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500/525 Series Breakout Session

Cessna Citation CJ2+ · Service Bulletins

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Overview

This document is a service bulletin for the Cessna 500 and 525 series aircraft, including the Citation CJ2 and CJ2+. It provides important updates, technical support information, and maintenance recommendations for operators and maintenance personnel. The bulletin covers various topics such as troubleshooting procedures, maintenance practices, and safety advisories relevant to the aircraft models mentioned. It aims to enhance operational safety and efficiency by informing users of best practices and necessary actions to maintain the aircraft in optimal condition.

  • The 525A (CJ2/CJ2+) fleet size is 468 with a total flight time of 1,239,219 hours.
  • Speed brake actuator screws should be replaced and sealed to prevent hydraulic fluid loss.
  • Avoid starting the engine in tailwinds or crosswinds exceeding AFM limitations to prevent damage.
  • Perform water rinse procedures after flights in marine environments to protect engines.
  • Corrosion severity maps are provided to guide maintenance based on environmental factors.

Document

Source

Originally published by ncjp2023test.s3.us-east-2.amazonaws.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Service Bulletins
Year
2018
Pages
73
File size
4.3 MB
Publisher
ncjp2023test.s3.us-east-2.amazonaws.com
How rare is it?
97Cessna Citation CJ2+ registered worldwide · 0 active

Common. Rarer than 1% of the aircraft models we track.

Documentation completeness
4/7

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In this document

Fleet Statistics

The document provides fleet statistics for the 525 series, indicating a fleet size of 468 for the 525A (CJ2/CJ2+) with a total flight time of 1,239,219 hours. This information is crucial for operators to understand the operational context of their aircraft.

Speed Brake Actuator Screw Replacement

There have been reports of speed brake actuator screws breaking, which may lead to loss of hydraulic fluid. The bulletin recommends replacing and sealing these screws as per the optional service documents released in May 2018.

Tail/Cross Wind Start Limitation

All models are cautioned against starting the engine with a tailwind or crosswind greater than the limitations specified in the Aircraft Flight Manual (AFM) to prevent potential damage to the aircraft.

Engine Water Rinse

Operators are advised to perform a water rinse procedure at the end of flight operations if operating in a marine atmosphere or within 5 miles of saltwater, especially if continuous operation in such environments occurs.

Corrosion Severity

The bulletin includes corrosion severity maps that classify areas based on potential corrosion risks, emphasizing the need for operators to be aware of their operating environments and take preventive measures.

Safety notes

  • Tailwind and crosswind limitations must be adhered to during engine starts to prevent damage.
  • Corrosion risks increase in areas using deicing fluids; operators should be vigilant.

