N522FE
Service difficulty reports · 338
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 = 'N522FE' 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 = 'N522FE' 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 FDEA201308221999Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT HOLE HAS SURFACE CORROSION. REPAIRED IAW EA 1-5750-104703C PART 2 STEPS 1,2, AND 4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117.SDR FDEA201308222000Hinge Fitting · corrodedLEFT WING INBD FLAP, OTBD FWD (WING SIDE) HINGE PIVOT HOLE HAS SURFACE CORROSION. REPAIRED IAW EA 1-5750-104702C PART 2 STEPS 1,2 AND 4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100 REVISION 117.SDR FDEA201308221998Hinge · corrodedLEFT WING OTBD FLAP INBD AFT HINGE PIVOT INBD BORE CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-04 REVISION 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0302073 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 117.SDR FDEA201308191960Hinge Fitting · damagedLT WING INBD FLAP, OTBD AFT (HINGE SIDE) PIVOT INBD BORE FOUND DAMAGED AFTER BUSHING REMOVAL. FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. REPAIRED IAW EA 1-5750-104706D, PART 2, STEPS 1,2,3 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308191959Hinge Fitting · damagedLT WING INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BORE FOUND, EXCEEDED LIMIT AFTER BUSHING REMOVAL. REPAIRED IAW EA 1-5750-104706D, PART 2, STEPS 1, 2, 4 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308191958Hinge Fitting · corrodedLT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44-07, REV 76. REPAIRED IAW EA 1-5750-104702C, PART 2, STEPS 1, 2 AND 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308191957Hinge Fitting · corrodedRT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT CORROSION. FOUND EXCEEDED LIMIT IAW CMM 57-44-07, REV 76. REPAIRED IAW EA 1-5750-104703C, PART 2, STEPS 1, 2, AND 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181946Skin · crackedFASTENER HOLES FOUND CRACKED DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED IAW EA 1-5710-T0302030 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201308181947Skin · crackedFASTENER HOLES FOUND CRACKED DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER EA 1-5710-T0302029 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116SDR FDEA201308181945Bulkhead · canningCENTER LANDING GEAR WHEEL WELL - OIL CANNING FOUND AT RT KEEL BEAM WEB X=31.50, Y=1435 , 43" ABOVE FWD DOOR HINGE LINE. OIL CANNING MEASURED 0.215", MAXIMUM ALLOWABLE 0.19". REPAIRED IAW EA 1-5310-T0301907. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308181944Hinge Fitting · corrodedRT WING INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. REPAIRED IAW EA1-5750-104705D, PART 2, STEPS 1, 2, 3 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181943Hinge Fitting · corrodedRIGHT WING INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. REPAIRED IAW EA 1-5750-104705, PART 2, STEPS 1, 2, 4 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181942Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE BARREL NUT HOLES SURFACE CORROSION. REPAIRED IAW EA 1-5750-T0302028A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181941Hinge Fitting · corrodedRT WING OTBD FLAP, INBOD FWD (WING SIDE) HINGE LOWER MOUNT INBD HOLE HAS SURFACE CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1-5750-T0302028A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181940Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL NUT HOLES SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09, REV 76. REPAIR CLASSIFIED MINOR GMM 6-2-100, REV 117.SDR FDEA201308181939Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL NUT LOWER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0302072, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181938Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT UPPER BORE CORRODED. REPAIRHED IAW EA 1-5750-T0302072, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181937Hinge Fitting · corrodedLT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORRODED. REPAIRED IAW EA 1-5750-T0302026, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308181936Structure · corrodedLT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1-5750-T0302070A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.SDR FDEA201308181935Hinge · corrodedLT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44- 09, REV 76. REPAIRED IAW EA 1-5750-T0302070A, PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117SDR FDEA201308181934Hinge · corrodedLT WING OTBD FLAP, INBD FWD( WING SIDE) HINGE PIVOT HOLE BORE CORROSION. FOUND EXCEEDED LIMITS. REPAIRED IAW EA 1-5750-T0302026. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308181933Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. REPAIRED IAW CMM.SDR FDEA201308151893Longeron Splice · crackedCENTER CARGO LONGERON SPLICE CRACKED AT BS 5-123 LONGERON 34RT. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308151895Longeron Splice · crackedCENTER CARGO LONGERON SPLICE CRACKED AT BS 5-123, LONGERON 39R. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308151897Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING CRACKED AT BS 5-123, LONGERON 49L. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REVISION 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308151896Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING CRACKED AT BS 5-123 LONGERON 49R. R & R WITH NEW FABRICATED SPLICE SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308151894Longeron Splice · crackedCENTER CARGO LONGERON SPLICE CRACKED AT BS 5-123 LONGERON 37R. R & R IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308141876Strap · crackedRT WING LOWER SURFACE L/E PANEL 626GB CUTOUT FOUND LOWER STRAP CRACKED XOS 993.237. REPAIRED IAW SRM 57-40-03, REPAIR 1, FIG 201, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308141874Skin · crackedRT WING LOWER SURFACE L/E NR 6 SLAT INBD COMMON IDLE TRACK CUTOUT FOUND SKIN CRACKED AT XOS 775. REPAIRED IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308141879Slat Track · crackedLT WING FIXED L/E AT NR 18 SLAT TRACK CUTOUT FOUND CRACKED AT XOS 1116.032. REPAIRED IAW EA NR 1-5730-T0301989 REV A PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117.SDR FDEA201308141875Seat Track · corrodedMAIN DECK BS 1600, X=-8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1531 TO 1631 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 53. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308141873Access Panel · crackedRT WING LOWER SURFACE L/E REFUEL PANEL CUTOUT FOUND CRACKED AT FWD INBD CORNER AT XOS 602. REPAIRED IAW SRM 57-40-02, FIG. 202, REPAIR 7, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308131851Seat Track · corrodedMAIN DECK BS 750, X=8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 745 - 834 IAW SRM 53-00-52, FIG 201. REPAIR 1 REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308131849Seat Track · corrodedMAIN DECK BS 1080, X=8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1069 TO 1129 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116SDR FDEA201308131853Door Frame · crackedMAIN DECK R3 DOOR AFT FRAME LOWER CORNER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 116.SDR FDEA201308131852Panel · delaminatedRT WING NR 1 SPOILER PANEL UPPER SURFACE FOUND THREE LOCATIONS DELAMINATED. REPAIRED IAW EA 1-5750-T0302163, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308131850Door Frame · crackedMAIN DECK R3 DOOR FORWARD FRAME LOWER CORNER WEB FOUND ONE CRACK. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201308131848Trunnion · crackedNLG LT TRUNNION FITTING FOUND CRACKED AT STATION Y=595. REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305151004Coalescer Bag · dirtyIN HIGH HUMIDITY CONDITIONS, APPROACHING GATE, COCKPIT FILLED WITH VISIBLE MOISTURE AND GOT MOMENTARY CABIN AIR SMOKE LIGHT AND WARNINGS. (NR 2 ENG WAS SHUTDOWN). R & R THE NR 1 WATER SEPARATOR COALESCER ASSY IAW AMM 21-54-05-01. OPS TEST NORMAL IAW AMM 21SDR FDEA201301250184Control Unit · burnedCONTROL UNIT REMOVED FROM ACFT DUE TO THE PUNGENT ELECTRICAL ODOR EMANATING FROM IT. INSTALLED ABSCU. OPS TEST NORMAL, REF MM 32-48-01-4.SDR FDEA201212064257Structure · damagedLEFT WINGLET DAMAGED & AFT LIGHT ASSY. WINGLET REPLACED & ACFT RETURNED TO SERVICE.SDR FDEA201203231086Battery Pack · inoperativeL1 DOOR PRESS TO TEST SWITCH FOR EVACUATION SLIDE BOTTLE PRESSURE CHECK, INOPERATIVE. FOUND NO POWER BEFORE SWITCH. R & R BATTERIES, PERFORMED TEST, LIGHT COMES ON IAW MM 25-61-15-4. OPS CHECKED OK.SDR FDEA201109073740Spar · crackedVERTICAL STABILIZER LEFT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201109073739Spar · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201109073738Seat Track · corrodedMAIN DECK CARGO COMPARTMENT - WHILE CARRYING INSPECTION AS PER WORKCARD ITEM 1, FOUND SEAT TRACK AT STA.5-0, X=-27.5 WITH CORROSION ON CHANNEL. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA. 5-0 TO STA. 5-43 X= -27.5 AS PER SRM 53-00-52 FIG. 201 RSDR FDEA201109023632Seat Track · corrodedMAIN DECK CARGO COMPARTMENT WHILE CARRYING OUT INSPECTION IAW WORKCARD ITEM 2, FOUND SEAT TRACK AT STA 6-10, X= 8.5 WITH CORROSION ON THE CHANNEL SURFACE. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV.47 REPAIR CLASSIFSDR FDEA201108313597Vane · delaminatedLEFT INBD VANE LOWER SURFACE FOUND DELAMINATED. VANE ASSY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV.70. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV. 70. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV.112.SDR FDEA201108313596Vane · delaminatedRT INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. VANE ASSY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV 70.0. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV.70.0. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.SDR FDEA201108313595Skin · crackedRIGHT WING SLAT NR 14 TRACK CUT OUT CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02 REV 47 FIG.201 REPAIR 7. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.SDR FDEA201012154688Shoulder Belt · malfunctionedCAPTS LT SHOULDER HARNESS WILL NOT RELEASE. PERFORMED OPS OF CAPT'S SHOULDER HARNESS IAW AMM 25-11-04-4-0. NO DEFECTS NOTED AT THIS TIME. NO HISTORY IN LAST 30 DAYS. (CLOSED)
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