N221DL
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.
13 reports on file, 1999-10-25 – 2003-11-05.
Part: IRU — FAILED (NR 1) · airframe 41,197 hrs · 21,674 cycles
DIV DUE TO LOSS OF ALL HEADING INFORMATION. REPLACED NR 1 IRU.
Part: WIRE — SHORTED (OUTFLOW VALVE) · airframe 40,850 hrs · 21,191 cycles
UPON LANDING A ACRID ELECTRICAL ODOR NOTICED IN COCKPIT AND CABIN. REPAIRED SHORTED WIRE IN FWD CARGO COMPARTMENT AND REPLACED CABIN PRESSURE CONTROLLER
Part: COFFEEMAKER — SPARKS (FWD GALLEY) · airframe 40,701 hrs · 20,980 cycles
COFFEEMAKER HAS ELECTRICAL SPARKS. REPLACED DISPENSER.
Earlier reports · 1999–2002 · 10 reports
2002
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,385 hrs · 20,595 cycles
L1 WINDOW SHATTERED IN FLIGHT. REPLACED WINDSHIELD.
Part: WARNING LIGHT — FALSE INDICATION (COCKPIT) · airframe 39,591 hrs · 19,760 cycles
ON APPROACH TO LANDING HAD UNSAFE GEAR INDICATION. NO GREEN LIGHTS AND ONLY NOSE GEAR RED UNSAFE. JACKED AIRCRAFT AND CYCLED GEAR. UNABLE TO DUPLICATE.
2001
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 38,925 hrs · 19,125 cycles
AFT MEGAPHONE INOP. REPLACED AFT MEGAPHONE.
Part: LIGHT — DAMAGED (CABIN) · airframe 38,773 hrs · 18,976 cycles
LAV AFT RT EMERGENCY TRACK LIGHT DAMAGED , LIGHT ASSY REPLACED, CHK OK.
Part: A/C PACK — FAILED (A/C BAY) · airframe 38,424 hrs · 18,636 cycles
AFTER T/O, A/C WILL NOT PRESSURIZE WITH LEFT PACK IN AUTO AND RT PACK ON DEFERRAL. REPAIRED RT PACK. PRESSURIZED AIRCRAFT, OK FOR SERVICE.
Part: SKIN — CRACKED (R1 DOOR) · airframe 38,379 hrs · 18,594 cycles
DOOR SKIN CRACKED N/R 123 C-1 CK OPN 8727 IN DFW. ITEM:R-1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT AT AFT UPPER AND LOWER CORNERS. STOP DRILLED AND REMOVED CRACK AT UPPER AND LWR CORNERS PER SRM 52-00-01. PERFORMED HFEC PER NDT PART 6 CH 51-00-00, FIG 4. MADE UP DOUBLER PER SRM 52-00-01. OK TO INSTALL. INSTALLED REPAIR PER SRM 52-00-01.
Part: SKIN — CRACKED (R1 DOOR) · airframe 38,379 hrs · 18,594 cycles
DOOR SKIN CRACKED N/R 122 C-1 CK OPN 8727 IN DFW. ITEM: R-1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT AT LOWER AFT CORNER.
1999
Part: TRANSMITTER — MALFUNCTIONED (TE FLAP)
SPLIT FLAP INDICATION AT 1 DEGREE FLAPS DURING DESCENT. MADE 1 DEGREE FLAP LANDING. REPLACED LEFT FLAP POSITION TRANSMITTER. PERFORMED CHECK OUT PER M/M CHAP 27. FLAPS OPERATE NORMAL AND ALL INDICATIONS CHECK OK.
Part: SKIN — MISDRILLED (FUSELAGE)
IMPROPER FASTENER SPACING WAS FOUND AT THE VHF ANTENNA RESULTING IN A 2.0 INCH DIAMETER HOLE FOR DAMAGE REMOVAL. THE DAMAGE WAS REPAIRED PER ERA 333724-14 AT MV.
Part: BULKHEAD WEB — CRACKED (BS 178)
THE FS 178 BULKHEAD WEB WAS FOUND TO HAVE 3 CRACKS. TWO CRACKS WERE AT APPROXIMATELY LBL 4.7 AND WL 205, THE THIRD WAS AT RBL 4.7 AND WL 205. THE DAMAGE WAS REPAIRED BY ERA 333717-14 ATMV.