N800NK

Part: ACM — FAILED (A/C BAY)

RIGHT PACK CAUSING SMOKE IN CABIN, GATE RETURN. FOUND OIL AT OUTLET OF RIGHT ACM TURBINE. REMOVED AND REPLACED RT ACM AND COALESCER BAG. OPS CHECK GOOD. (M)

Part: CONNECTOR — FAULTY (E/E BAY)

NR 1 VOR NEEDLES WON’T POINT TO STATION AND DOESN’T PULL BARBER POLE, FLAGS INDICATOR. AIRCRAFT TAIL SWAP WITH 817. REMOVED R50-318 NR 1 NAV RECEIVER RACK CONNECTOR. REPLACED ALL PINS, RETERMINATED BOTH VOR/ILS COAX AND SHIELD CONNECTORS. REINSTALLED CONNECTOR IN RACK. ALL CHECKS GOOD. (M)

Part: RACK — DEFECTIVE (NR 1 & NR 2)

DURING RTS CHECK FOR LMP UPGRADE, FOUND CAPT`S RMI SYNC INDICATION NOT MOVING, COMPASS CARD DOES NOT MOVE BACK TO COMPASS HEADING, TAIL SWAP WITH AC 808. REMOVED AND REPLACED COMPASS RACK FOR CAPT`S COMPASS SYSTEM. (NR 2) NO HELP, INSTALLED NEW DG. NO HELP, RE-INSTALLED ORIGINAL COMPASS RACK AND DG. SWAPPED CAPT`S AND F/O`S RMI`S. NO HELP, SWAPPED BACK TO ORIGINAL POSITIONS. INSTALLED NEW FLUX VALVE. NO HELP, REMOVED AND REPLACED F/O`S COMPASS RACK, BOTH NR 1 AND NR 2 COMPASS SYSTEMS. OPS CHECK OK. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 195-200 14 INCH LBL. REMOVED CORROSION AND FLOOR SUPPORT, FABRICATED FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN FLOOR SUPPORT CORRODED AT FS 169, 4 INCHES RBL. REMOVED CORROSION AND PORTION OF FLOOR SUPPORT, FABRICATED FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

FOUND CABIN FS 330, FS 1022-1041, FS 1041-1060, FS 1060-1079, FS 1079-1098, FS 1307 L-18L CUSP WEB CORRODED. REMOVED CORROSION AND WEB, DRILLED AND LOCATED NEW WEB FITTING ALONG L18L, TREATED, PRIMED AND INSTALLED DOUBLER AND NEW WEB SECTION. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND PAX CABIN FLOOR SUPPORT CORRODED AT FS 230 10 INCH RBL. REMOVED CORROSION AND FLOOR SUPPORT AT FS 230, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR. (M)

Part: CUSP WEB — DAMAGED (FUSELAGE)

REPAIRED CRACK AT CUSP WEB FS 788 LBL 44, NUMEROUS OVERSIZED HOLES IN CUSP WEB TO FS 845 LBL 44. REMOVED CUSP WEB FROM FS 778-798 LBL 44, FABRICATED CUSP WEB FROM 7075-T6 .025, TREATED, PRIMED AND INSTALLED CUSP WEB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 9 INCH LBL 13 INCH LBL. REMOVED CORRODED FLOOR SUPPORT, FABRICATED FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

LOWER APB AREA STATION 1338 STRINGER 28R STIFFENER CORRODED AND LEFT ANGLE CORRODED. REMOVED AND REPLACED STIFFENER AND ANLE. LOCATED AND DRILLED HOLES AND INSTALLED. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FORWARD ENTRYWAY CORROSION AT FS 200 CUSPLINE, LONG 18L FRAME TO CUSP FITTING. REMOVED FRAME TO CUSP FITTING STATION 200 L18L-L, REMOVED CORROSION ON CUSP, REMOVED WEB L1 DOOR STATION TO 208 L18L TO L13L. FABRICATED CUSP SECTION FROM STATION 180 TO STATION 230, TREATED, PRIMED AND INSTALLED NEW CUSP SECTION. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FOUND LEFT AFT FUSELAGE LONGERON 8L FS 1338 INTERCOSTAL HAS CORROSION. REMOVED INTERCOSTAL 8L FS 1338, LOCATED, DRILLED NEW INTERCOSTAL, TREATED PRIMED AND INSTALLED. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFT PIT FS 1338 APB FWD SIDE LOTER T-CHORD CORRODED L28L TO L28R. REMOVED CORROSION OUT OF LIMITS, REMOVED T-CAP (CHORD) STA 1338, L28L TO L29L, DRILLED AND LOCATED NEW T-CAP STA 1338. OK TO TOP COAT AND INSTALL NEW T-CAP. (K)

Part: DOUBLER — CORRODED (FUSELAGE)

AFT PIT FS 1338 APB FWD SIDE STIFFNER LOWER DOUBLER CORRODED L30. REMOVED CORROSION AND FOUND EVIDENCE OF CORROSION BETWEEN DOUBLER AND APB. REMOVED DOUBLER, REMOVED LONGERON END FITTING STA 1338 L28R, L29R, L28L AND L29L, REMOVED WEB STIFFNER ON FALSE BULKHEAD L29R TO L29L. DRILLED AND LOCATED HOLES IN SHEARTIE DOUBLER, TREATED, PRIMES AND INSTALLED REPAIR ANGLES, DOUBLERS AND END SPLICES. (K)

Part: BULKHEAD — CORRODED (FUSELAGE)

AFT PIT FS 1338 APB FORWARD WEB CORRODED AT LONG 29L TO LONGERON 29R. REMOVED CORROSION, CUT OUT DAMAGED AREA. FABRICATED DOUBLERS AND FILLERS, TREATED PRIMED AND INSTALLED. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160 7 INCHES LBL. REMOVED CORROSION AT FLOOR SUPPORT, FABRICATED BRACKET, LOCATED AND DRILLED AND INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 55,125 hrs · 25,715 cycles

FTW - FOUND MID PIT STATION 655 CEIING RBL 2 FLOORBEAM GOUGED. FABRICATED FILLER, ANGLE AND SHIM. TREATED, PRIMED AND INSTALLED. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CABIN SEAT TRACKS LEFT OUTBOARD STATION 200-484750, STATION 1022-1307 NUMEROUS AREAS HAVE GOUGES AND CORROSION OUT OF LIMITS. REMOVED CORROSION, BLENDED GOUGES AND REPLACED OUT OF LIMIT SEAT TRACKS, PRIMED AND TREATED SEAT TRACKS. (M)

Part: STRINGER — CRACKED (FUSELAGE)

AFT ACCESSORY COMPARTMENT STATION 1418 STRINGER 2R CRACKED. CUT AND REMOVED CRACKED STRINGER 2R STATION 1418, LOCATED AND DRILLED NEW STRINGER AND REPAIR SPLICE. TREATED, PRIMED AND INSTALLED. (M)

Part: LANYARD — LOOSE (L1 DOOR SLIDE) · airframe 54,483 hrs · 25,416 cycles

L1 DOOR GIRT BAR WAS DIFFICULT TO UNLATCH. FOUND LANYARD LOOSE, RESECURED LANYARD AND CLEANED GIRT BAR LATCH, OPS CHECK GOOD.

Part: HANDLE — LOOSE (L1 DOOR)

L1 DOOR HANDLE LOOSE. SECURED HANDLE.

