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 FDEA201809252691Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE FOUND CORROSION. NR 7 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2SDR FDEA201809252690Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE FOUND CORROSION. BOLT HOLE NR 7 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS SDR FDEA201809252689Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44SDR FDEA201809252688Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44SDR FDEA201809252687Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE BORE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2B. EO SDR FDEA201809252686Hinge Bracket · corrodedLEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STSDR FDEA201809252685Hinge Bracket · corrodedLEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STESDR FDEA201809252684Hinge Bracket · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT O/B HOLE BORE( #7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHSDR FDEA201809252683Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT I/B HOLE BORE (#7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHINSDR FDEA201809252682Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) BARREL NUT HOLE SURFACE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) BARREL NUT HOLE SURFACE CORROSION REWORKED AS PER MD1 CMM57-44-08. NEW REPAIR SHIM FABRICATED AND INSTALLED PER MD11 CMM57-4SDR FDEA201809252681Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) PIVOT HOLE BORE FOUND CORROSION. LH WING ( WING SIDE ) O/B FLAP I/B HINGE PIVOT HOLE BORE #4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM 57-44-08. NEW OVERSIZED BUSHING FABRICATED BY MACHINING ASDR FDEA201809252706Skin · puncturedRIGHT WING INBD FLAP VANE LOWER SURFACE FOUND PUNCTURED AT XIFH 193.875. SKIN REPAIR CARRIED OUT METAL BONDED WITH FILLER AND DOUBLER AS PER SRM 51-71-00 PARAGRAPH 20 AN EA 1-5750-T0342536 PART 1. REPAIR ON RT INBD FLAP VANE ARC2557-54 LOWER SKIN. REPAIR CLASSSDR IPXA2018092634411Drive Chain · brokenL1 DOOR EMERGENCY ASSIST BOTTLE DRIVE CHAIN WAS BROKEN. INSTALLED A DRIVE CHAIN IAW CMM 52-11-09. OPS CHECKED GOOD.SDR IPXA2018092634413Drive Chain · brokenL1 DOOR EMERGENCY ASSIST BOTTLE DRIVE CHAIN WAS BROKEN. INSTALLED THE DRIVE CHAIN IAW CMM 52-11-09. OPS CHECKED GOOD,SDR IPXA2018092654400Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-51-01-401. OPS CHECKED GOOD.SDR FDEA2018092542661Skin · crackedDURING HIGHFREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT FOUND HOLE #7, #33, #34 AND #36 WITH CRACK INDICATION. (AT BETWEEN STA XORS 690 AND STA XORS 700 ). RIGHT HAND WING LOWSDR IPXA2018092654360Fan · inoperativeDURING A PREFLIGHT, THE CREW REPORTED ACC SYS TEST FAILED, SHOWS AVIONIC RACK FAN 2 FAILED. OPENSDR IPXA2018092654393Battery Pack · inoperativeEMERGENCY LIGHT BATTERY 1 LOW LEVEL 1 WARNING, DURING TEST. REPLACED THE EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW MM 33-51-01-401. OPS CHECKED GOOD.SDR FDEA2018092532657Transducer · failedPDIS 595 32-42 1218 22SEP18 LAX FACT U LOGPAGES:2871877 BEFORE TAKEOFF RECEIVED LEVEL 2 "TIRE FAIL" ALERT. #9 TIRE DISPLAY LOST - RETURNED TO GATE. REMOVED & REPLACED WHEEL SPEED TRANSDUCER IAW MM 32-45-03-4 & 32-45-03-5 OPS CHECK NORMAL.SDR IPXA2018092434304Seal · damagedFWD, LOWER CARGO DOOR SEAL WAS DAMAGED. REPAIRED THE AREA IAW AMM 52-00-00-801.SDR FDEA201809212645Floor Support · corrodedFWD CABIN, UPON LAVATORY MODULE REMOVED FOR FLOORBEAM ATTACH ANGLE REPAIR ACCESS, FOUND RT FLOOR SUPPORT AT STA 413, X= -25 CORROSION. FLOOR SUPPORT CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. FLOOR SUPPORT REMOVED AND REPLACSDR FDEA201809212644Doubler · crackedRIGHT WING LEADING EDGE COMPT LOWER SURFACE PANEL CUTOUT FWD EDGE DOUBLER AT STA XOS 604 FOUND CRACK. CRACKED DOUBLER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DRAWING ARB2933 REVISION AJ. INSTALLED NEW DOUBLER AT RIGHT WING LEADING EDGE COSDR FDEA201809202720Door · crackedDURING WALK AROUND FOUND POSSIBLE CRACK IN THE #1 PACK BAY CUT OUT ON UPPER AFT CORNER. INFO 20SEP18 21:14 COMPLETED REPAIR OF #1 PACK DOOR IN REF TO MD11 SRM 53-20-15-2R. COMPLIED WITH EA# 1-5330-T0342533 PART 1 FOR TRACKING ONLY. REPAIRED REF MD11SDR FDEA2018100202720Skin · crackedMDIS 618 53-30 7104 20SEP18 MEM FACT U DURING WALK AROUND FOUND POSSIBLE CRACK IN THE NR 1 PACK BAY CUT OUT ON UPPER AFT CORNER. INFO 20SEP18 21:14 FACT 25SEP18 07:14 MEM U COMPLETED REPAIR OF NR 1 PACK DOOR IN REF TO SRM 53-20-15-2R. COMPLIED WITH EA 1-5330-SDR IPXA2018092134237Lamp · inoperativeDURING PREFLIGHT, THE R1 SLIDE WILL NOT TEST. REPLACED THE