N810NK

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR B00182-05N-00119, 00121, 00124; CABIN SEAT TRACK CORRODED, STA 807-984 RBL 24 IB AND LBL 24 AND LBL 43 IB, STA 905 RBL 43 OB. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK, TREATED, PRIMED AND TOP COATED NEW SEAT TRACK.

Part: GIRT BAR — SHORT (L2 DOOR)

SAS NR B00182-05N-11136; L2 DOOR EMERGENCY SLIDE DID NOT DEPLOY PROPERLY. FOUND L2 DOOR SLIDE GIRT BAR TOO SHORT, REMOVED AND REPLACED GIRT BAR.

Part: RECEPTACLE — CORRODED (ESCAPE LINE)

SAS NR B00182-05N-00118; OVERWING ESCAPE LINES REEL ASSY LT FWD AND AFT AND RT FWD AND AFT ATTACH HARDWARE SHEARED AND RECEPTACLES CORRODED. REMOVED AND REPLACED HARDWARE AND RIVNUTS ON LT AND RT OVERWING ESCAPE LINE REEL ASSY.

Part: SKIN — CRACKED (FUSELAGE)

2 INCH CRACK ABOVE FWD CARGO DOOR, CLASS II REPAIR. REMOVED EXISTING REPAIR DOUBLER, CUTOUT SKIN SECTION BETWEEN STA 351-389 AND BETWEEN L16R AND 18R (14 INCH BY 18 INCH), FABRICATED NEW SKIN FROM 2024T3-0.50, FABRICATED FINGER DOUBLER, LOCATED AND DRILLED DOUBLER, TREATED, PRIMED AND INSTALLED DOUBLER AND SKIN REPAIR.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

NR 2 ENGINE (B) LOOP FLICKERS ON T/O AND DURING FLT. NR 2 ENGINE CHANGED WITH LOOP ON IT. NOTE: ENGINE CHANGE ACCOMPLISHED ON 10/10/04, OCCURRENCE DATE CHANGED TO REFLECT CLOSURE OF REPORT.

Part: BULB — FAILED (OIL TEMP)

RT ENGINE OIL TEMP HIGH 145 IN CLIMB, 12 MINUTES STABILIZED IN CRUISE, HIGH ON APPROACH 150, 5 MIN. REMOVED AND REPLACED NR 2 ENGINE OIL TEMP BULB. ENGINE OPS CHECK, OK. MM 79-32-01.

Part: ENGINE — SHUTDOWN (NR 2)

INFLIGHT SHUTDOWN, EMERGENCY AIR RETURN. RT OIL TEMP HIGH IN CLIMB, SHUTDOWN ENGINE AT 165 DEGREES. REMOVED AND REPLACED NR 2 ENGINE IAW MM. LEAK CHECK OK.

Part: FIRE LOOP — INTERMITTENT (NR 2 B-LOOP) · airframe 66,618 hrs · 41,937 cycles

ON TAKEOFF, AFTER ROTATION, WITH FLEX POWER 1.86, THE NR 2 B-LOOP FIRE LIGHT BEGAN TO FLICKER UNTIL GEAR RETRACTION. ALL OTHER ENGINE INDICATIONS NORMAL. NOTE: NOSE WHEEL VIBRATION AFTER T/O UNTIL RETRACTION SEEMS TO COINCIDE WITH THE LIGHT FLICKER.

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

DTW - VERIFY LOWER FORWARD VIBRATION ISOLATOR ALIGNMENT MARKS ARE WITHIN LIMITS. REMOVED AND REPLACED FORWARD LOWER NR 1 ENGINE ISOLATOR MOUNT. (M)

Part: ENGINE — VIBRATION (LEFT)

FLT 197 - LGA - LEFT ENGINE UNUSUAL NOISE AND VIBRATION ON CRUISE POWER CHECK (L) HYD PUMP OFF PACK (L) OFF AND NOT CHANGES. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: CABLE — MISINSTALLED (L2 DOOR GIRT BAR)

FLL - FOUND L2 DOOR EMERGENCY EXIT SLIDE GIRT BAR CABLE ROUTED IMPROPELY. REROUTED CABLE. (M)

Part: HANDLE — LOOSE (L1 DOOR)

FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) GTIA

Part: FILTER HOUSING — CRACKED (RT HYD SYS)

JUST AFTER SELECTING SLATS EXTEND, RT HYD QTY FOLLOWED BY PRESSURE FELL TO ZERO. FOLLOWED QRH PROCEDURE AND LANDED STOPPING ON RUNWAY UNTIL MAINTENANCE CAME OUT TO SECURE DOORS. TOWED TO GATE. TSHOOT, FOUND RT SYSTEM PRESS FILTER HOUSING IN AFT AIRSTAIRS MISSING DELTA P INDICATOR ASSEMBLY. REMOVED AND REPLACED RT SYSTEM PRESSURE FILTER HOUSING. REMOVED AND REPLACED RT CASE DRAIN FILTER ELEMENT SERVICED RT HYDRAULIC SYSTEM. OPS AND LEAK CHECK BOTH FILTERS. NO DEFECTS NOTED. A/C OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)

MCO - AFT AIRSTAIRS EMERGENCY LIGHT OUT, CENTER. REINSTALLED MISSING SCREW FROM LIGHT. OPS CHECK NORMAL. (M)

Part: LIGHT — INTERMITTENT (MLG INDICATOR)

NOSE GEAR LIGHT FLICKERS ON AND OFF IN FLIGHT. REMOVED AND CLEANED CANNON PLUG.

