N804NK

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,902 hrs · 35,809 cycles

FRAME CANT 1463 AT APPROX LONGERON 19 AND 20 ON AC RT HAS CRACKED WEBBING. INSTALLED PERMANENT REPAIR ON CANTED FRAME FS 1463 BETWEEN R18L AND R25L, IAW EA REV ORIGINAL HAS BEEN ACCOMPLISHED. (K)

Part: ACM — LEAKING (LEFT)

DTW - SMOKE DETECTOR AFT LEFT ON, SOME HOT ELECT CHEMICAL SMELL AFT END OF AIRCRAFT, SMELL CAME BACK AFTER LANDING, AIR RETURN BACK TO DTW, AIRCRAFT TAIL SWAP WITH N810NK. REMOVED AND REPLACED AFT LEFT LAV SMOKE DETECTOR WITH UPDATED P/N FOR PRECAUTION. REMOVED BOTH WATER SEPARATORS AND INSTALLED NEW COALESCER BAGS. FOUND NO CONTAMINATION. REMOVED AND INSPECTED INLET AND OUTLET DUCTS ON BOTH ACM`S. NO CONTAMINATED NOTED. LEFT ACM LEAKING WATER. FOUND FLANGE RETAINING BOLTS LOOSE, SECURED. RIGHT ACM INLET HAS TORN HOSE. REMOVED AND REPLACED CONNECTOR, LEAK CHECKS GOOD. (M)

Part: AUGMENT VALVE — STUCK (NR 1 ENGINE)

NR 1 ENGINE AUGMENTATION VALVE APPEARS TO STICK OPEN AT HIGHER POWER SETTINGS, AIRCRAFT TAIL SWAP WITH N821NK. FOUND LINE BEHIND AUG VALVE ON DUCT TO PNEUMATIC PRESSURE REGULATOR LOOSE, FOUND CRUSH GASKET WORN. REPLACED GASKET AND SECURED LINE. ENGINE RUN ACCOMPLISHED, OPS CHECK NORMAL. (M)

Part: SEAL — LEAKING (HEAT EXCHANGER)

AFTER TAKEOFF LEFT AC SUPPLY PRESSURE DROPS TO ZERO, QRH FAILS TO RESTORE SUPPLY PRESSURE, LEFT PACK IS INOPERATIVE. UPON ENTERING ICING CONDITIONS A 2ND ATTEMPT TO RESET THE PACK RESULTED IN A TEMP RESTORATION OF LEFT PACK, SUBSEQUENT OPERATION OF ENGINE AND AIRFOIL ANTI-ICE SYSTEMS CAUSED AN ABNORMAL SURGE IN LEFT SUPPLY PRESSURE, AIRFOIL ICE PRESSURE ABNORMAL LIGHT ILLUMINATED, PACK FAILED, DIVERTED INTO MYR. FOUND CONNECTOR PERI-SEAL LEAKING ON DUCTING AT SECONDARY HEAT EXCHANGER. REMOVED AND REPLACED PERI-SEALS AT LEFT HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. NO OTHER DEFECTS NOTED. (M)

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE)

ENGINE WAS REMOVED NR 2 POSITION FOR COMPRESSOR SURGE AT TAKEOFF. TEARDOWN AND INSPECTION REVEALED IMPACT DAMAGE STARTING AT THE 8TH STAGE OF THE N2 COMPRESSOR. ONE EACH VANE WAS MISSING FROM THE C-8 STATOR WITH INCREASING LEVELS OF DAMAGE REARWARD OF THE MISSING VANE.

Part: O-RING — WORN (RT WING)

FUEL SEEPAGE FROM RIGHT WING OVER RIGHT MAIN LANDING GEAR, TAIL SWAP WITH AIRCRAFT 829. REPLACED O-RING ON JUNCTION PROBE. LEAK CHECK GOOD. (M)

Part: SKIN — DENTED (FUSELAGE)

SKIN DENT AT STA 1174, BETWEEN LONGERON 17L AND 18L. REMOVED SAF-T-GLO, GALLEY 4 AND SIDE WALL PANEL TO FOM AT LT FS 1184. FOUND DENT TO BE (D=1.5 INCH, X=0.050, D/X=30) COND 2. REFORMED DENT AREA TO ORIGINAL CONTOUR. INSTALLED DOUBLER IAW SRM 53-04, FIG 38. INSTALLED SIDE WALL PANEL, G4 GALLEY AND SAF-T-GLO IAW MM. (K)

Part: SKIN — DENTED (FLAP VANE)

LT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K)

Part: FLOOR SUPPORT — BROKEN (FUSELAGE)

FLOOR SUPPORT STA 1136 BROKEN AFT PIT 28R-28L. REMOVED FLOOR SUPPORT AND LOCATED NEW FLOOR SUPPORT AT STA 1136, 28R-28L. INSTALLED FLOOR SUPPORT FS 1136, 28R-28L, AFT PIT IAW SRM. (K)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

THRESHOLD SUPPORT ANGLE, STA 1212, ON DOOR JAMB BEAM IS CORRODED. REMOVED CORROSION AT SUPPORT ANGLE. MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT ANGLE AT STA 1212. FABRICATED NEW SUPPORT ANGLE, HEAT TREATED REPAIR PART. INSTALLED SUPPORT ANGLE AT STA 1212 IAW SRM. (K)

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN DENTED AT FS 304 BETWEEN LONGERON 28L-29L. (D=0.5 INCH, X=0.015 INCH D/X= 33.3). DENT WAS FOUND TO BE LESS THAN 1.0 INCH FROM FRAME REQ A CUT OUT REPAIR. CUT OUT DAMAGED SKIN AT FS 304 BETWEEN LONGERON 28L-29L. FABED NEW SKIN SECTION, REPAIR DOUBLER AND FABED NEW 4 EA STRAPS. TREATED, PRIMED AND INSTALLED AT FS 304 BETWEEN 28L-29L. (K)

Part: SKIN — DENTED (FUSELAGE)

DENT AT FS 245, LONGERON 18L (D=1.250 INCH, X=0.054 D/X=23.14). REMOVED AIRCRAFT SKIN AT STA FS 245, LONGERON 18L (20 INCHES X 14 INCHES). FABRICATED REPAIR PARTS IAW SRM. INSTALLED, REPAIR AT FS STA 245 LONGERON 18L. (K)

Part: SKIN — DAMAGED (FUSELAGE)

FLUSH REPAIR FS 622 LONGERON 22R-24R HAS NO FINGER DOUBLER. REMOVED TEMP REPAIR. FABRICATED PERMANENT REPAIR PARTS. TREATED AND PRIMED ON FINAL REPAIR. INSTALLED REPAIR IAW SRM. (K)

Part: WEDGE — DAMAGED (T/E FLAP)

LT WING, IB FLAP, OB T/E WEDGE HAS TEMPORARY REPAIR LOWER SIDE IB. REMOVED TEMP REPAIR, REMOVED DAMAGED AREA (2 INCH DIA) FABRICATE DOUBLER AND FILLER, TREATED, PRIMED DOUBLER AND FILLER. INSTALLED REPAIRED DOUBLER AND FILLER IAW SRM. (K)

Part: STIFFENER — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT, STA 1338, 27L-27R AFT SIDE OF FALSE BULKHEAD, LOWER STIFFENERS ARE CORRODED. REMOVED CORROSION AT STIFFENER STA 1338L, 29L. MATERIAL LOSS OUT OF LIMITS. REMOVED STIFFENER AT STA 1338L, 29L, LOCATED AND DRILLED NEW STIFFENER. INSTALLED STIFFENER AT STA 1338 IAW SRM. (K)

