N818NK

Part: HANDLE — LACK OF LUBE (PAX DOOR)

MAIN ENTRANCE DOORS OUTSIDE HANDLE STAYED EXTENDED WITH DOOR LOCKED, HAD IT PUSHED IN. LUBRICATED DOOR HANDLE ASSEMBLY OPS CHECK NORMAL AT THIS TIME. (M)

Part: LANYARD — MISINSTALLED (R1 DOOR SLIDE)

FLL - R1 DOOR ESCAPE SLIDE LANYARD INSTALLED INCORRECTLY. ROUTED LANYARD CORRECTLY. (M)

Part: LIGHT — DISCONNECTED (TAIL COMPARTMENT)

DTW - FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT NOT CONNECTED. CONNECTED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT. (M)

Part: VANE — DELAMINATED (T/E FLAP)

FTW - FOUND RIGHT WING INBOARD FLAP INBOARD FIXED VANE DELAMINATED. REPAIRED RIGHT WING INBOARD FLAP FIXED VANE. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND MID PIT BILGE, SHEAR TIE CORRODED AT STATION 579. CUT OUT DAMAGED SHEAR TIE. SUB CHART FOR 2014-T6 IS 7075-T6. FABRICATED NEW SHEAR TIE AND DOUBLERS. INSTALLED SHEAR TIE AND TWO DOUBLERS. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND MID PIT BILGE, SHEAR TIE CORRODED AT STATION 598. CUT OUT SHEAR TIE. FABRICATED NEW SHEAR TIE. SUB CHART FOR 2014-T6 IS 7075-T6. INSTALLED NEW SHEAR TIE. (M)

Part: FITTING — CORRODED (FUSELAGE)

FOUND LONGERON 28L END FITTING CORRODED AT APB. REMOVED END FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED NEW FITTING. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

FRAME SUPPORT CRACKED STATION 218 STRINGER 18L-17L, HIDDEN DAMAGE. REMOVED CRACKED SHEAR CLIP. FABRICATED SHEAR CLIP. INSTALLED FRAME, SHEAR CLIP. (M)

Part: FITTING — CRACKED (NGL WW)

FOUND NLG W/W STATION 69.5 LEFT SIDE UPPER OUTBOARD TEE FITTING CRACKED LBL 16 INCHES. REMOVED DAMAGED FITTING. INSTALL NEW TEE FITTING. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 208 BETWEEN LONGERONS 17L AND 18L, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. REMOVED DAMAGED SKIN. SKIN CUTOUT (13 INCHES BY 40 INCHES). FABRICATED NEW SECTION OF SKIN, DOUBLER AND FINGER DOUBLER. FABRICATED 7 STRAP AND 23 DOUBLER. INSTALLED REPAIR PARTS. (M)

Part: ENGINE — FAILED

FOUND ENGINE HAS LEAK AT N1 TACH GENERATORS. ENGINE FAILED BORESCOPE INSPECTION ENGINE TO BE SENT OSV FOR REPAIR. (M)

Part: FLOOR PANEL — DETERIORATED (FUSELAGE)

FTW - FOUND FLOOR PANEL STATION 1174-1287 DETERIORATING, BROKEN INSERTS EDGE SEAL BROKEN OUT. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FTW - FOUND FLOOR PANEL STATION 148-160 EDGES SEPARATING. FABRICATED NEW FLOOR PANEL. (M)

Part: SUPPORT FITTING — CRACKED (CARGO DOOR)

FTW - FOUND AFT CARGO DOOR CRACKED ANGLE SUPPORT UPPER AFT SIDE. REMOVED CRACKED ANGLE SUPPORT. INSTALLED NEW ANGLE SUPPORT FITTING. (M)

Part: FLOOR PANEL — DETERIORATED (FUSELAGE)

FTW - FOUND FLOOR PANEL AFT ENTRY DOOR, EDGE SEAL DETERIORATING. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FOUND RIGHT COCKPIT FLOOR PANEL, EDGE BROKEN, METAL L ANGLE BRACKET CORRODED, PLASTIC BARRIER BROKEN. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FTW - FOUND FLOOR PANEL STATION 207-299, CORNERS DELAMINTATED, EDGE SEAL BROKEN OUT. FABRICATED NEW FLOOR PANEL. (M)

Part: RECEPTACLE — CRACKED (EMERGENCY EXIT)

FTW - FOUND RIGHT AFT EMERGENCY EXIT DOOR JAMB AFT LOWER LOCK PIN RECEPTACLE CRACKED. REMOVED CRACKED RECEPTABLE. INSTALLED RECEPTACLE. (M)

Part: CHANNEL — CRACKED (FLOOR PANEL)

