N957FD
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
118 reports on file, 2011-11-21 – 2018-05-25.
Part: ENGINE — FAILED (NR 2) · airframe 55,815 hrs · 33,862 cycles
DURING A TEST FLIGHT, 2 HOURS 39 MINUTES INTO FLIGHT, THE RIGHT ENGINE OIL QUANTITY WENT TO ZERO & OIL PRESSURE DECREASED TO 4 PSI IN THE RED BAND. SHUT THE RT ENGINE DOWN. RT ENGINE VIBRATION BITE COMPLETED. NR 2 ENGINE REPLACED IAW TC 7180260-02-02. PERFORMED A SATISFACTORY LEAK CHECK OF FUEL SYSTEM, OIL SYSTEM AND HYDRAULIC SYSTEM IAW TC 7180260-02-02. PERFORMED A SATISFACTORY ENGINE OPS CHECK IAW TC 7180260-02-02.
Part: SHEAR TIE — CORRODED (BS 680) · corrosion level 2 · airframe 55,812 hrs · 33,861 cycles
FWD CARGO BILGE, BS 680 SHEAR TIE CORRODED BETWEEN STRINGERS 27L - 28L. EVALUATED AREA OF CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A, FIG 101, DETAIL II. REMOVED, FABRICATED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 143N1069, REV - , REV F.
Part: KEELBEAM — CORRODED (BS 660-680) · corrosion level 2 · airframe 55,812 hrs · 33,861 cycles
EVIDENCE OF CORROSION, STRINGER 28L-FORWARD LOWER CARGO BAY BETWEEN BS 660 - 680. COMPLIED WITH EA T F-5310-T0339895 .
Part: SKIN — DENTED (BS 520-540) · airframe 55,812 hrs · 33,861 cycles
LOWER LOBE EXTERNAL SKIN HAS TWO PROTRUDING DENTS AT APPROX BS 524, BETWEEN STRINGERS 26L & 27L. COMPLIED WITH EA F-5330-T0339825, P1.
Earlier reports · 2011–2015 · 114 reports
2015
Part: ADC — FAILED (LEFT) · airframe 555 hrs · 33,723 cycles
ON TAKEOFF ROLL, CAPTAIN ADC FAILED. DUPLICATED DADC FAIL ON GND. R & R LT DADC IAW AMM 34-12-01-4. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.
Part: GIRT BAR — BENT (R1 DOOR) · airframe 555 hrs · 33,720 cycles
RIGHT ESCAPE SLIDE CAME LOOSE. R & R RT 1 DOOR GIRT BAR ASSEMBLY IAW AMM 25-66-10-2-0. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 550 hrs · 33,412 cycles
DURING PREFLIGHT L1 DOOR EMER & SLIDE LIGHTS INOPERATIVE. INSTALLED NEW BATTERY PACK, NO HELP. R & R L1 EMER LIGHTS BATTERY CHARGER & BATTERY PACK IAW AMM 33-51-07-2, OPERATIONS CHECKED NORMAL. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE · airframe 548 hrs · 33,312 cycles
RIGHT SLIDE ARM LIGHT INOPERATIVE. RELAMPED DOOR SLIDE ARM LIGHT IAW SMP. OPERATIONS CHECKED GOOD.
Part: COVER — DAMAGED (L1 SLIDE COVER) · airframe 548 hrs · 33,296 cycles
DURING LT ENTRY DOOR CLOSING, SLIDE COVER DISLODGED ON L1. REPAIRED SLIDE COVER PER SRM 51-70-03-G. REINSTALLED L1 SLIDE COVER PER AMM 25-66-01-4. ACFT OKAY FOR SERVICE.
2014
Part: FRAME — PUNCTURED (BS 239) · airframe 54,094 hrs · 32,786 cycles
PUNCTURE TO FRAME AT FWD ACCESSORY EQUIPMENT BAY BS 239 LOWER LOBE DOOR CUT OUT. REPAIRED IAW EA F-5310-T0306819 REV A P1.
Part: COVER — DELAMINATED (L1 DOOR) · airframe 53,984 hrs · 32,709 cycles
L1 DOOR ESCAPE SLIDE COVER HAS ONE EACH LATCH BROKEN. RELEASED FOR SERVICE IAW MEL 52-11-01-A. L1 DOOR SLIDE INOPERABLE, IDENTIFY INOPERABLE OR MISSING. REPAIRED AREA UNDER LATCH & REPLACED FOUR INSERTS THAT ATTACH LATCH ASSEMBLY IAW AMM 25-00-00-8.
