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 FDEA201803140684Skin · crackedLEFT WING FIXED LEADING EDGE AT XOS 991.5 LEADING EDGE SKIN FOUND CRACKED ABOUT 8 INCHES. REPAIRED IAW SRM 57-40-01-2R, FIG 261, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140683Doubler · crackedLEFT WING FIXED LEADING EDGE AT XOS 991.5 LOWER SURFACE DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140680Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140679Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201803140678Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140681Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140682Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140677Door Frame · crackedMAIN DECK L3 DOOR FRAME LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26L TO 27L FOUND CRACKED. THE L3 DOOR FRAME LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803130667Seat Track · chafedRT EXISTING REPAIR AT MAIN DECK CARGO FLOOR SEAT TRACK STA.625 TO STA.645 X = -47.5 RT EVALUATED AND FOUND CHAFED DAMAGE AT SEAT TRACK CROWN. MAIN DECK CARGO FLOOR SEAT TRACK AT STA.625 TO STA.645 X = -47.5 RT CARRIED OUT REPAIR PER SRM 53-00-52-2R FIG 201 REPSDR IPXA2018031327394Cable · brokenWIRE CABLE FOR THE L1 DOOR FOUND BROKEN AND HANGING OUT OF CEILING. CABLE REMOVED. L1 DOOR UPPER DRIVE CABLE ASSY REPLACED IAW AMM 52-11-03, REV 90.05.SDR FDEA201803120700Elbow · crackedNOTICED EXCESSIVE FUEL BURN ON THREE CONSECUTIVE WAYPOINTS, SHORTLY THEREAFTER RECIEVED A LEVEL 2 FUEL QTY USED CHECK, POSSIBLE FUEL LEAK. RAN QRH PRCEDURE AND THE NR 2 TANK OR ENGINE ISOLATED AS SOURCE OF LEAK. FURTHER TROUBLESHOOTING DETERMINED IT WAS SDR IPXA2018040328154Vane · delaminatedINSPECTION TYPE: 2C, RT INBD FLAP VANE LOWER SURFACE HAS MULTIPLE AREAS OF DELAMINATION. REPAIRED THE FLAP VANE IAW EA 011-5753-01-A7178, REV IR AND EO MD11-5750-68016-A. MAJOR.SDR IPXA2018033128026Skin · crackedINSPECTION TYPE: 2C, RT WING LOWER SKIN HAS TWO CRACKS AROUND FUEL ACCESS PANEL LANDING BETWEEN XORS 683.4 - 713.6. REPAIRED THE SKIN IAW SRM 57-20-02, REPAIR 5, FIG 201.SDR IPXA2018033028006Skin · crackedINSPECTION TYPE: 2C, LEFT WING SKIN LOWER SURFACE HAS SIX CRACKS AROUND FUEL ACCESS PANEL LANDING BETWEEN XORS 683.4 AND 713.6. REPAIRED THE SKIN IAW SRM 57-20-02.SDR IPXA2018032727884Stringer · crackedINSPECTION TYPE: 2C, WHILE CLEANING UPPER AUX FUEL TANK FOR NDT INSPECTIONS FOUND STRINGER 47 CRACKED AT X46, X17, X-17 & X-46. REPAIRED THE STRINGER IAW SRM 57-10-03 REPAIR 1, FIGURE 201. MAJORSDR IPXA2018032827931Stringer · crackedINSPECTION TYPE: 2C, WHILE CLEANING UPPER AUX FUEL TANK FOR NDT INSPECTIONS FOUND STRINGER 51 CRACKED AT STA X46. