# Fokker F.28 MK 0100 - Type: Aircraft model (FAA registry) - Registry code: 4990807 - Manufacturer (registry): FOKKER - Model: F.28 MK 0100 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 111 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/fokker-f-28-mk-0100 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Information bulletins (advisory) (1) - [SAIB NM-06-71](https://openairdocs.org/saib/NM-06-71): . Issued Sep 26, 2006 ## Registered aircraft None registered with this model now. ## NTSB investigations (17) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC03FA190](https://openairdocs.org/ntsb/NYC03FA190), Sep 4, 2003: Fokker F.28 Mk 0100 (N1450A), Flushing, NY, substantial damage. Probable cause: An in-flight collision with birds. - [NTSB CHI02IA270](https://openairdocs.org/ntsb/CHI02IA270), Sep 5, 2002: Fokker 100 (N1473K), Minneapolis, MN, incident, minor damage. Probable cause: The improper installation of the #2 main landing gear wheel, including the axle nut not being properly torqued and safetied, which resulted in the wheel separation during takeoff. - [NTSB FTW02LA088](https://openairdocs.org/ntsb/FTW02LA088), Mar 6, 2002: Fokker F-28 MK-100 (N1425A), Dallas, TX, substantial damage. Probable cause: The ground crew inadvertent application of deicing fluid in the auxiliary power unit resulting in an overspeed and turbine wheel burst. A contributing factor was the gusty wind. - [NTSB FTW02FA003](https://openairdocs.org/ntsb/FTW02FA003), Oct 3, 2001: Fokker F28 Mk 0100 (N1448A), DFW Airport, TX, substantial damage. Probable cause: The collapse of the nose landing gear as a result of the failure of company maintenance personnel to follow the proper procedures for a towing the airplane with an unsafe nose landing gear… - [NTSB FTW01FA127](https://openairdocs.org/ntsb/FTW01FA127), May 23, 2001: Fokker F28 Mk 0100 (N1419D), DFW Airport, TX, substantial damage. Probable cause: A forging fold that was introduced during the manufacture of the right main landing, which resulted in a fatigue crack in the right main landing gear cylinder, and its subsequent failure during… - [NTSB CHI01IA102](https://openairdocs.org/ntsb/CHI01IA102), Mar 6, 2001: Fokker F28 MK 0100 (N1426A), Montreal, Canada, incident, minor damage. Probable cause: the inaccurate aircraft deicing service the ground personnel performed alowing fluid injestion and the auxiliary power unit's turbine failure while standing. A factor was the auxiliary power unit's… - [NTSB NYC01LA077](https://openairdocs.org/ntsb/NYC01LA077), Feb 6, 2001: Fokker F28 MK 0100 (N1457B), Boston, MA, substantial damage. Probable cause: the failure of the flight crew to follow the checklist prior to engine start, and their subsequent diverted attention during engine start. - [NTSB NYC00IA231](https://openairdocs.org/ntsb/NYC00IA231), Aug 17, 2000: Fokker F-100 (N860US), Norfolk, VA, incident, no damage. Probable cause: The failure of the airplane's ground/flight switch and a malfunction of the thrust reverser deploy switch, which resulted in an in-flight thrust reverser deployment. - [NTSB CHI00LA076](https://openairdocs.org/ntsb/CHI00LA076), Feb 21, 2000: Fokker F28 MK100 (N1403M), Chicago, IL, substantial damage. Probable cause: the driver of the refueling truck fell asleep which resulted in him not maintaining clearance with the parked aircraft. Factors associated with the accident were severe obstructive sleep apnea and… - [NTSB CHI98LA154](https://openairdocs.org/ntsb/CHI98LA154), May 13, 1998: Fokker F-28 MK100 (N1400H), Ft. Wayne, IN, no damage. Probable cause: In-flight encounter with turbulence. - [NTSB NYC98LA075](https://openairdocs.org/ntsb/NYC98LA075), Mar 12, 1998: Fokker F-100 (N863US), Philadelphia, PA, substantial damage. Probable cause: The driver's failure to maintain clearance