N625FE

Service difficulty reports · 266

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 = 'N625FE' 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 FDEA201211013795Cargo Track · crackedMAIN DECK CARGO TRACK FLANGE AREA CRACKED AT STATION 635, X= 27.5 (LBL 27.5). REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 1, 2012 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111144918Seat Track · corrodedSEAT TRACK CORRODED FROM FR45 TO FR47. REMOVED CORROSION IAW SRM 51-74-10, PARA (S). WITHIN LIMITS IAW SRM 53-10-16, PAGE 105, REPROTECTED AREA IAW SRM 51-21-10, PAGE 8 AND 51-75-10, PAGE 203.Nov 14, 2011 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108043090Structure · crackedLT WING OTBD FLAP - DURING HFEC OPEN HOLE INSP ON OTBD LOWER FASTENER HOLE COMMON TO ARC4008 AND ARC4009 SUPPORT IAW EO 1-5750-7-5008 PART 1 FOUND 1 EA FASTENER WITH CRACK. THE HOLE WAS OVERSIZED AND HAS MORE THAN 2D EDGE DISTANCE. THE HOLE WAS BUSHED BACK FAug 4, 2011 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201107272990Inlet · dentedENGINE NR 2 - INLET COWL LIP FOUND WITH FOUR DENTS. DENTS MEASURED AND FOUND EXCEEDED LIMITS PER SRM 54-42-02 REV 46, TABLE 102. DENT DIMENSION: DEPTH = 0.065 INCH; DIAMETER = 0.380 INCH DEPTH OF DENT IS MORE THAN 10% OF THE DENT DIAMETER AND THE DISTANJul 27, 2011 · N625FE · Doug MD11F · Engine Air Intake SystemSDR FDEA201107112641Seat Track · corrodedCABIN SEAT TRACK BETWEEN STA 1256 AND 1305 SILL PLATE ATTACHMENT HOLES FOUND CORRODED. TRIMMED OUT AND REPAIRED CARRIED OUT IAW SRM 53-00-52, REV 46, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 11, 2011 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107012527Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD HINGE (FLAP SIDE), PIVOT OTBD HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMITS CMM 57-52-03, REV 70. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-150749, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 112.Jul 1, 2011 · N625FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201010204118Door Frame · misrepairedEXISTING REPAIR - AFT CARGO DOOR AFT JAMB AT STA 1964, LONGERON 39 TO 42 LT. EXISTING REPAIR AT AFT CARGO DOOR AFT JAMB AT STA 1964, LONGERON 39 TO 42 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53-00-15, FIG 203, REPAIR 8 REV 44. HOWEVER, REPAIOct 20, 2010 · N625FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201010134061Skin · crackedCRACKED RT AFT FUSELAGE SKIN STA 2140, LONGERON 36. REPAIRED IAW SRM 53-70-01, FIG 201, REPAIR 2, REV 44. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 111.Oct 13, 2010 · N625FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201010134060Skin · corrodedCORROSION - RT AFT FUSELAGE SKIN STA 2140 AT ENCLOSED AREA OF FIXED FAIRING NR 347DF. REMOVED IAW SRM 51-21-01, REV 44 AND FOUND EXCEEDED LIMIT IAW SRM 53-70-01, FIG 201, SHEET 3, REV 44. REPAIR CARRIED OUT IAW SRM 53-70-01, FIG 201 REPAIR 3, REV 44. REPAOct 13, 2010 · N625FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201010113995Doubler · crackedCRACKED BEADED DOUBLER AT XOS646 IN RT WING FIXED L/E. REPAIRED IAW SRM 57-40-00, FIG 203, REPAIR 9, REV 44. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Oct 11, 2010 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201010113994Doubler · crackedCRACK - BEADED DOUBLER AT XOS701 IN RT WING FIXED L/E. REPAIR CARRIED OUT IAW SRM 57-40-02, FIG 203, REPAIR 9 REVISION 44. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Oct 11, 2010 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201010113993Doubler · crackedCRACKED BEADED DOUBLER INBD OF SLAT TRACK NR11 AT LT WING FIXED L/E COMPARTMENT. CRACKED BEADED DOUBLER INBD OF SLAT TRACK NR11 AT LT WING FIXED L/E COMPARTMENT REPAIRED IAW SRM 57-40-02 FIG 203, REPAIR 9 REV 44. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, Oct 11, 2010 · N625FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201010073967Skin · misrepairedEXISTING REPAIR - RT WING NR2 SLAT INNER SKIN AT XIS 247. EXISTING REPAIR AT RT WING NR 2 SLAT INNER SKIN AT XIS 247 EVALUATED AND FOUND NOT IAW ANY APPROVED DATA. NEW REPAIR CARRIED OUT IAW SRM 57-40-01, FIGURE 201, REPAIR 1, REV 44. REPAIR CLASSIFIED MAJOROct 7, 2010 · N625FE · Doug MD11F · Leading Edge DevicesSDR FDEA201010073968Skin · crackedCRACK - LT WING NR3 SLAT TELESCOPIC DUCT UPPER DOOR CUTOUT INBD AREA. CUTOUT INBD AREA. REPAIRED IAW SRM 57-40-01, FIG 201, REPAIR 10, REV 44 AND NR1-5710-143456, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 111.Oct 7, 2010 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201010053931Skin · crackedRT WING NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT INBOARD AND OUTBOARD CORNER SKIN CRACKED. CUTOUT INBD AND OTBD CORNER SKIN REPAIRED IAW SRM 57-40-01, FIG 201, REPAIR 10, REV 44 AND EA NR1-5710-143457, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 111.Oct 5, 2010 · N625FE · Doug MD11F · Wing, Plate/SkinSDR 05FDEA00205Skin · corrodedDURING AIRPLANE PASSENGER TO FRIGHT CONVERSION: FOUND MANY SEVERE CORROSION ON UPPER SKIN OF THE CTR BOX WING LT SIDE STA 1199;1219 AND 1229 X= 100 RH SIDE STA 1199;1219 AND 1229 X=-100. REMOVE FASTENERS IN THE AFFECTED AREA, REMOVED CORROSION PER SRM 57-20-Jan 31, 2005 · N625FE · Doug MD11 · Wing, Plate/Skin
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