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIGURE 201.SDR IPXA2018032827930Stringer · crackedINSPECTION TYPE: 2C, WHILE CLEANING UPPER AUX FUEL TANK FOR NDT INSPECTIONS FOUND STRINGER 50 CRACKED AT STA X46. REPAIRED THE STRINGER IAW SRM 57-10-03 REPAIR 1, FIGURE 201.SDR IPXA2018031827564Hinge Fitting · corrodedRIGHT OTBD FLAP OTBD HINGE FITTING HAS CORROSION. REPAIRED HINGE FITTING IAW CMM 57-44-08.SDR IPXA2018031827563Hinge Fitting · corrodedRIGHT OTBD FLAP INBD HINGE FITTING HAS CORROSION. REPAIRED HINGE FITTING IAW CMM 57-44-08.SDR IPXA2018031627511Support · corrodedINSPECTION TYPE:SVRMLG WING ATTACHMENT SUPPORT ASSEMBLY CORRODED IN LOWER AFT BOLT BORE FOR THE GEAR RETRACT CYLINDER SUPPORT BRACKET.REPAIRED WING ATTACHMENT SUPPORT ASSEMBLY PER MD11 SRM 57-20-14 REPAIR 1.SDR FDEA201803120672Elbow · crackedNOTICED EXCESSIVE FUEL BURN ON 3 CONSECUTIVE WAYPOINTS, SHORTLY AFTER, RECEIVED A LEVEL 2 FUEL QTY USED CHECK, POSSIBLE FUEL LEAK, RAN QRH PROCEDURE AND NR 2 TANK OR ENGINE ISOLATED AS SOURCE OF LEAK. FURTHER TROUBLESHOOTING DETERMINED IT WAS NR 2 ENG ASSDR IPXA2018040428165Floorbeam · corrodedINSPECTION TYPE: 2C, AFT CARGO BAY FLOORBEAM ANGLE CORRODED, BS 1841 BETWEEN BL 0 AND RBL 36. REPAIRED THE FLOORBEAM ANGLE IAW EA 011-5310-01-A7171, REV IR, AND EO MD11-5310-68023-A. MAJOR.SDR IPXA2018033128025Stiffener · crackedINSPECTION TYPE: 2C, LOWER FWD CARGO, BS 6-73 ABOVE LONGERON 43R HORIZONTAL STIFFNER CRACKED. REMOVED AND REPLACED THE STIFFENER IAW DWG ADA7667, SRM 51-31-01, 51-35-01, & 51-33-01.SDR IPXA2018032927947Longeron Splice · crackedINSPECTION TYPE: 2C, CENTER CARGO BAY LONGERON SPLICE 40L CRACKED AT BS 1537. REMOVED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7114, AND SRM 51-31-01 & 51-33-01.SDR IPXA2018032727905Longeron · corrodedINSPECTION TYPE: 2C, CENTER CARGO BAY LONGERON 37R HAS CORROSION AT THREE LOCATIONS BETWEEN BS 1561 TO 1601.REPAIRED THE LONGERON IAW EA 011-5310-01-A7175, REV IR, AND EO MD11-5310-67916-A.SDR IPXA2018032027666Door Frame · crackedINSPECTION TYPE: 2C, L3 DOOR FWD FRAME CRACKED. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIGURE 201. MAJOR.SDR IPXA2018032127696Door Frame · crackedINSPECTION TYPE: 2C, R3 DOOR FWD FRAME CRACKED AT LOWER WEB LIGHTENING HOLE. REPAIRED THE DOOR FRAME WEB BS 1254 IAW SRM 53-40-15, REPAIR 3, FIGURE 201. MAJOR.SDR IPXA2018031627530Door Frame · crackedINSPECTION TYPE: 2C, R3 DOOR FRAME AFT WEB CRACKED AT LOWER WEB LIGHTNING HOLE. REPAIRED THE DOOR FRAME WEB IAW SRM 53-40-15, REPAIR 3, FIGURE 201. MAJORSDR IPXA2018031627516Fitting · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING NR 1 IS CORRODED. REMOVED AND REPLACED THE FLOOR FITTING IAW EO MD11-2520-58701-D.SDR IPXA2018031627526Longeron · crackedINSPECTION TYPE: 2C, MAIN CABIN LONGERON 15R CRACKED AT BS 1341. REMOVED, FABRICATED AND INSTALLED A NEW LONGERON 15R IAW SRM 51-33-01, & 51-21-01, AND DWG AEA7568.SDR FDEA201803110648Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 1406, RBL 47.5. FOUND CROWN DAMAGED. GOUGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803110647Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 5-6 X= 27.