N821NK

Part: BLADE — FRACTURED (NR 2 ENGINE)

ENGINE WAS REMOVED FROM 821NK NR 2 POSITION FOR VISIBLE TURBINE DAMAGE. INSPECTION REVEALED THE T-4 BLADES MISSING/FRACTURED AT THE BASE OF BLADE WITH CORRESPONDING DAMAGE TO THE T-3 VANES.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 36,831 hrs · 18,330 cycles

AT STA 200, NR 1 SEAT TRACK LT FLOOR WEB HAS A PUNCTURE. CUT OUT PUNCTURE FROM FLOOR WEB STA 200, NR 1 SEAT TRACK. FABRICATE DOUBLERS AND FILLERS. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER IAW SRM. (K)

Part: SLIDE — FAILED (SERVICE DOOR)

AFT SERVICE DOOR EVAC SLIDE DID NOT DEPLOY DURING OPS CHECK, FIRING LANYARD FAILED TO PULL OUT OF FIRING MECHANISM. AFT SERVICE DOOR EVAC SLIDE TO BE REPLACED ON WORK CARD 7809-1-01086/05. (M)

Part: INDICATOR — FAULTY (COCKPIT)

ON APPROACH, RECEIVED NO DOWN AND LOCKED INDICATION (GREEN LIGHT) ON FORWARD PANEL, MECHANICAL PIN ON PEDESTAL WAS EXTENDED, AIRCRAFT TAIL SWAP WITH 818. REMOVED AND REPLACED LANDING GEAR POSITION INDICATORS. OPS HEK NORMAL. (M)

Part: SUPPORT ANGLE — CRACKED (CARGO BAY) · airframe 36,831 hrs · 18,330 cycles

AFT CARGO DOOR FWD UPLOCK SUPPORT ANGLE CRACKED. REMOVED AND FABRICATED NEW ANGLE IAW SRM. TREATED AND PRIMED, INSTALLED SUPPORT ANGLE IAW SRM. (K)

Part: WEB — CORRODED (FUSELAGE)

CABIN STA 180-200, RBL 54, RBL59, SUB FLOOR CORRODED. REMOVED CORROSION AT WEB. MATERIAL LOSS OUT OF LIMITS. REMOVED FWD AIRSTAIR. REMOVED FLOOR SUPPORT RT STA 160 TO 200. CUT OUT DAMAGED AREA AND FABED DOUBLER. PRIMED AND TREATED, INSTALLED FLOOR SUPPORT AND DOUBLER IAW SRM. INSTALLED FWD AIRSTAIR IAW MM. (K)

Part: STRAP — CORRODED (FUSELAGE)

ALUMINUM STRAP ON LOWER SIDE OF L2 DOOR THRESHOLD HAS CORROSION. STRAP CORROSION IS OUT OF LIMITS. FABRICATED NEW STRAP IAW SRM. TREATED AND PRIMED, INSTALLED STRAP ON L2 DOOR THRESHOLD IAW SRM. (K)

Part: DOUBLER — CORRODED (G2 GALLEY)

G-2 GALLEY, CART ENCLOSURE, AFT LOWER LIP AND (2 EA) DOUBLERS ARE CORRODED. REMOVED LOWER LIP AND DOUBLERS, FOUND LIP AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS. TREAT AND PRIMED. INSTALLED LIP CHANNEL AND DOUBLERS IAW SRM. (K)

Part: SUPPORT ANGLE — CORRODED (G2 GALLEY)

G-2 GALLEY, UPPER SECTION, LOWER EDGE AND SUPPORT ANGLE ARE CORRODED. REMOVED CORROSION ON LOWER EDGE AND SUPPORT ANGLE. FOUND SUPPORT ANGLE OUT OF LIMITS FABRICATED SUPPORT ANGLE IAW SRM. PRIMED AND INSTALLED SUPPORT ANGLE. (K)

Part: DOUBLER — CRACKED (HORIZ STAB) · airframe 36,831 hrs · 18,330 cycles

HORIZONTAL STABILIZER, RT SIDE IB UPPER BRACKET SUPPORT HAS CRACK ON DOUBLER. REMOVED CRACKED DOUBLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM. (K)

Part: ANGLE — CRACKED (FUSELAGE)

