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 IPXA2017091521752Torque Tube · scoredR1 DOOR FWD DRIVE TORQUE TUBE FOUND SCORED, CIRCUMFRENTIALLY NEAR SPLINED END. REMOVED AND REPLACED THE TORQUE TUBE.SDR IPXA2017091521751Cable · disconnectedR1 DOOR FOLLOW UP PANEL CABLE DISCONNECTED. CONNECTED THE CABLE AT CLEVIS.SDR IPXA2017091821850Control Unit · malfunctionedDURING CLIMBOUT, HAD A LEVEL 1 NR 2 ENG ANTI-ICE OFF ALERT. R & R THE ANTI ICE DUCT LEAK DETECTION CONTROL UNIT IAW AMM 30-22-10, AND THE ENGINE COWL ANTI-ICE MANIFOLD FAILURE SENSOR IAW AMM 30-42-11. SYSTEM CHECKED GOOD.SDR FDEA201709152569Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON THE RIGHT WING FUEL TANK LOWER ACCESS PANEL 636AB, FOUND THREE FASTENER HOLES 10, 28 AND 34 CRACKED. REPAIRED IAW SRM 57-20-02-2R, FIGURE 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709152568Rib · crackedLEFT WING NR 3 SLAT INNER RIB AT XOS 435.446 FOUND CRACKED. REPAIRED THE RIB IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 7, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709152567Skin · dentedLEFT WING NR 3 SLAT FOUND DENTED AT XOS 435.446. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 11, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709152566Roller · bindingDURING GEAR RETRACTION WE GOT A RIGHT MAIN UNSAFE GEAR UP INDICATION. RAN QRH PROCEDURE AND OBTAINED A GOOD GEAR UP INDICATION. DURING TROUBLESHOOTING FOUND RIGHT MAIN GEAR DOOR FELL OPEN WITH NO HYDRAULIC PRESSURE AND DOOR HANDLE IN THE UP POSITION. INSPECTSDR FDEA201709142556Doubler · crackedRIGHT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 546, FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201709142555Frame · chafedMAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 24L. THE REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G. A NEW REPAIR ANGLE WAS FABRICATED IAW SRM 53- 20-07-2R, FIGURE 201, REPAIR 1, AND INSTALLED IAW SRM 53-20-07-2R, FIGURE 2SDR FDEA201709142554Frame · chafedMAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 19L. REMOVED THE REPAIR IAW SRM 51-33-01-0G. A NEW OUTER REPAIR ANGLE, FABRICATED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE NEW REPAIR ANGLE WAS INSTALLED IAW SRM 53-20-07SDR FDEA201709142553Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 907 FOUND CRACKED. REPAIRED THE LEADING EDGE LOWER AREA IAW SRM 57-40-03-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709142552Fitting · crackedDURING HFEC INSPECTION AT RT FWD FLANGE LOCATED AT THE UPPER SECTION REAR SPAR CAP OF THE NR 4 BANJO FITTING OF THE VERTICAL STABILIZER, Y=2164 A CRACK WAS FOUND APPROXIMATELY 0.25 INCH LENGTH. REPAIRED IAW EA 1-5530-T0335558, PART 1. THE REPAIR WAS CLASSISDR IPXA2017091421712Relay · inoperativeR1 DOOR WILL NOT OPERATE. REPLACED THE R1 DOOR ACTUATOR CONTROL RELAY IAW FIM 52-11-03. TESTED GOOD.SDR FDEA201709132532Frame · dentedMAIN DECK CARGO FRAME DENTED AT BS 1721, LONGERON 12L. REPAIRED THE FRAME IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2.SDR FDEA201709132531Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 27.5. REPLACED THE SEAT TRACK FROM BS 625 TO 665, LBL 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132530Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 47. REPLACED THE SEAT TRACK FROM BS 625 TO 665 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132529Cargo Track · crackedMAIN DECK CARGO TRACK FOUND CRACKED AT BS 755, LBL 49. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132528Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM BS 665 TO 705 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132527Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 8.5. REPLACED THE SEAT TRACK FROM BS 625 TO 705, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132526Seat Track · crackedMAIN DECK CARGO FLOOR SEAT TRACK FOUND CRACKED AT STA 635 X= -8.