Part: SWITCH — BROKEN (CABIN)

FTW - FOUND FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH BROKEN. REPLACED FORWARD LIGHT ATTENDANT EMERGENCY LIGHT SWITCH. (M)

Part: GLOWSTRIP — MISSING (CABIN)

DTW - FOUND SAFETY GLO FLOORPATH STRIP MISSING IN AFT GALLEY, L2 DOOR. RESECURED SAFETY GLO FLOORPATH LIGHTING. NO OTHER DEFECTS NOTED. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - FOUND CABIN STATION 807-826 STRINGER 1 INTERCOSTAL CORRODED. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT CABIN INBOARD SEAT TRACK CORRODED AND WORN STATION 200-1307. REMOVED CORROSON LEFT CABIN INBOARD SEAT TRACK STATION 200-1307. REMOVED SEAT TRACK STATION 200 TO SPLICE STATION 260. LOCATED AND DRILLED NEW SEAT TRACK STATION 200 TO SPLICE STATION 260. INSTALLED SEAT TRACK STATION 200 TO SPLICE STATION 260. (M)

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

DTW - FOUND FIRST OFFICERS SMOKE GOGGLES CRACKED. REMOVED AND REPLACED FIRST OFFICERS SMOKE GOGGLES. (M)

Part: LIGHT — INOPERATIVE (TAIL CONE)

MCO - FOUND EMERGENCY LIGHT OVER SLIDE IN TAIL CONE INOPERATIVE. CLEAN ALL SOCKET CONTACTS AND TERMINAL ENDS, OPS CHECK OK. (M)

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG)

NOSE GEAR UNSAFE LIGHT ILLUMINATED ON CLIMB-OUT PASSING 20,000 FT THROUGH 23,000 FT THE LIGHT WENT OUT AFTER THAT AND REMAINED OUT. ALL OTHER NORMAL INDICATIONS. IT JUST FLICKERED ON AND OFF. FOUND AIR GAP ON NOSE DOWN LOCK PROXIMITY SWITCH OUT OF LIMITS. ADJUSTED AIR GAP TO WITHIN LIMITS. PERFORMED GEAR RETRACTION CHECK ON NOSE GEAR. OPS CHECKED GOOD. PROXIMITY BOX BITE CHECKED GOOD. NO OTHER DISCREPANCIES NOTED. (M)

Part: STRUCTURE — BROKEN (RT WING)

RIGHT WING LEADING EDGE LIP AT RE-FUELING PANEL OPENING IS BROKEN OFF AT INBOARD LATCH. TRIMMED OUT DAMAGE. FABRICATED 11 DOUBLER. FABRICATED 13 FILLER. I NSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: TERMINAL — SHORTED (EMERGENCY LIGHTS)

FOUND OVERHEAD EMERGENCY LIGHT AT SEAT 31 SHORTED. TROUBLESHOT EMERGENCY LIGHTS AND FOUND LOOSE TERMINAL AT LIGHT FIXTURE. TIGHTENED LOOSE TERMINAL. (M)

Part: FLOORBEAM — BROKEN (FUSELAGE)

FOUND FS 655 CABIN FLOORBEAM BROKEN OFF AT RIVETS. DRILLED EXISTING HOLES. INSTALLED FLOOR PANEL SUPPORT. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

FOUND FLOORBOARD STATION 1156-1254 LBL 44 STIFFENERS CRACKED AND DEBONDED. REPAIRED FLOORBOARD. (M)

Part: FLOOR PANEL — DEBONDED (CABIN)

FOUND FLOOR PANEL OUTBOARD G-2 STIFFENERS CHAFING AND DEBONDED. REPAIRED FLOOR PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CABIN STATION 182 UPPER SURFACE CORRODED FS 234-241, CUSP. CUT OUT DAMAGE IN WEB. DRILLED AND LOCATED WEB AND REPAIR DOUBLER. INSTALLED WEB AND DOUBLER. (M)

Part: FITTING — CORRODED (FUSELAGE)

FOUND MID PIT STATION 636 FRAME END FITTING CORRODED. LOCATED AND DRILLED HOLES NEW FITTING. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT FS 359 BETWEEN LONGERONS 20 AND 21R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED ONE DOUBLER. INSTALLED ONE DOUBLER REPAIR. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 321 BETWEEN LONGERONS 25 AND 26R, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

FOUND RIGHT CO-PILOT CONTROL COLUMN FLOOR PANEL CRACKED. REMOVED DAMAGED FLOOR PANEL. LOCATED AND DRILLED NEW FLOOR PANEL. INSTALLED NEW FLOOR PANEL SKIN. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 218 BETWEEN LONGERON 15 AND 16L, DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT AT FS 360 BETWEEN LONGERONS 19 AND 20R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED 1 DOUBLER. INSTALLED 1 DOUBLER REPAIR. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT FS 350 BETWEEN LONGERONS 25 AND 26R. DENT WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED WITH SOLID FASTENERS. (M)

Part: SKIN — DENTED (FS)

FTW - FOUND DENT AT FS 350 BETWEEN LONGERONS 26 AND 27R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DUOBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

SCRATCH WITH DENT AT FS 800 BETWEEN LONGERONS 5 AND 6R REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)

Part: FRAME — CORRODED (FUSELAGE)

FOUND MID CARGO FS 693 FRAME AND FITTING CORRODED AT JAMB BEAM. LOCATE AND DRILLED NEW FITTING. (M)

Part: DOOR FRAME — CORRODED (MLG DOOR)

FOUND LT-RT MLG DOOR JAMB HINGE SUPPORT CORRODED. FABRICATED NEW LT FITTING. LOCATED AND DRILLED NEW LT AND RT HINGE SUPPORTS FOR DOOR JAMB. INSTALLED NEW LT AND RT HINGE SUPPORTS FOR DOOR JAMB. REMOVED LT HINGE SUPPORT. INSTALLED LT HINGE SUPPORT. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

FOUND FLOORBOARD, OUTBOARD LEFT AFT, STATION 1250 TO 1361, STIFFENER DISBONDED. INSULATION MISSING AND TORN. REPAIRED FLOORBOARD. (M)

Part: STRUCTURE — GOUGED (SUBFLOOR)

FTW - SUBFLOOR GOUGED STATION 180 RBL 34. MATERIAL FOUND TO BE CRACKED. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR FILLER AND DOUBLER. (M)

Part: STIFFENER — CRACKED (FLOOR)

