N245FE

Part: ENGINE — FAILED (NR 2) · airframe 41,833 hrs · 33,069 cycles

WHILE ADVANCING POWER FOR TAKEOFF, AT 80 PERCENT N1 ON ENG NR 2. EPR SLOW TO INCREASE, COMPRESSOR STALL OCCURED. TOWER WITNESSED FLAMES FROM NR 2 ENGINE. R & R NR 2 ENGINE IAW WORK CARD 70T0002. INSTALLED ENGINE IAW WORK CARD 70T0002.

Part: BEAM — CORRODED (BS 312 S27L) · airframe 41,790 hrs · 33,029 cycles

HORIZONTAL WALKWAY BEAM HAS CORROSION AT BS 312 STR 27L. R & R HORIZONTAL WALKWAY BEAM. REF SRM 51-30-2.

Part: INDICATOR — FAILED (STANDBY ATTITUDE) · airframe 41,166 hrs · 32,492 cycles

STANDBY ADI PRECESSED 20 MIN. AFTER TAKE OFF, AT CRUISE. RECAGED BUT 2-3 MIN. LATER, PRECESSED AGAIN. 20-30 DEG RIGHT BANK, 10 DEG NOSE HIGH. REMOVED AND REPLACED STANDY BY ATTITUDE INDICATOR IAW MM 34-25-011-4. SYSTEM OPS CHECKED NORMAL. OK TO CONTINUE.

Part: SHEAR TIE — CORRODED (BS 950E) · corrosion level 2 · airframe 41,108 hrs · 32,429 cycles

SHEAR TIE CORRODED STA 950E BETWEEN STR 28L AND 29L. REMOVED SHEAR TIE REPAIR, FABRICATED NEW SHEAR TIE, FABRICATED NEW VERTICAL STIFFENER , HEAT TREATED PARTS TO T6 CONDITION AND INSTALLED IAW SRM 51-30- 2, 53-10-2, 51-10-1, AND 53-10-4.

Part: SKIN — DAMAGED (ZONE 600) · airframe 41,108 hrs · 32,429 cycles

RT WING INBD FOREFLAP, OUTBD END, PREVIOUS REPAIR IS GOUGED REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 57-50-11 FIG 1.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,108 hrs · 32,429 cycles

AFT CARGO COMPARTMENT, CORROSION AROUND FASTENERS IN STRINGER 30 AT BS 990. REMOVED CORROSION AND FOUND OUT OF LIMITS, FABRICATED NEW STRINGER SECTION, FABRICATED NEW SPLICE AND INSTALLED PARTS IAW SRM 51-10-6, 53-10-1, 51-30-2, 53-10-3, AND 51-30-5.

Part: FUEL TANK — DAMAGED (BS 744) · airframe 41,108 hrs · 32,429 cycles

DAMAGE AT STA 744 ON CTR TANK WEB RBL 60. REPAIRED CENTER TANK WEB IAW EA 7-5710-126825. REPAIR BY CUTTING OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW EA 7-5710-126825.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 41,108 hrs · 32,429 cycles

NR 5 SLAT HAS CRACKED RIB ON INBOARD SIDE OF ACTUATOR FORWARD MOUNT. REMOVED AND REPLACED RIBS WITH NEW RIBS IAW SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,108 hrs · 32,429 cycles

STRINGER 27L CORRODED STA'S 950F TO 1030 REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER SECTIONS. FABRICATED REPAIR SPLICES AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53-10-2 AND 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 41,108 hrs · 32,429 cycles

FWD PIT BS 720C BETWEEN STR 25L TO 26L SHEAR TIE CORRODED

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 41,108 hrs · 32,429 cycles

FWD PIT BS 720C BETWEEN ST 25RT TO 26RT SHEAR TIE CORRODED.

Part: FRAME — DAMAGED (BS 520) · airframe 41,108 hrs · 32,429 cycles

STATION 520 FRAME DAMAGED AT STRINGER 21L TO 26L. REMOVED DAMAGED FRAME, FABRICATED NEW FRAME, HEAT TREATED TO T6 CONDITION, AND INSTALLED PARTS IAW SRM 51-30-2, 53-10-2.

