N990FD
Service difficulty reports · 143
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 = 'N990FD' 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 = 'N990FD' 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 FDEA202512122239Torque Tube · damagedWHEN CONFIGURING AFTER START SETTING FLAPS TO 5 RECEIVED LE SLAT DISAG EICAS. UPON INSPECTION FOUND THE CONTROL CABLE INPUT FOR THE LE SLAT PDU BROKEN AND FRAYED. THE CABLE IS IDENTIFIED AS LESA IAW FIM 27-81, FAULT TREE 803, FIGURE 104, & IPC 27-51-25-0SDR FDEA202511112160Skin · delaminatedLH HORIZONTA STABILIZER UPPER SKIN HAS POSSIBLY DELAMINATION STAB STA 104.248 AREA APPLIED PERMANENT REPAIR AT LH HORIZONTAL STABILIZER UPPER SKIN I.A.W B757 SRM 55-10- 01-1A, TABLE I, NOTE 'A' AND "I", FIG 101, SHEET 2, I.A.W B757 SRM 51-70-10-2RSDR FDEA202511112159Skin · dentedRH HORIZONTAL STABILIZER LOWER SURFACE HAS TWO DENTS STAB STA 176.249 AREA TWO DENTS FOUND OUT OF LIMITS AT RH HORIZONTAL STABILIZER LOWER SURFACE STAB STA 176.248. AND APPLIED PERMANENT REPAIR I.A.W B757 SRM 55-10-01-1A, TABLE I, NOTE 'I' FIG 101, SHEET 3SDR FDEA202511082146Stringer · corrodedLH OUBD W/W TUNNEL WAS FOUND STRINGER S-23LH AT STA 399.5 (TUNNEL BEGINING) WITH CORROSION CORROSION FOUND OUTSIDE PERMITTED LIMITS ON S-23 LH STA 399.5 IAW B757 SRM 53-00-03-1A, STRINGER SECTION WAS FABRICATED AND REPLACED IN S23 LH BETWEEN STA 365.25 TOSDR FDEA202511062138Skin · gougedL/H WING OUTB AFT FLAP UPPER SKIN MIDDLE SECTION WITH GOUGE. GOUGE WITH CRACK AT L/H WING OUTB AFT FLAP UPPER SKIN MIDDLE SECTION WAS REPAIRED IAW B-757 SRM 57-53-01-2R AND SRM 51-70-04-0GSDR FDEA202511062137Skin · gougedL/H WING OUTB AFT FLAP, UPPER SKIN INB SECTION WITH GOUGE. GOUGE WITH CRACK AT L/H WING OUTB AFT FLAP, UPPER SKIN INB. SECTION WAS REPAIRED IAW B-757 SRM 57-53-01-2R AND SRM 51-70-04-0GSDR FDEA202511062136Skin · gougedRIGHT OTBD FLAP TE AFT FLAP UPPER SURFACE WITH 02 EA GOUGES. GOUGES REPAIRED IAW SRM 57-53-01-2R AND SRM 51-70-17-0G.SDR FDEA202509231767Lamp · failedR1 SLIDE LIGHT WILL NOT ILLUMINATE. IAW AMM 52-10-00-5 RELAMPED. CKD OK.SDR FDEA202502070191Lens · brokenON SERVICE CHECK FOUND EMERGENCY EXIT LIGHT HOUSING BROKEN ABOVE R1 DOOR. R/R R1 DOOR EMERGENCY EXIT SIGN COVER AND OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. REF B757 AMM 33-51-01-2.SDR FDEA202412021761Collar · damagedL1 HOLD-OPEN LOCK COLLAR BROKEN. AMM: 52-11-08-8 REMOVED AND REPLACED HOLD-OPEN LOCK COLLAR PER B757 AMM 52-11-08-8. OPS CK GOOD. A/C OK TO CONTINUE.SDR FDEA202411011626Unknown · unknownINFLIGHT EMERGENCY DECLARED TO GET PRIORITY HANDLING IN ORDER TO LAND AT KRNO DESPITE A RAMP CLOSURE DUE TO TFR FOR VIP MOVEMENT BEFORE ACHIEVING EMERGENCY FUEL STATE OF 4400 POUNDS. EMERGENCY DECLARED. NO MAINTENANCE ACTIONSDR FDEA202312141939Frame · crackedCRACK FOUND ON AFT SIDE OF T-SUPPORT CLIP BTWN STR-14L AND STR-15L ON FRAME 1640 LH FUSELAGE-MAINFRAME-STA 1640 FRAME SPLICE REPAIR BETWEEN STRINGER I-9F AND S-20L-EO F-5310-E0367020A P1 CRACK INDICATIONS REPAIR-PARTIAL FRAME REPLACEMENT. ACCOMPLISHED REPSDR FDEA202312051908Floorboard · damagedZONE 220 COURIER FLOORBOARD 222MAF DAMGED FABRICATED ZONE 220 COUREIR