N144FE

Part: NONE — NONE (N/A) · airframe 8,641 hrs · 3,934 cycles

AFTER LOWERING THE LANDING GEAR ON FINAL APPROACH, THE LEFT MAIN GEAR LIGHT AND THE LEFT HALF OF THE RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE. PERFORMED GA, RECEIVED GROUND VISUAL CONFIRMATION THAT LEFT MAIN GEAR APPEARED DOWN, AND RAN QRH PROCEDURES. LANDED UNEVENTFULLY. LIGHT TEST SHOWED ALL 3 LAMPS INOP. REMOVED AND REPLACED 3 EA LAMPS. OPS CHECK GOOD. REF AMM 33-13-00-2.

Part: WEDGE — DELAMINATED (NR 2 SLAT) · airframe 6,578 hrs · 2,893 cycles

LT WING LEADING EDGE, NR 2 SLATS WEDGES DELAMINATED AT INBOARD SIDE UPPER SURFACE. REPAIRED LT WING LEADING EDGE, NR 2 SLATS WEDGE DELAMINAITED AT INBOARD UPPER SURFACE, IAW B767 SRM B767 SRM 57-43-02, 51-70-10-2R AND B767 AMM 51-21-01.

Part: FORMER — CRACKED (RT WING) · airframe 6,578 hrs · 2,893 cycles

RIGHT WING L/E LES 560 WEB SUPPORT BRACKET CRACKED. REMOVED AND REPLACED FORMER ASSEMBLY P/N'S 114T2512-14 AND 114T2512-12.

Part: SEAL — CRACKED (RT WING LE) · airframe 6,578 hrs · 2,893 cycles

RIGHT WING LEADING EDGE NR 8 SLAT LES 505, INTERNAL LEADING EDGE DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER AT RT WING LEADING EDGE LES 505, IAW B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C.

Part: ANGLE — CRACKED (RT WING LE) · airframe 6,578 hrs · 2,893 cycles

RIGHT WING LEADING EDGE NR 8 SLAT OUTBOARD ROTARY ACTUATOR ARM CUTOUT, FORMER IS CRACKED. REMOVED AND REPLACED FORMER AT OSS 499 RIGHT WING LEADING EDGE NR 8 SLAT, IAW B767 SRM 51-40-02 AND BAC DWG 114T2161REV-.

Part: ANGLE — CRACKED (BS 246) · airframe 6,578 hrs · 2,893 cycles

E & E BAY LEFT HAND SIDE, MAIN CABIN FLOOR BEAM, VERTICAL STIFFER ANGLE AT STA 246 APPROX LBL 50 IS CRACKED. REMOVED AND REPLACED ANGLE, PER BAC DWG 141T5600 REV AND B767 SRM 51-40-02.

Part: ANGLE — CRACKED (BS1578) · airframe 6,578 hrs · 2,893 cycles

BEHIND BULK PIT AFT BULKHEAD, AT STA 1578, MAIN CABIN FLOOR SUPPORT CANTILEVER L-ANGLE IS CRACKED. REMOVED AND REPLACED NEW L-ANGLE, PER B767 SRM 51-40-02 AND BAC DWG 146T5650 REV C.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 6,578 hrs · 2,893 cycles

FWD PIT FLOOR PANEL 122CF HAS A PUNCTURE IN THE PANEL SKIN. REPAIRED FLOOR PANEL 122CF, IAW B767 SRM: 53-00-50 FIG 201. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 6,578 hrs · 2,893 cycles

MAIN CABIN FLOOR PANEL 241GFF HAS A PUNCTURE IN THE SKIN. REPAIRED MAIN CABIN FLOOR PANEL 241GFF PUNCTURE, IAW B767 SRM: 53-00-50 FIG 201. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 6,578 hrs · 2,893 cycles

MAIN CABIN FLOOR PANEL 242FFF HAS MULTIPLE PUNCTURES IN THE SKIN. REPAIRED MAIN CABIN FLOOR PANEL 242FF MULTIPLE PUNCTURES, IAW FEDEX SRZ-25-005 REV R. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 6,578 hrs · 2,893 cycles

MAIN CABIN FLOOR PANEL 242GFF HAS MULTIPLE PUNCTURES IN THE SKIN. REPAIRED MAIN CABIN FLOOR PANEL 242GFF PUNCTURES, IAW FEDEX SRZ-25-005 REV R. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 6,578 hrs · 2,893 cycles

MAIN CABIN FLOOR PANEL 241ZFF HAS A PUNCTURE IN THE SKIN. REPAIRED CABIN FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50 FIG 201.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 6,578 hrs · 2,893 cycles

MAIN CABIN FLOOR PANEL 241FFF HAS A PUNCTURE IN THE SKIN. REPAIRED CABIN FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50 FIG 201.