Part: DUCT — LOOSE (TEMP VALVE)

DURING CLIMB-OUT, TAIL COMPARTMENT HIGH LIGHT CAME ON 1 OR 3 TIMES SO RETURNED TO DEPARTURE AIRPORT. T/S FOUND RT TEMP CONTROL VALVE DUCT LOOSE. SECURED PRIMARY HEAT EXCHANGER EXHAUST DUCT.

Part: HANDLE — LOOSE (L1 DOOR)

FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M)

Part: HANDLE — LOOSE (L1 DOOR)

FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE. (M)

Part: CABLE — MISINSTALLED (EVAC SLIDE)

L-1 DOOR ESCAPE SLIDE GIRT BAR CABLE IMPROPERLY INST. REPOSITIONED CABLE ON GIRT BAR.

Part: ENGINE — FAILED (NR 1)

AIR RETURN, NR 1 ENGINE FAILED AFTER TAKEOFF AT 1000 AGL-FLEX PWR T/O AT 1000 AGL. WE HAD AN ABRUPT BANG AND VIBRATION AND NR 1 ENGINE ROLLED BACK. ENGINE WINDMILLED N1 30 PERCENT TILL LAND-EGT WAS OK. DID NOT NOTICE OIL PRESSURE. DID NOT TRY TO RESTART ENGINE. NO SMOKE OR FLAME NOTICED. REMOVED AND REPLACED NR 1 ENGINE. OPS AND LEAK CK OK.

Part: CLIP — DISLODGED (L1 DOOR SLIDE)

RSW - FOUND L1 DOOR SLIDE PACK LANYARD CLIP FELL OFF. INSTALLED SLIDE PACK LANYARD CLIP. CLIP SECURE. (M)

Part: SIGN — MISSING (CABIN)

LGA - FOUND AFT GALLEY FLOOR EXIT GLOW SIGN MISSING. REPLACED MISSING AFT GALLEY FLOOR EXIT GLOW SIGN, OK FOR SERVICE. (M)

Part: SLIDE — DISLODGED (L2 DOOR)

ORD - FLT 433 - SLIDE PACK FELL OFF L2 DOOR. REMOVED AND REPLACED L2 DOOR SLIDE PACK. REMOVED SHIPPING PIN AND ATTACHED PULL CABLE. (M)

Part: BLADE — DAMAGED (NR 1 COMPRESSOR)

DTW - FOUND SEVERAL C1 BLADES HAVE FOD DAMAGE NR 1 ENGINE. REMOVED AND REPLACED 12 EACH C1 BLADES. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

EMERGENCY LIGHT IN TAIL COMPARTMENT BELOW WATER SEPARATORS HAS BROKEN WIRE. REPAIRED BROKEN WIRE TO EMERGENCY LIGHT IN TAIL COMPARTMENT, BELOW WATER SEPARATORS. OPS CHECK OK. (M)

Part: ACM — ODOR (RIGHT)

WITH RIGHT AC PACK ON, OILY ODOR IN THE CABIN, ODOR CEASES WITH RIGHT PACK OFF, OIL FOUND ON SIDE PANELING AT THE END RIGHT OVERWING EXIT. INSPECTED RIGHT ACM FOUND VERY LITTLE, CLEANED OIL AND RAN ACM NO LEAKS NOTED, NO ODOR IN CABIN, OPS CHECKS NORMAL. (M)

Part: FLOOR PANEL — DELAMINATED (GALLEY)

FOUND PASSENGER CABIN UNDER G-4 GALLEY FLOOR PANEL DELAMINATED, INSERTS BAD. FABRICATED NEW PANEL. INSTALLED FLOOR PANEL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CABIN LEFT OUTBOARD SEAT TRACK CORRODED ON UPPER AND LOWER SIDES FS 1155-1231 HIDDEN DAMAGE FOUND UPON PANEL REMOVAL. REMOVED LEFT OUTBOARD SEAT TRACK. LOCATED AND DRILLED TWO SEAT TRACK WITH TWO SPLICE. INSTALLED SEAT TRACK. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FOUND L-1 AND R-1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE AND EMERGENCY PASSAGEWAY LIGHTING INOPERATIVE. FOUND CONNECTOR LOOSE AT L1- AND R1 EMERGENCY BATTERY PACK RE-CONNECTED. FOUND BROKEN COPPER TERMINAL GROUND FOR EMERGENCY PASSAGEWAY LIGHTING RE-TERMINATED. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND AFT ACCY COMPARTMENT WEB CRACKED AT FS 1485 APPROX 20 INCHES RBL. REMOVED CRACKED WEB. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. UPON FURTHER INSPECTION FOUND CHAFING AND CRACK. STOP DRILLED CRACK. NO DOUBLER REQUIRED. INSTALLED REPAIR WEB. (M)

Part: FLOOR PANEL — DAMAGED (COCKPIT)

FTW - HIDDEN DAMAGE COCKPIT FLIGHT OFFICERS FLOOR PANEL DIRECTLY UNDER SEAT CORRODED. FABRICATED NEW PANEL. (M)

Part: FLOOR PANEL — BROKEN (COCKPIT)

FOUND FLIGHT COMP, F/O'S RIGHT FORWARD FLOOR PANEL BROKEN. REMOVED FLOORBOARD. FABRICATED NEW FLOORBOARD. INSTALLED F/B RIGHT. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

AFT CARGO INNER DOUBLER CORRODED FS 1174 BELOW STRINGER 18L. REMOVED LONGERON 19L. REMOVED DAMAGED AREA. FABRICATED DOUBLER, TRIPLER AND FILLER. INSTALLED FASTENERS IN DOUBLER AND TRIPLER FROM L18L UPPER FLANGE TO L17L STATION 1168 TO 1180. INSTALLED FASTENERS IN DOUBLER AND TRIPLER FROM L18 LOWER FLANGE TO L18L STA 1168 TO 1180. FABRICATED 15 LONGERON SPLICE. INSTALLED L19L FROM STATION 1146-1203 AND LONGERON SPLICE. (M)

Part: FLOOR PANEL — BROKEN (FUSELAGE)

FOUND PASSENGER CABIN FLOOR PANEL AT FS 1250-1303 CENTER, PANEL HONEY COMB EDGE BROKEN. FABRICATED FLOOR PANEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FLOORBOARD STATION 1056-1136 LBL 44-54 CRACKED AND DELAMINATED IN SEVERAL AREAS. REPAIRED FLOORBOARD. (M)

Part: FLOORBOARD — CRACKED (CABIN)

FTW - FLOORBOARD STATION 1174-1294 LBL 44-54 CRACKED AND DELAMINATED IN SEVERAL AREA. REPAIRED FLOORBOARD. (M)

Part: ISOLATOR — CORRODED (NACELLE)

FTW - RIGHT AFT VIBRATION ISOLATOR CAD PLATING CORRODED. REMOVED RIGHT AFT VIBRATION ISOLATOR. INSTALLED RIGHT AFT VIBRATION ISOLATOR. (M)

Part: STRUCTURE — CRACKED (ELEVATOR)