FTW - FOUND LT OUTBOARD FLOOR PANEL STATION 945 HAT CHANNEL CRACKED. REPAIRED CRACKED AREAS. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - E/E COMPARTMENT STATION 160 L25L CRACKED. REMOVED SHEAR TIE SECTION AT STATION 148 LONGERON 26L-24L. REMOVED LONGERON SECTION FROM STATION 141-170. FABRICATED LONGERON SECTION AND TWO LONGERON SPLICES. FABRICATED SHEAR TIE SPLICE. INSTALLED NEW LONGERON SECTION. INSTALLED NEW SHEAR TIE SPLICE. (M)

Part: FLOOR PANEL — DETERIORATED (FUSELAGE)

FTW - FOUND FLOOR PANEL LEFT MID DETERIORATING, WRONG INSERTS, MISSING INSERTS. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — CRACKED (COCKPIT)

FOUND LT COCKPIT FLOOR PANEL 4415A, NON SKID WORN OFF, CRACKED, CHAFING/SURFACE CORRODED. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLERS. (M)

Part: STRAP — CORRODED (CARGO DOORWAY)

FOUND AFT CARGO DOOR JAMB BEAM AND REPAIR STRAP CORRODED. JAMB BEAM REPAIR STRAP IS FOUND TO BE OUT OF LIMITS. REMOVED JAMB BEAM REPAIR STRAP. FABRICATED NEW REPAIR STRAP. INSTALLED NEW JAMB BEAM REPAIR STRAP. (M)

Part: FLOOR PANEL — CRACKED (COCKPIT)

FOUND RT COCKPIT FLOOR PANEL HAS CRACK, HAT CHANNEL BENT, DELAMINATED AT RUB STRIP, CORRODED, PLASTIC BARRIER BROKEN SEAL LOOSE AND TORN. FABRICATED NEW PANEL. (M)

Part: SPLICE — CORRODED (FUSELAGE)

FTW - FOUND CABIN STATION 1338 STRINGER 18L WEB CORRODED TOP AND BOTTOM. REMOVED SPLICE. FABRICATED NEW SPLICE. INSTALLED NEW SPLICE. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FTW - FOUND COCKPIT CENTER FLOOR PANEL, INSERT DRILLED THROUGH, INSERT MISSING, DELAMINATED AT EDGES. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FTW - FOUND FLOOR PANEL STATION 207-256, CORNERS DELAMINATED, INSERTS MISSING, EDGE SEAL MISSING. FABRICATED NEW FLOOR PANEL. (M)

Part: PRESSURE PANEL — CORRODED (RT MLG WW)

FOUND RIGHT MLG W/W CEILING PRESSURE WEB HAS CORROSION RUNNING UNDER STIFFENERS IN NUMEROUS AREAS. FABRICATED PRESSURE FLOOR DOUBLER AND INTERNAL FINGER DOUBLER. INSTALLED REPAIR PARTS. (M)

Part: FLOOR PANEL — DETERIORATED (FUSELAGE)

FTW - FOUND FLOOR PANEL CENTER STATION 945-980, DETERIORATING, MISSING INSERTS. FABRICATED NEW FLOOR PANEL. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - FOUND CABIN STATION 1315 STRINGER 18L CORRODED. FORMED NEW ANGLE REPAIR. INSTALLED ANGLE DOUBLER. REPAIR ACCOMPLISHED EA 5310-0325. REMOVED FITTING. DRILLED UP NEW FITTING. INSTALLED NEW FITTING. (M)

Part: FRAME — CORRODED (FUSELAGE)

FOUND AFT PIT STATION 1338, FRAME CORRODED BOTH SIDES AT LONGERON 22-23L, WEB WALL CORRODED ON AFT SIDE AT LONGERON 26-25R, WEB WALL AND STIFFENER AT LONG 26L. REMOVED CORROSION AT WEB AND SITFFENER AT L26L STATION 1338. MATERIAL LOSS OUT OF LIMITS. REMOVED STIFFENER, HAT. FABRICATED TWO DOUBLER. INSTALLED REPAIR AT WEB. LOCATED AND DRILLED NEW PART. INSTALLED NEW PART. (M)

Part: FITTING — WORN (FUSELAGE)

FTW - FOUND CABIN STATION 1309 LBL 34 - LBL 49 B/H L BRACKET WORN IN SEVERAL AREAS. UPON FURTHER EVALUATION, FOUND FITTING CRACKED AT STATION 1309 LBL 34. REMOVED FITTING. DRILLED AND LOCATED NEW FITTING. INSTALLED NEW FITTING. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND NLG W/W STATION 69.5 LEFT AND RIGHT UPPER TEE FITTINGS HAVE CORRODED AT RBL 16 AND LBL 16 AND WEB CORRODED AT LEFT SIDE. REMOVED DAMAGED FITTING. FURTHER INVESTIGATED LEFT FITTING CRACKED, REMOVED CRACKED FITTING. INSTALLED TWO TEE FITTINGS. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CABIN SUBFLOOR CORRODED AT FS 200 6 INCHES LBL TO 6 INCHES RBL. REMOVED CORRODED WEB. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: HORN — CORRODED (RT ELEVATOR)