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN DENTED AT FS 310, LONGERON 29L-28L. (D=0.5 INCH, X=0.010 INCH, D/X=50). DENT WAS FOUND TO BE LESS THAN 1.0 INCH AND REQ A CUT OUT REPAIR. FAB`D NEW SKIN SECTION, REPAIR DOUBLER, FINGER DOUBLER, FABED (4 EA) STRAPS. TREATED, PRIMED AND TOP COATED REPAIRED PARTS. INSTALLED REPAIRED SKIN FILLER, FINGER DOUBLER, AND (4 EA) STRAPS PART AT FS 304, L28L-29L IAW SRM. (K)

Part: DOOR — DENTED (AFT CARGO DOOR)

DENT ON AFT CARGO DOOR AT STA 1183, 14 INCHES FROM UPPER EDGE/ 23 INCHES FROM AFT EDGE (D=1.0, X=0.015, D/X=66.7). REMOVED AFT CARGO DOOR TO FOM DENT FOUND TO BE COND 1B. COLD WORK PERFORMED TO ORIGINAL CONTOUR. DYE PENETRANT PERFORMED FOR CRACKS. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED REPAIR DOUBLER. INSTALLED DOUBLER IAW 53-04, FIG 38. INSTALLED AFT CARGO DOOR IAW 52-31-00. (K)

Part: SKIN — DENTED (AFT CARGO DOOR)

DENT ON AFT CARGO DOOR AT STA 1165, 13 INCHES FROM FORWARD EDGE, 14 INCHES FROM UPPER EDGE (D=2.0, X=0.05, D/X=40). FOUND DENT TO BE COND. 1B. PERFORMED COLD WORK AREA BACK TO ORIGINAL CONTOUR. DYE PENETRANT PERFORMED FOR CRACKS. FABRICATED DOUBLER. TREAT AND PRIMED DOUBLER AND SKIN. INSTALLED DOUBLER IAW SRM. (K)

Part: LONGERON — CORRODED (FUSELAGE)

LONGERON 28R STA 1140 HAS CORROSION AROUND FASTENERS THROUGH SKIN IN AFT PIT. REMOVED FASTENERS THROUGH SKIN AND REMOVED CORROSION. LONGERON 28R AT STA 1140 IS OUT OF LIMITS. LOCATED AND DRILLED FABED LONG SECTION AND SPLICE. TREAT AND PRIMED, INSTALLED LONG. SECTION AND REPAIR SPLICE 28R IAW 51-30-5. (K)

Part: ANGLE — CORRODED (FUSELAGE)

DOOR FRAME TO SKIN CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM ARE CORRODED IN AFT PIT. REMOVED CORROSION ON DOOR FRAME TO SKIN CORNER ANGLES AND DOOR JAMB. MATERIAL LOSS OUT OF LIMITS. DRILLED AND LOCATED NEW ANGLE, TREATED, PRIMED AND INSTALLED NEW ANGLE. (K)

Part: ANGLE — CRACKED (MID CARGO DOOR)

MID PIT DOOR INTERNAL ANGLE CRACKED AT LOWER CENTER EDGE. REMOVED INTERNAL ANGLE FROM MID CARGO DOOR LOWER CENTER EDGE. LOCATED AND DRILLED NEW INTERNAL ANGLE (FITTING), INSTALLED NEW FITTING IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

AFT PIT LOWER DOOR JAMB BEAM CORRODED AND HAS BARE METAL. REMOVED CORROSION, FABRICATED REPAIR IAW SRM. OK TO TREAT, PRIME AND TOPCOAT REPAIR. LOCATED AND DRILLED 2 DOOR STOP FITTINGS AND INSTALLED DOOR JAMB BEAM REPAIR. (K)

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE EXTERIOR STA 1485 CANT. LT LOWER SKIN CRACKED. CUT OUT DAMAGED AREA 2 INCH X 4.8 INCH AT STA 1485. FABED FINGER DOUBLER, TREATED AND PRIMED. INSTALLED REPAIR ON LT LOWER SKIN, STA 1485 CANT IAW SRM. (K)

Part: ANGLE — CORRODED (FUSELAGE)

DOOR FRAME TO SKIN CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM ARE CORRODED IN AFT PIT. REMOVED CORROSION ON DOOR FRAME SKIN, CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM. CORNER ANGLE IS OUT OF LIMITS STA 1212 AND LOCATED NEW ANGLE, INSTALLED ANGLE AT STA 1212. CORNER ANGLE AT STA 1155 WITHING LIMITS IAW 53-01. (K)

Part: SKIN — DAMAGED (FLAP VANE)

RT WING OB FLAP MID FIXED VANE DAMAGED. REMOVED DAMAGED SKIN AND CORE TO OB FLAP VANE, FABRICATED REPAIR DOUBLER AND HONEYCOMB CORE. TREATED METAL, BONDED CORE AND DOUBLER. INSTALLED REPAIRED CORE AND SKIN IAW SRM. (K)

Part: SKIN — DENTED (MID CARGO DOOR)

(1EA) MINOR DENT ON MID CARGO DOOR EXTERNAL SKIN AT LOWER L/R MARKED. DENT MEASURE IS OUT OF LIMITS CONDITION. 2(D=0.25, X=0.75). REMOVED CARGO DOOR FOR FOM, APPLIED DYE PENETRANT FOR CRACKS. FABED (3 SHIMS) AND REPAIR DOUBLER. TREATED SKIN, SHIMS AND DOUBLER IAW SRM. INSTALLED MID CARGO DOOR. (K)

Part: ENGINE — MALFUNCTIONED (NR 2)

TAKEOFF ROLL A/T ENGAGED AT APPROX 40 KNOTS, THROTTLES AT FLEX POWER FELT SOMETHING LIKE A BLOWN TIRE, RT ENGINE SLIGHT YAW, ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE. (M)

Part: SMOKE DETECTOR — INACTIVE (RT LAVATORY)

LP NR 273191-1; RT LAV SMOKE DETECTOR DID NOT ACTIVATE WHEN PAX WAS SMOKING IN AIRCRAFT LAV. OPS TESTED SMOKE DETECTOR, NO FAULTS WERE NOTED.

Part: SKIN — CRACKED (LT MLG DOOR)

LP NR 0167013; LT MAIN GEAR DOOR SKIN CRACKED ABOVE AND BELOW SKIN PLATE. UNSCHEDULED CHANGE OF AIRCRAFT EN ROUTE. PERFORMED REPAIR AND INSTALLED DOUBLER.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKES)

FLL - FLT 478 - FOUND BRAKE PEDAL DEPRESSION ON LEFT SIDE IS ALMOST TWICE THE RIGHT SIDE BEFORE BRAKE PADS MAKE CONTACT. REMOVED AND REPLACED LEFT WHEEL WELL BRAKE CONTROL VALVE. BLED ALL FOUR BRAKES FREE OF AIR. (M)

Part: MECHANISM — STICKING (DOOR INTERLOCK)

DTW - FLT 417 - FOUND MAIN CABIN DOOR WILL NOT CLOSE. INSPECTED AND FOUND INTERLOCK MECH STICKING, LUBED AND ADJUSTED INTERLOCK ARM. OPS CHECK GOOD. INSPECTED L1 DOOR. (M)

Part: SLIDE — MISRIGGED (R1 DOOR)

FOUND R1 ESCAPE SLIDE IMPROPERLY RIGGED, PULL HANDLE NOT ATTACHED. ATTCHED MANUAL PULL HANDLE. (M)

Part: SLIDE — MISRIGGED (R1 DOOR)

