N521FE
Service difficulty reports · 471
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 = 'N521FE' 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 = 'N521FE' 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 FDEA202108282133Hinge Bracket · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE (A AND B HOLE) REWORKED AND FOUND EXCEEDSDR FDEA202108282132Hinge Bracket · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE (F AND G HOLE) REWORKED AND FOUND EXCEED LSDR FDEA202108282131Hinge Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE (A AND B HOLE) REWORKED AND FOUND EXCEEDSDR FDEA202108282130Hinge Bracket · corrodedLEFT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP ASSEMBLY. OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE (F AND G HOLE) REWORKED AND FOUND EXCEED LSDR FDEA202108262100Skin · crackedCABIN - STATION 1250.75 TO STATION 1256.75 RIGHT 3 DOOR CUTOUT FORWARD UPPER JAMB WEB BOX FOUND CRACKED. CRACKED AT CABIN - STATION 1250.75 TO STATION 1256.75 RIGHT 3 DOOR CUTOUT FORWARD UPPER JAMB WEB BOX, STOP DRILL CARRIED OUT AT CRACK AREA AS PER SRM 5SDR FDEA202108262101Door Frame · crackedCABIN - STATION 1305.25 TO STATION 1315.42 RIGHT 3 DOOR CUTOUT AFT LOWER JAMB WEB BOX FOUND CRACKED.SDR FDEA202108252094Longeron · corrodedFUSELAGE - RIGHT HAND STATION 1289 OUTER SKIN PANEL LONGERON 28 RIGHT FOUND CORROSION. CORROSION AT FUSELAGE RIGHT HAND STATION 1289 OUTER SKIN PANEL LONGERON 28 RIGHT REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 SHEET 1. LONGERON 28 SDR FDEA201706251757Skin · delaminatedRIGHT WING OTBD FLAP TRAILING WEDGE TOP SURCFACE FOUND DELAMINATED BETWEEN XOF 622 & 628. REPAIRED IAW SRM 57-50-80, REPAIR 1, PARA 4A (1)A, AND EA 1-5750-333865, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706211733Seat Track · corrodedCABIN - RT STA 1199 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1199 X= -8.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CABIN - RT STA 1199 X= -8.5 DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLSDR FDEA201706211732Seat Track · corrodedCABIN - RT STA 1441 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1441 X= -8.5 SEAT TRACK CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 AND REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1431 TO STSDR FDEA201706211731Seat Track · corrodedCABIN - RT STA 5-43 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 5-43 X= -8.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CABIN - RT STA 5-43 X= -8.5 DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLSDR FDEA201706211730Seat Track · corrodedCABIN - RT STA 1551 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1551 X= -8.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CABIN RT STA 1551 X= -8.5 DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLASDR FDEA201706211724Seat Track · corrodedCABIN - RT STA 1531 X= -27.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1531 X= -27.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 (STA SDR FDEA201706191707Web · crackedR3 DOOR FWD DOOR FRAME LOWER WEB BOX BS 1250.75 - 1256.75, LONGERON 26 - 27R FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191706Web · crackedL3 DOOR FWD DOOR FRAME LOWER BOX BS 1250.75 - 1256.75, LONGERON 26 - 27L FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191705Door Frame · crackedL3 DOOR AFT FRAME LOWER WEB BOX BS 1305.25 - 1315.42, LONGERON 26 - 27L FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201706191704Frame · dentedBS 1701, LONGERON 12L EXISTING FRAME REPAIR FOUND DENTED. REPAIR REMOVED IAW SRM 51-33-01-0G, AND