LEFT. INSTALLED NEW SERVICEABLE ANGLE ON STIFFENER UPPER END OF STATION 1338 BULKHEAD AT LONGERON 4 LEFT PER SRM 51-01-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,891 hrs · 32,355 cycles

CORROSION ON FLOORBOARD SUPPORT STATION 200 BETWEEN SEAT TRACKS 5 AND 6. AREA OF DISCREPANCY IS ONE INCH BY SIX INCHES WITH A DEPTH OF .020 INCH. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-01.

Part: BRACKET — CRACKED (ZONE 200) · airframe 50,891 hrs · 32,355 cycles

CENTER DOORSTOP BRACKET CRACKED AT LEFT SIDE OF VAULT DOOR JAMB. REMOVED AND REPLACED CENTER DOORSTOP BRACKET AT LEFT SIDE OF VAULT DOOR JAMB PER SRM 51-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT AFT SERVICE DOOR EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT SERVICE DOOR EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD TAIL COMPARTMENT INOPERATIVE. REPAIRED WIRE NUMBER L795B16 AT L2 637 FOR EMERGENCY LIGHT AT OVERHEAD TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT FORWARD EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT COCKPIT AND FORWARD CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT COCKPIT AND FORWARD CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY FLASHLIGHT IN CABIN INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — STALLED (RT ENGINE)

DURING CLIMB, AIRCRAFT EXERIENCED LOUD BANK AND FIVE DEGREES OF YAW AT 2600 FEET. CREW RETURNED TO MSP AND LANDED WITHOUT INCIDENT. CREW REPORTED NUMBER TWO ENGINE GIVING LITTLE MORE THAN IDLE THRUST ON SHORT FINAL. REPLACED NUMBER TWO ENGINE ON 20 MARCH AT MSP DUE TO STALLS DURING CLIMB POWER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,734 hrs · 24,862 cycles

THE OVERHEAD EMERGENCY LIGHTS WERE INOEPRATIVE FROM ROW 18 TO 22, EGRESS LIGHT AT ROW 20, AND EGRESS LIGHTS ROW 27 TO AFT CABIN. RESEATED BATTERY PACKS FOR ROW 18 TO 22, REPLACED LAMP PN 7732 FOR ROW 20 EGRESS LIGHT, AND RESEATED PLUG AT ROW 26 FOR AFT CABIN EGRESS LIGHTS. CHECK-C 11-06-02 STL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,728 hrs · 24,858 cycles

THE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE AT THE L2 DOOR, FWD AND AFT OF L2 DOOR IN AISLE, MID SECTION OF AIRCRAFT APPROXIMATELY 8 ROWS OF EGRESS LIGHTS, AND AFT MOST EGRESS RED LIGHT ADJACENT TO LAVS. REPLACED POWER SUPPLY PN 60-0304-51LB FOR L2 DOOR AND ADJACENT AISLE, BATTERIES RECHARGED FOR MID CABIN EGRESS LIGHTS, AND REPLACED MODULE PN 010-5606-004 FOR RED LIGHT ADJACENT TO AFT LAVS. CHECK-C 11-6-02 STL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,728 hrs · 24,858 cycles

THE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE IN AREA OF ROW 9, AFT AIRSTAIR AREA OVERHEAD, AND 2 OF 3 TAIL CONE LIGHTS. REPLACED BATTERIES FOR ROW 9, PN 408822-101, AND REPLACED ONE SET OF BATTERIES FOR THE OTHER TWO AREAS, PN 408822-101. CHECK-C 11-6-02 STL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,695 hrs · 24,840 cycles

THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,051 hrs · 24,471 cycles

FOUND OVERWING EMERGENCY LIGHTS AND TWO EGRESS LIGHTS INOPERATIVE. REPLACED THE OVERWING LIGHT BATTERY PACK AND TWO EGRESS LAMPS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,874 hrs · 21,971 cycles

