N803NK

Part: BUTTON — SPARKS (PA SYSTEM)

F/A "A" CALL C/P TO INFORM OF "SMOKE SMELL" BEWEEN ROWS 28 PLUS 31. SEEMED TO ORGINATE FROM F/A STATION NR 2 PILOT INFORMED F/A TO PULL ALL C/B`S IN AREA, COFFEE POT (1 & 2). ONE AND HALF MINUTE AFTER PULLING C/B`S, SMELL WENT AWAY. MONITORED AREA FOR ANY TRACK OF SMOKE/FIRE FOR DURATION OF FLIGHT (1HR). AT SOME POINT F/A NOTICED A SPARK NEAR F/A STATIO NR 2 HANDSET AREA, PAX COMPLAINED OF SMOKE BRIEFLY. REST OF FLIGHT NORMAL. REMOVED AND REPLACED MID F/A P/A BUTTON. (M)

Part: RECEIVER — FAILED (VOR-ILS)

GPR POS FAIL EN ROUTE, HEADING INDICATION ON RADAR DISPLAY, AIRCRAFT TAIL SWAP WITH N814NK. PERFORMED OPERATIONAL CHECK OF UNS1K SYSTEM, OPS CHECK GOOD. REMOVED AND REPLACED NR 1 RECEIVER VOR/ILS. OPS CHECK GOOD. (M)

Part: NOZZLE — CRACKED (NR 1 ENGINE)

NR 1 ENGINE NOZZLE HAS A 1 INCH CRACK AT 7 O`CLOCK POSITION NEAR EDGE OF NOZZLE, AIRCRAFT TAIL SWAP WITH N811NK. ACCOMPLISHED EA 7830-0501 IN LEFT THRUST REVERSER OUTBOARD EXTERNAL NOZZLE, INTERIM STOP DRILL REPAIR INSTALLED. LP NR 0299826-2. REMOVED AND REPLACED LEFT THRUST REVERSER ASSEMBLY, OPS CHECK AND LEAK CHECK GOOD. (M)

Part: CHECK VALVE — FAILED (APU)

ON APU START UP BOTH ENGINES WOULD GET ONLY 12 PERCENT N2, APU OIL TEMP HIGH LIGHT CAME ON, TAIL COMPARTMENT HIGH CAME ON, AIRCRAFT TAIL SWAP WITH N834NK. REMOVED AND REPLACED AIRSTART CHECK VALVE, LEAK CHECK GOOD. (M)

Part: ENGINE — DAMAGED

ENGINE WAS REMOVED FROM N803NK FOR INFLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED THE HPC, HPT AND LPT MODULES HAVE HEAVY IMPACT DAMAGE.

Part: PROXIMITY SENSOR — FAULTY (NLG)

ON TAKEOFF, THE GEAR RETRACTED BUT THE NOSE (RED) UNSAFE LIGHT REMAINED ON, AIRCRAFT TAIL SWAP WITH 819NK. T/S FOUND NOSE GEAR DOWNLOCK PROX SENSOR AT MAX CLEARANCE. REMOVED AND REPLACED PROXIMITY SENSOR AND RESHIMMED PROXIMITY SWITCH FOR DESIRED TARGET SENSOR CLEARANCE - PERFORMED BITE CHECK ON NLG. (K)

Part: DOOR — LACK OF LUBE (NLG)

ACY - FLT 341 - AFTER TAKEOFF CYCLED NLG AND HAD A GEAR UNSAFE INDICATION AND A LOUD NOISE FROM GEAR DOORS BEING OPEN, DID A FLY BY AND TOWER NOTICED GEAR RETRACTED WITH GEAR DOORS STILL OPEN AND GEAR LEVER UP. AIRCRAFT RETURN TO ACY AND PERFORMED AN OVERWEIGHT LANDING. LUBED NLG DOOR ASSY AND JACKED NOSE WITH BALLAST WEIGHT AND PERFORMED NOSE GEAR RETRACTION AND EXTENSION. OPS CHECK NORMAL. CHECKED NOSE UPLOCK AND SAFE PROX SIGNAL OK. (M)

Part: ENGINE — FAILED (RIGHT)

FLT 1581 - ACY - ENGINE FAILURE AT FL 240, SURGE ON AIRCRAFT, RIGHT ENGINE FAILED AIRCRAFT YAWED RIGHT, NO FIRE WARNING OR INDICATION. EGT, N1 AND N2 DECREASED RAPIDLY, SHUT DOWN ENGINE AND DIVERTED IN ACY. REMOVED AND REPLACED NR 2 ENGINE. (M)

Part: WINDSHIELD — DELAMINATED (COCKPIT)

TPA - F/O'S WINDSHIELD HAS AREA OF DELAMINATION NEAR BOTTOM AND CENTER, AREA IS APPROX 2.5 BY 4, AIRCRAFT TAIL SWAP. REMOVED AND REPLACED F/O'S SIDE WINDSHIELD. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

FLT 1504 - RSW - UPON L1 DOOR CLOSURE AT PUSHBACK THE SLIDE PACK FELL OFF DOOR. RE-INSTALLED L1 SLIDE PACK ASSEMBLY. (M)

Part: SLIDE — MISINSTALLED (L2 DOOR)

DTW - FOUND CHECK L2 SLIDE FOR CORRECT INSTALLATION. REMOVED AND REPLACED L2 SLIDE PACK. ESCAPE SLIDE REMOVAL AND INSTALLATION. (M)

Part: GUIDE VANE — CRACKED (NR 1 ENGINE)

DTW - NR 1 ENGINE IGV HAS A HAIRLINE CRACK ON THE VANE ATTACHMENT WELD AT THE 3:30 POSITION APPROX 2.750 INCH LONG. REMOVED AND REPLACED IGV. (M)

Part: ENGINE — LEAKING (NR 1)

POSSIBLE FUEL LEAK ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: ISOLATOR — SHIFTED (NR 2 NACELLE)

RSW - FOUND FORWARD LOWER ISOLATOR FOUND SHIFTED ON NR 2 PYLON. REPLACED FORWARD LOWER ISOLATOR. (M)

Part: ENGINE — FAILED (RIGHT)

FOUND RIGHT ENGINE FAILED AT 800 FEET DURING CLIMB-OUT FROM RSW. REPLACED NR 2 ENGINE. (M)

Part: SLIDE — DISLODGED (PAX DOOR)

DTW - FLT 8111 - FOUND LEFT SLIDE PACK FELL OFF DOOR. INSTALLED SLIDE PACK. (M)

Part: GIRT BAR — CONTAMINATED (L2 DOOR SLIDE)

FLT 861 - LGA - FOUND L2 DOOR GIRT BAR WILL NOT UNLOCK FROM THE FLOOR DOOR IS STILL ARMED. UNARMED L2 DOOR REMOVED EXCESS PAINT FROM GIRT BAR AND ATTACH BRACKETS. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

DTW - FOUND SLIDE PACK FELL OFF. REINSTALLED L1 DOOR SLIDE PACK. (M)

Part: WIRE — MISWIRED (EMERGENCY LIGHT)

FOUND O/H EMERGENCY LIGHT AT ROW 30 IS INOPERATIVE. FOUND LIGHT L2-633 WIRED INCORRECTLY. CORRECTED WIRING. (M)

Part: SKIN — DENTED (L1 DOOR)

FOUND DENT ON LOWER EDGE OF L1 DOOR 10 INCHES BY 1 INCH BY .375 INCH. REMOVED DAMAGED 1 INCH BY 23 INCH. FABRICATED 3 DOUBLER AND 5 FILLER. INSTALLED DOUBLER AND FILLER. (M)

Part: NOSE COWL — CRACKED (NR 2 NACELLE)

FTW - FOUND RIGHT INLET COWL HAS TWO CRACKS APPROX 8 INCHES IN LENGTH IN MOUNT RING FLANGE, INTERNALLY AT 4 AND 6 O'CLOCK POSITION. REMOVED NR 2 ENGINE INLET. INSTALLED SERVICEABLE NR 2 ENGINE INLET. (M)

Part: SKIN — DELAMINATED (RT WING SPOILER)

FTW - FOUND RIGHT WING GROUND SPOILER TOP SIDE HAS DENTS AND DELAMINATED. REPAIRED TWO DELAMINATIONS. (M)