from the parked airplane. Related factors were night conditions and the driver's diverted attention. - [NTSB MIA98FA089](https://openairdocs.org/ntsb/MIA98FA089), Feb 26, 1998: Fokker F28 MK 0100 (N867US), Birmingham, AL, substantial damage. Probable cause: Were the 1) the inoperative alternate anti-skid control valve due to the disconnected electrical connector on the parking brake shut-off valve, the area was inspected 2 days earlier 2) the total loss… - [NTSB MIA98FA025](https://openairdocs.org/ntsb/MIA98FA025), Nov 7, 1997: Fokker F100 (N865US), Charlotte, NC, substantial damage. Probable cause: Improper written instructions (job/task card) by company maintenance personnel. The procedures did not reflect the correct manufactures maintenance manual servicing procedure, and did not ensure that… - [NTSB ATL94IA088](https://openairdocs.org/ntsb/ATL94IA088), May 1, 1994: Fokker F28 MK 0100 (N890US), Charlotte, NC, incident, minor damage. Probable cause: THE IMPROPER RIGGING OF THE NOSE WHEEL STEERING SYSTEM BY COMPANY MAINTENANCE PERSONNEL. - [NTSB BFO93IA070](https://openairdocs.org/ntsb/BFO93IA070), May 7, 1993: Fokker F28-MK-0100 (N867US), Pittsburgh, PA, incident, minor damage. Probable cause: THE IMPROPER INSTALLATION OF THE SPACERS BY THE MECHANIC AND THE UNCLEAR INFORMATION SUPPLIED FROM THE MANUFACTURER AND OPERATOR REGARDING THE INSTALLATION OF THE SPACERS. - [NTSB CHI93IA110](https://openairdocs.org/ntsb/CHI93IA110), Mar 13, 1993: Fokker 100 (N895US), Chicago, IL, incident, minor damage. Probable cause: FAILURE OF THE COMPANY STATION MANAGER TO FOLLOW PROPER DISPATCH PROCEDURES, AND ICE ACCUMULATION ON THE NOSE GEAR LOCKING MECHANISM. FACTORS RELATED TO THE INCIDENT WERE: WET SNOW (SLUSH) ON THE… - [NTSB ATL91IA017](https://openairdocs.org/ntsb/ATL91IA017), Nov 11, 1990: Fokker F28 MK0100 (N850US), Atlanta, GA, incident, no damage. Probable cause: FROZEN MOISTURE IN THE STABILIZER ACTUATOR HYDRAULIC SERVO VALVE WHICH RESULTED IN REDUCED MOVEMENT OF THE SERVO VALVE AND LIMITED ITS ABILITY TO RESPOND TO FLIGHT CONTROL INPUTS. THE LACK OF… ## FAA accident and incident reports (111, newest 50) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20030924030729I](https://openairdocs.org/incident/20030924030729I), Sep 24, 2003: Fokker F28MK0100 (N1466A), Buffalo, NY. (-23) On September 24, 2003, at 2040 EST, American airline, flt. 1485 Fokker 100, landed at the Buffalo airport, Buffalo, NY after reporting a vibration in the… - [Accident 20030904021109A](https://openairdocs.org/incident/20030904021109A), Sep 4, 2003: Fokker F28MK0100 (N1450A), New York, NY, Substantial damage. (-23) On September 04, 2003, at 0624E, American airlines flight 549, a Fokker-28-MK100, registration number N1450A (2CG), serial number 11459, departed on… - [Incident 20030708019089I](https://openairdocs.org/incident/20030708019089I), Jul 8, 2003: Fokker F28MK0100 (N1414D), Chicago, IL, Substantial damage. (-23) On July 8, 2003, at 12:30 central standard time, an American airlines F-100 aircraft, N1414D, was parked at gate H-12 at o'Hare international airport in… - [Incident 20020912027199I](https://openairdocs.org/incident/20020912027199I), Sep 12, 2002: Fokker F28MK0100 (N1455K), Omaha, NE. (-23) American airline flight 1718, F-28-MK0100, was being pushed back from the gate at Omaha, NE, when the number one engine starter failed during atempt to… - [Incident 20020905029409I](https://openairdocs.org/incident/20020905029409I), Sep 5, 2002: Fokker F28MK0100 (N1473K), Chicago, IL, Minor damage. (-23) On Thursday September 05, 2002 an inspector from the o'Hare flight standards district office (FSDO) received a telephone call from the amrcmo pmi terry… - [Incident 20020620036109I](https://openairdocs.org/incident/20020620036109I), Jun 20, 2002: Fokker F28MK0100 (N1460A), Memphis, TN. (-23) American airlines, flight #2069, registration N1460, F-28 Fokker, flight plan cvg-dfw, diverted into mem, declaring an emergency. The number one engine… - [Incident 20020610011909I](https://openairdocs.org/incident/20020610011909I), Jun 10, 2002: Fokker F28MK0100 (N1461C), Chicago, IL, Minor damage. (-23) On June 10, 2002 the o'hare (FSDO) flights standards district office received a notice by fax from the great lakes operation center. The notice was that… - [Incident 20020409035729I](https://openairdocs.org/incident/20020409035729I), Apr 9, 2002: Fokker F28MK0100 (N1411G), Chicago, IL, Minor damage. (.23) Notified by o'Hare city operations of the following incident: an American airlines Fokker-100, N1411G, flight 1949, blew four main landing gear tires… - [Accident 20020306003829A](https://openairdocs.org/incident/20020306003829A), Mar 6, 2002: Fokker F28MK0100 (N1425A), Dallas-Ft Worth, TX, No damage. (-23) During deicing at dfw type I deicing fluid and possibly ice runoff was ingested into the APU inlet. The substance ingested caused the APU to overspeed… - [Incident 20011011027249I](https://openairdocs.org/incident/20011011027249I), Oct 11, 2001: Fokker F28MK0100 (N851US), Louisville, KY, Minor damage. (-23) No narrative. - [Accident 20011003037319A](https://openairdocs.org/incident/20011003037319A), Oct 3, 2001: Fokker F28MK0100 (N1448A), Dallas-Ft Worth, TX, No damage. (-23) On October 3, 2001, prior to landing at dfw and following gear extension a message appeared on the mfdu indicating the nose landing gear was unsafe.… - [Accident 20010523009809A](https://openairdocs.org/incident/20010523009809A), May 23, 2001: Fokker F28MK0100 (N1419D), Dallas-Ft Worth, TX, No damage. (-23)On may 23, 2001, at approximately 304 pm CDT, during the landing roll-out phase of flight on runway 17 center at the Dallas/fort Worth, Texas airport… - [Accident 20010206000489A](https://openairdocs.org/incident/20010206000489A), Feb 6, 2001: Fokker F28MK0100 (N1457B), Boston, MA, No damage. (-23) American flight 1813 bos>dca during pushback from gate 19 a/c lurched forward when second engine was started causing towbar to bend in half and a/c then… - [Incident 20001229037789I](https://openairdocs.org/incident/20001229037789I), Dec 29, 2000: Fokker F28MK0100 (N861US), Middletown, PA. (-23) Pilot reported that "going through 1000 ft AGL, aircraft pitched up to approx. 25 degrees nose up. Airspeed started bleeding off. Disconnected autopilot.… - [Incident 20001018029879I](https://openairdocs.org/incident/20001018029879I), Oct 18, 2000: Fokker F28MK0100 (N883US), Richmond, VA, Minor damage. (-23)On October 18, 2000, 1517 local a us airways flight 1449 a folker F28MK0100 landed RW34 after reporting a hydraulic problem inbound and executed a missed… - [Incident 20000817026129I](https://openairdocs.org/incident/20000817026129I), Aug 17, 2000: Fokker F28MK0100 (N860US), Norfolk, VA. (-23) On 8/17/2000 at 1522 EDT, a U.S. Airways flight 471 was enroute from lga to ric, when flight 471 diverted to orf and landed on runway 05 after the left… - [Incident 20000726036039I](https://openairdocs.org/incident/20000726036039I), Jul 26, 2000: Fokker F28MK0100 (N855US), Syracuse, NY. (-23)On Wednesday, July 26, 2000, U.S. Airways flight 1802, an F-100, N855US, was enroute from pittsburg, pa (pit) to new york, NY (lga) when the crew noted a… - [Accident 20000221017949A](https://openairdocs.org/incident/20000221017949A), Feb 21, 2000: Fokker F28MK0100 (N1403M), Chicago, IL, Substantial damage. (.4)They reported seeing the refueling truck parked at a 45 degree angle to the lead in line on the right side of the airplane. The truck then moved forward… - [Incident 19990924029159I](https://openairdocs.org/incident/19990924029159I), Sep 24, 1999: Fokker F28MK0100 (N1417D), Little