N316FE
Service difficulty reports · 107
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 = 'N316FE' 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 = 'N316FE' 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 FDEA201703020748Vane · delaminatedLEFT OTBD FLAP VANE, RUBSTRIP NR 6 FROM THE INBD END IS DELAMINATED. DELAMINATION FOUND UNDERNEATH RUBSTRIP ON TOP SKIN, 2.75 INCH DIA. REPAIRED THE FLAP VANE RUBSTRIP IAW SRM 51-71-00, VOL 2, FIG 72, PG 154.SDR FDEA201703020731Skin · crackedRIGHT WING FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACK 0.75 IN LENGTH. REPAIRED IAW SRM 57-10-00, FIG 107, SHEET 2.SDR FDEA201702280687Intercostal · corrodedRIGHT WHEEL WELL AFT BULKHEAD TOP INTERCOSTAL CORRODED. REMOVED AND REPLACED THE BULKHEAD INTERCOSTAL IAW DWG AEA0026-6.SDR FDEA201702250942Support · corrodedAFT WASTE COMPT: UNDERSIDE OF UPPER CENTER SEAT TRACK SUPPORT HAS MULTIPLE AREAS OF EXFOLIATION CORROSION. INSTALLED CENTER SEAT TRACK SUPPORTS REF DWG AGA7442, SEC JPF STEPS 11 & 12 JPF ATTACH.SDR FDEA201605251731Pitot Line · contaminatedON TAKEOFF ROLL RNWY 18R, AT 80 KNOTS CALL, HUD SHOWED NO AIRSPEED TAPE & 36 KNOTS INDICATED. CAPTAIN'S PFD SHOWED ACCURATE AIRSPEED, BUT NO AIRSPEED TAPE. REJECTED TAKEOFF AT 95 KNOTS. FIRST OFFICERS PFD INDICATIONS ARE NORMAL. PURGED BOTH CAPTAIN`S & FIRSDR FDEA201604031140Skin · damagedLEFT WING LIGHTNING STRIKE REPAIR, REF WRI 57-10/0236, WAS ACCOMPLISHED IAW EA 8-5700-T0324518 REV A, WHICH IS CLASSIFIED AS A MAJOR REPAIR. THIS REPAIR WILL REQUIRE AN RII BUYOFF FOR ALL REPAIR STEPS LISTED IN THE EA. COMPLIED WITH EA 8-5700-T0324518 A.SDR FDEA201512214060Battery · lowEMERGENCY LIGHT BATTERY 1 LOW. PERFORMED EMER LIGHT ADJUSTMENT TEST, PASSED IAW AMM 33-51-00-5.SDR FDEA201504101209Warning System · activatedAFTER LANDING WITH FIRM BRAKE APPLICATION AT APPROX 80KTS, ACFT SHUTTERED FOLLOWED BY UNSAFE GEAR INDICATION ON CTR GEAR & LOSS OF NR 1, 1 & 3 HYD SYS.SDR FDEA201503130920Fire Bottle · low pressureENGINE FIRE AGENT LOW ALERT ON DEU. TROUBLESHOT IAW FIM 26-21-00-2-0. FOUND NR 1 ENGINE FIRE BOTTLE 1 WITH LOW PRESSURE SWITCH BAD. R & R THE NR 1 ENGINE FIRE BOTTLE IAW AMM 26-21-01-4. OPS CHECKED GOOD IAW 26-21-01-5. ACFT OK FOR SERVICE.SDR FDEA201502270612Tee Fitting · crackedRIGHT LE HORIZONTAL STAB MOST INBD SECTION HAS TWO CRACKS ON STIFFENERS. REMOVED CRACK FROM UPPER HORIZONTAL LE ALC7272-45 IAW SRM 55-00-01 FIG 1A. INSTALLED REPAIR ON LOWER TEE CHORD AT STATION XFS166 IAW EA 8-5510-T0315704.SDR FDEA201502270604Access