Boeing MD-11F
Service difficulty reports · 31,317
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202203200603Stiffener · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 STIFFENER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRISDR FDEA202203200602Doubler · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-0-OG. RIB DOUBLER FABRICATEDSDR FDEA202203200601Former · crackedLEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 FORMER FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2930SDR FDEA202203200600Skin · crackedLEFT HAND WING # 8 SLAT INTERIOR SURFACE FOUND CRACK. LEFT HAND WING #8 SLAT INTERIOR SURFACE AT STATION XOS 1146.814 CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-T0367711 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202203190607None · nonePDIS 620 21-30 7092 19MAR22 MEM FACT U ON DEPARTURE OUT OF KMEM AT APPROX 2000 FT AS WE BEGAN OUR CLIMB WE GOT A LEVEL 1 CABIN RATE ALERT. OUTFLOW VALVE WAS CLOSED AND AVIONICS FAN WENT TO OVERRIDE. AS WE CONTINUED TO CLIMB THE CABIN ALT CONSDR FDEA202203190599None · nonePDIS 595 24-40 5629 19MAR22 ANC FACT U ON SHUTDOWN, WHILE TRANSFERRING TO EXTERNAL POWER, DEU 3,4,AND 5 WENT BLANK, MCDU 2 AND 3 WENT BLANK CIRCUIT BREAKERS STANDBY ALTIMETER VIBRATOR, AVIONICS COMPARTMENT EXHAUST FAN, CAC FAN 1,2, AND 3, AVISDR FDEA202203190598Adc · failedAFTER TO AT APPROX 6000 FT, WE GOT ALT DISAGREE WARNING ON BOTH PFDS. INITIALLY BOTH ALT TAPES WERE AT MOST 20 FT OFF FROM EACH OTHER. AS WE CONTINUED TO CLIMB UP TOSDR FDEA202203190597Mfc · failedAPPROXIMATELY T/O PLUS 1 HOUR, RECEIVED A LEVEL 1 AIR SYS 2 OFF ALERT. NOTED A RED MANF LIGHT ON R&R ESC PER MM 21-08-01-4, AIR SYSTEM TEST PASS, RAN ALL 3 ENGSDR FDEA202203190588Doubler · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 670 BEADED DOUBLER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 670 BEADED DOUBLER CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAISDR FDEA202203180585Proximity Sensor · inoperativeAFTER TAKEOFF WITH GEAR HANDLE IN THE UP POSITION, ALL RED GEAR LIGHTS REMAINED ILLUMINATED ON THE PRIMARY AND SECONDARY INDICATORS. PER QRH INSTRUCTIONS, LOWERED GEAR AND GOT ALL GREEN INDICATIONS; RAISED GEAR AND RECEIVED ALL NORMAL INDICATIONS. REMOVSDR FDEA202203180584Computer · failedELEVATOR CONTROLLER FEEL LOST AT FL 390 WITH LOSS OF FO AIRSPEED. PERFORMED ORH PROCEDURE UNRELIABLE AIRSPEED FO. REMOVED AND REPLACED #2 CENTRAL AIR DATA COMPUTER IAW MD-11 AMM 34-16-01-4 OPS CHECK NORMAL, PERFORM SDR FDEA202203170537Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE (#3 HOLE) REWORKED AND FOUNDSDR FDEA202203170561Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-0SDR FDEA202203170560Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 SDR FDEA202203170559Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD SPOT FACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM57- 44-08 AND EA.