2013
Part: PRESSURE SWITCH — FAILED (HYD SYSTEM) · airframe 53,765 hrs · 32,540 cycles
AT LEVEL OFF, FL 380, RUDDER RATIO, EICAS FOLLOWED IMMEDIATLLY BY LT HYD SYS PRESSURE. CHECKED SYS, PRESSURE ON STATUS PAGE, IT SHOWED DECREASING. LT YAW DAMPER, IAW QRH TURNED LT ENG AND LT ELECTRIC PUMPS OFF AND PRESSURE BEGAN INCREASING. IAW CREW VERBAL LT ENG PRESS AND LT ELEC PRESS LIGHTS NEVER CAME ON, T/S IAW FIM 27-21 FAULT TREE 809, LT YAW DAMPER MODULE FAULTED PRESSURE SYS. R & R LT HYD PRESSURE SWITCH IAW MM 29-11-17-4 LEAK AND OPS CHECKS GOOD, RAN LT ENG AND LT ELEC HYD PUMP NO FAULTS ENG RUN.
Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 53,481 hrs · 32,294 cycles
RT EMERGENCY SLIDE LIGHT INOPERATIVE. LIGHT SOCKET CORRODED. FUSE BLOWN IN EMERGENCY POWER SUPPLY. REPLACED LAMP AND R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07-2 & 33-51-06-2-1. OPS CHECKED NORMAL.
2012
Part: SLIDE — DISLODGED (PAX DOOR) · airframe 53,040 hrs · 31,982 cycles
F/O DISARMED DOOR & CHECKED. RAMP OPEN DOOR AND SLIDE DEPLOYED. FOUND SLIDE HAD DEPARTED FROM DOOR AND WAS NOT INFLATED. R & R L1 SLIDE USING AMM 25-66-01-4.
Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHTS) · airframe 53,011 hrs · 31,963 cycles
EMERGENCY EXIT LIGHT OVER R1 DOOR INOPERATIVE WHEN SWITCHED TO ON IN COCKPIT. FOUND EXIT LIGHT BATTERY PACK IMPROPERLY INSTALLED. INSTALLED CORRECTLY IAW AMM 33-51-07. EXIT LIGHTS OPERATE NORMALLY. OK TO CONTINUE.
Part: LIGHT — UNKNOWN (CABIN) · airframe 52,998 hrs · 31,957 cycles
INTERIOR EMERGENCY EXIT SIGN ABOVE DOOR 1R INOPERATIVE. CHECKED OPERATION OF EMERGENCY LIGHTS IAW AMM 33-51-00-5, ALL OPS CHECK GOOD FOR CONTINUED SERVICE AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,918 hrs · 31,903 cycles
THE RT CABIN DOOR EXIT EMERGENCY LIGHT WAS NOT ILLUMINATED DURING TEST. THE CABIN OVERHEAD EXIT LIGHT ALSO WAS NOT ILLUMINATED. EMERGENCY EXIT LIGHT SYS IAW MM 33-51-01-2. R & R LIGHT.
Part: SAFETY WIRE — WRONG PART · airframe 52,651 hrs · 31,704 cycles
DURING FLIGHT DECK INSPECTION, FOUND WRONG SAFETY WIRE ON THE LEFT GUARDED GEN DISC SWITCH. DURING FLIGHT DECK INSP FOUND RT GUARDED GEN DISC SWITCH WITH THE WRONG SAFETY WIRE. DURING FLIGHT DECK INSP FOUND PASS O2 GUARDED SWITCH WITH THE WRONG SAFETY WIRE. DURING FLIGHT DECK INSPECTION FOUND THE RAT GUARDED SWITCH WITH THE WRONG SAFETY WIRE INSTALLED. DURING FLIGHT DECK INSP FOUND CARGO ISOL GUARDED SW WITH THE WRONG SAFETY WIRE. INSTALLED CORRECT SAFETY WIRE ON ALL SWITCHES IAW MM 20-10-23-4. FINAL CLOSED.