FOUND FLOORBOARD, RIGHT OUTBOARD FS 928-1003, LOWER STIFFENER CRACKED. REMOVED DAMAGED AREA. FABRICATED DOUBLR AND FILLER. INSTALLED DOUBLER AND FILLER. (M)

Part: BEAM — CORRODED (CARGO DOOR)

FTW - FOUND MID CARGO COMP, JAMB BEAM CORRODED STATION 636 TO 693. REMOVED BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 148-200 RBL 7 HAS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: STRUCTURE — CRACKED (SUBFLOOR)

SUBFLOOR CRACKED AND HOLE PUNCTURED STATION 199 RBL 50. CUT OUT DAMGAED SECTION OF WEB. FABRICATED NEW SECTION OF WEB AND DOUBLER. INSTALLED WEB AND DOUBLER. (M)

Part: FLOOR PANEL — DELAMINATED (COCKPIT)

FOUND FLIGHT COMPARTMENT OBSERVER SEAT FLOOR PANEL DELAMINATED. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (COCKPIT)

FOUND FLIGHT COMPARTMENT CENTER FLOOR PANEL AND SUPPORT DAMAGED DELAMINATED. FABRICATED FLOOR PANEL. (M)

Part: FLOOR PANEL — GOUGED (FUSELAGE)

PILOT FLOOR PANEL GOUGE AND BARE METAL. UPON FURTHER INVESTIGATION GOUGE IS A CRACK. FABRICATED PLATE AND DOUBLER. INSTALLED PLATE AND DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLOOR SUPPORT HAS CORROSION STATION 160-200 RBL 43. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOORBOARD — DELAMINATED (CABIN)

FOUND CABIN FLOOR PANEL AFT OF R-1 DOOR IS DELAMINATED. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

EPC PANEL LOWER FLANGE HAS CORROSION STATION 160 LBL 13-57. UPON REMOVAL OF THE EPC PANEL LOWER FLANGE, THE FLOOR SUPPORT BELOW EPC PANEL IS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORTS FOUR EACH AT STATION 200 RBL 5-57 ARE CORRODED. REMOVED FOUR EACH FLOOR SUPPORTS. FABRICATED NEW FLOOR SUPPORTS. INSTALLED FLOOR SUPPORTS. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND AFT PIT INTERCOSTAL CRACKED AT FS 1309-1320 LONGERON 28R. REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT STATION 160-200 LBL 44 HAS CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: PANEL — DELAMINATED (SPOILER)

RIGHT INBOARD SPOILER PANEL DELAMINATED. REPAIRED RIGHT INBOARD SPOILER PANEL. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLOOR SUPPORT STATION 190 RBL 9-43 HAS LT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: TAB — DENTED (RT AILERON)

FOUND RT WING AILERON CONTROL TAB HAS NUMEROUS DENTS ON UPPER SIDE. ON REMOVAL OF PAINT, CORROSION WAS LOCATED ON THE RT TAB LOWER SKIN IN SEVERAL AREAS AS MARKED. REPLACED RT AILERON CONTROL TAB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND TWO SMALL FLOOR SUPPORTS LBL 53 AND 1 LONG SUPPORT LBL 57 STATION 160-200 ARE CORRODED. REMOVED LONG FLOOR SUPPORT. REMOVED SMALL FLOOR SUPPORT. FABRICATED LONG AND 1 SMALL FLOOR SUPPORT. INSTALLED 1 SMALL FLOOR SUPPORT LBL 53 AND 1 LONG FLOOR SUPPORT. (M)

Part: SKIN — CORRODED (FUSELAGE)

FTW - FOUND CORROSION AROUND FASTENER HOLES AT STATION 237 ON WEB AT RBL 47 TWO PLACES. CUT OUT DAMAGED AREA. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORTS FOUR EACH STATION 200 LBL 9-57 ARE CORRODED. FLOOR SUPPORTS AT STATION 200 LBL 16 TO 43, 44-53, 55-57 OUT OF LIMITS. REMOVED FLOOR SUPPORTS. FABRICATED NEW FLOOR SUPPORTS. INSTALLED FLOOR SUPPORTS. (M)

Part: ANGLE — CORRODED (DOOR FRAME)

MID PIT DOOR OPENING LOWER AFT CORNER STATION 693 FRAME CORRODED. REMOVED LOWER 6 INCH OF FS 693 FRAME. FABRICATED FILLER AND REPAIR ANGLE. INSTALLED FILLER AND REPAIR ANGLE. (M)

Part: VANE — DELAMINATED (RT FLAP)

FOUND RT OUTBOARD FLAP MIDDLE VANE LOWER SIDE DELAMINATED. RIGHT OUTBOARD REMOVED FLAP MIDDLE VANE. VANE DELAMINATED BEYOND BOEING DC-9 MD-80 ACCEPTABLE REPAIR LIMITS AND TRAILING EDGE HAS HEAVY CORROSION. INSTALLED NEW RIGHT OUTBOARD FLAP MIDDLE VANE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED FS 1309-1338 LBL 17. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FLOOR SUPPORT STATION 218 LBL 13-RBL 10 HAS CORROSION. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: WEB — CORRODED (FUSELAGE)

LT CUSP CORRODED STA 200-229. PRIOR TO STEP 7, FOUND CORRODED WEB TO BE BEYOND ECONOMICAL REPAIR. REMOVED L1 DOOR WEB STATION 200-208. CORRODED ON CUSP WAS FOUND TO BE OUT OF LIMITS. FABRICATED CUSP, WEB WAS FOUND TO BE OUT OF LIMITS. REMOVED CORROSION ON WEB STATION 218-236 LBL 44 TO LBL 54. WEB WAS FOUND TO BE OUT OF LIMITS. FABRICATED WEBS STATION 218-236 AND 200-218. REMOVED COROSION ON L1 DOOR WEB. INSTALLED NEW SECTION OF CUSP STATION 180 TO 230. INSTALLED L1 DOOR WEB STATION 200-208. INSTALLED WEB STATION 200-218. INSTALLED WEB STATION 218-236. (M)

