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 FDEA201405201083Skin · crackedWHILE ACCOMPLISHING FEA1-5710-F0308148 FOUND POSSIBLE CRACK ON NR 13 LT WING SLAT TRACK CUT OUT. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. THIS IS AT SLAT TRACK 14 CUT OUT NOT AT 13. NO CRACK AT SLAT TRACK 13 FOUND. REMOVED DAMAGSDR FDEA201405191070Longeron · crackedBS 1315, LONGERON 28R FOUND CRACKED. REMOVED AND REPLACED LONGERON IAW SRM 51-33-01 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405191082Skin · crackedRIGHT WING PRESSURE REFUEL PANEL 619CB CRACKED. FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. REPAIRED IAW EA 1-5730-T0308294.SDR FDEA201405191081Skin · crackedLT WING LE SKIN FWD OF OTBD SIDE OF SLAT DRIVE MECHANISM PANEL FOUND TO BE CRACKED. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F03081 48. CONFIRMED CRACK DURING HFEC INSPECTION IAW NDTSPM PT 6. CRACK EXTENDS FROM CORNER OF CUT OUT TO 1/4 INCH PAST FASTENER.SDR FDEA201405191072Skin · crackedFOUND POSSIBLE SMALL CRACK RT WING ROOT LE. COMPLIED WITH HFEC IAW SPM 06-10-01001. CRACK NOTED .750 INCH LONG. REMOVED CRACK AT OTBD CORNER OF FIRE BOTTLE ACCESS DOOR LOWER SKIN. MADE CUT OUT IAW SRM 57-10-00 FIG 68. PERFORMED HFEC INSPECTION IAW NTMSDR FDEA201405191080Skin · crackedFOUND CRACK ON INBD FWD CORNER OF SLAT DRIVE MECHANISM DOOR CUT OUT LT WING. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. PERFORMED HFEC INSPECTION IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. INSPECTED DAMAGE REMOVAL, NOT ACCEPTED. RADIUS ON DAMAGE SDR FDEA201405191079Skin · crackedCRACK IN LOWER LE PANEL ON LT WING JUST INBD OF OTBD SLAT MARKED. INSTALLED REPAIR ON ARB2933-13 IAW EA 1-5710-T0308224 P1. INSTALLED REPAIR ON LE SKIN IAW SRM 57-40-02 REPAIR 7 & EA 1-5710-T0308224 P 1. PAINTED REPAIR AREA IAW SRM 51-51-02.SDR FDEA201405191071Skin · crackedRIGHT WING NR 10 SLAT TRACK CUT OUT HAS POSSIBLE CRACK ON LE OF WING. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. VERIFIED CRACK, MARKED END OF CRACK. HFEC IAW NDTSPM PART 6,06-00-06. CUT OUT DAMAGED AREA IAW SRM 57-40-02 REPAIR 7. COMPLIED WITSDR IPXA2014061383287Tee Fitting · chafed4C INSPECTION, NR 2 ENGINE PYLON ACCESS PANEL 458AR AFT FAIRING TEE FITTING FOUND CHAFED. FABRICATED AND REPLACED TEE FITTING IAW EA 011-5450-01-A5397, REV I/R AND EO 5450-54528-A.SDR IPXA2014060983234Floor Panel · corroded4C INSPECTION, RIGID CARGO BARRIER FLOOR PANEL HAS CORROSION AT BS 475 X-47.50 REPAIRED FLOOR PANEL IAW EA 011-5310-01-A5383 AND EO 5310-54594-A.SDR FDEA201405171059Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 SDR FDEA201405171058Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 273HF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405171057Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 293DF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405171056Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 233DF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR IPXA2014060683230Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL AT STRINGER 15 HAS CORROSION STA 1225-1231, X=-75.25 TO X=-107.25. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN AT STRINGER 15 STA 1225-1231, X=-75.25 TO X=-107.25 IAW EA 011-5730-01-A5396 REV I/RSDR IPXA2014060683229Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION AT STRINGER 15 STA 1225-1231, X=-47.50 TO X=-75.25. ACCOMPLISHED REPAIR ON CENTER WING UPPER SKIN PANEL AT STRINGER 15 STA 1225-1231, X=-47.50 TO X=-75.25 IAW EA 011-5730-A5396, REV I/R AND 57SDR IPXA2014060683228Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER PANEL SKIN HAS CORROSION AT STRINGER 15 STA 1225-1231 X=-27.50 TO X=-47.