N741DA
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.
30 reports on file, 1995-11-16 – 2000-10-11.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,302 hrs · 17,923 cycles
R-2 DOOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY FOR R-2 DOOR LIGHT, OPS CHECKS GOOD.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,742 hrs · 17,789 cycles
STA 1083 FRAME CRACKED APPROX 1 INCH BELOW FLOOR LINE LT SIDE. REPAIRED PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,742 hrs · 17,789 cycles
STA 1063 FRAME CRACKED APPROX 2 INCHES ABOVE FLOOR LINE LT SIDE. REPAIRED FRAME.
Part: FRAME — CRACKED (CABIN) · airframe 71,742 hrs · 17,789 cycles
STA 1103 FRAME CRACKED RT SIDE APPROX 3 INCHES BELOW FLOOR LINE MARKED. REPAIRED FRAME.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,742 hrs · 17,789 cycles
STA 1123 FRAME CRACKED, APPROX 1 INCH ABOVE FLOOR LINE LT SIDE. REPAIRED SAME.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,742 hrs · 17,789 cycles
STA 1123 FRAME CRACKED, APPROX 1 INCH ABOVE FLOOR LINE, LT SIDE. REPAIRED SAME.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,742 hrs · 17,789 cycles
HFEC INSP FOUND CRACK AT FS 1212 BLKD RBL 22.5 WL 182 REF OPN50424AD. REPAIRING CRACK PER SRM 53-11-00 FIG 854.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,936 hrs · 17,590 cycles
THE FS 1363 BULKHEAD WEB WAS FOUND WITH A .4 TYPICAL CRACK EMANATING FROM A FASTENER HOLE AT THE LBL 42.5 WEB JOINT AT WL 126. THE CRACKED AREA WAS TRIMMED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER L1011 SRM 53-11-00 FIG 851, LAC S/B 93-53-268, AND ER/A 377470-14AD.
Earlier reports · 1995–1999 · 22 reports
1999
Part: LINE — FAILED (NR 2 ENGINE)
1.5 HRS AFTER T/O, C-SYS HYD LO QTY LIGHT SAME ON AND QTY WENT MOMENTARILY TO 1/4 THEN BACK TO 3/8. FOLLOWED POM AND WITH NO PUMPS ON / NO SYS PRESS / QTY SLOWLY DECREASED OVER NEXT 3 HRS TO 1/16 LEVEL AND REMAINED THERE. EDP LOW PRESS LIGHT WAS ON BRIEFLY UNTIL EDP TURNED OFF. FOUND C-SYS PRESS LINE LEAKING. REPLACED SAME. LEAK CHECK OK AND SERVICED HYD SYS.
Part: STIFFENER — CRACKED (BS 983)
THE RBL 22.5 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR (FS 983) WAS FOUND WITH A TYPICAL CRACK EMANATING FROM A LIGHTENING HOLE IN THE STIFFENER WEB NEAR THE UPPER END. THE STIFFENER WAS REMOVED AND REPLACED WITH A NEW STIFFENER MANUFACTURED WITHOUT LIGHTENING HOLES PER ER/A 368106-14AD.
Part: LINE — LOOSE (NR 2 ENGINE)
NR 2 ENG NACELLE PYLON OVERHEAT LOOPS A & B LIGHTS ON AFTER TAKEOFF. BOTH LOOP LIGHTS WENT OUT WHEN THROTTLE/POWER REDUCED AND HIGH PRESSURE BLEED OFF. WHEN POWER INCREASED, LOOP LIGHTS CAME ON WITH HIGH PRESSURE BLEED OFF. INSPECTED DUCTING AND TIGHTENED CLAMPS IN SPLITTER AREA. INSPECTED AND TIGHTENED CLAMPS IN PYLON ABOVE ENGINE. FOUND B-NUT ON PNEUMATIC DUCT FWD OF EJECTOR VALVE BACKED OFF. TIGHTENED SENSE LINE B-NUT. APPLIED PNEUMATICS, RAN ENG PER PFHB AND CKS GOOD.
Part: FIRE WIRE — CHAFED (NR 2 ENGINE)
INTERMITTENT FIRE WARNING A LOOP NR 2 ENG OCCURRED AFTER T/O AT 1500 FT AGL, EPR 1.631 OAT 11 DEG C. NR 2 IDG DISCONNECTED, HYD PUMPS B1 C1 UNLATCHED, NO FIRE. REPAIRED WIRES FROM SPLITTER TO LOOP.
Part: FIRE WIRE — DAMAGED (NR 2 ENGINE)
NR 2 ENG A LOOP WARNING OCCURRED AFTER TAKEOFF AT 1500 FT AGL. REPAIRED WIRING ON ENGINE AND IN SPLITTER AREA.
1998
Part: DECK — CRACKED (BS 380)
THE FUSELAGE HORIZONTAL PRESSURE DECK WAS FOUND CRACKED AT RBL 102 AND FS 380. A DOUBLER/TRIPLER REPAIR WAS ACCOMPLISHED.
