N049FE
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.
11 reports on file, 1996-05-16 – 2000-07-31.
Part: UPLOCK SENSOR — INOPERATIVE (RT MLG)
AFT T/O, GEAR RETRACTION UNSAFE RED IND IN BOTH S/O AND MAIN PANEL RT MAIN GEAR IND (RED LIGHT) ILLUM. REMOVED AND REPLACED RT GEAR UPLOCK SENSOR AND CORRECTLY ROUTED CONDUIT IAW MM 32-61-03-2. REMOVED AND REPLACED PROX BOX IAW 32-61-01-2. OPS CK OK.
Part: CONNECTOR — LOOSE (UPLOCK SENSOR)
AFT T/O, GEAR RETRACTION UNSAFE IND IN BOTH S/O AND MAIN PNL, RT MAIN GEAR IND RED LIGHT ON. FOUND UPLOCK PROX SENSOR CANNON PLUG ON LOOSE. TIGHTENED C/P AND SAFETIED PLUG ASSY, PERF PROX BOX TEST IAW MM 32-30-00 PG 104 & 32-30-00. OPS CK NORM. OK FOR SERVICE.
Part: PROXIMITY SWITCH — FAILED (LT MLG)
ON GEAR RETRACT AFT T/O, LEFT MAIN GEAR RED LIGHT ILLUM. ACCOMPLISH RED TAB PROC. REMOVED AND REPLACED PROXIMITY ELECTRONIC UNIT IAW DC-10-10 MM 32-61-01-2. PERFORMED LANDING GEAR EXT AND RETRACT CK IAW DC10-10 MM 32-30-00-5. SYS OPS CHECK NORM.
Part: ENGINE — FAILED (NR 3)
99-0047 - NR 3 ENGINE SUFFERED CATASTROPHIC FAILURE JUST AFTER ROTATION NR 3 EGT 999 DEG FOR 35 SEC. REMOVED AND REPLACED NR 3 ENG IAW FEC DC-10 PWRPLT WORK CARD 71T01101 UP TO ITEM 24. COMPLIED WITH (SEE AML 01224000).
Part: ACCESS PANEL — TORN (NR 3 PYLON)
98-213 - NR 3 ENG PYLON PNL 400GL TORN OFF ON INBD SIDE. AIRCRAFT LANDED EWR WITHOUT INCIDENT. REPLACED ACCESS PANEL. ALL NUTPLATES APPEAR TO BE IN GOOD WORKING ORDER.
Part: WIRE — SHORTED (BS 1800)
SNRM NR N01247, AFT ENGINE INLET DUCT ACCESS PANEL NR 364GR POWER FEEDER CABLES SHORTED AT ADEL CLAMP CENTER FRAME. SPLICED NEW CABLE 3X3 BO CAL FWD OF PRESSURE BULKHEAD, STA 1880 (SPLICED IN MAIN CABLE) PER MM 20-10-03. OPS CK ON ENG RUN CK'D NORMAL PER JRH 8-2.
Part: RIB — CRACKED (NR 2 NACELLE)
NR 2 ENG INLET INTERNAL 7TH RIB AFT OF FWD WEB CRACKED, UPPER CAP APPROX 7 LONG, 5:00 POSITION. * S/D* REPAIRED RIB CAP WITH ANGLE DOUBLER IN REF TO SRM 54-10-00. INSTALLED REPAIRED RIB CAP REF SRM 54-10-00. 4-16-98.
Part: WEB — CRACKED (NR 2 NACELLE)
NR 2 ENG INLET INTERNAL WEB BETWEEN 7TH AND 9TH RIB AFT OF FWD WEB CRACKED, 7:00 POSITION. *S/D* REMOVED RIB AND FABRICATED NEW RIB REF SRM 51-00-01. INSTALLED NEW RIB REF SRM 54-10-00. 4-16-98.
Part: STIFFENER — CRACKED (NR 2 NACELLE)
NR 2 INLET INTERNAL 7TH RIB AFT OF FWD WEB ANGLE STIFFENER CRACK, 7:00 POSITION. *S/D* REMOVED ANGLE STIFFENER AND FABRICATED NEW STIFFENER IN REF SRM 51-00-01. INSTALLED STIFFENER REF SRM 54-10-00. 4-16-98.
Part: RIB — CORRODED (NR 2 LE SLAT)
LEFT WING NR 2 LEADING EDGE SLAT, INBOARD CLOSURE RIB IS BADLY CORRODED ON THE INSIDE, EXFOILATED. *S/D* COMPLIED WITH EA 8-5750-38493.
Part: BELLFRAME — CORROSION (BS 1942)
SNRM 1144, SURFACE CORROSION ON BELLFRAME AT STA 1942 STR 51L AND 51 R. BURNISHED SURFACE CORROSION AND REMOVED DAMAGED AREA PER SRM 51-21-01, FABRICATED NEW SPLICES AND SECTION OF FRAME PER SRM 53-30-00, INSTALLED REPAIR SRM 53-30-00 FIG 5.