FTW - MID PIT FORWARD BULKHEAD STATION 522 LEFT LOWER CORNER HAS CRACKED ANGLE. REMOVED CRACKED ANGLE STATION 522. FABRICATED NEW ANGLE IAW SRM 51-10-2. TREATED AND PRIMED, INSTALLED ANGLE AT STATION 522 IAW SRM 51-30-2. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

MID PIT STA 522-636, A LONG 18, RBL 52, FLOOR PANEL UNDER FEDDER CABLES CORRODED. REMOVED CORROSION FROM 522-636, FOUND OUT OF LIMITS. REMOVED WEB STA 503-598, FABED NEW WEB, PRIMED AND TREATED. INSTALLED WEB AT STA 503-598, RBL 52, IAW SRM. (K)

Part: SKIN — DENTED (CARGO DOOR)

DENT ON AFT CARGO DOOR SKIN 21 INCHES FROM AFT EDGE AND 11 INCHES FROM BOTTOM EDGE OF DOOR (X=0.035 INCH, D=1.75 INCH, D/X=50). STRIPPED AREA OF DENT ON AFT CARGO DOOR FS 1185 IS UNDER CONDITION IAW SRM. DYE PENETRANT INSP, NO CRACK FOUND. REMOVED LATCH HANDLE MECHANISM PAN GOUGED BEYOND 50 PERCENT IN CUP. CUT OUT DENT AREA (1.5 INCH DIAMETER) IAW SRM. FAB FILLER AND REPAIR DOUBLER IAW SRM. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER. INSTALLED DOOR PAN HANDLE AND MECHANISM IAW SRM. (K)

Part: STRUCTURE — DENTED (R1 DOOR)

DENT ON R1 DOOR FS 199 ONE INCH FROM AFT EDGE AND 13 INCHES FROM BOTTOM EDGE, D=.3, X=0.018 INCH, D/X=16/6. REMEASURED DENT AT R1 DOOR (D=0.3, X=.026 D/X 11.5). CUTOUT DAMAGED (DENTED) AREA. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER ON AFT R1 DOOR IAW SRM 51--30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

DENT ON FUSELAGE SKIN FS421 BETWEEN LONGERONS 19R AND 20R (D=0.5 INCH, X=0.008 INCH, D/X - 62.5 INCHES). REMOVED CARGO DOOR TO FOM IAW SRM. FOUND DENT HAS GOUGED IN CENTER, REMOVED DAMAGED AREA OF SKIN (1.5 INCH X 0.8 INCH) IAW SRM. FABRICATED DOUBLER AND FILLER IAW SRM. TREATED AND PRIMED, INSTALLED REPAIRED PARTS IAW SRM. INSTALLED FWD CARGO DOOR IAW SRM. INSTALLED FWD PIT BARRIER DOOR IAW SRM. LEAK AND FAIR CHECK IAW MM. (K)

Part: FAIRING — CRACKED (LT ELEVATOR)

LEFT ELEVATOR FAIRING EDGE CRACKED STATION XE 171. TRIMMED LEFT ELEV FAIRING EDGE AT STATION XE 171. MATERIAL LOSS WITHIN LIMITS. TREAT AND PRIMED IAW SRM 51-10-3. (M)

Part: SEAT TRACK — CRACKED (FUSELAGE)

RT OB SEAT TRACK HAS AREA OF CORROSION AT FS 229. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK. FOUND WEB OB OF SEAT TRACK FS 218 CRACKED, FABED DOUBLER AND FILLER IAW SRM. PRIMED AND TREATED. INSTALLED DOUBLER, FILLER AND SEAT TRACK IAW SRM. (K)

Part: STIFFENER — CRACKED (FUSELAGE)

FS 190 RBL 34 FLOOR WEB STIFFENER IS CRACKED. REMOVED DAMAGE STIFFENER, FOUND OUT OF LIMITS. FABRICATE NEW STIFFENER IAW SRM 51-10-2 AND 51-10-4. TREAT AND PRIMED, INSTALLED STIFFENER IAW 51-30-2. (M)

Part: FAIRING — GOUGED (VERTICAL STAB)

VERT STAB TIP FAIRING HAVE SCRATCHED/GOUGED ON BOTH SIDE. BLENDED DAMAGED AREA AT VERT STAB MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER IAW SRM 55-01 FIG 4. TREATED AND PRIMED, INSTALLED FILLER AND DOUBLER IAW SRM 51-30-2. (M)

