N607FE
Service difficulty reports · 454
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 = 'N607FE' 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 = 'N607FE' 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 FDEA201403140502Support Fitting · corrodedLEFT WING OTBD FLAP VANE NR 1 SUPPORT FITTING FOUND CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 57-50-02 FIGURE 201 REPAIR 5 REVISION 54. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403140500Skin · canningFUSELAGE SKIN OIL CANNING BS 1445, RBL 31.50 ABOUT 45 INCHES ABOVE FWD DOOR HINGE LINE. DEPTH OF OIL CANNING MEASURED 0.265 INCH, MAXIMUM ALLOWABLE 0.190 INCH. REPAIRED IAW EA 1-5310-T0306647 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403110479Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, FWD MOUNT OTBD LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-122591B PART 3. REPAIR CLASSIFIED MAJOSDR FDEA201403110477Fitting · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE OTBD ACTUATOR LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-122591B PART 3. REPAIR CLASSIFIED MAJOSDR FDEA201403110475Hinge Fitting · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-122591B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-1SDR FDEA201403110476Fitting · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE INBD ACTUATOR LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 15750-122591B PART 3. REPAIR CLASSIFIED MAJOR ASDR FDEA201403110474Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHINGS FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306652 PART 1. REPAIR CLASSIFIED MAJOSDR FDEA201403110473Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING BARREL NUT HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. NEW BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306612 PART 1. REPAIR CLASSDR FDEA201403110486Longeron Splice · crackedCENTER CARGO RT SIDEWALL STATION 5-123 LONGERON SPLICE 41RT FOUND CRACKED. LONGERON SPLICE FABRICATED IAW DWG A5A7115 REVISION D. LONGERON SPLICE REMOVED AND REPLACED WITH NEW LONGERON SPLICE IAW SRM 51-33-01 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-SDR FDEA201403110485Support · crackedDURING OTBD SLAT DRIVE CABLE INSPECTION, RIGHT WING XOS 995 LE PANEL SUPPORT FOUND CRACKED. REPAIRED IAW SRM 57-40-01 REPAIR 9 FIGURE 201 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403110484Skin · damagedRIGHT WING INBD FLAP OTBD EDGE RIB SKIN FOUND WITH MISSING MATERIAL ABOUT 4.0 INCHES X 4.5 INCHES. DAMAGED SKIN REMOVED AND REPLACED IAW SRM 51-35-01 REVISION 55. SKIN FABRICATED IAW DWG ARC2305 REVISION C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION SDR FDEA201403110483Skin · crackedDURING INSPECTION, FOUND RIGHT WING XOS 995 FIXED LE NOSE SKIN FOUND CRACKED. REPAIRED IAW SRM 57-40-01 REPAIR 9 FIGURE 201 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403110482Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD AFT HINGE PIVOT INBD LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04 REVISION 78. REPAIRED IAW EA 1-5750-160605A PART 2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 120.SDR FDEA201403110481Fitting · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, OTBD ACTUATOR LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306611 PART 1. REPAIR CLASSIFIED MASDR FDEA201403110480Fitting · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, INBD ACTUATOR LUG FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306611 PART 1. REPAIR CLASSIFIED MAJOR SDR FDEA201403100471Door Frame · crackedMAIN DECK CARGO BAY BS 1305, LONGERON 26L AFT OF L3 LOWER DOOR FRAME WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403100470Door Frame · crackedMAIN DECK CARGO BAY BS 1256 LONGERON 26R FWD R3 LOWER DOOR FRAME WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201403100469Door Frame · crackedMAIN DECK