N902DA

Part: LIGHT — BROKEN (AC BAY) · airframe 58,411 hrs · 31,766 cycles

FOUND EMERGENCY LIGHT BROKEN AT AFT TAILCONE OVERHEAD CATWALK. REMOVED AND REPLACED POWER SUPPLY AND BATTERY. OPERATION CHECKS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 56,495 hrs · 30,600 cycles

LIGHT SMOKE AND ODOR IN CABIN AFTER LANDING. INSPECTED BOTH ENGINES AND APU FOR CONTAMINATE. NONE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. ALL CHECKS OK.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 56,223 hrs · 30,426 cycles

AFT CARGO DOOR SILL BEAM CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-60-02, FIG 9.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 56,202 hrs · 30,416 cycles

LOWER FUSELAGE, AFT CARGO DOOR SILL BEAM CORRODED. REPAIRED.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 56,202 hrs · 30,416 cycles

TAILCONE RECEPTICLES WORN. REPLACED IAW SRM 51-30-02.

Part: SUPPORT FITTING — CORRODED (CARGO DOORWAY) · airframe 56,202 hrs · 30,416 cycles

LOWER FUSELAGE AFT CARGO DOOR CUTOUT FORWARD CORNER, SUPPORT FITTING CORRODED. NEW ANGLE INSTALLED IAW SRM 53-00-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,003 hrs · 30,298 cycles

AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK AND POWER SUPPLY AT ROW 27CDE. OPERATION CHECKS OK.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 54,733 hrs · 29,498 cycles

WHILE CLOSING THE L1 DOOR THE SLIDE DEPLOYED. R & R L1 DOOR SLIDE.

Part: WEB — CRACKED (VENTRAL STAIRS) · airframe 51,393 hrs · 27,414 cycles

TAIL INTERIOR VENTRAL STAIRS WEB CRACKED LT SIDE FORWARD OF SPRING LOCK MECHANISM. REPAIRED LT VENTRAL STAIRWAY SLANTED SIDE WEB IAW PRI AND ERA 523510-14, REV O.

Part: WEB — CRACKED (VENTRAL STAIRS) · airframe 51,393 hrs · 27,414 cycles

TAIL INTERIOR VENTRAL STAIRS WEB CRACKED RT SIDE JUST FORWARD OF SPRING LOCK MECHANISM. REPAIRED RIGHT VENTRAL STAIRWAY SLANTED SIDE WEB IAW PRI AND ERA 523510-14, REV O.

Part: DOOR — CRACKED · airframe 51,384 hrs · 27,409 cycles

CRACKS FOUND COMMON TO SLANTED SIDE WEB NEAR THE AFT END OF THE FIXED VENTRAL DOOR.

Part: STIFFENER — CRACKED (BS 1549) · airframe 51,384 hrs · 27,409 cycles

TAIL INTERIOR, STAIR WAY INTERCOSTAL, FWD DIAGONAL SUPPORT STIFFENER CRACKED, RT SIDE AT CANTED FRAME BS 1549. VERIFIED CRACK, R & R STIFFENER IAW DWG 9911946.

Part: STIFFENER — SEVERED (BS 1549) · airframe 51,384 hrs · 27,409 cycles

TAIL INTERIOR, LOWER SUPPORT CHANNEL SEVERED, RT SIDE AT CANTED FRAME, BS 1549 AT AND BELOW STAIRWAY INTERCOSTAL ATTACH POINT. R & R SUPPORT STIFFENER IAW DWG 9911992.

Part: FRAME — CRACKED (BS 1531) · airframe 51,384 hrs · 27,409 cycles

TAIL INTERIOR, FORWARD SIDE OF CANTED FRAME WEB CRACKED BS 1531, FROM UPPER ANGLE BETWEEN L8-9R. REPAIRS COMPLETE IAW PRI 52348-14, REV O.

Part: SKIN — CRACKED (BS 1531) · airframe 51,384 hrs · 27,409 cycles

FUSELAGE EXTERIOR SKIN CRACKED AT CANTED FRAME, BS 1531 LT SIDE. REPAIRED IAW SRM 53-00-01, FIG 6.

Part: LIGHT — MISSING (CABIN) · airframe 49,406 hrs · 26,266 cycles

DURING SERVICE CHECK, FOUND EMERGENCY PATHWAY LIGHTS MISSING SECTION BETWEEN ROW 27 AND 28 EDF. INSTALLED EMERGENCY LIGHT SECTION IAW EA 02-477506-03 REV A. ACFT OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,871 hrs · 25,947 cycles

DURING SERVICE CHECK, FOUND SEVERAL INOPERATIVE BULBS IN TAIL COMPARTMENT EMERGENCY LIGHT SIGNS. REPLACED LAMPS AS REQUIRED. OPS CHECKED GOOD.