LAMP IN THE R1 DOOR SLIDE REMOTE PTT INDICATOR IAW MM 25-61-01-400-801. OPS CHECKED NORMAL IAW MM 25-61-04-710-801.SDR FDEA201809202632Warning System · activatedALT FL350 CABIN ALTITUDE LEVEL 3 ALERT. FASE 1S TO QRH. REF FIM 21-33-00-2 FIG 103 CHECKED BOTH CPC'S FOR BLOCKAGE AND NONE FOUND. CFDS FAULTS ACC1 WITH PK 1 RAD ACT IN LAST LEG BUT NO CURENT FAULTS. DEFERED PACK NR 1 RAM AIR ACTUATOR WRI 21-52-1583. PERFORMESDR FDEA201809202614Skin · corrodedEMPENNAGE - AFT ACCESSORY COMPARTMENT, RIGHT HAND SURFACE AREA FOUND SKIN CORROSION AROUND ANCHOR NUT AT STA Y = 2159 TO Y = 2149. LONGERON 33 RIGHT TO LONGERON 35 RIGHT. AFT ACCESSORY COMPARTMENT, RIGHT HAND SURFACE AREA SKIN CORROSION AROUND ANCHOR NUT AT STSDR FDEA201809192586Floor Support · corrodedMAIN DECK CARGO FLOOR SUPPORT FOUND WITH CORROSION AT STA 1902 X = 57. FLOOR SUPPORT CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. ORIGINAL THICKNESS: 0.188 INCH MATERIAL REMOVED: 0.100 INCH, REMAINING THICKNESS: 0.088 INCH. FSDR FDEA2018092092585Former · crackedLEFT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG AND 51-33-01-OG. FORMER PART NUMBER ARB2920-13 FABRICATED AS PER DRAWING ARB2920 REVISION BB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR FDEA2018092092584Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 655. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018092092583Doubler · crackedRIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 543. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.SDR FDEA2018092092582Doubler · crackedRIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 626. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018100134602Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP AFT FLANGE WAS CORRODED BETWEEN XORS 561 - 575. REPAIRED THE SPAR UPPER CAP AFT FLANGE IAW EA 011-5710-01-A7477, REV I/R, AND EO MD11-5710-70099-A. MINOR.SDR IPXA2018092874480Web · crackedCENTER FUEL TANK UPPER AFT WEB WAS CRACKED AT BS 1372, RBL 80 AND WL 54. REPAIRED THE WEB IAW EO MD11-5710-70026-A. MAJOR.SDR FDEA201809182574Hinge · corrodedLEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT OUTBD LUG HOLE FOUND CORROSION. HOLE A AND B REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MSDR FDEA201809182573Hinge · corrodedLEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFSDR FDEA201809182572Hinge · corrodedRIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED OUTBD LUG HOLE FOUND CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2BSDR FDEA201809182571Hinge · corrodedRIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2B. RSDR FDEA201809182579Intercostal · crackedVERTICAL STAB REAR CENTER SPAR TO REAR SPAR INTERCOSTAL STA 2164, RIGHT SIDE AFT END FOUND CRACKED. INTERCOSTAL REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 204 REPAIR 7 AND EA 1-5530-T0342479 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809182564Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RIGHT HAND STA 535 LONGERON 19 RIGHT. FRAME REPAIR AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809182563Frame · chafedCABIN MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RIGHT HAND STA 535, LONGERON 24 RIGHT. FRAME REPAIR AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809182570Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 763. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809182569Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 618. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809182568Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 612. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201809182567Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 626. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091872559Stringer · crackedUPPER AUX FUEL TANK STRINGER NR 47 FROM XCW=50 TO XCW=57 FOUND CRACK. UPPER AUX FUEL TANK STRINGER REPAIRED AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091872558Stringer · crackedUPPER AUX FUEL TANK STRINGER 52 FROM XCW=50 TO XCW=56 FOUND CRACK. UPPER AUX FUEL TANK STRINGER 52 FROM XCW=35.5 TO XCW=59.5 AREA REPAIRED AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018092874473Longeron Splice · crackedLONGERON SPLICE 1R WAS CRACKED AT STATION 5-123. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-31-01, AND 51-33-01. MINOR.SDR IPXA2018091974101Structure · dentedFWD, LOWER CARGO DOOR DENTED AT BS 937. REPAIRED IAW EO MD11-5230-68305-B.SDR IPXA2018100534697Fastener · looseNR 2 ENGINE INLET NOSE SKIN HAD LOOSE BLIND FASTENERS. REPAIRED IAW EA 011-7110-01-A7465, REV IR, AND EO MD11-7110-58061-B. MINOR.
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