Part: SKIN — DELAMINATED (LT WING SPOILER)

FOUND LT WING INBOARD FLIGHT SPOILER TOP SIDE HAS DENTS AND AREA OF DELAMINATED. REPAIRED DELAMINATED AREA. (M)

Part: SKIN — DENTED (RT WING SPOILER)

FTW - FOUND RIGHT WING OUTBOARD FLIGHT SPOILER BOTTOM SIDE DENTED/DELAMINATED. REPAIRED BOTTOM SIDE OF OUTBOARD FLIGHT SPOILER. (M)

Part: SKIN — DELAMINATED (RT WING SPOILER)

FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER TOP SIDE HAS DENTS AND AREAS OF DELAMINATED. REPAIRED AREA OF DELAMINATED. (M)

Part: STOP FITTING — CORRODED (CARGO DOOR)

FTW - FOUND FORWARD PIT LOWER DOOR STOP FITTING CRACKED AND DOOR STOP CORRODED. REMOVED CRACKED FITTING. INSTALLED NEW DOOR STOP FITTING. (M)

Part: SLIDE — DEPLOYED (L1 DOOR)

FTW - DEPLOYED L1 DOOR SLIDE FOR FUNCTIONAL CHECK. (M)

Part: GIRT BAR — DAMAGED (GALLEY DOOR)

ACY - FLT 341 - FORWARD GALLEY DOOR GIRT BAR CAN NOT BE REMOVED FROM ARMED POSITION. CLEANED DEBRIS FROM GIRT BAR RECEIVING LATCH AND LUBRICATED. (M)

Part: COVER — DISLODGED (R1 DOOR SLIDE)

ACY - R1 SLIDE PACK COVER FELL OFF. REPOSITIONED AND RESECURED R1 SLIDE PACK COVER. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

FLL - FLT 1174 - BURNING SMELL IN CABIN TWICE ONCE AT TAKEOFF AGAIN AT 18000 FT CARGO SMOKE DETECTOR FAILED TEST FAILURE LIGHTS AND FIRE DETECTOR LOOP LGHT REMAINED ON FOR DURATION OF FLIGHT TEST OK AT GATE ON GROUND POWER. PERFORMED INSPECTION OF CARGO AREA BAYS AND CABIN AREA FOR SMOKE WITH ENG RUNNING AND PACKS ON, NO SMOKE OR SMELLS NTOED ALSO PERFORMED, OPS CHECK OF CARGO SMOKE DETECTOR SYSTEM, TEST FUNCTION OK. (M)

Part: SLIDE — DISLODGED (L2 DOOR)

FLT 503 - DTW - L2 SLIDE PACK FELL OFF. FOUND SLIDE PACK COVER LANYARD DISCONNECTED, REINSTALLED LANYARD. (M)

Part: SLIDE — LOOSE (L1 DOOR)

DTW - FLT 599 - FOUND L1 SLIDE PACK NEEDS TO BE SECURED. RESECURED L1 SLIDE PACK. (M)

Part: SLIDE — UNSECURE (R1 DOOR)

R1 DOOR SLIDE PACK FELL OFF DOOR. INSTALLED R1 DOOR SLIDE PACK COVER.

Part: COVER — CRACKED (ESCAPE SLIDE)

R1 DOOR SLIDE PACK FELL TO THE GROUND AND HOUSING IS CRACKED. REMOVED AND REPLACED R1 DOOR SLIDE PACK.

Part: LANYARD — DISCONNECTED (L2 DOOR SLIDE)

L2 DOOR SLIDE PACK NEEDS REATTACHED. REATTACHED L2 SLIDE PACK LANYARD.

Part: SLIDE — DISLODGED (R1 DOOR)

FLL - FLT 433 - FOUND SLIDE PACK FELL OUT OF R1 DOOR INTO CABIN. SECURED SLIDE AT R1 DOOR. (M)

Part: ISOLATOR — OUT OF LIMITS (NR 1 ENGINE)

NR 1 ENGINE FORWARD LOWER VIBRATION ISOLATION MOUNT OUT OF LIMITS. REMOVED AND REPLACED FORWARD LOWER VIBRATION ISOLATOR. (M)

Part: ACCOUSTIC LINER — DAMAGED (NR 1 ENGINE)

DTW - FOUND ACCOUSTIC LINE DAMAGE AT 12 O'CLOCK POSITION ON NR 1 ENGINE REAR FAN CASE SECTION. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: RETAINER — BROKEN (SLIDE COVER)

FLL - FOUND LEFT AFT SLIDE PACK COVER GIRT BAR RETAINING CLIP BROKEN. REMOVED AND REPLACED LEFT AFT SLIDEPACK COVER GIRT BAR RETAINING CLIP. OPS CHECK GOOOD. (M)

Part: FIRE LOOP — FAULTY (LT ENGINE)

DTW - FLT 631 - ON FINAL INTO TPA, NR 1 ENGINE A-LOOP FLICKERED WITH NO ASSOCIATED WARNING EXCEPT M-CAUTION FLICKERED ONCE FOR 2 SECONDS, SELECTED B-LOOP AND EXECUTED TEST. TEST WAS NORMAL. REMOVED AND REPLACED LEFT ENGINE FIRE LOOP. (M)

Part: SLIDE — DISLODGED (R1 DOOR)

R1 DOOR SLIDE FOUND ON GALLEY FLOOR DURING DAILY INSPECTION. REMOVED AND REPLACED R1 SLIDE PACK.

Part: SLIDE — DAMAGED (R1 DOOR)

FLL - R-1 DOOR EMERGENCY/ESCAPE SLIDE WILL NOT STOW PROPERLY, GIRT OPENING DRAGS. REMOVED AND REPLACED R-1 DOOR EMERGENCY/SLIDE. (M)

Part: BLADE — DAMAGED (COMPRESSOR)

L/P 60611-3 NR ENG DAMAGE ON FAN BLADE. L/P 60612-1 NR 2 ENG FWD OF REAR CLAM SHELL ACOUSTIC LINER DAMAGED AT 12 OCLOCK POSITION TO 9 OCLOCK POSITION. L/P 60612-3 NR 2 ENG FOUND ACOUSTIC LINER DAMAGE JUST AFT OF IGV, FWD OF C1, 12 OCLOCK POSITION. C/A: L/P 60611-3 REPAIRED FAN BLADE. REPAIRS TEST 1 FOR FINAL RETURN SERVICE. L/P 60612-1 (TRANSFERRED TO NEW SDR FORM GTIA03-0313 ON CARRYOVER) L/P 60612-3 REPAIRED NR 2 ENG ACOUSTIC LINER JUST AFT OF IGV, FWD OF C1 12 OCLOCK POSITION.

Part: SLIDE — DISLODGED (CABIN)

RIGHT 1 SLIDE PACK CAME OFF WHEN DOOR WAS OPENED AND LOCKED BACK DIFFICULT TO LOCK BACK. INSTALLED NEW SLIDE PACK RT 1 DOOR. NO OTHER DEFECTS NOTED. DOOR OPEN LATCH OPS CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

INTERCOASTAL STA 1346 RBL 18 HAS CORROSION UPPER AND LOWER SURFACE, IN RIGHT AFT LAV AREA. FABRICATED REPAIR DOUBLER 1 EA AND FILLER 1 EA. INSTALLED REPAIR.