Part: CLAMP — SEPARATED (LT A/C PACK) · airframe 48,580 hrs · 25,795 cycles

DIVERTED, DUE TO PRESSURIZATION ISSUES AT FL140. STARTED DESCENT TO 10,000. THE LT PACK SHOWED ZERO FLOW AND THE RT PACK WAS OPERATING NORMALLY AND SHOWING GOOD FLOW. THE CREW NOTICED THE FLOW LIGHT ILLUMINATED AND THE CABIN CLIMBING. MAINTAINED CABIN UNTIL LANDED. MX FOUND THE LT COALESCER BAG WATER SEPARATOR CLAMP SEPARATED. THE CLAMP WAS REPLACED. THE LEFT PACK LEAK CHECKED GOOD AND OPERATED NORMALLY. THE ACFT PRESSURIZED NORMALLY.

Part: STRUCTURE — CRACKED (TAILCONE) · airframe 47,978 hrs · 25,475 cycles

F/A REPORTED STRANGE NOISES FROM TAIL COMPARTMENT UPON ROTATION. SUSPECTED CATWALK DOES NOT RAISE PROPERLY WHEN AFT AIRSTAIRS ARE DOWN AND FELL TO THE DOWN POSITION. MX FOUND THE RT FLAP OF THE CATWALK DOESN'T STOW PROPERLY. WIRED THE CATWALK IN THE DOWN POSITION. REMOVED CRACKED MEMBER. STOP DRILLED CRACKED TO .246. HFEC INSPECTED. DAMAGE CONTAINED. FABRICATED REPAIR ANGLE, DRILLED, TREATED AND PRIMED PART. INSTALLED.

Part: STRUCTURE — OUT OF POSITION (TAILCONE) · airframe 47,718 hrs · 25,322 cycles

FLIGHT CREW REPORTED THAT AFT AIRSTAIR WILL NOT RAISE WITH STAIRS DOWN. MX FOUND CATWALK SIDES CATCHING ON CEILING CUTOUT. AFT VENTRAL STAIRS FORWARD TO MCO/PLAC IAW MEL 52-62-01. VERIFIED CATWALK DOWN AND SECURED.

Part: TIRE — FAILED (NR 2 MLG) · airframe 47,171 hrs · 24,994 cycles

NUMBER 2 MAIN LANDING GEAR TIRE BLEW ON ROTATION. INNER LOWER LEFT WING BUTT DOOR WAS RIPPED OFF LEFT WING. LEFT MAIN LANDING GEAR ANTI-SKID AND GROUND PROXIMITY HARNESS DAMAGED. EVIDENCE OF TIRE INGESTION IN LEFT ENGINE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CORROSION ON FRAME IN AFT CARGO COMP AT STA 1379 LNGR 28R TO LNGR 25L. CORROSION OF FRAME WAS FOUND OUT OF LIMITS. CORROSION ON SHEAR TIE FOUND OUT OF LIMITS. INTERCOSTAL HAD LIGHT CORROSION. LOCATED AND DRILLED FRAME AND SHEAR TIES, INSTALLED NEW FRAME AND SHEAR TIE. RE-INSTALLED INTERCOSTAL AND FRAME SUPPORT. TREATED, PRIMED AND PAINTED ALL PARTS REF SRM 51-30-02 REF AAR (N/R 861750).

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CORROSION FOUND ON SUPPORT BEAM UPPER CORD AT STA 1364 LBL 10 TO LBL 20. REMOVED CORRODED AFT FLOOR SUPPORT BEAM SECTION AND COMPLIED WITH ERA 498694-14 REV 0 FOR REPAIR.

Part: SUPPORT FITTING — UNKNOWN (RT MLG) · airframe 46,416 hrs · 24,595 cycles

INSPECT RT MLG ACTUATOR SUPPORT FITTING. REMOVED ACTUATOR, SUPPORT FITTING, BUSHING, AND BEARING. INSPECT (GVI) GEAR SUPPORT FITTING BEARING BORE AND BUSHING BORE. INSTALLED REPLACEMENT SUPPORT FITTING BEARING, BUSHING, AND SUPPORT FITTING. RE-INSTALLED ACTUATOR REF EA 02-093855-03 AD AND AD 2010-16-11.

Part: SUPPORT FITTING — UNKNOWN (LT MLG) · airframe 46,416 hrs · 24,595 cycles

INSPECT LT MLG RETRACT ACTUATOR SUPPORT FITTING. REMOVED ACTUATOR, SUPPORT FITTING, BUSHING, AND BEARING. INSPECT (GVI) GEAR SUPPORT FITTING BEARING AND BUSHING BORE 2EA. ITEMS GENERATED ON AAR N/R 862175 AND 862174 AND C/W. INSTALLED BEARING, BUSHING, SUPPORT FITTING, AND ACTUATOR. REF EA 02-093855-03AD AND AD 2010-16-11.

