N959U

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - AFT OVERWING EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT)

DFW - FLIGHT ATTENDANT SWITCH WILL NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH AND AFT CARGO EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 43,145 hrs · 22,051 cycles

MAL-FWD OVERHEAD GALLEY LIGHT PN 293-0077 GETS VERY HOT AND SMELLS OF ELECTRICAL BURNING ODOR. DEACTIVATED AND REMOVED BULB. PLACARDED PER MEDP 33-2. PULLED AND BANDED FWD MIS CABIN AND LAV LT CB. HEAT AND SMELL GONE. LAST CHECK-C STL 6/28/01

Part: LIGHT — CONTAMINATED (CABIN) · airframe 41,408 hrs · 20,966 cycles

THE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. CLEANED AND DRIED OUT THE LIGHT STRIP. CHECK-C 6-28-01 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,196 hrs · 20,858 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21 TO 26. REPLACED BROKEN CONTACT ON POWER STRIP AT THE LIGHT TRACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,384 hrs · 20,420 cycles

THE EGRESS LIGHTING IN THE FIRST CLASS SECTION WAS INOPERATIVE. REMOVED THE LIGHT STRIP. CLEANED THE TRACK AND ELECTRICAL CONTACTS. PRESERVED CONTACTS WITH MOISTURE LOCKOUT BEFORE RE-INSTALLING. CHECK-C 12-3-00 MCI.

Part: CASTING — CORRODED (LT WING) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT ON LT WING THE O/B FLAP I/B MOUNT CASTING ON SPAR TOP I/B STUD WAS EMITTING RUST. REPLACED 2 UPPER STUDS AND INSTALLED NEW HINGE CASTING PER MM 57-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND FASTENER HOLES FOR FLOOR AND SIDEWALL PANELS CORRODED AT LT FLOOR TRACK STA 1170 TO STA 1221. REPLACED CORRODED SECTION OF TRACK PER SRM 53-05, FIG 4G.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT A FORMER WAS CORRODED AT STA 1308, LONGERON 28R TO 23L. REMOVED FRAME FROM LONGERON 18R TO 18L. INSTALLED NEW FRAME. INSTALLED SPLICE BETWEEN LONGERON 25R AND 26R PER SRM 53-03, PAGE 4C, AND FIG 2A FOR THICKNESS 0.071 TO 0.080.

Part: BEAM — CORRODED (CARGO BAY) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND DOOR BEAM CORRODED AT STA 1155 TO 1211. REMOVED CORROSION PER SPM 6-80-01. BEAM OUT OF LIMITS AND REPLACED PER DRAWING 5936038-501. INSTALLED PER SRM 51-30-02 AND 51-30-05. TREATED AND PAINTED PER 51-10-3.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND MEMBRANE CRACKED AT STA 237, RBL 46. REPLACED CRACKED MEMBRANE WITH SHOP FABRICATED NEW ONE. INSTALLED WITH FASTENERS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON TRACK AT STA 200 TO 237, RBL 44. REMOVED CORROSION PER SPM 6-80-1. REPLACED 47 INCHES OF TRACK PER SRM 53-08 FIGURE 4F.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT STA 200 RT SIDE, AND UNDER T-ANGLE BOTTOM DOOR FRAME (JAMB) SUPPORT. INSTALLED NEW MEMBRANE FROM STA 160 TO 200, RBL 44 PER SRM 53-01 PAGE 9, FIG 2, DRAWING 993634.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 200, RBL 46 TO 50, AND ON MEMBRANE RT SIDE AT SIDEWALL TO FLOOR SUPPORT ANGLE STA 160 TO 180, RBL 53 TO 57. INSTALLED NEW MEMBRANES FROM STA 160 TO 200, RBL 44 TO RBL 57, PER SRM 53-01 PAGE 9 FIGURE 2, DRAWING 9936534, SRM 51-30-5. SEALED PER SRM 51-20-0.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CUSP AT STA 170 TO 200, AT FWD SERVICE DOOR SILL AREA. RE-INSTALLED FASTENERS REMOVED FOR CORROSION REMOVAL. REMOVAL PER SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 170 TO 200, RBL 56 TO 58, AND ON MEMBRANE UNDER FLOOR SUPPORT AT STA 180 TO 200, RBL 53. INSTALLED NEW MEMBRANES FROM STA 160 TO 200, RBL 44 TO 57, PER SRM 53-01 PAGE 9 FIGURE 2, DRAWING 9936534, SRM 51-30-2, AND SRM 51-20-5 FOR SEALING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT STA 180, RBL 10 TO RBL 44. NEW FLOOR SUPPORT FABRICATED PER DRAWING 9936534. PAINTED PER SRM 51-10. INSTALLED FASTENERS PER SRM 51-30-2, SRM 51-30-05. SEALED STIFFENER PER SRM 51-20-0.