Part: INLET GUIDE VANE — CRACKED (NR 2 ENGINE)

MCO - FOUND LEFT NR 2 ENGINE 10 O'CLOCK POSITION FACING FRONT OF ENGINE CRACK ON IVG NEAR BASE APPROXIMATELY 2 INCHES IN LENGTH UNABLE TO STOP DRILL. REMOVED AND REPLACED THE NR 2 ENGINE IGV. (M)

Part: LANYARD — MISSING (ESCAPE SLIDE)

FTW - FOUND TAILCONE ESCAPE SLIDE LANYARD MISSING. INSTALLED LANYARD. (M)

Part: WIRE — DAMAGED (TAIL BAY)

FTW - FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT, DO NOT COME ON WITH EMERGENCY POWER. FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT NOT CONNECTED. SPLICED WIRING FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT. (M)

Part: RIB — CRACKED (HORIZONTAL STAB)

FTW - FOUND LT INBOARD HORIZONTAL STABILIZER INBOARD RIB FLANGE WAS A 3 INCH CRACK. REMOVED DAMAGED AREA AT RIB FLANGE. FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHTS)

FTW - FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT ROW 2, 4, 5, 7, 9, 11, 15, 19, 21, 22, 29, 30 AND 32. REPAIRED WIRING. (M)

Part: FLOORBEAM — BROKEN (CABIN)

FTW - FOUND PASSENGER CABIN CENTER FLOORBEAM BETWEEN STATION 537 AND 615 BROKEN PLACES. REMOVED PASSENGER CABIN CENTER FLOORBOARD. FABRICATED FLOORBOARD. INSTALLED PASSENGER CABIN CENTER FLOORBOARD. (M)

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB)

FTW - FOUND LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE CRACKED, APPROXIMATELY 1 INCH. REMOVED LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE. NEW FORMED ANGLE. INSTALLED LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE. (M)

Part: FLAP TRACK — CRACKED (RT WING)

FTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD TRACK, HINGE FITTING STUD HOLE HAS A CRACK. REMOVED REPAIR DOUBLERS. LOCATED AND DRILLED -44 AND -46, REPAIR DOUBLERS. INSTALLED 44 AND 46 DOUBLERS. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

FTW - FOUND L-1 DOOR UPPER FRAME CRACKED IN FORWARD AND AFT RADIUS. STOP, DRILLED AFT AND FORWARD SIDE AT L-1 DOOR UPPER FRAME. INSTALLED FITTINGS AND DOUBLER. (M)

Part: SUPPORT BRACKET — CORRODED (E/E BAY)

FTW - FOUND E/E COMPARTMENT TWO RIGHT INBOARD LATCH SUPPORT BRACKETS CORRODED. FOUND RIGHT OUTBOARD AFT LATCH SUPPORT BRACKET TO BE OUT OF LIMITS. REMOVED FRAME RIGHT STATION 148 LONGERON 28. FOUND FRAME RIGHT STATION 148 LONGEORN 28 TO BE OUT OF LIMITS. FORMED NEW SECTION OF FRAME. INSTALLED NEW SECTION OF FRAME. INSTALLED NEW BRACKET RIGHT OUTBOARD AFT LATCH SUPPORT. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

FTW - FOUND L1 DOOR 2ND FRAME LOWER FRAME AFT RADIUS CRACKED. STOP DRILLED END OF BEAM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FLIGHT COMPARTMENT SUB FLOOR IS CRACKED 2 PLACES BELOW CAPTAINS MID/LOWER SEAT TRACK STATION 135, 160, CORRODED AT STATION 133-160 AS VIEWED FROM E/E COMPARTMENT. REMOVED COCKPIT FLOOR WEB FROM STATION 133, 160 LBL 40 RBL 20. FABRICATED NEW FLOOR WEB FS 133-160 LBL 40 RBL 20. INSTALLED COCKPIT FLOOR WEB. (M)

Part: FLOOR PANEL — DETERIORATED (CABIN)

FTW - FOUND CABIN FLOOR PANEL STATION 769-826 LEFT DETERIORATING, MISSING INSERT. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

FTW - FOUND FLOOR PANEL STATION 1079-1155 LEFT INBOARD HAS CRACK/SOFT CORROSION AT INSERTS AND ELONGATED HOLES. FABRICATED NEW FLOOR PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND FS 835-853 LBL 44 INCHES TO 45 INCHES CORRODED ON WEB WITH CRACKS IN WEB UNDER OUTBOARD SEAT TRACK. REMOVED CORRODED AREAS AND CRACKED AREAS. FABRICATED/LOCATED/DRILLED DOUBLER AND FILLER. INSTALLED PARTS. (M)

Part: FLOOR PANEL — CORRODED (CABIN)

FTW - FOUND CABIN FLOOR PANEL STATION 693-769 LEFT, DENTED AND CORRODED. FABRICATED NEW FLOOR PANEL. (M)

Part: PANEL — DELAMINATED (RT WING TE)

FTW - FOUND RIGHT WING UPPER TRAILING EDGE PANEL HAS COMPOSITE MATERIAL EXPOSED AND PANEL IS DELAMINATED ON LOWER SIDE. REMOVED DAMAGED PANEL. REPAIRED RIGHT WING UPPER TRAILING EDGE INBOARD PANEL. INSTALLED WING PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 693-769 LEFT HAS CORROSION AND LOOSE TORN INSULATION. REMOVED OLD SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR PANEL STATION 796-826 LEFT OUTBOARD HAS CORROSION. INSTALLED NEW SKIN PANEL. (M)

Part: FLOOR PANEL — DENTED (CABIN)

FTW - FOUND LEFT INBOARD FLOOR PANEL STATION 1271 TO STATION 1309 INBOARD FACE HAS DENTED/DAMAGES AND CRACKED SEVERAL AREAS. FABRICATED PANEL. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

FTW - FOUND FLOOR PANEL STATION 1271-1309, RIGHT SIDE INBOARD HAS CRCKED/DAMAGED AT BOTTOM PANEL. FABRICATED NEW PANEL. (M)

Part: FLOOR PANEL — DETERIORATED (CABIN)

FTW - FOUND CENTER FLOOR PANEL STATION 1309 TO STATION 1338 HAS SOFT/MUSHEY DETERIORATED, LOCATED AND DRILLED. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND AT FS 795 LB2 44A CRACK IN FLOOR WEB 2 INCHES LONG FROM EOP TO LIGHTENING HOLE, AT FS 795 LBL 44 A PIECE OF FLOOR WEB 1 INCH BY .500 INCH MISSING, AT FS 800 LBL 44 A TOOL MARK OF .75 INCH BY .75 INCH WITH HOLE IN WEB. REMOVED DAMAGED AREAS. FABRICATED, LOCATED AND DRILLED DOUBLERS AND FILLE. INSTALLED DOUBLER AND FILLER. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FOUND CENTER FLOOR PANEL STATION 1271 TO STATION 1309 HAS CRACKED, SOFT/MUSHEY, CORRODED AT INSERTS ELONGATED HOLES. DRILLED AND LOCATED NEW PANEL. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, LOWER SIDE OF 'Z' FRAME AT FS 1258 AT L18L. REMOVED DAMAGED AREA OF 'A' FRAME. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER, FILLER. (M)

Part: FRAME — BULGED (BULKHEAD DOOR)

FTW - FOUND AFT PRESSURE BULKHEAD VAULT DOOR JAMB LOWER FRAME HAS CORROSION BULGE RBL 9 INCHES AT FLOOR LINE. FORMED NEW REPAIR AT LOWER JAMB. INSTALLED NEW REPAIR, FILLER AND DOUBLER. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN FLOOR WEB STATION 200-218 CORRODED. FABRICATED NEW WEB. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 1332-1352, BETWEEN LONGERONS 21R AND 23R, (X=096, D=1) DX=10.41. FABRICATED INNER DOUBLER. INSTALLED INNER DOUBLER. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

FTW - FOUND AFT PRESSURE BULKHEAD FORWARD SIDE FRAME SHEAR TIE BENT AND CRACKED LBL 31 INCHES WL 84 INCHES STRINGER 5L. REMOVED/CUTOUT DAMAGED SHEAR TIE. FABRICATED REPAIR SECTION, COMPLETED REPAIR INSTALLATION. (M)

Part: FLOOR PANEL — CORRODED (CABIN)

FTW - FOUND AFT PIT FLOOR PANEL STATION 1007-1155 DELAMINATED AND CORROSION. FABRICATED NEW FLOORBOARD. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT FS 93 BETWEEN LONGERONS 18 AND 19L IS TOO CLOSE TO STRUCTURE (X=.034, D=1.0) DX=29.41. CUTOUT DENTED/DAMAGED AREA (2 PLACES) AT FS 93 AND FS 96. FABRICATED REPAIR DOUBLER AND FILLERS. INSTALLED FABRICATED REPAIR DOUBLER AND FILLER. (M)

Part: PANEL — CORRODED (LT ELEVATOR LE)

FTW - FOUND LEFT L/E ELEVATOR PANEL HAS CORROSION ALL OVER. FORMED NEW PART. INSTALLED LEFT L/E ELEVATOR PANEL. (M)