Part: STRINGER SPLICE — CORRODED (BS 660) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
STRINGER SPLICE 28R, BS 660, FOUND WITH CORRODED. STRINGER SPLICE R & R WITH FABRICATED STRINGER SPLICE IAW SRM 51-40-05, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
BS 1787 S3R, CORROSION ON THE AFT SIDE OF THE FRAME WHERE IT ATTACHES TO THE SKIN. REPAIR CARRIED OUT IAW EA F-5310-157138, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
BS 1787 AT S3R, CORROSION ON THE AFT SIDE OF THE FRAME WHERE IT ATTACHES TO THE STRINGER. REPAIRED IAW EA F-5310-157138, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — CORRODED (ZONE 300) · airframe 52,597 hrs · 31,677 cycles
RT SIDE INTERIOR, CORROSION ON STRINGER 6R WHERE IT IS ATTACHED TO THE BS 1787 BULKHEAD ON THE AFT SIDE OF THE BULKHEAD. REPAIRED IAW EA F-5310-157138 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: DOOR FRAME — MISINSTALLED (CARGO DOOR) · airframe 52,597 hrs · 31,677 cycles
NR 2 CARGO DOOR FRAME FOUND SHORT EDGE MARGIN ON LOWER CHORD OF AFT SIDE FRAME. R & R WITH FABRICATED CHORD IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY FRAME AT BS 1300 HAS CORROSION ON UPPER FLANGE BETWEEN STRINGERS 26 -27R. REPAIRED IAW EA F-5310-158002. REPAIR IS CLASSIFIED AS MINOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1220. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1340. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY TIE DOWN FITTING HAS CORROSION AT BS 1220. REPAIRED IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 740. REPAIRED IAW EA F 5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1480. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 820. REPAIRED IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 520. REPAIRED IAW EA F-5340-154493. REPAIR CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 540. REPAIRED IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 520. REPAIRED IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1620. REPAIRED IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 760. REPAIR CARRIED OUT IAW EA F-5340-154493 . REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 1260. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 800. REPAIR CARRIED OUT IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 839. REPAIR CARRIED OUT IAW EA F-5340-154493. REPAIR CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1600. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 1480. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY LEFT TIE DOWN FITTING HAS CORROSION BS 1240. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LOWER CARGO BAY, FRAME UPPER SURFACE AT BS 1380 HAS DENT BETWEEN STRINGERS 25 -26L. DENT REPAIR CARRIED OUT IAW EA F-5310-158005, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FORWARD LOWER CARGO BAY, AFTER REMOVAL OF RT TRANSITION PANEL FRAME AT STA 700 UPPER SURFACE HAS DENT BETWEEN STRINGERS S24R - S25R. REPAIR CARRIED OUT IAW EA F-5310-158004, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
RIGHT WING UPPER SURFACE FIXED T/E SKIN PANEL (SRM 57-51-01) L/E ROW OF RIVETS FOUND SUNKEN IN AT WBL 79.02 OTBD 28" TO 38". REPAIRED IAW EA F-5730-15300, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD LOWER CARGO BAY, AFTER REMOVAL OF RT TRANSITION PANEL FRAME AT BS 680. UPPER SURFACE HAS DENT BETWEEN STRINGERS 23- 24 RIGHT. REPAIR CARRIED OUT IAW EA F-5310-158003. REPAIR IS CLASSIFIED AS MAJOR.
