N274FE

Part: SKIN — DAMAGED (LT NR 5 SLAT) · airframe 3,324 hrs · 1,604 cycles

LEFT WING SLAT NO. 5 TRAILING EDGE WITH MISSING MATERIAL. LEFT WING SLAT NO 5 TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG. 201 SHEET 1-2, PAGE 1-2 AND SRM 51-70-10-2R REP. 4, FIG. 202 SHEET 8, PAGE 149, 162, 163 REV. 82 12-15-21

Part: WIRE — DAMAGED (CARGO DOOR) · airframe 44,653 hrs · 28,374 cycles

AFTER TAKEOFF AND GEAR RAISED. "MAIN CARGO DOOR B" LIGHT ILLUMINATED. FOLLOWED QRH. DOOR LIGHT EXTINGUISHED RETURNED TO IND. DOOR LIGHT REILLUMINATED ON SHORT FINAL FOR 10 SECONDS. DURING T/S FOUND PIN B PUSHED BACK AT SW S9056 C/P D9834J. THIS IS THE GROUND WIRE FOR THE CARGO DOOR WARNING B SYSTEM. MCD AND MCD WARNING LIGHTS OP NORMAL. OK FOR SERVICE.

Part: PLATE — DAMAGED (TE FLAPS) · airframe 44,517 hrs · 28,271 cycles

ON CLIMB-OUT ACFT UNUSUAL VIBRATION PASSING 11,000 FT & ACCELERATING THROUGH 335 KIAS. DECREASED AIRSPEED & VIBE STOPPED AT 315 KIAS. ACCELERATED AGAIN & AT FL 180, 325 KIAS VIBE RETURNED, DEPLOYED SPOILERS & VIBE SMOOTHED OUT. STOWED SPOILERS & VIBE RETURNED. CLIMBED TO FL 320 - PASSING MACH .83 VIBE RETURNED. FOUND NUT & ECCENTRIC MISSING ON SIDE PLATE ON LT INBD AILERON. BEARING IS STILL IN PLACE, UNSURE OF CONDITION. R & R LT FLAP TE SIDE PLATE ASSY. NO DAMAGE NOTED ON TRACK ASSY. AT REMOVAL, ADJUSTED LT TE FLAP IAW MM 27-51-001-5. ADJUSTED LT & RT INBD & OUTBD TE FLAPS PER MM 27-51-001-5 & 27-51-011-5. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: ACTUATOR — OUT OF ADJUST (MLG) · airframe 44,008 hrs · 27,837 cycles

TEST FLIGHT, RMG SHOWED UNSAFE IND ON THIRD EXTENSION. NO GREEN DOWN AND LOCKED LIGHT, RED DOOR OPEN LIGHT ON. VISUAL INSPECTION BY TOWER AND OTHER A/C CONFIRMED RIGHT MAIN GEAR WAS STILL UP. CYCLED IAW RED TABS AND GOT SAFE DOWN AND LOCKED INDICATION. ADJUSTED RT MLG DOOR AND ACTUATOR AS REQUIRED IAW FX 727-200 MM 32-12-001-5. PERFORMED GEAR SWING AND OPS CHECK GOOD IAW FX 727-200 MM 32-32-000-5. ALSO PERFORMED MANUAL EXTENSION CHECKS ON MLG, OPS CHECK GOOD IAW FX 727-200 MM 32-34-000-0. NO FURTHER DISCREPANCIES AT THIS TIME.

Part: ANGLE — CRACKED (RT WING TE FLAP) · airframe 44,006 hrs · 27,834 cycles

RT WING INBOARD MID FLAP LOWER AFT CHORD ANGLE IS CRACKED AT WBL 110. CUT OUT DAMAGED SECTION DIM 47 1/4 INCH IAW B727 SRM 51-10-1, FABRICATED FILLER REPAIR USING BAC1503-100046 7075-T6 PO NR 8177105 DIM 47 1/4 INCH BY 2 INCH AND SPLICE USING BAC1503-100046 7075-T6 PO NR 8177105 IAW B727 SRM 51-30-5 AND 57-50-2 FIG 5. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR ANGLES IAW B727 SRM 51-30-2 AND 51-40-4 FIG 1.