Part: SUPPORT BRACKET — DAMAGED (L1 DOOR) · airframe 46,416 hrs · 24,595 cycles

FWD ENTRY DOOR L-1 HOLD OPEN HOOK SHAFT SUPPORT BRACKET DAMAGED & EXTERNAL PREVIOUS REPAIR CHAFED. REMOVED & REPLACED HOLD HOOK SHAFT BRACKET, REMOVED & REPLACED EXTERNAL REPAIR IN REF WITH MD90 SRM 52-10-01 FIG 2 VOL 1.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT PRESSURE BULKHEAD DOOR JAMB AT LT AND RT LWR SIDE WITH CORROSION. REMOVED LT AND RT LOWER DOOR JAMB CHANNELS AND LOWER DOOR JAMB FOUND WITH TOTAL MATERIAL LOSS. CUT AND REMOVED AFT PASS DOOR JAMB FRAME IN REF WITH MD90 SRM 53-60-02 FIG 3. DRILLED AND INSTALLED REPAIR SPLICES AND NEW JAMB SECTION P/N 59174463-503 IN REF WITH MD 90 SRM 53-60-02 FIG 3 VOL I.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

LEFT SIDE FLOOR SUPPORT FROM STA 1364 TO 1402 LBL 24 WAS FOUND CORRODED AND OUT OF LIMITS. REPLACED WITH NEW FLOOR SUPPORT SRM 51-10-05 FIG 1 PG 2 VOL 2 (AAR NR 862385).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

RIGHT SIDE FLOOR SUPPORT FROM STA 1364 TO 1402 RBL 24 WAS FOUND OUT OF LIMITS. REPLACED FLOOR SUPPORT PER MD 90 SRM 51-10-05 FIG 1 (NR 862386).

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

DUE AT HMV/PSV CHECK, ERA 487631-14 REV A CODE 53-31. PERMANENT REPAIR TO FUSELAGE SKIN STA 1475 BTW 2L-3L CRACK. ACTL LN 2151. COMPLIED WITH ON N/R 862522.

Part: SLAT — GOUGED (RT WING) · airframe 46,416 hrs · 24,595 cycles

DURING INSTALLATION OF #0 RT SLAT NR 2 TRACK FOUND I/B FWD RIB FWD/LWR EDGE GOUGED. BLENDED GOUGE AT #0 RT SLAT NR 2 TRACK INBD RIB FWD LOWER EDGE AS PER MD-90 SRM 57-00-01 PG 3. NO CRACKS NOTED AS PER NDT S.P.M. 06-10-01-01-001 MAT LOSS .040 LENGTH 2.65 AT I/B SIDE FOUND LOBE WITHIN LIMITS AS PER MD-90 SRM 57-00-01 AND ERA 498700-14 PG 1-3. TREATED AND PRIMED AS PER MD-90 SRM 51-10-03 VOL ID REPAIR AS PER DPS 900-5-1 NO.4 (ERA 498700-14).

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

REMOVED CORRODED SKIN DOUBLER AT STA 826 LNGR 28R. FABRICATED NEW DOUBLER OF 7075-T6 .063 AND .071 7075-T6 TRIPLER PER MD90 SRM 53-30-01 PG 70 VOL 1. PERFORM HFEC TO EXISTING CUTOUT AND FASTENER HOLES AND THICKNESS CHECK TO VERIFY LENGTH OF DOUBLER BND AND SPM 06-10-01.001. TREATED AND PRIMED REPAIR AND AREA AS PER MD90 SRM 51-10-03. INSTALLED FASTENERS AS PER MD90 SRM 53-30-01 VOL II. WING TO BODY RIB REPAIR TO BE COMPLETED ON N/R 862678 (N/R 862414).

Part: SKIN — CRACKED (R1 DOOR) · airframe 46,416 hrs · 24,595 cycles

FWD GALLEY DOOR R-1 OUTER SKIN LOWER FWD CORNER BENT. CRACKED STOP DRILLED CRACK IN REF MD90 SRM 52-10-01 FABRICATED REPAIR DOUBLER IN REF WITH MD90 SRM 52-10-01 FIG 3. INSTALLED REPAIR IN REF MD90 SRM 53-10-01 FIG 3. REF AAR N/R 861595.

Part: FITTING — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT CARGO TIE FITTING HAS CORROSION AT STA 1376 LNGR23L. REMOVED FASTENERS AND CORROSION FROM TIE FITTING AND OUT OF LIMITS. DRILLED NEW FITTING P/N 3936440 AND INSTALLED PER MD90 SRM 51-30-01, 51-10-03, 53-00-01, AND 51-10-05. REF (N/R 862161).

