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 FDEA201407241938Support Rib · crackedRIGHT WING LE COMPARTMENT FIXED LE SUPPORT RIB AT XOS 584 FOUND CRACKED. REMOVED AND REPLACED IAWSRM 51-31-01 REVISION 56, DWG ARB2931 REVISION H, AND SRM 51-33-01 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.SDR FDEA201407241937Attach Angle · crackedRIGHT WING LE COMPARTMENT FIXED LE SUPPORT RIB OTBD ATTACHED ANGLE AT XOS 584 FOUND CRACKED. REMOVED IAW SRM 51-31-01 REVISION 56. NEW ANGLE FABRICATED IAW DRAWING ARB2931 REVISION H. ANGLE INSTALLED IAW SRM 51-33-01 REVISION 56. REPAIR CLASSIFIED MAJOR SDR FDEA201407241952Warning Light · false activationAFTER PUSHBACK, LEVEL 1 ALERT FOR EMERGENCY LIGHTS DISARMED. SWITCH POSITION WAS IN ARM. TROUBLESHOT, NO FAULTS FOUND WITH NR 1 DEU OR EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL. NO 30 DAY HISTORY, SYSTEM OK FOR SERVICE.SDR FDEA201407241954Hmu · failedAT TOP OF CLIMB, RECEIVED LEVEL 1 ALERT, NR 2 ENGINE FADCE MAINT. R & R HMU, OPS CHECKED GOOD.SDR FDEA201407231926Doubler · crackedRIGHT WING LE LOWER ACCESS COMPARTMENT BEADED DOUBLER FOUND CRACKED XORS 695 DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407231932Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT FOUND CORRODED BS 420 LBL 47. FLOOR SUPPORT REMOVED AND REPLACED IAW AMM 20-50-02 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407231931Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT FOUND CORRODED BS 420 X= -27. FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 56.SDR FDEA201407231929Skin · crackedNR 1 PACK BAY DOOR CUT OUT HAS TWO POTENTIAL CRACKS IN PREVIOUS REPAIR DOUBLER & TRIPLER. BOTH APPROX 1.5 INCHES LONG REQUESTED NDT TO DETERMINE IF CRACKED. PERFORMED HFEC IAW NTM PT6 TO VERIFY TWO POTENTIAL CRACKS, CRACKS VERIFIED & ADDITIONAL CRACK NOTED &SDR IPXA2014072583767Sign · dislodgedEXIT SIGN FELL OFF FROM MOUNT RT SIDE (R1 DOOR). INSTALLED LENS COVER IAW MM 33-52-05.SDR IPXA2014072583761Valve · failedAIR TURNBACK, LEVEL 2 ALERT HYD 2 FAILURE. R & R NR 2 EDP ELECTRIC DEPRESSURIZATION VALVE IAW MM 29-11-21-400-802. OPS AND LEAK CHECK GOOD. THIS WAS THE LT PUMP (UPPER) IPC REF 29-11-22-01.SDR FDEA201407231930Battery · faultyEMERGENCY POWER TEST FAIL & BATTERY VOLTS LOW. R & R MAIN ACFT BATTERIES IAW AMM 24-34-02-4-0.SDR KO0R201407220002Skin · corrodedFUSELAGE SKIN IS CORRODED FROM BS 2123 - 2135 AT LONGERON 12R.SDR KO0R201407220001Skin · corrodedFUSELAGE SKIN PANEL IS CORRODED AT BS 2160 AT LONGERON 33L.SDR IPXA2014081884003Fairing · chafedINSPECTION 4C, CHAFING WEAR AROUND FASTENER HOLES ON FAIRING 487AR. REPAIRED FAIRING IAW EA 011-5430-01-A5540 AND EO 5430-55229-A.SDR IPXA2014081383966Longeron Splice · crackedINSPECTION 4C, UPPER CARGO LONGERON SPLICE CRACKED L12L BS 1129. R & R LONGERON SPLICE IAW SRM 51-33-01.SDR IPXA2014081383965Longeron Splice · crackedINSPECTION 4C, UPPER CARGO LONGERON SPLICE CRACKED AT L24L BS 1129. R & R LONGERON SPLICE IAW SRM 51-33-01.SDR IPXA2014081383963Longeron Splice · crackedINSPECTION 4C, UPPER CARGO LONGERON SPLICE CRACKED AT L3L, BS 1521. R & R LOINGERON SPLICE IAW SRM 51-33-01.SDR IPXA2014072383727Warning Message · false activationEMERGENCY