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 FDEA201701240244Clamp · out of positionAFTER TAKE OFF WITH AIR MANUAL AND ICING ANTICIPATED, ENGINE & WING ANTI-ICE WAS ON & ARMED. WHEN THE WING ANTI-ICE VALVE ATTEMPTED TO OPEN LEVEL 2 WING ANTI-ICE DISAGREE ILLUMINATED. NO LONGER IN ICING CONDITIONS, DESELECTED WING ANTI-ICE AND ALERT EXTINGSDR IPXA2017012513242Switch · failedL1 SLIDE FAILED TO TEST. R & R TEST SWITCH. OPS CHECKED NORMAL IAW AMM 25-61-00SDR FDEA201701230239Rib · crackedRIGHT WING L/E NR 6 SLAT HAS A CRACKED NR 7 RIB. REMOVED AND REPLACED THE SLAT IAW AMM 27-80-30-5.SDR FDEA201701230238Rib · crackedLEFT WING L/E SLAT NR 6 HAS A CRACKED RIB NR 6. THE RIB WAS REMOVED AND REPLACED IAW AMM 27-80-30-5.SDR IPXA2017013113514Skin · wornINSPECTION TYPE: 3C, FUSELAGE SKIN HAS DEEP FRETTING WEAR BETWEEN BS 1139 - 1168 AND LONGERONS 43 - 45L. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG. 201. (MAJOR)SDR IPXA2017013113513Skin · gougedINSPECTION TYPE: 3C, FUSELAGE SKIN HAS DEEP FRETTING WEAR BETWEEN BS 1139 - 1168 & LONGERONS 43 - 45R. REPAIRED IAW SRM 53-40-01 REPAIR 3 FIG. 201. (MAJOR)SDR IPXA2017012913383Skin · puncturedINSPECTION TYPE: 3C, TAIL CONE LOWER SKIN HAS A PUNCTURE AT BS 2224 - 2229. REPAIRED THE SKIN IAW EA 011-5350-01-A6597 AND EO MD11-5350-63071-A.SDR IPXA2017012313074Skin · crackedLEFT WING INBD FLAP 10, A .250 CRACK IN UPPER SKIN SURFACE 59 INCHES INBD OF OTBD EDGE AND 25.250 INCHES FWD OF TRAILING EDGE. REPAIRED IAW EO MD11-5750-63011-A.SDR IPXA2017020113572Lug · wornINSPECTION TYPE:3C, THE UPPER SURFACE OF THE LOWER TRACK LUG OF THE NR 1 ENGINE LT THRUST REVERSER HAS WEAR DAMAGE. REPAIRED THE THRUST REVERSER IAW EA 011-7830-01-A6598 REV. I/R, AND EO MD11-7830-63117-A.SDR IPXA2017012012979Door · intermittentL1 DOOR OPERATION IS INTERMITTANT. 50% OF THE TIME USING EITHER INTERIOR OR EXTERIOR SWITCHES RESULTS IN HEARING A RELAY ACTIVATE BUT NO DOOR OPERATION. COMPLIED WITH A ADJUSTMENT CHECK OF THE L1 DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06-830-801. OPS TESDR FDEA201701180223Start Valve · damagedSTART VALVE NR 2 ILLUMINATED DURING FLIGHT. REPLACED THE START CONTROL VALVE AND STARTER PRESSURE SWITCH IAW MM 80-12-03-4-2 AND MM 80-11-01-4-2. FOUND START CONTROL VALVE BUTTERFLY BROKEN. DURINING OPS CHECK OF THE NR 2 ENGINE FOR START CONTROL VALVE ANDSDR FDEA201701170212Seat Track · corrodedAFTER FLOOR PANEL REMOVAL, FOUND STA 1790, X=75 SEAT TRACK CORRODED AT FLOOR PANEL CONTACT AREA. CORROSION REMOVED AS PER SRM 51-21-01-0G AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. REPAIR CARRIED OUT PER SRM 53-00-52-2R FIGURE 20SDR FDEA201701170211Seat Track · corrodedFOUND BS 655, RBL 47 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, ALLOWABLE DAMAGE 1, FIGURE 101. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201701170210Seat Track · corrodedFOUND BS 615, RBL 47 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-21- 01-0G AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A ALLOWABLE DAMAGE 1, FIGURE 101. REPAIR CARRIED OUT ON SEAT TRACK AT STA 605, X = -47 AS PER SRM 53-00-52-2R, FIGURE 201, REPAISDR FDEA201701170206Seat Track · corrodedMAIN DECK BS 5-45 TO 5-53, LBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1.SDR FDEA201701170205Seat Track · corrodedMAIN DECK BS 5-40 TO 5-46, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201701170204Seat Track · wornMAIN DECK BS 1407 TO 1417, RBL 47 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201701170203Seat Track · corrodedMAIN DECK BS 1405 TO 1412, LBL 8 SEAT TRACK FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1, THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFISDR FDEA201701170202Seat Track · corrodedMAIN DECK BS 1432 TO 1440, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR IPXA2017011812901Power Supply · lowEMERGENCY LT BATT 1 LOW MSG DURING PREFLIGHT. R&R BATT POWER SUPPLY PER AMM 35-51-01-401. CHKS OK. IPC 33-51-01 -01, ITEM 5.SDR FDEA201701170219Valve · crackedDURING CRUISE, OBSERVED A LEVEL 1 ALERT FOR HYD 2 OFF. NR 2 HYD 2.7. AFTER TAXI IN, OBSERVED LEVEL 2 ALERT FOR HYD 2 QTY LOW AND NR 2 HYD QTY 1.6. REMOVED AND REPLACED THE RT OTBD FLAP LOCK VALVE IAW MM 27-52-11-4. OPS AND LEAK CHECKED GOOD.SDR FDEA201701170213Skin · chafedRIGHT NR 8 SLAT COVE PANEL INNER SKIN IS CHAFED AT OUTBOARD RIB XOS 1185. BLENDED OUT CHAFED AREA IAW SRM 57-00-00-2R FOUND TO BE OUT OF LIMITS, PERFORMED A DOUBLER REPAIR IAW SRM 57-40-01-2R AND EA 1-5750-T0330795.SDR IPXA2017020313660Skin · gougedINSPECTION TYPE: 3C, LEFT INBD FLAP L/E UPPER SKIN HAS GOUGES AT XIFH215.3 & XIFH 217.3. REPAIRED IAW EA 011-5753-01-A6608 REV. I/R AND EO MD11-5750-63129-A.SDR IPXA2017013113522Fitting · wornINSPECTION TYPE: 3C, RIGID CARGO BARRIER SIDE FITTING NR 6 HAS DEEP WEAR. REPAIRED FITTING IAW EA 011-5310-01-A6603 REV. I/R AND EO MD11-5340-63110-A.SDR FDEA201701160201Actuator · lack of lubeRUDDER TRIM KNOB IS FROZEN AT CRUISE & AFTER LANDING. UNFROZE ONCE BLOCKED IN. PERFORMED LUBRIFICATION OF RUDDER TRIM ACTUATOR IAW MM 12-24-06-3. PERFORMED OPERATIONAL TEST OF THE RUDDER IAW MM 27-20-00-2. NO DEFECT FOUND.SDR FDEA201701160197Seat Track · corrodedMAIN DECK BS 1276, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG. 