N289F
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.
21 reports on file, 1996-05-09 – 1998-06-03.
Part: SWITCH — MALFUNCTIONED (NLG)
LANDING PAKN UNSAFE GEAR INDICATION ON NOSE GEAR, RECYCLED GEAR HAD THREE GREEN LIGHTS, SAFE INDICATION. INSPECTED NOSE GEAR, NO DEFECTS NOTED, INSTALLED GEAR PIN, FERRIED A/C TO PANC, REPLACED NOSE GEAR DOWNLOCK SWITCH IAW L-188 WDM G-2. OPS CHECKS NORMAL.
Part: GEARBOX — FAILED (NR 2 ENGINE)
NR 2 ENGINE SHUTDOWN AT 1545Z DUE TO LOW ENGINE AND REDUCTION GEARBOX OIL PRESSURE. FOUND TACH DRIVE GEARS AND OIL PUMP DRIVE GEARS WOULD NOT TURN WHEN PROP WAS TURNED.
Part: ENGINE — FAILED (NR 2)
NR 2 ENGINE LOSS OF HP WITH UNCONTROLLABLE RISE IN TIT. ENGINE SHUTDOWN AT 1305Z.PROBABLE CAUSE: FOD
Earlier reports · 1996–1997 · 18 reports
1997
Part: ENGINE — FAILED (NR 4)
PROP BRAKE INEFFECTIVE ABOVE 200 KTS (NR4). REMOVED AND REPLACED ENGINE AND PROP ASSEMBLIES PER ONE-120 AND ONE-115 OPS CHECKS GOOD PER ONE-113 AND ONE-112. (SEE LR7A9732)
Part: ENGINE — FAILED (NR 4)
SHUTDOWN NR 4 ENGINE AT 1451Z DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED ENGINE AND PROP ASSEMBLIES PER ONE-120 AND ONE-115. OPS CHECKS GOOD PER ONE-113 AND ONE-112.
Part: PROP ASSY — FAILED (NR 2 ENGINE)
NR 2 ENGINE RPM DECAYED SHUTDOWN ENGINE AT 2300Z. REMOVED AND REPLACED NR 2 PROP IAW CARD NR ONE115.
Part: SEAL — WORN (NR 3 PROP)
NR 3 ENGINE PROP OVERSPEED PROP PITCH LOCKED. SHUTDOWN NR 3 ENGINE WHEN RPM DECREASED TO 13,600. RESEALED NR 3 PROP RESERVOIR, OPERATED AND LEAK CHECKED NORMAL ON GROUND RUN.
Part: SEAL — WORN (NR 3 PROP RESERV)
NR 3 ENGINE PROPELLER OVERSPEED PROP PITCH LOCKED. SHUT DOWN NR 3 EN ROUTE WHEN RPM DECREASED TO 13,600. RE-SEALED NR 3 PROPELLER RESERVOIR, OPERATED AND LEAK CHECKED ON GROUND RUN. (X)
Part: INTERCOSTAL — CRACKED (BS 300)
YIP - DURING SCHEDULED INSPECTION, FOUND AT FS 300, LONGERON 49, INTERCOSTAL FORMER FOR DOOR HOOK SUPPORT CRACKED .625 INCHES. REPAIRED IAW L-188 SRM 53-2-3. (M)
Part: PANEL — CRACKED (WS 202)
YIP - DURING SCHEDULED INSPECTION, AT LEFT WING LOWER SURFACE, (DRY-BAY AREA), PLANK 3 AT 3/4 JOINT, WS 202-204, FOUND 2 INCH CORROSION/CRACK RPEC AND UT INDICATION. REPAIRED IAW ZIA DER (COTNEY ENGINEERING) DWG NR C73-R01. (M)
Part: INTERCOSTAL — CRACKED (BS 280)
YIP - DURING SCHEDULED INSPECTION, FOUND AT FS 280, LONGERON 49, INTERCOSTAL FORMER FOR DOOR HOOK SUPPORT CRACKED .500 INCHES. REPAIRED IAW L-188 SRM 53-2-3. (M)
Part: INTERCOSTAL — CRACKED (BS 360)
