N820NK

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

DTW - FOUND L1 DOOR EVAC SLIDE DEPLOYMENT LANYARD DISCONNECTED FROM SLIDE ASSY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE. (M)

Part: ENGINE — MALFUNCTIONED (NR 1)

LT 283881; INFLIGHT SHUTDOWN - DIVERSION, SHUTDOWN LT ENGINE DUE TO LOW OIL PRESSURE, LOW OIL QTY. REMOVED AND REPLACED NR 1 ENGINE.

Part: SPRING — BROKEN (SERVICE DOOR)

R1 SVC, DOOR BAYONET ROLLER HELICAL TORSION SPRING BROKEN. REMOVED AND REPLACED R1 DOOR BAYONET ROLLER HELICAL TORSION SPRING. OPS CHECK GOOD IAW 52-41-00.

Part: BEARING — FAILED (TORQUE TUBE)

FLT 380 - LT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. GEAR RECYLE SATISFACTORY. REPLACED BEARING ON LEFT TORQUE TUBE VERIFIED PROPER RIGGING. PERFORMED MULTIPLE GEAR SWINGS CHECKS GOOD. (M)

Part: CONTROL VALVE — MALFUNCTIONED (MLG)

AFTER TAKEOFF, AIRCRAFT SPEED APPROX 150 KNOTS THERE WAS NO DRAG 100 FEET AGL 12 DEGREE PITCH UPLEFT MAIN GEAR, GEAR WAS UP RED LIGHT STAYED ON AFTER GEAR RETRACTION GEAR DOOR OPEN LIGHT WAS NOT ON AND NOSE AND RIGHT MAIN GEAR LIGHTS NOT ON AT SPEED 200 KNOTS CLIMBING THROUGHOUT 3000 MSL CYCLED GEAR. GEAR UP NORMAL DURING APPROACH TO LANDING WITH GEAR DOWN THREE GREEN THE GEAR DOOR OPEN LIGHT STAYED ON LONGER THAN NORMAL APPROX 180 KNOTS SPEED. PERFORMED RIG CHECK OF LANDING GEAR CONTROL VALVE, JACK AND CYCLED GEAR. (M)

Part: CONDUIT — OUT OF POSITION (MLG WIRE)

DTW - FLT 563 - AFTER TAKEOFF LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON/RED FOR ONE MINUTE AFTER ALL OTHER LANDING GEAR LIGHTS OUT. AS SLOWED TO 230 KIAS FOR QRH PROCEDURE LIGHT WENT OUT AND REMAINED OUT FOR REMAINDER OF FLIGHT. FOUND WIRE CONDUIT FROM GEAR UPLATCH SENSOR ARM IN THE PATH SLIGHTLY OF THE GEAR SWING MOTION. REPOSITIONED CONDUIT AND GEAR SWING PATH IS GOOD. (M)

Part: ROLLER — OUT OF ADJUST (MLG DOOR)

DURING CRUISE FLIGHT, GEAR DOOR OPEN LIGHT CAME ON, PUT HYDRAULIC PUMPS ON HIGH AND LIGHT WENT OUT AFTER APPROXIMATELY 3 MINUTES. FOUND DOOR ROLLER TO HOOK CLEARANCE OUT OF ADJUSTMENT. ADJUSTED CLEARANCE. (M)

Part: PROXIMITY SENSOR — MALFUNCTIONED (LT MLG)

LGA - FLT 779 - FOUND LEFT MAIN GEAR UNSAFE LIGHT CAME ON AND STAYED ON IN FLIGHT. FOLLOW QRH PROCEDURES CONT TO FLL AT .700 MACH. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. (M)

Part: PROXIMITY SENSOR — MALFUNCTIONED (LT MLG)

ORD - FLT 1525 - LEFT MAIN LANDING GEAR INDICATOR STAYED RED AFTER GEAR RETRACTION FOLLOWED QRH AND HAD NORMAL INDICATIONS AFTER. REMOVED AND REPLACED LEFT MLG UPLOCK PROX SENSOR. PERFORMED OPS CHECK OF SENSOR THROUGH PROX SWITCH ELECT. (M)

Part: LINE — LEAKING (MLG HYD SYS)

LGA - FLT 779 - JUST AFTER TAKEOFF LGA, STRANGE ODOR CAME THROUGH VENTS. BRAKE TEMP INDICATOR LIGHT WAS FLASHING AND TEMP NEEDLE MOVING, LEFT LANDING GEAR DOWN TO MAKE SURE NO BRAKE HEAT, LIGHT WENT OUT, ODOR WENT AWAY. FOUND NR 2 BRAKE AFT HYD LINE LOOSE AND LEAKING, RE-INSTALLED, TIGHTEN AND SAFETY WIRED NR 2 BRAKE AFT HYDRAULIC LINE LEAK AND OPS CHECK OK BRAKE SYSTEM OPERATED LEFT AND RIGHT A/C PACKS, NO ODOR NOTICED IN A/C SYSTEM. (M)

Part: WARNING LIGHT — MALFUNCTIONED (MLG)

FOUND LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. (M)

Part: LATCH — STUCK (TAIL CONE)

LGA - FLT 1174 - FLIGHT ATTENDANT SAYS THAT AFT CABIN DOOR IS VERY HARD TO CLOSE. AFT FLIGHT ATTENDANT REPORTED SAFETY DOOR FOR TAIL CONE HANDLE ABOVE FLIGHT ATTENDANT SEAT WOULD NOT LATCH. FREED LATCH, OPS CHECK NORMAL. NO FAULT REPORTED OR FOUND WITH AFT CABIN DOOR. (M)

Part: UPLOCK SENSOR — OUT OF ADJUST (MLG)

ORD - FLT 1525 - FOUND LEFT MAIN GEAR INDICATES UNSAFE, RED LIGHT, WITH GEAR HANDLE UP DURING CLIMB AND CRUISE ONLY. T/S LEFT INDICATING SYSTEM CHECKED AIR GAPS ON MAIN GEAR LEFT UPLOCK, DOOR OPEN, AND DOWNLOCK PROX SENSORS. FOUND LEFT UPLOCK SENSOR OUT OF ADJUST TO WIDE ADJ PROX SENSOR. PERF PROX BITE CHECK OF EFFECTIVE SENSOR, NO FAULTS NEAR FAR PASS. (M)

Part: SENSOR — INOPERATIVE (RT MLG)

RT MAIN GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RAISED. GEAR WAS CYCLED AND LIGHT EXTINGUISHED. ADJUSTED RT MLG UP LATCH PROXIMITY SENSOR TO TARGET CLEARANCE. JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS. ALL INDICATIONS NORMAL.