Part: SHEAR TIE — DAMAGED (BS 640 S27L) · airframe 44,006 hrs · 27,834 cycles

FWD CARGO COMPARTMENT FRAME STA 640 SHEAR TIE LOWER FLANGE HAS A HOLE DRILLED THRU ABOVE STR 27L. FABRICATED 2 EACH FREEZE PLUGS, 2 RETAINING PLATES. INSTALLED FREEZE PLUGS AND RETAINING PLATES IAW EA 7-5310-116985, SRM 51-30-2 AND 51-10-7.

Part: SKIN — DENTED (BS 297) · airframe 44,006 hrs · 27,834 cycles

LOWER FUSELAGE DENTED BS 297.5 BELOW STR 20R, BELOW FWD LAV SERVICE PANEL CUTOUT FWD LWR CORNER. REWORKED DENT IAW B727 SRM 51-40-1 AND EA 7-5330-116984 AND B727 SRM 53-30-01. REMOVED AND REPLACED RIVET IAW B727 SRM 51-30-. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2.

Part: STRINGER — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 44,006 hrs · 27,834 cycles

FWD CARGO COMPT STR 28R LEVELING COMPOUND IS CRACKED AND BULGING AT SPLICE STA 680 PLUS 10 INCHES CUT OUT DAMAGED AREA APPROX DIM 6 3/8 INCH LENGTH, FABRICATED REPAIR SPLICE FROM BAC1498-132 PO NR 8177148 DIM 19 1/2 INCH LENGTH AND FILLER FROM BAC1498-143 PO NR 8177148 DIM 6 3/8 INCH LENGTH. INSTALLED REPAIR PARTS AT BS 680 10 INCH STR 28R IAW B727 SRM 53-10-3 FIG 1 SRM 53-10-2 FIG 9 AND SRM 51-30-2.

Part: SKIN — DAMAGED (ZONE 100) · airframe 44,006 hrs · 27,834 cycles

STA 660 AT PREVIOUS REPAIR STR 28L TO 28R EXTERIOR SKIN BULGED AND CRACKED NEAR L/E OF REPAIR, BULGING NEAR T/E. MANY FASTENERS SHOW EVIDENCE OF WORKING AND CORROSION. REMOVED PREVIOUS DOUBLER IAW B727 SRM 51-30-2, CUTOUT DAMAGED AREA DIM 17 INCH BY 11 INCH AND FABRICATED REPAIR DOUBLER FROM 2024-T3 .080 PO NR 9005551 DIM 25 3/4 INCH BY 21 3/4 INCH AND 2 FILLERS FROM 2024-T3 .071 PO NR 9007126 DIM 10 INCH BY 1 INCH EACH IAW B727 SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 51-30-2 AND 53-30-3 FIG 1.

Part: SKIN — DAMAGED (ZONE 100) · airframe 44,006 hrs · 27,834 cycles

SKIN BULGE LT FUSELAGE STA 1323 ABOVE STRL 18. CUTOUT DAMAGED AREA APPROX 2 7/8 INCH BY 2 INCH IAW B727 SRM 53-30-3 FIG 14, FABRICATED DOUBLER REPAIR MATERIAL 2024-T3 .063 PO NR 9006773 DIM 11 INCH BY 10 INCH FILLER MATERIAL 2024-T3 .050 PO NR 9006742 DIM 2 INCH BY 1 INCH AND STRUCTURAL FILLER MATERIAL 2024-T3 .050 PO NR 9006742 DIM 2 INCH BY 13 1/4 INCH IAW SRM 53-30-3 FIG 14 AND 53-30-2 FIG 3. INSTALLED REPAIR PARTS ON LT FUSELAGE STA 1323 STR 18 IAW SRM 51-30-2 AND 53-30-3 FIG 14.

