# N701AL: 2014 Cessna 525C

- Status: Valid registration
- Airframe: [Cessna 525C](https://openairdocs.org/model/cessna-525c) (registry code 2076618, 11 seats)
- Engine: [Williams FJ44-4A](https://openairdocs.org/engine/williams-fj44-4a) (registry code 66011)
- Data sheets: [TCDS A1WI](https://openairdocs.org/tcds/A1WI) (Textron Aviation Inc.), [TCDS E3GL](https://openairdocs.org/tcds/E3GL) (Williams International Company L.L.C.) (OpenAirDocs)
- Serial number: 525C0169
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: December 12, 2014
- Certificate issued: July 27, 2022
- Expires: July 31, 2029
- Mode S code: A95850
- Registered owner: [Pnc Bank Na](https://openairdocs.org/faa-owner/PNC%20BANK%20NA)
- Location: [Boise, ID](https://openairdocs.org/faa-place/ID/Boise)
- Owner type: Corporation
- Owner's area on the map: 43.5914° N, 116.1942° W: Placed by OpenAirDocs at the center of ZIP code 83706, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=701AL
- Page: https://openairdocs.org/aircraft/N701AL

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 4 in force

### Matched by airframe (Cessna 525C)

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017
- [AD 2011-21-51](https://openairdocs.org/ad/2011-21-51): Battery/Charger · Cessna 525C. Effective Nov 1, 2011
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998

### Matched by engine (Williams FJ44-4A)

None in force.

## Information bulletins (advisory) (1 in force)

- [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011
- [SAIB CE-10-49](https://openairdocs.org/saib/CE-10-49) (historical): Equipment/Furnishings Drain Mast Heater. Issued Sep 23, 2010

## NTSB investigations

None matched to N701AL.

## FAA accident and incident reports

None matched to N701AL.

## Reports on N701AL not matched to an aircraft (3)

They name N701AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20000326018709I](https://openairdocs.org/incident/20000326018709I), Mar 26, 2000: Skrsky S76 (N701AL), Patterson, LA, Minor damage. (-23)On March 26, 2000, a Sikorsky, model S-76-A, experienced an engine cowl fire seven (7) to eight (8) minutes after engine start up. The investigation…
- [Incident 19941207046659I](https://openairdocs.org/incident/19941207046659I), Dec 7, 1994: Skrsky S76 (N701AL), Venice, LA, Minor damage. During hover taxi. Engine lost power. Dropped to ground. Collapsed left gear. Pilot held craft level to unload.
- [Incident 19900417025189I](https://openairdocs.org/incident/19900417025189I), Apr 17, 1990: Skrsky S76 (N701AL), New Iberia, LA, Minor damage. Main rotor blades hit tail of parked helicopter while taxiing to refueling area.

## Service difficulty reports (1)

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

- [SDR WI5R201906270001](https://openairdocs.org/sdr/WI5R201906270001), Jun 27, 2019: BLADE. MISSING. DURING TROUBLE SHOOTING FOR A REPORTED "WHINE" NOISE WHEN N1 IS ABOVE 71%, A FIELD BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMB

## Service difficulty reports on N701AL not matched to an aircraft (9)

They name N701AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ALG2005F00039](https://openairdocs.org/sdr/ALG2005F00039), Jul 16, 2005: CONNECTOR. FAULTY. ON PRE START, NR 1 ENGINE FIRE TEE HANDLE LIGHTS WOULD NOT TEST IN FORWARD POSITION. THE MECHANIC REMOVED AND REPLACED THE FAULTY CONNECTOR AND THE AIRCRAFT WAS
- [SDR ALG2001F00008](https://openairdocs.org/sdr/ALG2001F00008), Jun 18, 2001: PROXIMITY SWITCH. OUT OF ADJ. DURING TAKEOFF RT MAIN GEAR RETRACT UNSAFE LIGHTS. ADJUSTED UPLOCK PROXIMITY SWITCH ON RT MAIN GEAR, PERFORMED RETRACTION TEST. NO DEFECTS NOTED.
- [SDR 98ZZZX3597](https://openairdocs.org/sdr/98ZZZX3597), Sep 10, 1998: SWITCH. LOOSE. INADVERTANT FLOAT INFLATION DURING FINAL APPROACH TO OFFSHORE PLATFORM. FOUND COPILOT CYCLIC GRIP CRACKED AROUND FLOAT INFLATION SWITCH. SWITCH WAS LOOSE IN GRI
- [SDR 97ZZZX927](https://openairdocs.org/sdr/97ZZZX927), Jan 15, 1997: FILTER CAP. FAILED. SHORTLY AFTER TAKEOFF FROM AN OFFSHORE PLATFORM IN THE GULF OF MEXICO, THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND THE NR 1 ENGINE OIL PRESSURE BEGAN TO 
- [SDR 96ZZZX1824](https://openairdocs.org/sdr/96ZZZX1824), Mar 2, 1996: SCAVENGE BODY. WORN. UPON DISASSEMBLY OF GEARBOX, REMOVED OIL PUMP ASSY. VISUALLY INSPECTED, SHOWED WEAR AT SCAVENGE BODY SURFACE, AND IN THE TUBE BONE. SCAVENGE TUBE WORN IN SCAVEN
- [SDR 96ZZZX746](https://openairdocs.org/sdr/96ZZZX746), Jan 4, 1996: FUEL CONTROL. WATER CONTAM. DURING FLIGHT CHECK/HOVER, COMPRESSOR STALLED. REMOVED FROM ENGINE, INSPECTED PX-AIR CIRCUIT ON FUEL CONTROL, FOUND EXCESSIVE AMOUNT OF WATER.
- [SDR 95ZZZX2803](https://openairdocs.org/sdr/95ZZZX2803), May 11, 1995: OUTER HOUSING. CORRODED. DISASSEMBLY FOR OVERHAUL FOUND EXCESSIVE CORROSION ON MOUNT LUGS BEYOND MAXIMUM ALLOWABLE CLEAN-UP LIMITS.
- [SDR 95ZZZX2802](https://openairdocs.org/sdr/95ZZZX2802), May 11, 1995: TUBE ASSY. DEBONDED. DISASSEMBLY FOR OVERHAUL FOUND T/R DRIVE TUBE DEBONDED BEYOND MANUFACTURER'S MAXIMUM ALLOWABLE LIMITS.
- [SDR 95ZZZX2804](https://openairdocs.org/sdr/95ZZZX2804), May 2, 1995: COMBUSTION CASE. CRACKED. THIS DEFECT WAS DISCOVERED AT 1750-HOUR OVERHAUL. OUTER COMBUSTION CASE WAS CRACKED IN ARMPIT UNDER THE SCREEN PATCH REINFORCEMENT AND EXTENDED ON SEAM AND INTO

