N661FE
Service difficulty reports · 318
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 = 'N661FE' 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.
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 = 'N661FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201408142165Fitting · crackedFOUND FUSELAGE CTR SECTION LOWER FRAMES FITTINGS BASE. FITTING CRACK ABOUT 0.500 INCHES AT FRAME 45. PERFORMED FRAME FEET MODIFICATION BTW STATION FRAME 41 & 46 IAW EO 6-5310-7-5015 01 PART 2. TITLE FUSELAGE, CTR WING, FRAME, FRAME FEET, FRAME 41 - 46, STRISDR FDEA201408142164Fitting · crackedFOUND FUSELAGE CTR SECTION LOWER FRAMES FITTINGS BASE. FITTING CRACK ABOUT 0.375 INCHES AT FRAME 46 POSITION. PERFORMED FRAME FEET MODIFICATION BTW STATION FRAME 41 & 46 IAW EO 6-5310-7-5015 01 PART 2. TITLE FUSELAGE CTR WING, FRAME, FRAME FEET, FRAME 41 THSDR FDEA201404240837Diaphragm · puncturedDURING ARMING R1 DOOR, TEST BUTTON WAS PUSHED & ALARM SOUNDED. HANDLE WAS PULLED UP & SLIDE DID NOT DEPLOY BUT FELL OUT BOTTOM OF DOOR WITH GIRT BAR ATTACHED TO FLOOR SEAL. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY OPERATION BOTTLE. ALL INDICATIONS NORMSDR FDEA201301170122Windshield · crackedRIGHT WINDOW HEAT FAULT, SELECTED OFF IAW ECAM. ABOUT 1 MINUTE LATER RT WINDSHIELD CRACKED. WINDOW ON GROUND SEEMED WARMER THAN NORMAL BUT NOT EXCESSIVE OR HOT. R & R F/O'S WINDSHIELD PANELS IAW AMM 56-11-11-04. PRECAUTIONARY, REPLACED WINDOW HEAT PROTSDR FDEA201212044243Slide · malfunctionedRIGHT DOOR DOES NOT INDICATE "SLIDE" WHEN DOOR CLOSE AND ARMED. WHILE MX WAS WORKING ON THE RT DOOR "SLIDE" INDICATION, OPEN DOOR AND THE SLIDE FELL OUT OF THE DOOR. DOOR HAD BEEN ARMED. R & R DUAL ESCAPE SLIDE IAW AMM 25-61-21-04. ACFT OK FOR SERVICE. RSDR FDEA201209133309Fitting · corrodedRIB 5 FWD LUG CORRODED. REPAIRED IAW EA 6-5740-149059.SDR FDEA201209043215Floorbeam · crackedFWD CARGO COMPT CEILING AREA OF M/D FLOORBEAM RT SIDE EDGE AREA GOT CRACK AT FR29 POSITION. REPAIRED IAW EA 6-5310-149065 WITH AB6F SRM 53-10-15. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA201209043217Seat Track · corrodedCENTER MAIN DECK, FOUND RT 5TH SEAT TRACK CORROSION AREA FROM FR45 TO 54 AT -Y1959 POSITION. FABRICATE AND R & R THE SEAT TRACK IAW DWG NR A53813618 AND AB6F SRM 51-40-21. REINSTALLED THE CROSSBEAMS OF FR45-FR54 -Y1959 WITH CHECK OK FOR SERVICE IAW AMM 20-21SDR FDEA201208263168Cover · crackedLT WING T/E FOUND 1EA COVER CRACKED POSITION NEAR LT MAIN LT MLG AFT TRUNNION INBD SIDE. REMOVED COVER FOR FABRICATION IAW DWG A57240775 THEN REPLACED IAW SRM 51-72-10 & 51-40-21. INSTALLED COVER AND CONDITION CHECKED GOOD. REPAIR CLASSIFIED AS MINOR PER GMSDR FDEA201208263172Floor Panel · damagedFWD CARGO FLOOR PANEL 131QG EDGE AREA HAS IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201208263171Adapter · damagedAFT MAIN DECK COMPT FLOOR LEVEL AREA FOUND CROSSBEAM FITTED WITH CARGO LOADING SYSTEM ADAPTER HAS EXCESS CHAFED MARKS ON CROWN AREA LOCATION AT FR58/BETWEEN Y1456 AND Y1959. TRANSFER THE HOLE FROM OLD PART TO NEW PART AND R/R ADAPTER BY FASTENER IAW SRM 51-7SDR FDEA2012082631710Floor Panel · damagedCENTER MAIN DECK FLOOR PANEL 242EJ HAS INSERT DAMAGE.SDR FDEA201208223107Floor Panel · corrodedCARGO BAY 162HF FLOOR PANEL INNER SURFACE CORRODED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATE A NEW FLOOR PANEL IAW SRM 53-10-20 & DWR.A53279962. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04. PER GMM 6-2-100 REPAIR CLASSIFIED AS MAJOR.SDR FDEA201208223111Floor Panel · debondedCARGO BAY 16HF FLOOR PANEL EDGE AREA DEBONDED. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279961. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201208223110Floor Panel · damagedCARGO BAY 162DF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201208223109Floor Panel · debondedCARGO BAY 161AF FLOOR PANEL EDGE AREA DEBONDED. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201208223108Floor Panel · dentedCARGO BAY 162EF FLOOR PANEL UPPER SURFACE HAS SEVERAL SMALL DENTS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201208142975Frame · crackedONE CRACK (2MM) WAS FOUND AT FRAME 44 RT HOLE "B" AREA INBD DIRECTION. REPAIRED IAW EO E6-5310-7-5006.SDR FDEA201207062495Tire · deflatedAFTER BLOCK-IN, INFORMED OF A DEFLATED TIRE ON RT MAIN GEAR. ALL INDICATIONS IN COCKPIT WERE NORMAL DURING TAXI IN. AFTER LANDING A "POP" WAS HEARD IN THE COCKPIT. IT APPEARED TO COME FROM UNDERNEATH CAPTS SEAT.SDR FDEA201106042119Priority Valve · leakingBLUE HYD SYS, AIR TURN BACK. LOST BLUE HYR PRESSURE AFTER TAKEOFF. ON RETURNING TO GATE FOUND HYD LEAK IN LT WHEEL WELL AFT BULKHEAD. LEAK FROM BLUE SYS MANIFOLD L/E FLAP PRIORITY VALVE. NEEDS VALVE-NIS MSN. BLED RESERVOIR PRESS AND REMOVED PRIORITY VALVE FRSDR FDEA201104301683Idg · failedLOST NR 2 GEN AT 80 KIAS ON TAKEOFF. RTO RESET GEN, GEN FAILED AGAIN AT 80 KIAS. PROCEEDED TO DESTINATION. REJECTED TAKEOFF AT 80 KIAS. R & R NR 2 IDG IAW AMM 24-11-11-04-01, OPS CHECK AND LEAK CHECK IS GOOD.SDR FDEA201008112936Pressure Switch · failedTAKE-OFF POWER APPLIED & DURING ROLL. AT APPROX 60 KTS, NR 1 ENG FUEL FILTER CLOGG LIGHT ILLUMINATED WITH ECAM ALERT. TAKEOFF ABORTED, THROTTLES REDUCED. ECAM WARNING EXTINGUISHED, ALL ENGINE INDICATIONS NORMAL. SUBSEQUENT T/O NORMAL, BUT NR 1 ENG CLOG ECAM SDR FDEA201007202601Skin · wornRT WING NR1 SLAT ERODED ABOVE NR 2 PYLON. BLEND OUT (2) ERODED AREAS TO SMOOTH CONTOUR AND DAMAGE AREAS MAY DIMENSION ARE 1.1" X 1", PENETRANT TO HONEYCOMB 2. 3" X 0.7", (2) LAYERS DAMAGED, THEN REPAIR WITH FIBERGLASS AND RESIN COMPOUND (CURE AT 180 DEGREE SDR FDEA201007202624Skin Panel · crackedLT WING LWR SKIN PANEL INBD OF RIB 9 SUPPORT FLANGE CRACKED, JOGGLED SECTION. DAMAGED FLANGE CUT AND REPAIRED IAW E 6-5710-7-5013 PT5.SDR FDEA201007202622Skin Panel · crackedOPEN R 1EA BOLT HOLE (POSITION G) WAS FOUND CRACK AT THE RI B 9 BOTTOM SKIN PANEL OF RT WING. IAW EO E6-5710-7-501 PT6. SKIN CRACK AREA REPAIRED IAW