Mcdonnell Douglas MD-11
Service difficulty reports · 7,956
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 = 'MD11' 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 = 'MD11' 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 WRLA2009071Seal · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LEFT WING T/E BEAM SEAL LAND Y=1474 Z=-100. REPLACE THIS CRACK SEAL LAND IAW SRM 51-35-01 AND 51-33-01 VOL 2 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA2009070Rib · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON RT RIB OF RT MLG GR JAMB INSTALLED AT Y-1474 Z=-100. REMOVE RT RIB OF RT MLG JAMB PER SRM 51-33-01 VOL 2 REV 40, INSTALLED NEW RIB PER MD-11 SRM 31-33-01 VOL 2 REV 40, JOB COMPLETED AS NORMAL.SDR WRLA2009069Seat Track · corrodedDURING C3 CHECK IN TPE INSPECTION FOUND CABIN SEAT TRACK HAD CORROSION AT STA 846 X=43. REPAIRED THIS CORRODED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA2009068Vane · debondedDURING C3 CHECK IN TPE INSPECTION FOUND LT INBOARD FLAP VANE HAS DISBOND AT XIFH196 AND XIFH249. PER AMM 27-50-22-000-081 & 27-50-24-000-081 REV 63. REMOVED THIS DISBONED FLAP VANE, REPAIRED THE FLAP VANE AS JOB CARD ATTACHMENT SHEET 079554, PER AMM 27-50-22SDR WRLA2009067Wedge · debondedDURING C3 CHECK IN TPE INSPECTION FOUND EGAT LT OUTBOARD AILERON WEDGE DISBOND AT XOA 842. REMOVE AND CLEANUP AREA. REPAIR THIS WEDGE PER DRAWING SG11570003. CHECK REPAIRED AREA WAS SATISFIED, CALCULATED THE REWORK BALANCE MOMENT IS 66.65 LB-IN PER SRM 57-5SDR WRLA2009063Fitting · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON 1EA RT CLIP OD CAC COMPARTMENT. REMOVE THIS DAMAGED CLIP PER SRM 51-33-01 VOL 2 REV 40, FABRICATE THIS CLIP PER EGAT EI W2009P53B-354 REV 00, INSTALLED THIS CLIP PER SRM 51-33-01 VOL 2 REV 40, AND JOB COMPLETEDSDR WRLA2009065Door · damagedUPON LANDING, MX FOUND NR 3 ENG REVERSER DOOR OPEN, ON FURTHER INSPECTION FOUND DOOR DAMAGED (BENT ALONG RIVET LINE OF HINGE). REMOVED AND REPLACED T/R & THEREFORE NR 3 ENG REVERSER DOOR.SDR WRLA2009061Skin · dentedDURING A-2 CHECK IN ATL INSPECTION FOUND C-2 CARGO DOOR CUTOUT AFT SKIN HAS VERTICAL DENT 22 INCHES LONG AT STA 1781 STR 40-42. DAMAGED SKIN CUT OUT AND REPAIRED IAW ERA 473349-14 AND PRI REV 4 WORLD ERA 09-53-362. APPROVAL ON FAR FORM 8100.SDR WRLA2009060Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND NR 3 ENGINE PYLON PRECOOLER LT SIDE UPPER STRUCTURE ANGLE CRACKED (REF EGAT N/R U05114). REPLACED WITH NEW PART 1EA ON NR 3 ENGINE PRECOOLER LT SIDE UPPER IAW MD11 SRM VOL II 51-35-01 REV 40.SDR WRLA2009058Stiffener · crackedDURING C-CHECK INSPECTION, FOUND CRACK ON STIFFENER ON RIGHT MLG DOOR AFT O/B JAMB ASSY Y=1472 X=115.1. REPLACED WITH NEW STIFFENER 1EA PER SRM VOL 2 51-35-01 REV 40.SDR WRLA2009059Stiffener · crackedDURING C-CHECK IN TPE INSPECTION FOUND LT MAIN GEAR W/W AFT LOWER SIDE HAS STIFFENER CRACKED TOTAL 1 EA AT STA Y=1461. REPLACED THE STIFFENER 2EA IAW SRM VOL 2 51-35-01 REV 40.SDR WRLA2009055Fitting · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT WING T/E LOWER PANEL I/B SIDE CLIP AT XOHF453. REF EGAT N/R U05059. REMOVED AND REPLACED THE SUPPORT BRACKET AT O/B FLAP I/B SIDE. FABRICATED SUPPORT PER EGAT EI W2009P57B-078 AND SRM VOL 2 51-35-01 