N964FD
Service difficulty reports · 184
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 = 'N964FD' 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 = 'N964FD' 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 FDEA202212082893Flap · chafedR/H WING, OTBD MAIN FLAP L/E IS WORN NEAR THE INBD EDGE. REPAIRED RH WING, OTBD MAIN FLAP LE SKIN IAW EA F-5750-T0371953-P1.SDR FDEA202212072885Beam · corrodedRIGHT WING, AILERON BALANCE WEIGHT ATTACH BEAM IS CORRODED REMOVED AND REPLACED BEAM IAW BAC DWG 113N7100, SHEET 2, REVISION L AND B757 SRM 51- 40-02.SDR FDEA202212072884Bracket · crackedLEFT WING LEADING EDGE UNDER PANEL 511KT OUTBOARD SIDE L-BRACKET BROKEN/CRACKED REMOVED AND REPLACED CRACKED L-BRACKET ON LEFT WING LEADING EDGE UNDER PANEL 511KT OUTBOARD SIDE, WITH NEW BRACKET P/N 313N5004Y15, P.O # 1044727.1 IAW BAC DWG 313N5004, REV CSDR FDEA202212072882Skin · damagedRH O/B AFT FLAP O/B EDGE HAS COMPOSITE DAMAGE EVALUATED AND REPAIRED RH O/B AFT FLAP O/B EDGE IAW B757 SRM 57-53-01-2R, 51-70-04-0G.SDR FDEA202212062880Scuff Plate · crackedR1 CABIN ENTRY DOOR CUTOUT AFT LOWER CORNER AND FWD SCUFF PLATE IS CRACKED ON THE TOP EDGE. REPAIRED THE R-1 DOOR FWD AND AFT LOWER CORNER SCUFF PLATES IAW DWG SR57- 53-003, REV. B. REMOVED AND REINSTALLED SCUFF PLATES IAW AMM 53-13-01-4.SDR FDEA202212022867Seal Depressor · crackedMCD CUT OUT AFT EDGE LOWER SEAL DEPRESSOR IS CRACKED AND DEFORMED AT THE BOTTOM EDGE REMOVED, FABRICATED AND INSTALLED NEW SEAL DEPRESSOR P/N 143N8724-2 AT THE MCD CUTOUT AFT LOWER EDGE IAW BAC DWG 143N8724, REV. - AND 143N8720, REV. A.SDR FDEA202211302862Skin · dentedRIGHT WING OUTBOARD AFT FLAP LOWER SURFACE IS DELAMINATED BETWEEN THE INBOARD AND OUTBOARD FLAP TRACKS REMOVED PAINT FINISH ON DENT AREA AND FOUND NO DELAMINATION OR BROKEN FIBERS. REPAIRED DENT IAW B757 SRM 57-53-01-2R FIG. 201 TABLE 2, SRM 51-70-04-0G PARASDR FDEA202211252843Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS944-960, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK ORG MAT .230, REMOVED .012, FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15SDR FDEA202211252842Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS900-BS928, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT .230, REMOVED .035, FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15SDR FDEA202211252841Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS973-BS994, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT .230, REMOVED .016, FOUND TO BE IN LIMITS PER B757 SRM 53- 00=52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15SDR FDEA202211252840Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS917 - BS1037, RBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT IS .230, REMOVED .011, FOUND TO BE IN LIMITS PER B757 SRM 53-00-52-1A, ALODINED, PRIMED AND PAINTED PER B757SRM 51-20-01 AND B757 AMM 51-21SDR FDEA202211252839Seat Track · corrodedMAIN CABIN SEAT TRACK IS GOUGED AND CORRODED BETWEEN BS914 - BS1037, LBL 45.5 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT .230, REMOVED .030, FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15SDR FDEA202211252838Seat Track · corrodedMAIN CABIN SEAT TRACK GOUGED AND CORRODED BETWEEN BS1018 - BS1039, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT .230, REMOVED .019, FOUND TO BE WITH IN LIMITS PER B757 SRM 53-00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-SDR FDEA202211252837Seat Track · corrodedMAIN CABIN SEAT TRACK GOUGED AND CORRODED BETWEEN STA 915 TO 1037, RBL45.5 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT .230, REMOVED .022 FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01-0G AND B757 AMM 51-21-1SDR FDEA202211232835Floor Panel · crackedMAIN CABIN FLOOR PANEL CRACKED @ BS879 - BS900 LBL 25 - LBL 44 FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005SDR FDEA202211232833Flap · delaminatedRH WING O/B MAIN FLAP UPPER SURFACE IS DELAMINATED APPROX 40" O/B FROMT THE I/B EDGE REPAIRED RH WING OB MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01 51-70-17. MAJOR REPAIRSDR FDEA202211232832Flap · delaminatedRH WING O/B MAIN FLAP UPPER SKIN IS DELAMINATED APROX 20" OB OF THE IB EDGE REPAIRED RH WING OB MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01 51-70-17. MAJOR REPAIRSDR FDEA202211232831Flap · delaminatedRH WING OB AFT FLAP UPPER SURFACE IS DELAMINATED BETWEEN THE I/B AND O/B TRACKS REPAIRED RH WING O/B AFT FLAP UPPER SURFACE IAW B757 SRM 57-53-01-2R AND 51-70-17-0G. MAJOR REPAIRSDR FDEA202211152793Floor Panel · crackedMAIN CABIN, FLOOR PANEL 242MBF IS DENTED/CRACKED FROM STA 900-1000, RBL 25-44. FABRICATED NEW FLOOR PANEL PER SRZ DWG SRZ -25-005.SDR FDEA202211152792Floor Panel · crackedMAIN CABIN, FLOOR PANEL 232MYF IS DENTED/CRACKED FROM STA 879-900, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005.SDR FDEA202211152791Floor Panel · crackedMAIN CABIN, FLOOR PANEL 232MUF IS DENTED/CRACKED FROM STA 780-879, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005.SDR FDEA202211152790Floor Panel · crackedMAIN CABIN, FLOOR PANEL 232MQF IS DENTED/CRACKED FROM STA 720-780, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005.SDR FDEA202211152789Floor Panel · crackedMAIN CABIN, FLOOR PANEL 232MLF IS DENTED/CRACKED FROM STA 680-720, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005SDR FDEA202211152788Floor Panel · crackedMAIN CABIN, FLOOR PANEL 232MGF IS DENTED/CRACKED FROM STA 625-680, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005SDR FDEA202210112544None · nonePDIS 964 52-10 8695 11OCT22 MEM OPEN U NO SLIDE LIGHT ON L1 RELAMPED SLIDE LIGHT. SYSTEM INDICATION OP CK'S NORMAL IN ACC B757 AMM 25-66-11-2-0SDR FDEA202208282091Reservoir · dischargedMDIS 964 52-10 8566 28AUG22 OAK FACT U EMERGENCY POWER RESERVOIR FOR R1 DOOR DISCHARGED. FACT 28AUG22 09:48 OAK U R&R EMERGENCY POWER RESERVOIR REF 757 AMM 52-11-30-4. OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202204291087Gust Lock · crackedMDIS 964 52-10 8328 29APR22 RST OPEN U DURING DAILY CK FOUND THE L1 ENTRY DOOR GUST LOCK COLLAR BROKEN FACT 30APR22 17:07 TYS REMOVED AND REPLACED L1 PASSENGER DOOR HOLD OPEN LOCK. REFERSDR FDEA202201100776None · noneL1 DOOR EXTERIOR EMERGENCY LIGHTING LAMP INOP. RELAMPED L1 DOOR SLIDE EMERGENCY LIGHT ASSEMBLY PER AMM REF 33-51-06-2-1, PERFORMED SUCCESSFUL EMERGENCY LIGHT TEST, OK FOR SERVICE.SDR FDEA202110082490Unknown · faultedON APPROACH INTO OAK GOT TE FLAP DISAGREE WHILE EXPENDING FLAPS THROUGH 15 . WENT AROUND. DISCOVERED HANDLE WAS STUCK BETWEEN FLAPS 15 AND 20. RAN QRH. DECLARED EMERGENCY. LANDED UNEVENTFUL IN OAK. FLAPS RETRACTED NORMALLY AFTER LANDING. REFERENCE WRISDR FDEA202101100034Skin · damagedREPAIRED MAIN CARGO DOOR SKIN AT AFT ACTUATOR ON WRI 52-30/7347. THIS WRITEUP IS FOR TRACKING EA F-5230-T0359030, WRI IS FOR TRACKING EA F-5230-T0359030. COMPLIED WITH SKIN REPAIR, PER SRM 52-30-01-2R REPAIR 4. COMPLETED ON WRI 52-30/7347.SDR FDEA202011032764Skin · puncturedNR 6 SLAT HAS A PUNCTURE BLENDED NR 6 SLAT, IAW B757 SRM 51-10-02. ORIG MATERIAL .080, REMAINING .049, LOSS .031. FOUND OUT OF LIMITS, IAW B757 SRM 57-43-01-1A. REPAIRED SLAT, IAW B757 SRM 57-43-01-2R REP 9.SDR FDEA202010292711Skin · chafedCHAFE MARK LEADING EDGE OF RIGHT OUTBOARD MAIN FLAP INBOARD SIDE. REMOVED DAMAGE ON LEADING EDGE OF RT OUTBOARD MAIN FLAP INBOARD SIDE, IAW B757 SRM 51-10-02. ORIG MAT .080 REM .030 LOSS .050 FOUND TO BE OUT OF LIMITS, IAW B757 SRM 57-53-01-1A FIG 101. REPSDR FDEA202010282681Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT LBL 24 STA 1322. REMOVED CORROSION ON SEAT TRACK STA 1322 LBL 24, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL .090, REMAINING .034, LOSS .056 OUT OF LIMITS, IAW B757 SRM 53-00-52-1A. REMOVED, FABRICATED, AND INSTALSDR FDEA202010252648Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL 45 STA 366. ALL WORK ACCOMPLISHED, IAW FEDEX EA F-5310-T0357429 P1. FUSELAGE-MAINFRAME-RBL 45.50 SEAT TRACK CORROSION REPAIR FROM STA 365 TO 377.SDR FDEA202010232626Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT LBL 45 STA 1320. REMOVED CORROSION ON SEAT TRACK STA 1320 LBL 45, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-52 FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK, IAW B75SDR FDEA202010212580Skin · damagedLEFT WING OUTBOARD FLAP TRAILING EDGE UPPER EXTERNAL SURFACE HAS MULTIPLE AREAS OF BARE COMPOSITE. EVALUATED LT WING OUTBOARD FLAP TRAILING EDGE UPPER EXTERNAL SURFACE AND FOUND TO BE OUT OF LIMITS, IAW B757 SRM 51-10-06-2R. REPAIRED AREA IAW B757 SRM 57-53SDR FDEA202010152518Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-24 STA 1540. REMOVED CORR ON SEAT TRACK STA 1540 RBL 24, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL .090, REMAINING .034, LOSS .056, OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED AND SDR FDEA202010152517Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-45 STA 1540. REMOVED CORR ON SEAT TRACK STA 1540 RBL 45, IAW B757 SRM 51-10-02. ORIGINAL MAT .090, REMAINING .040, LOSS .050, OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED, AND INSTASDR FDEA202010142493Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT LBL-24 STA 1320 EVALUATED SEAT TRACK STA 1320 LBL 24. 100% MATERIAL LOSS, OUT OF LIMITS, IAW B757 SRM 53-00-5252-1A. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK, IAW B757 SRM 51-40-02, 53-6060-52-01 FIG 1 ASDR FDEA202010142490Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-45 STA 1320. REMOVED CORROSION FROM MAIN CABIN SEAT TRACK STA 1320 RBL 45, IAW B757 SRM 51-10-02-0G. ORIGINAL MATERIAL .090, 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-00-52-1A. REMOVED, FSDR FDEA202010142489Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-24 STA 1320. REMOVED CORROSION ON SEAT TRACK STA 1320 RBL 24, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIG 101. REMOVE, FABRICATED AND INSTALLED NEW SEAT TRACK, IAW BSDR FDEA202010142494Floorbeam · corrodedMAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN RBL 26 AND RBL 45 STA 1055. REMOVED CORROSION ON FLOOR SUPPORT PLATE STA 1055 RBL 26-RBL 45, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS FOUND OUT OF LIMITS, IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATEDSDR FDEA202010142491Floorbeam · corrodedMAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN LBL 24 AND LBL 45 STA 900. REMOVED CORROSION ON FLOOR SUPPORT PLATE STA 900 LBL 24-LBL 45, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED, AND ISDR FDEA202010132481Floorbeam · corrodedMAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN RBL 1 AND RBL 24 STA 1020. REMOVED CORROSION ON FLOOR SUPPORT STA 1020 RBL 1-RBL 24, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLEDSDR FDEA2020081431879Transmission · lowON APPROACH WHEN WE SELECTED FLAPS 20 DEGREES WE RECEIVED A "TE FLAPS DISAGREE" MESSAGE. COMPLIED WITH QRH. VISUAL INSPECTION OF T/E FLAPS SHOWED NO MECHANICAL DAMAGE. RESTORED FLAP SYSTEM TO NORMAL AND OPERATED NORMALLY. FSEU #1 FAULT CODE 305, #2 FAULTSDR FDEA2018122433599Charger · inoperativeR1 EXTERIOR EMERGENCY SLIDE LIGHT WILL NOT TEST. RELAMPED BUT NO HELP.REF WDM 33-51-12, NO VOLTAGE AT LIGHT L30 ,HAS GOOD GROUND.REMOVED AND REPLACED POWER SUPPLY M730 REF MM 33-51-07-2.EMERGENCY LIGHT OPS CHECK NORMAL REF MM 33-51-00-5.A/C OK FOR SDR FDEA201811283388Battery Pack · dischargedL1 DOOR SLIDE LIGHT INOP. R&R EMERGENCY BATTERY PACK M731 PER MM 33-51-07-2, PN 2013-1A S/N 54663.SDR FDEA201811233359Light · inoperativeR1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT LIGHT BULB (P/N GE767) REF AMM 33-51-01. OPERATIONAL CHECKS GOOD.SDR FDEA201810232973Seal · leakingA WHINE STARTED AT APPROXIMATELY 6K FT MSL. IT GOT LOUDER AS WE CLIMBED TO 15K FT MSL. WE SLOWED FROM 285 KTS IAS TO 210 KTS IAS AT 15K FT MSL, THE WHINE DECREASED SOME BUT NOT AS MUCH AS DESCENDING. WHINE STOPPED AT 7K FT MSL. BOTH INTERNAL AND EXTERNAL COMMSDR FDEA201810082811Skin · crackedRT OTBD FLAP UNDERSIDE HAS SMALL CRACK ON THE INBD SIDE NEAR THE INBD FLAP TRACK FAIRING. REPAIRED RT OUTBD FLAP UNDERSIDE SMALL CRACK ON THE INBD SIDE NEAR THE INBD FLAP TRACK FAIRING IAW SRM 51-70-04-OG FIG 14 SHEET 2 AND EA WORK CARD TF-5750-T0342790 P1. RT
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