N789FD
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
RIGHT WING INB MAIN FLAP TRAILING EDGE OTBD SECTION, UPPER AND LOWER SURFACE SHOWS MULTIPLE DENTS APPLIED PERMANENT REPAIR AT UPPER AND LOWER SURFACE ON RH WING INBD MAIN FLAP TRAILING EDGE IAW SRM 57-53-01-2R REP 1, DETAIL I, FIG 201, SHEET 2 AND SRM 51-70-10- 2R, REP 4.
LH NOSE WHEEL ASSY INNER RETAINING RING OUT OF PLACE, FLOATING ON AXEL. REMOVED AND REPLACED LEFT NOSE TIRE. REF AMM 32-45-02-4. OK FOR SERVICE.
AFT MAIN CABIN FLOOR PNL #252 MWF HAS DAMAGE AND MISSING SHALLOW INSERTS, DOT 4-123 PANEL RACK L/H FABRICATED ZONE 250 FLOORBOARD PANEL #252 MWF ON VTMAE TRAVELER # T24/1767887 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
FLOORBOARD 232MXF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MXF ON VT MAE TRAVELER T24/1767270 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
FLOORBOARD PANEL 221BF DAMAGED. FABRICATED ZONE 220 FLOORBOARD PANEL 221BF ON VT MAE TRAVELER T24/1767197 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
FLOORBOARD PANEL 222AF DAMAGED. FABRICATED ZONE 220 FLOORBOARD PANEL 222AF ON VT MAE TRAVELER T24/1767264 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
#1 PYLON UPPER SKIN AND OUTBD FITTING HOLE #4 HAS REJECTABLE INDICATON OF CORROSION AT 4 TO 7 O'CLOCK TITLE: WINGS - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS . ACCOMPLISHED STEPS 1-25 PER EA F-5730-T0369611 PT 1. MAJOR REPAIR
#1 PYLON UPPER SKIN AND OUTBD FITTING HOLE #9 HAS REJECTABLE INDICATIONS OF CORROSION AT 3 TO 5 O'CLOCK TITLE: WINGS - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS . ACCOMPLISHED STEPS 1-25 IAW EA F-5730-T0369611 PT 1. MAJOR REPAIR
#1 PYLON UPPER SKIN AND OUTBD FITTING HOLE #5 HAS REJECTABLE INDICATONS OF CORROSION AT 4 AND 11 O'CLOCK TITLE: WINGS - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATION . ACCOMPLISHED STEPS 1-25 PER EA F-5730-T0369611 PT 1. MAJOR REPAIR
#1 PYLON UPPER SKIN AND INBD FITTING HOLE #3 HAS REJECTABLE INDICATIONS OF CORROSION SKIN 4 AND 7 O'CLOCK AND INBD FITTING 4 AND 10 O'CLOCK. TITLE: WINGS - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS . ACCOMPLISHED STEPS 1-25 PER EA F-5730-T0369611 PT 1. MAJOR REPAIR
#1 PYLON UPPER SKIN AND DRAG FITTING HOLE #17 HAS REJECTABLE CRACK AT 7 O'CLOCK AND CORROSION INDICATION IN THE OUTBD FITTING AND SKIN AT 7 TO 10 O'CLOCK TITLE: WING - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS . ACCOMPLISHED STEPS 1-25 PER EA F-5730-T0369611 PT 1. MAJOR REPAIR
#1 PYLON INBD FITTING HOLE #2 HAS REJECTABLE INDICATIONS ON CORROSION 6 TO 10 O'CLOCK. TITLE WING - PLATES AND SKIN - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS. ACCOMPLISHED STEPS 1-25 PER EA F-5730-T0369611 PT1. MAJOR REPAIR
