N507FE
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.
32 reports on file, 1995-02-04 – 1997-06-11.
Part: SKIN — CORRODED (BS 1075)
NR 0325 004, LIGHTNING STRIKE ON EXTERIOR SKIN BS 1075, WL 205, BETWEEN 16 RT AND 17 RT. *S/D* REMOVED LIGHTNING STRIKE ON EXTERIOR SKIN 1075, WL 205 BETWEEN STRINGER 16 RT AND 17 RT. UPON REMOVAL OF DAMAGE FOUND SKIN IN DOUBLER DAMAGED AT BS 1075, STR 17 RT. TRIMMED SKIN, BLEND OUT CORROSION ON BONDED DOUBLER. INSTALLED FILLERS AND EXTERNAL DOUBLER OVER AREA PER FED-EX EA7-5310-34070.
Part: CHORD — CORRODED (BS 1176)
NR 0123 003, CORROSION BETWEEN AND ON WEB AND CHORD AT BS 1176, RBL 12, WL 208. *S/D* REMOVED 1176 CHORD FROM RBL 32.75 TO LBL 65. FOUND CORROSION ON WEB UNDER 1176 CHORD. REMOVED WEB AT 1150 TO 1176, RBL 20 TO LBL 20 AND FABRICATED NEW WEB. INSTALLED NEW CHORD AND WEB IAW FED-EX SRM 53-10-1, 51-10-1, 51-10-2, 51-10-6, 51-20-1, 51-20-3, 51-30-2.
Part: FRAME — CRACKED (BS 930)
NR 0320 001 WHILE WORKING 7-5300-7-2304 M1, FOUND BS 930 FRAME TO BE CRACKED AT BS 930, WL 188-194, LBL 62. REPAIRED CRACK AT BS 930 FRAME W/L 188-194, LBL 62 PER SB. 727-53-0130 REV 2 FIGURE 6.
Earlier reports · 1995 · 29 reports
1995
Part: MECHANISM — WORN (TE AFT FLAPS)
FL 31.0, MACH .84 NOTICED 10 TO 12 DEG R/YOKE DISPLACEMENT. ATTEMPTED TO TRIM RUDDER AND GOT A MOD-SEVERE BUFFET, CONTINUED AFTER SLOWING TO .80 MACH. BUFFET STOPPED WHEN EXTENDING SPEED BRAKES SLIGHTLY 1 TO 2 DEGREES. BUFFET WOULD BEGIN AGAIN AFTER RETRACTING SPEEDBRAKE. DECLARED AN EMERGENCY LANDING INTO ICT. VISUALLY INSP/OPS FLT CONT, T/E AFT FLAPS LOOSE. REPLACED CARRIAGE PLATES AND ECCENTRIC BUSHING ON RT I/B AFT FLAP AND ADJ MM 27-51-2. ADJ ECCENTRIC BUSHING ON LT I/B AND RE-ADJ DROOP ON BOTH I/B FLAPS MM 27-51-2. REPLACED 2 CARRIAGE PLATE ASSYS ON RT O/B AFT FLAP ADJ ECCENTRIC BUSHINGS AND RE-ADJ DROOP O/B FLAPS AND INSP AFT FLAP T/E FLAP RIG MM 27-51-12.
Part: FRAME — DOUBLE DRILLED (BS 600)
DOUBLE HOLE IN FRAME BS 600, STR 4R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 51-40-3.
Part: FLOORBEAM — CORRODED (BS 276)
CORROSION FOUND ON TOP CHORD OF FLOORBEAM BS 276, RBL 12, WL 208. REPAIRED TOP CHORD FLOORBEAM IAW 727 SRM 51-40-04, 51-20-01.
Part: FLOORBEAM — CORROSION (BS 560)
FOUND CORROSION ON FLOORBEAM STA 560, RBL 16, WL 198. REMOVED CORROSION AND REPAIRED FLOORBEAM AT BS 560, RBL 16, WL 198 PER FEDEX EA 7-5310-23795.
Part: FLOORBEAM — CORROSION (BS 312)
CORROSION ON TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208. REPAIRED TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208 IAW EA 7-5310-23790.
Part: FLOORBEAM — CORROSION (BS 1110)
CORROSION (72C237-02) UNDER TOP CHORD OF FLOORBEAM AT NUTPLATES HOLES BS 1110, RBL 10-50, WL 208. REPAIRED FLOORBEAM BS 1110, RBL 10-50, WL 208 PER FEDEX EA 7-5310-23793.
Part: FLOOR BEAM — CORRODED (BS 344)
CORROSION ON TOP AND BOTTOM OF TOP CHORD OF FLOORBEAM AT BS 344 RBL 17 - LBL 61 WL 208. REPLACED TOP CHORD FROM LBL 707 - RBL 70. IAW FEDEX DRAWING NUMBER SR 27 53-007.
Part: FLOOR BEAM — CORRODED (BS 680)
CORROSION FLOOR BEAM UPPER CHORD BS 680 LBL 36 WL 208. REMOVED CORRODED CHORD, FABRICATED AND INSTALLED REPLACEMENT CHORD AT BS 680 LBL 36 TO RBL 14 WL 208 PER FEDEX SRM 53-10-8.
Part: SHEAR TIE — CRACKED (FS 441)
FOUND SHEAR TIE CRACKED AT AFT SIDE STA 441 RT BETWEEN STR 18 AND 19, RBL 65. REMOVED CRACKED SHEAR TIE STA 441 RT STR 18 AND 19 (AFT SIDE) RBL 65 AND REPLACED WITH FABRICATED SHEAR TIE.