Part: FITTING — CORRODED (BULKHEAD)

FOUND STRINGER 29L APB TEE NUTS NOT SELF CENTERING IAW SB-53-201 AND REQUIRE GOUGE INSPECTION UPON REMOVAL. AFTER REMOVAL OF NUTS DISCOVERED CORROSION ON TEE FITTING. REMOVED TEE FITTING. LOCATED AND DRILLED NEW TEE FITTING. INSTALLED TEE FITTING. (M)

Part: VANE — DENTED (RT FLAP)

FOUND RIGHT INBOARD FLAP OUTBOARD VANE DENTED AND DELAMINATED. REPAIRED RIGHT INBOARD FLAP OUTBOARD VANE DENTS AND DELAMINATION THREE PLACES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT CORRODED FS 1309-1338 RBL 17 INCHES. REMOVED DAMAGED SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR PANEL — CRACKED (COCKPIT)

FLIGHT COMPARTMENT, RIGHT FLOOR PANEL CRACKED, BACKSIDE HAS SURFACE CORROSION AND BARE METAL. CUT OUT CRACK IN PANEL, FABRICATED NEW PLATE AND DOUBLER. INSTALLED PLATE AND DOUBLER. (M)

Part: STRUCTURE — CRACKED (NLG DOOR)

FOUND RIGHT FORWARD NOSE GEAR DOOR, EXCESSIVE PLAY IN AFT HINGE. UPON FURTHER INSPECTION, FOUND STIFFENER JUST OUTBOARD OF AFT HALF HINGE FOR RT NLG FORWARD DOOR TO BE CRACKED. FABRICATED NEW STIFFENER. INSTALLED NEW AFT HALF HINGE AND NEW OUTBOARD STIFFENER. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

FOUND LT MLG FORWARD DOOR JAMB IS CRACKED AT T-CAP DOUBLER. REMOVED DOUBLER. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M)

Part: FITTING — CRACKED (NLG WW)

FOUND NOSE WHEEL WELL, STATION 70 LBL 16 AND RBL 16, TWO FITTINGS CRACKED. REMOVED TWO FITTINGS. LOCATED AND DRILLED HOLES ON TWO NEW FITTINGS. INSTALLED TWO NEW FITTINGS. (M)

Part: ANGLE — CRACKED (FUSELAGE)

NOSEWHEEL WELL, STATION 40 LBL 5 AND RBL 5, TWO ANGLES CRACKED AT AFT END IN RADIUS. REMOVED TWO ANGLES. FABRICATED TWO ANGLES. INSTALLED TWO ANGLES. (M)

Part: SUPPORT — SHEARED (NLG WW)

FOUND NOSE WHEEL WELL, STATION 38-43 RBL 16, FOUR SHEARED RIVETS AT OUTBOARD LOWER END OF BULKHEAD SUPPORT. REMOVED BULKHEAD SUPPORT. ON FURTHER INSPECTION FOUND BULKHEAD SUPPORT CRACKED. LOCATED AND DRILLED HOLES ON NEW SUPPORT. INSTALLED SUPPORT BULKHEAD STRUCTURE. (M)

Part: SKIN — CHAFED (TE FLAPS)

LEFT WING INBOARD FLAP, OUTBOARD VANE BARE METAL AT LOWER SURFACE AND CHAFED ON FIXED TRAILING EDGE. DISCOVERED CRACK ON BOTTOM SIDE OF VANE. ON REMOVAL OF RUBSTRIPS, FOUND SKIN DELAMINATION. REPAIRED DELAMS UNDER RUBSTRIPS. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

FOUND FORWARD SIDE OF FORWARD BULKHEAD, STATION 36 RBL 4, SUPPORT ANGLE ON SHELF BELOW RADAR ANTENNA IS CRACKED IN RADIUS (DOT LP005) PEELING PAINT/BARE METAL UPPER SURFACE ON SHELF. REMOVED CRACKED SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M)

Part: PRESSURE PANEL — CRACKED (NLG WW)

NOSE WHEEL WELL STATION 38 RBL 11, BULKHEAD SUPPORT WEB IS CRACKED. REMOVED CRACKED WEB. LOCATED AND DRILLED ON NEW WEB. INSTALLED WEB. (M)

Part: FLOOR PANEL — BROKEN (CABIN)

FOUND CABIN FS 815 LEFT MID FLOOR PANEL HAS BROKEN INSERT AND MISSING SCREW. FABRICATED NEW PANEL. (M)

Part: BEAM — CORRODED (CARGO DOOR)

AFT PIT DOOR BEAM CORRODED. FORMED NEW DOUBLER. INSTALLED NEW REPAIR. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND CABIN FS 1112 RIGHT FLOOR PANEL CRACKED. REMOVED OUTBOARD RIGHT FLOOR PANEL. FABRICATED DOUBLER REPAIR. INSTALLED DOUBLER REPAIR. INSTALLED FLOOR PANEL. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

FOUND EMERGENCY LIGHTS INOPERATIVE, ROW 1, 20, 29 AND 31. REPAIRED WIRES. (M)

Part: FLOORBOARD — BROKEN (FUSELAGE)

MAIN CABIN FS 754 RIGHT CENTER FLOOR PANEL HAS BROKEN INSERT. REMOVED PANEL. FABRICATED PANEL. INSTALLED FLOORBOARD. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CABIN RIGHT INBOARD SEAT TRACK CORRODED FS 1073-1309. SEAT TRACK OUT OF LIMITS AT STATION 1287. CUT OUT DAMAGED SECTION OF RIGHT INBOARD SEAT TRACK FROM FS 1223 TO 1309. FABRICATED REPLACEMENT SECTION OF SEAT TRACK. INSTALLED NEW TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CABIN RIGHT INBOARD SEAT TRACK CORRODED FS 692-886. REMOVED TRACK. DRILLED AND LOCATED NEW TRACK AND SPLICES. INSTALLED NEW TRACK. (M)

