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 SRXR201809040038Stiffener · corrodedFWD AVIONICS COMPARTMENT AFT PRESSURE BULKHEAD SUPPORT STRUCTURE IS CORRODED AT STA 475 LBL17 TO RBL 29. REMOVED, FABRICATED AND INSTALLED FWD AVIONICS COMPARTMENT AFT PRESSURE BULKHEAD FRAME STIFFENER AT STA 475 LBL 10 TO RBL 10 PER SRM 51-31-01 PG 1 AND DWG SDR FDEA201809032339Control Unit · inoperative"ANTI-SKID FAIL" AFTER GEAR EXTENSION ON APPROACH. WENT AROUND COMPLIED WITH QRH. LANDED UNEVENTFUL AT PHX. MULTIPLE A/S CONTROL UNIT FAULTS LAST LEG. REMOVE AND REPLACED ANTISKID CONTROL UNIT AS PER MM 32-45-01-4, WILL REQUIRE OPERATIONAL TEST AS PER MM 32-4SDR FDEA2018090532340Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE ACCESS DOOR CUTOUT CORNERS, FOUND 01 EACH CRACK AT CORNER 11 APPROXIMATELY 0.3 INCH IN LENGTH. ACCESS DOOR CUTOUT STA XOS 610 CARRIED OUT REPAIR AS PER SRM 57-SDR FDEA2018090522350Skin · crackedFOUND DAMAGE ON LOWER PORTION OF L1 DOOR. 15 TO 20 INCH CREASE RUNNING FWD TO AFT. CREASE TRAVELS OVER A DOOR FRAME. DAMAGE IS OUT OF ALLOWABLE LIMITS. INSPECTED REWORKED AREA PER NDT SPM PT6 FOUND TWO CRACK INDICATIONS IN AREA. REMOVED AND REPLACED DAMAGED SDR FDEA2018090512335Floor Support · corrodedUPON REMOVAL OF FLOOR PANEL FOR ACCESS, SEAT TRACK REPAIR FOUND CORROSION ON FLOOR SUPPORT AT RT STA 1761, X=- 8.5 TO X=-27.5. FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 202. MATERIAL THK 0.70", SDR FDEA2018090512334Floor Support · corrodedUPON REMOVAL OF FLOOR PANEL FOR ACCESS OF SEAT TRACK REPAIR FOUND CORROSION ON FLOOR SUPPORT AT RT STA 1821, X=- 8.5 TO X=- 27.5. FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51- 21-01-0G AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 202. MATERIAL THK 0.0SDR FDEA2018090512333Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 5TH AND 6TH RIBS, XOS 696 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 696 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR SDR FDEA2018090512332Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT INBOARD OF ACCESS PANEL 626FB CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA2018090512331Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 4TH AND 5TH RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 687 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 687 TRIMMED AND REPAIR CARRIED OUT AS PER SSDR FDEA2018090512330Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 2ND AND 3RD RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 677 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02SDR FDEA2018090512329Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 AT XOS 665 CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK . CRACKED BEADED DOUBLER AT XOS 665 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PESDR FDEA2018090512328Seat Track · corrodedMDCC CORROSIONS ON SEAT TRACK FLANGE AT RT STA 1830, X=-107. SEAT TRACK CORROSION REMOVED 0.048" REMAIN 0.032", REMAIN 0.032", MATERIAL THK 0.080" AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK REPAIRED AS PERSDR FDEA2018090512327Floor Support · corrodedMAIN DECK CARGO AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STA 1887 - STA 2007 X=-25. FLOOR PANEL SUPPORT CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING TSDR FDEA2018090512326Floor Support · corrodedMDC AFT FLOOR SUPPORT ASSY FOUND WITH CORROSION AT STA 1887 TO STA 2007 X=0. FLOOR SUPPORT CORROSION REMOVED PER SRM 51- 21-01-0G ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020" AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. SUPPORT SDR FDEA2018090512323Seat Track · corrodedMAIN DECK CARGO COMPT CORROSION ON SEAT TRACK FLANGE AT RT STA 1037, X =-75.25. SEAT TRACK CORROSION REMOVED 0.046", REMAIN 0.025", MATERIAL THK 0.071" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT SEAT TRACK REPAIRSDR FDEA2018090512322Seat Track · corrodedMAIN DECK CARGO COMPT CORROSION ON SEAT TRACK FLANGE AT RT STA 975, X=-75.25. SEAT TRACK CORROSION REMOVED 0.056" REMAIN 0.015" MATERIAL THICKNESS 0.071" AND FOUND EXCEEDED LIMT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK ASDR FDEA2018090512325Longeron Splice · crackedCRACK LINE IMAGE FOUND ON X-RAY FILM AT FWD TRANSVERSE SKIN SPLICE ASSY AT STA 6-100, LT LONGERON 4, NR 5 HOLE TO NR 6 HOLE (FROM CENTER OF SPLICE ASSY) OF CENTER FASTENER ROW. CRACK LONGERON SPLICE AT STA 6-100, LT LONGERON 4 REMOVED AND REPLACED WITH NEW FABSDR FDEA2018090512324Seat Track · corrodedMAIN DECK CARGO COMPT SEAT TRACK CORROSIONS AT RT STA 485, X= - 27.5. CORROSION REMOVED 0.070", REMAINING THK: 0.020", ORIGINAL MATERIAL THK: 0.090" AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101 AND EXCEEDED LIMIT SEAT TRACK REPSDR FDEA2018090512321Seat Track · corrodedLOWER CTR CARGO COMPT CEILING FOUND CABIN FLOOR SEAT TRACK WITH CORROSION AT STA 5-73 TO 5-113 X =-75. CORROSION REMOVED 0.044", REMAINING THK 0.027", ORIGINAL THK 0.071" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMISDR FDEA2018090512320Hinge Bracket · corrodedRT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722" MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHINSDR FDEA2018090512319Hinge Bracket · corrodedRT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. HINGE UPPER MOUNT O/B BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.944", FINAL HOLE DIA 0.950" MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERSDR FDEA2018090512318Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE PIVOT BORE(NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 2.309", FINAL HOLE DIA: 