Panel · damagedLEFT HORIZONTAL STAB INBD DETACHABLE ELEVATOR ACCESS PANEL 344AT DAMAGED. EXPOSED HONEYCOMB AT OTBD TE AREA. REPAIRED LT HORIZONTAL STATION INBD DETACHABLE ELEVATOR ACCESS PANEL 344AT IAW SRM 51-71-00 & PAINTED IAW SRM 51-21-02 VOL II.SDR FDEA201502250594Panel · delaminatedLEFT HORIZONTAL OTBD LOWER HINGE PANEL 334KB HAS DELAMINATION. REPAIRED DELAMINATED PANEL 334KB IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.SDR FDEA201502250593Cowling · delaminatedNUMBER 2 ENG LT FAN COWL IS DELAMINATED AT UPPER FWD OUTER SURFACE. REPAIRED NR 2 ENG LT FAN COWL AT UPPER FWD OUTER SURFACE IAW SRM 51-71-00 VOL II, SRM 54-32-01 VOL III. PAINTED IAW SRM 51-21-02 VOL II.SDR FDEA201502220577Skin · crackedLEFT WING, FWD PANEL LAND IS CRACKED JUST INBD OF PANEL 526FB. FABRICATED REPAIR DOUBLER IAW SRM 57-10-11 VOL 1 FIG 49. INSTALLED FABRICATED REPAIR DOUBLER IAW SRM 57-10-00 VOL 1 FIG 49.SDR FDEA201502210567Skin · corrodedBS 1219, RBL 48 SKIN PANEL FWD OF CTR WING TANK HAS CORROSION. REPAIRED IAW EA 8-5710-T0315698.SDR FDEA201502190553Panel · crackedRIGHT HORIZONTAL STAB LE PANEL 341 EZ HAS TWO CRACKS ON BULKHEAD OPENING. REMOVED DAMAGED AREA, FABRICATED SPLICE DOUBLERS IAW DWG ALC7222. INSTALLED REPAIR DOUBLERS IAW EA 8-5510-T0315537.SDR FDEA201502170539Panel · crackedRIGHT WING, LOWER SURFACE PANEL LAND IS CRACKED AT AFT INBD OF SLAT TRACK NR 8. R & R THE PANEL IAW SRM 57-21-01 FIG 5 & 51-31-01.SDR FDEA201502120517Wire · damagedWIRE NR M1103B20C DAMAGED, RT SIDE ABOVE AUX TANK. REMOVED AND REPLACED WIRE.SDR FDEA201502110512Landing · crackedRIGHT WING, SLAT TRACK NR 7 PANEL LAND CRACKED. R & R IAW SRM 57-00-01, 51-31-01, V2.SDR FDEA201502110511Skin · gougedRIGHT WING NR 5 SLAT HAS A GOUGE ON INNER SECTION OF SKIN. GOUGE IS OUT OF LIMITS. INSTALLED INNER DOUBLERS & FLUSH REPAIR IAW SRM 57-10-00 FIG 11 SH 1.SDR FDEA201408272332Coalescer Bag · dirtySMOKE CAME OUT OF OVERHEAD VENT AT REAR OF COCKPIT FOR APPROX 5 SECONDS. JUST TURNED UP COCKPIT & COURIER TEMPS FROM 67 TO 74 DEGREES. DONNED O2 MASKS & TURNED DOWN BOTH TEMPS TO 70 DEGREES. FIRST SMELLED SOMETHING HOT & THAT PROMPTED US TO TURN AROUND. TSDR FDEA201403290603Adiru · inoperativeDURING CRUISE, IAS MISCOMPARE ALERT CAME ON BOTH CAP & FO`S PFD. AIRSPEED MISCOMPARE STARTED AT 4 KTS THEN WENT TO APPROX 50 KTS MISCOMPARE BETWEEN BOTH PFD'S, FOLLOWED BY AUTO THROTTLES DISENGAGED, AUTOPILOT DISENGAGED & FLIGHT DIRECTOR DISAPPEARED. ALTITUSDR FDEA201303290688Duct · blownAT FL330, LEVEL 2 "AIR SYS