N12536

Part: ISOLATOR — CORRODED (NR 2 ENGINE)

DTW - NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR IS CORRODED AND PLATING IS FLAKING OFF ON INNER CONICAL AREA. REMOVED AND REPLACED NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR (CLOSED 10/15/02). (M)

Part: ODOR — DETECTED (CABIN)

ACY - FLT 276 - FLIGHT ATTENDANTS DETECTED A FAINT ODOR DURING THE INITIAL CLIMB BUT IT DISSIPATED BY LEVEL OFF. COULD NOT DETECT ANY ODOR WITH PACKS ON AND A/C RUNNING, OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (MLG INDICATOR)

FLT 276 - TPA - FOUND RIGHT LANDING GEAR BUTTON INDICATOR LIGHT INOPERATIVE, GREEN LENS. REMOVED AND REPLACED GEAR DOWNLOCK SWITCH ON RIGHT MAIN GEAR AND OPS CHECKED IAW MM 32-60-01. OPS CHECK NORMAL. CLOSED AS OF 8/28/02. (M)

Part: STRUCTURE — DAMAGED (TE FLAPS)

DTW - FOUND RIGHT FLAP TRAILING EDGE SPLICE APPROX 1.5 INCHES INBOARD END OF FLAP AT FIRST EXPANSION JOINT. SANDED AND INSTALLED FIBERGLASS LAYUP REPAIR ON RIGHT FLAP TRAILING EDGE. (M)

Part: SERVO — FAULTY (AUTOPILOT SYS)

TPA - FLT 276 - AUTO PILOT AILERON SERVO IS ERRATIC IN ALL REQUIRES OF FLIGHT 276. REMOVED AND REPLACED SERVO AUTO DRIVE. OPS CHECK OK. BITE CHECK FOR SERVO PORTION OF CHECK ON ROLL COMP. NO DEFECTS NOTED. (M)

Part: MOTOR — MALFUNCTIONED (HORIZ STAB)

ACY - PRIMARY TRIM HESITATES NOSE UP DIRECTION OCCURS USING BOTH CAPTAINS OR F/O'S YOKE SWITCHES AND USING SUIT CASE HANDLES. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPERATIONAL CHECKS GOOD. (M)

Part: UPLOCK SWITCH — FAULTY (LT MLG)

FLT 8019 - DTW - PUT GEAR UP, LEFT GEAR UNSAFE LIGHT CAM ON, UP LATCH CHECK RED LIGHT STAYED ON AND GEAR DOOR LIGHT (AMBER) CAME ON COMPLETED QRH PROCEDURE. REPLACED LT MLG UPLOCK SWITCH AND LT MLG DOOR SWITCH. VERIFIED LANDING GEAR RIGGING. NO DEFECTS. LUBED LT MLG. INSPECTION LT MLG BUMPER CLEARANCES. CHECKED UPLATCH HOOK AND ROLLER. ALL SATISFACTORY ON GEAR SWING. (M)

Part: CONTROL VALVE — MALFUNCTIONED (LT MLG)

DTW - FLT 9536 - LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RECYCLED GEAR. UPLATCH CHECK GEAR DOOR OPEN LIGHT ILLUMINATED. REPLACED LANDING GEAR CONTROL VALVE AND ADJUSTED LEFT GEAR DOOR LATCH MECH. PERFORMED GEAR SWING. ALL SATISFACTORY AND LEAK CHECK GOOD. (M)

Part: LATCH — OUT OF ADJUST (LT MLG DOOR)

DTW - FLT 9536 - FOUND LEFT LANDING GEAR UNSAFE LIGHT AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. GEAR RECYCLED IAW QRH SAME INDICATIONS. FOUND LEFT MAIN GEAR DOOR LATCH MECHANISM ASSEMBLY OUT OF ADJUSTMENT. ADJUSTED AND PERFORMED TEST IAW DC-9. OPS CHECKS GOOD. (M)

Part: ADC — FAULTY (E/E BAY)

FLT 616 - ACY - AUTO PILOT PITCH CONTROL PORPOISES DURING CLIMB AND DESCENTS AND WILL NOT HOLD ALTITUDE ALL OTHER FUNCTIONS OK FLT 616. REMOVED AND REPLACED AIR DATA COMPUTER PERFORMED PITOT STATIC LEAK CHECK. GROUND CHECK OK AT THIS TIME. (M)

Part: CONTROLLER — FAULTY (AUTOPILOT SYS)

ACY - FLT 8012 - A/P WILL NOT STAY ENGAGED. REMOVED AND REPLACED AUTOMATIC PILOT CONTROLLER. OPERATIONAL CHECK NORMAL IAW DC9 MM 22-10-2. (M)

Part: COMPUTER — MALFUNCTIONED (PITCH AXIS)

FLT 8011 - ACY - ON STABILIZED DESCENT AUTOPILOT SUDDENLY PITCHED DOWN THEN PITCHED UP. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 27-13-1, OPS CHECK NORMAL. (M)

Part: WEB — CRACKED (NR 1 PYLON)

FTW - NR 1 ENGINE PYLON LOWER SURFACE AFT HINGE PANEL OUTBOARD LOWER WEB CRACKED AT ANGLE. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. REMOVED DAMAGED SECTION OF ANGLE. FABRICATED REPAIR ANGLE AND DOUBLERS. INSTALLED REPAIR ANGLE AND DOUBLERS IAW DC9 SRM 51-30-2. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM, OPS CHECK GOOD PER DC9 MM 33-53-01. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM. OPS CHECK GOOD PER MM 33-53-01. (M)

Part: OXYGEN MASK — MALFUNCTIONED (CABIN)

FTW - FOUND OXYGEN MASK DID NOT DROP IN AUTO. PERFORMED TROUBLE SHOOTING AND FOUND OXYGEN LEAK ON OXYGEN LINES. INSTALLED PROPERLY OXYGEN LINES. OPS CHECK GOOD IAW DC9 MM 35-20-0. (M)

Part: RIB — CRACKED (RT WING SLAT)

FTW - FOUND RIGHT WING NR 4 SLAT 8TH INNER RIB FROM OUTBOARD END OF SLAT IS CRACKED. REMOVED RIB. FABRICATED NEW RIB. INSTALLED NEW RIB IAW DC9 SRM 51-30-2. (M)

Part: PANEL — WARPED (SPOILERS)

FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER WARP. REMOVED RIGHT INBOARD SPOILER PANEL. INSTALLED RIGHT INBOARD SPOILER PANEL IAW MM DC9 27-61-1. (M)

Part: DOUBLER — CRACKED (NR 2 COWLING)

FTW - NR 2 ENGINE NOSE COWL 2ND INTERNAL RIB (FROM AFT) 6 O'CLOCK POSITION REPAIR DOUBLER CRACKED. REMOVED DOUBLER REPAIR CRACKED. FORMED NEW SPLICE DOUBLER, INSTALLED NEW REPAIR IAW DC9 SRM 51-30-5. (M)

Part: WEB — CRACKED (RT NOSE COWL)

FTW - RIGHT NOSE COWL INBOARD AREA AT 6 O'CLOCK POSITION DOUBLER CRACKED. REMOVED CRACKED DOUBLER. AFTER FURTHER EVALUATION FOUND WEB ALSO CRACKED. CUT DAMAGED AREA (ON WEB). FABRICATED DRILLED AND LOCATED REPAIR PARTS FILLED DOUBLER. INSTALLED REPAIR PARTS PE SRM DC9 51-30-2. (M)

Part: SPLICE — CORRODED (LT WING SPAR)

FTW - FOUND LEFT WING LEADING EDGE UPPER FRONT SPAR PREVIOUS REPAIR HAS CORROSION FROM XFS 550-XFS 77. REMOVED CORROSION. SPLICE PLATE FOUND TO BE OUT OF LIMITS. FABRICATED SPLICE PLATE. INSTALLED SPLICE PLATE IAW MD80 SRM 51-30-5. (M)

Part: CHANNEL — CRACKED (FLOOR PANEL)

FTW - FOUND FORWARD ENTRY FLOOR PANEL HAT CHANNEL HAS CRACKED. REMOVED CRACKED CHANNEL. FABRICATED CHANNEL. INSTALLED CHANNEL IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (COCKPIT)

FTW - CO-PILOT FLOORBOARD DAMAGED AT UPPER FACE. PUNCTURE AT STATION Y=150. REMOVED DAMAGED AREA. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER PER DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND FLOORBOARD WEB HAS HOLE Y211-X27. REMOVED DAMAGE. FABRICATED REPAIR PARTS FILLER AND DOUBLER. INSTALLED PER DC9 SRM 53-01. (M)

Part: ANGLE — CHAFED (L/E SLAT)

NR 4 SLAT RIGHT CHORD ANGLE CHAFFED MORE THAN 50 PERCENT THICKNESS OF MATERIAL. REMOVED CHAFFED ANGLE. FABRICATED NEW CHORD ANGLE. INSTALLED NEW CHORD ANGLE IAW DC9 SRM 51-30-2. (M)

Part: ANGLE — CHAFED (L/E SLAT)

FTW - FOUND NR 3 RIGHT SLAT OUTBOARD LOWER CHORD ANGLE CHAFFED MORE THAN 50 PERCENT OF MATERIAL THICKNESS. FORMED NEW CHORD ANGLE. INSTALLED FASTENERS IAW DC9 SRM 51-30-2. (M)

Part: RETAINER — CRACKED (CARGO DOOR)

