N651FE
Service difficulty reports · 421
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 = 'N651FE' 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 = 'N651FE' 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 FDEA2020082041954Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04SDR FDEA2020082041953Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04SDR FDEA202008041952Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04SDR FDEA2020082041951Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04SDR FDEA2020082041950Bolt · corrodedCORROSION BOLT ON SCREWJACK 2 FWD POSITION ON RH WING (1 EA) REPLACED BOLT ON SCREWJACK 2 FWD POSITION ON RH WING (1E/A) IAW AMM 27-84-22-04 STEP 2.D(5) LOCATION OF THE SCREWJACK 2 IS BETWEEN WING RIB 5 AND 6 IAW AMM 06-31-57- 00SDR FDEA2020082041949Failsafe · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 8 FWD LOWER POSITION ON LH WING REPLACED BOLT ATTACHMENT SLAT TRACK 8 FWD LOWE POSITION ON LH WING (1E/A) IAW AMM 27-80-12-04SDR FDEA2020082041948Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 1 FWD UPPER POSITION ON LH WING REPLACED BOLT ATTACHMENT SLAT TRACK 1 FWD UPPER POSITION ON LH WING IAW AMM 27- 80-11-04SDR FDEA202007302306Bracket · crackedMACHINE BRACKETS (2E/A) ITEM 4, IAW EA NR 6-5313-T0355604 P1 STEP 10 FIGURE 2. MACHINED BRACKETS (2E/A) ITEM 4, AS PER EA NR 6-5313-T0355404 P1 STEP 10, FIG 2 AND DWG 13A53774203.SDR FDEA202007302255Spar · crackedCRACK INDICATION FOUND ON HOLE C ON REAR SPAR AND BOTTOM PANEL JUNCTION AREA RT SIDE AT CENTER FUEL TANK, CRACK DIRECTION IS 12 O'CLOCK, 1 E/A. ACCOMPLISHED REPAIR ON REAR SPAR AND BOTTOM PANEL JUNCTION AREA RT SIDE AT CENTER FUEL TANK, IAW EA NR 6-5710-T0355SDR FDEA2020009092122Rib · gougedWEAR RIB LOCATED AT OUTER WING REAR SPAR WI AX 21.90 BETWEEN RIB 6A AND RIB 7A ON RT WING (1 EA). PERFORMED PERMANENT REPAIR ON RIB LOCATED AT OUTER WING REAR SPAR WI AX 21.90 BETWEEN RIB 6A AND RIB 7A ON RT WING (1EA), IAW EA NR 6-5710-T0355668 P1 EA; TITLE:SDR FDEA2020090421696Frame · gougedGOUGE FRAME 73 RT AT LEVEL STR 21 ON UPPER FUSELAGE REPAIRED FRAME 73 RT AT LEVEL STR 21 ON UPPER FUSELAGE, IAW A300-600 SRM 53-10-13 PAR 5C FIG 202. THIS MUST BE INSPECTED AT DEFINED INTERVALS. THE INSPECTION INSTRUCTION REFERENCE IS 53-10-13-2-002-00 TABLESDR FDEA2020073011696Frame · gougedGOUGE FRAME 73 RH AT LEVEL STR 21R ON UPPER FUSELAGESDR FDEA2020083122062Mount · corrodedCORROSION ENGINE MOUNT FWD PYRAMID ON LH PYLON PERFORMED REPAIR LOC ON BASE PLATE AND (2E/A) HOLES OF THE BOLTS OF FORWARD MOUNT RIB 1 ATTACHED FITTING PYRAMID ON LH PYLON IAW EA N. T6-5450-T0355859 P1, #1 ENGINELH FORWARD MOUNT BASE PLATE CORROSION REPAIRSDR FDEA2020073122061Mount · corrodedCORROSION FORWARD MOUNT RIB 1 ATTACHED FITTING (PYRAMID) ON RH PYLON PERFORMED REPAIR LOC. ON BASE PLATE AND 3EA HOLES OF THE BOLTS OF FWD MOUNT RIB 1 ATTACHED FITTING PYRAMID ON RH PYLON IAW EA NO T6-5450-167628 B P3, #2 PYLON FWD ENG MOUNT FITTING CORROSSDR FDEA2020080321741Structure · crackedBROKEN RUDDER UPPER HOIST POINT