# Service difficulty reports: N105ML, cancelled May 15, 2001 A list on [N105ML, cancelled May 15, 2001](https://openairdocs.org/deregistered/N105ML-2001-05-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR JBXA000275](https://openairdocs.org/sdr/JBXA000275.md): Valve · out of adj · Apr 29, 2001 · N105ML · Fokker F28MK0100 · Landing Gear Retraction/Extension System > UPON GEAR RETRACTION LEFT GEAR REMAINED DOWN WOULD NOT RETRACT. REINSPECTED AIR/GROUND TEST VALVE FOUND VALVE JUST OFF OF DETENT. REPOSITIONED TEST VALVE IN THE FULL FLIGHT DETENT AND SAFETIED VALVE IAW AMM 32-00-00-710-813A. - [SDR JBXA000220](https://openairdocs.org/sdr/JBXA000220.md): Uplock Sensor · failed · Nov 22, 2000 · N105ML · Fokker F28MK0100 · Landing Gear Position and Warning > UPON LANDING AT LGA GEAR UNSAFE MESSAGE ILLUMINATED WHEN GEAR HANDLE WAS SELECTED TO THE DOWN POSITION. CYCLED GEAR HANDLE AND LIGHT WENT OUT. A/C WAS INSPECTED AND GEAR PINS INSTALLED. A/C WAS THEN FERRIED TO RDU. MX REPLACED THE RIGHT MLG UPLOCK SENSOR IA - [SDR JBXA0000192](https://openairdocs.org/sdr/JBXA0000192.md): Valve · failed · Jul 30, 2000 · N105ML · Fokker F28MK0100 · Aircraft Fuel Distribution System > RETURNED TO RDU DUE TO FUEL VENTING OVERBOARD ON RT WING. REMOVED AND REPLACED RT WING TANK OVERFLOW VALVE IAW AMM 28-21-07. OPS CHECK AND LEAK CHECK GOOD. - [SDR JBXA0000160](https://openairdocs.org/sdr/JBXA0000160.md): Sequence Valve · malfunctioned · Mar 28, 2000 · N105ML · Fokker F28MK0100 · Landing Gear Retraction/Extension System > NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT. ON SECOND ATTEMPT IT EXTENDED NORMALLY. INSPECTED AIRCRAFT, PINNED GEAR AND PERFORMED MX FERRY FLIGHT IAW MIDWAY AIRLINES GMM CHAPTER 6 SECTION 4 FROM TPA TO RDU. REMOVED AND REPLACED NLG DOOR SEQUENCING VALVE AND - [SDR JBXA0000153](https://openairdocs.org/sdr/JBXA0000153.md): Uplock · malfunctioned · Mar 14, 2000 · N105ML · Fokker F28MK0100 · Landing Gear System > AFTER TAKEOFF, THE LT MAIN LG DOOR AND RT MAIN LG DOOR SHOWED OPEN ON THE MFDU. RECYCLED THE LANDING GEAR WHICH WAS UNSUCCESSFUL IN CLEARING THE INDICATION ON THE MFDU. THE BLUE LIGHT IN THE GEAR HANDLE WAS ON WITH THE LANDING GEAR SELECTED UP AND OFF WITH T - [SDR JBXA0000152](https://openairdocs.org/sdr/JBXA0000152.md): Selector Valve · malfunctioned · Mar 13, 2000 · N105ML · Fokker F28MK0100 · Main Landing Gear > UPON SELECTING GEAR DOWN, RIGHT MAIN DID NOT GET A DOWN AND LOCKED INDICATION (RECIEVED LEVEL THREE ALERT). CYCLED GEAR AND BOTH MAIN GEAR DID NOT DOWN AND LOCK. EXECUTED MISSED APPROACH. CYCLED GEAR AGAIN AND GOT THREE GREEN, LANDED NORMALLY. REMOVED AND - [SDR JBXA0000138](https://openairdocs.org/sdr/JBXA0000138.md): Valve · contaminated · Jan 13, 2000 · N105ML · Fokker F28MK0100 · Pneumatic Distribution System > FLIGHT NR 119 FLL TO RDU AIR RETURNED BLEED NR 1 AND NR 2 FAULTED AT 5000 FEET. WOULD NOT RESET IN FLIGHT. CLEANED NR 1 AND NR 2 ENGINE BLEED AIR MUSCLE SHUTTLE VALVES AND 80 PERCENT SWITCHES ON ENGINE NR 1 AND NR 2 OPS CHECK GOOD AT THIS TIME IAW AMM 36-11- - [SDR JBXA9900122](https://openairdocs.org/sdr/JBXA9900122.md): Bleed Air · failed · Nov 8, 1999 · N105ML · Fokker F28MK0100 · Pneumatic Distribution System > BLEED 1 AND BLEED 2 FAULTED ON TAKEOFF AT 60 KNOTS. ABORTED TAKEOFF. ACCOMPLISHED CHECK PER MM 36-00-5, OPS CK GOOD. - [SDR JBXA9900120](https://openairdocs.org/sdr/JBXA9900120.md): Comm Sys · tripped · Nov 3, 1999 · N105ML · Fokker F28MK0100 · Communications System > FLIGHT 119 FROM FLL TO RDU, ON CLIMBOUT NR 1 AUDIO FAILED