Full document text

500/525 Series Breakout Session 2018 Citation Jet Pilots Convention Textron Aviation Leadership Ron Draper President and CEO 2 North America Aftermarket Leadership Kriya Shortt SR VP Customer Service April Gerber VP Parts & Programs Scott Howell Director Field Service Tracy Leopold Director Aftermarket Sales Roxanne Howell VP North American Service Centers Chris Hearne VP Product Support Previn Kulkarni Director Engineering 3 Phil Murphey Director Aftermarket Sales Textron Aviation Service Directory App & Online Access 4 • Service Directory App – Support Contacts – Service Centers – Flight Assurance – Diagnostics – More Features In Development • Free Download Available – Android: Google Playstore – Apple: App Store • Textron Aviation Service Directory Online • https://support.cessna.com/docs/custsu pt/onlineDirectory Textron Aviation Breakout Support 5 Chris Provencio Service Center Cybill Zimmer TAPD & Programs Product Support Management Jessica Busse Manager Light and Legacy Jet jbusse@txtav.com Desk: +1 (316) 517-5458 Cell: +1 (620) 313-0113 Team Legacy teamlegacy@txtav.com +1 (316) 517-7786 Team 525 team525@txtav.com +1 (316) 517-7785 Team Mustang teammustang@txtav.com +1(316) 517-5490 Team Beechjet Beechjet400xp@txtav.com +1(316) 517-9350 Team Premier Premier@txtav.com +1(316) 517-9350 Light and Legacy Jet Product Support Manager 6 Team Legacy 7 Sam Kofoot Phil Ciholas Walt Glosson Connor Brem Toll Free +1(855) 832-6919 Intl +1 (316) 517-7786 teamlegacy@txtav.com 8 Product Support Alignment Team 525 Team 525 Team CJ Joins Forces with Team M2 ✓ Align CJ fleets & Citation M2 with the experts ✓ Robust level of technical service ✓ Response within 24 hours of contact Team 525 9 Jeff Bowen Blake Barnard Cameron Teel Adam Balvanz Toll Free +1(855) 832-9831 Intl +1 (316) 517-7785 team525@txtav.com Mike Bryant Technical Support: Team Twilight European Support (United States Off Shift) Carl Fischer Friday – Sunday 7 PM – 7 AM CST John Moody Friday – Sunday 7 AM – 7 PM CST Jake Weiss Monday - Friday 2 PM – 10 PM CST Don Sweet Monday - Thursday 10 PM – 7 AM CST Hank Weyland Monday - Thursday 2 PM – Midnight CST 10 Michael Holler Friday – Sunday 7 AM – 7 PM CST Fleet Statistics 500 Series Fleet Maturity • 500/501 • Produced: 1972 – 1985 • Age: 33 – 46 Years • 550/551 • Model 550 • Produced: 1978 – 1984 • Age: 34 – 40 Years • 550 Classic • Produced: 1987 – 1994 • Age: 24 – 31 Years • Bravo • Produced: 1997 – 2006 • Age: 12 – 21 Years • S550 • Produced: 1984 – 1988 • Age: 30 – 34 Years • 560 • CV • Produced: 1989 – 1994 • Age: 24 – 29 Years • Ultra • Produced: 1994 – 2000 • Age: 18 – 24 Years • Encore/Encore+ • Produced: 2000 – 2010 • Age: 8 – 18 Years 525 Fleet Statistics • 525 (CJ/CJ1/CJ1+) • Fleet Size: 659 • Fleet Total Time: 1,989,014 • 525A (CJ2/CJ2+) • Fleet Size: 468 • Fleet Total Time: 1,239,219 Team Powerplants Team Powerplant +1 (316) 517-6232 teampowerplants@txtav.com Phil Pankratz Rollin Rising 14 Team Powerplants Light and Legacy Jet Models • Team Powerplants are here to assist! • Contact Textron Aviation Team Powerplants for any operational questions • Team Powerplants has direct support contacts at Williams, Honeywell, and Pratt & Whitney • Team Powerplants provides guidance to technicians • Free Service – 24 hours a day 15 Troubleshooting ECS Annunciations Williams Engines • Issue: Troubleshooting Engine Control System Faults Require Tooling • Status: FADEC EMT Kit Available P/N TL-221207 • Fits All FADEC Controlled FJ44-Series Engines • Includes EMT Communication Cable and Quatech Serial Port Adapter • EMT Basic Computer Software Available on Williams International Website for Free Tail/Cross Wind Start Limitation All Models • Issue • Tailpipe fire when attempting engine starts with tailwind or crosswind greater than AFM limitation • Can cause damage to pylon and tailcone skin • Status • Adhere to tailwind/crosswind limitations listed in AFM • Textron Aviation added notes to AFM cautioning operators of dangers when starting beyond limits 17 Engine Water Rinse • Marine atmosphere • Operation over salt water or within 5 miles (8 kilometers) of a body of salt water • Affected by weather patterns and winds • Recommended to perform a water rinse procedure at the end of flight operations each day if: • Continuous operation in a salt or smog laden environment • Frequency may be optimized based on operators experience • Recommended to perform a water rinse procedure at the end of each week if: • Occasional operation in a salt or smog laden environment • Adjust washing frequency to suit engine condition Technical Updates Battery Start versus GPU Start All Models • Battery Starts • No issues when using a healthy battery • Degraded battery can result in slow engine spool up time and increased ITT during engine start • Observe AFM battery voltage limits for engine start • GPU Starts • Reduced engine spool up time and lower ITT during engine start • Eliminate battery discharge/recharge cycle • Increased battery service life • Observe GPU requirements in AFM 20 Ground Power Unit Procedures All Models • Textron Aviation GPU procedures • Connect Main Ship Battery • Turn on GPU and Allow Voltage to Stabilize • Connect Energized Cord to Airplane • Disconnect Energized GPU from Airplane • Turn off the GPU • Not adapted as common practice • Training is different, FBO’s may not practice this method • Testing documented aircraft spikes occur when deenergized GPU plugged into aircraft induces voltage spikes on aircraft • Overvoltage and current protection incorporated in design may not react fast enough • Circuit boards and sensitive hardware damaged from GPU’s • Spikes May Occur if GPU is Connected with Main Ship Battery Disconnected from Aircraft Ground Power Unit Procedures All Models • Did you know? • Small Pin in External Power Receptacle Allows GPU Main Contacts to Engage Before Aircraft External Power Relay Energizes

