N644FE, cancelled Mar 2, 2024
Service difficulty reports · 117
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 = 'N644FE' AND deregistration_id = 'N644FE-2024-03-02' 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 = 'N644FE' AND deregistration_id = 'N644FE-2024-03-02' 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 FDEA201411063539Fire Bottle · dischargedMULTIPLE BIRD STRIKES DESCENDING TO 7000 FT. RECEIVED ENGINE FIRE AGENT LOW, AGENT 2 LOW NR 3 ENG, ALERT. NO ADDITIONAL ENG ANOMALIES NOTED. REMOVED NR 3 ENGINE, AND NR 2 FIRE BOTTLE IAW AMM 26-21-01-4. VERIFIED BOTTLE WAS DISCHARGED. CHECKED WIRING FROM FSDR FDEA201311022674Pump · leakingLEVEL 2 NR 3 HYD FAIL ON SHORT FINAL, 3.9 GAL LEFT BOTH PUMPS WERE OFF. FOUND NR 3 FWD EDP LEAKING AT PUMP HSG ON ENGINE. R & R NR 3 ENGINE FWD EDP IAW AMM 29-11-20-4-2, SERVICE NR 3 HYD SYS TO PROPER LEVEL IAW AMM 12-13-02-3, DRY MOTORED NR 3 ENGINE IAW JSDR FDEA201305100964Skin · crackedLEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6, SIX FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFSDR FDEA201305100963Skin · crackedRIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6. THREE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLSDR FDEA201305080941Frame · dentedMAIN DECK BS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305080940Frame · dentedMAIN DECK BS 1661, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305080939Frame · dentedMAIN DECK BS 1741, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305080938Frame · dentedMAIN DECK BS 1701, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305080937Frame · dentedMAIN DECK BS 1661, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305060918Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R RT WING INBD FLAP VANE IAW AMM 27-50-22-4, REV 76.1 CARRIED OUT FLAP VANE ADJUSTMENT TEST IAW AMM 27-50-22-5, REV 76.1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.SDR FDEA201305060917Seat Track · corrodedCABIN - RT BS 1019 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1009 TO 1049 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REV 52 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201303200618Pitot Line · blockedRTO DUE TO IAS ALERT AT 90 KTS ON CAPTAIN`S SIDE. REPLACED CAPTAINS PITOT TUBE, FOUND BLOCKAGE.SDR FDEA201302210401Buss · malfunctionedON FINAL, RECEIVED "EMER PWR ON" ALERT. AFTER LANDING, RECYCLED EMERGENCY POWER SWITCH AND CPT DISPLAY UNITS 1,2,3 WENT BLANK/DARK WITH NR 2 DISPLAY RED "X". TRIED TO RECYCLE AGAIN WITH NO CHANGE. DUPICATED SYMPTOMS AT BLOCK-IN. ON ELECTRICAL PAGE, FOUNDSDR FDEA201107092624Computer · failedON TAKEOFF F/O AND STBY FLT INSTRUMENTS WERE ERRATIC. FOUND BOTH FCC'S AND ALL 3 IRU'S WITH NUMEROUS FAULTS ON NR2 ADC, REPLACED NR2 ADC IAW AMM 34-16-01-4 CK'S GOOD. WHILE INSPECTING PITOT PROBES FOUND DEBRIS IN THE F/O'S PROBE AND SOME IN THE STANBY PROBSDR FDEA201106012060Doubler · crackedWHEEL COMPARTMENT LT FWD SIDE SPOILER MIXER ROD CUT-OUT DOUBLER FOUND CRACK. R & R AS SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201105302026Skin · chafedRT WING L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON NR1- TO -WING FAIRING CONTACTS. CHAFED SKIN REMOVED AS PER SRM 51-33-01 AND SRM 51-35-01 REV 46. FABRICATED SKIN AS PER DWG ARB2363 AND INSTALLED AS PER SRM 51-33-01 AND MD-11 SRM51-35-01 REV 46.SDR FDEA201105302025Skin · chafedLEFT WING FIXED L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON-TO-WING CONTACTS. REFER TO SNRM N01217: LT WING FIXED L/E SKIN CHAFED. R & R SRM 51-33-01, REV 46 AND SRM 51-35-01, REV 46 AND DAC DWG ARB2363. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, RESDR FDEA201105302031Rib · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT NR 16 SLAT TRACK INBOARD SUPPORT BRACKET FOUND CRACKED RIB REMOVED AS PER SRM 51-33-01 & 51- 35-01 REV 46. FABRICATED RIB AS PER DWG ARB2850 REV G & INSTALLED AS PER SRM 51-33-01 & 51-35-01 REV 46. REPAIR AREA SDR FDEA201105292023Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA STA 1651, LONGERON 47R, FOUND CORROSION ACCOMPLISHED EA ED E.A. 1-5310-149713 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201105292022Longeron · corrodedCENTER ACCESSORY COMPARTMENT - STA 6-70 TO STA 6-90, LONGERON NR 49R CORRODED CENTER ACCESSORY COMPARTMENT - CORRODED LONGERON NR 49R CUT-OUT AT STA 6-90 IAW SRM 53-00-05, REV 46, REPAIR 1. HFEC INSP CARRIED OUT IAW NDT SPM, REV 13, PART 6-10-01-001 FOUNDSDR FDEA201105282017Spar Cap · crackedCRACK INDICATION FOUND ON THE LOWER VERTICAL STABILIZER LEFT HAND UPPER FORWARD FLANGES OF THE REAR SPAR CAP. ACCOMPLISHED E.A.1-5530-149805, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201105241959Longeron · corrodedLOWER AFT CARGO STA 1853 TO STA 1863, LONGERON 48R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-31-01, REV 46. FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 46, FIG 205. NEW SPLICE CHANNEL FABRICATED IAW DWG AGA7438 AND INSTALLED IAW SRM 51-31-01, REV 46. RESDR FDEA201105161844Support Bracket · crackedRIGHT WING FIXED L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. RT WING L/E COMPT NR 16 SLAT TRACK INBD SUPPORT RIB REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED RIB IAW DWG ARB2850, REV G AND INSTALLED IAW SRM 51-33-01 & 51-3SDR FDEA201105121821Seat Track · corrodedCABIN