Boeing MD-11F

Service difficulty reports · 31,317

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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 aircraft_model_key = 'MD11F'
  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 FDEA202307211457Skin · crackedLH WING, LEADING EDGE, NO. 8 SLAT TRACK CUTOUT, OUTBD EDGE HAS HORIZONTAL CRACK APPROX .500", MARKED ORANGE DOT & RED GREASE PENCIL. REPAIRED PER EA # 1-5730-T0375548 P1.Jul 21, 2023 · N597FE · Doug MD11F · Leading Edge DevicesSDR IPXA2023072493716Slide · inoperativeR1 DOOR SLIDE REMOTE PRESS INDICATOR DOES NOT LITE WHEN PRESSED. ACCOMPLISHED DMP 25-61-2 DEFERRED ITEM M810655.R/R R1 DOOR SLIDE PER AMM 25-61-15. OPS CHECK GOOD REF AMM 25-61-15. THIS CLEARS M810655Jul 21, 2023 · Doug MD11F · Service DoorsSDR FDEA202307211263Angle · crackedEXISTING REPAIR FOUND AT LEFT HAND WING #2 SLAT OUTER SKIN TRAILING EDGE OUTBOARD CORNER XDLES 327.289 EXISTING REPAIR AT LEFT HAND WING NUMBER 2 SLAT OUTER SKIN TRAILING EDGE OUTBOARD CORNER XDLES 327.289 EVALUATED AND FOUND REPAIRED AS PER EA # 1-5750-T0Jul 21, 2023 · N643FE · Doug MD11F · Wing StructureSDR IPXA2023081193878Hinge Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE I/B FLAP O/B HINGE BRACKET #3 LUG I/B FACE HAS CORROSION AT STA XW=-254, YW=495.961.REPAIRED CORRODED HINGE BRACKET AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE AT STA XW=-254, YW=495.961 IAW VTSAA EA 011-5740Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081193877Hinge Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE I/B FLAP O/B HINGE BRACKET #3 LUG O/B FACE HAS CORROSION AT STA XW=254, YW=495.961.REPAIRED CORRODED HINGE BRACKET AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE AT STA XW=254, YM=495.961 IAW VTSAA EA 011-5740-0Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081093866Hinge Bracket · corrodedINSPECTION TYPE:4CL/H WING A/C SIDE I/B FLAP O/B HINGE BRACKET #3 LUG I/B FACE HAS CORROSION AT STA XW=254, YW=495.961.REPAIRED CORRODED HINGE BRACKET AT THE L/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE AT STA XW=254, YW=495.961 IAW VTSAA EO 011-5740-0Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080993860Flap · corrodedINSPECTION TYPE:4CR/H WING I/B FLAP SIDE O/B HINGE #6 LUG BORE HAS PITTING AT STA XW=-254.REPAIRED HINGE AT THE R/H WING I/B FLAP SIDE O/B HINGE #6 LUG BORE AT STA XW=-254 IAW VTSAA EA 011-5740-01-B0054 I/R AND UPS EO MD11-5750-87788-A DATED 08/07/23 AND FAA FJul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080993858Flap · wornINSPECTION TYPE:4CR/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE IS WORN AT STA XW=-486.403.REPAIRED WORN HINGE AT THE R/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE AT STA XW=-486.403 IAW VTSAA EA 011-5740-01-B0060 I/R AND UPS EO MD11-5750-87840-A DATED 