DTW - FOUND ESCAPE SLIDE IMPROPERLY RIGGED, PULL HANDLE NOT ATTACHED. REMOVED AND REPLACED R1 DOOR SLIDE PACK. (M)

Part: LINK — BROKEN (CYLINDER)

AFTER TAKEOFF LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. GAR SAFE LIGHT ILLUMINATED ON GEAR EXTENSION. REMOVED AND REPLACED LEFT MLG RETRACT CYLINDER LOWER LINKS. UPON INSPECTION FOUND LOWER LINK BROKEN. OPS CHECK GOOD. (M)

Part: GLOWSTRIP — CRACKED (CABIN)

DTW - FOUND SAFETY GLOW COVER CRACKED, FORWARD LAV AREA ALSO NEEDS CLEANED. REPLACED SAFETY GLOW. (M)

Part: SIGN — DEFECTIVE (AFT GALLEY)

FLOOR EXIT SIGN IN AFT GALLEY UNREADABLE. REPLACED FLOOR EXIT SIGN (SAFETY GLOW) IN AFT GALLEY.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

FLLT - FLT 1751 - FOUND R1 SLIDE DEPLOYED WHEN CATERING OPENED DOOR. R1 SLIDE DID NOT DEPLOY, LANYARD CAME OFF COVER RESECURED LANYARD. (M)

Part: CABLE — MISROUTED (L2 DOOR SLIDE)

FLL - L2 DOOR ESCAPE SLIDE GIRT BAR CABLE ROUTED INPROPERLY. REROUTED CABLE. (M)

Part: LANYARD — MISROUTED (EVAC SLIDE)

FLL - R-1 DOOR EMERGENCY SLIDE GIRT BAR LANYARD ROUTED INCORRECTLY. RE-ROUTED R-1 DOOR SLIDE GIRT BAR LANYARD. (M)

Part: LANYARD — LOOSE (EVAC SLIDE)

FLL - FOUND R-1 DOOR EVACUATION SLIDE LANYARD LOOSE. RE-INSTALLED R-1 DOOR EVACUATION SLIDE LANYARD. (M)

Part: LANDING GEAR — MALFUNCTIONED (NOSE)

DTW - FLT 461 - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. SERVICE NOSE STRUT CHECKED SYSTEM, RIGGING AND PERFORMED NOSE GEAR RETRACTION. NO DEFECTS NOTED. (M)

Part: LANYARD — OUT OF POSITION (TAILCONE SLIDE)

LGA - FOUND AFT TAILCONE SLIDE LEFT LANYARD NOT IN BRACKET. SECURED LANYARD IN BRACKET FOR TAILCONE SLIDE. OK FOR SERVICE. (M)

Part: DOWNLOCK SENSOR — FAILED (NLG)

DTW - FLT 417 - FOUND NOSE GEAR DOWN LIGHT FAILED TO COME ON FOR 3 MINUTES AFTER GEAR EXTENSION. T/S NOSE GEAR DOWN LIGHT. REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR AND NOSE GEAR POSITION INTLK LIGHT SWITCH. JACKED AND SWUNG NOSE GEAR, NO DEFECTS NOTED. (M)

Part: SENSOR — DEFECTIVE (NLG)

DEN - FLT 980 - NOSE GEAR UNSAFE LIGHT DID NOT EXTINGUISH DURING GEAR EXTENSION. WENT AROUND, FOLLOWED QRH-LANDED NORMALLY LIGHT EXTINGUISHED DURING QRH PROCEDURE AFTER RE-CYCLING GEAR. REMOVED AND REPLACED UNSAFE SENSOR. (M)

Part: LIGHT — WILL NOT TEST (CABIN)

PORTABLE EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AIRCRAFT HAD TWO INBOUND ITEMS, 'AFT CABIN DOOR' LIGHT CAME ON AT ALT PRESSURE NORMAL, STAYED ON FOR APPROX 1 HOUR. DOOR WAS LATCHED PROPERLY, CAME BACK ON LAST HOUR OF FLIGHT. 'AUTO SLAT FAIL' CAME ON DEP/AND APP. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)

Part: BATTERY — WEAK (FLASHLIGHT)

TOP AFT EMERGENCY FLASHLIGHT WAS WEAK BATTERY. RESECURED CONNECTION TO FLASHLIGHT BATTERY, OPS CHECKS NORMAL. (M)

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG)

NOSE GEAR RED INDICATOR LIGHT REMAINED ON FOR APPROX 3 MINUTES AFTER GEAR EXTENSION NLG INDICATOR FULLY EXTENDED. INSPECTED AND CLEANED NOSE GEAR PROX SENSORS JACKED NOSE GEAR AND PERFORMED RETRACTION SEVERAL TIMES. GEAR LIGHTS OPERATED NORMAL. (M)

Part: WIRE — SHORTED (CABIN)

FTW - FOUND OVERWING EMERGENCY EXIT SIGNS ARE INOPERATIVE. TROUBLESHOOT OVERWING EMERGENCY EXIT SIGNS AND FOUND SHORTED WIRES TO THE EXIT LIGHTS. REPAIRED SHORTED WIRING. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

FOUND L2 DOOR AND AFT ENTRY DOOR EMERGENCY EXIT SIGNS ARE INOPERATIVE. FOUND BATTERY PACK CONNECTOR DISCONNECTED. CONNECTED CANNON PLUG TO BATTERY PACK. (M)

Part: MOUNT — CORRODED (T/E FLAP)

FTW - LEFT INBOARD FLAP VANE RIGHT AFT MOUNT CORRODED. LEFT INBOARD FLAP VANE HAS .75 INCH DIAMETER DENT IN LEADING EDGE VERTICAL CRACK THROUGH CENTER OF DEN. DUE TO INTERNAL DAMAGE FROM CORROSION IN ATTACH FITTINGS UNIT EXCHANGE. INSTALLED LEFT INBOARD FLAP VANE. (M)

Part: CHANNEL — DEBONDED (FLOOBOARD)

FTW - FOUND CABIN FLOORBOARD AT FS 1250-1309 LEFT OUTBOARD BOTH 'HAT' CHANNELS DISBONDED. RE-BONDED 2 EACH HAT CHANNELS ON FLOORBOARD. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - LEFT FLOOR PANEL, FS 886, SKIN CRACKED WITH MATERIAL MISSING AND EDGE FILLER DAMAGED AROUND PERIPHERY. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD CORRODED, BROKEN INSERTS, EDGES BROKEN, FS 1271-1338. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTIA - FOUND CABIN FLOORBOARD AT FS 1271-1338 CTR CORRODED AND BROKEN INSERTS AND BROKEN CORNER/EDGES. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - MAIN CABIN LEFT SIDE STATION 1174 TO 1250 SUB-FLOOR PANEL (PHENOLIC) HAS DISBONDED AT LOWER HATS SECTION AND CRACKS AT FORWARD EDGE. REPAIRED LOWER HAT SECTIONS AND CRACKS ON SUB FLOOR PANEL STATION 1174 TO 1250. (M)

Part: FITTING — CORRODED (SPOILER)

FTW - FOUND LEFT OUTBOARD SPOILER TORSION BAR INBOARD FITTING HAS CORROSION. REMOVED FITTING. LOCATED AND DRILLED NEW ORDERED TORSION BAR FITTING. INSTALLED NEW FITTING. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND WEB CORRODED STATION 236-256 RBL 44-54. REMOVED WEB. FABRICATED NEW WEB. INSTALLED NEW WEB. (M)

Part: SUPPORT — BROKEN (LT SPOILER)

FTW - FOUND LEFT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT BROKEN. REMOVED LEFT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: STRUCTURE — CORRODED (SUB FLOOR)

