N166FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DELAMINATION ON LWR SURFACE OF THE SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE, LH WING SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE LH WING WAS REPAIRED IAW B767 SRM 57-70-01-2R FIG 201 REP 1 SHEET 2 AND SRM 51-70-17-0G PAR 4 "A" FIG 10 SHEET 1 REV 94 DEC 15/2025
CRACK L=2.500" ON UPPER SURFACE OF FLOOR PANEL 242SFF AT MDC. FLOOR PANEL 242SFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025
DENT ON UPPER SKIN WEDGE OF SLAT NR 8 OSS 457 SLAT NR 8 OSS 457 WAS REPAIRED IAW SRM 57-43-02-2R FIG 201 SHEET 1 AND SRM 51-70-10-2R PAR G FIG 209, SHEET 1, REV 94. DEC 15 /2025
TWO PUNCTURES ON UPPER SURFACE OF FLOOR PANEL 242VFF AT MDC FLOOR PANEL 242VFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025
SEVEN CRACKS L=1.200" ON UPPER SURFACE OF FLOOR PANEL 241WFF AT MDC FLOOR PANEL 241WFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025.
PUNCTURE ON UPPER SURFACE OF FLOOR PANEL 241ZFF AT MDC FLOOR PANEL 241ZFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 12/2025.
PUNCTURED FLOOR PANEL 232EFF.SEC 43 OF MDC. FLOOR PANEL 232EFF SEC 43 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15,2025.
PUNCTURED FLOOR PANEL 242AFF. SEC 45 OF MDC. FLOOR PANEL 242AFF. SEC 45 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2. REV. 94 DEC 15,2025.
ACTIVE HYDRAULIC LEAK FROM RIGHT WING JUST OUTBOARD OF RIGHT MAIN GEAR FOUND LINE LEAKING FLUID FROM LG UP CTR SYSTEM. OPENED RIGHT WING PANEL 651TB TO ACCESS LINE THAT IS LEAKING IN REFERENCE TO AMM LISTED ABOVE. REMOVED CENTER HYDRAULIC SYSTEM RIGHT MAIN GEAR ACTUATOR -UP- HYDRAULIC TUBE AND INSTALLED TEMP FLEX HOSE IAW ABOVE, BLED LINE IAW 32-32-01-4 AND FLEX HOSE LEAK CHECKED GOOD. ITEM PLACED ON OIL AND REQUIRES REINSPECTION EVERY 7 DAYS AND PERMANANET REPAIR AT NEXT LSY CHECK
RIGHT WING SPOILER NO. 8 LOWER SURFACE WITH PUNCTURE R.H. WING SPOILER NO. 8 LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01 REP. 1, FIG 201 SHEET 1, 2, 4, PAGE 1-4 AND SRM 51-70-17-0G PARA. 4.C. PAGE 1, 25, 26, 36, 49; FIG. 11 REV. 82 DEC15/2021
RIGHT WING SPOILER NO 7 LOWER SURFACE WITH PUNCTURE. RIGHT WING SPOILER NO 7 LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01 REP. 1, FIG. 201 SHEET 1, 2, 4, PAGE 1-4 AND SRM 51-70-17-0G PARA. 4.C. PAGE 1, 25, 26, 36, 49; FIG. 11 REV.82 DEC15/2021
ON FINAL APPROACH, CAPTAIN`S FLIGHT AND NAV DISPLAY WENT BLANK FOR 5 SECONDS AFTER APP TILE SELECTED. DISPLAY RETURNED TO NORMAL. UPON SHUTDOWN, STBY INVERTER ON STATUS PAGE. R & R STATIC INVERTER IAW AMM 24-33-03-4. OPS CHECK GOOD.
