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 IPXA2017111523611Fuel Tank · crackedOVERWING UPPER FUEL TANK WEB IS CRACKED AT BS 1372, LBL 80. REPAIRED THE TANK WEB IAW EO MD11-5710-66397-A. MAJOR.SDR IPXA2017111523610Fuel Tank · crackedOVERWING UPPER FUEL TANK WEB IS CRACKED AT BS 1372, RBL 80. REPAIRED THE TANK WEB IAW EO MD11-5710-66397-A. MAJOR.SDR IPXA2017111423579Light · brokenL1 DOOR EMERGENCY LIGHT FORWARD DOOR HANDLE ASSY BROKEN. R & R THE ASSY IAW MM 33-52-02-000.SDR FDEA201711113235Duct · crackedLEVEL 2 ENG 2 ICE DUCT FAIL WARNING AFTER T/O PASSING 3000', PER QRH SHUT DOWN NR 2 ENG AND RETURNED TO BASE. DISCOVERED THAT THE DUCT GOING AFT IS CRACKED.SDR IPXA2017111423580Control Unit · warning messageL2 FUEL QTY, USED CHECK ALERT QTY WAS APPROX 3000 LBS LESS THAN EXPECTED, PERFORMED FAULT REVIEW OF CFDS AND FUEL QTY BITE UNIT AND NO CURRENT FAULTS FOUND PERFORMED REVIEW OF HISTORY AND NO FAULTS FOUND CW FIM 28-14-00-101, FIEL 102, SHEET 17, 18, AND STEP 2SDR FDEA201711103238Warning System · false activationON PREFLIGHT DURING EMERGENCY LIGHT TEST GOT "EMER LT BAT 1 LO" DISPLAYED. PERFORMED OPERATIONAL TEST 4 TIMES, ALL OPS NORMAL. NO HISTORY IN 30 DAYS. REF AMM 33-51-01-5.SDR 9WGA201711140001Aileron Sys · malfunctionedDURING CLIMB, THE AILERON DEFLECTION DISENGAGED. DUMPED FUEL, PERFORMED UNSCHEDULED LANDING.SDR FDEA201711103218Battery · faultedDURING PREFLIGHT, DURING AN EMERGENCY LIGHT TEST RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW DISPLAYED. PERFORMED AN OPERATIONAL TEST 4 TIMES, ALL OPS NORMAL. NO HISTORY IN 30 DAYS. IAW AMM 33-51-01-5SDR FDEA201711093211Hinge · wornCARGO DOOR FWD 6 HINGE LOBES OVER CMM LIMITS. COMPLIED WITH EA 1-5230-T0336506, REAMED LUG HOLES TO OVERSIZE CONDITION AND INSTALLED BUSHINGS.SDR FDEA201711083196Hinge · damagedCABIN UPPER CARGO DOOR FWD HINGE ON A/C. HINGE LOBE BUSHING LOOSE(MIGRATION 3RD HOLE). UPPER CARGO DOOR FWD HINGE ON AIRCRAFT HINGE LOBE BUSHING. REMOVED PER CMM 20-10-07. ELONGATED HOLES REWORKED AND FOUND EXCEEDED LIMIT PER SRM 52-30-16-1A FIG 101 NR 1, EXISSDR FDEA201711083195Hinge Bracket · corrodedLEFT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE CORRODED. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-76743E, P6, STEP 2.A, AND STEP 2.B. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711083194Hinge Bracket · corrodedLEFT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE CORRODED. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-76743E, P6, STEP 2.A, AND STEP 2.B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711083193Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE CORRODED. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0322446D P6 STEP 2A AND STEP 2B. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711083192Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM57-52-03. AN OVERSIZED BUSHING WAS FABRICATE AND INSTALLED IAW EA 1-5750-T0322446D, P6, STEP 2.A AND STEP 2.B, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-SDR FDEA201711083191Hinge · corrodedRT WING I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0331058A P1 STEP F(1) AND STEP F (3). RT WING INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201711083190Hinge · corrodedLT WING INBD FLAP OUTBD FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0331052A P1 STEP F(1) AND STEP F (3). LT WING INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR 9WGA52017110801Warning Message · multiple failAT 39,000 FEET, A WARNING ON PNEUMATIC MANIFOLD SYSTEM 3, CLOSED THE BLEED VALVE ON ENGINE 3. AFTER A CABIN RATE ANNUNCIATION, REQUESTED DESCENT TO 31,000 FT, FOLLOWED BY A SECOND RED WARNING ON SYSTEM 1, FOLLOWED