N592FE
Service difficulty reports · 362
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 = 'N592FE' 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 = 'N592FE' 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 FDEA201809252694Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-73333C PT 3 STEP 1. EO 1-5750-7-5002 RTSDR FDEA201809252693Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACH OUTBD LUG HOLE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2SDR FDEA201809252692Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD LUG HOLE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 SDR FDEA201809252691Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE FOUND CORROSION. NR 7 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2SDR FDEA201809252690Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE FOUND CORROSION. BOLT HOLE NR 7 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS SDR FDEA201809252689Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44SDR FDEA201809252688Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44SDR FDEA201809252687Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE BORE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2B. EO SDR FDEA201809252686Hinge Bracket · corrodedLEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STSDR FDEA201809252685Hinge Bracket · corrodedLEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STESDR FDEA201809252684Hinge Bracket · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT O/B HOLE BORE( #7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHSDR FDEA201809252683Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT I/B HOLE BORE (#7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHINSDR FDEA201809252682Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) BARREL NUT HOLE SURFACE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) BARREL NUT HOLE SURFACE CORROSION REWORKED AS PER MD1 CMM57-44-08. NEW REPAIR SHIM FABRICATED AND INSTALLED PER MD11 CMM57-4SDR FDEA201809252681Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) PIVOT HOLE BORE FOUND CORROSION. LH WING ( WING SIDE ) O/B FLAP I/B HINGE PIVOT HOLE BORE #4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM 57-44-08. NEW OVERSIZED BUSHING FABRICATED BY MACHINING ASDR FDEA201809252706Skin · puncturedRIGHT WING INBD FLAP VANE LOWER SURFACE FOUND PUNCTURED AT XIFH 193.875. SKIN REPAIR CARRIED OUT METAL BONDED WITH FILLER AND DOUBLER AS PER SRM 51-71-00 PARAGRAPH 20 AN EA 1-5750-T0342536 PART 1. REPAIR ON RT INBD FLAP VANE ARC2557-54 LOWER SKIN. REPAIR CLASSSDR FDEA201809212645Floor Support · corrodedFWD CABIN, UPON LAVATORY MODULE REMOVED FOR FLOORBEAM ATTACH ANGLE REPAIR ACCESS, FOUND RT FLOOR SUPPORT AT STA 413, X= -25 CORROSION. FLOOR SUPPORT CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. FLOOR SUPPORT REMOVED AND REPLACSDR FDEA201809212644Doubler · crackedRIGHT WING LEADING EDGE COMPT LOWER SURFACE PANEL CUTOUT FWD EDGE DOUBLER AT STA XOS 604 FOUND CRACK. CRACKED DOUBLER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DRAWING ARB2933 REVISION AJ. INSTALLED NEW DOUBLER AT RIGHT WING LEADING EDGE COSDR FDEA201809182574Hinge · corrodedLEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT OUTBD LUG HOLE FOUND CORROSION. HOLE A AND B REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MSDR FDEA201809182573Hinge · corrodedLEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFSDR FDEA201809182572Hinge · corrodedRIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED OUTBD LUG HOLE FOUND CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2BSDR FDEA201809182571Hinge · corrodedRIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2B. RSDR FDEA201809182579Intercostal · crackedVERTICAL STAB REAR CENTER SPAR TO REAR SPAR INTERCOSTAL STA 2164, RIGHT SIDE AFT END FOUND CRACKED. INTERCOSTAL REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 204 REPAIR 7 AND EA 1-5530-T0342479 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091872559Stringer · crackedUPPER AUX FUEL TANK STRINGER NR 47 FROM XCW=50 TO XCW=57 FOUND CRACK. UPPER AUX FUEL TANK STRINGER REPAIRED AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091872558Stringer · crackedUPPER AUX FUEL TANK STRINGER 52 FROM XCW=50 TO XCW=56 FOUND CRACK. UPPER AUX FUEL TANK STRINGER 52 FROM XCW=35.5 TO XCW=59.5 AREA REPAIRED AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142539Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X=-2 FOUND CORROSION ON FLANGE AT STA 1962 AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1962, X= -2 REPAIRED AS PER SRM 53-00-52-2R FISDR FDEA201809142536Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X= 2 FOUND CORROSION ON FLANGE AT STA 1910 AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1910, X= 2 REPAIRED AS PER SRM 53-00-52-2R FIG 20SDR FDEA201809142542Spar · crackedHFEC INSPECTION CARRIED OUT ON LT REAR SPAR CAP FORWARD FLANGE LOCATED AT THE UPPER SECTION OF NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER , STA Y=2164 AND FOUND CRACK APPROX. 