LT WING NR 5 SLAT LOWER SURFACE L/E AREA DAMAGE 2 (EA), PLACE AS MARK STREAMER ATTACH. REPAIRED NR 5 SLAT LOWER SURFACE 1EA AREA 89.5" FROM O/B, IAW B767 SRM 57-43-02-2R REPAIR 1 AND 51-70-10-2R REPAIR 4 FIG. 202; 1EA AREA 47.5" FROM O/B FOUND MISSING PAINT NO DAMAGE SKIN, NO DELAM, NO REPAIR, REQUIRED IAW B767 57-43-2R-1A FIG 101.
PDIS 166 24-50 0296 09JAN19 MEM LOST L AND R UTILITY BUS DURING APPROACH TO MEM. THEN LOST R GENERATOR. LOST AUTOPILOT, AUTO THROTTLES, GEAR INDICATIONS. EXECUTED MID ALTITUDE GO AROUND. COULD NOT RAISE GEAR OR FLAPS. RAN QRH FOR R GEN, CYCLED UTILITY BUSSES W/ NO HELP. BUT GEAR INDICATION RETURNED. LANDED KMEM 36L FLAPS 25. REFERENCE FIM 24-20-00-2 AND WDM 24-22-21. VERIFIED INTEGRITY OF RIGHT GCB TRIP ISOL DIODE, R5. DIODE CHECKS GOOD. REMOVED AND REPLACED THE RT IDG AMM 24-11-01-4. OPS CHECK AND LEAKS CHECK SATISFACTORY. REF ALSO TSI 24-10-0297, WORKED IN CONJUNCTION WITH.
F/O ESCAPE ROPE DOOR STILL FALLING OPEN IN FLIGHT. EMERGENCY ESCAPE ROPE COVER OVER FIRST OFFICERS HEAD WILL NOT STAY CLOSED. APPEARS LATCH IS NOT FULLY ENGAGED WHIN CLOSED. FOUND COVER LATCH STUCK. ADJUSTED LATCH. OPS CHECK GOOD PER AMM 25-61-03-2.
PDIS 166 27-80 0117 26OCT18 MEM FACT U LOGPAGES:2670727 LE SLAT DISAGREE WHEN GEAR SELECTED DOWN & FLAPS 20. RAN QRH, LANDED F20. RETURNED FLAPS ON DECK VIA ALT MEANS. NO OVERSPEED. FACT 26OCT18 08:17 MEM U WITH NO HISTORY NOTED. PERFORMED BITE CHECK OF PSEU REF FIM 32-09 FAULT TREE 803, NO FAULTS NOTED. PERFORMED BITE CHECK OF FSEU REF FIM 27-51 FAULT TREE 809, NO FAULTS NOTED. PERFORMED OPS CHECK OF FLAP AND SLAT PRIMARY DRIVES AND POSITION INDICATING SYSTEMS TEST REF AMM 27-51-00-705-508. SYSTEM TEST GOOD, NO AJUSTMENT WERE MADE. IN ADDITION PERFORMED SLAT ALTERNATE AND DRIVE SYSTEM TEST REF AMM 27-81-00-735-277. SYSTEM TEST GOOD, NO ADJUSTMENTS WERE MADE. A/C OK FOR SERVICE.
WX RADAR FAILED 5 MIN AFTER T/O CYCLED C/B NO JOY TURNED RT ON AND OFF SEVERAL TIMES REMAINED FAILED. REPLACED WX R/T, GRD OPS CK NORMAL MM 34-41-041. REMOVAL/INSTALLATION, OFF MFG 622-5132-101, POS ONL SRL 2652 TAG A03946 ON MFG 622-5132-101 SRL 3939 TAG A15647.
ON TAXI OUT, NR 1 STALL WARNING STICK SHAKER ACTIVATED MOMENTARILY THEN STOPPED. ABOUT 3 MINUTES LATER, IT REACTIVATED AND PULLED THE NR 1 STALL WARNING C\B TO DEACTIVATE. ON TAXI IN SMOKE BEGAN TO EMANATE FROM BEHIND GLARE SHIELD. EVACUATED AIRCRAFT. REMOVED AND REPLACED ACM TEMP SWITCH PER M/M REF 21-51-011-4.
