N171AA
Registered owner: CORSAIR TWO LLC, OR (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Aero Air LLC (O9IA) | Certificate holder | — | Matched by certificate designator |
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, 1995-11-12 – 2026-07-30.
Part: OIL SYSTEM — MALFUNCTIONED (ENGINE) · airframe 5,413 hrs · 5,414 cycles
RT ENG OIL PRESSURE DROPPED TO 0 ON APPROACH INTO HIO FROM PAE. PRESSURE JUMPED UP INTO GREEN & SPIKED INTO RED & STAYED THERE. ENG THEN SHUTDOWN INFLT ON APPROACH. PILOT DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. MAINT CHKD OIL LEVEL ON ENGS & BOTH WERE IN THE MIDDLE OF MIN/MAX BAR. IDLE RUN & POWER RUNS FOR 10 MINS CONDUCTED WITH NO ABNORMAL READINGS. AT THIS TIME ALL MAINT CHKS GOOD. MAINT INSPECTED INDICATION SYS WITH NO ISSUES NOTED. LAST MONTH THE RT ENG HAD OIL PRESSURE FLUCTUATIONS & REPLACED CONNECTOR TO OIL PRESSURE SENSOR AFTER WE FOUND THE RESISTANCE GOING TO OPEN. CONNECTOR CHECKED & NO ISSUES NOTED. IN 2024 THIS ENG HAD A LOW OIL PRESSURE ISSUE & NR 4 BEARING CARBON SEAL REPLACED. THERE HAVE BEEN NO ISSUES WITH OIL PRESSURE ON ENG BETWEEN THE 2024 WORK & REPLACEMENT OF CONNECTOR IN JUNE OF 2024. NO ISSUES WITH OIL PRESSURE SINCE THE JUNE 2024 CONNECTOR REPLACEMENT EITHER.
Earlier reports · 1995–1999 · 14 reports
1999
Part: TRU — FAILED (E/E BAY)
LAX - (ATB) APPROXIMATELY ONE HOUR AFTER TAKEOFF LAX, LOST DC BUS 1 AND L EMERGENCY DC BUS. RESET T/R 1 OUTPUT AND T/R 1 INPUT. OPS BACK TO NORMAL. NR 1 T/R. UNIT OPS CHECKED NORMAL. SYSTEM OK FOR SERVICE. (X)
Part: HOSE — FAILED (RT MLG)
SEA - FLT 21 - AIR RETURN - CAN'T RAISE GEAR AFTER TAKEOFF UNABLE TO RAISE GEAR HANDLE. THUS GEAR WOULD NOT COME UP. ATTEMPTED GEAR HANDLE RELEASE BUTTON. INSPECTED MAIN GEAR AND FOUND RIGHT MAIN TRIM CYLINDER SUPPLY HOSE RUPTURED AT AFT END OF RT MAIN TRUCK. REPLACED HOSE ASSY WITH REF TO MM TRIM CYLINDER REPLACEMENT, LEAK CHECK GOOD. SERVICED NR 3 HYD RES TO FULL. OK FOR SERVICE. (M)
Part: ENGINE — FAILED (NR 3)
GEN 3 OFF AND GEN FAIL LIGHTS BOTH ILLUMINATED AND NR 3 AC LOAD INDICATED ZERO. NR 3 CSD OIL PRESS LOW LIGHT ILLUMINATED CSD OIL OUTLET TEMP NORMAL AND RISE TEMP NORMAL FOLLOWED BY INCREASE IN OUTLET TEMP AFTER SEVERAL MINUTES. OUTLET TEMP REDUCED AFTER CSD DISCONNECT. CSD NR 3 DISCONNECTED AS PER FCOM. NR 3 ENGINE OIL PRESS IN YELLOW BAND JUST AFTER GEN OFF. 20 PSI PRECAUTIONARY SHUT DOWN ENGINE NR 3 AS PER THE FCOM. ENGINE NR 3 OIL QTY INDICATES ZERO AFTER GEN FAILURE. OIL PRESS 15 PSI AFTER SHUTDOWN. CHANGED ENGINE PER DR719401 CARD AND ACCOMPLISHED POWER ASSURANCE CHECK PER DR 71951 CARD. (M)
Part: ENGINE — FAILED (NR 1)
