N808NK

Part: ATTACH ANGLE — CRACKED (RT PYLON)

FTW - RIGHT PYLON T/E ATTACHED ANGLE IS CRACKED APPROX 16 INCHES FROM T/E ROOT. REMOVED DAMAGE AREA. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ANGLE. (M)

Part: SKIN — DENTED (BS 474-480)

FOUND DENT STATION 474-480, 18L X=0.028 D=1.0. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO AFT PRESSURE BULKHEAD PANEL (5318C) HAS A PULLED RIVET AND LIGHT SURFACE CORROSION, MISSING CAMLOCKS. CORROSION REMOVED, FOUND CRACK AND OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: ATTACH ANGLE — CRACKED (LT PYLON)

LEFT PYLON T/E ATTACH ANGLE IS CRACKED APPROX 16 INCHES FROM THE T/E ROOT. REMOVED DAMAGED SECTION. FABRICATED REPAIR ANGLE AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR ANGLE AND FILLER. (M)

Part: WEB — CRACKED (BS 212)

FOUND WEB CRACKED STATION 212 L15L. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLR AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (BS 389-408)

FTW - MAIN CABIN, LEFT SIDE STATION 389 TO STATION 408 CUSP WEB SURFACE HAVE CORROSION. REMOVED CORROSION FOUND WEB TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: SUPPORT — WORN (BS 351-370)

MAIN CABIN STATION 351-370 AT L4L HAS WORN SUPPORT. BLENDED WORN OUT SUPPORT STRUCTURES AND FOUND OUT OF LIMITS. FABRICATED SUPPORT STRUCTURE AT MAIN CABIN STATION 351-370. TREATED, PRIMED AND INSTALLED SUPPORT STRUCTURE. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND CRACK AT NLG RIGHT HINGE CUT OUT STATION 101. REMOVE AFT RIGHT NOSE GEAR DOOR. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED AFT RIGHT NOSE GEAR DOOR. (M)

Part: WIRE — FAILED (EPR INDICATOR)

FLT 461 - DURING CREW PREFLIGHT, FOUND NR 2 EPR GAUGE FLAG IN VIEW, AIRCRAFT TAIL SWAP WITH 829. REPAIRED WIRES AND REMOVED AND REPLACED TRI CONNECTOR, OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (RUDDER CONTROL)

UPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 1485, REPAIRED BROKEN WIRE IAW SRM. OPS CHECK, OK. (K)

Part: MOTOR — INOPERATIVE (TRIM SYS) · airframe 40,016 hrs · 22,633 cycles

PRIMARY LONG TRIM INOPERATIVE, TAIL SWAP WITH AIRCRAFT 829. REMOVED AND REPLACED LONG TRIM MOTOR AND REPAIRED MOTOR GROUNDS, SYSTEM OPS CHECK GOOD. (K)

Part: LANYARD — MISROUTED (ESCAPE SLIDE)

DTW - FOUND R1 DOOR SLIDE PULL HANDLE, INSPECT PULL HANDLE ROUTING. INSPECTED AND CORRECTED PULL LANYARD ON R1 DOOR SLIDE. NO OTHER DEFECTS NOTED. (M)

Part: LATCH — OUT OF RIG (L1 DOOR)

MAIN ENTRANCE DOOR WILL NOT LOCK. FOUND L1 DOOR INTERLOCK MECHANISM HANGING UP. LUBED SAME. ADJUSTED/RIGGED DOOR, HOLD OPEN LATCH WAS OUT OF RIG/ADJ.

Part: NOSE COWL — DELAMINATED (NR 1 ENGINE)

NR 1 ENGINE INLET COWL INNER BARREL 'DYNA RONR' WOVEN WIRE MESH DELAMINATING 3 O'CLOCK TO 9 O'CLOCK. INSTALLED CONDITION 2 REPAIR ON LEFT NR 1 ENGINE LOWER NOSE COWL, C/O NR 254595-2. (M)

Part: LANYARD — MISINSTALLED (ESCAPE SLIDE)

ACY - FOUND AFT SLIDE CONTAINER DEPLOYMENT LANYARD MANUAL DEPLOYMENT HAND STRAP AND TAILCONE DEPLOYMENT LANYARD IMPROPERLY INSTALLED. CORRECTED INSTALLATION OF CONTAINER AND TAILCONE DEPLOYMENT LANYARDS. ALSO, CORRECTED INSTALLATION OF MANUAL DEPLOYMENT HAND STRAP. (M)

Part: GIRT BAR — LOOSE (L2 DOOR)

FLL - FLT 702 - AFT GIRT BAR LOOSE ON L2. TIGHTENED SCREW AT ATTACHMENT POINT. (M)

Part: LATCH — CONTAMINATED (L1 DOOR)

MYR - FLT 1582 - FOUND LATCH ON L1 DOOR HARD TO OPEN AND SET IN GUST LOCK. CLEANED DEBRIS FROM DOOR OPEN LATCH ON L1 DOOR. (M)

Part: LANYARD — MISROUTED (SLIDE COVER)

FLL - FOUND SLIDE COVER QUICK DISCONNECT IS NOT ROUTED CORRECTLY. RE-ROUTED SLIDE COVER QUICK DISCONNECT. (M)

Part: CONTROL PANEL — INTERMITTENT (CARGO FIRE)

FLL - FOUND CARGO FIRE AND CARGO DET LOOP LIGHT ON IN FLIGHT INTERMITTENTLY. REMOVED AND REPLACED DETECTION CONTROL PANEL. SYSTEM OPS CHECK GOOD. (M)

Part: SLIDE — LOOSE (L1 DOOR)

LAS - FLT 711 - FOUND L1 SLIDE PACK COVER LOOSE. RESECURED SLIDE PACK CABLE LANYARD. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

CORRODED, ENLONGATED HOLE, AFT PIT INTERCOASTAL STA 1174. FORMED INTERCOASTAL. FABRICATED (L) FITTING.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

G2 GALLEY FLOOR BOARD AT STA 148 TO STA 200 (H) DELAMINATED. REMOVED FLOORBOARD. FAB NEW FLOORBOARD. INSTALLED FLOORBOARD.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

RT OB FLOORBOARD PANEL STA 1079-1117 PANEL DELAMINATED. BONDED FLOORBOARD.

Part: FLOORBOARD — DELAMINATED (CABIN)

G2 GALLEY FLOORBOARD AT STA 200 TO STA 256 (N) DELAMINATED. FAB NEW FLOORBOARD.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

G4 GALLEY FLOORBOARD AT STA 1117 TO STA 1287 (C) DELAMINATED. FABRICATED NEW FLOORBOARD.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

CABIN RT IB FLOORBOARD AT STA 1250-1309 DELAMINATED SEVERAL PLACES. FAB NEW CABIN FLOORBOARD.

