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 FDEA2019100752444Cable · failedUNABLE TO SET PARK BRAKE.PARK BRAKE KEEPS SPRINGING BACK. PARKING BRAKE CABLE AND ROD END REPLACED IAW AMM 32-44-00-5. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA2019100752457Brake · failedDURING PREFLIGHT, FOUND THE NR 8 BRAKE WITH MULTIPLE PIECES MISSING AND BROKEN. REMOVED AND REPLACED THE NR 8 MAIN BRAKE ASSY IAW 32-43-20-4. ACFT OK FOR SERVICE.SDR IPXA2019102328167Fairing · damagedINSPECTION TYPE:2C#1 ENG. I/B THRUST REVERSER BEAVER TAIL FAIRING HAS INCOMING OVERSIZE FASTENER HOLES EXCEEDING SRM LOIMITS.REPAIRED #1 ENG. I/B T/R BEAVER TAIL FAIRING IAW VT-SAA EA 011-7830-01-A7928 REV. I/R AND UPS EO MD11-7830-74334-A. (MINOR)SDR IPXA2019102184837Doubler · crackedINSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 610 - XOS. 616.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS. 610 - XOS. 616 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR FDEA201910042436Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52SDR FDEA201910042435Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201910042434Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201910042433Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR IPXA2019100447544Spring · brokenCABLE HANGING FROM LEFT SIDE OF L1 DOOR. R/R BROKEN TENSION SPRING & INSTALLED NEW CABLE ASSY. IAWAMM 52-11-03. OPS CK GOOD.SDR FDEA201910032418Stringer · crackedRIGHT WING, FIXED LEADING COMPARTMENT XOS 666, STRINGER CRACKED. THE STRINGER WAS REPAIRED IAW EA 1-5720-122505 A, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910032419Doubler · crackedCENTER LANDING GEAR COMPARTMENT, LEFT WEB DOUBLER AT BS 1380 WAS FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-33-01-0G, A NEW DOUBLER WA FABRICATED IAW DRAWING AEA 0526, REV NC, AND INSTALLED IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAWSDR FDEA201910032430Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TOE EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PARSDR FDEA201910032429Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, SDR FDEA201910032428Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, SDR FDEA201910032427Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CSDR FDEA201910032426Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CMM SDR FDEA201910032425Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3A, AND SDR FDEA201910032424Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T034988SDR FDEA201910032423Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTSDR FDEA201910032422Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED SDR FDEA201910032421Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED IAW CMSDR FDEA201910032420Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTSDR FDEA201910032431Battery Pack · failed"EMG BAT 1 LO" DURING PREFLIGHT. REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED GOOD.SDR FDEA2019100322401Rib · crackedRIGHT WING NR 5 SLAT INNER NR 8 RIB FROM INBOARD WAS FOUND CRACKED, FOUND DURING A BORESCOPE INSPECTION. THE NR 8 RIB WAS REPAIRED IAW EA 1-5750-T0350343 P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019100322400Rib · crackedLEFT WING NR 6 SLAT ASSEMBLY, INNER NR 3 RIB FROM INBOARD WAS FOUND CRACKED DURING A BORESCOPE INSPECTION. THE NR 3 RIB WAS REPAIRED IAW EA 1-5750-T0350336, P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019100322399Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750- T0349884, PART 1, STEP 3A, AND INSTALLED IAW CMM 57SDR FDEA2019100322402Skin · scratchedFUSELAGE SKIN BETWEEN BS 869 TO 929, LONGERON 9 RT WAS FOUND WITH SCRATCHES. THE SCRATCHES WERE REMOVED, 0.048", SKIN ORIGINAL THICKNESS 0.068", REMAINED THICKNESS 0.020" FOUND OUT OF LIMITD IAW SRM 53-00-00-2R, FIGURE 202. SKIN REPAIRED IAW SRM 53-00-01-SDR FDEA2019100322406Skin · corrodedRH WING UPPER SURFACE APPROX XORS 298 STRINGER 22 CORROSION AROUND FASTENER. REMOVED CORROSION IAW SRM 57-00-01-1A, SHEETS 6-8, AREA IS WITHIN LIMITS IAW SRM 57-00-01-1A, FIG 101, SHEET 1.SDR FDEA2019100322405Skin · corrodedRH WING UPPER SURFACE APPROX XORS 307 ABOVE STRINGER 16 CORRODED AROUND TWO FASTENERS. REMOVED CORROSION IAW