Part: PROXIMITY SWITCH — OUT OF LIMITS (NLG)

ON CLIMBOUT CENTER GER RED LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE (CYCLED GEAR DOWN AND UP) LIGHTS WENT OUT. JACKED AC NOSE GEAR AND PERFORMED NOSE GEAR RETRACTION TEST FOR UP/DOWN POSITION LIGHTS. NO FAULTS WERE NOTED ON SEVERAL CYCLES. FOUND RT MLG DOOR PROXIMITY SWITCH OUT OF LIMITS ON GAP CHECK. ADJUSTED GEAR DOOR TARGET. MAIN GEAR DOOR INDICATION CHECK OK W/ DOORS UP.

Part: CONTROL VALVE — LOOSE (LT MLG)

IN CLIMB AT GEAR RETRACT LT MAIN GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE UP. CK QRH AND FOLLOWED PROCEDURE WITH NO CHANGE. LEAVING 10,000 FT AND PUTTING HYD. PUMPS TO LOW AND OFF THE GEAR DOOR OPEN LIGHT ALSO CAME ON. SELECTED ENGINE PUMPS TO HIGH AND GEAR DOOR OPEN LIGHT WENT OUT. WE COULD NOT NOTICE ANY ABNORMAL VIBRATIONS LIMITED SPEED TO .70M/ 300K. L/P 1338401 ON GEAR RETRACTION LT GEAR RED LIGHT STAYED ON. FOUND LT FILLET ATTACHMENT LINK LOOSE, ADJUSTED AND TIGHTENED FILLET ATTACHMENT LINK. JACKED AIRCRAFT UP PERFORMED GEAR SWING. OPS CK GOOD, NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE. OPS AND LEAK CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG)

LT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. DURING ARRIVAL INTO FLL. QRH C/W GEAR DOOR OPEN EXTINGUISH WITH HYDRAULIC SYSTEM HI. 3000 GEAR DOOR LIGHT ILLUMINATED AGAIN WITH HYDRAULIC SYSTEM IN 1500 PSI LOW POSITION. CLEANED AND ADJUSTED LT GEAR DOOR PROXIMITY SWITCH AND REMOVED AND REPLACED LT MLG UP AND LATCH PROXIMITY SWITCH. CHECK NORMAL ON GROUND.

Part: STRAP — FRAYED (SLIDE PACK)

AFT TAIL SLIDE PACK COVER HOLD DOWN STRAP FRAYED AND PRESS GAUGE NOT IN WINDOW. REMOVED AND REPLACED FRAID COVER HOLD DOWN STRAP ON AFT TAILCONE SLIDEPACK. ADJUSTED PACK COVER SO GAUGE WAS VISIBLE.

Part: LINER — LOOSE (NR 2 ENG INTAKE)

ACY - NR 2 ENGINE INTAKE LINER LOOSE FOUND ON WALKAROUND. REMOVED DAMAGED ACOUSTIC PANEL LINER. INLET COWL INSPECTION AND REPAIR OF THE DYNA ROHR ACOUSTIC PANELS ACOUSTIC LINING MISSING BETWEEN 4 O'CLOCK AND 8 O'CLOCK POSITION NOSE COWL TO BE REPLACED ON C/O 146482-2. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

RSW - FLT 1605 - AFTER GEAR HANDLE SELECTED UP LT MAIN GEAR UNSAFE LIGHT (RED) REMAINED ON. CONSULTED QRH, GEAR UNSAFE LIGHT REMAINED ON ALL OTHER AIRCRAFT INDICATION NORMAL. INSPECTED LEFT MLG POSITION INDICATION SYSTEM. NO DEFECTS NOTED AT THIS TIME. (M)

Part: ODOR — DETECTED (CABIN)

LEFT AND RIGHT AIR COND SUPPLY TEMP HIGH LIGHTS CAME ON WITH BURNING ODOR IN CABIN WHEN AIRFOIL ANTI-ICE TURNED ON. ACCOMPLISHED QRH PROCEDURES LIGHTS WENT OUT, CONTINUED FLIGHT. PER COMPANY REQUEST AND ITEM ABOVE PERF EXTRA ENGINE RUN UP AT CRUISE PLUS POWER. PERFORMED TEST DISTRIBUTION SYSTEM, ICE PROTECTION SYSTEM OPERATION WITH BOTH ENGINE RUNNING. OPERATIONAL CHECK GOOD. ACCOMPLISHED TEST DISTRIBUTION SYSTEM, ICE PROTECTION SYSTEM. NO BURNING ODOR NOTED PLUS AIR CONDITION SUPPLY TEMP HIGH LIGHT NEVER CAME ON. FOUND AIRFOIL ANTI-ICE SYSTEM NORMAL. (M)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

FTW - FOUND EMERGENCY LIGHTS INOPERATIVE O/H STATION 800-1200 AND LEFT SIDEWALL LIGHTS INOPERATIVE IN VENTRAL STAIRWELL AREA. TROUBLE SHOT, FOUND LOOSE WIRE. RE-INSTALL LOOSE TERMINAL. (M)

Part: FITTING — CRACKED (CARGO DOOR FRAME)

AFT PIT DOOR UPPER STOP, FORWARD FITTING CRACKED. REMOVED DAMAGED FITTING. REPLACED FITTING. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CABIN FLOORBEAM, IN MID PIT, CHAFING AND CORRODED. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M)

Part: WEB — CORRODED (CABIN SUBFLOOR)

FOUND PAX CABIN SUBFLOOR CORRODED AT RBL 40 TO 54 STATION 180 TO 200. REMOVED DAMAGED WEB. FABRICATED NEW WEB. FABRICATED NEW SPLICE. INSTALLED NEW WEB AND SPLICE. (M)

Part: FLOOR PANEL — CORRODED (CABIN)

FTW - FOUND CABIN FLOOR WEB CORRODED UNDER GALLEY DRAIN PAN STATION 158 RBL - 44 INCHES. (M)

Part: LONGERON — DAMAGED (FUSELAGE)