THE OVERWING INTERIOR EMERGENCY LIGHT WAS ON ALL THE TIME. REPLACED THE BATTERIES FOR BOTH INTERIOR OVERWING EMERGENCY LIGHTS. CHECK-C 2-18-01 MCI.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT THE AFT CARGO COMPT TIE DOWN TRACK WAS CORRODED IN SEVERAL LOCATIONS FROM STA 1222 TO 1322, 16L BL. REMOVED AND REPLACED WITH NEW TRACK PER SRM 53-01, PAGE 1 ITEM C.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT AT STA 1106 TO 1221, AND 1168 TO 1222, THE AFT CARGO COMPT LT TIE DOWN TRACK WAS CORRODED IN SEVERAL LOCATIONS. FABRICATED NEW TRACK AND SPLICED AND INSTALLED PER SRM 53-05, FIG 46.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FLOORBEAM CORROSION REMOVED WAS BEYOND LIMITS AT STA 1322, LBL 19 INCHES. INSTALLED FLOORBEAM REPAIR PER SRM 53-05, PAGE 31. TREATED, PRIMED AND PAINTED WHITE AND REPAIR PARTS INSTALLED PER SRM 51-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN AFT CABIN FOUND FLOORBEAM CORROSION REMOVAL WAS BEYOND LIMITS AT STA 1322, LBL 41, UNDER LT AFT LAV. REPAIRED PER SRM 53-05, PAGE 31.

Part: WEB — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE ON LT SIDE WALL AREA OF MID-CARGO COMPT, STA 522 TO 541 (O/B TO SIDEWALL). REMOVED CORROSION PER SPM 6-80-01 AND SRM 51-10-3 PAGE 21. INSTALLED WEB REPAIR PER SRM 53-01, FIG 2 PAGE 9.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, IN THE AFT CARGO COMPT, FOUND CORROSION ON LONGERON 19L, BETWEEN STA 1287 AND 1209. REMOVED SECTION OF LONGERON AND CORROSION PER SRM 51-10-3. REPLACED PORTION OF LONGERON PER SRM 53-02, FIG 18.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, IN THE AFT CABIN, FLOORBEAM CORROSION WAS REMOVED BEYOND LIMITS AT STA 1338, LBL 19 AND LBL 26. INSTALLED REPAIR PER SRM 53-05, FIG 20A, PAGE 31.

Part: WEB — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, MEMBRANE AT STA 617, LONGERON 18R, WAS CORRODED ON LOWER SURFACE. INSTALLED NEW MEMBRANE PER SPM 6-70-01 PAGES 2 AND 3. INSTALLED FASTENERS PER SRM 51-30 AND 51-10-4. PAINTED PER SPM 1-20-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FOUND RT FLOOR MEMBRANE CORRODED AT CUSP LINE, STA 598 THRU 712. INSTALLED NEW MEMBRANE PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30 AND 51-10-4. PAINTED PER SPM 1-20-02.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, IN THE AFT CABIN, INTERCOSTAL LOWER LEG WAS CRACKED AT STA 1322, ZERO BL, JUST FWD OF FLOORBEAM. REMOVED LOWER LEG. REPLACED WITH NEW LEG USING MS20470AD5 RIVETS PER 53-01, FIG 2.

Part: WEB — CORRODED (CABIN FLOOR) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FOUND FLOOR MEMBRANE CRACKED AND CORRODED FROM STA 1287 TO 1309, BETWEEN LBL 54 TO LBL 60. CRACKS AND CORROSION RAN UNDER TRACK AND LAV FWD BULKHEAD. REMOVED CORROSION PER SRM 51-10-3, PAGE 21 PARAGRAPH 35. REPLACED MEMBRANE PER SRM 53-05, FIG 97.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT BETWEEN NUMBER 3 AND 4 TRACKS, STA 1308. REPLACED FLOOR SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 1174 TO 1212, RBL 58 INCHES. REMOVED CORROSION PER SRM 51-10-2. REPLACED MEMBRANE PER SRM 51-30-1, 51-30-02, AND 51-30-5.

Part: PLATE — CORRODED (SERVICE DOORWAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, THE BOTTOM SILL PLATE ON THE RT SIDE CABIN SERVICE DOOR ENTRY WAY HAD HEAVY CORROSION. REPLACED SILL PLATE PER SPM 6-70-01. INSTALLED RIVETS PER SRM 51-30-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON STRINGER 23L, STA 1021 TO 1041, AFT CARGO COMPT. INSTALLED NEW SECTION OF STRINGER AND 2 SPLICES PER SRM 53-02, FIG 18 SHEET 4.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FLOOR MEMBRANE WAS CRACKED BETWEEN STA 1298 AND 1309, STRINGER 18R. REPAIRED MEMBRANE PER 53-05-96 AND SPM 6-70-01 PAGE 1, 2, AND 3.