Rock, AR. (-23) On September 24, 1999, at 0915 CDT, N1417D, a Fokker F-28-MK0100, registered to and operated by American airline as flight 526, enroute from dfw to sdf,… - [Incident 19990807029949I](https://openairdocs.org/incident/19990807029949I), Aug 7, 1999: Fokker F28MK0100 (N1468A), Minneapolis, MN. (-23) After takeoff and gear retraction, nose gear light failed to go out. Gear cycled, light remained on. Reseated and relamped, operation check normal. - [Incident 19990803024279I](https://openairdocs.org/incident/19990803024279I), Aug 3, 1999: Fokker F28MK0100 (N889US), Nashville, TN. At cruise flight about 40 miles east of Nashville, TN, the captain, first officer and jumpseat rider all smelled noxious smoke smell. After crew troubleshot… - [Incident 19990722032619I](https://openairdocs.org/incident/19990722032619I), Jul 22, 1999: Fokker F28MK0100 (N1427A), Middletown, PA. (-23) The #1 hydraulic system low quantity light came on in cruise at FL29. A non-eventful landing was made at the destination airport, Middletown (MDT).… - [Incident 19990713023619I](https://openairdocs.org/incident/19990713023619I), Jul 13, 1999: Fokker F28MK0100 (N855US), Buffalo, NY. (-23) On Tuesday, July 13, 1999, at 1842 local, a usairways F100, N855US, reported a flap asymmetry problem inbound to Buffalo niagara airport. The aircraft… - [Incident 19990627022709I](https://openairdocs.org/incident/19990627022709I), Jun 27, 1999: Fokker F28MK0100 (N859US), Raleigh-Durham, NC, Minor damage. During pushback from jetway at rdu, the horizontal stabilizer of usaa 460 (N859) contacted the horizontal stabilizer of usa 1282 (N897) parked at an adjacent… - [Incident 19990626023629I](https://openairdocs.org/incident/19990626023629I), Jun 26, 1999: Fokker F28MK0100 (N862US), Buffalo, NY. (-23) On Saturday, June 26, 1999, a usairways Fokker F100, N862US, diverted to Buffalo niagra international airport after reporting smoke puffs above the… - [Incident 19990626022859I](https://openairdocs.org/incident/19990626022859I), Jun 26, 1999: Fokker F28MK0100 (N867US), Wilmington, NC, Minor damage. (-23) On June 26, 1999 at 18:10 EST a usairways F-28-MK0100 experienced a left main brake fire on landing at ilm. Once aircraft came to a stop airport fire… - [Incident 19990625022119I](https://openairdocs.org/incident/19990625022119I), Jun 25, 1999: Fokker F28MK0100 (N1468A), Wichita, KS. Aircraft N1468A diverted to ict due to low oil quantity #1 hydraulic system. Reservoir was serviced and the system was inspected. It was determined that the… - [Incident 19990609029939I](https://openairdocs.org/incident/19990609029939I), Jun 9, 1999: Fokker F28MK0100 (N1460A), Sioux Falls, SD. (-23) While N1460A was enroute from msp to dfw, flight attendant advised cockpit crew that something was burning in the galley, smoke and source could not be… - [Incident 19990521021819I](https://openairdocs.org/incident/19990521021819I), May 21, 1999: Fokker F28MK0100 (N882US), South Bend, IN, Minor damage. (From .19 this incident was investigated by NTSB) on may 21, 1999, at 1207 eastern standard time, a Fokker F-100, N882US, operated by us airways, incorporated,… - [Incident 19990328021369I](https://openairdocs.org/incident/19990328021369I), Mar 28, 1999: Fokker F28MK0100 (N885US), Indianapolis, IN. On taxi out, the pilot felt a vibration like a nose tire out of balance. When they were turning to return to the gate, the right inboard tire departed aircraft. - [Incident 19990315021399I](https://openairdocs.org/incident/19990315021399I), Mar 15, 1999: Fokker F28MK0100 (N896US), Indianapolis, IN. On 3/15/99 at 0135 local time a us airways F-28, N896US flight 569 enroute to ind from lga experienced nose gear indication problem on approach to ind. The… - [Incident 19990124009959I](https://openairdocs.org/incident/19990124009959I), Jan 