FTW - FOUND DAMAGED LONGERON STATION FS 1271 L24L. REMOVED DAMAGED LONGERON AT L24L FS 1322-1271. FABRICATED NEW LONGERON. LOCATED AND DRILLED SPLICE. INSTALLED SPLICE AND LONGERON. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 1276 TO FS 1315 BETWEEN LONGERONS 23 AND 24L, REQUIRES REPAIR. DENT AT FS 1276 SHOULD BE INCORPORATED INTO THIS REPAIR. CUT OUT DAMAGED SECTION OF SKIN FROM STATION 1276-1315. FABRICATED INNER DOUBLERS, FINGER DOUBLER AND NEW SKIN. INSTALLED DOUBLER AND SKIN. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FTW - FOUND PAX CABIN FLOORBOARD DELAMINATED AT FORWARD F/A SEAT AREA. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLOOR SUPPORT AT FS 146 TO 154 LBL 53 HAS CORROSION. FLOOR SUPPORT REMOVED. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: PLATE — CORRODED (FUSELAGE)

FTW - FOUND TWO CORRODED FLOOR PLATES AT FS 160, 18 INCHES LBL. FABRICATED FLOOR PLATE. TWO FLOOR PLATES ARE REMOVED AND INSTALLED ON SAS W/C B00104 18-R-15. (M)

Part: FITTING — CORRODED (FUSELAGE)

FOUND MID PIT STATION 693 TEE FITTING CORRODED/ELONGATED HOLES. FABRICATED NEW T-FITTING. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND SUBFLOOR CORRODED STATION 195 LBL 50. REMVOED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M)

Part: YOKE — DAMAGED (ENGINE MOUNT)

FTW - NR 2 YOKE ASSEMBLY UPPER ISOLATOR CONICAL SURFACE WORN. REMOVED NR 2 UPPER FORWARD ISOLATOR. INSTALLED NEW ISOLATOR. UPON INSTALLATION OF YOKE ASSEMBLY FOUND UPPER ISOLATOR INNER ASSEMBLY LOOSE. FOUND ISOLATOR INNER ASSEMBLY STILL LOOSE. REMOVED UPPER YOKE PLATE AND ISLOATOR. REMOVED NR 2 ENGINE PYLON YOKE. INSTALLED SERVICEABLE YOKE PLATE AND ISOLATOR. INSTALLED NR 2 YOKE ASSEMBLY. (M)

Part: FLOORBOARD — CORRODED (FS)

FTW - FOUND FORWARD CABIN STATION 200 TO STATION 180 RBL 8 INCHES TO RBL 44 FLOOR PANEL HAS SEVERAL INSERTS BROKEN OUT/CORRODED/SOFT/MUSHEY. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN FLOOR PANEL STATION 160-200 CENTER HAS SEVERAL INSERTS BROKEN OUT/CORRODED AND SOFT/MUSHEY. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND FORWARD CABIN FLOORBOARD STATION 180 TO STATION 160 RBL 8 INCHES TO RBL 44 HAS SEVERAL INSERTS BROKEN OUT, CORRODED AND SOFT/MUSHEY. FABRICATED NEW FLOOR BOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN FLOORBOARD STATION 200 TO STATION 256 LBL 14.5 TO LBL 21 HAS SEVERAL INSERTS BROKEN OUT, CORRODED, SOFT/MUSHEY. FABRICATED NEW FLOOR BOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FORWARD CABIN STATION 200 TO 256 CENTER FLOORBOARD HAS SEVERAL INSERTS BROKEN OUT/CORRODED SOFT/MUSHEY AND DAMAGED ALL CORNERS. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FORWARD CABIN STATION 200 TO 256 RBL 45.5 TO RBL 55 METALLIC PANEL HAS CRACKED/DAMAGED AT HAT CHANNEL AND EXPANSION JOINT CRACK/DISBONDED. FABRICATED REPAIRS. INSTALLED HAT CHANNEL REPAIRS. REPAIRED DISONDED AREA. (M)

Part: FLOORBOARD — BROKEN (FUSELAGE)

FOUND FORWARD CABIN STATION 200 TO 256 LBL 21 TO LBL 44 FLOORBOARD HAS SEVERAL INSERTS BROKEN OUT/CORRODED SOFT/MUSHEY AND DAMAGE ALONG EDGE. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR BOARD STATION 200 TO STATION 160 RBL 44 TO RBL 55 HAS SEVERAL INSERTS CORRODED/SOFT MUCHEY. FABRICATED NEW FORWARD CABIN FLOOR BOARD. (M)

Part: BEAM — CRACKED (FUSELAGE)

FOUND L1 DOOR FORWARD VERTICAL BEAM AND STRAP CRACKED/BENT. REMOVED T-ANGLE. REMOVED CRACKED STRAP. REMOVED FORWARD VERTICAL BEAM. FABRICATED REPLACEMENT VERTICAL BEAM AND STRAP. INSTALLED NEW VERTICAL BEAM, NEW STRAP AND T-ANGLE. (M)

Part: CAP — CRACKED (RT WING SLAT)

FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP IS CRACKED. REMOVED END CAP. LOCATED AND DRILLED NEW PART. INSTALLED NEW END CAP. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORROSION AT FS 160-200 62 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT 2 INCH LONG CORROSION AT FS 200 51 INCHES LBL. REMVOED FLOOR SUPPORT. FABRICATED NEW CABIN FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLOOR SUPPORT CORRODED AT FS 148-200, 0 INCHES BL, FLIGHT COMPARTMENT. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED HOLES AT NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FS)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200-255 22 INCHES LBL. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200-208 60 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORROSION AT FS 160-200 51 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200-205, 21 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW CABIN FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FS)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 16 INCHES-20 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 148-200 14 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 218 0 INCHES - 22 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180, 0-36 INCHES RBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLT COMPARTMENT FLOOR SUPPORT CORRODED AT FS 160 0 INCHES TO 11 INCHES LBL. REMVOED FLOOR SUPPORT. FABRICATED NEW PART. INSTALLED NEW FLOOR SUPPORT. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND CABIN SUB FLOOR CORRODED AT FS 200 16 INCHES LBL. CUT OUT CORRODED AREA. FABRICATED 1 FILLER AND 1 DOUBLER. INSTALLED FILLER AND DOUBLER. FLOOR SUPPORT CORRODED. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 0-36 INCHES RBL. REMOVED CABIN FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 22 INCH - 50 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FITTING — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200 48 INCHES RBL. FLOOR SUPPORT ATTACHMENTS 2 AT FS 165 AND 200 48 INCHES RBL OUT OF LIMITS. REMOVED FLOOR SUPPORT ATTACHMENTS TWO, LOCATED AND DRILLED NEW FITTINGS. INSTALLED FLOOR SUPPORT AT ATTACHMENTS TWO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200, 36 INCHES RBL. REMOVED CABIN FLOOR SUPPORT. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND FLOORBOARD SUPPORT BROKEN AND CRACKED AT STATON 864 OVER CENTER WING TANK. REMOVED FLOORBOARD SUPPORT. FABRICATED NEW FLOORBOARD SUPPORT. INSTALLED NEW SUPPORT. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND RIGHT AFT LAV STATION 1322 RBL 19-54, FLOORBEAM CORRODED. TRIMMED OUT DAMAGED AREA. DRILLED AND LOCATED ANGLE/FILLER. INSTALLED REPAIR ANGLE AND FILLER. (M)

