N659FE

Service difficulty reports · 213

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 = 'N659FE' 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 FDEA200910083508Skin · crackedLT WING LWR SKIN CUTOUT FOR PANEL 575 FB: APPROX 3/16 " (0.187") CRACK ON LWR WING SKIN, FWD EDGE OF PANEL CUTOUT, BEGINNING AT THE OUTBD HOLE (POS G), HOLE COMMON TO DOOR SURROUND ITEM (2) AS SHOWN IN FIGS 1,2 AND 3, PROTRUDING AFT APPROX 5 O-CLOCK DIREOct 8, 2009 · N659FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA200910063485Support · crackedNR 1 ENG PYLON ACCESS PANEL 413 BL HAS 2 EA CRACKS AT SEAL SUPPORT CORNERS. REMOVED SEALS AND RETAINERS AND FABRICATED 2 EA DOUBLERS REF SRM 54-52-51; FIG 205. INSTALLED REPAIR DOUBLERS REF SRM 51-40-21; PARA 6. REINSTALLED SEALS AND RETAINERS SRM 54-52-5Oct 6, 2009 · N659FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910063483Mount · corrodedNR 2 ENG PYRAMID FITTING HAS CORROSION ON LWR SURFACE AND AFT LT MOUNT HOLE. REAMED LT AFT MOUNT HOLE SRM 54-51-81; FIG 104; SHEET 2 TO 0.965 IN 4TH OVER-SIZE. REMOVED 0.002 IN PITTING CORROSION IN LT AFT MOUNT HOLE BY LOCAL BLEND OUT SRM 54-51-81; FIG 104; Oct 6, 2009 · N659FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA200910063484Web · bentWEB BENT FROM FRAME 85 TO 83; STR 32R. REMOVED BENT STRAP AND WEB AND INSTALLED NEW STRAP AND WEB PN 660142.1 AND 660153.1 IAW SRM 51-40-21; PARA 6 AND PARA 7. DRILLED HOLES IN NEW STRAP AND WEB IAW SRM 51-40-44; TABLE 8.Oct 6, 2009 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200910063481Profile · crackedAFT CARGO DOOR; AFT DOOR CUTOUT CRACKED PROFILE AT FASTENER HOLE LWR AFT CORNER. REMOVED OLD PROFILE AND INSTALLED NEW PROFILE PO NR 664219.4 IAW SRM 51-40-21; PARA 5 AND 13. DRILLED NEW PROFILE IAW SRM 51-40-44; TABLE II.Oct 6, 2009 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200910053477Seat Track · wornMAIN CABIN SEAT TRACK IS GOUGED AND SCALLOPS ARE WORN FROM BS 1446 TO BS 1471; RBL 37. BLENDED WORN AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. MAX ALLOWABLE MATERIAL LOSS IS 0.028. MATERIAL REMOVED IS 0.008. ALODINED; PRIMED AND TOP COAT APPLIED.Oct 5, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910013454Seat Track · wornMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 28; LBL 68 - LBL 70. REMOVED CORROSION AND BLENDED WORN AREA AND FOUND TO BE WITHIN ALLOWABLE LIMITS. MAX ALLOWABLE MATERIAL LOSS IS 0.028 IN. ACTUAL MATERIAL LOSS IS 0.011 IN. ALODINED; PRIMED Oct 1, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910013453Seat Track · wornMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 27; LBL 68 - LBL 70. REMOVED CORROSION AND BLENDED WORN AREA AND FOUND TO BE WITHIN ALLOWABLE LIMITS. MAX ALLOWABLE MATERIAL LOSS IS 0.028 IN. ACTUAL MATERIAL LOSS IS 0.016 IN. ALODINED; PRIMED AOct 1, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910013452Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT THE RT OF THE TAIL SKID ON FRAME 77. REPAIRED DAMAGED AREA IAW SRM 53-10-12; FIG 209 AT FRAME 77; STRINGER 51R TO STRINGER 51R.Oct 1, 2009 · N659FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200910013451Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT THE LT SIDE OF THE TAIL SKID ON FRAME 77. REPAIRED DAMAGED AREA IAW SRM 53-10-12; FIG 209 AT FRAME 77; STRINGER 51L TO STRINGER 51L.Oct 1, 2009 · N659FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200910013450Skin · gougedEXTERNAL FUSELAGE SKIN AT THE FWD CARGO DOOR CUTOUT (FWD SECTION) IS GOUGED FROM FRAME 