FTW - FOUND RIGHT ELEVATOR BALANCE HORN CORRODED AROUND ATTACHED STRUCTURE INSIDE. REMOVED RIGHT ELEVATOR BALANCE HORN. INSTALLED NEW BALANCE HORN. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND MAIN CABIN F/B STATION 807-927 RIGHT OUTBOARD IS CRACKED AT BOTH ENDS. TRIMMED DAMAGED AREA AT FORWARD END WITHIN LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORTS CORRODED THREE AT FS 160 15 INCHES, 32 INCHES, AND 42 INCHES LBL. MATERIAL LOSS ON CABIN FLOOR SUPPORT FS 160 15 INCHES AND 42 INCHES LBL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED TWO CABIN FLOOR SUPPORT AT FS 160 15 INCHES AND 42 INCHES LBL. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND MAIN CABIN F/B STATION 807-927 RT OB IS CRACKED AND SPACER MISSING. FABRICATED MAIN CABIN OB FLOOR PANEL. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 176, 25 INCHES RBL. REMOVED CORRODED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND R1 DOOR THRESHOLD AREA CORRODED AT FS 168-200 57 INCHES RBL. FOUND CORROSION ON FLOOR SUPPORT AT FS 154-200 RBL 52 INCHES. FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 6 INCHES RBL - 6 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180 8 INCHES -43 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND RIGHT AFT LAV FLOORBEAM CORRODED AT FS 1322 27 INCHES RBL AND 3 CORRODED BROKEN NUT PLATES. (M)

Part: WEB — DAMAGED (FUSELAGE)

FTW - FOUND CABIN STATION 905-927 STRINGER 17L DAMAGED WEB AND FASTENERS INSTALLED INCORRECTLY. FABRICATED NEW WEB. INSTALLED WEB. (M)

Part: BAR — CORRODED (T/E FLAP)

FTW - FOUND LEFT WING FLEX JOINT HAS CORROSION AT UPPER LUG, AND LOWER BAR. REMOVED LEFT FLEX JOINT BAR ASSEMBLY. INSTALLED SERVICEABLE LEFT FLEX JOINT BAR ASSEMBLY. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - CABIN METAL FLOOR PANEL IS CRACKED AT FS 484 RIGHT OUTBOARD PANEL. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FTW - FOUND PAX CABIN CRACKED ANGLE UNDER CABIN FLOOR AT FS 828, 42 RBL. STOP DRILLED AT CRACKED ANGLE. FABRICATED TWO REPAIR ANGLES. INSTALLED ANGLE REPAIR. (M)

Part: FLOOR PANEL — CRACKED (FS)

FTW - FOUND CABIN CENTER FLOOR PANEL STATION 886-946 MISSING EDGE FILLER, TWO METAL SIDE SUPPORTS CRACKED/WORN. BAD INSERTS. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FTW - FOUND CABIN CENTER FLOOR PANEL STATION 946-1003 MISSING EDGE FILLER/DELAMINATED UPPER SURFACE TORN OFF. FABRICATED NEW CABIN CENTER FLOOR PANEL. (M)

Part: FITTING — CRACKED (T/E FLAP)

FTW - FOUND LEFT WING INBOARD FLAP INBOARD STRUCTURE FLAP ACTUATOR FITTING CRACKED. LOCATED AND DRILLED LEFT WING INBOARD FLAP ACTUATOR FITTING. INSTALLED LEFT WING INBOARD ACTUATOR FITTING. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FOUND FORWARD NOSE WHEEL WELL LONGERON AT NWW DOOR CUTOUT HAS A CRACK IN THE WEB AT FORWARD RT CORNER AT DOOR JAMB. UPON FURTHER INVESTIGATION, FOUND WEB NOT TO BE CRACKED, BUT DID FIND WEB SUPPORT ANGLE CRACKED. REMOVED SUPPORT ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW SUPPORT ANGLE. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND CABIN METAL FLOOR PANEL HAS PULLED FASTENERS AND TORN/CRACKED EDGE AT FS 1007-1079 LEFT OUTBOARD PANEL. REMOVED FLOOR PANEL. FABRICATED REPLACEMENT PANEL. INSTALLED FLOOR PANEL. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND CABIN METAL FLOOR PANEL IS CRACKED AT FS 389 RIGHT OUTBOARD PANEL. REMOVED CABIN FLOOR PANEL. TRIMMED OUT DAMAGE. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. INSTALLED RIGHT OUTBOARD FLOOR PANEL. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND CABIN CENTER FLOOR SUPPORT PANEL MISSING EDGE FILLER, TWO METAL SIDE SUPPORTS CRACKED, BAD INSERTS STATION 807-886. FABRICATED NEW CABIN CENTER FLOOR PANEL. (M)

Part: RELAY — FAILED (COCKPIT)