FTW - FOUND LEFT ELEVATOR STATION XHR 11 TWO DOUBLER CRACKED, DAMAGE. REMOVED DAMAGED UPPER AND LOWER TWO DOUBLERS. FABRICATED TWO DOUBLERS. INSTALLED FABRICATED DOUBLERS. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND AFT ACCY COMPARTMENT CANTED FRAME CRACKED AT FS 1485 18 INCHES RBL. FABRICATED 7 DOUBLER AND 25 DOUBLER FRAME. INSTALLED 7 DOUBLER AND 25 FRAME. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CORROSION AT PAX CABIN FLOOR SUPPORT FS 200. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT 58 JUST ABOVE FLOOR LEVEL. REMOVED DAMAGED SKIN SECTION AT FS BT STRINGER 17-18 LEFT, CUT OUT IS 5375 BY 8.75. FABRICATED REPAIR PARTS 5 BBL, 9 FINGER BDL 15 SKIN SEC INSTALLED ALL REPAR PARTS. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - AFT FUSELAGE STATION 1380 RIGHT SIDE CORRODED AT INTERCOSTAL AND ANGLE SUPPORT 'T' CAP. DRILLED AND LOCATED NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FTW - FOUND T-CHORD SUPPORT ANGLE IS CRACKED IN RADIUS. REMOVED SUPPORT ANGLE. INSTALLED CLIP. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 245 BETWEEN LONGERONS 18L AND 19L. FABRICATED REPAIR DOUBLERS AND FILLERS. UPON FURTHER EVALUATION. FOUND SHEAR TIE FRAME SECTION AT STATION 237 L18 - L20L TO BE CRACKED. REMOVED SHEAR TIE SECTION AT FS 237 L18L TO L20L. FABRICATED NEW SHEAR TIE SECTION. I NSTALLED SHEAR TIE. INSTALLED FABRICATED REPAIR DOUBELRS AND FILLERS. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT FS 40 RIGHT FUSELAGE NOSE LANDING GEAR CUT OUT. FABRICATED INTERNAL DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT FS 598 BETWEEN LONGERONS 21 AND 22R. REMOVED DAMAGED AREA. FABRICATED NEW SECTION OF SKIN 29, 19 FINGER DOUBLER, 27 DOUBLERS, 23 DOUBLERS. INSTALLED REPAIR PARTS. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENTS AT FS 265-313 AT LONGRONS 21R. CUT OUT DAMGAED AREA. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED NEW 11 SKIN, FINGER DOUBLER, AND 5 DOUBLER. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - ATTACH ANGLE STATION 592 MID PIT CORRODED. WHILE REMOVING CORROSION, ATTACH ANGLE WAS FOUND TO BE CRACKED. FABRICATED REPLACEMENT CLIP. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 351 BETWEEN LONGERONS 19 AND 20R. CUT OUT DAMAGE. FABRICATED 9 FINGER DOUBLER. FABRICATED 11 SKIN. FABRICATED 5 DOUBLER. INSTALLED 5 AND 9 DOUBLERS AND 11 NEW SKIN. (M)

Part: DOOR FRAME — BENT (FUSELAGE)

FOUND L-1 DOOR JAMB HAS SKIN EDGES BENT OUT AND REQUIRES REPAIR. PERFORMED DYE PENETRANT INSPECTION, FOUND CRACK IN SKIN. REMOVED CRACK IN SKIN. FABRICATED 19 TRIP. FABRICATED 21 DOUBLER. INSTALLED NEW REPAIR. (M)

Part: ISOLATOR — DAMAGED (NACELLE)

FOUND LOWER RIGHT FORWARD VIBRATION ISOLATOR ALIGNMENT MARKS BEYOND LIMITS. REMOVED RIGHT FORWARD LOWER VIBRATION ISOLATOR. INSTALLED RIGHT FORWARD LOWER VIBRATION ISOLATOR. (M)

Part: TAB — DELAMINATED (RUDDER)

FOUND RUDDER TAB AREAS OF DELAMINATED. REPAIRED DAMAGE ON RUDDER TAB. (M)

Part: SPLICE — CORRODED (FUSELAGE)

AFT PIT CORRODED FASTENERS ALL AT FS 1193-1212, 14 AT 25L, 14 AT 24L, 14 AT 231, 2 AT 221, 15 AT 241, 14 AT 201, 14 AT 19L. UPON FURTHER INSPECTION AT FS 1193-1212 L23L SPLICE IS FOUND TO BE CORRODED OUT OF LIMITS. REMOVED SPLICE. FABRICATE NEW LONGERON SPLICE. INSTALLED NEW LONGERON SPLICE. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

FTW - FOUND FORWARD CARGO JAMB BEAM CRACKED AT AFT DOOR STOP. REMOVED FORWARD CARGO JAMB BEAM. LOCATE AND DRILL NEW JAMB BEA. INSTALLED NEW JAMB BEAM. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

FOUND AFT FUSELAGE LEFT SIDE STATION 1429 TO 1418 HAS CORROSION AT SUPPORT FORWARD VENTRAL STAIRWAY. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: WEB — CORRODED (FUSELAGE)

AFT PIT CORRODED FLOOR WEB AT FS 1250 APPROX 10 INCHES INBOARD OF CUSP LINE RIGHT SIDE, CORRODED FASTENER AT CUSP LINE AFT SIDE OF FRAME 1250. FABRICATED NEW WEB. INSTALLED NEW WEB. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND CORRODED LONGERON STRAP AND ATTACHMENT HARDWARE AFT BAG BIN STATION 1320-1338 L23R TO L25R. REMOVED TWO LONGERON STRAP AT STATION 1320-1338 L24R-L23R. INSTALLED NEW LONGERON STRAP FITTING, L24R STATION 1320-1338. INSTALLED NEW LONGERON STRAP FITTING L23R STATION 1320-1338. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FOUND AFT FUSELAGE LEFT SIDE STATION 1429 TO 1448 HAS CORROSION AT T-CAP VENTRAL STAIRWAY. REMOVED INTERCOSTAL. REMOVED DAMGED CAP ANGLE. FORMED NEW INTERCOSTAL AND CAP ANGLE. INSTALLED NEW INTERCOSTAL. INSTALLED NEW CAP ANGLE. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND FLOOR WEB CORRODED AT BOTTOM OF L2 DOOR STATION 1136-1174 (2) Z-ANGLE BRACKETS CORRODED TWO EACH. CUT OUT FLOOR WEB. FABRICATED FILLER AND DOUBLER. INSTALLED DOUBLER REPAIR AND FILLER. (M)

Part: FITTING — CRACKED (FUSELAGE)

INTERNAL ANGLES ON DORSAL FITTINGS CRACKED BOTH SIDES, STATION 1437. REMOVED LEFT AND RIGHT INTERNAL ANGLES. LOCATED AND DRILLED NEW INNER ANGLE ON LEFT DORSAL FIN. INSTALLED LEFT AND RIGHT INNER ANGLES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND LEFT AFT LAVATORY STATION 1338 HAS CORROSION AT BRACKET AND SUPPORT FLOOR. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: HINGE BRACKET — CORRODED (RUDDER)

FTW - VERTICAL STAB RUDDER HINGE CENTER 'V' BRACKET ASSEMBLY HAS CORROSION STATION ZR 97.207. REMOVED VERTICAL STAB RUDDER HINGE CENTER 'V' BRACKET. INSTALLED BRACKET ASSEMBLY. (M)

Part: CLIP — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT CORRODED AND CRACKED ANGLE CLIP AT FS 1250 LONGERON 23L-24L. REMOVED CLIP. INSTALLED NEW CLIP. (M)

Part: BRACKET — CORRODED (RUDDER)

VERTICAL STAB RUDDER HINGE UPPER 'V' BRACKET ASSEMBLY HAS CORROSION STATION ZR 133. REMOVED VERTICAL STABILIZER RUDDER HINGE UPPER 'V' BRACKET. INSTALLED BRACKET ASSEMBLY. (M)

