N101FE
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
FSS DISPLAY SHOWS UNARMED STATUS WHILE INFLIGHT. AMM: 26-90-03-2 EA: H-2624-T0387831 C/W E.A. H-2624-T0387831 TO RE-PIN D2166D PIN G8 TO F8. REACTIVATED FSS SYSTEM PER AMM REF ABOVE. CLOSED ALL DOORS AND SYSTEM PASSED AUTO ARM. NO FURTHER DEFECTS NOTED. PLACARD REMOVED. THIS ACTION CLEARS MEL.
#1 ENG WERE OB SHEAR TIE (FWD OF SKIRT BEAM) HAS CHAFFED INTO THE FWD BULKHEAD OF TORQUE BOX. DURING CURRENT HMV CHECK IN INDIANAPOLIS, IN (IND), MAINTENANCE DISCOVERED CHAFE AND GOUGE DAMAGE TO THE LH PYLON AFT ENGINE MOUNT BULKHEAD FITTING, P/N 311T2261-10 (-9 ASSY). THE DAMAGE IS TO ONE OF THE FLANGES NEAR THE TOP OF THE PART AT THE OUTBOARD AREA. SEE FIGURE 1 FOR DAMAGE LOCATION AREA. THE DAMAGE WAS CAUSED BY A BROKEN SHEAR TIE, P/N 313T3310-1157, WHICH IS PART OF THE SKIRT BEAM ASSY. THE BROKEN PART OF THE SHEAR TIE (STEEL) GOUGED INTO THE BULKHEAD FLANGE (ALUMINUM) DURING OPERATION. REPAIRED FITTING AND REPLACED SHEAR TIE USING EA H-5450-T0381500P1 (ERS 24-03203). FABRICATION OF SHEAR TIE DONE ON NR 147 (WO 89281) TO INCLUDE EA H-5400-T0381470P1 REV A (ERS 24-3217). REFERENCE DRW'S 311T2261, 311T2260 & DRW313T3310.
FOUND 2ND FROM THE BOTTOM IN WEB, WHERE STIFFENER ATTACHES AT STA. 246 LBL 24 HOLE DAMAGED, DAMAGE REMOVAL AT LBL 24 HOLE IS CURRENTLY 0.359" IN WEB MADE OF 0.025 7075-T6 WEB ATTACHES TO ANGLE ON FWD SIDE PN #141T5814-136. REPAIRED PER E.A.#:H-5310-T0381485 TITLED: FUSELAGE - MAINFRAME - WEB DAMAGE FLOOR BEAM STA 246.0, LBL 25 - GOUGE DAMAGE TO A FASTENER HOLE - SPLICE REPAIR. "MAJOR REPAIR"
RH PYLON PNL# 447BL FOUND WITH MISSING TOP FIBERGLASS SKIN PLYS MISSING AND PAINTED OVER. REPAIRED TOP SKIN ON RH PYLON (PNL#447BL/MPN: 313T3341-9110) IN REF. TO 767 SRM 54-52-70- 2R FIG. 201 SHEET 4, AND 767 SRM: 51-70-08. THIS IS A MAJOR REPAIR. SEE JPF FOR OTHER WORK ACCOMPLSIHED.INSTALLATION OF PANEL WILL BE DONE ON SEQ# 831 WO#89281.
MAIN CARGO COMPARTMENT POSITION 12L APROX STA. 1383, FLOORBOARD ON LEFT SIDE HAS 1 PUNCTURE. MARKED WITH DOT #58. REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PANEL #251VFF, AT STA 1383 FLOORBOARD BETWEEN LBL 80.5"- LBL 82", P/N (146T5869-27), IN REF. TO SRM 53-00-50-2R FIG. 201 REPAIR 1 SHEET 1. THIS IS A MAJOR REPAIR.