FTW - WHEN EMERGENCY DC BUS FEED C/B IS PULLED THE CAPTAINS, F/O'S, LEFT PEDESTAL AND CENTER INSTRUMENT PANEL LEFT FLOODLIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED R2-22 RELAY. (M)

Part: PANEL — CORRODED (RT WING)

FTW - FOUND RIGHT WING PANEL 1242C HAS CORROSION 3 PLACES. FABRICATED NEW WING PANEL EA 5730-0311. (M)

Part: STRUCTURE — DELAMINATED (SPOILER)

FTW - FOUND RIGHT WING GROUND SPOILER DELAMINATED. REPAIRED DELAMINATION. (M)

Part: EXHAUST DUCT — DELAMINATED (THRUST REVERSER)

FTW - FOUND RIGHT ENGINE T/R S/N 49507 ACOUSTIC EXHAUST DUCT INTERIOR NUMEROUS AREAS OF DELAMINATION. REPAIRED DAMAGED AREA. (M)

Part: JOINT — CORRODED (T/E FLAP)

FTW - FOUND RIGHT WING FLEX JOINT CORRODED. REMOVED RIGHT WING FLEX JOINT BAR. INSTALLED NEW RIGHT WING FLEX JOINT BAR. (M)

Part: CLIP — BROKEN (GIRT BAR)

DTW - FLT 461 - R1 DOOR SLIDE COVER RIGHT GIRT BAR CLIP BROKEN. REMOVED BROKEN CLIP. INSTALLED NEW CLIP ASSY. (M)

Part: CONNECTOR — INOPERATIVE (MLG UPLOCK)

WITH GEAR UP ON DESCEND INTO LGA THE RED NOSE GEAR LIGHT ILLUMINATED SEVERAL TIMES-OUT FOR LANDING. PERFORMED BITE ON PSEU OF NOSE GEAR LOCKED AND NOSE GEAR UP POSITION SENSORS, BOTH PASS. CLEANED AND RESET CONNECTOR UPSTREAM OF D1-31 NOSE GEAR UP POSITION SENSOR. OPS CHECKED NORMAL.

Part: UPLOCK — INOPERATIVE (MLG)

RED NOSE GEAR LIGHT ILLUMINATED BRIEFLY TWO TIMES APPROACHING SJU GEAR HANDLE WAS UP NO USUAL NOISE NOTED GEAR EXTENDED NORMALLY. PERFORMED BITE TEST ON PSEU OF NOSE GEAR UPLOCK, CLEANED SENSOR OF EXCESS GREASE, CHECKED CONNECTOR AND WIRING. OPS CHECK GOOD, NO FAULTS FOUND AT THIS TIME.

Part: PROXIMITY SENSOR — INTERMITTENT (NLG)

ORD - FLT 433 - NOSE GEAR UNSAFE LIGHT CAME ON AT FL330, LIGHT EXTINGUISHED AFTER PRESSURIZING HYDRAULICS. DETERMINED THE NLG GEAR UP PROXIMITY SENSOR IS OPERATING INTERMITTENTLY. REMOVED AND REPLACED THE NOSE GEAR UP SENSOR. (M)

Part: CHARGER — FAILED (CABIN)

FTW - FOUND SEVERAL EMERGENCY LIGHTS IN TAIL SECTION INOPERATIVE. FOUND BAD BATTERY CHARGER SUPPLY, AFTER FURTHER TROUBLESHOOTING FOUND DEFECTIVE WIRING, REPAIRED WIRING, OPERATION CHECKS GOOD. (M)

Part: WIRE — BROKEN (CABIN)

FTW - PORTABLE EMERGENCY LIGHT (L-1) NEON BULB INOPERATIVE. SPLICED BROKEN WIRE. LIGHT OPS CHECK GOOD. (M)

Part: CONTROL CABLE — LOOSE (SPOILERS)

FTW - FOUND SPOILER SURFACE POSITION INPUT FAILED DFDR GROUND CHECKED. T/S SYSTEM FLIGHT SPOILERS ONLY DEPLOY TO 37 USING SPEED BRAKE HANDLE. CHECK TENSION ON BODY CONTROL CABLE OF SPEED BRAKE CABLES RN 159 AND 160. FOUND TENSION LOW, RETENSION CABLES. (M)

Part: WIRE — BROKEN (EXIT SIGN)

FTW - FOUND EXITS SIGNS AT L1, R1 AND L2 DOORS INOPERATIVE. TROUBLESHOT EXITS SIGNS, FOUND WIRES BROKEN ON L1, R1, AND L2 EXIT SIGNS. REMOVED L1, R1, AND L2 EXIT SIGNS. INSTALLED EXIT SIGNS, OPS CHECK GOOD. (M)

Part: YOKE — CORRODED (RT ENGINE)

FTW - FOUND RIGHT MOUNT YOKE WITH CORROSION (PIT) ON THE BACK SIDE UPPER AND LOWER. REPAIRED YOKE ON BACKSIDE, UPPER AND LOWER AREAS PER SPIRIT AIRLINES EA 5410-0204, ORIGINAL ISSUE DATED 6-20-02. (M)