N01259 RT HAND HORIZONTAL STAB L/E UPPER CHORD CRACKED ON LWR SURFACE BETWEEN L/E STAB STA 1.0 TO L/E STAB STA 72.0. FOUND RT HORIZ STAB L/E UPR CHORD OUT OF LIMITS. TRIMMED OUT SEGMENT OF CHORD, FABRICATED NEW CHORD FROM REF. PO 179160, SPLICE FROM BAC1490-2811 & 7075T6, 586206, 7075T6 .071 514703. ALODINE, PRIMED AND INSTALLED UPR CHORD AND SPLICE REPAIR PER SRM 55-10-5, 51-30-5, 51-30-2.
EXTERNAL SKIN CRACKED AT AFT LWR CARGO DOOR CUTOUT 10 INCHES AFT OF THE FWD LWR CORNER 2 INCHES BELOW LWR EDGE. REPAIRED CRACKED SKIN, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA 7-5330-82517.
WHILE ACCESSING FRONT SPAR WEB FOR UPR SPAR REPAIR, LWR FRONT SPAR VERTICAL FLANGE CRACKED BETWEEN LT L/E STA 109 & 119. REPAIRED IAW SRM 55-10-5.
CORROSION LT HORIZONTAL STAB FIXED L/E INTERNAL VERTICAL WEB L/E STA 29. *S/D* REPAIRED PER SRM 55-10-1 FIG 1, 51-30-2, 51-10-1, 55-10-4, 51-30-5.
COMPLY WITH EO 7-5330-7-2319 PART 5 BS 441 AT STR 19-20 RT AND STR 20-21 RT. *S/D* REPAIRED FUSE SKIN BS 441 STR 19-21 RT IAW EO 7-5330-7-2319 AND EA 7-5330-82513.
UPPER EXTERNAL SKIN BS 761, 2 INCHES ABOVE STR 4 LT IS GOUGED. BLENDED GOUGE ON SKIN BS 761, 2 INCHES ABOVE STR 4 LT, OUT OF LIMITS. REPAIRED DAMAGE SKIN AT BS 761 STR 4 LT PER SRM 53-30-3 FIG 5.
LT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING.
CORROSION BS 480 STR 4R - STR 6R UNDER FWD SIDE OF THE SPLICE. FOUND VISUALLY, DURING DETAILED VISUAL INSPECTION. CORROSION NOT FOUND DURING LOW FREQUENCY INSPECTION. CORROSION BS 480 STR 4R TO 6R UNDER FWD SIDE OF SPLICE REPAIR ON W/C N01202 AND EO 7-5330-7-2319 PT 5.
CORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE.
CORROSION LT FWD EMERGENCY ESCAPE DOOR UNDER SIDE OF LWR FRAME BACK SIDE OF OUTER SKIN 7 INCH UP FROM LWR AFT CORNER.
AFT CARGO FRAME DENTED AT BS 970, STR 26R.
FRAME BS 1010 LT BETWEEN STR 24 AND 25 DENTED.
CORROSION MECHANICAL DAMAGE ON FLOORBEAM BS 680 UPPER CHORD LWR SURFACE AT LBL 64 WL 208.
LT WING I/B MID FLAP TRAILING EDGE CHORD CRACKED AT THE I/B AFT FLAP ACTUATION ROD CUT OUT. REPAIRED PER SRM 51-40-4, 51-30-2, OHM 20-50-01, 20-50-02.
CORROSION LT HORIZONTAL STAB UPPER FRONT SPAR CHORD INTERNAL SURFACE IN AREAS FROM STAB STA 4.45 TO STAB STA 33. REPAIRED IAW SRM 51-10-6. 51-30-2, 51-10-2, 55-10-5.
