N320FE
Service difficulty reports · 183
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 = 'N320FE' 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 = 'N320FE' 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 FDEA202110062471Fuse · leakingON SHORT FINAL AT KIND WITH SLATS EXTENDED AND FLAPS 22 DEG WE EXTENDED THE LANDING GEAR. VERY SOON AFTER EXTENDING THE LANDING WHILE PERFORMING THE BEFORE LANDING CHECKLIST, WE RECEIVED A LEVEL 2 HYD 3 FAIL ALERT. WE IMMEDIATELY CALLED UP THE HYD SYNOPTIC ASDR FDEA202007311734Warning Message · illuminatedLEVEL 1 AIR SYS 3 OFF ILLUMINATED FOURTEEN MINUTES INTO FLIGHT AT FL 280. ASSOCIATED BLEED (3) AND PACK (3) OFF. RED DUCT LINE ILLUMINATED ON AIR SYNOPTIC. COMPLIED WITH QRH. REF MM 36-00-01-5, PERFORMED DECAY CHECK OF #3 PNEUMATIC SYSTEM, DECAY CHECK PASDR FDEA2020071091474Warning Light · false activationLVL 1 AIR SYS OFF ALERT. AIR SYS AUTOMATICALLY SHUT OFF NR 3 BLEED AND NR 3 PACK. NR 3 DUCT WENT MOMENTARILY RED PRIOR TO AUTO SHUTDOWN OF NR 3 AIR SYS. CHECKED PNEUMATIC MANIFOLD FAULT INDICATOR IN CAC. NO FAULT BALLS ARE ILLUMINATED. CHECKED AIU'S, SDR FDEA202006201300Warning Message · false activationEMER LT BAT 1 LOW ON PREFLIGHT PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MD-10-30 AMM 33-50-00-5-0. OPS CHECK GOOD; OK FOR SERVICE.SDR FDEA2020062301300Battery · low voltageEMER LIGHT BAT 1 LOW ON PREFLIGHT.SDR FDEA202006161253Control Module · failedON APPROACH SLATS EXTENDED, FLAPS WOULD NOT MOVE, HANDLE STUCK. EXECUTED A GO AROUND. SPENT SOME TIME WIGGLING THE HANDLE AND DIAL- AND-FLAP AND FINALLY GOT THEM TO MOVE. AFTER LANDING CLEANED UP THE WING AND ATTEMPTED TO EXTENDED FLAPS AGAIN . HANDLE STUSDR FDEA2019112633066Beam · corrodedCORROSION ON NUT PLATES FOR FLOOR ATTACHMENTS, AFT CARGO COMPARTMENT AT STA 1902. REMOVED CORROSION IAW SRM 53-00-01 VOL II. ORIG THICKNESS 0.063". AFTER REWORK 0.045". OUT OF LIMITS. FABRICATED ANGLE ON T19/1450803. INSTALLED ANGLE IAW SRM 51-31-01 VOL SDR FDEA2019111542960Landing · crackedH-STAB ACCESS PANEL 311AB LANDING ON LH HAS A CRACK REMOVED DAMAGE IAW SRM 53-00-01 FIG 4 SHT 2. PERFORMED HFEC IAW SOPM 06-10-01-001. NO FURTHER CRACKS REMAIN. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO 8- 5310-T0350635 PT1 TITLE: FUSELAGE - MAIN FSDR FDEA2019111542959Stop · wornLATCH STOPS WORN ACCESS PANEL 311AB RH SIDE. TITLE: FUSELAGE - PLATES AND SKINS - 311AB ACCESS DOOR CUTOUT LANDING SKIN RH FWD DAMAGE REPAIR WAS ACCOMPLISHED ON EA 8-5310-T0350318. MAJOR REPAIRSDR FDEA2019111522935Nut Plate · damagedLT I/B FLAP INBOARD HOIST FITTING HAS 2 EACH NUT PLATES STRIPPED OUT. REMOVED AND REPLACED 2 EA NUT PLATES ON LT I/B FLAP I/B HOIST FITTING IAW DWG ARC2369 AND SRM 51-31-01 VOL II. SKIN SPLICE REPAIR IAW SRM 57-10-00 FIG 86 VOL I. RSC TRACKING ON EA T8-5750SDR FDEA2019102412717Floor Panel · damagedMAIN CARGO FLOOR PANEL BETWEEN STA 595 AND STA 675 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 595 TO STA 675 BETWEEN X27.5 AND X47.5 FABRICATED ON VTMAE TRAVELERR T19/1448546 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.SDR FDEA2019102412716Floor Panel · damagedMAIN CARGO FLOOR PANEL BETWEEN STA 765 AND STA 795 BETWEEN X91.5 AND X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 765 TO 795 BEWTEEN X91.5 AND X107.5 FABRICATED ON VTMAE TRAVELER T19/1448549 IAW SRZ-25-005 CAT "A" MAJOR REPAIRSDR FDEA2019102412715Floor Panel · damagedMAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 FABRICATED ON VTMAE TRAVELER T19/1448544 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.SDR FDEA2019102412714Floor Panel · damagedMAIN CARGO FLOOR PANEL BETWEEN STA 675 AND STA 735 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 675 - STA 735 BETWEEN X27.5 TO X47.5 FABRICATED ON VTMAE TRAVELER T19/1448545 IAW SRZ-25-005 CAT "A" MAJOR REPAIRSDR FDEA2019102412713Floor Panel · damagedMAIN CARGO FLOOR PANEL BWTWEEN STA 595 AND STA 675 BETWEEN -X75.5 AND -X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 595-675 AND BETWEEN -X75.5 AND -X107.5 FABRICATED ON MAE TRAVELER T19/1448049 IAW SRZ 25-005. CAT "A" MAJOR REPAIR.SDR FDEA2018042601108Light · malfunctionedDURING PREFLIGHT, WHEN SELECTING EMERGENCY PWR SWITCH TO ARM, THE ON LIGHT REMAINED ILLUMINATED. RESET FUEL LEVERS. ACFT HAD POWER DROP OFF DURING PREFLIGHT. COMPLIED WITH AN OPS TEST IAW AMM 24-00-00-5. OK FOR SERVICE.SDR FDEA201712283460Transmitter · out of adjustAT 121 KNOTS DURING TAKEOFF, RECEIVED AN AUDIBLE WARNING FOR THE FLAPS, FOLLOWED BY A WARNING FOR THE SLATS. . REJECTED TAKEOFF AT 130 KNOTS. PERFORMED A FLAP INDICATION TEST, FOUND TRANSMITTER IN LIMITS . LIB, RIB, & LOB ARE BELOW OR AT LOW END OF TOLERANSDR FDEA201711043166Bulkhead · crackedNR 3 AC PACK COMPARTMENT STA 475 BULKHEAD WEB, A/C CHECK VALVE FASTENER HOLE AT 4:30 POSITION HAS A .5 INCH CRACK PROPAGATING THROUGH HOLE. REPAIRED PER EA 8-5310-T0336280.SDR FDEA201710102886Panel · delaminatedLT WING, PANEL 541 LB IS DELAMINATED/SPLIT. REPAIRED LT WING, PANEL 541 LB AT THE DELAMINATED/SPLIT AREA REF SRM 51-71-00 VOL 2 PG 1-47 AND DRAWING NUMBER ARC0357.SDR FDEA201710042856Seat Track · wornMAIN DECK APPROX STA 1265, CENTER LINE X.8.5 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.SDR FDEA201710042855Seat Track · wornSEAT TRACK AT BS 625, RBL 27.5 IS DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1.SDR FDEA201710042854Seat Track · damagedSEAT TRACK BS 1581, LBL 75 DAMAGED. REPAIRED IAW SRM 53-70-00, FIG 1.SDR FDEA201710042853Seat Track · damagedMAIN DECK SEAT TRACK BS 565, LBL 8.5 SHOWS DAMAGE. REPAIRED IAW SRM 53-70-00, FIG 1.SDR FDEA201710033020Channel · crackedNR 3 A/C COMPARTMENT BS 555, LONGERON 34R FRAME J-CHANNEL HAS A 1.5 INCH CRACK. INSTALLED A TYPICAL FORMED CHANNEL REPAIR IAW SRM 53-00-01, FIG.8, SHEET 2, PAGE 30 & 31, VOL I.SDR FDEA201710032846Seat Track · damagedMAIN CARGO COMPT APPROX STA 1601 RBL 75 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.SDR FDEA201710032844Seat Track · wornMAIN DECK, APPROX STA 1039 LBL 75 GROOVE/ GOUGE WORN INTO TRACK. SEAT TRACK IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1.SDR FDEA201710012877Frame · crackedCENTER CARGO BAY, APPROXIMATELY BS 1841, LBL 6 AND RBL 6, FRAME WEB IS CRACKED. REPAIRED THE FRAME IAW SRM 51-00-01, FIG 10, SHT 5, VOL I.SDR FDEA201709303046Skin · crackedLEFT OTBD FLAP UPPER SKIN HAS A .75 INCH CRACK AT XOF 572. 5 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2.SDR FDEA201709303045Skin · crackedLEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A .4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.SDR FDEA201709303044Skin · crackedLEFT OTBD FLAP UPPER SKIN HAS A 2.0 IN. CRACK AT XOF 563. 