N9620D

Part: SKIN — CRACKED (FWD FUSELAGE) · airframe 59,582 hrs · 29,670 cycles

FUSELAGE SKIN WAS FOUND CRACKED AT THE NOSE GEAR LEFT AFT DOOR, AFT HINGE CUTOUT. REPAIRED THE SKIN IAW 53-05-00-001, PARA 162, FIGURE 158.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,582 hrs · 29,670 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT ACCESSORY COMPARTMENT FRAME AT BS 1401 AND LONGERON 1. REPAIRED COMPARTMENT FRAME PER SRM 53-01-00-0001.

Part: PITOT TUBE — FAILED (CAPTAIN'S) · airframe 59,272 hrs · 29,471 cycles

DURING CLIMB, CADC LIGHT ILLUMINATED AND THE CAPTAIN`S AIRSPEED CLIMBED QUICKLY TOWARD THE BARBER POLE. SWITCHED TO ADC BOLT ON 2 AND CAPTAIN`S AIRSPEED RETURNED TO NORMAL. AFTER A FEW MINUTES, AND LATER WITH SEVERAL OVERSPEED WARNINGS AT 280KTS. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE CAPTAIN`S PITOT TUBE AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 34-11-02.

Part: GUST LOCK — BENT (L1 DOOR) · airframe 59,211 hrs · 29,430 cycles

L1 DOOR GUST LOCK LATCH IS BENT AND WILL NOT ENGAGE IN FUSELAGE. ALIGNED THE GUST LOCK LATCH, ENGAGES FUSELAGE AND HOOKS PROPERLY IAW AMM 52-11-04.

Part: ANGLE — CORRODED (BS 947-953) · airframe 58,886 hrs · 29,217 cycles

CORROSION ON THE HORIZONTAL LEG OF ANGLE AT THE LT GEAR WELL INBOARD SIDE OF TRAPEZOIDAL PANEL AT BS 947 - 953. AIRCRAFT WAS GROUNDED. REPLACED THE ANGLE IAW 51-00-05

Part: ANGLE — CORRODED (BS 947-953) · airframe 58,886 hrs · 29,217 cycles

CORROSION ON HORIZONTAL LEG OF ANGLE AT RT GEAR WELL, INBOARD SIDE OF TRAPEZOIDAL PANEL AT BS 947 - 953. AIRCRAFT WAS GROUNDED. REPLACED ANGLE IAW 51-00-05-1

Part: GUST LOCK — LOOSE (L1 DOOR) · airframe 58,495 hrs · 28,982 cycles

L1 DOOR GUST LOCK DOES NOT STOW. ADJUSTED THE L1 DOOR GUST LOCK IAW 52-11-00.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 57,517 hrs · 28,332 cycles

THE AIRCRAFT WAS NOT GROUNDED. FORWARD LEFT AND RIGHT OVERWING EXIT SIGNS WOULD NOT TURN OFF. REMOVED AND REPLACED EMERGENCY BATTERY PACK B5-207 PER AMM 33-53-00. OPERATIONS CHECK GOOD.

Part: DOOR FRAME — CRACKED (WING) · airframe 57,342 hrs · 28,218 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FUEL SERVICE DOOR LANDING BENT, POSSIBLE CRACK. REPAIRED THE LANDING FOR THE DOOR IAW SRM 57-06A-00-001.

Part: GIRT BAR — DETACHED (ZONE 800) · airframe 57,012 hrs · 27,996 cycles

AIRCRAFT NOT GROUNDED. AFT GALLEY DOOR GIRT BAR DETACHED. REINSTALLED AFT GALLEY DOOR SLIDE GIRT BAR IAW GPM 25-62-00.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 56,961 hrs · 27,962 cycles

EMERGENCY LIGHT HAS AN EXPOSED WIRE AT SEAT 14D. ALL OTHER EMERGENCY LIGHTS OPERATIONAL. EXPOSED WIRE CAPPED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-60-98. OPS CHECKED GOOD.