Part: WEB — DAMAGED (FUSELAGE)

FTW - FOUND LEFT CABIN FLOOR WEB CORRODED AND BROKEN AT SIDEWALL STATION 218-237. PASSENGER CABIN STATION 218 TO STATION 237 MEMBRANE WEB IS CRACK/PUNCTURE LBL 44. REMOVED MEMBRANE WEB. FABRICATED NEW MEMBRANE WEB. INSTALLED NEW MEMBRANE WEB. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

FTW - FOUND LEFT MLG, FORWARD DOOR JAMB HAS CRACK AT AFT BRACKET SUPPORT IN INTERCOSTAL. REMOVED CRACKED INTERCOSTAL SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M)

Part: SKIN — GOUGED (PAX DOOR)

FTW - FOUND OUTSIDE BOTTOM EDGE OF L1 DOOR IS GOUGED, DENTED AND CRACKED. REMOVED LOWER SKIN ATTACH ANGLE. ANGLE FOUND TO BE CRACKED. FABRICATED NEW ANGLE. REMOVED DAMAGE AT FORWARD LOWER CORNER. FABRICATED 7 REPAIR FILLER. FABRICATED 5 REPAIR DOUBLER. INSTALLED REPAIR PARTS AND ATTACH ANGLE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER SEAT TRACK CORRODED AT FS 1026-1309, LEFT SIDE OUTBOARD TRACK. (M)

Part: DOOR — DELAMINATED (MLG)

FTW - FOUND RIGHT MAIN LANDING GEAR FLYING DOOR DELAMINATED. REMOVED RIGHT MAIN LANDING GEAR OUTBOARD GEAR DOOR. REPAIRED DELAMINATED AREA. INSTALLED RIGHT MLG DOOR. (M)

Part: WEB — CORRODED (PAX DOORWAY)

FTW - FOUND L1 DOOR WEB STATION 200-208 CORRODED. FABRICATED L-1 DOOR WEB. (M)

Part: PANEL — DELAMINATED (LT WING)

FTW - FOUND LT WING TRAP PANEL DELAMINATED. REMOVED LT WING TRAP PANEL. REPAIRED LT WING TRAP PANEL. INSTALLED LT WING TRAP PANEL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER SEAT TRACK CORRODED AT FS 826-840, 850-880, 893-927, 933-955, 965-984, 994-1003 RIGHT SIDE OUTBOARD TRACK. FOUND ONE AREA BETWEEN STATION 896 AT TO BE DAMAGED BEYOND LIMITS. CUT OUT RIGHT OUTBOARD SEAT TRACK FROM STATION 877-917. FABRICATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PASSENGER SEAT TRACK CORRODED AT FS 613-840, LEFT SIDE OUTBOARD TRACK. LEFT SIDE OUTBOARD TRACK FROM STATION 734-854 IS OUT OF LIMITS. REMOVED LEFT OUTBOARD SEAT TRACK. FABRICATED DRILLED AND LOCATED NEW TRACK SECTION AND SPLICES. INSTALLED NEW TRACK SECTION AND SPLICES. (M)

Part: FLOORBOARD — CORRODED (CABIN)

FTW - FOUND CABIN FLOORBOARD STATION 927-1300 BENT, TORN, CORRODED. FABRICATED NEW FLOORBOARD. (M)

Part: DOOR FRAME — DENTED (PAX DOOR)

FTW - FOUND R1 DOOR CUTOUT FRAME DENTED MIDWAY DOWN AFT AREA. REMOVED DOOR JAMB PAN. LOCATED AND DRILLED NEW PANEL. INSTALLED DOOR PAN. (M)

Part: DOOR FRAME — CRACKED (MLG)

FTW - FOUND LEFT MLG FORWARD DOOR JAMB CUTOUT DOUBLER REPAIR CRACKED. REMOVED DAMAGE AREA. FABRICATED CHANNEL. FABRICATED SPLICE TWO EACH. INSTALLED REPAIR PARTS. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FTW - FOUND PASSENGER SEAT TRACK CORRODED AT FS 613-840 LEFT SIDE OUTBOARD TRACK. LEFT SIDE OUTBOARD TRACK FROM STATION 734-854 IS OUT OF LIMITS. REMOVED LEFT OUTBOARD SEAT TRACK. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK SECTION AND SPLICES. INSTALLED NEW TRACK SECTION AND SPLICES. (M)

Part: FLOOR PANEL — DETERIORATED (CABIN)

FTW - FOUND CABIN FLOOR PANEL STATION 927-1003 DETERIORATED, DRILLED AND LOCATED. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT CRACKED FLOOR INTERCOSTAL AT FS 1271-1287 '0'BL. LOCATED AND DRILLED PART. INSTALLED INTERCOSTAL. (M)

Part: FLOORBOARD — BROKEN (CABIN)

FTW - FOUND CABIN FLOORBOARD RIGHT STATOIN 869-886 CORNER BROKEN, CORROSION. FABRICATED PANEL. (M)

Part: PANEL — CRACKED (PAX DOOR)

FTW - FOUND FORWARD PASSENGER DOOR HAS CRACK ON DOOR PANEL ASSEMBLY LOWER FORWARD EDGE OF DOOR AT LOWER HINGE. DRILLED OFF CRACKED PANE ASSEMBLY. LOCATED AND DRILLED NEW PANEL. INSTALLED NEW PANEL. (M)

Part: DOUBLER — CRACKED (MLG DOOR)

FTW - FOUND RIGHT MLG WING DOOR FORWARD LOWER DOUBLER IS CRACKED. REMOVED REPAIR DOUBLER. FABRICATED NEW DOUBLER. INSTALLED NEW DOUBLER. (M)

Part: DOOR FRAME — CORRODED (CARGO BAY)

FTW - AFT CARGO DOOR JAMB LOWER, HAS CORROSION UNDER SET SCREW PLATES AND THROUGH PUT LENGTH OF DOOR JAMB. REMOVED AFT CARGO DOOR JAMB BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED JAMB BEAM. (M)

Part: FLOORBOARD — BROKEN (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 886-946 CENTER, BROKEN OUT INSERTS, CORROSION ON METAL SUPPORTS. FABRICATED PANEL. (M)

Part: BEAM — CORRODED (CARGO DOORWAY)

FTW - FOUND MID PIT CORROSION AT 2 ANGLE FORWARD RIGHT SIDE STATION 636 TO STATION 598. MID PIT LOWER DOOR CUTOUT OUTBOARD BEAM CORRODED STATION 693 TO STATION 636. REMOVED JAMB BEAM. LOCATED AND DRILLED BEAM. INSTALLED MID PIT LOWER DOOR JAMB BEAM. (M)

Part: FLOORBOARD — CORRODED (CABIN)

FTW - FOUND CABIN FLOORBOARD STATION 826-886, DETERIORATED, METAL SUPPORTS HAVE GOUGES, CORROSION, TORN. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (CABIN)

FTW - FOUND CABIN LEFT OUTBOARD FLOORBOARD STATION 807-916, HAS CORROSION ELONGATED HOLES, TORN INSULATION, BENT CORNERS. REMOVED OLD SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN. (M)

Part: FLOORBOARD — BROKEN (CABIN)

FTW - FOUND CABIN FLOORBOARD RIGHT STATION 826-844 BROKEN OUT INSERTS, CORROSION. FABRICATED NEW PANEL. (M)

Part: FLOORBOARD — CORRODED (CABIN)

FTW - FOUND CABIN FLOORBOARD LEFT INBOARD STATION 864-886 INSERTS PULLED THROUGH, CORROSION. LOCATED AND DRILLED FLOORBOARD. (M0

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CUSP WEB CORRODED AT STATION 220 LBL 54 AT FRAME. REMOVED CUSP STAITON 180-230 L18L. FABRICATED NEW SECTION OF CUSP AND SPLICE TO 230 LBL 54. INSTALLED CUSP SECTION AND SPLICE. (M)

Part: DOOR FRAME — CRACKED (MLG)

FTW - FOUND RIGHT WHEEL WELL FORWARD INBOARD DOOR FRAME IS CRACKED. REMOVED DAMAGE. LOCATED AND DRILLED U-CHANNEL AND SPLICES. INSTALLED U-CHANNEL AND SPLICES. (M)