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM-6-2-100.SDR FDEA201701160196Seat Track · corrodedMAIN DECK BS 1254 TO 1259, RBL 8 SEAT TRACK FOUND CORRODED. FOUND EXCEEDED LIMITS SRM 53-00-52-1A, FIGURE 101. REMOVED AND REPLACED IAW SRM 51-21-01-0G, AND SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201701160194Support · crackedLEFT WING FIXED LEADING EDGE XOS 546 ACCESS PANEL FWD SUPPORT STRUCTURE FOUND CRACKED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DWG ARB2933 REV T & AJ. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201701160193Hinge Bracket · corrodedLEFT WING OUTBD FLAP, INBD FWD HINGE BRACKET ACTUATOR INBOARD LUG BORE FOUND CORRODED. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1D.SDR FDEA201701160192Hinge Bracket · corrodedLEFT WING OUTBD FLAP, INBD FWD HINGE BRACKET ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1D.SDR FDEA201701160191Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET PIVOT BORE FOUND CORROSION. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806 PART 1 STEP 1B.SDR FDEA201701160190Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE CORRODED. EXCEEDS LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1A.SDR FDEA201701160189Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET UPPER OUTBOARD MOUNT BORE CORRODED. EXCEEDS LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED EA 1-5750-T0330806, PART 1, STEP 1A.SDR FDEA201701160188Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET LOWER INBOARD MOUNT BORE CORRODED. EXCEEDS LIMITS IAW CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1C, AND STEP 1.SDR FDEA201701160187Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBOARD FWD HINGE BRACKET LOWER OTBD MOUNT BORE CORRODED. EXCEED LIMITS IAW CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1C, AND STEP 1.SDR FDEA201701160186Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET ACTUATOR INBOARD LUG BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789, PART 1, STEP 1D.SDR FDEA201701160185Hinge Bracket · corrodedLEFT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBOARD LUG BORE FOUND CORROSION. CORROSION. AT LEFT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBOARD LUG BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09.SDR FDEA201701160184Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE ATTACH UPPER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789, PART 1, STEP 1C.SDR FDEA201701160183Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE ATTACH LOWER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789, PART 1, STEP 1C.SDR FDEA201701160182Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET LOWER INBOARD MOUNT BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1B AND STEP 1.SDR FDEA201701160181Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET LOWER OUTBOARD MOUNT BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1B AND STEP 1.SDR FDEA201701160180Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1A.SDR FDEA201701160179Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE BRACKET, UPPER OTBD MOUNT BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1A.SDR FDEA201701160195Seat Track · wornMAIN DECK SEAT TRACK BS 1276, LBL 8 FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR IPXA2017020213630Stanchion · corrodedINSPECTION TYPE: 3C, VERTICAL STANCHION AT BS 6-79 ABOVE LONGERON 48L HAS HEAVY CORROSION. REPAIRED THE STANCHION IAW EA 011-5310-01-A6583 REV. I/R AND EO MD11-5310-63122-A.SDR FDEA201701150172Hinge Bracket · corrodedRT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER INBD MOUNT BORE NR 2 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 0.943", FINALSDR FDEA201701150171Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE BRACKET UPPER OUTBOARD MOUNT BORE FOUND CORROSION. HINGE BRACKET REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.943", FINAL HOLE DIA 0.952" MAXIMUM ALLOWABLE HOLE DIA 0.944 OVERSIZE BUSHINGSDR FDEA201701150167Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET ACTUATOR INBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 10.SDR FDEA201701150166Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET LOWER INBD MOUNT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 1.SDR FDEA201701150165Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE, LOWER OTBD MOUNT BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 1B AND STEP 1.
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