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 FDEA201207302744Skin · misrepairedLEFT WING INBD FLAP UPPER SURFACE XIFH 216 - YIFH 70 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 57-00-01 REPAIR 1 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207302743Frame · misrepairedLEFT SIDEWALL FRAME BS 535, LONGERON 19 LT MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 53-20-07 REPAIR 1 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REVISION 115.SDR FDEA201207302758Frame · dentedFRAME, BS 1661, L11L FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207302757Frame · dentedFRAME, BS 1701 L11R FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00.07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207302756Frame · dentedFRAME BS 1661, L11R FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207302755Frame · dentedFRAME BS 1681, L11R, FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00.07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207302752Longeron · corrodedCENTER ACCESSORY COMPARTMENT BS 6-70 TO 6-80, LONGERON 49L FOUND CORRODED. CORROSION ON LONGERON REMOVED AS PER SRM 51-21-01 REVISION 50. AND FOUND OUT OF LIMITS AS PER SRM 53-00-00 FIGURE 205 REVISION 50. DAMAGED LONGERON REMOVED AND REPAIRED AS PER SRM SDR IPXA12M74767Door Frame · crackedINSPECTION TYPE:4C, R3 DOOR BS 1305 AFT JAMB LOWER LIGHTNING HOLE CRACKED IN CORNER. REPAIRED R-3 AFT DOOR JAMB LOWER LIGHTNING HOLE AT STA 1305 REF SRM 53-40-15, REPAIR 3, FIG 201.SDR IPXA2M74649Skin · damagedHOLE IN LT FUSELAGE BY APU INTAKE DUCT DUE TO APU FAILURE. REF EO MD11-5330-48041-A FOR REPAIR.SDR IPXA2M74647Bleed Valve · inoperativeWITH LEVEL II, AIR SYS 2 PRESSURE LOW ON DESCENT LEVEL II, AIR SYSTEM 1, PRESSURE LOW ILLUMINATED. EMERGENCY DECLARED. SHORTLY AFTER LEVEL II, AIR SYS 3, PRESSURE LOW (NO CABIN PRESSURE). ACCOMPLISHED EMERGENCY DESCENT. R & R APU LOAD BLEED VALVE IAW AMM 36-SDR IPXA12M74968Floor Panel · brokenINSPECTION TYPE: 4C, FLOOR PANEL 261FF HAS BROKEN INSERTS. FABRICATED FLOOR PANEL REF EO MD11-5320-27386-C, APPX A/B.SDR IPXA2M74890Stringer · crackedINSPECTION TYPE: 4C, LT WING STRINGER NR 9 CRACKED AT FUEL ACCES PANEL 538AB FWD SIDE. REPAIRED LT WING STRINGER NR 9 INSIDE FUEL ACCESS PANEL 538AB FWD SIDE REF SRM 57-00-03, FIG 202, REP, REV 49.SDR IPXA2M74889Stringer · crackedINSPECTION TYPE: 4C, LT WING UPPER STRINGER 11 AT XORS 683 CRACKED INSIDE FUEL TANK ACCESS 536AB. REPAIRED LT WING UPPER STRINGER NR 11 AT XORS 683 AT FUEL TANK ACCESS 536AB, REF SRM 57-00-03, REPAIR 5, FIG 202, REV 49.SDR IPXA2M74887Stringer · crackedINSPECTION TYPE:4C, RT WING UPPER STRINGER CRACKED INSIDE FUEL TANK ACCESS PANEL 636AB FWD SIDE AT XORS 683. REPAIRED RT WING UPPER STRINGER NR 11 AT XORS 683 REF SRM 57-00-03, REPAIR 5, FIG 202.SDR IPXA2M74662Cover · looseL1 FWD DOOR HANDLE EMERGENCY LIGHT COVER LOOSE. R & R LIGHT ASSY IAW MM 33-52-02. OPS CHECKED GOOD.SDR IPXA2M74892Doubler · crackedINSPECTION TYPE: 4C LT WING FIXED L/E UPPER BEADED DOUBLER CRACKED AT XOS 692-698. REPAIRED LT WING FIXED L/E UPPER BEADED DOUBLER FROM STA XOS692-698 REF SRM 57-40-02, REPAIR 9, FIG 202, REV 49.SDR FDEA201207282728Longeron Splice · crackedCENTER CARGO BETWEEN STA 5-113 AND STA 1561 LONGERON 47 LT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-1SDR FDEA201207282727Longeron Splice · crackedCENTER CARGO LONGERON 38 LT BETWEEN STA 5-113 AND STA 1561 , FOUND LONGERON SPLICE CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207282726Longeron Splice · crackedCENTER CARGO BETWEEN STA 5-113 AND STA 1561 LONGERON 43 LT SPLICE END, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 RSDR FDEA201207282725Longeron Splice · crackedCENTER CARGO BETWEEN STA 5-113 AND STA 1561, LONGERON 37 RT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7114 REVISION: E. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-SDR FDEA201207282724Longeron Splice · crackedCENTER CARGO BETWEEN BS 5-113 AND 1561 LONGERON 41 RT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50 NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7115 REVISION: D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISDR IPXA12M74963Doubler · crackedINSPECTION TYPE:4C, RT WING FIXED L/E BEADED DOUBLER CRACKED TWO PLACES AT APPROX XOS 661- 667. REPAIRED RT WING FIXED L/E BEADED DOUBLER AT XOS661-667 REF EA 011-5730-01-A4156 I/R, EO MD11-5730-48132-A AND SRM 57-40-02, REPAIR 9, FIG 202, REV 49.SDR IPXA12M74904Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED 5 EA PLACES AT XOS698 AND XOS703. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT STASA EA 011-5730-01 -A4157, EO MD11-5730-48202-A AND FAA FORM 8100-9.SDR IPXA12M74903Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED 3 PLACES AT XOS633 AND XOS636. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS633 AND XOS636 REF STASA EA 011-5730-01-A4158 REV I/R, EO MD11-5730-48203-A AND FAA FORM 8100-9.SDR FDEA201207272715Skin · misrepairedAGING AIRCRAFT - EXISTING REPAIR AT RT FUSELAGE SKIN AT STA 1830 BETWEEN LONGERONS 37 AND 38 MISREPAIRED. REPAIRED IAW EA 1-5330-160992. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR IPXA2M74893Doubler · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED 2 EA PLACES AT XFS 669-674. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XFS 669-674 REF SRM 57-40-02, REPAIR 9, FIG 202, REV 49.SDR FDEA201207272718Skin · crackedLEFT WING L/E NR 8 SLAT LOWER SURFACE MID AREA FOUND CRACKED. REPAIRED AS PER SRM 57-40-01 FIGURE 201 REPAIR 3 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207272719Engine · firePUSH CREW REPORTED NR 1 ENGINE EMITTING FLAMES ON START. START VALVE CLOSED AT 33 PERCENT N2, EARLY INDICATIONS 510 F/F, 168 EGT. CONTINUED TO MOTOR ENGINE WITH FUEL LEVER OFF FOR REJECTED START. FLAMES WERE REPORTED AT THIS TIME. TAILWIND OF 10 KTS. SUSDR FDEA201207272717Skin · corrodedRT FUSELAGE SKIN FROM STA 2027 TO 2024 (BENEATH FAIRING NR 341CF), FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, REV 50 ORIGINAL THICKNESS: 0.095 INCH, MATERIAL REMOVED: 0.085 INCH, REMAINING THICKNESS : 0.010 INCH AND FOUND EXCEEDED LIMIT IAW SRM 53SDR CLCA20120727001Button · out of positionDURING DEPARTURE, (VCP) CAPTAINS A/P DISCONNECT BUTTON CAME OUT OF ITS SOCKET, AND CAUSE ELECTRIC SHORT. RETURNED TO VCP. TROUBLESHOOT SYSTEM AND FOUND WIRE LOOSE AT CAPTAINS AP DISCONNECT SWITCH. SECURED WIRE AT CAPTAINS SWITCH CONNECTOR IAW MD-11 AMM 20-3SDR IPXA12M75008Floor Support · corrodedINSPECTION TYPE: 4C, AFT CARGO BAY BS 1841 AND RBL 46 FLOOR SUPPORT SCREW HOLE CORRODED ON SURFACE. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW EA 011-5310-01-A4189 REV I/R AND EO 5310-48286-A.SDR IPXA12M74964Angle · crackedINSPECTION TYPE:4C, RT WING T/E VERTICAL SUPPORT ANGLE BROKEN AT INBD OF RT MLG AFT TRUNNION. REMOVED, FABRICATED AND INSTALLED RT WING T/E VERTICAL SUPPORT INBD OF RT MLG AFT TRUNNION REF DWG ARC0298 AND SRM 51-33-01 PAGE 30 AND 45.SDR FDEA201207262699Skin · misrepairedAGING AIRCRAFT -EXISTING REPAIR AT RT FUSELAGE SKIN AT BS 488 BETWEEN LONGERONS 28 AND 29 MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 7, REV 50 EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR AS GMM 6-2-100, REV 115.SDR FDEA201207262698Frame · misrepairedBS 535 LONGERON 25LT FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201. REPAIR 1, REVISION 50 EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201207262697Stringer · misrepairedBS 535, LONGERON 21L MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 50 EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207262681Stringer · misrepairedRT WING STRINGER 43 MISREPAIRED. REPAIRED IAW EA 1-5710-162358. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207262696Frame · dentedFRAME BS 1701, LONGERON 12R FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.SDR FDEA201207262695Frame · dentedFRAME BS 1721, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.SDR FDEA201207262694Frame · dentedFRAME BS 1641, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207262693Trunnion · crackedNLG RT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR FDEA201207262692Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR FDEA201207262691Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 1421, X=8 FOUND CROWN WITH A HOLE ELONGATED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM BS 1411 TO 1471 X =8 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115SDR FDEA201207262690Seat Track · damagedMAIN DECK CARGO TRACK AT BS 1541, X=-8 FOUND CROWN HAS A HOLE ELONGATED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM BS 1531 TO 1571 X =-8 AS PER SRM 53-00-52 FIGURE 201, REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207262689Skin · crackedRIGHT WING OTBD L/E PANEL NR 619CB CUTOUT OTBD FORWARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING OUTBOARD LEADING EDGE PANEL 619CB CUTOUT OUTBOARD FORWARD CORNER AS PER SRM 57-40-02 REPAIR 7 FIGURE 201 REVISION 50 REPAIR CLASSIFIED MAJORSDR FDEA201207262688Vane · delaminatedLT WING INBD FLAP VANE LOWER SURFACES BETWEEN INBD AND MID TRACKS, FOUND DELAMINATED. REMOVED AND REPLACED LEFT HAND WING INBOARD FLAP VANE AS PER AMM 27-50-22-4 REVISION 72.0. FLAP VANE ADJUSTMENTS AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 72.0. SDR FDEA201207262721Relay · inoperativeAPPROX 6.5 HRS INTO FLIGHT BATTERY DISCHARGING ALERT ILLUMINATED IAW QRH, DIVERTION INITIATED, AFTER 5-7 MINUTES THE ALERT WENT OUT. ELECTED TO PROCEED TO DESTINATION. VOLTAGE WAS CONSTANT 33 VOLTS DURING AND AFTER THE ALERT. ILLUMINATED AGAIN ON SHORT FSDR FDEA201207262683Skin · crackedLEFT WING NR 14 SLAT TRACK CUT-OUT FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40.02, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207262682Skin · crackedLEFT WING TELESCOPIC DOOR CUT-OUT FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-01, FIG 201, REPAIR 10, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR IPXA12M74774Trunnion · crackedINSPECTION TYPE: 4C, APPROX 1 INCH CRACK AT TYPICAL CRACK LOCATION ON LT NLG TRUNNION FITTING. REPAIRED LT NLG TRUNNION FITTING REF SRM 53-10-14, REPAIR 2, FIG 202, REV 49.SDR FDEA201207252669Charger · malfunctionedEMERGENCY POWER TEST FAIL NOTED ON POST FLIGHT INSP. EPCU SHOWS BATTERY/INTFC UNDER CURRENT FAULTS AND LAST TWO FLIGHT LEGS. COMPLIED WITH FIM 24-30-03-00 BATTERY VOLTAGE FOUND TO BE WITHIN LIMITS. EMERGENCY POWER TEST ATTEMPTED THREE TIMES, TWO FAILED, P
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