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT CARGO COMP HAS CORROSION SPOT ON LNGR 30 FS 1300/1388. REMOVED CORROSION AT AFT CARGO COMP LNGR 30 BETWEEN 1300/1388 REF MD90 SRM 51-10-03. FOUND WITH IN LIMITS BETWEEN STA 1300/1379 AND OUT OF LIMITS BETWEEN STA 1379/1388 REF MD 90 SRM 53-00-01. REMOVED L30 FROM STA 1354/1388, ALSO REMOVED SPLICE BETWEEN STA 1344/1364 REF MD 90 SRM 51-30-02 & 51-30-05. LOCATED AND DRILLED AND INSTALLED L30 P/N 52912727 REF MD 90 SRM 51-10-03, 51-10-04, 51-30-02 & 51-30-05.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT CARGO HAS CORRSION ON LSTR 30 STA 1300-1388. REMOVED CORROSION ON LSTR 30 BETWEEN STA 1300-1388. OUT OF LIMITS FROM STA 1379-1388 REF MD90 SRM 53-00-01. REMOVED CORRODED SECTION STA 1354-1388 L STR 30. DRILLED NEW STR P/N 52912727. TREATED, PRIMED, AND TOP COATED REF MD90 SRM 51-10-03 & 51-10-04. INSTALLED REPAIR PER MD 90 SRM 51-30-02 & 51-30-05 (SRM 51-30-02).

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT CARGO FRAME STA 1344 FROM LNGR 27R TO 22L CORRODED. REMOVED SHEAR TIE FROM FRAME FROM LNGR 26L TO 26R. FABRICATED NEW SHEAR TIE REF DWG 9957739. INSTALLED NWE SHEAR TIE AT STA 1344 LNGR 26R TO 26L REF MD90 SRM 51-30-02. REF AAR N/R 862182 (SRM 51-30-05).

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB BETWEEN STA 1334 & 1364 CRACKED AT LIGHTNING HOLE OUTBD SIDE. REMOVED DAMAGED SECTION OF CUSP WEB BTWN STA 1334 & 1364 IN REF MD90 SRM 51-30-02 FIG 6. FABRICATED DOUBLER IN REF MD90 SRM 53-30-02. INSTALLED DOUBLER REPAIR ON CUSP WEB IN REF WITH MD90 SRM 53-20-02 FIG 6 CONFIG 7001.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB BETWEEN STA 1334 & 1364 CRACKED AT LIGHTENING HOLE OUTBD SIDE. REMOVED DAMAGE SECTION OF CUSP WEB BETWEEN STA 1334 & 1364 IN REF MD-90 SRM 51-30-02 FIG 6 FABRICATED DOUBLER REF WITH MD-90 SRM 53-30-02, INSTALLED DOUBLER REPAIR ON CUSP WEB IN REF WITH MD-90 SRM 53-20-02 FIG 6 CONFIG 7001. REF AAR N/R CARD 862337.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN RT CUSP WEB BETWEEN STA 1344 AND STA 1364 AT LIGHTENING HOLE EDGE CRACKED. REMOVED DAMAGE AND FASTENERS. FABRICATED DOUBLER, FILLER, AND INSTALLED REPAIR PARTS PER MD 90 SRM 53-20-02 FIG. 6.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

REMOVED EXISTING REPAIR BEAM STA 712 TO 731 AS PER MD90 SRM 51-30-04. FOUND TO BE OUT OF LIMITS AT STA 699 AND 744 AS PER MD90 SRM 53-00-01. AFTER FURTHER INSP, HOLE OF SHEAR FASTENERS TO BE ELONGATED. REPAIRED HOLES AS PER MD90 SRM 51-30-0 PG 1 INSTALLED FREEZE PLUGS AFTER OVERSIZING. INSTALLED NEW REPAIR AS PER MD90 SRM 53-60-02 (NR 861634).

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

REMOVED EXISTING REPAIR BEAM STA 712 TO 731 AS PER 51-30-04. FOUND TO BE OUT OF LIMITS STA 699 AND STA 744 AS PER MD90 SRM 53-00-01. AFTER FURTHER INSP, HOLE OF SHEAR FASTENERS TO BE ELONGATED. REPAIRED HOLES AS PER MD 90 SRM 51-30-00 PG 1. INSTALLED FREEZE PLUGS AFTER OVERSIZING. INSTALLED NEWREPAIR PARTS AS PER MD90 SRM 53-60-02 REF AAR N/R 861634 AND ERA 498685-14 (SRM 53-60-02).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

MAIN CABIN SEAT TRACK AT RBL 54.50 STA 452 TO 845 FOUND CORREDED & OUT OF LIMITS IN REF WITH MD90 SRM 53-40-01. FABRICATED SEAT TRACKS AT RBL 54.5 STA 452-845IN REF WITH DWG 5930565 SHT 1. INSTALLED SEAT TRACKS IN REF WITH MD90 AMM 53-42-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

MAIN CABIN SEAT TRACKS AT RBL 54.50, STA 452 TO STA 845 FOUND CORRODED & OUT OF LIMITS IN REF WITH MD 90 SRM 53-40-01. FABRICATED SEAT TRACKS AT RBL 54.50 STA 452 TO STA 845 IN REF WITH DWG 5930565 SHT 1. INSTALLED SEAT TRACKS IN REF WITH MD 90 AMM 53-42-01. REF N/R 862538.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CORROSION FROM STA 160 TO STA 200 LBL 10 ON CUSP WEB. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED WEB FROM 7075 T6 .020 AND DOUBLER FROM 7075 T6 .025. INSTALLED REPAIR PER MD 90 SRM 53-20-02