Part: SKIN — CRACKED (MLG DOOR) · airframe 41,108 hrs · 32,429 cycles

RMLG WING DOOR SKIN CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB 727-32-318 HFEC SHOWS AREA OF CUT OUT FREE OF CRACKS IAW NDTM 51-00-00 FIG 23 FABRICATED FILLER AND DOUBLER, ALODINED AND PRIMED PARTS IAW SRM 51-10-2 OPENED INNER SKIN PANEL IAW SB 727-32-318 INSTALLED REPAIR PARTS IAW EA 7-5280-127963 CLOSED PANEL IAW SRM 51-30-2

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,108 hrs · 32,429 cycles

SEAT TRACK CORRODED STA 690-720 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW ONE, REPAIR SPLICES, STRAP, AND INSTALLED REPAIR PARTS IAW 53-10-5 AND 53-10-2.

Part: SKIN — CRACKED (ZONE 500) · airframe 41,108 hrs · 32,429 cycles

LEFT MLG WING DOOR CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB B727-32-318 AND SRM 51-30-2 HFEC SHOWS AREA FREE OF CRACKS IAW NDTM 51-00-00 FIG 23 FABRICATED NEW FILLER AND DOUBLER IAW SB 727-32-318 ALODINED AND PRIMED PARTS IAW SRM 51-10-2 OPENED PANEL IAW SB 727-32-318 INSTALLED NEW PARTS IAW EA 7-5280-127969. CLOSED PANEL IAW SRM 51-30-2.

Part: STRINGER SPLICE — CORRODED (BS 950 S30) · airframe 41,108 hrs · 32,429 cycles

CORROSION ON STRINGER SPLICE AT STRINGER 30, BS 950. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE PN 69-44177-1 IAW SRM 51-30-2, AND 51-30-5.

Part: FITTING — CORRODED (BS 950) · airframe 41,108 hrs · 32,429 cycles

CORROSION ON STRINGER 29L KEELBEAM EXTENSION FITTING AT BS 950. FOUND OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PART NR 69-51272-1 IAW SRM 51-30-2 AND 53-10-1.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 41,108 hrs · 32,429 cycles

FORWARD CARGO DOOR, STA 520, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME AND INSTALLED NEW FABRICATED ONE IAW SRM 51-30-2, 51-20-1 AND DWG 53FX1350.

Part: SKIN — CRACKED (L1 DOOR) · airframe 41,108 hrs · 32,429 cycles

L-1 DOOR LOWER HINGE SKIN DOUBLER IS CRACKED. REPAIRED L-1 DOOR LOWER HINGE SKIN IAW EO 7-5330-7-2345 PART 2.

Part: FRAME — CRACKED (BS 560 S21-22L) · airframe 41,108 hrs · 32,429 cycles

FORWARD CARGO DOOR, STA 560, STRINGER 21-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME EXTENSION, FABRICATED NEW STUB FRAME, HEAT TREATED TO T-6 AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 41,108 hrs · 32,429 cycles

FORWARD CARGO DOOR, STA 500, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 41,108 hrs · 32,429 cycles

FORWARD CARGO DOOR, STA 540, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME, FABRICATED NEW ONE AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.

Part: FITTING — CORRODED (BS 950 S29R) · airframe 41,108 hrs · 32,429 cycles

CORROSION ON STRINGER 29 R KEEL BEAM EXTENSION FITTING AT BS 950. FOUND CORROSION ON FITTING OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PN 69-51272-2 IAW SRM 51-30-2 AND 53-10-1.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,108 hrs · 32,429 cycles

CORROSION ON SEAT TRACK FLANGE BS 1110-1116 LBL47. CORROSION ON SEAT TRACK OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-2, 53-10-5 AND 51-10-2.

Part: ANGLE — CRACKED (NR 3 SLAT ACT) · airframe 41,108 hrs · 32,429 cycles

NR 3 SLAT AFT LOWER ANGLE IS CRACKED AT ACTUATOR ATTACHMENT. UPON FURTHER INVESTIGATION SLAT REPAIR NOT FEASIBLE, SLAT REMOVED AND REPLACED.

Part: KEELBEAM — CRACKED (BS 875) · airframe 41,108 hrs · 32,429 cycles

LT W/W, LT KEEL BEAM IS CRACKED AT 2ND FASTENER STA 875, LBL 6. TRIMMED OUT CRACK DIMS 2 INCH X 1 INCH, FABRICATED DOUBLER, HEAT TREATED AND CADMIUM PLATED DOUBLER AND INSTALLED IAW EA 7-5310-127963.