FORWARD CARGO DOOR HAS TWO CRACKS AT RETAINER MOUNT HOLE 2 INCHES BELOW UPPER AFT CORNER. FABRICATED REPAIR DOUBLERS. INSTALLED DOUBLERS IAW DC9 SRM 52-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y=200 FROM -X47 INCHES TO -X=56 INCHES. REMOVED SUPPORT ANGLE. FORMED NEW FLOOR SUPPORT ANGLE IAW DC9 SRM 53-11-1. INSTALLED NEW SUPPORT ANGLE IAW DC9 SRM 53-11-1 OR 51-30-8. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y=200 FROM -24 INCH TO -X43, FOUND AFTER G-1 REMOVED DUE A CORROSION BEYOND LIMITS AT FLOOR SUPPORT. DRILLED AND LOCATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y = 160 FROM -X=1 TO -X=21. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-1. (M)

Part: SKIN — CRACKED (FUSELAGE)

FTW - FOUND ANGLE SUPPORT HAS ELONGATED HOLES, AT LEFT TRAPEZOIDAL PANEL AFT UPPER AREA STA Y 730. UPON FURTHER INVESTIGATION, FOUND CRACK IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

FTW - FOUND SUPPORT BRACKET CRACKED AT LEFT TRAPEZOIDAL PANEL STRUCTURE STA Y 729 X=59.500 Z=13.100. REMOVED BRACKET. INSTALLED NEW FILLER IAW DC9 SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CRACKED AT STATION Y=238 INCHES. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED LOCATED AND DRILLED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)

Part: DOUBLER — CRACKED (CARGO DOOR)

FTW - AFT LOWER CARGO, CARGO DOOR OUTBOARD LOWER CORNER DOUBLER PREVIOUS REPAIR CRACKED/WORN-OUT. REMOVED DAMAGE AREA. FORMED REPAIR. INSTALLED REPAIR IAW DC9 SRM 51-30-2. (M)

Part: SKIN — CRACKED (RUDDER)

FTW - FOUND RUDDER RIGHT UPPER SKIN, .50 INCH DIAMETER DENT IN SKIN BETWEEN RIBS 17 AND 18. UPON FURTHER INVESTIGATION CRACK FOUND IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STA Y=200 FROM X-24 INCH TO X-43 INCH. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT PER DC9 SRM 51-10-4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY FLOOR SUPPORT CORRODED FROM STA Y=162 TO Y=198. FABRICATED FLOOR SUPPORT. INSTALLED REPLACEMENT FLOOR SUPPORT IAW DC9 SRM 51-10-4 AND 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND ENTRY AREA, FLOOR SUPPORT CORRODED FROM STATION Y=160 TO STA Y=200. REMOVED FLOOR SUPPORT STA 160-200. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

FTW - FOUND E/E BAY LONGERON 28 LEFT HAS CORROSION AT STATION 170-180. CUT OUT DAMAGE AND REMOVED. INSTALLED LONGERON AND SPLICE PER DC9 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y200 FROM X2 INCHES TO -X21. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y200 FROM X= 1 INCH TO X= 20 INCHES. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: STRAP — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CARGO DOOR JAMB AFT STATION 427-438 WEB STRAPS HAVE TOOLING MARKS AND SURFACE CORROSION. FORMED STRAP. LOCATED AND DRILLED STRAP IAW DC9 SRM 51-10-4. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FTW - FOUND FORWARD CARGO DOOR JAMB WEB STRAP AND ANGLES HAVE TOOLING MARKS, CORROSION AND CRACKS STATION 427-436. ONE ANGLE WAS CRACKED FORMED A NEW ANGLE. FORMED ANGLE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

FTW - ANGLE SUPPORT CORRODED AT STATION Y916. FABRICATE NEW ANGLE SUPPORT. INSTALLED NEW ANGLE SUPPORT IAW DC9 SRM 51-30-1. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CUSP WEB CORRODED AT STATION Y=200 X=56. CORROSION WAS FOUND DURING OPEN UP FOR WEB REPAIR AT FRAME STATION -200, X=57. REMOVED CORROSION. REMOVED SECTION OF CUSP. WEB DAMAGED. FABRICATED AND LOCATED CUSPS WEB. INSTALLED IAW DC9 SRM 51-30-2. (M)

Part: WEB — DAMAGED (FUSELAGE)

FTW - FOUND LOWER INNER WEB FORWARD BAG DOOR FS 370 TO FS 427 HAS OVERSIZED HOLES, EXTRA HOLES, CORRODED HOLES, A BAD PREVIOUS REPAIR AND NUMEROUS DENTS FROM OVER DRIVEN RIVETS. LOCATED AND DRILLED NEW INNER WEB. INSTALLED INNER WEB IAW DC9 SRM 51-30-2. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

FTW - FORWARD CARGO COMPARTMENT HAS A CRACK BETWEEN STATION 465-484 BETWEEN LONGERON 30 AND 29L. FORMED INTERCOSTAL IAW DOUGLAS PRING SR09530005. FORMED AND INSTALLED REPAIR PARTS. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND FRAME CORRODED AT STATION 927 BETWEEN LONGERON 18L TO 15L. FRAME FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND CABIN LEFT SIDE CORRODED AT MEMBRANE WEB STATION 908. REMOVED MEMBRANE WEB FROM STATION 897 TO 964. FORMING MEMBRANE/WEB. INSTALLED NEW MEMBRANE/WEB IAW DC9 SRM 51-30-2. (M)

Part: FRAME — CRACKED (FUSELAGE)

FTW - FOUND FRAME CORRODED/CRACKED AT BRACKET ATTACH SUPPORT, LONGERON 18L. REMOVED BRACKET CRACKED. LOCATE AND DRILL. INSTALLED NEW FITTING IAW DC9 SRM 51-30-1. (M)

Part: AILERON — DELAMINATED (LT WING)

FTW - FOUND LEFT AILERON OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED LEFT AILERON OUTBOARD TRAILING EDGE IAW DC9/MD80 SRM 57-03. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT INBOARD FLOORBOARD STATION 237-313 GOUGED, HOLES ELONGATED, SURFACE CORROSION. FABRICATED DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND LEFT OUTBOARD FLOORBOARD STATION 756-832 CORNERS ARE BROKEN OFF. FABRICATED REPAIR DOUBLERS. INSTALLED DOUBLERS IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND LEFT INBOARD FLOORBOARD NR 2 COUNTERSINKS PULLED THROUGH, SURFACE CORROSION AND BARE METAL. CRACK WAS FOUND ON END. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND LEFT OUTBOARD FLOORBOARD STATION 832-894 BENT, CRACKED, OVERSIZE HOLES, SURFACE CORROSION. REMOVED CRACKED STRIP. FABRICATED NEW STRIP. INSTALLED NEW STRIP IAW DC9 SRM 51-70. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND RIGHT FLOORBOARD STATION 465 CRACKED AT FASTENER HOLES. FORM DOUBLER FOR FLOOR PANEL. INSTALLED DOUBLER PER DC9 SRM 53-04. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT INBOARD FLOORBOARD STATION 389 CRACKED AND TORN AT EDGE. FORM PATCH REPAIR FOR PANEL PER DC9 SRM 55-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 FROM STATION 323-417. CUT OFF SEAT TRACK DAMAGE IN STATION 323-417. DRILLED NEW SEAT TRACK IN STATION 323-417. DRILLED SPLICE IN STATION 417 SEAT TRACK. INSTALLED SEAT TRACK IN STATION 323-417. INSTALLED NEW SPLICE IN STATION 417 AT SEAT TRACK IAW SRM DC9 51-30-5. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - RIGHT INBOARD FLOORBOARD STATION 579-680 HAS BARE METAL AND SURFACE CORROSION AND DENTS. LOCATED AND DRILLED AND COUNTERSINK FLOORBOARD. INSTALLED FLOORBOARD FS 579-680 RIGHT CENTER IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND LEFT OUTBOARD FLOORBOARD STATION 894-974 HAS SURFACE CORROSION. REMOVED HAT CHANNEL TO FABRICATED PANEL. FABRICATED NEW FLOOR PANEL. INSTALLED HAT CHANNELS PER SRM DC9 51-30-2. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT X 44 SEAT TRACK FROM STATION 765 TO STATION 860. INSTALLED SECTION OF SEAT TRACK FROM STATION 765 TO Y 860 X 44 IAW SRM DC9 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND LEFT, OUTBOARD FLOORBOARD STATION 465-579 COUNTERSINKS BROKEN OUT AND SURFACE CORROSION. STOPPED DRILL CRACKED. FORMED DOUBLER REPAIR. INSTALLED DOUBLER. REMOVED SURFACE CORROSION IAW DC9 SRM 53-01. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND FLOORBOARD STATION 889 TO 965 HAS COUNTERSINKS BROKEN OUT,HOLE IN STIFFENER ON BACK, SURFACE CORROSION. REMOVED STIFFENER FROM FLOORBOARD. FORMED NEW PART. INSTALLED STIFFENER. DOUBLER MADE FOR BROKEN CSKS. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD FLOORBOARD STATION 389-465 FASTENER HOLES OVERSIZED, SURFACE CORROSION, BARE METAL. TWO OVERSIZED HOLES HAVE CRACKS AND PANEL, AFT END OF PANEL HAS FASTENER HOLE CRACK. INSTALLED DOUBLERS ON FORWARD END OF PANEL. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND LEFT MID FLOORBOARD STATION 200-237 HAS OVERSIZE FASTENER HOLES. REMOVED HAT SECTIONS. FABRICATED LOCATED AND DRILLED FLOORBOARD SKIN. INSTALLED HAT SECTIONS IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT INBOARD FLOORBOARD STATION 756-832 HAS SURFACE CORROSION, HOLES OVERSIZED AND COUNTERSINKS BROKEN OUT. FORMED PATH SHAPE FOR BROKEN OUT OVERSIZED HOLES PER DC9 SRM 55-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 FROM STATION 228-323. REMOVED DAMAGED SECTION OF SEAT TRACK STATION 228-323. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK STATION 228-323 IAW DC9 MM 53-40-1. (M)