Part: CONTROL BOX — FAULTED (ANTI-SKID SYS) · airframe 56,898 hrs · 27,911 cycles

WHEEL NOT TURNING LIGHT ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF AT 80 KNOTS. TRANSDUCER COUPLERS FOUND DAMAGED. REMOVED AND REPLACED THE NR 2 ANTI-SKID TRANSDUCER, NR 3 ANTI-SKID TRANSDUCER IAW AMM 32-43-02, AND THE ANTI-SKID CONTROL BOX IAW AMM 32-43-04. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: TRANSDUCER — DAMAGED (NR 2) · airframe 56,898 hrs · 27,911 cycles

WHEEL NOT TURNING LIGHT ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF AT 80 KNOTS. TRANSDUCER COUPLERS FOUND DAMAGED. REMOVED AND REPLACED NR 2 ANTI-SKID TRANSDUCER AND NR 3 ANTI-SKID TRANSDUCER IAW AMM 32-43-02 AND THE ANTISKID CONTROL BOX IAW AMM 32-43-04. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: TRANSDUCER — DAMAGED (NR 3) · airframe 56,898 hrs · 27,911 cycles

WHEEL NOT TURNING LIGHT ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF AT 80 KNOTS. TRANSDUCER COUPLERS FOUND DAMAGED. REMOVED AND REPLACED NR 2 ANTI-SKID TRANSDUCER, NR 3 ANTI-SKID TRANSDUCER IAW AMM 32-43-02, AND THE ANTISKID CONTROL BOX IAW AMM 32-43-04. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: CONTROL VALVE — FAULTY (ANTI-SKID SYS) · airframe 56,897 hrs · 27,910 cycles

AIRCRAFT WAS GROUNDED. WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF. REJECTED TAKEOFF AT 80 KNOTS. REMOVED AND REPLACED LEFT OUTBOARD ANTI-SKID CONTROL VALVE (VAL3149) PER AMM 32-43-03. OPERATIONAL CHECK GOOD.

Part: OVEN — SMOKE (NR 1 GALLEY) · airframe 56,525 hrs · 27,683 cycles

EMERGENCY DECLARED, AND DIVERTED DUE TO REPORTED SMOKE FROM FORWARD GALLEY OVEN. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 1 INBOARD OVEN IAW AMM 25-39-03. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: CABLE — DISCONNECTED (DOOR SLIDE) · airframe 56,204 hrs · 27,483 cycles

CABLE FROM RIGHT GIRT SLIDE PACK IS DISCONNECTED. ATTACHED AND SECURED THE CABLE IAW AMM 25-62-00. OPS CHECKED GOOD.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 56,112 hrs · 27,428 cycles

L1 DOOR OPENED WITH GIRT BAR STILL ATTACHED. EMERGENCY EVACUATION SLIDE IS HALF WAY OUT OF CONTAINER. REINSTALLED THE SLIDE IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: COMPRESSOR — STALLED (ENGINE) · airframe 55,661 hrs · 27,135 cycles

AIRCRAFT WAS GROUNDED. COMPRESSOR STALL ON APPLICATION OF TAKEOFF POWER. ABORTED TAKEOFF BELOW 30 KNOTS. REMOVED AND REPLACED LEFT ENGINE. ACCOMPLISHED ENGINE RUN-UP IAW MCM 71-91-99. OPERATIONAL CHECK GOOD.

Part: LANYARD — DETACHED (EVAC SLIDE) · airframe 55,648 hrs · 27,128 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE HAS A CABLE PROTRUDING FROM SLIDE PACK. REATTACHED LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 55,643 hrs · 27,125 cycles

CEILING EMERGENCY EXIT LIGHTS AT ROWS 18-21 AND ROWS 28-30 FAILED TEST. REMOVED AND REPLACED TWO BATTERY ASSEMBLIES IAW AMM 33-53-00. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 55,643 hrs · 27,125 cycles

CEILING EMERGENCY EXIT LIGHTS IN ROWS 18-21 AND ROWS 28-30 FAILED TEST. REMOVED AND REPLACED TWO BATTERY ASSEMBLIES IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 55,643 hrs · 27,125 cycles

CEILING EMERGENCY EXIT LIGHTS AT ROWS 8-11, FAILED TEST. REMOVED AND REPLACED THE BATTERY ASSEMBLY B5-101 IAW AMM 33-53-00. OPS CHECKED GOOD. AIRCRAFT GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,643 hrs · 27,125 cycles

CEILING EMERGENCY EXIT LIGHT LEFT SIDE ROW 14 HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD.