AT LEVEL RIB 13 LH SIDE ON VERTICAL STABILIZER REPAIRED RUDDER HOIST POINT AT LEVEL RIB 13 LH SIDE ON VERTICAL STABILIZER AS PER A300 SRM 55-41-12 P.B. 201 PARA. 26. THIS REPAIR IS APPLICABLE TO THE INSPECTION PROGRAM DEFINESDR FDEA2020082691976Beam · crackedCRACK TRAILING EDGE IN OVERWING PANEL BEAM 5 ON RT WING. PERFORMED PERMANENT REPAIR LOC. TRAILING EDGE IN OVERWING PANEL BEAM 5 ON RT WING, IAW EA 6-5720-T0355567 A WING. SECONDARY STRUCTURES TRAILING EDGE STRUCTURES OVER MLG BAY, INBOARD SHROUD, CRACK, PESDR FDEA202007181971Floor Panel · delaminatedDELAMINATED FLOOR PANEL MAIN DECK AFT CARGO COMPARTMENT 231TG, 231UG,23 1NG,231ZG,232VH,232FG IN PAX CABIN (6 EA). REPAIRED FLOOR PANEL MAIN DECK AFT CARGO COMPARTMENT 231UG, 231TG, 231NG, 231ZG IN PASSENGER CABIN AS PER A300 SRM 53-10-20 PAGE BLOCK 201 PARSDR FDEA2020090981901Floor Panel · crackedCRACKED FLOOR PANEL 252DH ZONA 250 IN AFT CARGO COMPARTMENT (1 EA). MANUFACTURED FLOOR PANEL 252DH ZONE 250 IN AFT CARGO COMPARTMENT, AS PER DWG NO. SRZ-25-005 REV. R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: FX B5327036100600 FDX AUG-11-2020, AS PER GMMSDR FDEA202007181895Floor Panel · delaminatedDELAMINATED PANEL 122DF IN FWD AVIONIC COMPARTMENT MANUFACTURED FLOOR PANEL 122DF IN FWD AVIONIC COMPARTMENT AS PER DWG NO. SRZ- 25-005. REV R. AUG-22-2019 MARKED NEW FLOOR PANEL WITH P/N FX A5321024400000FDX AUG- 11-2020. AS PER GMM 7-0-1001. FOR TRACIBILITSDR FDEA202008281692Frame · gougedGOUGE FRAME 31 AT LEVEL STR-17 LT SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN. REPAIRED FRAME 31 AT LEVEL STR 17 LT SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN, IAW SRM A300-600 53-10-13-201 PARA 5.C. THIS REPAIR MUST BE INSPECTED AT DEFINED INSDR FDEA2020082711901Floor Panel · crackedCRACK FLOOR PANEL 252DH ZONA 250 IN AFT CARGO COMPARTMENT (1 EA) MANUFACTURED FLOOR PANEL 252DH AS PER DWG SRZ-25-005 REV. R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: A30 B5327036100600 FDX AUG-11-2020 AS PER GMM 7-0-1000, FOR TRACIBILITY MATERIAL PO: 2020SDR FDEA202008261975Floor Panel · delaminatedDELAMINATED PANEL 121TF IN FWD AVIONIC COMPARTMENT. REPAIRED PANEL 121TF IN FWD AVIONIC COMPARTMENT, AS PER DRAWING SRZ-25-005 REV R.SDR FDEA2020082681974Frame · gougedGOUGE FRAME FR-54 BETWEEN STR-12 LT TO 13 LT SIDE ON AFT FACE IN PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME 54 BETWEEN STR 12 LT TO 13 LT SIDE ON AFT FACE IN PASSENGER CABIN, IAW EA 6-5310-T0355414 A P1 EA TITTLE: FUSELAGE-MAINFRAME-MAIN DECK CARGO SDR FDEA2020082681973Floor Panel · damagedPUNCTURE ON FLOOR PANEL 212HF IN COCKPIT. REPAIRED FLOOR PANEL 212HF IN COCKPIT AS PER DRAWING SR30-53-005SDR FDEA2020081871926Roller Track · corrodedCORROSION ROLLER TRACK ASSY BETWEEN FRAMES 32 TO 38.2, Y450 TO Y953 IN THE FWD CARGO COMPARTMENT. REPLACED THE ROLLER TRACK ASSY IAW SRM 51-72-10, AND DRAWING A25771363.SDR FDEA2020081871924Roller Track · corrodedCORROSION ROLLER TRACK ASSY LOC. AT FR37 AND BTW Y0 TO -Y453 IN FWD CARGO COMPARTMENT REPLACED ROLLER TRACK ASSY