Part: SPAR — CRACKED (LWS 118) · airframe 41,108 hrs · 32,429 cycles

LT WING FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. CUTOUT SECTION, FABRICATED NEW SECTION, FABRICATED WEB, FABRICATED 2 ANGLES, HEAT TREAT ANGLES IAW FASI ER 2-32153-801 REV. A, FABRICATED STRAP, 2 RADIUS FILLERS, LOCATED AND DRILLED NEW PARTS, ALODINED AND PRIMED AND INSTALLED IAW DRG SR27-57-038 REV C, REINSTALLED SPOILER FITTING IAW SRM 51-30-2

Part: SKIN — CRACKED (TE FLAP) · airframe 41,108 hrs · 32,429 cycles

RT WING INBD MID FLAP AFT LOWER ANGLE HAS 2 CRACKS, WBL 90. REMOVED R / WING I/B MID FLAP LOWER INNER SKIN PANEL IAW SRM 51-30-2. CUT OUT DAMAGE AREA ANGLE SECTION SRM 51-10-1 AND 51-40-4. FABRICATED REPAIR ANGLE AND SPLICE IAW SRM 57-50-2. TREAT AND PRIMED IAW SRM 51-10-2. INSTALL REPAIR PARTS AND INNER SKIN IAW SRM 51-30-2.

Part: ANGLE — CRACKED (RT WING) · airframe 41,108 hrs · 32,429 cycles

NR 6 SLAT AFT LOWER CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD REMOVED NR 6 SLAT COVE ACCESS PANELS IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED NEW ANGLE AND SPLICE IAW SRM 51-40-4 AND 57-50-2 FIG. 2. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. CLOSED COVE PANELS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (100) · corrosion level 2 · airframe 41,108 hrs · 32,429 cycles

SEAT TRACK CORRODED STA 560-620 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW TRACK, REPAIR SPLICES, STRAP, AND INSTALLED REPAIR PARTS IAW 53-10-5 AND 53-10-2.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 41,108 hrs · 32,429 cycles

PREVIOUS REPAIR AT STATIONS 970 TO 1010 STR 29L HAS FASTENERS WITH ZERO EDGE DISTANCE AT THE FORWARD END OF THE REPAIR. REPLACED PREVIOUS REPAIR AT STA 970-1010, S29R IAW EA NR 7-5330-127970.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 41,108 hrs · 32,429 cycles

RIGHT WHEEL WELL ANGLE CRACKED 870 BULKHEAD AND KEELBEAM. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-30-5 AND 51-30-2.

Part: SPAR — CORRODED (CENTER WING) · airframe 41,108 hrs · 32,429 cycles

LEFT LOWER FORWARD CENTER TANK SPAR CORRODED AT STA 744 LBL 20 TO LBL 30. REMOVED CORRODED SPAR, LOCATED AND DRILLED NEW SPAR AND INSTALLED IAW EA 7-5710-127966 AND SRM 51-30-5 AND SRM 51-30-2.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 41,108 hrs · 32,429 cycles

NR 1 ENGINE NOSE COWL AFT EXTERIOR SKIN OTBD SIDE AT 9 O'CLOCK POSITION. AFT T/E SKIN EDGE IS BENT OUT AND CRACKED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR AND FILLER AND INSTALLED REPAIR IAW SRM 54-30-3, 51-30-2, 51-10-1 AND 51-10-2.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 41,108 hrs · 32,429 cycles

FASTENER WITH ZERO EDGE DISTANCE IN MAIN CARGO DOOR DOUBLER STA 460 STR 27L. REMOVED EXISTING FASTENER, TRIMMED OUT AREA WITH A 2" RADIUS, TREATED AND PRIMED, INSTALLED FASTENER AND SEALED EDGE OF DOUBLER IAW EA 7-5330-126822. REPAIR DETERMINED TO BE MINOR IAW EA 7-5330-126822.

Part: SKIN — CRACKED (NR 3 NOSE COWL) · airframe 41,108 hrs · 32,429 cycles

NR 3 ENGINE NOSE COWL EXTERIOR SKIN CRACKED AND CHAFED AT T/E, APPX 4 O'CLOCK. CUT-OUT DAMAGE AREA IAW SRM 51-10-1 AND FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 54-30-3 FIG 3A.

