Boeing MD-11F
Service difficulty reports · 31,320
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 FDEA201810062798Seat Track · crackedAGING AIRCRAFT-EXISTING REPAIR AT MAIN DECK CARGO - SEAT TRACK STATION 625 TO 665 X=27.5 LEFT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO -SEAT TRACK STATION 625 TO STATION 665, X=27.5 LEFT HAND EVALUATED AND FOUND LOWER FLANGE CRACKED. SEAT TRACK AT STATIONSDR FDEA201810062804Door Frame · crackedFUSELAGE NR 3 AIR CONDITIONING COMPARTMENT AFT UPPER DOOR JAMB FOUND CRACKED AS MARKED. DOOR JAMB REPAIR PER SRM 53-20-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.SDR FDEA201810062803Sensor · faultySLAT DISAG LEVEL 2 ALERT AFTER SLAT EXTENSION ON APPROACH. INTERMITTENT ALERT FROM FLAPS 28 THROUGH TOUCHDOWN. CALL TO MOCC ON SATCOM INDICATED THAT IT WAS A SENSOR PROBLEM AS REPORTED BY ACFT TELEMETRY. REMOVED AND REPLACED LT NR 4 SLAT POSITION SENSOR A P/N SDR FDEA201810062801Doubler · crackedLEFT HAND WING LEADING EDGE AT STATION XOS 645 FOUND BEADED DOUBLER CRACKED AS MARKED. LEFT HAND WING- LEADING EDGE AT STATION XOS 645 BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.SDR FDEA201810062800Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 635 X=-8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665 X=-8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201810062799Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 635 X= 8.5 FOUND CRACKED AS MARKED. MAIN DECK FLOOR, CRACKED SEAT TRACK AT STA 635 X= 8.5, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201, REPAIR 1. REPAIR CLASDR FDEA201810052791Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 5-120 X= 27.5 FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5SDR FDEA201810052790Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1129 X= 8.5 FOUND CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLSDR FDEA201810042784Skin · crackedL/H WING L/E SKIN CRACK AT AXIS 247-0280 EA 1-5730-T0342552 CUT OUT DAMAGE AND INSTALLED L/E DOUBLER.SDR FDEA201810042776Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND BEYOND REWORK LIMIT AS PER CMM57-44-09. NEW REPAIR SHIM FABRICATED AND INSTALLED PER CMM57-44-09 AND EA NR 1-5750-73336C PT 3 STEP 1. REPASDR IPXA2018100534707Warning Message · false activationEMERGENCY LIGHT BATTERY 1 LOW LEVEL 1 ALERT DURING AN EMERG LIGHT TEST. REVERSED DMP 33-50-4. COMPLIED WITH FIM 33-51-00-101, & AMM 33-51-00, EMERGENCY LIGHTS CHECKED GOOD.SDR FDEA2018100542789Container · fireMDIS 619 05-50 5502 04OCT18 MEM OPEN U DURING ONLOAD OF CENTER CARGO, A FIRE WAS DISCOVERED EMANATING FROM A LD-3 CONTAINER, FIRE SERVICES WERE SUMMONED. IN AN ATTEMPT TO SUPPRESS THE FIRE. WATER WAS APPLIED TO THE CONTAINER, THUS CONTAMINATING THE COMPLETE SDR FDEA2018100542784Skin · crackedLT WING L/E SKIN CRACK AT AXIS 247-0280 EA 1-5730-T0342552 CUT OUT DAMAGE AND INSTALLED L/E DOUBLER.SDR IPXA2018100594664Lamp · inoperativeL1 DOOR EVAC SLIDE REMOTE PRESSUTE PTT LIGHT INOPERATIVE. REPLACED THE LAMP, OPS NORMAL IAW AMM 25-61-04.SDR IPXA2018101094860Doubler · corrodedLOWER VHF ANTENNA DOUBLER WAS CORRODED AT BS 1721. REMOVED AND REPLACED THE ANTENNA DOUBLER BETWEEN BS 1721 - 1740, LONGERON 51L - 51R IAW SRM 51-31-01, 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018101094859Finger Doubler · corrodedINTERNAL FINGER DOUBLER WAS CORROSION AT BS 1721. REMOVED AND REPLACED THE FINGER DOUBLER BETWEEN BS 1721 - 1740, LONGERONS 50L & 50R IAW SRM 51-31-01, 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018101034891Longeron · corrodedLONGERON 52 WAS CORRODED AT BS 1721. REMOVED AND REPLACED THE LONGERON, BETWEEN BS 1712 - 1755 IAW SRM 53-00-05, REPAIR 1, FIGURE 201, & 202. MAJOR.SDR FDEA2018100532773Piston · leakingUPON ARRIVAL FOUND L GEAR NR 6 BRAKE AREA ON FIRE, FOUND EVIDENCE OF HYD LEAK FROM NR 6 BRAKE PISTON. ALL TIRES PRESSURE ARE NORMAL, BRAKES TEMP ARE NORMAL ALSO. REMOVED AND REPLACED NR 6 BRAKE AS PER AMM 32-43-20-4 AND TESTED NORMAL PER AMM 32-46-00-5, NO LEASDR IPXA2018100594658Indication Sys · no testR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYSTEM WILL NOT TEST. REPLACED L1 DOOR EMERGENCYASSIST BOTTLE DRIVE CHAIN IAW CMM 52-11-09. OPS CHECKED GOOD.SDR IPXA2018100534704Control Panel · malfunctionedFIRE WARNING TEST CONTINUOUSLY ON. R & R THE APU CONTROL PANEL IAW AMM 49-04-01-000-801, AND 49-04-01-400-801. OPS TESTED IAW 49-10-00-700-801, OPS NORMAL.SDR FDEA201810022763Channel · crackedRIGHT HAND WING LEADING EDGE FORMER AT STATION XOS 629 FOUND CRACK AS MARKED. CRACKED FORMER REMOVED AS PER SRM 51-35-01-0G. NEW FORMER (CHANNEL) FABRICATED AS PER DRAWING ARB2925 REVISION F AND INSTALLED AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR PER SDR FDEA201810022762Channel · crackedRIGHT HAND WING LEADING EDGE FORMER AT STATION XOS 584 FOUND CRACK AS MARKED. CRACKED FORMER REMOVED AS PER SRM 51-33-01-0G. NEW FORMER (CHANNEL) FABRICATED AS PER DRAWING ARB2931 REVISION H AND INSTALLED AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER SDR FDEA201810022761Doubler · crackedRIGHT HAND WING LEADING EDGE DOUBLER AT STATION XOS 667 FOUND CRACK AS MARKED. CRACKED DOUBLER REMOVED AS PER SRM 51-33-01-0G. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954 REVISION K AND INSTALLED AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA201810022760Doubler · crackedRIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 669 FOUND CRACKED AS MARKED. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STATION XOS 669 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201810022759Doubler · crackedRIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STATION XOS 614 FOUND CRACKED AS MARKED. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STATION XOS 614 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018100394638Bracket · crackedRT WING T/E BRACKET WAS CRACKED, BELOW THE NR 1 SPOILER, INBD MOUNT. REMOVED AND REPLACED THE BRACKET IAW SRM 51-33-01. MINOR.SDR FDEA201809302746Support Frame · corrodedDURING REPLACEMENT OF RT MLG RETRACT SUPPORT FRAME LOWER TWO MOUNT BOLT PLI WASHER FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED, FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1)(A)(1) REPAIR 1. NEW REPAIR BUSHING FABRICATED AND INSSDR FDEA201809302749Support Frame · corrodedDURING REPLACEMENT OF LT MLG RETRACT SUPPORT FRAME LOWER FWD MOUNT BOLT PLI WASHER, FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1) (A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTSDR FDEA201809302748Support Frame · corrodedDURING REPLACEMENT OF RT MLG RETRACT SUPPORT FRAME LOWER AFT MOUNT BOLT PLI WASHER, FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1) (A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTSDR FDEA201809302747Support Frame · corrodedAFTER REMOVED RT MLG RETRACT SUPPORT FRAME FOR REPAIR, FOUND UPPER AFT BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1)(A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5740-SDR FDEA201809282724Warning System · activatedAFTER TAKE OFF WE RECEIVED LEVEL 1 BRAKE TEMP DIFF ALERT. BRAKE 2 INDICATED PEAK TEMP OF 503 DEGREES. ALL OTHER BRAKES WERE 150 DEGREES OR COOLER. REMOVED AND REPLACED BTMTPI IAW AMM 32-46-02-4 AS A PRECAUTION SINCE THERE IS HISTORY FOR OTHER BRAKE POSITIONSSDR IPXA2018100834816Attach Fitting · crackedFUEL LEAKING FROM THE RT WING TE, OTBD AILERON ACTUATOR ATTACH FITTING ON THE REAR SPAR WAS CRACKED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-33-01, FIG 2, PARA 6. MINOR.SDR FDEA201809272721Skin · corrodedFUSELAGE SKIN CORROSION AT STA 2122-2163 LONGERON 33R-35. COMPLY WITH EA 1-5310-T0342510 REV NR POS P1. COMPLIED WITH T1-5310-T0342510P1.SDR IPXA2018092634415Cable Assy · damagedL1 DOOR FWD DRIVE CABLE AND UPPER PULLEY COMPONENTS WERE DAMAGED. R & R THE L1 DOOR LOWER CABLE IAW 52-11-09. OPS CHECKED GOOD.SDR IPXA2018092634414Packing · leakingNR 1 ENGINE LEAKING FUEL FROM THE FUEL FILTER BOWL. REMOVED AND REPLACED THE PACKING ON THE FUEL FILTER BOWL COVER PLATE.SDR FDEA201809252680Power Supply · inoperativeEMER LT BAT 1 LO ON PREFLIGHT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY REF AMM 33-51-01-4. OPS CK SATISFACTORY.SDR FDEA201809252705Bracket · corrodedRIGHT WING OUTBD FLAP INBD (WING SIDE) CLEVIS FITTING HOLE BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-16. OVERSIZED BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED PER CMM57-44-16 AND EA 1-5740-130969A PT 2 STEPS 2, 2A SDR FDEA201809252704Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) FWD MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 6 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CSDR FDEA201809252703Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. SDR FDEA201809252702Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPSDR FDEA201809252701Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPASDR FDEA201809252700Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR SDR FDEA201809252699Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIESDR FDEA201809252698Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. REPAIR EVALUATED FOUND ACTUATOR ATTACHED I/B LUG SURFACE REMAINING THICKNESS 0.317" ACCEPTED PER SDR FDEA201809252697Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 AND EA 1-5750-73333C PT 3 STEP 1. SDR FDEA201809252696Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 AND EA 1-5750-73333C PT 3 STEP 1. ESDR FDEA201809252695Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) FWD MOUNT OUTBD HOLE BORE FOUND CORROSION. NR 6 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-73333C PT 3 STEP 1. EO 1-5750SDR FDEA201809252694Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-73333C PT 3 STEP 1. EO 1-5750-7-5002 RTSDR FDEA201809252693Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACH OUTBD LUG HOLE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2SDR FDEA201809252692Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD LUG HOLE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2
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