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 IPXA2016062004815Fitting · corrodedINSPECTION TYPE:M15, RIGID CARGO BARRIER FLOOR FITTING NR 7 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING NR 7 IAW VT-SAA EA 011-5340-01-A6317, REV I/R AND EO MD11-5340-61069-A.SDR IPXA2016062004814Fitting · corrodedINSPECTION TYPE:M15, RIGID CARGO BARRIER FLOOR FITTING NR 4 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING IAW EA 011-5340-01-A6317 AND EO MD11-5340-61069-A.SDR IPXA2016062004813Fitting · corrodedINSPECTION TYPE:M15, RIGID CARGO BARRIER FLOOR FITTING NR 6 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING NR 6 IAW VT-SAA EA 011-5340-01-A6317 REV I/R AND EO MD11-5340-61069-A.SDR IPXA2016062004812Fitting · corrodedINSPECTION TYPE:M15, RIGID CARGO BARRIER FLOOR FITTING NR 5 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING NR 5 IAW VT-SAA EA 011-5340-01-A6317 REV I/R AND EO MD11-5340-61069-A.SDR IPXA2016061604684Cover · looseSLIDE COVER ON L1 IS LOOSE. RE-SECURED SLIDE COVER.SDR IPXA2016070205319Elevator · damagedINSPECTION TYPE:1C, LIGHTNING STRIKE DAMAGE ON LT OTBD ELEVATOR TIP REQUIRES PERM REPAIR. REPAIRED NOTED LIGHTNING STRIKE DAMAGE IAW EA 011-5520-01-A6330, REV IR AND EO MD11-5520-61152-A.SDR IPXA2016070205317Skin · corrodedINSPECTION TYPE:1C, FUSELAGE EXTERIOR SKIN CORRODED STA 2138-2163, L33R - L35R, CORROSION REPAIRED IAW EA 011-5330-01-A6323, REV IR AND UPS EO MD11-5330-61142-A.SDR IPXA2016070105282Attach Bracket · damagedINSPECTION TYPE:1C, RT OTBD FLAP INBD HINGE T/E FAIRING ATTACH BRACKET, ALL MOUNT HOLES ELONGATED. REPAIRED FAIRING ATTACH BRACKET IAW EA 011-5730-01-A6337, REV IR AND EO MD11-5740-61140-ASDR IPXA2016063005229Shear Tie · crackedINSPECTION TYPE: 1C, SHEAR TIE CRACKED IN 316 COMPT CROWN AREA. REPAIRED THE SHEAR TIE IAW SRM 53-70-07 REPAIR 1 FIG. 201. (MAJOR)SDR IPXA2016062805166Skin · damagedINSPECTION TYPE:SV, FUSELAGE SKIN DENTED AND GOUGED STA 1921, L48L-L48R. REPAIRED NOTED SKIN DAMAGED BETWEEN STA 1921-1941, L48L-L48R IAW EA 011-5330-01-A6316, REV IR AND EO MD11-5330-61108-A.SDR FDEA201606141996Limit Switch · malfunctionedRIGHT FORWARD PASSENGER DOOR WILL CLOSE, BUT WILL NOT OPEN ELECTRICALLY. R & R GIRT BAR LIMIT SWITCH AND POWER INTERLOCK SWITCH IAW AMM 52-11-02-5. OPS CHECK GOOD. ACFT OK FOR SERVICE.SDR IPXA2016062004821Fitting · corrodedINSPECTION TYPE:M15, RIGID CARGO BARRIER FLOOR FITTING NR 2 HAS CORROSION. R & R RCB FLOOR FITTING NR 2 ON EO MD11-2520-58701-D.SDR IPXA2016062004842Structure · corrodedINSPECTION TYPE:M15, RIGID CARGO BARRIER WALL HAS CORROSION AT FLOOR ATTACH FITTINGS. R & R RIGID CARGO BARRIER WALL IAW EO MD11-2520-58701-D AND AMM 25-59-13-400-801.SDR IPXA2016062004838Fitting · crackedINSPECTION TYPE:M15, RIGID CARGO BARRIER FLOOR FITTING NR 1 IS CRACKED. R & R RCB FLOOR FITTING NR 1 IAW EO MD11-2520-58701-D.SDR FDEA201606141999Cover · unsecureLEFT ENTRANCE DOOR, L1 WILL NOT ARM, JAMMED LEVER. RESECURED SLIDE COVER IAW MM 25-61-15-4. OPS CHECK GOOD, ACFT OK FOR SERVICE.SDR FDEA201606141993Fitting · corrodedRIGHT WING OTBD FLAP VANE HORN FITTING-D, FWD HOLE CORROSION. CORROSION FOUND TO EXCEED LIMIT IAW SRM 57-50-02, REPAIR 5, FIGURE 201. EXISTING SLOT: 0.890", LENGTH, 0.625", WIDTH. FINAL SLOT: 0.965", LENGTH, 0.662", WIDTH. MAXIMUM ALLOWABLE: 0.940", LENGTHSDR FDEA201606141991Hinge · corrodedLT WING OTBD FLAP, INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.162", MAXIMUM ALLOWABLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750SDR FDEA201606131975Skin · cracked12 EA, NR 7, 8, 9, 10, 11, 12, 13, 14, 28, 32, 33, 34, FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS =683.4 AND STA XORS =713.6. CARRIED OUT BUSHING REPAIR IAW SRM 57-20-02-2R,SDR FDEA201606131974Skin · cracked02 EA, 10, NR 11, FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS =683.4 AND STA XORS =713.6. CARRIED OUT BUSHING REPAIR IAW SRM 57-20-02-2R, FIG 201 REPAIR 5. THE INITIAL INSPESDR IPXA2016061304588Battery Pack · dischargedEMERGENCY LT BAT 1 LOW DURING PREFLIGHT. R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-01, OPS TEST SATISFACTORY.SDR FDEA201606131981Hinge · corrodedLEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE SURFACE CORROSION. CORROSION FOUND EXCEEDED LIMIT AS CMM 57-52-03, EXISTING THICKNESS: 0.260", MATERIAL REMOVED: 0.074", REMAINING THICKNESS: 0.186", MINIMUM ALLOWABLE THICKNESS: 0.205". STRAP RESDR FDEA201606131976Rib · crackedLEFT FIXED L/E COMPARTMENT AT STA XOS 667, FOUND RIB CRACKED. RIB R & R IAW SRM 51-31-01-0G. THE NEW RIB FABRICATED IAW DWG ARB2930, REV "F". THE REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.SDR FDEA201606121964Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 1285, X=-8.75 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.SDR FDEA201606121957Skin · cracked1EA FASTENER HOLE FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN BS XORS =683.4 AND XORS =713.6. REPAIR BUSHING CARRIED OUT AT RT WING LOWER SKIN ACCESS DOOR CUTOUT IAW SRM 57-20-02-2R, FIG 201, REPSDR FDEA201606121970Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 755, X=-8.75, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 745 TO STA 783 X = -8.75 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121969Seat Track · damagedMAIN DECK CARGO COMPARTMENT. APPROXIMATELY AT STA 1159, X=75.5 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-100 TO STA 1169, X =75.5 IAW SRM 53-00-52-2R FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100SDR FDEA201606121968Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 6-4, X= 27.5, SEAT TRACK CROWN FOUND DAMAGED. FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-0 TO STA 6-40, X=27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM SDR FDEA201606121967Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 1149, X= 27.5, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121966Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 1531/5-4, X= 8.75 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121965Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 5-53, X= 47.5, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121963Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT STA 1520, X=47.5, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPLACEMENT FROM STA 1491 TO STA 5-0, X=47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121962Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT BS 1299, X= 8.5 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121961Seat Track · damagedMAIN DECK CARGO COMPARTMENT, APPROXIMATELY AT BS 1341, X= 27.5 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPLACEMENT FROM STA 1311 TO STA 1351, X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121960Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE FOUND CORRODED AT BS 1601- BS 1621, X= 8.0, OTBD. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121959Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE FOUND CORRODED AT BS 1621- BS 1641, X= 75, INBD. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121956Skin · cracked6 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA, XORS =683.4 AND XORS =713.6. REPAIR BUSHING CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XSDR IPXA2016061304538Switch · inoperative1L1 DOOR REMOTE PRESS TO TEST FOR EVAC SLIDE INOPERATIVE. R & R REMOTE PRESSURE INDICATOR SWITCH AND BATTERY IAW AMM 25-61-04.SDR FDEA201606101934Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT DENTED FRAME AT RT BS 5-53, LONGERON 12R. FRAME REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14500 FLT CYCLES AND REPETITIVE INSPECTION AT 9500 FLT CYCLES TO BE CARSDR FDEA201606101931Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.286", FINAL HOLE DIA 1.290", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783C, PASDR FDEA201606101930Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.253", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783, CSDR FDEA201606101929Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.375", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PSDR FDEA201606101928Hinge · corrodedLT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PT5,SDR FDEA201606101927Hinge · corrodedRT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA 0.644", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE DIA 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IAW EASDR FDEA201606101926Hinge · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA 0.594", FINAL HOLE DIA 0.705", MAXIMUM ALLOWABLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-SDR FDEA201606101925Hinge · corrodedLT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA 1.214", FINAL DIA 1.224", MAX ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892SDR FDEA201606101924Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.643", FINAL HOLE DIA: 0.716", MAXIMUM ALLOWABLE DIA: 0.709". REPAIR BUSHING FABRICATED AND INSTALLED ISDR FDEA201606101923Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDING LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.306", FINAL HOLE DIA: 2.3290", MAXIMUM ALLOWABLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201606101922Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.325" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED ANDSDR FDEA201606101921Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.324" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201606101920Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.582" FINAL HOLE, DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INS
Back to Boeing MD-11F