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• Prevents GPU Main Contacts from Arcing During Insertion and Removal Toilet Fluid Spill Prevention All Models • Toilet Fluid Spills Primary Cause is Improper Maintenance • Toilet fluid is corrosive and extreme caution must exercised to prevent spills • Refer to the Maintenance Manual Chapter 12 Servicing • Follow the maintenance manual procedures for proper removal/installation and servicing of the flush-type toilet • Use only approved materials listed in Chapter 12 23 Toilet Fluid Spill Prevention All Models • Visually inspect toilet area for evidence of leakage during removal/installation. • Supply hoses and coupling • Servicing cap • Tank condition • Pump • Tank to bowl connection • Knife valve 24 Toilet Fluid Spill Prevention All Models • Fluid Spills • Clean up should be done as quickly as possible • Aircraft should not be dispatched until spill is properly cleaned • Web article “Team Structures Addresses Toilet Spills” published on TxtAvSupport.com website November 23, 2010 • YouTube video “Toilet Spill (Blue Water) Cleaning Procedures” viewable on Cessna YouTube Channel https://www.youtube.com/watch?v=Xn7304qocqE • Key Points • Verify toilet tank is serviced with correct amount of fluid • Verify toilet tank is correctly installed and secured • Verify pump supply line coupling is properly connected to the tank • Verify knife valve is fully open before toilet use and fully closed before toilet removal 25 Corrosion Severity All Models • Corrosion Severity Maps • Citation Standard Practices Manual (Rev 1) 51-10-10 (Original Issue) • Maps define areas of potential corrosion for mild, moderate or severe • Corrosion severity zones are affected by atmospheric factors. • Maps in this section are for guidance for frequency • CAUTION: • Airports that use deicing fluids such as potassium formate must be classified as severe corrosion • CAUTION: • Aircraft operating in any severe corrosion areas are classified as operating in a severe zone 26 Corrosion Map North America 27 Corrosion Map South America 28 Corrosion Map Africa 29 Corrosion Map Asia 30 Corrosion Map Europe & Asia Minor 31 Corrosion Map South Pacific 32 Tire Pressure Maintenance All Models • Maintain Proper Tire Pressure • Single Most Important Action to Prevent Tire-Related Events • Check Tire Pressure Before First Flight of the Day • Measure Tire Pressure When Wheel, Tire and Brakes are Cool • Use Accurate Gauge When Checking Tire Pressure • Incorrect Tire Pressure can Result in Abnormal Wear • Under Inflation • Accelerates Tread Shoulder Wear • Elevates Operating Temperature • Increased Risk of Shoulder and Sidewall Damage • Over Inflation • Accelerates Center Tread Wear • Reduces Traction • More Susceptible to Cutting Tire Pressure Maintenance All Models • Basic Aircraft Tire Pressure Gauge • TRONAIR 0-300 PSI Tire Pressure Gauge P/N 14-6806-6011 • Available from Textron Aviation Parts Distribution 34 Tire Pressure Maintenance All Models • High Tech Tire Pressure Measurement • Crane SmartStem Wireless Tire Pressure Measurement System STC: • P/N KIT83-022001-01 (3-Wheel) • STC is approved on majority of Citation Models • Available at Textron Aviation Service Centers 35 Correct Nose Tire Importance All Models • Install only approved nose and main tires listed in the IPC • Approved nose tire(s) also listed in limitations section of AFM • Correct nose tire is critical to performance of tire on wet runways • Nose tire has specially shaped chine on sidewall of tire • Chine serves to deflect water away from engine intakes • Incorrect tire can result in water ingestion 36 Pitot Probe Covers All Models • Issue: FOD May Buildup in Pitot Probes • Status: Use Plastic or Nonfraying Covers Only • Covers That Fray May Introduce FOD Into Pitot System • Pitot Probe Covers Offered • WP81338-4 • WP102406-1 • CJMD110-001 Wing Tip Deformation 525/525A/525B • Issue • Reports of deformed wing tips, not impact related 38 Wing Tip Deformation 525/525A/525B • Status • Currently being investigated • Deformation is not considered