24, 1999: Fokker F28MK0100 (N1461C), Charlotte, NC, Minor damage. The half couplings that connect the hydraulic supply/return lines to the brake shuttle valve were found to have worn teeth on brake #3 preventing a positive… - [Incident 19981221044019I](https://openairdocs.org/incident/19981221044019I), Dec 21, 1998: Fokker F28MK0100 (N897US), Greensboro, NC. (-5) Pilot reported left main gear problem. Pilot made a fly-by to okay gear down. Landed without incident. Maintenance replaced left landing gear light bulb… - [Incident 19980910035789I](https://openairdocs.org/incident/19980910035789I), Sep 10, 1998: Fokker F28MK0100 (N888AU), Norfolk, VA. Usair flt 1041 departed Norfolk (orf) 09:46 1C1 en route to pittsburg (pit). After rotation a no. 2 engine fire light illuminated. The crew shut down the no. 2… - [Incident 19980530023209I](https://openairdocs.org/incident/19980530023209I), May 30, 1998: Fokker F28MK0100 (N1458H), Rochester, NY. Aircraft struck a deer on takeoff. Circled field and landed uneventfully. - [Accident 19980513046339A](https://openairdocs.org/incident/19980513046339A), May 13, 1998: Fokker F28MK0100 (N1400H), Ft. Wayne, IN. (.4)The #1 flight attendant suffered a fractured ankle when she got up from a passenger seat to answer the interphone during moderate turbulence. The captain… - [Accident 19980311024789A](https://openairdocs.org/incident/19980311024789A), Mar 11, 1998: Fokker F28MK0100 (N863US), Philadelphia, PA, Substantial damage. (.4)After the airplane was pushed back from the gate at night, a fuel truck travelling eastbound on the outer service road struck the left wing tip of the… - [Accident 19980226007449A](https://openairdocs.org/incident/19980226007449A), Feb 26, 1998: Fokker F28MK0100 (N867US), Birmingham, AL, Substantial damage. Lightning strike on final. Blew holes in hydro system lines. Alternate used blew tires ldg. Nose gear sheared off. (.4)while flying in precipitation deviating… - [Accident 19971107032609A](https://openairdocs.org/incident/19971107032609A), Nov 7, 1997: Fokker F28MK0100 (N865US), Charlotte, NC, Substantial damage. Right main laning gear attach fittings failed on landing roll. (.4)the Fokker F100 was on landing rollout when the right main landing gear collapsed. Review of… - [Incident 19971104035589I](https://openairdocs.org/incident/19971104035589I), Nov 4, 1997: Fokker F28MK0100 (N1410E), Albany, NY, Minor damage. Narrative: #2 engine tailpipe fire indication during engine start crew attempted to blow out fire by re-energizing starter motor. Via radio, adjacent aircraft… - [Incident 19970423011509I](https://openairdocs.org/incident/19970423011509I), Apr 23, 1997: Fokker F28MK0100 (N864US), Buffalo, NY. Narrative: on April 23, 1997, at 1530 EST, a Fokker 28, N864US, flight 821, operated by us airways, during the takeoff phase from Buffalo international airport… - [Incident 19970421011189I](https://openairdocs.org/incident/19970421011189I), Apr 21, 1997: Fokker F28MK1000 (N1448A), Minneapolis, MN. Narrative: while deplaning passengers,the ramp personnel noticed smoke coming over fuselage from the left engine. Fire contained inside core engine and… - [Incident 19970407012699I](https://openairdocs.org/incident/19970407012699I), Apr 7, 1997: Fokker F28MK0100 (N850US), Philadelphia, PA, Minor damage. Narrative: us airways flight 1446 departed bos enroute to phl on 4/7/97. The crew noted in the aircraft's log that "left lg downlock switch" fault indicated on… - [Incident 19970305007289I](https://openairdocs.org/incident/19970305007289I), Mar 5, 1997: Fokker F28MK0100 (N859US), Middletown, PA, Minor damage. Narrative: on March 5, 1997, at 1855 hours a Fokker 28, model MK0100, registration number 859US, registered to us air inc, and made an emergency landing at the… - [Incident 