REV 40SDR WRLA2009054Support Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND LT AFTER BODY INTERCOSTAL APU DRAIN CAN SUPPORT ANGLE CRACKED AT Y: 2080 (REF EGAT N/R U05033). REPLACED WITH NEW ANGLE IAW SRM 51-35-01.SDR WRLA2009051Doubler · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER RT WING FIXED LEADING EDGE AT STA XOS605 (REF EGAT N/R U05122). REPLACE WITH NEW DOUBLER ON RT WING FIXED L/E AT XOS605 IAW SRM VOL 2 51-33-01 REV 40 AND EGAT EI W2009P57B-076.SDR WRLA2009041Hinge Bracket · brokenDURING C-CHECK IN TPE INSPECTION FOUND LT O/B FLAP INBOARD FORWARD HINGE BRACKET BROKEN. REPLACED WITH NEW BRACKET IAW SRM VOL 2 51-31-01 REV 40.SDR WRLA2009048Support Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND PANEL 15AZ - LT STA 463 X:+10 ANGLE CRACKED FORWARD AVIONICS COMPARTMENT. (REF EGAT N/R U05132). REPEAT INSPECTION AT AVIONICS COMP STA 463 X=10, NO CRACK FOUND. REF IAW SRM VOL II 51-50-00 REV 40. REF EGAT N/R U05132.SDR WRLA2009039Support Bracket · crackedDURING C-CHECK IN TPE INSPECTION FOUND RT FUSELAGE BODY FAIRING 154GB PANEL SUPPORT BRACKET CRACKED AT STA 1521. REPLACED WITH NEW FABRICATED PART IAW EGAT EI NO W2009P53B-081 REV 0.SDR WRLA2009037Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 2 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 2 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94 - JOB CARD 004589. REINSTALLED NR 2 LT SSDR WRLA2009036Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 2 RT SPOILER PANEL UPPER SURFACE. REMOVED NR 2 RT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PANEL ON NR 2 RT PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. REINSTALLED NR 2 RT SSDR WRLA2009035Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 3 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 3 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94 - JOB CARD 004587. RE-INSTALLED NR 3 LT SDR WRLA2009034Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 3 RT SPOILER PANEL UPPER SURFACE. REMOVED PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED SPOILER PANEL PER AMM 27-60-30-400-801.SDR WRLA2009033Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 4 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 4 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED PANEL PER AMM 27-60-30-400SDR WRLA2009032Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 4 RT SPOILER PANEL UPPER SURFACE. REMOVED NR 4 RT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED PANEL PER AMM 27-60-30-400-801.SDR WRLA2009031Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 5 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 5 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED NR 5 LT SPOILER PANEL PER SDR WRLA2009030Skin · damagedDURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 5 RT SPOILER PANEL UPPER SURFACE. REMOVED NR 5 RT SPOILER PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN SURFACE SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94 ATTACHING JOB CARD 004581. SDR WRLA2009044Tee Fitting · crackedDURING C-CHECK IN TPE INSPECTION FOUND LT WING I/B AILERON LEADING EDGE O/B SIDE HAD TEE CHORD CRACKED AT XORS 412.369. REPLACED WITH NEW TEE CHORD IAW SRM VOL II 51-33-01 REV 40.
