N559FE, cancelled Mar 2, 2024
Service difficulty reports · 138
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N559FE' AND deregistration_id = 'N559FE-2024-03-02' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N559FE' AND deregistration_id = 'N559FE-2024-03-02' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201908181932Power Supply · inoperativePREFLT EMERGENCY LIGHT TEST RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY, IAW AMM 33-51-01-4. OPS CHECKED GOOD, A/C OK FOR SERVICE.SDR FDEA2019082081933Battery Pack · inoperativePREFLT EMERGENCY LIGHT TEST RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY, REF AMM 33-51- 01-4. OPS CHECKS GOOD, A/C OK FOR SERVICE.SDR FDEA201908021793Line · disconnectedHYD 3 FAILED ENROUTE DUE TO LOSS OF ALL HYD IN SYS 3. QUANTITY 0.0 LOST IN CRUISE AT 340. FOUND AUTO PRIME AND BLEED HYDRAULIC LINE CHAFED THROUGH ON SUPPORT BRACKET IN NR 3 PYLON. AUTO PRIME, BLEED SYSTEM DETERMINED TO BE NOT ACTIVE ON THIS A/C AS LINE WSDR FDEA201902140414Trim Switch · inoperativeDURING T/OFF COULD NOT ENGAGE AUTOPILOT AT 500' AGL. ACCELERATING THROUGH 230KIAS ELEVATOR TRIM BECAME UNUSABLE. HAD TO DECELERATE TO 200 KIAS TO CONTROL PITCH DECLARED EMERGENCY RTB TO KMIA. DURING APPROACH AT LESS THAN 200 KIAS ELEVATOR TRIM BEGAN RESPONDINGSDR FDEA201802200444Control Cable · brokenL1 DOOR LOWER CABLE BROKEN. INSTALLED THE L1 DOOR LOWER AFT DOOR CONTROL CABLE. CABLE RIG AND OPS CHECKED GOOD IAW AMM 52-10-02-2.SDR FDEA201712113358Spar Cap · crackedL/W WING REAR SPAR AFT LOWER CAP HAS .400 IN. CRACK PROPAGATING AFT FROM FASTENER HOLE AT XORS 412. REPAIRED L/H REAR SPAR CAP REF EA 8-5710-T0336600 PARTS 1 - 4. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201711273311Skin · crackedRT HORIZ STAB DROOP ELEVATOR HAS A 1.5 CRACKED ON UPPER SKIN. CUT OUT DAMAGED AND INSTALLED REPAIR PER SRM 55-00-01 FIG 3 SHT 2 VOL 1.SDR FDEA201711223295Floorbeam · corrodedFWD CARGO COMP LT FLOORBEAM AT STA LBL 56 IS CORRODED. REPAIRED FLOOR BEAM IAW SRM 53-00-01 FIG 8 V1.SDR FDEA201711193284Skin · corrodedRT HORIZONTAL STABILIZER CENTER LOWER FARING (AJC7412-2) HAS NUMEROUS AREAS OF CORROSION AT LOWER SECTION UNDER ATTACH AREA AND SEALANT (MARKED) REPAIRED AREA PER SRM 51-21-01 VOL II.SDR FDEA201711193283Skin · corrodedLT HORIZONTAL STABILIZER LOWER FAIRING CORROSION ON SKIN AT LOWER AFT STABILIZER FAIRING (AJC7470-1) LOWER ATTACH AREA UNDER SEALANT TREATED AREA PER SRM 51-21-01 VOL II.SDR FDEA201711173256Stanchion · corrodedAFT FUSELAGE WASTE TANK BS 1970, CTR STANCHION AT THE BULKHEAD IS CORRODED. REMOVED AND REPLACE STANCHION SRM 51-31-01.SDR FDEA201711173255Attach Angle · corrodedAFT FUSELAGE WASTE TANK, BS 1970 UPPER PANEL ATTACH ANGLE