Part: RELAY — FAULTY (ZONE 100) · airframe 55,542 hrs · 27,056 cycles

AIRCRAFT WAS NOT GROUNDED. FUEL ODOR IN THE CABIN AFTER THE APU STARTED. REMOVED AND REPLACED APU DOOR CLOSE RELAY. ACCOMPLISHED HIGH PRESSURE PNEUMATIC DUCTING BURNOUT. OPERATIONAL CHECK GOOD.

Part: ACCESS DOOR — MISSING (LT ENGINE) · airframe 55,256 hrs · 26,882 cycles

AIRCRAFT NOT GROUNDED. ON POSTFLIGHT, FIRST OFFICER DISCOVERED THE LEFT ENGINE STARTER ACCESS DOOR WAS MISSING. ACCOMPLISHED REPAIR OF ACCESS DOOR IAW AA REPAIR DOCUMENT 71-11-04-1. OPERATIONAL CHECK GOOD.

Part: WIRE — BURNED (LAVATORY) · airframe 53,500 hrs · 25,815 cycles

FOUND BURNT WIRES BEHIND LAVATORY MIRROR LIGHT ASSEMBLY. WIRES BURNT & SHORTED ON CORNER OF LIGHT ASSEMBLY. WIRE LAV129A22YE BURNT IN TWO PIECES. SPLICED WIRE LAV129A22YE IAW CHAP 20-10-03. NO DAMAGE FOUND TO OTHER WIRES IN BUNDLE. OPERATIONS CHECKED EPL ON LT AFT LAVATORY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01. LIGHTS, SIGNS & CALL OPERATIONS GOOD IAW AMM 33-23-00. THE ACFT WAS GNDED.

Part: ENGINE — FAILED (RIGHT) · airframe 53,224 hrs · 25,659 cycles

RIGHT ENG LOST OIL PRESS & QUANTITY DURING DESCENT. ENG SHUTDOWN. AN EMER WAS DECLARED. ENG WIND MILLED ABOUT 5 MINUTES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENG TIME WAS ABOUT 10 MINUTES. R & R RT ENG IAW MCM 71-91-99. THE ACFT WAS GNDED.

Part: BATTERY PACK — DISCHARGED (AC BAY) · airframe 52,267 hrs · 25,101 cycles

EMERGENCY LIGHTS IN TAIL COMPARTMENT OVER CATWALK FAIL TO TEST IAW WC 0801. REPLACED EMER LIGHT BATTERY PACK B5-28 IAW AMM 33-53-00. TESTED OK.

Part: SUPPORT FITTING — DAMAGED (LT WING) · airframe 50,471 hrs · 24,067 cycles

LEFT WING CANT TRAILING SUPPORT CLIP HOLES ARE ELONGATED. REPAIRED SUPPORT CLIP IAW SRM 51-30-10 & EA 57-038442.

Part: CASTING — CRACKED (LT SPOILER) · airframe 50,471 hrs · 24,067 cycles

LEFT WING GND SPOILER CASTING CRACKED AT FWD END ON INBD SIDE. R & R FITTING IAW AARD 51-00-05 & DWG SRO9570010.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,283 hrs · 23,958 cycles

EPL LIGHTS INOPERATIVE FROM ROW 21 - 31 USING BATTERY PACK MODULE AB5-3 ON TEST. R & R BATTERY FOR MODULE AB5-3. LIGHT OPERATIONS CHECKED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,283 hrs · 23,958 cycles

TAIL SECTION EMER LIGHTS OPERATED BY BATTERY PACK B5-28 ARE INOPERATIVE DURING TEST. R & R BATTERY PACK B5-28. SYS CHECKED NORMAL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 48,846 hrs · 23,214 cycles

NUMBER 2 AUTO CABIN PRESS CONTROLLER FAILED & THEN AFT GALLEY DOOR LIGHT ILLUMINATED ON ANNUNCIATOR PANEL. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 2 AUTO CABIN PRESS CONTROLLER. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: ACTUATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 48,739 hrs · 23,161 cycles

PRESSURIZATION PROBLEMS. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED OUTFLOW VLV ACTUATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,996 hrs · 22,789 cycles

EMERGENCY LIGHT NEXT TO LT NR 1 DOOR WOULD NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT NEXT TO LT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 47,339 hrs · 22,460 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 19D. OPERATIONS CHECKED NORMAL.