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB CRACKED AT STA 1136. REMOVED DAMAGE CUSP WEB. FABRICATED CUSP WEB IN REF DWG 9910151 SHEET 8. INSTALLED CUSP WEB IN REF MD90 SRM 53-20-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

FWD LWR CARGO COMPT DOOR JAMB FROM STA 389 - 427 FOUND AREAS CORRODED. CORROSION FOUND OUT OF LIMITS OF MD 90 SRM 53-00-01. CUT OUT DAMAGED LWR DOOR JAMB PER SRM 53-60-02. FABRICATED REPAIR SPLICE AND PARTS. INSTALLED REPAIR IAW MD-90 SRM 53-60-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB CRACKED AT STA 1136. REMOVED DAMAGED CUSP WEB FABRICATED CUSP WEB IN REF DWG 9910151 SHT 8. INSTALLED CUSP WEB IN REF MD90 SRM 53-20-02 REF N/R 862342 (53-20-02).

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

FWD CARGO COMP CORRODED AT INNER SKIN O/B OF L26L FWD OF STA 237. REPLACED SKIN AND DOUBLER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

FWD CARGO COMPT CORRODED AT INNER SKIN O/B OF L26L, FWD OF STA 237. REMOVED CORROSION ON INNER SKIN & LONGERON L26L & FOUND WEAR. REMOVED CORROSION OF FINGER DOUBLER & FOUND OUT OF LIMITS. REMOVED DAMAGED FINGER DOUBLER. FABRICATED NEW FINGER DOUBLER. INSTALLED FINGER DOUBLER AND INSTALLED REPAIR IN REF WITH MD90 SRM 53-31-03. REF AAR(N/R 862112)

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN RT CUSP WEB CORRODED AT STA 1079 TO STA 1098. REMOVED FASTENERS AND CUTOUT DAMAGED AREA. FABRICATED DOUBLER REPAIR PARTS. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR DOUBLERS REF AAR N/R 862366 (53-20-02 FIG 11)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB BETWEEN STA 962 TO 984 LIGHTENING HOLES CRACKED IN TWO PLACES. REMOVED FASTENERS AND CUTOUT DAMAGED AREA. FABRICATED DOUBLER REPAIRS. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR IN REF WITH MD90 SRM 53-20-02. REF AAR N/R 862345 (SRM 53-20-02).

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB BETWEEN STA 962 & STA 984 LIGHTNING HOLES CRACKED IN TWO PLACES. REMOVED FASTENERS & CUT OUT DAMAGED AREA FABRICATED DOUBLER REPAIRS, TREATED & PRIMED REPAIR PARTS. INSTALLED REPAIR IN REF WITH MD90 SRM 53-20-02. REF SRM 53-20-02 FIG 7.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN LT CUSP WEB BETWEEN STA 1079 AND STA 1098 CORROSION AROUND LIGHTENING HOLES. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUT OUT DAMAGE AND REMOVED FASTENERS. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED NEW PARTS. INSTALLED REPAIR DOUBLER. REF N/R 862336 (53-20-02 FIG 15).

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

RT CUSP MEMBRANE CORRODED AT STA 712 18R. REMOVED CORROSION, FOUND OUT OF LIMITS. CUT DAMAGED, FABRICATED REPAIR DOUBLER. TREATED AND PRIMED, TOP COAT NEW PARTS. INSTALLED REPAIR DOUBLER. REF N/R 862303.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN RT CUSP WEB AT STA 1280 AREA HAS EXFOLIATION CORROSION. REMOVED FASTENERS AND CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR TREATED & PRIMED NEW PARTS, INSTALLED REPAIR DOUBLER REF SRM 53-20-02 FIG 19 SHEET 1. REF AAR (N/R 862347).

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

CABIN RT CUSP WEB AT STA 1280 AREA HAS EXFOLIATION CORROSION. REMOVED FASTENERS AND CUTOUT DAMAGED AREA. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED NEW PARTS. INSTALLED REPAIR DOUBLER. REF N/R 862347 (53-20-02 FIG 19).

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

DURING REPAIR OF FLOOR WEB, FOUND CABIN FLOOR SUPPORT TRACK CRACKED FWD END RBL 6 FROM STA 148 TO STA 200. REMOVED AND REPLACED IT WITH A NEW SECTION OF TRACK FROM STA 148-STA 200. AS REF MD-90 SRM 51-10-05 & DWG 9936534. REF AAR N/R 862026.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

REMOVED FASTENERS TO GAIN ACCESS FOR REMOVAL OF CORROSION AT AFT CARGO COMPT LNGR 29R SPOTS FS 1345-1375 REF MR-90 SRM 51-30-02. FOUND OUT OF LIMITS, REF MD-90 SRM 53-00-01. FABRICATED NEW U-CHANNEL REF MD-90 SRM 53-10-01. TREATED PRIMED AND TOP COATED REWORKED AREA REF MD-90 SRM 51-10-03 & 51-10-04. INSTALLED FASTENERS, REF MD-90 SRM 51-30-02. REF N/R 962323.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

