DENTS WERE REPAIRED IN ACCORDANCE WITH B767 SRM 54-15-01-2R-3 REPAIR 3 AND EO 1971A291
) - [SDR UIEA2022102001156](https://openairdocs.org/sdr/UIEA2022102001156.md): None · none · Oct 24, 2022 · N1013A · Boeing 767 > SEVERAL DENTS WERE FOUND ON LH INLET COWL ACOUSTIC PANEL(DENTS WERE REPAIRED IN ACCORDANCE WITH E.O 1971A291
) - [SDR CALA2022102402923](https://openairdocs.org/sdr/CALA2022102402923.md): None · none · Oct 23, 2022 · N62883 · Boeing 737 > FOUND PANEL 412AR UNLATCHED AND OPEN ON #1 ENG NOSE COWL ON ARRIVAL -- SEE PHOTO LOTS IF HISTORY UNDER ATA 71; 72 AND 54 PHOTO ADDED -- SUSPECT AIR LEAK FROM SEAL MISSING AROUND DUCT -- PHOTO -- CMM 71-11-22 FIG 1 SHEET 4 SHOWING REQUIRED SEAL ASSLY NOTE: THI - [SDR CALA2022101802859](https://openairdocs.org/sdr/CALA2022101802859.md): Duct · missing · Oct 18, 2022 · N14242 · Boeing 737824 > PDA 3 #1 ENG T.A.I. DUCT HAS 1 LOUVER COMPLETELY MISSING (OUT OF 3)...SEE PHOTO LOUVER IN 800 HOURS. #1 ENG HAS ONLY 1 LOUVER MISSING WITH NO CRACKS IN SLOTTED AREAS, PER AMM 71-11-01-200-801-F00, ISSUE DIP TO REPAIR MISSING DIP APPROVED FOR #1 ENG T.A.I. DUC - [SDR CALA2022100302637](https://openairdocs.org/sdr/CALA2022100302637.md): Louver · missing · Oct 3, 2022 · N13720 · Boeing 737724 > PDA 3 #2 ENG TAI DUCT AT 6-0 CLOCK POS HAS ONE LOUVER COMPLETELY MISSING.FOR #2 ENG ONLY 1 LOUVER MISSING WITH NO CRACKS IN SLOTTED AREAS, FOR #2 ENG TAI DUCT AT 6-0 CLOCK POS HAS ONE LOUVER TOMC-APPROVAL FROM SC1ELBYC COMMENT COMPLETELY MISSING. SHOULD BE RE - [SDR SWAA2022082545977](https://openairdocs.org/sdr/SWAA2022082545977.md): Skin · cracked · Aug 13, 2022 · N737JW · Boeing 7377H4 > # 1 ENGINE OUTBOARD FAN COWL HAS A SKIN CRACK APROX 4 LONG 7.5 ABOVE THE IDG SERVICE DOOR. / [01] REMOVED AND REPLACED LH ENGINE OUTBOARD FAN COWL IAW AMM 71-11-02 - [SDR CALA2022071801808](https://openairdocs.org/sdr/CALA2022071801808.md): None · missing · Jul 18, 2022 · N1902U · Airbus A320232 > PDA 3 #2 ENG AIR INTAKE COWL OUTER LIP AT INBD SIDE (11 O-CLOCK POS) HAS ONE RIVET HEAD BROKEN OFF / MISSING -- SEE PHOTO ADDED PHOTO INSTALLED NEW FASTENER REF AIRBUS SRM 51-42-00. - [SDR NACA2022071100001](https://openairdocs.org/sdr/NACA2022071100001.md): Cowl Door · damaged · Jul 11, 2022 · N351CM · Boeing 767323 > RH ENGINE OB CORE COWL DUCT PRECOOLER EXIT DAMAGE. REMOVED AND REPLACED RH ENGINE OUTBOARD CORE COWL IAW AMM 71-11-06 PART INFO PENDING CHECK DOCUMENTATION - [SDR UIEA2022061300589](https://openairdocs.org/sdr/UIEA2022061300589.md): Rod · unserviceable · Jun 13, 2022 · N664GT · Boeing 76731B > ENG # 2 O/B FAN COWL, AFT HOLD OPEN ROD DON'T RETRACT. REMOVED AND REPLACED # 2 ENG O/B CORE COWL HOLD OPEN