Part: CHECK VALVE — LEAKING (AC BAY) · airframe 46,940 hrs · 22,235 cycles

DFW TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES & LIGHT WENT OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEAKING GROUND AIR CONDITIONING CHECK VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SENSOR — MALFUNCTIONED (AC BAY) · airframe 46,933 hrs · 22,230 cycles

DFW MASTER WARNING WITH TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED QRH & LIGHT WENT OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH OVERTEMP SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

FORWARD KEEL BEAM LT & RT WEB CRACKED AT UPPER FORWARD ATTACH POINTS. REPAIRED FORWARD KEEL BEAM LT & RT INTERCOSTAL WEB AT UPPER ATTACH POINTS IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION ON LT CUSP FROM BS 1176 TO 1178. INSTALLED NEW LT SECTION OF CUSP SHEET FROM BS 1174 TO 1193 IAW 53-05-00 FIGURE 131A-23.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,876 hrs · 22,203 cycles

SEAT TRACK NR 6 FROM BS 218 TO 586 CORRODED. REPLACED SEAT TRACK IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

SEAT TRACK NUMBER 6 FROM BS 218 TO 586 CORRODED. REPLACED SECTION OF SEAT TRACK NR 6 IAW AMM 53-40-01-2 & AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CUSP UNDER NR 6 SEAT TRACK AT BS 218 CORRODED. INSTALLED NEW CUSP SHEET BETWEEN BS 218 TO 237 IAW AARD 53-20-00-16, SRM 51-30-05 & SRM 51-30-02.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,876 hrs · 22,203 cycles

FWD G-1 GALLEY FWD MID FLOOR MOUNT HAS CORROSION. INSTALLED NEW MID GALLEY MOUNT IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CABIN SUB FLOOR HAS CORROSION BETWEEN SEAT TRACKS 5 TO 6 FROM BS 200 TO 210. INSTALLED CUSP DOUBLER FROM BS 200 TO 219 IAW AARD 53-20-16, 51-30-05 & 51-30-02.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,876 hrs · 22,203 cycles

FWD G-1 GALLEY FORWARD OTBD FLOOR MOUNT CORRODED. INSTALLED NEW OTBD GALLEY MOUNT IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

SEAT TRACK NR 3 CORRODED FROM BS 1183 TO 1309. INSTALLED SEAT TRACK NR 3 FROM BS 1183 TO 1231 IAW AMM 53-40-01-2 & INSTALLED SPLICE FROM BS 1183 TO 1190 IAW SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

HEAVY CORROSION DAMAGE ON RT CUSP FROM BS 1060 TO 1066. ACCOMPLISHED CUSP REPAIR IAW AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION ON CABIN FLOOR AFT OF FLOORBEAM AT BS 60 & RBL 44 TO 46. INSTALLED SUBFLOOR DOUBLER FROM BS 160 TO 200 RT IAW AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION UNDER GALLEY ONE DRAIN PAN. INSTALLED SUBFLOOR DOUBLER UNDER GALLEY ONE DRAIN PAN IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,876 hrs · 22,203 cycles

CORROSION ON RT CUSP AT BS 857. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,876 hrs · 22,203 cycles

FWD CARGO LIGHT CORROSION ON BOTTOM SIDE OF RT CUSP FROM BS 375 TO 390. ACCOMPLISHED SUCP REPAIR IAW SRM 53-05-00 FIGURE 131A-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

SEAT TRACK NR 6 CORROSION FROM BS 1182 TO 1184. REMOVED CORROSION & INSTALLED SEAT TRACK PLUG IAW 53-05-00 FIGURE 4.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION ON SUB FLOOR UNDER G1 GALLEY OTBD & MID MOUNTS. INSTALLED DOUBLER & OVERLAY DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,876 hrs · 22,203 cycles

SEAT TRACK NR6 FROM BS 588 TO 797 CORRODED. REPLACED SEAT TRACK FROM BS 588 TO 797 IAW AARD 51-00-05-1.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION FOUND ON INTERNAL DOUBLER AT BS 1310 ABOVE LONGERON 22 LT. CUT OUT CORROSION & INSTALLED FLLER & TITANIUM DOUBLER IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION UNDER RT CUSP FROM BS 857 TO 861. INSTALLED DOUBLER ON RT CUSP IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION ON SEAT TRACK FROM BS 1058 TO 1059. INSTALLED PLUG DDK2704-7 & CHANNEL 7452952-7 IN SEAT TRACK NR 6 IAW AARD 53-20-00-10.