Part: DRIVE LINK — CRACKED (SPOILERS)

FTW - FOUND OUTBOARD SPOILER DRIVE LINK, INBOARD LUG CRACKED. REMOVED DRIVE LINK LEFT OUTBOARD SPOILER. INSTALLED DRIVE LINK ON LEFT OUTBOARD SPOILER AS PER DC9 MM 27-61-1. (M)

Part: PAN — CRACKED (CARGO DOOR)

FTW - FOUND AFT LOWER CARGO DOOR PAN CRACKED AT FORWARD END OF NR 1 BEAM. FORMED NEW DOUBLER. INSTALLED NEW STRIPS IAW DC9 SRM 51-30-2. (M)

Part: STRUCTURE — CRACKED (CARGO DOOR)

FTW - FORWARD LOWER CARGO DOOR PANE CRACKED, APPROX 3 INCHES, AT LOWER FORWARD STOP FITTING. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLE DOUBLER PER DC9 SRM 51-10-3. (M)

Part: FITTING — CRACKED (CARGO DOOR)

FTW - AFT LOWER CARGO DOOR, CENTER INTERCOSTAL TO PAN ANGLE FITTING CRACKED. REMOVED CRACKED ANGLE FITTING. INSTALLED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 940 TO 965, CRACKS ON PANEL EDGES SURFACE CORROSION AND BARE METAL AREAS ON SKIN, LOWER SIDE INSULATION TORN. REPAIRED CRACKS ON FLOOR PANEL PER DC9 SRM 53-05. (M)

Part: RETAINER — BROKEN (CABIN FLOOR)

FTW - FOUND CABIN FLOORBOARD LEFT, OUTBOARD STATION 389-465, LOWER SIDE RETAINER BROKEN IN HALF (FIBERGLASS) SURFACE CORROSION AND BARE METAL AREAS ON SKIN. AREA FOUND OUT OF LIMITS. FABRICATED NEW FLOORBOARD PER DC9 SRM 51-10-2. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD RIGHT, OUTBOARD STATION 680 TO 756, MOUNT HOLES CRACKED IN SEVERAL AREAS, SEVERE CORROSION ON SKIN. FORM DOUBLERS. INSTALLED IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD, LEFT, OUTBOARD STATION 237 TO 313 STIFFENER DETACHED FROM BACKSIDE SKIN, CRACK AT FORWARD END EDGE, SEVERE CORROSION ON SKIN. REATTACHED STIFFENER. FABRICATED DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD LEFT, INBOARD STATION 465 TO 525, LOWER SIDE STIFFENERS CRACKED, INBOARD, OUTBOARD AND ONE IN CENTER SKIN HAS SURFACE CORROSION AND BARE METAL. REMOVED HAT CHANNELS. FABRICATE 4 HAT CHANNELS. INSTALLED HAT CHANNELS AND INSULATION BLANKETS IAW DC9 SRM 53-05-0. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD CENTER LEFT STATION 832 TO 889, LOWER SURFACES UPPER CORNER HAS AN AREA OF METAL CRACKED 9 INCHES LONG. FLOORBOARD DAMAGE ARE FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOORBOARD IAW SRM DC9 51-01. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD RIGHT, INBOARD STATION 237 TO 313, TWO CRACKS AT FORWARD OUTER EDGE, SURFACE CORROSION AND BARE METAL AREAS ON SKIN. STOPPED DRILL CRACKS, LOCATED AND DRILLED. INSTALLED TWO DOUBLERS IAW DC9 SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD LEFT, INBOARD STATION 313 TO 389 TWO CRACKS AT FORWARD END EDGES, SEVERE CORROSION AROUND FASTENER HOLES, BARE METAL AREAS ON SKIN. FABRICATED THREE DOUBLERS FOR CRACKS AT FORWARD END. INSTALLED THREE DOUBLERS. ALL AREAS BUT ONE WITHIN LIMITS. FABRICATED REPAIR DOUBLERS TWO FOR AREA OUT OF LIMITS. INSTALLED TWO DOUBLERS IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD RIGHT INBOARD STATION 465-579, FORWARD AND AFT END RIVETS PULLING THROUGH STIFFENERS, SEVERAL CRACKS AT AFT END FASTENER HOLES, SURFACE CORROSION AND BARE METAL AREAS ON SKIN. FABRICATED DOUBLERS. INSTALLED DOUBLERS IAW MD80 SRM 51-30-2. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - PAX CABIN FLOOR WEB HAS CRACK STATION 220 X44. FORMED WEB. INSTALLED WEB IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD FLOORBOARD NR 2 HAS ELONGATED HOLES, SURFACE CORROSION AROUND FASTENER HOLES, TORN SKIN. REMOVED DAMAGE AREAS AND FABRICATED REPAIR PARTS. INSTALLED DOUBLER FILLER IAW DC9 SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOOR PANEL FS 699-756 LEFT LOWER COMPOSITE CHAFED STRIPS DISBONDED, BROKEN AND MISSING, UPPER SURFACE CORROSION CORNER MATERIAL BROKEN OFF AND IMPROPERLY INSTALLED BLIND RIVETS. FORMED NEW FLOOR PANEL PER DC9 SRM 53-24-0. (M)

Part: STRUCTURE — CRACKED (CARGO DOOR)

FTW - FORWARD LOWER CARGO DOOR PANEL CRACKED APPROXIMATELY .75 INCH AT UPPER AFT STOP FITTING AREA. STOP DRILLED CRACK. FABRICATED OUTER FLANGE DOUBLER. INSTALLED REPAIR DOUBLER AND INTERCOSTAL PER DC9 SRM 53-02. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD LEFT CENTER STATION 889-956. SEVERE CORROSION AFT END, CRACKED WITH AREAS OF MISSING METAL AND ELONGATED MOUNT HOLES. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD STATION 889-956 IAW DC9 SRM 51-30-1. (M)

Part: SEAT TRACK — WORN (COCKPIT)

FTW - FOUND CAPTAIN SEAT TRACKS ARE WORN. REMOVED UPPER DAMAGED TRACKS. FORMED NEW TRACK. INSTALLED CAPTAINS SEAT TRACKS IAW DC9 SRM 51-30-1. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR PANEL LEFT MID STATION 237 TO 313 CORROSION. REMOVED DAMAGE 3 AREAS. FABRICATED DOUBLERS TWO EACH. INSTALLED TWO DOUBLERS IAW MD80 SRM 53-05. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND WEB CRACKED AT STATION Y=954. REMOVED MEMBRANE/WEB FROM STATION 897 TO 964. INSTALLED NEW MEMBRANE/WEB IAW DC9 SRM 51-30-2. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND WEB CRACKED AT LEFT FORWARD ENTRY DOOR JAMB AREA, STA Y-208, X-51, X=63. REMOVED CRACK FROM WEB. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-5. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND WEB CRACKED AT LEFT FORWARD ENTRY DOOR JAMB AREA STA Y-208, Z=26, X63. CUT OUT DAMAGED AREA. FABRICATE NEW DOUBLER AND FILLER. INSTALLED NEW DOUBLER AND FILLER IAW DC9 SRM 53-01. (M)

Part: SUPPORT — BROKEN (FUSELAGE)

FTW - FOUND AFT ACCESSORY COMPARTMENT RIGHT STATION 1076 RIGHT LONGERON 14 ROD SUPPORT BROKEN. REMOVED DAMAGED PART. FORMED NEW SUPPORT. INSTALLED SUPPORT IN A/C AFT COMPARTMENT IAW SRM DC9 51-30-1. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

FTW - FOUND AFT PRESSURE BULKHEAD , AFT SIDE BELOW ENTRY DOOR THRESHOLD, THE 15910130-37 CHANNEL HAS A 1.3 INCH LONG CRACK 7 INCHES INBOARD FROM LEFT EDGE. REMOVED FITTING. DRILLING NEW FILLING. INSTALLED NEW FITTING IAW DC9 SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - E/E BAY FLOOR SUPPORT BEAM, STATION 200 HAS DRILL MARKS AND CORROSION NEXT TO NUT PLATES, BOTH INBOARD AND OUTBOARD ENDS OF FRAME. FORMED NEW REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-1 AND 51-30-2. (M)

Part: PANEL — CHAFED (NR 1 PYLON)

NR 1 ENGINE PYLON L/E PANEL CHAFFING INTO FUSELAGE. FORMED REPAIR DOUBLER. INSTALLED DOUBLER IAW SRM DC9 51-30-2. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

FTW - FOUND AFT LOWER CARGO COMPARTMENT CORRODED X17 CHANNEL FROM STATION 937 TO 889. REMOVED DAMAGE SECTION FROM STATION 889 TO 937, LOCATE AND DRILL. INSTALLED CHANNEL IAW DC9 SRM 51-30-2. (M)

Part: DOUBLER — BROKEN (NR 2 NACELLE)

NR 2 ENGINE PYLON UPPER OUTBOARD LE STRUCTURE FRAME HAS BROKEN DOUBLER. REMOVED BROKEN DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: SKIN — DAMAGED (L1 DOOR)

FTW - PREVIOUS REPAIR AT UPPER EDGE OF L1 DOOR NEEDS REPLACED, INADEQUATE REPAIR DOUBLER MATERIAL. REMOVED OLD REPAIR AND DAMAGED SKIN. INSTALLED FLUSH PATCH REPAIR ON L1 DOOR IAW DC9 SRM 53-05. (M)

