N147FE

Part: FLOOR PANEL — GOUGED (UNKNOWN) · airframe 10,547 hrs · 4,901 cycles

MAIN DECK CARGO FLOOR PANEL DAMAGED AT STA. 1137 AND 3 INCHES LEFT OF CENTER. REF WRI 25-50 5384 AND SEQ 150 OF WORK ORDER 86663. FABRICATED AND INSTALLED NEW FLOOR PANEL. REF SRZ -25-005 REV. R AND B767 AMM 53-01-06-4. ALSO SEE WRI # 25-50/5384 AND SEQ.150 OF W/O 86663. THIS IS A MAJOR REPAIR.

Part: FORMER — CRACKED (ZONE 600) · airframe 9,129 hrs · 4,217 cycles

L/E EDGE FORMER CRACKED AT STATION 499 R/H WING MARKED WITH TAPE 0000493008 : CRAIL, ROGER L - 19-AUG-2022 01:16 REPLACED FORMER AS REQUIRED. REF E.A TH-5720-T0370175 P1

Part: FORMER — CRACKED (ZONE 600) · airframe 9,129 hrs · 4,217 cycles

L/E EDGE FORMER CRACKED AT STATION 441 R/H WING MARKED WITH TAPE. REPLACED FORMER AS REQUIRED PER EA H-5720-T0370175.

Part: SENSOR — INOPERATIVE (LE FLAPS) · airframe 7,213 hrs · 3,317 cycles

AFTER NORMAL TAKEOFF AND COMPLETING AFTER TAKEOFF CHECKLIST WE WERE CLIMBING THROUGH 11,000' WHEN WE RECEIVED A CAUTION AND LE FLAP DISAGREE EICAS MESSAGE WITH BOTH FLAP INDICATORS SHOWING BETWEEN UP AND 1. A FEW TIMES THEY MOMENTARILY RETURN TO UP BUT THEN RETURN TO BETWEEN UP AND 1 WHERE IT EVENTUALLY STAYED. COMPLIED WITH QRH, DECLARED AN EMERGENCY AND COMPLETED AIR-TURNBACK. REMOVED & REPLACED LEADING EDGE SLAT SENSOR S294 #12 OUTBOARD. REF. AMM 27-88- 01-2. OPS CHECKS GOOD. NO DEFECTS NOTED.

Part: STIFFENER — CRACKED (BS 246) · airframe 5,879 hrs · 2,670 cycles

MAIN CABIN FLOOR BEAM AT STA 246 HAS 1 EA VERTICAL STIFFENER ANGLE CRACKED AT LBL 50. REMOVED AND REPLACED CRACKED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV.

Part: STRAP — CRACKED (RT WING LE) · airframe 5,879 hrs · 2,670 cycles

RIGHT WING LES 508 LEADING EDGE NOSE STRAP CRACKED. REMOVED AND REPLACED RIGHT WING LES 508 NOSE STRAP, PER B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C.

Part: SHEAR TIE — CRACKED (NR 2 NACELLE) · airframe 5,879 hrs · 2,670 cycles

NR 2 PYLON INBOARD WING FITTING CLIP IS CRACKED ON FWD END. REMOVED AND REPLACED SHEAR TIE P/N 313T3310-1156, IAW BAC DWG 313T2310 REV AND B767 SRM 51-40-02.

Part: FORMER — CRACKED (RT WING) · airframe 5,879 hrs · 2,670 cycles

RIGHT WING LES 490 APPROXIMATELY LEADING EDGE NOSE FORMER CRACKED. REMOVED CRACKED FORMER AND INSTALLED NEW FORMER PN 114T2511U14.

Part: FORMER — CRACKED (RT WING LE) · airframe 5,879 hrs · 2,670 cycles

RIGHT WING LES 560 LEADING EDGE NOSE FORMER ANGLE CRACKED. REMOVED CRACKED FORMER AND INSTALLED NEW FORMER P/N 114T2512U14, REF BAC DWG 114T2162 REV.

