N7550

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 76,285 hrs · 40,527 cycles

FIRST OFFICERS WINDSHIELD IS DELAMINATED AT THE BOTTOM, MEASURING APPROXIMATELY 2.75 INCHES FROM BOTTOM OF THE WINDSHIELD OUTER GLASS PLY. NOT ACCEPTABLE, AREA GREATER THAN 075 INCH OF DELAMINATION. GREATER THAN ALLOWED. REMOVED AND REPLACED, AND OPS CHECKED GOOD. OK FOR SERVICE FOR THE FOS WINDOW CHANGE IAW AMM 56-10-02. THE AIRCRAFT WAS GROUNDED.

Part: CSD — LOW PRESSURE (RIGHT) · airframe 76,195 hrs · 40,456 cycles

DURING CRUISE, RIGHT CONSTANT SPEED DRIVE OIL PRESSURE LOW LIGHT AND RIGHT GENERATOR OFF LIGHT CAME ON. DISCONNECTED CONSTANT SPEED DRIVE IAW QUICK REFERENCE HANDBOOK AND DIVERTED. MAINTENANCE REPLACED THE RIGHT ENGINE CONSTANT SPEED DRIVE AND GENERATOR IAW AMM 24-10-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: GENERATOR — LOW PRESSURE (RIGHT) · airframe 76,195 hrs · 40,456 cycles

DURING CRUISE, RIGHT CONSTANT SPEED DRIVE OIL PRESSURE LOW LIGHT AND RIGHT GENERATOR OFF LIGHT CAME ON. DISCONNECTED CONSTANT SPEED DRIVE IAW QUICK REFERENCE HANDBOOK AND DIVERTED. MAINTENANCE REPLACED THE RIGHT ENGINE CONSTANT SPEED DRIVE AND GENERATOR IAW AMM 24-10-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED

Part: ATTACH BRACKET — BROKEN (R1 DOOR SLIDE) · airframe 75,247 hrs · 39,849 cycles

R1 DOOR SLIDE BUSTLE ATTACH BRACKET IS BROKEN. REMOVED AND REPLACED THE TWO BRACKETS IAW 30-10-15. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: ATTACH BRACKET — BROKEN (R1 DOOR SLIDE) · airframe 75,247 hrs · 39,849 cycles

R1 DOOR SLIDE BUSTLE ATTACH BRACKET IS LOOSE OR BROKEN. REMOVED AND REPLACED THE TWO BRACKETS SRM 30-10-15. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: FRAME — WORN (BS 1510) · airframe 75,222 hrs · 39,830 cycles

WORN AREA ON AFT ACCESSORY LEFT CANTED FRAME AT BS 1510, BETWEEN LONGERONS 25 - 27L, LOWER AFT SURFACE AT THE 7 OCLOCK POSITION DUE TO TAIL CONE RUBBING. REPAIRED THE FRAME IAW SRM 53-01-00-001, AND EA 273968.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,097 hrs · 39,736 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK INDICATIONS ON LONGERON 24L AT FUSELAGE STATION 200 FRAME ATTACHMENT POINT. REPAIRED LONGERON PER SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,097 hrs · 39,736 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK INDICATIONS ON LONGERON 23L AT FUSELAGE STATION 200. REPAIRED LONGERON PER SRM 53-02-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,656 hrs · 39,459 cycles

THE AIRCRAFT WAS NOT GROUNDED. WITH A/C POWER OFF THE AFT INTERIOR EMERGENCY LIGHTS STAY ON. REMOVED AND REPLACED BATTERY PAC PER MM 33-53-00. PAC B5-27. OPS CHECK NORMAL.