MAIN CABIN FLOOR SUPPORT BEAM AT STA 1364 LBL 24 TO RBL 24 CORRODED AT UPPER AND LOWER CHORD. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR PER ERA 498694-14.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT CARGO HAS TRIANGLE DOUBLER CORRODED AT AFT CARGO STA 1395. AFT PRESSURE BULKHEAD CTR LWR FWD FACE REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS 51-10-03. LOCATED AND DRILLED NEW TRIANGLE DOUBLER 51-10-05 AND INSTALLED NEW DOUBLER 51-30-05. REF AAR(N/R 862111)

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

AFT CARGO HAS TRIANGULAR DOUBLER CORRODED AT AFT CARGO STA 1395 AFT PRESSURE BULKHEAD CTR LOWER FACE. REMOVED DOUBLER, THEN REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS PER MD90 SRM 51-10-03. LOCATED AND DRILLED NEW DOUBLER PER MD90 SRM 51-10-05, AND RE-INSTALLED NEW DOUBLER PER MD 90 SRM 53-30-05.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

REMOVED CORRODED DOUBLER FABED NEW DOUBLER & TRIPLER MAT USED 7075-T6 .063 DOUBLER & 7075T6 .071 TRIPLER IAW MD-90 SRM 53-30-01 PG 70. PERFORMED HFEC TO EXISTING CUTOUT & FASTENERS HOLES & THICKNESS CHECK TO VERIFY LENGTH OF DOUBLER IAW BND&SPM 06-10-01 001, TREATED & PRIMED REPAIR AND AREA AS PER MD-90 SRM 51-10-03. INSTALLED FASTENERS REF AS PER MD-90 SRM 53-30-01 VOL II WING TO BODY RIB REPAIR TO BE COMPLETED ON N/R.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,416 hrs · 24,595 cycles

FOUND CORROSION AT AFT CARGO FRAME STA 1364 BETWEEN L30 AND L29R. REMOVED CORROSION AND OUT OF LIMITS PER MD 90 SRM 53-00-01. REMOVED DAMAGED AREA AND REPAIRED PER MD 90 SRM 53-10-02 VOL I.

Part: BOTTLE — BLOWN (EVAC SLIDE) · airframe 46,003 hrs · 24,389 cycles

THE 1L SLIDE BOTTLE BLEW WHEN SHUTTING CABIN DOOR FOR PUSHBACK, SLIDE DID NOT DEPLOY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,277 hrs · 23,557 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE AT ROW 24. MAINTENANCE FOUND PATHWAY NEEDS LIGHT ASSEMBLY AND BULB. FORWARD TO MCO AND PLACARD PER MEL 33-51-01A.

Part: ACOUSTIC LINER — DEPARTED (THRUST REVERSER) · airframe 43,788 hrs · 23,368 cycles

FLIGHT CREW DIVERTED, DUE TO REPORTS OF DEBRIS ON DEPARTURE RUNWAY OUT OF MSP WHICH "MAY HAVE COME OFF OF OUR JET". DEBRIS IDENTIFIED AS ACOUSTICAL LINER AND ACFT WAS THE LAST TO DEPART. MX FOUND ACOUSTIC MATERIAL MISSING ON THE NR1 ENGINE THRUST REVERSER. UPPER REVERSER HALF REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,455 hrs · 23,231 cycles

FUSELAGE RT SKIN TAIL SECTION FS 1494, L-2R TO L-3R REPAIRED IAW ERA 487196-14.

Part: SKATE ANGLE — DAMAGED (FUSELAGE) · airframe 43,455 hrs · 23,231 cycles

FUSELAGE RT DORSAL TO FUSELAGE ATTACH SKATE ANGLE SPLICE REPAIR PER ERA 487528-14.

Part: SKATE ANGLE — DAMAGED (FUSELAGE) · airframe 43,455 hrs · 23,231 cycles

FUSELAGE LT DORSAL TO FUSELAGE ATTACH SKATE ANGLE SPLICE REPAIR PER ERA 487507-14.

Part: SKIN — CRACKED (BS 1475 L2-3L) · airframe 43,455 hrs · 23,231 cycles

A CRACK WAS FOUND ON THE 5911432-81 SKIN PANEL AT STA 1475 BETWEEN LONGERON 2 LT AND 3 LT SKIN IS 2024-T3 (DLM90103296)

Part: SKIN — CRACKED (BS 1475 L1-2R) · airframe 43,455 hrs · 23,231 cycles

A CRACK WAS FOUND UNDER THE PREVIOUSLY INSTALLED DOUBLER AT STA 1475 LONGERON 1 AND 2 RT. NEW CRACK WAS TRIMMED OUT AND DOUBLER ENLARGED TO REPAIR BOTH SKIN CUT-OUTS.

