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 FDEA201209103270Flange · corrodedMAIN DECK BS 1761 - 1801, X=8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209103269Seat Track · corrodedMAIN DECK BS 1801- 1821, X=-8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR FDEA201209103268Seat Track · corrodedMAIN DECK BS 1761 - 1801, X=-8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR IPXA12M75337Fitting · corrodedINSPECTION TYPE:3C, RCB FLOOR FITTING NR 10 RT SIDE CORRODED. AFTER REMOVAL FOUND PART CRACKED. FABRICATED REPLACEMENT FITTING IAW DWG WSP0750 AND SP11250221.SDR FDEA201209103278Shutoff Valve · leakingON TAKE OFF ROLL, AT APPROX 75 KTS, NR 1 THRUST REVERSER PRESSURE FAULT ILLUMINATED. REJECTED TAKE OFF. REPLACED PRESSURE REGULATING AND SHUTOFF VALVE IAW AMM 78-31-07-4-1.SDR IPXA2M75279Power Supply · failedON PREFLIGHT, EMERGERNY BATTERY 1 LOW MESSAGE APPEARS ON TESTING OF EMERGENCY EXIT LIGHT SYS. R & R EMERGENCY LIGHTS BATTERY POWER SUPPLY REF MM 33-51-01-400. OPS CHECKED GOOD AT THIS TIME.SDR FDEA201209083260Shutoff Valve · failedPRESSURE FAULT. REMOVED REPLACED NR 1 THRUST REVERSER PRESSURE SWITCH PER AMM 78-31-08-2-1 OPS CHECKED NORMAL ACFT OK FOR SERVICE.SDR FDEA201209073249Seat Track · corrodedMAIN DECK CARGO TRACK AT BS 1880, X=-8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1751 TO STA..1887 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063239Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 1689, X=-8.5 , FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1571 TO 1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REFER TO SNRM N00262 FOR WORK DETAILS. REPAIR CLASSIFIED MAJORSDR FDEA201209063238Rib · crackedRIGHT WING RIB NR 16 AT FIXED L/E AREA (INBD SIDE) FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 REV. 50 AND REPLACED WITH NEW RIB 16 AS PER DWG ARB7565 REV. C REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063237Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 997, X= 75 , FOUND CROWN CHIPPED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 989 TO 1049 , X=75 AS PER SRM 53-00- 52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063236Cargo Track · corrodedMAIN DECK CARGO SEAT TRACK AT BS 1581, X=-8.5, FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1571 TO STA..1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6- 2-100 REVISISDR FDEA201209053606Control Unit · malfunctionedBATTERY DISCHARGING LEVEL 1, ALERT. INTERMITTENT AT FIRST, THEN CONTINUOUS. BATTERY VOLTAGE SHOWED 30V-34V. R & R EPCU REF AMM24-08-01-4, OPS CHECKED NORMAL. ALL TROUBLESHOOTING PERFORMED IAW FIM 24-30-03-00. NO FAULTS NOTED, SYSTEM OPS CHECKS NORMAL.SDR IPXA12M75577Skin · damagedINSPECTION TYPE: 4C, RIGHT HORIZONTAL L/E, SKIN DAMAGED. REPAIRED