Part: SKIN — DAMAGED (ZONE 100) · airframe 44,006 hrs · 27,834 cycles

SKIN OIL CANNED LEFT FUSELAGE STA 1243 STR 18L TO 19L. CUT OUT DAMAGED AREA APPROX DIM 3 7/8 BY 1 7/8, FABBED REPAIR DOUBLER FROM 2024- T3 .063 PO NR 9006713 APPROX DIM 13 3/4 BY 8 1/2 AND INSTALLED REPAIR DOUBLER AT BS 1243 STR 18-19 LEFT IAW B727 SRM 53-30-3 FIG 3 AND SRM 53-30-2 FIG 3 AND SRM 51-30-2.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,006 hrs · 27,834 cycles

AFT CARGO COMPARTMENT AT BS 1105 UNDER STR 29R SHOWS CORROSION. FABRICATED NEW SUPPORT CHANNEL FOR STR 29R BS 1105 AND INSTALLED NEW CHANNEL IAW SRM 51-10-3, SRM 51-20- 01 FIG 3 AND DWG NR 65-56136, FABRICATED REPAIR DOUBLER, INSTALLED SHEAR TIE REPAIRS IAW SRM 53-10-4 FIG 11. ALL PARTS HEAT TREATED TO T6 CONDITION.

Part: SKIN — DENTED (ZONE 100) · airframe 44,006 hrs · 27,834 cycles

DENT RT FUSELAGE STA 540 STR 24R (RVSM AREA). REPAIRED DENT IAW EA 7-5330-116983.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 44,006 hrs · 27,834 cycles

EXISTING DOUBLER REPAIR TO THE FUSELAGE SKIN AT BS 1140 AND STR 20L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, FABRICATED NEW DOUBLER. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 3 AND SRM 53-30-3 FIG 14 AND SRM 51-30-2.

Part: ACTUATOR — FAILED (RT MLG) · airframe 43,931 hrs · 27,772 cycles

RED GEAR DOORS LIGHT AND RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AMBER RIGHT GEAR DOOR LIGHT ON S/O PANEL ALSO ILLUMINATED. REPLACED RT MAIN GEAR ACTUATOR IAW AMM 32-32-002-4, AND RT MAIN GEAR CYCLES UP AND DOWN NORMAL WITH NO LEAKS NOTED. PREMATURE REMOVAL/INSTALLATION OFF MFG 65-17830-13.

Part: CONTROL VALVE — FAILED (NR 2 ENGINE) · airframe 43,872 hrs · 27,709 cycles

AT ROTATION NR 2 DUCT ANTI-ICE OVERHEAT LIGHT ILLUMINATED TEMP OFF SCALE HIGH . AN QRH FOR ANTI-ICE DUCT OVERHEAT LIGHT. NR 2 ENGINE COULD NOT BE OPERATED ABOVE 1.25 EPR NR 2 DUCT OVERHEAT LIGHT ON MEL 30-11-A NR 2 ENGINE 13TH STAGE VALVE OPEN GOC ADVISED AIR TURN BACK TO MEM. REMOVED AND REPLACED NR 2 COWL ANTI-ICE THERMOSTATIC CONTROL VALVE IAW 727 MM-30-21-021-4. A/C OK FOR RETURN TO SERVICE.

Part: NONE — UNKNOWN (MLG DOOR) · airframe 43,356 hrs · 27,307 cycles

ON TAKEOFF, RT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH, RECYCLED GEAR AND LIGHT EXTINGUISHED. CONTINUED FLIGHT. INSPECTED GEAR DOOR SWITCHES CK GOOD, CYCLE DOOR OPEN CLOSED SEVERAL TIME. OPS CHECKS NORMAL IAW AMM 32-62-011-5.

Part: ACTUATOR — LEAKING (L/E SLAT) · airframe 43,097 hrs · 27,105 cycles

SHORT FINAL, LOSS OF A SYSTEM, LANDED STRAIGHT AHEAD. TOWED IN. AFTER T/S FOUND NR 2 L/E FLAP ACTUATOR LEAKING. CANCELED FIRST PART. REMOVED AND REPLACED NR 2 LE FLAP ACT IAW M/M 27-81-022-4. SERVICED HYD SYSTEM PER 12-12-000-2.

