N576FE

Service difficulty reports · 353

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 = 'N576FE' 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 05FDEA01228Intercostal · crackedMAIN DECK, STA 513 LONGERON 27L INTERCOSTAL BOTTOM SIDE FOUND CRACKED ABOUT 0.5 INCH. DISCREPANT INTERCOSTAL REMOVED AS PER SRM 51-31-01 VOL II. NEW INTERCOSTAL LOCATED AND INSTALLED AS PER SRM 51-31-01 VOL II.May 9, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01216Fairing · corrodedLEFT NR 1 AIR COND BAY BILGE AREA, FAIRING ASSY FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II ,MATERIAL ORIGINAL THICKNESS:0.04 REMOVED MATERIAL THICKNESS: 0.006, L:24, W:6, REMAIN THICKNESS: 0.034 AND FOUND WITHIN LIMIT AS PERMay 6, 2005 · N576FE · Doug MD11 · Aerodynamic FairingsSDR 05FDEA01215Fitting · crackedRIGHT WING O/B FLAP SECOND FLAP VANE TRACK FROM I/B UP-STOP FITTING FOUND CRACKED. CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01VOL II. CLASSIFIED AS MAJOR REPAIR PER GMM 6-1-100.May 6, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01213Tube · not closedAFT CARGO - REFERENCE EA 1-2520-7-78127 ITEM 39, AFTER REMOVAL OF WASTE TANK AND PLUMBING FOUND VACUUM PUMPS OUTLETS AND TANK DUMP TUBE OUTLET NOT BLANKED. REMOVED AND DISCARD AS PER AMM 20-50-02 AND SMR 51-33-01 VOL II, NEW PANEL AND COVER PLATE FABRICATEMay 5, 2005 · N576FE · Doug MD11 · Waste Disposal SystemSDR 05FDEA01190Floorbeam · corrodedCABIN FLOORBEAM FOUND CORRODED AT STA 1873 LBL 10 TO 26 AS MARKED. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT AT STA 1873 LBL 33 TO RBL 33 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S292Apr 30, 2005 · N576FE · Doug MD11 · Fuselage Main, Floor BeamSDR 05FDEA01188Spar · corrodedLT WING REAR SPAR TOPSIDE WING CORROSION FOUND AT XORS 725. SKIN TRIMMED, REPAIR DOUBLER AND FILER FABRICATED AND INSTALLED AS PER EA 1-5720-80383.Apr 30, 2005 · N576FE · Doug MD11 · Wing SparSDR 05FDEA01178Attach Fitting · crackedEMPENNAGE - LT FAIRING PANEL ATTACHMENT IN BETWEEN VERTICAL STABILIZER LOWER UPPER SECTION AND LOWER CENTER SECTION AT APPROX PIN 122 ADJACENT TO ACCESS PANEL 363PL FOUND CRACKED AT AFT EDGE AREA. REPAIR AS PER EA 1-5530-80384 AND SRM 51-33-01 AND 51-35-01 VApr 29, 2005 · N576FE · Doug MD11 · Vertical Stabilizer, Attach FittingsSDR 05FDEA01177Seat Track · corrodedMAIN DECK IN BETWEEN STA 420 & 495 RBL 95.5 SEAT TRACK FOUND CORRODED. SEAT TRACK REMOVED AND NEW SEAT TRACK P/N ABA 7681-503 INSTALLED AS PER SRM 51-31-01 VOL II.Apr 29, 2005 · N576FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01172Rib · damagedRT WING I/B FLAP ASSY FOUND NEW FLAP SEGMENT ASSY RIB DAMAGED. DAMAGED AREA TRIMMED. REPAIR DOUBLER & FILLER FABRICATED AND INSTALLED AS PER SRM 57-00-01 FIG. 7 VOL I AND 51-35- 01 VOL II. MINOR REPAIR PER GMM 6-2-100.Apr 28, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01156Seat Track · damagedCABIN, CURVE SEAT TRACK AT STA 1951 TO 1971 LBL 77 FOUND PREVIOUS REPAIRED AREA NON-STANDARD AS MARKED. SEAT TRACK TRIM OUT AS PER SRM 53-70-00 FIG 1 VOL I . NEW SEAT TRACK REMOVED AS PER SRM 53-70-00 FIG 7 VOL I. SPLICE ANGLE REWORKED AND SPLICE PLATE FAApr 27, 2005 · N576FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01151Floor Support · corrodedAFT CARGO CEILING AREA HAS CORROSION ON CABIN FLOOR SUPPORTS AT STA 1887 X=58. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT AT STA 1887 TO 2007 X=58 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FRApr 27, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01150Floor Support · corrodedCABIN, FLOOR SUPPORT FOUND VARIOUS PLACES CORROSION AT STA 1959 TO 2007 AND RBL 56 TO 59 AS MARKED. REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT AT STA 1887 TO 2007 RBL 56 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLApr 27, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01149Floorbeam · corrodedCABIN FLOOR SUPPORT AT STA 1913 RBL 42 FOUND PREVIOUS REPAIRED NON- STANDARD AS MARKED. FLOOR SUPPORT REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2929348 AS PER DRAWING AGA 7501 AND REPROTECTED AS PER SRM 51-21-01 VOL II. NEW FLOOR Apr 27, 2005 · N576FE · Doug MD11 · Fuselage Main, Floor BeamSDR 05FDEA01148Floorbeam · corrodedCABIN, FLOOR SUPPORT FOUND CORROSION AT STA 1911 RBL 70 AND 75 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT FABRICATED FROM S2929348 AS PER DRAWING AGA 7501 AND REPROTECTED AS PER SRM 51-21-01 VOL II. NEW FLOOR SUPPORT LOCATED AND INSTALLApr 27, 2005 · N576FE · Doug MD11 · Fuselage Main, Floor BeamSDR 05FDEA01147Floor Support · corrodedCABIN, LONGITUDINAL FLOOR SUPPORT FOUND CORROSION AT STA 1888 TO 1913.5 RBL 22 AS MARKED. CORROSION ON FLOOR SUPPORT AT STA 1888 TO 1913.5 RBL 22 REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT FROM STA 1887 TO 2007 Apr 27, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01146Floor Support · corrodedCABIN, FLOOR SUPPORT FOUND CORROSION AT VARIOUS PLACES FROM STA 1911 TO 2007 RBL19 AS MARKED. CORROSION ON FLOOR SUPPORT AT STA 1911 TO 2007 RBL 19 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT REMOVED AT STA 1887 TO Apr 27, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01145Floor Support · corrodedCABIN, FLOOR SUPPORT AT STA 1911 LBL 22 TO 28 FOUND VARIOUS PLACES OF CORROSION AS MARKED. CORROSION ON FLOOR SUPPORT AT STA 1911 RBL 22 TO LBL 28. REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT FROM STA 1887 TO 2007 RApr 27, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01061Attach Fitting · crackedMAIN DECK, AT STATION 510 LONGERON 27L FRAME TO FLOORBEAM INTERSECTION FOUND WITH 1 INCH CRACK. CARRIED OUT REPAIR AS PER EA 1-5310-80388.Apr 22, 2005 · N576FE · Doug MD11 · Fuselage Main, Attach FittingsSDR 05FDEA01057Seat Track · corrodedMAIN DECK, UPON REMOVAL OF FLOOR PANEL 291GF FOR SHEETMETAL ACCESS AT STA 1887 LBL 60 INCH SEAT TRACK FOUND CORRODED. CORROSION ON SEAT TRACK REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. SEAT TRACK REWORKED AS PER SRM 53-70-00 FIG.1 VOL I.Apr 21, 2005 · N576FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01042Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 34 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 18, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01038Floor Support · corrodedMAIN DECK, UPON REMOVAL OF FLOOR SUPPORT STRUCTURE, FLOOR SUPPORT STRUCTURE TO TEE CHORD AT STA 2007 RBL 60 INCH FOUND WITH CORROSION. CORROSION ON TEE CHORD AT STA 2007 RBL 60 REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-40-00 FIG. 7 VOL I. DISCREPANT TEE CHApr 17, 2005 · N576FE · Doug MD11 · Fuselage Main, Attach FittingsSDR 05FDEA01037Door Frame · corrodedSNRM N1749: CABIN, 3R ABOVE UPPER DOOR JAMB STA 1278 FOUND LONGERON L-14 CORROSION AS MARKED.Apr 17, 2005 · N576FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01036Door Frame · corrodedCAIN, DOOR 3R ABOVE UPPER DOOR JAMB STA 1263 LONGERON L-12 FOUND CORROSION AS MARKED. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG 1A VOL I. MATERIAL THICKNESS: 0.080, REMAIN THICKNESS: 0.049, REMOVED THICKESS: 0.031 FASTENER ON DISCREPANT AREAApr 17, 2005 · N576FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA01027Vane · damagedRT WING I/B FLAP VANE I/B T-FITTING FOUND OUT OF LIMIT. REMOVED AND REPLACED AS PER CMM 57-52-03.Apr 16, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01026Vane · corrodedRT WING I/B FLAP VANE O/B T-FITTING FOUND CORRODED. RT WING I/B FLAP VANE O/B TEE FITTING REMOVED AND REPLACED AS PER CMM 57-52- 03, REFER WORK CARD E1-5750-7-5005 A2 PT 2.Apr 16, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00997Hinge · corrodedLT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. LT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR CORROSION REMOVED & FOUND