CORRODED AT NUMEROUS FASTENERS AREA. REMOVED THE CORROSION IAW SRM 51-21-01, VOL 2. WITHIN LIMITS.SDR FDEA201711173287Floor Support · corrodedAFT CARGO COMPT, STA 1902, FLOOR SUPPORT CORROSION FROM APPROX LONGERON 45L TO 48R. CRACKED AND FLAKING METAL AROUND NUMEROUS NUTPLATES AT APPROX LONGERON 46R. (NOTE:PRIMARY STRUCTURE) REPAIR PER SRM 53-00-01 FIG 8 SHT 1 VOL 1SDR FDEA201711163312Flap · dentedRT I/B FLAP TOP SURFACE HAS A DENTED CREASE. REPAIRED PER SRM 57-10-00 FIG 85 VOL 1.SDR FDEA201711163285Stanchion · corrodedAFT FUSELAGE WASTE TANK STA 1970 CTR STANCHION AT BULKHEAD IS CORRODED. REPAIRED PER 51-21-01 VOL II.SDR FDEA201711163248Skin · crackedRIGHT LOWER WING SKIN AT THE FUEL ACCESS DOOR FWD INBOARD CORNER HAS A .400 INCH CRACK. REPAIRED THE SKIN IAW SRM 57-10-00, FIG 106, SHT 2.SDR FDEA201711143291Frame · crackedBS 1721, LONGERON 13R, FUSELAGE FRAME CRACKED. REPLACED THE FRAME SECTION IAW SRM 53-30-00, VL 1, PAGES 15-16, FIG 5, SHEETS 1-2, AND DWG AFA0019.SDR FDEA201711123333Doubler · dentedVERTICAL STAB LT SIDE DENTED JUST AFT OF ACCESS PANEL NR 373GL. REPAIRED VERTICAL STAB LT SIDE REF SRM 55-00-01 FIG 3 SHT 2 VOL I.SDR FDEA201711123332Doubler · dentedUPPER AT RUDDER, LT CENTER AREA GOUGED APX 1 INCH. REPAIRED UPPER AFT RUDDER LT SIDE REF SRM 55-00-01 FIG 3 SHT 3 VOL I.SDR FDEA201711113264Hinge · corrodedFOUND THE CARGO DOOR HINGE AND BACK UP STRUCTURE CORRODED. REPAIRED IAW SRM 51-21-01, VOL II.SDR FDEA201711103344Doubler · crackedL/H WING L/E LOWER SURFACE, CRACK NOTED AT FWD I/B CORNER OF FUEL ACCESS DOOR. MARKED DOT #1. CUT OUT CRACKED SKIN AND INSTALLED WING LEADING EDGE SKIN REPAIR REF. SRM 57-10-00 FIG.106 (SHEET 2) PAGE 509 VOL I.SDR FDEA201711083263Hinge · corrodedAFT CARGO DOOR HINGE CORRODE. REPAIRED IAW SRM 51-21-01, VOL II.SDR FDEA201711083262Skin · corrodedAFT CARGO DOOR CORRODED ON THE EXTERIOR SURFACE, BELOW THE DOOR HINGE. REPAIRED IAW SRM 51-21-01, VOL II.SDR FDEA201711083239Channel · corrodedCENTER CARGO LT CHANNEL AT SIDEWALL BASE IS CORRODED AT BS 1521, LBL 72. REMOVED AND REPLACED THE CHANNEL IAW SRM 53-31-01 VOL IISDR FDEA201705101384Link · failedDURING APPROACH, NLG INDICATION WENT FROM GREEN TO RED ON PRIMARY AND SECONDARY DISPLAY. FROM THAT POINT NLG DOWN INDICATION WAS INTERMITTENT. REMOVED AND REPLACED THE LOWER LOCK LINK ASSY IAW MM 32-00-01-4. REPLACED TARGET ASSY IAW MM 32-61-17-4. PERFORMSDR FDEA201705101383Target · detachedAFTER INITIAL LANDING GEAR RETRACTION, NLG DID NOT RETRACT, RED LIGHT IN PRIMARY AND SECONDARY DISPLAY. CYCLED GEAR DOWN THEN UP AGAIN. LANDING GEAR RETRACTED NORMALLY IAW QRH, AS INDICATED ON PRIMARY & SECONDARY DISPLAY. HYDRAULIC PRESSURES NORMAL THROUGSDR FDEA201607012207Actuator · failedNOSE