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.

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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Wing, Plate/SkinSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Fuselage Main, FrameSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Fuselage Main, FrameSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Fuselage Main, FrameSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 26, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Jun 25, 2015 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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 SERVICMay 19, 2015 · N628FE · Doug MD11F · Smoke DetectionSDR 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.Mar 27, 2015 · N628FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201502280613Battery Pack · dischargedEMERGENCY LIGHTS FAILED TEST. R & R BATTERY PACK IAW MM 33-51-01-4-0. OPERATIONS TESTED GOOD.Feb 28, 2015 · N628FE · Doug MD11F · Emergency LightingSDR 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 UNIAug 25, 2014 · N628FE · Doug MD11F · Hydraulic System, MainSDR 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 1May 20, 2014 · N628FE · Doug MD11F · Wing, Plate/SkinSDR 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 NTMMay 19, 2014 · N628FE · Doug MD11F · Wing, Plate/SkinSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Fuselage Main, StructureSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Wing, Plate/SkinSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Passenger/Crew DoorsSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Wing, Plate/SkinSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Wing, Plate/SkinSDR 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 REQUIRJul 29, 2013 · N628FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 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.Jul 29, 2013 · N628FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 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 SNov 18, 2011 · N628FE · Doug MD11F · Control Column SectionSDR 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.Aug 22, 2011 · N628FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 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.Aug 22, 2011 · N628FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 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.Aug 20, 2011 · N628FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 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.Aug 12, 2011 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Aug 12, 2011 · N628FE · Doug MD11F · Passenger/Crew DoorsSDR 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. REPAIAug 12, 2011 · N628FE · Doug MD11F · Fuselage Main, KeelSDR 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. REPAug 12, 2011 · N628FE · Doug MD11F · Fuselage Main, KeelSDR 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.Aug 11, 2011 · N628FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 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.Aug 11, 2011 · N628FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 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.Aug 11, 2011 · N628FE · Doug MD11F · Trailing Edge FlapsSDR 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.Aug 11, 2011 · N628FE · Doug MD11F · Trailing Edge Flaps
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