N797FD
Service difficulty reports · 113
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 = 'N797FD' 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 = 'N797FD' 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 FDEA202404160464Warning Light · false activationL FWD ENTRY DOOR EICAS MESSAGE WHILE TAKING THE RUNWAY. MESSAGE APPEARED TWO MORE TIMES DURING TAXI. DID NOT NOTICE AN OVERHEAD PANEL LIGHT. LEFT DOOR WAS NOT USED ON THIS FLIGHT. OPENED ACCESS PANEL FOR S10094 AND PERFORMED VISUAL INSPECTION OF LEFT SDR FDEA202402040136Transmission · wornON APPROACH TO RWY 27 RECEIVED TE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 25. WENT AROUND, RAN QRH, AND LANDED ON 36C WITHOUT INCIDENT. AMM: 27-51-11-4 AMM: 27-51-06-4 FOUND L/H I/B FLAP TRANSMISSION TRIPPED AND BALLSCREW KNIFE EDGED. REMOVSDR FDEA202209122313Deck Plate · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA 1695 AT APPROX LBL 8 REPAIRED AFT DECK PRESSURE PLATE CORROSION, UPPER SURFACE @ STA 1695, LBL 8 IAW FEDEX EA F-5310-T0370248, RELEASED SEP 08, 2022, TITLED" FUSELAGE - MAINFRAME - AFT DECK PLATE, SDR FDEA202209122312Deck Plate · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA 1689 AT APPROX LBL 8 REPAIRED AFT DECK PRESSURE PLATE CORROSION UPPER SURFACE @ STA 1689, LBL 8 IAW FEDEX EA F-5310-T0370248-P1, RELEASED SEP 08, 2022, TITLED " FUSELAGE - MAINFRAME - AFT DECK PLATSDR FDEA202209122311Deck Plate · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA 1684 AT APPROX LBL 8 REPAIRED AFT DECK PRESSURE PLATE CORROSION UPPER SURFACE @ STA 1684, LBL 8 IAW FEDEX EA F-5310-T0370-P1, RELEASED SEP 08, 2022, TITLED "FUSELAGE - MAINFRAME - AFT DECK PLATE STSDR FDEA202209122302Seat Track · crackedMAIN CABIN SEAT TRACK SUPPORT INBD FLANGE IS CRACKED AT FLOOR PANEL FASTENER HOLE AT APPROX. STA 682 , RBL 44 REMOVED AND REPLACED SEAT TRACK SUPPORT AT MAIN CABIN AT APPROX. STA 640 TO STA 740 RBL 44 IAW VTMAE DRAWING 3458 , B757-200 SRM 51-40-02 , BAC DSDR FDEA202209112285Web · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA1684 AT APPROX LBL16. REPAIRED AFT PRESSURE DECK WEB CORROSION ON UPPER SURFACE APPROX STA 1684, LBL16 REF EA F-5310-T0370248-P1 REV A FUSELAGE-MAINFRAME-AFT DECK PLATE-STA1681- 1720-LBL20-RBL45-CORRSDR FDEA202209102282Web · corrodedMAIN CABIN FLOOR STRUCTURE HAS CORROSION AROUND FASTENER HOLE STATION 600, LBL 53 REPAIRED MAIN CABIN FLOOR STRUCTURE AT STA 580 AND STA 600, LBL 53 IAW FEDEX E.A. F- 5310-T0370288-P1, TITLE: FUSELAGE - MAINFRAME - SHEAR WEB, STA 520, 580, 600, LBL 53, CORRSDR FDEA202209102281Web · corrodedMAIN CABIN FLOOR STRUCTURE HAS CORROSION AT STA 520, LBL 53 REPAIRED MAIN CABIN FLOOR STRUCTURE AT STA 520, LBL 53 IAW FEDEX E.A. F-5310-T0370288- P1, TITLE: FUSELAGE - MAINFRAME - SHEAR WEB, STA 520, 580, 600, LBL 53, CORROSION.SDR FDEA202209072243Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1694 AT APPROX RBL 17 REPAIRED CORROSION ON AFT DECK PRESSURE PLATE UPPER SURFACE APPROX STA 1694, RBL7. REF FEDEX EA F-5310-T0370248-P1REV. A. FUSELAGE-MAINFSDR