Part: ATTACH ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
THE APU INLET DOOR ASSY ATTACH ANGLE AT RT STRINGER 3 HAS CORROSION BETWEEN BS 1787-1806. CORRODED ATTACHMENT ANGLE R & R WITH FABRICATED ANGLE IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSION AT STA 922. REPAIRED IAW EA F-5310-15127. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT BS 989 TO 1006. REPAIRED IAW EA F-5310-157127, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT BS 1022 TO 1027. REPAIRED IAW EA F-5310-157127, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSION AT BS 955 TO 959. REPAIRED IAW EA F-5310-15727, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT STA 930 TO STA 937. REPAIRED IAW EA F-5310-157127. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT BS 974 TO 984. REPAIRED IAW E.A. F-5310-157127 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSION AT STA 918. REPAIRED IAW EA F-5310-157127, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT STA 895 TO STA 908. REPAIRED IAW EA F-5310-157127, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: WEB — DAMAGED (ZONE 300) · airframe 52,597 hrs · 31,677 cycles
WEB BS 1885 AFT SIDE DAMAGED AT RBL 7. DAMAGED WEB REMOVED AND REPAIR CARRIED OUT IAW SRM 53-80-08, FIG 201, REPAIR 2, DETAIL I, REV. 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME SPLICE — GOUGED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO COMP FRAME AT STA 1480 HAS 2 EA GOUGE MARKS ON SPLICE DOUBLER UPPER SURFACE BETWEEN STRINGER S24-25R. R & R WITH FABRICATED DOUBLER IAW SRM 51-40-02. REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — GOUGED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO COMP, FRAME AT BS 1480, HAS 1EA GOUGE MARK ON SPLICE DOUBLER UPPER SURFACE BETWEEN STRINGERS S23 & 24R. R & R WITH FABRICATED DOUBLER IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — CHAFED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY FRAME AT BS 1320, HAS CHAFE MARK ON UPPER FLANGE BETWEEN STRINGERS 26--27L. REPAIRED IAW EA F-5310-153473, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — GOUGED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO COMP, FRAME AT STA 1480, HAS 1 EA GOUGE MARK ON FRAME UPPER SURFACE BETWEEN STRINGERS S25 & 26R. REPAIRED IAW EA F-5310-153498. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
RIGHT WING OVERWING FILL PORT CUTOUT FOUND CORRODED. REPAIRED IAW EA F-5730-154486 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CORROSION ON MOST OTBD CREASE BEAM AT BS 1320-1330, RBL 64. CREASE BEAM ANGLE R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON FLOORBEAM UPPER CAP LOWER SURFACE AT STA 324, RBL 58. CORROSION REPAIR CARRIED OUT IAW EA F-5300-154492, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
LEFT WING OVERWING FILL PORT CUTOUT FOUND CORRODED. REPAIRED IAW EA F-5730-154486, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER SPLICE — CORRODED (BS 1460) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
FUSELAGE SKIN AT BS 1460 BUTT JOINT OBSERVED WITH BULGES FROM S26L TO 26R ESPECIALLY OBVIOUS AT STR 28 L AND STR 29 L. FOUND STRINGER 29L SPLICE SHIM CORRODED. R & R STRINGER SHIM AND SPLICE SHIM IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRAP — CORRODED (APU BAY) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
BS 1780 AT S3R TO 5R THERE IS CORROSION ALONG THE FWD EDGE OF THE APU INLET ATTACH POINT ON THE INTERIOR SIDE OF THE SKIN. R & R IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY, DENT ON FRAME STA 1500 UPPER FLANGE BETWEEN STRINGERS 25 - 26 RIGHT. REPAIR CARRIED OUT IAW EA F-5310-153494, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DENTED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO BAY FRAME AT BS 1580 UPPER FLANGE HAS DENT BETWEEN S25 & 26 RIGHT. REPAIR CARRIED OUT IAW EA F-5310-153493 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
EMPENNAGE-RT SIDE-INTERIOR SIDE-THE OTBD MATING ANGLE FOR THE APU INLET DOOR HAS CORROSION. THIS IS STRINGER 6 AT BS 1780-1800. FABRICATED ANGLE IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
AFTER REMOVAL OF STRINGER SPLICE AT BS 1460 STR 28L FOUND SPLICE TO BE CORRODED. REMOVED AND INSTALLED FABRICATED STRINGER SPLICE IAW SRM 51-40-02 REV 105. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — DENTED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
AFT LWR CARGO COMP STRINGER S20R HAS DENT BETWEEN STA 1520 -1540.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
