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 IPXA2018100394641Inlet · crackedNR 2 ENGINE INLET LIP HAD A CRACK AT THE 1:00 O`CLOCK POSITION, AT A FASTENER. REPAIRED THE NR 2 ENGINE INLET LIP IAW SRM 54-10-01, REPAIR 4. MINOR.SDR FDEA2018091852548Shear Tie · damagedDURING DVI INSPECTION PER EA 1-5330-T0342358 PART1 P9 NO DAMAGE WAS NOTED TO FUSELAGE FRAMES. HOWEVER, DAMAGE TO FRAME SHEAR TIE BETWEEN LONGERON L51L AND L50L AND ALSO BETWEEN LONGERON L50L AND L49L WAS NOTED. REPLACED DAMAGED SHEAR TIE IRW EA 1-5330-T0342358SDR FDEA201809142539Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X=-2 FOUND CORROSION ON FLANGE AT STA 1962 AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1962, X= -2 REPAIRED AS PER SRM 53-00-52-2R FISDR FDEA201809142536Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X= 2 FOUND CORROSION ON FLANGE AT STA 1910 AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1910, X= 2 REPAIRED AS PER SRM 53-00-52-2R FIG 20SDR FDEA201809142542Spar · crackedHFEC INSPECTION CARRIED OUT ON LT REAR SPAR CAP FORWARD FLANGE LOCATED AT THE UPPER SECTION OF NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER , STA Y=2164 AND FOUND CRACK APPROX. 1.5 " LENGTH. SPAR CAP FORWARD FLANGE TRIMMED AS PER SRM 55-30-02-2R FIGURE 201SDR FDEA201809142541Spar · crackedHFEC INSPECTION CARRIED OUT ON RT REAR SPAR CAP FORWARD FLANGE LOCATED AT THE UPPER SECTION OF NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER, STA 2164 AND FOUND CRACK APPROX 0.2" LENGTH. SPAR CAP FORWARD FLANGE TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAISDR FDEA201809142537Floor Support · corrodedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X= 25 FOUND CORROSION. FLOOR SUPPORT CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICASDR IPXA2018100394619Trunnion · damagedNLG, RT TRUNNION, INBD HAT BUSHING WAS BROKEN. FOUND THE RT NLG TRUNNION, INBD BUSHING BORE SPOT FACE OUT OF LIMITS. REPAIRED THE NLG TRUNNION BUSHING BORE IAW EA 011-5310-01-A7469, REV IR, AND EO MD11-531070137-A. MINOR.SDR FDEA201809142540Web · crackedFLIGHT COMPARTMENT RT OBSERVER SEAT BASE CUTOUT WEB FOUND CRACK, AT STA 360, X=- 8. CRACKED WEB REPAIRED AS PER SRM 53-10-51-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142538Seat Track · corrodedMAIN DECK AFT LT CURVE SEAT TRACK AT STA 1940 TO STA 2007, X= 107 FOUND CORROSION. SEAT TRACK CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED LT CURVED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA SDR FDEA201809142535Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X= 56 FOUND CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142534Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X=-56 FOUND CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142533Floor Support · crackedMAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X=-25 FOUND CRACKED. MAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X=-25 CRACKED FLANGE LOBE REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142531Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION AT LT WING LEADING EDGE SKIN ADJACENT TO CUTOUTS AND ACCESS DOORS, FOUND 1EA CRACK INDICATION AT CORNER NR 13, APPROXIMATE 0.2" IN LENGTH. REPAIR CARRIED OUT AT LT WING FIXED LEADING EDGE AT CORNER NR 13, AT STA XOS 65SDR FDEA201809142530Doubler · crackedLT WING LEADING EDGE CAVITY AT STA XOS 744 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE CAVITY AT STA XOS 744 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142529Doubler · crackedRT WING LEADING EDGE CAVITY AT STA XOS 587 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY AT STA XOS 587 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809142528Splice · not reportedRT WING, DURING ACCOMPLISHMENT OF EA 1-5710-T0329981 PART 2 FOUND UNABLE TO COMPLY WITH STEP 3 WORK INSTRUCTIONS AS P/N ARB3143-2 NOT AVAILABLE FOR REPLACEMENT EXISTING SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ARB3143 REVISIOSDR FDEA201809142527Splice · not reportedLT WING, DURING ACCOMPLISHMENT OF EA 1-5710-T0329978 PART 2 FOUND UNABLE TO COMPLY WITH STEP 3 WORK INSTRUCTIONS AS P/N ARB3143-1 NOT AVAILABLE FOR REPLACEMENT EXISTING SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ARB3143 REVISIOSDR IPXA2018100124508Longeron · corrodedLONGERON 51L HAD CORROSION AT BS 1857. REPAIRED THE LONGERON BETWEEN BS 1862.47 TO 1887.0 IAW SRM 53-00-05, REPAIR 1, FIG 201, & 202. MAJOR.SDR IPXA2018100134604Skin · crackedNR 1 ENGINE, RT CORE COWL WAS CRACKED AND HAS A DOUBLER REPAIR AT THE AFT LATCH. REPAIRED IAW EA 011-5430-01-A7482, REV I/R, AND EO MD11-7110-70101-A. MINOR.SDR IPXA2018100134603Filler · damagedTAILCONE HAD CHAFE DAMAGE ON THE RT INTERNAL FILLERS AND LONGERONS BETWEEN BS 2163.685 AND 2165.061, Z=45 & Z=60.1. REPAIRED THE DAMAGED TAILCONE IAW EA 011-5350-01-A7464, REV I/R, AND EO MD11-5350-62358-B. MINOR.SDR IPXA2018092834501Spoiler · corrodedRT WING UPPER SURFACE SPOILER SILL WAS CORRODED BETWEEN XOSP 530 TO 