Part: FLOOR PANEL — CRACKED (COCKPIT)

COCKPIT FLOOR PANEL CRACKED AND NON SKID MISSING. FABRICATED NEW PANEL.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

G2 GALLEY FLOORBOARD AT STA 200 TO STA 256 (P) DELAMINATED. FAB FLOORBOARD.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

G4 GALLEY FLOORBOARD AT STA 1155 TO STA 1287 (D) DELAMINATED. REPAIRED DELAMINATED AREAS.

Part: ACOUSTIC LINER — CRACKED (THRUST REVERSER)

NR 2 ENGINE THRUST REVERSER, SN 119702, INNER ACOUSTIC LINER HAS HOLE AT 8 OCLOCK POSITION AND 2 EA CRACKS AT 3 OCLOCK POSITION. REWELDED DAMAGED AREAS.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM AT STA 1309 FROM RBL 22 TO LBL 22 CORROSION. REMOVED FLOORBEAM. FABED FLOORBEAM. INSTALLED FLOOR SUPPORT.

Part: LENS — BROKEN (EMERGENCY LIGHT)

CABIN SIDEWALL PANEL LT NR 18 EMERGENCY LIGHT LENSE IS MISSING. EMERGENCY LIGHT ASSY IS BROKEN AT THE BOTTOM. REPLACED LT NR 18 SIDEWALL PANEL EMERGENCY LIGHT ASSY.

Part: ATTACH ANGLE — CRACKED (WING)

CRACK ON RT LOWER ATTACH ANGLE FOR PYLON ON AFT END. TRIMMED CRACKED AREA. FABRICATED REPAIR ANGLE. FABRICATED FILLER. INSTALLED REPAIR DOUBLER AND FILLER.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

RT OB FLOORBOARD PANEL STA 1003-1079 RIVETS PULLED AND PANEL DELAMINATED, SPACER MISSING. FABRICATED REPLACEMENT FILLER. BONDED FILLER TO RT OB FLOOR PANEL.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

CRACKED INTERCOASTAL STA 1022 TO STA 1041 BODY LINE. REMOVED DAMAGED INTERCOASTAL. FABRICATED NEW INTERCOASTAL. INSTALLED NEW INTERCOASTAL.

Part: ANGLE — CRACKED (INTERCOSTAL)

AFT FUSELAGE COMPARTMENT STA 1483 CANT, LONG 21L, INTERCOASTAL IS CRACKED. FOUND SUPPORT ANGLE IB AFT SIDE OF INTERCOASTAL CRACKED ALSO. REMOVED CRACKED INTERCOASTAL (T) ANGLE. REMOVED CRACKED SUPPORT ANGLE. FORMED NEW INTERCOASTAL (T) ANGLE. DRILLED AND LOCATED NEW INTERCOASTAL SUPPORT. INSTALLED NEW (T) ANGLE AND INTERCOASTAL SUPPORT ANGLE.

Part: FLOOR PANEL — CRACKED (COCKPIT)

COCKPIT F/O`S FLOOR PANEL CRACKED AND DRILLED OFF SCREW. CUT OUT CRACKED PART. FABRICATED DOUBLER. INSTALLED FABED PARTS.

Part: SKIN — CORRODED (LT IB TE FLAP)

LT IB FLAP T/E, PITTING CORRODED ON SKIN. REMOVED SKIN. FABED NEW SKIN, INSTALLED NEW SKIN.

Part: SKIN — CORRODED (FUSELAGE)

AFT PIT STA 1150 L29R INTERNAL SKIN DOUBLER CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

MAIN CABIN STA 470 CENTER FLOORBOARD IS SPONGY UNDER FOOT. FAB FLOORBOARD. INSTALLED NEW FLOORBOARD.

Part: FLOOR PANEL — SEPARATED

FLOOR PANEL 1251-1309 SEPARATED. FAB NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (COCKPIT)

F/O STEERING COLUMN FLOOR PANEL DELAMINATED. REBONDED DELAMINATED AREA.

Part: WEB — CORRODED (FUSELAGE)

RT CUSP WEB FROM STA 579-617 CORRODED FROM BOTTOM SIDE. CUT OUT 2 EA SECTION CUSP WEB. AT STA 553-579 AND 579-602. FABRICATED 2 EA SECTION CUSP WEB. INSTALLED 2 EA REPAIR WEB SECTIONS.

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATOIN 1079-1117 L28L CORRODED AT FASTENERS AND SPOT CORROSION AT STATION 1114. REMOVED LONGERON AFT PIT L28L STATION 1050-1127. FABRICATED LONGEORN REPAIR. FABRICATED 2 LONGERON SPLICES. INSTALLED NEW SECTION LONGERON. INSTALLED TWO LONGERON SPLICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE SKIN)

AFT PIT CARGO DOOR CUT OUT INTERNAL SKIN DOUBLER CORRODED STA 1157-1211, L26R-28R. CUT OUT DAMAGED PORTION OF INTERNAL DOUBLER. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED 2 EA REPAIR DOUBLERS AND FILLER.

Part: SEAL — BROKEN (FLOOR PANEL)

FLOOR PANEL STA 1003-1079 CORNER BROKEN NO EDGE SEAL. FABRICATED NEW FLOOR PANEL.

Part: SKIN — DENTED (FUSELAGE)

DENT AND GOUGE AT FS 446 TO FS 457 BETWEEN LONGERONS 25 AND 26R, DENT IS WITHIN THE CRITICAL AND SEMI CRITICAL OF THE RVSM CONTROLLED AREA AND REQUIRES REPAIR. CUT OUT DAMAGED SKIN (10.5 INCH X 33.5 INCH) FABRICATED REPAIR FILLER. REPAIR DOUBLERS (5 EA) AND FINGER DOUBLER. INSTALLED REPAIR.

Part: BEAM — CORRODED (FUSELAGE)

AFT PIT DOOR JAM BEAM STA 1155-1212 REPAIRED STRAP AND LOWER OB FLANGE CORRODED. REMOVED JAM BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AFT PIT STA 1309-1322 LBL 17 CARGO TIE DOWN TRACK INTERCOASTAL CORRODED UNDER NUT PLATES. REMOVED INTERCOASTAL. FABRICATED INTERCOASTAL. INSTALLED INTERCOASTAL.

Part: CUSP WEB — CORRODED (FUSELAGE)

AFT CARGO STA 1287-1309 RT LOWER CUSP WEB CORRODED. UPON FURTHER EVALUATION, FOUND A CRACK IN CUSP WEB AT STA 1280. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.

Part: WEDGE — CRACKED (AILERON)

RT WING AILERON BETWEEN TRIM TAB AND CONTROL TAB CRACKED AT WEDGE TRAILING EDGE. REPAIRED CRACK USING 181 GLASS CLOTH.