Part: FLOOR PANEL — BROKEN (CABIN)

FOUND MAIN CABIN FS 730 CENTER FLOOR PANEL HAS BROKEN INSERT. REMOVED FLOORBOARD. FABRICATED FLOOR PANEL. INSTALLED NEW PANEL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CABIN LEFT INBOARD SEAT TRACK CORRODED FS 1309-1214. CUT OUT LEFT INBOARD SEAT TRACK. LOCATED AND DRILLED NEW SECTION OF SEAT TRACK. INSTALLED LEFT INBOARD SEAT TRACK. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND MID PIT CARGO STATION 636 AND STATION 693 RIGHT SUPPORTS CORRODED. PRIOR TO STEP 11 REMOVED CORRODED ANGLES. INSTALLED NEW ANGLES. FABRICATED TWO SUPPORTS CHANNELS. (M)

Part: PANEL — CRACKED (INTERIOR)

FOUND AFT ACCY COMPARTMENT OVERHEAD INTERNAL WEB PANEL CRACKED AT AFT END AT FS 1485 CANT FRAME 24 INCHES LBL. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CABIN LEFT MIDDLE SEAT TRACK CORRODED FS 1309-1214. CUT OUT SEAT TRACK. DRILL AND LOCATED NEW SECTION OF SEAT TRACK. DRILL AND LOCATED SPLICE REPAIR. INSTALLED MID SEAT TRACK FS 1204-1309 AND SPLICE REPAIR. (M)

Part: ISOLATION MOUNT — SLIPPED (NR 1 ENGINE)

NR 1 ENG. LOWER/ FORWARD ENGINE ISOLATOR SLIPPED AT.2500 INCH. CHANGED. REMOVED AND REPLACED NR 1 ENGINE LOWER/ FORWARD. (PRECAUTIONARY) ENG ISOLATOR.

Part: SKIN — CRACKED (FUSELAGE)

2.250 INCH CRACK ON AIRCRAFT RT SIDE, JUST AFT OF ELEVATOR ACCUMULATOR ACCESS DOOR. (UNPRESSURIZED AREA) TRANSFERRED TO COI, REPAIRED WITHIN 10 DAYS.

Part: SKIN — CRACKED (FUSELAGE)

FTW - FOUND UPPER FUSELAGE AT STATION 313, LONGERON 1 CRACKED UNDER NR 2 VHF ANTENNA. FORMED FILLER AND DOUBLER. INSTALLED NEW REPAIR. (M)

Part: SWITCH — OUT OF ADJUST (SLATS)

FLL - FLT 470 - FOUND AUTO SLAT FAIL ON TAKEOFF, DID NOT COME ON DURING LANDING. ADJUSTED FLAP/SLAT SWITCH IAW MM 27-84-02. (M)

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

DTW - FOUND RUDDER POWER CONTROL VALVE LINE, TO T-FITTING JUST FORWARD OF HYDRAULIC FILTERS IN TAIL SECTION RIGHT SIDE IS LEAKING. INSTALLED TEMP FLEX LINE, DEFECTIVE LINE IS REMOVED. PLACED TEMP FLEX LINE ON C/O 38818-2. REMOVED TEMPORARY FLEX LINE AND REPLACED WITH RIGID LINE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND STATION 166 RBL 10, FLOOR BOARD SUPPORT CORRODED. REMOVED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CABIN LBL STATION 896, INBOARD SEAT TRACK, HAS CORROSION. REMOVED SEAT TRACKS. FABRICATED NEW SEAT TRACKS. INSTALLED SEAT TRACKS. (M)

Part: HARNESS — OUT OF POSITION (FIRE DETECTION)

FLL - FLT 1765 - FOUND FIRE DETECTOR LOOP ANNUNCIATOR LIGHT CAME ON DURING DESCENT. LOOP 'B' WAS ILLUMINATED. LOOP 'A' OK NOT ILLUMINATED NO OTHER FIRE INDICATORS. FOUND HARNESS AT UPPER BURN THROUGH BARRIER ROUTED TO CLOSE TO APRON BRACKET. REPOSITIONED HARNESS AND CLEANED CONNECTIONS. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. (M)

Part: WIRE — OUT OF POSITION (COCKPIT)

MCO - FLT 927 - LEFT ENGINE FIRE DETECT LOOP 'B' LIGHT ILLUMINATED WITHOUT FIRE WARNING. COMPLETE QRH PROCEDURE. SWITCHED TO NR 1 'A' LOOP ONLY ON PANEL. TESTED A/B LOOP NR 2 ENGINE, OPS OK. INSPECTED ENTIRE LEFT ENGINE LOOP SYSTEM AND PERFORM BITE. FOUND LOOP B LEFT ENGINE (AMBER) LIGHT SWITCH ASSY IN COCKPIT ON OVERHEAD PANEL WIRES MAKING CONTACT WITH FRAME. ADJUSTED WIRE POST ON SWITCH IAW MD80 MM 26-11-00 OPERATION CHECK OK. (M)

Part: ACOUSTIC PANEL — CRACKED (THRUST REVERSER)

FTW - FOUND NR 1 ENGINE T/R HAS DENT AND CRACK AT ACOUSTIC PANEL. T/R REPLACED ON BOO03611-R-2. (M)

Part: CONNECTOR — DIRTY (L/E SLAT)

ACY - FLT 1265 - AUTO SLAT FAIL LIGHT ILLUMINATED DURING FLAP EXTEND FOR T/O TESTED STALL WARN BOTH 1 AND 2 TEST WAS SATISFACTORY. RETURNED TO GATE FOR MAINTENANCE. TESTED AND CLEANED CONNECTORS ON GROUND PROXIMITY UNIT-CYCLED NUMEROUS TIMES, OPS CHECKS OK PER MM 32-60-04 AND 27-80-00. (M)

Part: COMPUTER — INOPERATIVE (NR 1)

