N807FX
Service difficulty reports · 177
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 = 'N807FX' 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 = 'N807FX' 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 COEA2016072806807Stringer · crackedSTRINGER 1AL IS CRACKED AFT OF FRAME 20. REPAIRED IAW SRM 530000-300-824-A01.SDR COEA2016072805807Stringer · crackedSTRINGER 1L IS CRACKED AT DRAIN HOLE JUST AFT OF FRAME 20. REPAIRED IAW SRM 530000-300-824-A01.SDR COEA2016072704807Panel · corrodedRIGHT ENGINE INBOARD LATERAL PANEL AFT LANDING HAS CORROSION. REPAIRED IAW CETS-3523/16.SDR COEA2016072703807Panel · corrodedRIGHT ENGINE OUTBOARD LATERAL PANEL AFT LANDING HAS CORROSION. REPAIR IAW CETS-3523/16.SDR COEA2016052601807Generator · faultedFLIGHT 7202, AIR TURN BACK DISCREPANCY. DURING CLIMB OUT THE ACW NR 2 GEN FAULTED. THE CREW RESET THE SYS BUT THE FAULT RETURNED. THE CREW ELECTED TO RETURN & LANDED SAFELY & NO EMER WAS DECLARED. REPLACED THE NR 2 ACW GEN. LEAK & OPERATIONS CHECKED GOODSDR COEA2015121705807Wire Harness · defectiveFLIGHT 8663, AIR TURN BACK, DISCREPANCY SHORTLY AFTER TAKEOFF. THE LG HANDLE COULD NOT BE MOVED TO RETRACT GEAR. IN ADDITION, ATC WAS NOT RECEIVING ANY TRANSPONDER SIGNAL. CREW ELECTED TO RETURN, NO EMER WAS DECLARED. INTERNAL AND EXTERNAL HARNESSES ON RISDR COEA2015070604807Ahrs · malfunctionedFLIGHT 7202 EN-ROUTE, DISCREPANCY. ONCE AIRBORNE, AFTER TAKEOFF, THE NR 2 EADI STARTED SHOWING PITCH & ATTITUDE CAUTIONS. THE CREW ELECTED TO RETURN, NO EMER WAS DECLARED. REPLACED THE NR 2 AHRU. OPERATIONS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR COEA2015021803807Computer · malfunctionedFLIGHT 8234, WHEN CREW EXTENDED THE LT MLG, THE UNLOCK LIGHT ILLUMINATED ON LT MAIN PRIMARY & SECONDARY WENT OFF AT 4 - 5 SEC AFTER FREE FALL. ATTEMPTED THE GRAVITY ASSISTED PROCEDURES & WAS ABLE TO OBTAIN A FULL LOCKED GEAR INDICATION. AN EMERGENCY WAS NOTSDR COEA2015012302807Proximity Switch · out of adjustWHILE ON FLIGHT TO TEST GEAR FOR PREVIOUS LG DISCREPANCY, SDR COEA2015012101807, THE GEAR RETRACTED WITHOUT A PROBLEM. WHEN THE GEAR WAS PUT DOWN FOR LANDING, THE LT MAIN GEAR INDICATIONS DID NOT INDICATE DOWN & LOCKED. THE CREW ATTEMPTED TO USE THE EMER EXTSDR COEA2015012101807Actuator · failedON APPROACH, THE LG WOULD NOT EXTEND NORMALLY. THE LT MLG UNLOCK LIGHT REMAINED ILLUMINATED. THE CREW PERFORMED THE EMER LG GRAVITY EXTENSION PROCEDURE IAW THE QRH & THE PROCEDURE WAS SUCCESSFUL. DID NOT DECLARE AN EMER. TROUBLE SHOT & REPLACED THE LT MAINSDR COEA2014071103807Panel · corrodedRIGHT UPPER WING