20-20A; STRINGER 38R - STRINGER 41R. REPAIRED EXTERNAL SKIN GOUGE IAW EA 6-5310-127993. REMOVED AND REINSTALLED COVER PLATE AND CABLE GUIDE IAW AMM 53-10-53-4. IAW EA 6-5Oct 1, 2009 · N659FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200909303444Seat Track · corrodedMAIN CABIN SEAT TRACK IS GOUGED AND SCALLOPS WORN FROM BS 1446 - BS 1471; RBL 37. BLENDED GOUGES AND WORN AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16, FIG 101. MAX ALLOWABLE MATERIAL REMOVAL IS 0.028. MATERIAL LOSS IS 0.012. ALODINED; PRIMED AND TOP Sep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303443Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 32; LBL 68 - BL 70. REMOVED CORROSION AND WORN AREAS IAW 53-10-16. MATERIAL LOSS FOUND TO BE 0.024. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.028. MATERIAL LOSS WITHIN ALLOWABLE LIMITS IAW SRM 53-10Sep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303442Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 31; LBL 68 - BL 70. REMOVED CORROSION AND WORN AREAS IAW SRM 53-10-16. MATERIAL LOSS FOUND TO BE 0.018. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.028. MATERIAL LOSS WITHIN ALLOWABLE LIMITS IAW SRM 53-Sep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303441Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 30; LBL 68 - BL 70. REMOVED CORROSION AND BLENDED WORN AREA AND FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. MAX MATERIAL LOSS IS 0.028. ACTUAL MATERIAL LOSS IS 0.012. ALODINED; PRIMED AND TOP COSep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303440Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 29; LBL 68 - BL 70. REMOVED CORROSION AND BLENDED WORN AREA AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL LOSS IS 0.028. ACTUAL MATERIAL LOSS IS 0.015. ALODINED; PRIMED AND TOP COAT IAW 53-10-10, FSep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303439Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 26; LBL 68 - BL 70. REMOVED CORROSION AND BLENDED WORN AREA AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL LOSS IS 0.028. ACTUAL MATERIAL LOSS IS 0.010. ALODINED; PRIMED AND TOP COAT IAW SRM 53-10-1Sep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303438Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 25; LBL 68 - BL 70. REMOVED CORROSION AND WORN AREAS. MATERIAL LOSS FOUND TO BE 0.006. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.028. MATERIAL LOSS WITHIN ALLOWABLE LIMITS IAW SRM 53-10-16. ALODINEDSep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909303437Seat Track · corrodedMAIN CABIN SEAT TRACK IS CORRODED AND SCALLOPS WORN AT FRAME 24; LBL 68 - BL 70. REMOVED CORROSION AND WORN AREAS. MATERIAL LOSS FOUND TO BE 0.015. MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.028. MATERIAL LOSS WITHIN ALLOWABLE LIMITS IAW SRM 53-10-16. ALODINED Sep 30, 2009 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907292832Transmitter · failedGREEN RSVR LO LEVEL ALERT. FOLLOWED ECAMS, MANUAL GEAR EXTENSION. OVERHEAD GAUGE SHOWED GOOD QUANTITY. AFTER SHUTDOWN, BOTH QUANTITY INDICATORS SHOW MAX QUANTITY. RESTORED LANDING GEAR TO NORMAL OPERATIONS IAW MM 32-33-00-2. REMOVED AND REPLACED GREEN SYS Jul 29, 2009 · N659FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA200901290390Servo · malfunctionedECAM WARNING OF JAMMED GREEN SERVO RECEIVED ON TAKEOFF ROLL AT 83 KNOTS. REJECTED TAKEOFF, ALL CHECKLIST AND ECAM DIRECTIVES COMPLIED WITH. T/S GREEN SERVO JAM PER TSM 27-14-00, FIG 103, BLOCK 2. FOUND PIN B TO C OPEN