#2 PYLON UPPER SKIN AND DRAG FITTING HOLE #4 HAS A REJECTABLE CRACK INDICATION IN THE SKIN LAYER AT THE 4:00 POSITION COMPLIED WITH EA STEPS 1-29 F-5730-T0369535 P1, #2 PYLON, UPPER SKIN AND DRAG FITTING HOLE #4 HAS REJECTABLE CRACK INDICATION IN THE SKIN LAYER AT 4:00 POSITION. MAJOR REPAIR
AFT FUSELAGE APU INLET CUT-OUT LOWER ANGLE CORRODED. REMOVED AND REPLACED AFT FUSELAGE APU INLET CUT-OUT LOWER ANGLE IAW SRM 51-40-02. REMOVED CORROSION IAW 53-80-15-1A FIG 101 DET 11. FOUND TO BE OUT OF LIMITS. MAJOR REPAIR
APU AIR INLET DOOR MANIFOLD FWD SUPPORT FRAME AT STA 1787 IS CORRODED. REMOVED AND REPLACED APU AIR INLET DOOR MANIFOLD SUPPORT FRAME AT STA 1787 IAW SRM 51-40-02. REMOVED CORROSION IAW 53-80-15-1A FIG 101 DET 11. FOUND OUT OF LIMITS. MAJOR REPAIR
STA 1640, S-14 RIGHT HAND SIDE , LOWER OUTBOARD HOLE HAS A REJECTABLE CRACK INDICATION IN FRAME WEB LAYER. FUSELAGE - MAINFRAME - INSPECTION OF BODY STATION 1640 FUSELAGE FRAME WEB AT STRINGER S-14R - BOEING ALERT SERVICE BULLETIN 757-53A0112 - LOWER OUTBOARD HOLE - CRACK REPIAR ACCOMPLISHED PER EA F-5310-T0369609 STEPS 1-9 WITH NO DEVIATION. MAJOR REPAIR
PDIS 789 29-02 4718 05OCT21 MEM OPEN U DURING CRUISE THE C HYD ELEC 2 EICAS MESSAGE APPEARED FOLLOWED BY A COMPLETE REDUCTION OF C HYDRAULIC QUANTITY. SHORTLY AFTER THE FOLLOWING EICAS MESSAGES APPEARED: C HYD SYS PRESS C HYD RSVR PRES C HYD QTY R YAW DAMPER DECLARED AN EMERGENCY, COMPLETED THE QRH PROCEDURES, AND LANDED THE AIRPLANE SAFELY WITHOUT ANY OTHER ISSUES. FACT 06OCT21 07:10 MEM INSTALLED NEW ACMP REF. AMM 29-11-02-4. OPS CHECKS GOOD. NO LEAKS NOTED. REMOVED & REPLACED CENTER SYSTEM ACMP PRESSURE & CASE DRAIN FILTERS 4EA. REF. AMM 29-11-19-4. NO LEAKS NOTED. PERFORMED YAW DAMPER SYSTEM TEST REF. AMM 22-11- 00-5. AIRCRAFT OK FOR SERVICE.
RH SEAT TRACK RBL 58.22 CORRORED IN SEVERAL AREAS BETWEEN STA 1080R AND 1180R. REMOVED CORROSION AT RH SEAT TRACK RBL 58.22 SEVERAL AREAS BETWEEN STA. 1080 AND 1180 AND AFTER EVALUATION FOUND SEAT TRACK TO BE OUT OF LIMITS IAW B757 SRM 51-10-02-0G, 53-00-52-1A FIG 101 DET VII, REMOVED AND REPLACED BY FABRICATION SEAT TRACK FROM 900 TO 1180 IAW B757 SRM 51-40-05-0G, 51-40-02-0G AND BOEING DWG 657N3321 REV D
RH SEAT TRACK RBL 58.22 LIGHT SURFACE CORROSION AROUND NUT PLATES AT FS 1180R.
SEAT TRACK RBL 58.22 CORRORED IN SEVERAL AREAS BETWEEN BS 1080 AND 1180.
SEAT TRACK, RBL 58.22 HAD LIGHT SURFACE CORROSION AROUND NUT PLATES AT BS 1180. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, DET VII, AND DET I, CUT OUT SECTION OF SEAT TRACK FROM BS 1180 TO 1310, FABRICATED AND INSTALLED A NEW SEAT TRACK AND REPAIR CHANNEL IAW SRM 53-00-52-2R, REPAIR 3, OPTION 2. COMPLIED WITH EA F-5310-T0355374 P1.