AFT CARGO AT STA 1465, STR 30 STRINGER SPLICE CORRODED. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FWD CARGO DURING INSPECTION, BS 720 -740, STRINGER 27L HAS CORROSION AROUND FASTENERS. CORRODED STRINGER R & R IAW SRM 53-00-03, REV 104, DETAIL I, FIG 201, REPAIR 2. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 470 -480, RBL 45.5. R & R IAW SRM 53-00-52 REPAIR 1 FIG 201, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
2011
Part: FLOOR PANEL — CORRODED (BS 1681-1691) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
AFT CABIN CORROSION ON FLOOR PANEL AT STA 1681-1691, BL.0 TO LBL 68. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND SRM 51-20-01 REV.104. REPAIR CARRIED OUT IAW SRM 53-60-51 REPAIR 2, REV. 104, FIG. 201. REPAIR CLASSIFIED AS MAJOR.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
L2 DOOR HAS CRACK AT DOOR HINGE MID CUTOUT. REPAIRED IAW SRM 52-10-02, REPAIR 1, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CREASE BEAM ANGLE AT STA 1300 TO STA 1320 LBL 64 HAS CORROSION. R & R IAW SRM 51-40-02, REV 104. REPAIR CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
LEFT NR 3 EMERGENCY EXIT LOWER SILL PANEL CREASE BEAM WEB UPPER AND LWR SURFACE FOUND CORRODED. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON SEAT TRACK CROWN AT STA 385-395, RBL 45.5. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CREASE BEAM ANGLE AT STA 1320 TO STA 1350, RBL 60 HAS CORROSION. CREASE BEAM ANGLE R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON FLOOR PANEL AT BS 1681-1691, BL 0 TO LBL 68. REPAIR CARRIED OUT IAW SRM 53-60-51. REPAIR 2, REV.104, FIG 201. REPAIR CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CABIN CREASE BEAM AT STA 1326 TO STA 1380, RBL 64 HAS CORROSION ROUND FASTENER HOLES ON UPPER AND LOWER CHORDS. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CORROSION ON FLOORBEAM UPPER CAP AT STA 350, LBL 14-20. R & R IAW SRM 53-00-51, REPAIR 5, FIG 201, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
SEAT TRACK AT STA 365 TO 395 RBL 24 HAS CORROSION.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
RIGHT NR 3 EMERGENCY EXIT LWR SILL PANEL CREASE BEAM WEB UPPER AND LOWER SURFACE FOUND CORRODED. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON SEAT TRACK CROWN, CHANNEL AND FLANGE AT STA 365-377 RBL 45.5. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: WEB — CORRODED (ZONE 300) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
BS 1880 ON THE LOWER EMPENNAGE TRANSVERSE ON THE WEB PORTION THERE IS CORROSION AND A CRACK THROUGH THE WEB AT RBL 6.0. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
DAMAGED ON SEAT TRACK CROWN AT BS 420 -430, RBL 45.5. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON FLOORBEAM UPPER CAP AT STA S377, LBL 45.5 TO LBL 58. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CABIN CREASE BEAM ANGLE AT STA 1200 TO STA 1280 LBL 60, HAS AREAS OF CORROSION. R & R IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CABIN, BS 1280 TO 1300, CREASE BEAM INNER CHORD FOUND WITH EXISTING DOUBLE DRILLED HOLES AFTER WEB REMOVAL. R & R IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CREASE BEAM ANGLE AT STA 1320 TO STA 1350, RBL 64 HAS CORROSION. R & R IAW SRM 51-40-02, REV 104. REPAIR CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
NEAR LEFT NR 3 EMERGENCY EXIT, CREASE BEAM UPPER AND LOWER SURFACE FOUND CORRODED BS 1320-1326. R & R IAW SRM 51-40-02 REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHIM — DAMAGED (ZONE 400) · airframe 52,597 hrs · 31,677 cycles
NR 1 PYLON MID BULKHEAD, LOWER FLANGE OTBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS FRAYED AND MIGRATED.
Part: SHIM — DAMAGED (ZONE 400) · airframe 52,597 hrs · 31,677 cycles
NR 1 PYLON MID BULKHEAD, LOWER FLANGE, INBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS FRAYED AND MIGRATED.
Part: FRAME — CHAFED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
FRAME AT BS 1280, STR 13 - 14R CHAFED. REPAIRED IAW SRM 53-00-07, REPAIR 3, FIG 201, REV.104. REPAIR CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 1630-1640, LBL 45.5. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
SEAT TRACK AT STA 365 TO 377 HAS CORROSION ON TRACK FLANGES. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
SEAT TRACK AT STA 365 TO 395 RBL 24 HAS CORROSION. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CORROSION ON SEAT TRACK CROWN, CHANNEL AND FLANGE AT BS 365 -418 RBL 24.75. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CORROSION ON SEAT TRACK CROWN AND CHANNEL AT BS 1600-1620 LBL 45.5. R &R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: WEB — DAMAGED (BS 377) · airframe 52,597 hrs · 31,677 cycles
DURING FLOORBEAM REPLACEMENT FOUND L1 DOOR LOWER SILL WEB STA 377 HAS ELONGATED HOLES. REMOVED & REPLACED IAW SRM 51-40-02, REV 104. REPAIR CLASSIFIED AS MAJOR.
