N68057, cancelled Apr 23, 2020

Service difficulty reports · 73

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 = 'N68057' AND deregistration_id = 'N68057-2020-04-23'
  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 FDEA201503190989Switch · dirtyDOOR 1 LT FAILED OPEN FROM OUTSIDE & INSIDE. CYCLED SLIDE ARM LEVER & OPENED WITH DOOR SWITCH. INSPECTED & CLEANED DOOR SWITCH IAW AMM 52-10-01-6. DOOR OPERATIONS CHECKED NORMAL IAW AMM 52-10-01-5. ACFT OK FOR SERVICE.Mar 19, 2015 · N68057 · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201407191858Skin · crackedON POST FLIGHT WALK AROUND FOUND FUSELAGE SKIN CRACKED AT NR 1 PACK DOOR CUT OUT UPPER AFT CORNER. INSTALLED DOUBLER, TRIPLER & FILLER IAW SRM 53-50-00 FIG 3A & EA.Jul 19, 2014 · N68057 · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201406141448Skin · crackedFOUND A CRACK ON RT WING SKIN AT NR 3 SLAT TRACK BETWEEN NR 1 & 2 SLATS. TRIMMED OUT DAMAGED AREA. PERFORMED INTERNAL & EXTERNAL VISUAL INSPECTION WITH NO ADDITIONAL DAMAGE NOTED. HFEC INSPECTION DONE WITH NO CRACKS NOTED. REPAIRED IAW EA 8-5730-T0308776Jun 14, 2014 · N68057 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201406091367Skin · crackedFOUND TWO CRACKS ON RT WING TAI DUCT CUT OUT. VERIFIED CRACKS IAW NDT SPM PART 6. REPAIRED IAW EA 8-5710-T0308893 & SRM.Jun 9, 2014 · N68057 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201406091368Skin · crackedDURING POST FLIGHT INSPECTION, FOUND POSSIBLE LT WING LE CRACK AT REFUEL DOOR INBD CORNER CUT OUT. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6 CRACK TERMINATES AT FASTENER. CUT OUT CRACKED AREA IAW SRM 57-10-00 FIG 68 SHEET 2. COMPLIED WITH HFEC ONJun 9, 2014 · N68057 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201406091366Skin · crackedFOUND TWO CRACKS IN LEFT WING TAI DUCT. VERIFIED CRACK IAW NDT SPM PART 6. REPAIRED IAW EA.Jun 9, 2014 · N68057 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201312223028Transmitter · failedAT FL 320, NOTICED NR 2 FUEL FLOW 16150 PPH, ALL OTHER INDICATIONS NORMAL. FUEL USED SHOWED NR 2 HAD USED 2200 LBS MORE THAN 1 & 3. FUEL REMAINING WAS IN AGREEMENT WITH FUEL USED. WHEN THROTTLE RETARDED, FUEL FLOW REDUCED TO APPROXIMATELY 11000 PPH AT IDLEDec 22, 2013 · N68057 · Doug MD1010F · Fuel Indicating SystemSDR FDEA201305100968Fitting · crackedMAIN CARGO DOOR FRAME NR 1 SPOOL LOWER FITTING CRACKED IN FOUR LOCATIONS. VERIFIED WITH HFEC IAW NDT SPM93K0393, CRACK RUNS THOUGH FITTING. R & R MAIN CARGO DOOR FRAME SPOOL LOWER FITTING. IAW SRM 51-33-01, VOL II.May 10, 2013 · N68057 · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201301140091Strut · damagedAFTER T/O LDG GEAR HANDLE WOULD NOT RAISE. QRH C/W. HANDLE RAISED & ALL IN FLIGHT SYSTEMS OPERATED NORMALLY. R & R THE NLG ASSY, REF WC 32T2101 AND 32T2701.Jan 14, 2013 · N68057 · Doug MD1010F · Nose/Tail Landing Gear Strut/AxleSDR FDEA201301040056Intercostal · corrodedLEFT MLG WHEEL WELL AFT WALL LOWER SHELF HAS THE INTERCOSTAL JUST BELOW THE FLAP BUSS CABLE PULLEYS WITH A LARGE AREA BULGED. INSTALLED NEW INTERCOSTAL REF. SRM 51-31-01.Jan 4, 2013 · N68057 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201212294396Control Unit · malfunctionedAFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE. COMPLIED WITH QRH THEN GOT LEVEL 1 ANTI-SKID NO TEST ALERT. REMAINED ON UNTIL GEAR HANDLE DOWN. ANTI-SKID ALERT WENT OUT. ANTI-SKID WORKED ON LANDING ROLL OUT. LANDED WITHOUT INCIDENT. MX REMOVED AND REPLDec 29, 2012 · N68057 · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201209153328Scavenge Pump · leakingDURING CLIMB NR 1 OIL QUANTITY INDICATED '0'. ALL OTHER INDICATIONS NORMAL INITALLY. IN CRUISE NR 1 OIL PRESS DROPPED TO 14 PSI WITH AN AMBER INDICATION. CONFERRED WITH MAINT. THROUGHOUT, QRH COMPLIED WITH. DIVERTED. UPON ARRIVAL CHECKED NR 1 ENG. OIL, CSep 15, 2012 · N68057 · Doug MD1010F · Turbine Engine Oil SystemSDR FDEA201204241542Power Supply · failedDURING PREFLIGHT EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHTS POWER SUPPLY IAW MM 33-51-01-4, OPS CHECKS NORMAL.Apr 24, 2012 · N68057 · Doug MD1010F · Emergency LightingSDR FDEA201111164931Sensor · failedON TAKEOFF ROLL N2 VIA FAIL. REJECT AT 60 KTS. R & R NR 1, ENG N1 SENSOR.Nov 16, 2011 · N68057 · Doug MD1010F · Engine Indicating SystemSDR FDEA201111154928Sensor · failedNR 3 ENGINE N1 GAUGE FAILED ON DEPARTURE ROLL ALONG WITH AUTOTHROTTLE OFF - "VIA 1 FAIL" AND "VIA 2 FAIL" LEVEL 1 ALERTS. VIA 1 FAULT HISTORY SHOWED NR 3 ENGINE N1 DISAGREE AND VIA 2 SHOWED NR 3 ENGINE N1 INTERMITTANT. FCC'S 1 & 2 LIST NR 3 ENG TACH FAULT Nov 15, 2011 · N68057 · Doug MD1010F · Engine RPM Indicating SystemSDR FDEA201110124425Windshield · failedCAPT'S WINDSHIELD ARCING & SHATTERED. SHORTED IN WINDOW AT 18000 FT. REPLACED THE CAPT'S WINDSHIELD REF MM 56-11-00-2.Oct 12, 2011 · N68057 · Doug MD1010F · Flight Compartment WindowsSDR FDEA201107192814Floorbeam · crackedFLOORBEAM TEE CRACKED THROUGH ALL SIDES AT STA 1156 L29R. REPAIRED CRACKED FLOORBEAM REF SRM 53-30-00 FIG 7. COMPLIED WITH EA 8-5310-147795.Jul 19, 2011 · N68057 · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201012024537Lamp · inoperativeR1 DOOR PRESSURE, PRESS TO TEST INDICATOR INOP. FOUND P/N 387 HIGH VOLTAGE LAMPS IN DOOR SLIDE PUSH BUTTON SWT. INSTALED P/N 368 LAMPS PER IPC. GRD OPS CHECKS OK.Dec 2, 2010 · N68057 · Doug MD1010F · Emergency EquipmentSDR FDEA200911093915Actuator · damagedDURING WALK AROUND, FOUND LT OTBD FLAP INBD ACT BROKEN. INSPECTED FLAP FOR ANY PULLED RIVETS AND NONE FOUND. INSPECTED OTBD FLAP ACT"S ATTACKING POINTS TO MAKE SURE NO OTHER DAMAGE TO FLAPS, NONE FOUND. INSPECTED ALL OTHER FLAPS AND NO DAMAGE FOUND IAW AMM-Nov 9, 2009 · N68057 · Doug MD1010F · Trailing Edge Flap ActuatorSDR FDEA200906102018Smoke Detector · malfunctionedDECENDING THRU 14,000` RECEIVED "CARGO FIRE ALERT" COMPLIED WITH QRH AND DISCHARGED BOTH FIRE BOTTLES. NEVER HAD ANY SECONDARY INDICATIONS OF FIRE. REMOVED AND REPLACED ALL LOWER CARGO COMPARTMENT SMOKE DETECTOR PER MM 26-14-01-4. INSTALLED NR 2 CARGOJun 10, 2009 · N68057 · Doug MD1010F · Smoke DetectionSDR FDEA200807012617Seal · wornLOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WINDOW ARM. BUT COMMUNICATION WAS NEARLY IMPOSSIBLE WITH ATC. EVENTUALLY AN EMERGENCY WAS DECLARED. LOWER ALTITUDE AND LOWER AIRSPEED HELPEDJul 1, 2008 · N68057 · Doug MD1010F · Flight Compartment WindowsSDR 08FDEA02617Window Frame · damagedLOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WINDOW ARM. BUT COMMUNICATION WAS NEARLY IMPOSSIBLE WITH ATC. EVENTUALLY AN EMERGENCY WAS DECLARED. LOWER ALTITUDE AND LOWER AIRSPEED HELPED.Jul 1, 2008 · N68057 · Doug MD1010F · Fuselage Main, StructureSDR 07FDEA03587Skin · damagedFUSELAGE SKIN AND FRAME AT STA 642 HAVE OVERSIZED FASTENER HOLE. REPAIRED IAW EA 8-53-109196-FUSELAGE-EXISTING BUSHINGS FOUND AT STA 641.5 MCD, LOWER SILL-REPAIR. MAJOR REPAIR.Sep 11, 2007 · N68057 · Doug MD1010F · Fuselage Main, Plate/SkinSDR 07FDEA03403Floorbeam · corrodedAFT CABIN BULKHEAD FLOOR TEE ANGLE SUPPORT CORRODED UNDER FLOOR PANEL SUPPORT AT RBL 20 REMOVED CORROSION IAW MD10 SRM 53-40-00 VOL1 FIG 18. ORIGINAL THICKNESS .125 IAW MD10 SRM 53-40-00 VOL 1 FIG 18, REMAINING .094 MATERIAL REMOVED .031. REPAIRED IAW MD10Sep 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Floor BeamSDR 07FDEA03234Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION AT STA.720 AT LBL 107. REMOVED, FABRICATED AND INSTALLED SPLICED PLATE, SPLICE HAT AND SEAT TRACK IAW MD/DC10 SRM 53-70-00 VOL I PGE 3-4,51-31-01 VOL II PGE 1-10,53-70-00 PG E51 VOL I AND PART MARKED IAW FED EX GMM 7-0-1000Aug 29, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03006Stringer · corrodedCENTER W/WELL AREA L48L END FITTING CORRODED IN AREAS STA 1509 TO 1521. REMOVED, FABRICATED AND INSTALLED FITTING P/N AYB7020-1 STA 1509-1521 L48L IAW DC/MD10 SRM 51-33-01 VOL II, 53-00-01 FIG 1B VOLII , 51-21-01 VOL1, 51-21-02 VOLII AND DAC DWG AYB 7020.Aug 21, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/StringerSDR 07FDEA02982Seat Track · crackedCABIN SEAT TRACK FLANGE IS CRACKED AT STA 449 LBL 28.5 REMOVED SEAT TRACK AT STA 449 LBL 28.5 IAW DC-10 SRM 51-31-01 VOL 2 PG 1-10. FABRICATED IAW DC-10 SRM 53-70-00 PG 51 VOL 1. INSTALLED SEAT TRACK AT STA 449LBL 28.5 IAW DC 10 SRM 51-51-01 VOL 2 PG 1-2 .Aug 20, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02980Seat Track · gougedGOUGED CABIN SEAT TRACK SCALLOPS AT STA 879 TO 899 LBL 85 REMOVED AND REPLACED SEAT TRACK IAW DC-10 SRM 53-70-00 VOL 1 PG 51. FABRICATED SPLICE PLATES AND SPLICE HATS IAW DC-10 SRM 53-70-00 PG 4 VOL 1. INSTALLED SEAT TRACK SPLICE PLATE AND SPLICE HAT IAW DC1Aug 20, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02879Spar · crackedRT HORIZONTAL STAB REAR SPAR CAP CRACKED ON AFT SIDE NEAR RT UPPER AFT BARREL NUT AT STA XE 48.500 CRACK EXTENDS APPROX 3.0", HORIZONTALLY FROM INBD END OF FITTING PER EDDY CURRENT TEST. ACCOMPLISHED EA 8-5510-109187"STABILIZER-HORIZ- AD92-22-10-RH UPPER AFT Aug 14, 2007 · N68057 · Doug MD1010F · Horizontal Stabilizer, Spar/RibSDR 07FDEA02877Door Frame · corrodedFOUND MAIN CARGO LOWER DOOR JAMB HAS CORROSION ON LOWER BEAM AT STA 750. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB LOWER DOOR JAMB LOWER BEAM IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE 1, AND DAC DRAWING ACA7224 REV.G. MAJOR REPAIR.Aug 14, 2007 · N68057 · Doug MD1010F · Fuselage Main, StructureSDR 07FDEA02864Seat Track · gougedGOUGED/SCUFFED SCALLOPS ON CABIN SEAT TRACK AT STA 1199, TO 1219, RBL 47.5 REMOVED SEAT TRACK SECTION AT STA 1209-1269 RBL 47 IAW DC-10/MD-10 SRM 51-31-01, VOL2, PG 1. MAT ID FOR SEAT TRACK SECTION IS S4929405 PO 