Part: SUPPORT BRACKET — CRACKED (BARRIER DOOR)

FTW - MID PIT BARRIER DOOR AFT SKIN SUPPORT BRACKET CRACKED TWO PLACES. REMOVED AND REPLACED MID PIT BARRIER DOOR IAW SRM 51-30-1 AND 51-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT ON FUSELAGE SKIN FS 421 BETWEEN LONGERONS 19R AND 20R, D=.5, X=.008, D/X=62.5. REMOVED FORWARD CARGO DOOR TO FOM. REMOVED DAMAGED AREA OF SKIN 1.5 INCH BY .8 INCH. FABRICATED DOUBLER AND FILLER IAW 53-04. TREATED AND PRIMED, INSTALLED REPAIR DOUBLERS AND FILLERS IAW SRM 53-05. INSTALLED FORWARD CARGO DOOR PER MM 52-31-00. DOOR WARNING CHECK GOOD IAW MM 53-70-00. (M)

Part: SKIN — GOUGED (FUSELAGE)

FTW - GOUGE ON FUSELAGE SKIN FS 497 BETWEEN LONGERONS 20R AND 21R. BLEND OUT GOUGE FUSELAGE SKIN FS 497. AFTER BLENDED OUT LIFT .036 FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA. FABRICATED SKIN PLUG AND FINGER DOUBLER. TREATED AND PRIMED SKIN PLUG AND FINGER DOUBLER. INSTALLED INTERNAL DOUBLER AND FILLER IAW SRM 53-04. (M)

Part: SKIN — DENTED (CARGO DOOR)

DENT ON AFT CARGO DOOR FS 1183 22.5 INCH FROM TOP EDGE AND 26 INCHES FROM AFT EDGE OF DOOR, D=1 INCH, X=.016 INCH, D/X=62. DENT ON AFT CARGO DOOR FS 1183 UNDER CONDITION 1B IS ACCEPTABLE. DYE PENETRANT INSPECTION AFT CARGO DOOR FS 1183. CUTOUT DAMAGED SECTION. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER IAW SRM 52-05 FIG 1 AND 51-30-2. (M)

Part: STRUCTURE — WORN (CATWALK)

AFT AIRSTAIRS STATION 1370 AT FLOOR LINE HAS A HOLE WORN IN IT FROM THE CATWALK ON LEFT SIDE. TRIMMED OUT DAMAGED SECTION AT FLOOR LINE LEFT SIDE AT STATION 1370. FABRICATED REPAIR DOUBLER AND HEAT TREATED. TREATED AND PRIMED. INSTALLED DOUBLER IAW 51-70-4. (M)

Part: SUPPORT — DAMAGED (FUSELAGE)

FORWARD PIT CEILING, STATION 484 RBL 34, BUSTED NUT PLATE AND DAMAGED STRUCTURE SUPPORT. REMOVED AND REPAIRED DAMAGED SUPPORT IAW SRM 53-01. TREATED AND PRIMED, INSTALLED DOUBLER AND SUPPORT IAW 51-30-2. (M)

Part: STRUCTURE — CRACKED (CATWALK)

CATWALK SIDE FILLER STTION 1361 LEFT AND RIGHT IS CRACKED IN RADIUS. STOP DRILLED CRACKS ON CAT WALK STATION 1361 LEFT AND RIGHT. FABRICATED TWO REPAIR DOUBLER LEFT AND RIGHT WEB REPAIR. TREATED AND PRIMED, INSTALLED TWO REPAIR ON CATWALK STATION 1361 LEFT AND RIGHT IAW SRM 51-70-4 AND 51-30-2. (M)

Part: STRUCTURE — CRACKED (CATWALK)

CATWALK SIDE FILLER STATION 1510 IS CRACKED ON RIGHT SIDE. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM 51-30-2. (M)

Part: STRIP — CRACKED (FUSELAGE)

FTW - MID PIT LEFT SIDE STATION 541, UPPER SIDEWALL SUPPORT STRIP CRACKED. REPAIRED DAMAGED AREA IAW SRM 53-05 PG 137. FABRICATED DOUBLER, TREATED AND PRIMED. INSTALLED DOUBLER IAW SRM 51-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