Part: YOKE — CORRODED (RT ENGINE)

FTW - FOUND RIGHT MOUNT YOKE UPPER AND LOWER COVER PLATES WITH CORROSION AND TOOL MARKS. REPAIRED UPPER AND LOWER ENGINE MOUNT YOKE COVER PLATED PER SPIRIT AIRLINES EA 54-10-0204 ORIGINAL ISSUE DATED 6-20-02. (M)

Part: SUPPORT — CORRODED (CARGO BAY)

FTW - FOUND AFT CARGO STATION 1322 CENTER L30 POST SUPPORT CORRODED. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICATED NEW POST. POST SUPPORT WAS PREVIOUS REMOVED ON CARD B-3418NN00055. INSTALLED NEW POST. (M)

Part: BRACKET — CRACKED (L1 DOOR)

FTW - FOUND L1 DOOR UPPER BRACKET CRACKED. REMOVED CRACKED BRACKETS. FABRICATED NR 2 BRACKET. INSTALLED TWO BRACKETS. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

FTW - FOUND MID PIT FORWARD BULKHEAD, STATION 541 L29R, VERTICAL BULKHEAD POST IS CRACKED IN 2 PLACES AT LOWER FORWARD IN RADIUS. REMOVED BULKHEAD POST AT STATION 541 L29R. STOPPED DRILLED CRACKS. FABRICATED DOUBLERS TWO EACH. INSTALLED REPAIR DOUBLERS. INSTALLED BULKHEAD POST. (M)

Part: SPLICE — CORRODED (FUSELAGE)

FTW - FOUND TWO FRAME SPLICES CORRODED. FABRICATED TWO SPLICES. DRILLED UP AND LOCATED NEW SPLICES. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND END FITTING AT LONGERON 22L STATION 1338 WITH EXFOLIATION. FITTING BEYOND LIMITS. REMOVED FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED NEW FITTING. (M)

Part: ATTACH ANGLE — DAMAGED (TAIL)

FTW - FOUND REPLACED DORSAL FIN ATTACH ANGLE PER EA 5310-208A. REMOVED 5939711-501 AND 502 ANGLES. LOCATED AND DRILLED NEW. INSTALLED -3 AND -4 ANGLES. EA 5310-208A SIGN OFFS PERFORMED AND DOCUMENTED ON EOA W/C B00034-11R-00006. (M)

Part: DOUBLER — CORRODED (STRUT)

FTW - FOUND STRUT DOUBLERS CORRODED. DOUBLER FOUND TO BE OUT OF LIMITS. FABRICATED NEW DOUBLER PER SRM MD80. (M)

Part: PANEL — DELAMINATED (LT WING)

FTW - FOUND LEFT TRAPEZOID PANEL DELAMINATED, LEFT WING. REMOVED DELAMINATED PANEL. REPAIRED LEFT TRAPEZOID PANEL USING 181 GLASS CLOTH. INSTALLED TRAPEZOID PANEL. (M)

Part: SPLICE — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO LONGERON 30 STATION 589 SPLICE HAS CORROSION. LOSS FOUND TO BE OUT OF LIMITS. DUPLICATED LONGERON SPLICE, L30, AT FUSELAGE STATION 589. INSTALLED NEW SPLICE AT STATION 589 L30 IAW MD80 SRM 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND STATION 1322 ABOUT 4 INCHES AWAY FROM L22L, FRAME EXFOLIATED. AREA ON FRAME FOUND TO BE OUT OF LIMITS. AFTER FUTHER EVALUATION FOUND 2 INTERCOSTALS AT STATION 1322 L22L CORROSION OUT OF LIMITS. REMOVED FRAME DAMAGED SECTION FROM LONGERON 18L TO LONGERON 28R. FABRICATED TWO INTERCOSTAL, DRILLED AND LOCATED NEW FRAME SECTION. INSTALLED NEW FRAME SECTION AND STRUT DOUBLER TWO INTERCOSTAL AT STATION 1322. INSTALLED REPAIR SPLICE FOUD, TWO INTERCOSTALS AT STATION 1322 LONGERON 27L, THREE FROM ANGLES FROM L23L TO LONGERON 27R AT STATION 1322. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FTW - MID CARGO INTERCOSTAL STATION 541-560 LONGERON 26L CRACKED TWO PLACES. FORMED NEW INTERCOSTAL AND ATTACHING L-ANGLE. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND PAX CABIN CORRODED AT THE WEB STATION 180 PLUS X57 INCHES. CUT OUT DAMAGED WEB SECTION AND FABRICATED NEW WEB SECTION AND DOUBLER. INSTALLED WEB SECTION. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN WEB CORRODED AT THE STATION 180 PLUS X57 INCHES. CUT OUT DAMAGED WEB SECTION AND FABRICATED NEW WEB SECTION AND DOUBLER, INSTALLED WEB SECTION. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT THE FRAME STATION 731. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED FRAME ANGLE IN AREA. DRILLED AND LOCATED NEW FRAME ANGLE. INSTALLED NEW FRAME ANGLE. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO INTERCOSTAL STATION 541-560 LONGERON 29R CRACKED, TOOL MARKED AND CORROSION. FORMED NEW INTERCOSTAL. INSTALLED INTERCOSTAL AT STATION 541-560 L29R IAW MD80 SRM 51-30-5. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT HAS CORROSION AT LONGERON 23L STATION 1338. REMOVED CORROSION FROM AREA. FOUND FITTING TO BE OUT OF LIMITS. DRILLED UP AND LOCATED NEW FITTING. INSTALLED NEW FITTING. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND SUB FLOOR FROM STATION 218 TO 237 -X48 TO -X56 IS CRACKED. REMOVED CRACKED SUB FLOOR. FABRICATED NEW SUB FLOOR. INSTALLED SUB FLOOR. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND SUB FLOOR FROM STATION 200 TO 218, -X23 TO -X56 IS CORRODED AND CRACKED. REMOVED CORRODED WEB SECTION. FABRICATED NEW SUB FLOOR WEB. INSTALLED NEW SUB FLOOR. (M)

