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 IPXA2018012225747Battery Pack · no testEMERGENCY LIGHT TEST FAILED, R & R BATTERY IAW AMM 33-51-01-401.SDR IPXA2018011925675Cable · frayedR1 DOOR SLIDING CEILING PANEL CABLE SHOWING BROKEN STRANDS. R & R THE CABLE IAW MM 52-11-03; OPS GOOD.SDR IPXA2018012525890Door Frame · puncturedINSPECTION TYPE: 2C, MAIN CARGO DOOR FWD FRAME HAS A PUNCTURE. REMOVED, FABRICATED, AND REPLACED FRAME IAW DWG ACA7301-3, AND SRM 51-35-01.SDR FDEA201801170108Indicator · inoperativeDURING PREFLIGHT CHECK, FOUND THE L1 DOOR SLIDE PRESS TO TEST INDICATION INOPERATIVE.SDR IPXA2018011825632Cover · looseINSPECTION TYPE:NAR 1 ENTRY DOOR SLIDE COVER LOOSE, SECURED R1 ENTRY DOOR LOWER SLIDE COVER IAW AMM 25-23-07-400--802.SDR FDEA201801160099Hinge · wornFOUND TWO LOBES ON HINGE BEYOND SRM LIMITS EA T1-5310-T0337841 PT1 WAS ISSUED AND COMPLIED WITH.SDR IPXA2018011725605Adc · malfunctionedAIR TURNBACK DUE TO INCORRECT INFO ON PDF CONTRADICTORY FROM SIDE TO SIDE. R & R THE NR 1 ADC IAW AMM 34-16-01-000-801/400-801, REV 01/08/18. COMPLIED WITH AN OPS TEST IAW AMM 34-16-01-700-801, REV. COMPLIED WITH ADC IEIS INTERFACE TEST IAW AMM 34-16-01-7SDR IPXA2018011625542Channel · damagedFWD LWR CARGO COMP CEILING CHANNEL DAMAGED. REPLACED IAW EO-MD11-2550-67095-A.SDR IPXA2018012825968Jackscrew · wornINSPECTION TYPE:4C,, LT HORIZONTAL STAB JACKSCREW SPROCKET HAS EXCESSIVE WEAR. REMOVED AND REPLACED THE JACKSCREW ASSY IAW AMM 27-44-04-400-801, OPS CHECKED GOOD.SDR IPXA2018012825967Jackscrew · wornINSPECTION TYPE:4CR/H HORZ. STAB JACKSCREW SPROCKET HAS EXCESSIVE WEAR.REMOVED AND REPLACED R/H HORZ. STAB JACKSCREW ASSY IAW AMM 27-44-04-400-801, OP'S CHECK IS GOOD. (MINOR)SDR FDEA201801150097Sensor · failedENROUTE WHILE DESCENDING, SELECTED ENGINE ANTI-ICE ON. RECEIVED A LEVEL 1 NR 2 ENGINE. ANTI ICE DUCT FAILED MESSAGE. RETURNED TO DEPARTURE. COMPLIED WITH FIM, INSPECTED ANTI-ICE DUCT AND FOUND NO EVIDENCE OF LEAK. CHECKED ANTI-ICE SENSOR RESISTANCE AND SDR IPXA2018011625563Cover · unsecureL1 DOOR SLIDE COVER FALLING OUT. SECURED THE COVER IAW MM 25-61-15. OPS CHECKED GOOD.SDR IPXA2018011525513Floor Panel · damagedRIGHT FLOOR PANEL HAD DAMAGED INSERTS AND EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50, REPAIR 1, AND DRAWING ABA7143,SDR IPXA2018011525512Floor Panel · damagedLT FLOOR PANEL HAS DAMAGED INSERTS AND EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50SDR IPXA2018011525475Skin · puncturedLOWER VERTICAL STAB REAR PANEL ASSY , INNER SKIN HAS PUNCTURE