Part: WEB — CORRODED (SERVICE DOORSILL) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE UNDER RT SERVICE DOOR SILL AT STA 170 AND ON MEMBRANE AT STA 160, RBL 43. INSTALLED NEW MEMBRANE FROM STA 160 TO 200, RBL 44 TO 57 PER SRM 53-01, PAGE 9 FIG 2, DRAWING 9936534, SRM 51-30-2, AND SRM 51-30-5. SEALED PER SRM 51-20-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, THE CABIN FLOOR AND GALLEY DRAIN PAN SUPPORT WAS CORRODED AT STA 160, RBL 53 INCHES. INSTALLED SUPPORT ANGLE PER SRM 51-30. REMADE FLOOR SUPPORT FROM RAW STOCK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 160 TO 180, RBL 53 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. PAINTED PER SRM 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND FASTENER HOLES CORRODED FOR FLOOR AND SIDE WALL PANELS AT LT FLOOR TRACK STA 1221 THRU 1322. REPAIRED PER SRM 53-05, FIG 4G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200, RBL 10 IN TO RBL 48 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. PAINTED AND TREATED PER SRM 51-10-3. INSTALLED NEW SUPPORT PER SRM 51-30.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FLOOR SUPPORT WAS CORRODED AT STA 160 TO 200, RBL 44 IN. NEW FLOOR SUPPORT FABRICATED PER DRAWING 9936534. PAINTED PER SRM 51-10-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1287, FROM LONGERON 30 T0 23L, FWD SIDE. FORMER FRAME SEGMENT WAS REMOVED FROM LONGERON 18L AND BETWEEN L25R AND L26R. NEW FRAME WAS INSTALLED PER SRM 53-03, FIG 2A AND PER DRAWING 9957739.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION AT PREVIOUS REPAIR FWD SIDE OF FORMER STA 1287, LONGERON 29L THRU L29R. FORMER FRAME SEGMENT WAS REPLACED FROM LONGERON 18L TO AND BETWEEN LONGERON 25R AND L26R PER SRM 53-03, FIG 2A, AND DRAWING 9957739.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON SPLICE PLATE AFT SIDE OF FORMER STA 1287, LONGERON 30 AND 28L. FORMER FRAME SEGMENT WAS REPLACED FROM LONGERON 18L AND BETWEEN L25R AND L26R PER SRM 53-03, FIG 2A, AND DRAWING 9957739.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION AT FORMER FOOT STA 1287, BETWEEN LONGERON 30R AND LONGERON 29R. NEW FORMER FOOT WAS INSTALLED PER DRAWING 9957739.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, ON RT WING T/E THE I/B FLAP T/E WEDGE WAS DELAMINATED APPROX 65 INCHES TO 72 INCHES FROM I/B END OF FLAP. CLEANED DAMAGED AREA AND REPAIRED PER SRM 51-90-0.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, THE FUSELAGE SKIN WAS REMOVED TO A THICKNESS OF 0.029 IN AT LT STA 237 BETWEEN LONGERON 17L AND 18L, MEASURED WITH NDT U.T. THICKNESS STRESSTEL INSTRUMENT. REMEASURED SKIN THICKNESS WITH NORTEC 1000 AND KRAUTKRAMER PENCIL THINKNESS PROBE AND FOUND 0.008 IN MATERIAL REMOVED. MATERIAL LEFT FOUND TO BE 0.034 INCHES. INSTALLED REPAIR PER SRM 53-04-12B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON NUMBER 2 CHAIR TRACK O/B OF FLOOR PANEL 1 ATTACH FLANGE, STA 1265 TO 1309. ALSO CORROSION ON TRACK FLANGE STA 1193 TO 1212 AT LBL 48. REPLACED CHAIR TRACK FROM STA 1032 TO 1307 PER SPM 6-70-01. INSTALLED SPLICE PER SRM 53-05. INSTALLED FASTENERS PER SRM 51-30.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON TRACK AT LBL 59 AT GALLEY TIE DOWN STA 1208. ALSO CORROSION ON TRACK AT LBL 58 ON FLANGE AND AT GALLEY TIE DOWN STA 1236. CORROSION ALSO FOUND ON TRACK AT LBL 58 AT GALLEY TIE DOWN AT STA 1174. REPLACED TRACK FROM STA 1174 TO 1287 USING BOLTS PER SRM 51-30-1.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND CORROSION AT BOTTOM OF CABIN FLOOR MEMBRANE, STA 1163, LBL 5 INCHES. REMOVED CORROSION PER SPM 6-80-01. INSTALLED REPAIR PER SRM 53-01-18. PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION IN SEAT TRACK AT LBL 24 INCHES, STA 1205 TO 1309. MATERIAL .25 INCH THICK MISSING. REMOVED AND REPLACE CHAIR TRACK AT LBL 24 IN FROM STA 1180 TO 1309 WITH STOCK MATERIAL, SPLICE AND PLATE. ATTACHED WITH HI-LOKS, MS250 WASHERS, AND MS21042L4 NUTS. TRACK TO FLOORBEAM BOLTS NAS 6233, MS250 WASHERS, MS21042L3 NUTS PER SRM 53-05 FIG 4F, SRM 51-60-0, SRM 51-30-1 AND SRM 51-30-5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND FORMER CORRODED ABOVE LONGERON 29L, AT STA 1193. REMOVED FORMER, FABRICATED, HEAT TREATED AND INSTALLED NEW FORMER PER DRAWING 9936073.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND STRAP UNDER TRACK AT LBL 59 IN WAS CORRODED FROM STA 1136 TO 1142, AND THE FASTENER HEADS WERE POPPED. REPAIRED, REPLACED NEW STRAP PER SPM 6-70-01. PAINTED PER SRM 51-30-05. INSTALLED FASTENERS PER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION IN THE SEAT TRACK AT RBL 24, AT STA 247 AND FROM STA 206 TO 210. CUT OUT TRACK AT BOTH LOCATIONS AND INSTALLED NEW TRACK PER SRM 53-05, FIG F.