PANEL 623GT HAS LEVEL 2 CORROSION ON MATING SURFACE. REPLACED WITH NEW PART.SDR COEA2014071102807Panel · corrodedRIGHT UPPER WING FUEL ACCESS DOOR CUT OUT FOR PANEL 622CT & ASSOCIATED FOIL ON PANEL 622CT BOTH HAVE FRETTING DAMAGE. REPAIR IAW SRAS DO & TS-3854 07, 4243 ISSUE D DATED 7/10/2014.SDR COEA2014061701807Structure · crackedTHE FWD CARGO DOOR FWD LATCH FITTING & INNER SKIN WERE FOUND CRACKED UNDER THE LOWER LATCH LOCK MECHANISM FWD BEARING MOUNT ASSEMBLY. REPLACE WITH OEM PARTS.SDR COEA2013070302807Fdau · failedDURING CLIMB OUT, PILOT NOTICED THE FDAU LIGHT ON THE FLIGHT RECORDER, SHORTLY AFTER, BOTH PILOTS SMELLED SMOKE. TURNED BACK AND RETURNED TO DEPARTURE, LANDING WITHOUT INCIDENT.SDR COEA2013061401807Fdau · failedDURING APPROACH, CREW NOTICED A STRONG SMOKE ODOR IN THE COCKPIT AND DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. MX DETERMINED THE FDAU HAD FAILED IN FLIGHT CAUSING THE SMOKE ODOR. THE FDAU WAS REPLACED AND OPS CHECKS WERE SUCCESSFUL.SDR COEA2012083009807Tab · chafedHEAVY CHECK / MAJOR REPAIR: LEFT AILERON TRIM TAB BELLCRANK, CHAFE DAMAGE ON INSIDE OF CONTROL SURFACE LEVER TAB. BLEND AND LEAVE AS IS IAW SRM AND SRAS.SDR COEA2012080908807Strap · crackedHEAVY CHECK / MINOR REPAIR - CRACK: UPON SKIN REMOVAL FOUND .004" CRACK ON DOUBLER STRAP FR A7 AT RIGHT AFT GEARWELL CORNER. REMOVED AND REPLACED DOUBLER STRAP WITH OEM PART PER SRM.SDR COEA2012080307807Skin · dentedHEAVY CHEC MAJOR REPAIR: DENT 8.6 INCHES FORWARD OF FR 23A, .08 INCHES BELOW STR 13R. REPAIRED SINGLE RIVET REPAIR IAW ATR72 STRUCTURAL REPAIR MANUAL.SDR COEA2012080306807Skin · dentedHEAVY CHECK MAJOR REPAIR: DENT 2.3 INCHES FORWARD OF FR 16, .03 INCHES BELOW LAP JOINT EDGE AT STR 17L. REPAIRED SINGLE RIVET REPAIR IAW ATR72 STRUCTURAL REPAIR MANUAL.SDR COEA2012072305807Fitting · chafedHEAVY CHECK / MAJOR REPAIR: FWD CARGO DOOR LOWER CENTER FITTING AROUND MIDDLE DOOR LOCKED VIEWING WINDOW IS CHAFED. SUBMITTED TO ATR, REPAIR PER STRUCTURAL REPAIR INSTRUCTION FROM ATR.SDR COEA2012072303807Cleat · corrodedHEAVY CK / LEVEL 2 CORROSION: STRINGER 17L CLEAT IS CORRODED FR 38-39 (LENGTH 1.0", WIDTH .75", DEPTH .025"). REMOVED CORROSION AND REPLACED CLEAT WITH OEM PART.SDR COEA2012072302807Intercostal · corrodedHEAVY CK / LEVEL 2 CORROSION: STRINGER 17L INTERCOSTAL IS CORRODED FR 38-39 (LENGTH 3.0", WIDTH 4", DEPTH .048"). REMOVED CORROSION AND REPLACED INTERCOSTAL WITH OEM PART.SDR COEA2012072301807Angle · corrodedHEAVY CK / LEVEL 2 CORROSION: STRINGER 17L CHORD ANGLE IS CORRODED FR 38-39 (LENGTH 1.0", WIDTH .75", DEPTH .035"). REMOVED