N669FE

Service difficulty reports · 320

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 = 'N669FE' 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 FDEA201109234091Seat Track · corrodedAFT SEAT TRACK 2L CORRODED FROM FR 58 TO FR 69. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, PG 103 FIG 101. REPROTECTED ALL AREAS IAW SRM 51-21-10 AND 51-75-10.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109234090Seat Track · corrodedAFT SEAT TRACK 3L CORRODED BETWEEN FR 69 AND FR 72. AFTER REMOVAL OF LEVEL 1 CORROSION ALL AREAS WERE FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, PG 103, FIG 101. REPROTECTED ALL AREAS IAW SRM 51-21-10 AND 51-75-10.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109234089Seat Track · corrodedSEAT TRACK 2L CORRODED BETWEEN FR 72 TO FR 78. AFTER REMOVAL OF LEVEL 1 CORROSION, ALL AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. REPROTECTED AREAS IAW SRM 51-21-10 AND 51-75-10.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109234080Seat Track · corrodedSEAT TRACK 2R HAS AREAS OF CORROSION BETWEEN FR 46 AND FR 51 REMOVED LEVEL 1 CORROSION AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, PG 103. REPROTECTED AREAS IAW SRM 51-21-10 AND 51-75-10.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109234087Floor Panel · crackedFLOOR PANEL 232TG HAS 2 EA 9" CRACKS. FABRICATED REPLACEMENT FLOOR PANEL 232TG DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109234086Floor Panel · crackedFLOOR PANEL 242BF HAS 2 EA 10" CRACKS. FABRICATED REPLACEMENT FLOOR PANEL 242BF IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109234085Floorboard · damagedFLOORBOARD 152DG HAS EDGE DAMAGE, AROUND 50 PERCENT OF PANEL. FABRICATED REPLACEMENT 152DG IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109234084Floorboard · crackedFLOORBOARD 152 BG CRACKED IN SEVERAL PLACES. FABRICATED REPLACEMENT FLOORBOARD 152BG IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109234083Floorboard · damagedFLOORBOARD 151BG HAS 2 FOOT OF EDGE DAMAGE. FABRICATED REPLACEMENT FLOORBOARD 151BG IAW DWG SRZ25-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.Sep 23, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109224026Seat Track · corrodedCORROSION AT SEAT TRACK 31 FR 41. REMOVED CORROSION (3.7"X.5"X.048") AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 TABLE 102, REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 53-10-16-06 AND SRM 51-40-21.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224024Seat Track · corrodedCORROSION AT SEAT TRACK NR 2 LT FR40. AFTER REMOVAL OF LEVEL 1 CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK AND FABRICATED NEW SEAT TRACK IAW DWG A53832020. REPROTECTED SEAT TRACK IAW SRM 51-20-10 AND 51-75-10. INSTALLED SEAT TRACK IAW SRSep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224067Floor Panel · damagedFLOOR PANEL 131KG HAS 20" OF MISSING SKIN. FABRICATED REPLACEMENT PANEL 131KG IAW DWG SRZ 25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109224064Floor Panel · crackedFLOOR PANEL 242QJ HAS 2EA 10" CRACK FABBED FLOOR PANEL 242QJ IAW DWG NR SRZ 25-005 MAJOR REPAIR IAW GMM6-2-100.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109224059Skin · gougedR1 DOOR HAS A DENT AND A GOUGE AT LOWER EDGE APPROX 14" AFT FROM FWD EDGE. SMOOTHED AND BLENDED GOUGE IAW SRM 51-73-10 BEFORE THICKNESS .098" AFTER BLENDOUT .095" WITHIN LIMITS IAW SRM 52-11-00, TABLE 102, PG. 105. AFTER REWORK FOUND THAT DENT DOES NOT EXSep 22, 2011 · N669FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA201109224058Seat Track · gougedMAIN DECK ZONE 230 AT SEAT TRACK 5L 10" AFT OF FR 20 SEAT TRACK CROWN HAS A GOUGE .5" LONG, SMOOTHED AND BLENDED GOUGE. MATERIAL LOSS .015" MAX LOSS ALLOWED .028" WITHIN LIMITS IAW SRM 53-10-16, REPROTECTED AREA IAW SRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224057Seat Track · corrodedMAIN DECK ZONE 230 FROM FR 21-23 BETWEEN TRACKS 5L AND 6L TIE DOWN FITTING HAS LEVEL 1 CORROSION ON CROWN 3EA AREAS. AFTER REMOVAL OF LEVAL 1 CORROSION AT 3EA LOCATIONS, ALL WERE FOUND TO BE WITHIN LIMITS IAW SRM 53010-16. REPROTECTED ALL AREAS IAW SRM 51-Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224056Seat Track · gougedMAIN DECK ZONE 230 AT SEAT TRACK 5L 7 INCHES AFT OF FR 20 SEAT TRACK CROWN HAS A GOUGE, SMOOTHED AND BLENDED GOUGE IAW SRM 51-73-10 MATERIAL LOSS .015 " MAX ALLOWED .028" WITHIN LIMITS IAW SRM 53-10-16, REPROTECTED IAW SRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224055Seat Track · corrodedNR 2 SEAT TRACK RT 2 EA AREAS CORRODED FROM FR 72 TO FR79. AFTER REMOVAL OF LEVEL 1 CORROSION AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, REPROTECTED AREAS IAW SRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224054Seat Track · corrodedNR 1 SEAT TRACK FROM FR 72 TO FR 79, 4 EA AREAS OF CORROSION. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16 REPROTECTED IAW SRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224053Seat Track · corrodedAFT SEAT TRACK 3L CORRODED AT 1 EA LOCATION BETWEEN FR75 AND FR76 AFTER REMOVAL OF LEVEL 1 CORROSION FOUND TO BE WITHIN LIMITS IAW FSRM 53-10-16. REPROTECTED IAW FSRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224052Seat Track · damagedNR 2 SEAT TRACK RT 3 EA AREAS OF CORROSION FROM FR 65 THRU FR 71. AFTER REMOVAL OF LEVEL 1 CORROSION AREA'S FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16 REPROTECTED AREA IAW SRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224051Seat Track · corrodedMDCC NR 1 SEAT TRACK, 1 EA AREA OF COROSION AT FRAME 57 AFTER REMOVAL OF LEVAL 1 CORROSION WAS FOUND TO BE WITHIN LIMITS IAW SRM 51-21-10 AND 51-75-10.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109224021Floor Panel · crackedFLOOR PANEL 242UJ HAS 1 EA 10" CRACK. FABRICATED FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.Sep 22, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214015Seat Track · corrodedCORRSION ON SEAT TRACK NR4 LT FR 43 AROUND FASTENER HOLE. REMOVED CORROSION IAW SRM 51-74-10 CHECKED LIMITS, AREA IS .5 L X .5 W X .004 DEEP. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, REPROTECTED AREA IAW SRM 51-21-10 AND 51-75-10.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109214018Seat Track · corrodedNR 2 SEAT TRACK RT 4 EA AREA CORROSION FR 55 - FR 58. REMOVED CORROSION AT NR2 SEAT TRACK FR 55 TO FR 58 IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-10. ALL AREAS FOUND TO BE WITHIN LIMITS. REPROTECTED SURFACES IAW SRM 51-21-10 AND 51-75-10.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109214016Seat Track · corrodedSEAT TRACK 3L CORRODED AT 4 PLACES BETWEEN FR 57-58. REMOVED CORROSION AFT SEAT TRACK 3L IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16 AND FOUND TO BE WITHIN LIMITS, REPROTECTED SURFACE IAW SRM 51-21-10 AND 51-75-10.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109214014Seat Track · corrodedMAIN CABIN CAMPARTMENT AT FR 38.1 TO FR 26 SEAT TRACK SCALLOP 2R HAS 3 EA AREA OF CORROSION THAT MEASURE 25.5", 80", AND 34.0". REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS STEP 2 AREA DEPTH .003, STEP 3 AREA DEPTH .015, STEP 4 AREA DEPTH .003, MAXIMSep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109214011Seat Track · corrodedMAIN CABIN COMPARTMENT AT FR 26 AND FR27 RT SIDE SEAT TRACK SCALLOP 5R HAS CORROSION APPROX 6.0". REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS MEASURED AREA 6" WIDE .75 AND DEEP .31. FOUND TO BE WITHIN LIMITS IAW SRM 51-21-10 AND 51-75-10.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109214010Seat Track · corrodedSEAT TRACK 4R FRAME 54.2 AND 54.3 HAS A .5" SQUARE AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS, AREAS IS 2.1 L X .42W AND DEPTH OF .021. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, REPROTECTED AREA IAW SRM 51-21-10 AND 51-75-10.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109214008Floor Panel · damagedFLOOR PANEL 132LG HAS A 4 INCH SECTION MISSING AND SEVERAL PUNCTURES ON BACK. FABRICATED REPLACEMENT FLOOR PANEL 132LG IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214006Floor Panel · damagedFLOOR PANEL 131MG HAS MULTIPLE CRACKS ON BACKSIDE FABRICATED REPLACEMENT FLOOR PANEL 131MG IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214004Floor Panel · damagedFLOOR PANEL HAS 2EA. BAD INSERTS, 2 CRACKS AT CUT OUT AND DELAMINATED CORNER AND 8" EDGE DAMAGE FABRICATED REPLACEMENT FLOOR PANEL 131NG IAW DWG SRZ-25-005 REV.J. IDENTIFIED REPLACEMENT PANEL IAW GMM7-0-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214003Floor Panel · crackedFLOOR PANEL 251BH HAS 1EA 10" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 251 BH IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214002Floor Panel · crackedFLOOR PANEL 232YG HAS 2 EA 9" CRACKS. FABRICATED FLOOR PANEL 232YG IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214001Floorboard · crackedFLOORBOARD HAS 2 EA 6" CRACKS ON BACKSIDE AND 1EA DELAMINATED CORNER FABRICATED REPLACEMENT FLOORBOARD 132MG IAW DWG SRZ-25-005, REV J MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109214000Floorboard · damagedFLOORBOARD HAS MULTIPLE PUNCTURES ON BACK SIDE AND DELAMINATED CORNER. FABRICATED REPLACEMENT FLOORBOARD 132KG IAW DWG SRZ-25-005 REV J IDENTIFIED. REPLACEMENT FLOORBOARD IAW GMM 7-0-1001. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109213988Floorboard · crackedFLOORBOARD 242RG HAS 1EA 12" CRACK. FABRICATED REPLACEMENT FLOORBOARD 242 RG IAW DWG SRZ 25-005, REV J.Sep 21, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109203975Floor Panel · crackedFLOOR PANEL 251QH HAS 1EA 10" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 251QH IAW DWG SRZ 25-005 REV J.Sep 20, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109203974Floor Panel · crackedFLOOR PANEL 241DF HAS 2EA 10" CRACKS FABRICATED REPLACEMENT FLOOR PANEL 241DF IAW DWG SRZ 25-005, REV J.Sep 20, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109193957Floor Panel · crackedFLOOR PANEL 252VF HAS 3EA. 9" CRACKS FABRICATED REPLACEMENT FLOOR PANEL 252VF IAW DWG 25-005, REV J.Sep 19, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109193956Floor Panel · crackedFLOOR PANEL 252PH HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 252PH IAW DWG 25-005, REV J.Sep 19, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109193955Floor Panel · crackedFLOOR PANEL 252UH HAS 2EA 12" CRACKS FABRICATED REPLACEMENT FLOOR PANEL 252UH IAW DWG SRZ 25-005, REV J.Sep 19, 2011 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201105261995Actuator · malfunctionedAIRFRAME SHAKES AT HIGHER SPEEDS UNLESS PRESSURE APPLIED TO RUDDER, APPLYING A CONSTANT LOAD TO IT. IN 5 PREVIOUS OBSERVATIONS OF IDENTICAL SYMPTOMS, THE ISSUE IN EACH CASE TURNED OUT TO BE WORN RUDDER ACTUATORS. INSTALLED LOWER RUDDER ACTUATOR. TORQUED ANMay 26, 2011 · N669FE · Airbus A300F4605R · Rudder Control SystemSDR FDEA201104211566Landing Gear · malfunctionedLOWERED THE LANDING GEAR ON FINAL AND RECEIVED A DUAL SYSTEM NLG RED "UNLOCK" . MISSED APPROACH AND COMPLIED WITH ECAM ( AFTER REVEIWING QRH) TO GRAVITY EXTEND PROCEDURE. AFTER SAME RED "UNLOCK" OCCURRED. COMMUNICATION WITH MX AND REVERSED GRAVITY EXT. CRAApr 21, 2011 · N669FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201104081395Landing Gear · malfunctionedON LANDING WHEN GEAR SELECTED DOWN, INDICATION WERE ON BOTH MAINS WERE DOWN & LOCKED, GREEN, NLG RED, UNLOCKED, NO GREEN. UPPER PANEL INDICATIONS WERE SAME. GREEN LOW AIR PRESSURE LIGHT CAME ON GREEN HYD SYS. RAISED GEAR & LOWERED GEAR AGAIN & NLG SHOWED REApr 8, 2011 · N669FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA200903140920Skin · crackedLEFT WING T/E BOTTOM SKIN CRACKED FWD AND OTBD OF PANEL NR 575FB. REPAIRED BY ADDING PLATE DOUBLER IAW EA 6-5710-127918.Mar 14, 2009 · N669FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA200903140919Skin · crackedRIGHT WING T/E BOTTOM SKIN CRACKED FWD AND OTBD OF PANEL NR 675FB REPAIRED BY ADDING PLATE DOUBLER IAW EA 6-5710-127918.Mar 14, 2009 · N669FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA200903060857Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE CORRODED FR16A, RBL 37.5 FS X1305 - FS X1305, RBL -Y953 - BL -Y953, WL -Z180 - WL -Z180. DISCREPANCY WITH CORRECT BL, AND TO CAPTURE DOCUMENTATION FOR FABRICATION OF SEAT TRACK INCLUDING PART MARKING AND PROPER INSTALLATION REFEREMar 6, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903040846Floor Panel · damagedMAIN CABIN FLOOR PANEL 231 VG IS BROKEN. MATERIAL ID A402H P/O NR 626008.1. FABRICATED NEW FLOORBOARD 241RJ IAW DWG SRZ-25-005 REV G.Mar 4, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903040845Floor Panel · damagedMAIN CABIN FLOOR PANEL 242 LK IS BROKEN. FABRICATED NEW FLOORBOARD 242LK IAW DWG SRZ-25-005 REV G.Mar 4, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor Panel
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