SDR WRLA2009045Tee Fitting · crackedDURING C-CHECK IN TPE INSPECTION FOUND TEE CHORD AT RT WING OUTBOARD FIXED T/E AT STA 412.329 NEAR I/B AILERON L/E LOCKOUT CRACKED (REF EGAT N/R U5037). REPLACED THE TEE CHORD ON RT INBOARD AILERON FIXED T/E AT STA 412.329 IAW MD-11 SRM VOL II 51-33-01 REV 40SDR WRLA2009046Support Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND PANEL SUPPORT ANGLE FOR RT WING TO BODY UPPER FAIRING CRACKED AT STA 1341 L31L (REF EGAT N/R U05040). REMOVE SUPPORT AT LT WING TO BODY FAIRING STA Y=1431 L31L PER SRM 51-35-01 REV 40 MD-11 VOL II. REPEAT INSPECTION ANDSDR WRLA2009047Support Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND PANEL SUPPORT ANGLE FOR RT WING TO BODY UPPER FAIRING CRACKED AT STA 1341 L31R (REF EGAT N/R U05041). REMOVE SUPPORT AT RT WING TO BODY FAIRING STA Y=1341 L31R IAW MD SRM 51-35-01 VOL II REV. 40. REPEAT INSPECTION AND ASDR WRLA2009052Rib · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT WING FIXED L/E PANEL RIB AT STA XORS 441. REPAIRED CRACK AREA IAW SRM 57-00-01 FIG 11 REV 40.SDR WRLA2009049Support · crackedDURING C-CHECK IN TPE INSPECTION FOUND SUPPORT CRACKED BETWEEN LT FWD AND AFT AIR CONDITIONING BAYS AT STA Y =533 L33L. REF EGAT N/R U05004. REPAIRED CRACKED SUPPORT AT LEFT AND AFT AIR CONDITIONING BAY IAW SRM VOL I 53-00-01 FIG 3 REV 40.SDR WRLA2009050Support Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND AVIONICS COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT STA 420 PNL 1152AZ. REF EGAT N/R U05049. REPAIRED CRACK AREA IAW SRM VOL1 53-00-01 FIG 10 REV 40.SDR WRLA2009038Channel · crackedDURING C-CHECK IN TPE INSPECTION FOUND AFT FUSELAGE BODY STATION YID = 310.3 X = 0.00 CHANNEL CRACK (REF EGAT N/R U05126). REPAIRED CHANNEL CRACK AREA AT BODY STA YID=310.3 X=0.00 IAW SRM VOL1 53-00-01 FIG 3 REV 40.SDR WRLA2009053Hinge Bracket · brokenDURING C-CHECK IN TPE INSPECTION FOUND RT O/B FLAP I/B FORWARD FAIRING HINGE BRACKET BROKEN (REF EGAT N/R U05125). REPLACED BRACKET AT RT O/B FLAP I/B FWD FAIRING HINGE IAW SRM VOL 2 51-35-01 REV 40.SDR WRLA2009043Door · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK ON RT MLG DOOR AT FWD END (REF EGAT N/R U050007). REPAIRED RT FLIPPER DOOR CRACK AREA IAW SRM VOL 1 52-10-00 FIG 18 REV 40.SDR WRLA2009042Door · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT MLG FLIPPER DOOR AT FWD EDGE. REPAIRED CRACKED AREA IAW SRM VOL 1 52-10-00 FIG 18 REV 40.SDR WRLA2009040Intercostal · crackedDURING C-CHECK IN TPE INSPECTION FOUND LT FORWARD AIR CONDITIONING ACCESS DOOR HAS CRACKED INTERCOSTAL (INTERNAL) AT CENTER LINE UPPER END (REF EGAT N/R U05002). REPLACED WITH NEW INTERCOSTAL IAW SRM 51-35-01 VOL 2 REV 40.SDR WRLA2009057Support Fitting · corrodedDURING C-CHECK IN TPE INSPECTION FOUND LT MLG RETRACT ACTUATOR SUPPORT FITTING LOWER SIDE CORROSION. FOUND DURING HEAVY LANDING INSP AS PER MANUFACTURER LETTER. BOLT HOLES CORRODED 3EA. REMOVED LT MLG ACTUATOR ATTACH FITTING