Part: CSD — FAILED (LT ENGINE) · airframe 74,493 hrs · 39,355 cycles

THE AIRCRAFT WAS GROUNDED. LT CSD OIL PRESSURE LIGHT CAME ON WITH A CSD OVER TEMP INDICATION. THE CREW DISCONNECTED THE LT CSD, BUT THE AC VOLTS STAYED ON AFTER DISCONNECTION. THE SECOND ATTEMPT TO DISCONNECT THE CSD RESULTED IN ZERO VOLTS AND FREQUENCY. ADDITIONALLY, A LT ENG B LOOP FIRE WARNING LIGHT ILLUMINATED. THERE WAS NO ACCOMPANYING AURAL WARNING. THE CREW DECLARED AN EMERGENCY AND RETURNED TO SLC WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NO OIL IN THE LT CSD. MAINTENANCE REPLACED THE LT CSD IAW AMM 24-10-01. ALSO, DUE THE FAILURE OF THE CSD, REPLACED THE LT AC GENERATOR IAW AMM 24-20-01 AND THE LT CSD OIL COOLER IAW AMM 24-20-03. LEAK AND OPERATIONS CHECKED OK. LT CSD OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,789 hrs · 38,891 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST CLASS CEILING EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY AT ROW 6 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,789 hrs · 38,891 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN RIGHT AFT OVERWING FAILED TEST. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK AB5-3 (AALA20170301005) IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,789 hrs · 38,891 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS ROW 21-26 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY AT ROW 25 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,789 hrs · 38,891 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN RIGHT AFT OVERWING FAILED TEST. REMOVED AND REPLACED POWER SUPPLY (AALA20170227021) AND BATTERY PACK AB5-3 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,789 hrs · 38,891 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHTS ON THE LEFT AND RIGHT AFT OVERWING EXITS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY AT ROW 21 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: PRESSURE SWITCH — FAULTY (ENGINE OIL) · airframe 73,633 hrs · 38,789 cycles

DURING APPROACH, CREW REPORTED THE LEFT ENGINE OIL FILTER CLOGGED LIGHT ILLUMINATED. THE LEFT ENGINE WOULD NOT GO BEYOND IDLE POWER. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED AND REPLACED OIL DIFFERENTIAL PRESSURE SWITCH IAW AMM 79-35-01. LEAK AND OPERATIONAL CHECK GOOD.

Part: BATTERY — FAULTY (CABIN) · airframe 73,590 hrs · 38,759 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT IN THE MID GALLEY WAS ON WHEN THE AIRCRAFT WAS SHUTDOWN. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 73,576 hrs · 38,745 cycles

AIRCRAFT NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE LANYARD IS DISLOCATED. SECURED LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: SLIDE — DETACHED (L2 DOOR) · airframe 73,522 hrs · 38,707 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE DETACHED AND ON FLOOR. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED SLIDE IAW AM 25-62-00. OPERATIONAL CHECK GOOD.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,211 hrs · 37,888 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR BOTTOM FORWARD STOP PAD FITTING IS CRACKED. R & R FITTING IAW DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,211 hrs · 37,888 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR 3RD FROM TOP FORWARD STOP PAD FITTING IS CRACKED. R & R FITTING IAW DWG 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,211 hrs · 37,888 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR TOP AFT STOP PAD FITTING IS CRACKED. R & R FITTING IAW DWG 5910141.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 72,211 hrs · 37,888 cycles

ACFT WAS IN BASE MAINTENANCE. OTBD AFT CORNER OF L20R AT FUSELAGE STA 1303 WAS REMOVED AROUND A FASTENER WITH NO REINFORCING REPAIR ACCOMPLISHED. REPAIRED LONGERON IAW 53-10-00-18 AND EA 261696.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,211 hrs · 37,888 cycles

FORWARD CARGO DOOR STOP CRACKED, BOTTOM AFT STOP, INSTALLED FORWARD CARGO BOTTOM AFT STOP PAD FITTING IAW DWG 5910141 AND CDK2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 72,211 hrs · 37,888 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR TOP FORWARD STOP PAD FITTING IS CRACKED. R & R FITTING IAW DWG 5910141.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,211 hrs · 37,888 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FUSELAGE SKIN IS CRACKED AT FRAME 1474 AND L22R. REPAIRED SKIN IAW SRM 53-01-00 AND 53-30-00-03.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,757 hrs · 37,024 cycles

REFERENCE WORK CARD 5403. EGRESS POWER SUPPLY AB5-3 FAILED TEST. REPLACED AB5-3 EGRESS LIGHT POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. TESTED OK. THE ACFT WAS NOT GNDED.

Part: SWITCH — FAULTY (ZONE 400) · airframe 70,294 hrs · 36,753 cycles

RIGHT ENG OIL STRAINER CLOGGING LIGHT CAME ON DURING DEPARTURE. CREW RAN THE CHECKLIST, DECLARED AN EMER & RETURNED TO FIELD. DURING THE RETURN, THE RT ENG WAS SHUT DOWN. REPLACED CLOG LIGHT SWITCH.