08/07/23 Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080593801Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE O/B FLAP O/B HINGE BRACKET #1 LUG BORE HAS CORROSION AT STA XW=-638.3059.REPLACED CORRODED HINGE BRACKET ASSY. AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.3059 IAW AMM 57-53-01 (MINOR)Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080493793Bracket · corrodedINSPECTION TYPE:4CR/H WING A/C SIDE O/B FLAP I/B HINGE BRACKET #1 LUG BORE HAS PITTING AT BETWEEN STA XW= -486.403, YW=589.366.REPLACED R/H WING A/C SIDE O/B FLAP I/B HINGE BRACKET BETWEEN STA XW=-486.403, YW=589.366 IAW AMM 57-53-01-400-801. (MINOR)Jul 20, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR 9WGA2023072051301Unknown · unknownON CLIMB OUT AUTO PILOT 2 INOP. THREE HOURS INTO FLIGHT AUTO PILOT 1 INOP. REMOVED AND REPLACED LEFT OUTBOARD AILERON LVDT PER AMM 27-13-34. PERFORMED FCC 2 RTS, ALL TESTS PASSED. RECYCLED CB'S PER AMM 22-01-01. PERFORMED FCC 1 RTS, TESTS PASSED.Jul 20, 2023 · N513SN · Doug MD11F · Autopilot SystemSDR IPXA2023081693922Door Frame · gougedINSPECTION TYPE:3C*** MAJOR REPAIR *** MAIN CARGO DOOR FOUND FWD LOWER DOOR FRAME GOUGED AND CRACKED STA Y=624.625 .REPAIRED CRACKED LOWER FWD DOOR FRAME AT THE MAIN CARGO DOOR AT STA Y=624.625 IAW VTSAA EA 011-5230-01-B0045 I/R, UPS EO MD11-5230-87782-A DATEDJul 19, 2023 · N274UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2023081093870Hinge Bracket · corrodedINSPECTION TYPE:4CL/H WING I/B FLAP SIDE O/B HINGE BRACKET #6 LUG BORE HAS CORROSION AT STA XW=254, YW=495.96.REPAIRED CORRODED HINGE BRACKET AT THE L/H WING I/B FLAP O/B HINGE #6 LUG BORE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0052 I/R AND UPS EO Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023081093869Hinge Bracket · corrodedINSPECTION TYPE:4CL/H WING I/B FLAP SIDE O/B HINGE BRACKET #7 LUG BORE HAS CORROSION AT STA XW=254, YW=495.96.REPAIRED CORRODED HINGE BRACKET AT THE L/H WING I/B FLAP SIDE O/B HINGE BRACKET #7 LUG BORE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0052 I/Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080993859Flap · corrodedINSPECTION TYPE:4CL/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE HAS CORROSION AT STA XW=486.403.REPAIRED CORRODED HINGE AT THE L/H WING O/B FLAP SIDE I/B HINGE #6 LUG BORE AT STA XW=486.403 IAW VTSAA EA 011-5740-01B0061 I/R AND UPS EO MD11-5750-87789-A DATED 08Jul 19, 2023 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023072893757Angle · crackedINSPECTION TYPE:4C#3 PYLON UPPER WIRE HARNESS SUPPORT HAS A CRACKED ANGLE AT THE AFT SIDE ABOVE PRECOOLER.REMOVED, FABRICATED AND REPLACED ANGLE AT THE #3 PYLON AT THE AFT SIDE ABOVE PRECOOLER IAW SRM 54-05-41 AND DWG AUB7564. (MINOR)Jul 19, 2023 · N284UP · Doug MD11F · Nacelle/Pylon StructureSDR