ACY - FLT 259 - AUTO PILOT DOES NOT HOLD SELECTED VERTICAL SPD IN VERTICAL SPPED MODE OR SELECTED IAS MODE WHEN DESCENDING. FOUND INOPERATIVE DFGC COMPUTER NR 1 REMOVED AND REPLACED DFGC NR 1 AND RAN RETURN TO SERVICE TEST NO FAULT NOTED CHECKED GOOD. (M)

Part: ENGINE — LEAKING (RIGHT)

FLL - FLT 9810 - LEVEL AT 5000 FEET RIGHT ENGINE WENT FROM 65 PERCENT N1 TO 110 PERCENT, EPR WENT TO 2.30 EGT 670 NO CONTROL OVER ENGINE WITH POWER LEVER. DURING INITIAL RUN AFTER INSTALLING ENGINE FOUND FUEL LEAKING FROM COLD STREAM INTO REVERSER. REMOVED AND REPLACED ENGINE IAW 71-00-00 ON ENGINE RUN FOUND FUEL LEAK IN COLD STREAM. REMOVED AND REPLACED NR 2 ENGINE. RUN CHECK AND LEAK CHECK OK. (M)

Part: SWITCH — FAILED (LE SLATS)

DTW - FLT 595 - DURING SLAT EXTENSION, THE AUTO SLAT FAIL LIGHT ILLUMINATED AND THE SLAT DISAGREE LIGHT REMAINED ON. BOTH STALL WARNING SYSTEM PROPERLY. AUTO SLAT FAIL LIGHT REMAINED ILLUMINATED WITH SLATS RETRACTED. REMOVED AND REPLACED FLAP HANDLE SWITCH AND OPS CHECK GOOD IAW MM 27-80-07. (M)

Part: BATTERY — DISCHARGED (CABIN)

ACY - FOUND RIGHT AFT OVERWING EMERGENCY DOOR EXIT LIGHT AND LEFT AFT OVERWING EMERGENCY DOOR EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY OVER SEAT 23D OPERATION CHECK NORMAL IAW MM 33-53-00. (M)

Part: CIRCUIT BREAKER — FAILED (NAV TRANSFORMER)

FLL - NAV INST XFMR L C/B-F16 TRIPPED CAUSED 1, ALT WINDOWS TO GO BLANK 2 ART TO FIRE 3, NO AUTO THROTTLE. FOUND NR 1 NAV INST TRANSFORMER C/B WEAK NO HOLDING. REMOVED AND REPLACED THE 2A C/B IAW MM 31-15-01. OP CHECK NORMAL. PERFORMED OPERATIONAL CHECK OF AUTOTHROTTLE SYSTEM IAW MM 22-30-00 NORMAL. NO FAULT INDICATION FOR ART SYSTEM IAW 73-20-00. CHECK NORMAL. (M)

Part: VANE — DAMAGED (AOA SYSTEM)

DTW - FLT 1258 - AUTOTHROTTLE WORKED IN UNTIL REACHING CRUISE AT 29,000 THEN WENT OFF LINE COULD NOT RE-ENGAGE. REMOVED AND REPLACED RIGHT AOA VANE PER MD80 MM 34-19-01, SYSTEM OPS CHECK GOOD. (M)

Part: VANE — FAILED (AOA SYSTEM)

DTW - FLT 1258 - AUTOTHROTTLE WORKED UNTIL REACHING CRUISE AT 29,000 THEN WENT OFF LINE COULD NOT RE-ENGAGE. REMOVED AND REPLACED RIGHT AOA VANE PER MD80 MM 34-19-01, SYSTEM OPS CHECK GOOD. (M)

Part: RELAY — FAILED (AUTOTHROTTLE SYS)

FLT 953 - AFTER TAKEOFF FAST SLOW SPEED FLAG APPEARED ON BOTH CAPTAIN'S AND FO HSI. AUTO THROTTLES DISENGAGED AND WOULD NOT RE-ENGAGE DURING THE FLIGHT A/T DISENGAGE AT ALTITUDE CAPTURE AND AUTO THROTTLES WENT INTO SPEED SEL MODE. REMOVED AND REPLACED RELAY R2-6 IAW MD80 MM 20-50-00. OPS CHECK NORMAL IAW MD80 MM 34-24-00. (M)

Part: SMOKE DETECTOR — FAILED (LAVATORY)

DTW - FOUND LEFT AFT LAVATORY SMOKE DETECTOR TEST PANEL FAILED. OPS CHECK. REMOVED AND REPLACED LEFT AFT SMOKE DETECTOR. OPS CHECK GOOD. (M)

Part: CONNECTOR — DIRTY (FIRE LOOP)

FLT 779 - FLL - LOOP A FIRE DETECT LIGHT ON DESCENT. NO OTHER INDICATIONS FOLLOW ABNORMAL CHECK LIST. CHECKED AND CLEANED ENGINE NR 1 A LOOP SENSING ELEMENT CONNECTORS. REF WDM 26-11-00. OP CHECKED OK REF MM 26-10-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLL - EMERGENCY CEILING LIGHTS BETWEEN SEATS 16/18 ILLUMINATE WHEN A/C ELECTRICAL POWER REMOVED FROM A/C. REMOVED BATTERY FROM PACK AT STATION 731R. REMOVED AND REPLACED BATTERY PACK AND BATTERIES, IAW MM 33-53-00. OPS CHECK OK. (M)

Part: SLIDE — OUT OF POSITION (L2 DOOR)

FTW - L2 DOOR SLIDE FALLS OFF. INSTALLED SLIDER STOP IAW MD-80 MM 25-62-00. OPS CHECK GOOD. (M)

Part: LATCH — OUT OF ADJ (CABIN)

FTW - L-1 FLIGHT ATTENDANT MASK DIDN'T DROP DURING FLIGHT CHECK. ADJUSTED LATCHING MECH IAW MD80 MM 35-20-00. (M)

Part: SLIDE — FAILED (TAILCONE)

