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 FDEA2018091432505Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2B AND STSDR IPXA2018092434320Panel · gougedLEFT WING PANEL 516ET WAS GOUGED FROM THE NR 2 SLAT. REMOVED, FABRICATED, AND INSTALLED THE LT WING PANEL IAW DWG ARB2386, SRM 51-31-01, AND SRM 51-33-01. MINOR.SDR IPXA201809244282Former · crackedLEFT WING FIXED L/E FORMER WAS CRACKED AT XOS. 961. REMOVED, FABRICATED, AND REPLACED THE FORMER IAW DWG. ARB2920-13, AND SRM 51-33-01. MINOR.SDR FDEA2018091432497Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STSDR FDEA2018091432496Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STSDR FDEA2018091432495Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132148 C PART 5 STSDR FDEA2018091432494Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1- 5750-132148 C PART 5 SSDR FDEA2018091432504Doubler · crackedLT WING, ALONG NR 6 SLAT LOCATION, ALONG XOS 789, LT LEADING EDGE FORMER ATTACHED DOUBLER CRACKED. LEADING EDGE FORMER ATTACHED DOUBLER, REMOVED AND REPLACED AS PER SRM 51-31-01-0G AND SRM 51-33-01-0G, DOUBLER PART NUMBER: ARB3954-7 FABRICATED AS PER DRAWING ASDR FDEA2018091432502Skin · cracked05EA FASTENER HOLES (NR 6, 7, 15, 34 & 35) FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. SKIN REPAIR CARRIED OUT AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSISDR FDEA2018091432525Sensor · faultyRECVD "SLAT DISAG" ALERT SHORTLY AFTER TAKE OFF, CONFIG FLAPS 10, SLAT EXT, GEAR DOWN. "SLAT DISAG" WENT AWAY W/ FLAPS UP. "SLAT DISAG" CAME BACK ON WHEN CONFIG W/ SLATS EXT & FLAPS 10. DECLARED EMERGENCY / LANDED W/ SLATS RET & FLAPS 28. REPLACED RIGHT SLSDR FDEA2018091432493Pseu · failedRECEIVED "SLAT DISAG" ON FINAL APPROACH. EXECUTED GO-AROUND, RAN QRH, LANDED FLAPS 28? 0 EXT. T/S IAW FIM 31-71-07-00. FOUND TARGET NEAR ON PSEU FOR ALL TARGETS 1-6, AND 31-32. REMOVED AND REPLACED PSEU IAW AMM 31-71-01-2. OPS CHECKS GOOD. OK TO CONTINUE.SDR SRXR201809130040Fitting · damagedTAILCONE AFT BODY BULKHEAD RH ALIGNMENT PIN FITTING HAS ELONGATED HOLE. ACCOMPLISHED REPAIR ON FUSELAGE AFT BODY BULKHEAD RT ALIGNMENT PIN FITTING AT Y=2163.35 AND L-35 PER EA 011-5360-52-A7438 I/R AND DWG AJC7880-1.SDR FDEA2018091422469Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1541 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICSDR FDEA2018091422464Skin Panel · crackedEMPENNAGE LT SIDE LOWER VERTICAL STABILIZER IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN PANEL CRACKED. SKIN PANEL REPAIR CARRIED OUT AS PER EA 1-5530-T0342403 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018100134601Frame · gougedNR 1 ENGINE, LT CORE COWL FRAME WAS GOUGED AT NAC STA 300.0 AND THE 8 O'CLOCK POSITION. REPAIRED THE DAMAGE IAW EA 011-7110-01-A7466, REV I/R, AND EO MD11-7110-70005-A. MINOR.SDR IPXA2018092874481Floorbeam · crackedTHE FLOORBEAM WAS CRACKED AT STATION 6-70, LBL 57.5 AND WL 98. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, REPAIR 1, FIG 201. MAJOR.SDR IPXA2018092634436Longeron Splice · corrodedLONGERON 48L SPLICE FITTING WAS CORRODED BETWEEN BS 1701 - 1721. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-31-01, AND 51-33-01. MINOR.SDR IPXA2018092654387Floorbeam · crackedFLOORBEAM WAS CRACKED AT STATION 6-70 ABOVE LONGERON 43L. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, REPAIR 1, FIGURE 201. MAJOR.SDR FDEA2018091422472Angle · damagedMAIN DECK LT FRAME AT STA 1661 LONGERON 12L FOUND EXISTING REPAIR ANGLE DAMAGED. DAMAGED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.SDR FDEA2018091422470Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1541 X =-8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1571 TO EXISTINSDR FDEA2018091422467Seat Track · wornMAIN DECK FLOOR SEAT TRACK AT STA 5-11 X = 27.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-63 TO EXISTISDR IPXA2018092434319Beam · crackedHORIZONTAL BEAM WAS CRACKED AT STATION 6-73, ABOVE LONGERON 43L. REMOVED AND REPLACED THE HORIZONTAL BEAM IAW SRM 51-31-01, AND 51-33-01. MINOR.SDR IPXA20180924283Support Angle · crackedRIGHT WING FUEL CONTROL PANEL OTBD MOUNT ANGLE WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ARB2382, AND SRM 51-35-01. MINOR.SDR IPXA20180924281Skin · crackedRIGHT WING FIXED L/E LOWER SKIN WAS CRACKED AT XOS. 827. REPAIRED THE WING L/E SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.SDR IPXA2018092134235Stiffener · crackedNR 3 ENGINE, INBD THRUST REVERSER SUPPORT STIFFENER, SECOND FROM THE BOTTOM WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018092134234Stiffener · crackedNR 3 ENGINE, INBD THRUST REVERSER SUPPORT STIFFENER, 4TH FROM THE BOTTOM WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018092104203Pan · gougedRT MLG DOOR LOWER AFT CORNER JUST ABOVE OUTER DOOR WAS GOUGED. REMOVED AND REPLACED THE RT MLG DOOR LOWER AFT CORNER PAN IAW SRM 51-35-01, 51-35-02. MINOR.SDR FDEA2018091422471Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1541 X =-47.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLENDOUT AND EXCEEDED LIMIT AS PER SRM-53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1571 TO EXISTING SPLSDR FDEA2018091422468Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 775 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES STA 745 TOSDR FDEA2018091422465Seat Track · wornMAIN DECK FLOOR SEAT TRACK AT STA 5-11 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-43 TO EXSITING SPLICE STA 5-0SDR IPXA2018091433918Battery · dischargedLEVEL ONE MSG EMERG LIGHT BAT 1 LOW. R&R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01-000-802. OPS CK GOOD.SDR IPXA2018091433917Battery · dischargedEMERGENCY LIGHT BAT 1 LO ALERT. EMER LIGHT BATTERY PWR SUPPLY REPLACED IAW AMM 33-51-01. OPS CK OK.SDR FDEA2018091422458Angle · chafedCABIN MAIN DECK CARGO EXISTING REPAIR ANGLE FRAME LONGERON 24 LEFT AT STA 535 LEFT HAND FRAME FOUND CHAFFING MARK. REPAIR ANGLE LEFT HAND FRAME REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018091433903Sign · brokenLEFT ENTRY DOOR