CARGO BAY BS 1256 LONGERON 26L FWD L3 DOOR FRAME WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 55. CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR FDEA201205081762Feeder Cable · arcedFOUND FEEDER CABLE AT STA 1481 ARCED ON FLOORBEAM. R & R IAW SWPM 20-20-01, REV 26.0 AND AMM 20-30-10-2, REV 72.0 WIRING CONTINUITY CHECK CARRIED OUT IAW WDM 24-22-11, REV 74.0 FOUND SATISFACTORY. APU OPS TEST CARRIED OUT IAW AMM 49-10-00-2, REV 72.0 ASDR FDEA201205071758Frame · burnedDURING MASKING AND PREPARATION OF CPC AT MAIN DECK CARGO UNDER FLOORBEAM AT BS 1481, X=-24. FOUND ADJACENT TO APU FEEDER CABLE FRAME CUTOUT AREA BURNED THROUGH. REPAIRED IAW EA 1-5310-160606 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 114.SDR FDEA201205071757Support Fitting · corrodedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT RT SUPPORT FITTING AFT UPPER SPLICE FOUND CORRODED. R & R WITH NEW SPLICE IAW SRM 51-33-01 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205071756Support Fitting · crackedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT LT HAND SUPPORT FITTING FORWARD LOWER SPLICE FOUND CRACKED. R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205071755Support Fitting · crackedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT RT SUPPORT FITTING FORWARD LOWER SPLICE FOUND CRACKED. CRACKED SPLICE R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205071754Support Fitting · crackedCENTER LANDING GEAR-LINK ASSY UPPER DRAG BRACE MOUNT RT SUPPORT FITTING FORWARD UPPER SPLICE FOUND CRACKED. R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2- 100, REV 114.SDR FDEA201205051747Hinge Fitting · corrodedRIGHT WING FLAP SIDE OTBD HINGE, OTBD PIVOT HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA :1.342", FINAL HOLE DIA: 1.354", MAX ALLOWABLE DIA: 1.220" REPAIR ACCOMPLISHED IAW EA 1-5750-160603, PART 1. REPAIR SDR FDEA201205051746Hinge Fitting · corrodedRIGHT WING FLAP SIDE OTBD HINGE, INBD PIVOT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA :1.378" , FINAL HOLE DIA: 1.388" MAX.ALLOWABLE DIA.: 1.220" REPAIR ACCOMPLISHED EA 1-5750-160603, PART 1. REPAIR CLASSDR FDEA201205051745Hinge Fitting · corrodedLEFT WING FLAP SIDE HINGE FITTING, OTBD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03, REV 72, EXISTING HOLE DIA: 1.2575", FINAL HOLE DIA: 1.288" , MAX ALLOWABLE DIA: 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-160604SDR FDEA201205051744Hinge Fitting · corrodedLEFT WING FLAP SIDE HINGE FOUND CORRODED. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA : 1.220", FINAL HOLE DIA: 1.248" , MAX ALLOWABLE DIA : 1.220" REPAIR ACCOMPLISHED IAW EA NR 1-5750-160604 PART 1. REPAIR CLASSSSDR FDEA201205051743Hinge Fitting · corrodedDURING FLOURESCENT PENETRANT INSPECTION CORROSION FOUND AT LT WING OTBD FLAP INBD HINGE, INBD PIVOT HOLE . REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. EXISTING HOLE DIA : 1.187", FINAL HOLE DIA: 1.216", MAX ALLOWABLE DIA : 1.150". REPAIR ACCOSDR FDEA201205051742Bushing · wornLEFT WING FLAP SIDE HINGE BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED: DIA 1.187" AND FOUND EXCEED LIMIT IAW CMM 57-52-04 REV 72 MAX ALLOWABLE DIA: 1.150". NEW BUSHING FABRICATED AND INSTALLED REFER TO MASTER COPY EA 1-5750SDR FDEA201205031719Skin · crackedLT WING LOWER LEADING EDGE ACCESS PANEL 526DB FORWARD SUPPORT FLANGE AT STATION XORS 799 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-03, REPAIR 1, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR GMM 6-2-100 REV 114.SDR FDEA201205031718Panel · crackedNR 2 ENGINE AIR INTAKE REAR CENTER SPAR LT LOWER PANEL FOUND WITH CRACK. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2 REVISION 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205031717Panel · crackedLOWER VERTICAL STABILIZER NR 2 ENGINE AIR INTAKE REAR CENTER SPAR RT LOWER PANEL FOUND WITH CRACK. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201 REPAIR 2, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205031716Support Fitting · crackedAIR CONDITIONER DOOR AFT FRAME FITTING FOUND CRACKED. SUPPORT FITTING REMOVED AND REPLACED WITH FABRICATED SUPPORT FITTING AS PER SRM 51-33-01 REVISION 49. NEW SUPPORT FITTING FABRICATED AS PER DWG ACA3135-2 REVISION B . REPAIR CLASSIFIED AS MAJOR AS PER GMSDR FDEA201205021709Longeron · crackedCRACK INDICATION FOUND APPROX 0.5" IN LENGTH DURING X-RAY INSPECTION AT CABIN STA 5-0, LONGERON 3R FWD SECTION EDGE. REPAIRED SRM 53-00-05, FIG 202, REPAIR 1 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301684Seat Track · chippedCABIN FLOOR SEAT TRACK AT STA 635, X=-27.5 FOUND CROWN CHIPPED OFF. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301683Seat Track · chippedCABIN FLOOR SEAT TRACK AT STA 635, X=-8.5 FOUND CROWN CHIPPED OFF. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301682Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 5-10, X=27.5 FOUND WITH CORROSION. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301681Skin · crackedRT WING LOWER FIXED L/E AT NR 14 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201204301680Panel · crackedLT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204301679Skin · crackedLT WING LOWER FIXED L/E AT NR 12 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7, FIGURE 201, REVISION 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201112295458Switch · inoperativeRIGHT DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYS INOPERATIVE. REPLACED REMOTE SLIDE PTT SWITCH ASSY PER MM 25-61-04-4-0, SYS OPS CHECKED NORMAL.SDR FDEA201107132670Elevator · damagedON POSTFLIGHT INSPECTION, FOUND RT INBD ELEVATOR UNLOCKED. IN FLIGHT NO ABNORMAL FLIGHT CONTROL PROBLEMS. REMOVED RT ELEVATOR, INBD DETACHABLE IAW AMM 27-30-10-4-0. REMOVED RT ELEVATOR, INBD IAW AMM 27-30-20-4-0. INSTALLED RT INBD ELEVATOR, INBD AMM 27-30SDR FDEA201107092622Connector · dirtyR1 DOOR REMOTE PRESSURE TEST INOPERATIVE ON PREFLIGHT VERIFIED SLIDE PRESSURE IN GREEN BAND (3300PSI). REF SRM 25-61-0 AND AMM 25-61-06-5, CLEANED DISCONNECT PLUG AND RESEATED LENS MODULE. SLIDE LOW PRESSURE PRESS TO TEST FUNCTIONS NORMAL. OK FOR SERVICSDR FDEA201102080501Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED, ON PREFLIGHT BATTERY NR 1 LOW. RELEASED FOR SERVICE IAW MEL: 33-50-04 CATEGORY: C. R & R EMERGENCY EXIT LIGHTS POWER SUPPLY AND CHECKED NOT OK IAW MM 33-51-01.SDR FDEA201011204494Button · failedTHE ESCAPE SLIDE BOTTLE PRESSURE LIGHT ON THE 1R ENTRY DOOR IS ILLUMINATED FOUND THAT PUSH BUTTON PART OF INDICATOR LAMP HAS A BENT PIN CAUSING IT TO STAY IN THE TEST POSITION. REPLACED PUSH BUTTON INSIDE PORTION IN REF TO MM 25-61-04-4 LIGHT TEST GOOD PER MSDR FDEA201005131527Frame · misrepairedMAIN DECK CARGO - EXISTING REPAIR FOUND AT RT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS. EXISTING REPAIR AT MAIN DECK CARGO RT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS EVALUATED FOUND REPAIR NOT IAW ANY SRM REPAIR SCSDR FDEA201005131526Frame · misrepairedMAIN DECK CARGO - EXISTING REPAIR FOUND AT LT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS. EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS EVALUATED FOUND REPAIR NOT IAW ANY SRM REPAIR SDR FDEA201005051461Skin · misrepairedAGING INSP - EXISTING REPAIR ON RT WING SLAT ASSY NR 6 LOWER SURFACE. EXISTING REPAIR ON RT WING SLAT ASSY NR 6 LOWER SURFACE EVALUATED, FOUND NOT IAW SRM. SLAT ASSY NR 6 R & R IAW AMM 27-80-30. OPERATION TEST CARRIED IAW AMM 27-80-30 FOUND SATISFACTORY. EOSDR FDEA201005051460Rib · crackedRT WING - SLAT ASSY NR6, XOS 868 RIB FOUND CRACKED. RT WING SLAT ASSY NR 6, R & R IAW AMM 27-80-30-4, REVISION 64. SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-4, REV 64. FOUND SATISFACTORY.
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