Part: SKIN — DENTED (LT WING SLAT) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, THE LT WING O L/E SLAT HAD DENT IN L/E APPROX CENTER OF SLAT. ACCOMP NDT AND NO CRACK FOUND PER PART 6-51-08-03 HFEC OF AREA IN SHOP PER TWA NDT SPM NUMBER 3 REPAIR PART NUMBER 6, NO CRACK. FOUND OK TO CLOSE LOWER SKIN. REPAIRED L/E PER SRM 57-09, FIG 10A, PAGE 44A. INSTALLED LOWER SKIN PER DRAWING 5937415.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON GALLEY TRACK AT STA 1136 TO 1178. REPLACED 42.75 INCH SECTION OF GALLEY TRACK PER SRM 53-05, PAGE 11, FIG 4H. INSTALLED TRACK PER SRM 51-30-1.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOORBEAM CAP AT STA 1250, LBL 24 IN TO LBL 48 INCHES. REPLACED FLOOR PANEL SUPPORT PER DRAWING 9930612.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM CAP AT STA 1155, LBL 24 TO LBL 47. REMOVED AND REPLACED FLOORBEAM CAP PER SPM 6-70-01, PAGE 2 AND 3. INSTALLED BEAM CAP USING HI-LOKS PER SRM 51-30-5, PAGE 12, AND PER TORQUE VALUES SRM 51-30-1, PAGE 11 TO 13.

