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 FDEA2020080314754Skin · delaminatedTRAPPED WATER INDICATION ON RUDDER LH SIDE PANEL HONEYCOMB CORE CELLS. LOCATED AROUND THE TRAILING EDGE FASTENER N. 31 ON VERTICAL STABILIZER (1EA) (L=4.5INCH W=3 INCH) REPAIRED RUDDER LH SIDE PANEL HONEYCOMB CORE CELLS LOCATED AROUND THE TRAILING EDGE FSDR FDEA2020080314751Web · crackedCRACK ON WEB LOCATED FRAME 47 Y225 HORIZONTAL STABILIZER PRESSURE DECK L/H SIDE PERFORMED PERMANENT REPAIR ON WEB LOCATED FR 47 AND Y225 HORIZONTAL PRESSURE DECK LH SIDE AS PER A300-600 SRM 53-15-15 FIGURE 201 (SHEET 2). FOR INSPECTION THRESHOLD FROM REPAISDR FDEA2020080314742Web · crackedCRACKED WEB LOCATED FRAME 43 -Y1203 HORIZONTAL PRESSURE DECK RH SIDE PERFORMED PERMANENT REPAIR EXACTLY LOCATION ON WEB ON FR 47 ON -Y1203 HORIZONTAL PRESSURE DECK AREA RH SIDE IAW SRM 53-15-15, FIG 201, SHEET 2 .SDR FDEA202007131834Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 1 INCH. OUTBOARD FROM RIB 5 AND 4 INCH. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L=6 INCH. W=1.5 INCH) REPAIRED RH ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE SDR FDEA202007131816Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 12 INCH OUTBOARD FROM RIB 7 AND 16 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=7.5 INCH. W=3 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLSDR FDEA202007131815Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 10 INCH INBOARD FROM RIB 16 AND 8 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.75 INCH. W=2.25 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB COSDR FDEA202007131814Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCH OUTBOARD FROM RIB 13 AND 7 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.25 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORSDR FDEA202007131813Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 1 INCH INBOARD FROM RIB 13 AND 14 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=5.5 INCH. W=4.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE SDR FDEA202007131812Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 7 INCH INBOARD FROM RIB 7 AND 16 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1 EA) (L=2 INCH W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELSDR FDEA202007131811Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 20 INCH OUTBOARD FROM RIB 13 AND 18 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.5 INCH. W=2 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORESDR FDEA202007131810Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 3 INCH OUTBOARD FROM RIB 13 AND 19 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE SDR FDEA202007131809Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH INBOARD FROM RIB 5 AND 13 INCH FROM TRALING EDGE. ADDITIONALLY, A DISBONDED AREA WAS FOUND WITHIN THIS SPOT, ON LT HORIZONTAL STABILIZER (1 EA) (L=3 INCH. W=2.3 ISDR FDEA202007131808Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 17 INCH OUTBOARD FROM RIB 2 AND 5.5 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1 EA) (L=3 INCH. AND W=1 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CSDR FDEA202007131807Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCH OUTBOARD FROM RIB 13 AND 26 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=1.75 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CSDR FDEA202007131806Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 10 INCH INBOARD FROM RIB 16 AND 15 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=3.5 INCH. W=2.25 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANNEL HONEYCOMB COSDR FDEA202007131805Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 8 INCH OUTBOARD FROM RIB 16 AND 8 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2 INCH. W=1.8 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CSDR FDEA202007131804Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 4 INCH OUTBOARD FROM RIB 16 AND 17 INCH FROM TRAILING EDGE ON LT HORIZ STAB (1EA) (L=2 INCH. W=1.75 INCH). DUE TO THE DISTANCE BETWEEN DAMAGE AREA REPORTED ON NON ROUTINE SDR FDEA202007131803Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 4 INCH. OUTBOARD FROM RIB 16 AND 17 INCH FROM TRAILING EDGE ON LT HORIZ STAB (1EA) (L=2 INCH. W=1.75 INCH). DUE TO THE DISTANCE BETWEEN DAMAGE AREA REPORTED ON NON ROUTINESDR FDEA202007131802Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH OUTBOARD FROM RIB 7 AND 25 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=4.5 INCH. W=4 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELL SDR FDEA202007131801Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 6 INCH INBOARD FROM RIB 10 AND 15.5 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=3 INCH. W=2.25 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CESDR FDEA202007131799Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE C ELLS. LOCATED AT 19 INCH. INBOARD FROM RIB 16 AND 9 INCH. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1EA) (L=4.25 INCH. W=2.25 INCH) REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB COSDR FDEA2020082131967Floor Support · corrodedCORROSION FLOOR STRUCTURE Y1959 LOC. BTW FR14 TO FR16A AT FWD GALLEY AREA REPLACED FLOOR BEAM Y1959 AND FASTENERS LOC BTW FR14 TO FR16 AT FWD GALLEY AREA IAW SRM 51-73-10, 51-40-21 AND DWG A53612311 ISSUE M,SDR FDEA2020081031806Skin · damagedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. 