Part: LENS — BROKEN (ZONE 200) · airframe 69,917 hrs · 36,530 cycles

EMERGENCY TAIL CONE HANDLE LIGHT ASSEMBLY LENS BROKEN. R & R TAIL CONE HANDLE LIGHT ASSEMBLY IAW AMM 33-53-00 & WDM 33-51-15. PERFORMED OPERATIONAL CHECK, SYS CHECKED NORMAL.

Part: DOOR — MALFUNCTIONED (NLG) · airframe 69,091 hrs · 36,034 cycles

NOSE GEAR DOORS DID NOT CLOSE PROPERLY AFTER TAKEOFF. NO EMERGENCY DECLARED & LANDING UNEVENTFUL. PERFORMED NOSE GEAR SWING TO VERIFY PROPER OPERATION IAW MCC 32-96-14 NOSE GEAR WITH NORMAL OPERATIONS.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

RIGHT CUSP T ANGLE CORRODED BETWEEN FS 180 & 227. R & R ANGLE IAW SRM 53-30-05, SRM 53-05-00, SRM 51-10-03, SRM 51-30-05 & AMM 20-10-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

CABIN SEAT TRACK NR 5 HAS CORROSION FROM FS 210 TO 256 ON OTBD FLANGE. REPAIRED SEAT TRACK IAW SRM 53-05-00-4F.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CRACK IN STATION 1338 BULKHEAD STIFFENER UPPER END FWD SIDE ABOVE VAULT DOOR JAMB CTR AREA. R & R STIFFENER IAW SRM 51-30-05 & 51-60-00 5 B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

NUMBER 6 SEAT TRACK CORRODED FROM FS 215 TO 285. R & R SEAT TRACK SECTION IAW SRM 53-05-00-001 FIG 4F.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

NUMBER 2 GALLEY MOUNT AT FWD END OF NR 6 SEAT TRACK IS CORRODED. R & R GALLEY MOUNT IAW AARD 51-00-05-1 & DWG 5930547.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 68,376 hrs · 35,635 cycles

FORWARD ENTRY DOOR BEAM, NR 8 BEAM IS CRACKED AT FWD END. R & R BEAM IAW AARD 51-00-05 REPAIR 1 EA COMP-52-038127 DATE 01/14/2015 & DWG 5910081.

Part: DIAPHRAGM — DAMAGED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

SEVERAL RIVETS PULLED THROUGH DIAPHRAGM SHEET ON RT OF ELECTRONICS BAY BETWEEN FS 195 & 200 ABOVE PNEUMATIC DUCT. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

SUBFLOOR CRACKED AT FS 218, 3 INCHES OTBD OF NR 4 SEAT TRACK. INSTALLED REPAIR DOUBLERS IAW AARD 53-20-00-16.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

LONGERON 29 LT IS CORRODED AT FS 1287. SPLICE REPAIR INSTALLED IAW SRM 53-02-00-001 FIG 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CORROSION ON RT DIAPHRAGM DOUBLER CUSP SHEET BETWEEN STATIONS 200 & 218. INSTALLED CUSP SHEET BETWEEN STATIONS 200 & 218 IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

CORROSION ON RT CUSP BETWEEN STATIONS 218 - 235 OUT OF LIMITS. REPLACED CUSP SHEET IAW AARD 51-00-05-01 & DWG 9930538.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

RIGHT CUSP SHEET CORRODED BETWEEN FS 788 & 807. REMOVED & INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

LEFT CUSP CRACKED AT FS 241. INSTALLED CUSP DOUBLER IAW AARM 63-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CRACK IN CUSP UNDER HORSESHOE COLLAR AT FRAME STATION 845 LT SIDE. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: FORMER — CRACKED (LE SLAT) · airframe 68,376 hrs · 35,635 cycles

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

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

TAIL VERTICAL STABILIZER HAS CRACKED DOUBLER ON RT FUSELAGE TO VERTICAL STABILIZER SKATE ANGLE AT CANT FRAME 1463. R & R ANGLE DOUBLER IAW AARD 51-00-05-01.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT Z CHANNEL IS CORRODED BETWEEN FS 1155 & 1136 AT LONGERON 25 RT. R & R CHANNEL IAW IPC 25-52-00-03L & SRM 51-30-01.