Part: FLOORBOARD — BROKEN (CABIN)

FTW - FOUND CABIN FLOORBOARD STATION 927-1003 NR 5 CORNER BROKEN CORRODED. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT CRACKED FLOOR INTERCOSTAL AT FS 1287-1309 '0' BL. REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED NEW FABRICATED INTERCOSTAL. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 140-199 NR 5 DETERIORATED, LOCATED AND DRILLED. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - MAIN CABIN FLOORBOARD STATION 120-140 NR 3 DETERIORATED BLUE WATER STAINS. DRILLED AND LOCATED. (M)

Part: FLOOR PANEL — BROKEN (CABIN)

FTW - FOUND FLOOR PANEL MAIN CABIN STATION 198-250 NR 5 FIBERGLASS SUPPORT BROKEN AT ENDS. REPAIRED FLOOR PANEL. (M)

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 120-140 NR 2 DETERIORATED. DRILLED AND LOCATED PANEL. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND MAIN CABIN FLOORBOARD STATIN 140-199 NR 3 DETERIORATED. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 198-250 NR 4 MISSING INSERTS, DETERIORATED. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 198-250 NR 5 HAS CORRODED INSETS AND DETERIORATING BOARD. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOORBOARD — DETERIORATED (CABIN)

FTW - FOUND MAIN CABIN FLOORBOARD 199-250 NR 2 DETERIORATING AND BLUE WATER STAINS. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — DAMAGED (CABIN)

FTW - FOUND FLOOR PANEL MAIN CABIN STATION 198-250 NR 6 BROKEN FIBERGLASS SUPPORTS BLUE WATER STAINS, DETERIORATED. REPAIRED FLOOR PANEL. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 140-199 NR 5 MISSING INSERTS, DETERIORATING. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 120-140 NR 4 DETERIORATED, LOCATED AND DRILLED. (M)

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

FTW - FOUND MAIN CABIN FLOORBOARD STATION 120-140, NR 1 DETERIORATED. DRILLED AND LOCATED PANEL. (M)

Part: DOOR FRAME — CORRODED (CARGO BAY)

FTW - FOUND FORWARD CARGO LOWER DOOR JAMB HAS CORROSION UNDER DOOR STOP SET SCREW PLATES, UNDER SEALANT AND ENTIRE LENGTH OF DOOR AREA. REMOVED LOWER DOOR PAN SECTION. INSTALLED LOWER DOOR PANEL SECTION. (M)

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT)

FTW - FOUND AFT OVERWING EXIT RIGHT FORWARD INSIDE EDGE OF FRAME IS CRACKED. FABRICATED DOUBLERS REPAIR. INSTALLED DOUBLERS REPAIR ON INNER SKIN AND DOOR PANEL. (M)

Part: SKIN — GOUGED (LT WING LE FLAP)

FTW - FOUND LEFT WING INBOARD FLAP INBOARD LEADING EDGE CAP GOUGED. FABRICATED NEW PART. REMOVED LEFT INBOARD LEADING EDGE CAP. INSTALLED LEFT LEADING EDGE INBOARD FLAP NEW CAP. (M)

Part: DOOR FRAME — DAMAGED (PAX DOOR)

FTW - FOUND L1 DOOR AFT LOWER INSIDE LIGHTING HOLE HAS 1 INCH CRACK AND METAL DAMAGE. REMOVED AFT LOWER WEB. DRILLED/LOCATED NEW WEB. INSTALLED AFT LOWER WEB. (M)

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

FTW - FOUND LEFT COCKPIT FLOORBOARD STATION 120-183 DETERIORATED. FABRICATED NEW LEFT COCKPIT FLOORBOARD FS 120-183. (M)

Part: WEB — CORRODED (SUBFLOOR)

FTW - E/E COMPARTMENT SUBFLOOR WEB IS CORRODED AT STATION 206, LBL 12 STATION 196, LBL 6, STATION 200 RBL. REMOVED DAMAGED FLOOR WEB FS 200 FS 219 LBL 26 - RBL 26. FABRICATED NEW FLOOR WEB FS 160-200 LBL 16 - RBL 54. FABRICATED NEW FLOOR WEB FS 200-219 LBL 26 - RBL 26. FABRICATED FLOOR WEB REPAIR SPLICE REPAIR FS 160-200 LBL 26. INSTALLED SPLICE FOR WEB REPAIR. INSTALLED FLOOR WEB STATION 160-200 LBL 16 - RBL 54. INSTALLED FLOOR WEB STATION 200-219 LBL 26 - RBL 26. (M)

Part: ENGINE — FAILED (NR 1)

ACCOMPLISHED EMERGENCY LANDING, NO INCIDENT. AT 1900 VERY LOUD BANG THROUGHOUT AIRCRAFT, NR 1 ENGINE LOST POWER, N1 AND N2 STILL ROTATING, TRIED RELIGHT, NO RELIGHT. REMOVED AND REPLACED NR 1 ENGINE.

Part: SWITCH — FAILED (FLAPS AND SLATS)

ON FINAL, FLAPS 28 DEGREES, SLATS LANDING AT VREF PLUS 10, SLAT DISAGREEMENT AND LANDING LIGHT STARTED CYCLING BACK AND FORTH RECEIVED A STICK SHAKER AND EXECUTED GO AROUND. LEVEL AT 200 KIAS, 15 DEGREE FLAPS, THE SLAT INDICATION WAS CYCLING BETWEEN TAKEOFF, DISAGREEMENT. FOUND NO CHECK LIST ON Q/H APPLICABLE. COME BACK AROUND, FLAPS 40 DEGREE WITH REF PLUS 20, SLATS STAY IN LANDING UNTIL SLOWED IN FLAIR AND THEN CYCLED AGAIN. FOUND BAD LT WING SLAT "D" SWITCH. R/R LT WING SLAT "D" PROX SENSOR AND R/R RT WING SLAT "D" SWITCH AS PRECAUTIONARY. OPS CHECK GOOD PER MM. PERFORMED BIT CHECK ON BOTH STALL WARNING COMPUTERS. PER MM. OPS CHECKED GOOD. PERFORMED TEST ON PROX ELECT UNIT PER MM. OPS

Part: COMPUTER — INOPERATIVE (COCKPIT)

FLL - FLT 380 - NR 2 DFGS SELECTED, AUTO THROTTLE INOPERATIVE, FRO FD INTERMITTENTLY INOPERATIVE. REMOVED AND REPLACED NR 2 DFGC PER MM 22-01-01 SYSTEM TESTS NORMAL PER MM 22-01-05. AUTO THROTTLE TEST NORMAL PER MM 22-31-00. (M)

Part: PANEL — CRACKED (RT WING)

ACY - RIGHT WING LOWER TRAILING EDGE PANEL CRACKED BOTTOM SIDE INBOARD. PERFORMED MULTIPLE LAMINATION REPAIR ON RIGHT LOWER TRAILING EDGE PANEL BOTTOM INBOARD IAW 57-70-1 OF THE DC9/MD80 SRM. (M)

Part: PANEL — CRACKED (LT WING)

ACY - FOUND LEFT WING LOWER TRAILING EDGE PANEL CRACKED BOTTOM SIDE. PERFORMED MULTIPLE LAMINATION REPAIR ON LEFT LOWER TRAILING EDGE PANEL BOTTOM INBOARD IAW DC9/MD80 SRM 57-70-1. (M)

Part: CONTROL PANEL — FAILED (COCKPIT)

MCO - FLT 506 - INTERMITTENT AUTOTHROTTLE DISCONNECT ON APPROACH. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL, SYSTEM OPS CHECKS GOD IAW MD80 MM 22-01-05. (M)

Part: INDICATOR — OSCILLATES (NR 1 EPR)

FLL - FLT 380 - NR 1 EPR PERIODICALLY OSCILLATES BETWEEN .77 AND 2.2 DURING CRUISE AND DESCENT WITH IDLE POWER OSCILLATIONS CAUSE AUTO THROTTLES TO TRIP OFF. REMOVED AND REPLACED NR 1 EPR INDICATOR, OPS CHECK GOOD PER MM 72-00-00. (M)

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT)

MCO - FLT 594A - AUTO THROTTLE TURNED OFF ON APPROACH WHEN SPEED WAS CHANGED AUTO PILOT 2. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER IAW MD80 MM 22-13-00. OPS CHECK GOOD AT THIS TIME. (M)