HNL - FLT 21 - (LOG PAGE NR 4821636). DURING CRUISE, NR 1 ENGINE EXHIBITED CHARACTERISTICS OF COMPRESSOR STALLS. (RAISING EGT, AUDIBLE RUMBLES, AND N2 DECREASING). COMPLETED APPROPRIATE CHECKLIST AND SHUT DOWN ENGINE. (X)
1998
Part: PA SYSTEM — MALFUNCTIONED (CABIN)
SEA - FLT 23 - STATIC INTERFERENCE HEARD FROM OVERHEAD SPEAKER/HEADSET AT WHICH TIME THE NR 1 F/D, NR 1 FMA, AND NR 1 GPS WENT BLANK. AFTER STATIC STOPS, F/D, GPS RETURN TO NORMAL, FMA STAYS BLANK. WHEN MODE TEST SWITCH IS DEPRESSED, FMA RETURNS TO NORMAL. OCCURRED 3 TIMES ON FINAL. UNABLE TO DUPLICATE STATIC ON NR 1 OVERHEAD SPEAKER/HEADSET. OPS CHECK OK ON GROUND. OK FOR SERVICE. (M)
Part: SUPPORT — CORRODED (CABIN)
TULE - (LOG PAGE NR 0116521). CORROSION ON RT FORWARD LAVATORY FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT FOR FORWARD LAVATORY PER AARD 51-00-00-05. (X)
Part: FLAP TRACK — CORRODED (WS 118)
TULE - (NR 116312) - INBOARD FLAP TRACK POST HAS CORROSION IN VARIOUS HOLES ON INBOARD FLAP ON RIGHT-HAND WING. STA 118 XORS. REAMED HOLES TO REMOVE CORROSION AND INSTALLED BUSHINGS PER AARD 57-20-00-10. (X)
Part: FIRE LOOP — MALFUNCTIONED (NR 1 ENGINE)
SFO - FLT 15 - (LOG PAGE NR 4620938) - NR 1 ENGINE FIRE DETECTION LOOP 'A' LIGHT ON AFTER TAKEOFF. WENT OUT AFTER CLIMB POWER. REPLACED NR 1 ENGINE CONTROL BOX. (X)
Part: CONTROLLER — FAILED (NR 3)
FLT 10 - LAX - DURING CRUISE NR 3 MANIFOLD FAIL LIGHT CAME ON TEMP ABOUT 190 DEGRESS PSI AT 10 AFTER SHUT OFF. REPLACED MANIFOLD FAIL DET CONTROLLER, THE PNEU MANIFOLD FAULT INDICATOR, NO FAULT NOTED, OPS CHECKED OK. ON ENG RUN. (M)
Part: THROTTLE — OUT OF ADJUST (NR 3 ENGINE)
SFO - FLT 12 - NR 3 THROTTLE STIFF WHEN RETARDED. RE-TORQUED CLUTCH SHAFT RETAINING NUT AND ADJUSTED NR 3 THROTTLE CLUTCH TENSION PUSH/PULL FORCE CHECKS OK AT 4 POUNDS. THROTTLE FORCE WITHIN LIMITS PER MM 76-11-00. (X)
Part: PRESS CONTROL — FAILED (NR 1 ENGINE)
HNL - FLT 03 - NR 1 ENGINE MANIFOLD FAIL (RED) LAMP ILLUMINATED AT TOP OF DESCENT WHEN THROTTLES WERE CLOSED TO IDLE. TEMP 210 DEGREES CELSIUS LIGHT EXTINGUISHED IN ABOUT 5 SECONDS AFTER NR 1 BLEED SWITCH TURNED OFF. (M)
1997
Part: RCCB — FAILED (E/E COMPT)
FLT 2 - HNL - ON FINAL TO LAX WITH 35 DEGREES FLAPS SELECTED AND GPWS SW OFF, STICK SHAKER ACTUATED APPROX 15-20 KNOTS ABOVE VREF. ON DESCENT, TURNED NAV LIGHT SWITCH ON AC BUSS TIE '1' ISOL LIGHT CAME ON AND LOST ALL ASSOCIATED INSTRUMENTS. AIRCRAFT DIVERTED TO 'ONT' WHERE AN UNEVENTFUL LANDING WAS MADE. (M)
Part: WIRE — LOOSE (CABIN)
FLT 2 - HNL - 'C' CABIN EMERGENCY FLOOR LIGHTS ON IN CRUISE. SECURED WIRES. (M)
1995
Part: HOSE — PUNCTURED (AFT LAVATORY)
HNL - FLT 22 - INFORMATION TAKEN FROM LOG PAGE 3657248 - REAR LAVATORIES, DENSE SMOKE, STEAM, AND ODOR. FOUND HOSE, PN 159445, PUNCTURED IN NR 3 AFT LAVATORY, REMOVED AND REPLACED HOSE. OPS CHECK, LEAK CHECK OK. (X)