571558.2 IAW DC-10/MD10 SRM 53-42-01, VOL 2 PGAug 13, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02863Seat Track · gougedGOUGED, CABIN SEAT TRACK AT STA 1039 TO 1059, LBL 27.5 CHECKED LIMITS, GAP BETWEEN SCALLOPS FOUND TO BE GREATER THAN .500 (MAX ALLOWED) OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 21. REMOVED DAMAGE SEAT TRACK SECTION AND INSTALLED FAB`D SEAT TRACK SECTIAug 13, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02862Seat Track · damagedELONGATED SCALLOPS AT CABIN SEAT TRACK, STA 899 TO 919, RBL47.5. [08-29-07] CHECKED LIMITS, MAX ALLOW BETWEEN EDGE OF SCALLOP IS .500. FOUND TO BE GREATER THAN .500. OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 21. DIAL CALIPER T8878F REMOVED AND Aug 13, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02797Seat Track · damagedELONGATED SCALLOPS AT CABIN SEAT TRACK LBL 47.5, STA 939 TO 1019 (2-PLACES) REMOVED SEAT TRACK AT STA 879-1019 IAW DC10-SRM 53-70-00 VOL 1 PG5. SEAT TRACK WAS OUT OF LIMITS IAW DC10 SRM 53-20-00 PG 21. REPLACED SEAT TRACK IAW DC10 SRM 53-70-00 VOL 1 PG 1-10,Aug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02796Seat Track · damagedBROKEN SCALLOPS ON CABIN SEAT TRACK AT STA 755 REMOVED FLOOR PANEL IAW DC10/MD10 SRM 51-31-01 VOL 2 PGS 1-5. REMOVED SEAT TRACK AT STA 700-760 LBL 47.5 IAW DC10/MD10 SRM 51-31-01 VOL 2 PG 1-5, MAT ID 54929405 AND PO NR 570769.5 FOR SEAT TRACK IAW DC10/MD10 SRAug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02795Seat Track · wornELONGATED SCALLOPS ON CABIN SEAT TRACK AT RBL 47.5, STA 1019 TO 1039 CHECKED LIMITS, SEAT TRACK HAS SEVERAL BROKEN SCALLOPS OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL 1 PG 21. REMOVED OLD TRACK AND INSTALLED NEW TRACK IAW MD-DC10 SRM 53-42-01 VOL 3 PG 13/14Aug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02794Seat Track · gougedGOUGED, CABIN SEAT TRACK SCALLOPS AT STA 1159 TO STA 1099, RBL 27.5 STA 1099-1119, RBL 27.5 REMOVED GOUGE, REMAINING .434, FOUND TO BE WITHIN LIMITS IAW DC10/MD10 SRM 53-70-00, FIGURE 5 VOL 1 STA 1119-1159 RBL 27.5. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITSAug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02780Stringer · corrodedCENTER WHEEL AREA L48L END FITTING CORRODED IN AREAS STA1509 TO 1521. [08-21-07] ALL WORK ACCOMPLISHED ON SDR 07-3006 -W/O 37284.Aug 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/StringerSDR 07FDEA02779Stringer · corrodedCENTER WHEEL WELL AREA L52 END FITTING HAS CORROSION IN AREAS STA1509 TO 1521. [08-21-07] RMEOVED, FABRICATED, INSTALLED FITTING P/N AYB7020-2 IAW DC/MD10 SRM 51-33-01 VOLII, 53-00-01FIG 1B VOLII, 51-21-01 VOLII, 51-21-02 VOL II AND DAC DWG AYB 7020.Aug 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/StringerSDR 07FDEA02778Stringer · corrodedCENTER WHEEL WELL AREA L51R END FITTING HAS CORROSION IN AREAS STA 1509 TO 1521. [08-21-07] REMOVED, FABRICATED, AND INSTALLED FITTING P/N AYB 7020-1 STA.1509 TO 1521 L51R IAW DC/MD10 SRM 51-33-01 VOLII,53-00-01 FIG. 1B VOLII,51-21-01 VOLII,51-21-02 VOLIIAug 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/StringerSDR 07FDEA02728Fitting · crackedMAIN CARGO DOOR FITTING NR 3 BORES A, C AND D SHOWS CRACK INDICATION WITH BHEC BORES MARKE DIN BLACK. 