ROD. OPS CHECK NORMAL IAW B767-300 AMM 71-11-11. - [SDR CALA2022041400990](https://openairdocs.org/sdr/CALA2022041400990.md): Panel · missing · Apr 14, 2022 · N41140 · Boeing 757200 > PDA 2 L ENG OIL SERVICE ACCESS DOOR MISSING PANEL REFITTED WITH TEMP REPAIR IAW ECRA ON WALK AROUND FOUND L ENGINE OIL SERVICE DOOR MISSING. DOOR WAS TOMC-APPROVAL FROM SC1ELBYC COMMENT RECOVERED AND RETURNED TO AIRCRAFT. PER ECRA 7110-01125 COMPLY WITH TEMP R - [SDR SWIA202265163](https://openairdocs.org/sdr/SWIA202265163.md): None · cracked · Mar 25, 2022 · N748EV · Cndair CL6002C10 > DURING A4 INSPECTION OF THE LH ENGINE INLET, FOUND 2 DENTS WITH CRACKS AT THE 3 AND 5 O' CLOCK POSITIONS, BOTH ARE OUT OF LIMITS. (FILED - CLOSED) REMOVED AND REPLACED LH ENGINE INLET IN REFERENCE TO AMM 71-61-01 - [SDR SWIA202265651](https://openairdocs.org/sdr/SWIA202265651.md): None · dented · Feb 20, 2022 · N816SK · Cndair CL6002D24 > *DENT ON LH ENGINE UPPER TRANSCOWL EXTERNAL SKIN. MARKED. (C CHECK RO 5/23/22) REPAIRED L/H ENGINE UPPER TRANSCOWL REF REO# 690-54-21-413, REV --, DATED 3/10/22. COMPLIED WITH TASK CARD 51-900-1002-SKY SEE CONTINUATION SHEET FOR DETAILS. - [SDR CALA2021121402369](https://openairdocs.org/sdr/CALA2021121402369.md): Rivet · missing · Dec 14, 2021 · N851UA · Airbus A319131 > PDA 3 #1 ENG AIR INTAKE COWL INNER LIP SKIN HAS ONE RIVET HEAD BROKEN OFF/MISSING AT 6 O-CLOCK POSITION -- SEE PHOTO,S PHOTO,S ADDED REMOVED AND REPLACED REF ECRA7111-01387 NO FURTHER ACTION REQD - [SDR A6WA202101178068](https://openairdocs.org/sdr/A6WA202101178068.md): Skin · cracked · Dec 1, 2021 · N442AW · Cndair CL6002B19 > R/H UPPER MAIN CORE COWL UPPER FWD I/B CORNER IS BENT AND DEBONDING.FOUND CRACK IN DEBONDING FWD I/B CORNER LENGTH IS 1.437" &.010"W. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON DAMAGE ON OUTER SKIN P/N 228-50142-607 THAT MEASURES 2.5"L X.77 - [SDR UIEA2021111002388](https://openairdocs.org/sdr/UIEA2021111002388.md): Nose Cowl · none · Nov 8, 2021 · N1499A · Boeing 767328 > RH ENG NOSE COWL HAS A CRACK 5.325" LONG LE AT 11 O'CLOCK POSITION.(REMOVED AND REPLACED NOSE COWL IAW AMM 71-1-01. OPS CK GOOD.
) - [SDR SWIA202163376](https://openairdocs.org/sdr/SWIA202163376.md): None · gouged · Nov 6, 2021 · N824SK · Cndair CL600* > LH LOWER TRANSCOWL (PN CN624-2001-012, SN SB1003) HAS GOUGED LATCH DOOR COAMING (MARKED). (C CHECK RO 12-31-21) / REPAIRED LATCH DOOR COAMING ON LH LOWER TRANSCOWL PER ALL STEPS OF REO 670-54-21-1028 REV NC, DATED 2009-06-15. SEE CONTINUATION CARD FOR DE - [SDR SWIA202163871](https://openairdocs.org/sdr/SWIA202163871.md): None · damaged · Nov 3, 2021 · N770SK · Cndair CL600* > *RIGHT ENGINE NOSE