N9406W

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,770 hrs · 30,354 cycles

CENTER CARGO DOOR UPPER AFT STOP CRACKED. R & R STOP IAW AARD 51-00-05-1 & DWG 5910141.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,770 hrs · 30,354 cycles

SHEAR TIE CRACKED FWD SIDE OF FUSELAGE STATION 1380 AT LONGERON 14 RT. REPAIRED SHEAR TIE IAW AARD53-10-00-20.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,770 hrs · 30,354 cycles

SHEAR TIE CRACKED FWD SIDE OF FRAME AT FUSELAGE STATION 1380 & LONGERON 14 LT. REPAIRED IAW AARD 53-10-00-20.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,770 hrs · 30,354 cycles

LONGERON 2 RT CRACKED AT AFT SIDE OF FRAME AT FUSELAGE STATION 1418. PERFORMED SPLICE REPAIR IAW SRM 53-02-00-001.

Part: FORMER — CRACKED (LE SLAT) · airframe 62,645 hrs · 30,279 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: FORMER — CRACKED (LE SLAT) · airframe 62,645 hrs · 30,279 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06.

Part: LIGHT — DAMAGED (CABIN) · airframe 62,167 hrs · 30,034 cycles

AFT AIRSTAIR OVERHEAD EMER LIGHT ASSEMBLY DAMAGED. REPLACED AFT AIRSTAIR OVERHEAD EMER LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 62,167 hrs · 30,034 cycles

AFT STAIRWELL OVERHEAD LIGHT PANEL HAS BROKEN WIRE. REPAIRED WIRE FOR OVERHEAD EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: CSD — FAILED (LT ENGINE) · airframe 61,827 hrs · 29,837 cycles

INFLIGHT CREW REPORTED LT ENG GEN FAULTED. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED CONSTANT SPEED DRIVE & LT GEN MPN 976J2528. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CONNECTOR — LEAKING (AC BAY) · airframe 61,425 hrs · 29,613 cycles

LAS CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB OUT. ACCOMPLISHED QRH & LIGHT EXTINGUISHED. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. REPLACED PNEUMATIC GND CONNECTOR & CHECK VLV THAT WAS LEAKING. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: SKIN — DAMAGED (TE FLAP) · airframe 59,729 hrs · 28,725 cycles

LT WING OTBD FLAP UPPER SKIN HAS TWO LIGHTNING STRIKES. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW SRM 57-01 FIGURE 3 SHEET 2 & EA MD80-57-031130.

Part: DUCT — RUPTURED (LT ENGINE) · airframe 59,597 hrs · 28,651 cycles

DFW CREW REPORTED LT ENGINE FIRE WARNING JUST AFTER GEAR UP. LIGHT INDICATION WENT OUT WHEN THROTTLE MOVED TO IDLE. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND UPPER ANTI ICE DUCT RUPTURED. REPLACED ANTI ICE DUCT. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED)

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 58,284 hrs · 27,944 cycles

DFW - FLIGHT ATTENDANTS REPORTED BURNING SMELL IN THE CABIN AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED 23DEF POWER SUPPLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 55,247 hrs · 26,436 cycles

LAX - CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKE OFF. NUMBER 2 CABIN PRESSURE CONTROLLER CURRENTLY ON PLACARD. FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABIN PRESSURE OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 54,051 hrs · 25,841 cycles

SEAT ROW 32 EMERGENCY EGRESS LIGHT INOPERATIVE DURING FUNCTIONAL TEST. FOUND CONNECTOR DISCONNECTED AT SEAT ASSEMBLY. RECONNECTED AND RE-SECURED WIRING. OPS CHECK NORMAL.

Part: CONNECTOR — SEPARATED (CABIN) · airframe 54,051 hrs · 25,841 cycles

SEAT 19 EMERGENCY EGRESS FLOOR LIGHTING INOPERATIVE. FOUND CONNECTOR PINS PULLED OUT. REPINNED CONNECTOR AND SECURED WIRING. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,051 hrs · 25,841 cycles

ROW 20 LEFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 20 CEILING EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,226 hrs · 24,444 cycles

EMERGENCY EQUIPMENT COMPARTMENT HAS CORROSION ON LOWER SURFACE OF CABIN FLOOR WEBBING AT G1 GALLEY SERVICE PAN. COMPLETED INSTALLATION OF SUBFLOOR DOUBLER FROM STATIONS 160 TO 168 RIGHT UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: PUMP — LEAKING (LT WING) · airframe 51,077 hrs · 24,364 cycles