BETWEEN STA 1561 TO 1661, X = 7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. TRIMMED OFF AS PER SRM 53-00-52 REV 46, FIGURE 201. NEW SET TRACK REPAIR SECTION AND SPLICE FABRICATED AS SRM PER 53-00-52 REV 46, FIGURESDR FDEA201105121822Seat Track · corrodedCABIN BETWEEN STA 1561 TO 1661, X = -7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. ACCOMPLISHED "EA 1-5310-142539, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201105121820Seat Track · corrodedCABIN BETWEEN STA 1581 TO 1601, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201, NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46 SDR FDEA201105121819Seat Track · corrodedCABIN BETWEEN STA 1561 TO 1581, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201 NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46 , FIG 201 AND INSTALLED IASDR FDEA201105121817Floor Panel · wornCABIN BETWEEN STA 5-32 TO 5-53, X =-74 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND ELONGATED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SDR FDEA201105121816Seat Track · corrodedCABIN BETWEEN STA 1541 TO 1561, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK TRIMMED- OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIGURE 201, AND INSTALLESDR FDEA201105121813Seat Track · corrodedCABIN BETWEEN STA 5-113 TO 1541, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-0SDR FDEA201105121812Seat Track · corrodedCABIN BETWEEN STA 5-113 TO 1541, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF CORROSION IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IASDR FDEA201105121811Seat Track · corrodedCABIN BETWEEN STA 5-93 TO 5-113, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. SDR FDEA201105121809Seat Track · corrodedCABIN BETWEEN STA 5-53 TO 5-73, X = 10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. DAMAGED SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REVSDR FDEA201105121808Seat Track · corrodedCABIN BETWEEN STA 5-113 TO 1541, X =10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRSDR FDEA201105041746Access Panel · wornNR 2 PYLON ACCESS PANEL 475GR FOUND ONE (1) EACH WORN MOUNTING HOLE. ACCOMPLISHED EA 1-5480-142549, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201105031708Bulkhead · crackedAFT FUSELAGE COMPARTMENT - STA 2033 BULKHEAD, LT SIDE FORGING FOUND CRACK LINE NEAR TO UPPER CEILING CUT-OUT. ACCOMPLISHED EA 1-5310-149742, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201105031707Stop Fitting · crackedLT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED, R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2 FOUND SATISFACTORY.SDR FDEA201105031706Stop Fitting · crackedRT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED. R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201105031705Spar Cap · crackedCRACK INDICATION FOUND ON THE LWR VERTICAL STAB ON THE RT UPPER FWD FLANGE OF THE REAR SPAR CAP FITTING. ACCOMPLISHED EA 1-5530-149805, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201105021689Channel · damagedLOWER CTR CARGO COMPARTMENT BOTH AFT STA 1711 AND STA 1831, X= 38 AND X= -38 SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS BROKEN LOWER CTR CARGO COMPARTMENT AT STA 1711-STA 1831, X=38 AND X= -38, BOTH AFT SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS REMOVEDSDR FDEA201105011686Skin · chafedLT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. FABRICATED AS PER DWG ARB2363 AND INSTALLED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. REPAIR AREA PAINTED AS PER SRM SDR FDEA201105011685Skin · chafedRT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. NEW SKIN FABRICATED IAW DWG ARB236 AND INSTALLED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. REWORK AREA REPROTECTED & PAINTED IAW SRM SDR FDEA201104261624Seat Track · corrodedCABIN BETWEEN STA 457 AND 495, X = -29 SEAT TRACK UPPER AND LOWER FLANGE FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CSDR FDEA201104261623Stringer · crackedLT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104261622Stringer · crackedRT WING UPPER AUX TANK AT STA XCW 17 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104261621Stringer · crackedRT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104261620Support Bracket · crackedLT WING L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. SUPPORT REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED IAW DWG ARB2850, REV G, AND INSTALLED IAW SRM 51-33-01, REV 46 AND SRM 51-35-01, REV 46. REPAIR AREA REPROTECTED IASDR FDEA201104211542Skin · crackedLT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 0.375 INCH AND 0.3125 INCH CRACK. STOP DRILLED IAW SRM 57-40-01, REV 46, REPAIR 5 FIG 201. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND SRM 51-35-01, REV 46. REPASDR FDEA201104211541Skin · crackedRT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 1.75 INCH CRACKED. STOP DRILLED IAW SRM 57-40-01 REV 46, REPAIR 5, FIG 201. REPAIR DOUBLER FABRICATED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND INSTALLED IAW SRM 51-33-01, REV 46. REPAIR AREA REPROTESDR FDEA201104201525Seat Track · corrodedCABIN BETWEEN STA 1661 TO STA 1669, X = 73 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. FABRICATED REPAIR SECTION AND SPLICE IAW SRM 53-00-52 REV 46, FIG 201 AND INSTALLED IAW SRM 51-31
Back to N644FE, cancelled Mar 2, 2024