BY A RAPID CABIN CLIMB, EVEN THOUGH THE SYSTEMSDR IPXA2017110823385Door · defectiveCPT SEAT LIFE VEST DOOR WILL NOT STOW. REPAIR PER MM 25-11-00-201 OPS CHKS GOOD.SDR IPXA2017110623314Smoke Barrier · looseMCD FWD WALL LEFT SIDE SMOKE BARRIER CURTAIN LOOSE. SECURED MCD FWD WALL LEFT SIDE SMOKE BARRIER CURTAIN AS REQUIRED.SDR IPXA2017110623310Light · inoperativeR1 SLIDE BOTTLE PRESS TEST INOP. R&R 2EA CM368 BULBS IN R1 DOOR REMOTE PRESS TEST INDICATOR. OPS TEST GOOD PER AMM 25-61-04-710-702.SDR FDEA201711053168Skin · chafedRIGHT WING REPAIR DOUBLER OTBD OF SLAT TRACK NR 12 CUTOUT FOUND CHAFED, AT XOS 789. REPAIRED IAW EA 1-5730-T0323387A, P3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033139Doubler · crackedLEFT WING LEADING ACCESS LAND DOUBLER AT XOS 786 FOUND CRACKED. REPAIRED IAW EA 1-5730-T0336485, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033138Skin · crackedLEFT WING FIXED LEADING EDGE SKIN AT XOS 786 FOUND CRACKED. REPAIRED THE LE SKIN IAW EA 1-5730-T0336485, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033137Cargo Track · chippedMAIN DECK CARGO TRACK CROWN AT BS 1551, RBL 47.5 CHIPPED. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFEID AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033136Cargo Track · chippedMAIN DECK CARGO TRACK CROWN AT BS 5-5, RBL 47.5 CHIPPED. REPLACED THE CARGO TRACK FROM BS 5-0 TO STA 5-63, RBL 47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033135Cargo Track · corrodedMAIN DECK CARGO TRACK CORRODED BS 1491, LBL 8.5. REPLACED THE CARGO TRACK FROM BS 1471 - 1511, LBL 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033134Cargo Track · damagedMAIN DECK CARGO TRACK CROWN DAMAGED BS 1431, RBL 47.5. REPLACED THE SEAT TRACK FROM BS 1391 - 1451 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033133Cargo Track · corrodedMAIN DECK CARGO TRACK CORRODED AT BS 1159, LBL 47.5. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201711033162Gasket · cutAFTER TAKEOFF, PLUS 25 MINUTES, CLIMBING THROUGH FL250, THE NR 2 ENGINE FLAMED OUT. THROTTLES WERE SET AT CLIMB POWER WHEN CONFIRMED ENGINE OUT MESSAGE APPEARED ON MCDU SCRATCH PAD. NR 2 ENGINE PARAMETERS, N1 AT 51.4 %, EGT 335, N2 335, N2 AT 79.4%, FUEL FSDR IPXA2017110323227Switch · inoperativeR1 DOOR PRESS TO TEST LIGHT INOPERATIVE. INSTALLED NEW BATTERIES, INSTALLED NEW SWITCH ASSY. OPS CHECKED GOODSDR FDEA201711013120Hinge · wornMAIN DECK CARGO DOOR MOST HINGE SECTION ON FUSELAGE SIDE FOUND FWD 12EA HINGE LOBE HOLES WORN EXCEEDED LIMITS AT STA 635 -STA 652. HOLES REWORKED AND FOUND NR 1 - NR 7 HOLES EXCEED LIMIT AS PER SRM 52-30-16-1A FIGURE 101, NR 1 EXISTING HOLES DIA 0.452''-0.455'SDR FDEA201711013119Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 1780, X= -8.5 FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMIT OF SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPAIR PER SRM 53-00-52SDR FDEA201711013118Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 1760, X= 27.5 FOUND CORROSION MAIN DECK FLOOR AT SEAT TRACK STA 1760, X= 27.5. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM SDR FDEA201711013117Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 5-83, X= 8.5 FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMIT OF SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPAIR PER SRM 53-00-52-SDR 201710313114Cover · failedAFTER T.O. AIRSPEED BECAME UNRELIABLE, CAPTS A/S APPRX. 30KTS LOWER THAN F.O.'S SIDE. SEL ELEV FEEL MAN AND SEL FLAP LIM OVRD LEVEL 2 ALERTS, QRH DIRECTED TO AIRSPEED UNRELIABLE WHICH BROUGHT US TO SELECT OTHER CADC. SLECTED CAPT ON 2 AND ALERTS WENT AWAY, C/SDR FDEA201710303111Cargo Track · corrodedCABIN MAIN DECK CARGO TRACK CORROSION AT BS 1169 RBL 47.5. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710303110Skin · crackedRIGHT WING LEADING EDGE LOWER PANEL CUTOUT FWD DOUBLER AT OUTBD OF SLAT TRACK NR 9 FOUND CRACKED XOS 597. REMOVED AND REPLACED IAW SRM 51-31-01-0G. DOUBLER FABRICATED IAW DWG ARB2933, REVISION AJ. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710303109Doubler · crackedRIGHT WING LEADING EDGE CAVITY AT XOS 612 BEADED DOUBLER CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710303108Skin · corrodedEMPENNAGE AFT ACCESSORY COMPT RT STA 2164 SKIN FOUND CORROSION AS MARKED. CORROSION REMOVED FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THICKNESS : 0.100", MATERIAL REMOVED : 0.090" AND REMAINING THICKNESS : 0.010". AFT ACCESSORY COMPT RT STA 21SDR FDEA201710303106Slide · unsecureAFTER REPLACING L1 DOOR WARNING SWITCH, DURING OPS CHECK, WHILE ARMING DOOR SLIDE, ACTIVATED PNEUMATIC DOOR SYSTEM. SLIDE DID NOT DEPLOY, BUT DROPPED FROM BASKET FULLY INTACT. INSTALLED L1 DOOR SLIDE/RAFT CONTAINER, IAW AMM 25-61-01-4.SDR FDEA201710303104Web · crackedUPON REMOVING RT I/B FLAP EXISTING REPAIR, CRACK FOUND ON WEB AT STA XIFH 171.30 AS MARKED. RT INBD FLAP STA XIFH 171.30 WEB CARRIED OUT REPLACEMENT AS PER EA 1-5750-T0336221 PT 1. RT WING INBD FLAP ASSY CENTER BOX UPPER SKIN AND LOWER SEGMENT LOWER SKIN REPSDR IPXA2017103123121Floorboard · damagedMAIN CARGO DECK FLOORBOARD P/N AFA8942-11 DAMAGED. DEPRESSION IN PANEL 3.3"L X 1.3" W X .170 DEEP. FABRICATE NEW FLOOR PANEL PER EO MD11-5320-27386-C.SDR IPXA2017103123124Floorboard · damagedMAIN CARGO DECK FLOORBOARD P/N ADA7556-60 DAMAGED. DEPRESSION ACROSS PANEL FROM AFT EDGE 6"L X 3"W X 0.14"D. FABRICATED NEW FLOORBOARD PANEL PER EO MD11-5320-27386-C.SDR IPXA2017103123123Floorboard · damagedMAIN CARGO DECK FLOORBOARD P/N AEA7317-34 DAMAGED. DEPRESSION IN PANEL FORE TO AFT 60"L X 2.4"W X 0.10"D. FABRICATED NEW FLOORBOARD PER EO MD11-5320-27386-C.SDR IPXA2017103123122Floorboard · damagedMAIN CARGO DECK FLOORBOARD P/N AEA7575-24 DAMAGED. DEPRESSION ACROSS PANEL FORE TO AFT EDGES 102"L X 2.10"W X 0.15"D. FABRICATED NEW FLOORBOARD PANEL PER EO MD11-5320-27386-C.SDR FDEA201710293102Switch · looseFOUND WIRES LOOSE ON NR 1 ENG AGENT 1. REMOVED AND REPLACED ENGINE 1, AGENT 1 DISCHARGE SWITCH S1-161 PER AMM 26-21-02-4. SYSTEM OP CHECKS GOOD PER 26-21-01-5. SWITCH PART NUMBER BZ2RT, NO SERIAL NUMBER, MANUFACTURER, MICRO. REMOVED AND REPLACED ENGINE 1, SDR FDEA201710273083Skin · crackedDURING HFEC INSPECTION AT LTW FIXED LEADING EDGE SKIN AT CORNER 11, FUEL ACCESS DOOR FWD INBD CORNER, FOUND CRACK APPROX 0.25 INCH IN LENGTH, AT STA XOS 611. LT WING FIXED LEADING EDGE SKIN CORNER NR 11 FUEL ACCESS DOOR FWD I/B CORNER APPROX STA XOS 611 CRACKESDR FDEA201710273082Skin · crackedDURING HFEC INSPECTION AT RT WING FIXED LEADING EDGE SKIN AT CORNER 5 OF SLAT ACTUATOR ACCESS DOOR INBD CORNER, FOUND APPROX CRACK 1.00 INCH IN LENGTH, STA XOS 491. RT WING FIXED LEADING EDGE SKIN AT CORNER 5, SLAT ACTUATOR ACCESS DOOR FWD INBD CORNER STA XOS SDR FDEA201710273081Skin · chafedRIGHT WING - EXISTING REPAIR ON FIXED LEADING EDGE SKIN AT STA XOS 993. LOWER SKIN FOUND CHAFED RT WING XOS 993 FIXED LEADING EDGE SKIN EXISTING REPAIR DOUBLER CHAFFED MARK. REMOVED AND FOUND EXCEEDED LIMIT PER SRM 57-00-00-2R FIG 202. DAMAGED REPAIR DOUBLER SDR FDEA201710273080Skin · crackedDURING HFEC INSPECTION AT LTW FIXED LEADING EDGE SKIN AT CORNER NR 13 SLAT TRACK 10 CUTOUT AFT INBOARD CORNER, FOUND CRACK APPROX 0.25 INCH IN LENGTH, STA XOS 657. LT WING STA XOS 657 FIXED LEADING EDGE SKIN CORNER 13 SLAT TRACK 10 CUTOUT AFT INBOARD CORNER CR
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