Part: VERTICAL BEAM — DAMAGED (BULKHEAD) · airframe 41,108 hrs · 32,429 cycles

VERTICAL BEAM HAS FASTENERS WITH 0 SPACING BS 1183 LBL 17.8. REPAIRED BS 1183 BULKHEAD VERTICAL BEAM AT LBL 17.8 IAW EA NR 7-5310-127962. "BS 1183 BULKHEAD WITH INSUFFICIENT FASTENER SPACING AT LBL 20 BELOW WL190".

Part: WIRE HARNESS — BURNED (TE FLAPS) · airframe 40,736 hrs · 32,194 cycles

DURING CLIMB THROUGH 6,000 FT EXPERIENCED A PWR SURGE AND FOUND THE ALTERNATE FLAP MOTOR CIRCUIT BREAKERS (INBD AND OTBD) HAD POPPED. FOUND BURNED WIRE BUNDLE IN E&E COMPARTMENT, STILL TROUBLESHOOTING.

Part: INDICATOR — FAILED (AIRSPEED) · airframe 40,138 hrs · 31,782 cycles

CAPT'S AIRSPEED INDICATOR NOT WORKING. NO AIRSPEED INDICATION- AIARSPEED FLAG IN VIEW. REMOVED AND REPLACED CAPT'S AIRSPEED IND PER MM 34-12-021-4. AC OK TO CONTINUE.

Part: FLOORBEAM — CORRODED (BS 950) · airframe 39,064 hrs · 30,955 cycles

MCD STA 950 FLOORBEAM BETWEEN RBL0 -24 THE 4 NUT PLATES HAVE CORROSION BETWEEN THEM AND THE FLOORBEAM. CORROSION FOUND OUT OF LIMITS. REMOVED DAMAGED AREAS AND REPAIRED IAW SRZ27-53-033.

Part: FLOORBEAM — CORRODED (BS 540) · airframe 39,064 hrs · 30,955 cycles

FOUND CORROSION BETWEEN RBL 9 AND RBL 2 STA 540 FLOORBEAM, UNDERSIDE FWD PIT. REMOVED CORROSION, INSTALLED NEW FLOORBEAM AND SPLICES IAW SRM 51-40-4.

Part: SKIN — CORRODED (BS 1067-1070) · airframe 39,064 hrs · 30,955 cycles

FOUND SKIN CORRODED EXT FUSELAGE STA 1067 TO 1070 RBL 12, SKIN BULGE AT 3 FASTENERS STR 27R. REPAIRED FUSELAGE SKIN IAW SRM 53-30-3 FIG 3 STA 1067 - 1070 STR 29R.

Part: FLOORBEAM — CORRODED (BS 540) · airframe 39,064 hrs · 30,955 cycles

STA 540 LBL 9 FLOOR SUPPORT CORRODED FWD PIT REMOVED CORROSION FOUND OUT OF LIMITS. INSTALLED FLOOR SUPPORT AND REPAIR SPLICES IAW SRM 51-30-2 AND 53-10-5 FIG 4.

Part: STRINGER — CORRODED (BS 1062- 1119) · airframe 39,064 hrs · 30,955 cycles

FOUND STRINGER CORRODED EXT FUSELAGE STA 1071-1080 RBL10 STR 29 R 8 RIVETS DISHED IN EXT SKIN. PERFORMED STR REPAIR IAW SRM 53-10-3 FIG 1.

Part: SKIN — CORRODED (BS 1067-1070) · airframe 39,064 hrs · 30,955 cycles

EXTERNAL FUSELAGE STA 1067 TO 1070 RBL 12 SKIN BULGE AT (3) FASTENERS. REPAIRED FUSELAGE SKIN IAW SRM 53 -30-3 FIG3 STA 1067 - 1070 STR 29R.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 39,064 hrs · 30,955 cycles

FUSELAGE MAIN FRAME TAIL JACK FITTING DRILL START REPAIR, P/N 25FX990-45 COMPLY WITH EA 7-5310-101994. COMPLIED WITH EA 7-5310-101994 FUSELAGE MAINFRAME TALL JACK FITTING DRILL START REPAIR.

Part: SEAT TRACK — CORRODED (BS 948-958) · airframe 39,064 hrs · 30,955 cycles

MCD SEAT TRACK AT LBL 25, STA 948 - 958 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW 51-30-5. SEAT TRACK FABBED ON TRAVELER, T6/647796.