safety of flight • Analysis determined thinning of material • Confirmed proper material is being used • No root cause determined • Asking for field feedback: • Is it both sides? • Does it occur from one flight or is it a progression? • Buffing intervals (M.M. Chapter 20)? • Buffing materials? • History of any issues of anti-ice? • Contact Team Structures: csstructuresemea@txtav.com • Chapter 20 Standard Practices provides instructions, however no limitations on frequency of polishing/buffing 39 Radiant Power Emergency Standby Battery All Models • Issue • Standby battery discharge below 20 volts causing internal failure • Status • CBS28 is obsolete and has been replaced by CBS28-1 • CBS28-1 contains internal voltage monitor that prevents discharging to less than 20 volts • CBS28-1EX exchange units in stock • Replace upon attrition 40 Underwater Locator Beacon (ULB) All Models • Issue: 30-day ULB are no longer manufactured • Upgrade to 90-day ULB required when 30-day ULB reaches end of life and supplies are exhausted • Some regulatory authorities have imposed deadline to replace 30-day ULB regardless of remaining life • Status: Informational Service Letter CIL-31-01 released February 2018 • Covers Textron Aviation Engineered CVR, FDR & CVDR 90-Day Battery ULB Installation • Service letter directs operators to refer to manufacturer’s data for battery installation 41 Pressurization Systems 500/550/S550/560 • Original 500-Series aircraft use Garrett/AiResearch Systems • Controller operates outflow valve through pneumatic signals • Components connected thru plastic tubing 42 Pressurization Systems CJ/CJ1/CJ2/Bravo/Encore/Encore+ • 525-Series and later 500-Series use Kollsman system (KAPS 1) • Controller operates outflow valve with electrical signals • Components connected thru electrical wiring 43 Pressurization Systems Garrett/AiResearch vs. Kollsman • Garrett/AiResearch and Kollsman systems have different pressurization profiles 44 Aircraft Altitude Cabin Altitude Takeoff Takeoff FL200 Garrett/AiResearch System Kollsman System Pressurization Systems 500/550/S550/560 • Troubleshooting Garrett/AiResearch System • Leaks in pneumatic plumbing are a frequent cause of operational issues • Start troubleshooting by completing leak checks per maintenance manual Chapter 21 pressurization control – adjustment/test • Vacuum and pneumatic relay to outflow valve pneumatic connection leak test • Controller to pneumatic relay connection leakage test 45 Pressurization Systems CJ/CJ1/CJ2/Bravo/Encore/Encore+ • Troubleshooting Kollsman (KAPS1) System • Start troubleshooting by performing the “Cabin Pressurization Controller Built-In Tests” in Chapter 21-3X-00 Cabin Pressure Control – Maintenance Practices • Preflight EXER Mode Test • Ground Maintenance Test 46 Kollsman KAPS1 Pressurization System CJ/CJ1/CJ2/Bravo/Encore/Encore+ • Issue: Pressurization system oscillations noted after controller replacement • Issue observed when operating from airports near sea level • Status: Enviro Systems Inc. determined root cause to be pressurization controller internal pressure sensor • Original sensor obsolescence required change to new sensor which induced oscillations • Issue affects controller serial numbers 5050 and On • Controller serial numbers prior to 5050 overhauled before August 2018 may also be affected • Issue corrected with incorporation of controller Mod M • Mod level can be verified by checking controller data plate and/or 8130 form • Non Mod M controllers need returned to TAPD for upgrade 47 Crew Oxygen Mask Leakage CJ1/CJ2 • Issue • Crew oxygen mask P/N 9914771-1 may leak overnight • Status • Improved PVC attach point, swivel fitting, hose material and lengthened wires • Vendor P/N 174252-N6, Formerly 174252-96 • No change to Textron Aviation Part Number • Recommend unplugging masks between flights • All masks have normal leak rate 48 Speed Brake Actuator Screw Replacement CJ/CJ1/CJ1+/CJ2/CJ2+ • Issue • Reports of speed brake actuator screws breaking • May cause loss of hydraulic fluid • Status • Optional Service Documents