Part: SKIN — CRACKED (FUSELAGE)

FTW - WHEN L-1 DOOR IS FULLY OPEN, HOLD OPEN HOOK IS NOT ALIGNED WITH FITTING IN FUSELAGE, HOOK IS CHAFING AT BOTTOM OF OPENING. FOUND CRACK AT 12:00 POSITION. LOCATED AND DRILLING EXTERNAL DOUBLER AND INTERNAL DOUBLERS, TWO. INSTALLED COMPLETE IAW SRM DC9 53-04. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

FTW - AFT LOWER CARGO COMPARTMENT CORRODED AT CHANNEL FROM STATION 889-775. REMOVED DAMAGE SECTION FROM STATION 859-889. LOCATED AND DRILLED. INSTALLED CHANNEL. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

FTW - FOUND FORWARD SKIN PANEL CRACKED AT TWO FASTENER LOCATIONS BETWEEN LONGERON 2 LEFT AND 3 LEFT. FORMED NEW REPAIR DOUBLERS. INSTALLED REPAIR DOUBLER PER DC9 SRM. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FOUND LONGERON 13L CRACKED AT FUSELAGE FRAME STATION Y=965. REMOVED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED LONGERON 13 ON STATION 965 2ND SPLICE PER DC9 30 SRM 51-30-2. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

FTW - FOUND FRAME TO SKIN CLIP CRACKED AT FUSELAGE FRAME STA Y-980 ADJACENT TO LONGERON 14L. REMOVED EXISTING REPAIR CLIP. FORMED NEW CLIP. INSTALLED IAW DC9 RM 51-30-2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - FOUND LONGERON 17R CRACKED AT FS 965. REMOVED CRACKED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED REPAIR LONGERON AND SPLICE (TWO EACH) IAW DC9 SRM 53-02. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

FTW - FOUND FUSELAGE FRAME STATION Y-980 CRACKED AT LONGERON 16L. AFTER FURTHER EVALUATION FOUND THE FRAME SHEAR TIE TO BE ONE WITH CRACKS. REMOVED DAMAGED SHEAR TIE AT STATION 980. FABRICATED NEW SHEAR TIE IAW DC9 SRM 51-10-2. INSTALLED NEW SHEAR TIE IAW DC9 SRM 51-30-2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FOUND LONGERON 13R CRACKED AT FUSELAGE FRAME STA Y-965. REMOVED DAMAGED SECTION OF STRINGER. FORMED LONGERON AND SPLICE. INSTALLED LONGERON REPAIR IAW DC9 SRM 53-02. (M)

Part: PULLEY BRACKET — BROKEN (RUDDER)

FTW - FOUND BRACKET RUDDER TRIM PULLEY BROKEN. REMOVED RUDDER TRIM BRACKET. INSTALLED RUDDER TRIM PULLEY BRACKET AS PER DC9 MM 20-17-0. (M)

Part: WEB — CORRODED (FUSELAGE)

FTW - FOUND WEB CORRODED AT STA Y 200 X57 INCHES UNDER FLOOR LINE AFT OF FORWARD AIRSTAIRS CUT OUT. CUT DAMAGE AREA. FABRICATE FILLER AND DOUBLER. AFTER FURTHER EVALUATION. FOUND SUB FLOOR 2ND FLOOR SUPPORT ON STRAP 6/7 CORRODED OUT OF LIMITS. FABRICATED 2ND DRILLED SUB FLOOR. INSTALLED DOUBLER, FILLER AND ANGLE. FABRICATED FLOOR SUPPORT IAW DC9 SRM 51-10-2. INSTALLED SUB FLOOR. INSTALLED FLOOR SUPPORT. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FOUND LONGERON 16R CRACKED AT FUSELAGE FRAME STATION 965. REMOVED LONGERON 16R CRACKED FROM STATION 955-975. DRILLED AND LOCATED LONGERON AND SPLICE. INSTALLED LONGERON REPAIR AND SPLICES (TWO EACH) IAW DC9 SRM 53-02. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - FOUND LONGERON 17L CRACKED AT FUSELAGE FRAME STATION Y=980. REMOVED DAMAGED AREA OF LONGERON. FABRICATED NEW LONGERON SECTION AND SPLICE. INSTALLED LONGERON SECTION AND SPLICE PER DC9 SRM 53-02. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - FOUND LONGERON 16L CRACKED AT FUSELAGE FRAME STATION Y 965. REMOVED CRACKED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED REPAIR IAW DC9 SRM 53-02. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - E/E BAY INTERCOSTAL ABOVE 28L STRINGER HAS CORRODED. FABRICATED NEW INTERCOSTAL AND HEAT TREATED. INSTALLED INTERCOSTAL IAW DC9 SRM 51-30-2. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

FTW - FOUND FUSELAGE FRAME AT STATION Y 980 CRACKED AT LONGERON 16R. AFTER FURTHER EVALUATION. FOUND THE FRAME SHEAR TIE TO BE THE ONE WITH CRACKS TWO EACH BETWEEN LONGERON 16R-17R. REMOVED DAMAGE SHEAR TIE AT STATION 980. FABRICATED NEW SHEAR TIE IAW DC9 SRM 51-10-2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - FOUND LONGERON 12R CRACKED AT FUSELAGE FRAME STATION Y=945. REMOVED CRACKED LONGERON. FABRICATED DRILLED AND LOCATED NEW LONGERON AND SPLICE. INSTALLED NEW LONGERON AND SPLICE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FTW - FORWARD CARGO COMPARTMENT ANGLE SUPPORT AT STATION Y275 BETWEEN LONGERON 27R AND 26R HAS A CRACK. REMOVED CRACK ON STEEL FLOOR SUPPORT. FORMED REPAIR PARTS AND INSTALLED REPAIR PARTS PER DC9 SRM 53-03. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - FORWARD CARGO COMPARTMENT LOWER DOOR JAMB AREA CORRODED BETWEEN STA Y 330 AND STA Y 427. LOWER DOOR JAMB PAN OUT OF LIMITS. FABRICATED PAN PER DC9 SRM 53-05. INSTALLED DOOR JAMB DOOR PAN FORWARD AND PAN DOUBLERS AND WEB IAW SRM DC9. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -X44 INCH FROM STATION 342-440. REMOVED SEAT TRACK FROM STA 342-440. DRILLED AND LOCATED SEAT TRACK STATION 342-440. INSTALLED SEAT TRACK 342-440 -X44 IAW DC9 SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 200-303. CUT OFF THE SEAT TRACK DAMAGED STATION 200-303. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SPLICE TWO AND SEAT TRACK IAW DC9 MM 53-40-11 AND SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CORROSION NICK AND GOUGES AT SEAT TRACK -44 INCH FROM STA Y 532-648. REMOVED SEAT TRACK FROM STATION 532-648. FABRICATED, DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 INCHES FROM STA 417-532. CUT OFF SECTION SEAT TRACK FROM STATION 417-532. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE TWO IAW DC9 M 53-40-1. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

FTW - AFT PRESSURE BULKHEAD WEB CRACKED IN AREA BETWEEN 2 FASTENERS AND UNDER FINGER DOUBLER. CRACK IS LOCATED RIGHT SIDE OF VERTICAL DOOR NEXT TO THE CONTROL CABLE FAIRED BOX. REMOVED CRACK. FABRICATED FILLER, FINGER DOUBLER, AND DOUBLER INSTALLED REPAIR IAW DC9 SRM 51-30-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES ANS SEAT TRACK X22 INCH FROM STATION 860-964. REMOVED DAMAGE SECTION FROM STATION 860-964. LOCATE AND DRILLED SEAT TRACK. SEAT TRACK INSTALLED FROM 860-964. (M)

Part: FLAP — DAMAGED (LT WING)

FTW - FOUND LEFT WING TRAILING EDGE FLAP DAMAGED NEXT TO INBOARD HINGE. REMOVED TRAILING EDGE WEDGE. LOCATE AND DRILLING TRAILING EDGE. INSTALLED TRAILING EDGE IAW DC9 SRM 51-30-8. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK -X44 INCHES FROM STATION 766-964. REMOVED SEAT TRACK FROM STA 766-860. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED SEAT TRACK FROM 766-860. REMOVED SEAT TRACK DAMAGE FROM STATION 860-964. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK FROM STA 860-964. INSTALLED SEAT TRACK FROM STA 860-964 PER SRM DC9 53-05. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK -X22 INCH FROM STATION 440-532. REMOVED SEAT TRACK FROM STATION 440-532. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK FROM STATION 440-532 PER DC9 SRM 51-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK X22 INCH FROM STATION 200-228. REMOVED DAMAGED SECTION OF SEAT TRACK 200-228. LOCATED AND DRILLED. INSTALLED SEAT TRACK AND SPLICE SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 860-964. CUT OFF SEAT TRACK DAMAGE IN STATION 860-964. LOCATED AND DRILLED SEAT TRACK. INSTALLED NEW SEAT TRACK FROM STATION 860-964 IAW DC9 SRM 51-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK -X22 FROM STA Y532 TO STA 648. REMOVED SEAT TRACK FROM STATION 532-648. FABRICATED DRILLED AND LOCATED NEW SECTION FROM 532-648. INSTALLED NEW SEAT TRACK FROM 532-648. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND FRAME FOR FLOOR SUPPORT FS 218 LONGERON 30 TO L29 HAS EXFOLIATION CORROSION IN E BAY. REMOVED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)

Part: HOUSING — CRACKED (CABIN)