Part: ANGLE — CORRODED (FUSELAGE)

FORWARD CARGO DOOR JAMB FS 385 LONGERON 19R L-ANGLE EXFOLIATED. REMOVED L-ANGLE. FABRICATED L-ANGLE. INSTALLED L-ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

RT IB SEAT TRACK FS 1022-1309 CORRODED AND GOUGED. SEAT TRACK REMOVED FROM 1032-1309. LOCATED AND DRILLED SEAT TRACK AND SPLICES. INSTALLED RT IB SEAT TRACK AND SPLICES.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LT OB SEAT TRACK FS 927 THRU FS 1098 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACK FS 915, FS 1098. LOCATED AND DRILLED NEW SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND 2 EA SPLICES.

Part: SKIN PANEL — DENTED (RT FLAP)

RT FLAP TE NR 1 DENTED, RIVETS PULLING THROUGH. REMOVED DAMAGED SKIN. LOCATED, DRILLED NEW PANEL. INSTALLED NEW PANEL.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LT IB SEAT TRACK FS 1231 THRU FS 1309 GOUGED AND CORRODED. REMOVED LT IB SEAT TRACK. LOCATED AND DRILLED NEW TRACK. INSTALLED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LT OB SEAT TRACK FS 1098 THRU 1231 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACK. LOCATED AND DRILLED SEAT TRACK. LOCATED ADN DRILLED SPLICE. INSSTALLED SEAT TRACK AND SPLICE.

Part: ISOLATOR — OUT OF LIMITS (RT ENGINE)

RT ENGINE PYLON, LOWER VIBRATION ISOLATOR ALIGNMENT MARK MISMATCH EXCEEDS ALLOWABLE LIMITS. REMOVED LOWER VIBRATION ISOLATOR. INSTALLED VIBRATION ISOLATOR.

Part: SEAT TRACK — CORRODED (FUSELAGE)

RT OB SEAT TRACK FS1022- FS 1309 CORRODED AND GOUGED. SEAT TRACK REMOVED FROM STA 1032-1309. 3 EA SEAT TRACK SPLICES LOCATED AND DRILLED AR RBL 44 ON STA 1032, 1146 AND 1222. CRACK FOUND AS FS 1022. REMOVED DAMAGED AREA ON WEB. FABRICATED FILLER AND DOUBLER FOR WEB. INSTALLED REPAIR FILLER/ DOUBLER. INSTALLED RT SEAT TRACK SPLICES.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LT IB SEAT TRACK FS 1098 THRU 1231 CORRODED AND GOUGED. REMOVED LT IB SEAT TRACK. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND SPLICE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LT OB SEAT TRACK FS 1231 THRU FS 1309 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACKS. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED SEAT TRACK AND SPLICES.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LT IB SEAT TRACK FS 927 THRU 1098 CORRODED AND GOUGED. REMOVED LT IB SEAT TRACK FROM STA 896-1098. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND SPLICES.

Part: ANGLE — CRACKED (CARGO BAY)

AFT PIT FORWARD AND AFT DOOR LATCH SUPPORT ANGLES CRACKED. REMOVED 2 EA CRACKED SUPPORT ANGLES. FABRICATED 2 EA SUPPORT ANGLES. INSTALLED 2 EA SUPPORT ANGLES.

Part: RIB — CRACKED (RT WING)

RT WING L/E COMPARTMENT STA XRS267, L/E SUPPORT RIB IS CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.

Part: DOUBLER — CRACKED (THRUST REVERSER)

NR 1 ENGINE THUST REVERSER SN 11443, RT SIDE LOWER TR SHELL CRACKED AT PREVIOUS REPAIR DOUBLER. REMOVED CRACKED REPAIR DOUBLER. FORMED NEW REPAIR DOUBLER. INSTALLED NEW REPAIR DOUBLER.

Part: FITTING — CRACKED (CARGO BAY)

MID PIT DOOR FORWARD DOOR UPLATCH BRACKET BENT, FITTING CRACKED AND GUIDE WORN. REMOVED FITTING. INSTALLED FITTING.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (NLG)

FLL - FLT 1507 - NOSE GEAR UNSAFE LIGHT CAME ON IN CRUISE. COMPLIED WITH QRH, ACARS TO MAINTENANCE, LIGHT WENT OUT IN TURB. REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR. OPS CHECK OK ON GROUND. (M)

Part: PROXIMITY SENSOR — LOOSE (MLG)

MCO - FLT 1912 - NOSE GEAR RED LIGHT REMAINS ON WITH GEAR HANDLE UP, FOLLOWED QRH PROCEDURE. T/S FOUND NOSE GEAR UP/DOWN AND LOCKED SENSOR LOOSE. SECURED SAME. PERFORMED NOSE GEAR RETRACTION TEST SEVERAL TIMES, OPS CHECK GOOD AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (TAILCONE)

DTW - FOUND TAILCONE EMERGENCY LIGHT HAS ONE BULB INOPERATIVE. RESECURED LOOSE POWER WIRE AND RESEATED BULB TO CONTACT POWER TERMINAL. SYSTEM CHECKS GOOD. (M)

Part: COFFEEMAKER — ODOR (GALLEY)

RUBBER BURNING ODOR IN AFT GALLEY. TURNED GALLEY POWER OFF SMELL WENT AWAY. FOUND NR 1 COFFEEMAKER WOULD NOT ACCEPT WATER BUT HEATED OK. REMOVED AND REPLACED NR 1 C/M IN AFT GALLEY. OPS CHECK NORMAL AND NO ODORS. (M)

Part: MOUNT — SHIFTED (ENGINE)

DTW - FOUND FORWARD LOWER VIBE ISOLATION MOUNT SHIFTED. REPLACED FORWARD LOWER VIBE ISOLATION MOUNT. REPLACED FORWARD LOWER VIBE ISOLATION MOUNT. (M)

Part: APU — LEAKING (APU BAY)

ABOUT 2 MIN AFTER SELECTING AIRFOIL ANTI-ICE A BURNING ODOR ENTERED THE CABIN AND WAS DETECTABLE IN THE COCKPIT. SMELL WENT AWAY WHEN AIRFOIL ANTI-ICE WAS TURNED OFF. ODOR WAS APPARENT ALSO WHEN TAIL DE-ICE WAS SELECTED. REMOVED AND REPLACED APU. OPS AND LEAK CHECK GOOD. (M)

Part: ENGINE — FAILED (LEFT)

ORD - FLT 1442 - SHORTLY AFTER TAKEOFF, THE NR 1 ENGINE LOST OIL PRESSURE AND OIL QUANTITY AT 1000 FEET AGL, APPROX 2 MINUTES AFTER IDENTIFYING AND RUNNING CHECKLISTS NR 1 ENGINE WAS SHUTDOWN NR 1 HAD 0 OIL QTY AT SHUTDOWN AND HAD BEEN AT IDLE POWER FOR MORE THAN 1 MINUTE, OIL PRESSURE WAS AT APPROX ZERO ENGINE WAS AT WINDMILLING SPEED FOR ABOUT 4-5 MINUTES. REMOVED AND REPLACED ENGINE LEFT SIDE IAW SPIRIT AIRLINES TASK CARD 00191. LEAK AND OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