#: 1-5SDR FDEA202203170558Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE (HOLE #7) REWORKED AND FOUNDSDR FDEA202203170557Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE (HOLE #7) REWORKED AND FOUND ESDR FDEA202203170556Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLSDR FDEA202203170548Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 ASDR FDEA202203170547Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08SDR FDEA202203170546Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND SDR FDEA202203170545Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.# : 1-57SDR FDEA202203170544Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-575SDR FDEA202203170541Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750SDR FDEA202203170539Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T0SDR FDEA202203170538Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T03SDR IPXA2022031780220Bottle · noneL1 DOOR BOTTLE NOT IN GREEN BAND.C/W PRESSURIZATION OF THE PASSENGER DOOR PNEU STORAGE SYSTEM AS PER MM CHPTR 12-25-04-600-801 CURRENTLY SERVICED TO CENTER OF GREEN BAND.SDR IPXA2022033080667Former · crackedINSPECTION TYPE:C1L/H O/B WING L/E HAS A FORMER THAT IS CRACK JUST I/B OF THE #9 SLAT TRACK.REMOVED, FAB, REPLACED CRACK FORMER IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)SDR IPXA2022032780562Doubler · crackedINSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 537.2 TO 547.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 537.2 TO 547.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR FDEA202203160532Floorboard · delaminatedMAIN DECK AFT FLOOR BOARD PANEL 283EF DELAM. FABRICATED NEW FLOOR BOARD PANEL# 283EF, AFA3163 PER FEDEX DRWG SRZ-25-005.SDR FDEA202203160531Floorboard · damagedMAIN DECK- CENTER FLOOR BOARD IN BETWEEN THE 76-106 RBL AND STA 1159 AND 6-70 HAS MULTIPLE DAMAGED AND CORRODED INSERTS. FABRICATED NEW FLOOR BOARD BETWEEN THE 76-106RBL AND STA 1159 AND 6-70 PER SRZ- 25-005.SDR FDEA202203160529Floorboard · damagedMAIN DECK- CENTER FLOOR BOARD IN BETWEEN THE 76-106RBL AND STA 1256-1301 HAS MUTLIPLE DAMAGED AND CORRODED INSERTS, FABRICATED NEW MAIN DECK FLOOR BOARD BETWEEN THE 76-106RBL AND 1256-1301 PER FEDEX DRWG SRZ-25-005SDR IPXA2022031680180Sensor · faultedECOND FLIGHT IN A ROW THAT DURING CLIMB OUT RECIEVED A LVL 1 CARGO FWD FLO DISAG.R/R FWD CARGO FLOW SENSOR PER 21-27-02 OPS CHECK GOOD. NO DEFECT NOTED.SDR IPXA2022031680199Light · inoperativeEMER LT BAT 1 LO. REMOVED AND REPLACED EMERGENCY LIGHTING PWR SUPPLY REF 33-51-01 TEST PASSED.SDR IPXA2022031680191Fan · noneINSPECTION TYPE:NADURING FLIGHT LEVEL 1 AVNCS FAN OVRDTROUBLESHOT PER FIM 21-26-04-00 AND 021-26-06-00 SYSTEM OK FOR SERVICE NO FURTHUR FAULTS NOTED.SDR FDEA202203150944Seat Track · corrodedMAIN DECK SEAT TRACK INB LOBE LOCATED BETWEEN STA 1801 AND 1821 AT LBL74 HAS EXFOLIATION CORROSION. NEW SEAT TRACK SECTION PN:AFA7789-543 WAS REPLACED FROM STA 1771 TO 1887 AT LBL 75.25. THIS PRETAINS THE DAMAGED SECTIONS OF SEAT TRACK ON THIS NON-ROUTINE.SDR FDEA202203150943Seat Track · corrodedMAIN DECK SEAT TRACK OUTB LOBE LOCATED AT STA 1841 AT LBL74 HAS EXFOLIATION CORROSION. NEW SEAT TRACK SECTION PN:AFA7789-543 WAS REPLACED FROM STA 1771 TO 1887 AT LBL 75.25. THIS PRETAINS THE DAMAGED SECTIONS OF SEAT TRACK ON THIS NON-ROUTINE. SEE NON-ROSDR FDEA202203150942Seat Track · corrodedMAIN DECK SEAT TRACK INB LOBE AT STA 1782 