IPXA2023072893756Bracket · crackedINSPECTION TYPE:4CCAC COMP. RADIO RACK SHELF AT O/B LOWER SIDE IF SHELF JUST O/B OF THE FLASHER TIMING UNIT HAS A CRACKED BRACKET.REMOVED, FABRICATED AND REPLACED BRACKET AT THE CAC COMP. JUST O/B OF THE FLASHER TIMING UNIT IAW SRM 51-53-01 AND DWG AAN7185. (MJul 19, 2023 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2023071993695Frame · gougedINSPECTION TYPE:N/A*MAJOR REPAIR* DAMAGE ON FRAME STA 535 BETWEEN S32R - S33RREAPIRED IAW EO# MD11-5330-87120-B.Jul 19, 2023 · N289UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2023071993694Skin · crackedINSPECTION TYPE:N/A*MAJOR REPAIR* RT SIDE AIR CONDITIONING DOOR JAMB CORNEWR SKIN CRACKEDREPAIRED IAW EO# MD11-5330-87120-BJul 19, 2023 · N289UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2023081293882Skin · corrodedINSPECTION TYPE:C3*** MAJOR REPAIR *** MAIN CABIN AFTER FLOOR PANEL REMOVAL FOUND CORROSION AT THE CENTER WING SKIN AT STRINGER #15 L/H TUNNEL BETWEEN STA XCW=97,XCW=103.REPAIRED CORRODED SKIN AT THE CENTER WING UPPER SKIN AREA AT STRINGER #15 L/H TUNNEL BETWEJul 18, 2023 · N274UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2023081093872Tee Angle · corrodedINSPECTION TYPE:3CR/H WING I/B FLAP LOWER SURFACE SKIN BULGING O/B OF VANE SPRING CARTRIDGE.REMOVED, FABRICATED AND REPLACED TEE ANGEL AT THE R/H WING I/B FLAP LOWER SURFACE O/B OF VANE SPRING CARTRIDGE IAW DWG ARC2493 AND SRM 51-31-01 (MINOR)Jul 18, 2023 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2023080593806Tee Angle · crackedINSPECTION TYPE:4CFWD CARGO COMPARTMENT HAS A CRACKED T-CLIP BRACKET AT FS 6-60 LBL 55 ON AFT SIDE OF FLOOR BEAM.REMOVED, FABRICATED AND REPLACED CRACKED T-CLIP AT THE FWD CARGO COMPARTMENT AT FS 6-60 LBL 55 ON AFT SIDE OF FLOOR BEAM IAW SRM 51-33-01. (MINOR)Jul 18, 2023 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2023080393790Unknown · crackedINSPECTION TYPE:3CCENTER WING LOWER AUX L/H STRINGER 52 SPLICES REPAIR C AND Z HAS A CRACKED AT STA XCW=64.REMOVED, FABRICATED AND REPLACED CRACKED SPLICES REPAIR AT THE CENTER WING LOWER AUX L/H STRINGER 52 IAW SRM 57-10-03 FIG 201 REPAIR 1. (MAJOR)Jul 18, 2023 · N274UP · Doug MD11F · Fuselage Structure (General)SDR IPXA2023071993691Light · inoperativeEMERGENCY LIGHTS REQUIRES DEFERRAL REF ITEM 1 ABOVE. ITEM DEFERRED PER MEL 33-50-4 M 810483 ASSIGNED. PLACARD INSTALLED.L1 DOOR CEILING PANEL REPAIRED. C/W REF M810482 REACTIVATED EMERGENCY LIGHTING SYSTEM. REVERSE DMP 33-50-4 SYSTEM. OPS CHECK OK. CLEARS M810Jul 18, 2023 · N258UP · Doug MD11F · Emergency LightingSDR IPXA2023071993690Door · inoperativeL1 DOOR REQUIRES DEFERRAL. REF ITEM 1 ABOVE. ITEM DEFERRED PER MEL 52-10-3-1-2-1-2. M810484 ASSIGNED. PLACARD INSTALLED.REF LOG PAGE 610079 ITEM 1 FOR REPAIR. L1 SLIDING CEILING PANEL REACTIVATED IAW MD-11 AMM 