N628FE
Service difficulty reports · 234
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 = 'N628FE' 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 = 'N628FE' 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 FDEA201506262073Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT INBD HOLE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0318565 P1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262072Hinge Bracket · corrodedRIGHT WING FLAP OTBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHINGS FABRICATED & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262071Hinge Bracket · corrodedLEFT WING, OTBD FLAP INBD FWD HINGE BARREL NUT HOLE HAS CORROSION. WORKED IAW CMM 57-44-08 AND REPAIRED IAW EA 1-5750-T0318531 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262070Skin · gougedRIGHT WING, FIXED LE ABOVE NR 6 SLAT, FOUND WITH DEEP GOUGE AT XOS 855.964. REPAIRED IAW SRM 57-40-02-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506262069Frame · dentedMAIN DECK CARGO BS 1701, LONGERON 12L FRAME. REPAIR FOUND DENTED. FRAME TRIMMED OUT & REPAIRED IAW SRM 53-0-07-2R REPAIR 2 FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506262068Frame · chafedMAIN DECK CARGO BS 1661, LONGERON 12L FRAME. REPAIR FOUND CHAFED. REPAIR REMOVED IAW SRM 51-31-01-0G & INSTALLED WITH NEW FABRICATED REPAIR DOUBLER IAW SRM 53-00-07-2R FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506262067Frame · dentedMAIN DECK CARGO BS 1681, LONGERON 12L FRAME. REPAIR FOUND DENTED. REPAIR REMOVED IAW SRM 51-31-01-0G & INSTALLED WITH NEW FABRICATED REPAIR DOUBLER IAW SRM 53-00-07-2R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506262066Hinge Bracket · corrodedLEFT WING, OTBD FLAP INBD FWD HINGE LOWER INBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262065Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE LOWER OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262063Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262062Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262060Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252038Web · crackedCABIN MAIN DECK CARGO COMPARTMENT BS 1310, LONGERON 26L AFT L3 DOOR LOWER JAMB FOUND WEB CRACKED. REPAIRED IAW EA 1-5310-T0318727 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506252037Web · crackedMAIN DECK CARGO BS 1256, LONGERON 26L, FWD L3 DOOR LOWER JAMB WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201506252036Web · crackedMAIN DECK CARGO BS 1310, LONGERON 26R AFT R3 DOOR LOWER JAMB WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506252035Web · crackedCABIN MAIN DECK CARGO COMPARTMENT RT BS 1256, LONGERON 26R FWD R3 DOOR LOWER JAMB FOUND WEB CRACKED. REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED MAJOR IAW SMM 6-2-100.SDR FDEA201506252029Seat Track · corrodedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK BS 1159, X = 8.5 FOUND SURFACE CORRODED. REPAIRED IAW SRM 53-00-52-2R, REPAIR 1 FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506252027Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT LOWER HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318563 PART 1 STEP 1B.SDR FDEA201506252026Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT UPPER HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318563 PART 1.SDR FDEA201506252025Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT HOLE SURFACE CORROSION. WORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252024Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE SURFACE CORRODED. FOUND WITHIN LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW CMM 57-44-09. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252023Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD HOLE SURFACE CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0318563 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252022Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. SHOULDER BUSHING, FABRICATED IAW EA 1-5750-T0318563 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201505191543Smoke Warning · false activationLEVEL 3 CABIN SMOKE ALERT UPON LANDING, NO SMOKE PRESENT. PERFORMED OPERATIONAL TEST OF THE CARGO SMOKE DETECTOR IAW AMM 26-14-01-5, TEST PASSED. NO FAULT FOUND IN MSC CURRENT FAULT & FAULT REVIEW, NO HISTORY WITHIN 99 DAYS. ITEM CLOSED, ACFT OK FOR SERVICSDR FDEA201503271108Warning Message · illuminatedGENERATOR LOAD HIGH LEVEL 2 ALERT. RAN CHECKLIST, WHILE WORKING CHECKLIST, WENT AWAY. BATTERY DISCHARGE, WENT AWAY. ACFT TIE FAULT. ADG ELEC SWON. DUMPED FUEL TO LAND WT. ALL THIS OCCURRED AFTER APU STARTED & CREW SHUTDOWN.SDR FDEA201502280613Battery Pack · dischargedEMERGENCY LIGHTS FAILED TEST. R & R BATTERY PACK IAW MM 33-51-01-4-0. OPERATIONS TESTED GOOD.SDR FDEA201408252309Hydraulic Line · failedUPON TOUCHDOWN WITH FLAPS 35 & MEDIUM BRAKES SELECTED, EXPERIENCED COMPLETE LOSS OF NR 2 HYD SYS FLUID RESERVOIR WAS ZERO & PUMPS OFF. ALL THESE HAPPENED BETWEEN TOUCHDOWN & TAXI SPEED. NR 2 LT FAN COWL OPENED, FOUND PRESS LINE GOING INTO