COWL LIPSKIN HAS EROSION DAMAGE AROUND ITS CIRCUMFERENCE. (C CHECK RO 1/16/2022) REMOVED AND INSTALLED THE NEW FROM STOCK RH ENGINE INLET COWL ASSY REF CRJ-700 AMM 71-61-01-000-801-A01 & 71-61-01-400-801-A01. LEAK CHECK, OPEARATIONAL CHE - [SDR SWIA202163704](https://openairdocs.org/sdr/SWIA202163704.md): None · broken · Oct 11, 2021 · N207PS · Cndair CL6002B19 > RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET IS BROKEN ATTACHED TO NOSE INLET COWL (C-CHECK RO 1/5/2022) REPAIRED RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET ATTACHED TO THE NOSE INLET COWL IAW REO 601R-71-61-3941 REV B DATED5/2/2018 AND SKY CARD 51-900-10 - [SDR SWIA202162720](https://openairdocs.org/sdr/SWIA202162720.md): None · worn · Sep 25, 2021 · N774SK · Cndair CL600* > *RH UPPER TRANSCOWL HAS WEAR ON COAMING. AREA MARKED (C-CHECK RO 11-20-2021) REPAIRED DAMAGE ON R/H UPPER TRANSCOWL COAMING REF REO 670-54-21-1028 REV (NC) 2009-06-15 STEPS 1-9. FUCNTIONAL CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY. - [SDR SWIA202161732](https://openairdocs.org/sdr/SWIA202161732.md): None · none · Sep 1, 2021 · N946SW · Cndair CL6002B19 > WHILE REMOVING FASTENERS FOR LH ENGINE NOSE COWL ASSY. ATTACHMENT CLIP, MISDRILLED TWO FASTENER HOLES IN ATTACHMENT FLANGE. (C-CHECK RO 10/8/2021) REPAIRED LH ENGINE NOSE COWL ASSY. REF REO 601R-71-61-4336 REV -- 2021-09-10 COMPLIED WITH ALL STEPS. COM - [SDR SWIA202161149](https://openairdocs.org/sdr/SWIA202161149.md): None · dented · Jul 10, 2021 · N766SK · Cndair CL600* > N766SK-6893 / ON THE BOTTOM OF THE LH ENGINE NOSE COWL, APPROXIMATELY 6 O'CLOCK POSITION, THERE ARE MULTIPLE DENTS MARKED WITH YELLOW DOTS. PLEASE PLOT, MAP, AND EVALUATE THE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL DAMAGE USING AIRCRAFT STANDARD PRACTICE - [SDR SCNA20160929197](https://openairdocs.org/sdr/SCNA20160929197.md): Nose Cowl · damaged · Sep 29, 2016 · N711SY · Boeing 73773V > RT WING NR 2 ENGINE NOSE COWL, THUMBNAIL MATTING SURFACE HAS LIGHT WEAR AND MISSING PAINT. AREAS FROM 10 TO 2 O`CLOCK MARKED. REPAIRED NR 2 RIGHT WING ENGINE NOSE COWL. - [SDR 2015FA0000190](https://openairdocs.org/sdr/2015FA0000190.md): Housing · worn · May 11, 2015 · N679X · Piper PA28R201T > REPLACED COWL FLAP CABLE, PN LSM-SCD-032-1 DUE TO WORN SPOT NEAR CONNECTION TO COWL. COWL HAS BEEN REPLACE IAW STC SA03470AT. ACFT HAD TO MAKE AN UNSCHEDULED STOP DO TO SMOKE IN THE CABIN. INSPECTION FOUND CABLE COVERING MELTED DO TO BEING TO CLOSE TO THE EX - [SDR 2015FA0000189](https://openairdocs.org/sdr/2015FA0000189.md): Cable · worn · May 11, 2015 · N679X · Piper PA28R201T > COWL FLAP CABLE RUBBING ON EXHAUST ON LT SIDE OF ENGINE. RUBBED