Part: FORMER — CRACKED (LT WING LE) · airframe 5,879 hrs · 2,670 cycles

LEFT WING LEADING EDGE FORMER CRACKED AT NR 5 SLAT AUX TRACK. REMOVED AND REPLACED LEFT WING LEADING EDGE FORMER AND ANGLE, IAW BAC DWG 114T2241, REV. AND EA H AND EA: H-5720-T0357387, P1, RELEASE DATE: OCT 14, 2020, REV DATE: WINGS-SECONDARY WING STRCT SECONDARY WING STRCT-LT WING, LEADING EDGE, ANGLE, OSS 441 ALTERNATE FASTENERS.

Part: DETECTOR LOOP — FAILED (PYLON) · airframe 5,297 hrs · 2,370 cycles

17 MIN INTO FLT RECEIVED LEFT DUCT LEAK LIGHT ON OVERHEAD PANEL., NO EICAS. RAN CHECKLIST AND LIGHT WENT OUT FOR REMAINDER OF FLT. FLT CONDITION LEVEL CRUISE AT FL350. REMOVED AND REPLACED ELEMENT TS407 PER AMM 26-18-01-4-2. LOOP OPS CHECK IS GOOD. INSTALLED ALL PANELS UNDER LEADING EDGE AND OVER WING PYLON AREA IAW AMM 57-41-01-4-0. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 3,519 hrs · 1,536 cycles

LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE GREEN NO OTHER INDICATIONS PRESENT TO INDICATE UNSAFE GEAR. RELAMPED LEFT GEAR INDICATOR IAW AMM 33-13-00-2. OPS CHECKED GOOD. A/C OK FOR FLIGHT.

Part: CONTROL UNIT — MALFUNCTIONED (CARGO BAY)

WHILE HOLDING FOR T/O DURING CROSSBLEED START OF NR 3 ENG. AFT CARGO SMOKE WARNING AND BELL ACTIVATED. FIRED NR 1 FIRE BOTTLE INTO AFT CARGO COMPARTMENT. WARNING STAY ON. INPS AFT CARGO COMP. NO FIRE OR SMOKE. *S/D* REMOVED AND REPLACED AFT CARGO COMP CONTROL ELECTRONICS UNIT PER MM 26-16-012. SYS CK OK. REPLACED AFT NR 1 FIRE BOTTLE PER MM 26-16-014-2.

Part: COVER — CRACKED (PAX DOOR SLIDE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, THE EMERGENCY ESCAPE SLIDE COVER FOUND CRACKED IN SEVERAL PLACES. REPAIRED COVER PER IAW B727 SRM 51-40-8.

Part: FRAME — GOUGED (FUSELAGE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, BS 1342 FRAME FOUND GOUGED BEYOND ALLOWED LIMITS ABOVE STR 20R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW B727 SRM 51-40-3 AND B727 SRM 51-30-2.

Part: FRAME — WORN (FUSELAGE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, APPROX 4 IN OF FRAME AT BS 1342 FOUND WORN BEYOND LIMITS AT STR 15R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW B727 SRM 51-40-3 AND B727 SRM 51-30-2.

Part: SKIN — WORN (FUSELAGE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, FUSELAGE SKIN WAS FOUND WORN BEYOND LIMITS AT BS 1342 UNDER RAIN GUTTER. REMOVED AND REPLACED, FAB PER IAW B727 SRM 53-30-3.

Part: FRAME — WORN (FUSELAGE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, APPROX 5 IN OF THE FRAME AT BS 1342 WAS FOUND WORN BEYOND LIMITS AT STR 20R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW SRM 51-40-3 AND B727 SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, THE FUSELAGE SKIN FOUND CORRODED BEYOND ALLOWED LIMITS BETWEEN SKIN LAP AT BS 1338, STR 10L. REMOVED AND REPLACED, FAB DOUBLER AND FILLER PER IAW B727 SRM 53-30-3.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, A VERTICAL STIFFENER FOUND CRACKED AT BS 1070, BETWEEN STR 28R AND 29R. REMOVED, FAB AND INSTALLED PER IAW B727 SRM 51-20-1, 51-30-2.