Part: ENGINE — SEIZED (NR 3) · airframe 42,369 hrs · 26,535 cycles

AFTER T/O AT 1,000' WITH STD POWER, NR 3 ENGINE SEIZED AT QUIET OIL QUANTITY DROPPED TO ZERO. CONDUCTED EPR REDUCTION. QRH ENGINE FIRE/SEVERE DAMAGE CHECKLIST. RETURNED TO FIELD. CRASH CREW REPORTED OIL LEAKING FROM ENGINE. PERFORMED ENGINE SEIZURE INSP PER AMM 05-51-201. NO DEFECTS NOTED. REMOVED AND REPLACED NR 3 ENG ASSY PER W/C 70T0001-03.

Part: SKIN — GOUGED (BS 95E) · airframe 42,089 hrs · 26,282 cycles

A GOUGE FOUND AT BS 950E, STR 19R DURING PRIMARY INSPECTION, REPAIR ACCOMPLISHED WITH EA 7-5330-92374 ISSUED BY FEDEX ENGINEERING, REPAIR IS CLASSIFIED AS MAJOR PER EA 7-5330-92374.

Part: REPAIR — UNKNOWN (BS 1140) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1140, STR 20L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP OF THE INSTALLATION, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: REPAIR — MISINSTALLED (BS 1140) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR AT STA 1140, STR 22L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 1, TABLE 1, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — MISINSTALLED (BS 1183) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR AT STA 1183, STR 27R IS NOT IN CONFORMANCE WITH APPROVED FAA DATA. REMOVED EXISTING REPAIR, ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 28R TO 28L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 2, PAGE 9, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNDAMAGED · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY INSTALLED REPAIR AT STA 720D, STR 19R WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNDAMAGED · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY INSTALLED REINFORCEMENT DOUBLER AT STA 344 BETWEEN STR 4L AND 5L WAS ACCOMPLISHED IAW RIGID BARRIER MODIFICATION DOCUMENT EA 7-5340-7-5002, PAGE 1 AND VENTURA AEROSPACE DWG 2942, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNDAMAGED · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY INSTALLED REPAIR AT AFT LOWER CORNER OF FWD GALLEY DOOR CUT OUT WAS ACCOMPLISHED IAW SB 727-53-0188, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNDAMAGED · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY INSTALLED REPAIR AT STA 680, STR 28 WAS ACCOMPLISHED IAW SRM 51-40-3, FIG 1 PAGE 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY INSTALLED REPAIR AT LT ENTRY DOOR STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT.2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNDAMAGED (ELEVATOR) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY INSTALLED REPAIR ON UPPER SURFACE OF LT ELEVATOR WAS ACCOMPLISHED IAW ENGINEERING REPAIR NR 16-0193, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (LE FLAP) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR AT NR 5 KRUEGER FLAP WS 265.0 WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3, BASED ON EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, NUMBER OF FASTENERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: REPAIR — UNKNOWN (FOREFLAP) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR ON LT INBOARD FORE FLAP LEADING EDGE WAS ACCOMPLISHED IAS SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (N/A) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUS REPAIR ON LEFT WING NR 1 KRUEGER FLAP FWD SURFACE WAS ACCOMPLISHED IAW SRM 57-50-3, FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — UNKNOWN (BS 950A) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR AT STA 950A, STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 3 PAGE 13, BASED ON EXTERNAL VISUAL EVALUATION OF LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR.

Part: REPAIR — UNKNOWN (BS 950A) · airframe 42,089 hrs · 26,282 cycles

FOUND REPAIR AT STA 950A, STR 29R WAS DETERMINED HAD BEEN ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS, MATERIAL THICKNESS AND TYPE AND GENERAL WORKMANSHIP OF INSTALLATION, REPAIR CLASSISIFED AS MAJOR REPAIR PER GMM 6-2-100.

Part: REPAIR — UNKNOWN (FOREFLAP) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUS REPAIR ON LT OUTBOARD FOREFLAP LEADING EDGE WAS ACCOMPLISHED IAW SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR PER FEDEX GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUSLY REPAIR AT RT WING NR 6 KRUEGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, NUMBERS OF FASTENER AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR REPAIR.

