N944FD
Service difficulty reports · 130
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 = 'N944FD' AND registry_match = 'registration' 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 = 'N944FD' AND registry_match = 'registration' 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 FDEA202409041238Light · inoperativeL1 DOOR EMERGENCY EXIT LIGHT INOP. RELEASED FOR SERVICE PER MEL 33-51-01-01. ACFT OK FOR SERVICE.SDR FDEA202407251050Tach Generator · failedAFTER TAKEOFF, RECEIVED L ENG BLEED OFF EICAS RAN QRH 2.1.14 LEVELED AT FL360. NOTICED CABIN ALT AT 8000 WHILE 5 MIN CABIN ALT AT 9500 DESCENDED DOWN TO LOWER ALT IN DESCENT RECEIVED CABIN ALT HIGH MASTER WARNING AND EICAS MSG. RAN QRC THEN QRH 2.1.1 CONTISDR FDEA202302220332Engine · failedPDIS 944 79-01 0275 22FEB23 RSW OPEN U IN FLIGHT AT FL390 NOTICED R ENG OIL PRESS DISCREET LIGHT FLICKERING. ON EICAS NOTICED OIL QUANTITY 0, ALL OTHER ENGINE INDICATIONS APPEARED NORMAL. FOLLOWED QRH WHICH DIRECTED US TO REDUCE THROTTLE ANSDR FDEA202211042728Pan · gougedR1 DOOR EXTERIOR HANDLE PAN WORN REMOVED AND REPLACED R1 DOOR HANDLE PAN IAW DWG 141N6200 REV T AND AMM 52-11-13-02.SDR FDEA202211032725Wedge · delaminated#6 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 81-01-4SDR FDEA202211032724Wedge · delaminated#4 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4SDR FDEA202211032723Wedge · delaminated#3 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4SDR FDEA202211032722Wedge · delaminated#5 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-01-4SDR FDEA202211022713Floorbeam · corrodedMAIN CABIN FLOOR BEAM STA 1681 IS CORRODED ON THE AFT FACE AND LOWER SURFACE OF THE UPPER CAP AT APPROX RBL 48 ACCOMPLISHED FEDEX EA # F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL 5, RBL 48, CORRODED DAMAGE. ORIG SUBMISSION DATESDR FDEA202211022714Floorbeam · corrodedMAIN CABIN FLOOR BEAM IS CORRODED AT FASTENER HOLE BS 310 LBL 20 ACCOMPLISHED FEDEX EA # F-5310-T0371036 FUSELAGE - MAINFRAME - FLOOR BEAM TEE CAP, STA 310, LBL 20, CORROSION REPAIRSDR FDEA202211022712Panel · cracked#1 PYLON PANEL 434DR HAS A CORNER CRACKED REPAIRED #1 PYLON PANEL 434DR CRACKED CORNER WITH 350 DEGREE REPAIR IAW B757 SRM 54-50-70-2R FIG 201 REPAIR 1 SHEET 3, 51-40-02,51-70-04,54-50-70-0IAND AMM 51-24-02-7, 51-21-00/701, B757NDTM PART 1 51-01-01.SDR FDEA202210312701Fitting · corrodedMAIN CABIN - STA 324-345 RBL2 INTERCOSTAL IS CORRODED AT FLOOR PANEL HOLES REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW B757 DWG 141N5160 REV CD AND 141N5161 REV -SDR FDEA202210282687Stringer · crackedAFT CARGO COMPARTMENT STA 1680-1701 STR29R HAS CRACKED STINGER REMOVED CRACKED STINGER SECTION ON STA 1680 - 1701 STR29 R/H FABRICATED -1 HAT SECTION AND -2 FILLER INTALLED IAW B757 SRM 53-00-03-2RSDR FDEA202210282685Floorbeam · corrodedMAIN CABIN - ZONE 250 - STA 1681 FLOOR BEAM IS CORRODED ON LOWER SURFACE - LBL5 ACCOMPLISHED FEDEX EA #: F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL5, RBL48, CORROSION DAMAGESDR FDEA202210252660Web · corrodedMAIN CABIN FLOOR SUPPORT PLATE IS CORRODED AFT OF CABLES BS 340, LBL 27 REMOVED, FABRICATED AND INSTALLED NEW FLOOR WEB IAW B757 DWG 141N5170 REV CSDR FDEA202210242651Intercostal · corrodedMAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 25 - RBL 39 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW BAC DWG 141N5160 REV C. ORIG SUBMISSION DATE: 10/24/2022SDR FDEA202210242650Intercostal · corrodedMAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 4- RBL 23 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW B757-2 DWG 141N5160. ORIG SUBMISSION DATE: 10/24/2022SDR FDEA202210242652Floorbeam · corrodedMAIN