Part: BEAM — CORRODED (DOOR FRAME)

FTW - AFT PIT LOWER DOOR CUT OUT HAS CORROSION AT OUTBOARD BEAM SURFACE ANGLE ALONG EDGE BEAM. BEAM OUT OF LIMITS AT STATION 1188 AND STATION 1171. FABRICATED DOUBLER AND SPACER. INSTALLED DOUBLER AND SPACER. (M)

Part: BRACKET — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT CORRODED AT GANG CHANNEL LEFT ATTACH BRACKET END OF CARGO TRACK SIDE, AND TWO RUSTED NUTS. MATERIAL LOSS IS FOUND TO BE OUT OF LIMITS. INSTALLED ATTACHING FITTING. (M)

Part: FITTING — CORRODED (FUSLEAGE)

FTW - FOUND AFT PIT CORRODED AT LONGERON 30 STATION 1007 TO STATION 1022. FABRICATED BATHTUB FITTING PER SPIRIT AIRLINES EA 5310-0231. INSTALLED BATHTUB FITTING. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 200-256 LEFT FOUR BROKEN INSERTS AND CORE BROKEN. FABRICATED A NEW FLOORBOARD STATION 200-256, LEFT. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND WEB CORRODED AT FS 83, X=48 Z=11. AFTER CORROSION THE WEB IS FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW IAW MD80 SRM 51-30-2 AND 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT THE FRAME STATION 636. REMOVED FRAME AT STATION 636 BETWEEN L29R-L26L. FABRICATED NEW FRAME. INSTALLED NEW REPAIR PART. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND PAX CABIN HAS CORROSION AT SUPPORT FLOOR STATION 200 PLUS 55 INCHES. FLOOR SUPPORT IS OUT OF LIMITS. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FITTING — CRACKED (FUSELAGE)

FTW - FOUND MID PIT CORROSION AT AFT FITTING SUPPORT CARGO STATION 693. REMOVED FITTING. FOUND THAT FITTING WAS CRACKED. INSTALLED NEW FITTING. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN HAS CORROSION AT SUPPORT FLOOR STATION 218 PLUS X2 INCHES. FLOOR SUPPORT FOUND OUT OF LIMITS. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION BARE METAL AT RIGHT AFT Z-ANGLE. REMOVED Z-ANGLE AT MID PIT STATION 693 MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED Z-ANGLE. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND MID PIT CORRODED AT LONGERON 30 STATION 788. MATERIAL LOSS OUT OF LIMITS. FABRICATED -3 STRAP. REV 0 DATED JUNE 19, 2002 AND EA 5310-0230. INSTALLED 3 STRAP. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND MID PIT HAS CORROSION AT LONGERON 30 SPLICE AND RUSTED NUTS AND HI-LOCKS (20 EACH) STATION 598, 579, 560 AND STATION 617. LONGERON 39 IS OUT OF LIMITS STATION 549-588. FABRICATED LONGERON 30. INSTALLED LONGERON 30 FROM STATION 496 TO 589. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