25-23-23-400-801. ACCOMPLISHED PERMANENT REPAIR. TJul 18, 2023 · N258UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023071993692Door · inoperativeL1 DOOR HAS CEILING PANEL DAMAGE. PANEL REMOVED AND REPLACED IN FPM ITEM DEFERRED PER EO MD11-2520-87659-A D 810482 ASSIGNED.ACCOMPLISHED PERMANENT REPAIR IAW MD-11 SRM 51-71-00-06-0 STEP 20 C. REACTIVATED SLIDING CEILING PANEL ASSY IAW MD-11 AMM 25-23-23-400Jul 18, 2023 · N258UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202307181232Skin · noneEXISTING REPAIR FOUND AT LEFT HAND WING DROOPED LEADING EDGE UPPER SKIN APPROXIMATELY STATION XDLE 320. EXISTING REPAIR AT LEFT HAND WING DROOPED LEADIING EDGE UPPER SKIN APPROXIMATELYSTATION XDLE 320 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 5Jul 18, 2023 · N643FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2023081693923Unknown · crackedINSPECTION TYPE:3C*** MAJOR REPAIR *** RCB WALL INSIDE #2 INSPECTION HOLE R/H SIDE HAS A CRACKED GOING FROM NUT-PLATE TO NUT-PLATE AT STA Y=489.12 AND X=73.340.REPAIRED CRACKED RCB WALL INSIDE #2 INSPECTION HOLE AT STA Y=489.12 AND X=73.340 IAW VTSAA EA 011-53Jul 17, 2023 · N274UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2023081093871Stiffener · crackedINSPECTION TYPE:3CAFT CARGO COMP. AT STA 1841 FLOOR BEAM AREA AT LONGERON 47R HAS A STIFFENER WITH A CRACKED.REMOVED, FABRICATED AND REPLACED STIFFENER AT THE AFT CARGO COMP. STA 1841 FLOOR BEAM AREA AT LONGERON 47R IAW DWG AGA7170 AND SRM 51-33-01. (MINOR)Jul 17, 2023 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2023072893754Bracket · crackedINSPECTION TYPE:3CCAC COMP. HAS A CRACKED BRACKET AT THE RADIO RACK LOCATED AT UPPER FWD I/B SIDE OF RADIO RACK.REMOVED, FABRICATED AND REPLACED BRACKET AT THE CAC COMP. UPPER FWD I/B SIDE OF RADIO RACK IAW SRM 51-33-01 AND DWG AAN7180. (MINOR)Jul 17, 2023 · N274UP · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA202307171231Skin · noneEXISTING REPAIR FOUND AT LEFT HAND WING DROOPED LEADING EDGE UPPER SKIN APPROXIMATELY STATION XDLE 330. EXISTING REPAIR AT LEFT HAND WING DROOPED LEADING EDGE UPPER SKIN APPROXIMATELY STATION XDLE 330 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-Jul 17, 2023 · N643FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2023080493795Doubler · crackedINSPECTION TYPE:4C*MAJOR REPAIR* R/H WING L/E HAS A BEADED DOUBLER THAT IS CRACKED JUST I/B OF SLAT TRACK #12 AT STA XOS=755.REPAIRED CRACKED BEADED DOUBLER AT THE R/H WING L/E JUST I/B OF SLAT TRACK #12 AT STA XOS=755 IAW SRM 57-40-02 FIG. 205 REPAIR 15. (MAJJul 16, 2023 · N284UP · Doug MD11F · Leading Edge DevicesSDR IPXA2023080193769Stringer · crackedINSPECTION TYPE:4CR/H WING L/E LWR STRINGER HAS A CRACKED ON EXISTING DOUBLER JUST O/B OF SLAT TRACK #14 AT STA XOS=906.5607.REPAIRED EXISTING CRACKED DOUBLER AT THE R/H