Part: ANGLE — CRACKED (CENTER WINGBOX)

FOUND WEB ANGLE ATTACHMENT STATION 864 OVER CENTER WING TANK CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

FTW - FOUND RIGHT SIDE MLG FORWARD DOOR JAMB FRAME ATTACHED KEEL BEAM CRACKED AT DOUBLER. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED NEW REPAIR DOUBLERS. INSTALLED REPAIR DOUBLER. (M)

Part: WEB — CRACKED (FUSELAGE)

FOUND CABIN STATION 1309 RBL 46 FLOOR WEB CRACKED UNDERNEATH SEAT TRACK. TRIMMED OUT DAMAGED/CRACKED AREA. DRILLED AND LOCATED FILLER AND DOUBLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FTW - FOUND LEFT AFT LAV STATION 1338 LBL 19 LBL 54 FLOORBEAM CORRODED. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR ANGLE AND FILLER. INSTALLED REPAIR PARTS. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND AFT FUSELAGE EXTERNAL AIR CONDITION DOOR OPENING TWO CRACKS. REMOVED CRACKED DOUBLER. FABRICATED DOUBLER. INSTALLED FABRICATED DOUBLER. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FOUND FLOORBOARD STATION 598-636 DENTED/CRACKED. FABRICATED NEW FLOORBOARD. (M)

Part: DOOR FRAME — CORRODED (L1 DOOR)

FTW - FOUND L1 DOOR LOWER JAMB CORRODED AT MATING SURFACE WHERE THRESHOLD ATTACHS. REMOVED LOWER DOOR JAMB. FABRICATED NEW PART. INSTALLED L1 LOWER DOOR JAMB. (M)

Part: STRUCTURE — CRACKED (L1 DOOR)

FTW - FOUND L1 DOOR CRACKED 2 PLACES IN RADIUS AT AFT SIDE 2ND ACCESS FROM TOP AND FORWARD SIDE 2ND ACCESS HOLE FROM TOP. STOP DRILLED CRACKS. (M)

Part: PANEL — DELAMINATED (RT WING)

FOUND RIGHT WING BOTTOM TRAILING EDGE TRAP PANEL JUST FORWARD OF RT MLG DELAMINATED. REMOVED RIGHT WING BOTTOM TRAP PANEL. REPAIRED RT WING BOTTOM TE TRAP PANEL INSTALLED RIGHT BOTTOM TE TRAP PANEL. (M)

Part: PANEL — DELAMINATED (LT WING)

FOUND LEFT WING LOWER TRAP PANEL MLG DELAMINATED. REMOVED LEFT WING LOWER TRAP PANEL. REPAIRED LEFT TRAP PANEL. INSTALLED PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND E/E BAY FS 216 CEILING WEB CORRODED AND CRACKED. CUT OUT CORRODED AND CRACKED AREA. FABRICATED NEW WEB SECTION AND DOUBLER. INSTALLED REPAIR PARTS. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FTW - FOUND MID PIT STATION 636, STATION 30-29L FRAME SUPPORT CORRODED AND STRINGER 29R-30 FRAME SUPPORT CORRODED. REMOVED SHEAR TIE. DRILL AND LOCATE NEW SHEAR TIE. INSTALLED NEW SHEAR TIE. (M)

Part: PAN — CORRODED (FUSELAGE)

FOUND FORWARD PIT DOOR PAN CORRODED FS 372-376 STRINGER 28R. FABRICATED TWO EACH 23 AND TWO EACH 25 REPAIR ANGLES. LOCATED AND DRILLED REPLACEMENT SEC OF FORWARD DOOR PAN AND TWO EACH 23 AND 25 SPLICE REPAIR ANGLES. INSTALLED REPAIR ANGLES 23 AND 25 FORWARD PIT PAN AND WEB. (M)

Part: SPOILER PANEL — DELAMINATED (LT WING)

FTW - FOUND LEFT WING INBOARD FLIGHT SPOILER DELAMINATED AT REPAIR. REMOVED DAMAGED AREA. CUT CORE AND REPLACED LOWER SKIN IN DAMAGED AREA. (M)

Part: BEAM — CORRODED (CARGO DOOR FRAME)

FOUND MID CARGO DOOR JAMB BEAM CORRODED AT FS 636-693. REMOVED JAMB BEAM. LOCATE AND DRILLED NEW JAMB BEAM. INSTALLED NEW JAMB BEAM. (M)

Part: SLIDE — LOOSE (R1 DOOR)

SLIDE PACK ON R1 DOOR IS LOOSE. RESET SLIDE PACK AS REQUIRED ON R1 DOOR. (M)

Part: CONNECTOR — LOOSE (PSEU)