DFW - IN-FLIGHT SJD-ORD. CREW REPORTED AIRCRAFT LOSING FUEL AT RAPID PACE. EMERGENCY DECLARED DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH CENTER BOOST PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OIL FILTER — CLOGGED (RT ENGINE) · airframe 50,234 hrs · 23,932 cycles

SJC - CREW REPORTED RIGHT ENGINE OIL FILTER CLOGGED INDICATION ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED RETURNED SJC LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE OIL FILTER AND FOUND CARBON DEPOSITS BUT NO METAL. REPLACED OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 49,040 hrs · 23,422 cycles

INFLIGHT SJD TO ORD. IN CLIMB AND CRUISE, CENTER FUEL PRESSURE LOW WARNING INDICATION ILLUMINATED FOLLOWED BY INLET FUEL PRESSURE LOW LIGHT INDICATION. CREW ALSO NOTED IN LOG THAT WHEN THE CENTER WARNING STARTED, FELT A CAVITATION AS IF THE TANK WAS EMPTY. LANDED DFW WITHOUT INCIDENT. REPLACED FORWARD CENTER TANK BOOST PUMP.

Part: FITTING — CRACKED (ZONE 700) · airframe 47,589 hrs · 22,761 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL, BRACKET ABOVE DOOR ACTUATOR FITTING CRACKED AT RADIUS AFT INBOARD AREA. REPAIRED PER ESO 80559 DATED 1/26/09.

Part: WIRE HARNESS — INOPERATIVE (BOOST PUMP)

ORD INFLIGHT T346/30JUL - FORWARD CENTER FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. UNABLE TO BURN CENTER FUEL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FORWARD CENTER FUEL BOOST PUMP AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT L2 637 THROUGH 639 INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS AT L2 637 THROUGH 629. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN)

CENTER SECTION OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER SECTION EMERGENCY LIGHT BATTERY CHARGER AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CSD — OVERTEMP (RT ENGINE) · airframe 26,432 hrs · 12,741 cycles

THE RH CSD OIL TEMP INCREASED. THE CSD WAS DISCONNECTED AND APU STARTED. SEVERAL MINUTES LATER THE FREQUENCY STARTED TO FLUCTUATE AND APU SPEED DROPPED. MADE UNSCHEDULED LANDING AT TPA. CHANGED THE RT CSD AND ADJUSTED THE APU LOAD STAT.

Part: ENGINE — FAILED (NR 2) · airframe 24,745 hrs · 11,901 cycles

DURING CLIMB OUT NUMBER 2 ENGINE FAILED. CAUSE-UNKNOWN. CHANGED NUMBER 2 ENGINE. LAST CHECK C 012201 JFK ---OPEN---

Part: BLADE — FRACTURED (ENGINE) · airframe 26,236 hrs · 12,650 cycles

DURING CLIMB OUT NUMBER ONE ENGINE FAILED. FLIGHT RETURNED TO MIA FOUND TURBINE DAMAGE. CHANGED NUMBER ONE ENGINE. A FIRST STAGE TURBINE BLADE FRACTURED DUE TO OVER STRESS, DAMAGING ALL PARTS AFT OF THE FIRST STAGE TURBINE.

Part: ELEVATOR — JAMMED (TAIL) · airframe 25,011 hrs · 12,041 cycles

DURING FLIGHT CONTROL CHECK FOLLOWING FWD MOVEMENT OF ELEVATOR, SUBSEQUENT REARWARD MOVEMENT JAMMED CONTROL COLUMN IN NEUTRAL POSITION ONLY ALLOWING THE CONTROL COLUMN TO BE MOVED FORWARD AGAIN. ACCOMPLISHED EXTENSIVE CHECKS OF CABLES, LINKAGE, PULLEYS, CONTROL COLUMN, ETC. LUBED ALL APPLICABLE AREAS AND PERFORMED NUMEROUS CONTROL CHECKS. CHECK-C 1-22-01 JFK.

Part: LIGHT — INOPERATIVE (ROWS 29 & 30) · airframe 24,214 hrs · 11,625 cycles

THE EGRESS LIGHTING WAS INOPERATIVE AT ROWS 29 AND 30. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 3-21-00 MCI.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE AFT CARGO BIN CARGO TIE DOWN TRACK, LT SIDE STA 1081 TO 1318, HAD CORROSION IN NUMEROUS PLACES. REMOVED CORRODED TRACK FROM STA 1081 TO 1220 PER SPM 6-80-01 PAGE 1 PARA 2(A)(2). REPLACED TRACK FROM STA 1220 TO 1320 PER SPM 6-70-01. INSTALLED TRACK SECTION PER SRM 53-09 FIG 4G.