DTW - FLT 1253 - AIRFOIL DE-ICE ON LEFT AND RIGHT ICE PROTECTION LOW LIGHTS STAY ON 90 PERCENT OFF TIME, FLT IDEL LIGHT STAYS ON 100 PERCENT OF THE TIME MAX SUPPLY PRESSURE 7 LBS. BOTH SIDES CABIN PRESSURE FLOW LIGHT COMES ON. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)

Part: ENGINE — FAILED (LEFT)

DEN - FLT 980 - IN FLIGHT ENGINE FAILURE OF LEFT ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: WIRE — BROKEN (CABIN)

FTW - FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE. L1 DOOR EMERGENCY CARRY AROUND LIGHT STAYS ON WHEN NOT ARMED AFTER ARMING AND DISARMING. FOUND LOOSE TERMINAL WIRING ON EMERGENCY LIGHTING BATTERY CHARGER, REPAIRED WIRING. FOUND BROKEN WIRES ON CONNECTOR AT PORTABLE BATTERY CHARGER LIGHT AT L1 DOOR, REPAIRED WIRES. (M)

Part: TERMINAL — LOOSE (CABIN)

FTW - FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND TERMINAL LOOSE ON TERMINAL STRIP 53-384, SECURE TERMINAL LUG. (M)

Part: SKIN — CORRODED (FUSELAGE)

EXT FUSELAGE STA 1474 (AT RAIN GUTTER) LEFT SIDE CORROSION ON SKIN. CUT OUT DAMAGED AREA OF SKIN, FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER.

Part: SOCKET — DIRTY (A/C BAY)

FTW - FOUND FLIGHT COMPARTMENT EMERGENCY FLOOD LIGHTS INOPERATIVE. TAIL COMPARTMENT RIGHT SIDE OF SLIDE LIGHT INOPERATIVE. FOUND LAMP SOCKETS NEED CLEANING, CLEANED SOCKETS. TROUBLE SHOT TAIL EMERGENCY LIGHT ON RT SIDE SLIDE AND FOUND SOCKETS NEEDED TO BE CLEANED, CLEANED SOCKET. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND CORRODED FORMER IN UNPRESSURIZED TAIL SECTION FS 1418 LBL 18. REMOVED FORMER. LOCATED AND DRILL FITTING. INSTALLED NEW FORMER FITTING. (M)

Part: SKIN — CRACKED (CARGO DOOR)

FTW - FOUND FORWARD CARGO DOOR HANDLE CUT OUT IS CRACKED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

CABIN FLOOR PANEL HAS EXPOSED INTERNAL HONEYCOMB STRUCTURE. FS 1249, LBL 35. REPAIRED DAMAGED AREA IN CABIN FLOOR PANEL.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AFT FUSELAGE STA 1380-1401 L28L, INTERCOSTAL IS CORRODED. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, INSTALLED NEW INTERCOSTAL.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO PIT: LONGERON 30L FS 1212, CORRODED. REMOVED L30 SECTION. FABRICATED LONGERON 30 SECTION AND SPLICE REPAIR. INSTALLED L30 AND SPLICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED STATION 190 JUST INBOARD OF MAIN ENTRY DOOR. REMOVED FLOOR SUPPORT ANGLE. FABRICATED NEW FLOOR SUPPORT ANGLE. INSTALLED FLOOR SUPPORT ANGLE. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - E/E COMPARTMENT LONGERON 30 STATION 120 TO 133 HAS CORROSION FOUND ON REMOVAL OF BATTERY TRAY TO FOM. DRILLED NEW STRINGER 30, INSTALLED L30. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - E/E COMPARTMENT LONGERON 30 STATION 120 TO 133 HAS CORROSION FOUND ON REMOVAL OF BATTERY TRAY TO FOM. DRILLED NEW STRINGER 30. INSTALLED L30. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

FTW - FOUND AFT FUSELAGE STATION 1497 RT AFT PLATFORM IS CRACKED AT RT FRAME. STOP DRILLED CRACK. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: FLOOR PANEL — CRACKED (COCKPIT)

FLIGHT COMPT, STA 120 TO STA 140.8 FLOOR PANEL HAS CRACK/ CORROSION. FABRICATED NEW FLOOR PANELS. INSTALLED NEW FLOOR PANELS.

Part: FLOORBOARD — CRACKED (FUSELAGE)

FLOORBOARDS, STA 160 TO STA 190 RIGHT CENTER PANEL IS CRACKED AND DELAMINATED, CORRODED. FABRICATED NEW FLOORBOARD, INSTALLED NEW FLOORBOARD.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FLIGHT COMPARTMENT, FLOOR PANEL STATION 120 TO STATION 160 CENTER SOFT/MUSHY CORROSION. FABRICATED NEW FLOORBOARD. INSTALLED NEW FLOORBOARD. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN, RIGHT STATION 120 TO 200 HAS TWO FITTINGS CORRODED. LOCATED AND DRILLED NEW FITTINGS. INSTALLED NEW FITTINGS. (M)

Part: FLOORBOARD — DELAMINATED (LAVATORY)

LT AFT LAV ASSY, SEVERAL AREA OF DELAMINATED AND DAMAGED FLOORBOARD SUPPORT LAV ASSY. FABBED NEW LAV FLOOR BOARD, INSTALLED NEW LAV FLOORBOARD.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND FLOORBOARD LEFT INBOARD STATION 160 TO 196 CRACKED/DAMAGED AND CORRODED. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND FLOORBOARD RIGHT INBOARD STATION 160 TO STATION 180 SOFT/DAMAGED. FABRICATED FLOORBOARD PANEL. INSTALLED FLOORBOARD PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND FLOORBOARD RIGHT OUTBOARD STATION 196 TO 256 SOFT/MUSHY CORROSION. FABRICATED FLOORBOARD. INSTALLED FLOORBOARD. (M)

Part: SUPPORT BRACKET — DAMAGED (FUSELAGE)

AFT FUSELAGE STA 1380 LOWER ANGLE CAP SUPPORT AFT CANTED BULKHEAD. REMOVED LOWER (T) ANGLE, LOCATED AND DRILLED NEW LOWER (T) ANGLE. INSTALLED NEW (T) ANGLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AFT FUSELAGE, LEFT STA 1380 TO STA 1401, CORRODED AT INTERCOSTAL. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, INSTALLED NEW INTERCOSTAL.