DENT AT FS 1304 BETWEEN LONGERONS 18R AND 19R, D=1 INCH BY .020 INCH D/X=50, CONDITION 1B. INSPECTED FOUND FURTHER DAMAGE IN DENT (GOUGE) REQUIRING REPAIR. CUT OUT DAMAGE SKIN SECTION (2.10 DIAMETER). FABRICATED SKIN FILLER AND INTERNAL DOUBLER IAW SRM 53-04 FIG 38 SHT 23. TREATED AND PRIMED, INSTALLED SKIN FILLER AND INTERNAL DOUBLER IAW SRM 53-04 FIG 38. (M)

Part: FRAME — CRACKED (RT WING)

FROM C/O 0155770 RT WING L/E 2 EA FORMERS ST APPROX STA 351 CRACKED. FABRICATED DOUBLER IAW SRM. HEAT TREATED 2 EA DOUBLER IAW SRM. TREATED AND PRIMED INSTALLED REPAIR DOUBLER IAW SRM. LP NR 01476783. (K)

Part: ATTACH ANGLE — CRACKED (FWD AIRSTAIRS)

FORWARD AIRSTAIR UPPER ATTACH ANGLE ON SHROUD IS CRACKED AND DAMAGED. REMOVED ANGLE FROM FORWARD AIRSTAIR SHROUD. FABRICATE NEW ANGLE. TREATED AND PRIMED, INSTALLED ANGLE IAW SRM 51-30-1. (M)

Part: SKIN — DENTED (CARGO DOOR)

DENT AT FS 1174 BETWEEN LONGERON 21R AND 22R ON AFT CARGO DOOR, D=1.5, X=0.035, D/X=42.85, CONDITION 1B. REMOVED 2 INCH ROUND CUT OUT DAMAGED AREA OF DOOR. FABRICATED FILLER AND DOUBLER FOR AFT CARGO DOOR STATION 1174 BETWEEN L21R AND 22R IAW SRM 51-10-4 AND 52-05. TREATED AND PRIMED DOUBLER. INSTALLED DOUBLER AND FILLER ON AFT CARGO DOOR STATION 1174 BETWEEN 21R=22R IAW SRM 52-05 AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT, STA 1174, LBL 12, MAIN CABIN FLOORBEAM UPPER FLOOR SUPPORT ANGLE IS CORRODED (EXFOLIATION). REMOVED DAMAGED FLOORBEAM AND FOUND OUT OF LIMITS. FABRICATED NEW SUPPORT ANGLE, PRIMED AND TREATED. INSTALLED FLOOR SUPPORT ANGLE IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT, STA 1309. CABIN FLOORBEAM IS CORRODED (EXFOLIATION) AT RBL 20. FOUND LWR AFT ANGLE SUPPORT CRACKED. CORROSION FOUND TO BE ALL THE WAY THROUGH FLOORBEAM AND IS OUT OF LIMITS. DETENTIONED CABLE RUNS, DISCONNECTED 2 HYD LINES AND POT. WATER AND HEATING ELEMENT. FABED SUPPORT ANGLE, PRIMED AND TREATED IAW SRM.. FABED FLOORBEAM CUT OUT SECTION, PRIMED AND TREATED IAW SRM. FABED REPAIR DOUBLERS AND FILLERS, PRIMED AND TREATED. REINSTALLED POT. WATER, HYD LINES, PULLEY BRACKETS AND RE-TENSIONED CABLE RUNS IAW MM. (K)

Part: LINE — LOOSE (LT ENGINE PT2)

DTW - FLT 689 - ON TAKEOFF ROLL, AUTO THROTTLES ON SETTING NORMAL POWER LEFT ENGINE EPR 1.70 ONLY WHILE N1 WENT OT 103 PERCENT, EGT WAS 500 DEGREES, ABORTED TAKEOFF, AIRCRAFT SWAP. FOUND PT2 LINE IN NOSE BULLET CONNECTIONS ON BOTH ENDS LOOSE, TIGHTENED LINES, OPS CHECK GOOD. (M)

Part: ENGINE — BIRD INGESTION (NR 2)

LP NR 0252843; MULTIPLE BIRD STRIKES ON APPROACH TO LGA, NR 2 LT EGT HIGH. REMOVED AND REPLACED NR 2 ENGINE.

