N528FE

Service difficulty reports · 229

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 = 'N528FE' 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 FDEA201507272395Support · corrodedRIGHT OTBD FLAP, INBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-04. REPAIRED IAW EA 1-5750-T0319122 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 27, 2015 · N528FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201507242375Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BARREL NUTS HOLE SURFACE CORRODED. FOUND WITHIN LIMITS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242374Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. REPAIRED IAW EA 1-5750-T0319119 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242373Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT INBD HOLE BORE CORRODED. REPAIRED IAW EA 1-5750-T0319119 PART 1. REPAIR CLASSIFIED AS MINOR GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242372Stringer · crackedRIGHT WING FIXED LE CAVITY XOS 667 UPPER STRINGER FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 57-57-40-03-2R FIGURE 2 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Wing, Longeron/StringerSDR FDEA201507242371Stringer · crackedLEFT WING XOS 667 FIXED LE UPPER STRINGER FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-03-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Wing, Longeron/StringerSDR FDEA201507242370Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT INBD HOLE SURFACE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0319116 A PT 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242369Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0319116 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242368Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, LOWER MOUNT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0319116 PT 1. REPAIR CLASSIFIED AS GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242367Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BARREL NUTS HOLE SURFACE CORRODED. CORROSION REMOVED IAW CMM 57-44-08. FOUND WITHIN LIMITS IAW DWG & CMM. A REPAIR SHIM WAS FABRICATED & INSTALLED IAW CMM 57-44-08.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242366Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BARREL NUTS HOLE SURFACE CORRODED. REMOVED CORROSION IAW CMM 57-44-09. FOUND WITHIN LIMITS BASED THE DIFFERENCE BETWEEN DWG LIMITS & CMM. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507242365Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE LOWER BARREL NUT HOLE BORE CORRODED. REWORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR ACCOMPLISHED IAW EA 1-5750-T0319117 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 24, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507222298Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 24L FRAME, EXISTING REPAIR FOUND CHAFED. EXISTING REPAIR R & R WITH NEW REPAIR IAW SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 22, 2015 · N528FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201507222297Frame · dentedCABIN MAIN DECK CARGO BAY BS 535, LONGERON 19L FRAME DENTED. REPAIRED IAW SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 22, 2015 · N528FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201507222296Frame · dentedMAIN DECK CARGO BAY BS 1741, LONGERON 12R FRAME DENTED. REPAIRED IAW SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 22, 2015 · N528FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201507222295Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE CORRODED. REWORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR ACCOMPLISHED IAW EA 1-5750-T0319115 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 22, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507222294Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT HOLE SURFACE CORRODED. WORKED IAW CMM 57-44-09. WITHIN LIMITS BASED ON THE DIFFERENCE BETWEEN DWG LIMITS & CMM. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 22, 2015 · N528FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201507172254Switch · malfunctionedCABIN DOOR FWD LT, DISARM LIGHT WOULD NOT TEST OR COME ON WHEN DOOR WAS IN SAFE POSITION. OUTSIDE HANDLE WAS NOT ALL THE WAY OUT. UNABLE TO GET ELEC SWITCH TO OPEN DOOR. FINALLY OUTSIDE RAMP MANUALLY RAISED HANDLE, THE ELEC SWITCH OUTSIDE WORKED. R & R LT Jul 17, 2015 · N528FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201507082186Light · damagedL1 EMERGENCY LIGHT DAMAGED WHEN SLIDING CEILING PANEL HIT DOOR. REPAIR CARRIED OUT IAW AMM 25-00-00-8.Jul 8, 2015 · N528FE · Doug MD11F · Emergency LightingSDR FDEA201406211505Fmu · failedREJECTED TAKEOFF, ATTEMPTED TO PUSH UP NR 2 ENGINE TO TAKEOFF POWER & COULD NOT GET REQUIRED POWER DURING TAKEOFF ROLL. HIGHEST POWER WAS 1.3 EPR. TAXIED BACK TO RAMP. REMOVED AND REPLACED NR 2 FMU, PUMP, AND PB SENSE LINE IAW AMM 73-21-01-4-2. PERFORMED Jun 21, 2014 · N528FE · Doug MD11F · Fuel Controlling SystemSDR FDEA201406021284Compensator · malfunctionedDURING CLIMB OUT, RECEIVED RUDDER STANDBY UPPER OFF, THREE TIMES. INTERROGATED, HSC UPPER RUDDER STANDBY POWER FAULT NOTED. R & R FWD COMPENSATOR LOW LEVEL SWITCH IAW AMM 27-26-31-4. R & R AFT LOW LEVEL COMPENSATOR SWITCH TO STEP 2 D CONNECTER WILL NOT LOCKJun 2, 2014 · N528FE · Doug MD11F · Rudder Control SystemSDR FDEA201404280868Control Valve · inoperativeAFTER TAKE OFF, RECEIVED A NR 3 PACK FLOW DISAGREE. AIR SYS WAS IN AUTO. SOON AFTER, RECEIVED A NR 2 AIR SYS, AIR SYS 1 OFF & AVIONICS FAN OVERRIDE. BLEED 1 & 2 WERE BOTH CLOSED. SWITCHED CONTROLLERS, BACK TO AUTO, PROBLEM REAPPEARED. LEAVING NR 3 BLEEApr 28, 2014 · N528FE · Doug MD11F · Cabin Cooling SystemSDR FDEA201312273045B-Nut · looseLEVEL 1 ANTI-ICE SENSOR FAILED ONE AND A HALF HOURS INTO FLIGHT AT FL 370. NR 1 INTERMEDIATE PRESSURE SENSORS PI1 & PI1B ARE FAULTED & READINGS ARE OUT IN PSC 1 & 2 SENSOR READOUTS. PRESSURE TESTED PI LINES & FOUND B-NUT LOOSE AT UNION BETWEEN PRESSURE PILODec 27, 2013 · N528FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA201311142822Light · pulledEMERGENCY LIGHT PANEL PULLED OUT OF THE NEXT INBD PANEL. HAD MOUNT HOLES RIPPED OUT. REPLACED R1 DOOR PASSENGER SLIDING CEILING PANEL PER AMM 25-23-23-2. EMERGENCY LIGHTS OPS CHECKED GOOD.Nov 14, 2013 · N528FE · Doug MD11F · Emergency LightingSDR FDEA201311142781Sign · damagedWHEN CLOSING THE R1 DOOR FOR PUSHBACK, THE PANEL WHICH HOUSES THE EMERGENCY EXIT SIGN LIGHT ASSY MOVED OUT OUT OF SEQUENCE AND CAUGHT ON THE DOOR. ENTRY PANEL CAUGHT AND WAS RIPPED OUT OF POSITION. NO RESTRICTION IAW AMM 25-23-23-2. R1 DOOR SLIDING CEILINNov 14, 2013 · N528FE · Doug MD11F · Emergency LightingSDR FDEA201308161909Fitting · crackedMAIN DECK CARGO LOWER FRAME NR 2 FITTING SHOWING A CRACK INDICATION. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 117.Aug 16, 2013 · N528FE · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA201308161908Door Frame · crackedMAIN DECK CARGO LOWER FRAME NR 1 FITTING FOUND HOLE "B", 3RD LAYER AFTER REAMING TO MAXIMUM IAW SRM STILL SHOWING CRACK INDICATION.Aug 16, 2013 · N528FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201201260344Tiller · erraticAFTER LANDING DURING TAXI-IN NOSE TILLER STEERING BECAME ERRATIC & UNRESPONSIVE. STOPPED THE ACFT & CALLED FOR A TOW-IN. NO ALERTS & NO HYD PROBLEMS NOTED THAT WOULD EXPLAIN THE LOSS OF STEERING. PERFORMED VISUAL INSP OF THE STEERING MECHANISM AND RELATED CJan 26, 2012 · N528FE · Doug MD11F · Steering UnitSDR FDEA201109063715Longeron · crackedLONGERON 38 LEFT CRACKED AT STA 6-100. LONGERON REMOVED AS PER SRM 51-31-01 REV 47 AND INSTALLED NEW LONGERON AS PER SRM 51-33-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 6, 2011 · N528FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201109063714Longeron Splice · corrodedLOWER FWD CARGO BAY, LONGERON 52 BETWEEN STA 1119-6-10, FOUND SPLICE FITTING WITH CORROSION. SPLICE FITTING REMOVED AND REPLACED WITH NEW MACHINED SPLICE AS PER SRM 51-33-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 6, 2011 · N528FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201109063713Skin · damagedLOWER FWD CARGO DOOR FWD FUSELAGE DOOR CUTOUT FOUND REPAIR WITH CHAFFED. CARRIED OUT REPAIR AS PER SRM 53-00-15 FIG.202 REPAIR 8 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.Sep 6, 2011 · N528FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201109063716Seat Track · chippedMAIN DECK SEAT TRACK FOUND CHIPPED. REPAIR CARRIED OUT AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV 47. SEAT TRACK REPLACED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 6, 2011 · N528FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103241159Bolt · crackedAFTER TAKEOFF, RT MLG UNSAFE UP. ATTEMPTED RECYCLE, BUT STILL UNSAFE. FOUND RT MLG PIVOT BOLT SHEARED. REMOVED AND REPLACED RT MLG PIVOT BOLT PER AMM 07-11-00-2-0, 32-12-10-4-0, 32-12-20-4-0 AND 32-11-01-3-1. COMPLIED WITH EA 1-3210-148281 AND 1-3210-14Mar 24, 2011 · N528FE · Doug MD11F · Main Landing GearSDR FDEA201102120550Battery · dischargedDURING PREFLIGHT CHECK, PERFORMED EMERGENCY LIGHT TEST FAIL. CHECK FOUND HAS EMERGENCY LIGHT BATTERY 1 LOW MESSAGE IN EAD, R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-01-4-0, PERFORMED OPS TEST OF THE EMERGENCY LIGHT PACK ALL SATIS IAW MM 33-51-01-5-0.Feb 12, 2011 · N528FE · Doug MD11F · Emergency LightingSDR FDEA201101270387Pressure Switch · failedON DEPARTURE AIR SYS, MANIFOLD ILLUMINATED RED MOMENTARILY. LEVEL 2 ALERT WING ANTI ICE LIGHT. DIVERTED. LANDED UNEVENTFULLY. MANIFOLD FAIL ALERT CAME ON BEFORE WING ANTI ICE ALERT RECEIVED. ESC FAULT REVIEW SHOWS LT WING ANTI-ICE MANIFOLD & PSC-2 STORJan 27, 2011 · N528FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA201012024539Line · crackedHYD 2 FAIL. BEHIND NR2 PYLON STRUCTURE PANEL 364KR FOUND NR2 HYD LINE CRACKED. REPAIRED SAME LINE IAW REF TO MM CHAP 20-10-01-2-0 PERMANENT PIPING REPAIR. MX PRACTICES WITH 3000 PSI APPLIED TO SYS, NO LEAKS FOUND. SYS OK FOR SERVICE. (CLOSED)Dec 2, 2010 · N528FE · Doug MD11F · Hydraulic System, MainSDR FDEA200910043473Bracket · damagedRT REAR SPAR MOUNTED FITTING NR 3 SPOILER OTBD IDLER MOUNTING POINT FOUND BUSHING HOLE ELONGATED. COMPLIED WITH E.A. 1-5740-133898, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.Oct 4, 2009 · N528FE · Doug MD11F · Wing, Attach FittingsSDR FDEA200909243381Fuel Tank · corrodedDURING MAIN DECK FLOOR PANEL INSP AT STA 1234 X= -47.5 CTR WING TANK TOP SURFACE, FOUND CORROSION. COMPLIED WITH EA 1-5710-133877, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.Sep 24, 2009 · N528FE · Doug MD11F · Fuel StorageSDR FDEA200909243380Skin · damagedFUSELAGE SKIN PANEL AT FWD JACK POINT FOUND WITH TOOL MARKS. REPAIR CARRIED IAW EA 1-5330-132902. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100 REV 108.Sep 24, 2009 · N528FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200903251036Pump · failedNR 3 ENG FLAME OUT DURING DESCENT, 280KTS/13000. PERFORMED LEVEL 3 ENG RPM LOW CHECKLIST, FOLLOWED BY ENG RESTART IN FLIGHT CHECKLIST, GOOD RESTART 10000/270 KTS. CKD ALL DEU AND FADEC NO FAULT SHOWN, INSP INLET & EXHUAST, CORE AREA NO DEFECT NOTED, R & R Mar 25, 2009 · N528FE · Doug MD11F · Engine Fuel PumpSDR 08FDEA04011Relay · malfunctionedDURING CRUISE RECEIVED LEVEL 1 "R EMER AC OFF". F/O LOST MCDU NR 2 AND FMC2, DEU NR 2, DU4, 5 AND 6 NOTE: VERBAL FROM CREW ON POST FLIGHT, DUMPED 62.0 LB FUEL DUE ATB. CHECKED EPCU FAULT REVIEW AND FOUND "LEG 1 IN AIR" REAC SENSE RELAY/INTFC. CHECKED CURRESep 23, 2008 · N528FE · Doug MD11F · AC InverterSDR 08FDEA01792Frame · chafedFORWARD CABIN AT APPROXIMATELY STATION 535 LONGERON 20 LEFT FRAME FOUND CHAFED. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.May 8, 2008 · N528FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01791Frame · chafedFORWARD CABIN LEFT SIDE 9-G NET YOKE AREA, FRAME FOUND CHAFED AT STATION 535 LONGERON 24 LEFT. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.May 8, 2008 · N528FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01766Frame · dentedCABIN : AFT CABIN AT APPROXIMATELY STATION 1741 LT LONGERON 12 FOUND FRAME DENTED. REPAIRED PER SRM 53-30-00 FIG.1, VOL.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PERMay 6, 2008 · N528FE · Doug MD11 · Fuselage Main, FrameSDR 08FDEA01769Frame · dentedAFT CABIN AT APPROXIMATELY STATION 1681 LEFT SIDE LONGERON 12 FOUND FRAME DENTED. REPAIRED AS PER SRM 53-30-00 FIG.1,VOL.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER May 6, 2008 · N528FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01768Frame · dentedAFT CABIN AT APPROXIMATELY STATION 1701 LEFT SIDE LONGERON 12 FOUND FRAME DENTED. REPAIRED PER SRM 53-30-00 FIG 1, VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SMay 6, 2008 · N528FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01767Frame · dentedAFT CABIN AT APPROXIMATELY STATION 1721 LT LONGERON 12 FOUND FRAME DENTED. REPAIRED AS PER SRM 53-30-00 FIG.1,VOL.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES AS PER SRM 53-30-00, FIG.1, VOL.May 6, 2008 · N528FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00374Inlet · looseNR 2 ENGINE INLET JUST FWD OF THE ENGINE FAN BLADES HAS NUMEROUS LOOSE FASTENERS AT THE 12:00, 9:00, AND 3:00 O'CLOCK POSITION (REFERENCE MD 11 IPC 55-32-01-01, CIRCLED ITEM K). REMOVED AND REPLACED LOOSE FASTENERS INSIDE INLET PER AMM 20-00-00.Feb 8, 2008 · N528FE · Doug MD11F · Engine Air Intake SystemSDR 06FDEA04143Fitting · damagedLT WING I/B FLAP I/B ENCLOSURE AFT UPPER BIG ROLLER BEARING ATTACHMENT FITTING FOUND HOLE ELONGATED AS MARKED. REPAIRED AS PER EA 1-5750-106545. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.Nov 30, 2006 · N528FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03906Skin · chippedFWD CARGO COMPARTMENT AT STA 895 LONGERON 41 RT DOOR CUTOUT AREA FOUND SKIN WITH EDGE CHIPPED OFF AS MARKED. DAMAGE ALONG EDGE OF FWD CARGO DOOR CUTOUT AREA AT STA 895 LONGERON 41 RT REMOVED APPROX 2" X 1/4" AND REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 16 VNov 6, 2006 · N528FE · Doug MD11 · Fuselage Main, Plate/Skin
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