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 FDEA2019101092516Seat Track · damagedMAIN DECK SEAT TRACK AT BS 5-60, RBL 7.5 FOUND WITH CROWN DAMAGE. EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 5-43 TO EXISTING SPLICE BS 5-0 IAW SRM 53SDR FDEA2019101092517Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 1521, RBL 47.5 WAS FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1511 TO EXISTING SPLICESDR FDEA2019101092541Warning Message · false activationDURING CLIMBOUT RECIEVED LEVEL ONE ALERT FOR REV 2 PRESS FAULT, AND RED U/L ALERT. ON ARRIVAL A VISUAL CHECK OF REVERSER SHOWED FULLY STOWED, IAW CREW DEBRIEF WHEN THE THROTTLE WAS REDUCED TO FLIGHT IDLE, ALL INDICATIONS EXTINGUISHED. CHECKED FCC 1 AND FSDR IPXA2019103098432Landing · corrodedINSPECTION TYPE:2CR/H WING T/E AT PANEL # 641FB, THE PANEL LANDING IS CORRODED.REMOVED, FABRICATED AND REPLACED LANGING/TEE IAW DWG. ARC0307 AND SRM 51-33-01. (MINOR)SDR IPXA2019103098431Floor Support · corrodedINSPECTION TYPE:2CAFT CARGO FLOOR SUPPORT ANGLE IS CORRODED BETWEEN STA. 1902-16-967 R/H SIDE.REMOVED, FABRICATED AND REPLKACED SUPPORT ANGLE IAW DWG. AGA3857 AND SRM 51-35-01. (MINOR)SDR IPXA2019103098429Beam · crackedINSPECTION TYPE:2CFWD. CARGO TRANVERSE BEAM IS CRACKED AT STA. 6-73 ABOVE LONG. 43 R/H.REMOVED, FABRICATED AND REPLACED TRANVERSE BEAM AT STA. 6-73 AND LONG. 43 R/H IAW DWG. ADA7667 AND SRM 51-35-01. (MINOR)SDR IPXA2019102538217Skin · gougedINSPECTION TYPE:2CRT WING FIXED L/E SKIN UPPER SURFACE O/B OF #8 SLAT IS GOUGED.REPAIRED GOUGED RT WING FIXED L/E SKIN UPPER SURFACE O/B OF #8 SLAT IAW MD-11 SRM 57-40-01, REPAIR 16, FIGURE 201. (MAJOR)SDR IPXA2019102548269Longeron Splice · crackedINSPECTION TYPE:2CCENTER CARGO LONGERON 30R SPLICE FITTING IS CRACKED BETWEEN STA. 1661-1681.REMOVED, FABRICATED AND REPLACED CENTER CARGO LONGERON 30R SPLICE FITTING IAW DWG. AFA7797 AND SRM 51-31-01. (MINOR)SDR IPXA2019102548267Longeron Splice · crackedINSPECTION TYPE:2CCENTER CARGO LONGERON 29R SPLICE FITTING IS CRACKED BETWEEN STA. 1661-1681.REMOVED, FABRICATED AND REPLACED LONGERON 29R SPLICE FITTING BETWEEN STA. 1661-1681 IAW DWG. AFA7797 AND SRM 51-51-31-01. (MINOR)SDR IPXA2019102548238Floor Support · corrodedINSPECTION TYPE:2CAFT CARGO FLOORBOARD LANDING HAS CORROSION AT STA. 1887 L/H SIDE.REMOVED, FABRICATED AND REPLACED LANDING IAW DWG. AGA3857 AND SRM 51-35-01. (MINOR)SDR IPXA2019102348196Angle · crackedINSPECTION TYPE:2CCENTER CARGO L/H SIDE FLOOR SUPPORT ANGLE IS CRACKED AT STA. 1781.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG.AFA7295 AND SRM 51-33-01. (MINOR)SDR IPXA2019102348195Stiffener · crackedINSPECTION TYPE:2CAFT CARGO R/H SIDE VERTICAL STIFFNER IS CRACKED AT STA. 1841.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2019101877991Tee Fitting · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15R TEE ANGLE IS CRACKED AT STA. 1339.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15R TEE ANGLE AT STA. 1339 IAW MD-11 SRM 51-35-01. (MINOR)SDR IPXA2019101877990Tee Fitting · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15L TEE ANGLE IS CRACKED AT STA. 1339.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15L TEE ANGLE IAW MD-11 SRM 51-35-01. (MINOR)SDR FDEA201910102491Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 1282, LBL 47.5 FOUND CROWN DAMAGED. EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1313 IAW SRM 53-00-52-2R, FIGURESDR IPXA2019101657949Vane · damagedINSPECTION TYPE:2CLT WING I/B FLAP VANE L/E I/B END PREVIOUS REPAIR IS DAMAGED.REPAIRED DAMAGED LT WING I/B FLAP VANE L/E I/B END IAW MD-11 SRM 57-50-80, REPAIR 2, PAR. 2.A.(2).(A)(5), FIGURE 201. (MAJOR)SDR FDEA2019101082490Seat Track · corrodedFORWARD CABIN FLOOR SEAT TRACK AT STA 445, RBL 35 FOUND CORROSION. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . SEAT TRACK REMOVED AND REPLACED FROM BS 440 TO 495, RBL 35 IAW SRM 51-31-01-0G . REPAIR CSDR IPXA2019100987670Transmitter · false indicationTIRE FAILURE ON TAKE OFF, AIR TURN BACK. ALL TIRE PRESSURES NORMAL. INDICATION FAULT. R & R THE NR 5 TRANSMISSION TIRE PRESSURE BRAKE TEMP IAW AMM 32-46-08-401. OPS CK GOOD.SDR FDEA201910072479Floor Support · corrodedBS 1982 RBL 25 FLOOR SUPPORT FOUND CORRODED. FOUND TO EXCEED LIMITS IAW SRM 53-00-00-2R, FIGURE 206, ALLOWABLE DAMAGE . FABRICATED A NEW FLOOR SUPPORT IAW DRAWING AGA 7087, REVISION M. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN BS 1887 TO 2007 IAW SRSDR IPXA2019103098457Skin · chafedINSPECTION TYPE:2CL/H WING #8 SLAT LOWER SKIN IS CHAFED BETWEEN STA. XOS.1005.124 & 1015.511.REPAIRED L/H WING # 8 SLAT IAW VT-SAA EA 011-5710-01-A7932 REV. I/R AND UPS EO MD11-5740-74426-A. (MINOR)SDR IPXA2019102868322Intercostal · crackedINSPECTION TYPE:2CLOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR R/H INTERCOSTAL AFT END IS CRACKED BETWEEN STA. YID=375, XID=-7.1 AND ZID=65.REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR R/H INTERCOSTAL AFT END BETWEEN STA.SDR IPXA2019102548245Landing · corrodedINSPECTION TYPE:2CL/H WING SPOILER PANEL SILL IS CORRODED BETWEEN STA. XOFH=453.931 TO XOSP=499.36.REPAIRED L/H WING SPOILER PANEL SILL BETWEEN STA. XOFH=453.931 TO XOSP=499.36 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)SDR IPXA2019102548270Skin · crackedINSPECTION TYPE:2CR/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS= 487.REPAIRED CRACKED R/H WING L/E LOWER SKIN BETWEEN STA. XOS=487.351 TO 490.850 IAW VT-SAA EA 011-5740-01-A7926 REV. I/R AD UPS EO MD11-5740-74435-A. (MAJOR)SDR IPXA2019102248165Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E SPLICE DOUBLER IS CRACKED AT STA. XOS.=799.REMOVED, FABRICATED AND REPLACED SPLICE DOUBLER ON L/H WING AT STA. XOS.=799 IAW DWG. ARB3954 AND SRM 51-33-01. (MINOR)SDR IPXA2019102328162Skin · crackedINSPECTION TYPE:2CL/H WING L/E UPPER SKIN IS CRACKED AT STA. XOS.=464 TO 470.REPAIRED CRACKED L/H WING L/E UPPER SKIN BETWEEN STA XOS.=464-470 IAW SRM 57-40-01 REPAIR 10 FIG. 201. (MAJOR)SDR IPXA2019102328182Skin · chafedINSPECTION TYPE:2CLT WING FIXED L/E O/B BULLNOSE (SKIN) UPPER SURFACE O/B OF #8 SLAT IS CHAFED.REPAIRED CHAFED LT WING FIXED L/E BULLNOSE (SKIN) UPPER SURFACE O/B OF #8 SLAT IAW MD-11 SRM 57-40-01, REPAIR 16, FIGURE 201. (MAJOR)SDR IPXA2019102104877Skin · crackedINSPECTION TYPE:2CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS.=717.REPAIRED CRACKED L/H WING L/E SKIN AT STA. XOS.=717 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)SDR IPXA2019102104876Doubler · gougedINSPECTION TYPE:2CR/H WING L/E SKIN REPAIR DOUBLER IS DAMAGED AT STA. XOS.=734.7 TO 763.6.REMOVED AND REPLACED DOUBLER ON R/H WING L/E SKIN IAW SRM 57-40-02 REPAIR 5 FIG. 201.SDR IPXA2019102184838Doubler · crackedINSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS. 661.71 - XOS. 667.67.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS. 661.71 - XOS. 667.67 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR IPXA2019101848014Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS. 667.6 - XOS. 673.6.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS. 667.6 - XOS. 673.6 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR IPXA2019101877988Support Angle · crackedINSPECTION TYPE:2CAFT ACCESSORY COMPARTMENT 316 UPPER R/H SUPPORT ANGLE FOR SURGE DUCT IS CRACKED.REMOVED AND REPLACED CRACKED AFT ACCESSORY COMPARTMENT 316 UPPER R/H SUPPORT ANGLE FOR SURGE DUCT IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2019101877985Rib · crackedINSPECTION TYPE:2CRT WING O/B FIXED L/E RIB O/B OF #19 SLAT TRACK IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FIXED L/E RIB O/B OF #19 SLAT TRACK IAW MD-11 SRM 51-33-01. (MINOR)SDR IPXA2019101877983Intercostal · crackedINSPECTION TYPE:2CCENTER ACCESSORY COMPARTMENT CEILING R/H O/B INTERCOSTAL