WITH GEAR UP, LANIDNG GEAR DOOR OPEN LIGHT WAS ON, THERE WERE NO GER UNSAFE LIGHTS ON LIGHT STAYED ON AN HR AND THEN EXTINGUISHED. IN CLIMB, THE LANDING GEAR DOOR OPEN LIGHT CAME ON WITHOUT A GEAR UNSAFE LIGHT. AFTER LEVELING OFF AT ALT, THE LIGHT EXTINGUISHED. GEAR DOOR OPEN LIGHT COMES ON ITNERMITTENTLY IN FLIGHT. GEAR DOOR OPEN LIGHT ILLUMINATES INTERMITTENTLY. FOUND LOOSE CONNECTOR FOR GEAR DOOR UP, SECURED CONNECTOR AND CYCLED GEAR DOOR SEVERAL TIMES, NO DEFECTS NOTED. T/S MLG DOOR INDICATOR DETERMINED THE TARGET TO SENSOR GAP OUT OF LIMITS ON BOTH GEAR DOORS, ADJUSTED GAP ON BOTH DOORS, OPS CHECK GOOD. REMOVED AND REPLACED PSEU OPS CHECK PASS. T/S PSEU, FAILED LEFT MAIN GEAR DOOR SENSOR R/R LEFT MA

Part: TARGET — DIRTY (PROXIMITY SWITCH)

GEAR DOOR OPEN LIGHT (AMBER) CAME ON IN CRUISE FOR ABOUT 5 MIN AND THEN WENT OUT FOR DURATION OF FLIGHT. NO GEAR RED LIGHTS WERE ON AT ANY TIME. PERFORMED BITE CHECK ON ELECTRONICS PRO BOX, NO FAULTS FOUND. INSPECTED PROX SWITCH AND TARGET FOR GEAR DOORS, FOUND LEFT MAIN TARGET DIRTY, CLEANED SAME. OPS CHECKED GOOD.

Part: COWLING — DAMAGED (NR 2 ENGINE)

LGA - NR 2 ENGINE ACCOUSTIC LINER MATERIAL MISSING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED RN 2 ENGINE NOSE COWL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD EMERGENCY LIGHT INOPERTIVE. REMOVED AND REPLACED LIGHT ASSEMBLY, CHECKS GOOD.

Part: SMOKE — DETECTED (CABIN)

RSW - FLT 1504 - AFTER TAKEOFF FLIGHT ATTENDANT IN AFT CABIN REPORT ODOR OF SMOKE. INSPECTED BOTH AFT LAV'S, ABOVE AND AREA AROUND AFT F/A SEAT, OPENED OVERHEAD PANELS AND REINSTALLED, INSPECTED AC SYSTEM AND DUCTING IN TAILCONE AREA WITH ENGINES AND APU AS SUPPLY OF AIR SOURCE, NO DEFECTS NOTED A/C OK FOR SERVICE. (M)

Part: SLAT — CRACKED (LT WING)

RSW - FLT 4978 - LEFT WING NR 3 SLAT HAS CRACK ON INBOARD SIDE APPROX 6 INCHES LONG. REMOVED AND REPLACED LEFT WING NR 3 SLAT. (M)

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

AFT SERVICE DOOR SLIDE CAME OFF OF DOOR. NEED TO BE REINSTALLED. AFT SERVICE DOOR SLIDE REINSTALLED. (M)

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY)

DTW - FLT 313 - FOUND FORWARD GALLEY-LOW POT SMELLED SMOKE, SMELLED LIKE PLASTIC BURNING. PULLED C/B'S AND TURNED OFF GALLEY POWER SMELL STOPPED. REMOVED AND REPLACED FORWARD GALLEY LOWER COFFEE MAKER. OPS CHECK OK. (M)

Part: CONTROL HANDLE — LACK OF LUBE (TE FLAPS)

LGA - FLT 197 - FLAP TAKEOFF SELECTOR DOES NOT LOCK FLAPS IN THE 'OPTIUM FLAP' POSITION, ALTHOUGH THE DETENT CAN BE SEEN THE FLAP HANDLE DOES NOT 'LOCK' INTHE DETENT AND CAN BE BUMPED AND CHANGE POSITION FOR TAKEOFF. INSPECTED, LUBED AND OPERATED DIAL A FLAP MECH SEVERAL TIMES, FOUND TO WORK NORMAL IAW MM 27-50-00. (M)

Part: CASE — SPLIT (HYD PUMP)

FLT 1863 - LGA - RIGHT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS ILLUMINATED IN FLIGHT. RIGHT HYD PRESS '0' RIGHT HYD QUANTITY 2 QUARTS LANDING MANUAL EXTENSION USD. PROBLEM OCCURRED AT FL240 WITH ENGINE PUMPS ON LOW XFER AUX PUMP OFF. FOUND RIGHT AUX HYD PUMP CASE SPLIT APART. REMOVED AND REPLACED SAME PER MM 29-10-06. REMOVED AND REPLACED RIGHT SYSTEM RETURN FILTERS PER MM 29-10-14. SERVICED RIGHT HYD SYSTEM PER MM 12-13-02. OPS AND LEAK CHECK GOOD. (M)

Part: SWITCH — INTERMITTENT (ELEVATOR TRIM)

LGA - FLT 1765 - ALT TRIM SWITCHES STOP OPERATING INTERMITTENT. REMOVED AND REPLACED ALT LONG TRIM MOTOR CONTROL SWITCH IAW MM 27-40-09, OPS NORMAL. (M)

Part: ARM — LACK OF LUBE (ELEVATOR TRIM)

LGA - FLT 1765 - ALT TRIM INOPERATIVE UP, OPERATED NORMALLY DOWN POSITION. LUBED ATTACHING ARM TO S10-7 ALT SWITCH. SYSTEM OPS CHECKS OK PER MM 27-40-01. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — BROKEN (COCKPIT)

DEN - FLT 980A - SETTING MAX POWER FOR DEPARTURE GOT THE FLAP AURAL WARNING WITH FLAPS SELECTOR 4.5 OPTIUM. TROUBLE SHOT SYSTEM FOUND FLAP TAKEOFF SETTING WARNING S/W AT CONNECTOR AT D-1 1194 PINE BROKEN WIRE REPAIRED IAW MM CH 20 TAKEOFF WARNING SYSTEM. OPS CHECKED GOOD IAW MD MM 27-52-00 OK TO CONTINUE. (M)

Part: LANDING GEAR — VIBRATION (NLG)

FLL - FLT 380 - ON INITIAL TAKEOFF ROLL, A HARD SHIMMY SEEMING TO COME FROM THE NOSE WHEEL OCCURRED. ABORTED TAKEOFF AT 70 KNOTS. INSPECTED ALL TIRES AND BRAKES NO DEFECTS MWA'S. INSPECTED AND LUBRICATED NOSE LANDING GEAR. NO DEFECTS NOTED. (M)