09-04-07 REMOVED AND REPLACED NR 3 DOOR FITTING AT STA 666 IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE 1. MAJOR REPAIR.Aug 2, 2007 · N68057 · Doug MD1010F · Fuselage Main, Attach FittingsSDR 07FDEA02727Door Frame · corrodedMAIN CARGO DOOR CUT-OUT LOWER JAMB TOP SIDE, JUST FWD OF NR 3 LATCH SPOOL FITTING WEB CORRODED. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB UPPER BEAM ACA7226-1 IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE1 AND DAC DRAWING ACA7224 REV G. MAJOR REPAIRAug 2, 2007 · N68057 · Doug MD1010F · Fuselage Main, StructureSDR 07FDEA02726Fitting · crackedMAIN CARGO DOOR FITTING NR 7 BORES A, B, C AND D SHOW CRACK INDICATIONS WITH BHEC BORES MARKED IN BLACK. 09-04-07 REMOVED AND REPLACED FITTING NR 7 IN REF TO DC/MD10 SRM 51-33-01 VOLI PAGE 1. MAJOR REPAIR MECH 3934 QC348Aug 2, 2007 · N68057 · Doug MD1010F · Fuselage Main, Attach FittingsSDR 07FDEA01117Bolt · corrodedLT MAIN LANDING GEAR SUPPORT FITTING-FWD TRUNNION BOLT DOES NOT TAKE GREASE AND IS FROZEN. UPON REMOVAL, FOUND BOLT CORRODED. REPAIRED BOLT PER SEQ NR 13 EA 8-5710-10593 "LT MLG SUPPORT FITTING, FWD TRUNNION BOLT (FROZEN)".Mar 23, 2007 · N68057 · Doug MD1010F · Wing, Landing Gear Attach FittingsSDR 06FDEA04310Engine · making metalSHUT DOWN NR 3 ENGINE IN FLIGHT BECAUSE OF LEVEL 2 ALERT, ENG NR 3 OIL FILTER. BEFORE SHUT DOWN OIL PRESS WAS NORMAL. OIL TEMP WAS 20 PERCENT HIGHER THAN OTHER ENGINES. AFTER SHUT DOWN IT WIND MILLED FOR 25 MIN WITH SOME OIL PRESS. CHECKED AIU FAULTS LASDec 22, 2006 · N68057 · Doug MD1010F · Engine (Turbine/Turboprop)SDR 06FDEA03439Cylinder · failedRT MAIN GEAR DOWN ON RETRACTION AFTER T/O. LIGHT WENT RED AND STAYED RED UNTIL GEAR HANDLE PLACED DOWN. RECYCLED, SAME THING. LANDED @ KOAK. PER CREW DEBRIEF, APPARENTLY THE RT MLG NEVER MOVED FROM THE DOWN AND LOCKED POSITION. SUSPECT RT MAIN DOWNLOCK CYCSep 26, 2006 · N68057 · Doug MD1010F · Main Landing GearSDR 06FDEA1616Dimmer · failedAPPROACHING TOP OF DESCENT A SLIGHT ELECTRICAL ODOR WAS NOTED IN COCKPIT. UNABLE TO LOCATE SOURCE, BUT A BRIEF SQUEAL WAS HEARD NEAR COCKPIT DOOR, FOLLOWED SHORTLY AFTER BY UNCOMMAND IRCD OPENING. DEACTIVATED IRCD AS A PRECAUTION. CONFIRMED ELECTRICAL ODOR Apr 25, 2006 · N68057 · Doug MD1010F · Flight Compartment LightingSDR 06FDEA1276Seal · leaking1 40 INTO FLIGHT AT FL370, WINDOW SEAL ON CAPT SIDE DEVELOPED LOUD SQUEAL. TOO LOUD TO CONTINUE FLIGHT. NOISE DISSIPATED UPON DESCENT THRU 15,000'. REMOVED AND REPLACED LEFT SLIDING CLEAR WINDOW PER MD-10-10 AMM 56-12-00-4. PRESSURIZED A/C PER MD10-10 AMM 2Mar 31, 2006 · N68057 · Doug MD1010F · Flight Compartment WindowsSDR 06FDEA0953Repair · noneREPAIR DOUBLER STATION 1059 - 1085 L51 - L52 MARKED NR 15 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR LOCATED AT STA 1059 - 1085 L51 - L52. ACCOMPLISHED PARTMar 6, 2006 · N68057 · Doug MD1010F · Standard Practices/StructuresSDR 06FDEA0924Repair · unknownREPAIR LT OB FLAP UPPER SKIN,STA.XOF 587 MARKED NR 71. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR AT LT OB FLAP UPPER SKIN, FOUND TO BE WITHIN SRM 57-20-00 FIMar 2, 2006 · N68057 · Doug MD1010F · Standard Practices/Structures
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