Part: WEB — CORRODED (CABIN) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE UNDER END OF SUPPORT AT STA 201, RBL 10 INCHES. REMOVED CORROSION PER SRM 6-80-01. TREATED CORROSION PER SRM 51-10-3. REPAIRED MEMBRANE PER SRM 53-01 PAGE 9.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, THE FWD CARGO DOOR INTERNAL DOOR SKIN HAD A 2 INCH CRACK IN THE RADIUS OUTBOARD SIDE OF AFT BOTTOM LATCH AND .5 INCH CRACK BETWEEN ADJACENT FASTENER HOLE. CRACK CONTAINED PER EDDY CURRENT PART L 51-00-03. INSTALLED DOUBLER PER SRM 52-05, FIG 26A.

Part: STRUCTURE — DENTED (LT WING SLAT) · airframe 39,119 hrs · 19,711 cycles

DURING CHECK-C MAINT, THE LT WING L/E NUMBER 3 SLAT INBOARD L/E HAD WIND EROSION ON DENT FILLER IN DENT APPROX 2 FEET FROM INBOARD END. ACCOMP NDT AND NO CRACK FOUND PER PART 6 OF 51-00-03. SANDED OUT OLD FILLER AND REPLACED WITH NEW PER SRM 57-03 PAGE 20A.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 38,367 hrs · 19,255 cycles

DURING OVERNIGHT INSPECTION FOUND EGRESS FLOOR LIGHTING AND FORWARD ENTRY DOOR EMERGENCY EXIT SIGNS INOP. REPLACED EGRESS BATTERY PACK. AC04 04-30-00 DFW.

Part: BATTERY PACK — DISCHARGED (ROW 7-8-11&33)

THE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 7, 8, 11 AND 33, AND THE AIRSTAIRS. REPLACED THE BATTERY PACK, PART NR 5822-2, IN THE CABIN AND REPAIRED WIRING IN THE AIRSTAIRS. CHECK-C 7-6-99 JFK.

Part: BATTERY PACK — DISCHARGED (ROW 20)

THE EGRESS LIGHTS AT ROWS 15 TO 21 CAME ON IN FLIGHT AND WOULD NOT RESET. REPLACED THE BATTERY PACK AT ROW 20. CHECK-C 10-10-98 STL.

Part: BATTERY PACK — DISCHARGED (ROW 15-20)

THE CABIN EGRESS LIGHTS AT ROW 15 TO 20 ILLUMINATED INTERMITTENTLY IN FLIGHT. REPLACED THE MID CABIN EGRESS LIGHT BATTERIES. CHECK-C 10-10-98 STL.

Part: EXCITOR — SHORTED (APU)

THE LT CSD TEMP WAS HIGH AND CREW DISCONNECTED THE CSD. ATTEMPTED TO START APU FOR GENERATOR BUT APU WOULD NOT START. CORRECTED THE APU BY REPLACING THE OIL PRESS SEQUENCE SWITCH, MFG 692525-9, THE IGNITION COIL, MFG 10-381175-9, AND THE IGNITOR PLUG MFG CH31723. PLACARDED THE CSD INOPERATIVE PER MEL. MAINTENANCE LATER FOUND THE CSD OIL LEVEL LOW AND THE SCAVENGE FILTER DIFFERENTIAL PRESSURE INDICATOR POPPED. REPLACED THE CHARGE AND SCAVENGE FILTER PRECAUTIONARY. CSD SERVICED TO PROPER LEVEL. THE APU IGNITION EXCITOR THAT WAS REPLACED WAS FOUND IN THE SHOP TO HAVE AN INTERNAL SHORT WHICH CAUSED THE APU TO NOT START. CHECK-C 10-10-98 STL.