I/B & O/B LUG HOLES EXCEED LIMITS AS PER CMM 57-44-09 .I/B & O/B LUG SPOTFACES THK W/I LIMITS AS PApr 13, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00970Spar · corrodedRT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED & FOUND I/B AND O/B LUG HOLES EXCEED LIMITS AS PER CMM 57-44-09.Apr 12, 2005 · N576FE · Doug MD11 · Wing SparSDR 05FDEA00969Spar · corrodedRT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE LWR MOUNT EVIDENT OF CORROSION. CORROSION REMOVED & FOUND I/B AND O/B BOLT HOLES EXCEED LIMITS AS PER CMM 57-44-09.Apr 12, 2005 · N576FE · Doug MD11 · Wing SparSDR 05FDEA00967Spar · corrodedRT WING O/B FLAP I/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE HAS EVIDENCE OF CORROSION. CORROSION REMOVED & FOUND I/B & O/B LUG HOLES EXCEED LIMITS PER CMM 57-44-08.Apr 12, 2005 · N576FE · Doug MD11 · Wing SparSDR 05FDEA00931Panel · corrodedRIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 33 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 33 RT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 33, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 05FDEA00938Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 32 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00937Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 30 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00936Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 28 HAS BORE CORROSION EXCEEDING LIMIT. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00935Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARRREL NUT NR 34 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00934Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 27 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00933Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 29 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00932Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 31 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00930Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 35 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00929Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 24 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00928Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 20 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00927Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 18 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 11, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00925Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 16 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 10, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00924Structure · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT NR 4 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 10, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00922Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 01 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 10, 2005 · N576FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00909Hinge · corrodedLEFT WING O/B FLAP, O/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PERCMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00908Hinge · corrodedLT WING O/B FLAP, O/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00907Hinge · corrodedLT WING O/B FLAP, I/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00906Hinge · corrodedLEFT WING O/B FLAP, I/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. REMOVAL & REPAIR. REFER TO EO E1-5750-7-5002 CI. PT 1.Apr 8, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00905Hinge · corrodedRIGHT WING O/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-00.Apr 8, 2005 · N576FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00904Hinge · corrodedRIGHT WING O/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11 · Trailing Edge Flaps
Back to N576FE