Part: SKIN — CRACKED (BS 1475 L2L) · airframe 43,455 hrs · 232,311 cycles

A CRACK WAS FOUND IN LONGERON 2 LT AT STA 1475. THIS CRACK FOUND DURING INSP OF TAIL AREA, AFTER FINDING FUSELAGE SKIN CRACKS AT STA 1494 BOTH LT AND RT SIDES. A NEW SECTION OF LONGERON WAS FABRICATED AND A SPLICE MADE IAW ERA.

Part: SKIN — CRACKED (BS 1494 L3R) · airframe 43,455 hrs · 23,231 cycles

THE RT AFT FUSELAGE SKIN AT STA 1494 ABOVE LONGERON 3 RT AND JUST BELOW THE VERT STAB SKATE ANGLE WAS FOUND CRACKED. LENGTH OF CRACK APPROX 3.5 ". A REPAIR DOUBLER AND STRUCTURAL SHIM WERE INSTALLED.

Part: SKIN — CRACKED (BS 1494 L2-3L) · airframe 43,455 hrs · 23,231 cycles

THE LT SKIN AT STA 1494 BETWEEN LONGERON 2LT AND 3LT WAS FOUND CRACKED APPROX 3" LONG. DURING INSP IAW ERA 487106-14. DURING OPEN HOLE INSP MORE CRACKS WERE DETECTED AND A SECTION VERT STAB SKATE ANGLE WAS REMOVED. FINAL TRIM-OUT SIZE 4.3" X 5"A .063" DOUBLER AND A STRUCTURAL SHIM WERE INSTALLED. FOR VERT STAB SKATE ANGLE REPAIR.

Part: COALESCER BAG — DIRTY · airframe 41,343 hrs · 22,161 cycles

CABIN EXUDES STRONG EXHAUST FUMES REPORTED BY INBOUND CREW. CHECKED RECIRC FAN AND FILTER ALL OK REPLACED LT AND RT WATER BAGS LEAK CHECKS OK RAN PACKS NO ODOR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,326 hrs · 21,617 cycles

CORROSION ON FUSELAGE SKIN AT FS 826 LONGERON 29 AND 30 RT. REPAIRED PER ER/A 476999-14 REV 0.

Part: FITTING — DAMAGED (PYLON) · airframe 35,912 hrs · 19,096 cycles

NR 1 AND NR 2 PYLON AFT TORQUE BOX BACK UP FITTING REPAIRED IAW ERA 465731-14.

Part: VIDEO MONITOR — SMOKE (CABIN) · airframe 35,900 hrs · 19,089 cycles

VIDEO MONITOR AT 19 A/B BEGAN SMOKING. REPLACED MONITOR AT 19AB CKS OK. INSPECTED AREA, NO ABNORMAL CONDITIONS NOTED.

Part: CONVERTER — INOPERATIVE (NR 1 ENGINE) · airframe 31,489 hrs · 16,596 cycles

LEFT ENGINE GEN FAILED AFTER TAKEOFF. REPLACED NR 1 ENGINE GEN CONVERTOR UNIT. GEN CHECKED OK.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,009 hrs · 16,324 cycles

LOWER SURFACE OF FUSELAGE SKIN STA 826-864, L-28R-29R WAS FOUND WITH CORROSION. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER ER/A 386336-14.

Part: TIRE — FAILED (MLG) · airframe 31,005 hrs · 16,323 cycles

REPLACED 2 TIRES AND BOTH DACMS. REPAIRED DAMAGE.

Part: CABLE — FRAYED (SEAT) · airframe 29,961 hrs · 15,772 cycles

SEAT CABLE SPARKING AT SEAT LEG. FOUND CABLE FRAYED. REPLACED SAME.

Part: BOTTLE — UNSERVICEABLE (CREW) · airframe 29,735 hrs · 15,672 cycles

CREW OXYGEN PRESSURE DROPPED TO ZERO ON CLIMB. REPLACED CREW OXYGEN BOTTLE AND REGULATOR. NO LEAKS.

Part: FAN — SHORTED (CABIN) · airframe 26,976 hrs · 14,281 cycles

SMOKE AND FUMES IN CABIN, TURNED OFF RIGHT PACK AND GALLEY POWER SMOKE STOPPED. FOUND J9 C/B POPPED ON RECIRCULATION FAN. REPLACED SAME.

Part: TRANSMITTER — CORRODED (ELEVATOR) · airframe 24,285 hrs · 12,960 cycles

PYLON FLAP FAULT EOAP MESSAGE ILLUMINATED AT 100KTS ON TAKEOFF ROLL. AIRCRAFT TAKEOFF REJECTED AND RETURNED TO BLOCK AT GATE C-10. FOUND LEFT ELEVATOR POSITION SENSOR OUT OF RIG AND CAUSING INTERMITTENT ILLUMINATION OF PYLON FLAP FAULT. REPLACED SENSOR PER AMM. PERFORMED ADJ/TEST AND RETURN TO SERVICE TESTS. ALL CHECKED GOOD. OK FOR SERVICE.

