N241DL
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.
15 reports on file, 2001-02-01 – 2006-08-14.
Part: SPAR — CRACKED (BS 224) · airframe 43,357 hrs · 24,764 cycles
TWO FASTENER HOLES IN THE RIGHT REAR SPAR AT STA 224.14 (AT THE LANDING GEAR BEAM O/B ATTACH FITTING) CRACKED. REAMED ONE HOLE PER BOEING SB 737-1216R2 AND REAMED SECOND HOLE AND INSTALLED A FREEZE PLUG PER BOEING MESSAGE 1-210954789-9 WITH FAA APPROVED 8100-9 DATED 24 AUG 2006.
Part: SPAR — DAMAGED (BS 224) · airframe 43,357 hrs · 24,764 cycles
FASTENER HOLE IN THE LT UPPER REAR SPAR CHORD AT STA 224.14 (AT THE LANDING GEAR BEAM OB ATTACH FITTING) CRACKED .024 INCHES BEYOND ALLOWABLE LIMITS. REPLACED THE REAR SPAR CHORD SEGMENT FROM THE SIDE OF THE FUSELAGE BODY TO REAR SPAR STA 285. NOTE: PLEASE REMOVE PIDR AS THE OPERATOR DESIGNATOR IN ORDER TO IDENTIFY THE OPERATOR AS A GENERAL AVIATION OPERATOR.
Part: REPAIR — IMPROPER (FUSELAGE) · airframe 43,357 hrs · 24,764 cycles
EXISTING REPAIR AT BS887 AND STR25RT NOT IN COMPLIANCE WITH THE SRM. REPLACED EXISTING REPAIR IAW SRM 53-00-01 REPAIR 31.
Earlier reports · 2001–2005 · 12 reports
2005
Part: SPAR — CRACKED (WING, MID FLAP) · airframe 42,131 hrs · 23,080 cycles
DURING SHOP VISIT, THE NR 3 MID FLAP FRONT SPAR ASSEMBLY WAS FOUND WITH A CRACKED LOWER CHORD AND DENTED WEB. DAMAGE WAS DUE TO SERVICE DAMAGE. REPAIRED PER ERA 093135-14.
2004
Part: PCU — LEAKING (RUDDER) · airframe 41,555 hrs · 22,266 cycles
A SYSTEM HYD RESERVOIR APPROX 1/4 FULL. SUSPECT POSSIBLE HYD LEAK ON ENG DRIVEN SIDE, GOOD PRESSURE. FOUND RUDDER PCU LEAKING. REPLACED SAME.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,784 hrs · 21,160 cycles
EMERGENCY FLASHLIGHT BATTERY DEAD. REPLACED BATTERY PACK.
2003
Part: LENS — CRACKED (CABIN) · airframe 40,614 hrs · 20,931 cycles
REPLACED 2 LEFT EMERGENCY EXIT LIGHT ASSY, OPS CHECK NORMAL.
Part: FILTER — CONTAMINATED (HYD SYSTEM) · airframe 40,280 hrs · 20,470 cycles
LOST SYSTEM-B PRESSURE ON LGA FINAL. DIVERT JFK, NORMAL LANDING. PER MM REPLACED RESERVOIR PRESS MODULE FILTER DUE WATER FOUND IN BOWL CAP AND HOUSING ON ENG. RUN-UP SYSTEM OPS CHECK OK. LEAK CHECK OK.
2002
Part: CONNECTOR — MALFUNCTIONED (RT MLG WW) · airframe 39,287 hrs · 19,087 cycles
TAKEOFF WARNING HORN CAME ON UPON ADVANCING POWER FOR TAKEOFF. ALL INDICATIONS NORMAL FOR TAKEOFF EXCEPT HORN. RESEATED CONNECTOR PLUGS 4514P AND 5983P, TAKEOFF WARNING TEST NORMAL.
Part: RELAY — INTERMITTENT (CENTRAL WARNING) · airframe 39,287 hrs · 19,087 cycles
TAKEOFF WARNING HORN CAME ON WHEN ADVANCING POWER FOR TAKEOFF. REPEAT WRITEUP. SYSTEM REPLACED R274 PARK AND SQUAT RELAY DUE TO INTERMITTENT OPERATION. TAKEOFF WARNING TEST NORMAL.
Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 39,176 hrs · 18,987 cycles
AFT CABIN MEGAPHONE INOPERATIVE. INSTALLED NEW BATTERIES, MEGAPHONE STILL INOPERATIVE. REPLACED MEGAPHONE.
2001
Part: MODULE — DEFECTIVE (HYDRAULIC SYS) · airframe 38,851 hrs · 18,688 cycles
AFTER RT ENG START, TURNED RT PACK ON WHILE USING RT ENG AS PNEUMATIC SOURCE. CABIN FILLED WITH SMOKE. ACFT EVACUATED. ALL SLIDES DEPLOYED (1L, 2L, 1R, 2R). BORESCOPED 1-3 STAGES OF HPC AND FRAME TO BOOSTER INTERFACE. NO WETTING FOUND. REPLACED RT ACM AND WATER SEPARATOR BAG AND HEPA FILTER. REPLACED HYD PRESS RSVR MODULE. RAN ACFT TO TAKEOFF PWR. ALL CK'D GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,888 hrs · 17,747 cycles
2L EMERGENCY LIGHT INOP. RELAMPED LIGHT.
Part: WIRE — CHAFED (OVERHEAD) · airframe 37,289 hrs · 17,143 cycles
ON TOUCHDOWN SHOWER OF SPARKS FROM O/H PANEL BETWEEN F/C GALLEY AND FLT DECK.CONTRACT MTC FOUND WIRE BUNDLE W132 BURNED. FOUND SAME WIRING BUNDLE RUBBING ON PANEL LATCH CAUSING WIRES TO SHORT OUT. REPAIRED WIRING.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,206 hrs · 17,048 cycles
THE CENTER WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT WL 195 AT BOTH LBL 5 AND RBL 5. THE CRACKS WERE REPAIRED PER S/B 737-53A1173, REV 3.