DAMAGE. REPAIRED IAW EO MD11-5430-66477-A.SDR IPXA2018011525476Skin · damagedLOWER VERTICAL STABILIZER REAR PANEL ASSEMBLY. PANEL 364MR DAMAGE. REPAIR IAW MD11-5430-66477-B.SDR IPXA2018011525477Skin · puncturedLOWER VERTICAL STABILIZER REAR PANEL ASSY RT SIDE. NO 364MR HAS PUNCTURE ON INNER SKIN LOCATED 5.4 INCHES FROM PANEL T/E AND 17.5 INCHES FROM UPPER EDGE, PUNCTURE MEASURES .200 X .250. CLASSIFIED AS A MAJOR REPAIR.SDR IPXA2018012525885Beam · crackedINSPECTION TYPE: 2C, LOWER FWD CARGO AT BS 6-70, ABOVE LONGERON 43R, HORIZONAL BEAM IS CRACKED ON THE END. REMOVED, FABRICATED, AND REPLACED THE BEAM IAW DWG ADA7667, SRM 51-33-01, AND 51-35-01.SDR IPXA2018012425838Skin · chafedINSPECTION TYPE: 2C, FUSELAGE SKIN BETWEEN BS 1149 - 1156, LONGERON 44L CHAFED. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG 201.SDR IPXA2018012325807Skin · chafedINSPECTION TYPE: 4C, RT UNDER WING FUSELAGE SKIN IS CHAFED AT BS 1149 - 1156, LONGERON 44R. REPAIRED SKIN IAW SRM 53-40-01, REPAIR 3, FIG 201.SDR IPXA2018020226121Vane · delaminatedINSPECTION TYPE: 2C, LT WING INBD FLAP VANE LOWER SURFACE HAS MULTIPLE AREAS OF DELAMINATION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLAP VANE IAW AMM 27-50-22-400-801 AND PERFORMED AN ADJUSTMENT & TEST, CHECKED GOOD IAW AMM 27-50-22-830-801.SDR IPXA2018020126099Skin · chafedINSPECTION TYPE: 4C, TAIL CONE INTERNAL UPPER RT SKIN HAS A DEEP CHAFE FROM CONTACT WITH RIVETS. REPAIRED IAW EA 011-5350-01-A7076, REV IR AND EO MD11-5350-67142-A.SDR IPXA2018013026040Fitting · wornINSPECTION TYPE: 2C, RT OTBD FLAP FAIRING HAS A WORN FITTING. REMOVED AND REPLACED THE FITTING IAW EA 011-5700-01-A7079, REV I/R, AND EO MD11-5750-67143-A.SDR IPXA2018013026051Skin · corrodedINSPECTION TYPE: 2C, MAIN CARGO HAS CORROSION AT BS 1227 & LBL 108. REPAIRED THE SKIN AT STRINGER 15 AND XCW 118 IAW VT-SAA EA 011-5730-01-A7090 REV. IR AND UPS EO MD11-5730-67243-A.SDR IPXA2018013026052Vane · delaminatedINSPECTION TYPE: 2C, LEFT INBD FLAP VANE LOWER SURFACE HAS DELAMINATION AT THE OTBD END. REPAIRED THE FLAP VANE IAW SRM 57-50-80, REPAIR 2, PAR 2A(2)(A)(5) REV 64. MAJOR REPAIR.SDR IPXA2018013026043Spar Cap · corrodedINSPECTION TYPE: 2C, LT WING UPPER REAR SPAR VERTICAL LEG HAS CORROSION AT XORS 480. REPAIRED IAW EA 011-5710-01-A7077, REV IR, AND EO MD11-5710-67214-A.SDR IPXA2018012525889Support Fitting · crackedINSPECTION TYPE: 2C, LT WING OTBD FLAP INBD HINGE FAIRING SUPPORT FITTING AT INBD SIDE IS CORRODED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DWG ARC7729, AND SRM 