N624FE

Service difficulty reports · 311

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 = 'N624FE' 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 FDEA201311062702Skin · crackedRT WING L/E LOWER SURFACE AT NR 14, SLAT TRACK CUTOUT FOUND CRACKED WS XOS 892.5. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201311062701Frame · dentedBS 1721, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201311062700Frame · dentedBS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201311062699Frame · dentedBS 1641, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201311062697Frame · dentedBS 1741, LONGERON 12L FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201311062696Frame · dentedBS 1681, LONGERON 12L FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201311062695Skin · crackedRIGHT WING L/E DROOP UPPER SURFACE SKIN FOUND CRACKED AT XDLE 324. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Nov 6, 2013 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201311042678Intake · delaminatedNR 1 ENGINE INLET COWL INNER BARREL FOUND DELAMINATION AT 5 TO 7 O'CLOCK POSITION. REMOVED AND REPLACED IAW AMM 71-11-01-4-2 REVISION 76.2. CARRIED OUT ADJUSTMENT IAW AMM 71-12-01-800-868 REVISION 76.2. FOUND SATISFACTORY. FUNCTIONAL TEST IAW AMM 30-22-0Nov 4, 2013 · N624FE · Doug MD11F · Engine Air Intake SystemSDR FDEA201311042679Longeron · corrodedLONGERON 28R FOUND CORRODED BETWEEN BS 1249 AND 1289. LONGERON REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Nov 4, 2013 · N624FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201308211987Connector · failedRT EMERGENCY LIGHTS WILL NOT TEST. BATTERY 1 LOW ALERT, APPEARS WHEN TEST BUTTON IS HELD. R & R FWD EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-4. DURING FURTHER TROUBLESHOOTING FOUND LOOSE AND PUSHED BACK SOCKET "A2" AT RELAY R2-5700 RECEPTACLAug 21, 2013 · N624FE · Doug MD11F · Emergency LightingSDR FDEA201306181333O-Ring · crackedTWENTY MINUTES AFTER TAKE OFF, LEVEL 1 "HYD 3 ELEV OFF" CHECKED QRH. ALSO NOTED A STEADY REDUCTION IN HYD 3 QTY, RETURNED TO DEPARTURE. ENROUTE, LEVEL 1"HYD 3 FAIL", COMPLIED WITH QRH AND LANDED. FOUND NR 3 HYD SYS PRESSURE TRANSDUCER (APTE-150-5000G) LOOSEJun 18, 2013 · N624FE · Doug MD11F · Hydraulic System, MainSDR FDEA201301210153Control Panel · shortedWHEN DOING FIRE TEST APU FIRE HANDLE WILL NOT TEST. R & R LAMPS, NO GOOD. NEED NEW PANEL. ORDERED APU AND FIRE TEST PANEL. PART UPDATE. REMOVED APU CONTROL PANEL REF M/M 49-04-01-4. C/B'S PULLED. WHILE TROUBLESHOOTING APU CONTROL PANEL, LIGHT ASSY SHOJan 21, 2013 · N624FE · Doug MD11F · Fire DetectionSDR FDEA201207082517Switch · out of positionL1 DOOR SLIDE REMOTE PRESSURE TEST LIGHT WOULD NOT ILLUMINATE. SWAPPED L1 AND R1 DOOR LIGHT MODULES. MODULE IN R1 ILLUMINATED PROPERLY. SWAPPED BACK MODULES. FOUND BASE OF LAMP SWITCH LOOSE OUT OF POSITION,REINSTALLED & SECURED SWITCH BASE AND PERFORMEDJul 8, 2012 · N624FE · Doug MD11F · Emergency EquipmentSDR FDEA201207052486Switch · looseL1 SLIDE REMOTE PRESSURE INDICATOR ASSY INOPERATIVE. TROUBLESHOOTING FOUND BASE OF LAMP SWITCH LOOSE OUT OF POSITION,REINSTALLED & SECURED SWITCH BASE AND PERFORMED. OPS TEST SATIS, IAW MM 25-61-04-5.Jul 5, 2012 · N624FE · Doug MD11F · Escape SlideSDR FDEA201204121381Pseu · failedON APPROACH, LANDING GEAR DID NOT EXTEND. HAD 4 RED LIGHTS AND GEAR WARNING HORN. EXECUTED GO AROUND. RAN GEAR UNSAFE CHECKLIST. SELECTED GEAR HANDLE DOWN AND GEAR EXTENDED NORMALLY. ACCOMPLISHED BITE OF PSEU. REF FIM 32-30-05-01/31-71 HAD NUMEROUS GEAR Apr 12, 2012 · N624FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201111235010Spar · misrepairedVERTICAL STABILIZER REAR SPAR MISREPAIRED. REPAIRED IAW EA1-5530-155843 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 113.Nov 23, 2011 · N624FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201111114875Skin · misrepairedFUSELAGE SKIN AT STA Y=535 TO Y=555 , L-47-48L MISREPAIRED. CARRIED OUT REPAIRED IAW EA 1-5310-155836. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 11, 2011 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201111114876Bulkhead · misrepairedLOWER FWD CARGO BAY AFT PRESSURE BULKHEAD BS 595, RT LOWER SIDE X-45 MISREPAIRED. REPAIR CARRIED OUT AS PER EA 1-5310-150396. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 11, 2011 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201111094840Skin · misrepairedLT WING DROOP L/E INBD EDGE MISREPAIRED. REPAIRED IAW EA 1-5740-155839. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 113.Nov 9, 2011 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201111094836Skin · misrepairedLT WING L/E XORS 1065, MISREPAIRED. REPAIRED AS PER EA 1-5740-155840. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 113.Nov 9, 2011 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201111094834Rib · cutON REMOVAL OF NR 2 SLAT INNER SKIN, FOUND RIB HAS DEEP CUT. DAMAGED RIB REMOVED IAW SRM 51-31-01 REV 47. DRILLED NEW RIB AND INSTALLED IAW SRM 51-31-01 REV 47 AND SRM 51-33-01 REV 47 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 9, 2011 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA201111044747Skin · misrepairedRT WING L/E NR 2 SLAT, OTBD INNER SKIN MISREPAIRED. CARRIED OUT REPAIR IAW EA EI-5750-150400. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 4, 2011 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA201111044746Skin · misrepairedRT WING L/E NR 2 SLAT SKIN MISREPAIRED. CARRIED OUT REPAIR IAW EA EI-5750-150400. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 4, 2011 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA201111034736Skin · misrepairedFUSELAGE SKIN BS 1887-1902, L40-45 L MISREPAIRED. REPAIRED AS PER SRM 53-00-01 FIG 201 REVISION 47 REPAIR 1.Nov 3, 2011 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201111034734Skin · damagedFWD CARGO DOOR CUTOUT AFT FRAME FOUND DAMGED AT BS 999, L40R. REPAIRED IAW SRM 53-00-15 FIG.202 REPAIR 8 REV.47 & EO E1-5100-7-5001A5 PT1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 113.Nov 3, 2011 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201111034735Skin · misrepairedSKIN STA.1541, LONGERON 38L MISRPAIRED. CARRIED OUT REPAIR IAW EA 1-5310-155837. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 113.Nov 3, 2011 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201111024721Frame · dentedFRAME BS 1701, L12-13L FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 FIGURE 201, REPAIR 2, REVISION 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 113.Nov 2, 2011 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201111024720Vane · delaminatedLT WING OTBD FLAP VANE TOP SURFACE FOUND DELAMINATED. VANE R & R IAW AMM 27-50-32-4, REVISION 70.1. FLAP VANE ADJUSTED AND TEST CARRIED OUT IAW AMM 27-50-32-5, REVISION 70.1. FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 2, 2011 · N624FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201111014714Skin · crackedLT WING NR 8 SLAT, INNER SURFACE FOUND CRACKED AT FASTENER HOLE. CARRIED OUT REPAIR IAW SRM 57-40-01, FIG 201, REPAIR 3, REVISION 47. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 113.Nov 1, 2011 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA201106102205Door · malfunctionedDURING PRE-FLIGHT CHECK FOUND RT ENTRY DOOR "DOOR DISARM" LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 52-10-03-03, CATEGORY: B EXPIRATION: 13JUN11. REPLACED LAMP AND SECURED LT ASSY PER SMP. OPERATIONAL TESTED PER MM 52-10-01-2-0, SATISFACTORY. CLEAREDJun 10, 2011 · N624FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201005171558Engine · surgesNR 1 ENGINE SURGE - MODERATE VIBRATION ACCOMPLANIED BY LOW N1 AND OIL PRESSURE INDICATING BELOW REDLINE AND "ENG 1 OIL PRESSURE LO" ALERT SHUTDOWN NR 1 ENGINE USING ENGINE SHUTDOWN INFLIGHT PROCEDURE. R & R NR 1 ENGINE IAW W/C 71T0901-PW. OP CHECK AND LEAK CMay 17, 2010 · N624FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201004061087Landing Gear · malfunctionedAFTER TAKEOFF GEAR WOULD NOT RETRACT. COMPLIED WITH QRH/CHECKLIST AND STILL DID NOT RETRACT. LANDING GEAR HANDLE WOULD NOT MOVE FROM DOWN POSITION. RETURNED MEM AND LANDED WITHOUT INCIDENT AT INBD INSP NOTICE VALVE LEAKING, BLED AND LEAKED CHECK TRIM CYL RELApr 6, 2010 · N624FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA200912094388Frame · chafedCABIN STA 535, LONGERON 19L FRAME FOUND WITH CHAFED AS MARKED. REPAIR CARRIED OUT ON CABIN STA 535, LONGERON 19L, FRAME IAW EA 1-5310-135679. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.Dec 9, 2009 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200912094387Frame · chafedCABIN STA535, LONGERON 24L FRAME FOUND WITH CHAFED AS MARKED. REPAIR CARRIED OUT ON CABIN STA 535 LONGERON 24L FRAME IAW EA1-5310-135679. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.Dec 9, 2009 · N624FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200912044359Seat Track · corrodedMAIN DECK, CARGO COMPT STA 1341-1361 X=75.5 SEAT TRACK FOUND CORRODED. MAIN DECK CARGO COMPT CORRODED SEAT TRACK AT STA 1341 TO STA 1361 X=-75.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1279 TO STA 1391 X=-75.5 IAW SRM 53-00-52, FIG 201 REPAIR Dec 4, 2009 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912034353Skin · cracked(1) EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=700. REPAIR CARRIED OUT AT RT WING LWR SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS=690 AND STA XORS=700 IAW EA 1-5710-135677. REPDec 3, 2009 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200912034337Longeron · crackedCRACK INDICATION FOUND APPROX 0.5" IN LENGTH AT CABIN STA. 5-123, LONGERON -4R FWD SECTION EDGE AS MARKED. REPAIR CARRIED OUT AT CABIN STA 5-123 LONGERON 4R FWD SECTION IAW SRM 53-00-05, FIG 202, REPAIR 1 REV 42, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, Dec 3, 2009 · N624FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200912034336Longeron · crackedCRACKED INDICATION FOUND APPROX 2" IN LENGTH DURING X-RAY INSP AT CABIN STA 5-123, LONGERON 2L AFT SECTION EDGE AS MARKED. AT CABIN STA5-123 CRACKED LONGERON-2L AFT SECTION EDGE REPAIR IAW SRM 53-00-05, FIG 202, REPAIR REV 42. REPAIR CLASSIFIED AS MAJOR IAW Dec 3, 2009 · N624FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200912024323Skin · dentedFUSELAGE EXTERIOR - RT APPROX STA 1019 L-42 FOUND 01 EA LOCATION DENT AS MARKED. DENT AT FUSELAGE EXTERIOR RT APPROX STA 1019 L-24 REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 6, REV 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 108.Dec 2, 2009 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200911304229Skin · damagedRT WING L/E SLAT NR 4 LWR EDGE FOUND TRIM OFF AS MARKED. REPAIR CARRIED OUT AT RT WING L/E SLAT NR 4 LWR EDGE TRIMMED OFF AREA IAW EA 1-5750-135674. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 108.Nov 30, 2009 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA200911304227Structure · damagedRT WING L/E SLAT NR4 T/E TRIM-OFF AS MARKED. REPAIR CARRIED OUT RT WING L/E SLAT NR 4 T/E TRIMMED OFF AREA IAW EA 1-5750-135674. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 108.Nov 30, 2009 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA200911304225Rib · crackedRT WING L/E SLAT TRACK NR 16 INBD RIB SUSPECT CRACK AS MARKED. RT WING L/E SLAT TRACK NR 16 RIB INBD REMOVED AND NEW RIB NR 16 INSTALLED IAW SRM 51- 33-01 REV 42. RT WING NR 8 SLAT CABLE ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-00-05, REV 64 FOUND SATNov 30, 2009 · N624FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA200911304223Slat Track · crackedLT WING L/E SLAT TRACK NR16 SUSPECT CRACK AS MARKED. LT WING L/E SLAT TRACK NR 16 INBD RIB REMOVED AND NEW RIB NR 16 INSTALLED IAW SRM 51-33-01 REV 42. NR 8 SLAT CABLES ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-30-5, REV 64 FOUND SATISFACTORY. OPS CHECK ONov 30, 2009 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA200911304221Skin · misrepairedRT WING L/E SLAT NR 4 INNER SURFACE BETWEEN SLAT TRACK NR 9 AND NR 10 FOUND (1 EA) UNAPPROVED REPAIR PATCH AS MARKED. REPAIR CARRIED OUT RT WING L/E SLAT NR 4 INNER SURFACE BETWEEN SLAT TRACK NR 9 AND NR 10 IAW SRM 57-40-01 FIG 201, REV 42. REPAIR CLASSIFIED Nov 30, 2009 · N624FE · Doug MD11F · Leading Edge DevicesSDR FDEA200906162127Hydraulic System · leakingCREW REPORTED LOOSING FLUID FROM HYD SYS, NR 1,NR 2 AND NR 3. RAN ALL 3 ENGINES IAW JRH AND BLEED HYD SYS IAW AMM 29-03-00-2 BLEEDING HYD SYS. PERFORMED HYD SYS TEST OPS CHECKED ALL FLT CONTROLS AND BRAKES WITH VERY LITTLE FLUCTUATION IN QUANTITY (SYS 1; 6.9 Jun 16, 2009 · N624FE · Doug MD11F · Hydraulic System, MainSDR 08FDEA02202Frame · corrodedCABIN RT TRANSVERSE FRAME AT STA 1681 FOUND DENTED AT LONGERON 12.Jun 9, 2008 · N624FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA02201Frame · corrodedCABIN RT TRANSVERSE FRAME AT STA 1661 FOUND DENTED AT LONGERON 12.Jun 9, 2008 · N624FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA02084Skin · corrodedUPON AFT FUSELAGE RT LOWER WASTE VACUUM EXHAUST PLUG REMOVED AT STA 1959 BETWEEN LONGERON 39R TO 40R, FOUND EXISTING DOUBLER CORRODED. AFT FUSELAGE RT LOWER, AT STA 1959 BETWEEN LONGERON 39R TO 40R REPAIR CARRIED OUT AS PER SRM 53-20-00 VOL 1 FIG 2. REPAIRJun 2, 2008 · N624FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 08FDEA02082Skin · crackedCRACK FOUND QUANTITY 13 FASTENER HOLES ON RT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT-OUT BETWEEN STA XORS=683.4 AND XORS=713.6 RT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT-OUT BETWEEN STA XORS=683.4 AND XORS=713.6 13 FASTENER HOLES CRACKED. ARJun 2, 2008 · N624FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA02081Skin · crackedCRACK FOUND QUANTITY 3 FASTENER HOLES ON LT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND XORS=713.6. LT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND XORS=713.6 03 FASTENER HOLES CRACKED. AREAJun 2, 2008 · N624FE · Doug MD11F · Wing, Plate/Skin
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