RT HORIZ STAB UPPER SKIN LOWER SURFACE HAS CORROSION (C55-300-10(2)) EMANATING FROM BONDED DOUBLERS 33 INCHES FROM AFT EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN LOWER SURFACE FOUND TO BE OUT OF LIMETS REPAIRED PER FED-EX EA 7-5510-82519 AND FED-EX EA 7-5510-82518.
CORROSION ON LT HORIZONTAL STAB INTERNAL UPPER FRONT SPAR CHORD STAB STA 64. REPAIRED IAW SRM 51-10-6, 51-30-2, 51-10-2, 55-10-5.
FRAME BS 990 LT AT STR 24 DENTED. REPAIRED PER SRM 51-40-3.
RT HORIZ STAB UPPER SKIN HAS SHEARED FASTENER AND SKIN BULGE 31 INCH FROM TRAILING EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN FOUND TO BE CORRODED BEYOND LIMITS AND WILL BE REPLACED ON FED EX W/C N01050.
N01167 CORROSION ON LT. HORIZ. STAB UPPER SPAR AT STAB STA. 198. REPAIRED PER SRM 55-10-5 FIG 1
FLOORBEAM CORRODED RBL 18, W/L 200. REPAIRED PER SRM 53-10-8
MAIN CARGO BAY HAS 2 GOUGES ON STR 16R AT BS 554 AND BS 557. GOUGES ON STR 16R BS 554 AND BS 557 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED STR 16R IAW SRM 53-10-3.
CORROSION AT FLOORBEAM UPPER AND LOWER SURFACE BS 344 LBL 10 - RBL 10. REPAIRED FLOORBEAM BS 344 LBL 10 - RBL10 PER SRM 53-10-1 AND FEDEX SR 27-53-007.
MECHANICAL DAMAGE ON FLOORBEAM STA 700 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8
MECHANICAL DAMAGE ON FLOORBEAM BS 720 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8
FRAME BS 1030 LT AT STR 24 AND 25, DENTED. REPAIRED FRAME PER SRM 51-40-3.
CORROSION ON RT WING O/B AILERON I/B CTR FITTING A/C SIDE IS CORRODED ON LOWER SURFACE. REPAIRED PER MM 27-10-031-2, SRM 51-30-2, 51-30-5.
FUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED AT STA 880-890, LBL 47, WL 206. REPLACED VERTICAL WEB PER SRM 51-10-2, 51-30-2 & SRM 51-30-5.
MAIN CARGO BAY HAS GOUGE ON STRINGER 9R AT BS 600.
FUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED, STA 880-890 RBL 47, WL 206. REPAIRED PER SRM 51-30-2, 51-30-5, 51-10-3, 51-10-2
STRINGER CLIP CRACKED, STR 5L, BS 1010. REPLACED PER SRM 51-30-2, 51-30-5
FOUND CORROSION ON FLOORBEAM AT BS 620 BL O - LBL 8 (C53-111-01(3)). CORROSION REMOVED ON FLOORBEAM FOUND TO BE OUT OF LIMITS. FLOORBEAM TO BE REPAIRED ON N00920.
SEAT TRACK GOUGED AT BS 740, RBL 45, WL 208. REPAIRED SEAT TRACK PER SRM 53-10-5.
CORROSION FLOORBEAM STA 620 LWR CHORD LWR SURFACE CORRODED LBL 8 AROUND NUTPLATE HOLE. REPAIRED PER SRM 53-10-1, 53-10-8
CORROSION (C53-224-01) AT FLOORBEAM UPPER CHORD AT BS 620, LBL 45-65, WL 208.
BS 294, STR 21 RT, DENTS AROUND 3 FASTENERS. REPAIRED PER SRM 53-30-1, 53-30-3.
STRINGER CLIP CRACKED BS 1108 LT STR 20. REPLACED STRINGER CLIP PER SRM 51-30-2.
BS 1108 AFT CARGO DOOR FRAME AT STR 26 HAS A OPEN HOLE IN UPPER FLANGE. REPAIRED AFT CARGO DOOR FRAME PER FED EX EA 7-5310-825111.
