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 FDEA201307081499Frame · dentedLEFT FRAME BS 1701, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116SDR FDEA201307081498Frame · dentedLEFT FRAME BS 1681, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307081497Frame · dentedLEFT FRAME BS 1661, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307081503Hinge Bracket · corrodedRT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT, OTBD LUG BORE FOUND CORRODED. LUG BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 10. REPAIR ACCOMPLISHED IAW EA 1-5750-T0301169A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307081496Frame · crackedFRAME BS 1641, LONGERON 12L FOUND CRACKED. REPAIRED IAW EA 1-5310-T0301233, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307081494Trunnion · crackedNOSE LANDING GEAR LEFT TRUNNION FITTING CRACKED. REPAIRED IAW SRM 53-10-14, FIGURE 202, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 116.SDR FDEA201307081493Vane · delaminatedRT WING FLAP VANE LOWER SURFACE FOUND DELAMINATED. FLAP VANE ASSY R & R IAW AMM 27-50-22-4, REV 76.1. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 76.1. CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.SDR IPXA3M79292Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT BEADED DOUBLER FOUND WITH CRACKS AT XOS 704. 2851. REPAIRED RT WING FIXED L/E COMPT BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA3M79510Brace · crackedINSPECTION TYPE:1C, RT WING T/E VERTICAL BRACE CRACKED AT NR 1 SPOILER INBD ATTACH POINT. REPAIRED IAW EA 011-5700-01-A4792, REV I/R, & EO MD11-5710-51583-A.SDR IPXA201307229427Longeron Fitting · crackedINSPECTION TYPE:1C, LONGERON 51R END FITTING CRACKED AT STA 6-78. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L51R END FITTING AT STA 6-78. (MINOR)SDR IPXA3M79317Skin · dentedINSPECTION TYPE:1C, RT INBD FLAP UPPER SKIN DENTED/GOUGED. REPAIRED RH IB FLAP UPPER SKIN AT STA. XIFH165 PER MD11 SRM 57-00-01 REPAIR 1 FIG.201 SHT 3 (MAJOR)SDR FDEA201307061485Button · inoperativeDURING PRE DEPARTURE CHECK, R1 DOOR EVACUATION SLIDE REMOTE PRESS -TO-TEST PUSH BUTTON INOPERATIVE. REPLACED LAMPS WITH PROPER BULB 368 PER SMP OPS CHECKED GOOD.SDR IPXA201307229418Trunnion · crackedINSPECTION TYPE: 1C, APPROX 1.4 INCH LONG CRACK AT TYPICAL CRACK LOCATION ON LT NLG TRUNNION FITTING AS SHOW IN SRM 53-10-14, REPAIR 2, FIG 201. ACCOMPLISHED REPAIR IAW SRM 53-10-14, REPAIR 2, FIG 202.SDR IPXA13M79196Bleed Valve · inoperativeAFTER SELECTING ANTI-ICE ON ALL THREE ENGINES, WINGS, & TAIL, HAD MULTIPLE MALFUNCTIONS, STARTED WITH AVIONICS FAN OVERRIDE, BLEEDS 1 & 2 OFF, DUCTS 1 & 2 OFF CABIN IN FLOW LOW. REVERSED DMP 49-51-2-2, PERFORMED APU RTS OPS BITE TEST. TEST OK MM 49-00-00-SDR FDEA201307041478Transmitter · inoperativeSHORTLY AFTER BEGINNING TAKEOFF ROLL, NR 1 FUEL FLOW SHOWED AMBER X. REJECTED TAKEOFF AT ABOUT 60 TO 70 KTS. FUEL FLOW INDICATING NORMAL AGAIN WHILE TURNING OFF RUNWAY. TROUBLESHOOTING FOUND FUEL LEAK FROM THE FUEL FLOW TRANSMITTER. R & R NE 1 ENGINE FUELSDR FDEA201307041475Hydraulic System · leakingON DESCENT, LOSS OF NR 2 HYD SYS. IAW CREW DEBRIEF, FLIGHT LASTED 30 MORE MINS AFTER RECEIVING NR 2 HYD SYS FAIL ALERT. HYD FLUID ALL OVER THE TAIL UP TO THE NR 2 ENG COWL. HYD MANIFOLD FILTERS R & R AND LEAK CHECKED OK. LEAK CHECKED OF NEW SECTION OF HSDR FDEA201307021457Skin · delaminatedRT OTBD AILERON T/E WEDGE FOUND DELAMINATED AS MARKED AT INBD CORNER BETWEEN XOA 848.3 TO XOA 866. REPAIRED IAW EA 1-5750-T0300983A, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 116.SDR FDEA201307021456Vane · delaminatedRT INBD T/E FLAP VANE FOUND DELAMINATION AT LOWER SURFACE, BETWEEN INBD TRACK AND CENTER TRACK AREA. STATION XIFH 141.375 TO XIFH 183.300. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP VANE AS PER AMM 27-50-22-4, REV. 76.1. CARRIED OUT FLAP VANE ADJUSTMENT TSDR FDEA201307021466Skin · separatedRIGHT WING INBD AILERON T/E FOUND SKIN SEPARATED. REPAIRED RIGHT WING INBOARD AILERON TRAILING EDGE AS PER SRM 57- 50-02 REPAIR 3 FIGURE 201 REVISION 52 AND EA 1-5750-T0301032 PART 1. REPAIR CLASSIFIED CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201307011428Skin · delaminatedLEFT WING OTBD FLAP LOWER SURFACE T/E FOUND DELAMINATED XOFH 681.500 TO XOFH 689.500. REPAIRED IAW EA 1-5750-T0300982. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.SDR FDEA201307011427Skin · delaminatedLEFT WING OTBD FLAP LOWER SURFACE T/E FOUND DELAMINATED XOFH 553.00 TO XOFH 568.00. REPAIRED IAW EA 1-5750-T0300982. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 116.SDR FDEA201307011426Skin · delaminatedRIGHT WING OTBD FLAP LOWER SURFACE FOUND DELAMINATED XOFH 673.542 TO XOFH 667.542. REPAIRED IAW EA 1-5750-T0300985 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.SDR FDEA201307011425Skin · delaminatedRIGHT WING OTBD FLAP T/E, LOWER SURFACE FOUND DELAMINATED XOFH 527.690 TO XOFH 552.690. REPAIRED IAW EA 1-5750-T0300985, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 116.SDR FDEA201307011424Skin · delaminatedRIGHT WING OTBD FLAP T/E, UPPER SURFACE FOUND DELAMINATED AT XOFH 524.690 TO XOFH 554.690. REPAIRED IAW EA 1-5750-T0300985, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.SDR IPXA13M79141Tire · low pressureEMERGENCY DECLARED - LEVEL 1 TIRE PRESSURE LOW FOLLOWED BY TIRE FAIL MESSAGE. REPLACED FLAT LT NOSE WHEEL ASSY IAW AMM 32-42-01.SDR FDEA201306301421Structure · corrodedRT WING OTBD FLAP INBD FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION.SDR FDEA201306291415Battery · failedFOUND R1 ENTRY DOOR SLIDE REMOTE PRESSURE INDICATOR PRESS TO TEST LIGHT OUT. REPLACED REMOTE PRESSURE INDICATOR BATTERIES REF AMM 25-61-04-4. OPS CHECKS GOOD REF AMM 25-61-04-5.SDR FDEA201306271407Frame · chafedMAIN DECK CARGO COMPARTMENT BS 535, LONGERON NR 19L TO NR 21L AT YOKE ATTACHED FITTING EXISTING REPAIR OUTER ANGLE FOUND CHAFED. REMOVED AND REPLACED IAW SRM 53-20-07, FIGURE 202, REPAIR 1, REV. 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REV 116.SDR FDEA201306251392Doubler · crackedLT WING L/E LOWER COMPARTMENT, CRACK FOUND ON BEADED DOUBLER STIFFENER, XOS= 668 AND ZOS 35, OTBD OF SLAT TRACK NR 10. IAW DWG ARB3954, REV K AND SRM 51-33-01, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201306251390Skin · dentedCENTER CARGO DOOR CUTOUT LOWER AFT FOUND DENTED BS 1781 RT BETWEEN LONGERON 40R TO 41R. REPAIRED IAW SRM 53-00-15, REPAIR 8, FIG. 202, REV. 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV. 116. TO CARRY OUT INSPECTION AS PER SRM 53-00-15, TABLE 201, FSDR FDEA201306251389Beam · corrodedCENTER WHEEL WELL RT DIAGONAL BOOT STRAP HAS CORROSION. BS 1461 TO 1490, WL 100. REMOVED AND REPLACED PER SRM 51-31-01, REV. 52. NEW BOOT STRAP FABRICATED PER EA 1-5310-T0300908, PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV. 116.SDR FDEA201306251388Beam · corrodedCENTER WHEEL WELL LT DIAGONAL BOOT STRAP HAS CORROSION BS 1461 TO 1490, WL 100. REMOVED AND REPLACED IAW SRM 51-31-01, REV. 52. STRAP FABRICATED IAW EA 1-5310- T0300892, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 116.SDR FDEA201306251396Relay · burnedJUST PRIOR TO PUSH BACK, APU AUTO SHUTDOWN AND "BUS LT EMER DC OFF" MESSAGE DISPLAYED ON EAD AND SD. INTERROGATED EPCU CURRENT FAULT AND FAULTS REVIEW NO FAULTS NOTED, CHECKED C/B'S AND RCCB FOUND NO FAULTS T/S IAW FIM 24-30-04-00, STEP 1. R & R R2-5154 (CSDR FDEA201306241384Bulkhead Web · damagedNR 1 PYLON YN 286 BULKHEAD DAMAGED. REPAIRED IAW EA1-5450-81823B PART 2. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201306241383Bulkhead Web · damagedNR 1 PYLON YN 286 BULKHEAD DAMAGED. REPAIRED IAW EA 1-5450-81823B PART 2. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 116SDR FDEA201306241382Bulkhead Web · damagedNR 1 PYLON YN 286 BULKHEAD DAMAGED. REPAIRED.SDR FDEA201306241379Skin · crackedTEN FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS= 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFIED SDR FDEA201306241378Skin · crackedEIGHT FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS. DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ONE LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIRSDR IPXA13M79109Vane · delaminatedINSPECTION TYPE:4C, LT INBD FLAP VANE LOWER SURFACE SKIN DELAMINATED AT STA XIFH198, 21" FROM T/E REPAIRED LT INBD FLAP VANE SKIN IAW SRM 57-50-80, REPAIR 2, FIG 201 (MAJOR).SDR IPXA3M79091Skin · damagedINSPECTION TYPE:1C, EXISTING REPAIR DOUBLER DAMAGED IN LT WING FIXED L/E INTERIOR BETWEEN XOS 667 - 673. REPLACED BEADED DOUBLER REPAIR IN LT WING L/E INTERIOR BETWEEN XOS 667-673 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)SDR FDEA201306211365Frame · crackedLT WING INBD FLAP INBD FAIRING FRAME, AT YIFH 57 CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-31-01 REVISION 52 & EO 1-5100-7-5001 B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116SDR FDEA201306211363Fitting · corrodedLEFT WING INBD FLAP DRIVE ARM SUPPORT BORE FOUND CORRODED. BORE REWORKED IAW SRM 51-21-01 REVISION 52 REPAIRED IAW EA 1-5750-T0300933A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306211362Hinge · corrodedRIGHT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT OTBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300874 B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306211361Hinge · corrodedRIGHT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300874 B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306211360Hinge Bracket · corrodedLEFT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBOARD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300889. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306211359Hinge Bracket · corrodedLT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT OTBD LUG, BORE FOUND CORRODED. BORE REWORKED FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED IAW EA 1-5750-T0300889. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306211366Floor Skin · misrepairedCOCKPIT FLOOR UNDERNEATH OBSERVER SEAT AT BS 360 MISREPAIRED. REPAIRED IAW SRM 53-10-51 FIGURE 201 REPAIR 1 REVISION 52 & EO 1-5100-7-5001 B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201354Frame · misrepairedFUSELAGE FRAME AT BS 1921, LONGERON 51R MISREPAIRED. REPAIRED IAW EA1-5310-T0300934 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201353Skin · misrepairedLEFT WING INBD FLAP BETWEEN XIFH 159.300 TO XIFH 165.300 MISREPAIRED. REPAIRED IAW EA 1-5750-166138. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201306201352Skin · misrepairedRUDDER SKIN MISREPAIRED. REPAIRED IAW EA 1-5540-T0300978. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.
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