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803110646Seat Track · damagedMAIN DECK SEAT TRACK AT BS 6-80, RBL 47.5 CROWN DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2018031127324Floor Panel · damagedMCD POS 2L FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO MD11-5320-27386-C.SDR IPXA2018031127323Floor Panel · damagedMCD POS 2L FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO MD11-5320-27386-C.SDR IPXA2018031127322Floor Panel · damagedMCD POS 2L FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO MD11-5320-27386-C.SDR IPXA2018031127321Floor Panel · damagedMCD POS 2L FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO MD11-5320-27386-C.SDR IPXA2018031127320Floor Panel · damagedMCD L2 FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO MD11-5320-27386-C.SDR IPXA2018032627827Skin · corrodedINSPECTION TYPE: 2C, LT WING UPPER SURFACE HAS CORROSION AROUND RIVET AFT OF NR 2 L/E SLAT. REPAIRED THE LT WING UPPER FWD SKIN AT XORS 151 AND STRINGER 19 IAW EA 011-5730-01-A7170, REV IR, AND EO MD11-5730-67882-A.SDR IPXA2018032127685Skin · corrodedINSPECTION TYPE: 2C, LT WING UPPER SKIN HAS CORROSION FWD OF THE NR 2 SPOILER XORS 538.49. REPAIRED THE SKIN IAW EA 011-5730-01-A7168, IR AND EO 5730-67845-A.SDR IPXA2018031027294Smoke Goggles · damagedRIGHT COURIER SEAT SMOKE GOGGLES ARE DAMAGED. R & R THE SMOKE GOGGLES IAW MM 35-13-00.SDR IPXA201804068206Bonding Strap · brokenINSPECTION TYPE: 2C, BONDING STRAP BROKEN INSIDE LT WING-TO-BODY FILLET FAIRING AREA AT PANEL 153AB. FABRICATED A STRAP IAW EA 011-5350-01-A7192, REV IR, AND EO MD11-5350-68017-A.SDR IPXA2018032927956Frame · corrodedINSPECTION TYPE :2C, FOUND THE RT MLG RETRACT CYLINDER A FRAME LOOSE. AFTER REMOVAL, FOUND THE A FRAME ATTACH HOLES CORRODED. REPLACED THE RT MLG RETRACT CYLINDER FRAME IAW CMM 57-11-01.SDR IPXA2018032827935Skin · chafedINSPECTION TYPE: 2C, EXTERIOR FUSELAGE SKIN CHAFED AT BS 1159, LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-01-A7167, REV IR, AND EO MD11-5330-67934-A. MAJOR.SDR IPXA2018032727883Skin · crackedINSPECTION TYPE: 2C, NR 1 ENGINE OTBD CORE COWL UPPER AFT SKIN IS CRACKED AT RIVET. REPAIRED THE NR 1 THRUST REVERSER AFT FIXED INNER BARREL UPPER SKIN IAW EA 011-7830-01-A7162, REV IR, AND EO MD11-7830-67733-A.SDR IPXA2018032727904Skin · crackedINSPECTION TYPE: 2C, NR 1 ENGINE INBD CORE COWL UPPER AFT SKIN CRACKED AT RIVET. REPAIRED THE 1 ENGINE INBD THRUST REVERSER AFT FIXED INNER BARREL UPPER SKIN IAW EA 011-7830-01-A7163, REV IR AND EO MD11-7830-67734-A. (MINOR)SDR IPXA2018032827914Doubler · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E SKIN SPLICE DOUBLER CRACKED AT XRS 903. REMOVED FABRICATED AND INSTALLED REPLACEMENT SPLICE DOUBLER IAW DWG ARB3954 AND SRM 51-33-01.SDR IPXA2018032027665Skin · chafedINSPECTION TYPE: 2C, FUSELAGE EXTERIOR SKIN CHAFED AT BS 1153, LONGERON 44L. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG. 201. MAJOR.SDR IPXA2018032127686Doubler · crackedINSPECTION TYPE: 2C, LEFT WING FIXED LE COMPARTMENT BEADED DOUBLER CRACKED XOS 634. REPAIRED THE DOUBLER BETWEEN XOS 633.4 & XOS 636.8 IAW EA 011-5730-01-A7169, REV IR, AND EO MD11-5730-67848-A. MAJOR.SDR IPXA2018031627517Landing · crackedINSPECTION TYPE: 2C, LT WING FIXED L/E COMP. FWD PANEL LANDING IS CRACKED AT XOS. 605. REMOVED, FABRICATED AND REPLACED THE PANEL LANDING IAW DWG ARB 2933, AND SRM 51-33-01.
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