MAIN CARGO COMPARTMENT, CENTER FLOORBOARD BETWEEN POSITION 6 AND 7 HAS 3 EA PUNCTURES. MARKED WITH DOT #'S 55, 56, AND 57. REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PANEL # 241WFF, AT STA 1033- STA 1060 CENTER FLOORBOARD BETWEEN RBL 3"- LBL 5.5", P/N (145T5876-51), IN REF. TO SRM 53-00-50-2R FIG. 201 REPAIR 1 SHEET 1. THIS IS A MAJOR REPAIR.
MAIN CARGO DOOR EICAS MESSAGE AND CARGO DOORS LIGHT ILLUMINATED AT CRUISE FL350 TIME 0051Z. ALSO HAD RISING CABIN PRESSURE. RAN QRH AND DESCENDED TO 10,000 FEET PER QRH. AFTER LEVELING AT 10,000 FEET, EICAS MESSAGE AND CARGO DOORS LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES. DIVERT TO KIND UNEVENTFUL. DECLARED EMERGENCY. EMERGENCY DECLARED VERBAL DEBRIEF FROM CREW: AT FL 35,000 CABIN ALTITUDE SET TO 4,500FT AND IT ROSE TO 9,500FT. CABIN PRESSURIZATION AUTO 1 WAS IN USE DURING THIS. VISUALLY VERIFIED ALL DOOR LATCH CAMS LOCKED IN THE CLOSED POSITION. PROCEEDED TO MOVE THE UNLOCK SWITCH TO THE MAIN CARGO DOOR LATCH CAMS AND THE SWITCH WAS UNRESPONSIVE. THEN PROCEEDED TO ACTUATE THE SWITCH TO THE LOCKED POSITION AND AUDIBLY HEARD THE MAIN CARGO DOOR MOTOR ACTUATE FOR 1 SECOND. PROCEEDED TO THEN MOVE THE SWITCH TO THE UNLOCK POSITION AND THE MAIN CARGO DOOR OPERATED NORMALLY. VISUALLY INSPECTED MAIN CARGO DOOR LATCH CAMS, LATCHES AND SENSORS. NO DEFECTS NOTED. TROUBLESHOT PER B767 FIM 52-90-20-00 AND AMM 52-71-09-2 STEP 8 & 9. OPS CHECKED MULTIPLE TIMES, OPS CHECK GOOD. A/C OKAY FOR SERVICE.
FUSELAGE SKIN EXTERNAL SURFACE FOUND 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R REPAIRED THE FUSELAGE SKIN EXTERNAL SURFACE 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R PER B767 SRM51-40-02 & B767 SRM53-00-01-2R REPAIR.14. THE REPAIR IS CATEGORY B, FOLLOW UP INSPECTION PER B767 SRM53-00-01-2R REPAIR.14. TABLE V: INSPECTION THRESHOLD 30,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 6,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION, WHICH EVER COMES LATER. INTERVAL: 9,000 FLIGHT CYCLES. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
APU SHUTDOWN- FAULT LIGHT AFTER T.O. APPROXIMATELY 2000 FEET. APU IS REQUIRED PER MEL 24-00-01-01-B. ATTEMPT RESTART AS PER QRH. RESTART SUCCESSFUL. ON ARRIVAL APU SHUTDOWN AND FAULT INDICATED AGAIN. PERFORMED APU BITE PROCEDURE IAW FIM 49-11 FAULT TREE 987 SHOWS HIGH OIL TEMP. TROUBLESHOT IAW FIM 49-11 FAULT TREE 996 AND RESET APU ECU. RAN APU PER B767 JRH FOR ONE HOUR FOUND NO FAULT. APU STARTED NML AND ALL PARMETERS NML. ACFT OK FOR SERVICE.
.RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN CRACKED , LOC:APPROX 120CM FROM INBD EDGE TO OUTBD EDGE. PERFORMED THE REPAIR ON RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN PER B767 SRM 57-53-01-2R AND SRM 51-70-17. THE RSC TRACKING EA # :H-5750-T0362239 P1 WAS ISSUED AND COMPLETED. EA TITLE: WINGS-FLIGHT SURFACES-RH WING OUTBOARD FLAP NOSE SKIN REPAIR-RSC TRACKING. THIS REPAIR WAS CAT A REPAIR AND CLASSIFIED AS MAJOR REPAIR PER FEDEX GMM 6-2-100
VERY STRONG BURNING ODOR ON TAKEOFF ROLL. PERFORMED RTO AT 120 KNOTS. IAW TSI 72-00/7281 COMPLETED WITH BIRD STRIKE INSPECTION IAW FIM 71-05 FAULT TREE 872, COMPRESSOR STAGE 1 AND STAGE 12 BORESCOPE INSPECTION IAW AMM 72-00-00-6, NO DAMAGE FOUND. PERFORMED PACK INSPECTION AND OPERATION TEST WITH ENG RUN IAW AMM 21-00-21-2 & 21-51-00-5-3, NO ABNORMAL FOUND. PUT LT & RT PACK IN FULL COLD AND WARM POSITION TEN MIN, NO PECULIAR SMELL. FEELING RUN TEST, ALL PARAMETERS NORMAL.
ELECTRICAL FIRE IN LOWER LEFT SIDE OF OVERHEAD LIGHTS CONTROL PANEL CREW SAW AN ELECTRICAL FIRE ON OVERHEAD PANEL. SMOKE AND BURNING ODOR DETECTED. TROUBLESHOOT AND FOUND THE PANEL/FLOOD SWITCH S1 WIRES BURNED. REMOVED AND REPLACED THE LIGHT SWITCH IAW AMM 33-13-00-2, TESTED NORMAL IAW AMM 33-42-00-5, CHECKED NORMAL. REMOVED AND REPLACED THE LEFT LIGHTING CONTROL PANEL ASSY IAW MM 33-13-00-2, INSTALLED THE ORIGINAL LIGHT SWITCH TO THE OLD PANEL. ACFT OK FOR SERVICE.
PDIS 101 25-60 6211 18JUL19 ICN OPEN U LOGPAGES:3139917 F/O EMER ESCAPE ROPE DOORS KEEPS DROPPING OPEN AND WOULD NOT REMAINED CLOSED. ITEM DEFERRED PER THE NEF PROGRAM ITEM DEFERRED PER THE NEF: 25-10-26 FO ESCAPE ROPE STOWAGE COVER DOOR INOP. SECURE CLOSED. APPLIED FAR 25 COMPLIANT TAPE FABRICATE A STRIP OF TAPE WITH A 2 INCH PULL TAB ON THE END OF THE TAPE STRIP & APPLIED AS REQUIRED TO SECURE THE DOOR IN THE CLOSE POSITION ALSO COVER FUNCTION NORMALLY.
AT FL 340 HEARD LOW RUMBLING & LOW VIBRATION ON OUR FEET, NOISE & VIBRATION CEASED AT FL 160 ON DESCENT. ALL INDICATIONS NORMAL GOOD CABIN PRESSURE. AS A RESULT OF INSP FOUND RT RAD MISSING AND HINGE BROKEN. PERFORMED AIRFRAME VIBRATION CONDITIONAL INSPECTION PER AMM 05-51-38-2 IN PROGRESS. DETAILED INSP OF RT PACK RAD INLET, EXHAUST & NOZZLE-WATER SPRAY SYS FOUND NO DEFECTS NOTED. ALSO NO ANY OBSTACLES/DAMAGED RAD DOOR PER AMM 21-53-01-4, 21-53-02-4 & 21-53-05-6. INSTALLED THE RT RAD ASSY & PERFORMED POST-INSTALLATION TEST FAIL PER MM 21-53-01-4. R&R EXHAUST DOOR ACTUATOR & POST-INSTALLATION TEST NORMAL IAW AMM 21-53-04-4. ACFT OK FOR SVC.
THE HOOK AND LOOP STRIP FOR THE FIRST OFFIER`S EVAS WAS FOUND LOOSE. SECURED THE EVAS HOOK AND LOOP STRIP IAW AMM 25-99-99-6. ACFT OK FOR SERVICE.
