N050FE
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.
13 reports on file, 1996-10-31 – 2001-07-30.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,712 hrs · 23,827 cycles
BS 919 AFT SIDE OF FRAME BETWEEN LT AND RT LONGERON 49 AREAS OF LEVEL 1 CORRODED. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-00, 51-21-01, 51-41-01 & 51-35-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,712 hrs · 23,827 cycles
MAIN CABIN FLOORBOARD CROSSBEAM SUPPORT IS CORRODED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW SRM 51-21-01, 51-10-01.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,712 hrs · 23,827 cycles
MAIN CABIN SEAT TRACK IS SPLIT AND CRACKED AT O/B CLIP LUG. *S/D* REMOVED AND REPLACED TRACK PER SRM 53-60-01 FIG 1, 55-31-01.
Earlier reports · 1996–1998 · 10 reports
1998
Part: ANGLE — CRACKED (VERT STAB)
REPLACED UPPER VERTICAL STAB REAR SPAR BASE ANGLE (CRACKED). REPLACED AMC7279-1 BASE ANGLE WITH AMC727950, BASE ANGLE PER EO 8-5630-7-4303B PT 2.
Part: STRIKER — OUT OF ADJUST (AC DOOR)
A/C DOORS CAUTION LT ILLUM IN FLT FOR 25 SEC. FOLLOW RED TABS AND DIVERTED TO DEN. T/S SYS VERF SWITCH OPS, RELAY FUNCTION AND WIRING, NO PROBLEM FOUND. STRIKER PLATE THROW ON RIGHT DOOR OUT OF LIMITS. ADJUSTED STRIKER PER M/M 52-42-01-2. DOOR OPS AND LIGHT IND NORMAL. REMOVED MEL NR 39037.
Part: LATCH — LACK OF LUBE (MLG DOOR)
98-0077 - AFTER GEAR RETRACTION ON TAKEOFF, THE RED RIGHT GEAR LIGHT STARTED FLICKERING ON BOTH PANELS. THE GEAR WAS RECYCLED IN ACCORDANCE WITH THE RED TABS. THE LIGHT REMAINED EXTINGUISHED. FAULT CODE 32-30 APR. FOUND RIGHT MLG DOOR LATCH ROLLER LINK BINDING, LUBED AND CLEANED. CHECKED MLG DOOR PROX SENSOR IAW M/M 32-61-03. OPS CKS NORMAL.
1997
Part: SPAR — CRACKED (HORIZ STAB)
AFT FACE OF HORIZONTAL STAB CENTER SECTION UPPER SPAR LT SIDE CRACKED.
Part: SWITCH — FAILED (LE SLATS)
STA-MEM SLAT DISAGREE LIGHT ON AFTER TAKEOFF. * S/D* INSTALLED NEW LOB B SWITCH PER 27-84-01 EXCEPT FOR PG 204A NR 5, WHICH WAS C/W ABOVE JOB PROGRESS FORMS (2 EA) 108847CR JPF COMPLETE SLAT SYS CHECKS GOOD PER MM 27-84-01 PG 205 PARA 3.
1996
Part: CTR WING SECTION — CORRODED (BS 1185)
SNRM 232, MAIN CABIN, UPPER SURFACE OF CENTER WING SECTION CORROSION AT LT SIDE APPROX STA 1185, SIDEWALL AREA. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.
Part: CTR WING SECTION — CORRODED (BS 1341)
SNRM 227, MAIN CABIN, UPPER SURFACE OF CENTER WING SECTION CORROSION AT LT SIDE APPROX STA 1341, SIDEWALL AREA. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.
Part: CTR WING SECTION — CORRODED (BS 1205)
SNRM 222, MAIN CABIN, UPPER SURFACE OF CTR WING SECTION CORROSION AT RT SIDE APPROX STA 1205, SIDEWALL AREA. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.
Part: CTR WING SECTION — CORROSION (BS 1205)
SNRM 211, MAIN CABIN, UPR SURFACE OF CTR WING SECTION CORROSION AT LT SIDE APPROX STA 1205. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.
Part: SKIN — CRACKED (BS 1159)
SNRM 00152, FUSELAGE SKIN HAS A 5 INCH CRACK AT STA 1159 STR L-37. *S/D* NDT VERIFIED END OF CRACK, STOP DRILLED CRACK PER EA NR 8-5340-31737. FABRICATED DOUBLER AS PER DAC PRINT 53-40-00. OK TO INSTALL DOUBLER QA-20, INSTALLED REPAIR DOUBLER, REF SRM 53-40-00.