Part: FRAME — DAMAGED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
CABIN FRAME AT STA 1280, S13L TO S14L HAS DAMAGE. REPAIRED IAW SRM 53-00-07 FIG 201 REPAIR 3, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CABIN CREASE BEAM ANGLE AT STA 1280 TO STA 1288 LBL 64, HAS SEVERAL EXISTING DOUBLE DRILLED HOLES. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CABIN, AFTER REMOVAL FOUND LT CREASE BEAM WEB AT STA 1280 TO STA 1300, FOUND WEB HAS A DOUBLE DRILLED HOLES IN WEB. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: SILL — CORRODED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CABIN DOOR 3RDOOR SILL FOUND CORROSION ROUND FASTENER HOLES ON UNDERSIDE OF WEB. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CHANNEL — DAMAGED (BS 377) · airframe 52,597 hrs · 31,677 cycles
CABIN, DURING FLOORBEAM REPLACEMENT, BS 377 FOUND L1 DOOR SILL AREA 'U' CHANNEL HAS AN ELONGATED HOLE. REMOVED & REPLACED IAW SRM 51-40-02 REV 104. REPAIR CLASSIFIED AS MAJOR.
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
CABIN DOOR 3L SILL PLATE CREASE BEAM WEB HAS CORROSION ROUND FASTENER HOLES ON UNDERSIDE OF WEB. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
CABIIN, STA 1280 TO STA 1300, LT CREASE BEAM SPLICE FOUND WITH A DOUBLE DRILLED HOLES. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DAMAGED (ZONE 200) · airframe 52,597 hrs · 31,677 cycles
FRAME DAMAGED UNDER BRACKET AT STA 920, STR 5 - 6R. REPAIRED IAW SRM 53-00-07, REPAIR 3, FIG 201, REV 104. REPAIR CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (LT NACELLE) · airframe 52,597 hrs · 31,677 cycles
LEFT WING BETWEEN OTBD NAC FITTING AND LOWER WING SKIN FOUND WITH SHIMS MIGRATION AT WS 303.5. REPAIR CARRIED OUT IAW EA F-5740-153476, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (ZONE 600) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
RT WING UPPER SURFACE FIXED T/E SKIN PANEL (SRM 57-51-01, PG 2, ITEM 3) L/E ROW OF RIVETS FOUND SUNKEN IN AT WBL 79.02 OTBD 28" TO 38". REPAIRED IAW EA F-5730-15300 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
LT WING REAR SPAR UPPER SKIN CORROSION FOUND ADJACENT TO WBL 105. REPAIR CARRIED OUT IAW EA F-5730-153499, PART 1. REPAIR IS CLASSIFIED AS MINOR.
Part: BEAM — CORRODED (ZONE 300) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
BS 1862 AFT SIDE, THERE IS CORROSION AT LOWER BULKHEAD AT S26L OTBD BEAM APPROX 12" ABOVE THE SKIN. REPAIR CARRIED OUT IAW EA F-5310-157123, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: BEAM — CORRODED (ZONE 300) · corrosion level 2 · airframe 52,597 hrs · 31,677 cycles
EMPENNAGE - BS 1862 AFT SIDE - THERE IS CORROSION AT LOWER BULKHEAD AT S28L INBD BEAM APPROX 12" ABOVE THE SKIN. REPAIR CARRIED OUT IAW EA F-5310-157122, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
LOWER FUSELAGE OUTER SKIN FOUND CORROSION AT KEELBEAM COMPARTMENT STA 895 AFT 18.5", L15C LBL 5". REPAIRED IAW EA F-5730-157120, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
LOWER FUSELAGE OUTER SKIN FOUND CORROSION AT KEELBEAM COMPARTMENT STA 927 AFT 27", L-14C LBL 5". REPAIRED IAW EA F-5730-157120, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
LOWER FUSELAGE OUTER SKIN FOUND CORROSIONS AT KEEL BEAM COMPARTMENT STA 895 AFT 4", L-16C, LBL 5". REPAIRED IAW EA F-5730-157120. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 52,597 hrs · 31,677 cycles
FUSELAGE EXTERIOR SKIN AT STA 640 TO BS 660, STR 29 TO 30 LEFT HAS SCRATCHES. REPAIRED IAW EA F-5330-154495 PART 1. REPAIR IS CLASSIFIED AS MAJOR.