LBL 74 HAS EXFOLIATION CORROSION NEW SEAT TRACK SECTION PN:AFA7789-543 WAS REPLACED FROM STA 1771 TO 1887 AT LBL 75.25. THIS PRETAINS THE DAMAGED SECTIONS OF SEAT TRACK ON THIS NON-ROUTINE. SEE NON-ROUTINE N00068 WSDR FDEA202203150513Indicator · failedDURING POST FLIGHT CHECK FOUND THE R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP. REMOVED AND REPLACED R1 DOOR INDICATOR ASSEMBLY PER MM 25-61-04-4. OPS CHECK NORMAL.SDR IPXA2022031680179None · noneINSPECTION TYPE:NAAFTER TAKEOFF - LEVEL 1 CRG FLO FWD DISAGPERFORMED OP CHECK OF FWD CARGO COMP VENTILATION SYSTEM IAW AMM 21-27-09, OP CHECK NORMAL, NO FAULTS NOTED AT THIS TIME.SDR IPXA2022031680168Fan · noneINSPECTION TYPE:NALEVEL `1 ALERT 'AVIONICS FAN OVRD' ON WHEN POWER REDUCED FOR DESCENT @ FL 340 DIFF PRESS SHOWN 8.1 PSIFOUND APPROX 2 FEET OF MAIN CARGO DOOR SEAL OUT OF RETAINER. RESEATED SEAL. OPS CK GOOD. REF MD11 52-00-00-400--801. DISLOCATED SEAL IS AT FSDR FDEA202203140498Skin · crackedRIGHT HAND WING INBOARD FIXED LEADING EDGE STATION XIS247 UPPER SURFACE CRACKED. RIGHT HAND WING INBOARD FIXED LEADING EDGE STATION XIS247 UPPER SURFACE CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 8 FIGURE 201. REPAIR CLASSIFIED AS MSDR IPXA2022032180309Stiffener · crackedINSPECTION TYPE:1CRT MLG W/W 3RD STIFFENER CRACK AT LOWER END O/B AFT.REMOVED AND REPLACED CRACK STIFFENER IAW SRM 51-35-01 AND 51-35-02 (MINOR).SDR IPXA2022031580143None · noneINSPECTION TYPE:NAIN CRUISE FLIGHT AT FL 320 THE LEVEL 1 " AVNCS FAN OVRD " ANNUNCIATED.C/W FRM/FIM 21-26-04-00 TO BLK 7 NO FAULTS NOTED AND C/W 21-26-02-00 TO BLK 4 " SYSTEM OK ". MESSAGE EXTINGUISHED ON DESCENT, COULD NOT DUPLICATE.SDR IPXA2022031580140None · noneINSPECTION TYPE:NAFIRST OFICER IS UNABLE TO READ THE SLIDE RAFT PRESSURE ON L1 DOOR.ADJUSTED SLIDE SO THAT GAUGE IS VISABLE IN WINDOW W/REF TO M/M 25-61-15.SDR FDEA202203140499None · noneFORWARD CABIN - FLOOR PANEL #241GF FOUND DELAMINATED AT STA STATION 795 TO STATION 899. FORWARD CABIN FLOOR PANEL #241GF AT STATION 795 TO STATION 899 REMOVED AND REPLACED AS PER AMM 53-21-04. FLOOR PANEL FABRICATED AS PER FEDEX DRAWING SRZ-25- 005 REVISSDR IPXA2022031480076Fan · noneINSPECTION TYPE:NADURING DESCENT, LEVEL 1 "AVNCS FAN OVRD" ALERT. REPEAT FROM PREVIOUS TWO LOGPAGES.R&R OUTFLOW VALVE ASSY DUE TO TORN SEAL IAW AMM 21-31-01SDR FDEA202203130493Frame · noneAGING AIRCRAFT - EXISTING REPAIR FOUND ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 24 LEFT HAND. EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 24 LEFT HAND EVALUATED AND FOUND EXISTING REPAIR ANGLES WITH DEEPSDR FDEA202203130492Frame · noneAGING AIRCRAFT - EXISTING REPAIR FOUND ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 19 LEFT HAND. EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 19 LEFT HAND EVALUATED AND FOUND EXISTING REPAIR ANGLES WITH DEEPSDR IPXA2022032880588Support Angle · corrodedINSPECTION TYPE:1CAFT CARGO FLOOR BEAM SUPPORT ANGLE CORRODED AT X=3,Y=1841.REPAIRED CORRODED AFT CARGO FLOOR BEAM SUPPORT ANGLE IAW VT-SAA EA 011-5310-01-A9512 REV I/R AND UPS EO MD11-5310-83234-A BY P.LAU (AR-830967) DATED 03/25/2022 (MAJOR).
Back to Boeing MD-11F