FTW - FOUND SUB FLOOR AT STATION 200 RBL 24 HAS CORROSION. CUT OUT DAMAGED SECTION OF SUB FLOOR. FABRICATED NEW SUB FLOOR SECTION AND DOUBLERS. INSTALLED SUB FLOOR AND DOUBLERS. (M)

Part: STRUCTURE — CRACKED (SUBFLOOR)

FTW - FOUND SUBFLOOR AT STATION 210 RBL 24 CRACKED. REMOVED SUBFLOOR. INSTALLED SUBFLOOR. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LBL 54 INCHES SUB FLOOR WEB ELONGATED HOLES/CRACKED. REMOVED SUB FLOOR WEB FS 160-200. FABRICATED NEW SUB FLOOR WEB. INSTALLED NEW SUB FLOOR WEB. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FTW - FOUND CABIN FS 1338 FLOORBEAM UPPER SIDE CORRODED/BARE METAL LBL 57-RBL 57. CUT APPROX 2 INCHES BY 1 INCH SECTION OUT OF TOP FLANGE. FABRICATED REPAIR ANGLE-FILLER. INSTALLED REPAIR ANGLE AND FILLERS. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND FORWARD CABIN STATION 236 RIGHT SIDE L18R HAS CORROSION ON SUB FLOOR WEB. REMOVED DAMAGED SECTION. FABRICATED WEB SECTION AND SPLICE. INSTALLED WEB AND SPLICE. (M)

Part: FITTING — CORRODED (FUSELAGE)

FOUND CABIN FS 1309 FRAME TO FLOORBEAM ATTACH FITTING CORRODED AND FAST CORRODED STRINGER 18R. REMOVED OLD FITTING. INSTALLED NEW FITTING. (M)

Part: FLOOR PANEL — CORRODED (LAVATORY)

FTW - FORWARD LAVATORY VANITY WALL UNDER SINK AREA FLOOR CORRODED. REMOVED FLOOR. FABRICATED NEW FLOOR. INSTALLED NEW FLOOR. (M)

Part: FLOORBOARD — DELAMINATED (CABIN)

FOUND CABIN FLOOR BOARD FORWARD R1 DOOR CORRODED INSERTS, BOARD DELAMINATED, EDGE FILL INCOMPLETE. FABRICATED NEW PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND MAIN CABIN STATION 256 TO STATION 313 RBL 22 TO RBL 45 FLOORBOARD HAS CORROSION AND PUNCTURE HOLES AT BACKSIDE R5. FABRICATED NEW FLOORBOARD. (M)

Part: ANGLE — BROKEN (FLOORBOARD)

FTW - FOUND RIGHT COCKPIT FLOORBOARD ATTACHED SYNTHETIC ANGLE BROKEN, HEAVY FOOD/DIRTY DEPOSITS. REMOVED SYNETHETIC ANGLE. FORMED NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: ANGLE — CORRODED (FLOORBOARD)

FTW - FOUND COCKPIT FLOORBOARD FS 120-160 LEFT ATTACHED SYN ANGLE CRACKED, CORRODED AND DIRTY. REMOVED CRACKED ANGLE. FORMED NEW ANGLE. FABRICATED NEW FLOORBOARD. INSTALLED NEW ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-196, 44 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK UNDER G2 CORRODED AT FS 200-256. REMOVED SECTION OF SEAT TRACK, RIGHT INBOARD AT FS 200 TO 265. FABRICATED LOCATED AND DRILLED NEW SECTION OF SEAT TRACK. INSTALLED NEW SECTION OF TRACK. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - AFT PIT CORROSION AT FS 1271 LONGERON 26R. FOUND .25 INCH CRACK ON STRAP. FABRICATED REPAIR DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FLIGHT COMPARTMENT FLOOR SUPPORT CORRODED AT FS 149-160 12 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: ATTACH FITTING — CRACKED (FUSELAGE)

FTW - FOUND CABIN FS 864 FLOOR SUPPORT ATTACH FITTING CRACKED BL 0. REMOVED CRACKED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT ATTACH FITTING. INSTALLED FLOOR SUPPORT ATTACH FITTING. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 200 RBL 44 TO 23 INCHES FLOOR SUPPORT CORRODED. FABRICATED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180 7 INCHES TO 44 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND RIGHT AFT LAVATORY FLOOR STATION 1338 STRINGER 18 CORRODED. REMOVED 9 HI-LOCKS AND 1 GUSSET. FABRICATED NEW GUSSET. FOUND FRAME AT FS 1338 AND 18R TO BE CORRODED BEYOND LIMITS. FABRICATED NEW FRAME REPAIR SECTION, AND FABRICATED SPLICE SECTION. CUT OFF DAMAGED SECTION OF FRAME. INSTALLED NEW FRAME SECTION AND REPAIR SPLICE. INSTALLED GUSSET. (M)

Part: WEB — CORRODED (SUBFLOOR)

FTW - FOUND FLIGHT COMPARTMENT CORRODED SUBFLOOR AT FS 133-148 29 INCHES TO 48 INCHES RBL. REMOVED WEB. FABRICATED NEW SUB FLOOR. INSTALLED NEW WEB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200 44 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 44 INCHES RBL TO 15 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: MOUNT BRACKET — CRACKED (RT SPOILER)

FTW - RIGHT WING INBOARD SPOILER TORSION BAR INBOARD MOUNT BRACKET CRACKED. REMOVED AND REPLACED RIGHT WING INBOARD SPOILER TORSION BAR INBOARD MOUNT BRACKET. (M)

Part: FITTING — CRACKED (T/E FLAP)

FTW - FOUND LEFT INBOARD FLAP INBOARD ACTUATOR ATTACH FITTING CRACKED AT MLG TRAP FITTING. REMOVED CRACKED FITTING. INSTALLED NEW FITTING. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200 56 INCHES LBL L1 DOOR THRESHOLD. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND CORROSION AT R1 DOOR AFT LOWER CORNER AT FS 195-210 18R. REMOVED CORRODED CUSP AT R1 DOOR STATION 164 TO FS 230. FABRICATED NEW CUSP. FABRICATED CUSP SPLICE. INSTALLED NEW CUSP AND SPLICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 16 INCHES TO 25 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT FLOORBEAM INTERCOSTAL CRACKED IN NUTPLATE HOLES 0 BL AT FS 1287-1309. REMOVED INTERCOSTAL UPPER REPAIR. FABRICATED UPPER REPAIR. INSTALLED UPPER INTERCOSTAL REPAIR. (M)

Part: ACCOUSTIC LINER — DELAMINATED (THRUST REVERSER)

FTW - FOUND NR 2 ENGINE THRUST REVERSER INNER ACCOUSTIC CORE MISSING/DELAMINATED AND 1 PIN WELD LOOSE. REPAIRED DAMAGED AREA. (M)

Part: ACCOUSTIC LINER — DELAMINATED (THRUST REVERSER)

FTW - NR 1 ENGINE THRUST REVERSER INNER ACCOUSTIC CORE HAS COME OUT/DELAMINATED. REPAIRED DAMAGED ACCOUSTIC AREA. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOND AFT PIT FLOOR WEB CRACKED AT FS 1271-1309 LONGERON 18R. STOP DRILLED THE TWO ENDS OF THE CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR. (M)

Part: SKIN — TORN (RT ELEVATOR)

FTW - FOUND RIGHT ELEVATOR INBOARD UPPER LEADING EDGE SKIN TORN. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. INSTALLED SKIN. (M)

Part: CLIP — CRACKED (FUSELAGE)