Part: GYRO — INACCURATE (COCKPIT)

HEADING LIGHT ON IN FLIGHT 6 FT-8 FT OFF. REPLACED NR 1 DG AND SWITCHING UNIT.

Part: SLIDE — OUT OF LIMITS (R1 DOOR)

FOUND R1 DOOR EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVACUATION SLIDE. (M)

Part: STRUT — DISCHARGED (NLG)

RED NOSE UNSAFE LIGHT ON W GEAR HANDLE UP. SERVICED NOSE STRUT. LUBED NOSE GEAR. INSPECTED NOSE GEAR LINKAGE AND DOORS. (M)

Part: STRUT — OUT OF ADJUST (NLG)

AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT AND DOORS WOULD NOT CLOSE. RETURNED TO MYR. SERVICED AND ADJUSTED NOSE GEAR STRUT, JACKED NOSE OF A/C AND RETRACTED AND EXTENDED NOSE GEAR 4 TIMES WITHOUT ANY DEFECTS NOTED. (M)

Part: HOLDER — OUT OF ADJUST (GIRT BAR)

AFT GALLEY GIRT BAR NOT WORKING PROPERLY 'HOLDER'. ADJUSTED GIRT BAR HOLDER, OPS CHECK NORMAL. GTIA (M)

Part: LANYARD — DISLODGED (L1 DOOR SLIDE)

TPA - FLT 486 - L1 DOOR EMERGENCY SLIDE LANYARD OUT. RE-INSTALLED LANYARD. (M)

Part: FRAME — CRACKED (RT WING)

DTW - FOUND 2 RIGHT WING LEADING EDGE FORMERS AT APPROX STATION 351 CRACKED. (M)

Part: LANYARD — LOOSE (ESCAPE SLIDE)

DTW - FLT 565 - L2 DOOR SLIDE COVER LANYARD CAME OUT. REINSERTED L2 DOOR SLIDE COVER LANYARD. OPS CHECK GOOD. (M)

Part: WEB — CRACKED (FUSELAGE)

FOUND FORWARD CABIN CRACKED/DAMAGED ON WEB STATION 180 RBL 24 TO 30. REMOVED DAMAGED WEB AREA. FABRICATED NEW WEB AND SPLICE. INSTALLED WEB AND SPLICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 200 RBL 10 TO 44 FLOOR SUPPORT CORRODED. FABRICATED, LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 180 RBL 10 TO 44 INCHES FLOOR SUPPORT CORRODED. LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: STRUCTURE — CRACKED (SUB FLOOR)

SUBFLOOR HAS 1 INCH DIAMETER CRACK AT STATION 150 RBL 30. CUTOUT DAMAGED AREA, FABRICATED DOUBLER REPAIR. INSTALLED DOUBLER. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 218 TO 236 LBL 44 INCHES TO 54 INCHES CRACK FORWARD SIDE CORNER WEB. REMOVED DAMAGED SECTION OF WEB. FABRICATED REPAIR. INSTALLED REPAIR. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CORROSION ON L1 DOOR WEB, STATION 200 LOWER FORWARD CORNER LBL 54. REMOVED APPROX 8 INCHES FROM LOWER L1 DOOR WEB. FABRICATED L1 DOOR REPAIR. INSTALL REPAIR ON L1 DOOR WEB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 185 TO 195 LBL 52 INCHES FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD CABIN STATION 160 TO STATION 200 LBL 54 INCHES CORRODED AT THE FLOOR SUPPORT. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT STATION 160 TO 200 RBL 48 CORRODED. FLOOR GALLEY MOUNT CORRODED AT STATION 160 RBL 48. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT AT STATION 160 LBL 4 TO RBL 4 IS CORRODED. FABRICATED NEW FLOOR SUPPORT. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

