Boeing MD-11F
Service difficulty reports · 31,316
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 FDEA202605050557Fastener · looseENG PYLON HAS SEVERAL LOOSE FASTENERS ON OUTSIDE NEAR AFT MOUNTSDR FDEA202605050556Skin · pulledNR 1 ENG PYLON HAS 3 PULLED FASTENERS ON SKIN O/B SIDE ABOVE AFT ENG MOUNT POINT.SDR FDEA202605050555Fastener · looseSEVERAL LOOSE FASTENERS ON O/B SIDE OF # 1ENG PYLON JUST BELOW THE FWD PYLON ATTACH FITTING.SDR FDEA202605050554Pylon · not reportedWS-C 00091685 MOD TYPE T MOD NO. 1-5450-T0386257 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386257 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386257 REV NO: PS P4 EA: 1-5SDR FDEA202605050553Pylon · not reportedWS-C 00091685 MOD TYPE T MOD NO. 1-5450-T0386257 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386257 REV NO. POS. P2. COMPLY WITH E..A. 1-5450-T0386257 REV NO: PS P2 SRM: 5SDR FDEA202605050552Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P2. EA: 1-5450-T0386268 P2 COMPLIED WITH REV NO. PS PT.2 E.A SDR FDEA202605050551Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386268 REV NO: PS P1 EA: 1-5SDR FDEA202605050550Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NR POS. P2 PLND. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P2 SDR FDEA202605050549Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P1 EA: E.ASDR FDEA202605050548Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386263 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386263 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386263 REV NO: PS P4 EA: 1-5SDR FDEA202605050547Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386263 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386263 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386263 REV NO: PS P4 EA: 1-5SDR FDEA202605050545Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386807 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386807 REV NO. POS. P2. COMPLY WITH E..A. 1-5450-T0386807 REV NO: PS P2 EA: 1-5SDR FDEA202605050544Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386807 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAGE COMPLY WITH E..A. 1-5450-T0386807 REV NO. POS. P1 COMPLY WITH E..A. 1-5450-T0386807 REV NO: PS P1 EA: 1-54SDR IPXA2025121765208Slide · no discrepancyR1 SLIDE LOCK PIN INSTALLED INSTALLED LOCK PIN INTO REGULATOR/VALVE ASSY @ R1 SLIDE IRW MD11 AMM 25-61-15-000-801 STEP C (1) FOM SLIDE DEACTIVATION REF SUBTASK 10-10-07-550-008.SDR IPXA2025121600179Slide · no discrepancyL1 SLIDE LOCK PIN INSTALLED INSTALLED LOCK PIN INTO REGULATOR/VALVE ASSY @ L1 SLIDE IRW MD11 AMM 25-61-15-000-801 STEP C (1) FOM SLIDE DEACTIVATION REF SUBTASK 10-10-07-550-008. (T3F18E007XVZA STEP 10)SDR FDEA202511102154Skin · crackedTAIL ENGINE INTAKE DUCT LEADING EDGE FOUND MULTIPLE CRACKS. #2 ENGINE NOSE COWL REMOVED AND REPLACED AS PER AMM 54-22-01-04, CARRIED OUT NOSE COWL ANTI-ICE SYSTEM FUNCTIONAL TEST AS PER AMM 30-22-00-700-804, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR ASDR IPXA2025110768137Pulley · damagedLEFT ENTRY DOOR MAKES GRINDING NOISE WHILE OPENING REMOVED BOTH FWD DRIVE CABLES FROM CABLE DRUM. REMOVED AND REPLACED DAMAGED FWD LWR DRIVE CABLE PER AMM 52-11-03. REMOVED AND REPLACED DAMAGED PULLEYS IN REFERENCE TO AMM 52-11-03. REINSTALLED UPPER FWD DRIVSDR FDEA202511072141Brake · damagedBRAKE OVERHEAT AFTER LANDING AT 466K LANDING WEIGHT. OVERHEATS ON #4, #7, AND #8 WITH MAX TEMP 596 DEGREES. REMOVED AND REPLACED BRAKE ASSY LEAK AND OPS CHECKED GOOD ACFT OK TO CONTINUESDR FDEA202511062135Stiffener · corrodedVERTICAL STABILIZER CENTER SPAR UPON TRIM OUT OF STIFFENER FOUND CORROSION AT STATION 2122 X= -18.65 5 O'CLOCK AREA (REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00474). CORROSION ON STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT BS 2122 SDR FDEA202511052124Frame · crackedVERTICAL STABILIZER REAR CENTER SPAR