PER AMM 32-33-20-000-301 REV 63 SDR WRLA2009056Support Fitting · corrodedDURING C-CHECK IN TPE INSPECTION FOUND RT MLG RETRACT ACTUATOR SUPPORT FITTING LOWER SIDE CORROSION. FOUND DURING HEAVY LANDING INSP AS PER MANUFACTURER LETTER. BOLT HOLES CORRODED. REMOVED RT MLG ACTUATOR ATTACH FITTING PER AMM 32-33-20-000-301 REV 63 DRAWSDR WRLA2009029Longeron Splice · crackedDURING C-CHECK INSPECTION IN TPE - FOUND AFT CARGO LONGERON SPLICE CRACKED AT STA 1521-1541, 5-44L, 5-51L & 5-47R. FABRICATED LONGERON SPLICE, REPLACED LONGERON SPLICE IAW SRM 51-33-01 VOL 2.SDR WRLA2009028Longeron Splice · crackedDURING C-CHECK INSPECTION IN TPE - FOUND AFT CARGO STA 5-113, 5-38L, & 5-37R LONGERON SPLICE CRACKED. REMOVED CRACKED SPLICES IAW SRM VOL 2 51-33-01. FABRICATED SPLICES PER EI W2009P53B-086. INSTALLED NEW SPLICES PER SRM 51-83-01 REV 40.SDR WRLA2009027Longeron · crackedDURING C-CHECK INSPECTION IN TPE - FOUND THE FORWARD CARGO STRUCTURE LONGERON L45L CRACKED AT STA 755, .5 INCH. REPLACED WITH NEW FABRICATED SPLICE 1EA IAW SRM VOL II 51-33-01 REV 40 AND EGAT EI W209P53B-075. COND CHECK NORMAL AND JOB COMPLETED. REF EGAT N/SDR WRLA2009026Longeron · crackedDURING C-CHECK INSPECTION IN TPE - FOUND THE CARGO STRUCTURE LONGERON L46L CRACKED AT STA 1119 6-10. REPLACE WITH NEW FABRICATED SPLICE IAW EGAT EI W2009P53B-079 AND SRM VOL 2 51-33-01 REV 40.SDR WRLA2009025Seat Track · corrodedDURING C-CHECK INSPECTION, FOUND SEAT TRACK CORROSION AT STA 824 + 859 X= -74.5. REPAIR THE DAMAGE SEAT TRACK PER SRM VOL I 53-70-00 PAGE 2 REV 40. REF EGAT N/R U05053.SDR WRLA2009024Seat Track · corrodedDURING C-CHECK INSPECTION IN TPE - FOUND SEAT TRACK CORROSION AT STA 824-859 X= -44. REPAIRED DAMAGED SEAT TRACK PER SRM 53-70-00 VOL I PAGE 2 REV 40. REF EGAT N/R U03017.SDR WRLA2009023Seat Track · corrodedDURING C-CHECK INSPECTION, FOUND SEAT TRACK CORROSION AT STA 824-859 X= 8.5. REPAIR THE DAMAGE SEAT TRACK PER SRM 53-70-00 VOL I PAGE 2 REV 40. REF EGAT N/R U05054.SDR WRLA2009022Seat Track · corrodedDURING C-CHECK INSPECTION, FOUND SEAT TRACK CORROSION AT STA 824-859 X=27.5. REPAIR THE DAMAGE SEAT TRACK PER SRM 53-70-00 VOL I PAGE 2 REV 40. REF EGAT N/R U03018.SDR WRLA2009021Seat Track · corrodedDURING C-CHECK INSPECTION IN TPE - FOUND SEAT TRACK CORROSION AT STA 824-859 X=107.5. REPAIRED SEAT TRACK IAW VOL I SRM 53-70-00 FIG 01 REV 40.SDR WRLA2009016Doubler · crackedDURING C-CHECK INSPECTION TPE - FOUND MACHINE DOUBLER OF LEFT SIDE WEB AT Y=1385 AND X=31.50 HAD CRACK FROM FASTENER HOLES. REPLACED MACHINE DOUBLER ON LEFT SIDE OF WEB AT Y=1385 X=31.5 IAW SRM 51-35-01 VOL I REV 40. REF EGAT N/R U05022.SDR WRLA2009015Seat Track · corrodedDURING C CHECK IN TPE - CORROSION - FOUND CORROSION WITH CRACK ON SEAT TRACK AT STA 799 - STA 919 X = 91.25. REPAIRED SEAT TRACK AT STA 799 - STA 919 X= 91.25 IAW VOL I 53-70-00 FIG 1, REV 40 AND CONDITION CHECK NORMAL & JOB COMPLETED.
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