CABIN FLOORBOARD DELAMINATED AND NUMEROUS INSERTS CORRODED. FABRICATED NEW FLOOR PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FORWARD CABIN SUBFLOOR CORRODED AT FLOOR SUPPORT LBL 9 STAITON 160 TO 200 AND HAS A PINHOLE FROM SCREW STATION 168. CUTOUT FLOOR WEB. FABRICATED NEW WEB. FABRICATED SPLICE. INSTALLED FLOOR WEB. INSTALLED SPLICE REPAIR. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - AFT CARGO COMPARTMENTS AT STATIN 1218, LONGERON 18R, SUB FLOOR WEB IS CORRODED. SUB FLOOR WEB. DRILLED AND LOCATED SPLICE AND ODUBLER. INSTALLED WEB SPLICE/DOUBLER. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FOUND CABIN FLOORBOARD STATION 617-674 STIFFENER DELAMINATED FROM BOTTOM. RESEALED DISBONDED STRIPS. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN FLOOR SUPPORT STATION 197 LBL 8 TO LBL 40 CORRODED. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN FLOOR SUPPORT RBL 6 STATION 168.75 TO 205 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD CABIN FLOOR SUPPORT LBL 6 STATION 168.75 TO 205 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN FLOOR SUPPORT LBL 10 STATION 197 TO 256 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FTW - FOUND RIGHT AFT LAVATORY FLOORBOARD DELAMINATED. FABRICATED NEW FLOORBOARD. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FOUND MID PIT FS 630 STRINGER 28R INTERCOSTAL CORRODED. FABRICATED NEW T-ANGLE. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

FTW - FOUND MID PIT FS 635 STRINGER 29R DOVE TAIL CORRODED. FABRICATED DOVE TAIL SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD CABIN FLOOR SUPPORT STATION 200 RBL 6 TO LBL 22 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FTW - FOUND FORWARD LAV INBOARD SECTION FLOOR PANEL DELAMINATED AND CORRODED AROUND EDGES. REPAIRED DELAMINATION. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SUPPORT CORRODED FS 160-190 LBL 7 INCHES. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: STOP FITTING — CORRODED (AFT DOOR)

FTW - FOUND AFT VAULT DOOR LOWER STOPS CORRODED. REMOFED TWO EACH DOOR STOPS. INSTALLED NEW STOPS. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD FS 160-200 LBL 24 INCHES DELAMINATED AND CORRODED INSERTS AND FASTENERS. REMOVED FLOORBOARD. FABRICATED NEW PANEL INSTALLED NEW FLOORBOARD. (M)

Part: PAN — CRACKED (CARGO DOOR)

FTW - AFT CARGO DOOR, UPON REMOVAL OF BRACKET FOUND CRACK IN RADIUS OF CARGO DOORS PAN AT LOWER FORWARD CORNER. STOP DRILLED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FOUND MID PIT STATION 636-655 STRINGER 30-29L CORROSION AT FASTENERS. REMOVED LONGERON 30 FROM STATION 588 TO 665. FABRICATED NEW LONGERON SECTION. INSTALLED NEW LONGERON. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND FORWARD PIT STATION 450 TO 494 L30, LONGERON FLANGES CORRODED ON UPPER AND LOWER SURFACES. REMOVED 01 LONGERON 30 BETWEEN STATION 475 FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW LONGERON 30. INSTALLED NEW LONGERON 30. FABRICATED NEW LONGERON SPLICE FOR STATION 415 PER SPIRIT AIRLINES EA 5310-0317. INSTALLED NEW SPLICE. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - MID PIT STATION 769-775 STRINGER 30 CORRODED AND FASTENERS CORRODED. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FOUND MID PIT STATION 655 674 STRINGER 30 CORROSION AT FASTENERS. FABRICATED NEW LONGERON SECTION FROM STATION 665 TO STATION 798. FABRICATED NEW LONGERON SPLICE. INSTALLED SPLICE. INSTALLED STRINGER 30. (M)

Part: SKIN — CORRODED (FUSELAGE)

FTW - FOUND MID PIT STATION 750 STRINGER 29R-28R CORROSION ON SKIN. CUT SKIN TO FOM SIZE OF SKIN CUTOUT IS 7.5 INCHES BY 11 INCHES. CORROSION REMOVAL WITHIN ALLOWABLE LIMITS. FABRICATED REPAIR PARTS 1 EACH FILLER, 1 EACH DOUBLER, 2 EACH FINGER DOUBLER. INSTALLED FINGER DOUBLER, FILLER, AND REPAIR DOUBLER. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT STATION 1079 STRINGER 28L-28R FRAME CORRODED. REMOVED CORRODED FORMER ANGLE. FABRICATED REPAIR ANGLES. INSTALLED REPAIR ANGLE AND FRAME ANGLE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - AFT PIT STATION 1117 STRINGER 30-29L FRAME SUPPORT CORRODED. FABRICATED ANGLE REPAIR. INSTALLED REPAIR ANGLE. (M)