FTW - FOUND L1 DOOR LOWER THRESHOLD ATTACH ANGLE HAS CORROSION PLUS X60 INCH STATION 200 TO STATION 168. CUT OUT DAMAGED AREA. FORMED NEW REPAIR ANGLE. INSTALLED REPAIR ANGLE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN HAS CORROSION AT RIGHT OUTBOARD SEAT TRACK STATION 237, STATION 200. FOUND SEAT TRACK OUT OF LIMITS. DRILLED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - E/E COMPARTMENT STATION 189 -X6 WEB HAS CORROSION VIEWED, E/E CEILING. SUB FLOOR WEB FOUND OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN CORROSION AT RIGHT INBOARD SEAT TRACK -X23 STATION 237 STATION 200. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND PASSENGER CABIN CORRODED AT LEFT INBOARD SEAT TRACK STATION 207, 218, 229 PLUS X23 INCHES. SEAT TRACK CORRODED OUT OF LIMITS. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN HAS CORROSION AT THE WEB STATION 168.7 STATION 180 PLUS X57 INCHES. PASSENGER CABIN HAS CORROSION AT THE WEB FORWARD LEFT LOWER CORNER DOOR STATION 160 TO STATION 148.5 PLUS X55 INCHES. PASSENGER CABIN HAS CORROSION AT THE WEB STATION 218 PLUS X59 INCHES. REMOVED CUSP FROM STATION 155 TO 225 LEFT SIDE. FABRICATE CUSP. FABRICATED TWO DOUBLERS STATION 154 AND 180. INSTALLED TWO DOUBLER ON CUSP. INSTALLED CUSP FROM STATION 150 TO 230, PLUS 59. (M)

Part: INTERCOSTAL — CORRODED (CARGO BAY)

FTW - FOUND FORWARD PIT HAS CORROSION AT INTERCOSTAL STATION 465 TO STATION 484. SKIN CRACKED TO BE REPAIRED PER S/B 53-188. FABRICATED -85 DOUBLER. FABRICATED -79 DOUBLER AND -7 SKIN. FORMED PARTS -11, -13, -15, -17, -19, -21, -23, -25, -26, -27, -29, -31, -33, -149, -37, -39, -41, -43, -35, -103 IAW MD80 SRM 51-10-2. FORMED PARTS -3, -5, -6 INTERCOSTAL IAW MD80 SRM 51-10-2. FABRICATED -45 FITTING. INSTALLED ALL S/B NR 53-188 PARTS. (M)

Part: LONGERON — CHAFED (FUSELAGE)

FTW - FORWARD LIGHT CORROSION BARE METAL AT LONGERON 29L STATION 503, 484. MATERIAL LOSS OUT OF LIMITS. FABRICATRED -3 STRAP PER DWG NO 53100228-1 9SH 2 OF 2) EA 5310-0228. INSTALLED -3 STRAP. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

FTW - FOUND AFT FUSELAGE RIGHT BEHIND THE RUDDER TRIM AND LOAD-FEEL CABLE DRUM THERE IS A DOUBLER CRACKED. REMOVED EXISTING REPAIR DOUBLER. FABRICATED NEW REPAIR DOUBLER. INSTALLED REPAIR DOUBLER PER DC9 SRM 51-30-1. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND AFT FUSELAGE BESIDE RIGHT AIRSTAIR ACTUATOR, FLOOR PANEL CRACKED. REMOVED CRACKED FLOOR PANEL RIGHT SIDE AIRSTAIR. FABRICATED REPAIR. INSTALLED FABRICATED PARTS ON THE REMOVED PANEL. (M)

Part: STRAP — CRACKED (MLG)

FTW - FOUND LEFT WING LOWER SURFACE MLG STRAP HAS CRACK. PERFORMED HFEC INSPECTION OF SUSPECTED CRACKED HOLES IN STRAP AND LOWE WING SKIN PLANK. REPAIR DAMAGED AREA IAW MD80 SRM 57-03 AND SPIRIT AIRLINE DRAWING NR 57300206-1. (M)

Part: ISOLATION MOUNT — WRONG PART (NR 2 ENGINE)

FOUND ENGINE NR 2 LOWER VIBRATION ISOLATOR, INDEX YACK MISMATCH. REMOVED ENGINE NR 2 LOWER VIBRATOR ISOLATOR. INSTALLED NR 2 ENGINE LOWER VIBRATION ISOLATOR. (M)

Part: PANEL — CRACKED (RT WING)

FTW - FOUND RIGHT WING L/E PANEL NR 1246C HAS TOOL MARKS ARE BARE METAL ON BACK. UPON BLENDING CRACK FOUND AT FASTENER HOLE. FORMING DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 51-30-2. (M)

Part: WEB — CORRODED (FS 160-180)

FTW - FOUND CUSP WEB CORRODED FROM STATION Y150 TO STA Y160 PLUS X57 (L1 JAMB AREA. MATERIAL OUT OF LIMITS. REMOVED WEB STATION 160 TO STATION 180 PLUS 59. CUSP WEB WAS INSTALLED ON W/O B-34 PLUS 0. (M)

Part: PANEL — CORRODED (RT WING)

FTW - FOUND RIGHT WING L/E PANEL NR 1244C CHAFFED AND BARE METAL ON BACK, TOOL MARKS ON SKIN. IN THE PROCESS OF BLENDING CHAFING CORROSION WAS FOUND. FORMER STRAP REPAIR. INSTALLED STRAP REPAIR IAW SRM MD80 51-30-2. (M)