YIP - DURING SCHEDULED INSPECTION, FOUND AT FS 360, LONGERON 49, INTERCOSTAL FORMER FOR DOOR HOOK SUPPORT CRACKED 1 INCH. REPAIRED IAW L-188 SRM 53-2-3. (M)
Part: INTERCOSTAL — CRACKED (BS 837)
YIP - DURING SCHEDULED INSPECTION, FOUND AT FS 837, LONGERON 49, INTERCOSTAL FORMER FOR DOOR HOOK SUPPORT CRACKED .625 INCHES. REPAIRED IAW L-188 SRM 53-2-3. (M)
Part: ANGLE — DAMAGED (CARGO DOOR)
YIP - DURING SCHEDULED INSPECTION, FWD CARGO DOOR ASSY, TOP FRAME 'Z' ANGLE DAMAGED AT LOOP OPENINGS NR 2, NR 3, NR 4, NR 5, NR 6 AND NR 7. REPLACED TOP FRAME 'Z' ANGLE IAW LAC L-188 SRM 51-2-1, PAGE 2, PARA D. (M)
Part: FRAME — DAMAGED (CARGO DOOR)
YIP - DURING SCHEDULED INSPECTION, AFT CARGO DOOR ASSY, TO FRAME 'Z' ANGLE DAMAGED AT LOOP OPENINGS NR 1, NR 2, AND NR 3. REPLACED TOP FRAME 'Z' ANGLE IAW LAC L-188 SRM 51-2-1, PG 2, PARA D. (M)
Part: SUPPORT — CRACKED (BS 845)
YIP - DURING SCHEDULED INSPECTION, FOUND AT FS 845, LONGERON 49, REAR CARGO DOOR SILL, FLOORBEAM TO LONGERON SUPPORT ATTACHMENT CRACKED .75 INCH. REPAIRED IAW L-188 SRM 53-2-4. (M)
Part: INTERCOSTAL — CRACKED (BS 240)
YIP - DURING SCHEDULED INSPECTION, FOUND AT FS 240, LONGERON 49, INTERCOSTAL FORMER FOR DOOR HOOK SUPPORT CRACKED .750 INCHES. REPAIRED IAW L-188 SRM 53-2-3. (M)
Part: FIRE CONTROL AMP — MALFUNCTIONED (NR 1 ENGINE)
OTL - DURING CRUISE ENROUTE TO OTL, NR 1 ENGINE FIRE WARNING CAME ON. SHUT DOWN THE ENGINE AND FIRED BOTH FIRE BOTTLES. LANDED AT OTL. NO EVIDENCE OF FIRE AND FIRE LOOP SYSTEM TEST AS PER THE MM. REPLACED FIRE DETECTOR CONTROL AMPLIFIER AND BOTH FIRE BOTTLES. SYSTEM GROUND TESTS NORMAL WITH ENGIEN RUNNING OR SHUT DOWN. (M)
1996
Part: SKIN — CRACKED (WS 177-179)
YIP - DURING INSPECTION, FOUND CRACK IN UPPER RIGHT WING, 2/3 PLANK JOINT AT WS NR 177-179. REMOVED CRACKED AREA AS PER L-188 BS 620. INSTALLED REPAIR AS PER ZIA DER APPROVED DRAWING NR A81-R02. (M)
Part: SPAR CAP — CRACKED (WS 70)
YIP - DURING INSPECTION, FOUND RIGHT WING FRONT SPAR LOWER 'T' RAIL CRACKED AT STATION 70. INSTALLED REPAIR AS PER ZIAA DER APPROVED DRAWING NR A91-R01. (M)
Part: BEARING SUPPORT — CRACKED (NR 3 ENGINE)
ANC - DURING TAKEOFF FROM ADQ, HAD FIRE WARNING INDICATION ON NR 3 ENGINE. E-HANDLE PULLED AT 22.37Z. CREW ELECTED TO PROCEED TO ANC. FOUND NR 3 ENGINE REAR TURBINE BEARING SUPPORT COCKED AND CRACKED 75 PERCENT OF ITS CIRCUMFERENCE, THUS DIRECTING EXHAUST GASES/HEAT TO ZONE 4 FIRE DETECTION ELEMENT. REPLACED NR 3 REAR TURBINE BEARING SUPPORT. OPERATIONAL CHECK NORMAL. (M)