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FLIGHT COMPARTMENT, COPILOT SIDE STATION 148, FLOOR PANEL IS CRACKED/DAMAGED AT CORNERS, 2 EACH PLATE ATTACH PANEL IS CORRODED. FABRICATED NEW PANEL. INSTALLED NEW PANEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND FLOORBOARD RT INBOARD STATION 180-200 CRACKED/DAMAGED/CORRODED. FABRICATED FLOOR BOARD. INSTALLED FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND FLOORBOARD LEFT INBOARD STATION 160 TO STATION 196 SOFT/MUSHY CORRODED. FABRICATED FLOOR PANEL. INSTALLED FLOOR PANEL. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

FTW - FOUND VENTRAL STAIRWAY JAMB CORRODED AT LT SIDE STATION 1418-1485. AFTER CLEANING FOUND EXFOLIATED DOUBLER. REMOVED EXFOLIATED DOUBLER. FABRICATED ANGLE. INSTALLED ANGLE. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

AFT FUSELAGE STA 1437 TO STA 1418 CORRODED AT AFT ANGLE ATTACH TO FLANGE APU GROUND CONTROL AND FIRE DOOR. REMOVED CORRODED ANGLE, FORMED NEW ANGLE, INSTALLED NEW ANGLE.

Part: SKIN — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO PIT FS 520-693 SKIN CORRODED BETWEEN LONGERONS 27L-27R. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CARGO STRINGER 29R FLOOR SUPPORT CORRODED FS 351-427. REMOVED FLOOR SUPPORT. INSTALLED SUPPORT FLOOR. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FORWARD LAVATORY EQUIPMENT DAMAGED AT FLOORBOARD SUPPORT. REMOVED DAMAGED FLOORBOARD FORWARD LAVATORY. FABRICATED NEW FLOORBOARD FORWARD LAVATORY. INSTALLED NEW FLOORBOARD FORWARD LAVATORY. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CARGO PIT STRINGER 30 CORRODED FROM FS 389-446, FORWARD CARGO FS 389-408 STRINGER 30 CORRODED. FOUND FORWARD CARGO FS 427-446 STRINGER 30 CORRODED, FORWARD CARGO FS 408-427 STRINGER 30 CORRODED. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - PASSENGER CABIN FLOOR PANEL STATION 160 TO STATION 190 GOUGES, SOFT DAMAGE. FABRICATED FLOORBOARD. INSTALLED FLOORBOARD. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CARGO PIT STRINGER 29L CORRODED AT FS 376-446. FORWARD CARGO FS 427-446 STRINGER 29L CORRODED. FORWARD CARGO FS 408-427 STRINGER 29L CORRODED. FORWARD CARGO STRINGER 29L CORRODED FS 370-389. FORWARD CARGO FS 389-408 STRINGER 29L CORRODED. INTERCOSTAL FOUND TO BE OUT OF LIMITS STRINGER 29L STATION 446 TO BE OUT OF LIMITS. FORMED NEW INTERCOSTAL. CUT OUT EXISTING AREA. FABRICATED FORWARD SPLICE. INSTALLED NEW SPLICE AT STATION 416. FABRICATED NEW SPLICE FOR STATION 446-460. INSTALLED INTERCOSTAL. INSTALLED NEW LONGERON SECTION FS 416-455. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO PIT STRINGER 29R CORRODED AT FS 712-750, FS 788-817. MID CARGO FS 712-731 STRINGER 29R CORRODED. MID CARGO FS 731-750 STRINGER 29R CORRODED. MID CARGO STRINGER 29R CORRODED FS 807-817. MID CARGO FS 807-788 STRINGER 29R CORRODED. REMOVED DAMAGED LONGERON SECTION STATION 712-740. FABRICATED A NEW LONGERON SECTION AND SPLICE. FLOORBOARDS SUPPORT OUT OF LIMITS. LOCATED AND DRILLED AND DEBURRED REPAIR 'L' ANGLE 2. INSTALLED NEW LONGERON AND SPLICE. INSTALLED REPAIR 'L' ANGLES 2 STRAP ON FLOORBOARD SUPPORT BEAM. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND PASSENGER CABIN, FLOOR PANEL STATION 200-256, SOFT/MUSHY DAMAGED. FABRICATED PASSENGER CABIN FLOOR PANEL. INSTALLED FLOOR PANEL. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - AFT PIT CORROSION FS 1250-1287 LONGERON 29R AND LWR SIDE CORRODED AT SPLICE. REMOVED DAMAGED SECTION. FABRICATED LONGERON SECTION. INSTALLED THE LONGERON SECTION. FABRICATED LONGERON SPLICE. INSTALLED SPLICE REPAIR. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOORBOARD SUPPORT CORRODED, LBL45, STA200. REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT, INSTALLED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOORBOARD SUPPORT STA 218 LBL4, CORRODED. C/A: FABRICATED NEW EXTRUSION FLOORBOARD SUPPORT. INSTALLED FLOORBOARD SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOORBOARD SUPPORT CORRODED LBL 60 STATION 195. FORMED NEW ANGLE FLOOR SUPPORT. INSTALLED FLOOR SUPPORT ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOORBOARD SUPPORT CORRODED LBL 51 STATION 160-185. REMOVED SUPPORT ANGLE. FABRICATED SUPPORT ANGLE. INSTALLED FLOOR SUPPORT ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOORBOARD SUPPORT CORRODED RBL 1 STATION 180. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOORBOARD SUPPORT CORRODED, RBL16, STA 200. REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT CORRODED LBL63 STA 160-200. REMOVED FLOOR SUPPORT, FABBED NEW FLOOR SUPPORT, INSTALLED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOORBOARD SUPPORT LBL 8 STATION 200-256 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND WEBBING AT FORWARD LAVATORY LBL 41 STATION 233 CORRODED. CUT OUT THE DAMAGED AREA. FABRICATED DOUBLERS REPAIR AND FILLER. INSTALLED DOUBLERS REPAIR AND FILLER. (M)

Part: CLIP — CRACKED (FLOOR SUPPORT)

FORWARD CARGO FS 427 FLOOR SUPPORT CLIP, CRACKED. REMOVED FLOOR SUPPORT CLIP, FABRICATED SUPPORT CLIP, INSTALLED FLOOR SUPPORT CLIP.

Part: STRINGER — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO STRINGER 28L CORRODED FS 576-579. REMOVED DAMAGED AREA. FABRICATED SPLICE ON LONGERON SECTION. INSTALLED SPLICE AND LONGERON. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

FTW - FOUND AFT CABIN STATION 1338 CRACK AT STIFFENER SUPPORT AFT LEFT LOWER DOOR JAMB. REMOVED CRACKED STIFFENER. FABRICATED REPLACEMENT SUPPORT. INSTALLED REPLACEMENT SUPPORT. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FORWARD CARGO FS 220 CEILING AREA WEB CRACKED RBL 46 INCHES. CUT OUT DAMAGED SECTION OF WEB. FABRICATED FILLER AND DOUBLER. INSTALLED DOUBLER AND FILLER. (M)

Part: LONGERON — CORRODED (FUSELAGE)