Part: CONNECTOR — DIRTY (RT EPR)

DTW - FLT 313 - WHILE APPLYING TAKEOFF POWER RIGHT EPR GAUGE STUCK AT 148 AUTO THROTTLE DISENGAGED DURING TAKEOFF. FOUND RIGHT ENGINE EPR CANNON PLUG DIRTY CLEANED CANNON PLUG REINSTALLED, OPS CHECK NORMALLY. AUTO THROTTLES OPS NORMAL. (M)

Part: WHEEL — LACK OF LUBE (NLG)

FLT 604 - FLL - ON TAKEOFF ROLL AT 60 IAS NOSE WHEEL DEVELOPED SEVERE VIBRATION, REJECTED TAKEOFF AT 70 KIAS RETURNED TO GATE. LUBRICATED NOSE GEAR ASSEMBLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FTW - FOUND EMERGENCY LIGHTS INOPERATIVE AT COCKPIT CAPTAINS SIDE, FORWARD ENTRANCE (TWO EACH), LEFT AND RIGHT, STATION 7213 BETWEEN GALLEY AND LAVATORY, FORWARD. REMOVED BATTERY PACKS AT FS 211 CTR BS-23. INSTALLED SERVICEABLE BATTERY PACKS IN B5-23. (M)

Part: TERMINAL — LOOSE (CABIN)

FTW - FOUND EMERGENCY LIGHTS INOPERATIVE AT FORWARD OVERWING EXIT LIGHTS (LT/RT) L2 EXIT (FWD LOWER CORNER) SEAT 34 STANDBY LIGHT, BETWEEN SEATS 32 AND 33 STANDBY LIGHTS. RANG OUT STANDBY LIGHTING IN AFT CABIN SEAT 34 AND SEAT 32 AND 33. FOUND WIRES INSTALLED WRONG. SWAPPED WIRES. FOUND UNSECURED BATTERY TERMINAL. SECURED BATTERY TERMINAL. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

FTW - E/E BAY COMPARTMENT AT STA Y 16 INCHES BY 33 INCHES -2=11 SUPPORT CHANNEL CRACKED. REMOVED CHANNEL. FABRICATED NEW DOUBLER. INSTALLED CHANNEL. (M)

Part: TRIM TAB — DELAMINATED (ELEVATOR)

FTW - LEFT ELEVATOR ANTI-FLOAT TAB HAS THREE DENTS AND AREAS OF DELAMINATION. REMOVED ANTI-FLOAT TAB. INSTALLED LEFT ELEVATOR ANTI-FLOAT TAB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND AFT CARGO FLOOR SUPPORT STATION 1136 HAS CORROSION. REMOVED CORROSION. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - AFT CARGO COMPARTMENT STATION 1155/1212 L28R WEB HAS CORROSION, FOUND DURING BEAM REMOVAL. REMOVED CORROSION. FABRICATED NEW WEB. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

FTW - FOUND AFT CARGO TRACK RIGHT FORWARD 'Z' ANGLE GOUGED AND TRACK HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED TRACK. INSTALLED CARGO TRACK. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND AFT CARGO CORNER THRESHOLD SUPPORT STATION 1155 HAS CORROSION AROUND AND UNDER NUT PLATES. REMOVED CORROSION. FABRICATED THRESHOLD SUPPORT. INSTALLED NEW THRESHOLD SUPPORT. (M)

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER)

FTW - FOUND ENGINE NR 1 T/R INTERLOCK MECH SUPPORT BRACKET CRACKED. REMOVED BRACKET NR 1 ENGINE T/R INTERLOCK MECH. INSTALLED BRACKET ON NR 1 ENGINE T/R INTERLOCK MECH. (M)

Part: SKIN — DENTED (FLAP VANE)

FTW - FOUND RIGHT WING, NR 2 FLAP VANE HAS SEVERAL DENTS ON UPPER AND LOWER SURFACE. REPAIRED DAMAGE PER SPIRIT AIRLINES EA 5750-0205. (M)

Part: SKIN — DENTED (FLAP VANE)

FTW - FOUND LEFT WING INBOARD FLAP VANE NR 1 TWO EACH LARGE DENTS ON UPPER SURFACE OF VANE. REPAIRED DAMAGE, PER SPIRIT AIRLINES EA 5750-0205. (M)

Part: SKIN — DENTED (FLAP VANE)

FTW - FOUND RIGHT WING NR 5 FLAP VANE DENTED 2 PLACES ON UPPER SURFACE. REPAIRED BOTH DENTS ON UPPER SURFACE OF VANE PER SPIRIT AIRLINES EA 5750-0205. (M)

Part: FLOOR PANEL — BROKEN (FUSELAGE)

FTW - FOUND RIGHT COCKPIT FLOOR PANEL CRACKED AND BROKEN FORWARD CLOSEOUT. REPAIRED COCKPIT FLOOR PANEL USING 181 CLOTH. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1155-1212 L28R, REPAIR STRAP ON DOOR JAMB BEAM HAS AREAS OF CORROSION ENTIRE LENGTH OF REPAIR. AFT PIT STATION 1155-1212 L28R EVIDENCE OF CORROSION BETWEEN SKIN/DOUBLER AND LOWER FLANGE OF DOOR JAMB BEAM. AFT CARGO FLOOR SUPPORT STATION 1155 HAS CORROSION AND DOUBLE DRILLED HOLES. REMOVED REPAIR STRAP. AFTER REMOVING STRAP AND REPAIR DOUBLER FOUND CORROSION ON DOOR BEAM TO BE OUT OF LIMITS. REMOVED DOOR JAMB CORNER ANGLE STATION 1155. CORNER ANGLE HAS CORROSION OUT OF LIMITS STATION 1155. REMOVED AFT CARGO DOOR FLOORBEAM FROM STATION 1117-1250 L28R. LOCATED AND DRILLED NEW FLOORBEAM. INSTALLED NEW BEAM. (M)

Part: STIFFENER — CRACKED (FLOORBOARD)