Part: SEAT TRACK — CORRODED (BS 950) · airframe 39,064 hrs · 30,955 cycles

MCD - SEAT TRACK SPLICE AT LBL 25, STA 950-950 PLUS 20" HAS CORRODED FASTENERS, EXFOLIATION BETWEEN PARTS REMOVED SPLICE ANGLES. REMOVED CORROSION, SPLICE ANGLES OUT OF LIMITS. FABBED NEW ANGLES BATCH NR 9R000776001. TREATED AND PRIMED NEW ANGLES, INSTALLED NEW SPLICE ANGLES IAW SRM 51-30-5, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-880) · airframe 39,064 hrs · 30,955 cycles

MCD, BL 0 SEAT TRACK BETWEEN STA 870 - 880 HAS CORRODED NUT PLATE HOLES, TOP AND BOTTOM SIDES OF TRACK. BLENDED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1,FIG 3. REMOVED SEAT TRACK IAW SRM 51-10-5, FABRICATED NEW SEAT TRACK ON TRAVELER T6/647662, LOCATED AND DRILLED IAW SRM 3-10-5. TREATED AND PRIMED AND INSTALLED NEW TRACK IAW 51-10-2 AND 53-10-5.

Part: SPAR — CRACKED (RT WING) · airframe 39,064 hrs · 30,955 cycles

RIGHT WING REAR SPAR UPPER CAP SURF STRIP HAS A CRACK AT SPOILER NR 11 STOPPED DRILLED CRACK. FABRICATED REPAIR PLATE AND REPAIR WASHERS, TREATED AND PRIMED, AND INSTALLED REPAIR IAW SRM 57-30-4, 51-10-2.

Part: SOLENOID — FAILED (MLG LOCK) · airframe 37,117 hrs · 29,416 cycles

PDIS 245 32-10 0006358 12OCT04 LAX CLOSE R LOGPAGES: 00900921 LANDING GEAR LEVER LATCH FAILED TO RAISE ON TAKEOFF PAST OFF POSITION. RAN QRH. CHECK/RESET LEVER LATCH CB (IAW QRH) AND PULLED AURAL WARNING CB (QRH) AND RETURNED.

Part: SUPPORT FITTING — CORRODED (CENTER WING) · corrosion level 2 · airframe 36,884 hrs · 29,244 cycles

CENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT FS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,884 hrs · 29,244 cycles

CENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT BS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1.

Part: MOTOR — LEAKING (TE FLAPS) · airframe 36,546 hrs · 28,966 cycles

DURING CLIMBOUT FROM EWR AT 25,000 FT CREW NOTICED A RAPID LOSS OF HYDRAULIC SYSTEM-A FLUID FOLLOWED PROPER CHECKLISTS AND RETURNED TO BASE. EVENTUALLY LOST ALL SYSTEM-A FLUID. FOUND HYDRAULIC FLUID POURING OUT OF CASE DRAIN OVERFLOW LINE FROM FLAP DRIVE MOTOR IN RT WHEEL WELL. REMOVED FLAP DRIVE MOTOR. REPLACED RT HYDRAULIC FLAP DRIVE MOTOR IAW M/M 27-51-062-4, OPS CHECKS GOOD. BECAUSE OF WRITE-UP, ALSO REPLACED BOTH NR 1 AND 2 ENGINE CASE DRAIN FILTERS IAW M/M 29-11-041-2. THERE WAS NO CONTAMINATION FOUND IN OLD FILTERS.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 36,021 hrs · 28,550 cycles

MDIS 245 53-30 0005255 27MAY03 BFM CLOSE R COMPLY WITH E.A. NR 7-5330-70910 FUSELAGE - MAIN CARGO-RE WORK OF ATTACHMENT HOLE (AD 2002-16-19). FACT 30 MAY 03 15:18 BFM R COMPLIED WITH E.A. 7-5330-70910 - FUSELAGE - MAIN CARGO - REWORK OF HINGE ATTACHMENT HOLE (AD2002-16-19).

Part: COMPRESSOR — STALLED (ANTI-ICE SYSTEM) · airframe 35,862 hrs · 28,413 cycles

UPON LEVELING AT FL310 WITH CRUISE POWER SET AND AFTER CLOSING ENGINE, ANTI-ICE COMPRESSOR STALLS. NR 2 ENGINE EPR DROPPED FROM 1.8 TO 1.2,EGT STARTING TO CLIMB, NR 2 THROTTLE TO IDLE. SLOWLY RESTORED NR 2 POWER AND CYCLED ENGINE ANTI-ICE BACK TO OFF, COMPRESSOR STALLS RE-OCCURRED, NR 2 THROTTLE BACK TO IDLE, OBSERVED 3 HARD COMPRESSOR STALLS, SHUTDOWN ENGINE IAW QRH. REMOVED AND REPLACED NR 2 ENGINE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON INTERNAL SKIN BS 1160, STR 30. R&R SKIN.