Part: WEB — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, THE RT SIDE FLOOR MEMBRANE WAS CORRODED AT CUSP LINE, STA 484 THRU 598. REMOVED AND REPLACED FLOOR MEMBRANE AS REQUIRED PER SPM 6-70-01, PAGE 2 PARA 4, AND PER DOUGLAS DRAWING 9930538.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FLOOR FRAME FITTING AT STA 1174, LT AFT SIDE OF AFT SERVICE DOOR WAS CORRODED. FABRICATED NEW FITTING PER DRAWING 3936091. INSTALLED PER DRAWING 5930490.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON NUMBER 4 TRACK AT STA 1142 TO 1309. REPLACED TRACK WITH NEW. INSTALLED PER SRM 53-05 PAGE 106.

Part: WEB — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1174 TO 1250, MEMBRANE WAS CORRODED AROUND LIGHTENING HOLES. REPLACED MEMBRANE AT STA 1174 TO 1250, PER SRM 51-30-0.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND IN MID CABIN ON LT SIDE, STA 940, LBL 58 INCHES, CORROSION AROUND LIGHTENING HOLE IN MEMBRANE. REMOVED CORROSION PER SRM 51-30-3, PAGE 21 PARAGRAPH 35. REPAIRED PER SRM 51-70-4, FIG 2 SHEET 2.

Part: WEB — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON THE LT FLOOR MEMBRANE AT STA 1174. REPLACED MEMBRANE FROM 1174 TO 1250 AT CUSP ANGLE TO CHAIR TRACK, PER SRM 51-30-02.

Part: GALLEY TRACK — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, FOUND NUMBER 1 CABIN TRACK, GALLEY TIE DOWN HAD CORROSION AT STA 1174. REPLACED TRACK FROM STA 1174 TO 1308, PER SRM 51-30-1.

Part: WEB — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE LT SIDE WALL AREA STA 389 TO 408. REPLACED MEMBRANE PER SPM 6-70-01. INSTALLED HI-LOK PER SPM 51-30-05. INSTALLED BOLTS PER SRM 51-30-01. INSTALLED RIVETS PER SRM 51-30-02. MEMBRANE FROM STA 389 TO 503 REPLACED.

Part: WEB — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN FWD CARGO COMPT CORROSION WAS ON MEMBRANE LT SIDEWALL AREA STA 503 TO 522. REMOVED CORROSION PER SPM 6-80-01 AND SRM 51-10-3 PAGE 21. REPAIRED WITH DOUBLER PER SRM 53-01 FIG 4 SHEET 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM AT STA 160, LBL 8 INCHES. MADE NEW FLOOR SUPPORT PART, INSTALLED PER SRM 51-30-02 AND SRM 51-30-05.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS ON UNDERSIDE OF FLOOR MEMBRANE AT STA 1041 TO 1060 RT SIDE, STA 1060 TO 1079, AND STA 1079 TO 1098. REMOVED AND REPLACED MEMBRANES PER DRAWING 9930612-25 AND SPM 6-70-14A AND B.

Part: WEB — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE FWD CABIN LT, CORROSION WAS FOUND AROUND LIGHTENING HOLES ON WEB MEMBRANE AT STA 699 LBL 58 INCHES, STA 683 LBL 58 IN, STA 663 LBL 58 INCHES, AND STA 617 TO 636 LBL 58 INCHES. REPLACED MEMBRANE AT EACH LOCATION PER DRAWING 9930538.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON UNDERSIDE OF MEMBRANE AT STA 1022 TO 1041. REPLACED MEMBRANE PER DRAWING 9930612-2. INSTALLED DOUBLERS AT STA 1022 AND 1032 PER SRM 53-01 FIG 4.