CABIN FLOOR SUPPORT BEAM IS CORRODED UPPER SIDE AT NUTPLATE HOLE BS 344 LBL20 - LBL22 REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT BEAM ISW B757-2 DWG 141N5161 REV A AND 141N5170 REV CSDR FDEA202210242649Floor Panel · damagedMAIN CABIN FLOOR PANEL AT STA 480-500 LBL 45 IS DAMAGED REPAIRED FLOOR PANEL IAW B757SRM 53-00-50-2R REPAIR 1SDR FDEA202210242648Floorbeam · corrodedMAIN CABIN FLOOR BEAM IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES AND FWD EDGE IS GOUGED AND CORRODED BS 344 LBL0-LBL20 REPAIRED FLOOR BEAM IAW B757-2 SRM 53-00-51-2R REPAIR #10SDR FDEA202210242647Floor Panel · delaminatedMAIN CABIN ZONE 240 - FLOOR PANEL 242MCF IS DELAMINATED REPAIRED FLOOR PANEL 242 MCF IAW B757 SRM 53-00-50-2R, REMOVED AND INSTALLED INSERTS IAW B757 SRM 53-00-50-2RSDR FDEA202210222642Skin · damagedRIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER SURFACE HAS AREA OF BARE METAL REPAIRED #8 SLAT UPPER TRAILING EDGE LOWER SURFACE ARE OF BARE METAL IAW FEDEX EA# F-5750-T0370952SDR FDEA202210222641Wedge · delaminated#8 SLAT T/E WEDGE IS DISBONDED REPAIRED #8 SLAT T/E WEDGE DISBOND ON 3EA. AREA IAW FEDEX EA# F-5750-T0370952.SDR FDEA202210052470Panel · crackedRW LEADING EDGE PANEL BEHIND #7 SLAT IS CRACKED AT OB SPLICE AREA. REPAIRED RW LEADING EDGE PANEL BEHIND #7 SLAT IAW B757-200 SRM 57-41-02-2RFIG 201 SHEET 8 AND 51-70-07SDR FDEA202210052469Panel · damagedLH VERTICAL PANEL 322CL DAMAGED REPAIRED L/H VERTICAL STAB PANEL 322CL SKIN IAW B757-200 SRM 55-30-01-2R FIG 201 REPAIR 4 SHEET1 AND SRM 51-70-07-0G.SDR FDEA202011202924Drag Fitting · crackedTHE RT WING OUTBOARD DRAG FITTING HAS INDICATIONS OF DEFECTS ON THE NR 4 & NR 13 HOLE. THE NR 4 HOLE HAS INDICATION AT THE 3 O`CLOCK LOCKING AFT AND NR 13 HAS INDICATION ALSO AT THE 3 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLSDR FDEA202011202923Drag Fitting · corrodedTHE RT INBOARD DRAG FITTING UPPER SURFACE HAS CORROSION AT NR 3 AND NR 8 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLACED INBOARD FITTING.SDR FDEA202011202922Drag Fitting · crackedTHE RT WING INBOARD DRAG FITTING HAS INDICATIONS ON THE NR 3, NR 8 HOLE AND THE 3RD HOLE FROM THE BOTTOM THAT ATTACHES TO THE SPAR. THE 2 HOLES THAT ATTACH TO THE SKIN HAVE MULTIPLE SIGNALS AND UNABLE TO CLOCK POSITION. THE 3RD HOLE FROM THE BOTTOM THAT ATTASDR FDEA202011202921Drag Fitting · crackedTHE RT UPPER SKIN DRAG FITTING NR 3 AND NR 5 HOLES HAVE INDICATIONS OF DEFECTS NOTED. THE NR 3 HOLE HAS INDICATION AT THE 1 O`CLOCK LOOKING AFT. THE NR 5 HOLE HAS INDICATION AT THE 12 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINSDR FDEA202011202918Drag Fitting · corrodedTHE RT WING OUTBOARD DRAG FITTING UPPER SURFACE HAS CORROSION ON NR 4 AND NR 13 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR. REPLACED OUTBOARD FITTING.SDR FDEA202011192911Skin · dentedLH ENGINE PYLON IB SIDE ABOUT MID SECTION ON LWR FACE HAS DENT. COMPLIED WITH FEDEX EA. F - 5430-T0358210 P1 NACELLS / PYLON - SKIN /PLATES/ PANELS - LH ENGINE PYLON INBOARD SIDE SKIN PANEL REPAIR NEAR PPS 136. PERFORMED SATIFACTORY LEAK CHECK IAW B757 AMMSDR FDEA202011072791Frame · crackedTHE RT 1640 FRAME BY STR 14R LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING OUTBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT ALL WORK ACCOMPLISDR FDEA202011072790Frame · crackedTHE LT 1640 FRAME BY STR 14L LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING INBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT. ALL WORK ACCOMPLSDR FDEA2020040620689Reservoir · failedR1 DOOR EMERGENCY POWER RESERVOIR HAS NO PRESSURE. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR REF B757 AMM 52-11-30-4. OPS CHECK SATIS. A/C OK TO CONT SERVICE. RII BYSDR FDEA2019122313275Collar · inoperativeGUST LOCK ON L FWD ENTRY DOOR WILL NOT MOVE TO ALLOW DOOR TO CLOSE. REF MM 52-11-08-08, INSTALLED NEW HOLD OPEN LOCK COLLAR ON L1 DOOR. L1 DOOR HOLD OPEN LOCK COLLAR OPERATES NORMALLY. PART INSTALLED PN 10-N6008-1 / SN 20-024.SDR FDEA2019061741301Bottle · emptyFOUND POWER ASSIST RESIVOUR FOR L1 DOOR BLOWN. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE PER AMM 52-11-30-4-0 NOMENCLATURE-CYLINDER, EMERGENCY POWER RESERVOIR, /N 803300-35A, S/N 1394SDR FDEA2019022860509Hose · defectiveL HYD SYS PRESS LIGHT ILLUMINATED ON FINAL AFTER LANDING GEAR DOWN AND LOCKED AND FLAPS AT FINAL CONFIGURATION. FOLLOWED BY L HYD SYS PRESS AND L YAW DAMPER. CLEARED RUNWAY AFTER LANDING- MAINT TOW TO GATE . REMOVED AND REPLACED DEFECTIVE FLEX HOSE OSDR FDEA201811123187Shim · migratedRT PYLON UPPER AFT DRAG LINK SPAR FITTING SHOWS SIGNS OF SHIM MIGRATION. COMPLIED WITH EA F-5740-T0343112 PART 1. RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR.SDR FDEA201810303054Skin · crackedCRACK LIKE INDICATION WAS NOTED AROUND AND BELOW FASTENER DURING NDT INSPECTION OF REPAIR AREA AT BS 1360 APPROX 4 INCHES ABOVE STR 5L. STRIP/REMOVED PAINT AT MARKED AREA FOR FURTHER NDT INSPECTIONS OF THE AREA. COMPLIED WITH EA F-5330-T0343048 P1. FUSELAGE SKSDR FDEA201810283036Floorbeam · crackedSUB BEAM AT STA 580 IS CRACKED. TRIMMED ENTIRE UPPER FLANGE OF THE BS 580 FLOOR BEAM SPLICE. FABRICATED REPAIR ANGLE AND RADIUS STRAP AND INSTALLED IAW EA F-5310-T0343027 P-1.SDR FDEA201810263017Skin · corrodedCORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSISDR FDEA20181113017Skin · corrodedCORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSISDR FDEA201707282079Adc · malfunctionedAFTER TAKEOFF, LOST MULTIPLE AVIONICS, PILOTS ALTITUDE, AIRSPEED, RADIO ALTIMETER, AUTOTHROTTLES. FIRST OFFICER`S FLT DISPLAY WAS SIMILAR BUT REGAINED AIRSPEED, ALTITUDE, BUT NO AUTOTHROTTLES. LAST FLIGHT FAULTED ADC SYS L WITH FAULT CODES 110401, AND 13040SDR FDEA201707282078Landing Gear · malfunctionedAFTER TAKE OFF, PUT GEAR UP. GEAR RETRACTED. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR CAME DOWN. PUT GEAR DOWN FOR LANDING AND RECEIVED GOOD DOWN INDICATION. PERFORMED A BITE OF THE PSEU AND FOUND NO FAULTS ON THE BOX IAW AMM 32-09-06, STEP 4. E. JACKED AIRSDR FDEA201610013404Floorbeam · crackedSTUB FRAME BS 580 LBL 44-46 CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION REINFORCEMENT STUB FRAME IAW DWG 657N4311 REV - AND SRM 51-40-05-0G, 51-40-02-0G. MAJOR REPAIR.SDR FDEA201410173289Skin · delaminatedLEFT OTBD AFT FLAP UPSIDE OTBD END DELAMINATED. REPAIRED IAW EA F-5750-T0312494.SDR FDEA201409032431Windshield · crackedON CLIMB OUT FIRST OFFICERS R1 WINDOW BEGAN TO ARC. COMPLIED WITH QRH & WINDOW CRACKED AFTER COMPLETING CHECKLIST. LANDED AT NEAREST SUITABLE AIRPORT. R&R FIRST OFFICERS WINDSHIELD. COMPLIED WITH WINDOW HEATING SYS CHECK & WINDOW WIPER OPERATIONAL CHECK. SDR FDEA201212214349Slide · dislodgedL1 DOOR ESCAPE SLIDE FELL OFF OF DOOR. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHECKED NORMAL. ACFT OK TO CONTINUE.SDR FDEA201210293773Carriage · gougedNR 3 FLAP TRACK CARRIAGE OTBD LOWER FITTING GOUGED. COMPLIED WITH EA F-2750-154109 WINGS-LT INBD FLAP CARRIAGE ASSY-GOUGE ON ROLLER SUPPORT ASSY.SDR FDEA201209233412Sensor · dirtyTAXIING INTO POSITION FOR TAKE OFF, RECEIVED LEFT FWD ENTRY DOOR EICAS MESSAGE CAME ON INTERMITTENTLY DURING TAXI BACK TO GATE. INSPECTED ENTRY DOOR, FOUND GREASE, DIRT AND DEBRIS ON PROXMITY SWITCH, CLEANED AREA , OPERATED DOOR IAW AMM 52-11-01-6 SYS CHECKE
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