THROUGH THE OUTER COVER AND HALF THROUGH THE INNER CORE. THIS ACFT HAS HAD A REPLACEMENT COWL INSTALLED UNDER STC SA03470AT. - [SDR UALA2012100105556](https://openairdocs.org/sdr/UALA2012100105556.md): Cowling · dented · Sep 28, 2012 · N589UA · Boeing 757222 > CREW REPORT: ON PUSHBACK GRD CREW NOTICED RIGHT ENGINE COWL LEADING EDGE SMALL DENT AT 6 O'CLOCK POSITION NO DOT. FBO REPORTS DENT MEASURES 6 IN LONG BY 1.125 WIDE BY.040 DEEP. BEYOND LIMITS PER SRM 54-11-01 PG 104. INSPECTED WITH HFEC NO CRACKS NOTED. N - [SDR SWIA201231622](https://openairdocs.org/sdr/SWIA201231622.md): Cowl Flap · cracked · Aug 24, 2012 · N585SW · Emb EMB120ER > LEFT NACELLE FLAP CRACKED. (A-INSPECTION) REPLACED LEFT NACELLE FLAP IN REFERENCE TO EMB120 AMM. - [SDR CA100608010](https://openairdocs.org/sdr/CA100608010.md): Cowl Flap · failed · Jun 3, 2010 · Doug DC6B > (CAN) NR 4 COWL GILL FAILS TO ACTUATE. - [SDR VNAA0509010](https://openairdocs.org/sdr/VNAA0509010.md): Access Panel · punctured · Sep 16, 2005 · N242JS · Cndair CL6002B19 > A BELT LOADER HIT THE LT ENGINE NOSE COWL LOWER ACCESS PANEL. DAMAGE AT THE 5 O'CLOCK POSITION WAS A 6 X 2 HOLE. AFTER INSPECTION AND TEMPORARY REPAIR THE AIRCRAFT WAS FERRIED TO CKB WHERE MAINTENANCE REMOVED & REPLACED THE PANEL WITH A SERVICEABLE UNIT IAW - [SDR 2005FA0000022](https://openairdocs.org/sdr/2005FA0000022.md): Cowl Flap · inoperative · Dec 28, 2004 · N2663S · Cessna T337C > THE OWNER INSTALLED STC SA01091AT. THIS STC REMOVES THE ELECTRIC COWL FLAP MOTOR, AND INSTALLED A COMPLETELY MECHANICAL SYSTEM. THE OWNER COMPLAINED THAT HE COULD NOT THE CLOSE REAR COWL FLAP IN FLIGHT. - [SDR WTW2004F00000](https://openairdocs.org/sdr/WTW2004F00000.md): Channel · broken · May 12, 2004 · N66619 · Beech 58 > PILOTS REPORTED COWL FLAP HANDLE BROKE IN THEIR HAND WHEN THE COWL FLAPS WERE CLOSED. INSPECTION REVEALED THE LEVER PN 96324055-33 WORE AGAINST THE DETENT PLATE PN 96-324055-163 AND CUT A GROOVE IN THE LEVER. FURTHER INSPECTION REVEALED THE CHANNEL PN 96-324 - [SDR LO62004F00001](https://openairdocs.org/sdr/LO62004F00001.md): Actuator · inoperative · May 6, 2004 · N3427 · Cvac 34032 > RT SIDE, COWL FLAP ACTUATOR BECAME INTERMITTENT. FINALLY COWL FLAPS STOPPED PART WAY OPEN. REPLACED ACTUATOR WITH OVERHAULED UNIT. - [SDR CA040421004](https://openairdocs.org/sdr/CA040421004.md): Pan · corroded · Apr 21, 2004 · Cessna A185F > (CAN) DURING RIGHT COWL FLAP HINGE REPLACEMENT, FOUND COWL FLAP PAN ASSEMBLY HAS SEVERE CORROSION UNDER HINGE HALF. THIS AREA IS ONLY VISIBLE AFTER REMOVING THE HINGE. - [SDR UPS02239961](https://openairdocs.org/sdr/UPS02239961.md): Longeron · cracked · Dec 2, 2002 · N906UP · Boeing 