Part: SKIN — DAMAGED (LE SLAT) · airframe 46,876 hrs · 22,203 cycles

SLAT 19 INCHES FROM INBD END AT THE LE OF THE SKIN DAMAGED. CUT OUT DAMAGE & INSTALLED DOUBLER IAW SRM 57-09-00 FIGURE 10, SRM 57-01-00 FIGURE 1 SHEET 2 & EA MD80-57-014147.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION OUT OF LIMITS ON SEAT TRACK NR 4 FROM STATIONS 1275 TO 1277. INSTALLED SEAT TRACK & SPLICE IAW SRM 53-05-00 FIGURE 4F & AMM 53-40-01-2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

VAULT DOOR STIFFENER ON LT HAND SIDE OF DOOR JAMB IS CRACKED. INSTALLED NEW STIFFENER IAW SRM 51-30-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CORROSION BEYOND LIMITS AT SEAT TRACK NR 1 FROM STATIONS 300 TO 303. ALODINED & PRIMED IAW SRM 51-10-3. INSTALLED PLUG DDK2704-7 & CHANNEL 7452952-7 IAW AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

WINDOW RING PAN HAD CRACK AT STATION 1022, LT HAND AFT UPPER CORNER CLIP. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CRACK AT LT HAND WINDOW PAN LOWER AFT CLIP, STATION 905. INSTALLED WINDOW RING PAN CLIP REPAIR IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CRACK AT LT HAND WINDOW PAN UPPER AFT CLIP, STATION 1041. INSTALLED REPAIR DOUBLER & SHIM IAW AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,876 hrs · 22,203 cycles

CRACK AT LT HAND WINDOW PAN UPPER AFT CLIP, STATION 1060. INSTALLED REPAIR DOUBLER & SHIM IAW AARD 53-10-00-25.

Part: LENS — MISSING (CABIN) · airframe 46,598 hrs · 22,047 cycles

EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,598 hrs · 22,047 cycles

EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 5E. OPERATIONS CHECKED NORMAL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 44,207 hrs · 20,833 cycles

ROW 24DEF EMERGENCY AISLE LIGHT INOPERATIVE. REPLACED HARNESS FOR ROW 24DEF EMERGENCY AISLE LIGHT. OPS CHECK NORMAL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 44,207 hrs · 20,833 cycles

FOUND ROW 5 EMERGENCY AISLE LIGHT HARNESS AND SPLICE BAD. REPLACED SPLICE FOR ROW 5 EMERGENCY AISLE LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (AC BAY) · airframe 44,207 hrs · 20,833 cycles

TAILCONE EMERGENCY LIGHTS INOPERATIVE AT CENTER WALKWAY. REPLACED BATTERY PACK FOR TAILCONE EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 42,774 hrs · 20,131 cycles

LEFT AND RIGHT FORWARD OVERWING UPPER EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,756 hrs · 18,083 cycles

AFT SIDE OF FRAME 1418 IS CRACKED NEXT TO RADIUS BLOCK AT LONGERON 2 RIGHT. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,756 hrs · 18,083 cycles

FORWARD SIDE OF FRAME 1418 IS CRACKED NEXT TO RADIUS BLOCK AT LONGERON 2 RIGHT. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,756 hrs · 18,083 cycles

LONGERON 2 LEFT IS CRACKED ON AFT SIDE OF FRAME NUMBER 1418. REPAIRED LONGERON PER EA MD 80 -53-014152.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

INTERCOSTAL CRACKED, SUB FLOOR CENTERLINE STATION 1271 TO 1287. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

AFT CARGO, INTERCOSTAL BELOW CABIN FLOOR, ON CENTERLINE STATION 1297 TO 1309 CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-05 AND 51-30-2.

Part: SKIN — CORRODED (BS 1108) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

EXTERNAL SKIN CORROSION AT STATION 1108, LONGERON 28R. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIGURE 5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

TWO CRACKS ON CANT FRAME 1463, ONE INBOARD OF LONGERON 3L AND ONE OUTBOARD OF LONGERON 3R. REPAIRED CRACKS PER EA MD-80-53-006604 AND EA MD-80-53-006618.