Part: STIFFENER — CRACKED (RT WING) · airframe 68,376 hrs · 35,635 cycles

RIGHT UPPER WING STIFFENER ANGLE CRACKED IN VENT TANK ACCESS 1440C BETWEEN XW 486 & XW 536. R & R STIFFENER ON RT UPPER WING VENT TANK ACCESS 1440C BETWEEN XW 486 & XW 536.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 68,376 hrs · 35,635 cycles

RIGHT FWD TIE DOWN TRACK IN AFT CARGO CORRODED BETWEEN STATIONS 1136 & 1155 ABOVE, LONGERON 27R. INSTALLED NEW TIE DOWN TRACK IAW SRM 51-30-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

DENTS AT STATION 339 ABOVE & BELOW L 24L. INSTALLED DOUBLER IAW SRM 53-04-02 FIG 2 SHEET 2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 68,376 hrs · 35,635 cycles

AFT CARGO RT TIE DOWN TRACK HAS CORROSION IN SEVERAL AREAS BETWEEN STATION 1212 TO 1231. R & R TIE DOWN TRACK IAW SRM 51-30-01.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

STATION 180 FLOORBEAM INTERCOSTAL ANGLE CRACKED 11 INCHES LT OF CTR LINE. INSTALLED NEW BRACKET IAW SRM 53-14-01-001 & DWG 9923484.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

DENT AT STATION 324 BETWEEN L 24L & L 25L. INSTALLED DOUBLER IAW SRM 53-04-02 FIG 2 SHEET 2.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CABIN SIDEWALL TOP FWD TAB CRACKED ON WINDOW PAN BETWEEN RT OVERWING EXITS. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CRACK IN VERTICAL SUPPORT AT FS 927. REMOVED CRACKED VERTICAL SUPPORT & INSTALLED SERVICEABLE VERTICAL SUPPORT IAW AARD 51-00-05-1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CRACKED STIFFENER ABOVE AFT BULKHEAD DOOR STATION 1338. REMOVED DAMAGED STIFFENER & INSTALLED NEW STIFFENER IAW SRM 51-30-05, SRM 51-60-00 5 B & AMM 20-15-2.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

CABIN SIDEWALL LOWER AFT TAB CRACKED ON WINDOW PAN BETWEEN RT OVERWING EXITS. REPAIRED IAW 53-10-00-25.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 68,376 hrs · 35,635 cycles

RIGHT WING INBD FLAP LOWER SKIN PUNCTURED AT INBD END. REPAIRED SKIN IAW SRM 57-03-00 FIG 8.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

DAMAGE TO AFT LOWER RT CUSP AT FS 237. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

SEAT TRACK NR 6, FROM FS 403 TO 406, IS CORRODED OUT OF LIMITS IAW SRM 53-05-00 FIGURE 4B-1. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10 & SRM 53-05 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

SEAT TRACK NR 6, FROM FS 322 TO 326, IS CORRODED OUT OF LIMITS IAW SRM 53-05-00 FIGURE 4B-1. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10 & SRM 53-05 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,376 hrs · 35,635 cycles

SEAT TRACK NR 6, FROM FS 362 TO 367, IS CORRODED OUT OF LIMITS IAW SRM 53-05-00 FIGURE 4B-1. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10 & SRM 53-05 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,376 hrs · 35,635 cycles

SEAT TRACK NR 6, FROM FS 304 TO 306, IS CORRODED OUT OF LIMITS IAW SRM 53-05-00 FIGURE 4B-1. ACCOMPLISHED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10 & SRM 53-05 FIGURE 4A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,648 hrs · 34,629 cycles

CENTER CABIN EMERGENCY LIGHTS CAME ON AFTER POWER SHUT DOWN. REPLACED BATTERY PACK B5-106, OPERATIONS CHECKED NORMAL.

Part: TARGET — FAULTY (LANDING GEAR) · airframe 65,283 hrs · 33,858 cycles

PDX LANDING GEAR DOOR LIGHT INDICATION. EMERGENCY DECLARED FLIGHT LANDED PDX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DOOR OPEN PROXIMITY SENSOR TARGET & TWO BRACKETS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CASTING — CRACKED (LE SLAT) · airframe 64,982 hrs · 33,673 cycles

LT WING LE CASTING AT NR 4 SLAT TRACK, INBD SIDE, AFT OF REAR LUG IS CRACKED. REPLACED LT WING LE CASTING IAW AARD 51-00-05-1.

