N604FE

Service difficulty reports · 447

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 = 'N604FE' 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 05FDEA01710Hinge Fitting · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD STRUT HOLE FOUND CORRODED STRUT. COMPLIED WITH FEDEX EA 1-5750-87545. (CLOSED)Jun 28, 2005 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01672Frame · crackedNR 3 ENGINE, LT THRUST REVERSER COWL, FORWARD FRAME UPPER RADIUS SUSPECTED CRACKED. THRUST REVERSER COWL REMOVED AND REPLACED.Jun 23, 2005 · N604FE · Doug MD11 · Engine Thrust ReverserSDR 05FDEA01671Skin · bulgedRT WING TRAILING EDGE UPPER SURFACE AT XORS 826.50, OUTBOARD OF NR 5 SPOILER, FOUND BULGING. CORROSION REMOVED PER SRM 51-21-01 VOLUME II.Jun 23, 2005 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 05FDEA01668Track · crackedNR 2 ENGINE, RT THRUST REVERSER COWL, UPPER SLIDER TRACK END SUSPECTED CRACKED. THRUST REVERSER COWL REMOVED AND REPLACED.Jun 23, 2005 · N604FE · Doug MD11 · Engine Thrust ReverserSDR 05FDEA01669Support Fitting · crackedRT WING, WHILE ACCOMPLISHING EA NR 1-5750-87541, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5.Jun 23, 2005 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01670Splice · crackedMAIN DECK, LT LONGERON L-11 SPLICE BETWEEN STA 1641 TO STA 1661, FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01- VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 23, 2005 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01653Stringer · crackedLEFT WING, FUEL TANK UPPER STRINGER END S-10 BETWEEN XORS 799 TO XORS 827. FOUND WITH APPROXIMATELY 10 INCH CRACKED. TRIMMED OUT PER SRM 57-20-00 VOLUME I, FIGURE 10. FABRICATED REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II.Jun 22, 2005 · N604FE · Doug MD11 · Wing, Longeron/StringerSDR 05FDEA01644Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 1199, X= 47 FOUND WORN AEA7579-1. REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 22, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01643Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 1491, X= 47 FOUND WORN. REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1.Jun 22, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01642Seat Track · corrodedMAIN DECK, SEAT TRACK CROWN AT STA 625, X= 47 FOUND WORN ACA7399-501. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 22, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01641Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 635 , X= 8 FOUND WORN. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 22, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01639Sleeve · crackedNR 1 ENGINE, LT THRUST REVERSER TRANSLATING SLEEVE, UPPER SLIDER TRACK END SUSPECTED CRACKED. LT THRUST REVERSER COWL REMOVED AND REPLACED.Jun 21, 2005 · N604FE · Doug MD11 · Engine Thrust ReverserSDR 05FDEA01638Seat Track · wornMAIN DECK, SEAT TRACK CROWN FROM STA 1059 TO STA 1119 , X= -47 FOUND WORN. SEAT TRACK CUT AND REMOVED PER SRM 51-33-01 VOLUME II. REPAIR PARTS INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.Jun 21, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01637Seat Track · corrodedMAIN DECK, SEAT TRACK BASE AT STA 6 - 10, X= -8 FOUND WITH CORROSION. REMOVED AND TREATED AS PER SRM 51-21-01 VOLUME II.Jun 21, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01636Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 799, X= -47 FOUND WORN.Jun 21, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01635Seat Track · wornMAIN DECK, SEAT TRACK CROWN FROM STA 899 TO STA 923, X= 47 FOUND WORN.Jun 21, 2005 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03202Liner · damagedPOST FLIGHT WALK AROUND FOUND SEVERAL AFT LINER SEGMENTS WITH UPPER SKIN GONE AND HONEYCOMB MATERIAL DAMAGED. ALMOST EVERY SEGMENT DAMAGED ON NR 1 ENGINE. NR 3 ENGINE FOUND AFT LINER SEGMENT OUTER SKIN DELAMINATED AND HONEYCOMB MATERIAL DAMAGED ALMOST COMPNov 24, 2004 · N604FE · Doug MD11 · Nacelle/Pylon, Main FrameSDR 04FDEA00368Frame · misrepairedCABIN - PREVIOUS FRAME REPAIR AT RIGHT STA 1541 STR 12 - 13 WAS FOUND SECURED WITH RIVETS, INSTEAD OF HI-LOKS. CABIN - PREVIOUS FRAME REPAIR AT RT STA 1541 STR 12 - 13 DOUBLER REMOVED AND REPLACED IAW SRM 53-30-00 FIG 1 VOL I WITH REF TO EA 1-5310-74305, FUSEFeb 6, 2004 · N604FE · Doug MD11 · Fuselage Main, FrameSDR 04FDEA00308Hinge · misalignedRIGHT HORIZONTAL STABILZER SLOT DOOR 344AB FASTENER HOLES FOUND MISALIGNED. RT HORIZONTAL STAB SLOT DOOR 344AB FASTENER HOLES MISALIGN AREA CARRIED OUT REPAIR IAW EA 1-5510-74301, STABILIZERS - HORIZONTAL STABILIZER - RT NR 1 SLOT DOOR ASSEMBLY REPAIR.Feb 1, 2004 · N604FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA00288Structure · corrodedTAIL TANK, TO ACCOMPLISH E1-5510-7-5000 PT 1. LT NR 36 BARREL NUT HOLE CORROSION REMOVAL, WEB CUTTING REQUIRE FOR ACCESS. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF LT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REPAIR CARRIED OUT AS PFeb 1, 2004 · N604FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA00287Structure · corrodedMAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA HAS CORROSION IN TWO PLACES. MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA, CORRODED AREA CARRIED OUT REPAIR IAW SRM 53-70-00, FIG. 5, VOL.I.Feb 1, 2004 · N604FE · Doug MD11 · Fuselage Main, StructureSDR 04FDEA00223Fitting · wornLT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN, OUT OF LIMIT. LT INBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA# 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR.Jan 26, 2004 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00222Fitting · wornLT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. LT INBD FLAP VANE NR 1 TEE FITTING REPAIRED AS PER EA 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR.Jan 26, 2004 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00221Fitting · wornSNRM N1201 : RT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RT INBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA 1-5750-74292, WINGS -LT AND RT INBD FLAP VANE -NR 1 & 3 TEE FITTING WEAR REPAIR.Jan 26, 2004 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00220Fitting · wornRT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RH INBD FLAP VANE NR 1 TEE FITTING REPAIRED AS PER EA# 1-5750-74292, WINGS- LEFT AND RIGHT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR.Jan 26, 2004 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00243Seat Track · damagedMAIN CARGO DECK RT STA 795 SEAT TRACK REF. X = 27.5 SEAT TRACK DAMAGED IN TWO PLACES. MAIN CARGO DECK RT STA 795 SEAT TRACK REF = X =27.5 DAMAGED SEAT TRACK CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1.Jan 26, 2004 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA00219Strap · corrodedLT IB FLAP OB HINGE (FLAP SIDE), OB PIVOT HOLE FOUND CORRODED AT STRAP FACE. LT INBD FLAP OUTBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE ATTACH O/B STRAP REMOVED AND REPALCED AS PER SRM 51-33-01 VOL II & AMM 20-50-02. FABRICATED NEW STRAP AS PER DWG ARC2518.Jan 25, 2004 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00217Floorbeam · corrodedMAIN CARGO DECK RT FLOORBEAM 53.5 INCHES FROM CENTER LINE HAS EVIDENCE OF CORROSION. RT DAMAGED FLOOR SUPPORT STA 1891TO STA 2007, 53.5 INCHES FROM CENTER LINE REMOVED AS PER PER MM 20-50-02. FABRICATED AS PER DWG NR AGA7551. FABRICATED SUPPORT INSTALLED AJan 25, 2004 · N604FE · Doug MD11 · Fuselage Main, Floor BeamSDR 04FDEA00200Rib · chafedFOUND DEEP CHAFING MARK ON LEFT INBOARD FLAP OUTBOARD VANE TRACK OUTBOARD SUPPORT RIB AT LEADING EDGE AREA. DEEP CHAFING REWORKED AS PER SRM 51-21-01, VOL.II AND EA 1-5750- 74284. WINGS - LEFT INBOARD FLAP VANE SUPPORT - RIB CHAFED ) AT LT INBD FLAP, OUTBD Jan 21, 2004 · N604FE · Doug MD11 · Wing, Rib/BulkheadSDR 04FDEA00201Track · gougedLEFT INBOARD FLAP CENTER VANE TRACK CUTOUT FOUND GOUGES AT 4 PLACES. COMPLIED WITH FEDEX EA 1-5750-74283, WINGS - LEFT INBOARD FLAP VANE SUPPORT RIB CHAFED.Jan 21, 2004 · N604FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00199Skin · corrodedRIGHT WING - UPPER SURFACE, FASTENER (1 EA) POPPED UP AT XORS 230, STA 1413.Jan 21, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00179Floorbeam · corrodedMAIN CARGO DECK RT STA 1912 FLOORBEAM CORRODED BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5. CORRODED FLOORBEAM SUPPORT BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5 AT MAIN CARGO DECK RT STA 1912 REMOVED AND REPLACEJan 16, 2004 · N604FE · Doug MD11 · Fuselage Main, Floor BeamSDR 04FDEA00178Floor Support · corrodedMAIN CARGO DECK RIGHT STA 1896 TO STA 2007 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. RT STA 1896 TO STA 2007 FLOOR SUPPORT (01 EACH) REMOVED AND REPLACED IAW SRM 51-31-01 VOL IIJan 16, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA00177Seat Track · corrodedMAIN CARGO DECK LT STA 1341 TO STA 1361 SEAT TRACK REF X =75.25 SEAT TRACK HAS SURFACE CORROSION. MAIN CARGO DECK RH STA 1341TO STA 1365 SEAT TRACK REF. X =75.25 SEAT TRACK FLANGE CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 5 V1.Jan 16, 2004 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA00176Structure · corrodedTAIL TANK - RIGHT NR 36 BARREL NUT HOLE, BEARING SURFACE AND BOTTOM SURFACE FOUND CORRODED. REQUIRE CUTTING OF WEB FOR REAMING. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF RT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REPAIR CARRIED OUT ASJan 16, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA00175Channel · corrodedLEFT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. CORROSION BETWEEN STA 1541 TO STA 5-113 GUIDE RAIL UPPER FLANGE, CORROSION REMOVED. ORIGINAL THICKNESS 0.090. MATERIAL REMAINING 0.082. WITHIN LIMIT PER SRM 53-00-01, FIGJan 16, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA00174Skin · corrodedCENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION FROM STA 1235 LT X =13 TO RT X =5. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK STA 1235 LH X = 13 TO RT X = 5. CORRODED AREA CARRIED OUT REPAIR IAW EA 1-5710-74294, WINGS - CENTERJan 16, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00173Structure · corrodedCENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235 RT X =30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RT X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKJan 16, 2004 · N604FE · Doug MD11 · Wing, Center BoxSDR 04FDEA00172Skin · crackedRIGHT WING LEADING EDGE PANEL INTERIOR SEVERAL CRACKS AT XOS 546 OUTBD OF REFUELING PANEL. RT WING LEADING EDGE XOS 546 INNER DOUBLER. REPAIRED AS PER SRM 57-10-00 FIG 25 V1.Jan 16, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00171Skin · crackedLEFT WING LEADING EDGE 2 CRACKS AT RIVETS STA XOS 630 LEADING EDGE PANEL INTERIOR. LT WING LEADING EDGE : STA XOS 630 LEADING EDGE PANEL INTERIOR, 02 EACH CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.Jan 16, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00170Skin · crackedLEFT WING LEADING EDGE PANEL INTERIOR MANY CRACKS FROM EOS 560 TO 620 BETWEEN SLAT TRACKS 10 AND 11. LT WING LEADING EDGE SKIN PANEL INTERIOR STA XOS 560 TO XOS 620 BETWEEN SLAT TRACK 10 AND 11, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.Jan 16, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00169Skin · crackedLEFT WING - LEADING EDGE PANEL INTERIOR HAS SEVERAL CRACKS AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK. LT WING LEADING EDGE PANEL INTERIOR AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25Jan 16, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00168Skin · crackedLEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS STA XOS 510 UNDER REFUEL ACCESS PANEL. LT WING : LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.Jan 16, 2004 · N604FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA00163Seat Track · corrodedMAIN CARGO DECK RIGHT STA 1250 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 SEAT TRACK REF - X = 75.25 SEAT TRACK CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01, VOL.II. MATERIAL THICKNESS : 0.080 , THICKJan 15, 2004 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA00164Seat Track · corrodedMAIN CARGO DECK RIGHT STA 1250 TO 1361 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 TO 1361 SEAT TRACK REF. X = 75.25. CORROSION ON SEAT TRACK REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL. II. MATERIAL THJan 15, 2004 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA00165Channel · corrodedRT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. GUIDE RAIL UPPER FLANGE BETWEEN STA 1541 TO STA 5-113 CORROSION REMOVED. ORIGINAL THK 0.090 MATERIAL REMAINING 0.078 MIN. WITHIN LIMITS PER SRM 53-00-01 FIG 3 VOL 1Jan 15, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA00162Seat Track · corrodedMAIN CARGO DECK RIGHT STA 1922 TO STA 2007 SEAT TRACK REF X = 20.0, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1922 TO STA 2007 SEAT TRACK REF. X = 20.0, FLOOR SUPPORT 01 EA REMOVED AND REPLACED AS PER MM 20-50-02 (AGA7088-2). SUPPORT AGA708Jan 15, 2004 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA00161Floor Support · corrodedFLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5. FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5 P/NO AGA7559-3N REMOVED AND REPLACED IAW MM 20-50-02. AGA7080 SUPPORT FABRICATEF AS PER DWG AGA7080 AND INSTALLED AS PER MM 20-Jan 15, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA00160Stiffener · crackedMAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 27.5 AND X = 47.5 STIFFENER CRACKED. MAIN CARGO DECK RT STA 1169 BETWEEN SEAT TRACK REF. X = 27.5 AND X = 47.5 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01, VOL.II. STIFFENER FABRICATED IAW DRAWING NRJan 15, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA00159Stiffener · crackedMAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 STIFFENER CRACKED. MAIN CARGO DECK RT 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED STIFFENER AS PER DWG NR NPBJan 15, 2004 · N604FE · Doug MD11 · Fuselage Miscellaneous Structure
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