FTW - TAILCONE DOOR SLIDE DEPLOYMENT SYSTEM FAIL TEST ESCAPE SLIDE, BECAME UNPACKED DURING TEST. REMOVED TAIL SLIDE IAW MD80 MM 25-61-00. INSTALLED SLIDE IAW MD80 MM 25-62-01 PERFORMED OPERATIONAL CHECK TAIL CONE SLIDE DEPLOYMENT SYSTEM PER SPIRIT AIRLINES TASK CARD 05-R-00079, ALL CHECKS NORMAL. (M)

Part: FLOORBOARD — CORRODED (COCKPIT)

FTW - FLIGHT COMPARTMENT CAPTAINS SIDE FLOORBOARD CORRODED, UPPER SEAT AREA. REMOVED FLOOR BOARD PER MD80 SRM 51-30-1. FORMED NEW FLOOR PANEL. INSTALLED FLOOR PANEL PER MD80 SRM 51-30-1. (M)

Part: WEB — DAMAGED (NR 1 NOSE COWL)

FTW - NR 1 ENGINE NOSE COWL AFT WEBBING DENTED AND DAMAGED AT 9 O'CLOCK POSITION. CUT DAMAGE AREA PER SRM MD80 54-01. FABRICATED SECTION AND SPLICES TWO PER SRM MD80 54-01. INSTALLED SPLICES AND WEB IAW MD80 SRM 51-30-2 AND 51-30-1. (M)

Part: ATTACH FITTING — BROKEN (FUSELAGE)

FTW - AFT BAGGAGE BAY FS 1231 R28 LONGERON TITANIUM STRIP FOR FLOOR ATTACH, HOLE BROKEN OUT AFT SIDE OF FS 1230 FRAME. INSTALLED REPAIR DOUBLERS IAW MD-80 SRM 51-30-05. (M)

Part: SKIN — DELAMINATED (NOSE COWL)

FTW - NOSE COWL AT 6 O'CLOCK POSITION O/B SURFACE HAS DELAMINATION. REMOVED DAMAGED PLIES OF CARBON SKIN IAW DC9/MD80 SRM 51-90-0. REPAIRED DELAMINATION AREA IN NOSE COWL AT 6 O'CLOCK POSITION IAW DC9 MD80 SRM 51-90-0. (M)

Part: LATCH — FAILED (CABIN)

FTW - OXYGEN MASK AT AFT INOPERATIVE CEILING PANEL DO NOT PASS TEST ON AUTO AND MANUAL MODES. REMOVED BAD LATCH AND INSTALLED NEW ONE IAW MD80 MM 35-21-01. OPS CHECK GOOD IAW MD80 MM 35-20-00. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - AFT LOWER CARGO COMP, AFT CORNER CUTOUT DOOR AS MARKED. CORROSION FOUND ON LT SUPPORT. INSTALLED SUPPORT PER SRM MD-80 51-10-5. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - SUPPORT ANGLE STATION 1155 BETWEEN LONGERON 27R AND 28R ATTACHED TO SKIN CORRODED. REMOVED SUPPORT ANGLE IAW MD-80 SRM 51-10-04. LOCATED AND DRILLED NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE AT STATION 1155 BETWEEN LONGERON 27R AND 28R. (M)

Part: COMPUTER — FAULTY (NR 2)

FTW - NR 2 DFGC P/N 4034241-971, S/N 88081643 WILL NOT ALLOW AUTO PILOT TO ENGAGE. ALSO, NR 2 FLIGHT DIRECTOR FLAG IN VIEW. REMOVED NR 2 DFGC IAW MD80 MM 22-01-01. INSTALLED NR 2 DFGC IAW MD80 MM 22-01-01. (M)

Part: SKIN — CORRODED (FUSELAGE)

FTW - RIGHT WING TO BODY FAIRING RUB STRIP HAS CORROSION. REMOVED CORROSION PER MD80 SRM 51-10-3 AT RIGHT SKIN FUSELAGE FROM STATION Y 745 TO STA Y 815 BETWEEN LONGERON 29, 28 RIGHT. FOUND BLENDED AREA TO BE OUT OF LIMITS PER SRM MD80 53-01. FABRICATED AND INSTALLED DOUBLERS IAW MD80 SRM 51-30-5. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - FORWARD LOWER CARGO COMP, FORWARD SIDE OF LOWER DOOR JAMB CORRODED AT STATION 370 TO STATION 427. INBOARD FACE OF AREA FOUND TO BE OUT OF LIMITS IAW MD-80 SRM 53-01-00. CUT OUT DAMAGE SECTION OF PAN. INSTALLED ANGLES REPAIR AT FORWARD AND AFT SECTION PER SRM MD-80 53-05. (M)

Part: ACOUSTIC PANEL — SEPARATED (NR 2 COWLING)

FTW - NR 2 ENGINE AT 3:00 POSITION LE OF ACOUSTICAL PANEL SEPARATED 1.4 INCHES SPAN INLET COWL. REPAIR ACOUSTICAL PANEL PER MD80 SRM WITH EA 934 IAW MD80 SRM 54-04. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - AFT LOWER CARGO COMPARTMENT FORWARD SIDE OF LOWER DOOR CORRODED FROM STATION 1155 TO 1212 AS MARKED. CORRODED OUT OF LIMITS AT LOWER CARGO DOOR JAMB. REMOVED CARGO DOOR JAMB BEAM. LOCATED AND DRILLED HOLES CARGO DOOR JAMB BEAM. INSTALLED LOWER CARGO COMP JAMB BEAM PER SRM MD-80 SRM 51-30-05. (M)

Part: STIFFENER — CORRODED (AFT AIRSTAIRS)

FTW - AFT AIRSTAIRS, LEFT SIDE WALL DOUBLER CORRODED BETWEEN STEP SIDE WALL AND DOUBLER. REMOVED DOUBLER (STIFFENER) IAW MD80 SRM 51-30-2, ALL ITEMS ARE ON W/O 500013-11-N-00005. (M)

Part: HINGE — CORRODED (AFT AIRSTAIRS)

