N225DL
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.
12 reports on file, 1998-10-13 – 2005-04-18.
Part: SKIN — GOUGED · airframe 32,729 hrs · 19,801 cycles
AT MID VISIT FOUND FUSELAGE SKIN GOUGED AT STA 1129-1138 WL 265. REPAIRED PER ERA 098117-14. TIME LIMITED REPAIR. ADDITIONAL ER/A IS REQUIRED FOR CONTINUED SERVICE LONGER THAN 12 MONTHS FROM REPAIR ACCOMPLISHMENT ACTL LINE 2050.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,776 hrs · 18,495 cycles
ON PRE-DEPARTURE FOUND ROWS 1 AND 2 DEF EMERGENCY LIGHTS INOP ON SEATS. PINS WERE FOUND OUT OF THE CONNECTOR AND RE-INSERTED INCORRECTLY RESULTING IN THE FUSABLE LINK AT THE BATTERY CHARGER M1132 FAILING. REPLACEMENT OF FUSABLE LINK CORRECTED THE SITUATION.
Part: BULB — INOPERATIVE (LT OVERWING) · airframe 31,375 hrs · 17,926 cycles
LEFT OVERWING EMERGENCY LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SAME PER A.M.M. - OPS CKS GOOD
Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 31,100 hrs · 17,552 cycles
SEVERAL EMERGENCY LIGHTS INOP. REPAIRED WIRING, CHECKS NORMAL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 29,222 hrs · 15,222 cycles
EMERGENCY EVACUATION LIGHTING DIM IN CABIN AISLE BETWEEN ROWS 11 AND 24. REPLACED BATTERY FOR CABIN LIGHTING SYSTEM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 27,803 hrs · 13,835 cycles
A CRACK WAS FOUND IN THE LT SIDE CHORD OF THE FS 178 BLKHD. THE DAMAGE WAS REPAIRED PER S/B 737-53-1173 SECTION IX. THE CRACK WAS FOUND DURING THE AD INSPECTION AT HMV.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 26,816 hrs · 12,829 cycles
FIRST CLASS MEGAPHONE INOP ON LAYOVER CHECK IN STL. REPLACED SAME.
Part: SENSOR — FAILED (AFCS) · airframe 26,047 hrs · 12,056 cycles
B-SYSTEM A/P APPROACHING FL 350, RAPID ROLL LEFT, DISCONNECTED AT FL 350, RE-ENGAGED B A/P, SLOWLY ROLLED RT DISCONNECTED, ENGAGED A A/P. ALSO, UNCOMMANDED SLOW ROLL TO RT, DISCONNECTED, HAD FLEW REST OF FLT. REPLACED AILERON POSITION SENSOR AND MCP PANEL.
Part: RELAY — MALFUNCTIONED (E/E BAY)
TAKEOFF CONFIGURATION WARNING CAME ON DURING TAKEOFF ROLL WITH AIRCRAFT CONFIGURED CORRECTLY. REPLACED R2-238 AND R2-239 RELAYS. INSPECTED SWITCHES S-130, S-132, S-546 AND 1 & 4 LEADING EDGE SENSORS. REPLACED M983 PRECAUTIONARY.
Part: FITTING — CORRODED (BS 685)
FUSELAGE LT MLG SIDE STRUT SUPPORT FITTING FS 685, CORRODED LUG REPAIR. THE FS 685 LEFT MLG SIDE STRUT SUPPORT FITTING WAS FOUND WITH CORROSION IN THE LUG BORE. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLE. AN OVERSIZE BUSHING WAS INSTALLED PER ER/A 367246-14, REV A.
Part: BATTERY PACK — DISCHARGED (ROW 20)
EMER SEAT TRACK LIGHTING INOP AT ROWS 18 TO 24. FOUND BATTERY PACK BAD AT ROW 20. REPLACED SAME.
Part: BATTERY — DISCHARGED (CABIN)
OVERWING EXIT IDENTIFIERS ONLY ILLUMINATE FOR 15 SECONDS. REPLACED BATTERY PACK, CHECKS GOOD.