STIFFENER CRACKED AT STATION 2122 5 O' CLOCK AREA. CRACKED STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT STATION 2122 5 O' CLOCK AREA REPAIRED AS PER EA# 1-5530-T0385238 P1 TITLE: STABILIZERS - VERTICALSDR IPXA2025110279653Battery · inoperativeDURING PREFLIGHT EMERGENCY 1 LT BAT LOW ALERT APPEARED DURING THE EMERGENCY LIGHT TEST. RAN QRH. REMOVED AND REPLACED EMERGENCY POWER BATTERY PER AMM 33-51-01. OPS CHECK GOOD AT THIS TIME. MEL CLEARED, PLACARD REMOVED.SDR IPXA2025110464431Battery · faultedEMERGENCY LIGHTING SYSTEM LIGHTS ILLUMINATED WITH EMERGENCY LIGHT IN ARM POSITION. CYCLED EMERGENCY LIGHT SWITCH OFF AND EMERGENCY LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01. OPS CHECK GOOD.SDR IPXA2025110364431Battery Pack · inoperativeEMERGENCY LIGHTING SYSTEM LIGHTS ILLUMINATED W/EMER LT IN ARM POSITION. CYCLED EMER LT SWITCH OFF AND EMERGENCY LIGHTS REMAINED ILLUMINATED. REMOVE AND REPLACE EMERGENCY POWER SUPPLY BATTERY<BR>REF MD11 AMM 33-51-01. OPS CHECK GOOD AT THIS TIME.SDR FDEA202510312117Skin · corrodedRIGHT INBD AILERON UPPER SURFACE OUTBOARD SIDE TRAILING EDGE AREA FOUND CORRODED. RIGHT HAND INBOARD AILERON ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-10-20-4. NEUTRAL POSITION ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-10-00-5. RSDR FDEA202510302115Indicator · failedENTRY DOOR 1R CIRCUIT CONTINUITY LIGHT INOP. RELEASED FOR SERVICE PER MEL 25-61-02 CATEGORY : C R1 DOOR EVAC SLIDE REMOTE PRESS INDICATOR INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. MEL: 25-6SDR FDEA202510292102Floor Panel · damagedFLOOR PANEL #231HF AT LEFT BS 595 TO 675 SURFACE FOUND DAMAGED. DAMAGED FLOOR PANEL #231HF AT CABIN LEFT HAND STATION 595 TO STATION 675 REMOVED AND REPLACED IAW AMM 53-25-04-4. FLOOR PANEL #231HF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. REPAIR CLASDR FDEA202510282101Controller · failedCAC MANF DECAY CK AT FL380. FOLLOWING THE CHECK, LEVEL 1 AVNCS FAN OVRD, AIR SYS 3 OFF, AND AIR SYS 2 OFF. REMOVED AND REPLACED ENVIRONMENTAL SYSTEM CONTROLLER, ADJUSTMENT/TEST PASSED PER ABOVE REFERENCES. REMOVED AND REPLACED ENVIRONMENTAL SYSTEM CONTROLSDR FDEA202510272095Beam · crackedCABIN L2 DOOR NR 6 BEAM FORWARD STOP FOUND CRACKED AT BS 794 CRACK LENGTH 1.0". AT L2 DOOR CRACKED NR 6 STOP BEAM. R & R IAW SRM 51-31-01-0G & DRAWING ADA3462, REVISION AC. L2 DOOR NR 6 STOP BEAM FABRICATED BY MACHINING IAW EA 1-5210-T0385415 PART 1. REPASDR FDEA202510272094Beam · crackedUPON REMOVAL OF R3 DOOR UPPER FORWARD DOOR BEAM FOUND WITH CRACK APPROXIMATELY 1.0". AT R3 DOOR, CRACKED UPPER FORWARD DOOR BEAM REMOVED AND REPLACED AS PER MD-11 SRM 51-35-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA202510272092Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRY OUT ON THE FUSELAGE SKIN EDGE AT THE SECOND COAX PENETRATION HOLES OF INMARSAT SATCOM, BETWEEN STATION 939 AND STATION 959, FOUND CRACK INDICATION ON THE EDGE OF THE SKIN. CRACK ON THE FUSELAGE SKIN EDGE SDR IPXA2025103135405Slide · misinstalledAPG FOUND L-1 DOOR EVACUATION SLIDE CONTAINER NOT INSTALLED PROPERLY ATA 25-61. REMOVED L1 DOOR UPPER DOOR LINER, REMOVED THE L-1 DOOR EVACUATION SLIDE/RAFT AND CONTAINER, REPOSITIONED SLIDE/RAFT AND CONTAINER IN REF TO MD11 AMM 25-23-06-000-802, AMM 25-61-01SDR IPXA2025102735405Container · misinstalledAPG FOUND L-1 DOOR EVACUATION SLIDE CONTAINER NOT INSTALLED PROPPERLY ATA 25-61. OPENSDR FDEA202510242087Hinge Bracket · corrodedRIGHT WING :(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORRROSION AT RIGHR HAND WING: (FLAP SIDE) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PERSDR FDEA202510242086Hinge Bracket · corrodedRIGHT WING :(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING : ( FLAP SIDE ) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PESDR FDEA202510242085Hinge Bracket · corrodedLEFT WING :(FLAP SIDE) LEFT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING : ( FLAP SIDE ) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MSDR FDEA202510242084Hinge Bracket · corrodedLEFT WING:(FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING ( FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER SDR FDEA202510242083Hinge Bracket · corrodedRIGHT WING: WING SIDE RIGHT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING : WING SIDE RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44SDR FDEA202510242082Hinge Bracket · corrodedLEFT WING: (ON WING SIDE), LEFT INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOTFACE AREA FOUND CORRODED. CORRODED AT LEFT HAND WING : (ON WING SIDE) , LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOT FACE AREA REWORKED AND FOUND EXCEED LSDR FDEA202510242081Hinge Bracket · corrodedLEFT WING: WING SIDE LEFT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORRODED. ORROSION AT LEFT HAND WING : WING SIDE LEFT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. RSDR FDEA202510222069Doubler · crackedFUSELAGE: #1 AIRCONDITION RAM AIR EXHAUST ASSY CUT OUT PRODUCTION DOUBLER SUSPECT CRACKED. CRACKED DOUBLER AT FUSELAGE #1 AIRCONDITION RAM AIR EXHAUST ASSEMBLY AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51- SDR FDEA202510222068Doubler · crackedFUSELAGE: #1 AIRCONDITION RAM AIR EXHAUST ASSY CUT OUT PRODUCTION DOUBLER SUSPECT CRACKED. CRACKED DOUBLER AT FUSELAGE #1 AIRCONDITION RAM AIR EXHAUST ASSEMBLY AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51- SDR FDEA202510222063Beam · crackedLOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM FOUND CRACKED AT BS 1746.925. LOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM CRACKED AT STATION 1746.925 REPAIRED AS PER MD-11 SRM 53-50-15-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR FDEA202510212062Proximity Sensor · faultedRIGHT MLG UNSAFE BOTH PRI & SEC WITH GEAR HANDLE UP. COMPLIED WITH QRH. LOWERED LG. SAFE INDICATIONS ALL FOUR. RAISED GEAR HNDLE PER QRH. UNSAFE RMLG & NLG. UPON ARRIVAL, SLOWED FROM 250 TO 230. NLG AUDIBLE CHANGE AND INDICATED SAFE UP. SUBSEQUENT LOWERINGSDR IPXA2025111846321Support Beam · corrodedLEFT WING OTBD FLAP INBD HINGE STRUCTURE FAIRING 535 DL AREA UPPER SUPPORT BEAM HAS EVIDENCE OF CORROSION, INSTALLED FAIRING SUPPORT BEAM AND 3EA ANGLES IN LH WING OUTBOARD FLAP I/B HINGE REF EA# 011-5700-01-B0623 REV P1 STEP 9, MD-11 SRM 51-33-01-0G-0 AND SSDR IPXA2025111246321Support Beam · inoperativeLEFT WING OTBD FLAP INBD HINGE STRUCTURE FAIRING 535 DL AREA UPPER SUPPORT BEAM HAS EVIDENCE OF CORROSION, ACCOMPLISHED REPAIR IAW VT-SAA EA 011-5700-01-B0623, REV IR.SDR IPXA2025110748720Spar Cap · corrodedRIGHT WING T/E UPPER FLANGE LOCATED AT STA XORS 484 HAS CORROSION. ACCOMPLISHED IN ACCORDANCE WITH EO-95601-REQ1 AND VT-SAA EA 011-5710-01-B0604 REV IR. EO 95601 ACCOMPLISHED ON T3F18E007R61J.SDR IPXA2025110726508Longeron · corrodedMAJOR REPAIR, CENTER CARGO COMPART. LONGERON SPLICE HAS EVIDENCE OF CORROSION APPROX BTW STA 1681 AND STA 1701, L51L AREA, ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95636-REQ1 AND VT-SAA EA 011-5310-01-B0598 REV IRSDR IPXA2025110724277Floorbeam · corrodedCTR CGO COMP FLOOR AREA STA 1841 FLOOR BEAM FLOOR PANEL SUPPORT CHANNEL TOP SURFACE HAS CORROSION FROM LBL 7 TO RBL 24.SDR IPXA2025111106150Cargo Track · crackedFWD CARGO COMPARTMENT. CEILING AREA, SEAT TRACK HAS CRACK LOCATED BETWEEN STA859 AND 879, RBL 75. INSTALLED SEAT TRACK SECTION AT MAIN CABIN BS 859 - 879 RBL 75 IAW SRM 53-00-52-2R-1. ACCOMPLISHED REPAIR IAW SRM 53-00-52-2R-1, REPAIR 1, REV 72.SDR IPXA2025110406631Support Bracket · brokenFWD CARGO COMPARTMENT CEILING STRUCTURE SUPPORT BRACKET BROKEN APPROX BTW STA 979 AND STA 999, X=-103, ID STICKER NUM. (085-067). CUT OUT DAMAGE AREA AT FWD CARGO COMPARTMENT CEILING STRUCTURE SUPPORT BRACKET APPROX BTW STA 979 AND STA 999, X=-103 IAW MD-11 SR
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