Part: HMU — FAILED (LT ENGINE) · airframe 5,907 hrs · 2,584 cycles

OPEN U DURING CLIMB DEPT KORD APPROX 5000 LOUD BANGING NOISE FOLLOWED BY YAW, A/P ENGAGED, LE N1 30%, FUEL FLOW APPROX. 4000PPH, RT ENG NORMAL, LT ENG BACK TO NORMAL. SECOND OCCURRENCE BANGING LOW N1 & FF ON LT ENG EICAS "L ENG HPSOV" ( SOUNDED LIKE COMPRESSOR STALL) TAT 14 DEG. RAN QRH, ENG HPSOV CHECKLIST, NO OTHER OCCURRENCE. RETURNED TO ORD. PERFORMED BORESCOPE INSP PER 767 MM 72-00-00-6 FOR STALL, NO DEFECTS NOTED. HMU REQ R & R PER TSI WRI 72-00/2710. REMOVED HMU IAW MM 73-21-14-4, BREAKERS D25 ON P11 AND E1 ON P6, PULLED AND COLLARED. REMOVAL COMPLETED PLATES FOR HARD LINES MUST BE REMOVED FROM NEW OTHER FASTENERS AND HARDWARE IF REQ. CONT R & I PER AMM 73-21-14-4 THRU INSTALLATION STEP 3,E,(8). DUE TO OTHER MX. CLOSE UP AND HMU TEST STILL NEEDS TO BE ACCOMPLISHED. COMPLIED WITH REMAINING STEPS PAGE 25. STEP F. 1-2-3-4-5 END IAW AMM-73-21-14-4 REF-71-00-00-5-3. COMPLIED WITH TESTS 2-3-5-11. ALSO COMPLIED WITH MAX POWER ASSURANCE IAW AMM-71-00-00-5-3 AND JRH-7-6 AND JRH-4-6 THROUGH 4-11. ALSO COMPLIED WITH MAX POWER ASSURANCE AND BOTH MIN IDLE AND APP IDLE PARAMETERS WITHIN LIMITS REF-JRH AND-AMM-71-00-00-5-3. ALL PARAMETERS WITHIN LIMITS. ALSO COMPLIED WITH FIM-36-10 FAULT TREE 833. OK FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 5,238 hrs · 2,267 cycles

ENGINE EXAUST (BURNING OIL) SMELL AT 10000 FT DECENDING AND SLOWING FROM 290 IAS TO 230 KNOT IAS. CABIN ALT 1000', CABIN DIF 4.0. SMELL WENT AWAY AT 7,000 FT, 230 KIAS, 500 CABIN ALT, DIF 3.0. SMELL CAME BACK ON THE TAXI TO THE GATE WHEN RIGHT ENGINE SHUT DOWN. REMOVED PNEUMATIC GROUND AIR CONNECTOR IN REFERENCE TO AMM 36-11-03-4 TO FOM. INSTALLED PNEUMATIC GROUND AIR CONNECTOR, PERFORMED LEAK CHECK NO AIR LEAKS FOUND REF TO AMM 36-11-03-4. PERFORMED SMOKE/FUME CONTAMINATION PROCEDURES NO SMOKE/FUME CONTAMINATION NOTED AT THIS TIME. REF TO AMM 21-00-21-2.