2.315", MAXIMUM ALLOWABLE DIA: 2.3135. OVERSIZE BUSHING FABRICATED ANSDR FDEA2018090512316Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. HINGE UPPER MOUNT O/B BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.943", FINAL HOLE DIA: 0.9465", MAXIMUM ALLOWABLE DIA: 0.944. OVERSIZE SDR FDEA2018090512315Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE (WING SIDE) LOWER MOUNT O/B BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.712", MAXIMUM ALLOWABLE DIA: 0.709SDR FDEA2018090512314Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE ACTUATOR ATTACH I/B BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 1.2105", FINAL HOLE DIA: 1.222", MAXIMUM ALLOWABLE DIA: 1.220. OSDR FDEA2018090512312Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE ACTUATOR ATTACHED OUTBD BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.224" MAXIMUM ALLOWABLE HOLE DIA 1SDR FDEA2018090512311Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE ACTUATOR ATTACHED INBD BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 1.2205", FINAL HOLE DIA 1.224" MAXIMUM ALLOWABLE HOLE DIA 1SDR FDEA2018090512309Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.327", FINAL HOLE DIA 0.406" MAXIMUM ALLOWABLE HOLE DIA SDR FDEA2018090512308Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE SURFACE CORROSION. HINGE LOWER MOUNT OUTBD BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING THICKNESS 0.408", MATERIAL REMOVED FWD FACE 0.004", AFT FACE 0.011", REMSDR FDEA2018090512307Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE SURFACE CORROSION. HINGE LOWER MOUNT INBD BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING THICKNESS 0.408", MATERIAL REMOVED FWD FACE 0.004", AFT FACE 0.014", REMAISDR FDEA2018090512305Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT OUTBD BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.612" MAXIMUM ALLOWABLE HOLE DIA 0.584", SHSDR FDEA2018090502294Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 695 X =27.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT STA 685 TO STA 705 X=27.5 SEAT TRACK. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018090502295Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 755 X = 47.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR 1 AT CABIN STA 725 TO 765 X= 47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018090502293Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT INBD BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.599" MAXIMUM ALLOWABLE HOLE DIA 0.584", SHOULDER BUSHISDR FDEA2018090502292Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 1.231", FINAL HOLE DIA: 1.252", MAXIMUM ALLOWABLE DISDR FDEA2018090502291Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. HINGE BARREL NUT HOLE (NR 10 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.678", FINAL HOLE DIA: 0.707", MAXIMUM ALLOWABLE DIA: 0.667. OVERSIZE BUSHING FASDR FDEA2018083102290Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.408"; LOWER: 0.408", MATERIAL REMOVED: UPPER: 0.012"; LOWER: 0.012", REMAINING THICKNESSDR FDEA2018083102289Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. HINGE BARREL NUT LOWER BOLT (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.390", FINAL HOLE DIA 0.410" MAXIMUM ALLOWABLE HOLE DIA 0.39SDR FDEA2018083102288Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.390", FINAL HOLE DIA: 0.410", MAXIMUM ALLOWABLE DIA: 0.391SDR FDEA2018083102287Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.595", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BSDR FDEA2018083102286Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT I/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.587", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BSDR FDEA2018083102285Skin · corrodedRT WING OUTBD ISLAND AREA UPPER T/E SURFACE STA XORS 1070 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018083102284Skin · corrodedRT WING OUTBD AILERON AREA UPPER T/E SURFACE STA XORS 1040 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018083102282Skin · crackedLOWER VERTICAL STABILIZER LT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341902 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018083102281Skin · crackedLOWER VERTICAL STABILIZER RT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341903 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018083102280Hinge Bracket · corrodedLT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-07. EXISTING HOLE DIA: 1.064", FINAL HOLE DIA: 1.1065", MAXIMUM ALLOWABLE DIA: 1.0935SDR FDEA2018083102273Hinge Bracket · wornLT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING AT FWD HINGE (WING SIDE) PIVOT BORE, REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0332025 A PART 1 STEP 1F (1) AND STEP 1F (3). REPAIR CLASSIFIED AS MAJOR PER GSDR FDEA201808292239Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 635 X = 47.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 605 TO STA 655 X=47.5. SEAT TRACK REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201808292237Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 635 X= 8.5. CRACKED SEAT TRACKED REPAIRED PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 625 TO STA 705 X= 8.5. SEAT TRACK REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201808292236Seat Track · corrodedMDC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 1821, X=- 8.5. SEAT TRACK CORROSION MATERIAL REMOVED 0.055", MATERIAL REMAIN 0.016", MATERIAL THK 0.071" FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK REPAI
Back to Boeing MD-11F