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 FDEA201308021745Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE FOUND DENTED AT XIFH 250 AND ONE INCH FROM T/E. REPAIRED IAW SRM 57-50-01, REPAIR 1, FIGURE 201, REV 53 AND EA 1-5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR WRNA201308070011Oil System · overheatedON DEPARTURE, "OIL TEMP HIGH" ANNUNCIATION WITH OIL TEMP ON THE NR 1 ENGINE AT 166 DEGREE C. REDUCED POWER ON NR 1 IAW THE QRH. IDLE POWER WAS REQUIRED TO KEEP THE TEMPERATURE FROM EXCEEDING LIMIT. MAXIMUM OIL TEMPERATURE ACHIEVED 168 DEGREE C. WITH IDLE PSDR IPXA2013082100886Doubler · crackedINSPECTION TYPE:1C, LT WING L/E INNER SKIN BEADED DOUBLER REPAIR STA XOS 75 9-763, REQUIRES REPAIR. PREVIOUS REPAIR INSTALLED IAW EO MD11-5730-47 906-A. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW EA 011-5730-01-A48-39, REV I/R AND EO MD11-5730-47906-CSDR IPXA2013082100885Doubler · crackedINSPECTION TYPE:1C, LT WING L/E INNER SKIN DOUBLER STA 584-589 REQUIRES REP AIR. PREVIOUS REPAIR INSTALLED IAW EO MD11-5730-47904-A. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED DOUBLER IAW EA 011-5730-01-A4840, REV I/R AND EO MD11-5730-47904-C.SDR IPXA2013082100878Doubler · crackedINSPECTION TYPE:1C, REF D-484950, LT WING L/E INNER SHIM BEADED DOUBLER REQUIRES REPAIR STA XOS 625-629. PREVIOUS REPAIR INSTALLED IAW EO MD11-5730-47903-A. REMOVED, FABRICATED AND REPLACED BEADED DOUBLER AND FILLER IAW EA 01 1-5730-01-A4846, REV I/R AND EO MSDR IPXA13M79804Intercostal · crackedINSPECTION TYPE:2C, APPROX 1 INCH LONG CRACK, ALONG AFT EDGE OF INTERCOSTAL, AT VERTICAL STAB REAR SPAR RELIEF CUTOUT, AS SHOWN IN SRM 55-30-02, REPAIR 7, FIG 203. INSTALLED REPAIR AT VERTICAL STAB REAR SPAR INTERCOSTAL AFT EDGE AT RELIEF CUTOUT IAW SRM 55-3SDR IPXA3M79712Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 667. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 661-667 IAW SRM 57-40-02, REPAIR 15, FIG 206. (MAJOR)SDR FDEA201308011741Light · inoperativeR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST, HAS NO INDICATION.SDR FDEA201308011738Wheel · failedLEVEL 2 TIRE FAIL ON LANDING ROLL, R & R NR 10 MAIN WHEEL ASSY IAW 32-41-01-4 UP TO STEP 5F(6).SDR FDEA201308011734Button · inoperativeR1 ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST, NO INDICATION. R & R AND OPS CHECKED OK IAW MM 25-61-04-4.SDR WRLA20130731598Skin · corrodedCORROSION WAS FOUND ON SKIN AJC7060, FROM STA Y:2140 TO 2163, L-33R TO L-35R. REPAIR CORROSION AREA IAW EI W2013A53B-1996, REV 1. COND CHECKED NORMAL.SDR FDEA201307311706Door Frame · crackedBS 1305.25 - 1315.42, R3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201 REPAIR 3 REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201307311705Door Frame · crackedBS 1250.75 - 1256.75, R3 DOOR FWD FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53 -40-15, FIG 201, REPAIR 3, REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307311704Door Frame · crackedBS 1305.25 - 1315.42 L3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100, REV 116.SDR FDEA201307311703Door Frame · crackedBS 1250.75 - 1256.75 L/E DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM
6 -2-100, REV 116.SDR FDEA201307311739Battery Pack · failedPRE-DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS BATTERY LOW DURING TEST. R & R EMERGENCY EXIT LIGHTS POWER SUPPLY BATTERY. OPS CHECKED OK IAW AMM 33-51-01-4 & AMM 33-51-01-5.SDR WRLA201310020597Frame · corrodedCORROSION WAS FOUND ON FUSELAGE FRAME, AT STA Y 410, BETWEEN X 15 AND X -10. REPLACE DAMAGE FRAME WITH NEW FRAME IAW SRM 51-35-01 AND 51-33-01, REV 53 AND EI NR W2013A53B-2032, REV 1.SDR IPXA13M79780Stringer · crackedINSPECTION TYPE:1C, RT WING STRINGER 15 CRACKED NEAR XORS 433. REPAIRED RT WING STRINGER 15 AT XORS433 IAW STASA EA 011-5710-01- A4828 REV IR AND IPXA EO MD11-5710-51790-A FAA 8100-9.SDR IPXA3M79776Stringer · crackedINSPECTION TYPE:1C, STRINGER 11 CRACKED AT FUEL ACCESS 536AB INBD OF NR 1 TANK LT WING. REPAIRED LT WING UPPER STRINGER S-11 FROM XORS 683 TO 713 IAW EA 011-5710-01-A4822 REV I/R, EO MD11-5710-51785-A.SDR IPXA3M79765Stringer · crackedINSPECTION TYPE:1C, STRINGER 15 CRACKED IN LT WING NEAR PANEL 534AT XORS433 -435. REPAIRED STRINGER IAW EA 011- 5700-01-A4825, REV IR AND EO MD11-5710-51771-A.SDR IPXA3M79764Stringer · crackedINSPECTION TYPE: 1C, RT WING STRINGER 11 CRACKED NEAR ACCESS PANEL 636AB BETWEEN XOS 683 -713. REPAIRED RT WING STRINGER 11 BETWEEN XOS 683 - 713 IAW STASA EA 011- 5700-01-A4826 REV IR AND EO MD11-5710-51644-A.SDR FDEA201307301698Skin · damagedNOSE SKIN DAMAGED AT JACK POINT BS 595-625 LONGERON 36 - 48R. REPAIRED IAW SRM 53-20-01. REPAIR 2, REV 53.SDR FDEA201307301697Rib · crackedAFTER REMOVAL OF EXISTING REPAIR, FOUND L/E RIB DAMAGED AT ZFS =596.972. DAMAGED RIB REMOVED IAW SRM 51-35-01, REV 53. NEW RIB FABRICATED IAW DWG AMC7130, REV E. RIB INSTALLED IAW SRM 51-35-01, REV 53. REPAIR CLASSIFIED MAJOR GMM 6-2-100, REV 116.SDR FDEA201307301696Rib · damagedAFTER REMOVAL OF EXISTING REPAIR, FOUND L/E RIB DAMAGED AT ZFS =603.132. CRACKED RIB REMOVED IAW SRM 51-35-01, REV 53. NEW RIB FABRICATED IAW DWG AMC7130, REV E. RIB INSTALLED IAW SRM 51-35-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307301695Rib · damagedAFTER REMOVAL OF EXISTING REPAIR, FOUND L/E RIB DAMAGED AT ZFS =596.972. CRACKED RIB REMOVED IAW SRM 51-35-01, REV 53. NEW RIB FABRICATED IAW DWG AMC7130, REV E. RIB INSTALLED IAW SRM 51-35-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR IPXA3M79566Light · inoperativeEMERGENCY LIGHTS ARE INOPERATIVE IN THE ARM AND ON MODE. EMERGENCY LIGHT TEST SHOWS LIGHT TEST PASSED. R & R L1 DOOR AFT EMERGENCY LIGHT ASS IAW MM 33-52-01. OPS CHECKED GOOD.SDR IPXA13M79679Support Bracket · crackedINSPECTION TYPE: 1C, LT WING FIXED L/E SUPPORT BRACKET CRACKED AT AFT END JUST OTBD OF NR 7 SLAT TRACK XOS 559. REMOVED FABRICATED AND INSTALLED REPLACEMENT SUPPORT BRACKET IAW DWG ARB1162, SRM 51-31-01 AND 51-33-01. (MINOR)SDR FDEA201307291688Seat Track · corrodedFORWARD CABIN BS 610, X=-47.5 SEAT TRACK FOUND WITH SURFACE CORROSION. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM STATION 605 TO STATION 645 X = -47.5 IAW SRM 53-00-52, FIG 201. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM BS 605 - 645 IAW SRM 53-0SDR IPXA13M79789Skin · chafedINSPECTION TYPE:1C, RT WING FIXED L/E SKIN REPAIR DOUBLER FOUND CHAFED FROM XOS 839 TO XOS 867. REPAIRED RT WING FIXED L/E CHAFED REPAIR DOUBLER WITH REPLACEMENT REPAIR FROM XOS 839 TO XOS 867 REF STASA EA 011-5730-01-A4830 REV I/R, EO MD11-5730-51806-A AND 8SDR FDEA201307291690Skin · crackedDURING SPOILER UPPER SURFACE INSPECTION, RT WING L/E DROOP UPPER SURFACE FOUND CRACKED ABOUT 2 INCHES LONG AT XDLE 324. REPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201, REVISION 53. REPAIR DOUBLER INSTALLED IAW SRM 57-40-01, REPAIR 5, FIGURE 201, REV 53. SDR IPXA3M79769Fitting · damagedINSPECTION TYPE: 1C, WHILE REPAIRING CRACKED NLG LT TRUNION FITTING FOUND BUSHING IN LT SIDE LOAD FITTING FASTENER HOLE COMMON TO LT TRUNION FITTING. REPAIRED BUSHED FASTENER HOLE IAW STASA EA 011-5310-01-A4818, REV IR AND EO MD11-5310-51773-A.SDR IPXA3M79768Trunnion · crackedINSPECTION TYPE:1C, NLG LEFT TRUNION FITTING CRACKED. REPAIRED NLG LT TRUNION FITTING IAW STASA EA 011-5310-01-A4818, REV IR AND EO MD11-5310-51773-A.SDR FDEA201307291689Spar Cap · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON NR 4 BANJO FITTING OF VERTICAL STABILIZER STA 2164, A CRACK FOUND ON RADIUS OF THE RT SIDE OF REAR SPAR CAP FWD FLANGE LOCATED AT THE UPPER SECTION APPROX. 