FTW - FOUND MAIN CABIN OVERHEAD CEILING PANEL BETWEEN ROWS, AFT 15 L/R INNER LIGHT HOUSING CRACKED. REMOVED EMERGENCY LIGHT ASSY. INSTALLED EMERGENCY LIGHT ASSY IAW MD9 33-53-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 303-417. CUT OFF THE SEAT TRACK DAMAGED STATION 303-417. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK 303-417 IAW DC9 53-40-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -22 INCHES FROM STA 342-440. REMOVED DAMAGED SEAT TRACK FROM STA 342-437. LOCATE AND DRILL SEAT TRACK. INSTALLED SEAT TRACK AND SPLICES 342-437 IAW DC9 SRM 51-30-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICKS GOUGES AT SEAT TRACK -X44 INCHES FROM STATION 648-766. REMOVED SEAT TRACK. LOCATE AND DRILL FROM 648-766. INSTALLED NEW SEAT TRACK AT STATION 648-766 RIGHT SIDE IAW DC9 SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGED AT SEAT TRACK -X22 INCH FROM STATION 766-964. REMOVED SEAT TRACK FROM STATION 860-965. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK FROM 860-965. FABRICATED DRILLED AND LOCATED SPLICE. INSTALLED SEAT TRACK SPLICE. REMOVED SET RACK FROM 766-860. FABRICATED DRILLED AND LOCATED NEW SECTION OF SEAT TRACK. INSTALLED SEAT TRACK FROM STATION 766-860 PER DC9 SRM 51-30-1. (M)

Part: SKIN — CRACKED (FUSELAGE)

FTW - FOUND CRACK IN SKIN 1 INCH LONG ON FORWARD SIDE OF FASTENER HOLE, 1 INCH LONG ON AFT SIDE OF FASTENER HOLE, 2 INCHES OVERALL LENGTH. STOP DRILL CRACK. FABRICATE REPAIR DOUBLER. INSTALLED NEW REPAIR IAW DC9 SRM 53-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICK AND GOUGES AT SEAT TRACK -X44 INCHES FROM STA 440-532. REMOVED SEAT TRACK FROM STATION 440-532. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK AT STA 440-532. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -X22 INCH FROM STATION 200-342. REMOVED SEAT TRACK FROM STATION 285-342. FABRICATED DRILLED AND LOCATED SEAT TRACK FROM STATION 285-342. DRILLED AND LOCATE SPLICE. INSTALLED SEAT TRACK FROM STATION 285-342 AND SPLICE. REMOVED SEAT TRACK FROM STATION 200-285. LOCATE AND DRILLED SEAT TRACK STATION 200-285. LOCATE AND DRILL SPLICE STATION 285. INSTALLED SEAT TRACK AND SEAT TRACK SPLICE IAW DC9 SRM FROM STATION 200-342. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 INCH FROM STATION 200-342. REMOVED SEAT TRACK FROM STATION 200-285. DRILLED AND LOCATED NEW SEAT TRACK IAW DC9 SRM 51-10-4 AND 53-05. INSTALLED NEW SEAT TRACK FROM STATION 200-285. REMOVED SEAT TRACK FROM STATION 285-342. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK AT STATION 265-342 RT IAW DC9 SRM 51-30-2. (M)

Part: DOUBLER — CRACKED (LT WING SPAR)

FTW - FOUND LEFT WING LEFT REAR SPAR DOUBLER CRACKED IMMEDIATELY OUTBOARD OF THE STATION XCW=58.688 TRAPEZOIDAL PANEL TO REAR SPAR ATTACH FITTING. REMOVED DAMAGE AREA. REPAIR DOUBLER FABRICATE. INSTALLED REPAIR DOUBLER IAW DC9. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 649 TO STATION 765. INSTALLED SECTION OF SEAT TRACK FROM STA Y 649 TO Y 765 X 44 IAW SRM DC9 53-05. (M)

Part: LIGHT — MISSING (CABIN)

FTW - FOUND MAIN CABIN, OVERHEAD CEILING PANEL BETWEEN ROWS 13L AND RIGHT LIGHT ASSY MISSING. REMOVED EMERGENCY LIGHT ASSY. REPAIRED WIRING. INSTALLED EMERGENCY LIGHT ASSY IAW MD9 MM 33-53-0. (M)

Part: SKIN — CRACKED (RT COWLING)

FTW - FOUND RIGHT ENGINE NOSE COWL, CRACK IN INNER LIP SKIN AT 6:00 POSITION. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR PARTS PER DC9 SRM 51-30-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 INCHES FROM STATION 532-649. CUT OFF SEAT TRACK DAMAGE IN STATION 532-649. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE IAW DC9 SRM 51-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 INCH FROM STATION 765-860. REMOVED DAMAGE SECTION FROM STATION 766-860. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK IAW SRM DC9 51-30-5. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK BY 44 INCHES FROM STATION Y 532 TO STA 649. INSTALLED SECTION OF SEAT TRACK FROM STA 532 TO STA 649. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X22 INCH FROM STATION 417-532. REMOVED DAMAGE SECTION OF SEAT TRACK STATION 417-532. DRILLED NEW SEAT TRACK 417-532. INSTALLED NEW SEAT TRACK IN STATION 417-532. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CORROSION NICKS AND GOUGES AT SEAT TRACK -X22 FROM STATION Y648 TO STA Y766. REMOVED SEAT TRACK FROM STA 648-766. DRILLED AND LOCATE SEAT TRACK FROM STATION 648-766 AND SPLICE. INSTALLED SEAT TRACK PER SRM DC9 51-30-1. (M)

Part: WEB — CRACKED (LT COWLING)

FTW - FOUND LEFT POWER PLANT NOSE COWL AFT INNER SECTION CRACK. REMOVED CRACKED WEB DOUBLER FROM NOSE COWL. FABRICATED NEW DOUBLER AND WEB. INSTALLED DOUBLER ON WEB. INSTALLED WEB PER DC9 SRM 51-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - DENT LEFT FUSELAGE STATION 207, JUST ABOVE CUSP. FABRICATE DOUBLER REPAIR. INSTALLED NEW DOUBLER REPAIR IAW DC9 SRM 53-04. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND STATION 1143 L16, 2.5 L CREASE IN SKIN AFT OF FRAME, 2 INCH LONG SCRATCH FORWARD OF FRAME. FORMED DOUBLER IAW DC9 SRM 53-04. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD FLOORBOARD NR 2 FROM STATION 237 TO STATION 313 HAS CORROSION, ELONGATED HOLES AND EDGES BROKEN OFF. FABRICATED REPAIR DOUBLER FOR ELONGATED HOLES. FABRICATED REPAIR DOUBLER FOR BROKEN EDGES. INSTALLED REPAIR DOUBLER FOR ELONGATED HOLES. INSTALLED REPAIR DOUBLER FOR BROKEN EDGES IAW DC9 SRM 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT INBOARD FLOORBOARD NR 3 FROM STA Y314 TO STA Y329 HAS BROKEN EDGE (FWD ONE) AND STIFFENERS CRACKED. FORMED DOUBLER FOR RIGHT INBOARD FLOORBOARD. STOP DRILLED CRACKS, ROUNDED OUT CRACK IN STIFFENER. INSTALLED FORMED DOUBLER IAW DC9 IAW SRM 51-30-2. (M)

Part: JACKSCREW — DAMAGED (HORIZONTAL STAB)

FTW - ACME SCREW AND NUT END PLAY CHECK IN EXCESS OF .040, REPLACEMENT OF HORIZONTAL STAB ACTUATOR ASSY REQUIRED. REMOVED LONGITUDINAL TRIM CONTROL SYSTEM ASSY (JACKSCREW). INSTALLED JACKSCREW ASSY IAW DC9 MM 27-40-1. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FTW - FOUND FORWARD GALLEY FLOOR WHEN WALKING ON SOUNDS AND FEELS LIKE SOMETHING LOOSE OR MISSING. REMOVED FLOOR. FORM NEW PANEL AND HATS. INSTALLED FLOOR PANEL IAW DC9 SRM 51-30-1. (M)

Part: SKIN — DELAMINATED (AILERON TAB)

FTW - FOUND RIGHT WING, INBOARD AILERON TAB, INBOARD CORNER UPPER SIDE DELAMINATION, 1.500 INCH SPAN BY 1 INCH, CHORD. REMOVED DAMAGE TO AILERON TAB. REPAIR TAB PER DC9 MD80 SRM 57-04. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND RIGHT INBOARD FLOORBOARD NR 10 FROM STATION 639 TO 680 HAS EDGES BROKEN OFF. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - RIGHT INBOARD FLOORBOARD NR 5 FROM STATION 579-617 HAS EDGES BROKEN, ELONGATED HOLES AND INSULATION TORN. FORMED NEW PNL IAW DC9 SRM 53-24-0. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD FLOORBOARD NR 2 FROM STATION 237-313, PREVIOUS REPAIR AT CORNER PEELING OFF HAS CORROSION AND GOUGES. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED DOUBLER AND FILLER IAW DC9 SRM 51-30-2. (M)

Part: FLOOR PANEL — DETERIORATED (FUSELAGE)

FTW - FOUND FORWARD GALLEY FLOOR LOOSE AND DETERIORATED. FORMED NEW PANEL, FORMED HAT SECTION. INSTALLED FLOOR PANEL IAW DC9 SRM 51-30-1. (M)

Part: RIB — CRACKED (RT WING)

FTW - FOUND RIGHT WING FUSELAGE MOUNTED VERTICAL RIB, INBOARD OF TRAILING EDGE FLAP HAS A .250 CRACK ON ITS LOWER EDGE. REMOVED DAMAGE PART. FORMED ANGLE FOR REPAIR ON VERTICAL RIB. INSTALLED REPAIR ANGLE IAW DC9 SRM 51-30-2. (M)