## STCs that may be installed (OpenAirDocs) (37)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cessna 525C)

- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12030NY](https://openairdocs.org/stc/SA12030NY): Installation of the position/anti-collision LED lights and LED beacon light. Whelen Aerospace Technologies
- [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC
- [STC SA12014LA](https://openairdocs.org/stc/SA12014LA): Installation of aluminum and fiberglass wheel covers. Premiere-Aviation Inc
- [STC SA04619CH](https://openairdocs.org/stc/SA04619CH): INSTALL SMARTSKY LITE SYSTEM. Apcela IFC JV, LLC dba Apcela ATG
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA01848WI](https://openairdocs.org/stc/SA01848WI): Modification of a Rockwell Collins Global Positioning System (GPS). Rockwell Collins Inc
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00120IB](https://openairdocs.org/stc/SA00120IB): Installation of the Universal Kapture Cockpit Voice Recorder (CVR) with Recorder Independent Power Supply (RIPS). Avmax Aviation Services Inc
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA11299DS](https://openairdocs.org/stc/SA11299DS): An update to the exisiting Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 23 aircraf. BHE & Associates LTD
- [STC SA01990WI](https://openairdocs.org/stc/SA01990WI): Installation of Gogo Biz AVANCE L5 4G ATG System. Textron Aviation Inc
- [STC SA02272SE](https://openairdocs.org/stc/SA02272SE): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Corporation
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA04525NY](https://openairdocs.org/stc/SA04525NY): Installation of dual GPS/NAV/COMM Garmin GNS430/530(A)W. Avionik Straubing GmbH
- [STC SA04520NY](https://openairdocs.org/stc/SA04520NY): ADS-B Out GNSS source modification for transponder #2. CESSNA Duesseldorf Citation Service
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01903CH](https://openairdocs.org/stc/SA01903CH): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc
- [STC SA03241CH](https://openairdocs.org/stc/SA03241CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SA01872WI](https://openairdocs.org/stc/SA01872WI): Installation of Honeywell UHF Provisions and Rockwell Collins TCN-500 TACAN System. Duncan Aviation Inc
- [STC SA01684WI](https://openairdocs.org/stc/SA01684WI): Installation of Rockwell Collins, Inc. Aircraft Information Management (AIM) System. Rockwell Collins Inc
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA01775WI](https://openairdocs.org/stc/SA01775WI): Installation of Norwegian Special Mission UNIFIS 3000 Flight Inspection System. Duncan Aviation Inc
- [STC SA03934NY](https://openairdocs.org/stc/SA03934NY): Installation of Garmin GTN 725. CESSNA Duesseldorf Citation Service
- [STC SA00797DE](https://openairdocs.org/stc/SA00797DE): Installation of Teledyne Battery Products P/N 7638-44T Lead-Acid Battery. Teledyne Battery Products
- [STC SA01430WI-D](https://openairdocs.org/stc/SA01430WI-D): Modification of a Rockwell Collins, Inc. Data Base Unit (DBU). Rockwell Collins Inc
- [STC SA01434WI-D](https://openairdocs.org/stc/SA01434WI-D): Modification of a Rockwell Collins, Inc. Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC SA01676WI](https://openairdocs.org/stc/SA01676WI): Modification of a Rockwell Collins, Inc. File Server Unit (FSU). Rockwell Collins Inc
- [STC SA01636WI-D](https://openairdocs.org/stc/SA01636WI-D): Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations. Rockwell Collins Inc

## Related

- Other Cessna 525C aircraft: https://openairdocs.org/model/cessna-525c/aircraft.md
- The Williams FJ44-4A engine: https://openairdocs.org/engine/williams-fj44-4a.md

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