Part: FRAME — CORRODED (FUSELAGE)

AFT PIT STATION 1022 STRINGER 28L-29L FRAME CORRODED. CUT OUT DAMAGED AREA. FABRICATED REPAIR. INSTALLED REPAIR. (M)

Part: FLOOR PANEL — CORRODED (CARGO BAY)

AFT PIT STATION 1117-1155 STRINGER 18L FLOOR WEB CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: DOOR FRAME — DAMAGED (FUSELAGE)

FTW - FOUND FRAME AT STATION 370 LONGERON 27R HAS DAMAGE FORWARD CARGO DOOR CUTOUT. REMOVED TWO SECTION FRAMES FROM STATION 370 B/N 27L-27R AND B/N 27R-18R. INSTALLED NEW FRAME FROM STRINGER 18R-28L STATION 370. (M)

Part: SPLICE — CORRODED (FUSELAGE)

E/E COMPARTMENT STATION 180 TO STATION 195 CORRODED AT L30 SPLICE. REMOVED CORRODED SPLICE. HOLES LOCATED AND DRILLED. INSTALLED NEW SPLICE. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND MID PIT STATION 636-712 STRINGER 18L FLOOR WEB CORRODED. REMOVED FLOOR WEB FROM LEFT SIDE AT STATION 598-712. LOCATED AND DRILLED NEW WEB. INSTALLED NEW FLOOR WEB. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FTW - FOUND MID PIT STATION 522-563 STRINGER 30 CORROSION AT FASTENERS. (M)

Part: STOP FITTING — CORRODED (CARGO DOOR)

FTW - FOUND FORWARD PIT, DOOR STOPPER CORRODED 4 EACH AS MARKED. REMOVED AND REPLACED 4 EACH FORWARD PIT DOOR STOPS. (M)

Part: STOP FITTING — CORRODED (CARGO DOOR)

FTW - FOUND MID PIT 8 EACH DOOR STOPPER CORRODED AS MARK. REMOVED AND REPLACED 8 EACH MID PIT DOOR STOPPERS. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

FTW - MID PIT STATION 598-610 STRINGER 27L-30 ANTENNA CUTOUT CORRODED. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED NEW ANTENNA DOUBLER. INSTALLED ANTENNA DOUBLER. (M)

Part: PANEL — DELAMINATED (LT WING)

FTW - FOUND LEFT WING UPPER FORWARD TRAP PANEL PAINT CRACK THROUGH OUT TOP COAT AND VISABLE TO COMPOSITE MATERIAL. FOUND LEFT WING UPPER FORWARD TRAP PANEL DELAMINATED. REPAIRED TWO DELAMINATES ON LEFT WING UPPER TRAP PANEL. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - AFT PIT STATION 1287-1309 STRINGER 18R FLOOR PANEL CRACKED. TRIMMED OUT DAMAGED AREA. LOCATED AND DRILLED DOUBLER/FILLERS. INSTALLED DOUBLER/FILLERS. (M)

Part: PANEL — DAMAGED (RT WING)

FTW - FOUND RIGHT WING UPPER TRAPAZOIDAL PANEL HONEYCOMB COMPOSITE DAMGED AND DELAMINATED AT TWO PLACES 34 INCHES OUTBOARD OF FUSELAGE AND 7 INCHES AFT OF PANELS L/E. REMOVED RIGHT WING UPPER TRAPAZOIDAL PANEL. REPAIRED TWO EACH DELAMINATES. INSTALLED RIGHT WING UPPER TRAPAZOIDAL PANEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND AFT PIT CEILING STATION 1338 LBL 49 LAV FLOOR CRACKED. FOUND FLOORBOARD FRAME CORRODED AND OUT OF LIMITS. FABRICATED LEFT AFT LAV FLOORBOARD FRAME. FABRICATED LEFT AFT LAV FLOORBOARD. INSTALLED LEFT AFT LAV FLOORBOARD. (M)

Part: PAINT — CRACKED (LT WING)

FTW - FOUND LEFT WING UPPER TRAILING EDGE TRAP PANEL PAINT CRACKED THROUGH OUT TOP COAT AND VISABLE TO COMPOSITE MATERIAL. REPAIRED DAMAGED AREAS. (M)