0.75" LENGTH. REPAIRED IAW EA 1-5530-T0301678, PART 1.SDR FDEA201307291687Floor Support · crackedFORWARD CABIN FLOOR SUPPORT AT BS 400-430, LBL 32 FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291686Door Frame · crackedLOWER FUSELAGE RT A/C PACK NR 3 DOOR FRAME AFT UPPER CORNER AREA FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 53-20-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291691Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, FOUND ONE CRACK INDICATION ON NR 7 MAIN DECK CARGO DOOR LOWER FRAME FITTING AT HOLE "A". SUPPORT FITTING R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291685Doubler · crackedRT WING FIXED L/E COMPARTMENT AT XOS 794 BEADED DOUBLER FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 57-40-02, FIG 203, REPAIR 15, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291684Longeron Splice · crackedMAIN DECK LONGERON 11R SPLICE AT BS 1651 FOUND CRACKED. R & R SRM 51-31-01, REV 53. SPLICE FABRICATED IAW DWG AFA7181, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291683Longeron Splice · crackedMAIN DECK LONGERON 12L SPLICE AT BS 1631 FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. FABRICATED IAW DWG AFA7181 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291682Stop Fitting · crackedMAIN DECK L3 PLUG DOOR, ONE DOOR STOP FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291681Skin · crackedLEFT HAND WING FIXED L/E XOS 715, SLAT TRACK 11 CUTOUT CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291680Skin · crackedLEFT WING FIXED L/E XOS 660, SLAT TRACK NR 10 CUTOUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307291679Trunnion · crackedNOSE LANDING GEAR WHEEL WELL RT TRUNNION FITTING LOWER AREA FOUND CRACKED. AREA TRIMMED OUT AND REPAIRED IAW SRM 53-10-14, FIG 202. REPAIR 2, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. INITIAL INSP AT 1500 CYCLES AND REPETITIVE INSP REQUIRSDR FDEA201307291678Trunnion · crackedNOSE LANDING GEAR WHEEL WELL LEFT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED IAW EA 1-5340-T0301502A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR IPXA13M79692Web · crackedINSPECTION TYPE:1C, COCKPIT FLOOR WEB CRACKED AT OBSERVERS SEAT POSITION. REPAIRED IAW SRM 53-10-51, REPAIR 1, FIG 202. (MAJOR)SDR IPXA13M79688Stringer · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT PANEL 626FB STRINGER LANDING AND PREVIOUS REPAIR FILLER CRACKED AT XOS 906.5807. REPAIRED IAW SRM 57-40-03, REPAIR. 1, FIG 201. (MAJOR REPAIR)SDR IPXA13M79687Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS 880.7835. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203. MAJOR REPAIR.SDR IPXA13M79686Doubler · crackedINSPECTION TYPE: 1C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 711.7851. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA13M79685Doubler · crackedINSPECTION TYPE: 1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS 653.7174. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA13M79644Doubler · crackedINSPECTION TYPE: 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 554. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 551-555 IAW SRM 57-40-02 REPAIR 15, FIG 206. (MAJOR)
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