LIGHT BATTERY LOW. PERFORMED OPS TEST OF THE EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00-700-802. ALL TESTS PASS.SDR WRNA201407230015Engine · making metalON REACHING TOP OF CLIMB, A LEVEL 2 OIL PRESSURE LOW DISPLAYED. CREW FOLLOWED THE QRH PROCEDURES SIMULTANEOUSLY FOLLOWING THE QRH PROCEDURES "ENGINE SHUTDOWN IN FLIGHT" FOR ENG NR 2. THE CREW ACCOMPLISHED THE CHECKLIST THEN PROCEEDED TO DUMP APPROXIMATELY 50SDR IPXA2014081383964Torque Tube · chafedINSPECTION 4C, R1 DOOR LOWER TORQUE TUBE CHAFED IN TWO PLACES, ACCOMPLISHED REPAIR IAW EA 011-5200-01-A5519, REV I/R AND EO 5230-55191-A.SDR IPXA2014081383962Longeron Splice · crackedINSPECTION 4C, UPPER CARGO LONGERON SPLICE CRACKED AT L18L BS 1521. R & R LONGERON SPLICE IAW SRM 51-33-01.SDR IPXA2014081383957Longeron Splice · crackedINSPECTION 4C, LONGERON SPLICE 13R CRACKED AT BS 1521. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SPLICE IAW DWG.A5A7112 AND SRM 51-33-01.SDR FDEA201407201872Skin · crackedLEFT FUSELAGE NR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT UPPER AFT CORNER SKIN FOUND CRACK ABOUT 1 INCH IN LENGTH. DOOR CUTOUT UPPER AFT CORNER SKIN CARRIED OUT REPAIR AS PER SRM 53-20-15 REPAIR 3 FIGURE 201 REV 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2SDR FDEA201407201876Repair · damagedEXSITING REPAIR FOUND AT RIGHT WING INBOARD FLAP OUTBOARD WEB AT APPROXIMATELY XIFH 133.9. EXISTING REPAIR EVALUATED AND FOUND DAMAGED. REPAIR REMOVED AND REPLACED AS PER DRAWING NR ARC2305 REVISION C AND SRM 51-35-01 REVISION 56. EO 1-5100-7-5001 B4 PART 1SDR IPXA2014081183919Longeron Splice · crackedINSPECTION 4, UPPER CARGO LONGERON L18R SPLICE CRACKED BS 1521. R & R LONGERON SPLICE IAW SRM 51-33-01.SDR FDEA201407201881Floor Panel · corrodedCARGO FLOOR PANEL 232BF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407201884Seat Track · corrodedFOUND CORROSION ON CABIN SEAT TRACK FLANGE LOWER SURFACE FROM BS 1761 TO 1841, LBL 75. REPAIRED IAW EA1-5321-T0309846 PART1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407201883Floor Panel · corrodedCARGO METAL FLOOR PANEL 231AF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407201882Floor Panel · corrodedCARGO METAL FLOOR PANEL 231PF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407201880Floor Panel · corrodedRIGID CARGO BARRIER METAL FLOOR PANEL 233PF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1.SDR FDEA201407201877Floor Panel · corrodedCABIN - UPON REMOVAL OF RIGID CARGO BARIER METAL FLOOR PANEL 232PF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL FABRICATED PER DRAWING WSP0790 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-1SDR FDEA201407201879Floor Panel · corrodedMAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 232VF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL FABRICATED PER DRAWING WSP0785 REVISION B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 1SDR FDEA201407201878Floor Panel · corrodedMAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 233SF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL FABRICATED PER DWG WSP0785 REVISION B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122SDR FDEA201407201875Floor Panel · corrodedMAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 233UF FOUND CORRODED. REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL 233UF FABRICATED PER DRAWING WSP0785 REVISION B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122SDR FDEA201407201874Floor Panel · corrodedMAIN DECK CARGO FWD CABIN FLOOR METAL PANEL 231VF FOUND CORRODED RCB PANEL. REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122SDR FDEA201407201873Floor Panel · corrodedMAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 231BF FOUND CORRODED. REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122SDR IPXA2014080483852Angle · corrodedINSPECTION 4C, ANGLE LOCATED AFT OF CARGO DOOR CUTOUT BS 1142 BETWEEN L51 - 52R CORRODED. R & R ANGLE IAW SRM 51-33-01 AND SRM 51-35-01.SDR IPXA2014073083802Stringer · crackedINSPECTION 1C, STRINGER 51 CRACKED. REPAIRED STRINGER IAW EA 011-5710-01-A5492, REV.IR AND EO 5710-55061-A. MAJOR REPAIR.SDR IPXA2014081884001Stringer · crackedINSPECTION 4C, LT WING STRINGER 13 CRACKED BETWEEN XORS 562 AND 592. REPAIRED STRINGER IAW EA 011-5710-01-A5514, REV I/R AND EO 5710-55215-A.SDR IPXA2014081884000Stringer · crackedINSPECTION 4C, RT WING UPPER STRINGER 14R CRACKED AT XORS 506. REPAIRED STRINGER IAW EA 011-5710-01-A5515, REV I/R AND EO 5710-55214-A.SDR IPXA201408083889Intercostal · crackedINSPECTION 4C, APPOXIMATELY ONE INCH LONG CRACK AT NR 2 LOWER PYLON REAR CENTER SPAR TO REAR SPAR LOWER INTERCOSTAL. ACCOMPLISHED DOUBLER REPAIR IAW SRM-55-30-02, FIG 204, REPAIR 7.SDR IPXA2014080483846Stringer · crackedINSPECTION 4C, RT WING UPPER STRINGER 12 CRACKED. REPAIRED STRINGER IAW SRM 57-00-03, REPAIR 5, FIGURE 202, REV 56.SDR IPXA2014080483845Stringer · crackedINSPECTION 4C, LEFT WING UPPER STRINGER 11 CRACKED. REPAIRED STRINGER IAW SRM 57-00-03, REPAIR 5, FIGURE 202, REV 56. MAJOR REPAIR.SDR IPXA2014080483844Stringer · crackedINSPECTION TYPE:4C, LT WING UPPER STRINGER 9 OTBD END CRACKED APPROXIMATELY FOUR INCHES AT PREVIOUS REPAIR AREA. REPAIRED STRINGER 9 IAW SRM 57-00-03 REPAIR 5, FIG 202.SDR IPXA2014073083785Torque Box · crackedINSPECTION 4CL3, DOOR FRAME AFT TORQUE BOX CRACKED AT THE BOTTOM LIGHTNING HOLE. ACCOMPLISHED PERMANENT REPAIR TO L3 DOOR JAM AFT TORQUE BOX BOTTOM LIGHTNING HOLE IAW SRM 53-40-15, REPAIR 3, FIG 201, REV 55.SDR IPXA2014073083784Stringer · crackedINSPECTION 4C, RT WING UPPER STRINGER 9 CRACKED AT OTBD END APPROXIMATELY 4" IN LENGTH. ACCOMPLISHED PERMANENT REPAIR TO RT WING STRINGER 9 AT OTBD END IAW SRM 57-00-03, REPAIR 5, FIGURE 202, REV 55.SDR IPXA2014081884002Stringer · crackedINSPECTION 4C,STRINGER 51 CRACKED. REPAIRED IAW EA 011-5710-01-A5506, REV I/R AND EO 5710-55225-A.SDR IPXA2014081883999Stringer · crackedINSPECTION 4C, STRINGER 47 CRACKED. REPAIRED IAW EA 011-5710-01-A5508, REV I/R AND EO 5710-55226-A.SDR IPXA2014081883997Stringer · crackedINSPECTION 4C STRINGER 52 CRACKED. ACCOMPLISHED SPLICE REPAIR IAW EA 011-5710-01-A5507, REV I/R AND EO 5710-55216-A.SDR IPXA2014081583977Skin · corrodedINSPECTION 4C, RT WING UPPER SKIN PANEL HAS CORROSION AT STRINGER 3R, BETWEEN XORS 480.25 AND 538.49. REPAIRED SKIN IAW EA 011-5730-01-A5521, REV I/R AND EO 5730-55194-A.
Back to Boeing MD-11F