Part: TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

TIE DOWN TRACK AT STRINGER 30 CORRODED. REPLACED TIE DOWN TRACK PER SRM 51-30-05.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

MISDRILLED HOLE IN MOUNT FOR NR 1 SEAT TRACK. REAMED OUT DAMAGED HOLE AND INSTALLED BUSHING PER EA MD80-53-006637.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

CORROSION ON SHEAR TIE STATION 1287, LONGERON 28 LEFT TO 28 RIGHT. REMOVED AND REPLACED SHEAR TIE FROM LONGERON 26 RIGHT TO 26 LEFT PER SRM 51-30-2, 51-30-05. MRT 021564.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

CORROSION AFT SIDE OF FRAME 1309, LONGERON 28L TO 28R. INSTALLED NEW SECTION OF FRAME FROM LONGERON 26L TO 26R AND PERFORMED SPLICE REPAIRS PER SRM 53-30-00, 51-30-05, AND 51-30-02, TREATED AND PAINTED PER SRM 51-10-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

CORROSION AT STATION 1170 - 1174 ON SEAT TRACK NR 1. INSTALLED NEW SEAT TRACK AT STATION 1170 - 1309 PER SRM 51-30-01.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

NR 32 WINDOW RING PAN AND RING CRACKED AT 12:00 POSITION, LEFT HAND SIDE, STATION788. (TOOL DAMAGE) REPLACED LEFT HAND WINDOW PAN.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

HOLE IN CUSP AT STATION 1212 ON LEFT SIDE AT AREA OF NUMBER 1 SEAT TRACK MOUNT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — DAMAGED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

WINDOW RING PAN BENT AT 12:00 POSITION, LEFT SIDE, WINDOW NUMBER 33, STATION 807. REPLACED WINDOW RING PAN.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

NR 32 WINDOW RING PAN AND RING CRACKED AT 12:00 POSITION, LEFT HAND SIDE, STATION788. (TOOL DAMAGE) REPLACED LEFT HAND WINDOW RING.

Part: DOUBLER — GOUGED (ENTRY DOOR) · airframe 34,593 hrs · 16,222 cycles

CABIN AFT ENTRY DOOR SKIN GOUGED AFT SIDE AT BOTTOM MARKED. REPAIRED DOUBLER UNDER SRM 53-04 FIGURE 38.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

TOOLING MARK IN SKIN BETWEEN LONGERON 25L-26L. BLENDED DAMAGE, INSTALLED DOUBLER PER SRM 53-04 FIGURE 38 SHEET 20.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

CORROSION ON LONGERON 30. REMOVED DAMAGED LONGERON, SPLICED IN NEW SECTION PER SRM 53-02 FIGURE 18.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

CORROSION ON AFT CARGO DOOR CUTOUT BEAM STATION 1155-1212. INSTALLED AFT CARGO DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

OUTBOARD FLOORBOARD SUPPORT AT STATION 150, UNDER FLOORBOARD FC-11 AND INBOARD EDGE OF G-1 GALLEY DRAIN PAN, IS CORRODED. REPLACED FLOORBOARD SUPPORT, INBOARD OF NR 1 GALLEY DRAIN PAN PER SRM 51-30-02.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

SUBFLOOR CORRODED INBOARD OF FORWARD SERVICE DOOR, STATION 160-200 UNDER HAT CHANNEL. CORROSION REMOVED AND AREA REPAIRED PER AARD 53-20-00-16 AND EA MD80-53-006595.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,593 hrs · 16,222 cycles

FORWARD CARGO DOOR CRACKED. REMOVED AND REPLACED FORWARD CARGO DOOR FITTING NR 4 PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

APPROXIMATE .25 INCH CRACK IN UPPER AFT CORNER OF WINDOW PAN BETWEEN LEFT STATION 1060-1079. ROUTED OUT CRACK, INSTALLED DOUBLER AT UPPER AFT CORNER OF WINDOW PAN, LEFT STATION 1060-1079 PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,593 hrs · 16,222 cycles

CARGO DOOR CRACKED. REMOVED AND REPLACED CARGO DOOR STOP FITTING PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

LOWER FORWARD CORNER OF WINDOW PAN CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

CRACK IN UPPER FORWARD CORNER OF WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

LOWER AFT CORNER OF WINDOW PAN CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

CORROSION ON LEFT CUSP. INSTALL CUSP REPAIR PER AARD53-20-00-16.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

NR 3 SEAT TRACK WORN BEYOND LIMITS STATION 1089-1176. SPLICED IN SERVICEABLE SECTION OF SEAT TRACK STATION 1089-1176 PER SRM 51-01.