MID CARGO PIT STA 28R CORRODED. REMOVED LONGERON, DRILLED AND LOCATED NEW LONGERON SECTION, INSTALLED NEW SECTION OF LONGERON.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FTW - FOUND AFT CABIN STATION 1338 FLOORBEAM CORRODED RBL 20 INCHES. REMOVED DAMAGED AREA. FABRICATED ANGLE AND FILLER. INSTALLED ANGLE AND FILLER. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FTW - FOUND RIGHT KEEL BEAM INTERIOR STRUCTURE HAS SEVERAL AREAS OF CORROSION STATION 826-843. REMOVED SUPPORT FITTING. REMOVED BATHTUB FITTING. REMOVED CORROSION FROM RIGHT KEEL BEAM HORIZONTAL FLANGE FOUND TO BE OUT OF LIMITS. FABRICATED NEW FITTING AT STATION 826, LONGERON 29R. LOCATED AND DRILLED LONGERON 29R FITTING. INSTALLED LONGERON 29R FITTING. FABRICATED REPAIR DOUBLER -3. LOCATED AND DRILLED NEW FITTING AT STATION 843 RIGHT. LOCATED AND DRILLED BATHTUB FITTING. INSTALLED -3 DOUBLER IAW SPIRIT AIRLINES EA 5310-0247. INSTALLED 3936377-2 FITTING AT STATION 843 RIGHT. INSTALLED RIGHT BATHTUB FITTING. (M)

Part: FLOORBEAM — CORRODED (CABIN)

AFT CABIN STA 1322 CORROSION ON FLOORBEAM. FABRICATED REPAIR ANGLE AND FILLER INSTALLED REPAIR PARTS.

Part: LONGERON — CORRODED (FUSELAGE)

AFT PIT, CORROSION FS 1250-1271 LONG 28R, LWR SIDE CORRODED AT SPLICE. REMOVED DAMAGED SECTION, DRILLED NEW LONGERON, FABRICATED LONGERON SPLICE, INSTALLED SPLICE AND LONGERON SECTION.

Part: LONGERON — CORRODED (FUSELAGE)

FTW - AFT PIT FS 1287 LONGERON 29R CORROSION OUTBOARD FLANGE UNDERSIDE, HI-LOCK. INSTALLED LONGERON. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT FS 1174-1193 SUBFLOOR WEB OUTBOARD OF OUTBOARD SEAT TRACK CORRODED. REMOVED DAMAGED WEB. FABRICATED NEW WEB AND DOUBLER. INSTALLED NEW WEB AND DOUBLER. (M)

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO PIT FRAME AT STA 1200 BETWEEN LONGERONS 28L AND 30 HAS CORROSION AT SPLICE. LONGERON 28L AT STA 1203 IS CORRODED OUT OF LIMITS. FABRICATED LONGERON 28L SECTION AND SPLICE. INSTALLED LONGERON AND SPLICE.

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND AFT CARGO PIT FS 1287-1309 RIGHT SIDE OUTBOARD SEAT TRACK SUB FLOOR WEB CRACKED AT LIGHTENING HOLE OR STIFFENER HOLE, SEVERAL AREAS OF CORROSION AND MISSING OR PULLED FASTENERS. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: LIGHT — BROKEN (AFT AIRSTAIRS)

FTW - THREE AFT AIRSTAIRS EMERGENCY LIGHTING ASSEMBLY BROKEN. REMOVED THREE AFT AIRSTAIRS EMERGENCY LIGHTING ASSEMBLY. INSTALLED THREE AFT AIRSTAIR EMERGENCY LIGHTING ASSEMBLY. DURING INSPECTION FOUND A FOURTH LIGHT BROKEN. INSTALLED ONE AFT AIRSTAIR EMERGENCY LIGHTING. (M)

Part: LONGERON — CRACKED (FUSELAGE)

AFT PIT STA 1287-1309 L25L, LONGERON SPLICE IS CRACKED ALONG RADIUS AT LONGERON TO SKIN FASTENERS. REMOVED SPLICE, LOCATED AND DRILLED NEW SPLICE/ INSTALLED NEW SPLICE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

MID CARGO STA 28R JAMB BEAM CORRODED FS 535 OUTBOARD SIDE AND INBOARD SIDE. REMOVED MID CARGO JAMB BEAM. HOLES LOCATED AND DRILLED ON NEW JAMB BEAM, INSTALLED NEW JAMB BEAM.

Part: STRAP — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO ST 628 SUB FRAME UPPER STRAP CORRODED UNDER SUPPORT. FABRICATED NEW STRAP. INSTALLED NEW STRAP. (M)

Part: NOSE COWL — OVERHEATED (RT ENGINE)

FTW - FOUND RIGHT ENGINE NOSE COWL INLET LIP HAS EVIDENCE OF OVERHEATING FROM 9 TO 8 O'CLOCK POSITION. REMOVED NR 2 ENGINE NOSE COWL. INSTALLED SERVICEABLE NOSE COWL. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

AFT PIT STA 1287-1309 BLO, INTERCOSTAL UPPER FLANGE IS CRACKED AT FASTENER HOLES, AREAS OF CORROSION AT AFT END. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL.

Part: CLIP — CRACKED (FUSELAGE)

FTW - FOUND FS 840 KEEL BEAM LEFT BATHTUB FITTING UPPER T-CLIP CRACKED. REMOVED BATHTUB FITTING. REMOVED T-CLIP. FABRICATED NEW TEE CLIP. LOCATED AND DRILLED TEE. INSTALLED TEE CLIP. LOCATED AND DRILLED LEFT BATHTUB FITTING. INSTALLED LEFT BATHTUB FITTING. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1338 L29R-L29L EXISTING T-CHORD REPAIR ON AFT SIDE OF FRAME HAS EXFOLIATION CORROSION. FOUND OUT OF LIMITS. REMOVED CORROSION ON BULKHEAD WEB AND LONGERON SUPPORT. FABRICATED WEB DOUBLER, REPAIR SPLICE, ANGLES AND SPLICERS. FABRICATED WEB DOUBLER, REPAIR SPLICE, ANGLES AND SPLICERS. LOCATED AND DRILLED NEW LONGERON SUPPORT FRAME, FITTINGS AND ANGLES. INSTALLED ANGLE SUPPORTS, REINFORCING ANGLES, BULKHEAD SPLICE REPAIR WEB AND NEW FITTINGS. (M)

Part: SPLICE — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1322-1338 L23R, LONGERON SPLICE IS CORRODED. REMOVED LONGERON SPLICE. DRILLED AND LOCATED NEW LONGERON SPLICE. INSTALLED NEW LONGERON SPLICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 1088-1183. REMOVED LEFT OUTBOARD SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN RIGHT INBOARD SEAT TRACK WORN AND CORRODED FS 1259 TO AFT END OF TRACK. REMOVED SEAT TRACK. DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 1012-1088. REMOVED LEFT INBOARD SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FTW - FOUND PASSENGER CABIN CENTER FLOOR PANEL FS 200 IS CAVED IN AND DELAMINATED. REMOVED FLOORBOARD. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M)

Part: SKIN — CRACKED (NR 1 SLAT)

RIGHT NR 1 SLAT OUTBOARD LEADING EDGE METAL STRIP UPPER SIDE IS CRACKED. FORMED NEW MATERIAL STRIP, INSTALLED NEW SLAT METAL STRIP.

