N612FE
Service difficulty reports · 360
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 = 'N612FE' 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 = 'N612FE' 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 FDEA201804251117Unknown · multiple failAFTER TAKEOFF AT VR, TR-3 FAIL LEVEL 1 ALERT, DISPLAYS 4-6 AND MCDU NR 2 WENT BLANK. RAN QRH. AT BLOCK IN WITH EXTERNAL POWER CONNECTED TR3 CAME BACK ON. OPS CHECKED THE R2-18 IAW AMM 24-25-03-2, TR3 OPS NORMAL IAW AMM 24-31-01-2, AND WDM 24-57-07.SDR FDEA201803250776Doubler · crackedLEFT WING STRINGER DOUBLER XOS 900 LEADING EDGE SKIN, FOUND CRACKED FROM FASTENER HOLE TO STRINGER EDGE. REPAIRED IAW SRM 57-40-03-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803190731Skin · crackedVERTICAL STAB ACCESS PANEL 363ML CUTOUT FOUND TWO CRACKS, VSS 2154. REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803190730Spar Cap · crackedDURING HFEC INSPECTION, CARRIED OUT AT LOWER VERTICAL STABILIZER REAR SPAR CAP RT FWD FLANGE UPPER SECTION, AND FOUND ONE CRACK 3.70 INCHES LONG, HSS 2164. REPAIRED IAW EA 1-5530-T0339048, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803190729Spar Cap · crackedDURING HFEC INSPECTION, CARRIED OUT AT LOWER VERTICAL STABILIZER REAR SPAR CAP, LT FWD FLANGE UPPER SECTION, FOUND ONE CRACK 1 INCH LONG AT HSS 2164. REPAIRED IAW EA 1-5530-T0339008, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140684Skin · crackedLEFT WING FIXED LEADING EDGE AT XOS 991.5 LEADING EDGE SKIN FOUND CRACKED ABOUT 8 INCHES. REPAIRED IAW SRM 57-40-01-2R, FIG 261, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140683Doubler · crackedLEFT WING FIXED LEADING EDGE AT XOS 991.5 LOWER SURFACE DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140680Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140679Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201803140678Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140681Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140682Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140677Door Frame · crackedMAIN DECK L3 DOOR FRAME LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26L TO 27L FOUND CRACKED. THE L3 DOOR FRAME LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803130667Seat Track · chafedRT EXISTING REPAIR AT MAIN DECK CARGO FLOOR SEAT TRACK STA.625 TO STA.645 X = -47.5 RT EVALUATED AND FOUND CHAFED DAMAGE AT SEAT TRACK CROWN. MAIN DECK CARGO FLOOR SEAT TRACK AT STA.625 TO STA.645 X = -47.5 RT CARRIED OUT REPAIR PER SRM 53-00-52-2R FIG 201 REPSDR FDEA201803110648Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 1406, RBL 47.5. FOUND CROWN DAMAGED. GOUGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803110647Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 5-6 X= 27.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803110646Seat Track · damagedMAIN DECK SEAT TRACK AT BS 6-80, RBL 47.5 CROWN DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803060613Switch · inoperativeDURING A POSTFLIGHT CHECK, FOUND RIGHT SIDE EVACUATION SLIDE, REMOTE PRESSURE PRESS-TO-TEST SWITCH INOPERATIVE. R1 DOOR REMOTE PRESSURE INDICATOR ASSEMBLY REMOVED AND REPLACED, OPS TEST CARRIED OUT IAW AMM 25-61-04-4, AND AMM 25-61-04-710-801. FOUND SATISFASDR FDEA201802200494Motor · failedHORIZONTAL STAB TRIM RATE 2 CIRCUIT BREAKER FOUND OPEN. CONFIGURED THE ACFT TO OPS CHECK THE STAB TRIM MOTOR IAW MM 27-41-00-5, THE CIRCUIT BREAKER TRIPS DURING OPS CHECK. REMOVED AND REPLACED THE NR 2 HORIZONTAL STAB TRIM MOTOR SOSV IAW AMM 27-43-31-4,SDR FDEA201712293471Slat · detachedINFORMED BY ATC SOMETHING FELL OFF OUR ACFT ON TAKE OFF. CONFERED WITH GOC AND MOC AND DECIDED TO RTB. REMOVED AND REPLACED THE RIGHT NR 1 SLAT IAW AMM 27-80-20-000-801, AND PERFORMED AN ADJUSTMENT TEST IAW AMM 27-80-20-820-801. OPS NORMAL, ACFT OK FOR SESDR FDEA201711033162Gasket · cutAFTER TAKEOFF, PLUS 25 MINUTES, CLIMBING THROUGH FL250, THE NR 2 ENGINE FLAMED OUT. THROTTLES WERE SET AT CLIMB POWER WHEN CONFIRMED ENGINE OUT MESSAGE APPEARED ON MCDU SCRATCH PAD. NR 2 ENGINE PARAMETERS, N1 AT 51.4 %, EGT 335, N2 335, N2 AT 79.4%, FUEL FSDR FDEA201710193005Cadc · no testAT 110 KTS, ALT & IAS AMBER ALERTS APPEARED ON THE CAPTAIN`S AND FIRST OFFICER`S PFOS. DURING TROUBLESHOOTING IAW FIM 34-11-01-03, AND 34-11-03-03, FOUND THE NR 2 CADC WOULD NOT TEST. REMOVED