Part: FILLER — CRACKED (FUSELAGE) · airframe 64,982 hrs · 33,673 cycles

AFT ACCESSORY 1463 CANT FRAME & INBD OF LONGERON 3 RT, FRAME TO SKIN FILLER CRACKED. INSTALLED INTERNAL & EXTERNAL DOUBLERS IAW EA MD80-53-031349.

Part: COVER — LOOSE (CABIN) · airframe 63,430 hrs · 32,768 cycles

EMERGENCY ESCAPE PATH LIGHT HOLDER AT 25D LOOSE. RE-ATTACHED 25D SIDE COVER. OPS CHECK NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 63,273 hrs · 32,679 cycles

PORTABLE EMERGENCY LIGHT BY LEFT NUMBER 1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSMEBLY BY LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,145 hrs · 32,044 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 28 INOPERATIVE. RESEATED BATTERIES AND REPLACED LAMPS. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

FRAME 1451 IS CRACKED ON FORWARD SIDE NEXT TO LONGERON 3 LEFT. INSTALLED REPAIR PER EA MD80-53-013194 AND SRM 51-70-05 FIGURE 1 ON FRAME 1451 FORWARD SIDE NEXT TO LONGERON 3 LEFT SIDE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

FUSELAGE - TEMPORARY DOUBLER REPAIR, UPPER AFT LEFT SIDE OF FUSELAGE SKIN, JUST AFT OF LEFT LOUVER BOX. REMOVED TEMPORARY AND INSTALLED PERMANENT REPAIR DOUBLER PER EA MD80-53-013210 AND SRM 53-01-00. REMOVED AND REPLACED INTERCOSTAL DUE TO TOOLING MARKS BEHIND DOUBLER PER EA MD80-51-013081, EA MD80-53-013256 AND SRM 51-10-04 LEFT FUSE UPPER AFT SIDE, JUST AFT OF LOUVER BOX.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

THERE IS A 5/16 INCH CRACK ON THE RIGHT BOTTOM OF FRAME 1497 AT RUDDER ACTUATOR INTERCOSTAL. INTERIM REPAIR ACCOMPLISHED PER ESO 80559 DATED 30JAN08. REINSPECT AT NEXT LIGHT C CHECK TO ENSURE NO CRACK PROPAGATION. INSTALLED PERMANENT REPAIR PER EA MD80-53-013098 DATED 9-22-2010.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

CORROSION ON TIE-DOWN TRACK SPLICE LEFT HAND SIDE AT STATION 1220. INSTALLED NEW TIE-DOWN SPLICE AT STATION 1220 PER SRM 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

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

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

CUSP T UPPER SPLICE ANGLE AT LEFT SIDE APPROXIMATE STATION 1088. HOLES DON"T LINE UP DUE TO DOUBLER IN SAME AREA. INSTALLED NEW CUSP T SPLICE PER SRM 51-01-00, SRM 51-30-05 AND EA MD80-51-013081.

Part: TEE FITTING — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION IN FRAME FOOT FORWARD SIDE OF STATION 200 JUST AFT OF FORWARD SERVICE DOOR CUTOUT (MARKED). INSTALLED CUSP TEE AT STATION 200 PER SRM 51-30-0 SATISFY THE DISCREPANCY PER SRM 51-30-05 AND ATTACHED EA MD80-51-013081.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

AFT CARGO CORROSION ON LEFT TIE DOWN TRACK EARS STATIONS 1225 TO 1250. MKD - INSTALLED NEW LEFT AFT TIE DOWN TRACK STATIONS 1220 TO 1322 PER SRM 51-30-01.

Part: TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

HEAVY CARGO/AFT - CORROSION ON TIE DOWN TRACK RIGHT SIDE STATIONS 1007 TO 1155. REMOVED AND REPLACED TRACK PER SRM 51-30-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

LEFT CUSP CRACKED AT STATION 1086. ROUTED OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION ON SUBFLOOR AT G-2 AFT INBOARD MOUNT STATION 218. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

AFT CARGO CORROSION ON TIE DOWN TRACK LEFT SIDE STATIONS 1007 TO 1220. REMOVED AND REPLACED TRACK PER SRM 51-30-01.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION ON G-2 AFT INBOARD MOUNT FITTING. REPLACED MOUNT FITTING PER SRM 51-30-05.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