GOUGE ON UNDERSIDE FLANGE OF STR 19 RT, BS 488, WL 174. REPAIRED STR 19 RT IAW SRM 53-10-3 FIG 1 AND 53-10-1.
FWD CARGO STA 540 FRAME DENTED AT STR 24 LT & 25 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-1, 51-20-4, 53-10-1.
FWD CARGO FRAME STA 660 DENTED STR 24 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-4 AND 53-10-1.
TOP FLANGE OF FRAME AT BS 640, RBL 32, WL 150 IS DENTED. REPAIRED PER SRM 53-10-1, 51-30-5, 51-20-4, 51-30-2, 51-10-1, 53-10-2 AND 51-40-3
RT ELEVATOR NR 5 HINGE SUPPORT RIB ELEVATOR STA 136.50 PREVIOUS REPAIR AT I/B LOWER FLANGE IS CRACKED. REPLACED PER E.O. 7-5510-7-5001 PT 2.
AFT CARGO FRAME DENTED AT BS 990, STR 26R. REPAIRED PER SRM 51-40-3.
AFT CARGO FRAME DENTED AT BS 990 STR 26 LT. REPAIRED PER SRM 51-40-3, 51-10-2 AND 51-30-2.
AFT CARGO FRAME DENTED AT BS 1030, STR 26R. REPAIRED PER SRM 51-40-3.
AFT CARGO FRAME DENTED AT BS. 1010 STR 26R. REPAIRED PER SRM 51-40-3
FRAME DENTED AT BS 1090, STR 23 LT. REPAIRED PER SRM 51-40-3.
STR L23 DAMAGED AT BS 376 TO 388. REPAIRED PER SRM 53-10-3.
AFT CARGO DOOR EXTERNAL SKIN GOUGED AT LWR EDGE, 17 INCH FROM AFT EDGE. REPAIRED SKIN IAW SRM 52-00-3.
MDIS 166 53-30 0004746 26JUN03 BFM CLOSER COMPLY WITH EA NR 7-5330-70966 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR (AD 2002-16-19). FACT 27JUN03 14:10 BFM R COMPLIED WITH EA NR 7-5330-70966, FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR (AD2002-16-19).
AFT GEAR RETRACTION, LMG DOOR RED AND AMBER LIGHT DID NOT EXTINGUISH. RECYCLED THE GEAR AND LIGHT EXT IND ALL GEAR DOOR UP. ADJUSTED LANDING GEAR DOOR SWITCH PER 727-100 MM 32-62-011-4. OPER CK NORM.
SHORT FINAL RUNWAY 36R MEM, NORM GEAR EXT CREW OBSERVED NO DOWN GROUND IND ON LEFT MAIN GEAR. NOSE AND R/M IND DOWN NORM. CAPT PERFORMED GO-AROUND AFTER RECYCLING GEAR TO NO AVAIL. DID MAN GEAR EXT CKLIST AND GOT VISUAL CONFIRMATION FROM TOWER. LANDED, PINNED GEAR AND TAXIED IN. INSP LEFT GEAR WELL, ALL SWITCH AND WIRING NORM. FOUND BULBS BURN OUT FOR LEFT GEAR IND. REMOVED AND REPLACED BULBS AND IND ON LEFT GEAR OPER NORM, OK FOR SERVICE.
CORROSION (C53-113-01,1) ON RT KEEL BEAM BETWEEN BS 620 TO 640, WL 148. *S/D* REPAIRED RT KEEL BEAM BETWEEN BS 620 TO 640, WL 148 PER FED-EX EA 7-5310-35067.
NR 0291 015 CORROSION ON UPPER SURFACE OF WING SKIN BS 850, LBL 82, WL 200. COMPLIED WITH EA 7-5730-35048.
