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 IPXA2M74613Skin · chafedINSPECTION TYPE:4C, LT WING UPPER SURFACE REPAIR UNDER NR 1 AND NR 2 SLAT SEAM GOUGED WITH ROLLED METAL ON PREVIOUS REPAIR DOUBLER. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED AND INSTALLED NEW REPAIR OF LT WING FIXED L/E EXTERIOR BETWEEN STA XIS243-250 IAW SSDR FDEA201207052486Switch · looseL1 SLIDE REMOTE PRESSURE INDICATOR ASSY INOPERATIVE. TROUBLESHOOTING FOUND BASE OF LAMP SWITCH LOOSE OUT OF POSITION,REINSTALLED & SECURED SWITCH BASE AND PERFORMED. OPS TEST SATIS, IAW MM 25-61-04-5.SDR IPXA2M74618Access Panel · damagedINSPECTION TYPE: 4C, FASTENER COUNTERSINK DOUBLE-DRILLED AT AFT CORNER OF VERTICAL STAB T/E ACCESS PANEL 374BL LT SIDE. REPAIRED LT UPPER VERTICAL STAB T/E AT ZFR 315 IAW STASA EA 011-5530-01-A4104 REV IR & EO MD11-5530-48022-A, FAA 8100-9.SDR IPXA12M74520Rib · gougedINSPECTION TYPE:4C, LEFT HORIZONTAL STAB FRONT SPAR NR 10 IS GOUGED ON FORWARD LOWER END. REPAIRED RIB IAW EA 011-5510-01-A4100, REV IR AND EO MD11-5510-47908-A.SDR IPXA2M74582Longeron Splice · crackedINSPECTION TYPE: 4C, LONGERON SPLICE 38R CRACKED BS 1521. REMOVED FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW SRM 51-31-01, 51-33-01 AND DWG A5A7114.SDR FDEA201207032457Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION FOUND CRACK INDICATION AT LEFT NR 4 BANJO FITTING LOWER VERTICAL STAB FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 55-30-02 REPAIR 3 FIGURE 201 REVISION 49. REPAIR CLASSIFIED MAJOR AS PER GMMSDR FDEA201207032456Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION, FOUND CRACK INDICATION AT RT NR 4 BANJO FITTING LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 53-30-02 FIGURE 201 REPAIR 3 REVISION 49 AND EA 1-5530-160973 PART 1. SDR FDEA201207032455Skin · crackedSEVEN FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6. REPAIRED AS PER EA 1-5710-160974 PART 1. REPAIR CLASSIFIED MAJOR SDR FDEA201207032454Skin · crackedELEVEN FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT, BETWEEN STA XORS=683.4 AND STA XORS=713.6. REPAIRED AS PER EA 1-5710-160975 PART 1. REPAIR CLASSIFIESDR IPXA12M74518Longeron Splice · crackedINSPECTION TYPE: 4C, LONGERON SPLICE 32R CRACKED AT BS 1521. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SPLICE IAW DWG A5A7112, SRM 51-31-01, 51-33-01, AND EO MD11-5100-47885-A.SDR IPXA2M74692Stringer Splice · corrodedINSPECTION TYPE:4C, CORROSION AROUND FASTENERS ON L50L AT BS 1957. R & R L50L SPLICE AT STA 1957 IAW SRM 51-31-01.SDR IPXA2M74679Skin · delaminatedINSPECTION TYPE:4C, LT INBD ELEVATOR LOWER OTBD T/E SKIN DELAMINATED. REPAIRED LT INBD ELEVATOR LOWER T/E SKIN AT XE180 IAW SRM 55-20-80. REPAIR 2 WET LAYUP.SDR IPXA2M74658Longeron Splice · corrodedINSPECTION TYPE: 4C, CORRODED LONGERON SPLICE 46R AT BS 1681. R & R LONGERON SPLICE IAW SRM 51-31- 01 AND 51-33-01.SDR IPXA2M74657Longeron · corrodedINSPECTION TYPE: 4C, LONGERON 46R CRACKED BETWEEN BS 1661-1681. REPAIRED CORRODED LONGERON IAW EA 011-5310-01-A4075, REV IR AND EO MD11-5310-48017-A.SDR IPXA2M74614Longeron · crackedINSPECTION TYPE:4C, LONGERON 45R CRACKED AT SPLICE FITTING STA 1661-1681. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF L45R BETWEEN STA 1651-1671 IAW STA SA EA 011-530-01-A4077, REV IR & EO MD11-5310- 48025-A FAA 8100-9.SDR IPXA2M74445Rib · crackedINSPECTION TYPE:4C, LT WING FIXED L/E SUPPORT RIB CRACKED APPROX AT STA XOS 829.5. R & R RIB IN LT WING FIXED L/E INTERIOR AT STA XOS.829.5 IAW SRM 51-31-01, 51-33-01, 51-35-01SDR FDEA201207022447Light · inoperativeON POST FLT CHECK, EMERGENCY LIGHT TEST FOUND ALERT "EMERGENY LIGHT BATTERY 1 LOW" STATUS IAW FIM 33-51-02-00 & FAULT. REPLACED EMERGENCY LIGHT IAW MM 33-51-01 & TESTED OK IAW MM 33-51-00.SDR IPXA2M74610Longeron · corrodedINSPECTION TYPE: 4C, CENTER CARGO BAY L38R CORRODED JUST AFT OF FRAME 1601. REMOVED FABRICATED & INSTALLED REPLACEMENT SECTION OF L38R BETWEEN STA 1531-1610 IAW EA 011-5310-01-A4092 REV IR & EO MD11 5310- 48021-A FAA 8100-9.SDR FDEA201207012433Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER, NR4 BANJO FITTING, RT SIDE FWD FLANGE. CARRIED OUT REPAIR AS PER DRAWING SR10550013 SHEET 7, 8, AND 9 REVISION P.SDR FDEA201207012431Frame · dentedFRAME AT BS 1661, LONGERON 11L, FOUND DENTED. REPAIRED IAW SRM SRM 51-33-01 REVISION 49. AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201207012430Frame · dentedFRAME AT BS 1721, LONGERON 11R FOUND DENTED. REPAIRED IAW SRM 51-33-01 REVISION 49 AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201207012429Frame · dentedFRAME AT BS 1661, LONGERON 11R FOUND DENTED. REPAIRED IAW 51-33-01 REVISION 49 AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201207012428Frame · dentedFRAME AT BS 1641, LONGERON 11, FOUND DENTED. CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201207012432Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER NR 4, BANJO FITTING, LT SIDE, FORWARD FLANGE. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIGURE 201 REPAIR 3 REVISION 49.SDR IPXA2M74418Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XOS 759-768. REPAIRED RT WING FIXED L/E BEADED DOUBLER AT BETWEEN XOS759-768 REF STASA EA 011-5730-01-A4031, REV I/R, EO MD11-5730-47835-A.SDR FDEA201206302421Gearbox · damagedENGINE NR 1 IDG FEEDER CABLE ADJACENT AREA LT SIDE ACCESSORY GEARBOX FOUND WITH ARCING DAMAGE. ACCOMPLISHED EA 1-7260-161492 PART 1. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201206302420Feeder Cable · burnedENGINE NR 1 IDG FEEDER CABLE HARNESS FOUND WITH CHAFING AND BURNED. R & R IAW AMM 71-50-04-4-1, REV 72.0, NR1 ENGINE AT 9 O`CLOCK POSITION ELECTRICAL WIRING MOUNTING BRACKET. R & R IAW STANDARD MX PRACTICES. NR 1 ENGINE IDG OPS CHECK CARRIED OUT IAW AMM 24-SDR FDEA201206292408Skin · cracked03 EA FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. CARRIED OUT REPAIR AS PER EA 1-5710-162348. REPAIR CLASSIFIED AS MINOR SDR FDEA201206292407Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGITUDINAL SPLICE FOUND CRACKED AT STATION 5-113 TO STA 1551, LONGERON 47RT. LONGERON REMOVED AS PER SRM 51-31-01 REVISION 49 AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING A5A7116 REVISION D AND INSTALLED AS PER SRM 51-33-0SDR FDEA201206292401Hinge Fitting · damagedRT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2865", REWORKED HOLE DIAMETER 1.313", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISSDR FDEA201206292400Hinge Fitting · damagedRT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.228", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED ASDR FDEA201206292399Hinge Fitting · damagedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2215", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISSDR FDEA201206292398Hinge Fitting · damagedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.255", REWORKED HOLE DIAMETER 1.2834", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHSDR FDEA201206292409Skin · crackedTHREE FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. CARRIED OUT REPAIR AS PER EA 1-5710-162349. REPAIR CLASSIFIED AS MINOR AS PSDR FDEA201206292406Seat Track · dentedBS 765, X= 8.5 SEAT TRACK FOUND DAMAGED. SEAT TRACK REMOVED AS PER SRM 51-33- 01 REVISION 49. NEW REPAIR SEAT TRACK AND SPLICE REWORKED AS PER SRM 53-00-52 REVISION 49 AND INSTALLED AS PER SRM 51-33-01 REVISION 49. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2SDR FDEA201206292405Frame · chafedFRAME BS 535, 9G NET LOWER SUPPORT YOKE FOUND CHAFED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49.SDR FDEA201206292404Frame · chafedFRAME BS 535, 9G NET UPPER SUPPORT YOKE FOUND CHAFED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49.SDR FDEA201206292403Splice · crackedCENTER CARGO COMPARTMENT LONGERON 42L SPLICE FOUND CRACKED AT STATION 5-113 TO 1541. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7115 REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISDR FDEA201206292402Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON 40R SPLICE FOUND CRACKED AT STA 5-113 TO 1541. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49. SPLICE FABRICATED AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR IPXA2M74624Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED BETWEEN XORS 518-523. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS625-629 IAW STA SA EA 011-5730-01-A4074 REV IR & EO MD11-5730-47975-A, FAA 8100-9.SDR IPXA2M74623Doubler · crackedINSPECTION TYPE:4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT APPRX STA, XORS444. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BEWTEEN XOS542-547 IAW STASA EA 011-5730-01-A4072, REV IR & EO MD11-5730-47977-A FAA 8100-9.SDR IPXA2M74622Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XORS 562-567. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS667-673 IAW STASA EA 011-5730-01-A4071, REV IR & EO MD11-5730-47976-A, FAA 8100-9.SDR IPXA2M74621Doubler · crackedINSPECTION TYPE:4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XORS580. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS679-685 IAW STASA EA 011-5730-01-A4070 REV IR & EO MD11-5730-47978-A FAA 8100-9.SDR IPXA12M74554Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XORS 683. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 783-789 IAW STASA EA 011-5730-01-A4080, REV IR AND EO MD11-5730-47966-A FAA 8100-9.SDR IPXA12M74519Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT APPROX STA XORS 552. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER IAW SRM 57-40-02. REPAIR 9, FIG 203 & EO MD11-5730-42916-D.SDR IPXA2M74341Stringer · crackedINSPECTION TYPE:4C, RT WING FIXED L/E COMPT AT APROX STA XORS562 (XOS667) UPPER STRINGER CRACKED. REPAIRED RT WING FIXED L/E UPPER INTERNAL STRINGER BETWEEN XOS667-671 IAW SRM 57-40-03, REPAIR 2, FIG 202.SDR IPXA2M74126Landing Gear · unknownON APPROACH WITH A/P ENGAGED, GEAR HANDLE WAS LOWERED. AP2 DISENGAGED AND NO GEAR LOWERED. ALL GEAR INDICATION UNSAFE. LANDING GEAR EXTENSION/RETRACTION ADJUSTED AND TESTED IAW AMM 32-32-00-5. NO FAULTS NOTED.SDR IPXA2M74119Smoke Detector · false activationFIFTY TWO MINUTES INTO FLIGHT "MAIN CABIN SMOKE ALERT, LVL 3" ALERT AURAL WARNING ANNUNCIATED FOR 2-3 SECONDS. DONNED 02 MASKS BUT ALERT SILENCES IMMEDIATELY LAND NO SMOKE DETECTORS APPEARED ON AIR SYNOPTIC. PERFORMED OPS TEST ON SMOKE DETECTOR SYS IAW MM 26SDR CLCA20120626001Structure · corrodedDURING REPAIRS OF FUEL LEAK IN THE TAIL TANK CORROSION WAS FOUND IN THE AREA OF BARREL NUT HOLE 27 RR SIDE. REMOVED BOLT AND BARREL NUT PER SB MD11-55-023 REV 3, CORROSION WAS REMOVED IAW OPTION 2 PAGE 38 OF REF SB. A TWO (2) STAGE APPROVAL PROCESS WAS USED SDR IPXA2M74340Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XOS610 AND XOS636. REPAIRED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS610 AND XOS636 REF STASA EA 011-5730-01-A4028 REV I/R, EO MD11-5730-47797-B AND 8100-9.
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