Part: REPAIR — UNKNOWN (RT WING ROOT) · airframe 42,089 hrs · 26,282 cycles

FOUND REPAIR LOCATED ON RIGHT WING L/E WING ROOT REPAIR REQUIRES EVALUATION FOR COMPLIANCE WITH FAA APPROVED DATA. REPAIR WAS DETERMINED ACCOMPLISHED IAW SRM 57-30-4 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBER, MATERIAL THICKNESS AND TYPE AND GENERAL WORKMANSHIP OF PREVIOUS INSTALLATION, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUS REPAIR ON UPPER LEADING EDGE OF LEFT WING AT NR 3 LEADING EDGE SLAT WAS ACCOMPLISHED IAW SRM 57-30-4, FIG 1. BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (RT WING) · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUS REPAIR ON RIGHT WING NR 7 L/E SLAT WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 1 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 42,089 hrs · 26,282 cycles

FOUND PREVIOUS REPAIR ON LOWER SURFACE OF RIGHT INBOARD AFT FLAP WAS ACCOMPLISHED IAW SRM 57-50-4 FIG 5, PAGE 12, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SWITCH — FAULTY

02-51 ON RETRACT OF FLAPS AMBER LED LIGHT ON. R&R #1 L/E FLAPS POSITION SWITCH PER IAW MM 27-82-001-4. OPS CHECK GOOD.

Part: FLOORBEAM — DAMAGED (FUSELAGE)

NR 911 DOUBLE FASTENER HOLES IN FLOORBEAM AT BS 380, LBL 13, WL 208. ** S/D ** R&R PER FEDEX SRM 53-10-8, FIG 8.

Part: FRAME — DENTED (FUSELAGE)

NR 339- DENTED FRAME BS 660, 2 INCHES ABOVE STRINGER 26R. ** S/D ** R&R PER FEDEX SRM 51-40-3.

Part: FLOORBEAM — DAMAGED (FUSELAGE)

NR 907 MECHANICAL DAMAGE ON FLOORBEAM BS 312, LBL 3, WL 208. ** S/D ** R&R PER FEDEX EA 7-5310-53867.

Part: FRAME — DENTED (FUSELAGE)

NR 333, DENTED FRAME BS 600, 2 INCHES ABOVE STR 26L. ** S/D ** R&R PER FEDEX SRM 51-40-3, 51-30-2.

Part: STRINGER — CORRODED (FUSELAGE)

NR 340 CORROSION (C53-111-01(2)) AT STRINGER 28L SPLICE BS 685-675. ** S/D ** R&R & FAB PER FEDEX SRM 51-10-6, 51-30-2

Part: FRAME — DENTED (FUSELAGE)

NR 332 DENTED FRAME BS 580, 2 INCHES ABOVE STRINGER 26L. ** S/D ** R&R PER FEDEX SRM 51-40-3, 51-30-2.

Part: FRAME — CORRODED (FUSELAGE)

NR 836 CORROSION (C53-224-01(2)) ON SEVERAL NUTPLATES AND FASTENER HOLES ON LONGITUDINAL BEAM FROM BS 740 TO 850, LBL 45, WL 208. ** S/D ** R&R PER DWG 65-16279, FEDEX SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE)

NR 862 (C53-224-01) CORROSION ON FLOORBEAM BS 620, LBL 25, TO LBL 44.5, WL 208. ** S/D ** R&R PER FEDEX SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (BS 1130)

NR 327 CORROSION C53-224-01 ON LOWER FLANGE OF FLOORBEAM BS 1130, RBL 50 - LBL 38, WL 200. ** S/D ** R&R PER IAW FEDEX EA 7-5310-53873.

Part: KEELBEAM — CORRODED (FUSELAGE)

NR 303 CORROSION ON KEELBEAM BS 780, LBL 5, WL 148. ** S/D ** R&R PER FEDEX EA 7-5310-53871.