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 4,263 hrs · 1,811 cycles

LEFT MAIN GEAR LIGHT OUT AFTER SELECTING GEAR DOWN. PERFORMED LAMP CHECK LIGHT STILL OUT. REPLACED BOTH LEFT MAIN GEAR LIGHT. PERFORMED LAMP CHECK LIGHTS WORKED GOT 3 GREEN AFTER SELECTING GEAR DOWN. PER CREW DEBRIEF, VERIFIED LAMPS REMOVED BY THE CREW TO BE BURNED OUT. REMOVED LEFT MAIN GEAR INDICATION LAMPS AND VERIFIED CORRECT PART # INSTALLED. RE-INSTALLED LAMPS REF 767AMM 33-13-00-2 AND PERFORMED LAMP TEST AND FOUND SATISFACTORY. REF 767AMM 32-09-04-4, PERFORMED PSEU TEST AND ALL TESTS PASSED. VISSUALLY INSPECTED LEFT MAIN GEAR FOR ANY DEFECTS, NONE NOTED. NO HISTORY ON ITEM LAST 99DAYS. A/C OK FOR SERVICE.

Part: SKIN — DAMAGED (NR 6 SLAT) · airframe 3,829 hrs · 1,619 cycles

MDIS 144 27-80 1755 20MAR19 MEM OPEN U #6 SLAT DAMAGED BY BIRD IMPACT. SHGN 20MAR19 05:04 MEM U #6 SLAT L/E SKIN IS OUT OF LIMITS IN REF. TO B767 SRM 57-43-01-1A FIG 101 FACT 23MAR19 18:10 MEM COMPLETED INSTALL OF #6 L/E SLAT, REF B767 27-81-01-4.

Part: WIRE — DAMAGED (ELEVATOR)

DURING TAXI ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON. LOW PRESS LIGHT C/B ON. HYD A & B FILTERS CHECK GOOD. PITOT TUBES ON TAIL WERE CLEAN. SPLICED IN NEW SECTION OF WIRE PER SMP, OPS CHECK NORMAL.

Part: DOOR — NOT CLOSED (SERVICE DOOR)

AIRFRAME VIBRATION AND HUMMING SOUND. INSP GROUND PWR SERVICE DOOR. NO DEFECTS NOTED. RESECURED DOOR CLOSED.

Part: HANDLE — WORN (MLG)

ON FINAL APPROACH, GEAR HANDLE DOWN, HEARD NOISE. FELT MUSHY. NOSE GEAR AND NOSE DOORS UNSAFE RED LIGHT ON RECYCLED GOT GOOD IND ON ALL 3 GEAR. LANDING GEAR CONTROL HANDLE CABLE TENSION LOW. ADJUSTED PER MM 32-31-000-5 PG 501-505. REMOVED AND REPLACED SELECTOR VALVE ACTUATION LINK ROD PER MM 32-31-031-4.

Part: WARNING SWITCH — INOP (RT MLG DOOR)

ON DEPART, RT MLG DOOR APPEAR TO REMAIN OPEN EVEN AFTER CYCLING MLG PER RED TAB PROC. REMOVED AND REPLACED RT GEAR DOOR WARN SWITCH PER MM 32-62-011-4 ADJ & TEST PER MM 32-62-011-5. OPS CK GOOD.

Part: HOSE — LEAKS (AFT AIRSTAIRS)

99-113 - LWR AFT BODY O/H LIGHT ILLUM. LIGHT WENT OUT AFTER CLOSE NR 1 BLD AND BEFORE TURN OFF NR 1 PACK. 3RD TIME WRITTEN UP. REMOVED AND REPLACED SENSE LINE. OPER AND LEAK CK NORM.

Part: OVERHEAT LOOP — INOPERATIVE (LWR AFT BODY)

99-112 - LWR AFT BODY LIGHT ILLUM. LIGHT EXTINGUISH WHEN RT PACK AND RT BLD TURN OFF. REMOVED AND REPLACED LOOP PER MM 26-14-001-4. OPER CK NORM.

Part: OVERHEAT LIGHT — MALFUNCTIONED (LWR AFT BODY)

LOWER AFT BODY O/H LIGHT ON. LIGHT WENT OUT WHEN NR 1 BLD AND LT PACK TURN OFF. INSP DUCT IN AFT AIR STAIRS, CEILING, KEEL BEAM AREA AND NO LEAKS FOUND. COULD NOT DUP O/H COND. OK TO CONTINUE SERVICE.