POST FLIGHT, NOTED ONE ESCAPE HARNESS D-RING MISSING BELOW THE RT SUPERNUMERARY SEAT. INSTALLED THE NEW ESCAPE HARNESS D-RING.
DURING POST FLIGHT, FOUND DEMO ESCAPE HARNESS CARABINER MISSING. THE ESCAPE HARNESS WAS REMOVED AND A NEW CARABINER WAS INSTALLED IAW AMM 25-61-03-2. ACFT OK FOR SERVICE.
ACRID ODOR IN THE COCKPIT, IN BEGINNING DESCENT. NO SMOKE OR OBSCURATION. INTENSE ODOR FOR 15-20 SECONDS THEN RAPIDLY DISSIPATED . NO ENGINE OR WING ANTI-ICE. NOT LIKE AN ELECTRICAL BURNING ODOR. ODOR OCCURRED THREE TIMES DURING DESCENT ON PREVIOUS FLT . ON THIS FLIGHT, ODOR OCCURRED ONCE DURING TAKEOFF (NOT A STRONG) AND ONCE DURING DESCENT(INTENSE). ODOR DOES NOT COME FROM ANY PARTICULAR AREA OF COCKPIT. REMOVED AND REPLACED LT & RT OZONE CONVERTERS. LEAK CHECKED GOOD. RAN PACKS ON APU AIR WITH NO ABNORMAL ODORS NOTED. RAN ENGINES NR 1 & 2 WITH PACKS ON, NO ABNORMAL ODORS NOTED IAW AMM 21-51-22-4.
INTERMITTENT BURNING ODOR, DURING DESENT. CREW STATED DID NOT SEE ANY SMOKE, IT WAS A RUBBER ODOR AND NOT OVERPOWERING. PERFORMED SNIFF TEST OF THE AVIONICS IN AVIONICS BAY. MAIN CARGO COMPT, FLT DECK AND BELLIES WITH PACKS RUNNING ON APU. RAN BOTH ENGINES IAW JRH USING ENG PNEUMATICS AND PACKS RUNNING AND NO ODOR WAS PRESENT. PERFORMED CHECKS AS OUTLINED IN AMM 21-00-21-2 NO ABNORMALIES PRESENT.
ENTRY DOOR SHOWED OPEN UPON LANDING. ACFT BLOCKED IN BEFORE DOOR WAS OPENED. RELEASED FOR SERVICE IAW MEL 52-71-01-01 CAT C. CREW ENTRY DOOR INDICATION SYS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT ASSOCIATED DOORS ARE CLOSED, LATCHED, & LOCKED PRIOR TO EACH DEPARTURE. ALL DOORS EXCEPT MAIN DECK CARGO DOOR, ACFT OK FOR SERVICE. INSTALLED SHIM IN DOOR CLOSED SENSOR S194, REINSTALLED TARGET IAW AMM 52-71-01-4. CHECKED GAP FOUND 2.692 MM 0.10598 INCHES, ALLOWANCE IS 1.78-3. 3MM .13-.07 INCHES. CHECKED DOOR LOCKED SENSOR S195 GAP .005 INCHES ALLOWANCE 0.005-.02 INCHES IAW AMM 52-71-01-4. OPENED & CLOSED ENTRY DOOR NUMEROUS TIMES WITH NO INDICATION PROBLEM. INSTALLED INTERI OR DOOR PANEL IAW SMP.
LANDING GEAR FAILED TO RETRACT AFTER T/O. REMOVED AND REPLACED LANDING GEAR VALVE ACTUATING LINK PER AMM 32-31-00-5. TEST OK FOR SERVICE.
DURING ROUTINE INSPECTION, LWR FLOORBEAM CORROSION AT BS 848 FROM RBL 0 - 24 AND CRACKED AT RBL 1. REMOVED CORROSION IAW SRM 51-10-6, STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE AND SUPPORT DOUBLER IAW 51-40-3 & 51-30-2.