REPAIRED IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191703Web · crackedRIGHT OBSERVER`S SEAT BASE WEB FOUND CRACKED ON EXISTING REPAIR. WEB TRIMMED IAW 53-10-51-2R, FIG 201, REPAIR 1. REPAIR DOUBLER AND WEB FABRICATED AND INSTALLED IAW SRM 53-10-51-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191702Skin · crackedHFEC INSPECTION CARRIED OUT AT THE RT WING SLAT TRACK NR 9. CUTOUT AFT INBD CORNER AND FOUND CRACKED, 1/4 INCH IN LENGTH. REPAIRED IAW SRM 57-40-02-2R, FIGURE 201, REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191701Doubler · crackedRIGHT WING FIXED L/E LOWER ACCESS PANEL ATTACHMENT FOUND CRACKED XOS 549. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE DOUBLER WAS FABRICATED IAW DRAWING ARB2933, REVISION AJ. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191700Doubler · crackedRIGHT WING L/E INTERNAL SKIN SUPPORT BEADED DOUBLER FOUND CRACKED AT XOS 737. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191699Doubler · crackedLEFT WING FIXED L/E LOWER ACCESS PANEL ATTACHMENT FOUND CRACK AT XOS 602. REMOVED AND REPLACED IAW SRM 51-31-01-0G . DOUBLER FABRICATED IAW DRAWING ARB 2933, REVISION AJ. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100.SDR FDEA201706191698Doubler · crackedRIGHT WING FIXED L/E SKIN SUPPORT BEADED DOUBLER FOUND CRACKED AT XOS 642. REPAIRED IAW SRM 57-40 -02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201706191697Support · crackedRIGHT WING FIXED L/E INTERNAL SKIN SUPPORT BEADED DOUBLER FOUND CRACKED AT XOS 617. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611013790Indicator · unsecurePRE-FLT CHECK, FOUND R1 DOOR SLIDE REMOTE PRESSURE INDICATOR INOPERATIVE. REMOTE PRESSURE INDICATOR PROPERLY SECURED R1 LENS AND LAMP RETAINER, ADJ/TEST IS NORMAL WITH NO DEFECTS. IAW AMM 5-61-04-5.SDR FDEA201608273055Control Valve · leakingAT TOP OF DESCENT RECEIVED A LEVEL ONE HYD 3 ELEVATOR OFF ALERT. FLUID DECREASED TO 1.2 AT SHUTDOWN. USED NORMAL GEAR EXTENSION, NORMAL TAXI IN AND NORMAL HYDRAULIC TEMPERTURE OF 37 DEGREES C. FOUND O-RING EXTENDED OUT OF NR 3 STABILIZER TRIM CONTROL UPPER SDR FDEA201601090093Hydraulic System · lowON DEPARTURE FL320, HYD 1 FAIL ALERT 0 HYD QTY, 0 PRESS. SERVICED NR 1 HYD SYS IAW AMM 12-13-02-3. PRESSURIZED SYS WITH AUX PUMPS & OPERATED ALL ITEMS UNDER SYS 1, VERIFIED SYS 1 PRESS & FLUID QTY HELD. RAN NR 1 ENG IAW JRH & OPERATED ALL FLIGHT CONTROLS & SDR FDEA201511203728Wire · damagedDURING ACFT B CHECK, FOUND ACFT NOSE GEAR TAXI LIGHTS ON DIM. CYCLED GND SERVICE & ACFT POWER CONTROL SWITCHES. DUE TO SMOKE IN THE COCKPIT, TROUBLE SHOT WIRING TO STATION 464 RT SIDE LOWER, FEED THROUGH FROM FWD AVIONICS COMPARTMENT TO RT PACK BAY. WIRING SDR FDEA201507252382Skin · crackedUPPER AFT FUSELAGE CTR FRAME NEAR CANT BS 2069, HAS CRACK UNDER FRAME CLIP UPPER LT SKIN INTERNAL. REPAIRED CRACK IAW EA T 1-5330T0319026 PART 1.SDR FDEA201507192268Spar Cap · corrodedLEFT WING UPPER REAR SPAR CAP, FROM STATION XORS 486 - ORS 1042, 27 LOCATIONS ARE CORRODED ON UPPER SURFACE. ALL AREAS ARE IDENTIFIED 1 - 27. REMOVED CORROSION & TREATED AREA IAW SRM 51-21-01 & WC 57C1501. SEQ 439 WO 63971.SDR FDEA201507192267Spar · corrodedRIGHT WING UPPER SURFACE AFT SPAR AREA APPROX XORS 704, FWD OF NR 4 SPOILER, BULGE UNDER PANEL MARKED. REMOVED CORROSION IAW SRM 51-21-01 & EA 1-5710-T0318839.SDR FDEA201507162253Seat Track · corrodedMAIN DECK SEAT TRACK AT STATION 1537, RBL 8 HAS CORROSION. REPAIRED MAIN DECK SEAT TRACK AT STATION 1537, RBL 8 AS REQUIRED IAW SRM 53-00-52-2R.SDR FDEA201507162252Seat Track · corrodedMAIN DECK SEAT TRACK AT STATION 1557, RBL 8 FLOOR