FTW - FOUND FORWARD PIT STRINGER 21L INTERCOSTAL CLIP CRACKED AT FS 237. REMOVED INNER COSTAL CLIP. FABRICATED NEW CLIP. INSTALLED INNER COSTAL CLIP. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO FORWARD BULKHEAD LOWER SUPPORT HAS CORROSION UPPER LOWER SURFACES FROM STRINGER 27L-27R. REMOVED LOWER SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: SKIN — CORRODED (ELEVATOR)

FTW - FOUND RIGHT ELEVATOR ALL UNPAINTED UPPER AND LOWER SKIN HAS LEFT SURFACE CORROSION. ELEVATOR SKINS FOUND TO BE OUT OF LIMITS. ELEVATOR REPLACED WITH NEW ELEVATOR. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT CORRODED FLOOR WEB AROUND DOME NUT AT FS 1174-1193 LONGERON 18L. FABRICATED REPAIR PARTS FILLER AND DOUBLER. INSTALLED DOUBLER AND FILLER. PRIOR TO STEP 6 PAGE 1 REMOVED DAMAGED AREA OF WEB. (M)

Part: RIB — CRACKED (L/E SLAT)

FTW - RIGHT WING OUTBOARD SLAT EDGE SEAL TORN, FOUND CRACKED CASTING. REMOVED CASTING. LOCATED AND DRILLED NEW RIB. INSTALLED NEW RIB. (M)

Part: WEB — CORRODED (SUBFLOOR)

FTW - FOUND CABIN SUBFLOOR CORRODED AT FS 207 24 INCHES RBL, VISIBLE FROM E/E COMPARTMENT. REMOVED WEB STATION 200 TO 218. FABRICATED NEW SUBFLOOR. INSTALLED NEW SUBFLOOR WEB. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - DENT AT FS 408 BETWEEN LONGERON 29R. REMOVED DAMAGED SKIN BETWEEN L29R TO L29L AND BETWEEN FS 406 TO 409. FABRICATED NEW SKIN FILLER. FABRICATED NEW FINGER DOUBLER. FABRICATED NEW DOUBLER. MATERIAL ID FOR REPAIR STRAP. INSTALLED STRAP FINGER DOUBLER, REPAIR DOUBLER, AND FILLER. (M)

Part: STRUT — UNDERSERVICED (NLG)

DTW - FLT 1691 - AIRCRAFT OVERWEIGHT LANDING. NOSE GEAR DOORS DID NOT CLOSE, COMPLIED WITH QRH AIRCRAFT WEIGHT 137,000 LBS. INSPECTED NOSE GEAR, FOUND NOSE STRUT TO REQUIRE SERVICING. SERVICED NOSE STRUT, PERFORMED GEAR SWING. NO FAULTS NOTED AT THIS TIME. (M)

Part: FIRE LOOP — MALFUNCTIONED (FIRE DETECTION)

DEN - FLT 980 - FIRE DETECTOR LOOP LIGHT ILLUMINATED AFTER TAKEOFF AND WAS HANDLED IAW QRH. REMOVED AND REPLACED LOWER BURN B-LOOP. SYSTEM OP CHECKS GOOD. (M)

Part: STRUCTURE — WARPED (SPOILER)

FTW - FOUND LEFT WING, OUTBOARD FLIGHT SPOILER WARP/DELAMINATED. REMOVED LEFT OUTBOARD SPOILER. INSTALLED LEFT OUTBOARD FLIGHT SPOILER. (M)

Part: COWLING — DAMAGED (LT ENGINE)

FTW - FOUND P/N 11-N-00304 LEFT ENGINE NOSE COWL ACCOUSTIC LINER IS FASTENERS AT 3 O'CLOCK POSITION AND 1 FASTENER AT 9 O'CLOCK ARE PULLED THROUGH. P/N 11-N-00316, REMOVE NR 1 ENGINE NOSE COWL TO SEND OSV, REINSTALL AFTER SERVICE. INSTALLED SERVICEABLE NOSE COWL. (M)

Part: COWLING — DAMAGED (RT ENGINE)

FTW - RT ENGNE NOSE COWL ACCOUSTIC LINING HAS APPROX 48 FASTENERS PULLED THROUGH, RIGHT ENGINE NOSE COWL ACCOUSTIC LINING HAS BAD REPAIR AT 6 O'CLOCK POSITION. RT ENGINE NOSE COWL ACCOUSTIC LINING HAS THREE BAD REPAIRS FROM 12-10 O'CLOCK POSITIONS. RIGHT ENGINE NOSE COWL L/E HAS ERROSION AND PITTING. REMOVED NR 2 ENGINE NOSE COWL TO SEND OSV, REINSTALL AFTER SERVICE. INSTALLED SERVICEABLE NR 2 NOSE COWL. (M)

Part: FLOORBOARD — DELAMINATED (CABIN)

FTW - PAX CABIN FLOORBOARDS TWO DELAMINATED AT AFT GALLEY SERVICE DOOR THRESHOLD. REMOVED DELAMINATED FLOORBOARDS. REPAIRED PAX CABIN FLOORBOARDS. INSTALLED FLOORBOARDS AT AFT GALLEY SERVICE DOOR THRESHOLD. (M)

Part: STRUCTURE — CORRODED (LAVATORY)

FORWARD LAVATORY HAS CORROSION AT LOWER FLOOR, INSIDE TRASH CAN AREA CORROSION FOUND AFTER TRASH CAN REMOVAL. MATERIAL OUT OF LIMITS. FABRICATED PART. INSTALLED PART IAW MD80 SRM 51-30-2. (M)

Part: BOLT — MISSING (ENGINE MOUNT)

FTW - FOUND NR 2 ENGINE FORWARD MOUNT CONE BOLT THROUGH BOLT HAS MISSING ALIGNED BOLT ON ANTI-ROTATION ASSY. REMOVED AND REPLACED TOP FORWARD CONE BOLT PER MD80 MM 71-20-01. (M)

Part: WEB — CRACKED (EMERGENCY EXIT)

FTW - RIGHT, LEFT OUTBOARD CUSP WEB AT EMERGENCY EXIT CRACKED IN SEVERAL PLACES. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER RIGHT SIDE. FABRICATED DOUBLER AND FILLER LEFT SIDE. INSTALLED LEFT AND RIGHT DOUBLERS AND FILLERS IAW MD80 SRM 51-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1334 L18L-L18R CORROSION ON FRAME WEB, STIFFENERS, UPPER/LOWER FLANGES (AFT SIDE OF FRAME). ONE VERTICAL STIFFENER OUT OF LIMITS. FABRICATED DRILLED AND LOCATED NEW STIFFENER. INSTALLED NEW STIFFENER PER SRM MD80 51-30-2. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FTW - FOUND STATION 205 L15L, SHEAR TIE ON FORWARD END OF INTERCOSTAL IS CRACKED. REMOVED CRACKED INTERCOSTAL. FABRICATED SHIM AND DOUBLER. INSTALLED SHIM AND DOUBLER IAW MD80 SRM 51-30-2. (M)

Part: ISOLATOR — OUT OF POSITION (ENGINE MOUNT)

FOUND LEFT ENGINE FORWARD LOWER VIBRATION ISOLATOR ROTATION MARKS ARE MISMATCHED. REMOVED LEFT LOWER VIBRATION ISOLATOR. INSTALLED LOWER LEFT VIBRATION ISOLATOR IAW MD80 MM 71-20-02. (M)

Part: ISOLATOR — OUT OF POSITION (ENGINE MOUNT)