Part: SKIN — GOUGED (RT WING TE FLAP)

FOUND RIGHT WING INBOARD FLAP GOUGED AT NOSE CAP 3RD HINGE FROM INBOARD. MATERIAL ID 2014-T6.090. MATERIAL SUB 2014-T6.090 TO 7075-T6.090. FABRICATED WEB DOUBLER REPAIR. INSTALLED DOUBLER. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

RIGHT DORSAL FIN VERTICAL ATTACH ANGLE HAS CRACKING VERTICAL LEG. ALSO, DOUBLER ATTACHMENT IS OUT OF LIMITS. REMOVED RIGHT DORSAL FIN VERTICAL ATTACH ANGLE. REMOVED DOUBLER ATTACHMENT. FABRICATED NEW DOUBLER ATTACHMENT. FABRICATED NEW GUSSET. LOCATED AND DRILLED NEW OUTER DORSAL FIN ATTACH ANGLE. INSTALLED RIGHT DORSAL FIN OUTSIDE ATTACH ANGLE. INSTALLED NEW DOUBLER ATTACHMENT. INSTALLED GUSSET. (M)

Part: PAN — CORRODED (FWD CARGO DOOR)

FOUND FORWARD CARGO LOWER DOOR JAMB BEAM CORRODED. REMOVED FORWARD CARGO DOOR JAMB PAN. REPLACED FORWARD CARGO DOOR JAMB PAN. LOCATE AND DRILLED FORWARD CARGO DOOR JAMB PAN. FABRICATED SPLICE REPAIR. INSTALLED SPLICE REPAIR ON STAITON 370 PLUS STATION 427. (M)

Part: PANEL — DELAMINATED (RT WING)

RIGHT WING INNER WING UPPER FORWARD TRAP PANEL DELAMINATING. FITTED AND DRILLED NEW RT WING INNER UPPER FORWARD TRAP PANEL. INSTALLED NEW RT WING INNER UPPER PANEL. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO LOWER DOOR JAMB BEAM CORRODED. REMOVED MID CARGO LOWER DOOR JAMB BEAM. LOCATE AND DRILLED NEW JAMB BEAM. INSTALLED NEW JAMB BEAM IN MID CARGO. (M)

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB)

LEFT DORSAL FIN VERTICAL ATTACH ANGLE HAS CRACK IN VERTICAL LEG. REMOVED LEFT DORSAL FIN VERTICAL ATTACH ANGLE. LOCATED AND DRILLED NEW DORSAL FIN VERTICAL ANGLE. INSTALLED LEFT DORSAL FIN OUTSIDE ATTACH ANGLE. (M)

Part: DOOR — CRACKED (FUEL SERVICE)

RT WING LEADING EDGE STATION XRS 240 REFUELING ACCESS DOOR CRACKED AND WORN ON INTERIOR. REMOVED REFUELING ACCESS DOOR. INSTALLED NEW FUEL DOOR. (M)

Part: PANEL — DELAMINATED (LT WING)

FOUND LT WING LOWER TRAP PANEL DELAMINATING. REPAIRED LEFT WING LOWER TRAP PANEL AT DELAMINATED. (M)

Part: PANEL — CRACKED (LT WING)

FTW - FOUND LEFT WING INNER WING UPPER AFT TRAILING EDGE TRAP PANEL CRACKED/DAMAGE TO COMPOSITE MATERIAL. REPAIRED CRACK/DAMAGED AREA. (M)

Part: PANEL — CORRODED (RT WING)

FOUND RIGHT WING LEADING EDGE PANEL 1248C CORROSION AT FASTENER HOLES AND NUMEROUS GOUGES. MATERIAL OUT OF LIMITS. RECEIVED NEW R/W L/E PANEL. (M)

Part: SUPPORT — CRACKED (RT WING)

FTW - FOUND RIGHT WING LEADING EDGE STATION XFS 624 CRACKED AND BENT, SUPPORT. REMOVED SUPPORT. LOCATED AND DRILLED NEW SUPPORT. INSTALLED THE NEW SUPPORT. (M)

Part: DOUBLER — CORRODED (LT WING LE)

LEFT WING LEADING EDGE PANEL, 1118C CORROSION AT FASTENER HOLES. FABRICATED DOUBLER. INSTALLED DOUBLER.

Part: SKIN — CORRODED (LT WING)

LT WING LE PANEL 1117C CORROSION AT FASTENER HOLES. FABRICATED DOUBLER. INSTALLED DOUBLER.

Part: ODOR — DETECTED (CABIN)

TPA - FLT 632 - ON APPROACH INTO DTW 'BURING' RUBBER SMELL FROM ROW 19-23 DISSIPATED QUICKLY. PERFORMED AN INSPECTION ON THE LIGHTING SYSTEM INCLUDING BALLASTS ON ROW 19 TO 23, BOTH SIDES. NO DEFECTS WERE NOTED. (M)

Part: LANYARD — MISSING (ESCAPE SLIDE)

FLL - LS DOOR EVACUATION SLIDE LANYARD ASSEMBLY MISSING. INSTALLED LANYARD ASSY ON L2 EVACUATION SLIDE IAW MD80 MM 25-62-00. (M)

Part: SLIDE — DISLODGED (CABIN)

FLL - FLT 1751A - FOUND ESCAPE SLIDE AT L2 DOOR CAME LOOSE. REINSTALLED ESCAPE SLIDE AT L2 DOOR IAW MD80 MM 25-62-00. (M)

Part: SWITCH — OUT OF POSITION (TE FLAPS)

DTW - FLT 503 - RECEIVED TAKEOFF WARNING, RETURN TO GATE, DIAL A FLAP WAS STOWED. ADJUSTED FLAP HANDLE POSITION SWITCH PER MM 27-51-00. TAKEOFF WARNING, OPS CHECK GOOD AT THIS TIME. (M)

Part: COMPUTER — MALFUNCTIONED (TRIM)

MCO - FLT 506 - TAKEOFF CONDITION LONG TRIM COMPUTER HAS EXCESSIVE PLAY, CAN ROLL CG WHEEL UP TO TWO UNITS AND THE INDICATOR WILL NOT MOVE. FOUND LONG TRIM COMPUTER POINTER STICKING FREED POINTER, OPS CHECK GOOD IAW MD80 MM 27-41-00. (M)

Part: RECEIVER — FAILED (COCKPIT)

FLT 9826 - ACY - FOUND ON TWO ILS APPROACHES TO RWY 4L TO DTW (FREQ 111.95) AUTOPILOT DISCONNECTED AFTER 'S' TURNING AT 300 FEET AGL. AUTOPILOT WORKS OK DURING ALL OTHER PHASES OF FLIGHT. NR 1 HAD MULTIPLE FAIL CODES IN THE FLIGHT FAULT REVIEW. REMOVED AND REPLACED NR 1 VHF NAV RECEIVER. OPS CHECKS GOOD. (M)

Part: LIMITER — OUT OF ADJUST (RUDDER)

FLT 1225 - RSW - RUDDER TRAVEL UNRESTRICTED LIGHT ILLUMINATED IN CRUISE FLIGHT. FOLLOWED PROCEDURE AND SELECTED RUDDER TO MANUAL. ON DESCENT, LIGHT WENT OUT AT 310 KTS ON APPROACH WE SELECTED RUDDER TO POWER AND IT OPERATED NORMALLY. ADJUSTED RUDDER THROW LIMITER IAW MD80. NO FURTHER DEFECTS NOTED. (M)

Part: PROXIMITY SWITCH — FAULTY (CARGO DOOR)