Part: VANE — DEBONDED (TE FLAP) · airframe 34,593 hrs · 16,222 cycles

RIGHT WING FLAP-VANE BELOW GROUND-SPOILER HAS DISBONDING AT RUBSTRIP. REMOVED RUBSTRIP AND REPLACED DAMAGED CORE AND FABRICATED AND INSTALLED DOUBLERS WITH HOY-BOND PER SRM 57-04-00.

Part: STOP FITTING — CRACKED (DOOR) · airframe 34,593 hrs · 16,222 cycles

DOOR STOP CRACKED. REPLACED DOOR STOP IN ACCORDANCE WITH ESO 80174.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

NR 6 SEAT TRACK CORROSION REMOVAL OUT OF LIMITS AT STATION 709. ROUTED OUT DAMAGE, INSTALLED PLUG REPAIR PER SRM 53-05 FIGURE 4A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,593 hrs · 16,222 cycles

FLOORBOARD SUPPORT IS CORRODED BEYOND LIMITS JUST INBOARD OF NR 4 SEAT TRACK. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 53-10.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

WEB IS CRACKED FOWARD END OF LONGERON 15 LEFT STATION 210. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,593 hrs · 16,222 cycles

WEB IS CRACKED FORWARD END OF LONGERON 10 LEFT STATION 210. INSTALLED DOUBLER PER 53-10-00-11.

Part: APU — LEAKING (APU BAY) · 32,526 cycles

INFLIGHT T4XG/24SEP CREW REPORTED NOXIOUS FUMES IN CABIN AND COCKPIT. COCKPIT CREW USED OXYGEN MASKS. RETURNED TO MCI AND LANDED WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT (APU) AND PERFORMED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 6 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 6 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 20 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 20 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT CENTER ROW BY FORWARD LAVATORY FAILED TEST. REPLACED BATTERY PACK AT CENTER ROW BY FORWARD LAVATORY FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 29 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 29 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 20 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 20 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 25 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 25 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,295 hrs · 14,801 cycles

TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 13 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 13 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (TURBINE TEMP)

STL INFLIGHT T4XG/07OCT - TAIL COMPARTMENT TEMPERATURE LIGHT ILLUMINATED. SHUT OFF LEFT AIR CONDITIONING PACK AND LIGHT WENT OUT AFTER TWO MINUTES. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED TURBINE INLET TEMPERATURE SWITCH AND COMPRESSOR DISCHARGE SWITCH AND LEFT AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS CAME ON WHEN SELECTED OFF. CIRCUIT BREAKER Z37 POPPED. FOUND SHORTED WIRE ON BATTERY PACK B5105. REPOSITIONED AND SECURED WIRE ON BATTERY PACK B5105 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED. NORMAL OPERATION.

Part: PIN — LOOSE (CONNECTOR)

MSP - EMERGENCY LIGHT ON INBOARD EDGE OF SEAT 18D HAS LOOSE WIRE PIN AT PLUG. REINSERTED PIN INTO RECEPTICAL FOR EMERGENCY LIGHT ON INBOARD EDGE OF SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HARNESS · airframe 15,664 hrs · 7,946 cycles

DURING OVERNIGHT INSPECTION ROW 21 FLOOR PATH LIGHTING INOP. REPLACED BROKEN HARNESS 105606-003 CPN 4096971 BETWEEN ROW 22 AND 23. OPS CHECK NORMAL PER MD80 MM33-53-01. CHECK-C STL 10-19-02. --CLOSED--