Part: RIB — CRACKED (VERTICAL STAB)

STR 5 LT IN VERTICAL STAB CRACKED AT NR 2 RIB FIN STA 6.37. R&R VERT STAB.

Part: SKIN — DAMAGED (VERTICAL STAB)

DRILL START DAMAGE IN VERTICAL STAB SKIN STR 5 LT, NR 2 RIB. R&R SKIN.

Part: STRINGER — CRACKED (FUSELAGE)

STR 1 HAS A CRACK ON LT WEB AT BS 480. R&R STR.

Part: STRINGER — CRACKED (FUSELAGE)

BS 478, STR 2 RT, L FLANGE EDGE CRACKED AND BENT. R&R STR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON INTERNAL JACK PAD FITTING, BS 1183, STR 3. R&R JACK PAD FITTING PER SRM 51-30-2.

Part: FASTENER — DAMAGED (FUSELAGE) · corrosion level 2

1 EA MISSING & 10 EA DISHED FASTENERS IN EXTERNAL FUSELAGE SKIN, BS 1168-1183 AT STR 30. R&R STR PER SRM 53-10-3 FIG 1.

Part: RIB — CRACKED (VERTICAL STAB)

RIB CRACKED IN VERTICAL STABILIZER LT STR 9, FIN STA 110.4. R&R RIB.

Part: SKIN — GOUGED (CARGO DOOR)

N 965 NR 1 LOWER CARGO DOOR HAS GOUGE ON INNER SKIN. R&R SKIN

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

N 926 CORROSION ON FLOORBEAM BS 344, RBL 5- LBL 65, WL 208 AT FASTENER HOLES. R&R UPR FLOORBEAM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION AROUND BROKEN FASTENER IN THE CREASE BEAM AT BS 1170, WL 208, RBL 61. R&R CREASE BEAM

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

N 676 CORROSION AROUND NUTPLATE HOLES ON LWR CHORD OF 1130 BEAM, LBL 1 TO LBL 38. R&R CHORD PER E.A. 7-5310-62713 & SRM 53-10-1.

Part: KEELBEAM — CORRODED (FUSELAGE)

KEELBEAM LOWER WEB IS CORRODED ON EDGE OF LIGHTENING HOLE AT BS 748. REMOVED AND REPLACED PER SRM 51-40-02.

Part: KEELBEAM — CORRODED (FUSELAGE)

KEEL BEAM LWR WEB IS CORRODED ON EDGE OF LIGHTNING HOLE AT BS 766. REMOVED AND REPLACED WEB PER SRM 53-30-1, 53-30-3.

Part: FRAME — CORRODED (BS 970)

NR 502 - WHILE WORKING NR 252 FOUND SHEAR TIE CORRODED AT BS 970, STR 29-30R, WL 156. REMOVED AND REPLACED CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 GAINED ACCESS IAW FEDEX SRM 53-10-4.

Part: STRINGER — CORRODED (BS 960-1007)

NR 252 - CORROSION LEFT KEEL BEAM BS 1000 IN POCKET OR U-SECTION. REMOVED DAMAGED SECTION OF STR 29L FROM BS 1007 TO 960 AND SPLICED NEW STR 29L SECTION PER FEDEX EA NR 7-5310-46997.

Part: SKIN — DENTED (BS 1070)

DENT ON EXTERNAL SKIN AT BS 1070, STR 19L. *S/D* REPAIRED SKIN IAW FEDEX SRM 53-30-3.

Part: SPLICE — CORRODED (BS 1005-1012)

CORROSION ON LT KEEL BEAM STRINGER SPLICE BS 1005-1012 O/B FLANGE (SPEC C53-113-01(2)). *S/D* LT KEEL BEAM STR SPLICE TO BE REPLACED ON NR 252.

Part: STRINGER — CORRODED (BS 675)

WHILE WORKING NR 233 FOUND CORROSION IN STR 27 RT, BS 675 (FWD BAY). *S/D* REPAIRED STR 27 RT, BS 668-680 IAW FEDEX SRM 53-10-3.