FTW - RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR ROTATION IND MARKS ARE MISMATCHED. REMOVED RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLED RIGHT LOWER VIBRATION ISOLATOR. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - PAX CABIN SEAT TRACK RIGHT INBOARD CORRODED FROM STATION 200-237. REMOVED SEAT TRACK FROM STATION 200-265 RIGHT INBOARD. INSTALLED NEW SEAT TRACK IAW MD80 SRM 53-05. (M)

Part: WEB — CORRODED (SUB FLOOR)

FTW - FOUND STATION 160-200 -55 SUBFLOOR (WEB) HAS ELONGATED HOLES AND OUT OF LIMITS CORROSION, DEEP PITS, FROM APPROX STATION 180-200. CUT OUT DAMAGED SUBFLOOR. FORMED REPAIR DOUBLER AND FILLER. INSTALLED FILLER AND DOUBLER IAW MD80 SRM 51-30-5. (M)

Part: FRAME — CORRODED (BULKHEAD)

FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT FORMER SUPPORT BULKHEAD STATION 1322, L30 TO 26L. FOUND OUT OF LIMITS. FORMED SUPPORT IAW MD80 SRM 51-10-3. (M)

Part: FLOORBOARD — BROKEN (CABIN)

FTW - FOUND COCKPIT CENTER FLOORBOARD BROKEN OUT AND CRUSHED AND TORN AT EDGES. FORMED NEW FLOORBOARDS IAW MD80 MM 20-10-19. (M)

Part: STRUCTURE — CORRODED (SUB FLOOR)

FOUND STATION 148-200 PLUS X6 LEFT SUB FLOOR MEMBRANE HAS CORROSION AROUND FASTENER HOLES AND 1 ELONGATED HOLE. REMOVED CORROSION. LOCATED DRILLED AND TRIMMED REPAIR PARTS. REMOVED DAMAGE AND ENLONGATED HOLE. (M)

Part: FLOOR PANEL — PUNCTURED (COCKPIT)

FTW - FOUND COCKPIT FLOOR PANEL HAS HOLE PUNCHED IN SKIN. HOLE AND CRACK IN FLOORBOARD OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALL DOUBLER IAW DC9 MD80 SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN)

FTW - FOUND STATION 200 -X5 TO PLUS X5 FLOORBOARD SUPPORT ANGLE HAS HEAVY CORROSION. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALL FLOOR SUPPORT IAW DC9 MD80 SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-200 -X45 FLOOR SUPPORT ANGLE HAS HEAVY CORROSION. FORMED NEW FLOOR SUPPORT ANGLE. FORMED NEW SUPPORT ANGLE. INSTALLED NEW FLOOR SUPPORT ANGLE IAW MD80 SRM 51-30-2. (M)

Part: FLOORBOARD — CHAFED (CABIN)

FTW - FOUND FLOORBOARD PANEL NR A-10 HAT CHANNEL CHAFED, DENTS IN SKIN AND NEEDS CLEANING. FABRICATED DOUBLER. GOUGE IS OUT OF LIMITS ON HAT CHANNEL NR 2. FABRICATED NR 2 HAT CHANNEL DOUBLER. INSTALLED REPAIR DOUBLER. INSTALLED HAT NR 2 REPAIR DOUBLER IAW MD80 SRM 51-30-8. (M)

Part: SUPPORT BRACKET — CHAFED (CARGO DOOR)

FTW - FORWARD LOWER CARGO COMPARTMENT CARGO DOOR CHAFING / DAMAGE AT AFT BRACKET SUPPORT UPPER LATCH. REMOVED BRACKET SUPPORT. INSTALLED NEW BRACKET SUPPORT IAW MD80 SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 160-200 -X55 (RT) FLOOR SUPPORT ANGLE EXFOLIATING. REMOVED FLOOR SUPPORT ANGLE. INSTALLED FLOOR SUPPORT IAW MD80 MM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 148-20 PLUS X46 LEFT FLOORBOARD SUPPORT ANGLE HAS HEAVY CORROSION. FLOOR SUPPORT ANGLE OUT OF LIMITS. LOCATED AND DRILLED HOLES ON NEW SUPPORT ANGLE. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 148-200 -46 RIGHT HAS HEAVY BLOWN OUT, CORRROSION ON FLOORBOARD SUPPORT ANGLE. CORROSION ON SUPPORT OUT OF LIMITS. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT PER MD80 SRM 51-30-1. (M)

Part: WEB — CORRODED (SUB FLOOR)

FOUND STATION 185 AT MAIN ENTRY DOOR SUB-FLOOR HAS SURFACE CORROSION. REMOVED SUB FLOOR (WEB) TO FORM NEW ONE. FORMED AND LOCATED DRILLED SUB FLOOR (WEB). INSTALLED SUB FLOOR (WEB) IAW MD80 SRM 53-14-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD PAX ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y=198 INCH X55 INCH. FOUND CORROSION OUT OF LIMITS. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED LOCATED AND DRILLED NEW FLOOR SUPPORT IAW MD80 SRM 51-10-2. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

FTW - FOUND FORWARD CABIN, LEFT SIDE FLOOR SUPPORT FRAME AT X46, STATION 160 TO 218 HAS APPROX 8 FASTENERS BROKEN OFF IN FRAME. CORROSION OUT OF LIMITS. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED, LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW MD80 SRM 53-14-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD CAIN, LEFT SIDE, FLOOR SUPPORT FRAME STATION 180 FROM X14 TO X39 HAS CORROSION IN SEVERAL AREAS. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED ANGLE Z-ANGLE. INSTALLED ANGLE FLOOR SUPPORT Z IAW MD80 SRM 53-14-1. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND CENTER FLOORBOARD IN CABIN FROM STATION 250-313 IS SPONGY. REMOVED FLOOR PANEL. FABRICATED FLOOR PANEL. INSTALLED PASSENGER CENTER FLOOR BOARD PANEL ROM STATION 250-313 IAW MD80 MM 53-20-1. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