WING L/E LWR STRINGER JUST O/B OF SLAT TRACK #14 STA XOS=906.5607 IAW SRM 57-40-03 FIG.201Jul 16, 2023 · N284UP · Doug MD11F · Wing, Longeron/StringerSDR FDEA202307161227Tire · failedTIRE PRESSURE LOW ALERT AFTER EXTENDING THE GEAR. NUMBER 8 TIRE READ APPROXIMATELY 160 WHEN CHECKED ON SYSTEM SCREEN. APPROXIMATELY IN THE FLAIR, TIRE FAILURE ALERT ANNOUNCED. TOWER CONFIRMED FLAT TIRE AFTER RUNWAY EXIT. REMOVED AND REPLACED NUMBER 8 Jul 16, 2023 · N528FE · Doug MD11F · TireSDR IPXA2023081593918Skin · corrodedINSPECTION TYPE:3C*** MAJOR REPAIR *** MAIN CABIN AFTER REMOVAL OF FLOOR PANEL ON CENTER WING AREA FOUND CORROSION ON L/H TUNNEL AT STA 1239, XCW= 101.8 AND XCW= 108.REPAIRED CORRODED AREA AT THE CENTER WING L/H TUNNEL AT STA XCW=101.8 AND XCW=108 IAW VTSAA EAJul 15, 2023 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2023081493899Skin · corrodedINSPECTION TYPE:4CMAIN CABIN AFTER REMOVAL OF FLOOR PANEL CENTER WING AREA FOUND CORROSION AT STRINGER #8 BETWEEN STA XCW=101.8, XCW=108.REPAIRED CORRODED SKIN AREA AT THE CENTER WING ON MAIN CABIN AT STRINGER #8 BETWEEN STA XCW=101.8, XCW=108 IAW VTSAA EA 01Jul 15, 2023 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2023071493659Door · inoperativeL1 DOOR WILL NOT REMAIN CLOSEDACCOMPLISHED OPS CHECK OF L1 DOOR REF AMM 52-11-02 OPS CHECK GOOD OK FOR SERVICEJul 13, 2023 · N257UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2023071393657Handle · inoperativeINSPECTION TYPE:NAF.O. OVERHEAD HADLE INOP SCREW STRIPPEDRESERVED HANDLE ON FO'S OVERBD REF AMM 20 00 00/001 STARTED ILLEG OPS CHECK GOODJul 13, 2023 · N273UP · Doug MD11F · Emergency EquipmentSDR IPXA2023071393655Door · inoperativeL1- MAIN ENTRY DOOR/SLIDES - ALL CARGO CONFIG DOORS L1/R1 [EXTENDED OVERWATER] USE R1 DOOR. L1 DOOR DEFERRED PER MEL 52-10-3-1-2-1-2 / M810363 PLACARD INSTALLED.R&R FORWARD PASSENGER DOOR LOCK PIN RELEASE SOLENID REF AMM 52-10-06 OP CHECK GOOD AT THIS TIME THIJul 13, 2023 · N289UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202307131212Skin · crackedMAIN DECK CARGO COMPARTMENT - CRACK (APPROXIMATELY 0.5 INCH) FOUND ON L3 DOOR FORWARD JAMB LOWER WEB BETWEEN STATION 1250.750 AND STATION 1256.750 LONGERON 26 LEFT TO 27 LEFT. MAIN DECK CARGO COMPARTMENT - CRACK AT L3 DOOR FORWARD JAMB LOWER WEB BETWEEN Jul 13, 2023 · N643FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202307131211Skin · crackedCRACK (APPROXIMATELY 1 INCH) FOUND ON THE FUSELAGE SKIN AT THE RIGHT AIR- CONDITIONING COMPARTMENT UPPER AFT CORNER OF THE DOOR CUTOUT. FUSELAGE - CRACK (APPROXIMATELY 1 INCH) FOUND ON THE FUSELAGE SKIN AT THE RIGHT AIR- CONDITIONING COMPARTMENT UPPER AFT COJul 13, 2023 · N643FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA202307131210Unknown · unknownWHILE ACCOMPLISH AN INTERAL BORESCOPE INSPECTION OF NUMBER 8 SLAT