AFT CARGO CORROSION ON DOOR CUTOUT LOWER FORWARD FITTING. INSTALLED NEW FITTING PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION UNDER FORWARD GIRT BAR BRACKET AT AFT SERVICE DOOR STATIONS 1142 TO 1143. INSTALLED CUSP REPAIR DOUBLER AT FORWARD GIRT BAR BRACKET AT AFT SERVICE DOOR STATIONS 1142 TO 1143 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION RIGHT CUSP STATIONS 1142 TO 1147. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION ON BOTTOM RIGHT CUSP STATION 1174. INSTALLED CUSP REPAIR FROM STATIONS 1170 TO 1197 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION UNDER AFT GIRT BAR BRACKET AT AFT SERVICE DOOR STATIONS 1168 TO 1169. INSTALLED LEFT CUSP DOUBLER REPAIR AND CUSP DOUBLER FILLER PER AARD 53-20-00-16, AT STATIONS 1164 TO 1170.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

CABIN, OVERWING STRUCTURE, STATION 927 BELOW SEAT TRACK 2 VERTICAL SUPPORT IS CRACKED AT BOTTOM FORWARD FASTENER AREA. REPAIRED PER EA MD80-53-013130 DATED 9/22/2010.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 57,130 hrs · 29,202 cycles

DORSAL FIN ANGLE CRACKED RIGHT SIDE 6 INCH AFT OF FORWARD ACCESS OPENING. REPLACED DORSAL FIN ATTACH ANGLE RIGHT SIDE PER AARD 55-30-00-7.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

HOLE IN SUB FLOOR NEAR STATION 170 LEFT BUTTLINE 14. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

RIGHT CUSP IS CRACKED AT STATION 218 TO 223 UPPER SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

FORWARD CARGO AT STATION 224 HAS INTERM REPAIR TO 2 AND 1/2 INCH CRACK AT LIGHTENING HOLE ON LEFT CUSP MEMBRANE PER EA MD80-53-006092 PERMANENT REPAIR TO BE ACCOMPLISHED AT OR BEFORE NEXT HEAVY C-CHECK. INSTALLED SERVICEABLE CUSP SHEET PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

SEAT TRACK NUMBER 2 STATIONS 1152 TO 1154 OUT OF LIMITS AT 1152. ROUTED OUT DAMAGE ON SEAT TRACK PER AARD 53-20-00-10. INSTALLED PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

RIGHT CUSP IS CRACKED AT STATION 740 TO 742 UPPER SIDE. REMOVED DAMAGED STRUCTURE, FABRICATED AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,130 hrs · 29,202 cycles

CORROSION ON LEFT CUSP AT LIGHTENING HOLE BOTTOM SIDE STATION 498. INSTALLED DOUBLER AT STATION 498 LEFT CUSP PER AARD 53-20-00-16 AND SRM 51-10-03.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 57,130 hrs · 29,202 cycles

MID CARGO DOOR OUTER SKIN BELOW HANDLE HAS DEEP BLENDS 3 INCH BY 4 INCH. INTERNAL REPAIR DOUBLER INSTALLED BELOW MID CARGO DOOR HANDLE PER SRM 52-04-00.

Part: PAN — CRACKED (WINDOW) · airframe 57,130 hrs · 29,202 cycles

RIGHT WINDOW PAN CRACKED AT LOWER EAR, AFT OF STATION 807 MARKED. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,130 hrs · 29,202 cycles

RIGHT WINDOW PAN CRACKED AT UPPER EAR. REMOVED CRACK INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,130 hrs · 29,202 cycles

WINDOW PAN CRACKED AT LOWER EAR. REMOVED CRACK INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,130 hrs · 29,202 cycles

FORWARD CARGO AT STATION 224 HAS INTERIM REPAIR TO 2 AND 1/2 IN CRACK AT LIGHTENING HOLE ON LEFT CUSP MEMBRANE PER EA MD80-53-006092 PERMANENT REPAIR TO BE ACCOMPLISHED AT OR BEFORE NEXT HEAVY C CHECK. INSTALLED CUSP SHEET AT STATION 218 TO 237 PER AARD 53-20-00-16.