Part: CONTROLLER — FAILED (AUTOTHROTTLE)

MCO - FLT 594A - AUTO THROTTLE TURNED OFF ON APPROACH WHEN SPEED WAS CHANGED AUTO PILOT 2. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER, OPS CHECK GOOD AT THIS TIME. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

RSW - FLT 926 - STABILIZER WARNING SOUNDED ON TAKEOFF ROLL, REJECTED TAKEOFF AT 10 KTS. PERFORMED TAKEOFF WARNING SYSTEM IAW MM 27-00-00. NO DEFECTS NOTED. (M)

Part: ENGINE — FAILED (NR 2)

ENGINE SHUTDOWN, RIGHT ENGINE FAILURE DURING DEPARTURE. VIBRATION FOLLOWED RAPID ROLLBACK. AFTER FAILURE NR 1, 12 PERCENT, NR 2, 25 PERCENT EGT WENT OVER 800 DEGREES RETURNED TO 200 DEGREES. COMPLETED ENGINE FAILURE CHECKLIST DECLARED EMERGENCY, LANDED AT ACY EVACUATED AC ON RECOMMENDATION OF FIRE/RESCUE PERSONNEL. (QRH PROCEDURES) REMOVED AND REPLACED NR 2 ENGINE.

Part: SENSE LINE — CRACKED (ENGINE)

FLL - FLT 380 - ON TAKEOFF ROLL, THE THROTTLES MATCHED N1 BUT THE EPRS WERE OFF, NR 1 1.70, NR 2 1.99, UPON PUSHING NR 1 THROTTLE UP TO MATCH EPRS THE NR 1 N1 WENT TO 101, ABORTED AT SPEED 105 MAX. PERFORM OPERATIONAL CHECK ON NR 1 ENGINE EPR INDICATION. PERFORMED TROUBLESHOOTING PER MM 77-11-01. FOUND VERY LOOSE B-NUT AT PT7 LINE JUNCTION. TIGHTENED B-NUT, CHECKED ALL LINES FOR SECURITY AND CHECKED ALL FITTINGS, PT2 AND PT7 LINES LEAK CHECK OK. ITEM DUE OPS CHECK ON R/U SEE ITEM 31267-1. FOUND 2 PT7 LINES CRACKED AND LEAKDING REMOVED AND REPLACED LINES ALSO TRIMMED NR 1 AND NR 2 ENGINE PER MM 71-00-00 OPS AND LEAK CHECK OK. (M)

Part: BATTERY — DISCHARGED (CABIN)

DTW - FLT 461 - FOUND EMERGENCY CEILING LIGHTS INOPERATIVE AT AFT OVERWING EXIT DOOR. REMOVED AND REPLACED BATTERIES. OPS OK PER MM 33-53-00. (M)

Part: BATTERY — DISCHARGED (CABIN)

FLT 461 - DTW - FOUND EMERGENCY CEILING LIGHTS INOPERATIVE BETWEEN SEATS 6 THROUGH 9. REMOVED AND REPLACED BATTERIES AND CLEANED CONTACTS OF BATTERY PACK CLIPS, OPS OK ON CHECK PER MM 35-53-00. (M)

Part: BATTERY — DISCHARGED (CABIN)

FLL - FLT 9803 - ON CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM STATION 845 THROUGH 1155. REPLACED BATTERIES IN BATTERY PACKS B5-73, B5-26 AND B5-58. REPLACED BATTERY PACK B5-26, STATION 1079 REF MM 33-53-00, OPS CHECK OK. (M)

Part: AMPLIFIER — FAILED (COCKPIT)

DTW - FLT 56 - AUTO THROTTLE WILL NOT ENGAGE. FOUND NR 1 INSTRUMENT AMP BAD. REMOVED AND REPLACED NR 1 INSTRUMENT AMP. (M)

Part: WIRE — LOOSE (TAIL BAY)

FLL - EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. CEILING PANEL BETWEEN FLOURSCENT LIGHTS. SECURE WIRES AT SOCKET OF EMERGENCY LIGHT IN TAIL COMPARTMENT CEILING BETWEEN FLOUR. LIGHTS AND RELAMPED OPS CHECK OK IAW MM 33-50-00. (M)

Part: POWER SUPPLY — FAILED (CABIN)

ORD - DURING PREFLIGHT, COULD NOT GET CABIN EMERGENCY LIGHTS TO TEST. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY POWER SUPPLY. OPS CHECKED IAW MM 33-51-00. OPS NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLL - FOUND L-1 DOOR AND R-1 DOOR EMERGENCY LIGHT EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERIES IN EMERGENCY LIGHT BATTERY PACK ON DROP CEILING BETWEEN FORWARD LAVATORY, OPS CHECK NORMAL IAW MD80 MM 33-50-00. (M)

Part: WIRE — DISCONNECTED (CABIN)

FLL - FOUND AFT EMERGENCY LIGHT OVER L-2 DOOR INOPERATIVE. SECURED DISCONNECTED GROUND WIRE IN OVERHEAD. OPS CHECK NORMAL IAW MD80 MM 33-50-00. (M)

Part: LATCH — BROKEN (GIRT BAR)

ACY - FLT 1304 - LATCH HOLDING GIRT BAR TO R1 DOOR IS BROKEN. FOUND BRACKET FOR GIRT BAR LATCH LOOSE RE-SECURED BRACKET IAW MM 25-62-00, OPS CHECK NORMAL. (M)

Part: BOTTLE — LOW (EVAC SLIDE)

DTW - AFT EVAC SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED AFT EVAC, SLIDE AS REQUIRED IAW MD80 MM 25-62-00. (M)

Part: BATTERY — DISCHARGED (CABIN)

FLL - OVERHEAD EMERGENCY LIGHTS ROW 9 FOUND INOPERATIVE. REPLACED BATTERY IN OVERHEAD LIGHTS ROW 9 FORWARD IAW MD80 MM 33-53-00. (M)

Part: PAN — DAMAGED (CARGO DOOR)

FTW - FORWARD CARGO DOOR PAN FLANGE DAMAGED JUST BELOW LOCKING MECH, LEFT SIDE AFT. REPAIRED DAMAGE AREA PER MD-80 SRM 52-01. (M)

Part: SLIDE

DFW - FOUND L2 SLIDE PACK DEPLOYED. REMOVED AND REPLACED L2 SLIDE PACK IAW MD-80 MM 25-62-00. (M)

Part: SMOKE DETECTOR — FAULTY (CARGO BAY)

FTW - FORWARD PIT CARGO SMOKE DETECTOR FORWARD A AND AFT PIT CARGO B. T/S SYSTEM FOUND TWO BAD SMOKE DETECTOR IN FORWARD CARGO BAY AND IN AFT CARGO BAY IAW BARFIELD MM 26-22-00. REMOVED AND REPLACED BAD SENSOR IAW BARFIELD SMOKE DETECTOR MM 26-22-00. (M)

Part: PUMP — FAILED (LAVATORY)

FTW - RIGHT AFT LAVATORY SMOKE DETECTOR SOUNDS WHEN ENGINE POWER IS APPLIED. NOTED STRONG SMELL OF EXHAUST FUMES AND LAV WILL NOT FLUSH. REPLACED PUMP ON RIGHT AFT LAV IAW MD80 MM 38-30-00. (M)

Part: WIRE — BROKEN (SPOILER SYS)

FTW - SPOILER DEPLOYED LIGHTS INOPERATIVE. T/S SYSTEM FOUND OPEN WIRE BETWEEN R2-292 (2) AND R2-241 (D2). REPLACED WIRE IAW MD80 WDM 27-66-00 AND MD-80 MM 20-50-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - CORROSION FOUND UNDER L-1 DOOR THRESHOLD. ITEM FOUND DURING MOON MAT INSTALLATION. FABRICATED NEW FLOOR SUPPORT IAW MD80 SRM 57-10-01. INSTALLED FLOOR SUPPORT IAW SRM MD-80 SRM 57-10-01. INSTALLED FLOOR SUPPORT IAW SRM MD-80 51-30-2. (M)

Part: RIB — CRACKED (L/E SLAT)