THE HYD CONTROL UNISDR FDEA201405201093Skin · crackedDURING COMPLIANCE OF FCD 1-5710-F0308148, FOUND SKIN CRACKED NEAR ZONE 519, LT WING INBD OF NR 1 ENGINE, JUST AFT OF INBD SLATS. PERFORMED HFEC OF THE SUSPECTED CRACK IN THE LT WING. CRACK APPROXIMATELY INCHES INCHES. INSTALLED FILLER AND DOUBLER IAW EA 1SDR FDEA201405191072Skin · crackedFOUND POSSIBLE SMALL CRACK RT WING ROOT LE. COMPLIED WITH HFEC IAW SPM 06-10-01001. CRACK NOTED .750 INCH LONG. REMOVED CRACK AT OTBD CORNER OF FIRE BOTTLE ACCESS DOOR LOWER SKIN. MADE CUT OUT IAW SRM 57-10-00 FIG 68. PERFORMED HFEC INSPECTION IAW NTMSDR FDEA201307291691Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, FOUND ONE CRACK INDICATION ON NR 7 MAIN DECK CARGO DOOR LOWER FRAME FITTING AT HOLE "A". SUPPORT FITTING R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291685Doubler · crackedRT WING FIXED L/E COMPARTMENT AT XOS 794 BEADED DOUBLER FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 57-40-02, FIG 203, REPAIR 15, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291684Longeron Splice · crackedMAIN DECK LONGERON 11R SPLICE AT BS 1651 FOUND CRACKED. R & R SRM 51-31-01, REV 53. SPLICE FABRICATED IAW DWG AFA7181, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291683Longeron Splice · crackedMAIN DECK LONGERON 12L SPLICE AT BS 1631 FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. FABRICATED IAW DWG AFA7181 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291682Stop Fitting · crackedMAIN DECK L3 PLUG DOOR, ONE DOOR STOP FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291681Skin · crackedLEFT HAND WING FIXED L/E XOS 715, SLAT TRACK 11 CUTOUT CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291680Skin · crackedLEFT WING FIXED L/E XOS 660, SLAT TRACK NR 10 CUTOUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291679Trunnion · crackedNOSE LANDING GEAR WHEEL WELL RT TRUNNION FITTING LOWER AREA FOUND CRACKED. AREA TRIMMED OUT AND REPAIRED IAW SRM 53-10-14, FIG 202. REPAIR 2, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. INITIAL INSP AT 1500 CYCLES AND REPETITIVE INSP REQUIRSDR FDEA201307291678Trunnion · crackedNOSE LANDING GEAR WHEEL WELL LEFT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED IAW EA 1-5340-T0301502A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201111184977Unknown · unknownF/O YOKE IS APPROXIMATELY 5 LT (DOWN) WHEN IT SHOULD BE FULLY NEUTRAL (LEVEL). NO DIFFERENCE WHEN EITHER AUTOPILOT SELECTED. ACFT IS TRIMMED. PERFORMED OPS TEST OF AILERONS IAW AMM 27-10-00-5-0. FOUND ALL NORMAL. PERFORMED FCC 1 AND FCC 2 CONTROL WHEEL SSDR FDEA201108223398Skin · damagedFORWARD CARGO DOOR CUTOUT FOUND WITH SCRATCHES AT L39-41R. REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIG.202 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108223397Skin · damagedFORWARD DOOR CUTOUT AFT FUSLAGE SKIN FOUND WITH SCRATCHES AT L-38-39R. REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIG.202 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV112.SDR FDEA201108203389Skin · damagedAFT CARGO DOOR CUTOUT AFT JAMB FOUND WITH SCRATCHES AT L43-44L. CUTOUT AFT JAMB AREA, REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIG.202 REV47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV112.SDR FDEA201108123244Skin · misrepairedRT WING INBD FLAP LOWER SKIN AT STA XIFH 245 MISREPAIRED. REPAIR REMOVED AND NEW REPAIR CARRIED OUT AT RTWING I/B FLAP LWR SKIN AS PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. EA 1-5750-143656. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100 REV 112.SDR FDEA201108123243Beam · crackedCABIN L3 DOOR NR 1 BEAM AFT STOP SUPPORT FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 REV 47. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV112.SDR FDEA201108123246Skin · corrodedCABIN RT STA 1229 XCW=-90 - XCW=-100 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS 0.166", REMAINING THICKNESS 0.096", MATERIAL REMOVED 0.070" AND FOUND ACCEPTABLE AS PER EA 1-5710-143645. REPAISDR FDEA201108123245Skin · corrodedCABIN RT STA 1214 XCW=-100 - XCW=-103 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS 0.162", REMAINING THICKNESS 0.136", MATERIAL REMOVED 0.026" AND FOUND ACCEPTABLE AS PER EA 1-5710-143645. REPSDR FDEA201108113212Skin · unknownREPAIR AT FUSELAGE SKIN STA 990 BETWEEN LONGERON 40 TO 42RT. REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIGURE 202 REV 47. EO 1-5100-7-5001 A5 PT1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108113211Skin · unknownREPAIR AT FUSELAGE SKIN STA 1960 BETWEEN LONGERON 40 TO 42L. REMOVED AND REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIGURE 202 REV 47. EO 1-5100-7-5001 A5 PT1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108113218Skin · misrepairedLT WING INBD FLAP LOWER SURFACE XIFH198 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201108113217Skin · misrepairedLT WING INBD FLAP LOWER SURFACE XIFH245 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.
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