RH SEAT TRACK RBL 58.22 LIGHT SURFACE CORROSION AROUND NUT PLATES AT FS 1180R. REMOVED CORROSION AT SEAT TRACK RBL 58.22 STA. 1180 AND STA. 1300 AND FOUND TO BE OUT OF LIMITS IN BOTH LOCATIONS IAW B757 SRM 53-00-52-1A FIG 101 DET VII AND DET I, CUT OUT SECTION OF SEAT TRACK RBL 58.22 FROM STA. 1180 TO 1310, FABRICATED AND INSTALLED NEW SEAT TRACK AND REPAIR CHANNEL IAW B757 SRM 53-00-52-2R REPAIR 3, OPTION 2. C/W FEDEX EA# F-5310-T0355374 P1. FUSELAGE - MAINFRAME - RBL 58 SEAT TRACK REPAIR BETWEEN STA. 1180 - 1320 - SRM REPAIR DEVIATION FOR ALTERNATE FINISH.
MDIS 789 33-50 3480 01MAY20 RST OPEN U THE THREE MAIN DECK EMERGENCEY LIGHTS CONTROLLED BY M731 REMAIN ILLUMINATED WITH AIRCRAFT DOWN POWERED. REMOVED AND REPLACED CHARGER / POWER SUPPLY M731 REF MM 33-51-07-2. OPS CHECK NORMAL. OK FOR SERVICE.
DIVERTED INTO EWRZONE TEMP DROPPED TO 38/49/26. TRIM AIR WAS MEL'D FL 370, NO A/ICE, TRIED AUTO, N, W ON PACK CONTROLLER. TEMP CONTINUED TO DROP IN ALL SETTINGS. LOST 30 DEGREES IN 50 MINS. ETURNED TRIM AIR PRESSURE REGUALTING VALVE TO NORMAL CONFIG. REMOVED AND REPLACED ZONE TEMP CONTROLLER AS PER MM 21-61-03-4 AND REMOVED AND REPLACED LT PACK TEMP CONTROL VALVE AS PER MM 21-51-12-4. BOTH VALVES LEAKED CHECKED GOOD, BOTH VALVES AND SYSTEM OPS CHECKED GOOD AS PER MM 21-61-00-5. CLEARS PIREP, OK FOR SERVICE.
NR 6 LE SLAT INBOARD UPPER SURFACE, PREVIOUS REPAIR MISSING. REMOVED AND REPLACED NR 6 LE SLAT ASSY IAW AMM 27-81-01-4. PERFORMED SATISFACTORY OP CHECK IAW AMM 27-81-01-4.
AFT PIT FRAME STA 1520, B/T S21R HAS GOUGES. REMOVED GOUGES IAW-SRM-51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07-1A, FIG 101, DET II. R & R FRAME STA 1520, BET STR 24R TO STR 13R IAW SRM-51-40-02-06 AND DWG 146N1017, THIS IS A CAT-A REPAIR, MAJOR.
AFT PIT STA 1520, FRAME SPLICE S24R GOUGED. R & R SPLICE FRAME AT STA 1520, STR 24R, IAW-SRM-51-40-02-0G AND DWG 146N1017, THIS IS A CAT A REPAIR. REMOVED GOUGES IAW-SRM-51-10-02, ORIGINAL MATERIAL .071, REMAINING .041, OUT OF LIMITS IAW SRM-53-00-07-1A, FIG 101, DET II.
SCRIBE LINE DAMAGE FOUND AT LAP SEAM S-14R, BS 777 TO BS 779. COMPLIED WITH EA F-5330-T0325500, PT 1: FUSELAGE, PLATES AND SKINS, SECTION 43- SCRIBE LINE INSPECTIONS, STR S-14R, BS 777.032 TO BS 778.99, 1.65" LG. CLASSIFIED AS A CAT B MAJOR REPAIR.
WHILE WORKING THE INBD AFT FLAP RT SIDE, THE OTBD FITTING WAS FOUND WITH PITTING CORROSION. AFTER CORROSION REMOVAL, FOUND OUT OF LIMITS IAW DWG 113N2801 SHT 1 REV. COMPLIED WITH EA F-5750-T0325349 PT 1 DATED 05 27 16. CAT A MAJOR REPAIR FAA FORM 8100-9 ISSUED DATED MAY 26 2016.