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 705, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER SNRM N00528 FOR FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJORSDR FDEA2017091922504Hinge Bracket · corrodedTHE BORE WAS REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-08. EXISTING HOLE DIA: 0.873", FINAL HOLE DIA: 0.983", MAXIMUM ALLOWABLE HOLE DIA: 0.983". RIGHT WING OUTBD FLAP INBD FWD HINGE REMOVED AND REPLACED AS PER AMM 57-53-01-4. REPAIR CLASSIFIESDR IPXA2017091321679Roller · lack of lubeL1 DOOR DOES NOT OPERATE SMOOTHLY. OILED THE DOOR ROLLERS AND CHAINS. OPS CHECKED SMOOTH IAW AMM 12-25-05SDR FDEA201709122519Doubler · crackedLEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 616 FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 616 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709122518Doubler · crackedRIGHT HAND WING LEADING BEADED DOUBLER AT STA XOS 643 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 643 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201709122517Doubler · crackedRIGHT HAND WING LEADING BEADED DOUBLER AT STA XOS 543 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 543 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201709122516Doubler · crackedRIGHT HAND WING LEADING DOUBLER AT STA XOS 667 FOUND CRACKED. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED NEW DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE STA XOS 667 AS PER SRM 5SDR FDEA201709122515Doubler · crackedLEFT WING LEADING FORMER AT XOS 753 FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW FORMER IAW DRAWING ARB2923, REVISION D, AND INSTALLED IAW SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709122514Doubler · crackedLEFT HAND WING LEADING BEADED DOUBLER AT STA XOS 789 FOUND CRACKED. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED NEW DOUBLER AT LEFT HAND WING FIXED LEADING EDGE STA XOS 789 AS PER SDR FDEA201709122513Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION CARRIED OUT ON LEFT WING FIXED LEADING EDGE CUTOUTS AND ACCESS DOORS. FOUND ONE CRACK, TAI DUCT CUTOUT OTBD CORNER. 0.30 INCH IN LENGTH. REPARIED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJOSDR FDEA201709122512Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION CARRIED OUT ON LEFT WING FIXED LEADING EDGE CUTOUTS AND ACCESS DOORS. FOUND ONE CRACK TAI DUCT CUTOUT INBD CORNER, 0.30 INCH IN LENGTH. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJORSDR FDEA201709122511Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION CARRIED OUT ON RIGHT WING FIXED LEADING EDGE CUTOUTS AND ACCESS DOORS. FOUND ONE CRACK TAI DUCT CUTOUT OTBD CORNER (CORNER NR 2) APPROX 0.50 INCH IN LENGTH. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIRSDR FDEA201709122510Doubler · crackedLEFT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 653 XOS 657 FOUND CRACKED. REPAIR CARRIED OUT AT LH WING LEADING EDGE BEADED DOUBLER AT STA XOS 653 - XOS 657 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201709122509Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335333, PART 1, STEP 3A, AND 3C.SDR FDEA201709122508Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122507Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122506Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED, AND FOUND OUT OF LIMIT IAW CMM 57-44-08. THE OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122505Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122503Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE RIGHT WING OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122502Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.SDR FDEA201709122501Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.SDR FDEA201709122500Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C, AND STEP 1.SDR FDEA201709122499Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C AND STEP 1.SDR FDEA201709122498Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE SPOT SURFACE FOUND CORRODED. THE SPOT SURFACE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED THE AREA IAW EA 1-5750-T0335291A, PART 1, STEP 1.SDR FDEA201709122497Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED, AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1A.SDR FDEA201709122496Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1B.SDR FDEA201709122495Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.SDR FDEA201709122494Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.SDR FDEA201709122493Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.SDR FDEA201709122492Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.SDR FDEA201709122491Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.
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