FTW - FOUND CABIN CENTER FLOORBOARD FROM STATION 200-250 IS SPONGY. REMOVED FLOOR PANEL STATION 200-250. FORMED NEW FLOOR PANEL. INSTALLED PAX CENTER FLOOR PANEL FROM STATION 200-250 IAW MD80 M 53-20-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN, LEFT SIDE FLOOR SUPPORT FRAME AT X56 STATION 160 TO 200 HAS SEVERE CORROSION, FRAME UNDER L1 DOOR SCUFF PLATE. REMOVED FLOOR SUPPORT TO FORM NEW ONE. FORMED LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 53-14-01. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT LOWER AFT BELT FRAME PREVIOUS REPAIR STATION 750. REMOVED PREVIOUS REPAIR FROM BELT FRAME. BELT FRAME OUT OF LIMITS. FORMED AND DRILLED NEW REPAIR DOUBLER IAW SRM MD80 51-10-4 AND 53-01. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FORWARD ENTRY WAY FLOORBOARDS FS 160 TO FS 195 PLUS X8 INCH TO PLUS 57 INCHES, AND FLOORBOARDS FS 195 TO FS 235 -X22 INCH TO PLUS X57 INCHES HAS BLUE WATER STAINS AND ARE SPONGY. REMOVED 2 FLOORBOARD FS 195-256 LEFT 22-56. FABRICATED TWO FLOORBOARDS FS 195-235, PNL. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT INTERCOSTAL BETWEEN STATION 693 TO STATION 674. REMOVED CORROSION ON INTERCOSTAL AND FOUND TO BE OUT OF LIMITS. FORMED INTERCOSTAL. INSTALLED INTERCOSTAL IAW SRM MD80 51-30-5. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT CARGO ATTACH FITTING STATION 6363. FOUND BELT FRAME SUPPORT CRACKED. REMOVED BELT FRAME SUPPORT AT LONGERON 26L. REPAIRED DAMAGED AREA. INSTALLED BELT FRAME SUPPORT IAW SRM MD-80 51-30-2. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED SKINS BETWEEN STRINGERS 30 AT STRINGER STATION 712-731. REMOVED FRAME ASSEMBLY STATION 712. REMOVED FRAME ASSY STATION 731. REMOVED DAMAGED SKIN INTERNAL DOUBLER. FABRICATED REPAIR DOUBLERS AND FILLERS. INSTALLED DOUBLERS AND FILLER REPAIR. LOCATED AND DRILLED LONGERON 29 FROM STATION 665 TO 740. INSTALLED LONGERON SPLICE AT ONGERON 27 STATION 731-750. LOCATED AND DRILLED LONGERON SPLICE AT LONGERON 28 STATION 750-731. INSTALLED LONGERON SPLICE AT LONGERON 28, STATION 731-750. INSTALLED LONGERON 29L SPLICES. INSTALLED LONG SECTIONS OF LONGERON 27R, 28R, 29R, 30 INSTALLED L29L STATION 712-745. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT RECEPTICAL CRACKED AT LEFT ANGLE ATTACH TO BULKHEAD STATION 788. ROUTED OUT CRACK. FABRICATED REPAIR DOUBLER. INSTALLED PER MD80 SRM 51-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1322 L18L-L18R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB AT NUMEROUS LOCATIONS. FOUND 28L TO BE OUT LIMITS. REPAIRED FRAME. INSTALLED FRAME SPLICE IAW MD80 SRM 53-03. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT STRINGER L29L FROM STATION 693 TO STATION 674. AFTER BLENDING MATERIAL FOUND TO BE OUT OF LIMITS. REMOVED LONGERON FROM STATION 664-741. LOCATED AND DRILLED HOLE IN NEW SECTION. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1271 L23L-L23R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB. FABRICATED AND INSTALLED REPAIR IAW MD80 51-10-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1287 L23L-L23R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB AT NUMEROUS LOCATIONS. FITTING OUT OF LIMITS. INSTALLED NEW FITTING PER SRM MD80 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1309 L18L-L18R, CORROSION ON FRAME UPPER AND LOWER FLANGES AND WEB AT NUMEROUS LOCATIONS. FABRICATED 2 ANGLES AND 1 FRAME SEGMENT. REMOVED DAMAGE AREA. FABRICATED 2 PLATES. INSTALLED REPAIR PARTS IAW MD80 SRM 53-03. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT LOWER DOOR JAMB CUTOUT FROM STATION 693 TO 636. AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOOR JAMB STRAP. REMOVED OLD DOOR JAMB STRAP. INSTALLED STRAP IAW SRM MD80 51-30-5. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT INTERCOSTAL STATION 636 TO STATION 617. OUT OF LIMITS. FABRICATED NEW INTERCOSTAL FROM .040 7075-T6. INSTALLED INTERCOSTAL IN MID LOWER CARGO COMPARTMENT PER MD80 SRM 51-30. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT AFT BELT FRAME STATION 579 ABOVE STRINGER 30 AT DOT 135. MATERIAL OUT OF LIMITS. FORMER ANGLES FOR REPAIR. INSTALLED NEW REPAIR IAW MD80 SRM 53-03. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CRACKED AT AFT LEFT SUPPORT BELT FRAME STATION 636. REMOVED SUPPORT BELT FRAME STATION 636. INSTALLED NEW SUPPORT FITTING IAW MD80 SRM 51-30-5. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

FTW - MID LOWER CARGO COMPARTMENT CORRODED AT STATION 693 TO STATION 674 AT 655. REMOVED CORROSION. TEE ANGLE IAW MD80 SRM 51-30-2 AND 51-30-1. (M)

Part: INSERT — CORRODED (FLOORBOARD)

FTW - FOUND PAX CABIN ENTRY WAY, UNDER LEFT FORWARD LAVATORY, FLOORBOARD HAS 4 CORRODED INSERTS. REMOVED FLOOR PANEL. FORMED FLOOR PANEL. (M)

Part: FAIRING — DAMAGED (RT WING)

FTW - FOUND RIGHT WING HINGE COVER NR 1 DENTS, CHAFING, SEAL DAMAGE, TOOL MARKS. CHAFFED AREA WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW MD80 SRM 57-03. (M)

Part: SKIN — DENTED (ELEVATOR)

FTW - FOUND OUTBOARD LEFT ELEVATOR PANEL ACCESS DENTS, GAUGE, CHAFING, BARE METAL. AFTER FURTHER EVALUATION, FOUND CRACK ON PANEL. WELDED CRACK AREA FOR DPS. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1117 L28R CORROSION ON LOWER SURFACE OF FLOOR SUPPORT, FORWARD AND AFT SIDE. MATERIAL OUT OF LIMITS. REMOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW MD80 SRM 51-30-2. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND PREVIOUS REPAIR AT FS 759 BETWEEN LONGERON 27R AND 28R REQUIRES FINGER DOUBLER INSTALLATION. REMOVED EXTERNAL DOUBLER. FABRICATED NEW EXTERNAL DOUBLER AND FILLER. INSTALLED NEW DOUBLER AND FINGER DOUBLER IAW DC9 SRM 51-30-1. (M)

Part: SKIN — GOUGED (FUSELAGE)

FTW - FOUND GOUGE AT FS 1300 BETWEEN LONGERON 18R AND 19R REQUIRES REPAIR IAW DC9/MD80 SRM 53-04. CUT DAMAGE AREA. FABRICATED REPAIR PARTS DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW MD80 SRM 53-04. (M)

Part: FITTING — DAMAGED (FUSELAGE)

FTW - FOUND PREVIOUS REPAIR AT L1 PASSENGER DOOR HOLD OPEN FITTING REQUIRES REPLACEMENT WITH REPAIR IN DC9/MD80 SRM 53-04. REMOVED TEMP REPAIR. FABRICATED MATERIAL REPAIR. INSTALLED REPAIR PER MD80 SRM 53-04. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1155-1220 L29-28R WEB OVER DOOR THRESHOLD IS CORRODED ON UPPER AND LOWER SURFACE. DOOR BEAM FOUND TO BE OUT OF LIMITS. REMVOED DOOR BEAM FROM STATION 1111 TO 1250. REMOVED CORROSION FROM WEB OVER DOOR THRESHOLD AT STATION 1155-1220. MATERIAL LOSS ON WEB FOUND TO BE OUT OF LIMITS. DRILLED UP AND LOCATED NEW DOOR BEAM PER SRM MD80 51-10-4. (M)

Part: PANEL — CRACKED (RT WING)

FTW - RIGHT WING PANEL CRACKED AT WING STATION 120 -XFS CAN BE SEEN THROUGH WING PANEL 1679C. REMOVED RIGHT WING PANEL AT STATION 120 - XFS PANEL 1679C. INSTALLED NEW PANEL AT RIGHT WING AT WING STA 120 -XFS PANEL 1679C IAW MD80 SRM 51-30-2. (M)

Part: SPLICE — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1174 L26L CORROSION ON FRAME SPLICE STRAP AND CORRODED FASTENERS IN STRAP. MATERIAL OUT OF LIMITS. FORMED PART. INSTALLED IAW MD80 SRM 51-30-5. (M)

Part: FAIRING — DAMAGED (RT WING)