Part: BEAM — CORRODED (CARGO DOORWAY)

FTW - MID PIT INBOARD DOOR BEAM CORRODED. REMOVED DOOR BEAM. HOLES LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. (M)

Part: SKIN — CORRODED (FUSELAGE)

FTW - LEFT ALTERNATE STATIC PORT FAILED AERODYNAMIC CLEANLINESS TEST AT 2D, 3C, 41 ON MYLAR OVERLAY. UPON REMOVAL OF STATIC PORT DOUBLER CORROSION WAS FOUND UNDER DOUBLER ON SKIN AND ON FINGER DOUBLER. FABRICATE DOUBLER REPAIR. INSTALLED DOUBLER REPAIR. (M)

Part: PAN — CORRODED (CARGO DOOR)

FTW - FOUND FORWARD CARGO DOOR PAN AND STRAPS CORRODED AND SOME AREAS FORWARD AND AFT EXFOLIATED AT FS 370-427 ALL ALONG BOTTOM. FORMED NEW DOUBLERS. LOCATED AND DRILLED DOOR PAN. INSTALLED FORWARD CARGO PIT DOOR PAN. INSTALLED 4 EACH REPAIR DOUBLERS. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - FOUND MID CARGO DOOR CORRODED JAMB BEAM ALL ALONG BOTTOM AT FS 636-693. REMOVED OUT OF LIMIT DOOR BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED NEW BEAM. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - AFT CARGO JAMB BEAM CORRODED AT FS 1155-1212 ALL ALONG BOTTOM. REMOVED JAMB BEAM. LOCATED AND DRILLED HOLES NEW JAMB BEAM. INSTALLED NEW JAMB BEAM. (M)

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE)

DTW - FOUND RIGHT ENGINE LOOP A LIGHT ON WOULD NOT GO OUT IN FLIGHT. RIGHT ENGINE LOOP REMOVED AND REPLACED LOOP AS REQUIRED, OPS CHECK GOOD. (M)

Part: ISOLATION MOUNT — OUT OF POSITION (ENGINE)

DTW - FOUND FORWARD UPPER ISOLATOR MOUNT ALIGNMENT MARKS SHIFTED. REMOVED AND REPLACED FORWARD UPPER VIBRATION ISOLATOR MOUNT. (M)

Part: ISOLATION MOUNT — OUT OF POSITION (ENGINE)

DTW - FORWARD LOWER ISOLATOR MOUNTS ALIGNMENT MARKS SHIFTED. REMOVED AND REPLACED LOWER VIBRATION ISOLATOR MOUNT. (M)

Part: FIRE LOOP — LOOSE (NR 2 ENGINE)

FLT 594 - MCO - NR 2 ENGINE B-LOOP (FIRE WARN) FLICKERS. FOUND LOOSE GROUND WIRE AT P1-828 AND BAD CONNECTOR AT LOWER BURN THROUGH BARRIER P1-865. CORRECTED DISCREPANCIES. CHECKS GOOD. (M)

Part: CONTROL BOX — LOOSE (LANDING GEAR)

DTW - FLT 503 - DEPART DTW OUT OF 13,500 FEET AT 320 KTS, GEAR HANDLE UP, THERE WAS AN INTERMITTENT GEAR UNSAFE (ALL 3) INDICATION DURING LIGHT TURBULENCE. LIGHT WENT OUT IN SMOOTH AIR. AT 330, IN SMOOTH AIR, AT FL 200 GEAR UNSAFE LIGHTS CAME ON UNTIL FL330 IN SMOOTH AIR CONT UPON LIGHT TURBULENCE LIGHT WOULD COME ON AND OFF. NORMAL GEAR INDICATION UPON LANDING. INSPECTED THROTTLE SWITCHES AND LANDING GEAR LEVER SWITCH FOR SECURITY AND OPERATION. NO DEFECTS NOTED AT THIS TIME. PERFORMED BITE TEST, AFTER RESECURING PROXIMITY CONTROL BOX PER MM 32-60-05. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (TRIM)

MYR - FLT 1751 - PRIMARY TRIM INOPERATIVE, WILL NOT MOVE FORE OR AFT WITH EITHER YOKE MOUNTED CONTROLS OR LONG TRIM HANDLES. REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR PER MD80 MM 27-40-05. OPS CHECK GOOD. (M)