TRACK CORRODED. REPAIRED MAIN DECK SEAT TRACK AT STATION 1557, RBL 8 AS REQUIRED IAW SRM 53-00-52-2R.SDR FDEA201507162251Doubler · crackedRIGHT WING LE INTERNAL, PILLOW DOUBLER HAS A CRACK EMANATING FROM FASTENER AT XORS 565. TRIMMED OUT CRACK DOUBLER, FABRICATED 1 FILLER, -2 DOUBLER & -3 ANGLES IAW SRM 57-40-02. TREATED & PRIMED 1 FILLER, -2 DOUBLER & -3 ANGLES IAW SRM 51-21-01, OK TO INSTALLSDR FDEA201507162249Skin · corrodedRIGHT FUSELAGE EXTERIOR, CORROSION ON SKIN AROUND FASTENER, APPROX STATION 2033 BETWEEN LONGERON 38 - 39. REPAIR FUSELAGE SKIN IAW SRM 53-00-01 REPAIR 8.SDR FDEA201507152236Trunnion Pin · corrodedUPON ARRIVAL, LT MLG FWD TRUNNION FWD LOWER ZERK FITTING WOULD NOT TAKE GREASE. ATTEMPTS WERE MADE TO CLEAR GREASE PASSAGE WITH NO HELP. GEAR WAS SUPPORTED, ATTEMPTED TO REMOVE PIN WITH HYD INTERPACK REMOVAL TOOL, NO HELP. COMPLIED WITH EA 1-5710-T0318696SDR FDEA201507122202Skin · corrodedLEFT WING UPPER SURFACE XORS 197, STRINGER 16 CORROSION AROUND MULTIPLE FASTENER HEADS. REMOVED CORROSION & TREATED AREA IAW EA 1-5720-T0318742.SDR FDEA201507122201Angle · corrodedAFT CARGO COMPARTMENT, STATION 1841 WEB CAP ANGLE HAS CORROSION AROUND FASTENER HOLES & UNDER NUTPLATES. INSTALLED NEW WEB CAP ANGLE IAW DWG AGA7170.SDR FDEA201507082170Doubler · crackedRIGHT WING LE FIXED SKIN, XORS 683, CRACKED DOUBLER. R & R DOUBLER IAW DWG ARB3954.SDR FDEA201507082168Doubler · crackedRIGHT WING LE INTERNAL, PILLOW DOUBLER HAS SEVERAL CRACKS AT XORS 683. REPAIRED DOUBLER IAW SRM 57-40-02 FIG 203 REPAIR 15.SDR FDEA201507082167Support Angle · crackedRIGHT WING LE INTERNAL, FORMER SUPPORT ANGLE CRACKED AT XORS 683. REPAIRED SUPPORT ANGLE IAW SRM 57-40-03 FIG 201 REPAIR 2.SDR FDEA201507082166Doubler · crackedRIGHT WING LE INTERNAL, PILLOW DOUBLER HAS CRACKS EMANATING FROM FASTENER AT XORS 540. VERIFIED BY NDT HFEC. REPAIRED DOUBLER IAW SRM 57-40-02 FIG 203 REPAIR 15.SDR FDEA201409072503Control Panel · malfunctionedAUTOPILOT NR 1 & 2, AUTO THROTTLES WOULD NOT ENGAGE. NO FLIGHT FAULTS LOGGED FOR THE FCC1 OR FCC2. CHECKING THE FCC1 & FCC2 PREVIOUS FAULTS. BOTH FCC SHOW LEG 1 NO FAULTS, OR FLY INTO IND. LEG 2 FAULTS WERE ELEV FAULT, WHICH EWR RESOLVED. THEN NEXT FAULT SDR FDEA201408272321Skin · crackedRIGHT WING HAS EVIDENCE OF POSSIBLE CRACK IN ACFT SKIN AT SLAT TRACK NR 14. REMOVED DAMAGE, FABRICATED REPAIR, INSTALLED REPAIR IAW SRM 51-40-02.SDR FDEA201408272320Skin · crackedLEFT WING HAS EVIDENCE OF POSSIBLE CRACK IN ACFT SKIN AT SLAT TRACK NR 14. COMPLETED REPAIR IAW SRM 57-40-02.SDR FDEA201405231147Skin · crackedPOSSIBLE CRACK ON RT WING LOWER SLAT TRACK PANEL BETWEEN NR 5 & 6 SLAT, MARKED WITH TAPE. INSPECTION WILL VERIFY IF IT IS CRACKED. INSTALLED DOUBLER & FILLER IAW SRM 57-40-02.SDR FDEA201405231146Skin · crackedRIGHT WING, SKIN AT PRESS REFUEL DOOR, INNER FWD CORNER HAS SUSPECTED CRACK GOING FROM CORNER TO RIVET. INSTALLED REPAIR DOUBLER IAW SRM 57-40-02 REPAIR 7 FIGURE 202 & EA 1-5730-T0308359 PART 1.SDR FDEA201311062706Door · out of adjustR1 DOOR BINDS WHEN CLOSING. PERFORMED ADJUSTMENT AND TEST FOR R1 DOOR IAW AMM 52-11-02-5. NO DEFECTS NOTED. ACFT OK FOR SERVICE.SDR FDEA201307301698Skin · damagedNOSE SKIN DAMAGED AT JACK POINT BS 595-625 LONGERON 36 - 48R. REPAIRED IAW SRM 53-20-01. REPAIR 2, REV 53.SDR FDEA201307301697Rib · crackedAFTER REMOVAL OF EXISTING REPAIR, FOUND L/E RIB DAMAGED AT ZFS =596.972. DAMAGED RIB REMOVED IAW SRM 51-35-01, REV 53. NEW RIB FABRICATED IAW DWG AMC7130, REV E. RIB INSTALLED IAW SRM 51-35-01, REV 53. REPAIR CLASSIFIED MAJOR GMM 6-2-100, REV 116.
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