51-31-01.SDR FDEA201801120107Strut · failedDURING A POSTFLIGHT INSPECTION, FOUND CENTER LANDING GEAR NOT EXTENDED AND TIRES NOT TOUCHING THE GROUND. PERFORMED GVI OF CENTER GEAR. CENTER GEAR IS DOWN AND LOCKED. PRESSURE RELEASE CAP NEAR TOP OF STRUT IS INTACT AND THE NITROGEN PRESSURE GAUGE IS RESDR IPXA2018011225425Connector · looseAIR TURNBACK DUE TO A CARGO DOOR AFT A AND CARGO DOOR AFT B ALERTS. FOUND A LOOSE CONNECTOR FOR CARGO DOOR CONTROL PANEL.SDR IPXA2018013026039Channel · crackedINSPECTION TYPE: 2C, NR 2 ENGINE LT THRUST REVERSER FWD BULB SEAL CHANNEL IS CRACKED AND GOUGED. REPAIRED THE BULB SEAL CHANNEL IAW EA 011-5430-01-A7089, REV I/R, AND EO MD11-7830-67269-A.SDR IPXA2018013026050Skin · corrodedINSPECTION TYPE: 2C, LEFT WING UPPER SKIN HAS CORROSION FWD OF THE NR 2 SPOILER. REPAIRED THE SKIN IAW EA 011-5730-01-A7092, REV IR, AND EO MD11-5730-67268-A.SDR IPXA2018012725935Skin · gougedINSPECTION TYPE: 2C, LT WING FIXED L/E SKIN IS GOUGED AT XOS 342 AND AFT OF THE NR 2 SLAT BETWEEN XIS 341.55, & 346.55. REPAIRED THE SKIN IAW EA 011-5710-01-A7087, REV I/R, AND EO MD11-5710-67237-A.SDR IPXA2018012825959Skin · corrodedINSPECTION TYPE: 2C, LEFT WING UPPER SKIN HAS CORROSION IN FIVE LOCATIONS BETWEEN XORS. 97 & 210, STRINGER 18 & FRONT SPAR. REPAIRED THE SKIN IAW EA 011-5730-01-A7091, REV I/R, AND EO MD11-5730-67241-A.SDR IPXA2018012525888Skin · corrodedINSPECTION TYPE: 2C, LT WING UPPER SKIN HAS 2 AREAS OF CORROSION AT XORS 645.65, STRINGER 2L AND XORS 681.65 AT STRINGER 4. REPAIRED THE SKIN IAW EA 011-5730-01-A7083, REV I/R, AND EP MD11-5730-67187-A.SDR IPXA2018012525884Beam · crackedINSPECTION TYPE: 2C, FWD LOWER CARGO AT BS 6-70, ABOVE LONGERON 43L, HORZONTAL BEAM IS CRACKED ON THE END. REMOVED, FABRICATED, AND REPLACED THE BEAM IAW DWG. ADA7667, AND SRM 51-33-01.SDR FDEA201801100044Hinge · wornMAIN C DOOR AFT HINGE. R & R THE AFT HINGE.SDR IPXA2018012725934Sleeve · gougedINSPECTION TYPE: 2C, NR 3 ENGINE RT THRUST REVERSER TRANSLATING SLEEVE LOWER SLIDER IS GOUGED AT NAC STA 125.5. REPAIRED THE THRUST REVERSER SLEEVE IAW EA 011-7830-01-A7086, REV I/R, AND EO MD11-7830-67207-A.SDR IPXA2018012825958Skin · gougedINSPECTION TYPE: 2C, NR 1 ENGINE OTBD FAN COWL IS GOUGED ON THE UPPER SURFACE OF THE UPPER FWD HINGE FITTING. REPAIRED IAW EA 011-7110-01-A7075, REV I/R, AND EO MD11-7110-67121-A.SDR IPXA2018011825649Skin · crackedINSPECTION TYPE:4CWHILE PERFORMING EDDY CURRENT INSP. OF LOWER SKIN PANEL AT XORS 683.40 AND XORS 713.6 OF #1 FUEL TANK. FOUND 5 INDICATIONS AS MARKED.REPAIRED