EA:6-5710-141607.SDR FDEA201007202606Skin · crackedRT WING T/E SPOILER SHROUD SUPPORT SKIN CRACKED, ABOUT .0625" BELOW NR 5 SPOILER INBD EDGE IAW DWG NR A57240194-200 FABRICATED. NEW SKIN SUPPORT INSTALLED IAW GMM 6-2-100.SDR FDEA201007202605Skin · crackedRT WING T/E SPOILER SHROUD SUPPORT SKIN GOT CRACK ABOUT .5" BELOW NR 4 SPOILER OTBD EDGE. IAW DWG NR A57240194-201 FABRICATED. NEW SKIN SUPPORT INSTALLED IAW GMM 6-2-100.SDR FDEA201007202604Angle · crackedRT WING T/E CENTER FLAP OTBD EDGE 1 EA ANGLE CRACKED. REMOVED THE DAMAGE ANGLE AND INSTALL BY NEW ONE IAW SRM 57-53-11. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201007202603Angle · crackedRT WING T/E OUTER FLAP INBD EDGE 1EA ANGLE CRACKED. REMOVED THE DAMAGED ANGLE AND INSTALL BY NEW ONE. IAW SRM 57-54-11 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201007202600Skin · wornLT WING NR1 SLAT ERODED ABOVE NR1 PYLON, BLEND OUT THE EROSION AREA TO SMOOTH CONTOUR AND MEASURED THE AREA MAX DIMENSION IS 4" * 0.9" AND (3) LAYERS DAMAGED, THEN REPAIRED WITH FIBERGLASS AND RESIN COMPOUND. (CURE AT 180 DEGREE F) IAW EA NR 6-5750-141608. RSDR FDEA201007202599Skin · crackedRT WING NR 1 SLAT L/E PREVIOUS REPAIR FILLER CRACKED. CONFIRMED NO SKIN CRACK BUT ONLY LIMITED TO FILLER FROM A "DENT" REPAIR. REMOVED RT NR 1 SLAT ASSY IAW AMM 27-80-11-4 2. CUT-OUT DAMAGED AREA 98MM X 84MM IAW SRM 57-42-11-3. NDI WAS COMPLETED THE CUT-OSDR FDEA201007202626Skin Panel · crackedTPE OPEN R 1 EA CRACK WAS FOUND FROM THE FASTENER HOLE AT THE R IB 9 BOTTOM SKIN PANEL OF LT WING. THE CRACK LENGTH IS .5" IAW EO E6-5710-7-5013 PT1. SKIN CRACK AREA REPAIRED IAW EA 6-5710-141607. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201007202625Skin Panel · crackedTPE OPEN R 1 EA CRACK WAS FOUND FROM THE FASTENER HOLE AT THE R IB 9 BOTTOM SKIN PANEL OF RT WING. THE CRACK LENGTH IS .2500" IAW EO E6-5710-7-5013 PT2. SKIN CRACK AREA REPAIRED IAW EA 6-5710-141607. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201007202623Skin Panel · crackedOPEN R 1 EA BOLT HOLE (POSITION G) WAS FOUND CRACKED AT THE R INBD 9 BOTTOM SKIN PANEL OF LT WING . IAW EO E6-5710-7 -5013. SKIN CRACK AREA REPAIRED IAW EA 6-5710-141607 (WINGS-AD 2008-06-18-EO 6-5710-5013 PT1- INSPECT AND MOD LOWER SKIN PANEL INBD OF RIB 9 SDR FDEA200907222694Smoke Detector · failedON T/O ROLL AT APPROX 80KTS RECEIVED AVIONICS SMOKE WARNING REJECTED T/O & WARNING WENT OUT. WARNING REOCCURED DURING TAXI WHEN POWER WAS PUSHED UP. INSPECTED AVIONICS BAY FOR WATER & SMOKE. NONE FOUND. RECEIVED WARNING AT GATE AVIONICS SMOKE, DISCONNECTSDR FDEA200808293646Hmu · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURGING STOPPED. PERFORMSDR 08FDEA03646Hmu · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG. THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURGING STOPPED. PERFORSDR 08FDEA03603Engine · unstableNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP, THEN EGT EXCEEDED LIMITS AT 952 