N653FE

Service difficulty reports · 221

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 = 'N653FE' 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 FDEA201609083153Floor Panel · crackedAFT CARGO FLOOR PANEL 151XF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 8, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609083152Floor Panel · crackedAFT CARGO FLOOR PANEL 152PF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 8, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609083151Floor Panel · crackedAFT CARGO FLOOR PANEL 151SF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 8, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609083150Floor Panel · crackedAFT CARGO FLOOR PANEL 152WF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 8, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609083149Floor Panel · crackedAFT CARGO FLOOR PANEL 151TF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 8, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073140Floor Panel · crackedAFT CARGO FLOOR PANEL 152UF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073139Floor Panel · crackedAFT CARGO FLOOR PANEL 151WF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073138Floor Panel · crackedAFT CARGO FLOOR PANEL 151MF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073137Floor Panel · crackedAFT CARGO FLOOR PANEL 151UF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073136Floor Panel · crackedAFT CARGO FLOOR PANEL 151VF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073133Floor Panel · crackedCOURIER FLOOR PANEL 221LF HAS AN EIGHT INCH CRACK ON BOTTOM SIDE OF THE PANEL. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201609073132Floor Panel · damagedCOURIER FLOOR PANEL 221GF HAS MULTIPLE PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609073131Floor Panel · damagedCOURIER FLOOR PANEL 221MF DENTED, PUNCTURED, AND DAMAGED INSERTS. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005.Sep 7, 2016 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201606212101Indication Sys · malfunctionedR1 DOOR WOULD NOT ARM, NO SLIDE INDICATION ON ECAM. RELEASED FOR SERVICE IAW MEL 52-30-04, CATEGORY C, EXPIRATION 28JUN16, MEL 52-30-04, ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOJun 21, 2016 · N653FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201604031139Pump · malfunctionedYELLOW HYD PUMP LOW PRESS. WHEN ACFT RETURNED TO GATE ALL HYD INDICATIONS WERE NORMAL & THE HYD QUANTITIES WERE AT NORMAL LEVELS. PERFORMED A GND ENG RUN TO SEE IF THE FAULT WOULD RETURN. AFTER ENG START & OPERATION OF THE FLIGHT CONTROLS, THE FAULT RETURNEApr 3, 2016 · N653FE · Airbus A300F4605R · Hydraulic Pump (Electric/Engine), MainSDR FDEA201603311133Power Supply · malfunctionedL1 ESCAPE SLIDE LIGHTS WILL NOT ILLUMINATE WHEN PRESS TO TEST BUTTON IS ENGAGED. BUZZERS ARE OK. RELEASED FOR SERVICE IAW MEL 52-73-01-01 CATEGORY C, EXPIRATION 10 APR 16 MEL 52-73-01-01. R1 & L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYS LIGHTS INOPERATIVE.Mar 31, 2016 · N653FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201602230676Generator · faultedTAKEOFF ABORTED AT 80 KIAS DUE TO GENERATOR NR 2 FAULT. GEN 2 RESET NORMALLY IAW QRH. PER CREW DEBRIEF NR 2 GENERATOR RESET WITHOUT ANY FURTHER ISSUES, NO FURTHER ISSUES DURING FLIGHT, ACFT OK TO CONTINUE.Feb 23, 2016 · N653FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201503201034Rib · corrodedOPEN R MOD TYPE T MOD NR 6-5710-T0316275 REV NR PS P1 WINGS, BASIC WING STRUCTURE, TERMINATING ACTION OF RIB 5 FWD LUG RT COMPLY WITH EA 6-5710-T0316275 REV NR POS P1. COMPLIED WITH EA 6-5710-T0316275 P1 WINGS BASIC WING STRUCTURE & TERMINATING ACTION OF RMar 20, 2015 · N653FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201410123129Lug · corrodedLEFT RIB 5 MLG LUG FWD HAS CORROSION IN BORE, FWD & AFT FACE. REPAIRED IAW DWG R57240425 REV D & COMPLIED WITH EA 6-5710-T0311784 REV A PART 5.Oct 12, 2014 · N653FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201409192689Sensor · out of adjustDURING CRUISE ALTITUDE 35000, LT MAIN CARGO DOOR UNLOCK INDICATION CAME ON NO DISCERNABLE CHANGE IN CABIN PRESSURE, LIGHT REMAINED ON UNTIL 200 FL. DURING TROUBLESHOOTING WITH MAIN CARGO DOOR CLOSED & LOCKED FOUND DOOR WARNING SWITCH 49WS ADJUSTMENT AT MISep 19, 2014 · N653FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201405090970Fitting · crackedACFT COMPARTMENT FRAME 46, STRINGER 37 RT FRAME BASE FITTING FOUND CRACK 0.48 INCHES IN LENGTH. FUSELAGE CENTER SECTION, FRAME FEET, FRAMES 41 THRU 46 , STRINGERS 35 THRU 37 S/B: A300-53-6111 R5. THE JOB WAS ACCOMPLISHD. MAJOR REPAIR IAW FEDEX GMM 6-2-100May 9, 2014 · N653FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405090969Fitting · crackedACFT COMPARTMENT FRAME 45, STRINGER 37 RT FRAME BASE FITTING FOUND CRACK 0.44 INCHES IN LENGTH. FUSELAGE CENTER SECTION, FRAME FEET, FRAMES 41 THRU 46 , STRINGERS 35 THRU 37 S/B: A300-53-6111 R5. THE JOB WAS ACCOMPLISHD, MAJOR REPAIR IAW FEDEX GMM 6-2-100May 9, 2014 · N653FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405090968Fitting · crackedACFT COMPARTMENT FRAME 46, STRINGER 37 LT FRAME BASE FITTING FOUND CRACK 0.43 INCHES IN LENGTH. FUSELAGE CENTER SECTION, FRAME FEET, FRAMES 41 THRU 46 , STRINGERS 35 THRU 37 S/B: A300-53-6111 R5 , THE JOB WAS ACCOMPLISHD, MAJOR REPAIR IAW FEDEX GMM 6-2-100May 9, 2014 · N653FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405050947Splice · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING AT FRAME 44. FOUND TWO CRACK SIGNALS. REPAIRD IAW EA 6-5710-T0308161 PART 1. MAJOR REPAIR IAW GMM 6-2-100.May 5, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405050946Splice · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING AT 7 INCHES IN FRONT OF FRAME 44 STIFFENER LOCATION, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308161 PART 1. MAJOR REPAIR IAW GMM 6-2-100.May 5, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405050948Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE T FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 5, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040943Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE C FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040942Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE E FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040941Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040940Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE G FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040939Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE F FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040938Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE E FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307901 P1. MAJOR REPAIR IAW GMM6-2-100.May 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405040937Spar · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE S FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0307901 P1 EA TITLE, WINGS BASIC WING STRUCTURE AD2005-23-08--CRACK HOLES AT FRAME 47-SB57-6086 EMBODIMENT. REPAIRED THE FUSELAGE CTR WING BOX REAR SPAMay 4, 2014 · N653FE · Airbus A300F4605R · Wing SparSDR FDEA201405030927Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405030926Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405030925Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405030924Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405030923Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201405030922Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2014 · N653FE · Airbus A300F4605R · Fuselage, Wing Attach FittingsSDR FDEA201401230187Computer · faultedAT TAKEOFF CAPTAIN RECEIVED A FLASHING, SPD LIM, WARNING ON PFD NEXT TO SPEED TAPE. ALL SPEED LIMIT INFO WAS LOST ON CAPTAIN'S PFD. UPON RETRACTING SLATS, RECEIVED SLATS SYS 1 FAULT. CYCLED SLATS IAW QRH BUT FAULT REMAINED, REPEAT WU. SFCC NR 1 FAULTED, SJan 23, 2014 · N653FE · Airbus A300F4605R · Leading Edge Slat Control SystemSDR FDEA201212114281Power Supply · inoperativeON PREFLIGHT, FOUND R1 ESCAPE SLIDE WARNING LIGHT INOPERATIVE. REMOVED AND REPLACED AUTONOMOUS AS PER AMM 52-73-18-04, SLIDE CHECKED GOOD.Dec 11, 2012 · N653FE · Airbus A300F4605R · Escape SlideSDR FDEA201211204101Uplock · failedDURING GEAR RETRACTION, THREE GEAR UP & LOCKED INDICATIONS. UNSAFE NLG DOOR SYS 1 AND 2. COMPLIED WITH QRH GEAR DOWN AND LOCKED, NOSE DOOR REMAINED AMBER. RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING AND ROLLOUT. INSTALLED LT NLG DOOR UPLOCK ASSEMBLY IANov 20, 2012 · N653FE · Airbus A300F4605R · Landing Gear Door Retract SectionSDR FDEA201211204105Spring · brokenDURING GEAR RETRACTION THREE GEAR UP & LOCKED INDICATIONS, BUT UNSAFE NOSE GEAR DOOR SYS 1 AND 2. COMPLIED WITH QRH GEAR DOWN AND LOCKED, NOSE DOOR REMAINED AMBER. AIR TURNBACK WITH UNEVENTFUL LANDING AND ROLLOUT. FOUND BOTH SPRINGS FROM LT UPLOCK HOOK BRONov 20, 2012 · N653FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201112205377Skin · misrepairedLEFT WING INBD T/E FLAP LOWER SURFACE AT RIB 17 REAR SPAR, MISREPAIRED. CARRIED OUT REPAIR IAW EA 6-5750-155851.Dec 20, 2011 · N653FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201112205376Skin · misrepairedLT WING INBD T/E FLAP LOWER SURFACE AT RIB 12, REAR SPAR, MISREPAIRED. CARRIED OUT REPAIR IAW EA 6-5750-155851.Dec 20, 2011 · N653FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201112195364Bracket · chafedCASE DRAIN LINE LOOSE AND CHAFING AT NR 2 PYLON AFT END AT LOWER WING SKIN FEED THRU HOLE (AFT WING JACK PAD POINT). REPAIR ACCOMPLISHED IAW EA 6-5410-155854. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Dec 19, 2011 · N653FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201112155279Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 30, RBL 27 FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 6-5310-155850. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Dec 15, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201112155277Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 29, RBL 27 FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 6-5310-155850. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Dec 15, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201112155275Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 28 RBL 27 FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 6-5310-155850. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Dec 15, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201112145261Splice · dentedMAIN DECK CARGO RT FR 23 AT L8-9 BRACKET SPLICE FOUND DENTED. DENTED BRACKET SPLICE REMOVED AS PER SRM 51-40-21 REVISION 21. FABRICATED AS PER DRAWING A5377090320800 ISSUE "E" AND INSTALLED AS PER SRM 51-40-21 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM Dec 14, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Structure
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