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 FDEA201807171750Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.351", UPPER: 0.003", LOWER: 0.003", REMAINING THICKNESS USDR FDEA201807171749Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.2245", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZSDR FDEA201807171748Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.227", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZESDR FDEA201807171747Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.434", MATERIAL REMOVED FWD FACE: 0.008", AFT FACE: 0.009",SDR FDEA201807171746Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS 0.425", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.417"SDR FDEA201807171745Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.720", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABSDR FDEA201807171744Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABSDR FDEA201807171743Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.376", LOWER: 0.373", MATERIAL REMOVED UPPER: 0.003", LOWER: 0.003", REMASDR FDEA201807171742Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLSDR FDEA201807171741Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLE DIA 1.2SDR FDEA201807171740Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.650", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE HOLE SDR FDEA201807171739Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 2.3159", FINAL HOLE DIA 2.321", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSDR FDEA201807171738Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220SDR FDEA201807171737Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220" . OVERSDR FDEA201807171736Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE FOUND WITH CORROSION. LOWER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.384", FINAL HOLE DIA 0.409", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZSDR FDEA201807171735Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE UPPER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.384", FINAL HOLE DIAMETER: 0.409", MAXIMUM ALLOWABLE HOLE DIAMETER: 0.3SDR FDEA201807171734Pivot · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER: 0.5SDR FDEA201807171733Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER:SDR FDEA201807171732Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.627" MAXIMUM ALLOWABLE SDR FDEA201807171731Pivot · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION AT LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 2.310". FINAL HOLE DIAMETER: 2.354". MAXIMUSDR FDEA201807171730Hinge Bracket · wornRT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. RT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.500" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CSDR FDEA201807171729Hinge Bracket · wornLT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. LT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.526" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CSDR IPXA2018072031703Battery Pack · dischargedEMERGENCY LT TEST FND BAT 1 LO MSG. CHANGED BATTERY PACK IAW AMM 33-51-01 PB 401 REL 91.00. OPS TEST IAW AMM 33-51-01 PB SUCCESSFUL.SDR FDEA2018071641711Hinge Bracket · corrodedRT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.255", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSSDR FDEA2018071641710Hinge Bracket · corrodedRT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.290", FINAL HOLE DIA 1.326", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSDR FDEA2018071641709Hinge Bracket · corrodedLT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.254", FINAL HOLE DIA 1.2835", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVESDR FDEA2018071641708Hinge Bracket · corrodedLT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.1885", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVSDR FDEA2018071641707Skin · corrodedUPPER AFT RUDDER ASSEMBLY LT UPPER SKIN FOUND WITH CORROSION AT APPROX ZAR 554.920. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS AS PER SRM 55-00-00-2R FIG 202. ORIGINAL THK 0.016", THK REMOVED 0.015", THK REMAINED 0.001". CARRIEDSDR IPXA2018071631637Schrader Valve · defectiveFOUND R1 DOOR SIDE PNEUMATIC BOTTLE PRESSURE LOW. R&R SCHRADER VALVE PER IPC 52-11-33-01 P/N ON/OFF: 238126. SERVICED AIR PRESS CHK COND SATIS PER AMM 12-25-04/301 AND 52-11-04.SDR IPXA2018080132251Tee Fitting · crackedINSPECTION TYPE:3C, CENTER AUX TANK BULKHEAD SUPPORT TEE FITTING IS CRACKED AT STA 1156 AND X=46. REMOVED, FABRICATED AND REPLACED CENTER AUX TANK BULKHEAD SUPPORT TEE FITTING AT STA 1156 AND X=46 IAW DWG APB7351 AND SRM 51-33-01. (MINOR)SDR FDEA201807121697Life Vest · missingCREW REPORTED , CAPTS SEAT HAS MISSING LIFE PRESERVER. LIFE VEST, P/N 63600-105 C/7147186. INSTALLED NEW LIFE VEST PER MM 25-64-01-2.SDR FDEA201807121696Brake · delaminatedNORMAL LANDING USING MEDIUM AUTOBRAKES. AFTER FIVE MINUTES BRAKE DIFF TEMP ILLUMINATED. BRAKE NR 1, 158 DEGREES. BRAKE NR 2, 342 DEGREES. R&R NR 1 MAIN BRAKE PER MM 32-43-20-4. REMOVED AND REPLACED DEFECTIVE BRAKE.SDR FDEA201807121675Skin · cracked1 EA FASTENER HOLE NR 9 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 9 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR SDR FDEA201807121674Skin · cracked1 EA FASTENER HOLE NR 15 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 15 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAISDR FDEA201807121673Skin · cracked1 EA FASTENER HOLE NR 32 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 32 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAISDR FDEA201807121672Skin · cracked1 EA FASTENER HOLE NR 36 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 36 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAISDR FDEA201807121671Skin · cracked1 EA FASTENER HOLE NR 6 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 6 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR SDR FDEA201807121670Skin · cracked1 EA FASTENER HOLE NR 7 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 7 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIRSDR FDEA201807121669Skin · cracked1 EA FASTENER HOLE NR 27 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 27 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPASDR FDEA201807121668Seat Track · damagedCABIN LT STA 1521, X=8.5 SEAT TRACK CROWN FOUND DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-83 TO STA 5-123, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807121667Seat Track · damagedCABIN, RT STA 1541 - 1562, X=-8.5 SEAT TRACK CROWN FOUND DAMAGED. DAMAGED SEAT TRACK CROWN REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1591, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018071331609Strap · brokenFO'S ESCAPE LINE SECURING STRAP BROKEN. R&R ROPE STRAP ASSY PER MM 25-60-01-000-801.SDR IPXA2018081302651Stringer · crackedLEFT WING UPPER STRINGER 14 WAS CRACKED, BETWEEN XORS 506 AND XORS 538.49. REPAIRED THE STRINGER IAW EA 011-5710-01-A7374, REV IR, AND EO MD11-5310-69511-A. MAJOR.SDR IPXA2018081302650Stringer · crackedRIGHT WING STRINGER 13 WAS CRACKED BETWEEN XORS 562 AND XORS 592.6. REPAIRED THE STRINGER IAW EA 011-5710-01-A7373, REV IR, AND EO MD11-5310-69509-A. MAJOR.SDR IPXA2018081312669Stringer · crackedRIGHT WING STRINGER 43, XORS 298.5 WAS CRACKED. REPAIRED THE STRINGER IAW EA 011-5710-01-A7372-IR, AND EO MD11-5710-69524-A.SDR IPXA2018081312668Stringer · crackedLEFT OUTER WING STRINGER 43, XORS 298.5 WAS CRACKED. REPAIRED THE STRINGER IAW EA 011-5710-01-A7371-IR, AND EO MD11-5710-69522-A.SDR IPXA2018081312667Stringer · crackedLEFT WING STRINGER 15 BETWEEN XORS 433 AND XORS 455 WAS CRACKED. REPAIRED THE STRINGER IAW EA 011-5710-01-A7419-IR, AND EO MD11-5710-69541-A.SDR IPXA2018081032645Door · cutAPU DOOR INNER SKIN HAD A LARGE CUT. REPAIRED APU BAY DOOR INNER SKIN AT BS 2070, LB 0 TO LBL 8.5 IAW EA 011-5240-01-A7380, REV IR, AND EO MD11-5240-69526-A.SDR IPXA2018080832588Intercostal · crackedNR 2 PYLON CARRY THRU, REAR SPAR INTERCOSTAL WAS CRACKED, YID. 375, XID 71 AND ZID -7.1. REPAIRED THE SPAR INTERCOSTAL IAW SRM 55-30-02, REPAIR 7, FIG 204. MAJOR.SDR IPXA2018080832587Stringer · crackedLEFT WING STRINGER 13 WAS CRACKED, BETWEEN XORS 562 AND 592. REPAIRED THE STRINGER IAW SRM 57-00-03, REPAIR 5, FIG 202. MAJOR
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