FLOORBOARD 222MAF ON VTMAE TRAVELER # T23/1717925 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202312051907Floorboard · damagedZONE 220 COURIER FLOORBOARD 221MBF DAMGED FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VTMAE TRAVELR # T23/1717921 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202312051906Floorboard · damagedZONE 220 FLOORBOARD 222AF DAMAGED FABRICATED ZONE 220 FLOORBOARD 222AF ON VTMAE TRAVELR # T23/1717922 IAW DWG SRZ-25- 005 REVISION R, MAJOR REPAIRSDR FDEA202312051905Floorboard · damagedZONE 220 COURIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221BF ON VTMAE TRAVELER # T23/1717928 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIRSDR FDEA202312051904Floorboard · damagedZONE 220 COURIER FLOORBOARD 221AF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221AF ON VTMAE TRAVELER # T23/1717926 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202303310538Stringer · damagedPUNCTURE DAMAGE TO FUSELAGE AFT OF LOWER AFT CARGO DOOR. DAMAGE IS LOCATED FROM APPX FS 1650R-1680R, BETWEEN STR 22-23R. REMOVED FASTENERS AS NEEDED REF B757 SRM 51-40-02. REFERENCE E.A. # F-5310-T0373827. REF : SRM 53-00-01-2R TABLE 206/REPAIR 28 REPSDR FDEA202207121711Stator · failedAT FL 390 LEFT ENGINE FLAMED OUT. ALL ENGINE INDICATIONS LOOKED NORMAL EXCEPT FUEL FLOW WAS 0. OIL PRESSURE STILL REMAINED APPROXIMATELY 13PSI WHEN SHUTDOWN. NO VIBRATIONS NO OTHER ABNORMAL INDICATIONS. WE ATTEMPTED TO RESTART WITHIN IN A DESCENTSDR FDEA202205051127Gust Lock · crackedFOUND L1 DOOR GUST LOCK BROKEN DURING PREFLIGHT. ENT BY: MEL 05MAY22 23:43 BWI U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 08MAY22 "MEL 52-11-01-A: L1 DOOR - INOP." REMOVED DAMAGED GUST LOCK PIECES TO ALLOW DOOR TO BE CLOSSDR FDEA202112073041Skin · noneLEFT WING INBOARD MAIN FLAP UPPER SURFACE HAS 1 DENT REPAIRED LEFT WING INBOARD MAIN FLAP UPPER SURFACE SKIN IAW B757 SRM 57-53-01-2R AND B757 SRM 51-70-10-2RSDR FDEA202112063025None · cracked#2 PYLON FAIRING 441AT HAS CRACKED COMPOSITE ON THE AFT UPPER EDGE. ACCOMPLISHED A PERMANENT REPAIR TO THE #2 PYLON FAIRING 441AT CRACKED COMPOSITE ON THE AFT UPPER EDGE IAW B757 SRM 54-51-70 FIG 201 SHEET 1 AND EA F-5451-T0365702-P1 PYLON STRUCTURE-TAIL PSDR FDEA202112063024None · damaged#1 PYLON FAIRING 431AT HAS COMPOSITE DAMAGE AT OUBD AFT ATTACH HOLE.. ACCOMPLISHED PERMANENT REPAIR TO #1 PYLON FAIRING 431AT COMPOSITE DAMAGE AT OUTBD AFT ATTACHMENT HOLE IAW B757SRM 54-51-70 FIG 201 SHEET 1 AND EA F-5451- T0365724-P1 PYLON STRUCTURE TAILPSDR FDEA202112022981None · delaminatedLH WING MAIN FLAP INBD SIDE, EXISTING UPPER SKIN REPAIR IS DISBONDING AT APPROX WS 175. REPAIRED LH WING INBD MAIN FLAP I/B SIDE UPPER SURFACE PREVIOUS REPAIR IAW B757 SRM 57-53-01 FIG 201 SHEET 2, 51-70-10-2R, 51-40-02 WITH A PERMANENT REPAIR.SDR FDEA202112012955Skin · noneR4 CABIN SVC DOOR EXTERIOR SURFACE IS CREASED VERTICALLY AT THE AFT LOWER CORNER OF THE DOOR APPROX. 