Part: BATTERY — DISCHARGED (ROW 29)

EGRESS LIGHTS IN FLOOR AFT OF ROW 29 CAME ON IN FLIGHT AND REMAINED ON. REPLACED BATTERIES IN POWER SUPPLY. CHECK-C 10-1-98 STL.

Part: ACM — FAILED (RIGHT)

STL - FLT 30 - DURING TAKEOFF, THE RIGHT AIR CYCLE MACHINE TURBINE FAILED CAUSING SMOKE IN THE PASSENGER CABIN. REMOVED AND REPLACED THE RIGHT AIR CYCLE MACHINE, MFG P/N 204950-5-4, MANUFACTURED BY ALLIED SIGNAL AEROSPACE. OPERATIONAL CHECK NORMAL. (M)

Part: SOCKET — LOOSE (RT MLG)

STL - FLT 166 - DURING LANDING, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. FOUND LIGHT SOCKET PUSHED IN, REPOSITIONED AND SECURED SOCKET ASSEMBLY. OPERATIONAL CHECK NORMAL. (M)

Part: FRAME — CORRODED (BS 1271)

MCI - DURING OP-16, FOUND CORROSION IN AFT CARGO COMPARTMENT LONGERON 17L TO LONGERON 27R FRAME, FS 1271. REMOVED CORROSION PER SRM 51-10-3 AND INSTALLED REPAIR PER SRM 53-03, PAGE 4E, VIEW Q. (M)

Part: SKIN — CORRODED (BS 824)

MCI - DURING OP-16, FOUND CORROSION ON CENTERLINE FUSELAGE SKIN, LONGERON 30, FS 824. REMOVED CORROSION PER SRM 51-10-03 AND INSTALLED DOUBLER PER SRM 53-04, PAGE 321 AND ARA 10722.

Part: TRACK — CORRODED (BS 1280)

MCI - DURING OP-16, FOUND CORROSION ON LEFT OUTBOARD GALLEY TIEDOWN TRACK, STATION 1280. REPLACED GALLEY TIEDOWN TRACK PER SRM 51-01.

Part: BULKHEAD PANEL — CORRODED (BS 1322)

MCI - DURING OP-16, FOUND CORROSION ON ALL SUPPORTS ON VERTICAL BULKHEAD PANEL, FS 1322. REMOVED CORROSION PER SRM 91-01-3, AND REPLACED PARTS PER SRM 51-10. (M)

Part: SKIN — CORRODED (BS 807-820)

MCI - DURING OP-16, FOUND CORROSION ON LOWER FUSELAGE SKIN, STATION 807-820, RBL 5. REPAIRED PER SRM 53-04, FIGURE 53. (M)

Part: FLOOR BEAM — CORRODED (CABIN)

MCI - DURING OP-16, FOUND CORROSION ON CABIN LOWER FLOOR BEAM. INSTALLED NEW ANGLE PER SRM 51-01, PAGE 1, ITEM C. (M)

Part: RIB — CRACKED (VERT STAB)

MCI - DURING OP-16, FOUND LOWER LEADING EDGE PANEL VERTICAL STABILIZER LOWER ENDS OF RIBS CRACKED, LEFT AND RIGHT SIDE. REPAIRED PER SRM 55-30-102, FIGURE 201.