SRM 57-00-01-1A, SHEETS 6-8, AREA IS WITHIN LIMITS IAW SRM 57-00-01-1A, FIG 101, SHEET 1.SDR FDEA201910012792Structure · delaminatedLEFT WING UPPER ISLAND STRUCTURE DELAMINATED FROM STATION XORS1044 TO XORS1093 (FROM DAC DRAWING ARC7169). REPAIRED L/H WING UPPER ISLAND STRUCTURE PER SRM 57-50-80-2R. REPAIR #3 PAGE 39.SDR FDEA2019100312392Seat Track · corrodedFORWARD CABIN SEAT TRACK LBL 19, BS 455 WAS FOUND WITH CORROSION ON THE FLANGE. THE CORROSION WAS FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DRAWING SP11530SDR FDEA2019100312391Seat Track · corrodedSEAT TRACK, BS 795 - 849, RBL 75.25 WAS FOUND CORRODED. THE CORROSION WAS FOUND TOE EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED BETWEEN BS 869 TO EXISTING SPLICE AT BS 765 IAW SRM 53-00-52-2R, FIGURE 201, SDR FDEA2019100312390Seat Track · corrodedBS 795 - 849, RBL 107.25 SEAT TRACK WAS FOUND CORRODED. THE CORROSION WAS FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACEED FROM BS 869 TO EXISTING SPLICE AT BS 765 IAW SRM 53-00-52-2R, FIGURE 201, RESDR FDEA2019100312379Seat Track · corrodedRIGHT SEAT TRACK AT BS 425 TO 455, RBL 27.5 WAS FOUND CORRODED. FOUND EXFOLIATION EXCEED LIMITS IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE, DAMAGE 1. THE SEAT TRACK WAS REMOVED AND REPLACED FROM BS 421.5 TO EXISTING SPLICE AT BS 485 IAW SRM 51-31-01-0G AND DSDR FDEA2019102412743Skin · crackedL/H SIDE LOWER FUSELAGE APROX. STA 575, L46L - L48L, FWD LWR CORNER OF EXHAUST HAS SKIN REPAIR. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED IAW SRM 53-20-15 FIG. 201, REPAIR 3.SDR FDEA2019102412732Seat Track · wornREPAIR ASSESSMENT: UPPER FUSELAGE MAIN CARGO, APROX. STA 799 - 819, LBL 27, HAS A SEAT TRACK REPAIR REPAIRED PER SRM 53-00-52-2R.SDR FDEA2019100312389Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, OUTBOARD BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349884, PART 1, STEP 3A, AND INSTALLSDR FDEA2019100312388Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, INBOARD BORE SURFACE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PARSDR FDEA201910012387Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE BRACKET, INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PSDR FDEA2019100312386Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE BRACKET, OUTBOARD LUG BORE WAS FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PSDR FDEA2019100312385Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE FITTING OTBD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3C, SDR FDEA2019100312384Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR, INBOARD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEPSDR FDEA2019100312383Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750- T0349824, PART 1, STEP 3,SDR FDEA2019100312382Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57- 44-09 AND EA 1-5750-T0349824, PART 1, STSDR FDEA2019100312381Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0349824, PART 1, STEP 3B, AND SSDR FDEA201909302377Seat Track · corrodedCABIN - SEAT TRACK AT STATION 435 TO STATION 455 X = 0 FOUND CORROSION . CABIN - SEAT TRACK AT STATION 435 TO STATION 455 X = 0 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVESDR FDEA2019100732478Doubler · crackedRIGHT WING - INBOARD LEADING EDGE - FORWARD LEADING EDGE PANEL LAND IS CRACKED, INBOARD OF NR 9 SLAT TRACK. R & R THE DOUBLER PER DWG ARB1180, AND SRM 51-31-01.SDR 9WGA2019100493001Director · failedFLIGHT DIRECTOR 1 FAIL, NAV WON'T ENGAGE, WON'T COME OUT OF TAKEOFF THRUST GCP MODE FMS MODE NOT ENGAGING, NO PERFORMANCE DATA CLIMBSDR FDEA201909292375Floor Support · corrodedMAIN DECK - AFT CARGO WASTE COMPARTMENT CEILING FLOOR SUPPORT APPTOXIMATELY AT STATION 1936 TO STATION 2000 X= - 56 FOUND CORROSION . MAIN DECK AT AFT FLOOR SUPPORT STATION 1936 TO STATION 2000 X = - 56 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PERSDR FDEA201909292374Floor Support · corrodedCABIN LEFT HAND STATION 1965 X = 56 FLOOR SUPPORT FOUND CORROSION . CABIN AT LEFT HAND FLOOR SUPPORT STATION 1965 X = 56 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE . CORRODED FLOOR SUPPORT REMOVED AND
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