FOR RIB DAMAGE AT LOOSE RIVETS AREA (REFERENCE SNRM N00974) FOUND RIB CRACK AT APPROXIMATELY STATION XOS 1141.220.Jul 13, 2023 · N643FE · Doug MD11F · Leading Edge DevicesSDR FDEA202307131209Rib · crackedWHILE ACCOMPLISH AN INTERNAL BORESCOPE INSPECTION OF LEFT HAND WING NUMBER 8 SLAT FOR RIB DAMAGE AT LOOSE RIVETS AREA (REFERENCE SPECIAL NONROUTINE MAINTENANCE FORM N00974) FOUND RIB CRACK AT APPROXIMATELY STATION XOS 1141.220. LEFT WING NUMBER 8 SLAT CRACJul 13, 2023 · N643FE · Doug MD11F · Leading Edge DevicesSDR FDEA202307131208Skin · gougedRIGHT HAND NUMBER 3 SLAT LOWER SKIN AT APPROXIMATELY STATION XOS 480 FOUND WITH SCRATCHED MARK. CARRIED OUT REPAIR AS PER EA #1-5750-T0375227 PART 1 TITLE: WINGS - FLIGHT SURFACES - RHW #3 SLAT ASSY - INNER SKIN SRM SPLICE REPAIR BETWEEN XOS 455.085 AND XJul 13, 2023 · N643FE · Doug MD11F · Leading Edge DevicesSDR FDEA202307131207Rib · unknownADDITIONAL WORK REQUIRED - LEFT HAND NUMBLER 8 SLAT INNER RIB AT STATION XOS 1010.495 FASTENER HOLE FOUND ELINGATED AFTER LOWER SKIN REMOVAL. LEFT WING NUMBER 8 SLAT STATION XOS 1010.403 INNER RIB WITH ELONGATED HOLE CARRIED OUT REPAIR AS PER EA # 1-5750-Jul 13, 2023 · N643FE · Doug MD11F · Leading Edge DevicesSDR FDEA202307121452Stanchion · corrodedFWD CARGO COMPT, STA 6-73.5 RBL 9, AFT BULKHEAD, VERTICAL STANSION HAS CORROSION OUT OF LIMITS ON VERTICAL LEG AT NUTPLATE REPAIRED ATANCHION PER EA# 1-5310-T0375475 TITLE: FUSELAGE-FORWARD INTERMEDIATE- FORWARD CARGO COMPARTMENT AFT BULKHEAD, STANCHION AT Jul 12, 2023 · N597FE · Doug MD11F · Fuselage Main, StructureSDR IPXA2023071393653Door · inoperativeINSPECTION TYPE:NACREW DOOR LOUVRE PANEL DETACHED FROM DOORRESECURED AND INSTALLED FLIGHT COMPARTMENT CREW DOOR LOUVRE PANEL IAW AMM 52-54-02-400-801. NO DEFECTS NOTEDJul 12, 2023 · N260UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202307121204Unknown · unknownPANEL 345BB DELAMED. REPAIRED DELAMINTED PANEL 345BB PER SRM 51-62-01-0G PG.44 REPAIR "J" STEP 1-9Jul 12, 2023 · N597FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202307121202Actuator · unknownCLIMBING THROUGH 4000 FEET CABIN SEL MAN FOLLOWED BY CABIN RATE LEVEL 1. CABIN PRESSURE WOULD NOT STABILIZE INITIALLY IN MANUAL MODE. CABIN WAS INDICATING -5000 FEET . RETURNED TO INDY AND GOT THE CABIN TO STABILIZE ON DOWNWIND MANUALLY. SHGN 12JUL23 04:0Jul 12, 2023 · N621FE · Doug MD11F · Pressure Regulator/Outflow ValveSDR IPXA2023071293648Door · inoperativeL CREW DOOR WILL NOT CLOSE LOCK FROM SWITCH ON INSIDE PANEL. DEFERRED PER MEL 52-10-3-1-2-1 M 810294 ASSIGNEDCLOSED DEFERRAL DUE TO MEL REF. CHANGE REVISION. REOPENED DEFERRAL ON LP 636347/1 M810363.Ï¿½M810363: Ï¿½R&R FORWARD PASSENGER DOOR LOCK PIN RELEASE SJul 11, 2023 · N289UP · Doug MD11F · Passenger/Crew Doors
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