FTW - AFT AIRSTAIRS, CORROSION LOWER HINGE AREAS, BOTH RIGHT AND LEFT SIDES. REMOVED CORROSION ON LOWER HINGE (LEFT) AREA IAW MD80 SRM 51-10-3, REF WO 500013-11-N-00009. (M)

Part: SPLICE — CORRODED (FUSELAGE)

FTW - CENTER LOWER CARGO COMPARTMENT, L30 DOUBLER HAS CORRODED HIGH LOCK THROUGH THE HOLES AS MARKED. REMOVED CORRODED FASTENERS ON SPLICE. SPLICE OUT OF LIMITS. DUPLICATED SPLICE PER BOEING DC-9/MD-80 SRM 53-14-2. INSTALLED FWD SPLICE IAW MD-80 SRM 51-30-05. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND CENTER LOWER CARGO COMPARTMENT LONGERON 30, AT STATION 636 TO STATION 617 HAS CORROSION AS MARKED. REMOVED LONGERON SECTION. FABRICATED AND INSTALLED LONGERON IAW MD-80 51-30-5. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

FTW - FOUND LOWER COMPARTMENT CARGO DOOR CUTOUTS FROM STATION 1155 THROUGH 1212 CORRODED. REMOVED CORROSION, REF N/R 18-N-00027. (M)

Part: RETAINER — CRACKED (COCKPIT WINDOW)

FTW - FOUND COCKPIT OVERHEAD WINDOW OUTER RETAINER CRACKED. REMOVED UPPER WINDOW OUTER RETAINER. LOCATE AND DRILL NEW RETAINER WINDOW. INSTALLED RETAINER WINDOW. INSTALLED EXTERNAL DOUBLER IAW MD80 SERVICE BULLETIN 56-11-R3. (M)

Part: SKIN — CRACKED (FUSELAGE)

FTW - FOUND FUSELAGE STA Y160 LEFT FUSELAGE FORWARD FORWARD AIR STAIR CUT OUT FORWARD LOWER, CORNER HAS A CRACK. REMOVED DAMAGE AREA IN LOWER FORWARD CORNER IAW MD80 SRM 53-05. UPON REMOVAL OF PREVIOUS REPAIR FORWARD AIRSTAIR AFT LOWER CORNER FOUND ONE CRACK IN FUSELAGE SKIN BETWEEN FASTENERS. REMOVED DAMAGE ON AFT CORNER OF FUSELAGE SKIN IAW MD80 SRM 53-05. UPON REMOVAL OF DAMAGE AT AFT LOWER CORNER (FWD STAIRWELL CUT OUT) FOUND CRACK ON INNER DOUBLER. FABRICATED NEW DOUBLER FOR UPPER DOOR HINGE FOR FORWARD AIRSTAIR. INSTALLED FORWARD AND AFT SHIMS AND DOUBLERS. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - DENT IN FUSELAGE AFT OF ENTRANCE DOOR AT LONGERON 16-17 AND STATION 237. CUT OUT DAMAGE AREA AT FUSELAGE AFT ON ENTRANCE DOOR AT LONGERON 16-17. LOCATED AND DRILLED FINGER DOUBLER AND SKIN PLUG IAW MD80 SRM 51-10-04. INSTALLED REPAIR PARTS AT FUSELAGE AFT OF ENTRANCE DOOR AT LONGERON 16-17 AND STATION 237 IAW MD80 SRM 53-04. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND DENT AT STATION 224 BETWEEN LONGERON 18 AND 17R. FABRICATED REPAIR PARTS IAW MD80 SRM 53-04. INSTALLED REPAIR PARTS AT STATION 224 BETWEEN LONGERON 18 AND 17R IAW MD80 SRM 53-04. (M)

Part: GROUND WIRE — DIRTY (CABIN)

L2 SERVICE DOOR OVERHEAD DROP CEILING LIGHT (EMERGENCY OR STANDBY) INOPERATIVE. CLEANED AC GROUND AND DC GROUND AT LIGHT FIXTURE. RECONNECTED GROUND WIRE TO STUD IAW MD80 MM 23-50-01. (M)

Part: STARTER — FAULTY (LT ENGINE)

ORD - ABORTED START ON LEFT ENGINE MAX, EGT 500 DEGREE TEMP RISE WAS VERY RAPID BEFORE ABORT, MAX N2 BEFORE FUEL WAS PLACED ON 20 PERCENT PNEUMATIC PRESS -40 PSI NORMAL FUEL FLOW. REMOVED AND REPLACED LEFT ENGINE STARTER AND START VALVE, ENGINE RUN CHECKS GOOD WITH NORMAL PARAMETERS IAW MM 80-00-00. (M)

Part: APU — LACK OF LUBE (APU BAY)

ACY - FLT 1143 - APPROX 3 MINUTES AFTER STARTING APU INFLIGHT, APU OIL TEMP HIGH LIGHT CAME ON. PERFORMED QRH PROCEDURES VRF. DIVERTED TO ACY, NO OVERWEIGHT LANDING. SERVICED APU OIL IAW 12-12-01. SYSTEM OPS CHECK GOOD PER MM. (M)

Part: SLIDE — OUT OF POSITION (L2 DOOR)

MCO - FLT 1599 - FOUND SLIDE PACK FELL OFF L2 DOOR. RE-INSTALLED L2 SLIDE PACK PER MM 25-62-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FOUND EMERGENCY PATH LIGHTING NOT WORKING FROM SEAT ROW 28 AFT. REMOVED AND REPLACED BAD BATTERY PACK FOR EMERGENCY PATH LIGHTS, FLOOR ROW 28 AFT. OPS CHECK GOOD IAW MD80 MM 33-21-04. (M)

Part: SLIDE — DISLODGED (GALLEY DOOR)

DTW - AFT GALLEY DOORSLIDE PACK DOOR FELL OFF. RE-INSTALLED AFT GALLEY SLIDE PACK AS PER MD-80 MM 25-62-00. (M)