Part: WIRE — BROKEN (CONTROL PANEL)

FTW - FOUND WITH EMERGENCY POWER ON SOME FORWARD PANEL LIGHTS WENT OUT. FOUND WIRE BROKEN. REPAIR WIRING. REMOVED WIRING. REMOVED AND REPLACE LAMP. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND FLOOR PAN SUBFLOOR/WEB CORRODED AT STATION Y200, -X20 TO -X43, VIEWED FROM E/E BAY. REMOVED CORRODED WEB SECTION. FABRICATED NEW WEB SECTION. INSTALLED NEW SUB FLOOR. (M)

Part: FIRE LOOP — DEFECTIVE (CARGO BAY)

'B' LOOP FAIL LIGHT STAYS ON OVERHEAD CARGO FIRE EXTINGUISHER AND DETECTION PANEL FOR AFT CARGO COMPARTMENT. REMOVED AND REPLACED 'B' LOOP FIRE DETECTION UNIT, REF MM 26-30-00. OPS CHECK OK. (M)

Part: SMOKE DETECTOR — FAULTY (CARGO BAY)

FLL - 'A' LOOP FAIL LIGHTS STAYS ON OVERHEAD CARGO FIRE EXTINGUISHER AND DETECTION PANEL FOR AFT CARGO COMPARTMENT. REMOVED AND REPLACED AFT CARGO COMPARTMENT 'A' LOOP SMOKE DETECTOR, OPS CHECK IAW 26-50-00, OPS NORMAL. (M)

Part: WIRE — ARCED (CABIN)

ACY - EMERGENCY FLOOR PATH LIGHTING ARCING DURING GROUND TEST. REPAIRED AND REPLACED WIRES AND LIGHT STRIP ON EMERGENCY FLOOR PATH LIGHTING IAW 33-53-01, OPS CHECK GOOD. (M)

Part: COMPUTER — FAULTY (NR 1)

FLL - FLT 171 - AUTO THROTTLES WOULD NOT REMAIN ENGAGED WITH DFGC NR 1 SELECTED. WORKED NORMAL ON DFGC NR 2. REMOVED AND REPLACED NR 1 DFGC RTS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

FLL - CENTER AISLE OVERHEAD EMERGENCY LIGHTS OUT FIRST 5 SEAT ROWS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FOR ROWS 1 THROUGH 5. OPS CHECK GOOD IAW MD80 MM 33-53-00. (M)

Part: CONTROL CABLE — OUT OF RIG (ELEVATOR TAB)

FLL - FLT 779 - ELEVATOR POWER ON LIGHT ILLUMINATES IN FLIGHT WITH 1 UNITS NOSE UP TRIM. FOUND RIGHT CONTROL TAB SECTOR SLIGHTLY OUT OF RIG ADJUSTED CABLE SECTORS 5C AND 6C RIG CHECK OK IAW MM 27-30-00, 27-30-07. (M)

Part: SWITCH — LOOSE (T/E FLAP)

DTW - FLT 1521 - ON POWER ADVANCE AT TAKEOFF WITH AIRCRAFT CONFIGURED 'FLAP' AURAL WARNING CAME ON. RETRACTED AND LOWERED FLAPS AND SLATS STILL HAD WARNING. FOUND FLAP TAKEOFF SWITCH LOOSE ON MOUNT AND MISSING SCREWS. REPLACED SCREWS AND REPOSITIONED SCREWS IAW MM 27-53-01. UNIT OPS CHECKS GOOD. NO DEFECTS NOTED. (M)

Part: JACKSCREW — LOOSE (HORIZONTAL STAB)

DTW - FOUND HORIZONTAL JACK SCREW FREE PLAY FAILED DIMENSION. REQUIRES REPLACEMENT. REMOVED AND REPLACED HORIZONTAL JACK SCREW IAW MD 80 MM 27-40-01. OPS CHECK GOOD FREE PLAY .003 END PLAY .009. (M)

Part: CABLE — DISCONNECTED (EVAC SLIDE)

R1 DOOR GIRT BAR CABLE DISCONNECTED. CONNECTED R1 GIRT BAR IAW MD80 MM 25-62-04. OPS CHECK GOOD, NO OTHER DEFECTS NOTED AT THIS TIME. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - FLT 223 - AIRCRAFT FLOOR TRACK LIGHTING ILLUMINATED AND DRAINED WHEN APU GENERATOR DROPPED OFF LINE. RECHARGED EMERGENCY LIGHTING SYSTEM AS REQUIRED. ALL WORK IAW MX-80 MM. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

DTW - THREE EMERGENCY CEILING LIGHT REMAIN ILLUMINATED WITH EMERGENCY POWER OFF. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY WITH SERVICEABLE BATTERY POWER SUPPLY OPS CHECK GOOD IAW MD 80 MM 33-53-01. (M)