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 FDEA201808212147Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1880, X=-27.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1771 TO 1887, IAW SRM 53SDR FDEA201808212146Seat Track · corrodedMAIN DECK SEAT TRACK, BS 1880 X=-8.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT, FROM BS 1771 TO 1887 IAW SRM 53-00-5SDR IPXA2018083103386Landing · crackedRIGHT WING FUEL TANK ACCESS PANEL 636AB LANDING HAD FIVE CRACKS, AT FASTENER HOLES BETWEEN XORS 683.40 - 713.65. REPAIRED THE ACCESS PANEL LANDING IAW SRM 57-20-02, REPAIR 5, FIG 201. MINOR.SDR IPXA2018083133420Landing · crackedLEFT WING LOWER FUEL ACCESS PANEL 536AB LANDING HAD SEVEN CRACKS, AT THE FASTENER HOLES BETWEEN XORS 683.4 TO 713.65. REPAIRED THE ACCESS PANEL LANDING IAW SRM 57-50-02, REPAIR 5, FIG 201. MINOR.SDR FDEA201808212148Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 475, X=75.25 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK FLANGE IAW SRM 53-00-52-2R, FIG 201, REPAIR 5. THE REPAIR WAS CLASSSDR FDEA201808212145Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 455, X= 27.5 FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS421 - 467, IAW SRM 53-00- 52-2R, SDR IPXA2018082213306Battery · inoperativeL1 DOOR SLIDE REMOTE PRESS INDICATION INOPERATIVE. ACCOMPLISHED AN INSPECTION IAW DMP 25-61-2, SLIDE HAS ADEQUATE PRESSURE. R & R THE L1 DOOR SLIDE INDICATOR BATTERY IAW AMM 25-61-04-401 & CHECKED NORMAL.SDR IPXA2018082233091Engine · fireRETURNED TO BLOCKS DUE TO A FIRE ON THE NR 3 ENGINE DURING PUSH & START. ACCOMPLISHED K ALER K182779, AND EO 4000-7100-69656-A. ENGINE OK FOR SERVICE.SDR SRXR201808210024Skin · corrodedUPPER FWD RUDDER HAD CORROSION ON THE LOWER RT SIDE. REPAIRED IAW SRM 55-40-01, REPAIR 1, FIG 201.SDR SRXR201808210023Pin · wornFWD TAILCONE MID RH GUIDE PIN WORN THROUGH SURROUNDING STRUCTURE. ACCOMPLISHED REPAIR AT FWD TAILCONE IAW SRM 53-80-07 REPAIR 1.SDR SRXR201808210022Beam · gougedSTRUCTURE IS GOUGED INSIDE FWD TAILCONE ABOVE LADDER. REMOVED AND REPLACED FWD TAILCONE BEAM, SUPPRT FITTING AND UPPER LATCH FITTING PER MD-11 SRM 51-31-01 AND SRM 53-00-00 FIG 210 REF VT SAA NRC# A042754.SDR IPXA2018090433460Frame · crackedINSPECTION TYPE:4C, TAIL CONE LT SIDE FRAME AT CANT STA 2164 CENTER GUIDE PIN HOLE HAS APPROX .750" CRACK. REPAIRED TAIL CONE LT SIDE FRAME AT CANT STA 2164 CENTER GUIDE PIN HOLE IAW SRM 53-80-07 REPAIR 1. (MINOR)SDR IPXA2018090433459Beam · chafedINSPECTION TYPE:4C, TAIL CONE HORIZONTAL BEAM FWD SIDE REPAIR DOUBLER IS CHAFED THROUGH IN 2 PLACES. REPAIRED TAIL CONE HORIZONTAL BEAM IAW SRM 51-31-01 AND 53-00-00 REPAIR 1. (MINOR)SDR IPXA2018083133419Intercostal · wornTAIL CONE UPPER LT PATIO DOOR INTERCOSTAL WAS WORN THROUGH. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG AKC7868, AND SRM 51-31-01. MINOR.SDR IPXA2018083133418Intercostal · wornTAIL CONE UPPER RT PATIO DOOR INTERCOSTAL WAS WORN THROUGH. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG AKC7865, AND SRM 51-31-01. MINOR.SDR IPXA2018090733632Skin · chafedINSPECTION TYPE:4C, RT UPPER INNER SKIN DOUBLER IS HEAVILY CHAFED ON FWD TAIL CONE AT FUSELAGE MATING SURFACE. REPAIRED FWD TAIL CONE INNER SKIN AT CANT STA Y=2163.685 TO Y=2165.6, X=-36.5, Z=60.1 IAW EA 011-5350-01-A7440 REV IR AND EO MD11-5350-69674-A. (MINOSDR IPXA2018090433457Stiffener · crackedINSPECTION TYPE:4C, NR 1 PYLON PANEL STIFFENER (CLIP) JUST ABOVE AND O/B OF PRECOOLER IS CRACKED AT UPPER MIDDLE AREA. REMOVED AND REPLACED NR 1 PYLON PANEL STIFFENER (CLIP) JUST ABOVE AND O/B OF PRECOOLER IAW SRM 54-05-46 AND 54-05-41. (MINOR)SDR IPXA2018090433456Bracket · crackedINSPECTION TYPE:4C3, 1 PYLON ANGLE BRACKET (CLIP) JUST FWD OF PRECOOLER IS CRACKED AT UPPER END. REMOVED AND REPLACED NR 1 PYLON ANGLE BRACKET (CLIP) JUST FWD OF PRECOOLER IAW SRM 54-05-46 AND 54-05-41. (MINOR)SDR SRXR201808190021Stiffener · corrodedLEFT VERTICAL STIFFENER IN THE AVIONICS BAY DOOR CUTOUT WAS CORRODED. ACCOMPLISHED A REPAIR IAW SRM 51-33-01, PARA 8B.SDR IPXA2018100864736Rub Strip · damagedLEFT WING NR 2 SLAT, OTBD SIDE, UPPER T/E RUBSTRIP WAS DAMAGED ON THE LOWER SURFACE. REMOVED AND REPLACED THE RUBSTRIP IAW EA 011-5754-01-A7488, REV IR, AND EO MD11-5750-70152-A. MINOR.SDR IPXA2018090733667Seal · tornINSPECTION TYPE:4C, LT WING FLAP PANEL 535AL SEAL IS TORN. REPAIRED TORN LT WING FLAP PANEL 535AL SEAL IAW EA 011-5754-01-A7453 REV I/R AND EO MD11-5750-69819-A. (MINOR)SDR IPXA2018090733663Stringer · crackedINSPECTION TYPE:4C, LT WING STRINGER NR 9 IS CRACKED AT STA XORS 538.5. REPAIRED CRACKED LT WING STRINGER NR 9 BETWEEN STA XORS 506.0 TO XORS 565.39 IAW EA 011-5710-01-A7444 REV I/R AND EO MD11-5710-69818-A. (MAJOR)SDR FDEA2018082182101Fitting · crackedLOWER VERTICAL STABILIZER FRONT CENTER SPAR FITTING FOUND CRACKED AT AFT FUSELAGE COMPARTMENT LEFT HAND SIDE APPROXIMATE STA 2014. CRACKED LOWER VERTICAL STABILIZER FRONT CENTER SPAR FITTING AT AFT FUSELAGE COMPARTMENT LEFT HAND SIDE APPROXIMATE STA 2014 REPASDR IPXA2018090433455Support Angle · crackedINSPECTION TYPE:4C, NR 3 PYLON SUPPORT ANGLE (CLIP) ABOVE FWD SIDE OF PRECOOLER HAS 2 CRACKS AT UPPER END. REMOVED AND REPLACED NR 3 PYLON SUPPORT ANGLE (CLIP) ABOVE FWD SIDE OF PRECOOLER IAW SRM 51-31-01 AND 54-05-41. (MINOR)SDR FDEA2018082182100Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 642 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018082182099Seat Track · crackedMAIN DECK SEAT TRACK AT BS 755, LBL 47.5 WAS FOUND CRACKED. THE SEAT TRACK WAS REPLACED BETWEEN BS 725 & 765, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018082182098Seat Track · crackedMAIN DECK SEAT TRACK AT BS 755, RBL 8.5 FOUND CRACKED. SEAT TRACK REPLACED FROM BS 785 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018082182097Frame · damagedMAIN DECK LEFT FRAME AT BS 1641, LONGERON 12L WAS FOUND DAMAGED. THE FRAME WAS REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2018082983299Floorbeam · crackedLOWER CENTER CARGO, BS 1521, FLOORBEAM ANGLE WAS CRACKED BETWEEN LBL 8 TO LBL 25. REMOVED, FABRICATED, AND REPLACED THE FLOORBEAM ANGLE IAW DWG AEA0341, AND SRM 51-35-01. MINOR.SDR SRXR201808180020Bulkhead · crackedNR 1 PYLON CENTER STRUCTURE BULKHEAD, INBD SIDE WAS CRACKED AT YN 307. ACCOMPLISHED A REPAIR ON THE PYLON BULKHEAD IAW EA 011-5450-52-A7385, I/R.SDR SRXR201808180019Trunnion · gougedNLG TRUNION FITTING, LT SIDE WAS GOUGED. ACCOMPLISHED A BLEND OUT REPAIR IAW EA 011-5310-52-A7326, IR.SDR SRXR201808180018Plate · corrodedLEFT PRIMARY AND SECONDARY STATIC PORT PLATES, INTERIOR SIDE, HAD CORROSION. ACCOMPLISHED A BLEND OUT REPAIR ON THE LT PRIMARY AND SECONDARY STATIC PORT PLATES IAW EA 011-3411-52-A7389, I/R.SDR IPXA2018090733664Bushing · wornINSPECTION TYPE:4C, RT WING NR 1 SLAT O/B RIB LUG BUSHING IS WORN. REMOVED AND REPLACED RT WING NR 1 SLAT IAW AMM27-80-20-400-801. (MINOR)SDR IPXA2018090433454Rib · corrodedINSPECTION