Part: SILL — CORRODED (AFB DOOR FRAME) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CABIN, CORROSION WAS ON FWD SIDE OF SILL PLATE, AFT PRESSURE BULKHEAD DOOR JAMB. REMOVED CORRODED SECTION OF DOOR JAMB SILL PLATE. FABRICATED NEW LOWER SECTION OF JAMB ASSY PER DRAWING 5917463. SPLICED IN FABRICATED JAMB PER SRM 53-05 FIGURE 30.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION UNDERSIDE FLOOR MEMBRANE AT STA 1098 TO 1117, RT SIDE. INSTALLED NEW MEMBRANE PER DRAWING 993612-23 AND REINSTALLED FITTING PER SPM 6-70-01.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE ATTACH ANGLE OUTBOARD OF NUMBER 6 TRACK, STA 1155 TO 1174. INSTALLED NEW MEMBRANE PER DRAWING 9930612-23 AND SPM 6-70-01.

Part: ATTACH ANGLE — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN MEMBRANE ATTACH ANGLE OUTBOARD OF NUMBER 6 TRACK, STA 1136 TO 1155. INSTALLED NEW MEMBRANE ATTACH ANGLE PER DRAWING 9330612-23 AND SPM 6-70-01.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND UNDERSIDE RT FLOOR MEMBRANE AT STA 1117 TO 1136. INSTALLED NEW MEMBRANE PER DRAWING 9330612-23 AND SPM 6-70-01.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT AT STA 597 TO 604, BOTH SIDES OF FLOOR MEMBRANE WAS CORRODED AT LBL 58. REMOVED CORROSION PER SPM 6-80-01 AND SRM 51-10-3 PAGE 21. INSTALLED REPAIR PER SRM 51-70-4 PAGE 1 TO 4.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND HEAVY CORROSION ON LOWER CARGO DOOR BEAM AT STA 1155 TO 1212. REPLACED DOOR BEAM PER INSTALLATION PRINT 5930483 AND SPM 6-70-01, PAGE 3 ITEM B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT CABIN FLOOR SUPPORT WAS CORRODED AT STA 157 TO 207, RBL 7 INCHES. INSTALLED NEW PART AND INSTALLED WITH BOLTS PER SRM 6-70-01 AND SRM 51-30-1.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPT, CORROSION WAS FOUND ON RT FLOOR MEMBRANE TO CARGO DOOR FRAME, STA 1155 TO 1212. REPLACED MEMBRANE PER PRINT 5936442 AND SPM 6-70-01, PAGE 3 ITEM B.

Part: GALLEY TRACK — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE FWD CABIN, LIGHT CORROSION WAS ON GALLEY TIE DOWN ANGLE APPROX STA 210, RBL 10, AT NUT PLATE RIVETS. PART REMOVED AND REPLACED WITH NEW PART PER SPM 6-70-01. PAINTED WHITE PER SRM 51-10-03. INSTALLED NEW FASTENERS PER SRM 51-30-02. SEALED AREA PER SRM 51-20-0 PAGE 2.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOORBEAM AT STA 193 AND BETWEEN LBL 16 IN TO 43 IN. MADE NEW FLOOR SUPPORT EXTRUSION AND INSTALLED FLOOR SUPPORT PER SRM 51-30-0 RIVETS.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, COCKPIT FLOOR SUPPORT ANGLE HAD CORROSION AT STA 148 TO 157, CENTER FLOOR SUPPORT APPROX LBL 12. INSTALLED NEW FLOOR SUPPORT PER SRM 51-1-0 WITH BOLTS PER SRM 51-30-0.

Part: DOOR — TORN (NLG) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT ON THE NOSE LANDING GEAR, THE RT NOSE LANDING GEAR WHEEL WELL DOOR HAD CORROSION AND TORN METAL ON LEADING EDGE. REMOVED DAMAGE BY BLENDING PER SRM 52-01 FIG 1. REMOVED CORROSION PER SPM 6-80-01.

Part: WEB — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT ON THE RT CABIN SIDEWALL, STA 275 TO 237, RBL 58, CORROSION WAS FOUND ON TOP AND BOTTOM OF WEB MEMBRANE AROUND LIGHTENING HOLES. CLEANED CORROSION PER SPM 6-80-01. ALODINED AND PAINTED PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 53-01 FIG 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, CABIN FLOOR PANEL ATTACH ANGLE HAD CORROSION APPROX STA 160 TO 200, RBL 52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT WAS CORRODED FROM STA 157 TO 201, RBL 44 INCHES. FABRICATED NEW FROM EXTRUSION. REPLACED PER SPM 6-70-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT CABIN FLOOR SUPPORT WAS CORRODED AT STA 177, RBL 9 TO 42. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE FWD CARGO BILGE, FROM STA 370 TO 427, RBL 9 INCHES, FLOOR SUPPORT AT DOOR ENTRANCE HAD CORROSION AROUND NUT PLATE HOLES. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT THE NR 1 SEAT TRACK, GALLEY TIE DOWN HOLE HAD CORROSION AT STA 1117. FABRICATED NEW CHAIR TRACK AND INSTALLED PER SPM 6-70-01 PAGE 1 PARA 4, FROM STA 1030 TO 1136.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT CABIN SEAT TRACK NR 3, SEAT TRACK HAD CORROSION UNDER THE FWD LAVATORY. REMOVED CORROSION IN TRACK AREA. REPAIRED PER SRM 53-05 PAGE 10G AND 10H. REPLACED SECTION OF TRACK.