FLT 503 - MCO - ON TAKEOFF ROLL APPROXIMATELY 80 KTS FORWARD DOOR CARGO LIGHT CAME ON PERFORMED LOW SPEED ABORT LIGHT WENT OFF CLEARING RUNWAY. REMOVED AND REPLACED PROXIMITY SWITCH. ADJUSTED DOOR TARGET. OPS CHECK GOOD. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

FLT 1657 - DTW - GOT TAKEOFF WARNING DURING TAKEOFF ROLE. RETURNED TO GATE. PERFORMED TAKEOFF WARNING TEST OPS CHECKS GOOD IAW MD80 MM 27-00-0. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT APPROX STATION 217 BETWEEN LONGERON 18L AND 19L. FABRICATED DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 51-30-2 AND 51-30-5 AND 53-04. (M)

Part: OXYGEN MASK — MALFUNCTIONED (CABIN)

FTW - FOUND OXYGEN MASK AT ROWS 18 LEFT, 25 LEFT AND 31 RIGHT DIDN'T DROP. ADJUSTED OXYGEN DOORS IAW MD80 MM 35-20-00. (M)

Part: CONNECTOR — DAMAGED (SPOILERS)

FTW - RIGHT SPOILER POSITION FAILS DURING RETURN TO SERVICE TEST. T/S SYSTEM AND FOUND PIN OF 1 OF P10 398 RECESSED. RESEATED PIN IN CONNECTOR IAW MD80 WDM 20-50-04. (M)

Part: SUPPORT — CORRODED (GALLEY)

FTW - G-2 GALLEY LOWER OUTBOARD LEFT SUPPORT CORRODED. REMOVED CORRODED ANGLE. LOCATE AND DRILL ANGLE IAW MD80 SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160 AT BODY CENTER LINE, FLOORBOARD SUPPORT IS CORRODED. FLOORBOARD SUPPORT WAS REMOVED. LOCATED AND DRILLED NEW ANGLE. INSTALLED ANGLE SUPPORT IAW MD80 SRM 51-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT FS 1220 BETWEEN LONGERON 28L AND 29L, THIS DENT IS BEYOND LIMITS AND MUST BE REPAIRED. FABRICATED DOUBLER. INSTALLED PER MD80 SRM 53-04. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - PASSENGER CABIN STATION 1003/1079 FLOORBOARD OUTBOARD RIGHT DAMAGED. REMOVED FLOORBOARD PANEL TO REPAIR. FABRICATE NEW FLOOR PANEL. INSTALLED FLOOR PANEL IAW MD80 MM 53-20-1. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - PASSENGER CABIN FLOOR BOARD DAMAGED STATION 650 RIGHT SIDE. REMOVED FLOOR BOARD PANEL TO REPAIR. FABRICATED NEW FLOOR PANEL. INSTALLED FLOOR PANEL IAW MD80 MM 53-20-1. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND WEB CRACKED AT STA Y=1127 LONGERON 13L, L-2 DOOR WEB JAMB AREA. LOCATE AND DRILL WEB DOUBLER REPAIR. INSTALLED GUSSETS AND WEB REPAIR DOUBLER AT LONGERONS 12 AND 13 IAW MD80 SRM 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 408 BETWEEN L28L AND L29L IS BEYOND ALLOWABLE LIMITS. FABRICATE DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 53-04. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - CABIN CENTER FLOORBOARD STATION 617 IS CRACKED AND DAMAGED AT AFT END. REMOVED FLOOR PANEL, CABIN CENTER STATION 617 PER MD80 SRM 53-20-01. REPAIRED DAMAGED END, INSTALLED FLOOR PANEL PER MD80 SRM 53-20-01. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - LEFT OUTBOARD FLOOR PANEL CRACKED BETWEEN STATION 380 AND 305. STOP DRILLED CRACKS. FABRICATED DOUBLERS. INSTALLED DOUBLER IAW MD80 SRM 53-01. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, CHANNEL SUPPORT CORRODED AT STATION Y=160 FROM X40 TO X20, BETWEEN FLOOR SUPPORT AND UPPER CHANNEL. REMOVED CHANNEL SUPPORT. INSTALLED NEW CHANNEL SUPPORT IAW MD80 SRM 51-30-2. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - RIGHT OUTBOARD METALLIC FLOOR PANEL, CRACKED AT STATION 460. LOCATED AND DRILLED REPAIR DOUBLER. INSTALLED DOUBLER PER MD80 SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

L-1 DOOR THRESHOLD, LIGHT CORROSION ON THRESHOLD/FLOORBOARD SUPPORT ANGLE 6 INCHES INBOARD FROM DOOR CUTOUT. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-2. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND WEB CRACKED AT STATION Y 1009, X46 INCHES. REMOVED DAMAGED AREA AT WEB STATION Y 1009. LOCATE AND DRILLED DOUBLER AND FILLER IAW MD80 SRM 53-01. INSTALLED REPAIR PARTS. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR PAN CORRODED AT STATION Y200 FROM -X 10 INCHES TO -X30. REMOVED DAMAGED AREA. FABRICATED REPAIR PART. INSTALLED REPAIR PART IAW MD80 SRM 51-30-2. (M)

Part: YOKE — CORRODED (ENGINE MOUNT)

FTW - FOUND RIGHT ENGINE MOUNT YOKE HAS CORROSION INSIDE LOWER VIBRATION ISOLATOR CAVITY AND EXTERNAL AREA. REMOVED CORROSION. OK TO INSTALL SERVICEABLE YOKE. INSTALLED YOKE. REMOVED YOKE BOLTS. INSTALLED YOKE BOLTS PER MD80 MM 71-20-3. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FTW - ANGLE SUPPORT CRACKED AT STATION Y 1322 ABOVE LONGERON 30. FABRICATED DOUBLER. STOPPED DRILLED CRACK. INSTALLED DOUBLER IAW MX80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT HAS AN ELONGATED HOLE AT STA Y=166 X53 INCHES. REMOVED DISC. FABRICATED NEW PART. INSTALLED NEW PART IAW MD80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - PAX CABIN FLOOR SUPPORT CORRODED AT STA Y=200 -X47 TO -X57, LOWER SURFACE. FABRICATED NEW PART. INSTALLED NEW PART IAW MD80 SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=164, X31 INCHES. LOCATED AND DRILLED NEW FITTING. INSTALLED NEW FITTING IAW MD80 SRM 51-30-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - RIGHT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES FROM STATION 826 TO STATION 845. INSTALLED NEW SEAT TRACK, REF N/R 18-N-00214. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - AFT B/B LONGERON 30 CORROSION AT STATION 1005 AND STATION 1022 AND DAMAGED SEALANT AROUND PREVIOUS REPAIR. FABRICATED REPAIR FITTING. INSTALLED REPAIR FITTING IAW FLIGHT VEHICLES DRAWING 53-01-01-1. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 770 GOUGED. INSTALLED SEAT TRACK, REF N/R 18-N-00259. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

FTW - LEFT INBOARD SEAT TRACK STATION 368 TO 348 CHAFING. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 51-30-5. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

FTW - LEFT INBOARD SEAT TRACK STATION 596 TO 589 GAUGE WITH CHAFING. SEAT TRACK WAS FOUND OUT OF LIMITS IAW MD80 SRM 53-05. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 51-30-5 AND 51-3-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=164, X42. REMOVED FLOOR SUPPORT FITTING. BACK DRILLED NEW BRACKET. INSTALL NEW BRACKET IAW MD80 SRM 51-30-5. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