2.25" FWD. OF THE AFT EDGE OF THE DOOR REPAIRED R4 DOOR EXTERIOR SURFACE DENT IAW B757 SRM 52-10-01-2R, REP. 7 AND FEDEX EA# F-5210- T0365572-P1, RELEASE DASDR FDEA202111302953Stringer Splice · corrodedAFT CARGO , STRINGER SPLICE CORRODED AT STA 1620 LBL28 REMOVED CORROSION ON STRINGER SPLICE IAW B757-200 SRM 53-00-03-1A . ORIGINAL MAT. THICKNESS IS .100 , MAT. REMOVED .004 , REMAINING THICKNESS IS .096 . IN LIMITS IAW B757-200 SRM 53-00-53 DETAIL I FIG SDR FDEA202111302951Skin · wornL/H WING, OUTBD MAIN FLAP, UPPER SKIN HAS WEAR MARKS AT APPROX. WS 425 REPAIRED THE L/W OUTBD MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01-2R, FIG. 201, SHT. 3, AND SRM 51-70-10-2R.SDR FDEA202111262935Stringer · corrodedEXTERIOR FUSELAGE SKIN IS BUCKLED BETWEEN FASTENERS ON S-28L @ STATION 1468 AFTER FURTHER EVALUATION, "BUCKLE" IN SKIN FOUND TO BE TRAPPED FOD BETWEEN THE SKIN & STRINGER 28L NO DAMAGE NOTED TO SKIN, ONLY STRINGER. REPAIRED STRINGER 28L IAW FEDEX EA # F-5310SDR FDEA202111222921Skin · corrodedAFT LOWER VHF DOUBLER & TRIPLER HAVE CORROSION. REMOVED AND REPLACED REPAIR DOUBLER & TRIPLER FROM STA 1460 - 1480, S-29R - S-30 IAW FEDEX EA # F-5330-T0365525SDR FDEA202111112823Skin · noneEXTERNAL FUSELAGE HAS PROTRUDING DENT BETWEEN STA 1600 - STA 1620, S-24R - S-25R REPAIRED DENT IAW FEDEX EA # F-5330-T0365574-P1, RELEASED NOV 24, 2021 TITLED " FUSELAGE - PLATES & SKINS - STA 1600 - 1620, S-24R - S-25R, SRM REPAIR DEVIATION."SDR FDEA202111112821Skin · dentedEXTERNAL FUSELAGE SKIN HAS PROTRUDING DENT BETWEEN STATION 540 - 560, S24L - S25L REPAIRED FUSELAGE SKIN IAW B757 SRM 53-00-01-2R, FIGURE 201, REPAIR NO.7SDR FDEA202111082796None · crackedSTATION 1640, S-14R, LOWER INBD & OUTBD TEE CLIP ATTACHED FASTENERS HAVE CRACK INDICATIONS. ACCOMPLISHED AMOC REPAIR IAW FEDEX EA NO. F-5310-T0365342-P1SDR FDEA202106301621Adc · failedON TAKEOFF ROLL DURING 80KT CHECK, FO AIRSPEED INDICATION MALFUNCTIONED. CONTINUED ON CAPT INSTRUMENTS. MESSAGES: IAS DISAGREE, MACH/SPEED TRIM, & RUDDER RATIO. ON SHUTDOWN, ELEV ASYM STATUS MESSAGE. COMPLIED WITH QRH. FO AIRSPEED INCREASED STEADILY FRSDR FDEA202105191311Probe · failedPDIS 990 30-30 7688 19MAY21 MEM FACT U LOGPAGES:2903863 TAT PROBE AND ASSOCIATED EICAS MSG ON CLIMB OUT, EMERGENCY DECLARED APON LANDING SHGN 19MAY21 19:10 MEM U REFERENCE WDM 34-12-11, 34-12-12 & 30-33-11. DURING DISASSEMBLY OF CONNECTORSDR FDEA202105041101Gust Lock · brokenL1 DOOR GUST LOCK BROKEN. FACT 04MAY21 19:49 MEM U REMOVED AND REPLACED GUST LOCK ON L1 DOOR IAW AMM 52-11-08-8. OK FOR SERVICE.SDR FDEA202008252024Controller · failedCABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH NR 1 AND 2 AUTO PRESSURE CONTROLLERS PER MM 21-31-02-4, BOTH OPS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.SDR FDEA202008131878Clamp · out of adjustCABIN ALT WARNING AT FL 370. CABIN ALT WARNING AT FL 370 FOUND #1 PACK SUPPLY DUCT AT THE CHECK VALVE ( FWD LEFT PACK BAY) ORANGE SLEEVE AND CLAMPS LOOSE AND NOT SECURED WITH LARGE AIR LEAK. READJUSTED DUCT SLEEVE AND SECURED CLAMPS AND ACCOMPLISHED LEASDR FDEA202008111870Controller · failedPDIS 990 21-30 7143 11AUG20 SGF FACT U. CABIN ALTITUDE WARNING AT FL 340. FACT 12AUG20 00:20 SGF U. REMOVED AND REPLACED BOTH NR 1 AND NR 2 AUTO PRESSURE CONTROLLERS, PER MM 21-31-02-4. BOTH OPERATIONS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHASDR FDEA2020082511870Controller · failedCABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH NR 1 AND 2 AUTO PRESSURE CONTROLLERS IAW MM 21-31-02-4, BOTH OPS CHECKED GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.SDR FDEA2020081411870Controller · malfunctionedCABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH #1 AND #2 AUTO PRESSURE CONTROLLERS IAW MM 21-31-02-4, BOTH OPS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.SDR FDEA201912233284Floor Support · corrodedMAIN DECK BETWEEN STA 700-720 RBL 60 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 700-720 RBL 60 IAW SRM 51-10-02. 100% MAT LOSS FOUND OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT SDR FDEA201912233283Floor Support · crackedMAIN CABIN BETWEEN STA 680-700 RBL 60 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 680-700 RBL 60 IAW SRM 51-10-02. FOUND TO BE CRACKED OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT IAW SSDR FDEA201912233286Floor Support · bentMAIN DECK STA 1055 BETWEEN RBL 24.75 - RBL 45.5 FLOOR SUPPORT BENT. FOUND FLOOR SUPPORT PLATE TO BE OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT PLATE IAW SRM 51-40-02, 51-40-05 AND DWG 144N5070 SDR FDEA2019122323279Crease Beam · corrodedMAIN DECK BETWEEN STA 1600-1630 IB CREASE BEAM CORRODED RT SIDE. REMOVED CORR ON CREASE BEAM STA 1600-1630 RBL 60 IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-13-1A FIG 101. REMOVED SECTION OF CREASE BEAM, FABRICATED AND INSTALLED NEW SECTION AND REPSDR FDEA2019122323280Floor Support · corrodedFWD WET AREA BETWEEN STA 324-345 LBL 39 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 324-345 LBL 39 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-SDR FDEA201912203273Shear Tie · corrodedAFT CARGO PIT BELOW FLOOR STA 1280 FRAME SIDE BOTTOM SHEAR TIE BELOW RT TRANSITION FLOOR PANEL CORRODED 1SQ IN. REMOVED CORROSION ON SHEAR TIE AT AFT CARGO STA 1280 BELOW RT TRANSITION PANEL. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-OG AND SRM 53-00-07-1A SDR FDEA2019121323236Panel · crackedRT WING NR 9 SLAT OB MAIN TRACK LOWER COVER PANEL EVIDENCE CRACK. COMPLIED WITH EA F-5750-T0351385 P1. WINGS - FLIGHT SURFACES - SLAT NR 9 COVE PANEL- LOCAL FABRICATION AND REPLACEMENT.SDR FDEA2019121323229Tee Fitting · corrodedMAIN DECK BETWEEN STA 900 - 1040 LBL 45.5 T CHORD CORRODED. REMOVED CORROSION ON MAIN DECK STA 900 TO 1040 LBL 45.5 TEE CHORD IAW SRM 51-40-02-OG, EVALUATED DAMAGE AREA ORIG MAT .090",MAT REM .067", MAT LOSS .023" FOUND TO BE OUT FO LIMITS IAW SRM 53-00-51-1ASDR FDEA2019121323233Skin · gougedRT WING OB FLAP L/E HAS GOUGE. BLENDED GOUGE FOUND AREA OUT OF LIMITS. RT WING O/B FLAP L/E SKIN IAW SRM 57-53-01-1A FIG 101 DET I, REMOVED EXISTING REPAIR SKIN PLATE IAW SRM 51-40-02-OG. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SKIN REPAIR PART IAW SSDR FDEA2019121313224Crease Beam · corrodedMAIN DECK LT IB CREASE BEAM BETWEEN STA 900 - 1040 CORRODED. REMOVED CORROSION ON CREASE BEAM LT SIDE AT STA 900 TO STA 1040 IAW SRM 51-10-02-OG, ORIGINAL MAT .070",REM MAT .059", MAT LOSS .011", EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A FI
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