Part: SKIN — CRACKED (RUDDER)

FTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 12. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)

Part: SKIN — CRACKED (RUDDER)

FTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 11. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DC9 SRM 5-03. (M)

Part: SKIN — DENTED (FUSELAGE)

FTW - FOUND STATION 231 L17-18 LEFT, DENT IN SKIN. FORMED INTERNAL DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 53-04. (M)

Part: SKIN — CRACKED (RUDDER)

FTW - FOUND RUDDER LEFT UPPER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 21. TRIMMED OUT CRACKED SKIN WITH CIRCULAR CUTOUT. FORMED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 55-03. (M)

Part: DOUBLER — IMPROPER (FUSELAGE)

FTW - FOUND STATION 148 RIGHT HAS A DEN AS MARKED AROUND 02 BLOW OUT DISK. UPON FURTHER EVALUATION FOUND PRODUCTION INTERNAL DOUBLER HAVE NO CONTOUR. FABRICATE NEW INTERNAL DOUBLER. INSTALLED NEW INTERNAL DOUBLER IAW DC9 SRM 51-30-1. (M)

Part: PANEL — CRACKED (FUSELAGE)

FTW - FOUND RIGHT TRAPEZOIDAL PANEL CRACKED AT FASTENER LOCATIONS NR 8 AND NR 9. REMOVED DAMAGE. FABRICATED ANGLES AND FILLER. INSTALLED REPAIR ANGLES AND FILLER PER DC9 SRM 51-30-5. (M)

Part: RIB — CRACKED (RT WING)

FTW - FOUND RIGHT SIDE, FUSELAGE AREA, INBOARD OF NR 1 SLAT HAS A VERTICAL RIB, BENT AND CRACKED. REMOVED DAMAGED RIB. FORMED NEW RIB. HEAT TREATED RIB TO T-6 CONDITION. INSTALLED FORMED RIB IAW DC9 SRM 51-30-3. (M)

Part: SKIN — CRACKED (FLAP VANE)

FTW - FOUND LEFT WING FIXED FLAP VANE HAS A CRACK AT STATION XTE 206. LOCATE AND DRILL NEW (SKIN FIXED COVER). INSTALLED SKIN ASSEMBLIES PER SRM DC9 MD80 51-30-1. (M)

Part: VANE — GOUGED (T/E FLAP)

FTW - FOUND RIGHT WING FIXED FLAP VANE HAS A GOUGE AT STATION XTE 206 (OUTBOARD SURFACE). BLEND OUT LEADING EDGE COVER AND FOUND IT OUT OF LIMITS. LOCATE AND DRILL DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-2. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DCA - FLT 72 - ONE WHITE PATH AISLE LIGHT INOPERATIVE, ROW 13. REPLACED LAMP AND LENS. OPS HECK OK IAW MM 33-53-01. THIS CLEARS DMI 121510-1, PLACARDS REMOVED. (M)

Part: LIGHT — LOOSE (CABIN)

ACY - FLT 886 - AISLE PATH LIGHTING COMING UP. RESECURED AISLE PATH LIGHTING IAW DC9 MM 33-50-0. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

MYR - FLT 541 - AFT OVERWING EMERGENCY LIGHTS INOP. FOUND 1 BAD BATTERY AT PACK B5-25. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD PER DC9 MM 33-53-0. (M)

Part: SWITCH — MALFUNCTIONED (COCKPIT)

MYR - FLT 541 - FOUND 3 EMERGENCY LIGHTS AT FORWARD ENTRANCE COME ON WITH ENTRY LIGHT SWITCH AND DO NOT TEST WITH COCKPIT EMERGENCY SWITCH. REPOSITIONED INSULATION ABOVE FORWARD ENTRANCE LIGHT ASSY. OPS CHECKS GOOD PER DC9 MM 33-53-0. (M)

Part: WIRE — EXPOSED (CABIN)

ACY - FLT 828 - ESCAPE PATH LIGHT WIRES EXPOSED IN FORWARD CABIN. RESECURED PATH LIGHTING COVERING OVER WIRES IAW MM 33-50-03. (M)

Part: WIRE — EXPOSED (CABIN)

DTW - EMERGENCY TRACK LIGHTING HAS WIRES EXPOSED THROUGHOUT CABIN. REPOSITIONED EMERGENCY FLOOR TRACK WIRES. OPS CHECK GOOD IAW DC-9 MM 33-50-00. (M)

Part: TERMINAL — SHORT (CABIN)

ACY - FLT 541 - COCKPIT EMERGENCY LIGHT ILLUMINATES WHEN CABIN ENTRY OR ATTENDANT LIGHT SWITCHES ARE ON. IF ENTRY OR HTT LIGHT SWITCHES ARE OFF, THEN CABIN EMERGENCY LIGHT LOCATED IN ENTRY LIGHT FIXTURE WILL NOT ILLUMINATE WHEN THE EMERGENCY LIGHT SWITCH IS IN THE ON POSITION. FOUND INSULATION BLANKET IN THE OVERHEAD OF MAIN ENTRANCE CEILING HAD METALLIC TAPE WHICH WAS MAKING CONTACT WITH TERMINALS TO LIGHT SOCKETS OF MAIN CABIN ENTRY LIGHTS AND EMERGENCYLIGHTS. REPAIRED AS NEEDED AND OPS CHECKS GOOD IAW MM 33-53-0. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ACY - FLT 544 - CABIN EMERGENCY LIGHTS INOPERATIVE. COCKPIT EMERGENCY LIGHTS STAYS ON CONTINUOUSLY. FOUND EMERGENCY LIGHT AT L1 DOOR GROUNDED ON AIRFRAME. RELOCATED WIRE AND REPAIRED WIRE. CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 570 - CABIN EMERGENCY LIGHTS OVERHEAD INOPERATIVE. REPAIRED WIRE ON LIGHT ASSEMBLY AT FORWARD PASSENGER ENTRANCE DOOR. OPS CHECKED GOOD IAW DC-9 MM. (M)

Part: WARNING HORN — SOUNDED (MLG)

ACY - FLT 880 - UPON MOVING THE L/G HANDLE TO THE UP POSITION THE L/G WARNING HORN SOUNDED AND WOULD NOT SILENCE. L/G RETRACTED CORRECTLY WITH L/G EXTENDED ALL WARNING LIGHTS AND HORN WAS EXTINGUISHED. RETURNED TO ACY NO FURTHER PROBLEMS. (M)

Part: WIRE — FAILED (TAILCONE)

MYR - ONE EMERGENCY 'WHITE' FLOOR TRACK LIGHTING INOPERATIVE IN TAILCONE. FOUND WIRES BAD AT DIGITAL. REMOVED AND REPLACED AS NEEDED. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 7-12)

CABIN OVERHEAD EMERGENCY LIGHTS ROWS 7 TO 12 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-32 IAW MM CHAPTER 33-53-0. OPERATION CHECKS GOOD. (X)

Part: SLIDE — DISENGAGED (GALLEY DOOR)

DTW - GALLEY SLIDE PACK FELL OFF. REINSTALLED GALLEY SLIDE PACK IAW DC-9 MM 25-00. OPERATION CHECK GOOD. (M)

Part: SLIDE — DISENGAGED (GALLEY DOOR)

GALLEY SLIDE PACK FELL OFF. REINSTALLED GALLEY SLIDE PACK IAW DC-9 MM 25-00. OPERATION CHECK GOOD. (M)

Part: SLIDE — DISENGAGED (R1 DOOR)

DTW - SLIDE PACK FELL OFF GALLEY DOOR. REINSTALLED R1 SLIDE PACK IAW DC-9 MM 25-61-00. (M)

Part: CONNECTOR — LOOSE (CABIN)

DTW - AFT HALF OF EMERGENCY FLOOR TRACK LIGHTS ARE INOPERATIVE. RESECURED PLUG AND SOLDERED BROKEN LIGHTS. OPERATION CHECKS GOOD. (M)

Part: WIRE — BROKEN (RT EMER EXIT)

DTW - AFT LEFT AND AFT RIGHT OVERWING EXIT DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. SOLDERED BROKEN WIRE. OPERATIONAL CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (TAILCONE)

DTW - EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. AFT OF BULKHEAD (TAIL CONE). REMOVED AND REPLACED EMERGENCY BATTERY CHARGER AND OPERATIONAL CHECK GOOD IAW MM 33-50-00. PART TC: 321. (X)

Part: WIRE — LOOSE (CABIN)

ACY - FLT 876A - LAST SIX EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. FOUND WIRE DISCONNECTED. RECONNECTED WIRE, OPERATIONAL CHECK GOOD IAW 33-53-0. (M)

Part: WIRE — LOOSE (CABIN)

DTW - FOUND AFT SECTION EMERGENCY LIGHTS NOT WORKING. FOUND WIRES TO BE SHORTED IN SEVERAL PLACES. SPLICED IN NEW SPLICES IAW DC-9 MM 20-50-1. (M)

Part: SWITCH — INOPERATIVE (ROW 8-13)

MYR - OVERHEAD EMERGENCY LIGHTS ROWS 8 TO 13 AND 16 TO 21 INOPERATIVE WHEN SWITCH IN COCKPIT IS PLACED TO 'ON'. EMERGENCY LIGHTS ARM AND CHARGE AND EMERGENCY LIGHTS CHARGING C/B'S PULLED. FOUND SWITCH ON OVERHEAD TO BE FAULTY. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH AND OPERATIONAL CHECKS GOOD. ALL IAW MM 33-53-0. (M)

Part: TIRES — FAILED (RT MLG)