FDEA202209072242Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1690 AT APPROX RBL10 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX. STA1690, RBL 10. REF FEDEX EA F-5310-T0370248-P1 FUSELAGE-MAINFRAME-ASDR FDEA202209072241Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS COPRRODED ON THE UPPER SURFACE AT APPROX STA 1690 AT APPROX RBL 26 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX STA1690, RBL26 REF FEDEX EA F-5310-T0370248-P1. FUSELAGE-MAINFRAME-ASDR FDEA202209072240Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1714 SPANNING VETWEEN APPROX RBL31 TO RBL 38 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPER SURFACE APPROX STA1714 RBL31-RBL38 REF FEDEX EA F-5310-T037024SDR FDEA202209072239Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1699 AT APPROX RBL 15 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX STA 1699, RBL15. REF FEDEX EA F-5310-T0370248-P1. FUSELAGE-MAINFRAME-SDR FDEA202209072238Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE SPANNING BETWEEN APPROX STA 1686 AND STA 1699 AT APPROX RBL 9 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX STA 1686- 1699 REF FEDEX EA F-5310-T0370248-SDR FDEA202209072237Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1714 SPANNING BETWEEN APPROX LBL3 TO RBL 18 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX 1714 LBL3- RBL18. REF FEDEX EA F-5310-T0370248-PSDR FDEA202209072236Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1683 AT APPROX RBL 36 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX STA 1683, RBL36. REF FEDEX EA F-5310-T0370248-P1 FUSELAGE-MAINFRAME-ASDR FDEA202209072235Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE AFT DECK PRESSURE PLATE IS CORRODED ON THE UPPER SURFACE AT APPROX STA 1690 AT APPROX RBL15 REPAIRED AFT DECK PRESSURE PLATE CORROSION ON UPPER SURFACE APPROX STA1690, RBL15. RE FEDEX EA F-5310-T0370248-P1 FUSELAGE-MAINFRAME-AFT SDR FDEA202209062220Floor Panel · damagedMAIN CABIN FLOOR PANEL 251MXF HAS SEVERAL BROKEN AND SPINNING INSERTS REMOVED AND REPLACED DAMAGED INSERTS ON FLOOR PANEL 251MXF IAW B757 SRM 53-00-50- 2R, REPAIR 2, PARA. 4.B. AND FIG. 203, SHEET 1. ORIG SUB DATE: 9/6/2022SDR FDEA202209062217Floor Panel · damagedMAIN CABIN FLOOR PANEL 252MWF HAS SEVERAL BROKEN AND SPINNING INSERTS REMOVED AND REPLACED DAMAGED INSERTS ON FLOOR PANEL 252MWF IAW B757 SRM 53-00-50- 2R, REPAIR 2, PARA. 4.B. AND FIG. 203, SHEET 1: ORIG SUB DATE: 9/6/2022SDR FDEA202209052206Skin · gouged(AD RELATED) LH OB FLAP LE PREVIOUS REPAIR IS GOUGED AT OB SIDE OF REPAIR REPLACED DOUBLER IAW FEDEX EA F-5750-T0355303-P1, RELEASED JUL 24, 2020, TITLED "WINGS - FLIGHT SURFACES - LH OB MAIN FLAO LE PREVIOUS REPAIR. ORIG SUB DATE: 9/6/2022SDR FDEA202209042194Skin · dentedL/H WING INBD FWD FLAP LOWER SURFACE HAS MULTIPLE DENTS THROUGHTOUT. REPAIRD L/H WING INBD FLAP LOWER SURFACE DENT A AND DENT C IAW B757 SRM 57-53-01- 2R FIG 201 REPAIR 1 SHEET 2 AND 51-70-10-2R-2. ORG SUB DATE: 9/6/2022SDR FDEA202209022145Crease Beam · corrodedMAIN CABIN STA 1602 AND RBL 64, CREASE BEAM INBD CHORD HAS CORROSION