CRACK ON UPPER FLANGE OF FRAME BS 1050, RBL 9, WL 155 ON PREVIOUS REPAIR, CRACK EXTENDS .5 BEYOND STOP DRILL HOLE. *S/D* CUT OUT DAMAGED FRAME SECTION AND REPAIRED PER FED-EX SRM 53-40-3.
NR 0167 012 CORROSION (C53-132-02(1)) ON 870 CENTER WING ACCESS PANEL, BS 870, LBL 4, WL 170. (INTERNAL TANK ACCESS IS REQUIRED.) REMOVED .020 CORROSION IN A 2.3 BY 11.9 AREA ORIGINAL THICKNESS .050 OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED 870 CENTER WING SPAR WEB AND ACCESS PANEL PER FED-EX SRM 51-10-2 AND 51-30-2.
NR 0165 013 CORROSION (C53-224-05) ON T-CLIP, FWD SIDE, RBL 69, BS 760, WL 205. FOUND T CLIP TO BE CORRODED OUT OF LIMITS ON BS 760, WL 205, RBL 69. FABRICATED T CLIP AND INSTALLED IAW FED-EX SRM 53-30-5, 51-10-2, M/M 51-20-151, 51-20-21.
CORROSION ON NR 1 K-FLAP CENTER HINGE LUG ON AIRCRAFT SIDE UNDER BOTH I/B AND O/B LUG SCREWS. REMOVED AND REPLACED NR 1 K-FLAP CENTER HINGE FITTING.
CORROSION (C53-113-01,2) IN STR 27, RIGHT BS 970 TO 1035. *S/D* REMOVED CORROSION IN STR 27 RT, BS 970 TO 1035. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED STR 27 RT, BS 970 TO 1035 PER FED-EX SRM 51-30-2, AND 51-10-1.
CORROSION (C53-132-02- 1/2) WING CENTER SECTION LOWER FRONT SPAR CHORD BS 740, RBL 10 AND RBL 26 TO 30, WL 164.
CORROSION (C53-132-02 1/2) WING CENTER SECTION LOWER REAR SPAR CHORD VERTICAL LEG BS 870, LBL 10 TO RBL 10, WL 164.
CORROSION (C53-224-05) ON RT 70.5 PREVIOUS REPAIR ANGLE, BS 754 TO 760, RBL 70.5, WL 204. *S/D* CORROSION ON ANGLE, BS 754 TO 760, OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED ANGLE PER FED-EX SRM 51-10-1.
LT WING I/B MIDFLAP T/E WEDGE DELAMINATED FROM 18 TO 26 FROM I/B END. *S/D* REPAIRED LT WING I/B MIDFLAP T/E WEDGE IAW FED-EX SRM 51-40-06 AND 51-30-02.
CORROSION (C53-132-02 1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, LBL 70 TO RBL 70, WL 188.
CORROSION (C53-113-01, 2) IN STR 30, WL 148, BS 970 TO 1080. *S/D* REMOVED CORROSION IN STR 30, WL 148, BS 970 TO 1080. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED STR 30, WL 148, BS 970 TO 1080 PER FED-EX SRM 53-10-3, 51-30-2, AND 51-10-1.
NR 0308 003 CORROSION (C55-300-10-2) RT HORIZONTAL STAB UPPER T/E BEAM AT APPROX ELEV STA 147.5 (IN BALANCE BAY NR 4).
LEFT WING O/B MIDFLAP T/E WEDGE DELAMINATED IN SEVERAL AREAS FROM 17 TO 141 FROM I/B END. *S/D* REMOVED AND REPLACED LEFT WING OUTBOARD MIDFLAP IAW FED-EX M/M 27-51-11.
RIGHT WING O/B MIDFLAP T/E WEDGE DELAMINATED FROM 66 TO 72 INCHES AND 115 TO 124 INCHES FROM O/B END. *S/D* REMOVED AND REPLACED RIGHT WING O/B MIDFLAP IAW FED M/M 27-51-13, DUE TO CORROSION ON MIDFLAP FRONT SPAR UPPER SURFACE.