IAW EA 011-5510-01-A4222 I/R, EO MD11-5510-48705-A.SDR IPXA12M75379Trunnion · crackedINSPECTION TYPE:3C, NLG TRUNNION FITTING CRACKED, LT SIDE NEAR TRUNNION PIN. REPAIRED NLG LT TRUNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202. (MAJOR)SDR IPXA2M75166Switch · inoperativeRT SIDE DOOR ESCAPE SLIDE PRESSURE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED. R & R PRESSURE TO TEST SWITCH IAW MM 25-61-04. OPS CKS OK. THIS CLEARS M487705. PLACARD REMOVED.SDR IPXA12M75197Light · inoperativeEMERGENCY LIGHTS DO NOT PASS TEST MESSAGE, EMERGENCY BATTERY 1 LOW, TROUBLESHOT IAW FIM 33-51-00-101, FIG 104. EMERGENCY LIGHT TEST PASSED. PERFORMED OPS TEST IAW MM 33-51-01-700-802.SDR IPXA12M75166Light · inoperativeRIGHT SIDE DOOR ESCAPE SLIDE PRESSURE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED. OPEN.SDR IPXA12M75580Longeron Fitting · corrodedINSPECTION TYPE: 4C, LONGERON 27R FITTING BETWEEN STA 1239 TO 1250 HAS INTERGRANULAR CORROSION AND IS CRACKED. REPAIRED LONGERON 27R FITTING IAW EA 011-5310-01-A4266 REV I/R, EO MD11-5310-48706-A.SDR IPXA2M75443Longeron · crackedINSPECTION TYPE:4C, LONGERON 17L FITTING BETWEEN STA 1461 AND 1481 CRACKED. REPAIRED LONGERON 17L FITTING BETWEEN STA 1461 AND 1481 REF STA EA 011-5310-01-A4225, REV I/R, EO MD11-5310-48529-A AND FAA FORM 8110- 3.SDR IPXA12M75336Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 667. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 661-667 IAW EO MD11-5730-42916-D & SRM 57-40-02, REPAIR 9, FIG 203. (MAJOR)SDR IPXA2M75290Fitting · crackedINSPECTION TYPE: 3C, RT LOWER WINGLET FWD MOUNT FITTING CRACKED. REPLACED BOTH ATTACH FITTINGS ON RT LWR WINGLET WITH KIT SB11570063-5, APPX E. (MAJOR)SDR FDEA201209033211Switch · unsecureRT DOOR PRESSURE SENSING LIGHT INOPERATIVE. SECURED SWITCH BACK TO TEST LIGHT OPS CHECKS GOOD IAW AMM 25-61-04-4 .SDR FDEA201209023210Warning Message · false activationRTO DUE TO LEVEL 2 REVERSER FAILURE. FAULT WAS MOMENTARY AND DID NOT SPECIFY ENGINE. NO CURRENT OR LAST LEG FAULTS IN ECU 1A,B ECU 2A,B OR ECU 3A,B. OPERATED ALL REVERSERS IAW JRH 7-18, OPERATION AND INDICATIONS NORMAL. RAN ALL ENGINES IAW JRH CH6, BOOSTED SDR FDEA201209023209Mechanism · inoperativeCAPTAIN`S SLIDING WINDOW WILL NOT CLOSE. FOUND BROKEN LINK IN CHAIN FOR CRANK. R & R LT CLEAR VIEW WINDOOW DRIVE MECHANISEM IAW AMM 56-12-03-4. VERIFIED WINDOW DRIVE MECHANISM INSTALLATION REFER TO AMM 56-12-03-04. PERFORMED OPS TEST OF THE SLIDING CLESDR FDEA201209023206Battery · unknownBATTERY DISCHARGE ILLUMINATED SEVERAL TIMES STAYED ON FOR APPROX 2 MIN LAST DURATION THEN EXTINGUISHED. EPCU FAULT REVIEW SHOWED "COOLING VALVE 3/ INTFC", BATTERY CHARGER FAULT DISPLAY SHOWED "CHARGER FAIL, BATT FAIL, BUSS OK". TROUBLE SHOT IAW MM 24-30-0SDR IPXA2M75278Seat