19961018038599I](https://openairdocs.org/incident/19961018038599I), Oct 18, 1996: Fokker F28MK0100 (N852US), Elmira, NY. After departure from 1th, at 12,000 ft., during a left turn, the fuel totalizer was fluctuating. A precautionary, diverted landing was made in Elmira. Found no… - [Incident 19960921037869I](https://openairdocs.org/incident/19960921037869I), Sep 21, 1996: Fokker F28MK0100 (N887US), Pittsburgh, PA. Narrative: when descending into pit at approximately 50 NM southeast of the airport, the crew got an emergency DC bus failure message on the multi-function… - [Incident 19960821028169I](https://openairdocs.org/incident/19960821028169I), Aug 21, 1996: Fokker F28MK0100 (N852US), Atlanta, GA. Narrative: us air 1184 was enroute from new orleans to bwi. When just north of mgm, a female passenger seated in 13A showed a message written on the inside of… - [Incident 19960727025329I](https://openairdocs.org/incident/19960727025329I), Jul 27, 1996: Fokker F28MK0100 (N889US), Syracuse, NY. Narrative: usaa flight 1052 enroute from pwm to pit diverted to syr with a cracked windshield. The aircraft landed without incident. Usaa maintenance in syr… - [Incident 19960625024359I](https://openairdocs.org/incident/19960625024359I), Jun 25, 1996: Fokker F28MK0100 (N858US), Wilmington, NC, Minor damage. Narrative: on June 25, 1996, usair flight 909, a Fokker F-28-100, N858US, with richard w. kozel as PIC and george e. pence as SIC, landed at Wilmington, NC… - [Incident 19960621021899I](https://openairdocs.org/incident/19960621021899I), Jun 21, 1996: Fokker F28MK0100 (N851US), Pittsburgh, PA, Minor damage. Narrative: on June 21, 1996, usair aircraft N851US, a F28MK0100, departed Pittsburgh international airport as flight 1050. At lift off, flight crew felt slight… All 111: https://openairdocs.org/model/fokker-f-28-mk-0100/incidents.md ## Service difficulty reports (1,581, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA070608008](https://openairdocs.org/sdr/CA070608008), Jun 6, 2007: CONTROL CABLE. BROKEN. (CAN) FLIGHT CREW REPORTED DURING HEAD START CHECKS THAT THE FLIGHT CONTROL LOCK WOULD NOT LOCK THE ELEVATOR CONTROLS AND WAS VERY STIFF WHEN MOVING CONTROL LOC - [SDR CA070109005](https://openairdocs.org/sdr/CA070109005), Nov 8, 2006: VALVE. MALFUNCTIONED. (CAN) DATE OF DELAY NOV 8, 2006 CADORS NR: 2006C2915. THE FLIGHT CREW WAS NOTIFIED THAT DURING TAXI FOR DEPARTURE FUEL WAS LEAKING FROM LT WING. AIRCRAFT TAXIED - [SDR CA070110005](https://openairdocs.org/sdr/CA070110005), Oct 9, 2006: WARNING SYSTEM. MALFUNCTIONED. (CAN) THE REFERENCED AIRCRAFT AN EVENT INVOLVING THE AUTOMATIC SILENCING OF CABIN CHIMES. NORMALLY THE FLIGHT CREW WILL ADVISE THE FLIGHT ATTENDANTS TO TAKE THE - [SDR CA060919005](https://openairdocs.org/sdr/CA060919005), Sep 10, 2006: ACTUATOR. MALFUNCTIONED. (CAN) FLIGHT CREW REPORTED THAT THE SPEED BRAKE WOULD NOT RETRACT UPON SELECTION TO DO SO. FOLLOWING LANDING. BOTH PADDLES CONFIRMED OPEN. AIRCRAFT WAS FERRIED - [SDR 2006F00020](https://openairdocs.org/sdr/2006F00020), Mar 3, 2006: ARM. CRACKED. CENTER ARMREST CRACKED AT ATTACH BRACKET TO SEAT FRAME, HAVE SEEN OTHER SEATS WITH SAME CONDITION, FLIGHTLINE IN TULSA IS WORKING WITH FSDO IN CALIFORNIA AND FL - [SDR AU510002130](https://openairdocs.org/sdr/AU510002130), Dec 12, 2005: OXYGEN BOTTLE. LEAKING. COCKPIT OXYGEN BOTTLE LEAKING FROM VALVE. - [SDR AU510002116](https://openairdocs.org/sdr/AU510002116), Dec 12, 2005: CONTROL PANEL. FAULTY. NR 2 ATC TRANSPONDER SYSTEM CONTROL PANEL DISPLAY DIGITS NOT VISIBLE. - [SDR AU510002112](https://openairdocs.org/sdr/AU510002112), Dec 12, 2005: TRANSPONDER. FAILED. NR 2 ATC TRANSPONDER FAILED. INVESTIGATION CONTINUING. - [SDR AU510002107](https://openairdocs.org/sdr/AU510002107), Dec 12, 2005: SHUTOFF VALVE. FAULTY. RT BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAULTY. - [SDR