FTW - NR 3 RIGHT FLAP FAIRING TWO DENTS, SEAL CRACKED, CHAFING SEVERAL SPOTS, TOOL MARKS. ALL CHAFED SPOTS WITHIN MATERIAL LOSS LIMITS EXCEPT FOR ONE. INSTALLED REPAIR IAW MD80 SRM 51-30-2. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT 1174 L28L - FLOOR SUPPORT ANGLE IS CORRODED ON LOWER SURFACE. FOUND OUT LIMITS. REMOVED FLOOR SUPPORT ANGLE FROM STATION 1174. INSTALLED NEW ANGLE SUPPORT. (M)

Part: STRUCTURE — DAMAGED (RT NOSE COWL)

FTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM (4 O'CLOCK). REMOVED OLD FILLERS AND DOUBLERS REPAIR. FORMED DOUBLERS. INSTALLED DOUBLERS IAW MD80 SRM 51-30-8. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1015 L23L, CORROSION AROUND LONGERON TO SKIN FASTENERS. INSTALLED LONGERON AND SPLICE REPAIR IAW MD80 SRM 53-02. (M)

Part: INLET — DAMAGED (NR 2 ENGINE)

FTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM 8 O'CLOCK. REMOVED OLD FILLER AND DOUBLERS REPAIR. FORMED 2 NEW DOUBLERS IAW MD80 SRM 54-04. (M)

Part: INLET — DAMAGED (NR 2 ENGINE)

FTW - NR 2 ENGINE NOSE COWL INLET REPAIR NOT IAW SRM 1 O'CLOCK SRM. REMOVED DOUBLERS AND FILLER FROM NR 2 ENGINE NOSE COWL INLET REPAIR. FORM NEW DOUBLERS AND FILLERS IAW MD80 SRM 51-10-2. (M)

Part: LINER — CUT (NR 2 ENGINE)

FTW - NR 2 ENGINE INLET AT 9:00 POS HAS CUT IN NOISE SUPPRESSION LINER. CUT APPROX 4 INCHES LONG. CLEANED AND PREPARED SCRATCHED AREA. FILLED SCRATCH WITH ADHESIVE. (M)

Part: STIFFENER — BUCKLED (FUSELAGE)

FTW - AFT PIT STATION 1007 10 INCHES ABOVE L28R, VERTICAL STIFFENER ON FORWARD BULKHEAD IS BUCKLED/BENT. R&R STIFFENER IAW MD80 SRM 51-30-5. (M)

Part: SKIN — DELAMINATED (SPOILER)

FTW - RIGHT WING INBOARD FLIGHT SPOILER DELAMINATION. RIGHT WING INBOARD FLIGHT SPOILER REPLACED. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - FOUND MID LOWER CARGO COMP CORRODED AT INTERCOASTAL ATTACH TO CARGO TRACK BETWEEN R28 R27 FROM STATION 769 TO STATION 750. R&R INTERCOSTAL PER MD80 SRM 51-30-5. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - AFT PIT DOOR CUT OUT PANEL HAS CRACK CORROSION AND DIRTY. FABRICATED LOCATED AND DRILLED UP DOUBLER. INSTALLED REPAIR DOUBLER PER MD80 SRM SRM 51-30-2. (M)

Part: PANEL — DETERIORATED (LT WING)

FTW - FOUND LEFT WING LOWER SURFACE TRAPEZOIDAL PANEL DETERIORATED. REMOVED DAMAGED PLIES OF FIBERGLASS ON LEFT WING TRAPEZOID PANEL. REPAIR DELAMINATION AT AFECTED AREAS IAW DC9/MD80 SRM 51-90-0. (M)

Part: PANEL — DELAMINATED (RT WING)

FTW - FOUND RIGHT WING COMPOSITE TRAPIZOID PANLE HAS FASTENERS PULLING THROUGH PANEL AND POSSIBLE DELAMINATION. REMOVED DAMAGED PLIES OF FIBERGLASS FROM RIGHT WING TRAPEZOID PANEL. REPAIRED DELAMINATION AREAS ON RIGHT WING TRAPEZOID PANEL IAW DC9 MD80 SRM 51-90-0. (M)

Part: TAB — DELAMINATED (ELEVATOR)

FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB TOPSIDE HAS AREA OF DELAMINATION. BONDED REPAIR DOUBLER IAW DC9 MD80 SRM 51-70-2. (M)

Part: BOTTLE — DISCHARGED (FIRE EXTING)

FTW - APU EXTERNAL FIRE BOTTLE DISCHARGE INOPERATIVE, FAILED TEST. TROUBLESHOT AND FOUND BROKEN TERMINAL AT R2-61 APU FIRE SHUTDOWN RELAY. REPAIRED DEFECTIVE TERMINAL IAW MD80 49-31-01. (M)

Part: PANEL — DETERIORATED (LT WING)

FTW - FOUND LEFT WING LOWER SURFACE TRAPOZOIDAL PANEL DETERIORATED. REMOVED DAMAGED PILES OF FIBERGLASS ON LEFT WING TRAPEZOID PANEL. REPAIRED DELAMINATION AT AFFECTED AREAS IAW DC9 MD80 SRM 51-90-0. (M)

Part: STRUCTURE — CHAFED (CARGO DOOR)

FTW - FOUND FORWARD CARGO DOOR CHAFING SEVERAL SPOTS OUTER. LOWER AFT AT OUTER EDGE FOUND TO BE OUT OF LIMITS. FABRICATED, DRILLED AND LOCATED DOUBLER. INSTALLED DOUBLER AND FILLER PER MD80 SRM 52-05. (M)

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT)

FTW - FOUND OVERWING EMERGENCY EXIT RIGHT AFT LOWER DOOR FRAME CRACKED. REMOVED FITTING. INSTALLED FITTING IAW MD80 SRM 51-30-2. (M)

Part: FUSE — BLOWN (BATTERY CHARGER)

FLL - FOUND EMERGENCY PATH LIGHTING AFT CABIN INOPERATIVE. FOUND F1 FUSE IN BATTERY CHARGER 'OPEN' IN AFT 'PACK' ALSO FOUND LAMP MODULE SHORTED. REPLACED PICO FUSE P/N Z76005 AND LAMP MODULE, PERFORMED EMERGENCY PATH LIGHTING TEST REF MM 33-52-00, OPS CHECK OK. (M)

Part: WIRE — DAMAGED (CABIN)

DTW - FOUND EMERGENCY FLOOR TRACK LIGHTING LAST TWO INOPERATIVE. REPAIRED WIRES ON FLOOR TRACK, AFT LIGHTS. OPS CHECKS NORMAL ON GROUND IAW MM 33-53-01. (M)

Part: WIRE — BROKEN (CABIN)

DTW - FOUND EMERGENCY FLOOR TRACK LIGHTS LAST TWO IN THE BACK INOPERATIVE. FOUND BROKEN EMERGENCY FLOOR TRACK WIRE. REPAIRED WIRE ON LAST TWO EMERGENCY FLOOR TRACK LIGHTS. OPS CHECK GOOD, IAW MD-80 MM CHAPTER 33-50-01. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

FLL - FLT 439 - FOUND COCKPIT OVERHEAD EMERGENCY LIGHT OUT. RELAMPED OVERHEAD EMERGENCY LIGHTS, OPS CHECK GOOD OK IAW MM 33-50-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LGA - FLT 752 - FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS IS INOPERATIVE. RELAMPED COCKPIT OVERHEAD EMERGENCY LIGHT IAW 33-53-00. OPS CHECK NORMAL. (M)

Part: LIGHT — LOOSE (CABIN)

ACY - FLT 304 - EMERGENCY TRACK LIGHTING, FORWARD CABIN CAME LOOSE. FORWARD EMERGENCY TRACK LIGHTING REPAIRED AS REQUIRED IAW MD80 MM 33-50-01. (M)