72730C > INSPECTION TYPE:C ENG. #2 R/H FWD COWL CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK(DOOR SHEAR) LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON FABRICATED IAW SRM 5 1-30-1 NEW LONGERON INSTALLED IAW SRM 51-30-02 & REPORTECTED IAW MM 51-20-01 - [SDR 2002FA0000795](https://openairdocs.org/sdr/2002FA0000795.md): Circuit Breaker · failed · Jun 6, 2002 · N86076 · Cessna 337D > CIRCUIT BREAKER FAILED INTERNALLY WITHOUT TRIPPING. CAUSED OPEN CIRCUIT TO COWL FLAP MOTORS. FAILURE OCCURRED DURING GROUND MAINTENANCE. NEED TO IMPROVE QUALITY CONTROL IN PRODUCTION. - [SDR B202002F00004](https://openairdocs.org/sdr/B202002F00004.md): Bushing · worn · Aug 30, 2001 · N44911 · Doug C54BDC > NR 2 ENGINE COWL FLAP BUSHING WORN, REPACED WITH NEW.. - [SDR B2O2002F00000](https://openairdocs.org/sdr/B2O2002F00000.md): Bushing · worn · Aug 30, 2001 · N44911 · Doug C54BDC > BUSHING AT COWL FLAP, NR 4 ENGINE CHANGED NR 2 AND NR 4 OUTBOARD COWL BUSHING. - [SDR 2001FA0000043](https://openairdocs.org/sdr/2001FA0000043.md): Alt Air Door · loose · May 25, 2001 · N8379Y · Piper PA30 > ON TAKEOFF ROLL, THE RIGHT ENGINE WOULD NOT DEVELOP FULL POWER. UPON FUTURE INVESTIGATION FOUND THE ALT AIR DOOR CAME LOOSE AND WAS BLOCKING THE EJECTOR INTAKE. UPON FINDING THIS WE INSPECTED THE LEFT ALT AIR BOX AND FOUND THE ALT AIR DOOR LAYING IN THE COWL - [SDR SWIA972290](https://openairdocs.org/sdr/SWIA972290.md): Computer · failed · Jan 14, 2001 · N204SW · Emb EMB120ER > LEFT NACELLE FLAPS FAULT DISCREPANCY DURING RETRACTION. REPLACED FLAP COMPUTER. OPS CHECK BAD. REPLACED LEFT NACELLE FLAP ACTUATOR. OPS AND LEAK CHECK GOOD. WORK ACCOMPLISHED IAW EMB120 MM 27-50-00 AND RII 27-307. FLAP COMP P/N: 347200-1001, S/N ON: 02 - [SDR RRXA003331](https://openairdocs.org/sdr/RRXA003331.md): Nose Cowl · dented · Oct 30, 2000 · N500MH · Doug DC871F > DURING A MAINTENANCE VISIT FOUND A DENT TO THE NR 2 ENGINE NOSE COWL AT 9 O'CLOCK POSITION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 71-5-1 AND EO#00-262 WITH APPR - [SDR MALA000586](https://openairdocs.org/sdr/MALA000586.md): Shield · chafed · Sep 2, 2000 · N414XJ · Saab 340B > FOUND DURING C-CHECK, LOWER HEAT SHIELD ON ENGINE COWL 464 AT CHAFED. REFER TO CELSIUS TASK CARD 4526, W/O 18816. MAINTENANCE BLENDED CHAFED AREA ON LOWER HEAT SHIELD ON ENG COWL 464AT IAW SRM 51-70-40. MATERIAL REMOVAL OUT OF ALLOWABLE LIMIT REF SAAB SRM 5 - [SDR MALA000585](https://openairdocs.org/sdr/MALA000585.md): Shield · chafed · Sep 2, 2000 · N414XJ · Saab 340B > FOUND DURING C-CHECK, LOWER HEAT SHIELD ON ENGINE COWL 464 AT CHAFED. REFER TO CELSIUS TASK CARD 4526, W/O18816. MAINTENANCE BLENDED CHAFED