AU510002024](https://openairdocs.org/sdr/AU510002024), Dec 12, 2005: FAIRING. CRACKED. ENGINE EXHAUST SPOKE FAIRING CRACKED IN TWO PLACES AT THE 7:30 O`CLOCK AND 9 O`CLOCK POSITIONS. - [SDR AU510002019](https://openairdocs.org/sdr/AU510002019), Dec 12, 2005: SOLENOID. FAULTY. NR 2 ENGINE THRUST REVERSER INTERMITTENT WARNING. INVESTIGATION FOUND THE SECONDARY LOCK SOLENOID HAD A FAULTY INTERNAL SWITCH. - [SDR AU510002018](https://openairdocs.org/sdr/AU510002018), Dec 12, 2005: IGNITER. WORN. NR 2 ENGINE IGNITER WORN. - [SDR AU510001949](https://openairdocs.org/sdr/AU510001949), Dec 12, 2005: SKIN. LIGHTNING STRIKE. EVIDENCE OF LIGHTNING STRIKE ON FUSELAGE AT STN 9305, STN 9805 AND STN 10253. INVESTIGATION CONTINUING. - [SDR AU510001948](https://openairdocs.org/sdr/AU510001948), Dec 12, 2005: MOTOR. FAULTY. FUEL SYSTEM RT CROSS FLOW VALVE MOTOR FAULTY. VALVE STUCK IN CLOSED POSITION. - [SDR AU510001947](https://openairdocs.org/sdr/AU510001947), Dec 12, 2005: SHUTOFF VALVE. FAILED. LT ENGINE ANTI-ICE PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAILED. - [SDR AU510001935](https://openairdocs.org/sdr/AU510001935), Dec 12, 2005: STRINGER. CORRODED. NR 3 LT STRINGER LOCATED AT STN 13851 IN THE FORWARD CARGO COMPARTMENT CORRODED. - [SDR AU510001923](https://openairdocs.org/sdr/AU510001923), Dec 12, 2005: COOLING FAN. FAULTY. (AUS) AVIONICS COOLING FAN NOISY IN OPERATION. - [SDR AU510001915](https://openairdocs.org/sdr/AU510001915), Dec 12, 2005: CONTROL CABLE. MISRIGGED. (AUS) CONTROL CABLES FOR FLAPS ( F1 AND F2) WERE FOUND TO BE 43LB LOW IN TENSION. THE LT AILERON WING CABLE WAS 30LB LOW. THE LT AND RT AILERON UPFLOAT CABLES W - [SDR AU510001914](https://openairdocs.org/sdr/AU510001914), Dec 12, 2005: BOLT. LOOSE. (AUS) LT AILERON TAB OB HINGE BRACKET ATTACHMENT BOLTS LOOSE. BOLTS WERE THREADBOUND IN ANCHOR NUTS. INVESTIGATION FOUND INCORRECT BOLTS WERE FITTED BY A PREVIO - [SDR AU510001903](https://openairdocs.org/sdr/AU510001903), Dec 12, 2005: DRIVE SHAFT. SHEARED. (AUS) APU STARTER MOTOR DRIVESHAFT SHEARED. INVESTIGATION FOUND THAT THE BROKEN END WAS JAMMED IN THE CLUTCH ASSEMBLY. (CASA NR 510001903) - [SDR AU510001887](https://openairdocs.org/sdr/AU510001887), Dec 12, 2005: SWITCH. FAULTY. NR 1 ENGINE ANTI-ICE SWITCH FAULTY. - [SDR AU510001866](https://openairdocs.org/sdr/AU510001866), Dec 12, 2005: BOLT. LOOSE. NR 1 LT LIFT DUMPER SYSTEM BELLCRANK SPIGOT ATTACHMENT BOLTS LOOSE. - [SDR AU510001805](https://openairdocs.org/sdr/AU510001805), Dec 12, 2005: IRU. FAILED. NR 2 INERTIAL REFERENCE UNIT (IRU) INTERMITTENTLY FAILS CODE 2. INVESTIGATION CONTINUING. - [SDR AU510001804](https://openairdocs.org/sdr/AU510001804), Dec 12, 2005: BOLT. BROKEN. NR 2 MAIN WHEEL TIE BOLT BROKEN. BOLT HEAD MISSING. INVESTIGATION CONTINUING. - [SDR AU510001802](https://openairdocs.org/sdr/AU510001802), Dec 12, 2005: MOTOR. SHEARED. APU STARTER MOTOR DRIVE SHAFT SHEARED. - [SDR AU510001751](https://openairdocs.org/sdr/AU510001751), Dec 12, 2005: FUEL CONTROL. FAILED. (AUS) APU AUTO-SHUTDOWN IN FLIGHT. INVESTIGATION FOUND A FAULTY FUEL CONTROL UNIT. (CASA NR 510001751) - [SDR AU510001740](https://openairdocs.org/sdr/AU510001740), Dec 12, 2005: EXCITER. FAULTY. APU IGNITION EXCITER UNIT FAULTY. - [SDR AU510001726](https://openairdocs.org/sdr/AU510001726), Dec 12, 2005: PIPE. FRACTURED. HYDRAULIC PIPE LOCATED ON THE FORWARD WALL OF THE REAR CARGO HOLD LEAKING. INVESTIGATION FOUND A FRACTURED FLARE. PIPE WAS A -4 STAINLESS STEEL TYPE. - [SDR AU510001721](https://openairdocs.org/sdr/AU510001721), Dec 12, 2005: HOSE. FAILED. LT TOILET SMOKE DETECTOR TO AIR EJECTOR HOSE SPLIT AT EJECTOR END. RT SMOKE DETECTOR TO AIR EJECTOR TUBE SIDEWALL COLLAPSED. HOSES ALLOW FOR AIRFLOW THROUGH SMO - [SDR AU510001667](https://openairdocs.org/sdr/AU510001667), Dec 