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN AT STRINGE 15 STA 1225-1231 X=-27.50 TO X=-47.50 IAW EA 011-5730-01-A5396, REV I/R ANDSDR IPXA2014060683227Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION AT STRINGER 15 STA 1225-1231 X=-8.50 TO X=-27.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN PANEL AT STR 15 STA 1225-1231 X=-8.50 TO X=-27.50 IAW EA 01-5730-01-A5396, REV I/R EO 5SDR IPXA2014060683226Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION AT STRINGER 15, STA 1225-1231 X=8.50 TO X=-8.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN PANEL AT STR 15, STA 1225-1231 X=8.50 TO X=-8.50 IAW EA 011-5730-01-A5396 AND EO 5730-54SDR IPXA2014060683225Panel · corroded4C INSPECTION, CENTER WING AUX UPPER SKIN PANEL HAS CORROSION AT STRINGER 15 STA 1225-1231 X=27.50 TO X=8.50. ACCOMPLISHED REPAIR ON CENTER AUX UPPER SKIN PANEL AT STRINGER 15 STA 1225-1231, X=27.50 TO X=8.50 IAW EA 011-5730-01-A5396, REV I/R AND EO 5730-5456SDR IPXA2014060683224Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER SKIN PANEL HAS CORROSION ON STR 15 AT STA 1225-1231, X=27.50 TO X=47.50. ACCOMPLISHED REPAIR ON CENTER WING AUX TANK UPPER SKIN PANEL AT STR 15, STA 1225-1231 X=27.50 TO X=47.50 IAW EA 011-5730-01-A5396, REV I/R AND ESDR IPXA2014060683223Panel · corroded4C INSPECTION, CENTER WING AUX TANK UPPER PANEL HAS CORROSION AT STRINGER 15, STA 1225-1231, X=75.25 TO X=107.25. ACCOMPLISHED REPAIR TO CENTER AUX TANK UPPER SKIN PANEL AT STR 15, STA 1225-1231, X=75.25 TO X=107.25 IAW EA 011-5730-01-A5396 REV I/R AND EO 573SDR IPXA2014060683203Door Frame · cracked4C INSPECTION, L3 DOOR FRAME LOWER FWD LIGHTNING HOLE IS CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3.SDR IPXA2014060683201Door Frame · cracked4C INSPECTION, R3 DOOR FRAME LOWER FWD LIGHTNING HOLE IS CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201.SDR IPXA2014053083115Door Frame · cracked4C INSPECTION, R3 DOOR FRAME LOWER AFT LIGHTNING HOLE CRACKED. REPAIRED IAW SRM 53-40-15, REPAIR 3, REV 55.SDR IPXA2014060483163Vane · delaminated4C INSPECTION, RIGHT INBD FLAP VANE HAS DELAMINATION AT LWR SURFACE JUST OTBD OF CENTER TRACK. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201, REV 55.SDR IPXA2014060483162Vane · delaminated4C INSPECTION, RIGHT INBD FLAP VANE HAS DELAMINATION AT LOWER SURFACE JUST INBD OF CENTER TRACK. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201 REV 55.SDR IPXA2014060483161Vane · delaminated4C INSPECTION, LEFT INBD FLAP VANE LWR SURFACE HAS DELAMINATION BETWEEN CENTER AND OTBD TRACK. REPAIRED IAW SRM 57-50-80, REPAIR 2, FIG 201, REV 55.SDR FDEA201405151022Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 RSDR FDEA201405151021Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 SDR IPXA2014061183269Intercostal · cracked4C INSPECTION, CRACK FOUND ON NR 2 ENGINE UPPER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL Y 2164. ACCOMPLISHED DOUBLER REPAIR ON NR 2 ENG UPPER CENTER SPAR TO REAR SPAR INTERCOSTAL AFT EDGE AT STA Y 2164 IAW SRM 55-30-02, FIG 204, REPAIR 7.SDR IPXA2014060683231Stringer · cracked4C INSPECTION, RT WING UPPER STRINGER, NR 5 CRACKED BETWEEN STA XORS 1070 AND 1093. ACCOMPLISHED REPAIR ON RT WING UPPER STRINGER NR 5 BETWEEN STA XORS 1070 AND 1093 IAW EA 011-5710-01-A5381, REV I/R AND EO 5710-54584-A.SDR IPXA2014060683218Tripler · chafed4C INSPECTION, TRIPLER IS CHAFED ON RT LOWER FUSELAGE BS 1159, L44R. ACCOMPLISHED REPAIR TO TRIPLER IAW EA011-5330-01-A5403, REV I/R AND EO MD11-5330-54575-A.SDR FDEA201405141018Skin · delaminatedRIGHT