FTW - FOUND CABIN FLOORBOARD STATION 1155-1250 X46 TO X56 STIFFENER CHANNEL CRACKING, REPAIR DEBONDING, PHENOLIC BACKSTRIPS BROKEN AND FASTENER HOLE ENLARGED. REPAIRED CABIN FLOOR PANEL STATION 1155-1250. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - E/E BAY LONGERON 28L HAS CORROSION FROM STATION 190-210. REMOVED DAMAGED LONGERON. FABRICATED NEW PART. INSTALLED LONGERON. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - E/E BAY LONGERON 29L IS CORRODED FROM STATION 200-218. REMOVED CORROSION. LONGERON WAS REMOVED. INSTALLED LONGERON. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND E/E COMPARTMENT LONGERON 25 LEFT STATION 160 HAS CORROSION. REMOVED CORROSION AT LONGERON. LOCATED AND DRILLED LONGERON SECTION REPAIR AND SPLICE. INSTALLED LONGERON SECTION REPAIR AND SPLICE. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1007-1220, LEFT CARGO TRACK HAS AREAS OF CORROSION/BARE METAL ALONG ENTIRE LENGTH OF TRACK. FROM STATION 1089-1220 FOUND OUT OF LIMITS. REMOVED CARGO TRACK AND SPLICE FROM STATION 1089-1220. DRILLED UP AND COUNTERSANK NEW TRACK. INSTALLED CARGO TRACK AND SPLICES. (M)

Part: PANEL — CRACKED (CARGO BAY)

FTW - MID CARGO FORWARD DOOR JAMB CLOSE OUT PANEL CRACKED AND LIGHT CORROSION ON BACK. STOP DRILL CRACK OF PANEL. FORMED DOUBLER FOR REPAIR AREA. INSTALLED DOUBLER. REMOVED LIGHT CORROSION. FOUND TO BE WITHIN LIMITS MATERIAL LOSS. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT FS 1287-1307 TOP FLANGE CRACKED AT -X0. REMOVED CABIN FLOOR SUPPORT. FABRICATED CABIN FLOOR SUPPORT FS 1287-1307. INSTALLED FLOOR SUPPORT. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

FTW - FOUND FORWARD PIT CORRODED AT LEFT CARGO TRACK STATION 351, STATION 370, STATION 389, STATION 408, STATION 427, STATION 446, STATION 484 AND STATION 503. REMOVED CORROSION AT LEFT CARGO TRACK STATION 351-503. REMOVED DAMAGED CARGO TRACK FROM STATION 351-503. FABRICATED NEW TRACK. FABRICATED SPLICE TRACK REPAIR. INSTALLED SPLICE CARGO TRACK. INSTALLED CARGO TRACK. (M)

Part: STRAP — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1193 L26L, FRAME SPLICE STRAP CORRODED. REMOVED CORROSION. REMOVED STRAP. FABRICATED REPLACEMENT STRAP, INSTALLED. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

FTW - FOUND FORWARD PIT CORRODED AT RIGHT CARGO TRACK FROM STATION 370, STATION 351, STATION 313, STATION 294. REMOVED DAMAGED CARGO TRACK. FORMED CARGO TRACK. INSTALLED FORMED CARGO TRACK. (M)

Part: STRAP — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1060 L29R-L29L, CORRODED FRAME TO LONGERON FASTENERS. REMOVED CORROSION. LOCATED AND DRILLED NEW STRAPS. INSTALLED STRAPS. (M)

Part: ANGLE — CORRODED (FUSELAGE)

FTW - FOUND FORWARD PIT CORRODED/ELONGATED HOLES AT FORWARD ZEE ANGLE STATION 370. REMOVED DAMAGED ZEE ANGLE. FABRICATED NEW ZEE ANGLE. INSTALLED ZEE ANGLE. (M)

Part: SUPPORT FITTING — CRACKED (CARGO DOOR)

FTW - FOUND MID LOWER CARGO DOOR HAS CRACK AT LOWER FORWARD BRACKET SUPPORT FITTING. REWORKED LOWER FORWARD BRACKET SUPPORT FITTING. DRILLED UP AND LOCATED NEW FITTING. INSTALLED FITTING. (M)

Part: SUPPORT FITTING — CRACKED (CARGO DOOR)

FTW - FOUND MID LOWER CARGO DOOR HAS CRACK AT FORWARD UPPER BRACKET SUPPORT FITTING. REMOVED FORWARD UPPER BRACKET SUPPORT FITTING. DRILLED UP AND LOCATED NEW FITTING. INSTALLED FITTING. (M)

Part: BRACKET — CORRODED (YAW DAMPER)

FTW - YAW DAMPER ACTUATOR ATTACHED BRACKET CORRODED. REMOVED RUDDER YAW DAMPER ACTUATOR MOUNT BRACKET. INSTALLED NEW YAW DAMPER ACTUATOR MOUNT BRACKET. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

FTW - FOUND MID PIT CORRODED AT BRACKET SUPPORT FITTING CARGO. REMOVED CORROSION. REMOVED DAMAGED PART AND REPLACED WITH NEW PART. (M)

Part: HOOK — CORRODED (CABIN)

FTW - FOUND OVERWING EMERGENCY EXITS ESCAPE LINES FOUR EACH, HOOKS CORRODED, SURFACE CORROSION. UPON CORROSION REMOVAL ESCAPE ROPES STARTED FRAYING AND STILL HOOK CORRODED UNDER ROPES, 4 EACH. REMOVED RIGHT FORWARD ESCAPE LINE. REMOVED LEFT FORWARD ESCAPE LINE. REMOVED RIGHT AFT E-LINE. REMOVED LEFT AFT E-LINE. INSTALLED RIGHT AFT ESCAPE LINE. INSTALLED LEFT FORWARD ESCAPE LINE. INSTALLED LEFT AFT ESCAPE LINE, INSTALLED RIGHT FORWARD ESCAPE LINE. (M)

Part: FLOORBOARD — BROKEN (FUSELAGE)