12, 2005: SMOKE DETECTOR. FAULTY. REPORT OF CIGARETTE SMOKE SMELL IN CABIN. TOILET SMOKE DETECTOR DID NOT ACTIVATE ALARM. INVESTIGATION CONTINUING. - [SDR AU510001655](https://openairdocs.org/sdr/AU510001655), Dec 12, 2005: CONNECTOR. LEAKING. CREW OXYGEN MASK BOX ASSEMBLY CONNECTOR LEAKING. LOSS OF OXYGEN. - [SDR AU510001654](https://openairdocs.org/sdr/AU510001654), Dec 12, 2005: BEARING. WORN. LT ENGINE INLET GUIDE VANE BEARINGS PNO UP60336 (1OFF) AND PNO EU61711 (2OFF) WORN. FOUND DURING INSPECTION IAW SB TAY-75-1655. - [SDR AU510001648](https://openairdocs.org/sdr/AU510001648), Dec 12, 2005: PITOT HEAD. FAULTY. NR 3 PITOT HEAD HEATING SYSTEM FAILED. - [SDR AU510001540](https://openairdocs.org/sdr/AU510001540), Dec 12, 2005: PRESSURE SWITCH. FAULTY. RT ENGINE LP FUEL PRESSURE SWITCH FAULTY. - [SDR AU510001534](https://openairdocs.org/sdr/AU510001534), Dec 12, 2005: CONNECTOR. LOOSE. ENGINE INDICATION SYSTEM PRESSURE BULKHEAD CONNECTOR P2874 LOOSE. - [SDR AU510001521](https://openairdocs.org/sdr/AU510001521), Dec 12, 2005: IGNITER. FAILED. APU IGNITER PLUG FAILED. WORKSHOP INVESTIGATION FOUND THAT ONLY APPARENT FAULT WAS SLIGHT SOILING ON THE CERAMIC INSIDE OF THE CONNECTOR END OF THE IGNITER. THE - [SDR AU510001498](https://openairdocs.org/sdr/AU510001498), Dec 12, 2005: STRUT. CRACKED. RT MAIN LANDING GEAR STRUT BLEED PORT CRACKED, FOUND DURING INSPECTION IAW AD/F100/64. - [SDR AU510001497](https://openairdocs.org/sdr/AU510001497), Dec 12, 2005: STRUT. FAULTY. LT MAIN LANDING GEAR STRUT INTERNAL SLEEVE MIGRATED OUT OF POSITION AND BLOCKED BLEED PLUG HOLE, FOUND DURING INSPECTION IAW AD/F100/64. - [SDR AU510001481](https://openairdocs.org/sdr/AU510001481), Dec 12, 2005: NIPPLE. MISSING. (AUS) FLAP BALL NUT GREASE NIPPLE MISSING.(OTHER CAUSE: UNKNOWN ) (CASA# 510001481) - [SDR AU510001439](https://openairdocs.org/sdr/AU510001439), Dec 12, 2005: MICROPHONE. FAULTY. (AUS) HAND MICROPHONE SWITCH STICKING.(OTHER CAUSE: STICKY SWITCH - MATERIAL ) (CASA# 510001439) - [SDR AU510001988](https://openairdocs.org/sdr/AU510001988), Dec 10, 2005: APU. FAILED. APU AUTO SHUTDOWN. INVESTIGATION COULD FIND NO FAULTS. DURING TEST FLIGHT THE APU AGAIN SHUT DOWN. INVESTIGATION CONTINUING. - [SDR AU510001987](https://openairdocs.org/sdr/AU510001987), Dec 10, 2005: IGNITER. FAILED. NR 1 ENGINE IGNITER PLUG FAILED. - [SDR AU510001868](https://openairdocs.org/sdr/AU510001868), Dec 9, 2005: BEARING. WORN. RT WING FLAP TRACK BEAM ASSEMBLY FORWARD SUPPORT BEARING WORN. - [SDR AU510001867](https://openairdocs.org/sdr/AU510001867), Dec 9, 2005: BEARING. WORN. LT WING TRAILING EDGE FLAP TRACK FORWARD SUPPORT BEARING WORN. - [SDR AU510001864](https://openairdocs.org/sdr/AU510001864), Dec 9, 2005: ROD. CRACKED. RH LIFT DUMPER SYSTEM VERTICAL ROD CRACKED. - [SDR AU510001862](https://openairdocs.org/sdr/AU510001862), Dec 9, 2005: BEARING. LOOSE. RT LIFT DUMPER NR 3 BELLCRANK HORIZONTAL ROD ATTACHMENT BEARING MIGRATED OF POSITION. - [SDR AU510001861](https://openairdocs.org/sdr/AU510001861), Dec 9, 2005: BOLT. SHEARED. RT LIFT DUMPER SYSTEM NR 1 BELLCRANK INBOARD UPPER ATTACHMENT BOLT SHEARED. - [SDR AU510001708](https://openairdocs.org/sdr/AU510001708), Dec 8, 2005: APU. INOPERATIVE. APU FAILED TO START. INVESTIGATION CONTINUING. - [SDR AU510001588](https://openairdocs.org/sdr/AU510001588), Dec 7, 2005: SLIDE. FAULTY. (AUS) RT ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. FOLLOWING MANUAL OPERATION THE SLIDE INFLATED BUT WAS NOT CORRECTLY ORIENTATED TO THE DOOR OPENING. SUSPECT CA - [SDR AU510001587](https://openairdocs.org/sdr/AU510001587), Dec 7, 2005: COMPUTER. FAULTY. (AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. (CASA NR 510001587) All 1,581: https://openairdocs.org/model/fokker-f-28-mk-0100/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.