Part: TRACK — CORRODED (BS 1290)

MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK, STATION 1290, LBL 21. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK PER SRM 53-05, PAGE 4. (M)

Part: SKIN — CORRODED (BS 769)

MCI - DURING OP-16, FOUND CORROSION ON RIGHT SIDE OF FUSELAGE SKIN ABOVE LONGERON 29R, FS 769. REPAIRED PER SRM 53-543 AND TWA STANDARD PRACTICES. (M)

Part: FLOOR — DAMAGED (BS 1208)

MCI - DURING OP-16, FOUND HOLE IN CABIN FLOOR MEMBRANE ADJACENT TO LEFT SIDEWALL, FS 1208. INSTALLED REPAIR PER SRM 53-01, APGE 17, FIGURE 4. (M)

Part: TRACK — CORRODED (BS 1300)

MCI - DURING OP-16, FOUND CORROSION ON NR 2 FLOOR TRACK, STATION 1300. REPLACED CORRODED SECTION OF TRACK PER SRM 53-05, FIGURE 4F. (M)

Part: FORMER — CORRODED (BS 1322)

MCI - DURING OP-16, FOUND CORROSION ON FORMER WEB AND CAP, LONGERON 27L TO LONGERON 28R, STATION 1322. REMOVED CORROSION PER SRM 51-10-3 AND REPAIRED PER SRM 53-03 AND TWA STANDARD PRACTICES. (M)

Part: FORMER — CORRODED (BS 1287)

MCI - DURING OP-16, FOUND CORROSION ON FORMER CAP WEB FOOT, FS 1287, RBL 5 TO LBL 20. CUT OUT AND REMOVED CORRODED AREA INSTALLED REPAIR PER SRM 53-03, FIGURE 2A, VIEW Q. (M)

Part: RIB — CRACKED (WS 331)

MCI - DURING OP-16, FOUND A ONE INCH CRACK IN UPPER RADIUS OF RIGHT WING LE RIB AFT UPPER END, STATION 331. REPLACED LE RIB PER SRM 51-01 AND TWA STANDARD PRACTICES. (M)

Part: FRAME — CORRODED (BS 1250)

MCI - DURING OP-16, FOUND CORROSION ON FRAME, LONGERON 28R TO LONGERON 28L, STATION 1250. REMOVED CORROSION PER SRM 51-10-03, AND REPAIRED PER SRM 53-03, FIGURE 2A, VIEW Q, AND TWA STANDARD PRACTICES. (M)

Part: SPLICE — CRACKED (WS 164)

MCI - DURING OP-16, FOUND A 1 INCH CRACK IN RIGHT WING LE SPLICE PLATE, STATION 164. REPAIRED PER SSRM 57-40-103.

Part: RIB — CRACKED (WS 312)

MCI - DURING OP-16, FOUND A 1 INCH CRACK IN UPPER RADIUS OF RIGHT WING LE RIB U PPER END, STATION 312. REPLACED LE RIB PER SRM 51-01 AND TWA STANDARD PRACTICES.

Part: BULKHEAD SUPPORT — CORRODED (BS 1322)

MCI - DURING OP-16, FOUND CORROSION ON BULKHEAD FLOOR SUPPORT, FS 1322. INSTALLED NEW SUPPORT PER SRM 51-01 AND TWA STANDARD PRACTICES.

Part: CLIP — CORRODED (BS 1211-1329)

MCI - DURING OP-16, FOUND CORROSION AT CLIP NUT HOLES OF RIGHT CARGO TRACK IN AFT CARGO BIN, FS 1211 TO FS 1329. REPLACED TRACK PR SRM 51-01, PAGE 1.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

IND - FLT 160 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 3245, DUE TO VIBRATION AND COMPRESSOR STALLS. DURING GROUND RUN, ENGINE HAD OFF IDLE STALLS. REPLACED ENGINE AND OPERATONAL CHECKS WERE NORMAL. ENGINE TT: 26,119 HOURS; 13,618 CYCLES. CHECK C-1D - 7-28-95 - MCI.

Part: SCHRADER VALVE — FAILED (NLG STRUT)

STL - FLT 255 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. CYCLED LANDING GEAR. FOUND NLG STRUT LOW ON AIR PRESSURE. REPLACED SCHRADER VALVE, MFG PN A00314. SERVICED NLG STRUT. LANDING GEAR OPERATION CHECKED NORMAL. CHECK C-1D - 7-28-95 - MCI.