1.5 " LENGTH. SPAR CAP FORWARD FLANGE TRIMMED AS PER SRM 55-30-02-2R FIGURE 201SDR FDEA201809142541Spar · crackedHFEC INSPECTION CARRIED OUT ON RT REAR SPAR CAP FORWARD FLANGE LOCATED AT THE UPPER SECTION OF NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER, STA 2164 AND FOUND CRACK APPROX 0.2" LENGTH. SPAR CAP FORWARD FLANGE TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAISDR FDEA201809142537Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X= 25 FOUND CORROSION. FLOOR SUPPORT CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICASDR FDEA201809142540Web · crackedFLIGHT COMPARTMENT RT OBSERVER SEAT BASE CUTOUT WEB FOUND CRACK, AT STA 360, X=- 8. CRACKED WEB REPAIRED AS PER SRM 53-10-51-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142538Seat Track · corrodedMAIN DECK AFT LT CURVE SEAT TRACK AT STA 1940 TO STA 2007, X= 107 FOUND CORROSION. SEAT TRACK CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED LT CURVED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA SDR FDEA201809142535Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X= 56 FOUND CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142534Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X=-56 FOUND CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142533Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X=-25 FOUND CRACKED. MAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X=-25 CRACKED FLANGE LOBE REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142531Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION AT LT WING LEADING EDGE SKIN ADJACENT TO CUTOUTS AND ACCESS DOORS, FOUND 1EA CRACK INDICATION AT CORNER NR 13, APPROXIMATE 0.2" IN LENGTH. REPAIR CARRIED OUT AT LT WING FIXED LEADING EDGE AT CORNER NR 13, AT STA XOS 65SDR FDEA201809142530Doubler · crackedLT WING LEADING EDGE CAVITY AT STA XOS 744 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE CAVITY AT STA XOS 744 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142529Doubler · crackedRT WING LEADING EDGE CAVITY AT STA XOS 587 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY AT STA XOS 587 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142528Splice · not reportedRT WING, DURING ACCOMPLISHMENT OF EA 1-5710-T0329981 PART 2 FOUND UNABLE TO COMPLY WITH STEP 3 WORK INSTRUCTIONS AS P/N ARB3143-2 NOT AVAILABLE FOR REPLACEMENT EXISTING SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ARB3143 REVISIOSDR FDEA201809142527Splice · not reportedLT WING, DURING ACCOMPLISHMENT OF EA 1-5710-T0329978 PART 2 FOUND UNABLE TO COMPLY WITH STEP 3 WORK INSTRUCTIONS AS P/N ARB3143-1 NOT AVAILABLE FOR REPLACEMENT EXISTING SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ARB3143 REVISIOSDR FDEA201809142532Skin · chafedRT WING DROOP LEADING EDGE FOUND CHAFED, STA XDLE 309. REPAIR CARRIED OUT AT RT WING DROOP ASSEMBLY LEADING EDGE AT INBOARD STA XDLE 309 AS PER SRM 57-40--01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432518Former · crackedRIGHT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT RIGHT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PSDR FDEA2018091432517Frame · damagedMAIN DECK RT FRAME AT STA 535 LONGERON 19R FOUND DAMAGED. MAIN DECK DAMAGED RT FRAME AT STA 535 LONGERON 19R REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432516Frame · damagedMAIN DECK RT FRAME AT STA 535 LONGERON 24R FOUND DAMAGED. MAIN DECK DAMAGED RT FRAME AT STA 535 LONGERON 24R REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432515Angle · damagedMAIN DECK LT FRAME AT STA 535 LONGERON 24L FOUND EXISTING REPAIR ANGLE DAMAGED. REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432514Angle · damagedMAIN DECK LT FRAME AT STA 535 LONGERON 19L EXISTING REPAIR ANGLE DAMAGED MAIN DECK. REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432513Stiffener · crackedLEFT HAND WING LEADING EDGE FORMER/STIFFENER AT STA XOS 549 FOUND CRACKED. CRACKED FORMER(STIFFENER) REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2918 REVISION G. INSTALLED NEW FORMER (STIFFENER) AT LEFT HAND WING LEADING EDGE AT STASDR FDEA2018091432512Former · crackedLEFT HAND WING LEADING EDGE FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT LEFT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PER SRM 51SDR FDEA2018091432519Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 1229, X=-75.25 FOUND CORROSION MAIN DECK FLOOR. SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1169SDR FDEA2018091422469Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1541 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICSDR FDEA2018091422464Skin Panel · crackedEMPENNAGE LT SIDE LOWER VERTICAL STABILIZER IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN PANEL CRACKED. SKIN PANEL REPAIR CARRIED OUT AS PER EA 1-5530-T0342403 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Back to N592FE