DURING ROUTINE INSPECTION, FLOORBEAM BS 344 FOUND CORRODED BEYOND LIMITS ON UPPER CHORD AT RBL 50. CUT OUT DAMAGE, FAB AND INSTALL PER IAW SRM 53-10-8.
DURING ROUTINE INSPECTION, FLOORBEAM BS 344, RT O/B END FOUND CORRODED BEYOND LIMITS ON LWR FLANGE. CUT OUT DAMAGE. FAB AND INSTALLED PER IAW SRM 53-10-8.
DURING ROUTINE INSPECTION, STR 25R FOUND CRACKED BS 520. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-3.
DURING ROUTINE INSPECTION, BS 870 FLOORBEAM FOUND CORRODED AT THE NR 1 SEAT TRACK. REMOVED AND REPLACED PER IAW SRM 51-10-6. FOUND WITHIN LIMITS IAW SRM 53-10-1, 51-30-2.
DURING ROUTINE INSPECTION UPPER FUSELAGE SKIN FOUND CORRODED AND POPPED RIVETS FROM BS 430 - 440 AT STR 5L. REMOVED RIVET AND TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3. FAB REPAIR PARTS PER IAW SRM 53-30-3.
DURING ROUTINE INSPECTION, SUPPORT BRACKET FOR NR 7 SPOILER ACTUATOR FOUND CRACKED AT BOTH SIDES. REMOVED AND REPLACED NR 7 SPOILER AND ACTUATOR FITTING PER IAW SRM 51-10-1, 51-30-2, 27-62-001-4, AND 27-62-00. OPS CHECK GOOD.
DURING ROUTINE INSP BS 930 BELTFRAME FOUND CRACKED ON FWD SIDE OF STR 14R. REPAIRED BELTFRAME PER IAW FEDEX EO 7-2310-7-4330.
DURING ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. FUSELAGE SKIN REPAIR PER FEDEX EO 7-5330-7-2345 PART 2.
DURING ROUTINE INSP, FWD LWR CARGO DOOR, EXT SKIN CRACKED IN LWR AFT CORNER. BLENDED OUT CRACK AND INSTALLED EXT DOUBLER IAW SRM 52-00-3.
DURING ROUTINE INSP NR 2 ENG FIREWALL FOUND CRACKED AT APPROX 8 O''CLOCK POS AT FIRELOOP BRACKET. STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-10-1.
DURING ROUTINE INSPECTION, RIGHT I/B MIDFLAP REAR SPAR UPPER CHORD FOUND CRACKED AT WING BUTT LINE 120 UPPER ROW FWD FASTENER HOLE. REMOVED AND REPLACED PER IAW MM 27-51-1. RIG AND OP CHECK FLAP PER IAW MM 27-51-0.
DURING ROUTINE INSPECTION, FLOORBEAM BS 640 FOUND CORRODED BEYOND LIMITS 4 INCHES LEFT OF NR 4 SEAT TRACK. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-8.
00-6 - REPEAT FROM 1/4/00; AFT T/O DOORS LIGHT AND L MAIN GEAR DOOR LIGHT REMAINED ON WITH GEAR HANDLE UP AND OFF. RECYCLED DID NOT CORRECT. ALL IND NORM WITH GEAR DOWN. REMOVED AND REPLACED CANNON PLUG ASSY IAW SWP 20-60-06. OPS CK DOOR FOUND NORM MEL CLEARED.
WHEN LANDING GEARS WERE EXTENDED ON APPROACH, THE MAINS EXTENDED GREEN, BUT THE NOSE GEAR LIGHT REMAINED AMBER. NO NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL. CYCLED GEAR AND ALL GEAR EXTENDED NORMALLY. PERFORMED NOSE GEAR EXTENSION AND RETRACTION TEST PER MM 32-33-0 P 501 AND 502. CYCLED 10 TO 12 TIMES WITH NO INDICATIOIN PROBLEMS.