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 WRLA20121210571Support · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON SUPPORT (P/N: AGA7183-3) OF CARGO COMPARTMENT FLOOR AT STA 1942, L-49R.SDR WRLA20121210570Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7125-3) BETWEEN L-49L AND L-49R, STATION 1841.SDR WRLA20121210569Web · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON WEB (P/N: AGA7184-3) OF CARGO COMPARTMENT FLOOR AT STA 1921, X=5.SDR WRLA20121210568Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7351-31) BETWEEN L-51L AND L-52, STATION 1871.SDR WRLA20121210567Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA0016-3) BETWEEN L-51R AND L-52, STATION 1853.SDR FDEA201212104275Block · looseMX REPORTED THERE IS A GAP BETWEEN THE LT AFT PILLOW BLOCK BOLT AND THE PILLOW BLOCK. MX TORQUED THE BOLT TO THE AMM SPECS. HOWEVER THE BOLT WILL NOT PULL UP TO THE PILLOW BLOCK. THIS CONDITION IS ACCEPTABLE PROVIDED THE CLG IS DEACTIVATED. REMOVED CTR GESDR FDEA201212094271Line · leakingHYDRAULIC LEAKING NR 6 BRAKE. R & R HYD BRAKE LINE AND COUPLING, OPS AND LEAK CHECKED GOOD. REF MM 32-43-21-4 AND SMP.SDR FDEA201212084268Skin · looseLEFT WING INBD FLAP UPPER SURFACE AT XIFH= 171 RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01 FIGURE 201 REPAIR 4 REVISION 51 AND EA 1-5750-163534 STEP 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074261Access Panel · crackedSEVEN FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 690 AND XORS= 700. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 51. REPAIR CLASSDR FDEA201212074260Access Panel · crackedTWELVE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 690 AND STA XORS= 700. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 51. REPAIRSDR FDEA201212074267Bulkhead · misrepairedNLG HORIZONTAL PRESSURE PANEL, LT SIDE, BS 495 TO 515, "X"=30 TO "X"=39 MISREPAIRED. REPAIRED IAW EA 1-5310-163550. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074266Bulkhead · misrepairedNLG HORIZONTAL PRESSURE PANEL, LT SIDE, AT BS 495 TO 515, "X"=42 TO "X"=47 MISREPAIRED. REPAIRED IAW EA 1-5310-163550. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074265Floorbeam · misrepairedFLOORBEAM LOWER FLANGE AT BS 5-53 MISREPAIRED. REPAIRED IAW EA 1-5310-163551. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074264Hinge Bracket · corrodedRT WING, OTBD FLAP, INBD FORWARD HINGE BRACKET, LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER: 0.705", FINAL HOLE DIAMETER: 0.709", MAXIMUM HOLE: 0.709". REPAIR BUSHING FABRSDR FDEA201212064251Beam · crackedUPON REMOVAL OF MAIN DECK R3 DOOR FOUND UPPER BEAM AFT END CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201212064253Skin · delaminatedRT WING, OTBD AILERON, INBD T/E SURFACE FOUND DELAMINATED. REPAIRED IAW SRM 57-60-80, REPAIR 1, REVISION 51 AND COMPLIED WITH EA 1-5750-165176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212064257Structure · damagedLEFT WINGLET DAMAGED & AFT LIGHT ASSY. WINGLET REPLACED & ACFT RETURNED TO SERVICE.SDR WRNA201200016Idg · faultyIN CRUISE, OUT OF ANC, LEVEL 2 'GEN BUS 3 ALERT'. DEPLOYED ADG AND RETURNED TO FIELD. MAINTENANCE PERFORMED TROUBLESHOOTING IAW FIM 24-20-17. AIRCRAFT RELEASE TO SERVICE ON MEL 24-21-1. MEL 24-21-1 CLEARED ON 12-09-12 WITH REPLACEMENT OF IDG.SDR IPXA2M76376Unknown · odorFUMES IN COCKPIT. BECAME IRRITATING TO CREW SO CREW WENT ON 02, RETURNED TO DEPARTURE. RAN ALL THREE PACKS TOGETHER AND INDIVIDUALLY FROM FOUR SEPARATE AIR SOURCES, APU AND ALL THREE ENGINES, NO FUMES OR ODORS NOTED. REF 21-53-00-840-801, 21-62-700-802 ANSDR FDEA201212044239Beam · crackedCENTER CARGO DOOR ROTARY ACTUATOR BEAM FOUND CRACKED. REPAIRED IAW E.A. 1-5310-165173. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201212044238Skin · crackedRT WING SLAT TRACK NR 12 LOWER OTBD CUT-OUT CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201212044237Seat Track · corrodedMAIN DECK COMPARTMENT -FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1390 TO 1530, RBL 75. CARRIED OUT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201212044236Seat Track · corrodedMAIN DECK COMPARTMENT- FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1250 TO 1390 X=-75. CARRIED OUT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201212044235Seat Track · corrodedMAIN DECK COMPARTMENT- FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1220 TO 1250 X= -75. CARRIED OUT SEAT TRACK SEGMENT REPLACEMENT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201212044234Slat Track · crackedLEFT WING NR 8 SLAT TRACK UPPER DOOR CUT-OUT CRACKED. REPAIRED AS PER E.A. 1-5730-163557. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR CLCA20121204121Mechanism · crackedDURING APPROACH (SKBO) PHASE, LEVEL 2 HYD 3 FAIL ALERT. LANDED WITHOUT INCIDENT. DURING INSPECTION FOR CORRECTION ACTION, INBOARD SLAT DRIVE MECHANISM WAS FOUND CRACKED. FURTHER INSPECTION AND REPAIRS TBD.SDR FDEA201212034228Skin · crackedLEFT AIR CON COMPARTMENT NR 2 DOOR EXTERIOR UPPER SKIN EDGE CRACKED. REPAIRED AS PER SRM 52-40-01 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.SDR IPXA2M76386Battery · inoperativeEMERGENCY LIGHTING BATTERY POWER SUPPLY MESSAGE LOW VOLTAGE. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-000-802 AND AMM 33-51-01-400-802.SDR IPXA2M76346Structure · damagedLEFT WING INBD FLAP DAMAGED. REPAIRED IAW EO MD11-5750-49242-A.SDR FDEA201211304219Skin · corrodedLT WING T/E PANEL 541JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211304218Skin · puncturedRIGHT WING NR 2 SLAT LOWER SURFACE SKIN PUNCTURED. REPAIRED IAW EA 1-5750- 163560. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211304217Skin · corrodedRT WING T/E PANEL 641JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211304209Duct · crackedLT WING TELESCOPIC DUCT UPPER DOOR CUT-OUT CRACKED. REPAIRED IAW SRM 57-40- 01 REPAIR 10 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211304215Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162SDR FDEA201211304216Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162399 PSDR IPXA2M76366Cover · out of positionL1 DOOR WILL NOT ARM. REPOSITIONED L1 DOOR COVER.SDR FDEA201211294208Warning Light · false activationFLAX PWR, GOT REV-PRESS FAULT(SUSPECT ENG 3).REJECTED T/O AND RETURNED TO LINE DUE FLAGGED I TEM. UNABLE TO DUPLICATE, ACCOMPLISHED HIGH POWER RUNS PERFORMED ENG RUN IAW JRH, NO REV FAULT MESSAGE FOUND, PERFORMED REVERSER FUNTION TEST IAW MM 78-30-00-5.SDR FDEA201211294198Skin · looseRIGHT WING INBD FLAP UPPER SURFACE RIVETS XIFH 261 FOUND LOOSE. REMOVED AND REPAIR ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211294201Stop Fitting · crackedON REMOVAL OF R1 MED DUST COVER NR 3 DOOR BEAM AFT STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51 AND EA 1-5210-163538. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211294200Stop Fitting · crackedON REMOVAL OF R1 MED DUST COVER NR 2 DOOR BEAM AFT STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51 AND EA 1-5210-163538. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211284191Spar · crackedEMPENNAGE, RT LOWER VERTICAL STABILIZER REAR SPAR FRAME APPROX STATION YTN= 121 ACCESS THRU PANEL NR 364RR FOUND WEB CRACKED. REPAIRED IAW SRM 55-30-02, REPAIR 2, REV 51.SDR FDEA201211284190Spar · crackedEMPENNAGE, LT LOWER VERTICAL STABILIZER REAR SPAR FRAME APPROX STATION YTN= 121 ACCESS THRU PANEL NR 363PL FOUND WEB CRACKED. REPAIRED IAW SRM 55-30-02, REPAIR 2, REV 51.SDR FDEA201211284192Frame · crackedNR 1 ENGINE THRUST REVERSER AFT CASCADE SUPPORT FRAME AT POSITION 6 FOUND CRACKED AT NUTPLATE AREA. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SUPPORT FRAME AS PER EA 1-7830-163531. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211284189Skin · looseRIGHT WING INBD FLAP UPPER SURFACE AT "XIFH" = 269 FOUND LOOSE RIVETS. REMOVED AND REPAIRED ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211274186Skin · crackedONE FASTENER HOLE FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. REPAIR CARRIED OUT IAW SRM 57-20-02, FIGURE 201, REPAIR 5, REVISIOSDR FDEA201211264183Floor Support · corrodedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL SUPPORT AT STATION 1887, "X"=-60, FORWARD FLANGE CORRODED. FLOOR SUPPORT REMOVED AND REPLACED AS PER AMM 20-50-02, REVISION 74.1. NEW FLOOR SUPPORT FABRICATED IAW DRAWING AGA7551, REVISION "G". CLASSIFIED AS MAJOR SDR FDEA201211264182Floor Panel · crackedMAIN DECK FLOOR SUPPORT AT BS 1887, "X"=0, FOUND CRACKED. R & R IAW MM 20-50-02, REV 74.1. FLOOR SUPPORT FABRICATED IAW DWG AGA7081, REVISION "M". REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211264156Seat Track · corrodedCENTER CARGO COMPARTMENT, ABOVE CEILING AREA, AT BS 1661, "X"= 75, SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPLACED FROM BS 1651 TO 1711, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR, IAW MM 6-2-100, REV 115.SDR FDEA201211264155Seat Track · corrodedCENTER CARGO COMPARTMENT, ABOVE CEILING AREA AT BS 1701, "X" = 75, SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPLACED FROM BS 1651 TO 1711, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211264180Skin · corrodedAFT ACCESSORY COMPARTMENT, FUSELAGE RT SIDE, SKIN AT STATION 2163 TO 2140, BETWEEN LONGERON 33 RIGHT AND 35 RIGHT, FOUND SURFACE CORROSION ON INTERIOR AREA COMMON TO EXISTING EXTERIOR REPAIR DOUBLER. REPAIRED IAW SRM 51-21-01 REVISION 51. FOUND EXCEEDED L
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