FTW - AT CARGO FLOORBOARD STATION 1212-1231 BROKEN 2 PLACES AND HAS CORROSION. FORMED NEW PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND AFT CARGO FLOORBOARD STATION 1155-1212 HAS CORROSION AND BAD INSERTS. FABRICATED NEW FLOOR PANEL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT OUTBOARD SEAT TRACK X44 FS 1222 TO FS 1305 HAS CORROSION. REMOVED CORROSION. REMOVED SEAT TRACK FROM STATION 1222-1305. LOCATE AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD TRACK -X44 FS 261 HAS GOUGES. REMOVED CORROSION. REMOVED SEAT TRACK AT -X44 FROM STATION 248-275. INSTALLED SEAT TRACK AT -X44 STATION 248-275. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD SEAT TRACK -X44 FS 560 TO FS 582 HAS CORROSION, GOUGES, AND SCRATCHES. AREA FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK -X22 FS 673 TO FS 679 HAS CORROSION, GOUGES, AND SCRATCHES. AREA FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK. DRILLED AND COUNTERSANK HOLES IN SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND RIGHT INBOARD SEAT TRACK -X22 FS 532 HAS CORROSION AND GOUGES. AFTER FURTHER EVALUATION CORROSION WAS FOUND AT FS 549 RIGHT INBOARD S/T -X22. REMOVED DAMAGED SECTION OF SEAT TRACK. FABRICATED SEAT TRACK FROM STATION 532-627 DRILLED AND LOCATED. INSTALL NEW SEAT TRACK AT STATION 532-627 -X22. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD SEAT TRACK -X44 FS 983 HAS CORROSION AND GOUGES. REMOVED CORROSION. CUT DAMAGED SECTION OF TRACK. DRILLED AND COUNTERSANK HOLES IN NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: PANEL — DELAMINATED (RT WING)

FTW - FOUND RIGHT WING LOWER EXTERNAL TRAPEZOIDAL PANEL HAS DELAMINATION. REPAIRED RIGHT WING LOWER EXTERNAL PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND LEFT FLOORBOARD BETWEEN INBOARD SEAT TRACK X22 AND OUTBOARD SEAT TRACK X44 AT STATION Y257 CORRODED. REMOVED FLOORBOARD. FABRICATED A NEW PANEL. INSTALLED FLOOR PANEL. (M)

Part: PANEL — DELAMINATED (LT WING)

FTW - FOUND LEFT WING LOWER EXTERNAL TRAPEZOIDAL PANEL HAS DELAMINATED. REMOVED DELAMINATED PLIES. REPAIRED DELAMINATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK X22 FS 1222 TO FS 1305 HAS CORROSION. REMOVED SEAT TRACK. LOCATED AND DRILLED, INSTALLED. (M)

Part: CHANNEL — BROKEN (T/E FLAP)

FTW - FOUND RIGHT FLAP TRAILING EDGE INBOARD FLANGE BROKEN. REMOVED BROKEN U-CHANNEL. FABRICATED NEW CHANNEL, INSTALLED. (M)

Part: BRACKET — CRACKED (T/E FLAP)

FTW - FOND RIGHT T/E NR 3 FLAP INBOARD ATTACHED BRACKET CRACKED. REMOVED CRACKED BRACKET. FABRICATED BRACKET, INSTALLED. (M)

Part: CONTROL VALVE — FAILED (SPOILER)

FTW - FOUND DURING OPS CHECK OF AUTO SPOILER SYSTEM. ONLY THE FLIGHT SPOILERS DEPLOY. TROUBLESHOT AND FOUND OPEN COILS ON BOTH RIGHT AND LEFT GROUND SPOILER CONTROL VALVES. REMOVED LEFT AND RIGHT GROUND SPOILERS CONTROL VALVES. INSTALLED LEFT AND RIGHT GROUND SPOILERS CONTROL VALVES. (M)

Part: PANEL — DAMAGED (RT WING)

FTW - FOUND RIGHT WING L/E PANEL 1248C FASTENER HOLE BUSTED OUT FRONT AND BACK, TOOL MARKS, BARE METAL, CORROSION AND CHAFING. CUT OUT DAMAGED AREA. FABRICATED NEW SKIN SECTION. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER AND SKIN SECTION. (M)

Part: RAM AIR DOOR — CRACKED (APU)

FTW - FOUND APU RAM AIR DOOR CRACKED RIGHT HINGE CORNER APPROX .5 INCH. DURING INSTALLATION OF REPAIR, FOUND SKIN CRACKED LEFT CORNER OF SKIN AT HINGE, BOTH LEFT AND RIGHT STIFFENERS CRACKED AT THROUGH BOLT HOLE AND 2 FT BY 5 INCH PIECE OF METAL TORN OFF L/E OF RIGHT STIFFENER. REMOVED AIR INLET PANEL. INSTALLED NEW AIR INLET PANEL AND ORIGINAL ACTUATOR. (M)

Part: STIFFENER — CHAFED (NR 1 COWLING)

FTW - FOUND NR 1 ENGINE UPPER COWL AFT STIFFENER CHAFED. REMOVED DAMAGE. REPAIRED DAMAGED AREA, SPIRIT AIRLINES EA 5410-0202. (M)

Part: BEAM — BROKEN (LT PYLON)

FTW - FOUND LEFT FORWARD UPPER VIBRATION ABSORBER LONG BEAM PRETUNED BROKEN. BROKEN BEAM REMOVED. INSTALLED ABSORBER BEAM PRETUNED. (M)

Part: WIRE — BROKEN (ELEVATOR)

FTW - FOUND LEFT ELEVATOR POSITION SENSOR FAILS DFDR TEST, OCTAL DISPLAY DOES NOT CHANGE. T/S FOUND 2 WIRES BROKEN. REPAIRED BROKEN WIRES. (M)

Part: FIRE BOTTLE — CORRODED (LAVATORY)

FTW - ALL LAVATORY FIRE EXTINGUISHER BOTTLES BADLY CORRODED. REMOVED ALL LAVATORY FIRE EXTINGUISHERS. INSTALLED ALL LAVATORY FIRE EXTINGUISHERS. (M)

Part: BRACKET — BROKEN (FUSELAGE)

FTW - FOUND STATION 864 L18L, OVERWING-WING TO BODY FAIRING ATTACH BRACKET IS BROKEN. REMOVED BROKEN ATTACH BRACKET. FABRICATED ATTACH BRACKET. INSTALLED ATTACH BRACKET. (M)

Part: TRIM TAB — CORRODED (ELEVATOR)

FTW - FOUND LEFT ELEVATOR CONTROL TAB BOTTOM SIDE HAS TWO OUTBOARD WEEP HOLES CORRODED. REMOVED LEFT ELEVATOR CONTROL TAB. INSTALLED CONTROL TAB ON LEFT ELEVATOR. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

MCO - FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE MID CABIN. REPLACED EMERGENCY LIGHTS POWER SUPPLY AT ROW 17 RIGHT. OPS TEST OK IAW 33-53-00. (M)