N2826W
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.
8 reports on file, 1995-01-16 – 1996-02-29.
Part: BRAKES — REQD SERVICE (LEFT)
AFTER INITIAL BREAK APPLICATION ON RUNWAY, BRAKES WERE NORMAL. BUT ON SUBSEQUENT APPLICATION TO TURN OFF RUNWAY LEFT BRAKES WERE SOFT AND INEFFECTIVE. BLED NR 3 AND NR 4 BRAKES, ANTI-SKID TEST WAS NORMAL, RESET DEBOOST ON LEFT GEAR AND OPERATION NORMAL.
Part: BATTERIES — DISCHARGED (AIRSTAIRS)
EMERGENCY EXIT LIGHT OVER THE BOTTOM STEP OF THE AIR STAIRS IS INOP. REPLACED BATTERIES, OPS NORMAL.
Part: ANGLE — CRACKED (NR 7 LE SLAT)
FOUND DURING A-2 LETTER CHECK, .25 INCH CRACK IN NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0 PAR 5A.
Part: ACTUATOR — FAULTY (NR 1 LE FLAP)
ON CLIMB AFTER GEAR RETRACTION, NR 1 L/E KRUGER FLAP DID NOT RETRACT. FLIGHT RETURNED TO DFW. REPLACED NR 1 L/E FLAP ACTUATOR AND S202 POSITION SWITCH, OPERATION NORMAL.
Part: ANGLE — CRACKED (FS 1273)
DURING LETTER CHECK INSPECTION, THE RH TORQUE BOX FORWARD TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. ALSO, THE FWD TRANSVERSE BEAM WAS FOUND CRACKED. IN ACCORDANCE WITH B727 S/B 53-0129 REV 4, BOTH THE BEAM AND THE ANGLE WERE REPLACED.
Part: FLANGE — CRACKED (NR 7 SLAT)
FOUND ON A1 LTR CK, NR 7 SLAT CRACKED FLANGE TWO PLACES UNDER ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0 P 802.
Part: PUMP — SHEARED SHAFT (NR 2 ENGINE)
NR 2 ENGINE FLAMED OUT AT BEGINNING OF DESCENT WHEN THROTTLE WAS RETARDED. DID NOT RESTART. LANDED SLC. REPLACED FUEL PUMP AND CONTROL OPERATION NORMAL.
Part: NOSE COWL — CRACKED (NR 3 ENG)
DURING INITIAL INSPECTION, A 4 INCH CRACK WAS FOUND IN THE OUTER SKIN AT APROXIMATELY THE 11 O/C POSITION. THE CRACK WAS REPAIRED PER SRM 54-30-3 FIG 3A, WHICH REQUIRES A MRR, REF NR 5987.