Part: CONNECTOR — CONTAMINATED (MLG)

ON GEAR RETRACT, LV LATCH FAIL TO RELEASE. COMPLETED THE RED TABS STEP. PRECAUTIONARY CLEAN CONNECTOR AT LG ASSY UNIT, LG SYS TEST OK.

Part: SMOKE DETECTOR — MALFUNCTIONED (E & E COMPT)

99-128 PER CREW NR 3 MAIN CARGO DETECTOR SMOKE DETECTOR LIGHT FLICKERED ON LANDING. REMOMED AND REPLACED NR 3 SMOKE DETECTOR PER MM 26-16-011-4. OPER CK NORMAL.

Part: DUCT — FAILED (NR 3 ENGINE)

98-203 AFTER T/O NR 3 FIRE WARN LIGHT CAME ON. SHUT DOWN NR 3 ENGINE. NR 3 FIRE LOOPS TEST GOOD. FND APPROX 1.75 CRACK IN THE 13TH STAGE SADDLE DUCT ON NR 3 ENG AT CTR BOOSTER. REMOVED AND REPLACED DUCT PER BAC OHM 71-02-01 PG 578J, LEAK CHECKED DUCT CK OK. OK FOR SERVICE.

Part: OVERHEAT LOOP — OUT OF POSITION (AFT BODY)

LOWER AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT WITH WING ANTI-ICE ON. TURNED OFF WING ANTI-ICE, LIGHT WENT OUT. TURNED ENGINE NR 1 WING ANTI-ICE ON LIGHT CAME BACK ON. SECURED SYSTEM THEN RECHECKED WITH ENGINE NR 3 WING ANTI-ICE ON, LIGHT CAME BACK ON AGAIN. REMOVED KEEL BEAM PANEL AND PANELS IN AFT CARGO COMPARTMENT. LEAKED CHECKED ANTI-ICE LINE FROM AIRSTAIR AREA TO KEEL BEAM AREA NO LEAKS FOUND. DID FIND LOOP TOUCHING ANTI-ICE LINE IN KEEL BEAM REPOSITIONED LOOP AWAY FROM LINE. OPERATIONAL CHECKS GOOD ON GROUND RUN NEEDS PANELS REINSTALLED. REINSTALLED KEEL BEAM PANEL AND AFT CARGO COMPARTMENT PANELS.

Part: UPLOCK SENSOR — OUT OF ADJUST (LT MLG)

AFTER TAKEOFF LEFT GEAR RED LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN UP POSITION. RECYCLED GEAR PER RED TABS, GEAR LIGHT REMAINED ON (RED LIGHT). GEAR DOOR LIGHTS (FIRST OFFICER'S AND SECOND OFFICER'S) SIDE PANEL OUT. FLEW TO IND WITH GEAR HANDLE IN UP POSITION PER RED TABS. FOUND UPLOCK SENSOR ACTUATOR AND SENSOR GAP OUT OF TOLERANCE. ADJUSTED SENSOR AND ACTUATOR TO PROPER GAP. PERFORMED UPLOCK SENSOR TEST PER MAINTENANCE MANUAL 32-61-91 PG 401.

Part: FRAME — CRACKED (BS 640)

LOWER FWD CARGO FLOOR FRAME CRACKED STA 640 LBL 10. STOP DRILLED CRACK, INSTALLED REPAIRED PER SRM 51-40-3.

Part: BYPASS SWITCH — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENG LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON AT APPROX 0450Z FL240 CRUISE. OIL PRESS WAS 47 PSI QUAN AND TEMP NORMAL RANGE RETARDED NR 1 THRUST LEVER TO IDLE LIGHT REMAINED ON SHUTDOWN NR 1 ENG IAW CHECK LIST. LIGHT STAYED ON ABOUT 4 MINS AFTER ENG START BEFORE LIGHT GOES OUT. REMOVED AND REPLACED NR 1 ENG LOW OIL PRESS FILTER BYPASS SW. LEAK AND OPS CK GOOD. RAN NR 1 ENG PER JRH OIL LOW PRESS/FILTER BYPASS LIGHT OPS CK'D NORMAL.