N246FE

Part: SMOKE DETECTOR — FAILED (NR 6) · airframe 34,312 hrs · 27,726 cycles

DESCENT BELL SOUNDED MAIN FIRE LIGHT ILLUMINATED, SMOKE ILLUMINATED. EMERGENCY DECLARED. FUMES WERE PRESENT IN THE COCKPIT. ALL EMERGENCY QRH CHECKLIST ACCOMPLISHED. WHILE ENTERING A/C NOTICED NO ODOR OF ANY SORT, INSPECTED A/C FOR ANY SIGNS OF HEAT STRESS OR FIRE NONE FOUND, SUSPECT BAD SMOKE DETECTOR. REMOVED AND REPLACED NR 6 SMOKE DETECTOR OPS CHECKS NORMAL AS PER 727 M/M 26-16-001-4. A/C OK TO CONTINUE.

Part: RECEPTACLE — CRACKED (NR 3 PYLON) · airframe 33,941 hrs · 27,430 cycles

THREE RECEPTACLES DEFECTIVE ON NR 3 PYLON STRUCTURE WHERE PANEL 5402 MOUNTS TO PYLON. REPLACED THE DEFECTIVE RECEPTACLES AT PYLON PANEL 5502 MOUNT AREA. IAW 727-200 SRM 51-30-2. REINSTALLED PANEL 5502.

Part: BEAM — CRACKED (NR 3 CARGO DOOR) · airframe 33,806 hrs · 27,307 cycles

NR 3 CARGO DOOR, LWR BEAM CRACKED FWD END. REPAIRED IAW EA 7-5230-106835 PT1 REF WRI 52-30/8690.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,163 hrs · 26,787 cycles

ON TAKEOFF ROLL LED INDICATIONS WENT AMBER THEN BACK TO GREEN, AT 45-60 KTS WENT AMBER. TAKEOFF REJECTED.

Part: FRAME — CRACKED (BULKHEAD) · airframe 31,856 hrs · 25,703 cycles

RIGHT MLG WHEEL WELL 870 BULKHEAD I/B LWR SUPPORT FRAME IS CRACKED JUST I/B OF BLEED AIR SHUTOFF VALVE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

COMPLY WITH EO 7-5310-7-3367 PT 9 FOR CRACK IN 783.95 FRAME RT. *S/D* COMPLIED WITH EO 7-5310-7-3367 PT 9.

Part: SKIN — CHAFED (FUSLEAGE) · airframe 31,856 hrs · 25,703 cycles

FUSELAGE SKIN CHAFED STA 720D 12 STR 19L. *S/D* REPAIRED DAMAGED UPPER SKIN AT BS 720D PLUS 12 STR 19L PER SRM 53-30-3 DETAIL 2 & FED EX SR27-57-056 DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FRAME DAMAGED AT BS 1166, BETWEEN STRINGER 3 AND 4 RT. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1166 BETWEEN STR 3 & 4 IAW SRM 51-40-3.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

NR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TEAR STRAP AT STA 600 STR 9 RH PER SRM 53-30-4 FIG 9

Part: SKIN — BENT (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

AFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

CORROSION ON FWD FLANGE OF FRAME SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L. *S/D* REMOVED CORROSION ON FWD FLANGE OF FRAME SHEAR TIE STA 480 BETWEEN STR 27L AND 28L. REMOVED 021. 1 X 1 INCH FROM .063, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS FROM .071 7075.T6 LOT 562290, BAC1490-2865. ALODINED, PRIMED AND INSTALLED NEW SHEAR TIE, REPAIR PART IAW SRM 51-10-6, 51-30-02, 53-10-1, 53-10-4, FED EX MM 51-20-021-7, 51-20-151-7, FED-EX EA 7-5310-70677.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

CORROSION ON FLOORBEAM BS 312 WL 208 LBL 3-47 AT FASTENER AND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM STA 312, W/L 208, LBL 3-47, AT FASTENER & NUT PLATE HOLES, REMOVED 5 X 2 INCH LBL 3 FROM .090. LBL 4 4 X 2 X .0015 INCH. LBL 20 6 X 2 X .005 INCH, LBL 47, 3 X 2 X .0020 INCH, FOUND TO BE IN LIMITS. REMOVED 3 X 2 X .015 FROM .090, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS FROM BAC 1490-2730 7075- T6 .063 LOT 568596, FILLER 2024T3 .080 LOT 556309, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 51-30-02, FED EX SR 27-53-017A, FED EX MM 51-20-021-7, 51-30-151-7.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

CRACKED OUTER FRAME ANGLE STA 804.5 STR 14R. *S/D* REMOVED & REPLACED ANGLE AT BS 804.5 STR 14R PER SRM 51-30-2 & 51-10-1.