FTW - FOUND CRACKED RIB AT NR 3 SLAT INBOARD OF PULLEY. REMOVED RIVETS, INSTALLED COMPLETE IAW SRM MD-80 57-01. (M)

Part: PANEL — DELAMINATED (RT WING)

FTW - RIGHT WING INBOARD AFT LOWER PANEL DELAMINATED. REMOVED DELAMINATION IAW MD-80 SRM 51-90-0 PAR 5. REPAIRED DELAMINATION AREA IAW MD-80 PAR 8 SRM 51-90-0. (M)

Part: EYEBOLT — BROKEN (ELEVATOR)

FTW - LEFT ELEVATOR NR 6 HINGE, EYE-BOLT IS BROKEN. INSTALLED EYE BOLT NR 6 IAW MD80 MM 27-30-00. (M)

Part: BRACKET — DAMAGED (FUSELAGE)

FTW - FORWARD LOWER CARGO COMPARTMENT AFT LATCH FITTING SUPPORT BRACKET CLIP DAMAGE. REMOVED DAMAGED BRACKET IAW MD80 SRM 51-30-1. INSTALLED NEW BRACKET IAW SRM MX-80 51-30-1 P/N 5910141-116. (M)

Part: DOOR FRAME — DAMAGED (CARGO DOOR)

FTW - AFT CARGO DOOR AFT HINGE CUT OUT (LOWER SECTION) HAS A SECTION 3 INCHES LONG TORN OUT OF FRAME. REMOVED DAMAGED AREA IN CARGO DOOR AFT HINGE CUT OUT IAW MD80 SRM 52-05 PAGE 214A. FORMED REPAIR DOUBLER AND SHIM IAW MD80 SRM 52-05. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FUSELAGE SKIN REPAIR BETWEEN STATION 200-229 AND L15R AND L18R. CHECK FUSELAGE FOR SMOOTH SKIN LIMITS. DENT AT STATION 229 RIGHT OF FUSELAGE BETWEEN LONGERON 17 AND 18, FOUND TO BE OUT OF LIMITS IAW SRM MD-80 53-04 FIG 38. CUT DAMAGED AREA ON DENT OUT OF LIMITS IAW SRM MD80 53-04. FORMED REPAIR IAW MD80 SRM 53-04 OK TO TREAT AND PRIME. INSTALLED REPAIRED PARTS IAW MD80 SRM 53-04. (M)

Part: BRACKET — DAMAGED (FUSELAGE)

FTW - FORWARD LOWER CARGO DOOR, FORWARD LATCH FITTING SUPPORT BRACKET CLIP DAMAGE. REMOVED DAMAGE BRACKET IAW SRM MC-80 51-30-1. INSTALLED NEW BRACKET IAW SRM MD-80 51-30-1. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FORWARD CARGO DOOR LOWER FRAME INTERCOSTAL WEB AND ANGLE ON RIGHT SIDE IS CRACKED UNDER FORWARD STOP. REMOVED DAMAGED INTERCOSTAL WEB IAW MD-80 SRM 51-30-2. FABRICATED WEB. REMOVED ANGLE. DRILL AND LOCATE NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: DRAIN MAST — CORRODED (FUSELAGE)

FTW - E/E BAY, STATION 200 LONGERON 29R, WASTE WATER DRAIN HAS CORROSION. REMOVED CORROSION. VERIFIED OUTER OF LIMITS. FABRICATED NEW DOUBLER. INSTALLED DOUBLER IAW MD-80 SRM 51-30-02. (M)

Part: DOOR FRAME — CRACKED (CARGO DOOR)

FTW - FORWARD CARGO DOOR, LOWER STOPS FRAME CRACKED IN FOUR PLACES. STOP DRILL CRACK, FORMER AND LOCATED DRILL IAW MD-80 SRM 52-03. INSTALLED REPAIR DOUBLER IAW SRM MD-80 52-30-0. (M)

Part: TAB — DAMAGED (ELEVATOR)

FTW - FOUND DAMAGE ON ANTI-FLOAT TAB SPRING QUADRANT (RT HORIZ) DAMAGE IS ON CASTING ONLY (FRAME). REMOVED ANTI-FLOAT TAB SPRING QUADRANT AS PER MD80 MM 27-30-14. INSTALLED ANTI-FLOAT. TAB SPRING QUADRANT IAW MD80 MM 27-30-14. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND CORROSION ON ANGLE AT STRINGER 28R AT STATION 1136. REMOVED ANGLE IAW MD-80 SRM 51-30-1. FABRICATED ANGLE BRACKET IAW MD-80 SRM 51-10-03. (M)

Part: TAB — DELAMINATED (ELEVATOR)

FTW - RIGHT ELEVATOR GEARED TAB HAS DENTS AND AREA OF DELAMINATION. REMOVED DAMAGE TO AND AROUND AREAS OF DENTS AND DELAMINATION. REPAIRED DENTS AND DELAMINATION ON TAB USING CARBON GRAPHITE CLOTH OVERLAY PROCEDURES IAW DC9 MD80 SRM 55-04. (M)

Part: TAB — DELAMINATED (ELEVATOR)

FTW - RIGHT ELEVATOR ANTI-FLOAT TAB HAS DENTS AND AREA OF DELAMINATION. REMOVED AREAS OF DENTS AND DELAMINATION TO ANTI-FLOAT TAB IAW DC9 MD80 SRM 55-04. FABRICATED REPAIR IAW DC9 MD80 SRM 55-04. INSTALLED REPAIR ON ANTI-FLOAT TAB IAW DC9 MD80 SRM 55-04. (M)

Part: TAB — DELAMINATED (ELEVATOR)

FTW - RIGHT ELEVATOR CONTROL TAB HAS SEVERAL DENTS AND AREAS OF DELAMINATION. REMOVED DAMAGE TO AND AROUND DENTS AND DELAMINATED AREAS IAW DC9 MD80 SRM 55-04. FABRICATED REPAIR IAW DC9 MD80 SRM 55-04. INSTALLED REPAIR IAW DC9 SRM 55-04. (M)

Part: BRACKET — CORRODED (AILERON SYS)

FTW - AILERON AND TAB CONTROL MIXER BRACKET CORRODED IN NUMEROUS PLACES TO INCLUDE AROUND GUIDE PINS AND PULLEY MOUNTS. REMOVED RIGHT LATERAL CONTROL MIXER AS PER BOEING MD80 MM 27-61-04. INSTALLED REPLACEMENT LATERAL CONTROL MIXER BRACKET AS PER BOEING M80 MM 27-61-04. (M)

Part: BLADE — SHINGLED (RT ENGINE)

RIGHT ENGINE HAS 1 FAN BLADE WITH EVIDENCE OF SHINGLING. REMOVED 2 BLADE SETS WITH EVIDENCE OF SHINGLING. INSTALLED THE 2 BLADE SETS ON THE 1ST STAGE COMPRESSOR IAW MD80 MM 73-33-21 PAGE 401. (M)

Part: CHANNEL — DAMAGED (HORIZ STAB)

FTW - NR 2 RIGHT AFT SPAR HAT CHANNEL HAS DAMAGE DOT LEFT -30 (RT HORIZ) XHS 50.00 XHS 104.00. REMOVED HAT CHANNEL FOR REPAIR IAW BOEING MD80 SRM 55-01 FIG 1. PERFORMED CHANNEL IAW BOEING MD80 SRM 55-01 FIG 1. INSTALLED CHANNEL IAW BOEING MD80 SRM 55-01 FIG 1. (M)

Part: ANGLE — CRACKED (ENTRY DOOR)

FTW - MAIN ENTRY DOOR, LOWER GATE ANGLE IS CRACKED AND HAS SPINNING RIVETS. REPLACED LOWER GATE HINGE DOOR L1 IAW MD80 SRM 51-10-2. (M)

Part: SKIN — DENTED (AILERON TAB)

FTW - LEFT AILERON, TRIM TAB, UPPER SURFACE HAS TWO DENTS DOT 124. REMOVED DAMAGE TO AND AROUND DENTED TAB SURFACE IAW DC9 MD80 SRM 57-03. FABRICATED REPAIR IAW DC9 MD80 SRM 57-03. INSTALLED REPAIR IAW DC9 MD80 SRM 57-03. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - DENT AT LEFT STATION 110 6 FT BELOW L1 DOOR HOLD OPEN. FOUND DENT OUT OF LIMITS. REMOVED DAMAGED AREA, LOCATED AND DRILLED. INSTALLED DOUBLER AND FILLER IAW MD-80 SRM 53-04. (M)