Track · corrodedINSPECTION TYPE:3C SEAT TRACK CORRODED AT COURIER SEAT RT AFT ATTACH POINT. REPLACED CORRODED SEACTION OF SEAT TRACK ALONG RBL 36 BETWEEN STA 439-516 IAW DWG WSP0826 AND SRM 51-31-01. MINOR.SDR IPXA2M75277Seat Track · corrodedINSPECTION TYPE: 3C, SEAT TRACK CORRODED AT COURIER SEAT AFT CENTER ATTACH POINT. REPLACED CORRODED SEACTION OF SEAT TRACK ALONG RBL 17 BETWEEN BS 439 - 516 IAW DWG WSP0826 AND SRM 51-31-01. MINOR.SDR IPXA2M75528Angle · corrodedINSPECTION TYPE:4C, UPPER SURFACE OF CENTER WING AT STRINGER 1 TO REAR SPAR BETWEEN FS 136 1-1371 RT SIDE HAS INTERGRANULAR AND EXFOLIATION COROSSION. REMOVED, FABRICATED AND INSTALLED CENTER WING UPPER SURFACE OTBD SLAT PANEL ANGLE REF STASA EA 011-5310-0SDR IPXA2M75513Access Panel · crackedINSPECTION TYPE: 4C, NR 2 PYLON ACCESS PANEL 363PL, REAR SPAR LOWER PANEL CRACKED AT LT FWD UPPER CORNER JUST BELOW NR 3 BANJO FITTING. REPAIRED NR 2 PYLON ACCESS 363PL, REAR SPAR LOWER PANEL AT LT FWD UPPER CORNER JUST BELOW NR 3 BANJO FITTING REF STASA EA 0SDR IPXA2M75454Longeron Splice · corrodedINSPECTION TYPE: 4C LONGERON 48R SPLICE FITTING CORRODED AT STA 1531/5-123. REMOVED, FABRICATED AND INSTALLED LONGERON 48R SPLICE FITTING AT STA. 1531/5-123 REF DWG A5A7125, SRM 51-33-01, PAGE 1 AND 30, SRM 51-31-01, PAGE 1.SDR IPXA12M75175Web · crackedINSPECTION TYPE: 4C, R3 DOOR AFT JAMB LOWER WEB LIGHTNING HOLE CRACKED. REPAIRED R3 DOOR AFT JAMB LOWER WEB LIGHTNING HOLE REF SRM 53-40-15, REPAIR 3, FIG 201.SDR IPXA2M75297Skin · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E SKIN IS CRACKED AT INBD FWD CORNER OF PANEL 619CB. REPAIRED RT WING FIXED L/E SKIN AT INBD FWD CORNER OF PANEL 619CB REF SRM 57-40-02, REPAIR 7, FIG 201.SDR IPXA2M75284Skin · crackedINSPECTION TYPE:4C, RT WING FIXED L/E SKIN IS CRACKED AT NR 13 SLAT TRACK CUT-OUT. REPAIRED RT WING FIXED L/E SLAT NR 13 SLAT TRACK CUT OUT REF SRM 57- 40-02, REPAIR 7, FIG 201.SDR IPXA2M75196Longeron Splice · crackedINSPECTION TYPE:4C, SPLICE FITTING CRACKED ON FWD END AT L34R AND BS 1531/5-123. REPLACED SPLICE FITTING AT STA 1531/5-123 AND L34R REF SRM 51-33- 01, PG 30 AND 45.SDR IPXA12M75323Doubler · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AROUND FASTENERS AT STA XOS 667. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER REF EO MD11-5730-42916-D.SDR IPXA12M75322Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT STA XOS636. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS636 REF MD11-5730-42916-D.SDR IPXA12M75316Former · crackedINSPECTION TYPE:4C, LT WING FIXED L/E SUPPORT FORMER CRACKED BETWEEN FASTENERS AT APPX STA XOR 917. REMOVED, FABRICATED AND INSTALLED SUPPORT FORMER AT LT WING FIXED L/E AT STA XOR 917 REF SRM 51-31-01 PG 1 AND SRM 51-35-01.SDR IPXA2M75311Former · crackedINSPECTION TYPE:4C, LT WING FIXED L/E FORMER CRACKED AT AFT END XOR 377. REMOVED, FABRICATED AND INSTALLED LT WING FIXED L/E FORMER IAW DWG ARB1162, SRM 51-35-01, SRM 51-33-01.SDR IPXA2M75503Longeron Fitting · corrodedINSPECTION TYPE: 4C, LONGERON 52 END FITTING HAS EXFOLIATION CORROSSION ON LT SIDE AT FS 11 29/6-90. REMOVED, FABRICATED AND INSTALLED LONGERON 52 END FITTING AT STA 1129/ 6-90 REF STASA EA 011-5310-01-A4223 REV I/R AND EO MD11-5310-48626-A.SDR IPXA2M75442Fitting · damagedINSPECTION TYPE: 4C, FOUND LOOSE FASTENERS ON LT NR 4 BANJO FITTING TO PYLON CARRY-THRU CAP. REPAIRED 6EA VERTICAL STAB AFT SPAR LT NR 4 BANJO FITTING FASTENER HOLES COMMON TO THE NR 2 PYLON CARRY-THRU CAP ATTACHMENT REF EO MD11-553 0-46641-A APPROX B AND D.SDR IPXA2M75441Fitting · damagedINSPECTION TYPE: 4C, FOUND LOOSE FASTENERS ON NR 4 BANJO FITTING TO PYLON CARRY THRU CAP. REPAIRED VERTICAL STAB AFT SPAR RT NR 4 BANJO FITTING FASTENER HOLES COMMON TO THE NR 2 PYLON CARRY THRU CAP ATTACHMENT REF EO MD11-5530-46641-A APPX C AND E.SDR IPXA12M75382Floor Panel · puncturedINSPECTION TYPE: 4C, MAIN DECK FLOOR PANEL DENTED AND PUNCTURED. R & R FLOOR PANEL REF AMM 53-21-09-400-801.SDR IPXA12M75377Longeron · corrodedINSPECTION TYPE: 4C, LONGERON 52, EXFOLIATED BETWEEN STA 1129/6-73 AND 1129/6-90 ON LT, RT AND BOTTOM SIDES OF FLANGES. REPAIRED LONGERON 52 BETWEEN STA 1129/6-73 AND STA 1129/6-90 BY FABRICATION AND PART REPLACEMENT REF DWG A6A7027, SRM 51-33-01, PAGE 1 AND SDR FDEA201208283188Unknown · odorIN CLIMB TO ABOUT 12,000 FT AND DESCENT BELOW 17,000 FT THERE IS AN ACRID ODOR IN COCKPIT. PERFORMED OPS CHECK OF PACK OPERATION, FLIGHT COPMARTMENT HEATING AND COOLING IN REF TO AMM 21-40-00 AND 21-50-00, NO DEFECTS NOTED AND NO ODOR PRESENT. UNABLE TO DUSDR FDEA201208273189Charger · malfunctionedAFTER TAKEOFF RECEIVED LEVEL 2 BATTERY DISCHARGING ALERT REFERRED TO QRH RETURNED TO DEPARTURE. DURING DECENT ALERT WENT AWAY. SAME ALERT APPEARED ON FINAL FOR 15-30 SECONDS BUT WENT AWAY PRIOR TO TOUCHDOWN. R & R BOTH MAIN SHIPS BATTERIES. REF AMM 24-34SDR IPXA2M75079Lamp · inoperativeONE EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-12-15.SDR FDEA201208253167Latch · inoperativeEMERGENCY O2 MASK DOOR WILL NOT STAY LATCHED IN LAVATORY. RESET LOCK AND RESECURED PANEL IAW SMP.SDR FDEA201208233138Seat Track · wornMAIN DECK SEAT TRACK WORN AT BS 1531 X=-8. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201208223101Fuel Cell · corrodedMAIN DECK AUXILLIARY TANK UPPER SURFACE AT STA 1229, X=-85 TO -95 FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REV.50 ORIGINAL THICKNESS : 0.160 INCH, MATERIAL REMAINED: 0.106 INCH, MATERIAL REMOVED: 0.054 INCH FOUND EXCEEDED LIMIT AS PER SRM
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