MCO - FLT 216 - RIGHT INBOARD MAIN TIRE SEPARATED WITH SUBSEQUENT DAMAGE TO HYDRAULIC, ENGINE, AND FLAP SYSTEMS. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES IAW DC0 MM 32-40-00. REPLACED DAMAGED SECTION OF RIGHT FLAP TE IAW DC9 SRM 57-09, FIG 51-30 AND 51-61. REMOVED AND REPLACED DAMAGED HYDRAULIC LINES. REPAIRED 6 C-1 BLADES IAW PW MM 72-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FOUND EMERGENCY LIGHT IN CENTER CABIN INOPERABLE ON DAILY CHECK. REMOVED AND REPLACED FWD CENTER BATTERY PACK AS REQUIRED IAW DC-9 MM CHAPTER 33-53-0. (M)

Part: SWITCH — OUT OF ADJUST (LT MLG DOOR)

EWR - FLT 1600 - LEFT GEAR UNSAFE LIGHT ON WITH GEAR HANDLE IN UP POSITION. WHEN GEAR HANDLE IS IN DOWN POSITION, THE LIGHT GOES OUT. ADJUSTED LT GEAR DOOR POSITION SWITCH AW 32-60-3. (X)

Part: ARM — OUT OF ADJUST (LT MLG DOOR)

MYR - FLT 1606 - LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION ON TAKEOFF OUT OF EWR. ACCOMPLISHED PROCEDURES PER QRH. LIGHT EXTINGUISHED UPON LANDING AT MYR. FOUND ACTUATING ARM NOT MAKING LT DOOR POSITION SWITCH. ADJUSTED ARM AND VERIFIED PROPER OPERATION OF SWITCH. OPS CHECK GOOD IAW DC-9 MM 32-60-11. (X)

Part: SWITCH — OUT OF ADJUST (LT MLG DOOR)

CLE - FLT 1702 - LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF AT DTW WITH GEAR HANDLE UP. ACCOMPLISHED PROCEDURE IN QRH. RED LIGHT EXTINGUISHED UPON GEAR EXTENSION AT CLE. ADJUSTED LEFT DOOR POSITION SWITCH PER DC-9 MM 32-60-3. OPS CHECK GOOD. (X)

Part: WIRE — FAILED (NLG)

DTW - AIRCRAFT REQUIRED GEAR SWING FOR COMPANY TEST. UPON GEAR SWING, NOTED 'NOSE GEAR UNSAFE' LIGHT FLICKERS DURING EXTENSION AND RETRACTION. C/W GEAR SWING IAW DC-9 MM, CHAPTER 32-30. SYSTEM OPS CHECK NORMAL. NO DEFECTS NOTED. REMOVED AND REPLACED DEFECTIVE WIRE; SYSTEM GROUND CHECKED GOOD IAW DC-9 MM 32-60 AND 33-00. (X)

Part: LATCH ASSY — OUT OF ADJUST (RT MLG DOOR)

DTW - FLT 1703 - ON TAKEOFF AT CLE, RIGHT MAIN GEAR RED UNSAFE LIGHT STAYED ILLUMINATED. ACCOMPLISHED PROCEDURES PER QRH AND CONTINUED TO MYR WITH HYDRAULIC PUMPS ON HIGH. THE GEAR UNSAFE LIGHT EXTINGUISHED UPON GEAR EXTENSION AT MYR. (THREE GREEN ON AND ALL RED EXTINGUISHED). NORMAL HYDRAULIC PRESSURE AND QUANTITY THE ENTIRE FLIGHT. FOUND M-PIN (RT DOOR LATCH) OUT OF ADJUSTMENT. ADJUSTED RT MAIN GEAR DOOR LATCH ASSY. OPS CHECK DOOR. UNSAFE LIGHT IS EXTINGUISHED IN UP AND LOCK POSITION IAW DC-9 MM 32-31-4. (X)

Part: CONNECTOR — LOOSE (RT MLG)

MCO - FLT 503 - TAKEOFF DTW. RIGHT MAIN RED GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION ACCOMPLISHED PROCEDURE PER QRH. RE-SEATED LOOSE CONNECTOR ON RT MLG UPLOCK SWITCH. OPS CHECK GOOD IN UPLOCK POSITION IAW MM 32-31. (X)

Part: LIMIT SWITCH — FAILED (RT MLG)

DTW - FLT 506 - TAKEOFF MCO. RIGHT MAIN 'RED GEAR UNSAFE' LIGHT ILLUMINATED AFTER GEAR RETRACTION FOR ENTIRE FLIGHT. C/W QRH. REPLACED RIGHT MAIN GEAR UPLIMIT SWITCH. OPS CHECK GOOD IAW DC-9 MM 32-30. (X)

Part: WIRE — FAILED (RT MLG)

DTW - FLT 626 - RIGHT MAIN GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. FOUND SEVERAL FAULTY WIRES AT TERMINAL BLOCK 53-66. REPAIRED WIRES USING WIRING DIAGRAM MANUAL 32-61. OPS CHECK GOOD IAW DC-9 MM 32-60. (X)

Part: WIRE — FAILED (RT MLG DOWNLOCK)

DTW - FLT 511 - RIGHT MLG LIGHT WAS NOT ON DURING LANDING INTERMITTENTLY. THE LIGHT WOULD FLASH ON PRESS-TO-TEST INTERMITTENTLY. REPLACED WIRE IN RT MAIN DOWNLOCK HARNESS. INSPECTED SYSTEM. REPLACED RT MAIN DOWNLOCK SWITCH. SYSTEM CHECK GOOD IAW DC-9 MM 32-60. (X)

Part: COVER — MISSING (CABIN)

ACY - EMERGENCY FLOOR TRACK LIGHTING COVER (MID CABIN) OFF TRACK. INSTALLED EMERGENCY FLOOR TRACK LIGHTING COVER (MID CABIN) ON TRACK. (M)

Part: LOCKING MECH — FAILED (COCKPIT DOOR)

ACY - FLT 210 - COCKPIT DOOR LOCKING MECHANISM FELL APART IN FLIGHT. REPLACED COCKPIT DOOR MISSING LOCKING MECHANISM DOOR, OPS OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 655 - EMERGENCY TRACK FIRST ONE-QUARTER WILL NOT ILLUMINATE. REPLACED FAULTY FUSE IN FORWARD EMERGENCY TRACK LIGHTING BATTERY PACK. OPS CHECK GOOD PER DC-9 MM 33-50-0. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 655 - EMERGENCY TRACK FIRST ONE-QUARTER WILL NOT ILLUMINATE. REPLACED FAULTY FUSE IN FORWARD EMERGENCY TRACK LIGHT IN BATTERY PACK. OPS CHECK GOOD PER DC-9 MM 33-50-0. (X)

Part: RUDDER — DAMAGED (EMPENNAGE)

DTW - REMOVED RUDDER ASSEMBLY FOR REPAIR. INSTALLED NEW RUBBER IAW DC-9 MM 27-20-1. (M)

Part: RUDDER — DAMAGED (EMPENNAGE)

DTW - WHILE PERFORMING MAINTENANCE, THE DE-ICING VEHICLE THAT WAS BEING UTILIZED TO GAIN ACCESS TO THE RUDDER IMPACTED THE LEFT SIDE OF THE RUDDER CAUSING MAJOR DAMAGE. THE DAMAGE TO THE RUDDER CONSISTED OF A TEAR IN THE SKIN APPROXIMATELY 2.5 FEET IN LENGTH HORIZONTALLY BY 6 INCHES WIDE. THREE RIBS WERE CONTACTED RESULTING IN MAJOR DAMAGE TO THE RIBS. (M)

Part: EMERG LIGHTING — POPPED OUT (SEAT TRACK)

ACY - FLT 854 - EMERGENCY TRACK LIGHTING STRIP POPPED OUT OF SEAT TRACK FORWARD PART OF CABIN. REINSTALLED EMERGENCY TRACK LIGHTING STRIP AT FORWARD CABIN. OPS CHECK GOOD IAW MM 33-53-0. (M)

Part: CONNECTOR — LOOSE (RUDDER SWITCH)

FLT 210 - ACY - RUDDER TRAVEL UNCONTROLLED LIGHT ILLUMINATED IN CRUISE FLIGHT. EXTINGUISHED DURING DESCENT INTO ACY AT APPROX 290 KIAS OPERATED NORMALLY THEREAFTER. FOUND CONNECTOR LOOSE ON RUDDER REST LIMITER SWITCH. CHECK SYSTEMS IAW 27-20-13. NO DEFECTS FOUND. (M)

Part: WHEEL — DEFECTIVE (LT/RT NLG)

DTW - FLT 506 - NOSE WHEELS VIBRATE EXCESSIVELY AT HIGH SPEEDS 140-150 KNOTS. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL IAW MM CH 32-42. (M)

Part: TRAP PANEL — CRACKED (LEFT)

LEFT TRAP PANEL HAS CRACK INDICATIONS ALONG UPPER HORIZONTAL FLANGE BETWEEN AFT ATTACH BOLTS 3-4 AND 7-8 AND FORWARD BOLTS A-B AND AFT OF D. REF DC-9 SRM CHAPTER 57-09, FIG 6, SHEET 4. REPAIRED CRACKED PORTION OF LT FORWARD TRAP PANEL IAW DC-9 SRM 57-09, FIG 6, SHEET 4. POST NDT INSPECTION SHOWS NO FURTHER INDICATION OF CRACKS. INSTALLED REPAIR TO FUSELAGE LEFT TRAP PANEL UPPER AFT FLANGE IAW DC-9 SRM 57-09, FIG A. (M)

Part: SWITCH — MALFUNCTIONED (TAIL CONE)