Part: PAN — CRACKED (CARGO DOOR) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE MID CARGO DOOR INNER PAN WAS CRACKED ABOVE THE FWD LATCH CUTOUT. FABRICATED AND INSTALLED REPAIR PER ARA 16541-A.

Part: PAN — CRACKED (CARGO DOOR) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE UPPER INNER DOOR PAN ON THE C3 CARGO DOOR HAD CRACKS AND WEAR DAMAGE. REPLACED PAN PER DOUGLAS DRAWING 5910141 AND SPM 6-70-01 PARA 4 PAGE 2 AND 3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE CARGO TIE DOWN TRACK HAD CORROSION IN NUMEROUS PLACES RT SIDE AFT TRACK FRONT STA 1212 TO 1318. REMOVED CORRODED TRACK AND REPLACED WITH NEW TRACK (P/N 179803) PER SPM 6-70-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE AFT CARGO BIN ATTACH ANGLE ON FRAME AT STA 1148 O/B OF LONGERON 30, RBL 6 IN, WAS CORRODED. FABRICATED NEW ATTACH ANGLE AND INSTALLED PER SPM 6-70-01 PARA 4 PAGE 2 AND 3 FOR MATERIAL SPEC SRM 53-14-3 FIG 3 AND SRM 51-20-01 FOR PROTECTIVE TREATMENT OF MATERIAL.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE AFT CARGO BIN FLOOR FITTING WAS CORRODED AT STA 1150, ABOVE STRINGER 29R. REMOVED CORRODED FLOOR FITTING AND INSTALLED NEW FLOOR FITTING (P/N 3957317-501) PER SPM 6-70-01 PAGE 3B (1)(2) AND DRAWING 3957317.

Part: FRAME — CORRODED (FUSELAGE) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON FRAME AT STA 1306, FROM LONGERON 30 TO 29R. REPLACED CORRODED FRAME PER SRM 53-03 FIG 2A, SHEET 1 TO 5.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE AFT CARGO COMPT LOWER AFT CARGO DOOR JAMB HAD NUMEROUS CORRODED INSERTS. REMOVED CORROSION PER TWA SPM 6-80-01 PAGE 1-2. REPLACED BEAM (P/N 5936038-501) PER SPM 6-70-01 PAGE 3 PARA B AND DRAWING 5936038.

Part: FLOORBEAM — CORRODED (BS 1174 - 1193) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA, LONGERON 18R, FROM STA 1174 TO 1193. REPLACED WEB PN 9930612-21 PER SPM 6-70-01 AND SSRM 53-10-111. SEALED AND PAINTED PER 51-10-03.

Part: FLOORBEAM — CORRODED (BS 1193 - 1212) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA, LONGERON 18R FROM STA 1193 TO 1212. REPLACED MEMBRANE PER SSRM 53-10-111. PAINTED PER SRM 51-10-03.

Part: FLOORBEAM — CORRODED (BS 1117 - 1136) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA, LONGERON 18R, FROM STA 1117 TO 1136. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 9930612.

Part: FLOORBEAM — CORRODED (BS 1098 - 1117) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA AT LONGERON 18R, STA 1098 TO 1117. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 9930612.

Part: FLOORBEAM — CORRODED (BS 1136 - 1155) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON CABIN MEMBRANE AREA LONGERON 18R, FROM STA 1136 TO 1155. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 9930612.

Part: FLOORBEAM — CORRODED (BS 1155 - 1174) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, CORROSION WAS FOUND ON CABIN MEMBRANE AREA, LONGERON 18R FROM STA 1155 TO 1174. REPLACED MEMBRANE PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 9930612.

Part: GALLEY TRACK — CRACKED (BS 1174) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, NR 4 GALLEY TIE DOWN TRACK HAD A CRACK FWD INBD TRACK TIE DOWN STA 1174 LEFT. REPLACED SEAT TRACK PER SPM 6-70-01, PAGE 2 AND 3. INSTALLED SPLICE AT STA 1202 PER SRM 53-05, FIG 4F SHEET.

Part: GALLEY TRACK — CORRODED (BS 1117 - 1155) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, NUMBER 3 GALLEY TIE DOWN TRACK HAD CORROSION ON INBD TRACK, STA 1117 TO 1155. REPLACED TRACK USING TWA PART 16-0794 PER SPM 6-70-01, PAGE 2 AND 3, ITEM 4. SPLICED TRACK AT STA 1203 PER 53-05, FIG 4F, SHEET 1.