AT NUT PLATE HOLE REPAIRED THE MAIN CABIN RBL 64 CREASE BEAM INBD CHORD AT STA 1602 IAW FEDEX E.A. F- 5310-T0370357-P1, TITLE: FUSELAGE - MAINFRAME - CREASE BEAM, STA 1602, RBL 64, CORROSDR FDEA202209012137Angle · crackedRMLG W/W WING TO BODY SUPPORT SUB-STRUCTURAL CLIP IS CRACKED AT THE CORNER OF THE CUTOUT AT STA 1100 REMOVED & REPLACED CLIP IAW BAC DWG 149N7552, SHEET 1, REVISION F.SDR FDEA202209012136Skin · dentedLW I/B FLAP UPPER PANEL HAS SEVERAL DENTS AFT OF #6 SPOILER. REPAIRED 2 EACH DENTS #5 AND #6 DENTS ON STEP 9 AT THE LEFT WING I/B MAIN FLAP UPPER SKIN BY REMOVING DAMAGE, FABRICATING FILLERS AND DOUBLER, CLEANING AND PREPPING SURFACE, LAYING UP PARTS AND CSDR FDEA202208312116Seat Track · corrodedMAIN CABIN , SUPERNUMERARY SEAT TRACK HAS CORROSION , STA 345 TO STA 377 , LBL 7 REMOVED AND REPLACED SEAT TRACK IAW VTMAE DRW-3VKJ5 # 3470 , B757-200 SRM 53-10-52-01 AND SRM 51-40-02SDR FDEA202208302106Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED, BS 350 TO 360, RBL 10 REMOVED CORROSION ON FLANGE AND FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A, A.D. 1, FIG. 101, SHT. 4, DETAIL VII. ORIGINAL MATERIAL THICKNESS IS .100", REMAINING THICKNESS IS .053", .047" WASSDR FDEA202208282088Skin · wornLW IB FLAP UPPER OB REPAIR AREA IS WORN AT OB UPPER SKIN. REPAIRED LW IB FLAP UPPER SKIN WITH PERMENAT REPAIR IAW B757 SRM 57-53-01-2RFIG 201 REPAIR 1 SHEET 1 AND 51-70-10-2R REPAIR 3 AND 4.SDR FDEA202208282087Skin · crackedRIGHT WING OUTBOARD FIXED LEADING EDGE IS CRACKED AT LOWER FWD ATACH FASTENER HOLE. REPAIRED RIGHT WING OUTBOARD FIXED LEADING EDGE SKIN AT LOWER FWD ATTACH FASTENER HOLE IAW B757 SRM 57-41-01-2RFIG 201 REPAIR 1 SHEET 8AND 51-70-07-0G.SDR FDEA202208252067Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232MAF HAS SEVERAL AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 232MAF IAW FEDEX DWG SRZ-25-005, REV. R, FEDEX GMM 7-0- 1000, REV. 182, AND B757 AMM 51-24-05-7.SDR FDEA202208252065Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232MFF HAS SEVERAL AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 232MFF IAW FEDEX DWG SRZ-25-005, REV. R, FEDEX GMM 7-0- 1000, REV. 182, AND B757 AMM 51-24-05-7SDR FDEA202208252064Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231MFF HAS SEVERAL AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 231MFF IAW FEDEX DWG SRZ-25-005, REV. R, FEDEX GMM 7-0- 1000, REV.182, AND B757 AMM 51-24-05-7.SDR FDEA202208252063Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231MAF HAS SEVERAL AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 231MAF IAW FEDEX DWG SRZ-25-005, REV. R, FEDEX GMM 7-0- 1000, REV. 182, AND B757 AMM 51-24-05-7.SDR FDEA202208252061Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231MBF HAS SEVERAL AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 231MBF IAW FEDEX DWG SRZ-25 005, REV. R, FEDEX GMM 7-0- 1000, REV. 182, AND B757 AMM 51-24-05-7.SDR FDEA202208252068Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251MTF HAS SEVERAL AREAS OF DELAMINATION FABRICATED NEW FLOOR PANEL 251MTF