Part: VALVE — FAILED (NR 1 BLEED SYST)

LOWER AFT BODY O/H LIGHT ILLUMINATED. FOLLOWED CK LIST PROCEDURE, CLOSED NR 1 BLEED VALVE AND LEFT PACK. RETARDED NR 1 THROTTLE TO CLIMB POWER. LIGHT REMAINED OUT AND TEST OK, INDICATIVE OF LEAK BETWEEN NR 1 BLEED VALVE AND LEFT PACK VALVE. REMOVED AND REPLACED PURGE VALVE, OPER CK AND LEAK CK GOOD. REF M/M 36-13-11. NOTE: VALVE HOT AIR WAS LEAK AT HEAT DETECTOR.

Part: BEAR STRAP — CORRODED (BS 475)

STA-PAE: CORROSION (C53-224-02) INNER SKIN EMANATING FROM UNDER BEAR STRAP AT BS 475 BETWEEN STRINGER 3 AND 4 LT.

Part: SPAR CHORD — CORRODED (BS 745)

CORROSION (C53-132-01-1) ON WING CENTER SECTION SPAR CHORD (LOWER) AT BS 745, RBL 12 TO RBL 30, WL 160. *S/D* REMOVED AND REPLACED LOWER SPAR CHORD, BS 745 IAW FED-EX DRAWING 65C21537.

Part: SPAR CHORD — CORRODED (WS 456-467)

CORROSION (C57-562-02) RT WING SPAR LOWER CHORD HORIZONTAL LEG FS 456 TO 457. *S/D* REPAIRED RT WING FRONT SPAR LOWER SPAR CHORD AT FS 456 TO 467 IAW FED-EX EA 7-5710-35089.

Part: FLOORBEAM — CORRODED (BS 344)

CORROSION (C53-224-06) IN SEVERAL AREAS ON THE UPPER CHORD OF THE BS 344 FLOORBEAM FROM LBL 63 TO RBL 21. REMOVED, FABRICATED AND INSTALLED FLOORBEAM UPPER CHORD AT BS 344, LBL 65 TO RBL 65 IAW FEDEX SRDM 27-53-007.

Part: WEB — CORRODED (BS 1136)

WHILE WORKING NR 0840, FOUND CORROSION ON SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 ON UNDER SURFACE OF WEB. *S/D* REPAIRED SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 IAW FED-EX SRM 51-40-2.

Part: STRINGER — CORRODED (BS 560-580)

CORROSION (C53-224-02) ON STRINGER 1 BL 0 BS 560 TO 580, BS 520 TO 540. *S/D* REMOVED CORROSION FROM STR 1, FOUND IT TO BE OUT OF LIMITS. REPAIRED STR 1, BS 520 TO 540 IAW FED-EX SRM 53-10-3.

Part: STRINGER — CORRODED (BS 380-460)

CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380 TO 460. *S/D* REPAIRED STR 9 LT, BS 380 TO 480 PER FED-EX SRM 53-10-3.

Part: STRINGER — CORRODED (BS 950-1050)

NR 0684 044, CORROSION (C53-224-01(3)) ON STRINGER 2 LT, BS 950-1050. REPAIRED NR 2 LT STRINGER, BS 950-1050 IAW FED-EX SRM 53-10-3.

Part: FRAME — CRACKED (BS 254)

NR 0926 043, STA-PAE - WHILE WORKING NR 0920 FOUND FRAME BEHIND NR 3 WINDOW ON THE RT SIDE AT BS 254, STR 9-11 RT TO BE CRACKED. REMOVED FRAME RT SIDE AT BS 254, STR 9-11. FABRICATED FRAME FROM 7075-T6.040. ALODINED AND PRIMED. INSTALLED FRAME IAW SRM 51-10-3, 51-20-1, M/M 51-20-151 AND SRM 51-30-2.

Part: SKIN — CRACKED (BS 259.5)

NR 0920 042, WHILE PERFORMING HFEC INSPECTION OF FASTENER HOLES. FOUND CRACK EMANATING FROM HOLE AT BS 259.5, STR 8 R. REPAIRED CRACK AT BS 259.5, STR 8R PER EO 7-5330-7-2319G PT5 AND DRAWING 69-62161.