Part: ANGLE — CRACKED (FAIRING) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE LOWER FAIRING ATTACH STRUCTURE CRACKED FWD INBD CORNER OF RT MLG WHEEL WELL, STA 943 RBL 8. REPLACED ATTACHMENT CHANNEL PER SPM 6-70-01 PAGE 3, PARA 4B AND DOUGLAS DRAWING 5930584.

Part: GALLEY TRACK — CORRODED (BS 1155 - 1193) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE NUMBER 4 GALLEY TIE DOWN AREA TRACK HAD CORROSION ON THE OTBD TRACK, FWD AND AFT, STA 1155 TO 1193. REPLACED TRACK PER SRM 53-05, PAGE 10G. PRIMED PER 51-10-03.

Part: ANGLE — CRACKED (FAIRING) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FWD FAIRING ATTACH STRUCTURE WAS CRACKED, FWD INBD CORNER, LT MLG WHEEL WELL STA 943, LBL 8. REPLACED ATTACHMENT CHANNEL PER SPM 6-70-01, PAGE 3 PARA 4B AND DOUGLAS DRAWING 5930584.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE LT WHEEL WELL, FWD INBD CORNER AT KEEL BEAM AREA, ATTACH ANGLE CRACKED IN RADIUS .375 INCH LONG. REPLACED ATTACH ANGLE PER SPM 6-70-01, PAGE 3, PARA 4B, AND DOUGLAS DRAWING 9936368.

Part: GALLEY TRACK — CORRODED (BS 1117 - 1155) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, THE NUMBER 3 GALLEY TIE DOWN TRACK AREA HAD CORROSION ON OTBD TRACK, FWD AND AFT OF STA 1117 TO 1155. REPLACED TRACK PER SRM 53-05, PAGE 10G. PRIMED PER SRM 51-10-03.

Part: FLOORBEAM — CORRODED (BS 1155) · airframe 22,306 hrs · 10,547 cycles

DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 1155, BETWEEN NUMBER 3 AND 4 GALLEYS TIE DOWN TRACK. REPLACED FLOOR SUPPORT PER SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-03.

Part: FLOORBEAM — CORRODED (BS 160 - 200) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON SUB FLOOR MEMBRANE AT STA 160 TO 200, LBL 6 IN TO RBL 53 INCHES. REPLACED SUB FLOOR MEMBRANE STA 160 TO 200, LBL 12 TO RBL 59, WITH 0.020 7075-T6, INSTALLED WITH SEALER AND 3 ROWS OF ATTACHMENT FASTENERS PER SRM 53-01, PAGE 18 FIG 4 SHEET 3.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 22,306 hrs · 10,547 cycles

DURING CHECK-C MAINT, IN RT WHEEL WELL, FWD INBD CORNER AT KEEL BEAM AREA, ATTACHMENT ANGLE CRACKED IN RADIUS .5 INCH LONG. REPLACED ATTACH ANGLE PER SPM 6-70-01, PAGE 3 APRA 4B AND DOUGLAS DRAWING 9936368.

Part: SKIN — DAMAGED (FUSELAGE)

DURING CHECK-C MAINT, A 3 INCH DENT, .5 INCH WIDE AND .125 DEEP HAD A SCAB PATCH WITH BLIND FASTENERS, APPROX 3 FEET AFT OF THE FORWARD LEFT CABIN DOOR AND 1.5 FEET BELOW DOOR, ON SIDE OF FUSELAGE. ACCOMP SKIN PANEL REPAIR PER SSRM 53-10-107, PAGE 202 AND SRM 53-04 PAGE 283.

Part: FLOORBEAM — CORRODED (BS 660)

DURING CHECK-C MAINT, MEMBRANE WAS CORRODED ON LT SIDE LONGERON 18, STA 660 TO 665. REMOVED CORROSION PER SPM 6-80-01. ALODINED AND PRIMED PER SRM 51-40-3. FABRICATED DOUBLER FROM TWA SN 55-0261. INSTALLED DOUBLER WITH AD RIVETS. SEALED WITH RRC 1422 PER SRM 53-01 PAGE 9 AND SRM 51-20-2.

Part: FRAME — CORRODED (BS 579 & 598)

DURING CHECK-C MAINTENANCE, THE LT FUSELAGE BETWEEN STA 598 AND 579, AT LONGERON 18R HAD MEMBRANE CORRODED. REMOVED CORROSION PER SRM 51-10-3. CUT OUT MEMBRANE AND REPAIRED PER SRM 53-01, PAGE 18.