Part: DECK — CRACKED (BS 395-437)
THE NOSE LANDING GEAR PRESSURE DECK WAS FOUND CRACKED IN SIX LOCATIONS AT LBL 24 AND RBL 24 BETWEEN STA 395 AND 437. DOUBLER/TRIPLER REPAIRS ARE INSTALLED.
Part: FRAME — CORRODED (GALLEY DOORWAY)
THE FWD GALLEY DOORWAY FRAME WAS CORRODED NEAR THE LOWER SILL AT STR 25. THE DAMAGE WAS REMOVED AND A REPAIR SECTION SPLICED IN.
Part: RIB — CRACKED (RT & LT WING)
THE RT WING IWS 503 RIB UPPER CAP, LT WING IWS 555 RIB UPPER CAP WERE BOTH FOUND CRACKED. ALL CRACKED PARTS WERE REPLACED.
Part: BULKHEAD FITTING — CRACKED (WS 503)
THE RT WING PYLON BACKUP FITTING BULKHEAD WAS FOUND CRACKED. A DOUBLER REPAIR IS INSTALLED.
Part: CABLE — BROKEN (L3 DOOR)
L-3 DOOR TRACK LOCK PIN MECHANISM CABLE BROKEN UNABLE TO ACCOPMPLISH EMERGENCY OPS CHECK INSIDE AND OUTSIDE HANDLES. REPLACED CABLE.
Part: PS2 LINE — LEAKING (NR 2 ENGINE)
NACELLE NR 2 OVERHEAT ILLUMINATED ALONG WITH NR 2 ENG NAC/PYLON OVERHEAT, A & B ILLUMINATED. FOUND PRSOV PS2 LINE LEAKING. REPLACED LINE AND LEAK CHECKED. PERFORMED HIGH POWER RUN PER PFHB. NO FAULTS DETECTED.
Part: BULB — FAILED (CABIN)
EXTERIOR EMERGENCY LIGHT AT R-4 DOOR INOP. RELAMPED.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
EMERGENCY TRACK LIGHTING OUT AFTER 20 SEC IN F/C CABIN. REPLACED POWER SUPPLY.
1997
Part: WINDSHIELD — DEFECTIVE (COCKPIT)
SMOKE SMELL DETECTED IN THE COCKPIT WHILE EN ROUTE. SMOKE IDENT AND REMOVAL CHECKLIST IN THE POM WAS INITIATED. PART WAY THROUGH CHECKLIST SMOKE WAS VISUALLY DETECTED COMING FROM THE CAPTAINS WINDSHIELD HEAT SENSOR. LEFT WINDOW HEAT C/B'S WERE TRIPPED AND THE SMOKE ILLUMINATED. FOUND HEATER TEMINAL NR 2 ON CAPTS W/S BURNT. REPLACED TERMINAL BLOCK, CAPTS W/S, AND LT W/S HEAT CONTROLLER. OPS CKS OK.
Part: LIGHTS — OVERHEATED (GALLEY)
GOT STRONG SMELL THROUGH OUT CABIN WENT AWAY CAME BACK AS A/C TAXIED TO GATE. FOUND O/V HEAD LIGHTS AT MID GALLEY PLASTIC CLAMP WERE BURNT REPLACED ALL 6 LIGHT BULBS NO SMELL OK FOR SERVICE. ALSO CK CEILING O/H OF GALLEY AREA CK OK.
1996
Part: LIGHT — INOPERATIVE (CABIN)
ON LAYOVER, FOUND EMERGENCY LIGHT POWER SUPPLY AT 3R INOP.
Part: BATTERY — FAILED (BATTERY COMPT)
BATTERY CONDITION LIGHT CAME ON 3.5 HRS INTO FLT. NO AVIONIC OVERBOARD LIGHTS ON. CYCLED BATTERY CHARGER, C/B DID NOT CORRECT SITUATION. BATTERY CONDITION LIGHT WENT OUT 30 MINS AFTER IT CAME ON. BATTERY PHYSICALLY FELT WARM NOT HOT, 10 TO 15 MIN AFTER FIRST INDICATION. BATTERY CONDITION LIGHT ON A SECOND TIME 1 HR LATER.
Part: TRACK — DAMAGED (CABIN)
EMERGENCY LIGHT TRACK AT MID GALLEY DAMAGED. REPLACED SECTION OF EMERGENCY LIGHT TRACK, CHECKS GOOD.
Part: RETAINING RING — SHEARED (LT MLG)
LT LANDING GEAR TRUCK POSITION CYLINDER PISTON RETAINING RING HAD SHEARED FROM THE THREADED PORTION. LOST C-SYSTEM HYDRAULICS ON LANDING, CAUSED AUTO GROUND SPOILERS FAIL. REPLACED ACTUATOR, OPERATION NORMAL.
1995
Part: EEL POWER SUPPLY — INOPERATIVE (GALLEY)
ON LAYOVER, FOUND EMERGENCY LIGHTS IN LOWER GALLEY INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY. CHECKS GOOD.
Part: EEL LENS — MISSING (CABIN)
EXIT LIGHT LENS ON FWD SIDE OF FIRST CLASS GALLEY RIGHT SIDE MISSING. REPLACED LENS, LIGHT OP CHECKS NORMAL.