EXIT SIGN BROKEN. R&R EXIT SIGN ASSY REF 33-27-01. OPS CHECK GOOD 33-27-01-05.SDR IPXA2018100594662Pan · crackedLEFT FWD CENTER GEAR DOOR PAN WAS CRACKED AT THE FWD CORNER. REPAIRED THE DOOR PAN IAW SRM 52-82-07, REPAIR 1, FIG 201. MINOR.SDR IPXA2018100594660Stanchion · corrodedFWD CARGO STANCHION WAS CORRODED AT STATION 6-73, X=57, AND Z=-65 TO -95. REPAIRED THE VERTICAL STANCHION IAW EO MD11-5310-70016-A. MAJOR.SDR IPXA2018092874483Skin · splitLOWER AFT RUDDER, AFT LOWER T/E, ZAR 310, HAD A 10 INCH SPLIT IN COMPOSITE. REPAIRED RUDDER T/E IAW SRM 55-40-02, REPAIR 2, FIG 201. MAJOR.SDR IPXA2018092834500Skin · gougedEXTERIOR FUSELAGE SKIN AT BS 1153, LONGERON 44R WAS GOUGED. REPAIRED THE SKIN IAW EA 011-5340-01-A7467, REV IR, AND EO MD11-5330-70087-A. MINOR.SDR IPXA2018092834499Doubler · crackedRIGHT MLG WW, RT FWD PUSH ROD CUT OUT DOUBLER WAS CRACKED BETWEEN FASTENERS. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01, AND 51-33-01. MINOR.SDR IPXA2018092644330Doubler · crackedRT WING L/E BEADED DOUBLER WAS CRACKED AT XORS 571. REPAIRED THE RT WING L/E BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIGURE 205. MAJOR.SDR IPXA2018092634438Pan · crackedLT MLG DOOR CENTER FWD DOOR CORNER PAN WAS CRACKED. REMOVED AND REPLACED THE CORNER PAN IAW SRM 51-31-01, 51-35-01, AND 51-35-02. MINOR.SDR IPXA2018092634435Intercostal · crackedRT MLG WW, THE INTERCOSTAL BELOW LOWER AFT BRAKE ACCUMULATOR WAS CRACKED. REPAIRED THE INTERCOSTAL IAW SRM 53-00-00, FIG 203. MINOR.SDR IPXA2018092634434Mount Bracket · crackedLT MLG WW, NR 1 HYDRAULIC RESERVOIR LOWER MOUNT BRACKET WAS CRACKED IN THE RADIUS. REMOVED AND REPLACED THE MOUNT BRACKET IAW SRM 51-31-01, AND 51-33-01.SDR IPXA20180924285Web · crackedUPPER FUEL TANK AFT WEB WAS CRACKED AT BS 1372 AND RBL 80. REPAIRED IAW EO MD11-5710-69973-A. MAJOR.SDR FDEA201809112450Skin · crackedLT WING LEADING EDGE BOTTOM SURFACE AROUND STA XOS =787.5 FOUND CRACK. REPAIR CARRIED OUT AS PER EA 1-5730-T0342355 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018091233868Stud · shortAVIONICS COMPARTMENT EMERGENCY DOOR (FLIGHT COMPARTMENT ACCESS) ALIGNMENT STUDS FAIL TO ENGAGE (TOO SHORT) INTO FLOOR CATCHES. IPC: 52-52-05-01 ITEM 020 DOOR ITEM 090J-STUD. REPLACED STRUTS IAW AMM 20-00-00.SDR IPXA2018091233867Door · inoperativeL1 DOOR EMERGENCY. SERVICED PAX DOOR SYSTEM TO PROPER LEVEL IAW AMM 12-25-04-600-801.SDR IPXA2018100854711Bracket · gougedNR 1 ENGINE INBD THRUST REVERSER COWL, DEFLECTION LIMITER BRACKET WAS GOUGED. REPAIRED THE DEFLECTION LIMITER BRACKET IAW EA 011-7830-01-A7471, REV I/R, AND EO MD11-7830-70092-A. MINOR.SDR IPXA2018100594672Rib · damagedNR 1 INBD THRUST REVERSER COWL INNER RIB WAS DAMAGED, 16 INCHES FROM FWD EDGE. REMOVED AND REPLACED THE RIB IAW SRM 51-31-01, & 51-33-01. MINOR.SDR IPXA2018092104208Frame · damagedRIGHT FWD CENTER LANDING GEAR DOOR FWD EDGE, FRAME DAMAGED. REMOVED AND REPLACED MLG GEAR DOOR FWD EDGE FRAME IAW 51-35-01. MINOR.
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