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 IPXA2014061883334Doubler · cracked1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 702. REPAIRED LT WING DOUBLER BETWEEN XOS 698-705 IAW SRM 57-40-02, REPAIR 15, FIG 206.SDR IPXA2014061683315Doubler · cracked1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS640. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG.206.SDR FDEA201406051319Door Frame · crackedMAIN DECK CARGO BAY BS 1256, LONGERON 26 RT FWD R3 DOOR FRAME FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIGURE 201, REPAIR 3, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201406051309Skin · crackedLEFT WING SLAT TRACK NR 11 CUT OUT OTBD CORNER STATION XOS 720 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201406051318Skin · crackedCRACK ON RT WING LOWER SURFACE BETWEEN 6 & 7 SLATS. CONFIRMED END OF CRACK IAW NDTSPM PT 6. REMOVED CRACK IAW SRM 57-40-02 FIG 201. PERFORMED HFEC OF CUT OUT AREA. IAW NTSPM 06-10-01 010, NO DEFECTS NOTED. REPAIRED IAW SRM 57-40-02 REPAIR 7.SDR FDEA201406051314Skin · crackedPOSSIBLE CRACK FOUND ON LT WING LOWER SURFACE FOR SLAT TRACK CUT OUT BETWEEN 5 & 6 SLAT. NDT REQUESTED TO VERIFY CRACK. VERIFIED CRACK AT SLAT CUT OUT WITH HFEC IAW NDTSPM PT 6. CRACK APPROX 3/4 INCHES IN LENGTH. REMOVED LT WING LOWER LE PANEL 625DB FOR ACSDR FDEA201406041301Angle · crackedDURING INSPECTION, FOUND LEFT WING NR 2 SLAT OTBD INNER STRIP ANGLE FOUND CRACKED AT XDLE 328.106. REPAIRED IAW EA 1-5750-T0308746 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201406041300Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FITTING LOWER SECTION FOUND CRACKED. REPAIRED IAW SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201406041299Trunnion · crackedNOSE LANDING GEAR RT TRUNNION FITTING LOWER SECTION FOUND CRACKED. REPAIRED IAW SRM 53-10-14 FIGURE 202, REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201406041298Seat Track · corrodedCABIN MAIN DECK CARGO COMPARTMENT BS 1831, LBL 27.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201406041306Skin · damagedRT INBD FLAP DAMAGED. REPAIRED IAW EA 1-5750-T0308747 PART 1.SDR FDEA201406041304Seat Track · crackedRIGHT BS 1861 RBL 27.5 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201406031290Skin · crackedRIGHT WING DROOP LE UPPER SURFACE AT XDLE 325 FOUND CRACKED. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION 55 REPAIR. CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.SDR FDEA201406031289Skin · crackedRIGHT WING LOWER FIXED LE AT REFUELING PANEL CUT OUT INBD FWD CORNER AT XOS 643 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.SDR FDEA201406031288Skin · crackedLEFT WING LOWER FIXED LE AT NR 12 SLAT TRACK CUT OUT AT XOS 774 FOUND CRACKED. SKIN REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 121.SDR FDEA201406021260Vane · delaminatedRIGHT WING OTBD FLAP VANE UPPER SURFACE FOUND DELAMINATED FROM XOFH 558.820 - 586.820. RIGHT WING OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED IAW AMM 27-50-32- 4 REVISION 79. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-32-5 REVISION 79. FOUND SATISSDR FDEA201406021284Compensator · malfunctionedDURING CLIMB OUT, RECEIVED RUDDER STANDBY UPPER OFF, THREE TIMES. INTERROGATED, HSC UPPER RUDDER STANDBY POWER FAULT NOTED. R & R FWD COMPENSATOR LOW LEVEL SWITCH IAW AMM 27-26-31-4. R & R AFT LOW LEVEL COMPENSATOR SWITCH TO STEP 2 D CONNECTER WILL NOT LOCKSDR FDEA201406021275Receptacle · unsecureENTRY DOOR L1 DISARMED LIGHT HANGING LOOSE FROM RECEPTACLE. REPLACED L1 DOOR DISARM LIGHT RECEPTACLE IAW SWP & PERFORMED OPERATIONAL CHECK STEPS 1 & 2 IAW AMM 52-10-01-2. OPERATIONS CHECKED GOOD.SDR IPXA2014061883348Power Supply · no testEMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01.SDR FDEA201406011245Skin · crackedON PRE-FLIGHT INSP SUSPECT CRACK RT WING LE PANEL INBD RADIUS OF SLAT DRIVE MECHANISM DOOR CUT OUT. VERIFIED AREA TO BE CRACKED IAW NDT SPM PART 6. CRACK IS MARKED WITH PERMANENT MARKER. CUT OUT DAMAGE IAW SRM 57-40-02. NEED NDT TO INSPECT FOR DAMAGE REMSDR IPXA2014060283152Floor Panel · damagedCOCKPIT FLOOR PANEL SPONGY AND HAS TEMPORARY DOUBLER. FABRICATED NEW FLOOR PANEL IAW EO 5320-54353B.SDR FDEA201405301233Reservoir · lowDURING SERVICE CHECK FOUND R1 ESCAPE SLIDE PRESS IS LOW, REQUIRES SERVICING, FOUND TO BE WITHIN LIMITS. OBSERVED R1 DOOR PNEUMATIC STORAGE SYS TO BE IN NEED OF SERVICING. SERVICED DOOR.SDR IPXA2014060283142Cylinder · inoperativeAIR TURN BACK DUE TO LT MLG WOULD NOT RETRACT. R & R LT MLG RETRACT CYLINDER. LUBED LT MLG, JACKED ACFT AND CYCLED LANDING GEAR. OPS CHECKED GOOD.SDR FDEA201405291226Bolt · pulledDURING CONTROL CHECK, NO GREEN BOX ON RT AILERON. RETURNED TO GATE. FOUND RT INBD AILERON DROPPED WITH HYD POWER ON, FURTHER INSPECTION FOUND RT INBD ACTUATOR DETACHED FROM WING STRUCTURE, ALL FOUR BOLTS PULLED OUT FROM ACTUATOR. REMOVED AND REPLACED RT ISDR IPXA2014061183243Skin · cracked2C INSPECTION, FUSELAGE SKIN CRACKED AT UPPER AFT CORNER OF RT AIR CONDITIONING BAYDOOR CUTOUT BS 535 L31-33R. REPAIRED SKIN IAW SRM 53-20-15, REPAIR 3, FIG 201.SDR FDEA201405291224Skin · delaminatedRIGHT OTBD FLAP INBD TE UPPER SURFACE FOUND DELAMINATED AT XOFH 477.69 - 497. REPAIRED IAW SRM 57-50-80 PARAGRAPH 4A 1B. REPAIR 1 REVISION 55 & EA 1-5750-T0308362 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR IPXA2014053083121Slide · unwanted deployR1 DOOR SLIDE DEPLOYED. SLIDE REMOVED.SDR FDEA201405291228Handle · detachedL1 DOOR MANUAL LIFTING HANDLE IS DETACHED ON RT SIDE. REATTACHED L1 DOOR MANUAL LIFTING HANDLE IAW AMM 52-11-02-4. ACFT OK FOR SERVICE.SDR IPXA2014053083117Battery Pack · no testEMERGENCY LIGHT TEST FAILED. R & R POWER SUPPLY BATTERY, EMERGENCY LIGHT TEST PASSED IAW AMM 33-51-01/401, 501.SDR FDEA201405271203Skin · crackedFOUND CRACK ON RT WING AT OTBD SLAT TRACK CUT OUT FOR NR 6 SLAT. VERIFIED BY NDT. REMOVED LWR RT WING PANEL 626EB & PLACED IN COURIER COMPARTMENT. REMOVED DAMAGED SKIN IAW SRM 57-40-02 REPAIR 7 FIGURE 201. PERFORMED HFEC OF CUT OUT AREA IAW NTM PT 6. NO SDR FDEA201405271202Skin · crackedFOUND POSSIBLE CRACK ON LT WING AT INBD SIDE OF PRESS REFUEL DOOR, NDT NOTIFIED. LT WING LE LWR CRACK AREA, HFEC INSPECTION OF SUSPECT CRACK AREA, COMPLIED WITH & CONFIRMED CRACK IAW NTM 06-00-06. CUT OUT CRACK IAW 57-40-02. PERFORMED HFEC OF CUT OUT AREA IASDR CLCA20140526001Warning System · activatedDURING TAKEOFF LEVEL 1, REV 2 PRESS FAULT, DISPLAYED ON EAD. AFTER PARKING LEVEL 2, BRAKE OVERHEAT, NR 1 CAME ON.SDR FDEA201405261191Skin · crackedON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FUELING PANEL FWD INBD CORNER. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. TRIMED OUT CRACK AREA IAW SRM 57-40-02 REPAIR 7 FIG 202. PERFORMED HFEC OF DAMAGE CUT OUT IAW NTSPM 06-10-01.001. INSTALLEDSDR IPXA2014052783074B-Nut · looseAFTER LEVEL OFF RECEIVED A LEVEL 1 HYD 3 OFF, ACCOMPLISHED AOM PROCEDURE. HYD 3 BEGAN TO SLOWLY DECREASE FROM 11.4 TO 10.7 GALLONS. AIR TURN BACK ACCOMPLISHED. TROUBLESHOT IAW FIM 29-10-18, NO FAULT FOUND, NO EXTERNAL LEAK. R & R HSC IAW AMM 29-0 8-01 ANDSDR FDEA201405241153Engine · making metalWHILE LEVEL AT FL370, RECEIVE A LEVEL 2, NR 3 ENGINE OIL FILTER ALERT. COMPLIED WITH QRH DIRECTIVE & SHUTDOWN NR 3 ENGINE. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED MAIN CHIP DETECTOR & FOUND LARGE QTY OF LARGE METAL PARTICLES. REMOVED OIL FILTERSDR IPXA2014052783088Battery Pack · inoperativeEMERGENCY BATTERY 1 LOW MESSAGE DISPLAYED. R & R NR 1 BATTERY PACK IAW AMM 33-51-01-400-802. SYSTEM TESTED NORMAL IAW AMM 33-51-01-400-802. EFF IAW 33-51-01-5 ITEM NR 15.SDR FDEA201405231147Skin · crackedPOSSIBLE CRACK ON RT WING LOWER SLAT TRACK PANEL BETWEEN NR 5 & 6 SLAT, MARKED WITH TAPE. INSPECTION WILL VERIFY IF IT IS CRACKED. INSTALLED DOUBLER & FILLER IAW SRM 57-40-02.SDR FDEA201405231146Skin · crackedRIGHT WING, SKIN AT PRESS REFUEL DOOR, INNER FWD CORNER HAS SUSPECTED CRACK GOING FROM CORNER TO RIVET. INSTALLED REPAIR DOUBLER IAW SRM 57-40-02 REPAIR 7 FIGURE 202 & EA 1-5730-T0308359 PART 1.SDR WRNA201405230007Tire · failedDURING TAKEOFF ROLL, PRIOR TO V1, CREW REPORTED THEY FELT VIBRATION AND SIMULTANEOUSLY "LEVEL 2 ALERT" INDICATED "TIRE FAILURE," NR 1 TIRE FAIL DISPLAYED. THE CREW ABORTED TAKEOFF IAW PROCEDURE. ALSO, DUE TO THE HIGH-ENERGY STOP, THIS CAUSED AN OVER TEMP OF SDR FDEA201405221123Skin · crackedWHILE ACCOMPLISHING FEA 1-5710-F0308148 FOUND POSSIBLE CRACK ON CORNER OF LT WING REFUEL DOOR PNL 519CB. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. CUT OUT DAMAGE IAW SRM 57-40-02 REPAIR 7, FIG 202. PERFORMED HFEC INSPECTION IAW NSDR FDEA201405211113Indicator · inoperativeR1 DOOR SLIDE PRESSURE, PRESS TO TEST INDICATOR INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 25-61-04-4. OPS CHECKED GOOD IAW AMM 25-61-04-5. ACFT OK FOR SERVICE.SDR IPXA201409084202Structure · gougedINSPECTION 3C, GOUGES IN ATTACH BOLT HOLES IN LT UPPER WINGLET ATTACH BULKHEAD. REPAIRED LT UPPER WINGLET ATTACH BULKHEAD HOLES IAW EA 011-5710- 01-A5496, REV IR AND EO 5710-55420-A.SDR IPXA201409084201Structure · gougedINSPECTION 3C, GOUGES IN THE BORES OF ATTACH BOLT HOLES FOR LT WINGLET IN LWS 1093 BULKHEAD. REPAIRED LWS 1093, BULKHEAD IAW STASA EA 011-5710-01-A5495 REV IR AND EO 5710-55413-A.SDR FDEA201405201089Structure · wornMAIN DECK CARGO DOOR FOUR FWD HINGE PIN LOBE HOLES FOUND ELONGATED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 52-34-04 PARAGRAPH 2Y REVISION 78 AND EA1-5230-T0308187 PART1 STEP 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405201085Skin · crackedDURING PERFORMANCE OF FCD 1-5710-F0308148, FOUND LARGE CRACK AT RT WING NR 1 SLAT AT INBD SLAT TRACK CUT OUT. CUT OUT CRACK & REMOVED ALL DAMAGE IAW SRM 57-40-02. PERFORMED HFEC INSPECTION IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. PERFORMED RII INSPECTISDR FDEA201405201093Skin · crackedDURING COMPLIANCE OF FCD 1-5710-F0308148, FOUND SKIN CRACKED NEAR ZONE 519, LT WING INBD OF NR 1 ENGINE, JUST AFT OF INBD SLATS. PERFORMED HFEC OF THE SUSPECTED CRACK IN THE LT WING. CRACK APPROXIMATELY INCHES INCHES. INSTALLED FILLER AND DOUBLER IAW EA 1SDR FDEA201405201092Support Fitting · wornRIGHT WING INBD FLAP INBD SUPPORT STRUCTURE HAS SIX HOLE DIAMETERS FOUND TO EXCEED 0.2815 INCH. REPAIRED IAW EA1-5340-T0308227 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405201091Support Fitting · wornLEFT WING INBD FLAP INBD SUPPORT STRUCTURE SIX HOLE DIAMETERS FOUND EXCEEDING 0.2815 INCH. REPAIRED IAW EA1-5340-T0308226 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405201090Structure · corrodedCARGO BAY UNDER FLOOR AREA RT BS 229 FOUND CORRODED. REPAIRED AS PER EA 1-5750-T0308325 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405201084Skin · crackedRIGHT WING NR 16 SLAT TRACK CUT OUT HAS POSSIBLE CRACK ON LE SKIN. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. VERIFIED CRACK. CUT OUT DAMAGE IAW ERS 14-03138. PERFORMED HFEC INSPECTION OF DAMAGE REMOVAL IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED.
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