Part: FRAME — BENT (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FRAME BENT BS 950F AT STR 26 LT, AFT CARGO BAY. *S/D* FRAME DENT BS 950F AT STR 26 LT AFT CARGO FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FWD CARGO COMPARTMENT FRAME DENTED STA 500 BETWEEN STR 22L AND 23L. *S/D* REMOVED DAMAGE AREA OF FRAME BS 500 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

CRACKED STRINGER 15 RT BS 720B 4 INCHES. *S/D* REPAIRED STR 15R AT BS 720B 4 INCHES PER SRM 53-10-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IAW SRM 51-40-3 AND EA 7-5310- 70673.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

CRACKED STRINGER 15 LT AT BS 720B 4 INCHES. *S/D* REPAIRED STR 15L, BS 720B 4 INCHES IAW SRM 53-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2, 51-30-8.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LIMITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

N00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICATED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

N00636 CORROSION, ON KEELBEAM STR 29L .950F 3 ON FLANGE AROUND FASTENER. ** SD COMING **

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 53-10-3

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A.

Part: STRINGER — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

BS 848 STR 7R UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE AREA OF STRINGER 7 RT AT BS 848, FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & PER FED EX EA 7-5310-55358.

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

STRINGER DENTED AT BS 950 18, STRINGER 7 LT. *S/D* STR 7 LT ORIGINALLY FOUND OUT OF LIMITS (NO DENTS ALLOWED). REMOVED DENT BY BENDING EDGE OF STRINGER. MATERIAL LOSS A AS ALLOWABLE & STRINGER IS IN LIMITS PER SRM 53-10-1. ALODINED & PRIMED BLEND AREA PER FED EX MM 51-20-151-7.

Part: STRINGER — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

BS 848 STR 7L UPPER FLANGE OF STRINGER IS DENTED AND GOUGED. *S/D* REMOVED DAMAGE AREA OF STRINGER AT BS 848, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & FED EX EA 7-5310-55348.

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

DENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

STRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358

Part: STRINGER — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

DENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7-5310-55358

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

DENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

STRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

STRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358

Part: STRINGER — DENTED (FUSELAGE) · airframe 31,856 hrs · 25,703 cycles

DENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

STRINGER DENTED AT BS 950C 18, STRINGER 7 LT. *S/D* REPAIRED STR 7L BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358.

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

STRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **.

Part: STRINGER — DENTED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

DENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION (C53-224-01, 1) FLOORBEAM STRUCTURE BS 344 LBL 31 TO LBL 58 WL 208. *S/D* REMOVED AND REPLACED UPPER FLOORBEAM CHORD AND REPAIR ANGLES AT BS 344, LBL 65-RBL 16, WL 208 IAW SRM 27-53-007.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION BS 1090, STR 29 LT- 29 RT. CUTOUT SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION ON SKIN, AFT CARGO BAY BILGE NEXT TO O/B SIDE OF STR 28L BS 994 LBL 22 WL 136. REMOVED DAMAGED AREA OF SKINA T BS 994. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,856 hrs · 25,703 cycles

CORROSION AT FLOORBEAM BS 950D, LBL 10 DAMAGED, WL 208 (C53-224-01, 3). BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 31,006 hrs · 24,996 cycles

PASSING 17,000 FEET IN A NORMAL CLIMB BOTH HYDRAULIC SYSTEM "A" PUMP LOW PRESSURE LIGHTS CAME ON, FOLLOWED BY A COMPLETE LOSS OF SYSTEM "A" QUANITY. PERFORMED STABILIZERS EXECUTED CHECKLIST IAW QRH. DECLARED IFE AND LANDED UNEVENTFULLY AT IAH. INSTALLED NEW LINE ON 'A' SYSTEM PRESSURE TRANSMITTER.OPS. AND LEAK CHECK OK. REF: MM 29-11-00-6PG1B.OK FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 30,100 hrs · 24,265 cycles

FUEL HEAT ICING LIGHT ILLUMINATED ON ENG NR 3 APPROX 10-11000 MSL FOR ABOUT 1-2 MIN, THEN WENT OUT AND STAYED OUT. FUEL TEMP WAS +35DC. SUMPED ALL TANKS AND FOUND NO CONTAMINATION. FOUND FUEL FILTER PRESSURE SWITCH BACKSHELL EXTREMELY LOOSE AND WILL NEED TIGHTENING. REMOVED AND REPLACED CANNON PLUG BACKSHELL IAW 727-200 SMP'S NEEDS OPS CHECK, CANNON PLUG OPS CHECK GOOD. REMOVED AND REPLACED FUEL FILTER PRESS SWITCH FOR PRECAUTION IAW 727-200 M/M 73-14-021-4, LEAK CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NR 1 LE SLAT)

WITH FLAPS RETRACT AS A/C ACCEL THRU 270 KIAS, AMBER LEAD EDGE LIGHT ILLUM ON 2ND OFFICER AUXILIARY PNL AND A/C ROLL CONTROL WAS AFFECTED. ANTI ICE WAS ON. BELOW 250 KIAS ALL IND WERE NORM, FLAP EXTENSION AND LAND, ALL APPROPRIATE CK LIST WERE COMPLETE. *S/D* REMOVED AND REPLACED LEFT NR 1 LEAD EDGE SLAT ACTUATOR PER MM 27-81-32 OPER CK GOOD.