564. REPAIRED THE SPOILER IAW SRM 57-50-05, REPAIR 10, FIG 201, AND 51-38-01, 6D. MAJOR.SDR IPXA2018092634437Stiffener · crackedNR 2 ENGINE RT THRUST REVERSER STIFFENER, FWD OF THE CASCADE VANE AT 2:30 POSITION WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-42. MINOR.SDR FDEA201809142546Fitting · corrodedRT O/B FLAP VANE HORN FITTING "F" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STEP 1B. REPAIR CSDR FDEA201809142545Fitting · corrodedRT O/B FLAP VANE HORN FITTING "E" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'E' HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STSDR FDEA201809142544Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09, REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER SDR FDEA201809142543Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE BORE CORROSION. HINGE LOWER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T034SDR FDEA201809142532Skin · chafedRT WING DROOP LEADING EDGE FOUND CHAFED, STA XDLE 309. REPAIR CARRIED OUT AT RT WING DROOP ASSEMBLY LEADING EDGE AT INBOARD STA XDLE 309 AS PER SRM 57-40--01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018092434321Rib · chafedLEFT WING INBD FLAP, INBD TRACK FAIRING RIB WAS CHAFED. REMOVED AND REPLACED THE RIB IAW SRM 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018092104202Tee Fitting · crackedLEFT WING, OTBD FLAP, INBD FWD HINGE FAIRING, OTBD FWD LOWER PANEL SUPPORT TEE FITTING WAS CRACKED. REMOVED AND REPLACED THE TEE IAW SRM 51-33-01. MINOR.SDR IPXA2018091753998Power Supply · dischargedDURING AN EMERGENCY LIGHT TEST, LEVEL 1, EMERGENCY LIGHT BATTERY 1 LOW. TROUBLESHOT IAW FIM 33-51-00-101. REMOVE AND REPLACED THE EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS CHECKED GOOD.SDR IPXA2018100864735Longeron · corrodedCENTER CARGO COMPARTMENT LONGERON 48L HAD EXFOLIATION CORROSION AT STATION 5-63. REMOVED AND REPLACED THE LONGERON IAW SRM 51-21-01, 51-31-01, 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018100534698Support Beam · corrodedAFT CARGO SUPPORT BEAM WAS CORODED AT BS 1841 AND BETWEEN LBL 13 TO 23. REPAIRED THE SUPPORT BEAM IAW EA 011-5320-01-A7463, REV I/R, AND EO MD11-5320-70153-A. MAJOR.SDR FDEA2018091432518Former · crackedRIGHT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT RIGHT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PSDR FDEA2018091432517Frame · damagedMAIN DECK RT FRAME AT STA 535 LONGERON 19R FOUND DAMAGED. MAIN DECK DAMAGED RT FRAME AT STA 535 LONGERON 19R REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432516Frame · damagedMAIN DECK RT FRAME AT STA 535 LONGERON 24R FOUND DAMAGED. MAIN DECK DAMAGED RT FRAME AT STA 535 LONGERON 24R REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432515Angle · damagedMAIN DECK LT FRAME AT STA 535 LONGERON 24L FOUND EXISTING REPAIR ANGLE DAMAGED. REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432514Angle · damagedMAIN DECK LT FRAME AT STA 535 LONGERON 19L EXISTING REPAIR ANGLE DAMAGED MAIN DECK. REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091432513Stiffener · crackedLEFT HAND WING LEADING EDGE FORMER/STIFFENER AT STA XOS 549 FOUND CRACKED. CRACKED FORMER(STIFFENER) REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2918 REVISION G. INSTALLED NEW FORMER (STIFFENER) AT LEFT HAND WING LEADING EDGE AT STASDR FDEA2018091432512Former · crackedLEFT HAND WING LEADING EDGE FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT LEFT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PER SRM 51SDR IPXA2018092834506Longeron Splice · corrodedLONGERON 51L SPLICE FITTING WAS CRACKED AT BS 1857. REMOVED, FABRICATED, AND REPLACED THE LONGERON SPLICE IAW DWG 7414, AND SRM 51-33-01. MINOR.SDR IPXA2018092874484Stiffener · crackedNR 2 ENGINE, RT THRUST REVERSER BACK-UP FITTING, STIFFENER WAS CRACKED AT THE 5:00 O`CLOCK POSITION. REMOVED AND REPLACED STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018092874466Stiffener · crackedNR 2 ENGINE LT THRUST REVERSER BACK-UP FITTING STIFFENER WAS CRACKED AT THE 9:00 O`CLOCK POSITION. REMOVED AND REPLACED STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018092654385Bracket · crackedLEFT WING BRACKET AT THE FWD, INBD CORNER OF PANEL 541CB CUTOUT WAS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-31-01, & 51-33-01. MINOR.SDR FDEA2018091432519Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 1229, X=-75.25 FOUND CORROSION MAIN DECK FLOOR. SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1169SDR FDEA2018091432510Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER BARREL NUT HOLE BORE CORROSION. HINGE UPPER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T034SDR FDEA2018091432509Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432508Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432507Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432506Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS P
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