Part: WEB — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT CORROSION WAS FOUND ON LT FLOOR MEMBRANE AT STA 1174, AFT CARGO COMPT. FABRICATED AND INSTALLED DOUBLER .

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE AFT CARGO TIE DOWN TRACK HAD CORROSION FROM STA 1212 TO 1322, RT SIDE. INSTALLED NEW TRACK PER SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT CORROSION WAS FOUND ON CABIN FLOOR SUPPORT BETWEEN NUMBER 3 AND 4 TRACKS, STA 1287. FABRICATED NEW PART PER SPM 6-70-1 AND SRM 53-14-3. INSTALLED NEW PART PER SRM 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT THE FUSELAGE WAS FOUND DENTED AT STA 229, BETWEEN LONGERON 17L AND 18. REPAIRED PER SRM 53-04 FIG 12B.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT AT THE FWD CARGO DOOR, CORROSION WAS FOUND AROUND SCREW HOLES IN FWD LOWER DOOR JAMB. CUT OUT LOWER DOOR JAMB AND REMOVED CORROSION. REPAIRED PER SRM 53-05 FIG 44. MADE DOOR JAMB SPLICE REPAIR PER SRM 53-05 FIG 44.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT CORROSION WAS FOUND ON LONGERON SPLICE AT LONGERON 20, STA 1296. REMOVED OLD LONGERON SPLICE. DRILLED AND INSTALLED NEW LONGERON SPLICE PER DAC DRAWING 3913208, AND SRM 51-30-5 PARA 1-8 AND FIG 1-17.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FUSELAGE WAS DENTED AT STA 218 BETWEEN LONGERON 18L AND 19L. LENGTH WAS 8 INCHES AND WIDTH 4 IN BY DEPTH 0.060. MADE AND INSTALLED NEW SHEAR TIE AT STA 218 PER SPM 6-70-01 PAGE 2 AND 3 AND DOUGLAS PRINT 9951888. INSTALLED SKIN REPAIR PER SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT THE UPPER FUSELAGE WAS DENTED AT STA 427 BETWEEN LONGERON 17L AND 18L. LENGTH 2 INCHES BY WIDTH 0.025 AND DEPTH 0.040 (GOUGE). BLENDED GOUGES AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 PAGE 207 VIEW G. NDT INSPECTED FOR CRACKS AND NO CRACKS FOUND.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, LBL 6 TO RBL 6. FABRICATED AND INSTALLED NEW J-ANGLE FLOOR SUPPORT.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT FOUND CORROSION ON INTERCOSTAL BETWEEN STA 1271 AND STA 1250, LONGERON 25L.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT ON THE RT FUSELAGE AT STA 484, BETWEEN LONGERON 5R AND 6R, A METAL REPAIR WITH BLIND FASTENERS WAS FOUND. REMOVED CLASS III REPAIR. INSTALLED PERMANENT REPAIR PER SRM 53-04, FIG 38.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT IN THE FWD CARGO COMPT, FROM STA 229 TO 256, LONGERON 30 HAD CORROSION. REMOVED CORROSION PER 6-80-01. REPAIRED PER SRM 53-02 FIG 18.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT ON THE RT FUSELAGE, STA 555 AT LONGERON 5R A METAL REPAIR HAD BLIND FASTENERS. REMOVED TEMPORARY REPAIR. FABRICATED NEW INTERNAL AND EXTERNAL DOUBLER PER SRM 53-04 FIG 38. REPAIRED OLD CLASS III REPAIR TO PERMANENT REPAIR PER 53-04, FIG 38.