GEAR DID NOT RETRACT ON INTIAL TAKE OFF. RAN QRH HAD RED UNSAFE NOSE GEAR INDICATION. ANOTHER AIRPLANE SAID NOSE GEAR WAS EXTENDED. WHEN GEAR HANDLE WAS PUT DOWN, NOSE GEAR IMMEDIATELY TURNED GREEN. FOUND NOSE GEAR UNLOCK CYLINDER BYPASSING. R & R NLSDR FDEA201603020786Bracket · looseAFTER TAKEOFF, MLG HANDLE WOULD NOT MOVE TO UP POSITION. RAN QRH & RAISED MLG HANDLE USING MLG HANDLE RELEASE BUTTON. NLG INDICATED UP, LT & RT MLG INDICATED, UNSAFE, RED ON MLG PANELS & CONFIG PAGE. RETURNED MLG DOWN, 3 GOOD INDICATIONS, CONTINUED TO DESTISDR FDEA201602290722Structure · twistedDURING EMER STOP SITUATION WITH SIDE LOADS ON ACFT NOSE ENOUGH TWIST WAS APPLIED TO ACFT TO CAUSE THE RT ACFT ENTRY DOOR TO INDICATE OPEN, EVEN THOUGH IT WAS CLOSED & ARMED. PERFORMED GVI OF RT MAIN ENTRY DOOR INSPECTION & CHECK IAW AMM 52-10-01-6. PERFORMESDR FDEA201602110503Unknown · malfunctionedUNABLE TO RAISE LG AFTER TAKEOFF. SEVERAL TRIES UNSUCCESSFUL. RAN QRH USING HANDLE REL BUTTON, WAS ABLE TO RAISE GEAR HANDLE. ALL ACFT SYSTEMS SHIFTED TO FLIGHT MODE. CHECKED CABLE RUN FROM COCKPIT TO CRANK ASSEMBLY UNDER PILOT AT PRESS BULKHEAD. CABLE ASDR FDEA201512154003Fitting · corrodedCAC STATION 1119, FRAME BETWEEN LONGERON 47 & 48, SHEAR CLIP IS EXFOLIATED. R & R SHEAR CLIP IAW DWG AAA7046.SDR FDEA201512133982Seat Track · wornMAIN DECK SEAT TRACK DAMAGED AT STATION 1381, LBL 45.5. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.SDR FDEA201512123980Skin · corrodedEXTERIOR FUSELAGE, STATION 1119, BELOW LONGERON 47, SKIN HAS EXFOLIATION CORROSION, APPROX 2" IN DIAMETER, COMPLIED WITH EA 8-5310-T0322104.SDR FDEA201512093953Frame · crackedLOWER BILGE STATION 595 RT, AT LONGERON 39, ACA6044-65 T CAP FRAME CRACKED .300" LONG. REPAIRED CRACKED T CAP CUTTING OUT CRACK & REINFORCING T CAP WITH STRAPS IAW EA 8-5310-T0321525. REPAIR HAS BEEN CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201512073943Frame · crackedCAC RT STATION 1156, UPPER CORNER FRAME INNER VIEW ONE SHEARED 1/4" FASTENER & CRACK RUNNING THROUGH ANOTHER 1/4" FASTENER. CRACK RUNS ENTIRE LENGTH OF FRAME & IT APPEARS FRAME HAS BEEN SHIFTING. FRAME REPAIR HAS NOT BEEN ACCOMPLISHED IAW SRM 53-30-00, NO CUSDR FDEA201512073942Frame · crackedINSIDE CAC COMPARTMENT, RT SIDE AT STATION 1156, PREVIOUS REPAIR FUSELAGE FRAME AEAO159 HAS AN ADDITIONAL CRACK AT THE TOP ROW FASTENERS. CRACK ALSO EXTENDS INTO THE RADIUS & OTBD OF T LEG OF FITTING, APPROX 1 INCH. REPAIRED FUSELAGE FRAME IAW EA 8-5310-T032SDR FDEA201512023852Web · crackedRIGHT WING, INTERNAL WEB CRACKED AT STATION XORS 402 & APPROX STRINGER 39. REMOVED DOUBLER FROM RT WING INTERNAL WEB AT STATION XORS 402 & APPROX STRINGER 39 & REPAIRED IAW EA 8-5700-T0321488.SDR