Part: SKIN — CRACKED (CARGO DOOR)

AFT CARGO DOOR SKIN GOUGED AND CRACKED BELOW HANDLE. ROUTED OUT GOUGE AND CRACK FABBED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER.

Part: COMPUTER — MALFUNCTIONED (COCKPIT)

LGA - FLT 706 - WITH DFGC SELECTED TO POSITION 2 WHEN MACH VERTICAL SPEED SELECTED WILL NOT ENGAGE MACH BUT REMAINS IN IAS WHEN DFGC NR 1 SELECTED WORKS FINE. REMOVED AND REPLACED DFGC PER MD80 MM 22-01-01, SYSTEM OPS CHECK GOOD. (M)

Part: CONTROL PANEL — FAILED (COCKPIT)

FLT 706 - LGA - IAS/MACH BUTTON WILL NOT SWITCH TO MACH ON DFGS NR 2, OK ON NR 1. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL. PERFORMED OPS HECK IAW MM 22-01-05. OPS CHECKS NORMAL. (M)

Part: WIRE — CHAFED (AUTOPILOT)

ORD - AUTOPILOT AND AUTOTHROTTLES KICKED OFF AT 240. TAIL KICKED TO ONE SIDE TURNED OFF YAW DAMPER AND HAND FLEW AIRCRAFT. PERFORMED SYSTEM TROUBLESHOOTING AND SERVO/SENSOR OPERATION IAW MD80 MM 22-01-03. NOTED 2 CHAFED WIRE ON LUG NR 2 TERMINAL S-30-5. BUT SPLICED WIRES IAW MD80 MM 22-50-01. PERFORMED RTS CHECK IAW MD80 MM 22-01-05. NO FAULTS ERRORS DETECTED SYSTEM OPERATION NORMAL AT THIS TIM. (M)

Part: SERVO — FAILED (AUTOPILOT SYS)

FLT 386 - DTW - AUTOPILOT WILL NOT STAY ENGAGED, TRIPS OFF EVERY 2-3 MINUTES, DFGS NR 1 OR NR 2, ALT TRIM OK. FOUND ELEVATOR POWER SERVO FAIL IN FLIGHT FAULT REVIEW. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 21-12-01, PERFORMED AUTO PILOT CHECK AND RTS. OPS CHECK GOOD IAW MM 22-10-00 AND 22-01-01. (M)

Part: CONTROL VALVE — FAILED (SPOILERS)

DTW - FOUND INBOARD SPOILERS ON BOTH WINGS DO NOT DEPLOY ON GROUND. REMOVED AND REPLACED RIGHT GROUND SPOILER CONTROL VALVE PER MD80 MM 27-62-04, SYSTEM OP CHECK AND LEAK CHECKED GOOD. (M)

Part: ANNUNCIATOR — FAILED (COCKPIT)

FLL - FLT 774 - FMA DOES NOT DISPLAY IN ANY MODE. FAILED EN ROUTE. REMOVED AND REPLACED F/O'S FMA'S IAW 34-24-00. OPS CHECK NORMAL. (M)

Part: THROTTLE — LACK OF LUBE (COCKPIT)

LAX - DURING APPROACH AND DESCENT, THE RIGHT THROTTLE WOULD NOT ADVANCE FROM ITS IDLE STOP, ONCE THE RIGHT THROTTLE WAS MOVED FORWARD OFF TAIL STOP IT WOULD ADVANCE AND MATCH THE LEFT. CLEANED AND LUBED THROTTLES. PLACARD REMOVED. (M)

Part: GYRO — FAILED (COCKPIT)

FLT 923 - AUTO PILOT AND AUTO THROTTLE DISENGAGES AND FMA GO TO GO AROUND MODE. WHEN PERFORMING RTS FOUND AUX GYRO BAD. REMOVED AND REPLACED AUX GYRO IAW MD80 MM 34-23-01, PERFORMED RTS SYSTEMS OPS CHECK GOOD IAW MD80 MM 22-01-05. (M)

Part: HANDLE — UNSECURE (MLG WW)

FLL - FLT 1780 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. BURNED FUEL DOWN, LANDED AT 138,400 TURNED OFF R/W. GEAR DOOR LIGHT CAME ON STOPPED AIRCRAFT CALLED MAINTENANCE. INSPECTED MLG DOOR, FOUND BYPASS HANDLE IN UNSECURED POSITION. WITH HYDRAULICS ON, CYCLED GEAR DOOR (RT) CLOSED, RELEASED HANDLE (GEAR BYPASS) DROPPED DOOR. RESECURED BYPASS HANDLE, RIGHT DOOR CLOSED AND LOCKED NO DAMAGE TO HINGE OR ACTUATOR OR BUMPER FOUND ON VISUAL INSPECTION IAW MD80 MM 32-10-00/32-31/00. (M)

Part: BATTERY — DISCHARGED (CABIN)

FLL - EMERGENCY EXIT LIGHT AT LEFT AFT SERVICE DOOR INOPERATIVE, EMERGENCY LIGHTING SYSTEM. FOUND BATTERIES DEAD IN BATTERY POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY REF MM 33-53-00 AND WDM 33-51-14. OPS CHECK OK. (M)

Part: COMPUTER — FAULTY (COCKPIT)

FTW - P1 AT VARIOUS TIMES DURING FLIGHT, FLT GUIDANCE SYSTEM WOULD DEFAULT TO HEADING HOLD. NR 1 FGC REPLACED PER MD-80 MM 22-01-01. SYSTEM RETURNED TO SERVICE CHECK GOOD PER MD-80 MM 22-01-05. (M)

Part: COMPUTER — FAULTY (COCKPIT)

FTW - P2 COULD NOT ARM ILS OR VOR/LOC AUTOPILOT OR FLIGHT DIRECTOR. REMOVED AND REPLACED NR 1 DFGC PER MD-80 MM 22-01-01 SYSTEM OPS CHECK GOOD PER MD-80 MM 22-01-05. (M)

Part: AUTOTHRUST SYS — FAULTY (COCKPIT)

FTW - AUTOTHROTTLE WILL NOT STAY ENGAGED AT APPROACH. REMOVED AND REPLACED IAW MD-80 MM 22-01-02. SYSTEM GROUND TEST GOOD. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FTW - AFT STAIR LEFT SIDE SUPPORT ANGLE IS CRACKED. REMOVED DAMAGED ANGLE. FABRICATED NEW PART. (M)

Part: SKIN — DELAMINATED (CONTROL TAB)

RIGHT CONTROL TAB HAS DELAMINATION ON THE BOTTOM (MARKED IN RED) DOT NR 005. REMOVED AREAS OF DELAMINATION IAW DC-9 MM. FABRICATED REPAIR DOUBLER IAW DC-9 MM MD 80 SRM 55-04. INSTALLED DOUBLER IAW DC-9 MD-80 SRM 55-04. WEIGHED AND BALANCED TAB PER BOEING. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