OTBD FLAP INBD LOWER TE FOUND DELAMINATED. REPAIRED IAW SRM 57-50-80 PARA 4 1B REPAIR 1 REVISION 55 AND EA 1-5750-T0308362 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405141004Skin · crackedLEFT WING, SLAT TRACK NR 12 LOWER CUT OUT SKIN AT XOS 776 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR IPXA2014061683300Beam · cracked4C INSPECTION, LT WING T/E BEAM ASSY LOWER CAP CRACKED BETWEEN XW 332.76 AND XW 312. ACCOMPLISHED SPLICE REPAIR ON LT WING T/E BEAM ASSY LOWER CAP STA XW 332 TO XW 312 IAW EA 011-5720-01-A5361, REV I/R AND EO 5720-54420-A.SDR IPXA2014061183268Stringer · cracked4C INSPECTION, RT WING STRINGER 15 IS CRACKED AT STA XORS 433-455. REPAIRED STRINGER IAW EA 011-5710-01-A5382, REV I/R AND EO MD11-5710-54618-A.SDR IPXA2014053083118Stringer · cracked4C INSPECTION, LT WING UPPER STRINGER 9 HAS CRACK AT STA XORS 799.4 TO 826.5. REPAIRED IAW SRM 57-00-03 REPAIR 5, FIG 202.SDR FDEA201405131000Skin · crackedWRI 57-30/0648 UPPER SKIN ON LT INBD AFT FLAP HAS A 1.2 INCH CRACK. REPAIRED LT UPPER SKIN AFT FLAP DAMAGED AREA IAW SRM57-00-01 REPAIR 1, LEVEL 2 REPAIR CAT A & COMPLIED WITH EA1-5750-T0308108 PT 1 DTD 0513 & 14.SDR IPXA2014060683204Former · cracked4C INSPECTION, CRACKED FORMER IN RT WING FIXED L/E NEAR XORS 917. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB 2920, SRM 51-35-01, 51-31-01, 51-33-01.SDR IPXA2014060483167Duct · chafed4C INSPECTION, REPAIR DOUBLER IS CHAFED AND EDGE IS BENT AROUND LT TELESCOPIC DUCT CUTOUT. REPAIRED IAW SR M57-40-01 REPAIR 10, FIG 201, REV 55.SDR FDEA201405120985Engine · malfunctionedNR 3 ENG WOULD NOT ADVANCE TO MAX POWER, EPR OF 1.61, AUTO THROTTLES ADVANCED ENGINES 1 & 2 TO 1.61 EPR, NR 3 STOPPED AT 5% - 6% BELOW 1 & 2. THROTTLE NR 3 STOPPED 1/2 KNOB BEHIND NR 1 & 2. MANUALLY ADVANCED NR 3 THROTTLE UP, EPR & N1 SETTINGS WOULD NOT ADSDR IPXA2014061383277Skin · damaged4C INSPECTION, LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BS 1531, L49-50R FABRICATED AND INSTALLED REPAIR DOUBLER AT NOTED LOCATION IAW EA 011-5330-01-A5401, REV IR AND EO MD11-5330-54623-A.SDR IPXA2014060983238Skin · gouged4C INSPECTION, FIVE GOUGES ON FUSELAGE SKIN BETWEEN BS 655-675, STRINGER 32R REPAIRED IAW EA 011-5330-01-A5408 REV I/R AND 5330-54569-A.SDR FDEA201405110978Doubler · crackedLEFT WING FIXED LE BEADED DOUBLER AT XOS 664 FOUND CRACKED DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR IPXA2014051482954Switch · looseL1 EVAC SLIDE REMOTE PUSH TO TEST INDICATING SWITCH LOOSE. R & R L1 EVAC SLIDE IAW AMM 25-61-15-000-801 AND OPS CHECKED NORMAL.SDR WRNA20140513006Warning Message · illuminatedDURING CRUISE, AT APPROXIMATELY 100NM SOUTH OF AIRPORT, LEVEL 2, GEN 3 BUSS FAIL ALERTED. CREW FOLLOWED THE QRH PROCEDURES, DEPLOYED THE ADG. CONTINUED FLIGHT AS PLANNED AND LANDED AT FLIGHT DESTINATION WITHOUT ANY FURTHER INCIDENTS. PERFORMED ENGINE RUN. SDR FDEA201405110980Skin · crackedDURING WALK AROUND FOUND SUSPECTED CRACK IN RT WING AROUND SLAT DRIVE MECHANISM ACCESS DOOR. HFEC INSPECTED CRACK INDICATED IAW SOPM 20-30-00. REMOVED DAMAGE IAW SRM 57-40-02 REPAIR 7. PERFORMED HFEC OF CUT OUT AREA ON RT WING TO ENSURE CRACK REMOVAL IAW NTSDR FDEA201405090971Web · crackedCABIN MAIN DECK CARGO COMPARTMENT RT STATION 1256, LONGERON 26R FWD R3 DOOR LOWER JAMB, FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 55 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 121SDR IPXA2014060283131Bushing · worn1C INSPECTION, RT WING NR 4 SPOILER OTBD SUPPORT FITTING HAS WORN BUSHING. REPAIRED IAW EA 011-5755-01-A5378, REV I/R AND EO 5740- 54511-A.
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