N927HA
Registered owner: INDY HOT AIR LLC, IN (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.
18 reports on file, 1995-01-20 – 2002-11-21.
Part: WINDSHIELD — CRACKED · airframe 37,486 hrs · 42,158 cycles
L/H Forward Sindshield shattered in flight at 16,000 FT. A/C diverted to GSP the windshield fram was inspected and the windscreen replaced.
Part: WINDSHIELD — CRACKED · airframe 37,467 hrs · 42,147 cycles
After Take-off F/O's windshield cracked. A/C returned to DCA where windshield was replaced.
Part: CABLE — BROKEN (L/H WING ROOT) · airframe 35,550 hrs · 40,110 cycles
During aircraft taxi from terminal to hanger by maintenance, there was a loss of right brake control. Subsequent inspection found broken cable at #1 brake valve.
Part: FRAME — CORRODED (FUSELAGE) · airframe 35,439 hrs · 39,991 cycles
AT LEFT HAND EMERGENCY EXIT CORROSION FOUND ON FRAME AT STATION X366 AFT SIDE BELOW EMERGENCY EXIT. FRAME THICKNESS IS .040. DEPTH OF CORROSION AT EDGE OF FRAME IS .012. REPAIRED FRAME AREA IAW EO8-53-02-0141. BLEND OUT CORROSION, FABRICATED A REPAIR STRAP AND INSTALLED INSIDE OF FRAME INNER CHORD.
Part: SKIN PANEL — CORRODED (BOTTOM FUSELAGE) · airframe 35,439 hrs · 39,991 cycles
Skin corroded and cracked at station x182 and stringer 33. Replaced skin panel.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,439 hrs · 39,991 cycles
RT INBOARD SEAT RAIL CORRODED BETWEEN STATION X182 TO X222. REMOVED AND REPLACED SEAT RAIL IN ACCORDANCE WITH RD8-53-3074.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 35,439 hrs · 39,991 cycles
FOUND CORROSION ON GUSSET AT STATION X354 STRINGER 21 RT. MFG NEW GUSSET AND INSTALLED.
Earlier reports · 1995–2001 · 11 reports
2001
Part: ENGINE — DEFECTIVE (NR 2 ENGINE) · airframe 33,830 hrs · 38,230 cycles
SMOKE IN CABIN AND FLIGHT COMPARTMENT, SMELLED LIKE HOT DUCT. DECLARED EMERGENCY AND DIVERTED TO BUFFALO. AIRCRAFT FERRIED TO SBY. FOUND OIL IN HEAT EXCHANGER AND AIR CYCLE MACHINE DUCTING. REMOVED AND REPLACED ACM AND HEAT EXCHANGER. ON 15 APRIL PROBLEM RECURRED. ON GROUND RUN WHEN NR 2 ENGINE BLEEDS FLOW AT MAX AND MANUALLY SELECTING TEMP TO WARM, AIRCRAFT FILLED UP WITH OIL MIST. NR 2 ENGIND REMOVED AND REPLACED.
Part: BALLAST — OVERHEATED (CABIN) · airframe 33,817 hrs · 38,216 cycles
F/A NOTICED SMOKE AND ELECTRICAL SMELL IN CABIN. FOUND CENTER OVERHEAD LIGHT AT ROW 8 DIM AND BALLAST EXTREMELY HOT TO THE TOUCH. REPLACED THE LUMINAIRE/BALLAST ASSY.
1999
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)
BAGGAGE SMOKE WARNING LIGHT ILLUMINATED INFLIGHT AND EXTINGISHED ON LANDING. COULD NOT DUPLICATE PROBLEM ON GROUND. REMOVED AND REPLACED NUMBER 1 SMOKE DETECTOR, OPS CHECK GOOD.
Part: RETRACT MECH — MALFUNCTIONED (LDG GEAR DOORS)
LANDING GEAR DOORS WOULD NOT CLOSE UNTIL NOSE GEAR TOUCHED DOWN ON LANDING. REPLACED 3261-K9 (P/N DSC182-2) RELAY.
1998
Part: SKIN — CORRODED (BS 167-182)
UNDER COCKPIT FLOOR MINOR SURFACE CORROSION TO THE SKIN ADJACENT TO STRINGER 31 RT, .020 DEPTH CORROSION TO THE SKIN APPROXIMATELY 3 INCHES LONG AT STRINGER 32 RT. STRINGER 31 RT BETWEEN STATION 167.00 AND STATION 182.00 CORRODED APPROXIMATELY 11 INCHES EXCEEDING 50 PERCENT LOSS OF MATERIAL IN SOME AREAS AND STRINGER 32 RT BETWEEN STATION 167.00 AND 182.00 CORRODED APPROXIMATELY 3 INCHES LONG, .5 INCHES WIDE AND .025-.030 INCHES DEPTH. REPAIRED, TREATED AND PAINTED AS REQUIRED.
Part: STRINGER — CORRODED (FUSELAGE)
JAX - CORROSION WAS REPAIRED ON STRINGER 32 RT IAW EO8-53-98-385. (M)
Part: STRINGER — CORRODED (BS 167-182)
JAX - FOUND CORROSION ON STRINGER 31 RT BETWEEN STATION 167 AND 182 WITH A LOSS OF 50 PERCENT OF MATERIAL. REPAIRED IAW RD8-53-1243. (M)
1995
Part: EEL BATT PACKS — FAILED (CABIN)
PHN/BWI - FLT 3260 - DURING PRE-FLIGHT WALK-AROUND, FOUND NUMEROUS INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY PACKS AT LOCATIONS PS6 AND PS3.
Part: AUTO FEATHER LTS — MALFUNCTIONED (COCKPITS)
FLT 3068 - PHL-LYH - AIRCRAFT RETURNED TO THE GATE WHEN THE AUTO FEATHER LIGHTS WOULD NOT ILLUMINATE DURING STATIC TEST WHILE ENGINES WERE RUNNING, BUT THE PROPELLERS WERE FEATHERING. REMOVED AND REPLACED THE DC REMOTE CONTROL CIRCUIT BREAKER, NO FIX. PULLED CIRCUIT BREAKER FOR AUTO FEATHER PUMP INDICATION AND RESET.
Part: PROP — OUT OF BALANCE (NR 1)
FLT 72 - ORF-PHF - AIRCRAFT HAS VIBRATION ABOVE 180 KNOTS. AIRCRAFT TURNED BACK TO ORF AND LANDED WITHOUT INCIDENT. PERFORMED PROP BALANCE AND ADJUSTED PROP BALANCE WEIGHTS ON NR 1 PROP.
Part: OIL — REQ'D SERVICE (NR 2 ENG)
FLT 3264 - EWN-CLT - NR 2 ENGINE OIL PRESSURE CAUTION LIGHT AND ENGINE OIL PRESSURE GAUGE ILLUMINATED AFTER TAKEOFF. AIRCRAFT TURNED BACK AND LANDED IN EWN WITHOUT INCIDENT. CHECKED NR 2 ENGINE FOR OIL LEAKS, NO LEAKS FOUND. SERVICED WITH 2 QUARTS OF OIL. OPERATIONAL CHECK GOOD. (Z)