IN FWD CARGO IAW SRM 51-72-10 AND DRAWING A25774009.SDR FDEA2020081871923Roller Track · corrodedCORRODED ROLLER TRACK ASSY BETWEEN FRAMES 32 & 38.2, -Y450 TO -Y953 IN THE FWD CARGO COMPARTMENT. REPLACED THE ROLLER TRACK ASSY IAW SRM 51-72-10, AND DRAWING A25774009.SDR FDEA2020081871901Floor Panel · crackedCRACK FLOOR PANEL 252DH ZONA 250 IN AFT CARGO COMPARTMENT (1 EA) MANUFACTURED FLOOR PANEL 252DH AS PER DWG SRZ-25-005 REV. RSDR FDEA202008181895Floor Panel · delaminatedDELAMINATED PANEL 122DF IN FWD AVIONIC COMPARTMENT MANUFACTURED FLOOR PANEL 122DF IN FWD AVIONIC COMPARTMENT AS PER DWG SRZ-25- 005 REV. R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: A30 A5321024400000 FDX AUG- 11-2020 AS PER GMM 7-0-1000 FOR TRACIBILITY MSDR FDEA2020081271789Frame · crackedCRACK FRAME 26 BETWEEN STRINGERS 13R TO 14R IN PASSENGER CABIN. REPLACED THE SECTION OF FRAME IAW DRAWING A53777450, SRM 51-40-21, AND SRM 51-72-10.SDR FDEA202008071789Frame · crackedCRACKED FRAME 26, BETWEEN STRINGERS 13R TO 14R. REPLACED THE SECTION OF FRAME IAW DRAWING A53777450, SRM 51-40-21, AND SRM 51-72-10.SDR FDEA2020073081692Frame · gougedGOUGE FRAME 31 AT LEVEL STR-17 LH SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN REPAIRED FRAME 31 AT LEVEL STR 17 LH SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN IAW SRM A300-600 53-10-13-201 THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVALSSDR FDEA202007171898Floor Panel · crackedCRACK FLOOR PANEL 252BH (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 252BH IN PASSENGER CABIN ASPER DWG NO. SRZ-25-005. REV R. AUG-22-2019, MARKED NEW FLOOR PANEL WITH P/N FX B5327028700100FDX AUG-11-2020 ASPER GMM 7-0-1001 FOR TRACIBILITSDR FDEA202007171897Floor Panel · crackedCRACK FLOOR PANEL 232FG (MAIN DECK) IN PASSENGER CABIN MANUFACTURED FLOOR PANEL 232FG IN PASSENGER CABIN AS PER DWG SRZ-25-005 REV.R AUG-22-2019, MARKED FLOOR PANEL 232FG WITH P/N: FX B5327046000000 FDX DATE: AUG-11- 2020 AS PER GMM 7-0-1001, FOR TRACIBILITSDR FDEA2020081871899Floor Panel · crackedCRACK FLOOR PANEL 242GF (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 242GF AS PER DWG SRZ 25-005 REV. R AUG-22-2019. THIS JOB IS DOCUMENTED ON NON ROUTINE CARD N00346, FLOOR PANEL IDENTIFIED WITH P/N: A30 B5327048001700 FDX AUG-11-2020 ASSDR FDEA2020081871898Floor Panel · crackedCRACK FLOOR PANEL 252BH (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 252BH AS PER DWG SRZ-25-005 REV. R,SDR FDEA2020081871897Floor Panel · crackedCRACK FLOOR PANEL 232FG (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232FG AS PER DRAWING SRZ 25-005 REV R.SDR FDEA202007161900Floor Panel · crackedCRACK FLOOR PANEL PLATE 242SF IN PASSENGER CABIN (1EA) MANUFACTURED FLOOR PANEL 242SF IN PASSENGER CABIN AS PER DWG NO. SRZ-25-005 REV.R AUG-22-2019, MARKED NEW FLOOR PANEL WITH P/N: FX B5327061802100FDX AUG-11- 2020 AS PER GMM 7-0-1001, FOR TRACIBILITY MASDR FDEA2020082661972Floor Support · corrodedCORROSION SUPPORT FLOOR LOCATED BETWEEN FR 11 TO FR 13 AND BETWEEN Y450 TO Y953 AT FWD GALLEY