IAW FEDEX DWG SRZ-25-005, REV. R, VTMAE DWG 11864182, REV. A, AND BAC D6-55191, REV. CSDR FDEA202208252070Floor Panel · delaminatedMAIN CABIN, FLOOR PANEL 221MBF HAS A LARGE AREA OF DELAMINATION ON TOP SURFACE FABRICATED NEW FLOOR PANEL 221MBF IAW FEDEX DWG SRZ-25-005, REV. R, P/N 11861182-16SDR FDEA202208252069Floor Panel · delaminatedMAIN CABIN, FLOOR PANEL 222MAF HAS A LARGE AREA OF DELAMINATION ON TOP SURFACE FABRICATED NEW FLOOR PANEL 222MAF IAW FEDEX DWG SRZ-25-005, REV. R, P/N 11861180-1SDR FDEA202208252066Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231MCF HAS SEVERAL AREAS OF DELAMINATIONSDR FDEA202208252062Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231MEF HAS SEVERAL AREAS OF DELAMINATIONSDR FDEA202208252060Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231MGF HAS SEVERAL AREAS OF DELAMINATIONSDR FDEA202208252059Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251MEF HAS SEVERAL AREAS OF DELAMINATIONSDR FDEA202208252058Attach Bracket · cracked#2 PYLON AFT FAIRING, FWD HYD LINE CLAMP ATTACH BRACKET IS CRACKED ON INBD SIDE JUST AFT OF PYLON AFT BULKHEAD AT APPROX STA 203 LH REMOVED & REPLACED SHEAR BEAM & SPACER IAW BAC DWG 313N3052 SHEET 1 REVISION B & B757 SRM 51-40-02-0GSDR FDEA202208242047Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION ON UPPER SURFACES AT 6EA FLOOR PANEL FASTENER LOCATIONS FROM APPROX STA 720-735, RBL 59-64 REMOVED CORROSION ON MAIN CABIN FLOOR SUPPORT STRUCTURE, STA 720 TO 735, RBL 59 TO 64 IAW B757 SRM 53-00-51-1A, FIG.SDR FDEA202208242046Attach Fitting · cracked#2 PYLON AFT FAIRING OUTBD SIDE, FWD LOWER FAIRING ATTACH CLIP IS CRACKED AT NAC STA 203 CRACKED FWD ATTACH CLIP ON #2 PYLON O/B SIDE WAS REMOVED AND REPLACED IAW B757 SRM 51-40-02-0G ABD BAC DWG 313N3052, REVISION B.SDR FDEA202208232036Skin · crackedWHILE ACCOMPLISHING EO F-5730-E0340076-P1 (DIAGONAL BRACE AND WING SKIN INSPECTION) A CRACK INDICATION WAS NOTED IN THE NO.2 FASTENER HOLE COMMON TO THE SKIN & ATTACH FITTING COMPLIED WITH FEDEX EA F-5730-T0369921-P1, RELEASED SEP 07, 2022. TITLED "WINGS SDR FDEA202208232037Scuff Plate · crackedEXTERNAL FUSELAGE, R-1 DOOR SCUFF PLATE, THE AFT CORNER PLATE IS CRACKED REPAIRED THE R-1 DOOR AFT CORNER SCUFF PLATE AND RESTORED FINISH IAW FEDEX DWG SR57-53-003, REV. B.SDR FDEA202208232034Crease Beam · corrodedMAIN CABIN CREASE BEAM INBD CHORD UPPER SURFACE HAS CORROSION FROM APPROX STA 860-865, RBL 64SDR FDEA202208232033Frame · dentedMAIN CABIN FRAME IS DENTED AT STA 540, BETWEEN S6R AND S7R REPAIRED STA 540 FRAME BETWEEN S6R AND S7R IAW B757 SRM 53-00-07-2R, REPAIR 3, FIG. 201, SHEET 1.SDR FDEA202208232032Skin · gougedRIGHT WING OUTBOARD FWD FLAP OUTBOARD LEADING EDGE HAS GOUGESDR FDEA202208222027Floor Support · damagedMAIN CABIN FLOOR SUPPORT INTERCOSTAL HAS TOOLING MARKS ON UPPER RH SIDE AT APPROX STA 584, BL-0. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT INTERCOSTAL WEB, STA 584, BL-0 IAW B757SRM 51-40-02-0G AND VT MAE DWG 1182110, REV. -, P/N 11864112-2 FABRICATED
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