FTW - FOUND MID LOWER CARGO COMPARTMENT, CRACK AT BELT FRAME SUPPORT ABOVE STRINGER 29L STATION 655. REMOVED CRACKED SUPPORT PER MD-80 SRM 51-30-2. REPAIRED SUPPORT. INSTALLED SUPPORT PER MD-80 SRM 51-30-2. (M)

Part: BELTFRAME — CORRODED (FUSELAGE)

FTW - FOUND CORROSION ON BELT FRAME AT STATION 1041 BETWEEN 27L AND 27R. REMOVED CORROSION IAW SRM MD-80 SRM 51-10-3. FORMED NEW ANGLE FOR REPAIR IAW SRM MD-80 51-10-02. LOCATED AND DRILLED ANGLE IAW IAW MD-80 SRM 53-01. INSTALLED ANGLE IAW MD-80 SRM 51-30-2. (M)

Part: CLIP — CRACKED (FUSELAGE)

FTW - AFT B/B BOTTOM FORWARD DOOR CUTOUT CORNER CLIP IS CRACKED. REMOVED CRACKED CLIP IAW MD-80 SRM 51-30-2. FORMED CLIP IAW MD-80 SRM 51-10-02. LOCATED AND DRILLED CLIP IAW MD-80 SRM 51-10-02. INSTALLED CLIP IAW MD-80 SRM 51-30-02. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

FTW - AFT CARGO COMPARTMENT CRACKS AT LEFT BELTFRAME SUPPORT STATION 1212. REMOVED SUPPORT BRACKET IAW MD-80 SRM 51-30. FABRICATED NEW SUPPORT BRACKET IAW SRM 51-10-1. INSTALLED IAW MD-8- SRM 51-30-2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - FOUND CORROSION AND CRACKS FOUND ON LONGERON L-26 BETWEEN 2ND AND 3RD FRAME FORWARD OF MID CARGO DOOR. REMOVED FINGER DOUBLER UNDER LONGERON L26. FORMED FINGER DOUBLER IAW MC-80 MM SRM 53-01. INSTALLED FINGER DOUBLER IAW MD-80-MM 51-30-2. (M)

Part: RIB — GOUGED (L/E SLAT)

FTW - RIGHT WING NR 5 SLAT 4TH RIB FROM INBOARD HAS DEEP GOUGE. REMOVED DAMAGED RIB IAW MD-80 SRM 51-30-02. FORMED NEW RIB IAW MD-80 SRM 51-10-2. INSTALLED RIB IAW MD-80 SRM 51-30-2. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - MLG WHEEL WELL LEFT STATION 785-Z25 BETWEEN AFT BULKHEAD AND WIRING ROOT FRAME HAS A CRACK. REMOVED FRAME IAW BOEING DC-9 SRM 51-10-2. FABRICATED FRAME IAW BOEING DC-9 SRM 51-10-02. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 33 FLOOR PATH LIGHT COVER (RED) BROKEN. TRANSFERRED TO DMI 115800-2 IAW 33-24 OF MD 80 MEL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DTW - EMERGENCY CEILING LIGHTS ROWS 19-21 IS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY PACK AND OPS CHECK GOOD IAW MM 33-50-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - EMERGENCY PATH 1ST LIGHT NOT WORKING. RELAMPED 1ST SOCKET OF EMERGENCY PATH LIGHTING IAW MD 80 MM 25-62-05. OPS CHECK GOOT AT THIS TIME. NO DEFECTS NOTED. (M)

Part: WIRE — DISCONNECTED (CABIN)

LAX - FLT 606 - EXIT LIGHT FOR L2 DOOR INOPERATIVE. RECONNECTED WIRE FOR EMERGENCY LIGHT (EXIT) OF L2 DOOR. OPS CHECK OK. (M)

Part: WIRE — DISCONNECTED (ROW 29)

LAX - FLT 606 - EMERGENCY TRACK LIGHTING ROW 29 AND AFT INOPERATIVE. RECONNECTED WIRING OF EMERGENCY TRACK LIGHTING BETWEEN ROWS 29 AND AFT. OPS CHECK OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - EMERGENCY PATH LIGHTING NOT WORKING FROM ROW 29 AFT. GROUND CHECKED EMERGENCY PATH LIGHTING AND FOUND IT TO BE OPERATIONAL. ALL LIGHTS LIT UP. ALL IAW MD 80 MM SECTION 33-53-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 624 - EMERGENCY LIGHTING SYSTEM LIGHT IN CEILING LEFT SIDE AFT BURNED OUT. COULD NOT DUPLICATE DISCREPANCY. OPS CHECK ALL EMERGENCY LIGHTS GOOD IAW MD 80 MM 33-53-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 501 - ISLE PATH LIGHT IN REAR OF AIRCRAFT INOPERABLE. REMOVED AND REPLACED LENS ON EMERGENCY PATH LIGHTS; FUNCTIONAL CHECK GOOD REF - MK 80MM 33-53-01. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - EMERGENCY EXIT LIGHT ASSEMBLY IS NOT PROPERLY WORKING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM CH 33-00-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 419 - AISLE LIGHTS NOT ALL WORKING. REMOVED AND REPLACED EMERGENCY AISLE TRACK LIGHT IAW MD-80 MM 33-50-00. ALL OPS NORMAL. (M)

Part: LENS — MISSING (CABIN)

DTW - FLT 378A - LENS COVER FOR PATH LIGHTING LAST ROW, STARBOARD SIDE IS OFF LIGHT. HARDWARE IN FORWARD GALLEY. RELAMPED PATH LIGHTING AND REINSTALLED LIGHT COVER AND TRACKING IAW MD-80 MM 33-53-01. OPS CHECKS GOOD, NO DEFECTS NOTED. (M)

Part: LIGHT — DISCONNECTED (CABIN)

EWR - FLT 447 - EMERGENCY TRACK FLOOR LIGHTING IS OUT IN BACK. RECONNECTED EMERGENCY TRACK RED LIGHT. OPS CHECK OK. (X)

Part: LIGHT — LOOSE (CABIN)

DTW - AISLE PATH LIGHTING IN REAR OF AIRCRAFT IS COMING OFF THE FLOOR. REMOVED AND REPLACED CRACKED SECTIONS OF AISLE EMERGENCY LIGHT PATH AND TRIM IAW MD-80 MM 25-20-00. EMERGENCY LIGHTING FUNCTION NORMAL. (X)

Part: SWITCH — CONTAMINATED (FLAP WARNING)

TPA - FLT 632 - DURING POWER APPLICATION, TAKEOFF WARNING HORN SOUNDED (FLAPS). ALL FLIGHT CONTROLS WERE IN THEIR PROPER POSITION. FOUND FLAP HANDLE WARNING SWITCH S1-492 COVERED WITH DUST/FUZZ. CLEANED SWITCH. SYSTEM OPS GOOD PER MM 31-51-02. (X)