ON 27CB GREEN SERVO JAM SWITCH. NEEDJan 29, 2009 · N659FE · Airbus A300F4605R · Rudder Control SystemSDR 08FDEA04650Idg · underservicedON TAKEOFF, ROLL REJECTED AT 50 KTS FOR GEN1 FAULT ECAM ALERT. ACCOMPLISHED REJECTED AND ECAM PROC TAXIED CLEAR, TO RAMP FOR EXTRA FUEL. ACN RELEASED FOR SERVICE PER MEL/CDL: 24-11-01-A CAT: B EXP: 03NOV08 "MEL 24-11-01-A: GEN (IDENTIFY 1 OR 2) INOP APU GEN Oct 31, 2008 · N659FE · Airbus A300F4605R · AC Generator-AlternatorSDR 07FDEA05169Adapter · crackedCRACK AT FR 30 AND BETWEEN TRACKS Y-450 AND Y-953. ADAPTER REPLACED IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 07FDEA05176Skin Panel · delaminatedLT ELEVATOR, DISBOND AT INNER LOWER SKIN AT T/E AREA INBD. DISBOND AT INNER LOWER SKIN WAS REPAIRED IAW SRM 55-21-12, FIG 201.Dec 31, 2007 · N659FE · Airbus A300F4605R · Elevator, Plate/SkinSDR 07FDEA05175Seat Track · corrodedSEAT TRACK WITH CORROSION OUT OF LIMITS AT FR41, Y-450. SEAT TRACK REPLACED BETWEEN FR 40 AND FR 45 AT Y-450 IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05174Seat Track · corrodedSEAT TRACK WITH CORROSION OUT OF LIMITS AT FR42, Y0. SEAT TRACK REPLACED BETWEEN FR 40 AND FR 45 AT Y0 IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05173Seat Track · corrodedSEAT TRACK AT Y-953 WITH CORROSION OUT OF LIMITS BETWEEN FR45 AND FR49. TRACK REPLACED BETWEEN FR45 AND FR54 AT Y-953 IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05172Skin · gougedLWR AFT FUSELAGE GAUGE BETWEEN FR 38.2 AND 39 AND BETWEEN STR 40 AND 41 LT. REPAIRED IAW SRM 53-10-12, FIG 207, SHEET 5.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 07FDEA05171Adapter · crackedAT FR 28 AND BETWEEN TRACKS Y-450 AND Y-953 FOUND CRACKED. ADAPTER REPLACED IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 07FDEA05170Adapter · crackedAT FR 29 AND BETWEEN TRACKS Y-450 AND Y-953 WITH CRACK. ADAPTER REPLACED IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 07FDEA05168Seat Track · corrodedTRACK AT Y-953 AND BETWEEN FR 15 AND 19 WITH CORROSION. TRACK REPLACED IAW SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05167Floorbeam · crackedCROSSBEAM CRACKED AT FR 30 AND BETWEEN TRACKS Y 450 AND Y 953. REPAIRED IAW SRM 53-10-15, FIG 212.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA05166Floor Support · corrodedPAX CABIN, BEAM Y 735 BETWEEN FR 12A TO FR 13A WITH CORROSION. SUPPORT REPLACED IAW WITH SRM 51-72-16 AND PAINTED.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA05165Floorbeam · corrodedFLOORBEAM AT Y 1959 AND BETWEEN FR 12A AND 13A WITH CORROSION. FLOORBEAM REPLACED PER SRM 51-72-10.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA05164Seat Track · corrodedTRACK WITH CORROSION AT Y-953 AND BETWEEN FR 30 AND 31. TRACK REPAIRED IAW SRM 53-10-16 FIG 201.Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05163Floorbeam · crackedAFT CARGO COMP'T, CROSSBEAM CRACKED AT FRAME 64 BETWEEN TRACKS Y-953 AND Y- 1456. CROSSBEAM REPAIRED AT FRAME 64 BETWEEN TRACKS Y-953 AND Y-1456 IAW SRM 53-10-15, FIG 211, (SHEETS 1 AND 2).Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA05162Floorbeam · crackedAFT CARGO COMP'T, CROSSBEAM CRACKED AT FRAME 59 BETWEEN TRACKS Y-953 AND Y- 1456. CROSSBEAM REPAIRED AT FRAME 59 BETWEEN TRACKS Y-953 AND Y-1456 IAW SRM 53-10-15, FIG 211 (SHEET 1 AND 2).Dec 31, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA05152Floorbeam · crackedAFT CARGO COMP'T, CROSSBEAM CRACKED AT FRAME 66 BETWEEN TRACKS Y -953 AND Y- 1456. CROSSBEAM REPAIRED AT FRAME 66 BETWEEN TRACKS Y -953 AND Y -1456 IAW SRM 53-10-15, FIGURE 211 (SHEET 1 AND 2).Dec 28, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA05151Seat Track · crackedTRACK AT NR Y 2462 AND BETWEEN FR 18 AND 21 FOUND DAMAGED. SEAT TRACK WAS REPAIRED IAW SRM 53-10-16 FIGURE 203.Dec 28, 2007 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00003Floorbeam · crackedCROSSBEAM AT FR 65 WITH DEFORMITY BETWEEN Y953 AND Y1456. CROSSBEAM AT FR 65 REPAIRED BETWEEN Y953 AND Y1456 IAW SRM 53-17-15, FIG 203, SHEET 1 AND 2.Dec 13, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA00002Floorbeam · crackedCROSSBEAM AT FR 66 WITH DEFORMITY BETWEEN Y953 AND Y1456. CROSSBEAM AT FS 36 REPAIRED BETWEEN Y953 AND Y1456 IAW SRM 53-10-15, FIG 205, SHEET 2.Dec 13, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA05146Floorbeam · crackedAFT CARGO COMPT, CROSSBEAM CRACKED AT FRAME 60 BETWEEN TRACKS Y-1456 AND Y-1959. CROSSBEAM REPAIRED AT FRAME 60 BETWEEN Y-1456 AND Y-1959 IN ACCORDANCE WITH SRM 53-10-15 FIG 211 (SHEET 1 AND 2).Nov 29, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA00001Frame · crackedLT MLG, L/G MAIN DOOR LEANING WITH WEB FWD CRACKED WEB OF FRAME 48. REPAIRED IAW FEDEX EA NR 6-5320-115304.Nov 28, 2007 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR 06FDEA1222Control Unit · malfunctionedGEAR WOULD NOT RETRACT. BOTH GEAR POSITION INDUCTORS SHOWED 3 GREEN TRIANGLES AND 3 RED UNLOCKS. RETURNED HANDLE TO DOWN POSITION AND HAD ECAM STATUS MESSAGE OF L/G RETRACTION INOP, TRIED BOTH L/G POSITION DETECTION SYS 1 & 2. REMOVED AND REPLACED LANDING GMar 24, 2006 · N659FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 06FDEA1212Control Unit · malfunctionedGEAR WOULD NOT RETRACT. BOTH GEAR POSITION INDICTORS SHOWED 3 GREEN TRIANGLES AND 3 RED UNLOCKS. RETURNED HANDLE TO DOWN POSITION AND HAD ECAM STATUS MESSAGE OF L/G RETRACTION INOP, TRIED BOTH L/G POSITION DETECTION SYS 1 AND 2. REMOVED AND REPLACED LANDINGMar 23, 2006 · N659FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 05FDEA03310Skin · chafedLT WING CENTER FLAP UPPER SKIN HAD 4 SMALL CHAFED AREAS. INSTALLED REPAIR DOUBLER PER EA NR 6-5750-92547.Oct 7, 2005 · N659FE · Airbus A300F4605R · Trailing Edge FlapsSDR 05FDEA03184Seat Track · damagedMAIN DECK FLOOR ARTICULATED SEAT TRACK NR 6 RT ATTACH BOLT IS WORN BEYOND SERVICABLE LIMITS AT FRAME 54 MAX ALLOWABLE WEAR IS .039 ACTUAL MEASUREMENT .039. REMOVED SEAT TRACK IAW A300-600 SRM 51-40-21, RECEIVED NEW SEAT TRACK PO NR 499975.1. INSTALLED NEW SEOct 1, 2005 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02729Mount · corrodedNR 1 ENG FWD MOUNT 0/B AFT HOLE HAS PITTING CORROSION. REAMED HOLE WITHIN LIMITS IAW A300-600 SRM 54-51-81. CAD PLATED HOLE IAW A300-600 SRM 54-51-81 AND A300-600 SRM 51-21-10.Sep 1, 2005 · N659FE · Airbus A300F4605R · Engine Mount SectionSDR 05FDEA00307Line · leakingAFTER SLAT RETRACTION LOST YELLOW SYS HYD PUMP, FOLLOWED BY LOW PRESSURE. ONE MINUTE LATER LOST YELLOW SYS QUANTITY. APPROX 1 MIN PUMP WAS RUNNING. FOUND LEAK AT FLEX LINE JUST BEHIND TOP OF LT MAIN GEAR LEG. ADDED MPN A2714201300000, CPN 2713423 QTY 1, ADFeb 18, 2005 · N659FE · Airbus A300F4605R · Hydraulic System, MainSDR 04FDEA02958Windshield · failed56-10 0007810 20OCT04 MEM CLOSE L/P: 00949119 CAPT FWD WINDSHIELD OUTER PANEL SHATTERED AT FL 310 REMOVED CAPTAINS WINDSHIELD REF A 300-600 MM 56-11-1 1-4. R/I IAW MM 56-11-11-4 MFG NP175201-1 SRL 96113H6246 ON MFG NP175201-5 SRL 04278H7866 AIRBUSOct 20, 2004 · N659FE · Airbus A300* · Flight Compartment Windows
Back to N659FE