Part: LONG BEAM — CORRODED (BS 838-843)

NR 0557 041 STA-PAE - CORROSION (C53-224-01(2)) AROUND NUTCLIP HOLES LBL 45 LONGITUDINAL BEAM BS 838-843, WL 208. REMOVED AND REPLACED LBL 45 LONGITUDINAL BEAM WL 208 FROM BS 740 TO BS 848.5 PER BOEING 727 DRAWING 65-34144.

Part: BOTTLE FITTING — CORRODED (BS 870)

WHILE WORKING NR0748, DISCOVERED CORROSION ON AFT SIDE OF RT BOTTLE FITTING, BS 870, RBL 66, WL 184. *S/D* REMOVED CORROSION, BLENDED ON AFT SIDE OF RT BOTTLE PIN COATING, FOUND COATING TO BE IN LIMITS PER FED EA 7-5710-35103.

Part: SWITCHES — MOISTURE CONTAM (RT MLG DOOR)

RIGHT MAIN GEAR DOOR LIGHT ON SECOND OFFICER'S ANNUNCIATOR PANEL AND RED GEAR DOOR LIGHT ON GEAR POSITION PANEL REMAINED ILLUMINATED AFTER EXTENSION. GEAR INDICATION NORMAL AFTER RECYCLING. INSPECTED DOOR SWITCHES, FOUND SOME MOISTURE, CLEANED WITH CONTACT CLEANER. CYCLED DOOR, ALL LIGHTS NORMAL.

Part: SKIN — CORRODED (BS 1070)

BULGE IN SKIN LAP AT STR 20, BS 1070 LEFT HAND SIDE. *S/D* REMOVED CORROSION AND REPAIRED SKIN LAP AT STR 20 LEFT HAND BS 1070 PER FED-EX SRM 53-30-3 FIG 14.

Part: FLOORBEAM — CORRODED (BS 312)

CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 312, LBL 30, WL 208. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORROSION AT BS 312 FLOORBEAM UPPER CHORD LBL 30, WL 208 IAW FED-EX SRM 53-10-8 FED-EX SRM 53-10-1.

Part: SKIN — CORRODED (BS 867-872)

WHILE WORKING NR0768, DISCOVERED CORROSION ON UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190. *S/D* REMOVED CORROSION ON LOWER SURFACE OF UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190 AND REPAIRED PER FED-EX EA 7-5710-36144.

Part: CHORD — CRACKED (BS 760-770)

NR 0706 036 STA-PAE - CORROSION (C53-224-05) CRACK IN RT 70.85 PLUS CHORD IS CRACKED ON UPPER VERTICAL FLANGE IN RADIUS FROM BS 760 TO 770, WL 201, RBL 70.5 LONG CRACK REPAIR REQUIRED PER S/B 727-57-0112 REV 5. REPAIRED CRACK IN RT 70.8 PLUS CHORD PER EA 7-5710-39867 AND EA 7-5310-36807.

Part: FLOORBEAM — CORRODED (BS 620)

NR 0534 034 CORROSION (C53-224-06) AROUND FASTENERS IN THE CARGO TIE DOWN PUCK ON THE BOTTOM OF UPPER FLOORBEAM CHORD AT BS 620, RBL 62.5. REPAIRED UPPER FLOORBEAM CHORD AT BS 620, RBL 15 TO RBL 70 AS PER FED SRM 53-10-8.

Part: FLOORBEAM — CRACKED (BS 328)

NR 0857 035 WHILE WORKING NR 0822 DISCOVERED BS 328 FLOORBEAM WEB TO BE CRACKED T LBL 30, WL 206. REPAIRED BS 328 FLOORBEAM WEB AT LBL 30, WL 206 AS PER FED-EX SRM 51-40-2.

Part: CASTING — CORRODED (BS 370)

CORROSION (C53-224-06) IN FORWARD POCKET OF THE BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208. *S/D* REMOVED AND REPLACED BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208 PER FED-EX SRM 51-30-2. ALODINED AND PRIMED PER FED-EX SRM 51-10-2 AND FED-EX M/M 51-20-0.

Part: SKIN — CORRODED (BS 861.5)

NR 0832 032 CORROSION (C53-224-05) ON WING CENTER TANK UPPER SKIN LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5. REMOVED CORROSION ON WING CENTER TANK UPPER SKIN, TOP SURFACE AT LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5 AND REPAIRED PER FED-EX EA 7-5710-36144.