FTW - LEFT INBOARD SEAT TRACK STATION 747 TO 734 GAUGE AND CHAFING. SEAT TRACK WAS FOUND OUT OF LIMITS. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 53-05. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - RIGHT INBOARD SEAT TRACK HAS A GOUGE AT FS 1049. SEAT TRACK BEING REPLACED. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

RIGHT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGED AREAS FROM STATION 955 TO 967. REMOVED DAMAGED SEAT TRACK FROM STATION 914 TO 1032. INSTALLED NEW SEAT FROM STATION 924 TO 1032 IAW MD80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=200 -X5 TO +X5. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 51-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

RIGHT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES FROM STATION 851-865. REMOVED DAMAGED SEAT TRACK FROM STATION 797-914. INSTALLED NEW SEAT TRACK FROM STATION 740 TO STATION 914 IAW MD80 SRM 51-30-2. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 815 TO 806 CHAFING. UPON REMOVAL OF LEFT FLOOR PANEL STATION 779-826 FOUND CRACK IN LOWER WEB. CUT OUT DAMAGED SEAT TRACK STATION 760-840. FORMED REPAIR DOUBLER. APPLIED AND INSTALLED DOUBLER REPAIR. INSTALLED SEAT TRACK AND SPLICE STATION 760-840 IAW MD80 SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED AT STATION Y=198.0, -X54 INCHES FORWARD ENTRY AREA. FABRICATED OF PART, INSTALLED NEW PART IAW MD80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=238 X=0. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 53-14-2. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FLOOR SUPPORT CORRODED AT STATION Y 193, -X53 INCHES FORWARD ENTRY AREA. REMOVED CORROSION AT FLOOR SUPPORT. FOUND MATERIAL WITHIN LIMITS. FOUND WEB FLOOR PANEL CRACKED AND CORRODED. FORMED NEW WEB FLOOR. INSTALLED NEW WEB FLOOR IAW IAW MD80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y=218 X=0, INBOARD SURFACE. FORMED NEW SUPPORT. INSTALLED FLOOR SUPPORT PER MD80 SRM 53-14-1. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - LEFT INBOARD SEAT TRACK STATION 869 GAUGE AND BARE METAL. SEAT TRACK WAS FOUND OUT OF LIMITS FROM STATION 788-920. INSTALLED SEAT TRACK PER MD80 SRM 53-05. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR PAN CRACKED AT STA Y 2A-X43. CUT OUT DAMAGED AREA IAW MD80 SRM 53-01. FABRICATED NEW FLOOR PER REPAIR IAW MD80. INSTALLED NEW PER REPAIR IAW MD80 SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=160 TO STA Y=200, -X7. REMOVED FLOOR SUPPORT STATION 200 TO APPROX Y 145. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=200 FROM -X9 TO -X44. REMOVED FLOOR SUPPORT. FABRICATED NEW ANGLE. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND SUPPORT CORRODED AT STATION Y=173, -X54 INCHES FORWARD ENTRY AREA. FABRICATED SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED AND STATION 173-X53 INCH FORWARD ENTRY AREA. FOUND WEB FLOOR PANEL CRACKED AND CORRODED. FORM NEW WEB FLOOR. INSTALLED NEW WEB FLOOR IAW MD80 SRM 51-30-2. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FOUND RIGHT INBOARD SEAT TRACK HAS A GOUGE AT FS 1079. REMOVED SEAT TRACK SECTION FROM STATION 1032 TO STA Y 1032 TO STA Y 1146 (RIGHT INBOARD SEAT TRACK) IAW MD80 SRM 53-05. (M)

Part: ISOLATOR — UNSERVICEABLE (RT ENGINE)

FTW - FOUND RIGHT ENGINE, FORWARD LOWER VIBRATION ISOLATOR HAS MISMATCHED ROTATION MARKS. REMOVED VIBRATION ISOLATOR. INSTALLED O/H, RT ENGINE FORWARD LOWER VIBRATOR ISOLATOR IAW MM MD80 71-20-02. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

FTW - LEFT INBOARD SEAT TRACK STATION 1175 TO 1150 CHAFING. SEAT TRACK WAS FOUND OUT OF LIMITS FROM STATION 1150 TO 1122. LOCATED AND DRILLED PER MD80. INSTALLED SEAT TRACK AND SPLICE PER MD80 SRM 53-05. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - RIGHT INBOARD SEAT TRACK GOUGED AT FS 1160. LOCATED AND DRILLED RIGHT, INBOARD SEAT TRACK. INSTALLED SEAT TRACK AND SPLICE, FS 1146-1260 RT, INBOARD IAW MD80 SRM 51-10-4. (M)

Part: PAN — CRACKED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR PAN CRACKED AT STATION Y 200, -X40. REMOVED DAMAGED AREA. FORMED DOUBLER. INSTALLED NEW DOUBLER IAW MD80 SRM 51-30-2. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

FTW - RIGHT OUTBOARD SEAT TRACK HAS BARE METAL AT FS 1293 TO 1267. REMOVED (DAMAGE SEAT) TRACK SECTION FROM STATION 1240 TO STATION 1309. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK FROM STATION 1240 TO STATION 1309 IAW MD80 SRM 51-30-1. (M)

Part: ISOLATOR — UNSERVICEABLE (LT ENGINE)

FTW - FOUND LEFT ENGINE FORWARD, LOWER VIBRATION ISOLATOR HAS MISMATCHED ROTATION MARKS. REMOVED VIBRATION ISOLATOR. INSTALLED SERVICEABLE VIBRATOR ISOLATOR IAW MD80 71-20-02. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 977 GOUGED. INSTALLED SEAT TRACK AND SPLICES FROM STATION 920 TO STATION 1018 IAW MD80 SRM 53-05. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK FROM STATION 1035 TO 1150 DAMAGED. SEAT TRACK WAS FOUND OUT OF LIMITS. LOCATED AND DRILLED SEAT TRACK. INSTALLED PER MD80 SRM 53-05. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - LEFT OUTBOARD SEAT TRACK STATION 1007 GOUGE. CUT OUT SEAT TRACK FROM STATION 937 TO 1032. INSTALLED SEAT TRACK FROM STATION 937 TO 1032 IAW MD80 SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT FS 398.5 BETWEEN LONGERON 17R AND 18R. FABRICATED AND DRILLED REPAIR. INSTALLED DOUBLER IAW MD-80 SRM 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 1224 BETWEEN LONGERON 23R AND 24R. FABRICATED AND DRILLED REPAIR DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 51-30-2 AND SRM 51-30-5. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND EXTERNAL DOUBLER AT LEFT AFT NOSE GEAR DOOR HINGE CUT OUT. THIS DOUBLER MUST BE REPLACED WITH DOUBLER REPAIR GIVEN IN SRM 53-05. REMOVED OLD DOUBLER REPAIR. FORMED DOUBLER REPAIR. INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-05. (M)

Part: BRACKET — CRACKED (PAX DOOR)