Part: MOTOR — INOPERATIVE (ALTERNATE TRIM) · airframe 31,519 hrs · 21,781 cycles

DURING CLIMB AT 10,000 FT PRIMARY TRIM WAS INOPERATIVE IN BOTH DIRECTIONS AND ALTERNATE TRIM WAS INOPERATIVE NOSE DOWN. ALT TRIM OK IN NOSE UP. PERFORMED JAMMED STABILIZER APPROACH WITHOUT INCIDENT. REPLACED THE PRIMARY TRIM ACTUATOR MOTOR. ALSO CLEANED AND ADJUSTED AND LUBED THE ALT TRIM ACT LEVERS AND SW ASSY. CHECK-C 11-19-00 STL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,962 hrs · 21,451 cycles

THE FWD CABIN GALLEY EMERGENCY LIGHTS STAYED ON ALL THE TIME. REPLACED THE BATTERY PACK. CHECK-C 11-19-99 STL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT, THE FIRST CABIN FLOOR SUPPORT INSIDE THE LEFT SIDE NUMBER 1 CABIN DOORWAY HAD CORROSION FROM STA 157 TO 200. REMOVED AND REPLACED FLOOR SUPPORT ANGLE. FABRICATED NEW ANGLE. TREATED PER SRM 51-10-3. INSTALLED PER DRAWING 936535.

Part: STOP — CORRODED (VENTRAL DOOR) · airframe 31,869 hrs · 21,965 cycles

DURING CHECK-C MAINT AT THE AFT CABIN BULKHEAD, THE DOOR EXTRUSION STOP HAD HEAVY CORROSION, BOTTOM LT SIDE OF DOOR AS VIEWED LOOKING FROM AFT. REPLACED DOOR STOP PER SPM 6-70-01 WITH NEW PART.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 12-8-98 MCI.

Part: WIRE — BROKEN (ROW 12-24)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 12 THROUGH 24. FOUND AND REPAIRED A BROKEN WIRE. CHECK-C 12-8-98 MCI.

Part: LIGHT — INOP (ROW 11)

FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM CABIN ROW 11 AFT. FOUND WIRE DISCONNECTED AND RECONNECTED SAME. CHECK-C 12-8-98 MCI.

Part: BATTERY PACK — DISCHARGED (ROW 11-21)

CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 11 TO 21. REINSERTED WIRES IN EGRESS TRACK LIGHTING AND REPLACED THE BATTERY PACK. CHECK-C 12-8-98 MCI.

Part: BLADE — CRACKED (LT ENGINE)

STL - FLT 173 - DURING TAKEOFF ROLL AT 80 KNOTS, LT ENGINE OIL QUANTITY AND PRESSURE FELL TO ZERO. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED ENGINE. CHECK-C 12-9-97 MCI. S/D - FOURTH STAGE TURBINE BLADE AIRFOIL FAILED FROM FATIGUE CRACK AT BASE OF AIRFOIL ORIGINATING AT LEADING EDGE. DAMAGE WAS REPAIRED. (X)

Part: CONNECTOR — LOOSE (LT FUEL TANK)

DURING CRUISE, THE LT FUEL TANK SHOWED APPARENT LOSS OF FUEL. SECURED CANNON PLUG ON LEFT FUEL FLOW TRANSMITTER. OPS CHECK NORMAL. CK-C 01 12-9-97 MCI. (X)

Part: FRAME — CORRODED (BS 1250)

MCI - DURING CHECK 'C', FOUND CORROSION ON FORWARD SIDE AND AFT SIDE OF AFT BAG BIT FRAME 1250, STR 29L TO STR 29R. CUT OUT CORRODED AREA AND INSTALLED REPAIR PER SRM 53-03, PAGE 4A, AND SRM 51-30-1 AND SRM 51-30-2. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,595 CYCLES. (X)

Part: FRAME — CORRODED (BS 1271)

MC I - DURING CHECK 'A', FOUND CORROSION FRONT AND REAR SIDES OF AFT BAG PIT FRAME 1271, BETWEEN STR 29L AND STR 29R. CUT OUT CORRODED AREA AND INSTALLED REPAIR PER SRM 53-03, PAGE 4A. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,595 CYCLES. (X)

Part: BULKHEAD WEB — CORRODED (AFT PRESS BLKHD)