Part: BRAKE ASSY — FIRE (MLG) · airframe 22,122 hrs · 11,883 cycles

NR 2 BRAKE OVERHEAT ON ARRIVAL SOME FLAMES. COOLED BRAKES, NO FLAMES. REPLACED BRAKE ASSY AND NR 2 MAIN WHEEL ASSY. PERFORMED BRAKE TEMP SENSOR TEST, TESTS OK. NO LEAKS FOUND.

Part: GENERATOR — LACK OF LUBE (NR 2 ENGINE) · airframe 22,066 hrs · 11,852 cycles

RT AC POWER FAULT WITH R GEN OIL PRESS LIGHT DURING CLIMBOUT. FOUND RT GEN OIL LEVEL LOW. SERVICED SAME. RUN ENG PER PFHB AND NO LEAK. GEN OPS OK.

Part: JACKSCREW — CORRODED (HORIZONTAL STAB) · airframe 18,355 hrs · 9,936 cycles

HORIZONTAL STAB JACKSCREW FAILED OPEN 5936AD INSPECTION. LIGHT CORROSION FOUND ON LOWER 4 THREADS OF JACKSCREW CA: REPLACED JACKSCREW ASSY

Part: TRANSDUCER — FAILED (ANTI-SKID SYSTEM) · airframe 17,959 hrs · 9,708 cycles

LEFT OUTBOARD MLG TIRE BLOWN OUT DURING LANDING. MAX AUTOBRAKES WERE USED. UPON BLOWING TIRE DESELECTED AND DISC ABS. LEFT OAP SHOWED LEFT OUTBOARD AND ANTISKID FAULT. TAXI CLEARED AND TOWED TO RAMP. REPLACED NR 1 ANTISKID TRANSDUCER AND CONTROLLER.

Part: BULB — MISSING (CABIN) · airframe 16,964 hrs · 9,180 cycles

EMERGENCY TRACK LIGHTING IN FIRST CLASS IS MISSING LIGHT AND LIGHT COVER. RELAMPED AND REPLACED COVER, OPS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 16,106 hrs · 8,727 cycles

AFT EMER OVERHEAD LIGHTS FLICKERED THEN WENT OUT. REPLACED BATTERY PACK AND PWR SUPPLY.

Part: CONTROL CABLE — WORN (TAIL) · airframe 15,814 hrs · 8,566 cycles

ON A/C 9202 SAMPLE VISIT, THE ELEVATOR STANDBY INDEX CABLE WAS FOUND TO BE RUBBING AND WORN AT TWO LOCATIONS, AT A RUB BLOCK ON TOP OF THE RIGHT AIR CONDITIONING DIVERTER VALVE AND AT A MICARA RING JUST AFT OF THE RUB BLOCK. CORRECTION WAS TO REPLACE THE "Z" ANGLE THAT SUPPORTS THE RUB BLOCK WITH A ANGLE THAT WAS WITHIN DESIGN LIMITS AND TO LOWER THE RING PER ERA 3344405-14.

Part: WIRE — BROKEN (CEILING)

EMERGENCY LIGHTING CEILING INOP. FOUND BROKEN WIRES IN CEILING REPAIRED WIRES. OPS NORMAL.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L1 DOOR SLIDE REMOVED FOR DOOR MTC AND SLIDE COVER LATCH WOULD NOT RELEASE AND AFTER SLIDE COVER OPENED FOUND PIN PULLED OUT. REPLACED SLIDE PACK.

Part: SKIN — GOUGED (BS 297-313)

FUSELAGE SKIN FS 297-313 L-23R, DENT/GOUGE REPAIR. THE FUSELAGE SKIN AT LONGERON 23R WAS GOUGED AND DENTED BETWEEN FS 297 AND 313. THE DAMAGED AREA OF SKIN WAS CUTOUT WITH A 28 LONG BY 2 WIDE CUTOUT. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER THE GUIDELINES OF MD-90 SRM 53-30-01, FIG 2 AND ER/A 366348-14.

Part: GENERATOR — OIL LEAK (NR 1/2 ENGINE)

DURING CRUISE, RT AS POWER FAULT ILLUMINATED ALONG WITH OIL PRESSURE FAULT. STARTED APU, THEN LEFT GENERATOR AC POWER FAULT CAME ON WITH LEFT GENERATOR AND OIL PRESSURE STATUS LIGHT, THEN LEFT GENERATOR TRIPPED OFF LINE. LANDED EWR, FOUND BOTH GENERATORS WITH LOW OIL, EVIDENCE OF LEAKAGE IN ENGINE COWL. SERVICED GENERATORS AND FOUND LEFT GENERATOR FILTER BOWL HOUSING CRACKED AND THE RT GENERATOR PRESSURE SERVICING PORT LEAKING. REPLACED BOTH GENERATORS.