VERTICAL STAB AUXILIARY SPAR TO FRONT SPAR RT FIXED PANEL FROM STATION 195 - 270 HAS SEVERAL SPOTS OF DELAMINATION ON EXTERNAL & INTERNAL SURFACE. R & R VERTICAL STAB RT FIXED PANEL 175N2001-4 IAW SRM 51-40-02 -0G & DWG 175N2001 SH1 REV B. PN 175N2001-4 REPLACED DUE TO DELAMINATION FOUND TO BE OUT OF LIMITS IAW SRM 55-30-01-1A FIG 101 NOTE K. CAT A MAJOR REPAIR.
FORWARD CARGO DOOR OUTER SKIN AT BOTTOM HAS A DENT. EVALUATED & DETERMINED DENT TO BE OUT OF LIMITS IAW SRM 52-30-01-1A FIG 101 DET VIII. INSTALLED REPAIR DOUBLER IAW SRM 52-30-01-2R FIG 201 REPAIR 4, CAT B. REPAIR REF EA F-5230-TO325627 ISSUED FOR RSC TRACKING & REPETITIVE INSPECTION REQUIREMENTS. MAJOR REPAIR.
LEFT HORIZONTAL STAB FWD TORQUE BOX, INBD LOWER PANEL HAS LIMITED DENT REPAIR FOR 3 DENTS AT STATION 192 & 8.5" AWAY FROM PREVIOUS REPAIR & 1.25" AWAY FROM THE 3RD DENT, STAB STATION 195, 10.34" AFT OF THE AUX SPAR. REPAIRED LT HORIZONTAL STAB FWD TORQUE BOX INBD LOWER PANEL IAW-SRM-51-70-10-2A, REPAIR IS A CAT A MAJOR REPAIR. EXISTING REPAIRS DETERMINED TO BE OUT OF LIMITS DUE TO PROXIMITY IAW SRM-51-70-10-2R.
AFT PIT STATION 1260, CORROSION ON FRAME UPPER FLANGE AT FLOOR STRINGER LBL 2.29. REMOVED CORROSION IAW SRM 51-10-02-0G. AFTER REWORK AREA WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A.FIG 101 DET V, ORIG MAT .063, .016 MAT LOSS. R & R FRAME IAW SRM 51-40-02-0G & DWG 146N1004, STATION 1260, STRINGER 24L - 24R. FABRICATED ON T16 1201528. MAJOR REPAIR.
AFT PIT STATION 1500, BETWEEN STRINGER 29L - 30, SHEAR TIE HAS CORROSION. R & R SHEAR TIE IAW SRM-51-40-02-0G. REMOVED CORROSION IAW SRM-51-10-02, NO ALLOWABLE DAMAGE FOUND IN CHAPTER 53 OF SRM. REPAIR CATEGORIZED AS A MAJOR REPAIR.
RIGHT OTBD MAIN FLAPS LE, JUST IN FRONT OF NR 11 SPOILER HAS CHAFED MARK. EVALUATED CHAFE MARK, OUT OF LIMITS IAW SRM 57-53-01 FIG 101 DETAIL VI. REPAIRED IAW SRM 57-53-01-2R REPAIR 2 FIG 201 & SRM 51-40-02-0G, REF EA F-5750-T0325268 ISSUED FOR TRACKING. MAJOR REPAIR.
AFT PIT STATION 1500, FRAME AT FLOOR STRINGER RBL 7.55, CORRODED AT FLANGE. R & R FRAME AT STATION 1500, STRINGER 25L - 25R IAW SRM-51-40-02-0G & DWG 146N1030. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. CORROSION WAS REMOVED IAW-SRM-51-10-02. AFTER REWORK, AREA WAS FOUND TO BE OUT OF LIMITS, IAW-SRM-53-00-07-1A, FIG 101 DET II.
INCOMING LIGHTNING STRIKE REPAIR ON FUSELAGE SKIN AT STATION 1240, ABOVE STRINGER -8L, FOUND OUT OF LIMITS BY SRM, REQUIRES REPAIR. ACCOMPLISHED EA F-5330-T0324536 PT 1. CATEGORY A MAJOR REPAIR.
INCOMING CUT OUT FWD LOWER CORNER AFT CARGO DOOR, REQUIRES REPAIR REPAIRED DOOR IAW SRM 52-30-02-2R FIG 201 REPAIR 4. REF EA F-5230-TO324864 FOR TRACKING PURPOSES. THIS REPAIR IS CLASSIFIED AS CATEGORY B MAJOR REPAIR.