NR 1 PRESSURE LOW". SYS SHOWED 11 PSI W/BLEED NR 1 ON. PRESSURE WAS 42 WITH 1-2 ISOL ON. PERFORMED T/S IAW FIM 36-10-32 INTERROGATE CFDS PSC NR 1 FAULT REVIEW AND CURRENT FAULT FOUND PREVIOUS LEGS FAN AIR VALVE TORQUE MOTOR OPEN.SDR FDEA201301160106Lamp · inoperativeR1 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WILL NOT TEST, LIGHT INOPERATIVE. REPLACED LAMPS, OPS CHECKED GOOD IAW STANDARD MX PRACTICE.SDR FDEA201211023820Battery · overheatedON INSPECTION OF CAC, FOUND BATTERY SMOKING, OVERHEATED, REMOVED BATTERYS, RINSED AFFECTED AREAS WITH DISTILLED WATER. DRIED, RINSE FLUID AS REQUIRED. VISUAL INSPECTION REVEALED NO DAMAGE. CLEANED IAW THE AMM 24-31-11-04. OK TO CONTINUE.SDR FDEA201210253743Hinge · brokenDISCOVERED DROP PANEL OTBD OF CENTER FLAP FAIRING MISSING. HINGE THAT ATTACHES TO BOTTOM OF WING AND PANEL IS BROKEN AT EVERY LOBE. INSTALLED DOOR PANEL IAW EA 8-5720-164721. ACFT OK FOR SERVICE.SDR FDEA201210223727Switch · failedAFTER TAKEOFF, MASTER CAUTION ILLUMINATED, WITH LEVEL 1 AVNCS EXT ACC DR ALERT. MISC PAGE WAS CHECKED BEFORE T/O. ALERT WAS NOT DISPLAYED. REMOVED, REPLACED AVIONICS DOOR CLOSE SWITCH IAW MM 52-41-02-2. OP'S CHECK GOOD. FINAL CLOSED.SDR FDEA201210113598Unknown · odorDURING GROUND OPS, AFTER SELECTING PACK ONE AND 3 ON (WITH APU RUNNING), COCKPIT FILLED WITH THE ODOR OF RAW JET FUEL. NOT THE ODOR OF JET EXHAUST. PACKS WERE TURNED OFF AND COCKPIT WAS VENTILATED. FOUND APU LEAKING FUEL INTO APU INLET. SHUTDOWN APU AND CSDR FDEA201209133327Terminal · burnedTANK 2L AFT PUMP LO LEVEL 1 ALERT IN CRUISE FLIGHT. COMPLIED WITH LEVL 1 QRH CHECKLIST FUEL PUMP TNK 2, LT C/B (G-17) WAS POPPED BY FUEL PUMP. IN ADDITION, THERE WAS A SIGNIFICANT EVIDENCE OF FLAME/SMOKE/HEAT EXPOSURE TO TERMINAL STRIP S3-372 AND SEVERAL INSDR FDEA201206282394Proximity Switch · failedAFTER TAKE OFF AND RAISING SLATS, RECEIVED A SLAT DISAGREE LIGHT, SLATS OUT LIGHT WENT OUT, RAN QRH, RETURNED TO DEPARTURE AND LANDED OVERWEIGHT UNEVENTFULLY. INSTALLED PSEU IAW MM 31-71-01-2. COMPLIED WITH RTS OF PSEU IAW MM 31-71-01. RTS PASSED CYCLED FSDR FDEA201201310403Wire · damagedLEFT MLG UNSAFE INDICATION. BOTH SYNOPTIC AND PRIMARY AURAL WARNING "LANDING GEAR" CONTINOUS. ALTERNATE GEAR HANDLE REMAINS UP. CENTER GEAR IS STOWED. REPAIRED WIRES TO ELECTRICAL CONNECTOR R5-246 IAW WDM 32-61-11. WIRES CHECKED GOOD. FOUND LT GEAR TARGET SDR FDEA201107112643Skin · misrepairedRT INBD ELEVATOR UPPER SKIN EXISTING REPAIR NOT IN COMPLIANCE IAW ENGINEERING AND WITH SRM. REMOVED