Part: HYD MOTOR — FAILED (TE FLAPS)

'A' SYSTEM HYDRAULIC FAILURE. INITIALLY WHEN AT FLIGHT LEVEL 270 THE INBOARD TRAILING EDGE FLAP INDICATOR WENT TO 5' WITH NO LEADING EDGE DEVICES OR ANNUNCIATOR LIGHTS. WHILE RAISING FLAPS WITH ALTERNATE FLAPS SWITCH THE 'A' SYSTEM WENT TO ZERO. FOUND INBOARD FLAP POWER UNIT HYDRAULIC MOTOR LEAKING DUE TO INTERNAL SHAFT SEAL SCREWS LOOSE. REMOVED AND REPLACED LEFT MOTOR. PURGED SYSTEM PER MAINTENANCE MANUAL 27-51-62. ALSO, REMOVED AND INSPECTED RIGHT MOTOR PER SUPPLEMENT 27-51-62 SERVICED 'A' SYSTEM TO FULL AND BLED SYSTEM. OPERATIONAL AND LEAK CHECK GOOD. OK FOR SERVICE CHECKED GOOD OK FOR SERVICE PER MAINTENANCE MANUAL 29-11-0 PAGE 601 1.C. INSPECTED HYDRAULIC SYSTEM 'A' FILTERS, CHECKED OK.

Part: HINGE FITTING — CORRODED (RT AILERON)

NR 0468 004, CORROSION ON RT WING O/B AILERON I/B HINGE ON AILERON, WBL 492.0, WSS 655.5. *S/D* REMOVED RT WING O/B AILERON, AND REMOVED I/B AILERON HINGE FITTING AND REPLACED. REINSTALLED AILERON AND FUNCTIONAL TESTED. ALL WORK IAW FED-EX M/M 27-10-31 AND 27-10-0.

Part: KEEL BEAM — CORRODED (BS 720)

NR 0169 001, CORROSION ON KEEL BEAM BS 720F TO 720F + 8, LBL 5, WL 148. *S/D* REPAIRED KEEL BEAM IAW FED-EX EA 7-5310-32963.

Part: KEEL BEAM — CORRODED (BS 720)

NR 0170 002, CORROSION ON KEEL BEAM AT BS 720F TO 720F + 5, RBL 5, WL 148. *S/D* REPAIRED KEEL BEAM IAW FED-EX EA 7-5310-32963.

Part: SKIN — CORRODED (BS 681-740)

NR 0260 003, CORROSION UNDER PRESSURE NUT PLATES ON INTERIOR OF SKIN AT BS 704 TO BS 734, RBL 6 TO LBL 6, WL 149. *S/D* REMOVED CORROSION UNDER NUT PLATES ON SKIN, MATERIAL LOSS OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED SKIN BS 704 TO 734, RBL 6 TO LBL 6, WL 149 IAW FED-EX SRM 53-30-3.

Part: POS TRANSMITTER — MALFUNCTIONED (TE FLAPS)

SPLIT FLAP ON T/O, ON RETRACT TO 5 OUTBOARD FLAPS STOPPED AT 15 INBOARD FLAPS TO 5. ACCOMP EMERGENCY PROCED FLAPS EXTENDED NORMAL TO 30 DEGREE AND RECOVERED AT IND. F/F O/B FLAP POS IND. RAN FLAPS, FOUND O/B NEEDLES SPLIT AND OUT OF BAND AT POSITION EO DEGREE. ADJ RT AND LT O/B FLAP POS TRANSMITTERS OPS CHECKS NORMAL. ALL WORK DONE AS PER MM 27-52-13.

Part: CONNECTOR — DIRTY (LT MLG DOOR)

LT MGD RED LIGHT REMAINED ON AFTER RAISING GEAR. ACCOMPLISHED RED PAGES PROCEDURES, LIGHT WENT OUT AFTER RECYCLING GEAR. LIGHT FLICKERED AGAIN IN CRUISE, SLOWED TO 270 KNOTS LIGHT CONTINUED TO FLICKER THROUGHOUT FLIGHT. FOUND PLUG FOR DOOR SWITCH UNLOCKED. CLEANED AND RESECURED TESTED PER MM 32-62-11.