FTW - FORWARD PASSENGER DOOR L1 BRACKET CRACKED AT STATION Y-188, Z=32.9 BETWEEN LL BEAM NR 6 AND LL BEAM NR 5. FORMED L-1 ANGLE. INSTALLED V ANGLE IAW MD80 SRM 51-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 362 BETWEEN LONGERON 24R AND 25R. CUT DAMAGE AREA. FABRICATED PARTS REPAIR DOUBLER. INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-04. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - REPAIR AT FS 1212 AT AFT EDGE OF AFT CARGO DOOR. THIS REPAIR MUST BE REPLACED WITH REPAIR IN SRM 53-05. REMOVED OLD REPAIR. LOCATED AND DRILLED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS IAW MD80 SRM 53-05. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND REPAIR AT FS 1155 AT FORWARD EDGE OF AFT CARGO DOOR. FABRICATED NEW REPAIR. INSTALLED NEW REPAIR IAW MD80 53-05. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FTW - AFT AIRSTAIR STATION 1338 CANTED, VERTICAL ANGLE ATTACHED TO RT UPPER SIDE WALL SUPPORT CHANNEL IS CRACKED IN FORWARD FLANGE RADIUS. REMOVED CANTED VERTICAL ANGLE AT AFT AIRSTAIRS. FABRICATED FORWARD AND AFT FLANGE REPAIR DOUBLERS. INSTALLED CANTED VERTICAL ANGLE IAW MD80 SRM 51-30-2. (M)

Part: RIB — CRACKED (L1 DOOR)

FTW - FORWARD PAX DOOR L1 HAS LEAK AT STATION Y 190 Z34.5 BETWEEN LL BEAM NR 5 AND LL BEAM NR 4. REMOVED CRACKED RIB IAW MD80 SRM 51-30. FOUND BEAM IAW MD80 SRM 52-05. DURING REMOVAL FOUND TEE ANGLE CRACKED. FORMED 'T' ANGLE IAW MD80 SRM 52-05. DRILLED UP AND LOCATED RIB. INSTALLED RIB. INSTALLED 'T' ANGLE PER MD80 SRM 51-30-2. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR JAMB BEAM CORRODED, LEVEL 1. REMOVED JAMB BEAM. CARGO TRACK SUPPORT AT STATION 1219 FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW DOOR JAMB BEAM. INSTALLED CARGO TRACK SUPPORT BRACKET AT STATION 1219. INSTALLED DOOR JAMB BEAM IAW MD80 SRM 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT LEFT FUSELAGE STATION 323 BETWEEN LONGERON 23 AND 24. LOCATED AND DRILLED DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 53-04. (M)

Part: WIRE — BROKEN (CABIN)

DTW - FOUND EMERGENCY PATH LIGHTING NOT WORKING SEAT ROW 16-30. FOUND BROKEN WIRE AT SEAT 18 DEF. RESECURED BROKEN WIRE, OPS CHECK GOOD IAW MD-80 MM 20-50-01. (M)

Part: WIRE — DAMAGED (CABIN)

DTW - FOUND AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPAIRED WIRING AT AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING, OPS CHECKED GOOD IAW MD80 MM 33-53-01. (M)

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

NR 2 ENGINE HAD A COMPRESSOR STALL/PARTIAL POWER FAILURE DURING FINAL APPROACH AND LANDING INTO DTW ENGINE POWER EXCEEDED THAT QA LIMIT BY APPROX .05 FOR IMMEDIATELY PRIOR TO STALL/POWER LOSS. REMOVED AND REPLACED NR 2 ENGINE IAW MM 71-00-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MYR - FOUND EMERGENCY LIGHTS AT SERVICE DOOR AFT CENTER AISLE DON'T ILLUMINATE. TROUBLESHOT AND FOUND BATTERY PACK AT B5-107 TO BE DEFECTIVE REMOVED AND REPLACED BATTERY PACK MM 33-52-00 EMERGENCY LIGHTS OPS CHECK GOOD. (M)

Part: LIMITER — CRACKED (RUDDER)

FLT 931 - MCO - AT 200 KTS AND 31,000 FT, THE RUDDER TRAVEL UNRESTRICTED LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AND LANDED UNEVENTFULLY AT 320 KTS IN DESCENT LIGHT EXTINGUISHED. FOUND HARD LINE FROM SUMP CAN TO RUDDER THROW LIMITER BELLOWS CRACKED. REPLACED WITH FLEX LINE AND OPS CHECKED PER MM 27-20-06. NO DEFECTS NOTED AT THIS TIME. (M)

Part: BATTERY PACK — DISCHARGED (TAIL CONE)

FLL - WHILE PERFORMING WORK CARD 00409 OF A2 CHECK, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED TAIL CONE EMERGENCY BATTERY PACK B5-28 AND SECURED LOGIC CIRCUIT GROUND WIRES TO TERM 3 OF BOTH B527 AND B5-28 BATTERY PACKS, OPS CHECK OK IAW A2 CHK TASK CARD 00409. (M)

Part: CONNECTOR — DIRTY (NLG)

MYR - FLT 1572 - NOSE GEAR WARNING LIGHT ILLUMINATED AT END OF RUNWAY. REMOVED AND CLEANED PROX SWITCH CANNON PLUG. REINSTALLED CANNON PLUG GEAR WARNING. OPS CHECK GOOD PER MM 32-20-00. (M)

Part: CONNECTOR — LOOSE (CABIN)

DTW - FLT 656 - FOUND FLOOR TRACK LIGHTING OUT FROM ROW 16-23. UPON INSPECTION, FOUND LOOSE CONNECTION AT ROW 24. SECURED CONNECTION IAW MD-80 MM 33-53-01. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED. (M)

Part: LIGHT — LOOSE (CABIN)

FLT 572 - DTW - FOUND EMERGENCY LIGHTS NOT ILLUMINATING SEAT ROWS 16 TO 23. RESECURED EMERGENCY PATH LIGHTING ILLUMINATING STRIP TO FLOOR. SYSTEM NOW OPS CHECK GOOD REF 33-53-00 MD-80 MM. (M)

Part: CONTROL VALVE — DISCONNECTED (FLAPS)

FLL - FLAP CONTROL VALVE INPUT ROD DISCONNECTED IN LT MAIN W/W. RECONNECTED FLAP CONTROL VALVE IAW MM 27-52-02. OPS CHECK GOOD. (M)

Part: LIFE VEST — MISSING (CABIN)

FLL - LIFEVEST MISSING FROM SEAT 20F. REPLACED MISSING LIFEVEST IAW MM 25-63-00. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

DTW - FLT 474 - AFTER FLAP RETRACTION SLAT DISAGREE LIGHT CAME ON. LEFT WING HEAVY CONTROLS REQUIRED. PERFORMED OPS CHECK ON STALL AND FLAP SYSTEM IAW MM 34-19-00 AND 27-50-00. PERFORMED RTS AND FLIGHT FAULT REVIEW. NO DEFECTS NOTED. ALSO, PERFORMED SLAT TEST WITH SLAT DISAGREE BOX NO DEFECTS NOTED. OPS TEST GOOD. (M)

Part: CONTROL CABLE — BROKEN (LT FLAP)

FOUND LEFT W/W FLAP CONTROL EXTEND CABLE BROKEN. REMOVED AND REPLACED LEFT W/W FLAP CONTROL EXTEND CABLE IAW MD-80 MM 27-50-00. ALSO, RIGGED AND PERFORMED OPS CHECK IAW MM 27-50-00. (M)

Part: PROXIMITY SWITCH — DIRTY (NLG)

DTW - FLT 521 - AFTER PUSHBACK, NOSE GEAR INDICATOR FLUCTUATED FROM RED TO GREEN. CLEANED PROX SWITCH AND PLUG FOR NOSE GEAR. OPS CHECK GOOD IAW MD-80 MM 32-60-00. NO DEFECTS NOTED AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - EMERGENCY FLOOR TRACK LIGHTING OUT FROM SEAT ROW 15 TO 22. RECONNECTED RIBBON AT ROW 17. OPS CHECKED GOOD PER MD80 33-53-00. NO OTHER DISCREPANCIES NOTED. (M)