AND REPLACED THE NR 2 CADC IAW MM 34-16-01-4, 34-10-00-2, 22-00-00SDR FDEA201708062129Lug · wornMCD FWD HINGE HAS 8 EACH LUGS NEED REWORK LUGS/BUSHING REWORKED REF CMM 52-34-04.SDR FDEA201708062128Lug · wornMCD DOOR FWD DOOR HINGE LUG/BUSHING WORN LUG/BUSHING REWORKED REF CMM 52-34-04.SDR FDEA201708062127Lug · wornMCD HINGE LUGS NEED REWORK/WORN LUGS/BUSHING REWORKED REF CMM 52-34-04.SDR FDEA201708062126Lug · wornLUGS NEED REWORK/WORN LUGS/BUSHING REWORKED REF CMM 52-34-04.SDR FDEA201701120137Door · crackedAIR CONDITIONING DOOR STRUCTURE ON THE PLANE AFT UPPER CORNER APPEARS TO BE CRACKED. REPAIRED THE AREA IAW SRM 53-20-15.SDR FDEA201603301118Skin · crackedONE EACH FASTENER HOLE NR 6 FOUND CRACK INDICATION, DURING OPEN HOLE HFEC INSPECTION, AT LT WING LOWERS SKIN ACCESS DOOR CUT OUT, BETWEEN STATION XORS 690 - XORS 700. REPAIRED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2,000SDR FDEA201603291113Skin · corrodedAFT ACCESSORY COMPARTMENT, RT SKIN WITH ANCHOR NUT ATTACH, FWD OF STATION 2164, FOUND CORROSION. SKIN REPAIRED PER SRM 53-70-01-2R FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201603291112Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED FOUND EXCEEDED LIMITS IAW CMM 57-52-04. EXISTING HOLE DIAMETER 1.193", FINAL HOLE DIAMETER 1.196, MAXIMUM ALLOWABLE HOLE DIAMETER 1.15". NEW REPAIR BUSHINGSDR FDEA201603291111Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.190", FINAL HOLE DIAMETER 1.225" & MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR SDR FDEA201603291110Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.215", FINAL HOLE DIAMETER 1.250", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRSDR FDEA201603291109Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.255", FINAL HOLE DIAMETER 1.285", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABSDR FDEA201603291108Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.257", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRISDR FDEA201603291107Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE, FOUND CORRODED. CORROSION REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.248", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSDR FDEA201603291106Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.216", FINAL HOLE DIAMETER 1.226 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291104Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709".SDR FDEA201603291103Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, UPPER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.957", FINAL HOLE DIAMETER 0.961 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.944".SDR FDEA201603291102Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.228 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291101Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.284", FINAL HOLE DIAMETER 1.289 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603281090Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".SDR FDEA201603281089Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".SDR FDEA201603281088Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SURFACES, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.412", MATERIAL REMOVED 0.002" & MINIMUM ALLOWABLE THICKNESS 0.423". NESDR FDEA201603281087Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD. STUD ATTACH SURFACES FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.420", MATERIAL REMOVED: 0.010" & MINIMUM ALLOWABLE THICKNESS 0.423". NSDR FDEA201603281086Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44- 08. EXISTING HOLE DIAMETER 0.720", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.7SDR FDEA201603271081Doubler · crackedLEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271080Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 830, X=-8.5 FOUND CORROSION. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 785 - 907, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271079Doubler · crackedRIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 613. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271078Doubler · crackedLEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 543. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.220", FINAL HOLE DIAMETER 1.223 & MAX ALLOWABLE HOLE DIAMETER 1.220". NEW R
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