CORROSION AND REPLACED CHORD ANGLE WITH OEM PART.SDR COEA2011010701807Connector · contaminatedLEFT ENGINE FIRE WARNING SOUNDED APPROXIMATELY 4 MILES FROM LANDING IN PSC. DISCHARGED BOTH FIRE BOTTLES, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NO VISUAL SIGN OF SMOKE OR FIRE. FOUND WATER IN LOOP CONNECTORS CAUSING FALSE WARNING. REMOVED AND REPSDR COEA2010112402807Skin · leakingMAJOR REPAIR: RT WING FUEL LEAK AT LOWER SKIN TO RIBS 15-16 JOINT, STRINGERS 1-2 & 6. FASTENERS REMOVED, HOLES INSPECTED AND FILLED WITH SEALANT THEN BLIND BOLTS INSTALL FOLLOWING ATR INSTRUCTIONS. SRAS DO/TS-4176/10...6141 VALIDATED AS PERMANENT REPAIR.SDR 2010F00237Seat Track · corrodedUPON REMOVAL OF SEAT TRACK, FOUND PITTING CORROSION ON FLOORBEAM MATING SURFACE AT FLOORBEAM 23, FABRICATED REPLACEMENT FLOORBEAM SEGMENT FROM NTA 44770 7075-T-6511, PO 2059P. INSTALLED NEW FLOORBEAM & REPAIR SPLICES IAW SRM 53-00-00 435, REV 77.SDR 2010F00236Crease Beam · corrodedRH CREASE BEAM WEB FR40-41 IS CORRODED. WEB ASSY WAS REMOVED TO FOM ON NR 100070 W/O 97183. FABRICATED WEB WAS INSTALLED ON NR 100070 W/O 97183.SDR 2010F00235Stringer · corrodedJOINT STRINGER ON STR 19R AT FR23, SUSPECTED OUT OF LIMITS FOR CORROSION. REMOVED CORROSION REFERENCING SRM 51-21-42, REV 77. FOUND MATERIAL LOSS TO BE BEYOND SRM LIMITS IAW SRM 51-10-10, REV 77. SRM 53-51-26, FIG 101, ITEM 30, REV 77 AND SRM 51-31-60, FIG 4SDR 2010F00234Stringer · corroded(COER) FLIGHT DECK, STR 21R END TIE JUST AFT OF FRAME 12 HAS SURFACE CORROSION. (LEVEL II) REMOVED CORROSION IAW SRM 51-21-42, REV 77. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-10, REV 77. REMOVED STRINGER END TIE IAW SRM 51-25-01, REV 77. INSTALLED NEW STR SDR 2010F00233Stringer · corroded(COER) FLIGHT DECK, STRINGER 21L JUST AFT OF FRAME 12 HAS SURFACE CORROSION. (LEVEL II) REMOVED RIVETS TO FOM CORROSION REMOVAL IAW SRM 51-25-01, REV 77. REMOVED CORROSION IAW SRM 51-21-42, REV 77. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-10, REV 77. REMOVEDSDR 2010F00232Stringer · corroded(COER) FLT DECK, FRAME 12 FWD, AFT SIDE FROM STRINGER 20L-20R HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-42, REV 77. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-11-00, FIG 301 & 53-11-40, FIG 112, REV 77. ALL PARTS INSTALLED IAW SRM 51-25-01, 51-2SDR 2010F00231Spar · corrodedLEFT WING FRONT SPAR LOWER FLANGE AT RIB 31 HAS SMALL AREA OF DELAMINATED. REPAIRED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTION DO/TS-3386/10-13712 ISSUE A DATED JUNE 28, 2010. OK TO PAINT. RESTORED TOPCOAT IAW SRM 51-21-27, PP 