12 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.SDR FDEA201709283088Skin · crackedLOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT UPPER AFT CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-T0336191.SDR FDEA201709283087Skin · crackedLOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT, AFT LOWER CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-0336191. MAJOR REPAIR.SDR FDEA201709283028Door · crackedLOWER FUSELAGE NR 3 ACM ACCESS DOOR UPPER FLANGE PREVIOUS REPAIR HAS CONTINUED TO CRACK. REPAIRED THE NR 3 ACM DOOR UPPER FLANGE CRACK IAW EA 8-5240-T0336127.SDR FDEA201709273132Tee Fitting · crackedBS 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2 INCH. CRACK EXTENDED THROUGH THE RADIUS. REPAIED THE BULKHEAD TEE CAP IAW EA T 8-5310-T0335740, PART 1 & 2.SDR FDEA201709273003Bulkhead Web · crackedNOSE WHEEL WELL RIGHT VERTICAL PANEL AT APPROX STA 480 HAS A CRACK APPROX 6 INCH LONG. INSTALLED WEB SECTION AND DOUBLERS REF. SRM 53-00-01 FIG.10 (SHEET 5) VOLI.SDR FDEA201709272925Web · crackedNOSE WHEEL WELL LEFT VERTICAL WEB PANEL BS 315, HAS A CRACK BEHIND THE HYDRAULIC LINES. REMOVED AND REPLACED DAMAGED SECTION OF THE WEB IAW SRM 53-00-01, FIG 10, SHT 4, 5, 7, PGS 50, 51, 53, AND DWG NCA6046, AND ACA3837.SDR FDEA201704201245Warning Message · false indicationAT FL 350, HAD A LEVEL 3 AIR MANIFOLD 3 FAILURE. RAN QRH, ALERT WENT AWAY. DECLARED AN EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRPORT. CHECKED MANIFOLD FAILURE INDICATORS IN CAC AND FOUND RT MANIFOLD PRESSURE SWITCH FAULTING IAW AMM 36-23-03-4-0, 36-0SDR FDEA201701030027Warning Light · false activationR1 DOOR SLIDE LIGHT ILLUMITATED. PERFORMED OPERATIONAL CHECK OF THE R1 DOOR SLIDE BOTTLE PRESSURE LIGHT IAW AMM 25-61-03-5-0. TESTED GOOD SEVERAL TIMES. OK FOR SERVICE.SDR FDEA201602140557Test Switch · faultyR1 DOOR EVAC SLIDE, REMOTE PRESSURE PRESS TO TEST INDICATING SYS INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01, CATEGORY C, EXPIRATION 24 FEB 16. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH SDR FDEA201510263375Skin Panel · crackedLEFT HORIZONTAL STABILIZER SKIN PANEL 7281-1, HAS A .700" CRACK JUST FWD OF REAR SPAR CAP, FWD BARREL NUT HOLE. R & R SECTION OF SKIN PANEL, PLANK, IAW EA 8-5510-T0320816.SDR FDEA201510263374Spar Cap · crackedLEFT HORIZONTAL STABILIZER, UPPER OUTER REAR SPAR CAP, FWD BARREL NUT HOLE HAS A .400" VERTICAL CRACK EXTENDING FROM BELOW THE BARREL NUT AT THE 5:00 POSITION. R & R SECTION OF REAR SPAR CAP IAW EA 8-5510-T0320816.SDR FDEA201510233327Panel · delaminatedLEFT WING HINGE PANEL 551DB HAS DELAMINATION. REPAIRED THE HINGE PANEL IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.SDR FDEA201510223316Panel · delaminatedAFT ENG INLET DUCT, RT SIDE PANEL 364JR, LOWER SFT DELAMINATED. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.SDR FDEA201510223315Panel · delaminatedAFT ENG INLET DUCT, RT SIDE PANEL 364JR DELAMINATED, LOWER FWD. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL. II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.SDR FDEA201510203292Fuel Door · damagedRIGHT WING REFUEL & DEFUEL DOOR, PUNCTURED ON UPPER MID SURFACE. REPAIR IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.SDR FDEA201510203291Panel · delaminatedLEFT WING NR 5 SPOILER PANEL HAS DELAMINATION, UPPER SURFACE. REPAIR SPOILER IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.SDR FDEA201510203285Wire · damagedFOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE OF ACFT. SPLICED IN A NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 29-12-01, AND E8-2810-7-5002 PT 1.SDR FDEA201510203284Wire · damagedFOUND DAMAGED WIRE LOCATED AT BS 1346, RT SIDE OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 33-32-02, AND E8-2810-7-5002 PT1.SDR FDEA201510203283Wire · damagedFOUND WIRE DAMAGED, LOCATED AT BS 1240, RT SIDE OF CENTERLINE OF ACFT. REPLACED WIRE IAW SWPM 20-10-03, 20-00-16, WDM 28-21-03, AND E8-2810-7-5002 PT1.SDR FDEA201510203282Wire · damagedFOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00- 16, WDM 52-33-01 AND E8-7-2810-5002 PT1.
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