Released • Replace and Seal Speed Brake Actuator Screws • SL525A-27-07 Released May 2018 • 525A-0001 thru -0524 • SL525-27-09 Released May 2018 • 525-0001 thru -0701 49 Avionics Equipment Batteries All Collins Proline Models • Issue • Some avionics equipment require “keep alive” batteries • No specific maintenance event to proactively change out • Rockwell Service Information Letters (SIL) 11-1 issued • https://www.rockwellcollins.com/Search/TechPubs • Battery dependent components can include • Maintenance Diagnostic Computers (MDC) • RC SIL 523-0819323-101000 • Flight Management Computers (FMC): AOG • RC SIL: 523-0819333-001000 • Air Data Computers (ADC): AOG • RC SIL: 523-0819325-001000 • Customers can expect 50% discount off list price of rental/exchange units for battery when notifying RC • Units requiring additional repair beyond battery replacement will be charged accordingly 50 Avionics Equipment Batteries All Collins Proline Models • Status • Textron Aviation collaborating on Service Letter for maintenance event to determine proactive replacement cycle • Operators can request maintenance tracking to add replacement task, will need last battery replacement date or when unit was installed • Most batteries last three to five years • Refer to Rockwell Collins SIL’s for life expectancy for LRU’s • Based on operation frequency • Collins replaces batteries on exchange avionics if battery is over one year old 51 Rockwell: Avionics Equipment Battery Replacement 52 Climb To Temperature Compensation Databases All Collins Proline Models • Issue • Manually edited or temperature compensated “Climb to” altitudes may command a wrong turn • Affects FMS 3.3 through FMS 4.2 • July 14, 2017 Rockwell OPSB 0166-17 Released: Starting with the 1712 cycle, removed approx. 10,000 approaches from both the Jeppesen and Lufthansa (LSY) Navigation Database types 6, 7, and 8 • December 2017 – Reinstated approaches • Status • Textron Aviation released service letters notifying customers (August 2017) • FAA and Rockwell agreement to disable temperature compensation feature • Textron Aviation collaboration in work • Requires updates to Aircraft Flight Manuals and Type Certificates or Supplemental Type Certificates 53 Aviation Alerts and Advisories Rockwell Collins • Issue • Receiving Rockwell Collins Aviation Alerts and Advisories when released • Status • Subscribe to the Rockwell Collins website • https://www.rockwellcollins.com/Services_and_Support/Database_and_Software_Up dates/Navigation_Databases/Database_Alerts_and_Certifications.aspx Universal Avionics 525,525A,550,560 • Service Bulletin Number 1XXX.XX.( )-34-3703 • GNSS sensor embedded in the Universal FMS with SCN 802 and 803 exhibits a date and time error • Started Sunday, June 3, 2018 • Primary symptom is FMS date field will indicate an erroneous date • Erroneous date makes RAIM prediction non-available • FMS will present NO RAIM AT FAF and will not activate GPS approaches • VOR/DME, LOC, and BC approaches are still available if supported by the external sensor interface 55 Universal Avionics 525,525A,550,560 • Service Bulletin Number 1XXX.XX.( )-34-3703 • Solution: Service Bulletin Number 1XXX.XX.( )-34-3705 • On wing reset procedures will correct the anomaly with the GPS/GNSS sensor by performing a memory reset of the GPS/GNSS module • Customer Kit part number P12148 which includes an interface harness, USB memory stick with Terminal Monitor program and instructions Report No. 34-60-91 • Must read -34-3705 for units that can be fixed on-wing 56 Universal Avionics 525,525A,550,560 • Service Bulletin Number 1XXX.XX.( )-34-3703 • Solution: Service Bulletin Number 1XXX.XX.