FDEA201512013841Bulkhead · crackedLEFT STATION 595, PRESS BULKHEAD WEB HAS A 1.4 INCH CRACK FROM THE EDGE OF THE WEB EXTENDING THROUGH ONE FASTENER AT STATION X=78 & Z=87. COMPLIED WITH EA 8-5310-T0321453.SDR FDEA201512013839Bulkhead · crackedLEFT STATION 595, PRESS BULKHEAD T CAP AT LONGERON 39L, HAS A CRACK THROUGH THE VERTICAL & HORIZONTAL LEGS. CUT & REMOVED SECTION OF THE 595 T CAP FROM LONGERON 35L - 44L. COMPLIED WITH EA 8-5310-T0321379.SDR FDEA201511203726Skin · corrodedCENTER ACCESSORY COMPARTMENT, CORROSION & EXFOLIATION ON & UNDER FINGER DOUBLER, BETWEEN LONGERONS 47L & 48L. COMPLIED WITH EA 8-5330-T0321798 PART 1.SDR FDEA201511183704Skin · damagedNUMBER 2 FAN COWL LAND, LT SIDE, SKIN HAS MINOR DAMAGE. R & R SKIN IAW DWG AJC7415.SDR FDEA201511063508Seat Track · damagedMAIN DECK, SEAT TRACK DAMAGED, STATION 1386, LBL 45.50. R & R SECTION OF SEAT TRACK AS REQUIRED.SDR FDEA201511063506Seat Track · damagedMAIN CABIN, STATION 765, LBL 47 SEAT TRACK DAMAGED & NEEDS TO BE REPLACED. REPLACED SECTION OF SEAT TRACK IAW SRM 53-70-0-0 FIG 1 SHT 3.SDR FDEA201509202903Strip · damagedRAMP OFF LOAD CREW REPORTED, DAMAGE TO THE LOWER FWD CARGO COMPARTMENT CEILING STRUCTURE, AT THE AFT INBD SIDE OF THE DOOR MOTOR. R & R METAL TRIM STRIP ATTACHMENT TO LINER IAW SRM 51-31-01 VOLUME II.SDR FDEA201509012731Skin · crackedEVIDENCE OF A SKIN CRACK ON LT WING INBD FWD RADIUS OF SLAT DRIVE MECHANISM DOOR CUT OUT CONFIRMED BY NDT HFEC. VERIFIED CRACK TO BE 3/4 - 1". COMPLIED WITH NTM REF 20-30-00-PT6 WILL BE REQUIRED TO RE-CHECK AFTER S/M REMOVES METAL PRIOR TO INSTALLING FILLER.SDR FDEA201508042463Light · inoperativeEMERGENCY LIGHT PREFLIGHT TEST LEVEL 1 ALERT, EMERGENCY LIGHT BATTERY LOW. RELEASED FOR SERVICE IAW MEL 33-50-02, CATEGORY C EXPIRATION 13 AUG 15. EMERGENCY LIGHTS INOPERATIVE. ITEM PLACED ON MEL.SDR FDEA201507222331Warning Message · false activationON EMER LIGHTS TEST MSG DISPLAYED, EMER BAT 1 LOW. PERFORMED OPERATIONAL CHECK OF EMER LIGHT & POWER SYS. OPERATIONS CHECKED GOOD.SDR FDEA201502070470Power Supply · inoperativeDURING EMER LIGHTS TEST, EMER LT BATT 1 LOW, MSG DISPLAYED. REPLACED EMER LIGHTING BATTERY POWER SUPPLY IAW MM 33-51-01-4. OPERATIONS CHECKED GOOD.SDR FDEA201502040441Warning Light · false activationEMERGENCY LIGHTS WOULD NOT TEST. RECEIVED AN EMERGENCY LIGHT NR 1 BATTERY LOW INDICATION. PERFORMED SEVERAL EMERGENCY LIGHTING BATTERY POWER SUPPLY TESTS. NOFAULTS NOTED. OKAY FOR SERVICE.SDR FDEA201412114108Unknown · odorCOCKPIT SMELLED LIKE SOMEONE HAD BEEN SMOKING IN THE ACFT FROM PREFLIGHT THROUGH POST FLIGHT. RAN NR 1 ENGINE. OPERATED NR 1, 2 & 3 AIR CONDITIONING UNITS. NO ABNORMAL ODOR OF SMOKE WAS NOTED.
Back to N559FE, cancelled Mar 2, 2024