AREA. REPLACED SUPPORT FLOOR LOCATED BETWEEN FR11 TO FR13 BETWEEN Y450 TO Y953, IAW A300-600 SRM 51- 72-10 AND DWG A53612214 MEASURES OF DAMAGE L=4.699", W=1.697".SDR FDEA2020081861900Floor Panel · crackedCRACK FLOOR PANEL PLATE 242SF IN PASSENGER CABIN (1EA) MANUFACTURED FLOOR PANEL 242SF AS PER DWG SRZ 25-005 REV. R.SDR FDEA2020080316740Web · crackedCRACK ON WEB LOCATED AT FRAME 47, Y1203, HORIZONTAL PRESSURE DECK AREA LT SIDE PERFORMED PERMANENT REPAIR LOC. ON WEB IAW SRM 53-15-15, FIG 201, SHEET 2.SDR FDEA2020090941902Floor Panel · delaminatedDEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT. MANUFACTURED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT, AS PER DWG NO. SRZ-25-005 REV. R. AUG-22-2019. MARKED NEW ACCESS PANEL WITH P/N: FX A5321024200000 FDX AUG-11-2020, AS PER GMM 7-0-1001 FORSDR FDEA202007141754Skin · delaminatedTRAPPED WATER INDICATION ON RUDDER LT SIDE PANEL HONEYCOMB CORE CELLS. LOCATED AROUND THE TRAILING EDGE FASTENER 31 ON VERTICAL STABILIZER (1EA) (L=4.5INCH W=3 INCH). REPAIRED RUDDER LT SIDE PANEL HONEYCOMB CORE CELLS LOCATED AROUND THE TRAILING EDGE FASTENSDR FDEA202007141969Floor Panel · damagedIMPROPERLY ACCESS PANEL 121PF DUE TO MISSING INSERT IN FWD AVIONIC COMPARTMENT (1EA) INSTALLED NEW INSERT 1 EA ON FLOOR PANEL 121PF IN FWD AVIONIC COMPARTMENT ASPER DWG NO SRZ-25-005 REV. R AUG/22/2019 ITEM 8 TO15SDR FDEA202007141968Floor Panel · damagedIMPROPERLY ACCESS PANEL 121YF DUE TO MISSING INSERT IN FWD AVIONIC COMPARTMENT (1EA) INSTALLED NEW INSERT 1 EA ON FLOOR PANEL 121YF IN FWD AVIONIC COMPARTMENT ASPER DWG NO SRZ-25-005 REV . R AUG/22/2019 ITEM 8 TO 15SDR FDEA2020082711902Floor Panel · delaminatedDEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT MANUFACTURED ACCESS PANEL 121CF AS PER DWG SRZ 25-005 REV. R AUG-22-2019. MARKED NEW ACCESS PANEL WITH P/N: A30 A5321024200000 FDX AUG-11-2020 AS PER GMM 7-0-1000 FOR TRACIBILITY MATERIAL, PO: 2020-1615SDR FDEA2020082641970Frame · damagedWEAR ON FRAME 54 AT LEVEL STR 16 RT SIDE ON UPPER FUSELAGE. PERFORMED PERMANENT REPAIR ON FRAME 54 AT LEVEL STR 16 RT SIDE ON UPPER FUSELAGE, IAW EA 6-5310-T0355376 P1 EA TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGO COMPARTMENT - CHAFE/WORN DAMAGE COMMON TSDR FDEA2020082641742Web · crackedCRACK ON WEB LOCATED FRAME 47 -Y1203 HORIZONTAL PRESSURE DECK RH SIDE PERFORMED PERMANENT REPAIR EXACTLY LOCATION ON WEB ON FR47 ON -Y1203 HORIZONTAL PRESSURE DECK AREA RH SIDE IAW A300-600 SRM 53-15-15, FIG 201-C2 (SHEET 2) RECHECK REQUIRED INSPECTION THRSDR FDEA2020081841902Access Panel · debondedDEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT MANUFACTURED ACCESS PANEL 121CF AS PER DWG SRZ 25-005 REV. RSDR FDEA2020080314755Web · crackedCRACK ON WEB LOCATED FRAME 47 -Y225 HORIZONTAL PRESSURE DECK RH SIDE PERFORMED REPAIR ON WEB LOCATED FRAME 47 -Y225 HORIZONTAL PRESSURE DECK RH SIDE IAW A300-600 SRM 53-15-15 FIG 201. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT AT 24000 FC/FH NOT RELEVANT,
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