( )-34-3706 • Procedures for Correcting Erroneous Date Expired Database Message in the Flight Management System • All units described in table below must be returned to Universal Avionics for accomplishment of this Service Bulletin. • Must have current Warranty coverage 57 Aviation Alerts and Advisories Universal Avionics • Issue • Receiving Universal Avionics Aviation Alerts and Advisories when released • Status • Navigate to Universal Avionics Notices & Alerts website • https://www.uasc.com/home/support/noticesalerts • AD2012-17-05 Rotor Assembly Replacement issued in 2012 • 118 Citation 650s are affected • Must comply with Honeywell service bulletin TFE731-72-3768 satisfies the AD Honeywell Engines Citation 650 AD2012-17-05 Lighting CJ, CJ1, CJ2 • CJ Series Exterior LED Lights • CJ Wing-Tip light obsolescence • 04-1502-1408 Power supply for original strobe lights obsolete • SB In-work for upgrade • Tail Nav light available, direct replacement • No Service Bulletin 60 Avionics ADS-B Solutions • 2020 Mandate • Contact Textron Aviation regional sales rep for package options • Contact Textron Aviation Service Center for scheduling • Textron Aviation has solutions for all Citation platforms except Citation X EASA registered with winglets 61 62 ProMaintenance All Models • Some Operators Could Benefit From a Maintenance Manager • Status: • Developed in Response to Operators Needing a DOM • No Cost Service to Manage Maintenance Schedule • ProMaintenance Director of Maintenance Manages Your Aircraft • Coordinates Factory-Direct Service • CAMP, SB’s, Warranty • ProOwnership@txtav.com • ProMaintenance Manager Jeremy Caffrey, jcaffrey@txtav.com, 316-517-3982 64 Webinars Q4 2018 Light Jet REGISTER • All model webinars scheduled: • 500/650 Series: Thursday, November 8th, 2:00 CST • 525 Series: Wednesday, November 7th, 10:00 CST • 90 minutes • www.txtavsupport.com Full Webinar Schedule Details Billing & Invoice Accuracy CJP Annual Convention October 2018 We Heard You • “Almost no bill from the service center is correct...” • “I’ve had to spend weeks straightening out errors and confusion.” • “Every bill requires some correction…” • “Warranty work is often charged to programs…” • “Even the customer portal doesn’t help.” • “Still outstanding claims from January…” • “In dispute from February… • “Their billing practice sucks to put it mildly.” Ease of Doing Business 67 Same Day Invoicing – clear, timely, and accurate Reduce the number of customer disputes Reduce the cycle time for dispute resolution Project Activities • Cross-functional team (10 areas involved) • Current state process maps • Identified gaps and improvement opportunities • Identify robust solutions to gaps/opportunities (Q4 2018) • Solicit customer feedback before deployment • Develop and execute an action plan (Q4 2018 start) 68 Project Scope: Pre-Arrival • Aftermarket Sales Proposals & PDCs • Clarity on terms and customer expectations • Deposits • Improved tracking system • Scheduling & Pre-Buys • Visibility of customer account info, coverage, and customer transfers 69 Project Scope: Mx Visit 70 Mx Events: scheduled, drop-ins, MSUs SAP & Lawson Design/Performance Visibility to warranty/programs coverage Automation, speed, integration Quotes/Estimates during Mx events Warranty Claims Simplified process, consistent execution Timely processing Invoices Credit Cards / Checks Accurate, timely, master data integrity, program $$ value at line item level Timely processing Progressive Payments Fuel Payment Process Process and improved tracking system Timely processing Project Scope: Post Mx Visit 71 Customer Account Statements Warranty Claims / Adjudication Clear, drill down on portal, program balances Timely and accurate processing Fuel Payment Process Program & Warranty Administration Timely processing, no duplicate billings Accurate billing Technical Publications Billing Parts: Exchange, Mods, Returns No duplicate billings, on customer portal Improved visibility and processes Customer Portal / eBilling Dispute Process Program balances, drill down to invoices, sort by type, link all accounts to one Reduced cycle time What to Expect Next Phase 1 (3 - 6 months) • Process Changes / Standard Work / Metrics • Customer Portal Enhancements • Salesforce Enhancements • Communication & Training Phase 2 (6 - 12 months) • System Enhancements – SAP / eBilling Phase 3 (12+ months) • Improved Systems Integration 72 T h a n k Yo u QUESTIONS

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