N68049, cancelled Apr 23, 2020

Service difficulty reports · 89

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 = 'N68049' AND deregistration_id = 'N68049-2020-04-23'
  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 FDEA201510143210Strut · malfunctionedGEAR HANDLE WOULD NOT RAISE. IT TOOK SEVERAL ATTEMPTS & AFTER WORDS HAD LEVEL 1, ANTI-SKID NO TEST. R & R NLG SHOCK STRUT IAW WC 32T2101. PERFORMED GEAR SWING IAW MM 32-30-00-5. OPERATIONS CHECKED GOOD COMPLIED WITH SECOND WC 32T2701 FOR INSTALLATION. OKOct 14, 2015 · N68049 · Doug MD1010F · Main Landing Gear Strut/Axle/TruckSDR FDEA201510113164Unknown · malfunctionedGEAR HANDLE WOULD NOT RAISE INITIALLY, REQUIRED SEVERAL ATTEMPTS TO RAISE AFTER TAKEOFF. NO FAULT FOUND.Oct 11, 2015 · N68049 · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201510113206Unknown · malfunctionedGEAR HANDLE WOULD NOT RAISE. REQUIRED SEVERAL ATTEMPTS TO RAISE AFTER TAKEOFF. ACCOMPLISHED GENERAL VISUAL INSPECTION OF THE LG GND SENSING CONTROL MECHANISM & FOUND NO DEFECTS. LIFTED ACFT ON JACKS. ACCOMPLISHED CHECK FOR PROPER RIG OF LG GND SENSING MECHOct 11, 2015 · N68049 · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201508112531Unknown · malfunctionedON LANDING ROLL, DEPRESSED BRAKES TO FLOOR WITH VERY LITTLE DECELERATION. DID NOT FEEL ANTI-SKID ENGAGE OR CYCLE. WET RUNWAY. MX NOTE, ACFT LANDED DURING VERY HEAVY RAIN FALL. DURING POST FLIGHT CHECKS, NO ANTI-SKID FAULTS RECORDED. ANTI-SKID TESTED OK. Aug 11, 2015 · N68049 · Doug MD1010F · Landing Gear Brake SystemSDR FDEA201501020012Indicator · defectiveR1 SLIDE PRESSURE PRESS TO TEST BUTTON INOPERATIVE. AMM 25-61-03-2-0 R & R PRESSURE INDICATOR MODULE. OPERATIONS CHECKED GOOD.Jan 2, 2015 · N68049 · Doug MD1010F · Emergency EquipmentSDR FDEA201411053522Light · brokenL1 DOOR SLIDE DISARM LIGHT BROKEN. REPLACED L1 DOOR SLIDE DISARM LIGHT & SOCKET ASSEMBLY IAW AMM 20-30-08-2. LIGHT OPERATION CHECKS NORMAL.Nov 5, 2014 · N68049 · Doug MD1010F · Door Warning SystemSDR FDEA201404270867Skin · crackedHORIZONTAL STABILIZER LOWER RT FWD PLANK APPEARS TO BE CRACKED. TRIMMED OUT CRACK. FABRICATED DOUBLER, SPLICE, AND INSTALLED IAW DWG SR10550002, AND J060211.Apr 27, 2014 · N68049 · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR FDEA201303190615Panel · missingDURING WALK AROUND FOUND NR 1 ENGINE PYLON V-PANEL MISSING. REPLACED ALL PANEL NUT PLATES AND INSTALLED SERVICEABLE PANEL. REF SRM51-00-01, SRM 51-35-01.Mar 19, 2013 · N68049 · Doug MD1010F · Nacelle/Pylon, Plate/SkinSDR FDEA201205171830Coalescer Bag · dirtyDISTINCT ODOR OF MELTING PLASTIC COMING FROM PACKS. THIS IS WITH NR 2 PACK OFF. WHEN YOU CALL FOR 78 DEGREES & HIGHER, STRONG ODOR. RAN PACKS INDIVIDUALLY AND ISOLATED ODOR TO WHEN PACK 1 IS OPERATING. NR 1 PACK COALESCER BAG WAS VERY DIRTY, RAN NR 1 PACMay 17, 2012 · N68049 · Doug MD1010F · Humidity Control SystemSDR FDEA201205011697Valve · inoperativeHOT PLASTIC ODOR IN COCKPIT WHENEVER NR 1 SUPPLY DUCT TEMP APPROACHES 100 DEGREES. REPEAT WRITE-UP PERFORMED GVI OF RAM AIR DOOR INLET AND EXHAUST AREAS; NO DEFECTS NOTED. R & R FLIGHT COMPARTMENT TRIM AIR VALVE REF AMM 21-61-12-4. RAN ENGINES IAW JRH.May 1, 2012 · N68049 · Doug MD1010F · Air Distribution SystemSDR FDEA201205011696Coalescer Bag · odorODOR OF BURNED OR HOT PLASTIC FROM PACKS. ISOLATED NR 1 AND ODOR CEASED. REPLACED NR 1 PACK COALESCER BAG IAW MM 21-54-03-2-0, FUNCTIONAL TEST NR 1 PACK IAW 21-00-01-5-0. NO ODOR NOTICED, CHECKED OK.May 1, 2012 · N68049 · Doug MD1010F · Humidity Control SystemSDR FDEA201204141401Frame · crackedCENTER ACCESSORY COMPARTMENT LEFT FUSELAGE FRAME AEA0159 CRACKED AT STA 1158 Z= -28. REPAIRED CRACKED FRAME AEA0159-1 AT STA 1158 Z= -28 IN LT CENTER ACCY COMPARTMENT REF SRM 53-30-00, FIG 7.Apr 14, 2012 · N68049 · Doug MD1010F · Fuselage Main, FrameSDR FDEA201204071288Intercostal · corrodedINTERCOSTAL CORRODED AT STA 1521, LONGERON 39R IN RT WHEEL WELL. R & R INTERCOSTAL REF DWG AEA0024, SRM 51-33-01 VOL II. NO CORROSION FOUND ON SKIN, TREATED AND PRIMED AREA REF SRM 51-21-01, VOL II.Apr 7, 2012 · N68049 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201204071287Intercostal · corrodedCORRODED INTERCOSTAL AT BS 1521 AND LONGERON 35R IN RT WHEEL WELL. R & R INTERCOSTAL IAW DWG AEA0026 AND SRM 51-33-01 VOL II. TREATED AND PRIMED AREA IAW SRM 51-21-01 VOL II. NO CORROSION FOUND ON ACFT SIDE.Apr 7, 2012 · N68049 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201204031242Hinge · crackedAFTER REVIEW IN AN ATTEMPT TO REMOVE A CRACK IN THE FWD UPPER CARGO DOOR, FOUND FWD HINGE LOBE CRACKED COMPLETELY THROUGH ON THE FWD END. REMOVED .080 FROM UPPER FORWARD CARGO DOOR HINGE LOBE, FIRST LOBE FORWARD SIDE WITH COUNTERBORE .781 X .094. PERFORMED HApr 3, 2012 · N68049 · Doug MD1010F · Fuselage, Door HingeSDR FDEA201204031243Angle · crackedHFEC INSPECTED HORIZONTAL LEG BASE, FOUND TO BE CRACKED, LOCATED .5" FROM LT OTBD TO 1ST FASTENER, ON VERTICAL STABILIZER. LENGTH OF CRACK IS ABOUT .6250 INCHES LONG. REPLACED CRACKED BASE ANGLE IN REF TO W/C EO 8-5530-7-4303 C2, PART 2, STEP 5.Apr 3, 2012 · N68049 · Doug MD1010F · Vertical StabilizerSDR FDEA201108313593Sensor · failedFIVE MINUTES INTO CRUISE NR 3 ENGINE SHOWED N1 EXCEEDANCE UP TO 209.3 PERCENT BROUGHT NR 3 THROTTLE TO IDLE. INDICATIONS CAME BACK TO NORMAL, FIVE MINUTES LATER NR 3 N1 JUMPED AROUND THEN BACK TO NORMAL FOR REST OF FLIGHT. TROUBLESHOT IAW FIM MANUAL 77-11-Aug 31, 2011 · N68049 · Doug MD1010F · Engine RPM Indicating SystemSDR FDEA201105191878Fire Warning · false activationON PREFLIGHT, RECEIVED LOWER AFT CARGO FIRE WARNING. RAMP PERSONNEL COMMUNICATED SMOKE FROM AFT BELLY COMPARTMENT. DISCHARGED FLASHING, DISCHARGE SWITCH AND EVACUATED ACFT. PERFORMED COCKPIT CARGO COMP T FIRE TEST, OPS TESTED NORMAL. RAN APU AND APU PNEUMay 19, 2011 · N68049 · Doug MD1010F · Fire DetectionSDR FDEA201010073972Wheel · missingFOUND THE NR5 TIRE/ WHEEL ASSY MISSING. (NOT ON THE AXLE) REPLACED THE NR 5 WHEEL ASSY IN REF TO THE MM 32-41-01-2. R & R THE LT GEAR AFT BRAKE TORQUE LINK OTBD SIDE IN REF TO THE AMM 32-11-02-2. ALSO INSTALLED A NEW MAIN LANDING GEAR SPACER ON NR5 AXLE IN ROct 7, 2010 · N68049 · Doug MD1010F · Wheel/Ski/FloatSDR FDEA201006162022Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN AT STA 1159, BETWEEN LONGERON 39R AND 40R. EVALUATED AND FOUND STRAP PN SR10530073-27 AND SHIM PN SR10530073-29 NOT INSTALLED IAW DRAWING SR10530073 SHEET 2, REVISION F. NEW STRAP AND SHIM FABRICATED AND INSTALLED AS PER DRAJun 16, 2010 · N68049 · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201006162026Skin · misrepairedLT INBD T/E FLAP LOWER SURFACE FOUND 1 EACH EXISTING REPAIR AT OTBD OF INBD FLAP OTBD HINGE AREA. FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT PER DRAWING ARC2992 REVISION R AND AMM 20-50-02 REVISION 10. E.O. 8-5100-7-5001Jun 16, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006141988Skin · misrepairedEXISTING REPAIR - 1 EACH FOUND AT LT WING TIP UPPER SURFACE. 1 EACH EXISTING REPAIR ON LEFT HAND WING TIP UPPER SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR. EXISTING REPAIR REMOVED AND A NEW REPAIR CARRIED OUT AS PJun 14, 2010 · N68049 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006131974Skin · misrepairedEXISTING REPAIR 01 EACH FOUND AT LT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE, INBOARD AREA, LOCATION 15 INCHES FROM INBOARD EDGE. EXISTING REPAIR 01 EACH AT LT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE, INBOARD AREA, LOCATION 15 INCHES FROM INBOARD EDGE EJun 13, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006131973Skin · misrepairedRT WING FIXED L/E UPPER AREA FOUND 1 EACH EXISTING REPAIR AT NR 3 SLAT INBD VICINITY AREA. FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR. EXISTING REPAIR REMOVED AND AND A NEW REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 28 VOLUME I, RJun 13, 2010 · N68049 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006011744Hinge Fitting · corrodedLT WING - OTBD FLAP INBD FLAP MOUNTED HINGE FITTING PIVOT INBD BORE EXCEEDED LIMIT. REPAIR CARRIED OUT IAW EA NR 8-5750-140490 PART 1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.Jun 1, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201006011745Hinge Fitting · damagedRT WING - OTBD FLAP INBD FLAP MOUNTED HINGE FITTING PIVOT INBD BORE FOUND EXCEEDED LIMIT AFTER BUSHING REMOVED. REPAIRED IAW EA NR8-5750-140488. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Jun 1, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291729Skin · bulgedRT WING - OTBD AILERON UPPER SURFACE AT APPROX XOA 870, FOUND BULGING. RT OTBD AILERON R & R IAW AMM 27-10-02-4 REV 10.May 29, 2010 · N68049 · Doug MD1010F · AileronsSDR FDEA201005291728Skin · crackedRT WING - FIXED L/E AREA TELESCOPIC DUCT UPPER DOOR CUT OUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5740-139238, REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201005291727Skin · dentedRT WING - INBD FLAP INBD SEGMENT LOWER SURFACE FOUND WITH MULTIPLE DENTS. REPAIR CARRIED OUT AT RT WING INBD FLAP INBD SEGMENT LOWER IAW SRM 57-10-00, FIG 4, VOL I, REV. 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV. 110.May 29, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291724Skin · bulgedLT WING - INBD AILERON LOWER SURFACE FWD SIDE APPROX XIA 295 TO XIA 325 FOUND SKIN BULGING. REPAIRED IAW EA NR 8-5750-140484. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.May 29, 2010 · N68049 · Doug MD1010F · AileronsSDR FDEA201005291723Skin · bulgedLT WING - OTBD AILERON LOWER SKIN FWD SIDE APPROX XOA 1006 TO XOA 1025 FOUND BULGING. REPAIR CARRIED OUT IAW EA8-5750-140483, REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.May 29, 2010 · N68049 · Doug MD1010F · AileronsSDR FDEA201005291722Hinge Fitting · corrodedLT WING - OTBD FLAP OTBD FLAP MOUNTED HINGE FITTING PIVOT INBD BORE FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 8-5750-140486, REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 110.May 29, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291721Hinge Fitting · corrodedLT WING - OTBD FLAP OTBD WING MOUNTED HINGE FITTING AFT ATTACHMENT LOWER OTBD BORE FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 8-5750-140487, REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291720Hinge Fitting · corrodedLT WING - OTBD FLAP OTBD WING MOUNTED HINGE FITTING AFT ATTACHMENT LOWER INBD BORE FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 8-5750-140487, REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291718Hinge Fitting · corrodedLT WING - OTBD FLAP OTBD WING MOUNTED HINGE FITTING ATTACHMENT AREA FOUND SURFACE CORROSION. LT OTBD T/E FLAP OTBD WING MOUNTED HINGE FITTING SIDE ATTACHMENT FACE REPAIRED IAW CMM 20-11-02 REV 50. FOUND UPPER REMAINING THICKNESS: 0.492"; LOWER REMAINING THICMay 29, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291716Hinge Fitting · corrodedLT WING - OTBD FLAP INBD WING MOUNTED HINGE FITTING BARREL NUT ATTACHMENT BORE FOUND RUSTY. REPAIR CARRIED OUT IAW EA NR8-5750-140490 PART 2, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005291713Hinge Fitting · corrodedLT WING - OTBD FLAP INBD WING MOUNTED HINGE FITTING ATTACHMENT AREA FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 8-5750-140490 PART 2, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005291712Hinge Fitting · corrodedLT WING - OTBD