DAMAGE PER SRM 51-10-00, FABRICATED REPAIR SKIN. INSTALLED REPAIR IAW SRM 55-10-00, 51-31-01 AND 51-21-02 .SDR FDEA201107092630Skin · dentedLT WING NR 8 SLAT L/E HAS SEVERAL DENTS. FABRICATED REPAIR PARTS, UPPER AND LOWER DOUBLER, SPLICE PLATE, BAFFLES, UPPER AND LOWER SEAL, AND FILLER. INSTALLED REPAIR PARTS IAW SRM 57-10-00 VOL VI FIG 11. CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201107052586Floorbeam · corrodedCTR CARGO COMPT BS 1781 FLOORBEAM UPPER CHORD AFT FLANGE LOWER SURFACE CORRODED RBL 26-31. REMOVED FLOORBEAM AND ROLLER TRAYS TO GAIN ACCESS TO DAMAGED AREAS IAW SRM 57-31-01 VII. CLEANED UP CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-21-01 VII. AND 53-00-01SDR FDEA201106272432Seat Track · corrodedCOURIER AREA SEAT TRACK LBL 8, STA 430 HAS CORROSION. BLENDED CORRSION IAW SRM 51-21-01. ORIGINAL MAT. THICKNESS .090", BLENDED .065". MAT REMAINING .025. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG. 5. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01.SDR FDEA201106222703Skin · crackedLEFT STA 500, STR 37L, EXTERNAL FUSELAGE HAS DOUBLER NOT IAW SRM OR APPROVED DATA. COMPLIED, REPAIRED IAW EA 8-5330-152407, DATED 6-29-11. LEAK CHECKED IAW AMM21-00-01-5-0, NO LEAKS NOTED.SDR FDEA201104221590Engine · malfunctionedREJECTED T/O 18R, ENG FAIL LIGHT ON BETWEEN 80 & 90KTS. REJECTED BY 100 KTS. TO GW 377,000. N1 NR2 MORE THAN 11 PERCENT HIGHER THAN NR 3. IAW JRH DECREASED PART POWER TRIM SCREW ON NR 2 ENGINE APPROX .6250 TURN, COUNTERCLOCK WISE DIRECTION JRH SECTION 7, SDR FDEA201008052845Accumulator · leakingAT FL 340 LOST HYD SYST 3. COMPLIED WITH QRH. UNEVENTFUL LANDING, LEAK ENDED UP COMING FROM THE UPPER BRAKE PRESSURE ACCUMULATOR IN RT WHEELWELL. REMOVED AND REPLACED PER MM 32-44-01-2. LEAK AND OPS CHECK GOOD.SDR FDEA201008012755Engine · malfunctionedDURING TAKEOFF ROLL, WITH AUTOTHROTTLES ENGAGED AT 85 TO 90 KTS A LEVEL 1 ENG 3 EXCEDEANCES ANNUNCIATED. ABORTED TAKEOFF. COMPLIED WITH QRH. N2 NR 3, 109.6 INSPECTED ENGINE EXHAUST FOUND NO PARTICLES PRESENT. NR3 ENGINE, N2 EXCEEDANCE 109.6 REQUIRES BORESCOPSDR FDEA200912174477Fire Warning · illuminatedAFTER INS FOR ALIGN - 1 MIN GOT CARGO FIRE FLASHING - PUSHED BUTTON WITH ACW PHASE ONES. REMOVED LARGE(135 LB) CARGO FIRE EXTINGUISHER BOTTLE IAW MM 26-22-01-4 (3 EA) CIRCUIT BREAKERS PULLED AND COLLARED DISCHARGE CARTRIDGES AND DISCHARGE HEADS REMOVED IAWSDR 07FDEA02370Access Panel · missingCTR CARGO DOOR ACCESS PANEL FOR VENT DOOR MISSING ON ARRIVAL INTO PDX. OIL: NO RESTRICTION