TYPE:4C, RT WING TO FUSELAGE FILLET RIB AT STA Y=5-53 HAS CORROSION. REPAIRED RT WING TO FUSELAGE FILLET RIB AT STA Y=5-53 IAW SRM 53-00-00 FIG 209 DETAIL III, 51-31-01 AND 51-35-01. (MINOR)SDR IPXA2018082933368Skin · dentedA DENT WAS FOUND ON THE INNER SKIN OF THE LT NR 5 SLAT, APPROXIMATELY 22 INCHES OTBD OF THE SLAT TRACK NR 10, AND 10 INCHES BELOW THE T/E. REPAIRED THE LT WING SLAT LOWER SKIN BETWEEN XOS 680.893 AND 686.092, IAW EA 011-5754-01-A7443, REV IR, AND EO MD11-5SDR IPXA2018082983302Bushing · wornRIGHT NOSE GEAR TRUNNION BUSHING WAS WORN. REMOVED, FABRICATED, AND RELACED THE RT NOSE GEAR TRUNNION BUSHING IAW DWG ACA7007, AND SRM 53-10-14. MINOR.SDR IPXA2018082733253Skin · crackedRIGHT WING FIXED L/E SKIN LOWER SURFACE WAS CRACKED AT THE NR 5 SLAT TRACK CUT-OUT, XOS. 775. REPAIRED THE FIXED L/E SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.SDR IPXA2018082033008Wire Harness · shortedDURING DESCENT, RECEIVED A LEVEL 1 ENG 3 FADEC MAINT MESSAGE. ENGINE 3 THROTTLE WAS UNRESPONSIVE AND STUCK AT 7% N1. SELECTED FADEC ALTERNATE MODE WITH NO EFFECT. SHUTDOWN THE NR 3 ENGINE IN FLIGHT, UNEVENTFUL LANDING. REPLACED 3 NR 3 ENGINE FAN CASE WIRISDR FDEA201808172066Sleeve · damagedDURING A POSTFLIGHT INSPECTION, FOUND THE NR 9 BRAKE WAS COMING APART. THE AXLE SLEEVE WAS CRACKED AT THE LOCKING TAB AND THE BRAKE WAS COMING APART AT THE OUTER DISC, DAMAGED THE WHEEL ASSY. THE AXLE SLEEVE WAW REMOVED IAW AMM 32-15-00-4. THE BRAKE ANDSDR IPXA2018090733662Skin · dentedINSPECTION TYPE:4C, LT WING NR 4 SLAT UPPER SKIN BETWEEN STA XOS 571-580 HAS MULTIPLE DENTS AND PREVIOUS REPAIR. REPAIRED DAMAGED NR 4 SLAT BETWEEN STA XOS 571-580 IAW EA 011-5750-01-A7450 REV I/R AND EO MD11-5750-69820-A. (MAJOR)SDR IPXA2018090533576Seal · damagedINSPECTION TYPE:4C, LT SIDE WING TO FUSELAGE UPPER FAIRING SEAL HAS EDGE DAMAGE. REPAIRED DAMAGED LT SIDE WING TO FUSELAGE UPPER FAIRING SEAL IAW EA 011-5350-01-A7447 REV I/R AND EO MD11-5350-69781-A. (MINOR)SDR IPXA2018090533596Seal · tornINSPECTION TYPE:4C, RT WING PANEL 635AL HAS A TORN BULB SEAL. REPAIRED RT WING PANEL 635AL SEAL IAW EA 011-5754-01-A7448 REV I/R AND EO MD11-5750-69808-A. (MINOR)SDR FDEA2018081762060Skin · crackedNR 3 AIR CONDITIONING ACCESS DOOR 114AR. UPPER AFT CORNER SKIN CUTOUT WAS FOUND CRACKED AT BS 535. REPAIRED IAW SRM 53-20-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762063Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 626 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762062Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762061Doubler · crackedRIGHT WING LEADING EDGE CAVITY, BEADED DOUBLER AT XOS 652 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762059Doubler · crackedLEFT WING LEADING EDGE CAVITY BEADED DOUBLER, XOS 553 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762058Seat Track · wornMAIN DECK SEAT TRACK AT BS 775, RBL 75.25 CROWN WAS DAMAGED. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT BETWEEN BS 815 & 765 IAW SRM 53-00-52-2R, FISDR FDEA2018081760257Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 1560, LBL 27.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT, BS 1571 TO EXISTING SPLICE IAW SRSDR FDEA201808176056Seat Track · wornMAIN DECK SEAT TRACK AT BS 1421, LBL 47.5, WAS THE CROWN WAS FOUND DAMAGED. THE SEAT TRACK WAS BLENDED AND FOUN OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT, BS 1411 - 1451 IAW SRM
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