LT WING LOWER WING SKIN 5EA FASTENER HOLES IAW SRM 57-20-02 REPAIR 5.SDR IPXA2018011825648Skin · crackedINSPECTION TYPE: 4C, WHILE PERFORMING EDDY CURRENT INSPECTION. OF LOWER SKIN PANEL AT STA XORS 683.40 AND XORS 713.6 OF NR 3 FUEL TANK. FOUND 3 INDICATIONS. REPAIRED THREE FASTENER HOLES ON LOWER RT WING SKIN AT XORS 683.40 AND XORS 713.6 IAW SRM 57-20-02 RESDR IPXA2018011025337Window · out of positionL1 DOOR DISARM LEVER HARD TO MOVE TO DISARM. FOUND GIRT BAR INSPECTION WINDOW OBSTRUCTING ARMING HOOK. REPOSITIONED THE FWD GIRT BAR INDICATOR WINDOW. CHECKED GOOD.SDR FDEA2018082790040Limit Switch · failedFOUND THE L1 DOOR WILL NOT OPEN ELECTRICALLY. R & R LT FWD DOOR UP LIMIT SWITCH S1-592. PERFORMED A LT FWD DOOR OPS TEST, TESTED OK IAW AMM 52-11-02-5. OK FOR SERVICE.SDR IPXA2018010925297Door · out of adjustLEFT MAIN ENTRY DOOR DROPS BACK ON OPENING BUT REMAINS ON THE TRACK. PERFORMED AN ADJUSTMENT AND TEST OF DOOR IAW MM 52-11-02. DOOR NOW CHECKED NORMAL.SDR IPXA2018012525875Skin · corrodedINSPECTION TYPE: 4C, RT WING UPPER SKIN HAS CORROSION AT THREE LOCATIONS AT REAR SPAR AND STRINGER 2R BETWEEN XORS 475.6 AND XORS 516.6. REPAIRED THE SKIN IAW EA 011 5730-01-A7085, REV I/R, AND EO MD11-5730-67204-A.SDR IPXA2018012525874Skin · chafedINSPECTION TYPE: 4C, UNDERWING TO BODY FUSELAGE SKIN IS CHAFED AT BS 1153 & LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-01-A7074, REV I/R, AND EO MD11-5310-67206-A. MAJOR REPAIR.SDR IPXA2018012425844Skin · corrodedINSPECTION TYPE: 4C, RT WING UPPER SKIN HAS CORROSION AT 12 LOCATIONS AT THE REAR SPAR AND STRINGER 1R, BETWEEN XORS 170 AND 254. REPAIRED THE SKIN IAW EA 011-5730-01-A7082, REV I/R, AND EO MD11-5730-67183-A.SDR IPXA2018012425843Skin · corrodedINSPECTION TYPE: 4C, RT WING UPPER SKIN HAS CORROSION BETWEEN XORS 372 TO 402, BETWEEN STRINGERS 3 & 4R. REPAIRED THE SKIN IAW EA 011-5730-01-A7080, REV I/R, AND EO MD11-5730-67198-A.SDR IPXA2018012425832Skin · corrodedINSPECTION TYPE: 4C, RT WING UPPER SKIN AT REAR SPAR HAS CORROSION AT 3 LOCATIONS BETWEEN XORS 713 AND XORS 783. REPAIRED THE WING SKIN IAW EA 011-5730-01-A7078, REV I/R, AND EO MD11-5730-67196-A.SDR IPXA2018011725589Skin · chafedINSPECTION TYPE: 4C, FUSELAGE SKIN IS CHAFED AT BS 1149 - 1153, LONGERON 44L. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 2, FIG 201. MAJOR REPAIR.SDR IPXA2018010825242Battery Pack · dischargedDURING EMERGENCY LIGHT TEST, EMERGENCY LIGHT BATTERY 1 LOW ILLMINATED. R & R THE BATTERY OPS CHECKED GOOD AMM 33-51-01.
Back to Boeing MD-11F