N231DN
Registered owner: HENRYS INVESTMENTS LLC, CA (owner ≠ operator)
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.
11 reports on file, 1998-04-16 – 2006-06-19.
Part: SKIN — DENTED (BS 887-907) · airframe 44,808 hrs · 24,564 cycles
DURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, INSPECTION NOTED DENTS BEYOND ALLOWABLE LIMITS IN FUSELAGE SKIN FROM BS887 TO BS907 BETWEEN STR20RT AND STR22RT. REPAIRED IAW SRM 53-00-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 44,808 hrs · 24,564 cycles
DURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, INSPECTION NOTED A DENT IN THE FUSELAGE SKIN BEYOND ALLOWABLE LIMITS AT BS 887 STR 22 LT. REPAIRED PER SRM 53-00-01.
Part: SKIN — DAMAGED (HORIZ STAB) · airframe 44,808 hrs · 24,564 cycles
DURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, DAMAGE NOTED ON THE RIGHT HORIZONTAL STABILIZER APPROXIMATELY 8 FEET FROM THE INBOARD END. REPAIRED PER SRM 55-10-01.
Part: PROBE — OVERHEATED (PITOT SYSTEM) · airframe 44,605 hrs · 24,299 cycles
ATB DUE TO FO PITOT TUBE OVERHEATING AND CAUSING INSULATION IN COCKPIT SIDEWALL TO SMOLDER. REPLACED PROBE.
Part: BRAKE — DAMAGED (NR 4) · airframe 44,424 hrs · 24,039 cycles
ON TRANSIT CHECK, FOUND METAL SHARDS UNDERNEATH NR 4 BRAKE ASSY, SHARDS ARE FROM OUTER DISK. REPLACED NBR 4 MAIN BRAKE ASSY PER MM.
Part: SKIN — DAMAGED · airframe 41,438 hrs · 19,901 cycles
RT FUSELAGE SKIN / STA 312-360 / S14-S19. DAMAGED REPLACEMENT SKIN SECTION FABRICATED IAW ER/A 423343-14.
Part: SKIN — DEBONDED (LT WING LE FLAP) · airframe 41,438 hrs · 19,901 cycles
LT WING OUTBOARD FORE FLAP DISBONDED. TE WEDGE REBUILT IAW ER/A 423088-14.
Part: LIGHT — DAMAGED (SEAT 2) · airframe 39,354 hrs · 17,799 cycles
PASSENGER SEAT 02B EMERGENCY LIGHTING FLOOR LIGHT DAMAGED. REPLACED LIGHT ASSY, OPS NORMAL.
Part: MODULE — FAULTY (NR 2 ENGINE) · airframe 38,997 hrs · 17,463 cycles
UPON STARTING NR 2 ENG, GOT MASTER FIRE WARNING LIGHT AND HORN. NO TEE HANDLES ILLUMINATED. SHUT DOWN NR 2 ENG APU EGT WAS NORMAL. ALL TEST OK. RAN ENG, UNABLE TO DUPLICATE PROBLEM. REPLACED FIRE WARNING CONTROL MODULE AS PRECAUTIONARY. ALL TEST OK.
Part: LIGHT — INOPERATIVE (ROW 21D)
EMERGENCY EXIT BULLNOSE LIGHT AT 21D INOP. RELAMPED, OPS CKS NORMAL.
Part: SKIN — DENTED (BS 227)
TWO DENTS EXIST IN THE FUSE SKIN AT APPROX BS227 BETWEEN S17R AND S19R. PRIOR TO ENTERING REVENUE SERVICE; REPAIR PER ERA 331623-14.