N741DA

No registry detail on file · not in current registry

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.

NO TEST · 2000-10-11 Matched by certificate designator
ATA 3350

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.

Source: SDR DLL14001986
OTHER · 2000-08-23 Matched by certificate designator
ATA 5311

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.

Source: SDR DLL14001630
OTHER · 2000-08-22 Matched by certificate designator
ATA 5311

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.

Source: SDR DLL14001625
OTHER · 2000-08-22 Matched by certificate designator
ATA 5311

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.

Source: SDR DLL14001624
OTHER · 2000-08-16 Matched by certificate designator
ATA 5311

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.

Source: SDR DLL14001609
OTHER · 2000-08-16 Matched by certificate designator
ATA 5311

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.

Source: SDR DLL14001608
OTHER · 2000-08-14 Matched by certificate designator
ATA 5312

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.

Source: SDR DLL14001601
OTHER · 2000-06-05 Matched by certificate designator
ATA 5312

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.

Source: SDR DLL14001101
Earlier reports · 1995–1999 · 22 reports

1999

FLUID LOSS; WARNING INDICATION · 1999-10-21 Matched by certificate designator
ATA 2910

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.

Source: SDR DLL14992327
OTHER · 1999-08-29 Matched by certificate designator
ATA 5720

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.

Source: SDR DLL14991925
OVER TEMP; WARNING INDICATION · 1999-06-29 Matched by certificate designator
ATA 3610

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.

Source: SDR DLL14991475
FALSE WARNING · 1999-03-26 Matched by certificate designator
ATA 2612

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.

Source: SDR DLL14990670
WARNING INDICATION · 1999-03-26 Matched by certificate designator
ATA 2612

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.

Source: SDR DLL14990674

1998

OTHER · 1998-09-03 Matched by certificate designator
ATA 5320

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.

Source: SDR DLL14981829
OTHER · 1998-09-03 Matched by certificate designator
ATA 5320

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.

Source: SDR DLL14981830
OTHER · 1998-09-03 Matched by certificate designator
ATA 5320

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.

Source: SDR DLL14981832
OTHER · 1998-09-03 Matched by certificate designator
ATA 5712

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.

Source: SDR DLL14981828
OTHER · 1998-09-01 Matched by certificate designator
ATA 5712

Part: BULKHEAD FITTING — CRACKED (WS 503)

THE RT WING PYLON BACKUP FITTING BULKHEAD WAS FOUND CRACKED. A DOUBLER REPAIR IS INSTALLED.

Source: SDR DLL14981827
OTHER · 1998-07-26 Matched by certificate designator
ATA 5240

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.

Source: SDR DLL14981575
WARNING INDICATION · 1998-07-01 Matched by certificate designator
ATA 7320

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.

Source: SDR DLL14991489
NO TEST · 1998-05-02 Matched by certificate designator
ATA 3350

Part: BULB — FAILED (CABIN)

EXTERIOR EMERGENCY LIGHT AT R-4 DOOR INOP. RELAMPED.

Source: SDR DLL14980946
NO TEST · 1998-03-04 Matched by certificate designator
ATA 3350

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTING OUT AFTER 20 SEC IN F/C CABIN. REPLACED POWER SUPPLY.

Source: SDR DLL14980516

1997

SMOKE/FUMES/ODORS/SPARKS · 1997-10-26 Matched by certificate designator
ATA 5610

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.

Source: SDR DLL14972163
SMOKE/FUMES/ODORS/SPARKS · 1997-07-16 Matched by certificate designator
ATA 3320

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.

Source: SDR DLL14971396

1996

NO TEST · 1996-10-06 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN)

ON LAYOVER, FOUND EMERGENCY LIGHT POWER SUPPLY AT 3R INOP.

Source: SDR DLL14962233
WARNING INDICATION · 1996-08-23 Matched by certificate designator
ATA 2432

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.

Source: SDR DLL14961958
NO TEST · 1996-08-08 Matched by certificate designator
ATA 3350

Part: TRACK — DAMAGED (CABIN)

EMERGENCY LIGHT TRACK AT MID GALLEY DAMAGED. REPLACED SECTION OF EMERGENCY LIGHT TRACK, CHECKS GOOD.

Source: SDR DLL14961857
FLUID LOSS; WARNING INDICATION · 1996-02-20 Matched by certificate designator
ATA 3230

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.

Source: SDR DLL14960383

1995

NO TEST · 1995-12-16 Matched by certificate designator
ATA 3350

Part: EEL POWER SUPPLY — INOPERATIVE (GALLEY)

ON LAYOVER, FOUND EMERGENCY LIGHTS IN LOWER GALLEY INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY. CHECKS GOOD.

Source: SDR DLL14954714
OTHER · 1995-11-16 Matched by certificate designator
ATA 3350

Part: EEL LENS — MISSING (CABIN)

EXIT LIGHT LENS ON FWD SIDE OF FIRST CLASS GALLEY RIGHT SIDE MISSING. REPLACED LENS, LIGHT OP CHECKS NORMAL.

Source: SDR DLL14954407