N676FE
Service difficulty reports · 178
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 = 'N676FE' 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 = 'N676FE' 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 FDEA201303080520Bushing · wornACFT SHOOK IN SMOOTH AIR DURING DESCENT FROM LOWER 20`S THROUGH UPPER TEENS. ENGINE PAGE SHOWED NO VIBRATION ANOMOLIES. EXPERIMNTATION, DEMONSTRATED THAT VIBRATION WAS INDEPENDENT OF ENGINE RPM, BUT VARIED WITH SPEED AND COULD BE ALLEVIATED WITH A SLIGHT RUSDR FDEA201303010486Line · leakingON ARRIVAL AT THE ACFT GREEN HYD QTY WAS LOW, JUST ABOVE YELLOW RANGE MX SERVICED THE GREEN HYD BACK INTO TOP HAT MINIMUM. THEY STATED THERE WAS NO INDICATION OF A LEAK. DURING DESCENT WE HAD A LOW GREEN HYD QTY ALERT. THE OVHD QTY POINTER WAS AT RED DOSDR FDEA201210023530Pitot Tube · obstructedON TAKEOFF AT 80KTS - F/O'S PFD SHOWED "0" AIRSPEED, CAPTAIN'S PFD AND BOTH STBY AIRSPEED INDICATORS SHOWED 80KTS. FOUND F/O'S PITOT TUBE PARTIALLY BLOCKED. CLEANED BLOCKAGE, REF MM 34-11-15-04 , PERFORMED PRESSURE TEST ON PITOT SYS. OPS CHECK NORMAL. ACFT SDR FDEA201209083259Selector Valve · malfunctionedON DEPARTURE GEAR RETRACTION NORMAL. WHEN HANDLE MOVED TO CENTER POSITION GEAR CAME DOWN ECAM READ "L/G RETRACTION FAULT" DOORS SHOWED RED UNLOCKED. PUT GEAR HANDLE DOWN GEAR SHOWED LOCKED. NO FURTHER ATTEMPT TO RAISE GEAR. MEM U IAW VERBAL FROM CAPT. GOTSDR FDEA201209083258Control Switch · malfunctionedAFTER TAKEOFF LANDING GEAR RETRACTED NORMALLY, BUT WHEN GEAR HANDLE WAS PLACED IN THE NEUTRAL POSITION GEAR EXTENDED. INDICATIONS WERE 3 GREEN PLUS 3 UNLOCK LIGHTS. HANDLE RETURNED TO THE UP POSITION AND GEAR RETRACTED NORMALLY. HANDLE RETURNED TO NEUTRAL WSDR FDEA201208102938Plug · leakingYELLOW HYD SYSTEM FAILED IN FLT. HYD QTY LOW. FOUND TWO PLUGS ON ACTUATOR BODY LEAKING AND NOT SAFETIED. TORQUED BOTH PLUGS REF. AMM 20-21-12-00 AND SAFETIED. SERVICED YELLOW SYSTEM REF. AMM 12-12-29-00. PRESSURIZED ALL THREE SYSTEMS WITH ELECTRIC PUMPS SDR FDEA201204111354Proximity Sensor · failedAFTER TAKEOFF, COULD NOT RAISE SYS 2 GEAR HANDLE, USED SYS 1. LOST F/O PITOT HEAT & TAT PROBES. LOST PITCH TRIM NR 2 & NR 2 CABIN PRESSURE REGULATOR. WOULD NOT RESET IN AIR & ALL SYSTEMS RETURNED TO NORMAL ON LANDING. PSU SHOWS FAULT 14, RT MLG SYS 2 PROSDR FDEA201104231593Fairing · missingAFTER FLIGHT, A FAIRING WAS DISCOVERED MISSING ON LT WING, UNDERSIDE, OTBD OF AFT PART OF THE ENGINE PYLON. NEW FAIRING INSTALLED AS PER AMM 57-20-35 REV 52.0. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112SDR FDEA201104201532Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 54.2, NR 4 LEFT FOUND EXCEEDED LIMITS VALUE 0.023 INCH PER EO 6-5310-73322 P1 ITEM 11 (I) MAIN DECK SEAT TRACK AT CABIN FRAME 54.2, LEFT NR 4 REPAIRED PER E.O. 6-5310-7-3322B PART 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR FDEA201104201531Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 38.2, LT FOUND WORN EXCEEDED LIMITS VALUE 0.034 INCH IAW EO 6-5310-7-3322 P1 ITEM 11 (I). MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, LT