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 IPXA2016040701789Floor Panel · delaminatedINSPECTION TYPE:2C, MAIN DECK FLOOR PANEL WSP0825-19 DELAMINATED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND MD11-5320-27386-C.SDR IPXA2016040701788Floor Panel · delaminatedINSPECTION TYPE:2C, MAIN DECK FLOOR PANEL WSP 0825-41 DELAMINATED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND 5320-27386-C.SDR IPXA2016040701787Floor Panel · delaminatedINSPECTION TYPE:2C, MAIN DECK FLOOR PANEL, WSP 0825-50 DELAMINATED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW DWG WSP0825 AND MD11-5320-27386-C.SDR FDEA201603311124Stiffener · crackedAGEING ACFT, UPON REMOVAL OF STIFFENER AT LT WING LE STATION XOS 542, FOR ACCESS FOUND CRACKED. REFER SNRM N00744. R&R STIFFENER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2016041702220Floor Panel · corrodedINSPECTION TYPE:2C, RCB FLOOR PANEL WSP0785-502 CORRODED ON UPPER SURFACE BS 475-500, X=27 -36. REPAIRED NOTED FLOOR PANEL IAW EA 011-5320-01-A6206, REV IR AND EO MD11-5320-60498-A.SDR IPXA2016041702219Floor Panel · corrodedINSPECTION TYPE:2C, RCB FLOOR PANEL WSP 0785-501 CORRODED ON UPPER SURFACE BS 475-500 X=19 - 27. REPAIRED NOTED FLOOR PANEL IAW EA 011-5320-01-A6206, REV IR AND EO MD11-5320-60498-A.SDR IPXA2016033101455Line · leakingENGINE FAIL LIGHT ON T/O ROLL. REJECT ACCOMPLISHED DUE TO ENGINE MONITORING DATA SHOWING LOW PB PRESSURE NR 2 ENGINE, PERFORMED ENGINE CHECK 3, PB SENSE LINES. FOUND NR 2 ENGINE PB FLEX, PN 51U78 HAS SEVERE AIR LEAK. REPLACED LINE, PERFORMED ACCEL/DECEL TESTSDR IPXA2016033101436Indicator · inoperativeRIGHT SLIDE PRESSURE TO TEST LIGHT INOPERATIVE. R & R PRESSURE INDICATOR REMOTE KIT IAW AMM 25-61-04,SDR FDEA201603301119Power Supply · inoperativeEMERGENCY LIGHT BATTERY 1 LOW. R & R EMER EXIT LIGHTS POWER SUPPLY IAW 33-51-01-5. OPERATIONS CHECKED NORMAL AT THIS TIME. OK FOR SERVICE.SDR FDEA201603301118Skin · crackedONE EACH FASTENER HOLE NR 6 FOUND CRACK INDICATION, DURING OPEN HOLE HFEC INSPECTION, AT LT WING LOWERS SKIN ACCESS DOOR CUT OUT, BETWEEN STATION XORS 690 - XORS 700. REPAIRED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2,000SDR FDEA201603291095Skin · damagedAGEING ACFT, EXISTING REPAIR AT LT WING, INBD FLAP LOWER SEGMENT, UPPER SKIN STATION, XIFH 153.30 - XIFH 195.30. EXISTING REPAIR EVALUATED & FOUND REPAIR SKIN WITH NEW DAMAGE. REPAIR CARRIED OUT IAW SRM 57-00-01 REPAIR 2 FIG 201. REPAIR CLASSIFIED AS MAJOR SDR FDEA201603291115Girt Bar · obstructedL1 DOOR SHOWS OPEN ON STATUS PAGE WHEN CLOSED & SLIDE ARMED. CLEARED DEBRIS FROM GIRT BAR AREA. OPERATIONS CHECKED IAW MM 52-11-02-2. OK FOR SERVICE.SDR FDEA201603291113Skin · corrodedAFT ACCESSORY COMPARTMENT, RT SKIN WITH ANCHOR NUT ATTACH, FWD OF STATION 2164, FOUND CORROSION. SKIN REPAIRED PER SRM 53-70-01-2R FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201603291112Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED FOUND EXCEEDED LIMITS IAW CMM 57-52-04. EXISTING HOLE DIAMETER 1.193", FINAL HOLE DIAMETER 1.196, MAXIMUM ALLOWABLE HOLE DIAMETER 1.15". NEW REPAIR BUSHINGSDR FDEA201603291111Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.190", FINAL HOLE DIAMETER 1.225" & MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR SDR FDEA201603291110Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.215", FINAL