AND BACK-UP SYSTEM DID NOT WORK, COMPLETE COM FAILURE. RESET NR 1 AMU AND NR 2 AMU AND ALT AMU. PERFORMED OPERATIONAL CHECK IAW F-100 MM 23-51-00, OPERATIONAL CHECK GOOD. RESET NR 1 AND NR 2 VHF COMS - [SDR JBXA9900104](https://openairdocs.org/sdr/JBXA9900104.md): Bleed Valve · failed · Sep 9, 1999 · N105ML · Fokker F28MK0100 · APU Bleed Air System > ON CLIMB-OUT FROM RDU ON FLT 859, CREW REPORTED BLEED NR 1 AND 2 AND APU BLEED FAULTS. REMOVED AND REPLACED NR 2 HIGH PRESS BLEED VALVE IAW 36-11-00, OPS CHECK GOOD. ALSO, PERFORMED FUNCTIONAL CHECK FLT, ALL OPS CHECKED GOOD. - [SDR JBXA9900103](https://openairdocs.org/sdr/JBXA9900103.md): Switch · failed · Sep 9, 1999 · N105ML · Fokker F28MK0100 · Rudder Control System > FLT 220 RDU/MCO ON CLIMBOUT HAD A RUDDER NR 2 FAULT. AIR RETURN TO RDU. PERFORMED OPS CHECK OF RLMU IAW 27-23-01, NO FAULTS NOTED ON GROUND. GROUND OPERATED ENGS AND PUT RUDDER IN SEVERAL CONFIGURATION AND NO FAULTS FOUND. REMOVED AND REPLACED ACTIVE RUDDE - [SDR JBXA9900105](https://openairdocs.org/sdr/JBXA9900105.md): Bleed Air Contl · out of adjust · Sep 7, 1999 · N105ML · Fokker F28MK0100 · Pneumatic Distribution System > BOS- FLIGHT 668 ABORTED TAKEOFF, BLEED 1 AND 2 FAULT. NO RESET. ACCOMPLISHED BLEED AIR SUPPLY AND CONTROL. ADJUSTMENT AND TEST PER FOKKER 100 MM, CK'S OK PER 36-11-00. - [SDR JBXA9900102](https://openairdocs.org/sdr/JBXA9900102.md): Prsov · failed · Sep 2, 1999 · N105ML · Fokker F28MK0100 · Cabin Pressure Control System > FLT NR 668 RDU/MCO ON CLIMB-OUT HAD BLEED 1 AND 2 FAULT AND PRESS CONTROLLER FAULT ON MFDU. RETURN TO RDU AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 PROSV. OPERATIONAL AND LEAK CHECKS ARE GOOD IAW F-100 MM 36-11-05. ALSO, PERFORMED SELF T - [SDR JBXA9900100](https://openairdocs.org/sdr/JBXA9900100.md): Wheel · cracked · Aug 21, 1999 · N105ML · Fokker F28MK0100 · Wheel/Ski/Float > ON TAXI OUT CREW FELT SHIMMY IN TAIL OF AIRCRAFT. MAINTENANCE INSPECTED AND FOUND OUTER WHEEL BEARING JOURNAL ON NR 3 MAIN WHEEL HEAT DAMAGED AS A RESULT OF WHEEL FAILURE. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSY AND REMOVED AND REPLACE - [SDR JBXA9900092](https://openairdocs.org/sdr/JBXA9900092.md): Water Separator · dirty · Jul 17, 1999 · N105ML · Fokker F28MK0100 · Humidity Control System > RIGHT (AIR CONDITIONING) PACK BLOWING HOT AIR ONLY ON CLIMB-OUT, AIR RETURNED TO MCO. (LEFT AIRCONDITIONING PACK INOP UNDER MEL 21-51-1). AIRCRAFT REPOSITIONED TO RDU (CREW ONLY) BOTH PACKS INOP UNDER MEL 21-51-1. REMOVED AND REPLACED NR 1 PACK WATER SEPARA - [SDR JBXA9900090](https://openairdocs.org/sdr/JBXA9900090.md): O-Ring · failed · Jul 7, 1998 · N105ML · Fokker F28MK0100 · Hydraulic System, Main > HYDRAULIC SYSTEM NR 1 LOW QUANTITY MESSAGE, TURNED OFF PUMPS IAW MIDWAY PROCEDURE. VLANDED WITH 25 DEGREES FLAPS AND RAISED GEAR DOORS, HOWEVER NEGATIVE NOSE WHEEL STEERING. TOWED TO GATE. FOUND NR 1 ENGINE SYSTEM NR 1 HYDRAULIC PUMP QUICK DISCONNECT LINE LE - [SDR JBXA980030](https://openairdocs.org/sdr/JBXA980030.md): Bleed Valve · closed · Jan 11, 1998 · N105ML · Fokker F28MK0100 · Compressor Bleed Valve > RDU - FLT 17 - IN CLIMB, PACKS PRESSURE CONTROLLER PACK FAULTED, COULD NOT RESET, RETURN TO RDU. PERFORMED BITE CHECK ON PRESSURE CONTROLLER FAULTED DUE TO NR 2 ENGINE BLEED VALVE CLOSED. (M) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N105ML' AND deregistration_id = 'N105ML-2001-05-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N105ML-2001-05-15/reports --- 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.