LOWER CENTER CARGO DOOR VENT DOOR MISSING. (OK PER EA 8-5230-113246), (CK AFTER EA FLT) INSPECTED SCRATCH PER SMP 51-80-01 AND DOOR ALL WITHIN LIMITS. COMPLIED WISDR 05FDEA00801Strut · damagedON TAKEOFF FROM MEM, CENTER GEAR INDICATED UNSAFE UP. BOTH DISPLAYS SHOWED UNSAFE UP. COMPLIED WITH ALL CHECKLISTS AND LANDED KMEM 36C. REMOVED CENTER LANDING GEAR SHOCK STRUT, PER FEDEX WORK CARD 32T7101. REMOVED THE CTR LDG AFT W/W LT AND RT GEAR DOORS SDR 05FDEA00264Sill · crackedFOUND CRACK IN RIGHT WING ISLAND SILL PART ARC7008-2.SDR 04FDEA03410Selector Valve · leakingSHORTLY AFTER LEVEL OFF GOT LEVEL 1 ALERT HYD 3 ELEV OFF, NOTED THAT HYD 3 QUANTITY WAS DECREASING AT 2.5 GALS. HSC SHUTOFF NR 3 HYD. HYD 3 OFF LEVEL 1 ALERT. AFTER SLATS EXTENDED ON APPROACH, HYD 3 RESTORED. REMAINING FLUID LEAKED OUT, HYD 3 FAILED. GEARSDR 04FDEA02868Blanket · burnedIN CENTER ACCESSORY COMPARTMENT AT THE LT AND RT FUSELAGE FEED THROUGH FOR THE PNEUMATIC SUPPLY DUCTS 1-2 AND 1-3 HAVE FUSELAGE INSULATION BLANKETS SEVERELY BURNED AROUND THE DUCT. A/C FUSELAGE WAS INSTALLED WITH OLD TYPE OF INSULATION BLANKET. (P/N 392945SDR 03FDEA01984Regulator Valve · inoperativeSHORTLY AFTER TAKEOFF TRIM AIR OFF LIGHT ILLUMINATED COURIER SUPPLY TEMP INCREASED TO 215 DEG IT THEN DROPPED AND TRIM AIR OFF LIGHT EXTINGUISHED. SUPPLY TEMP ROSE AGAIN, CYCLED REPEATED MULTIPLE TIMES. RETURNED TO BASE. BOTH TRIM AIR PRESSURE REGULATOR VSDR 03FDEA01040Computer · malfunctionedAFTER TAKEOFF AT 1000 FEET AGL HAD RED MANIFOLD FAIL NR 2, RTB IN ACCORDANCE WITH QRH. RESET MANIFOLD FAILURE DETECTION LOOP NR 2 CIRCUIT BREAKER. PER SMP. PERFORMED AIR TEST, PASSES PER MM 36-23-01-5. RAN NR 2 ENGINE OP'S CHECK NORMAL 181623 PER JRH. REMSDR 03FDEA00864Warning System · malfunctionedON APP AT GEARDOWN 4 GREEN AND FLAPS 35 LVL 2 ALERT SLAT DISAG DURING GO-AROUND AT FLAPS 22 ALERT WENT OUT. CLEANED UP CONFIG AND RECYCLED GEAR AND FLAPS ON DOWNWIND. GEAR FLAPS AND SLATS ALL WORKED NORMAL. FLAPS 50 NORMAL LANDING. PERFORMED FCC RTS WITH NSDR 03FDEA00729Skin · crackedCOMPLY WITH E.A. 8-5722-70371, WINGS - REPAIR OF MINOR DAMAGE TO LEADING EDGE SLAT SKIN. ACT 07MAY03 06:26 BFM R COMPLIED WITH E/A 8-5755-70371 AT MAE/BFM.SDR 02FDEA00693Proximity Switch · faultyON APPROACH, WHEN LANDING GEAR HANDLE MOVED TO EXTEND, RECEIVED ALL UNSAFE GEAR INDICATIONS ON BOTH LANDING GEAR INDICATORS AND CONFIG PAGE. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT AND TESTED GOOD IAW MD 10-3
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