FLAP INBD WING MOUNTED HINGE FITTING PIVOT BORE FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 8-5750-140490 PART 2, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005291710Hinge Fitting · corrodedLT WING - OTBD FLAP INBD WING MOUNTED HINGE FITTING AFT ATTACHMENT LOWER OTBD BORE FOUND SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 8-5750-140490 PART 2, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 29, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005281706Skin · crackedLT WING - FIXED L/E AREA TELESCOPIC DUCT UPPER DOOR CUT OUT FOUND CRACKED. CUT OUT REPAIRED AS IAW EA 8-5740-139238, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 28, 2010 · N68049 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201005261679Skin · bulgedRT OTBD AILERON UPPER SURFACE AT APPROX XOA870 FOUND BULGING. RT OTBD AILERON R & R IAW AMM 27-10-02-4, REV 10.May 26, 2010 · N68049 · Doug MD1010F · AileronsSDR FDEA201005261678Skin · bulgedLT OTBD AILERON LOWER SKIN AT FWD SIDE APPROX XOA 910 TO XOA 945 FOUND WITH BULGING. REPAIR CARRIED OUT IAW EA NR 8-5750-140483, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 -110.May 26, 2010 · N68049 · Doug MD1010F · AileronsSDR FDEA201005261677Skin · bulgedLT OTBD AILERON LOWER SKIN AT FWD SIDE APPROX XOA 1000 FOUND WITH BULGING. REPAIR CARRIED OUT IAW EA NR 8-5750-140483, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100-110.May 26, 2010 · N68049 · Doug MD1010F · AileronsSDR FDEA201005261676Hinge Fitting · corrodedRT OTBD T/E FLAP OTBD WING MOUNTED HINGE FITTING WITH BUSHING REMOVED. FOUND CORROSION AT AFT ATTACHMENT LOWER OTBD BORE. REPAIR CARRIED OUT IAW EA NR 8-5750-140485 PART 1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 26, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005261675Hinge Fitting · corrodedRT OTBD T/E FLAP OTBD WING MOUNTED HINGE FITTING WITH BUSHING. REMOVED AND FOUND CORROSION AT AFT ATTACHMENT LOWER INBD BORE. REPAIR CARRIED OUT IAW EA NR 8-5750-140485 PART 1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.May 26, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005261674Hinge Fitting · corrodedRT OTBD T/E FLAP INBD WING MOUNTED HINGE FITTING WITH BUSHING. REMOVED AND FOUND CORROSION AT PIVOT BORE. REPAIR CARRIED OUT IAW EA NR 8-5750-140485 PART 2, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 26, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005261673Skin · crackedNLG WHEEL WELL - LT FWD DOOR, WHEEL WELL CUTOUT SKIN FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 53-50-00 FIG 25, VOLUME I, REVISION 96 AND EA 8-5350-139237, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.May 26, 2010 · N68049 · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201005261672Hinge Fitting · corrodedRT OTBD T/E FLAP INBD WING MOUNTED HINGE FITTING SIDE ATTACHMENT FACE AREA FOUND RUSTY. RT OTBD T/E FLAP INBD WING MOUNTED HINGE FITTING SIDE ATTACHMENT FACE REWORKED IAW CMM 20-11-02 REV 50 AND FOUND WITHIN LIMIT BASING ON THE DIFFERENCE BETWEEN CMM 57-44May 26, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005261671Hinge Fitting · corrodedRT OTBD T/E FLAP OTBD WING MOUNTED HINGE FITTING SIDE ATTACHMENT FACE FOUND RUSTY. RT OTBD T/E FLAP OTBD WING MOUNTED HINGE FITTING SIDE ATTACHMENT FACE REWORKED IAW CMM 20-11-02, REV 50 AND FOUND WITHIN LIMIT BASIN ON THE DIFFERENCE BETWEEN CMM 57-44-09 REV May 26, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201005261670Hinge Fitting · corrodedRT OTBD T/E FLAP OTBD WING MOUNTED HINGE FITTING AFT LOWER ATTACHMENT AFT OTBD BORE FACE FOUND RUSTY. REPAIR CARRIED OUT IAW EA NR8-5750-140485 PART 1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.May 26, 2010 · N68049 · Doug MD1010F · Wing, Control Surface Attach Fittings
Back to N68049, cancelled Apr 23, 2020