AREA ON LOWER HEAT SHIELD ON ENG COWL 464AT IAW SRM 51-70-40. MATERIAL REMOVAL OUT OF ALLOWABLE LIMIT REF SAAB SRM 51 - [SDR VNAA0004025](https://openairdocs.org/sdr/VNAA0004025.md): Latch · open · Apr 29, 2000 · N429JS · Dorner DO328100 > WHILE ON CLIMBOUT, A PASSENGER ALERTED THE FLIGHT ATTENDANT THAT THE RIGHT HAND INBOARD FORWARD COWLING DOOR WAS OPEN. THE FLIGHT ATTENDANT NOTIFIED THE PILOT WHO CONTACTED THE TOWER THAT FLIGHT 4090 WAS RETURNING AND REQUESTED A HOLD TO BURN OFF EXCESSIVE FU - [SDR RRXA001884](https://openairdocs.org/sdr/RRXA001884.md): Cowl Door · damaged · Apr 8, 2000 · N961R · Doug DC873F > DURING A MAINTENANCE VISIT FOUND A LARGE SCRATCH AND CREASE ACROSS RT FWD COWL DOOR LWR SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FILLED CREASES AND GOUGES WITH A ERODINAMIC DECON PUTTY AND PAINTED I - [SDR 2000ZZZX23](https://openairdocs.org/sdr/2000ZZZX23.md): Bracket · cracked · Dec 16, 1999 · N949SP · Cessna 172S > DURING PHASE 2 INSPECTION, FOUND LOWER COWL SHOCK MOUNT BRACKET CRACKED AT THE 4 O'CLOCK POSITION. THE OTHER HALF OF THE SHOCK MOUNT BRACKET WAS ALSO CRACKED, P/N 045303-3. REPLACED BOTH BRACKETS. - [SDR 2000ZZZX22](https://openairdocs.org/sdr/2000ZZZX22.md): Bracket · cracked · Dec 16, 1999 · N949SP · Cessna 172S > DURING PHASE 2 INSPECTION, FOUND LOWER COWL SHOCK MOUNT BRACKET CRACKED AT THE 4 O'CLOCK POSITION. THE OTHER HALF OF THE SHOCK MOUNT BRACKET WAS ALSO CRACKED, P/N 045303-3. REPLACED BOTH BRACKETS. - [SDR CA991231011](https://openairdocs.org/sdr/CA991231011.md): Motor · intermittent · Dec 3, 1999 · Piper PA31 > (CAN) PILOT REPORTED LT COWL FLAP REFUSED TO OPEN IN FLIGHT. MAINTENANCE DISCOVERED ACTUATOR MOTOR OPERATING INTERMITTANTLY. MOTOR (DUKESP/N:5142-00-1; PIPER P/N475-194) REPLACED.SUBMITTER NOTED THAT ASSEMBLY DATE FOR UNSERVICEABLE PART WAS MARCH 10,1999. - [SDR 99ZZZX4615](https://openairdocs.org/sdr/99ZZZX4615.md): Actuator · failed · Dec 1, 1999 · N830Q > BEGINNING 9-20-99 AT 646.5 HOBBS, COWL FLAP ACTUATOR WAS REPLACED. A PART WAS ORDERED THROUGH BEECHCRAFT. THE NEXT FAILURE OCCURRED AT 9-30-99 AT 672.4 HOBBS, AND, THEREAFTER, 10-19-99 AT 704.7 HOBBS, 11-4-99 AT 763.0 HOBBS, AND 11-30-99 AT 840.8 HOBBS. AT - [SDR AU990892](https://openairdocs.org/sdr/AU990892.md): Control Unit · seized · Sep 8, 1999 · Cessna 310R > (AUS) BOTH COWL FLAP CONTROLS UNSERVICEABLE. ONE CONTROL SEIZED. ONE CONTROL BROKEN WITH THE 'T' HANDLE REPLACED. Next page: https://openairdocs.org/jasc/7111/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 jasc_code = '7111' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/jasc/7111/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.