OpenAirDocs.org

N898PA

Open the Markdown

1997 Learjet 60 · Pratt & Whitney PW300 series

Open in FAA registry

© OpenStreetMap
Registered owner
Aviation Investment Group Inc
Location
Lewes, DE
Owner type
Corporation
Serial number
111
Year built
1997
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 11, 1997
Certificate issued
February 3, 2026
Expires
February 28, 2033
Mode S code
AC6452
Learjet 60Airframe model · 11 seats · 2 engines · 237 registeredTCDS A10CEAirframe · Learjet 60Engine modelPratt & Whitney PW300 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PW300 model are included below.

On this page

Airworthiness directives that may apply · 19

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1993In forceSuperseded2026
See all 23 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N898PAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Learjet 60 aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20140617010159ILanding: Rollout · Hailey, IDPIC had trouble deploying the thrust reversers during landing rollout. On second try, one thrust reverser deployed causing asymmetric thrust. Aircraft veered to the right with right main landing gear departing the runway. Right flap contacted runway light…Jun 17, 2014 · Minor damage

Service difficulty reports · 4

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR GQRA2019F00161Switch · failedIN LEVEL FLIGHT AT FL400 “L FUEL PRESS” AMBER ANNUNCIATOR ILLUMINATED. CREW INITIATED RELEVANT CHECKLIST. LEFT ENGINE ROLLBACK OCCURRED APPROXIMATELY 2 MIN AFTER ANNUNCIATION. AN INFLIGHT ENGINE RESTART WAS ATTEMPTED BUT UNSUCCESSFUL. IN THE PROCESS OF TROUBLEJan 1, 2019 · N898PA · Lear 60LEAR · Fuel Boost PumpSDR GQRA20140620001Thrust Reverser · malfunctionedON LANDING AFTER TOUCHDOWN PILOTS STATE THAT THRUST REVERSER LEVERS WERE PULLED BUT NEITHER THRUST REVERSER UNLOCKED. ON SECOND ATTEMPT PILOT STATES THAT RT REVERSER UNLOCKED & DEPLOYED PRIOR TO LT REVERSER UNLOCKING & DEPLOYING. ACFT YAWED TO THE RT & STRUCJun 17, 2014 · N898PA · Lear 60LEAR · Engine Thrust ReverserSDR GQRA2013F00000Wire · brokenACFT DEPARTED, AFTER SHORT VECTOR TO FINAL, CAPTAIN CALLED FOR GEAR DOWN AND NO INDICATION OF EXTENSION OCCURRED. CREW REQUESTED VECTOR TO SAFE AREA TO ASCERTAIN & DIAGNOSE PROBLEM. AFTER SERVERAL ATTEMPTS TO CYCLE GEAR, THE LOWERED GEAR USING " ALTERNATE Jun 26, 2013 · N898PA · Lear 60LEAR · Landing Gear System WiringSDR 2006FA0000361Flex Line · rupturedDURING FLIGHT, LOST NR 1 HYDRAULIC PRESSURE, DIVERTED INTO AIRPORT AND LANDED WITHOUT INCIDENT. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC FLEX LINE, PN 605700311 WHICH IS MOUNTED ON THE PRESSURE SIDE OF THE HYDRAULIC EDP. INSTALLED NEW HYDRAULIC FLEX LINE WIMar 10, 2006 · N898PA · Lear 60LEAR · Hydraulic System, Main

STCs that may be installed · 157

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 157 STCs