NR 5 REPAIRED IAW EO 6-5310-7-3322B, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVSDR FDEA201104201533Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 54.2, NR 5 LT, FOUND WORN EXCEEDED LIMITS, VALUE 0.020" IAW EO 6-5310-7-3322 P1 ITEM 11(I). MAIN DECK SEAT TRACK AT CABIN FRAME 54.2, NR 5 LT REPAIRED IAW EO 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVSDR FDEA201104201530Seat Track · wornMAIN DECK SEAT TRACK AT CABIN FRAME 38.2, NR.:4 LT FOUND WORN, EXCEEDED LIMITS VALUE 0.050 INCH IAW EO 6-5310-3322, P1 ITEM 11 (I). MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, NT.:4 LT REPAIRED IAW "EO 6-5310-7-3322B, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMMSDR FDEA201104201529Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 38.2, NR 3 LEFT FOUND EXCEEDED LIMITS VALUE 0.043 INCH PER 6-5310-7-3322 P1 ITEM 11(I) MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, RIGHT HAND NO.: 3 REPAIRED PER E.O. 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201104201528Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 38.2 LEFT FOUND EXCEEDED LIMITS VALUE 0.033 INCH PER EO 6-5310-7-3322 P1 ITEM 11 (I) MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, LEFT REPAIRED PER E.O. 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.SDR FDEA201104201527Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 38.2 NO.: 1 FOUND WORN EXCEEDED LIMITS VALUE 0.025 INCH PER EO 6-5310-7-3322 P1 ITEM 11 (I) MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, REPAIRED PER E.O. 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 1SDR FDEA201104201526Seat Track · wornCABIN SEAT TRACK AT FRAME 38.2, RIGHT HAND NO.: 3 FOUND 0.027 INCH WORN EXCEEDED LIMITS PER EO 6-5310-7-3322 ITEM 11(I), MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, RIGHT HAND NO.: 3 REPAIRED PER EO 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMMSDR FDEA201104071383Access Panel · delaminatedLEFT HAND AIRCON COMPARTMENT ACCESS PANEL 147DZ FOUND DELAMINATED MORE THAN 70%. LEFT AIR CON COMPARTMENT ACCESS PANEL 1487DZ REMOVED AND REPLACED PER AMM 25-72-41-04 REV 52.0. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA201104051322Attach Fitting · crackedDURING HFEC INSP, CRACK APPROX 0.7 INCH, FOUND ON FWD CARGO DOOR. (FRAME 22A) ACTUATOR ATTACH FITTING. REMOVED AND REPLACED PER SRM 52-31-00, FIGURE 204 REV 20. ACCOMPLISHED E.A. 6-5230-150306. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201103291239Rib · crackedRT WING INBD FLAP RIB 25A HORIZ UPPER FLANGE FOUND APPROX (2) INCH CRACKED. REMOVED AND REPLACED PER DRAWINGS: A5796000, 27A57960110 AND 57A5796005. ACCOMPLISHED E.A. 6-5750-143559. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.SDR FDEA201103291238Rib · crackedLT WING INBD FLAP RIB 25A HORIZ UPPER FLANGE FOUND APPROX (1) INCH CRACKED. REMOVED AND REPLACED PER DRAWINGS: A5796000, 27A57960110 AND 57A5796005. ACCOMPLISHED FEDEX E.A. 6-5750-143558. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR 08FDEA04117Seat Track · damagedTHE ADAPTER TRACK AT FRAME 61 RIGHT SIDE BUTT LINE 1456 HAS SCALLOPS BROKEN OFF. REMOVED FLOOR PANEL 252 UH TO GAIN ACCESS IAW AMM 53-10-25-4. RECEIVED A NEW ADAPTER TRACK PO 592553.5. LOCATED AND DRILLED THE NEW ADAPTER TRACK IAW SRM 51-40-40. INSTALLED TSDR 08FDEA04116Floor Panel · crackedMAIN CARGO FLOOR BOARD NR 242 AJ IS CRACKED AT FRAMES 50 - 54. MATERIAL ID FOR THE FLOOR PANEL IAW DWG SRZ 25-005, REV "G" AND ENGINEERING REPORT 91-019 QPL. MATERIAL P/N 402H35039-003, PO 626008.1. FABRICATED A NEW FLOOR PANEL PER DWG SRZ 25-005; REV "G"SDR 08FDEA04039Seat Track · wornMAIN CABIN SEAT TRACK AT FRAME 57.1, Y 45.0 IS WORN AT THE TANG. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16.SDR 08FDEA03940Adapter · gougedMAIN DECK CARGO COMPARTMENT CROSS TRACK AT FRAME 32; LBL 54. DAMAGE TO ADAPTER IS BEYOND LIMITS IAW SRM 53-10-15. REMOVED DAMAGED ADAPTER IAW SRM 51-40-21. LOCATED, DRILLED & INSTALLED THE NEW ADAPTER IAW DWG 10A53791837 & SRM 51-40-21.SDR 08FDEA03869Skin · chafedLEFT WING INBD FLAP TOP SKIN IS CHAFED AT APPROX 13 INCHES AFT OF THE FRONT SPAR AND 79 INCHES FROM THE INBD EDGE. BLENDED CHAFED AREA REF SRM SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 REF SRM 57-52-12. REMOVED MATERIAL 0.003. MATERIAL REMAINING 0.02SDR 08FDEA03831Floor Panel · crackedCABIN FLOOR BOARD 251 RG IS CRACKED BETWEEN FRAME 57.1 & FRAME 58; LBL 57 & LBL 77. FABBED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7-0-1000.SDR 08FDEA03830Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 60 AND FRAME 62, RBL 18 AND RBL 37. FABBED A NEW PANEL IAW DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7- 0-1000.SDR 08FDEA03829Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD 252 NH HAS A TORN CORNER BETWEEN FRAME 58 AND FRAME 60; RBL 0 AND RBL 18. FABBED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.SDR 08FDEA03828Floorboard · tornMAIN CABIN FLOOR BOARD IS TORN BETWEEN FRAME 58 AND FRAME 60, RBL 18 AND RBL 37. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.SDR 08FDEA03827Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOOR BOARD 252 GF IS TORN BETWEEN FRAME 57.1 AND FRAME 58, RBL 18 AND RBL 37. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7- 0-1000.SDR 08FDEA03822Floor Panel · contaminatedMAIN WHEEL WELL FLOOR PANEL 147 AF IS DELAMINATED AND SOAKED WITH HYDRAULIC FLUID. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7- 0-1000.SDR 08FDEA03823Floor Panel · delaminatedBULK CARGO PIT FLOOR PANEL 161 GF HAS NUMEROUS AREAS OF DELAMINATION AND DENTS. FABBED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV "G". MATERIAL ID A402H35039-003 IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.SDR 08FDEA03839Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 60 AND FRAME 62, RBL 18 AND RBL 37. 242 QJ FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03838Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 37 AND FRAME 38.2; RBL 17 AND RBL 34. NR 242 MF FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03837Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 34 AND FRAME 37; RBL 17 AND RBL 37. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03836Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 34 AND FRAME 37; RBL 17 AND RBL 37. NR 242 GF FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03835Floorboard · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 40 AND FRAME 43; LBL 57 AND LBL 77. NR 241 TH FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03834Floorboard · damagedMAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 43 AND FRAME 47; LBL 57 AND LBL 77. NR 241 WH FABRICATED FLOORBOARD IAW FEDEX DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03833Floorboard · crackedMAIN DECK CARGO COMPARTMENT FLOORBOARD IS CRACKED BETWEEN FRAME 77 AND FRAME 88; RBL 30 AND RBL 45. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03832Floorboard · damagedMAIN DECK CARGO COMPARTMENT FLOORBOARD 262 AH IS TORN BETWEEN FRAME 77 AND FRAME 80, RBL 57 AND RBL 70. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.SDR 08FDEA03826Floor Panel · damagedAVIONICS COMPARTMENT FLOOR PANEL 122 JF HAS EDGE DAMAGE. FABBED A NEW PANEL IAW PANEL IAW DWG SRZ 25-005 "G". PART MARKED IAW GMM 7-0-1001.SDR 08FDEA03825Floor Panel · damagedAVIONICS COMPARTMENT FLOOR PANEL 121 JF HAS EDGE DAMAGE. FABBED A NEW PANEL IAW DWG SRZ 25-005; REV "G".SDR 08FDEA03824Floor Panel · damagedFWD LOWER CARGO COMPARTMENT FLOOR PANEL 132 MG IS BROKEN AND PUNCTURED. FABBED NEW PANEL 132 MG IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.SDR 08FDEA03840Skin Panel · damagedEXTERNAL FUSELAGE SKIN HAS EVIDENCE OF LIGHTNING STRIKE AT FRAME 13 A; STRINGERS 20 R TO 21 R, (JUST FWD OF THE L-1 DOOR). COMPLIED WITH THE PERMANENT LIGHTNING STRIKE REPAIR PAE SRM 53-10-12; FIG 203; SHEET 1.SDR 08FDEA03796Floor Support · gougedDAMAGED FLOOR CAP AT FRAME 13 AND FWD; BL 0. REPAIRED DAMAGED FLOOR CAP IN REF TO SRM 51-71-50 & DWG A53612213.0SDR 08FDEA03797Seat Track · gougedMAIN DECK CARGO COMPARTMENT SEAT TRACK IS GOUGED BETWEEN FRAME 63 AND FRAME 64, RBL 18. BLENDED AREA AND FOUND THE REMAINING MATERIAL TO BE BEYOND ALLOWABLE LIMITS IAW A300-600 SRM 53-10-16, FIG 102, TOOL NR T8878G. REPAIRED THE SEAT TRACK IAW A300-600 SRM SDR 08FDEA03798Floorbeam · crackedTHERE ARE TOOL MARKS ON THE FLOOR CAPS IN THE MAIN CABIN AT FRAME 11, LBL 20 TO RBL 10. REMOVED DAMAGE. MATERIAL ID FOR REPAIR. FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-10. ALODINED AND PRIMED IAW AMM 51-75-10-8.SDR 08FDEA03800Fitting · crackedRIGHT THS INTERNAL FUEL TANK HOIST POINT FITTING IS CRACKED AT THE FWD SPAR, ACCESS 343 BB. WORK ACCOMPLISHED ON EA 6-5510-7-5001.SDR 08FDEA03799Fitting · crackedRIGHT THS INTERNAL FUEL TANK HOIST POINT FITTING IS CRACKED AT THE FWD SPAR, ACCESS 343 EB. WORK ACCOMPLISHED ON E.A. 6-5510-7-5001.SDR 08FDEA03742Skin · chafedTHE FWD LOWER CARGO DOOR INTERNAL SKIN IS CHAFFED AT DOOR FRAMES 7 AND 9. BLENDED IAW A300-600 SRM 51-74-10. UPON FURTHER INVESTIGATION MATERIAL REMAINING 0.050. FOUND TO BE WITHIN LIMITS IAW A300-600 52-30-00. ALODINED IAW A300-600 SRM 1-21-10; PARA 5-C.
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