Part: FITTING — CORRODED (BS 227)

NR 0839 031 CORROSION ON HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45. REMOVED AND REPLACED HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45 AS PER FED-EX SRM 51-10-2, 51-10-1, 51-30-2 AND M/M 51-20-151.

Part: FITTING — CRACKED (BS 1183)

NR 0764 030 FOUND CRACK ON OUTBOARD HOLE OF STRINGER 29R, BS 1103. REMOVED CRACKED STRINGER FITTING. REPLACED WITH A NEW STRINGER FITTING AT BS 1183, STR 29R, IAW FED-EX SRM 51-30-02.

Part: STRINGER — CORRODED (BS 640)

NR 0551 029 CORROSION (C53-224-06) ON STRINGER 9 LEFT IN SEVERAL AREAS BETWEEN BS 620 AND 740. REPAIRED 59L BETWEEN BS 620-740 IAW FED 53-10-1 AND FED SRM 53-10-3.

Part: FLOORBEAM — CORRODED (BS 328)

NR 0822 028 CORROSION (C53-224-06) ON UPPER SURFACE OF TOP CHORD OF FLOORBEAM BS 328, LBL 29-32, WL 208. REPAIRED TOP CHORD OF FLOORBEAM BS 328 FROM LBL 9 TO LBL 63, WL 208 IAW FED-EX SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 1130)

NR 0840 020 STA-PAE - WHILE WORKING NR0374 FOUND DOUBLE HOLES IN UPPER SIDE OF BS 1130 CHORD, BS 1130, RBL 32 AND 37, LBL 33 AND 38, WL 208 ALSO CORROSION AND CRACK INDICATION AT LBL 33. REPAIRED UPPER CHORD OF 1130 BEAM IAW FED-EX EA 7-5310-36165 AND EA 7-5310-36165A.

Part: STRAP — CORRODED (BS 988-1090)

CORROSION (C53-111-01,3) ON CENTER STABILIZER STRAP FROM BS 988 TO BS 1090, BL 0 WL 200. *S/D* REMOVED AND REPLACED BL 0 BS 950 TO 1158, WL 200 STABILIZER STRAP PER FED-EX SRM 51-10-1 AD 51-30-2.

Part: STRAP — CORRODED (BS 873)

NR 0848 023 WHILE WORKING NR 0748 DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, TENSION LOAD STRAP AT BS 873, WL 177, RBL 65 - LBL 65. REMOVED, FABRICATED AND REPLACED TENSION STRAP AT BS 870, WL 177 FROM RBL 65 TO LBL 65 ON FWD SIDE OF WHEEL WELL BULKHEAD IAW FED-EX DRAWING 65-15978.

Part: BULKHEAD DOUBLER — CORRODED (BS 873)

NR 0851 024 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD RT RING DOUBLER, AT BS 873, RBL 58, WL 183. REMOVED, FABRICATED AND REPLACED RT RING DOUBLER AT BS 870, RBL 58, WL 183 IAW FED-EX DRAWING 69-14467.

Part: SPAR — CORRODED (BS 870)

CORROSION (C57-174-01) ON BS 870 REAR SPAR LOWER CHORD, LBL 40 TO 45, WL 138. *S/D* REMOVED CORROSION, BLENDED ON BS 870 REAR SPAR LOWER CHORD. FOUND CHORD TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED SPAR CHORD PER EA NR 7-5710-36144.

Part: BULKHEAD WEB — CORRODED (BS 870)

CORROSION (C57-174-01) ON BS 870 BULKHEAD WEB, RBL 70 - LBL 70, WL 178 TO 138. *S/D* BLENDED, REMOVED CORROSION ON BS 870 BULKHEAD WEB, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED BS 870 BULKHEAD WEB PER FED SRM 51-10-1.

Part: BULKHEAD DOUBLER — CORRODED (BS 873)

NR 0847 026 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, LEFT RING DOUBLER AT 873, LBL 58, WL 183. REMOVED, FABRICATED AND REPLACED LEFT RING DOUBLER AT BS 870, LBL 58, WL 183 IAW FED-EX DRAWING 69-14467.

