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 FDEA201611264250Doubler · crackedRIGHT WING FIXED L/E BEADED DOUBLER IS CRACKED AROUND FOUR FASTENERS BETWEEN XOS 62 5- 629. REPAIRED IAW SRM 57-40-02-2R, REP 15, FIG 203.SDR FDEA201611264249Doubler · crackedLEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED AT XOS 587. REPAIRED IAW SRM 57-40-02-2R, FIG 203.SDR FDEA201611264248Doubler · crackedLEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED AT XOS 544. REPAIRED IAW SRM 57-40-02-2R, FIG 203.SDR 9WGA2016112501Regulator Valve · inoperativeENGINE NR 2 FIRE WARNING LEVEL 3 ALERT CLIMBING THROUGH FL190. ENGINE SHUT DOWN. FIRE EXTINGUISHER DISCHARGED. FOUND PRESSURE REGULATOR VALVE (PRV) INOPERATIVE. REPLACED PRV.SDR FDEA201611234230Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE SURFACE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1.SDR FDEA201611234229Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.SDR FDEA201611234228Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.SDR FDEA201611234227Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1A.SDR FDEA201611234226Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1B.SDR FDEA201611234221Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.SDR FDEA201611234220Hinge Bracket · corrodedLEFT WING OTBD, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09, A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.SDR FDEA201611234219Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND DTEP 1.SDR FDEA201611234218Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND 1.SDR FDEA201611234217Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1B.SDR FDEA201611234225Hinge Bracket · corrodedRIGHT WING OUTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1A AND STEP 1.SDR FDEA201611234224Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-7-TO329708 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234223Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234222Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1B AND STEP 1.SDR FDEA201611234216Hinge Bracket · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1C.SDR FDEA201611234214Hinge Bracket · corrodedRIGHT WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-70329763 PART 1 STEP 1B.SDR FDEA201611234213Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) BARREL NUTS HOLE BORE CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1D.SDR FDEA201611234212Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763. PART 1 STEP 1B.SDR FDEA201611234211Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND WITH SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.SDR FDEA201611234210Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE CORROSION. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.SDR FDEA201611234209Hinge Bracket · corrodedRIGHT WING, OUTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234208Hinge Bracket · corrodedRIGHT HAND WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.SDR FDEA201611234233Web · crackedMAIN CARGO BAY L3 DOOR FRAME LOWER TORSION BOX HASA WEB CRACKED, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-40-15-2R, FIG 201.SDR FDEA201611224194Structure · corrodedFORWARD AVIONICS COMPARTMENT BILGE AREA BS 470 FOUND WITH CORRODED. REPAIRED IAW EA 1-5310-T0330006 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR 9WGA5432016112201Fire Warning · illuminatedON APPROACH, AT APPROXIMATELY 7,000 FT, AN INTERMITTENT INDICATION OF FIRE ON THE NR 2 ENGINE. AFTER A FEW SECONDS THE INDICATION CAME BACK AND REMAINED ON. SHUTDOWN ENGINE AND DISCHARGED ONE ENGINE FIRE EXTINGUISHER. UNEVENTFUL LANDING.SDR FDEA201611214144Skin · crackedDURING HFEC INSPECTION ON RT WING FIXED LEADING EDGE SLAT TRACK NR 10 CUTOUT, AFT INBD CORNER NR 13, FOUND ONE CRACK APPROXIMATELY 0.25IN LONG. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611204124Door · malfunctionedL1 DOOR WILL NOT CLOSE ELECTRICALLY FORM INSIDE. CLOSE SWITCH, WILL CLOSE FROM OUTSIDE SWITCH. DUPLICATED THE PROBLEM WHEN USE INTERIOR CONTROL SWITCH TO CLOSE THE DOOR , THE DOOR AUTOMATICALLY REVERSERS DIRECTION TO UP WHEN SWITCH RELEASED TO CENTER POSITIOSDR IPXA2016111910809Floor Panel · damagedSUPERNUMERARY FLOOR PANEL DAMAGED. FABRICATE A NEW FLOOR PANEL IAW EO MD11-5320-61010-ASDR FDEA201611184087Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201611184086Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR ISDR FDEA201611184085Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING, BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184084Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184083Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184082Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184099Frame · damagedMAIN DECK LEFT FRAME AT BS 1741 FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184098Frame · damagedMAIN DECK RIGHT FRAME AT BS 1661 FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184097Frame · damagedMAIN DECK LEFT FRAME AT BS 1621 FOUND DAMAGED. REPAIRED THE FRAME IAW SRM 53-00-07-2R FIG 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-00.SDR FDEA201611184096Seat Track · crackedMAIN DECK SEAT TRACK AT BS 635, RBL 8.5 FOUND CRACKED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184095Seat Track · crackedMAIN DECK SEAT TRACK AT BS 635, LBL 27.5 FOUND CRACKED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184094Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 635, RBL 27.5 FOUND CRACKED. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184093Seat Track · crackedMAIN DECK SEAT TRACK AT BS 755, LBL 47.5 FOUND CRACKED. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184092Seat Track · crackedMAIN DECK SEAT TRACK AT BS 635, LBL 47.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184091Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 664 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611184090Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 767 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611184089Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72646B PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR FDEA201611184088Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72646B PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM6-
Back to Boeing MD-11F