Part: FRAME — CRACKED (FS 500)
WHILE ACCESSING FOR FUSELAGE 00124, FOUND FRAME CRACKED AT STA 500 RBL 24 WL 158. CUT OUT DAMAGE FRAME AREA. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3.
Part: BEAM — CRACKED (BS 758)
CRACK FOUND ON LONGITUDINAL BEAM AT BS 758 RBL 45 WL 208. REMOVED AND REPLACED LONGITUDINAL BEAM AT STA 758 RBL 45 WL 208.
Part: FRAME — CORRODED (BS 500)
FOUND CORROSION UNDER NUTPLATE ON FRAME STA 500 LBL 53 WL 175. CUT OUT DAMAGED AREA ON FRAME BS 500 LBL 53 WL 175 AREA OF 1 INCH BY .75 INCH FABRICATED FILLER-DOUBLER AND INSTALLED PER SRM 51-40-3.
Part: FRAME — CORRODED (FS 560)
FOUND CORROSION UNDERNEATH NUTPLATE ON FRAME STA 560 LBL 48 WL 170. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.
Part: HINGE FITTING — CORRODED (RT AILERON)
RIGHT O/B AILERON 2ND HINGE FITTING FROM I/B END HAS CORROSION. REMOVED AND REPLACED NEW AILERON HINGE FITTING.
Part: BLKHD WEB — CRACK (BS 950)
POSSIBLE CRACK AT BS 950 BULKHEAD LBL 40 WL 185. REPAIRED CRACK IS 950 BULKHEAD AT LBL 40 WL 185 PER FEDEX SRM 53-10-9 FIG 2.
Part: FRAME — CORRODED (BS 520)
CORROSION IS FWD CARGO BAY ON FRAME AT BS 520 STR 26 LBL 25. REMOVED CORROSION FROM FRAME OUT OF LIMITS PER SRM REPAIRED PER FEDEX SRM 51-40-3.
Part: BEAM — CORRODED (BS 760-840)
CORROSION FOUND ON TOP AND BOTTOM SIDE OF LONGITUDINAL BEAM IS SEVERAL AREAS FROM BS 760-840 WL 208 LBL 25. REMOVED AND REPLACED LONGITUDINAL BEAM IAW 53-10-2.
Part: SKIN — GOUGED (NR 4 LE FLAP)
FIXED L/E GOUGED ON LOWER SURFACE AT NR 4 SLAT I/B TRACK. REMOVED EXISTING REPAIR AND FABRICATED AND INSTALLED NEW REPAIR PER FEDEX SRM 5730-2.
Part: SKIN — OIL CANNING (BS 367)
SKIN IS OIL CANNING BS 367 BETWEEN STR 22 AND 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW FEDEX SRM 53-30-3.
Part: DOUBLER — CORRODED (BS 415-457)
BS 451-457 BETWEEN STR 18-19R RBL 65 INTERNAL DOUBLER ON E-BAY EXHAUST HAS SIGNS OF CORROSION. REMOVED OLD DOUBLER BS 451-457 STR 18 AND 19R RBL 65 AND INSTALLED NEW DOUBLER.
Part: SEAT TRACK — CORROSION (BS 620-627)
CORROSION ON SEAT TRACK FLANGE BS 620-627, LBL 45, WL 208.5 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK AT BS 590 - 650, LBL 45, WL 208.
Part: SKIN — CORRODED (NR 6 LE FLAP)
CORROSION (76C002-00) NR 6 K-FLAP DATAPLATE. REMOVED DAMAGE AROUND DATAPLATE, REPAIRED K-FLAP WEB AND RELOCATED DATAPLATE IAW SRM 5250-3, DWG SR 27-57-010 REV B.
Part: BEAM — CRACKED (PAX DOOR)
FWD ENTRY DOOR LOWER GATE BEAM HAS A 1.5 INCHES CRACK ON FWD SIDE. REMOVED AND REPLACED FWD ENTRY DOOR LWR GATE BEAM.
Part: SEAT TRACK — CORROSION (BS 344-347)
CORROSION ON SEAT TRACK FLANGE AT BS 344-347, LBL 42, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 344-400, LBL 45, WL 208.
Part: SEAT TRACK — CORRODED (BS 480-483)
CORROSION ON SEAT TRACK FLANGE BS 480-483 LBL 46 WL 208.5. REMOVED AND REPLACED SEAT TRACK AT BS 480-590 LBL 46 WL 208.5 PER FEDEX SRM 53-10-5.
Part: STRINGER — CORROSION (BS 435-440)
CORROSION (NRO246) FOUND ON STR 19R FROM BS 435-440 RBL 65. REMOVED AND REPLACED STR 19R FROM BS 410.5 - 441 IAW FEDEX SRM 53-10-3 FIG 1 DETAIL II.
Part: SEAT TRACK — DAMAGED (BS 600-720)
MECHANICAL DAMAGE ON SEAT TRACK AT BS 600 PLUS 16 INCHES - 620 PLUS 3, BL 0, WL 208.5 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM BS 600 - 720, BL 0, WL 208.5.
Part: SEAT TRACK — CORRODED (BS 490/540/640)
CORROSION ON SEAT TRACK FLANGE BS 490-540, 570 AND 640, RBL 25, WL 208.5. REMOVED AND REPLACED TRACK FROM BS 480-740 IAW FEDEX SRM 53-10-1.
Part: CLIP — DAMAGED (BS 4OO)
MECHANICAL DAMAGE FOUND ON STR CLIP AT BS 400 STR 6L. REMOVED AND REPLACED STR CLIP AT BS 400 STR 6L.