Part: SPAR CHORD — CORRODED (BS 870)

NR 0748 027 STA-PAE - CORROSION (C57-174-01) ON BS 870 REAR SPAR UPPER CHORD RBL 20-60, LBL 10-40, WL 178. BLENDED, REMOVED CORROSION ON UPPER REAR SPAR CHORD, BS 870, RBL 20-60, LBL 10-40, WL 178. CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED UPPER REAR SPAR CHORD PER FED-EX EA 7-5710-36144A.

Part: STRINGER — CORRODED (BS 380)

NR 0508 018 CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380-460.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION (C53-111-01(3)) ON LOWER CHORD OF FLOORBEAM AT BS 1130, RBL 26 TO 39, WL 200. *S/D* REPAIRED FLOORBEAM LOWER CHORD IAW FEDEX EA NR 7-5310-36166A.

Part: STRINGER — CORRODED (BS 480-580)

CORROSION (C53-224-02) ON STRINGER 2 RT, BS 480 TO 540, BS 560 TO 580.

Part: FLOORBEAM — CORRODED (BS 600)

NR 0229 017 CORROSION (C53-111-01-02) ON FLOORBEAM BS 600, WL 200, LBL 20 TO RBL 25. REPAIRED FLOORBEAM AT BS 600, WL 200, LBL 20 TO RBL 25 IAW FED-EX EA NR 7-5310-35035 REV A.

Part: CLIP — CRACKED (BS 970)

CRACKED STRINGER CLIP BS 970, STR 7 RT. *S/D* DRILLED OUT FASTENERS AND REMOVED CRACKED STRINGER CLIP. POSITIONED NEW STRINGER CLIP INTO PLACE AND BACKDRILL. INSTALLED FAYING SURFACES WET WITH SEALANT AND INSTALLED NEW STRINGER CLIP. ALL WORK DONE PER FED-EX SRM 51-10-1 AND 51-30-02.

Part: STRINGER — CORRODED (BS 360-460)

CORROSION (C53-224-02) ON STRINGER 8 LT, BS 360 TO 460. *S/D* REMOVED CORRODED STRINGER AND REPLACED STRINGER BS 360 TO BS 460, STR 8 LT IAW FED-EX SRM 53-10-3 FIG 3.

Part: CLIP — CRACKED (BS 1010)

FOUR CRACKED STRINGER CLIPS AT BS 1010 AT STR 6L, 2R, 7R, 8R. *S/D* REMOVED CRACKED STR CLIPS BS 1010 AT STR 6R, 2R, 7R, 8R. INSTALLED NEW STR CLIPS AT BS 1010, STR 6R, 2R, 7R, 8R PER FED-EX SRM 51-30-2.

Part: CLIP — CRACKED (BS 1010)

FOUR EACH CRACKED STRINGER CLIPS AT BS 1010 AT STR 6L, 2R, 7R, 8R. *S/D* REPLACED FOUR EACH STRINGER CLIPS AT BS 1010, STR 6L, 2R, 7R AND 8R PER FED SRM 51-30-2.

Part: CLIP — CRACKED (BS 990)

TWELVE EACH CRACKED STRINGER CLIPS AT BS 990 AT STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 4R, 3R AND 2R. * S/D* REMOVED STRINGER CLIPS AND INSTALLED NEW CLIPS AT BS 990, STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 3R, AND 2R PER FED SRM 53-10-1.

Part: STRINGER — CORRODED (BS 420-480)

NR 0298 012 CORROSION (C53-224-02) ON STRINGER 2 RT, BS 420-480. REPAIRED STR 2 RT, BS 420-480 IAW FED-EX SRM 53-10-3 AND 51-30-2.

Part: CLIP — CRACKED (BS 970)

CRACKED STRINGER CLIP AT BS 970 STR 5 RT. *S/D* REMOVED AND REPLACED STR CLIP AT BS 970, S5R IAW FED SRM 51-10-1 AND SRM 51-30-2.