FLT 423 - FLL - TAIL CONE UNSAFE LIGHT ON. DEFERRED TAIL CONE INDICATION IAW MEL 53-1, DMI NR 00088. TAIL CONE VISUALLY INSPECTED FOR SECURITY BY RSB. C-PLUG AT RELEASE HANDLE INSIDE IS COMING APART. REPLACED TAILCONE UNSAFE SWITCH. OPS CHECK GOOD ON GROUND IAW 52-70-0. THIS CLEARS DMI NR 00088. PLACARDS REMOVED. (M)

Part: WIRE — BROKEN (CABIN)

DTW - FLT 210 - CABIN EMERGENCY LIGHTS ARE OUT OF THE TRACK FLOOR BETWEEN ROWS 2 AND 7. FOUND BROKEN WIRE AT ROW 2 RE-CRIMPED, LIGHT TEST SHOWED NORMAL OPERATION IAW DC-9 MM 33-50. (M)

Part: AC CROSS TIE — LOCKED OUT (RIGHT)

DTW - FLT 1130 - APU GENERATOR FEEDER FAULT IN AIR WHICH CAUSED AC CROSS-TIE LOCK-OUT. NO INSTRUMENTS ON RIGHT SIDE. NO POWER TO RIGHT SIDE ELECTRICAL SYSTEM. RE-SET CROSS-TIE LOCK-OUT AND PERFORMED ELECTRICAL CHECK IAW DC-9 MM 24-20-0 PAGE 501. OP CHECKED NORMAL. (M)

Part: CSD — FAILED (NR 2)

MCO - FLT 301 - ON DESCENT COMPLETE LOSS OF RIGHT AC DISTRIBUTION SYSTEM CROSS-TIE LOCK-OUT. TRANSFERRED TO DMI NR 00072 PER MEL 24-1-1 CSD DISCONNECTED, GENERATOR SWITCH OFF PLACARD INSTALLED. REPLACED NR 2 CSD, IAW DC-9 MM 24-10-0. OP CHECKED GOOD. THIS CLEARS DMI NR 00072. PLACARDS REMOVED. (M)

Part: WINDOW — DELAMINATED (CAPT)

LOG PAGE NR 028273, ITEM NR P782. CLIMBING THROUGH 10,000 FEET, HEARD LOUD BANG. RT DV WINDOW APPEARED TO DELAMINATE AT FWD EDGE. RETURNED TO DTW. INSP F/O'S (CAPT) CLEARVIEW WINDOW AND FOUND ROUGH EDGE DELAMINATED ON FWD EDGE OF WINDOW, NO CORRECTIVE ACTION REQUIRED IAW DC-9 MM CH 56-00-0, CODE 1. CHECKED EXTERIOR OF AIRCRAFT AROUND SURROUNDING AREAS, NO DEFECTS FOUND. CLEARVIEW WINDOW LOCKING, LATCHING MECHANISM OPERATES NORMALLY, NO DEFECTS FOUND. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FORWARD RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPS CHECKS GOOD IAW 33-53-0. (M)

Part: RETRACT MECH — MALFUNCTIONED (SPOILERS)

SPOILERS FAILED TO DEPLOY ON TOUCHDOWN SMELL OF SMOKE OR BURNING INSULATION COMING FROM PEDISTAL. OPERATED SYSTEM FOUND AUTO SPOILER NOT RESETTING. FOUND NO DEFECTS ON ODOR. PLACED ON DMI PER MEL 27-19-1 CAT C. (M)

Part: BATTERY — DISCHARGED (CABIN)

FORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSEMBLY. OPS NORMAL IAW DC-9 MM CHAP 33. (M)

Part: WIRE — MISINSTALLED (CABIN)

LAST SIX FEET OF FLOOR TRACK LIGHTS IN CABIN, AND FLOOR TRACK LIGHTS IN TAIL CONE, NOT ILLUMINATING WHEN POT IN TEST MODE. SWITCHED CROSSED WIRES ON B5-27 AS REQUIRED. OPS CHECKS GOOD IAW DC-9 MM CHAPTER 33. (M)

Part: WIRE — CHAFED (RT ENGINE)

AT CRUISE, MCO-PHL, FIRE DETECTOR LOOP ANNUNCIATOR LIGHT AND RIGHT ENGINE 'B' LOOP LIGHT STARTED FLICKERING, COMPLIED WITH FCOM PROCEDURES. FOUND WIRES W255A16 AND W286A16N RUBBING TOGETHER. NO DAMAGE FOUND TO EXPOSED WIRES, REPAIRED WIRING IAW MM CHP 20. FIRE DETECTOR OP CHECKS GOOD. (M)

Part: SWITCH — INOPERATIVE (NLG)

NOSE GEAR DOWN 'GREEN' LIGHT FAILED TO ILLUNMINATE DURING GEAR EXTENSION. GEAR VERIFIED DOWN VISUALLY. LIGHT CAME ON DURING SECOND APPROACH. CONTACTS ON NLG UPLIMIT SWITCH INOP. REMOVED NLG UPLIMIT MICROSWITCH. OPS CHECK GOOD IAW MM 32. (M)

Part: BULBS — INOPERATIVE (CABIN)

FIRST TEN FEET OF FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BULBS AS REQUIRED. OP CHECKS GOOD. (M)

Part: DOOR — CORRODED (CARGO COMPT)

DURING C-CHECK, FOUND FOWARD CARGO COMPARTMENT DOOR STRUCTURE HAS SURFACE CORROSION AROUND SEVERAL RIV-NUTS. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)

Part: SEAT TRACK — CORRODED (BS 200-237)

DURING C-CHECK, FOUND SURFACE CORROSION BETWEEN STATION 200-237, SEAT TRACK AND FLOOR SUPPORT STRUCTURE. REMOVED CORROSION AND TREATED METAL IAW SRM 53-01-3, AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-05 PG 8P. (M)

Part: FLOOR — CORRODED (BS 160-200)

DURING C-CHECK, FOUND MAIN CABIN FLOOR HAS SURFACE CORROSION BETWEEN STATION 160 AND 200 LBL 12 - LBL 46. FABRICATED AND REPLACED FLOOR BOARDS AND TREATED METAL IAW SRM 51-10-4, 51-70-0, 51-10-3. (M)

Part: SKIN — CORRODED (RT ELEVATOR)

DURING C-CHECK, FOUND RIGHT ELEVATOR ABOVE OUTBOARD TRIM TAB ON ELEVATOR TRAILING EDGE SKIN BOTTOM CORRODED AND SEPARATED. TRIMMED AWAY EXCESS LAMINATED SHIM STOCK, REMOVED CORROSION AND TREATED IAW SRM 51-10-03. (M)

Part: ANGLE — CORRODED (BS 639)

DURING C-CHECK, FOUND STATION 639, 14R LONGERON, WINDOW LOWER FRAME 'L' SHAPE ANGLE HAS SURFACE CORROSION. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)

Part: LONGERON — CORRODED (BS 627)

DURING C-CHECK, FOUND STATION 627 LONGERON 14RH HAS CORROSION FROM SKIN TO SPLICE AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)

Part: SEAT TRACK — CORRODED (BS 200-237)

DURING C-CHECK, FOUND CORROSION AT STA 200-237, LBL 46 - RBL 56, ON SEAT TRACKS AND FLOOR SUPPORT STRUCTURE. REMOVED CORROSION AND TREATED METAL IAW SRM 53-01-3, AREAS WITHIN LIMITS. (M)

Part: FLOOR — CORRODED (BS 160)

DURING C-CHECK, FOUND SURFACE CORROSION ON CREW COMPARTMENT FLOOR PANEL AT STATION 160 LBL 12-RBL 12. REPAIRED FLOOR DOUBLER IAW SRM 53-05, FIG 2. REMOVED CORROSION AND TREATED METAL IAW SRM 53-10-3, AREA WITHIN LIMITS. (M)

Part: LONGERON — CORRODED (BS 639)

DURING C-CHECK, FOUND STATION 639, LONGERON 14R HAS SURFACE CORROSION FROM CLIP TO INTERCOSTAL AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)

Part: LONGERON — CORRODED (BS 617)

DURING C-CHECK, FOUND STATION 617 LONGERON 14 LEFT HAS SURFACE CORROSION FROM SKIN TO SPLICE AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)

Part: LONGERON — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT THE FOLLOWING STATIONS; STA 889 AND LONGERON 24LT TO 30LT, STATION 945 LONGERON 26LT TO 30LT, STATION 1030 LONGERON 26LT TO 27LT, STA 1129 LONGERON 29RT TO 30RT, STATION 1098 AND 113 FLOOR SUPPORT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. MATERIAL FOUND TO BE IN LIMITS. (M)

Part: FLOOR — CORRODED (GALLEY)

DURING C-CHECK, FOUND CORROSION THROUGHOUT THE GALLEY BOTTOM PANEL AND THE MAIN CABIN FLOOR. REMOVED CORROSION IAW SRM 51-10-3. FABRICATED DOUBLER AND INSTALLED, TREATED IAW SRM 51-01 AND SRM 51-10-3. (M)

Part: CHANNEL — CORRODED (BS 160-196)

DURING C-CHECK, FOUND FLOOR SUPPORT 'U' CHANNEL MAIN CABIN FLOOR AT STATION 160-196 LBL 46 HAS CORROSION. REPAIRED 'U' CHANNEL IAW SRM 51-01 FIG 2, TREATED METAL IAW SRM 53-01-3. (M)

Part: FLOOR — CORRODED (BS 120-218)

DURING C-CHECK, FOUND CABIN FLOOR FROM STATION 120-218 LBL 5 TO RBL 5 CORROSION. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)