DEG. THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURGING STOPPED. R&R N1SDR FDEA200808263600Sensor · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP, THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. REMOVED AND REPLACED THE FUEL FILTER AND THE TEMP INLET SENSOR (T 1.2). REF AMM 73-1SDR 08FDEA03600Sensor · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. REMOVED AND REPLACED THE FUEL FILTER AND THE TEMP INLET SENSOR (T 1.2). REF AMM 73-SDR 08FDEA03276Wire Harness · failedSHORTLY AFTER T/O, AUTO THROTTLES DISENGAGED AND WOULD NOT RESET. SIMULTANEOUSLY, N1 FOR NUMBER 1 ENGINE FAILED (BOTH ANALOG AND DIGITAL). AUTO THROTTLE REMAINED OFF THE REST OF FLT. FOUND DUCT FOR T/R VALVE WITH A HOLE BLOWN THRU. ALSO, THE HARNESS FOR NSDR 08FDEA01884Stiffener · crackedLEFT WING SPAR AREA, TOP SKIN STIFFENER AT WIAX 13-9 HAS A CRACK. MATERIAL ID FOR THE REPAIR IS 7075-T6 0.110 60-7018 EXTRUSION PO 566980.6 IAW A300-600 SRM 57-51-11, FIG 207 AND DWG NR A57241059. FABBED REPAIR ANGLE IAW A300-600 SRM 57-51-11, FIG 207. ALODSDR 08FDEA01804Skin · corrodedLEFT WING TIP INBD SIDE SKIN HAS CORROSION AROUND THE STATIC WICK BASE. REMOVED STATIC WICK BASE AND REMOVED THE CORROSION. ORIGINAL THICKNESS 0.056 IAW AA300-600 SRM 57-30-11. REMOVED MATERIAL 0.014. REMAINING THICKNESS 0.042 AND IS OUT OF LIMITS IAW A300SDR 08FDEA01788Seat Track · crackedFOUND THE FLANGE CRACKED ON THE DUMMY SEAT TRACK LEFT NR 3 AT FRAME 38.1 TO FRAME 40. REMOVED AND REPLACED THE TRACK A5327400500053, PO NR 617643.1. LOCATED AND DRILLED THE NEW TRACK IAW A300-600 SRM 51-40-44, PG 16. INSTALLED NEW TRACK IAW A300-600 SRM 51-SDR 08FDEA01777Floorbeam · corrodedCROSSBEAM AT FRAME 52 BETWEEN RBL 20 - RBL 40 IS CORRODED. REMOVED AND REPLACED THE CROSSBEAM IAW A300 SRM 51-40-21, PARA 5.SDR 08FDEA01776Seat Track · corrodedMAIN DECK FLOOR TRACK AT FRAME 53; RBL 20 IN CORRODED IN THE CENTER OF THE TRACK. REMOVED AND REPLACED SEAT TRACK IAW A300 SRM 51-40-21, PARAGRAPHS 5, 6 AND 7.SDR 08FDEA01953Access Door · chafedRIGHT WING PANEL HAS NUMEROUS CHAFED SPOTS ON PANEL 675 CB. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-51-12, PG 101. REMOVED PANEL IAW A300-600 SRM 51-40-21, PARA 5. REMOVED FASTENERS FROM PANEL IAW EA 6-5750-118484 AND A300-600 SRM 5SDR 08FDEA01734Intercostal · corrodedTHE MAIN CABIN INTERCOSTAL AT FRAME 13 LBL 35 IS CORRODED ON THE UPPER SURFACE. REMOVED CORROSION IAW SRM 51-73-10 PG 209 ITEM 5. ORIGINAL MATERIAL THICKNESS IS 0.079 IAW SRM 53-12-15 CONFIG 2 PG 4-2 (B). REMAINING THICKNESS IS 0.050. FOUND TO BE OUT LF LIMISDR 08FDEA01782Panel · damagedLEFT WING T/E PANEL 590 AB AFT CORNER IS BROKEN, BLENDED CORNER ON THE LEFT T/E PANEL, SEALED EDGE AND PAINTED IAW A300-600 SRM 51-42-20.SDR 08FDEA01775Seat Track · gougedMAIN CARGO COMPARTMENT, SEAT TRACK SCALLOPS ARE GOUGED AND ELONGATED AT FRAME C 58, 15 INCH, RBL 37 INCHES. THIS SDR WAS GENERATED IN ERROR. FOR DETAILS PLEASE SEE SDR TRACKING NR 08-1664.
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