Part: CLIP — CRACKED (BS 1050)

SEVEN EACH CRACKED STRINGER CLIPS BS 1050 AT STR 6L, 5L, 4L, 3L, 2L, 5R, 3R. *S/D* REPLACED 7 EACH STRINGER CLIPS, BS 1050, STR 6L, 5L, 4L, 3L, 2L, 5R AND 3R PER FED-EX SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 740)

CORROSION (C53-224-06) ON NOT CLIP AND DOUBLER UNDER AFT SIDE OF UPPER FLOORBEAM CHORD AT BS 740, RBL 49 AND ON PREVIOUS BLEND OUT UNDER FWD SIDE OF UPPER CHORD AT RBL 47. *S/D* REMOVED OUT OF LIMITS AREAS ON NUTCLIPS AND DOUBLER UNDER AFT SIDE OF UPPER FLOORBEAM CHORD AT BS 740, RBL 49 AND ON PREVIOUS BLENDOUT UNDER FORWARD SIDE OF UPPER CHORD AT RBL 47 BY CUTTING TEE INSERT AT BS 740, RBL 36 TO RBL 65 AND REPAIRED PER FED-EX SRM 53-10-4.

Part: CHORD — CORRODED (BS 460-740)

CORROSION (C53-111-01-02) ON BL 0 CHORD BS 500 TO BS 686, WL 200. *S/D* REMOVED AND REPLACED THE BL 0 CHORD BS 450 TO BS 740, WL 200 PER FED-EX SRM 51-10-01, AND SRM 51-30-02 AND PER BOEING DRAWING SR 27-53-009.

Part: CLIP — CRACKED (BS 1030)

SIX CRACKED STRINGER CLIPS AT BS 1030 AT STRINGERS 2L, 3L, 4L, 5L, 6L, 3R. *S/D* REMOVED 6 STRINGER CLIPS BS 1030, STR 2L, 3L, 4L, 5L, 6L AND 3R. INSTALLED NEW STRINGER CLIPS AT BS 1030, STR 4L, 5L, 6L AND 3R, IAW FED-EX SRM 51-30-2. STR CLIPS AT BS 1030 STRS 2L AND 3L WILL BE INSTALLED ON RO 684.

Part: CLIP — CRACKED (BS 1070)

SIX EACH CRACKED STRINGER CLIPS AT BS 1070 AT STR 8L, 3L, 2L, 8R, 6R, 3R. *S/D* REPLACED 6 EACH STRINGER CLIPS AT BS 1070 AT STR 8L, 3L, 2L, 8R, 6R AND 3R PER FED-EX SRM 51-30-2.

Part: STRAP — CORRODED (BS 366)

NR 0382 CORROSION UNDER SEAT TRACK AT BS 388, RBL 65, WL 208. REMOVED CORROSION UNDER SEAT TRACK FLANGE. CORROSION ON SEAT STRAP FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPLACED STRAP PER FED-EX SRM 51-10-1. CORROSION CLEAN-UP PER FED-EX SRM 51-10-6.

Part: RETRACT MECH — LACK OF LUBE (NLG)

CDG - UPON GEAR EXTENTION LT AND RT MAIN GEAR INDICATED DOWN AND LOCKED WITH GREEN LIGHTS, NOSE GEAR RED LIGHT ILLUMINATED, DID NOT HEAR ANY INDICATION THAT NOSE WHEEL EXTENDED. LUBRICATED NOSE GEAR ASSY PER MM 12-21-11, PERFORMED TEST NOTE GEAR RETRACTION AND EXTENSION, ALL NORMAL, 8 SEC FOR GEAR EXTENTION. INSPECTED LOCK ACTUATING ROD AND LOCK MECHANISM FOUND ALL OK, A/C OK FOR SERVICE.

Part: DOOR FRAME — CRACKED (PAX DOOR)

AFT ENTRY DOOR L/T SIDE FRAME PREVIOUS REPAIRED CRACK ISN'T CONTAINED AT STOP DRILL (2 PLACES). REMOVED DAMAGED AREA FROM WL 218 TO 239, FABRICATED AND INSTALLED NEW SEGMENT OF FRAME AND SPLICE DOUBLERS PER FED EX SRM 51-40-3.

Part: BONDING STRAP — CORRODED (NR 1 LE FLAP)

NR 1 K-FLAP O/B LOWER BONDING VAMPER UPPER ATTACH POINT IS CORRODED. CLEANED AND TREATED PER EWO NR 95-2426, CORROSION ON NR 1K-FLAP O/B LOWER BONDING VAMPER ATTACH POINT AS WELL AS FEDEX EA 7-5750-24438.