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,567 hrs · 7,884 cycles

CEILING EMERGENCY LIGHTS WERE INOPERATIVE ROWS 27 TO AFT END OF CABIN, ABOVE AFT FLT ATTEND SEAT, FWD OF RT AFT LAV, AND TWO CEILING LIGHTS ABOVE THE L2 FLIGHT ATTEND POSITION. REPLACED POWER SUPPLY BATTERIES FOR ROW 27 TO AFT DOOR AND FOR FORWARD OF THE RT AFT LAV. REPLACED BULBS FOR OTHER CEILING EMERGENCY LIGHTS.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 15,567 hrs · 7,884 cycles

THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 6 TO 15, ROWS 20 THRU 23, ROWS 26 THRU 30, AND MOST AFT POSITION IN TAIL CONE. REPLACED LAMPS PN 7732 FOR ROW 6 TO 15, ROW 20 TO 23, AND ROW 26 THRU 30. REPLACED BATTERIES IN POWER SUPPLY FOR TAIL CONE EMERGENCY LIGHT, PN 408822-101. CHECK-C 10-19-02 STL.

Part: COALESCER BAG — CONTAMINATED (AC PACK) · airframe 14,163 hrs · 7,047 cycles

SMOKE WAS PRESENT IN CABIN AFTER STARTING APU. CHECKED WATER SEPARATORS AND PERFORMED MD9-49-06 MAINTENANCE SHEET. LAST CHECK C PERFORMED 10/25/2001 AT MCI. --CLOSED--

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 12,351 hrs · 5,976 cycles

DURING CHECK-C MAINT FOUND CRACK BETWEEN 2 FASTENERS AT ATTACH ANGLE FROM FUSELAGE TO VERTICAL STABILIZER, 7 INCHES FROM AFT END OF THE STABILIZER AT RT SIDE. STOP DRILLED SMALL CRACK PER SRM 53-05, FIG 23. ACCOMP HIGH FREQ EDDY CURRENT PER NDT 51-00-03. CHECKED STOP DRILL. INSTALLED DOUBLER PER SRM 53-05 FIG 23. INSTALLED HI-LOKS PER SRM 51-30-5.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,319 hrs · 5,478 cycles

THE THREE AFT CABIN EMERGENCY FLASHLIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN EACH. CHECK-C 11-5-00 STL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,860 hrs · 4,818 cycles

THE EMERGENCY EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 12 TO 21. REPLACED THE BATTERY IN THE POWER SUPPLY. CHECK-C 11-5-00 STL.

Part: LIGHT — INOPERATIVE (ROW 2 & 3) · airframe 8,896 hrs · 4,344 cycles

THE EMERGENCY LIGHT IN THE FIRST CLASS AND FWD GALLEY WERE INOPERATIVE. REPLACED THE WIRE JUMPER BETWEEN ROWS 2 AND 3. CHECK-C 10-2-99 STL.

Part: SWITCH — WORN (COCKPIT)

THE CABIN EMERGENCY LIGHTS WOULD NOT OPERATE FROM THE COCKPIT SWITCH. REPLACED THE S1-177 COCKPIT SWITCH, (P/N 4TL11-10B) AND THE BATTERY PACK AT CABIN ROW 50, (P/N 60030451LB). CHECK-C 10-26-98 STL.

Part: TIP — DAMAGED (RT WING)

THE RT WING TIP AND TIP TRAILING EDGE WERE DAMAGED WHEN STRUCK ON THE GROUND. REPLACED WING TIP ASSY AND INSTALLED NEW TRAILING EDGE, PER SRM 51-30-1 AND STANDARD MAINT PRACTICES.

Part: RIB — DAMAGED (WS 610)

DURING MAINT, FOUND RT WING RIB DAMAGED AT SLAT TRACK OPENING XOS=610, IDLER TRACK NR 15. REMOVED AND REPLACED RIBS PER SRM 51-20-2, 51-30-5, AND 51-30-8, AND STANDARD MAINTENANCE PRACTICES.

Part: VALVE — FAILED (RT PACK)

JFK - FLT 763 - RIGHT AIR CONDITIONER PACK FAILED AFTER TAKEOFF. THIRTY-FIVE MINUTES AFTER TAKEOFF, PACK VALVE OPENED TO 10 PSI. SIX MINUTES LATER, VALVE OPENED COMPLETELY. PACK THEN FAILED ON LANDING. REPLACED AIR PRESSURE REGULATOR VALVE P/N 293-0033. OP-15. 10-01-97. NEW. (X)