Part: BEAM — CORRODED (LT HORIZ STAB)

BULGE ON LT HORIZONTAL STAB LOWER T/E BEAM I/B END (C55-391-20-1). *S/D* REMOVED AND REPLACED LT HORIZONTAL STAB LWR T/E BEAM IAW FEDEX MM 55-30-021-4, 27-30-005-4, 27-30-01, 27-30-05, 27-30-001-4, 27-30-000-5, 27-30-001-5, FEDEX SRM 51-30-2, 51-30-5, 51-30-8.

Part: TIRE — FAILED (LT MLG)

98-234 - NR 1 TIRE MISS OFF A/C UPON LAND AT MEM. REMOVED AND REPLACED LEFT MLG LWR PISTON CYLINDER ASSY AND REPACK STRUT PER M/M 32-11-11. DUE TO NR 1 AXLE DAMAGE. REPLACE NR 1 TIRE AND BRAKE ASSY. REPLACE NR 2 TIRE ASSY AS PRECAUTION PER MM 32-42 AND 32-43. REMOVED AND REPLACED NR 1 ANTI-SKID XDUCER PER MM 32-44 AS PRECAUTION. ALL SYS OPS CKD NORM.

Part: ACCESSORY UNIT — FAILED (E/E COMPT)

LANDING GEAR LEVER FAILED TO RELEASE AFTER TAKEOFF. AIRCRAFT STUCK IN GROUND FLIGHT MODE. REMOVED AND REPLACED R92. COOLING FAN WORKED BUT LEVER LATCH WOULD NOT PULL. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER 32-09-122, OPERATIONAL CHECK NORMAL. LEVER LATCH PULLS FOR LANDING GEAR CONTROL.

Part: AXLE — SHEARED (NR 1 WHEEL)

DURING WALKAROUND INSPECTION, FOUND THE NR 1 WHEEL ASSEMBLY AXLE TO BE SHEARED AT THE AXLE NUT. TIRE AND WHEEL REMAINED INTACT ON AXLE. *S/D* REMOVED AND REPLACED MAIN LANDING GEAR INNER STRUT, NR 1 AND NR 2 TIRES AND BRAKES, NR 2 ANTI-SKID DETECTOR. SERVICED STRUT, BRAKES AND ANTI-SKID OPERATIONAL CHECK GOOD.

Part: FUEL CONTROL — MALFUNCTION (NR 2 ENGINE)

INFLIGHT, NUMBER 2 THROTTLE BINDING. PERFORMED NR 2 ENG THROT PULL CK, CKS GOOD. REMOVED AND REPLACED NR 2 ENG FUEL CNTRL AND FUEL DIFF PRESS SWITCH LEAK AND OPER CK GOOD PER M/M 73-21-0 AND JET RUN HDBK 6-39. PULL CK PER 76-11-0. INSP CABLE AND PULLEY IN ELEC EQUP COMP FWD AND AFT CARGO COMP AFT AIRSTAIR AREA FOR KINKS, FRAYED CABLES AND FREEDOM OF MOVEMENT, NO DEF NOTED. REMOVED AND REPLACED NR 2 ENG CROSSOVER SHAFT AND BEAR PER 72-61-10. RAN ENG AT HI PWR 4 MIN ALONG WITH MANY OTHER SETTING. EACH TIME POWER WAS REDUCED THE THROT RESPOND NORM. NOT AS IT HAD SPRUNG BK ON PREV RUNS. OK FOR SERVICE.

Part: GUSSET — CRACKED (BS 783.95)

NR 0526 002. LEFT STA 783.95 FRAME GUSSET CRACKED AT 2ND FASTENER HOLE ABOVE FLOOR LINE, APPROXIMATELY WL 210, UPPER LOBE ON INBD CHORD OF FRAME. FASTENER HOLE ENLARGED 4/32 O.S. (MAX) PER E.O. 7-5310-7-3367, PT 3. HFEC INDICATES CRACK STILL PRESENT. REPAIRED FRAME PER E.O. 7-5310-7-3367B, PT 9 BY INSTALLATION OF REPAIR/MOD KIT - TERMINATING ACTION ACCOMPLISHED (65C36280). GROUP 2 AIRPLANE.

Part: SKIN — CORRODED (BS 1060-1070)

NR 0319 001. BULGES IN BELLY SKIN STA 1060-1070, STR 28R-29R. REMOVED BULGED AND CORRODED SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG. 3 PGS. 12-14A.