1-25, REV 77 FEB 01/10. SRI DO/TSDR COEA2010110303807Connector · mislocatedP TO F CONVERSION AT SAT: DURING MODIFICATION OF AFT PAX DOOR PER DWG 72-8100, THE CONNECTOR (FOR CARGO DOOR UNLOCK) WAS MISALLOCATED. PER ATR SRI DO/TS-5140/10-14251 AND SRAS DO/TS-5140/10...6062 FABRICATED AND INSTALLED REPAIR DOUBLER.SDR COEA2010091001807Door Frame · crackedAFT PASSENGER DOOR UPPER FRAME HAS A CRACK THAT MEASURES APPROXIMATELY 0.40 FROM E.O.P. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM.SDR 2010F00184Spar · corrodedRT HORIZONTAL STAB REAR SPAR WEB HAS AN AREA OF CORROSION BELOW PANEL 342 EZ BEYOND SRM LIMITS. REMOVED CORROSION IAW SRM 51-21-42, REV 77. MEASURED AFFECTED AREA MIN MATERIAL REMAINING .037" REF NTM 51-40-00 REV 34. CONFIRMED CRACK FREE CONDITION REF NTM 51-SDR 2010F00178Floorbeam · corrodedFLIGHT DECK, FLOORBEAM 11 ABOVE STRINGER 20L HAS SURFACE CORROSION ON UPPER SURFACE AND ON INTERCOSTAL JUST AFT OF BEAM CORROSION BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION IAW ATR 72 SRM 51-21-42 REV 77. VERIFY CORROSION REMOVAL ON FLOORBEAM 11. PRIMESDR 2010F00177Crease Beam · corrodedRT CREASE BEAM WEB AFT OF FRAME 39 HAS AREAS OF CORROSION BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION IAW ATR 72 SRM 51-21-42 REV 77. FOUND MATERIAL LOSS TO BE BEYOND SRM LIMITS IAW ATR 72 SRM 53-61-00 FIG 301 AND 53-67-70 FIGURE 109 ITEM 30 REV 77. REMSDR COER2010F00175Seat Track · corrodedRT INBD SEAT TRACK COMMON TO FRAMES 29-36 CORRODED BEYOND SRM LIMITS. REMOVED CORROSION FROM MULTIPLE AREAS FRAME 23-29 PITTING CORROSION AT PREVIOUS BLENDED, PRIMED AREAS AT MARKED AREAS FOUND TO BE "OUT OF LIMITS" PER SRM 51-21-42, 53-00-00 FIG 304 REV 77.SDR 2010F00174Seat Track · corrodedLT INBD SEAT TRACK COMMON TO FRAMES 29-36 CORRODED BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION PER ATR 72 SRM 51-21-42 REV 77. REMOVED LT INBOARD SEAT TRACK 29-36 PER ATR 72 SRM 51-25-01 REV 77. SEAT TRACK FABRICATED. INSTALLED SEAT TRACK FLOORBEAM 29SDR 2010F00173Seat Track · corrodedLT INBD SEAT TRACK COMMON TO FRAMES 29-36 CORRODED BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION PER ATR 72 SRM 51-21-42 REV 77. REMOVED LT O/B SEAT TRACK FROM FRAME 29L TO 36L PER ATR 72 SRM 51-25-04. SEAT TRACK FABRICATED. INSTALLED LT O/B SEAT TRACK FSDR 2010F00172Seat Track · corrodedRT INBD SEAT TRACK COMMON TO FRAMES 21-23 CORRODED BEYOND SRM LIMITS. (LEVEL II) REMOVED SEAT TRACK SECTION FROM BETWEEN FRAMES 20-21 UP TO FRAME 23 PER ATR 72 SRM 51-25-04 REV 77. INSTALLED SPLICE, SEAT TRACK, AND RADIUS BLOCK AT FRAME 23 IAW ATR 72 