FWD LOWER FLANGE IS CRACKED.REMOVED AND REPLACED CRACKED CENTER ACCESSORY COMPARTMENT CEILING R/H O/B INTERCOSTAL IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2019101874800Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT F/S 1152, RBL=108 AND STRINGER 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT F/S 1152, RBL=108 AND STRINGER 15 IAW VT-SAA EA 011-5730-01-A7927 REV. IR AND UPS EO MD11-5730-74362-A. (MINOR)SDR FDEA201910072484Adc · failedDURING CLIMBOUT, NOTICED FIRST OFFICER'S AIRSPEED AND CAPTAIN AIRSPEED DID NOT MATCH, DETERMINED F/O INDICATOR WAS UNRELIABLE. STANDBY AIRSPEED AND ALTIMETER MATCHED THE CAPTAIN'S, NR 2 ADC FAILED A FUNCTIONAL TEST, R & R THE NR 2 ADC IAW MM 34-16-01-SDR FDEA2019100762470Floorbeam · corrodedAFT CARGO COMPARTMENT RIGHT FLOORBEAM AT STATION 1902, BETWEEN X=-20 AND X=-30 FOUND CORRODED. REPAIRED THE FLOORBEAM IAW EA 1-5321-T0349919 A P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910062474Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 755, RBL 8.5 WAS FOUND WITH CROWN DAMAGE. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE DAMAGED SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 785 TO 745 IAW SRM 53-00-52-2R, FIGUSDR FDEA2019100762473Seat Track · damagedMAIN DECK SEAT TRACK AT BS 1282, LBL 8.5 WAS FOUND WITH CROWN DAMAGE. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1313 IAW SRM 53-00-52-2R, FIGURE 201, RESDR FDEA2019100762472Seat Track · damagedMAIN DECK SEAT TRACK AT BS 1282, RBL 8.5, WS FOUND WITH CROWN DAMAGE. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1313 IAW SRM 53-00-52-2R, FIGURE 201, REPASDR FDEA2019100762471Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 775, X = 75.25 FOUND CROWN DAMAGED. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 782 TO BS 765 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR SDR IPXA2019102328166Skin · crackedINSPECTION TYPE:2C#1 PYLON O/B SIDE SKIN ABOVE EXHAUST VENT IS CRACKED.REPAIRED #1 PYLON O/B SIDE SKIN IAW SRM 54-00-00 REPAIR GENERAL FIG. 204. (MINOR)SDR FDEA2019100752450Hinge Bracket · corrodedRIGHT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0330908 A, PART 1, STEP 1SDR FDEA2019100752449Hinge Bracket · corrodedLEFT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0330906 A, PART 1, STEP 1, F(1), ANSDR FDEA2019100752448Hinge Bracket · corrodedLEFT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-04. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-04, AND EA 1-5750-T0349971, PART 1,SDR FDEA2019100752447Hinge Bracket · corrodedLEFT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE FOUND CORRODED. CORROSION REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-04 , REPAIR EVALUATED AND FOUND THE LEFT OUTBOARD FLAP AFT INBOARD HINGE PIVOT INBOARD LUG SURFACE REMSDR FDEA2019100752446Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORRODED. CORROSION WORKED AND IAW CMM 57-44-08 FOUND TO EXCEED LIMITS. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0349923, PART 1, STEP 3. THESDR FDEA201910052440Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE APPROXIMATELY XOS 538 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE APPROXIMATELY XOS 538 BEADED DOUBLER AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GSDR FDEA2019100752442Doubler · crackedRIGHT WING FIXED WING LEADING EDGE APPROXIMATELY XOS 653, BEADED DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910052441Doubler · crackedRIGHT WING FIXED WING LEADING EDGE APPROXIMATELY XOS 593 BEADED DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019100752439Doubler · crackedRIGHT HAND WING FIXED WING LEADING EDGE APPROXIMATELY XOS 528 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE APPROXIMATELY XOS 528 BEADED DOUBLER AREA AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS M
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