Part: WIRE — BROKEN (PAX DOOR SLIDE) · airframe 53,504 hrs · 40,786 cycles

DURING ROUTINE INSP, THE EMERGENCY ESCAPE SLIDE LIGHT WIRE WAS FOUND BROKEN BETWEEN THE BATTERY AND LIGHT. REPAIRED BROKEN WIRE PER IAW WDM 33-51-02.

Part: SWITCH — INOPERATIVE (E/E DOOR)

EQUIPMENT ACCESS DOOR LIGHT INOPERATIVE. AIRCRAFT TOOK OFF WITH ELECTRICAL EQUIPMENT COMPARTMENT OPEN. RAMP ACCOMPLISHED PUSH BACK, INSPECTED ELECTRICAL EQUIPMENT BAY. NO DAMAGE NOTED. CLOSED ELECTRICAL EQUIPMENT DOOR. DEFERRED ELECTRICAL EQUIPMENT DOOR WARNING LIGHT AS INOPERTIVE PER MINIMUM EQUIPMENT LIST 52-4G CAT C CONTROL NR 25506 EXPIRES 23 NOV 97. ACCESS DOOR ANNUNCIATOR LIGHT INOPERATIVE. VERIFY EQUIPMENT ACCESS DOOR IS CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT. DOOR VERIFIED CLOSED. REMOVED AND REPLACED EQUIPMENT ACCESS DOOR WARN SWITCH. SYSTEM OPERATIONAL, CHECKS GOOD PER M/ M 52-70-0.

Part: TRIM MOTOR — FAILED (VERT STAB)

AFTER TAKEOFF, MAIN STABILIZER TRIM FAILED. RESET CIRCUIT BREAKER TO NO AVAIL, CRUISE TRIM WORKED NORMALLY. REPLACED MAIN ELECTRIC STABILIZER TRIM MOTOR PER MM 27-40-31 PAGE 201, OPS CHECK GOOD.

Part: CHORD — CORRODED (BS 1176.9)

CORROSION ON REINFORCEMENT CHORD STA 1176.9 RBL 55 WL 208. REMOVED PARTS, SECONDARY STRUCTURE AND REMOVED CORRODED REINFORCEMENT CHORD. INSTALLED NEW CHORD AND SECONDARY STRUCTURE. ALL WORK DONE IAW FEDEX SRM 53-10-1, 51-30-2. REPLACED CHORD BS 1176.9 LBL 65 RBL 55.

Part: CHORD — CORRODED (FUSELAGE)

CORROSION FOUND ON HORIZONTAL CHORD AT RBL 16.5 TO 20 WL 191.5. REPAIRED CORRODED AREA PER EA 7-5310-25687.

Part: SKIN — CORRODED (BS 1352-1420)

STR 9R STA 1352 TO 1420 PILLOWING SKIN. REMOVED AND REPLACED 30 INCHES OF SKIN AND REPAIRED SKINS BOTH FWD AND AFT OF STA 1365.5 STR 9R, PER FEDEX SRM 53-30-3, 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 840)

FLOOR SUPPORT FLANGE AT STA 840 LBL 24 WL 208 HAS INTERGRANULAR CORROSION THAT IS OUT OF LIMITS. FABRICATED REINFORCEMENT STRAP PER EWO NO 95-3069.

Part: SKIN — CORRODED (BS 1372-1389)

STRINGER 9L STA 1372 TO 1389 PILLOWING SKIN. REMOVED DAMAGE SECTION OF SKIN AND REPAIRED IAW FEDEX SRM 53-30-3, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 760-850)

CORRODED SEAT TRACK AND FASTENERS AT STA 760 TO 850 LBL 25. REMOVED AND REPLACED SEAT TRACK. ALL WORK DONE IAW FEDEX SRM 53-10-1 AND FEDEX MM 53-20-12.

Part: STIFFENER — GOUGED (BS 312)

GOUGE IN FLOORBEAM VERTICAL STIFFENER STA 312 RBL 52 WL 207. REMOVED AND FABRICATED FLOORBEAM VERTICAL STIFFENER. ALL WORK DONE IAW FEDEX SRM 53-20-1.