SRM 51-SDR 2010F00171Seat Track · corrodedRT INBD SEAT TRACK COMMON TO FRAME 23-29 CORRODED BEYOND SRM LIMITS. (LEVEL II) BLENDED OUT SCRATCHES AND CORROSION AT FR 27 LBL325 IAW ATR 72 SRM 51-21-58 REV 77. FOUND TO BE OUT OF LIMITS IAW ATR 72 SRM 53-00-00 REV 77 FIG 304. REMOVED LT I/B SEAT TRACK FSDR 2010F00170Seat Track · corrodedLT INBD SEAT TRACK COMMON TO FRAME 23-29 CORROSION BEYOND SRM LIMITS. (LEVEL II) BLENDED CORROSION ON LT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 29 IAW ATR 72 SRM 51-21-42 REV 77. MEASURED MATERIAL LOSS AT BLEND AREAS AND FOUND VARIOUS AREAS BETWEEN FRAMESSDR 2010F00169Seat Track · corrodedCARGO COMPARTMENT SEAT TRACK LT SIDE AT FLOORBEAM 36-41 HAS CORROSION BEYOND SRM LIMITS. (LEVEL II) REMOVED SEAT TRACK SECTION FROM 38-41 IAW ATR 72 SRM 51-25-04. LOCATED & DRILLED NEW SEAT TRACK FROM FB36-41 IAW ATR 72 SRM 51-25-04 ALL SRM REV 77. INSTALLESDR 2010F00168Seat Track · corrodedCARGO COMPARTMENT SEAT TRACK AT FLOORBEAM 41 RT SIDE HAS (6) INCH AREA IN TRACK WITH CORROSION BEYOND SRM LIMITS. (LEVEL II) REMOVED SEAT TRACK IAW ATR 72 SRM 51-25-04 REV 77. EVALUATED CORRODED AREA AND FOUND TO BE OUT OF LIMITS IAW ATR 72 SRM 53-00-00 FIG SDR 2010F00167Seat Track · corrodedRT OTBD SEAT TRACK FROM FLOORBEAM 29 TO FLOORBEAM 36 HAS PITTING CORROSION AND WEAR BEYOND SRM LIMITS FROM SEAT ATTACHMENTS. REMOVED CORROSION PER ATR 72 SRM 51-21-42 REV 77. REMOVED RIGHT O/B SEAT TRACK FROM 29 TO 36 PER ATR 72 SRM 51-25-01. SEAT TRACK FABSDR 2010F00166Beam · misrepairedFOUND UNAPPROVED SRM REPAIR ON FWD END OF PAX DOOR BEAM 8. REMOVED BEAM 8 IAW ATR 72 SRM 51-25-01 REV 77 AND ATR 72 SRM 51-25-04 REV 77. RECEIVED NEW BEAM PART NUMBER S5217620521401 & MATCH DRILLED TO EXISTING STRUCTURE. INSTALLED BEAM IAW ATR 72 SRM 51-25SDR 2010F00165Intercostal · corrodedPAX CREW DOOR LOWER FWD PAN IS CORRODED OUTSIDE SRM LIMITS APPROXIMATELY 3 INCHES FWD OF BOTTOM SPLICE AT INNER SKIN. (LEVEL II) REMOVED INTERCOSTAL IAW ATR 72 SRM 51-25-01 REV 77. REMOVED CORROSION FROM INTERCOSTAL IAW ATR 72 SRM 51-21-42 REV 77 AND ATR 72 SSDR 2010F00164Intercostal · corrodedPAX CREW DOOR 3RD INTERCOSTAL FROM FWD SIDE BETWEEN BEAM 3 AND 4 IS CORRODED OUT OF SRM LIMITS ON OUTER SKIN FLANGE.(LEVEL II)SDR 2010F00163Intercostal · corrodedPAX DOOR 3RD INTERCOSTAL FROM FWD SIDE BETWEEN BEAM 3 AND 4 IS CORRODED ON OUTER SKIN FLANGE BEYOND SRM LIMITS. REMOVED INTERCOSTAL IAW SRM 51-25-01 REV 77. REMOVED CORROSION FROM INTERCOSTAL IAW SRM 51-21-42 REV 77 & SRM 51-21-58 REV 77. FOUND TO BE OUT OF
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