Part: LIGHT — INOPERATIVE (ROW 5)

DTW - FLOOR TRACK AISLE LIGHTING ROW 5 FORWARD INOPERATIVE. FOUND LOOSE CONNECTION AT ROW 4. RESECURED CONNECTION. OPS CHECK GOOD PER MD 80 MM 33-50-00. NO OTHER DEFECTS NOTED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLOOR TRACK LIGHTS INOPERATIVE. FOUND WIRES FOR TRIGGER CIRCUIT DISCONNECTED, RECONNECTED WIRES, OPS CHECKS NORMAL IAW MD 80 MM 33-50-00. (M)

Part: LIGHT — INOPERATIVE (ROW 7)

DTW - EMERGENCY PATH LIGHTING NOT WORKING FROM ROW 7 FORWARD OF AIRCRAFT. REPAIRS WIRES EMERGENCY PATH LIGHTING AND OPS CHECK GOOD IAW MM 33-50-00. (M)

Part: PROX SWITCH — FAILED (MLG)

ISP - FLT 755 - WHEN LANDING GEAR WAS RETRACTED AFTER TAKEOFF THE 'RED' NOSE GEAR UNSAFE LIGHT REMAINED ON ACCOMPANIED BY A LOUD AIR NOISE IN THE FORWARD WHEEL WELL. THE A/C WAS NOT PRESSURIZING AND THE CABIN PRESSURE TRANSFER LOCKOUT AND STANDBY LIGHTS WERE ILLUMINATED. SWITCHED TO MANUAL PRESSURIZATION. ALSO, HAD AN 'AUTO SPOILER DO NOT USE' AND 'STALL INDICATION FAILURE' LIGHT ILLUMINATED ON THE ANNUNCIATOR PANEL. WHEN THE GEAR WAS EXTENDED ALL GEAR INDICATED DOWN AND LOCKED, HOWEVER, ALL AURAL WARNINGS BEGAN TO SOUND WHEN FLAPS WERE EXTENDED BEYOND 11 DEGREES. LATER ALL ANNUNCIATOR LIGHTS WENT OUT. A NORMAL LANDING WAS ACCOMPLISHED AT 111,000 LBS USING MANUAL SPOILERS. (M)

Part: ENGINE — FAILED (NR 2)

PBI - FLT 648A - LOUD BANG CLIMBING OUT OF 1400 FEET. NR 2 ENGINE FAILURE. ACCOMPLISHED ENGINE FAILURE CHECKLIST AND SHUTDOWN LIST. RETURNED TO PBI. OVERWEIGHT LANDING (140,00 LBS). (M)

Part: BULB — FAILED (CABIN)

DTW - SEVERAL CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BULBS. EMERGENCY AND STANDBY LIGHTS OPERATION CHECK GOOD IAW WITH MD80 MM 3351 AND 33-52. (X)

Part: ANGLE — CORRODED (BS 1338)

MHV - AFT LEFT LAV CUSP ANGLE AT CENTER OUTBOARD FLOOR LEVEL SHOWS EVIDENCE OF CORROSION. REMOVED DAMAGED PORTION OF LT CUSP STATION 1338 L18. INSTALLED DOUBLER AND EXTRUSION IAW DC9 MD80 SRM 53-14-3, 53-05 FIG 25 AND 51-10-3. (M)

Part: SUPPORT — CORRODED (BS 1129)

MHV - AFT CABIN GH LAB STATION Y1129 LBL 60 FLOOR SUPPORT PLATE 1 LAF CORRODED BEYOND LIMITS. FABRICATED NEW FLOOR SUPPORT PLATE AND INSTALLED IAW MD80 SRM 51-01 AND 51-30-5. (M)

Part: HAT SECTION — CORRODED (BS 1120)

MHV - STATION 1120 LBL 50 SMALL HAT SECTION NEAR GALLEY SERVICE DOOR HAS EXFOLIATION CORROSION AND INTERGRANULAR CORROSION. FABRICATED REPLACEMENT HAT SECTION SUPT PER EXAMPLE SUPPLIED IN REF MD MM 51-10 HEAT TREATED AND AGE HARDENED PER AMS-H-6088 DELIVERED TO A/C FOR FIT AND INSTALL ON W/O A093-S03-Y035. (M)

Part: THRESHOLD — CORRODED (BS 1155)

MHV - STATION 1155 LBL 25-38 APPROX CORROSION TOP AND BOTTOM OF TOP CAP NEAR GALLEY SERVICE DOOR THRESHOLD. REMOVED TOP CAP STATION 1155 ORDERED NEW PART P/N 5930544-97. REINSTALLED PART IAW SRM MD80 51-30-2 LOCATED AND DRILLED PART SRM MD80 51-10-4. (M)

Part: ANGLE — CORRODED (BS 1370)

MHV - STATION 1370 RIGHT LONGERON 18 OUTBOARD CUSP ANGLE HAS EXFOLIATION AT LAV FLOOR ATTACH HOLE. REMOVED DAMAGED CUSP ANGLE FABRICATED REPAIR PARTS FROM S2777976 QQA20013F 202473 EXTRUSION TREATED AND PRIMED REPAIR PARTS IAW SRM MD80 53-05 FIG 25. INSTALLED FILLER AND SPLICES IAW MD80 SRM 53-05 FIG 25. (M)

Part: SUPPORT — CRACKED (BS 1305)

MHV - PREVIOUS REPAIRED PANEL CRACKED AT LIGHTENING HOLE AND RIVETS FS 1305 LEFT SIDE BELOW FLOOR ON SUPPORT. REMOVED PREVIOUS REPAIR CUT OUT DAMAGE FABRICATED REPAIR DOUBLER PO NR B1056 7075T6.050 ALODINED AND PRIMED REPAIR PART IAW MD80 SRM 51-10-3. INSTALLED FASTENERS AND REPAIR PART WET WITH PR1422 SEALANT B.5 PER MD80 SRM 53-01 PAGE 9 FIG 2 SHEET 3 AND MD80 SRM 51-30-2. (M)

Part: WIRE — DAMAGED (ROW 3-6)

ACY - INSTANTLY PRIOR TO DEPARTURE, CAPTAIN FOUND APPROXIMATELY SIX FEET OR FLOOR EMERGENCY LIGHTING OUT. ROW THREE TO SIX. FOUND DAMAGED WIRE HARNESS ROW SIX. REPAIRED WIRES. SYSTEM CHECKS NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FLT 675 - TWO SECTIONS OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. CHARGED BATTERY PACK SYSTEM. OPERATION CHECK GOOD. (M)

Part: CONNECTOR — LOOSE (LT/RT EMER EXIT)

DTW - AFT OVERWING EMERGENCY EXIT LIGHTS LEFT AND RIGHT SIDE (ABOVE PLUG WINDOWS) INOPERATIVE. RESECURED AND CLEANED CONTACTS ON BATTERY PACKS FOR OVERWING LIGHTS ALL CHECKS GOOD. (M)

Part: WIRE — LOOSE (CABIN)

DTW - EMERGENCY FLOOR TRACK LIGHTING NEAR AFT LAVATORY INOPERATIVE. FOUND FLOOR TRACK STRIP DISCONNECTED, RECONNECTED. OPERATIONAL CHECK GOOD IAW MM 33-50-00. (X)