Part: FRAME — CORRODED (BS 788.5)

DURING CHECK-C MAINTENANCE, FOUND CORROSION ON LOWER FRAME BETWEEN AND ABOVE LONGERON 28 AND 30, STA 788.5. REMOVED COROSION PER STANDARD PROCESS MANUAL 6-80-1.

Part: SEAT TRACK — CORRODED (BS 347 - 367)

DURING CHECK-C MAINT, FOUND CORROSION IN CABIN CHAIR FLOOR TRACK RBL 55, STA 347 TO 349, AND 361 TO 367. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 AND 2. FOUND TRACK WITHIN LIMITS PER SRM 53-05, FIG 4B-1, SHEET 1 AND 2.

Part: SKIN — DAMAGED (BS 389)

DURING CHECK-C MAINT, FOUND FUSELAGE SKIN DAMAGED AT LONGERON 29L TO 29R, STA 389. INSTALLED EXTERNAL SKIN PATCH PER SRM 53-04, FIG 35 SHEET 1 AND SRM 53-04 FIG 12B SHEET 3.

Part: BATTERY — DISCHARGED (CABIN)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE ROWS 2 TO 5, AND DIM FROM ROWS 12 THRU 27. REPLACED THE LAMPS, (P/N 7732), AT ROWS 1 THRU 5, AND REPLACED THE MID CABIN BATTERIES, (P/N 408822-101), FOR THE DIM LIGHTS. CHECK-C 1-18-99.

Part: BLADE — FRACTURED (LT ENGINE COMP)

DURING APPROACH THE LT ENGINE STOPPED PRODUCING POWER AND EGT ROSE TO 800 DEG. ENGINE WAS SHUT DOWN. ON THE GROUND THE N1 COMPRESSOR WOULD NOT ROTATE AND THERE WAS METAL IN THE TAILPIPE. THE ENGINE WAS CHANGED. CHECK-C 1-18-99 ST. *S/D* FOUND 2 SEVENTH STAGE TITANIUM COMPRESSOR BLADES HAD FRACTURED FROM FOD AND FATIGUE.

Part: POWER SUPPLY — WORN (ROW 12-21)

FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM CABIN ROWS 12 THROUGH 21. REPLACED POWER SUPPLY. CHECK-C 1-15-98 STL.

Part: LAMP — FAILED (SEAT 23D)

DURING MAINT, FOUND EGRESS LIGHTS INOPERATIVE AT CABIN SEAT 23D AND 30D. REPLACED LAMPS. CHECK-C 1-15-98 STL.

Part: BULB — FAILED (ROW 16)

EGRESS LIGHTS WERE REPORTED INOPERATIVE AT CABIN ROWS 1, 3, 10 AND 16. CORRECTIONS WERE DEFERRED PER MEL. ON LAYOVER RESEATED BULBS AT ROWS 1, 3 AND 10. REPLACED BULB AT ROW 16. CHECK-C 1-15-98 STL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND EMERGENCY OVERWING LIGHTS INOP. REPLACED BATTERY PACK. CHECK-C 1-15-98 STL.

Part: STATOR VANE — LIBERATED (RT ENGINE)

BNA - FLT 505 - AT FL 270, RT ENGINE PRODUCED TWO LARGE COMPRESSOR STALLS FOLLOWED BY PARTIAL LOSS OF ENGINE POWER. DIVERTED TO BNA. ON APPROACH, EGT STARTED TO RISE AND ENGINE WAS SHUT DOWN. FOUND TURBINE FAILURE. REPLACED ENGINE. S/D: ON ENGINE TEAR DOWN, FOUND 8TH STAGE STATOR VANE HAD LIBERATED AND CAUSED SEVERE DAMAGE TO THE HIGH PRESSURE COMPRESSOR. THE PWA ENGINE MANUAL WAS REVISED TO REDUCE THE NUMBER OF STRAP WELDS ON 7C, 8C, AND 9C STATOR VANES.

Part: HANDLE — OUT OF POSITION (MAIN GEAR)

STL - FLT 347 - DURING TAKEOFF STL, THE LANDING GEAR FAILED TO RETRACT. RETURNED TO STL. MAIN GEAR BYPASS HANDLE WAS REPOSITIONED FROM THE BYPASS TO THE NORMAL POSITION. (M)

Part: LAMP — BROKEN (CABIN)

STL - FLT 169 - DURING ROUTINE MAINTENANCE, THE EMERGENCY EGRESS LIGHT AT ROW 6 WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE LAMP MODULE, MFG PN 0105606-003, MANUFACTURED BY LUMINATOR AIRCRAFT PRODUCTS. OPERATIONAL CHECK NORMAL. CHECK C - 1-23-97 - JFK. (X)