HOLE DIAMETER 1.250", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRSDR FDEA201603291109Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.255", FINAL HOLE DIAMETER 1.285", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABSDR FDEA201603291108Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.257", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSHING FABRISDR FDEA201603291107Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE, FOUND CORRODED. CORROSION REWORKED & FOUND EXCEEDED LIMITS IAW CMM 57-52-03. EXISTING HOLE DIAMETER 1.248", FINAL HOLE DIAMETER 1.283", MAX ALLOWABLE DIAMETER 1.220". NEW REPAIR BUSDR FDEA201603291106Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.216", FINAL HOLE DIAMETER 1.226 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291104Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709".SDR FDEA201603291103Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, UPPER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.957", FINAL HOLE DIAMETER 0.961 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.944".SDR FDEA201603291102Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.228 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291101Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.284", FINAL HOLE DIAMETER 1.289 & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220SDR FDEA201603291097Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT, FRAME CHAFED AT RT STATION 535, LONGERON 24R. REPAIRED IAW SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603291096Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT, FRAME CHAFED AT RT STATION 535, LONGERON 19R. REPAIRED IAW SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2016042902738Seat Track · corrodedINSPECTION TYPE:2C, MAIN CABIN SEAT TRACK HAS CORROSION BS 495, RBL 36. R & R MAIN CABIN SEAT TRACK BS 439 TO BS 515 AT RBL 36 IAW DWG DAC WSP0826 AND SRM 51-31-01.SDR IPXA2016041702221Barrier · crackedINSPECTION TYPE:2C, RIGID CARGO BARRIER WALL HAS A CRACK AT NR 10 FITTING INNNER LOWER CLOSE OUT AREA BS 488 X=72.5 ACCOMPLISHED CRACK REPAIR ON RCB INNER LOWER CLOSEOUT AREA BS 488 X=-72.5 IAW EA 011-5310-01-A6188, REV I/R AND EO MD11-5310-60517-A.SDR IPXA2016041001908Structure · corrodedINSPECTION TYPE:2C, 2 AREAS OF CORROSION ON RCB FWD SKIN AND ALONG LOWER SURFACE AT X=79. REPAIRED NOTED CORROSION IAW EA 011-5310-01-A6189, REV IR AND EO MD11-5310-60402-A.SDR FDEA201603281090Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".SDR FDEA201603281089Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.588", FINAL HOLE DIAMETER 0.596 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584".SDR FDEA201603281088Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SURFACES, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.412", MATERIAL REMOVED 0.002" & MINIMUM ALLOWABLE THICKNESS 0.423". NESDR FDEA201603281087Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD. STUD ATTACH SURFACES FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.420", MATERIAL REMOVED: 0.010" & MINIMUM ALLOWABLE THICKNESS 0.423". NSDR FDEA201603281086Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44- 08. EXISTING HOLE DIAMETER 0.720", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.7SDR FDEA201603271084Skin · damagedAGEING ACFT, EXISTING REPAIR AT FWD CARGO, FUSELAGE DOOR CUT OUT, FWD JAMB SKIN STATION 895.7, LONGERON 40RT - 41RT. EXISTING REPAIR EVALUATED & FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 1-5330-T0324500A P 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFESDR IPXA2016041502159Doubler · corrodedINSPECTION TYPE:2C, INTERNAL DOUBLER CORRODED BEYOND ALLOWABLE LIMITS, BS 1159, L51 - L52L . REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG NAA6254, SRM 51-21-01, 51-35-01.SDR FDEA201603271081Doubler · crackedLEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271080Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 830, X=-8.5 FOUND CORROSION. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 785 - 907, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271079Doubler · crackedRIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 613. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271078Doubler · crackedLEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT XOS 543. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603271077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.220", FINAL HOLE DIAMETER 1.223 & MAX ALLOWABLE HOLE DIAMETER 1.220". NEW RSDR FDEA201603271075Slide Raft · defectiveREPEAT WRITE UP. R1 ESCAPE SLIDE BOTTLE PRESS LIGHT ILLUMINATED DURING CRUISE FLIGHT. FOUND INTERMITTENT CONTINUITY ON ELEC JACK COMING FROM SLIDE RAFT. R & R R1 DOOR SLIDE RAFT. BOTTLE PRESS PTT LIGHT OPERATIONS CHECKED NORMAL.SDR IPXA2016032801318Battery Pack · dischargedDURING COCKPIT PREFLIGHT TEST OF EMERGENCY LIGHT SYS, DISPLAYED "EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT. PERFORMD OPS CK OK IAW MM 33-51-01, P 501.SDR FDEA201603261076Control Panel · looseUNABLE TO CLOSE DOOR L1. ON ARRIVAL DOOR OPERATED NORMALLY. FOUND INTERIOR CONTROL PANEL LOOSE. OPENED CONTROL PANEL & INSPECTED. NO DEFECTS OR DAMAGE NOTED. SECURED PANEL & OPERATIONS CHECKED NORMAL.SDR IPXA2016041502162Skin · crackedINSPECTION TYPE:2C, RT FIXED L/E EXTERIOR SKIN PANEL 616ET CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW DWG ARB2386 AND SRM 51-31-01.SDR IPXA2016041802303Fitting · corrodedINSPECTION TYPE:2C, RCB FLOOR FITTING HAS CORROSION ALONG UPPER EDGES. ACCOMPLISHED BLEND REPAIR ON RCB FLOOR FITTING BS 488 X=8.5 IAW EA 011-5310-01-A6203, REV I/R AND EO MD11-5340-60492-A.SDR IPXA2016041802318Fitting · damagedINSPECTION TYPE:C2, RIGID CARGO BARRIER FLOOR FITTING NR 8 HAS AREAS OF EDGE DAMAGE. REPAIRED DAMAGED RCB FLOOR FITTING NR 8 IAW EA 011-5310-01-A6205, REV A AND EO MD11-5340-60491-A.SDR IPXA2016041802316Fitting · corrodedINSPECTION TYPE:2C, RCB FLOOR FITTING HAS CORROSION ALONG UPPER EDGES. ACCOMPLISHED BLEND REPAIR ON RCB FLOOR FITTING BS 488 X=27.5 IAW 011-5310-01-A6203, REV I/R AND EO MD11-5340-60492-A.SDR IPXA2016041802314Fitting · corrodedINSPECTION TYPE:C2, RIGID CARGO BARRIER FLOOR FITTING NR 7 HAS AREAS OF CORROSION ALONG UPPER EDGES. REPAIRED CORRODED RCB FLOOR FITTING NR 7 IAW EA 011-5310-01-A6205 REV A AND EO MD11-5340-60491-A.SDR IPXA2016041802304Fitting · corrodedINSPECTION TYPE:C2, RIGID CARGO BARRIER FLOOR FITTING NR 6 HAS AREAS OF CORROSION ON UPPER EDGES. REPAIRED CORRODED RCB FLOOR FITTING NR 6 IAW EA 011-5310-A6205, REV A AND EO 5340-60491-A.
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