MCI - DURING CHECK 'C', FOUND CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE AT 6 O'CLOCK POSITION. CUT OUT DAMAGE AND REPAIRED WITH INSTALLATION OF DOUBLERS, LONGERON FITTINGS, 29L/28R. REINSTALLED WEB PER SRM 51-30, PAGE 11, AND SRM 51-30-2, SRM 53-30-3. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,595 CYCLES. (X)

Part: FLOOR TRACK — CORRODED (BS 1007-1167)

DURING CHECK 'C', FOUND CORROSION ON LEFT AND RIGHT HAND FLOOR TRACKS, STA 1007 - STA 1167. REMOVED AND REPLACED DAMAGED SEAT TRACK PER SRM 51-30-1 AND SRM 53-05-4G. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,595 CYCLES.

Part: FRAME — CORRODED (BS 1250)

MCI - DURING CHECK C, FOUND CORROSION ON FORWARD SIDE AND AFT SIDE OF AFT BAG PIT FRAME 1250, STR 29L TO STR 29R. CUT OUT CORRODED AREA AND INSTALLED REPAIR PER SRM 53-03, PAGE 4A AND SRM 51-30-1 AND SRM 51-30-2. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,595 CYCLES. (X)

Part: DOOR — CORRODED (GALLEY)

DURING CHECK 'C', FOUND CORROSION ON FORWARD GALLEY SERVICE DOOR, FORWARD AND AFT, DOOR JAMBS. REPAIRED PER SRM 53-05, FIGURE 55. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,595 CYCLES.

Part: SLIDE — FAILED (TAIL CONE)

ATL - FLT 641 - AS A RESULT OF AN INADVERTENT TAIL CONE DROP, THE TAIL CONE ESCAPE SLIDE DEPLOYED, BUT FAILED TO INFLATE. THE SLIDE AUTO INFLATE LANYARD WAS IMPROPERLY INSTALLED. REMOVED AND REPLACED TAIL CONE ESCAPE SLIDE. CHECK C - 1-1-97 - MZJ. (X)

Part: SKIN — CORRODED (BS 817)

DURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE KEEL BEAM EXTERNAL SKIN ALONG THE AREA OF CONTACT BETWEEN THE WING/BODY FAIRING. THE CORRODED AREA IS LOCATED AT THE CENTER OF THE EXTERNAL KEEL BEAM SKIN SURFACE AT LONGERON 30L, 4.0 INCHES AFT OF BS 817. BLENDED, NDT INSPECTED AND INSTALLED REPAIR DOUBLER. ACCOMPLISHED IAW EVERGREEN AIR CENTER - ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N9420-53-003-EAC.

Part: SKIN — CORRODED (BS 1211-1231)

DURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE FUSELAGE SKIN AT STA 1211 - STA 1231, BETWEEN LONGERONS 29R AND 30R. TRIMMED OUT DAMAGE, NDT INSPECTED AND INSTALLED REPAIR FILLERS AND DOUBLERS. ACCOMPLISHED IAW EVERGREEN AIR CENTER - ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N9420-53-010-EAC.

Part: SEAT TRACK — CORRODED (CABIN)

MCI - DURING CHECK C, FOUND CORROSION UNDER CLIP NUTS OF MAIN CABIN SEAT TRACK, LBL 45. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-2; SPLICED NEW SECTION PER SRM 53-05, FIGURE 4L. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X)

Part: BULKHEAD FITTING — CORRODED (AFT PRESS BLKHD)

MCI - DURING CHECK C, FOUND CORROSION ON AFT PRESSURE BULKHEAD FITTING, SEVERAL SPOTS. REMOVED AND REPLACED LONGERON FITTING PER SRM 51-00 AND INSTALLED FASTENERS PER SRM 51-30-2. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X)

Part: SEAT TRACK — CORRODED (BS 1106-1109)

MCI - DURING CHECK C, FOUND CORROSION ON MAIN CABIN SEAT TRACK SURFACE, LBL 45 TO LBL 22, STA 1106 - STA 1109. REMOVED CORRODED SEAT TRACK PER SRM 51-30-1, FABRICATED SPLICES PER SRM 53-05, FIGURE 4D; ALODINED AND PRIMED PER SRM 51-10-31 AND INSTALLED SEAT TRACK PER SRM 51-30-1. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X)