Part: FRAME — DAMAGED (FUSELAGE)

FTW - INTERIM REPAIR LEFT STATION 237 L17 AND L18 INSTALLED IAW EA 00-53-029. REMOVED INTERIM REPAIR. CUT OUT DAMAGED AREA. FABRICATED DOUBLER FILLER. LOCATED AND DRILLED NEW FRAME SUPPORT SRM 53-04. (M)

Part: TAB — DAMAGED (ELEVATOR)

FTW - INBOARD TRAILING EDGE OF RIGHT GEARED TAB HAS DAMAGED AREA. REMOVED DAMAGE TO INBOARD TRAILING EDGE OF RIGHT GEARED TAB IAW DC-9 MD-80 SRM 55-04. REPAIRED DAMAGE OF INBOARD TRAILING EDGE RIGHT GEARED TAB USING EPOXY RESIN REPAIRED IAW DC-9 MD-80 SRM 55-04. (M)

Part: RUDDER — DAMAGED (TAIL)

FTW - LEFT SIDE OF RUDDER TRAILING EDGE HAS SMALL DAMAGED AREA. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER IAW MD80 DC9 SRM 55-04. INSTALLED REPAIR IAW DC9 MD80 SRM 55-04. (M)

Part: ATTACH ANGLE — CRACKED (AILERON)

FTW - RIGHT AILERON INBOARD LOWER FLANGE CRACKED. REMOVED NOSE CAP ATTACHING ANGLE IAW SRM MD-80 51-30-2. FABRICATED ATTACH ANGLE IAW MD80 SRM 51-10-2. (M)

Part: DOUBLER — DAMAGED (ELEVATOR)

FTW - LEFT ELEVATOR OUTBOARD STATIC WICK BASE DOUBLER DAMAGED ON BOTTOM SIDE. REMOVED DAMAGED DOUBLER IAW MD80 SRM 51-30-2. FABRICATED NEW DOUBLER IAW MD80 SRM 51-10-2. INSTALLED WICK BASE IAW MD-80 SRM 51-30-2. (M)

Part: TIP CAP — DAMAGED (ELEVATOR)

LEFT ELEVATOR TIP TRAILING EDGE HAS AN AREA THAT AN OLD REPAIR NEEDS TO BE REWORKED. REMOVED DAMAGED TIP IAW MD-80 SRM 51-30-2. FABRICATED NEW TIP IAW MD-80 SRM 51-10-2. INSTALLED TIP REPAIR IAW MD-80 SRM 51-30-2 AND 55-20-2. (M)

Part: ESCAPE ROPE — FRAYED (COCKPIT)

FTW - CO-PILOT ESCAPE LINE IS FRAYED/DAMAGED. INSTALLED NEW ESCAPE LINE ON FIRST OFFICERS SIDE IAW MD-80 MM 25-61-00. (M)

Part: BRACKET — DAMAGED (CARGO BAY)

MID LOWER CARGO COMPARTMENT AFT LATCH FITTING SUPPORT BRACKET CLIP DAMAGE. INSTALLED BRACKET IAW SRM MD 80 51-10-2. (M)

Part: BRACKET — CRACKED (FUSELAGE)

FTW - AFT LOWER CARGO DOOR, FORWARD LATCH FITTING SUPPORT BRACKET CLIP CHAFING. UPON FURTHER INSPECTION, FOUND SUPPORT BRACKET CRACKED. REMOVED SUPPORT BRACKET IAW SRM MX-80 51-30-01. FORMED SUPPORT BRACKET, IAW MD80 SRM 51-10-2. INSTALLED SUPPORT BRACKET IAW SRM 51-30-01. (M)

Part: HANDLE — DAMAGED (EMERGENCY EXIT)

FTW - EMERGENCY ESCAPE HATCHES HAVE DAMAGED PULL TO RELEASE HANDLES, ALL FOUR DOT 101. REMOVED OLD HANDLES IAW 52-21-01 MM MD-80, INSTALLED NEW PULL TO RELEASE HANDLE COVER IAW 52-21-01 MM MD-80. (M)

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

MYR - FLT 7200 - SHUTDOWN NR 2 ENGINE DUE TO COMPRESSOR STALL AND VIBRATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

ACY - PASSENGER O/H EMERGENCY AISLE LIGHTS INOPERATIVE FROM ROWS 4 TO 10 AND 29 TO 34. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD IAW MD-80 MM 33-51-00. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

EWR - FLT 1135 - FOUND PEANUT LIGHTS (EMERGENCY COCKPIT) INOPERATIVE. RELAMPED COCKPIT EMEREGNCY LIGHTS OPS CHECK OK PER MM 33-53-00. (M)

Part: WIRE — BROKEN (CABIN)

DTW - FOUND TAIL EMERGENCY EXIT PATHWAY, 2 AFT WALL EMERGENCY LIGHTS NOT ILLUMINATING. REPAIRED BROKEN WIRES IAW MD-80 MM 33-50. SYSTEM OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M)

Part: SHAFT — SHEARED (LT ENGINE)

AFTER NORMAL TAKEOFF AT WEIGHT OF 124K LBS. WHILE PASSING THROUGH ABOUT 4000 FEET. FELT AND HEARD A THUMP, SLIGHT YAW AND LOOKED DOWN TO SEE LEFT ENGINE HAD SPOOLED DOWN. NO EVIDENCE OF VIBRATION OR COMPRESSOR STALLING. WE PERFORMED EMERGENCY CHECKLIST FOR ENGINE FAILURE/DAMAGE DECLARED EMERGENCY AND LANDED WITH NORMAL RESULT. LANDED AT APPROX 122K LBS. DURING DISASSEMBLY, FOUND HPT SHAFT SHEARED.

Part: CONNECTOR — LOOSE (CABIN)

RSW - FLT 1504 - EMERGENCY LIGHTS (AISLE PATH) WON''T TEST. RESEATED CONNECTOR ON BATTERY PACK. SYSTEM OPERATIONAL CHECKS GOOD IAW MD 80 MM 33-51-00. (M)

Part: CONNECTOR — LOOSE (CABIN)

RSW - EMERGENCY LIGHTS WON''T TEST. RESEATED CONNECTOR ON BATTERY PACK. SYSTEM OPERATIONAL, CHECKS GOOD IAW MD-80 MM 33-51-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLOOR TRACK LIGHTING HAS WIRING EXPOSED IN SEVERAL LOCATIONS. SLIDE TRACK LIGHTING INTO PROPER LOCATIONS AND INSTALLED 2 JOINT COVERS IAW BRUCE INDUSTRIES CATALOG NR 570-005 AND MD-80 MM 33-51-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - ON DAILY, FOUND EMERGENCY CEILING LIGHTS OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECKED GOOD IAW MD 80 MM 33-51. (M)

Part: LENS — MISSING (ROW 22)

DTW - LENS COVER MISSING ON EMERGENCY LIGHT AT ROW 22. REPLACED MISSING LIGHT COVER IAW MD 80 MM 33-00-00. (X)

Part: WIRE — EXPOSED (CABIN)

DTW - FLOOR TRACK LIGHTING HAS EXPOSED WIRES AT ROWS 34, 30, 17, 13, AND 5. ADJUSTED FLOOR TRACK TO REMOVE GAPS BETWEEN TRACK SECTIONS. (X)

Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT)

DTW - LIGHTS OVER EMERGENCY OVERWING EXITS DO NOT ILLUMINATE WHEN EMERGENCY LIGHTS SWITCH IS PLACED TO ON. REMOVED AND REPLACED BATTERIES IN BATTERY PACK B5-33 AND B5-25. REMOVED AND REPLACED BATTERY PACK ASSY B5-33. OPS CHECK GOOD ON RAMP AT THIS TIME IAW MM 33-50-0. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - OVERWING EMERGENCY EXIT SIGNS AFT POSITION, BOTH LEFT AND RIGHT, WILL NOT LIGHT. REMOVED AND REPLACED BATTERY PACK AT POSITION B5-25. OPS CHECK GOOD PER 33-53-00. (X)