AFT PIT STATION 1400, FRAME CORRODED AT STRINGER 27R. REMOVED CORROSION IAW SRM-51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07-1A FIG 101 DET III. R & R IAW SRM-51-40-02-0G & DWG 146N1011, FRAME AT STATION 1400, STRINGER 25L - 27R. REPAIR CLASSIFIED AS A CAT A MAJOR REPAIR.
AFT PIT STATION 1661, STRINGER 25L - 25R FRAME HAS CORROSION. REMOVED CORROSION FRAME STATION 1661, BETWEEN STRINGER 25L & 25R IAW SRM 51-10-02-0G. CHECKED LIMITS ORIGINAL MATERIAL .063, AFTER REWORK MATERIAL .043, A MATERIAL LOSS OF .020 WAS FOUND OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DET 2. R & R FRAME IAW SRM 51-40-02-0G. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR, DWG 146N1024.
BILGE INTERIOR HAS CORROSION ON STRINGER, APPROX BS 1701 - 1681, STRINGER 29R. R & R STRINGER STATION 1630 - 1721 AT STRINGER 29R IAW SRM 51-40-02-0G & DWG 146N3600 PM FX-146N3110-693 CATEGORY A MAJOR REPAIR.
FLOORBEAM AT STATION 1681, HAS SEVERAL AREAS OF CORROSION ON UPPER CHORD. REMOVED CORROSION & CHECK LIMITS IS FOUND OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. R & R FLOORBEAM IAW DWG 146N5091, PN 146N5111-4, STATION 1681 MATERIAL PN BAC 1518-827 A BATCH 0002877570 IAW SRM 51-40-02. CATEGORY A MAJOR REPAIR.
INCOMING LIGHTNING STRIKE. REPAIR FUSELAGE SKIN STATION 1343, ABOVE STRINGER 9L, FOUND OUT OF LIMITS IAW SRM REQUIRES REPAIR. ACCOMPLISHED EA F-5330-TO324418. LIGHTNING STRIKE REPAIR AT STATION 1343 & BETWEEN STRINGER 8L & 9L, CAT B MAJOR REPAIR.
AFT PIT STATION 1420, STRINGER 28L - 29L HAS CORROSION ON FRAME. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A DET 2. R & R FRAME IAW SRM 51-40-02-0G & DWG 146N1012. FRAME STATION 1420, STRINGER 25L - 27R, CATEGORY A MAJOR REPAIR.
INCOMING LIGHTNING STRIKE REPAIR, FUSELAGE SKIN STATION 1216, BELOW STRINGER 7L IS OUT OF LIMITS IAW SRM, REQUIRES REPAIR. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01-2R FIG 201 REPAIR NR 7. MAJOR REPAIR.
AFT PIT STATION 1580, FRAME CORRODED AT STRINGER 27L. REMOVED CORROSION IAW SRM 51-40-02-0G FOUND TO BE OUT OF LIMITS IAW SRM 53-60-07-01 FIG 101 DET 2. R&R FRAME IAW SRM 51-40-02-0G & DWG 146N1010 AT STATION 1580, FRAME STRINGER 25L - 25R. REPAIR CLASSIFIED AS CAT A MAJOR.
AFT PIT STATION 1380 FRAME CORRODED FROM RBL 2 29 TO LBL 7.55. REMOVED CORROSION IAW SRM 51-10-02-0G. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET 2. R & R FRAME IAW SRM 51-40-02-0G & DWG 146N1010, STATION 1380, STRINGER 25L - 27R CAT A MAJOR REPAIR. FRAME FABRICATED ON T16 1195925.
APPEAR TO HAVE SMOKE COMING FROM PACK ON TAKEOFF. TURNED PACKS OFF, SMOKE STOPPED. RETURNED FOR LANDING. DRAIN ALL THE ENGINE OIL AND RE-SERVICE TO A KNOWN QUANTITY. AFTER IDLE RUN THE ENGINES SERVICED OIL AS NEEDED. AFTER SEVERAL CYCLES OF IDLE, CRUISE POWER, AND FULL POWER PER THE JRH. NO DEFECTS NOTED.