Part: LIGHT — BROKEN (CABIN) · airframe 56,230 hrs · 28,718 cycles

LIGHTING COVER FOR EMERGENCY EXIT LIGHTS OPPOSITE FORWARD LAVATORY IS BROKEN. REPLACED LIGHT ASSEMBLY AT SEAT 3EF. OPS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 56,230 hrs · 28,718 cycles

EMERGENCY EXIT LIGHTS OPPOSITE FORWARD LAVATORY INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 3EF. OPS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (ZONE 100) · airframe 53,268 hrs · 27,062 cycles

LEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTING CRACKED. INSTALLED DOUBLER PER ESO 80559 DATED 04/08/09.

Part: SUPPORT FITTING — CRACKED (ZONE 100) · airframe 53,268 hrs · 27,062 cycles

RIGHT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTING CRACKED. INSTALLED DOUBLER PER ESO 80559 DATED 04/08/09.

Part: FRAME — CRACKED (ZONE 200) · airframe 53,268 hrs · 27,062 cycles

FRAME CRACKED AT ALIGNMENT PIN HOLES FOR TAIL CONE AT STATION 1510. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-01-00.

Part: STOP FITTING — CRACKED (ZONE 800) · airframe 53,268 hrs · 27,062 cycles

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

Part: STOP FITTING — CRACKED (ZONE 800) · airframe 53,268 hrs · 27,062 cycles

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

Part: STOP FITTING — CRACKED (ZONE 800) · airframe 53,268 hrs · 27,062 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,355 hrs · 26,561 cycles

EMERGENCY LIGHTS AT AFT LAVS INOPERATIVE. REPLACED BATTERY PACK, OPERATION CHECK GOOD.

Part: LENS — DAMAGED (CABIN)

DFW - EMERGENCY DOUBLE ARROW EXIT MARKER AT FORWARD ENTRY HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY DOUBLE ARROW EXIT MARKER AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

DFW - EMERGENCY DOUBLE ARROW EXIT MARKER AT FORWARD ENTRY INOPERATIVE. REPAIRED DAMAGED WIRING FOR EMERGENCY DOUBLE ARROW EXIT MARKER AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PSEU — INOPERATIVE (MLG)

DFW INFLIGHT T2422/06DEC - CREW REPORTED MAIN LANDING GEAR INDICATION ON APPROACH TO DFW. TOWER CONFIRMED GEAR DOWN. LANDED DFW WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHT ANNUNCIATOR RIGHT LAMP INOPERATIVE. RELAMPED EMERGENCY LIGHT ANNUNCIATOR RIGHT HAND LAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE)

AUS INFLIGHT T1705/3 MAR DESCENDING AT IDLE LEFT ENGINE DID NOT RESPOND AT LEVEL OFF. NUMBER 1 AND NUMBER 2 EPR WERE ALL SUB IDLE WITH NO THROTTLE RESPONSE. SHUT LEFT ENGINE DOWN AND SECURED VIA ENGINE FAILURE CHECKLIST. NO FURTHER ABNORMALITIES. REPLACED LEFT HAND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - CEILING EMERGENCY LIGHTS BETWEEN ROWS 8D AND 11D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 8D AND 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 10D)

DFW - SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 10D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS SEAT 20 TO END OF AIRCRAFT INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT SEAT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT AFT SEAT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY AFT LOWER OVERWING EXIT LIGHT DIM. REPLACED EMERGENCY AFT LOWER OVERWING EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — FAILED (NLG)

ORD - FLT 1197 - EN ROUTE ORD-PHX, SHORTLY AFTER TAKEOFF UNABLE TO RETRACT NLG. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE SLIDING MEMBER SEALS ON NLG STRUT. SERVICED NLG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (AFT STAIRWELL)

DFW - DURING OVERNIGHT MAINTENANCE, AIR STAIR EMERGENCY EXIT LIGHT AT CEILING PANEL HAS BROKEN WIRE. RE-PINNED EMERGENCY EXIT LIGHT AT CEILING PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TURBINE — FAILED (NR 2 ENGINE)

MIA - FLT 1381 - DURING GO-AROUND FOR LANDING AT MIA, NR 2 ENGINE FAILED AND SPOOLED DOWN. RE-START WAS NOT ATTEMPTED. AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED NR 2 ENGINE. PERFORMED ENGINE RUN-UP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: OVEN — DEFECTIVE (NR 3 GALLEY)

DFW - FLT 1403 - DURING DESCENT INTO DFW, ACRID ODOR WITH NO VISIBLE SMOKE NOTED IN CABIN AND COCKPIT. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NR 3 AFT GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (M)

Part: CONDUCTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 3E AND 6E FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 3E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)