10 INCHED INBOARD FROM RIB 16 AND 15 INCHES FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031804Skin · damagedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 4 INCHEC. OUTBOARD FROM RIB 16 AND 17 INCH. FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM A-300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J.SDR FDEA2020081031834Skin · damagedTRAPPED WATER INDICATION ON THE RT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS, LOCATED 1 INCH OUTBOARD FROM RIB 5, AND 4 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031815Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 10 INCHES INBOARD FROM RIB 16 AND 8 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031814Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 27 INCHES OUTBOARD FROM RIB 13, AND 7 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031813Skin · damagedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED ONE INCH INBOARD FROM RIB 13 AND 14 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031812Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 7 INCHES INBOARD FROM RIB 7, AND 16 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031811Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 20 INCHES OUTBOARD FROM RIB 13 AND 18 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201PARAGRAPH 5.J.SDR FDEA2020081031810Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 3 INCHES OUTBOARD FROM RIB 13 AND 19 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031809Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 9 INCHES INBOARD FROM RIB 5 AND 13 INCHES FROM TRALING EDGE. REPAIRED THE SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031808Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 17 INCHES OUTBOARD FROM RIB 2 AND 5.5 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031807Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCHES OUTBOARD FROM RIB 13 AND 26 INCHED FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031805Skin · damagedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. 8 INCHED OUTBOARD FROM RIB 16 AND 8 INCHED FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, BLOCK 201, PARAGRAPH 5.J.SDR FDEA2020081031802Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH. OUTBOARD FROM RIB 7 AND 25 INCH. FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12, PB 201, PARA 5.B.SDR FDEA2020081031801Skin · delaminatedTRAPPED WATER INDICATION ON THE LEFT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE C ELLS. LOCATED AT 6 INCH. INBOARD FROM RIB 10 AND 15.5 INCH. FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12, PB 201, PARA 5.B.SDR FDEA2020081031799Skin · damagedTRAPPED WATER INDICATION ON LEFT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 19 INCH. INBOARD FROM RIB 16 AND 9 INCH. FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12 PB 201 PARA. 5.B .SDR FDEA202007092254Support · crackedCRACK INDICATION ON INTERNAL STRUCTURE IN OPEN FASTENERS HOLE 2 EA ON DOOR ACTUATOR SUPPORT BEAM BETWEEN FR 61 TO FR 62 IN AFT CARGO COMPARTMENT. CRACK LOCATIONS ARE: CRACK HOLE 1 LOC FR 61 MORE 7 INCH; CRACK HOLE 2 LOC FR 61 MORE 18 INCH. PERFORMED PERMANENSDR FDEA202007092248Support · crackedCRACK INDICATION ON INTERNAL STRUCTURE IN OPEN FASTENERS HOLES 4 E/A ON DOOR ACTUATOR SUPPORT BEAM IN FWD CARGO COMPARTMENT. CRACK LOCATION ARE: CRACK HOLE 1 LOC FR 22 MORE 3 INCH; CRACK HOLE 2 LOC FR 22 MORE 8 INCH; CRACK HOLE 3 LOC FR 22 MORE 14 INCH; CRACKSDR FDEA2020082191965Skin · dentedDENT EXTERNAL SKIN FR24 PLUS 12INCH STR51R LOWER FUSELAGE PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FR 24 PLUS 12 INCH STR 51R LOWER FUSELAGE TITLE: FUSELAGE, PLATES AND SKIN: SKIN BETWEEN FR 24-FR 25, S51R, DENT, PERMANENT REPAIR EA # 6-5330-T0355526 "MSDR FDEA2020082191963Fitting · crackedCRACK INDICATION ON FRAME 4 LOC. ON WINDSHIELD LOWER FRAME (CLOSING PANEL) RH SIDE HOLE NUMBER 10, CRACK DIRECTION IS 3 AND 7 O CLOCK IN COCKPIT (1 EA) REPLACED FITTING (GUSSET) LOCATED ON FRAME 4 ON WINDSHIELD LOWER FRAME 4 (CLOSING PANEL) RH SIDE IN COCKSDR FDEA201907111528Idg · leakingPDIS 651 24-20 2816 10JUL19 EWR OPEN U LOGPAGES:3138907 LOW IDG OIL PRESSURE WARNING, FOLLOWED BY LOSS OF #2 GENERATOR ON INITIAL TAKEOFF ROLL. REJECTED TAKEOFF @ < 60 KTS. COMPLIED W/PROCEDURES AND DECIDED TO REMAN FOR BRAKE COOLING. LOTS OF OSDR FDEA201901170162Fairing · failedKRUGER FLAPS DID NOT DEPLOY AT 3000/210 KTS. RAN QRH. AFTER TWO MINS KRUGER FLAPS DEPLOYED. REPLACED RH FOLDING FAIRING AND SPRING ROD FOR KRUGER FLAP. IAW 27-87-14-04. INSTALLED RT KRUEGER FLAP ACTUATOR IAW AMM 27-88-11-04. RIG, LEAK AND OPS CHECKED NORMAL.SDR FDEA201809072420Unknown · malfunctionedMAIN CABIN DOOR R1 (COPILOT SIDE) WILL NOT ARM SLIDE. RELEASED FOR SERVICE PER MEL 52-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. PENDING T/S OF MEL ITEM, SDR ISSDR FDEA2018080311875Floorboard · crackedMAIN CARGO COMPARTMENT FLOOR BOARD 232CF CRACKED. FABRICATED A NEW REPLACEMENT BOARD FOLLOWING DWG SRZ-25-005 REV N GUIDE LINES.SDR FDEA2018080301860Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK FR28 AT LBL Y953. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.SDR FDEA2018080301859Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FR26 AND FR28 AT RBL Y2462. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-16 AND DWG A53781970 ISSUE D.SDR FDEA201807301856Bracket · corrodedCORROSION ON MAIN CARGO BAY THRUST BRACKET, BETWEEN FRAMES 27 AND 28, -Y1456 TO -Y1959. REMOVED AND REPLACED THRUST BRACKET IAW SRM 53-14-15, AND DWG A537819700000.SDR FDEA201807301855Bracket · corrodedCORROSION FOUND ON THE MAIN CARGO BAY THRUST BRACKET, BETWEEN FRAMES 26 AND 27, -Y1456 TO -Y1959. REMOVED AND REPLACED THE THRUST BRACKET IAW SRM 53-14-15, AND DWG A537819700000.
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