# Service difficulty reports: Boeing 727-2H3 A list on [Boeing 727-2H3](https://openairdocs.org/model/boeing-727-2h3.md). Newest first. General aviation reporting is voluntary. Page 1 of 11 · 547 reports - [SDR K11A2017062672201](https://openairdocs.org/sdr/K11A2017062672201.md): Link · out of adjust · Jun 26, 2017 · N722CK · Boeing 7272H3 · Trailing Edge Flap Control System > DURING TAKEOFF WITH FLAPS UP, L/E FLAP NR 2 LIGHT INDICATED NOT RETRACTED, SPEED 230 KTS. ADJUSTED THE NR 2 LEADING EDGE FLAP POSITION SWITCH LINK IAW AMM 27-82-01. - [SDR K11A2016080172201](https://openairdocs.org/sdr/K11A2016080172201.md): Actuator Valve · inoperative · Jul 30, 2016 · N722CK · Boeing 7272H3 · Cabin Pressure Control System > AFTER TAKEOFF, ACFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL. - [SDR K11A2016071472201](https://openairdocs.org/sdr/K11A2016071472201.md): Support Angle · cracked · Jul 13, 2016 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > CRACKED LOWER SUPPORT ANGLE BS 950 AFT SIDE RT LOWER - [SDR K11A2016080372203](https://openairdocs.org/sdr/K11A2016080372203.md): Structure · corroded · Jul 9, 2016 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > LOWER CHORD HAS EVIDENCE OF CORROSION AT STA 950, STR 29R. - [SDR K11A2016080372201](https://openairdocs.org/sdr/K11A2016080372201.md): Support · corroded · Jul 7, 2016 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > LEFT WW STA 950, LBL 67, AFT OTBD CORNER OF WHEEL WELL PRESSURE DECK SUPPORT CORRODED. - [SDR K11A2016080372202](https://openairdocs.org/sdr/K11A2016080372202.md): Support Angle · corroded · Jul 5, 2016 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > LT WW PRESSURE DECK SUPPORT ANGLE STA 950, LBL 67. - [SDR K11A2016080372204](https://openairdocs.org/sdr/K11A2016080372204.md): Shear Tie · corroded · Jun 23, 2016 · N722CK · Boeing 7272H3 · Fuselage Internal Mounting Structure > FRAME SHEAR TIE CORROSION AT STA 720D, STR 27-26L. - [SDR K11A2016071472203](https://openairdocs.org/sdr/K11A2016071472203.md): Bulkhead Web · corroded · Jun 15, 2016 · N722CK · Boeing 7272H3 · Fuselage Main, Bulkhead > CORROSION AT FWD BULKHEAD UNDER RAY DOME - [SDR K11A2016071472202](https://openairdocs.org/sdr/K11A2016071472202.md): Stiffener · corroded · Jun 15, 2016 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > VERTICAL STIFFNER CORRODED BS 918 LT MLG WW APU INLET FWD SUPPORT LOWER END. - [SDR K11A2015102272201](https://openairdocs.org/sdr/K11A2015102272201.md): Torque Tube · detached · Oct 22, 2015 · N722CK · Boeing 7272H3 · Trailing Edge Flap Control System > OTBD T/E FLAPS WENT ASYMMETRIC, FOUND LT T/E OTBD DRIVESHAFT TORQUE TUBE COUPLING CAME OFF. RESECURED TORQUE TUBE, SAFETY WIRED, PERFORMED ADJUSTMENT AND TEST. NO DEFECTS NOTED AT THIS TIME. - [SDR K11A2015070972201](https://openairdocs.org/sdr/K11A2015070972201.md): Shear Tie · corroded · Jun 10, 2015 · N722CK · Boeing 7272H3 · Fuselage Internal Mounting Structure > SHEAR TIE CORRODED. - [SDR K11A2015070972202](https://openairdocs.org/sdr/K11A2015070972202.md): Beam · corroded · Jun 4, 2015 · N722CK · Boeing 7272H3 · Fuselage Main, Structure > BEAM CHORD CORROSION, RT SIDE OF WALKWAY. - [SDR K11A2013112522002](https://openairdocs.org/sdr/K11A2013112522002.md): Skin · worn · Oct 3, 2013 · N722CK · Boeing 7272H3 · Nacelle/Pylon, Plate/Skin > NR 3 NOSE COWL AT 6 O'CLOCK POSITION, EXTERIOR SKIN WORN. - [SDR K11A2013112522001](https://openairdocs.org/sdr/K11A2013112522001.md): Stringer · corroded · Sep 25, 2013 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER 26L CORRODED AT BS 720F+15". - [SDR K11A2013110722001](https://openairdocs.org/sdr/K11A2013110722001.md): Mount · corroded · Sep 9, 2013 · N722CK · Boeing 7272H3 · Engine Mount Section > NR 2 AFT ENGINE MOUNT SHOWS EVIDENCE OF CORROSION. - [SDR K11A2013020823002](https://openairdocs.org/sdr/K11A2013020823002.md): Longeron · corroded · Jan 30, 2013 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > LEFT ABOVE WING FWD HALF OF OVERWING LONGERON HAS CORROSION ON BOTTOM SIDE. - [SDR K11A2013020823001](https://openairdocs.org/sdr/K11A2013020823001.md): Longeron · corroded · Jan 30, 2013 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > RIGHT ABOVE WING FWD HALF OF OVERWING LONGERON HAS CORROSION ON BOTTOM SIDE. - [SDR K11A2012092123001](https://openairdocs.org/sdr/K11A2012092123001.md): Fire Loop · defective · Sep 21, 2012 · N723CK · Boeing 7272H3 · Fire Detection > NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED, FOLLOWED EMERGENCY PROCEDURES SHUTTING DOWN NR 1 ENGINE AND DISCHARGING FIRE BOTTLES NR 1 AND NR 2. FIRE WARNING LIGHT REMAINED ILLUMINATED APPROX 5 MIN AFTER SECOND BOTTLE DISCHARGE. - [SDR K11A2012072022001](https://openairdocs.org/sdr/K11A2012072022001.md): Gasket · blown · Jul 20, 2012 · N722CK · Boeing 7272H3 · Pneumatic Distribution System > AFTER TAKEOFF FROM MCI AT APPROX 1500 FT, NR 1 ENGINE FIRE WARNING LIGHT. COMPLETED ENGINE FIRE CHECKLIST AND NOTIFIED TOWER, DECLARED EMERGENCY. REQUESTED TO RETURN RETURN TO MCI FOR LANDING, PROCEEDED TO DUMP FUEL AREA, DUMPED FUEL TO LANDING WEIGHT, FIRE - [SDR K11A201204242202](https://openairdocs.org/sdr/K11A201204242202.md): Skin · chafed · Apr 2, 2012 · N722CK · Boeing 7272H3 · Fuselage Main, Plate/Skin > SKIN CHAFED 1 X 1 INCH. - [SDR K11A201204242201](https://openairdocs.org/sdr/K11A201204242201.md): Stringer Fitting · corroded · Mar 30, 2012 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER END FITTING HAS CORROSION 1 X 1 INCH. - [SDR K11A2011090772204](https://openairdocs.org/sdr/K11A2011090772204.md): Stringer · corroded · Jul 31, 2011 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER CORROSION, LOWER SIDE OF EXTERNAL POWER RECEPTICAL 1X3 INCHES. - [SDR K11A2011083072201](https://openairdocs.org/sdr/K11A2011083072201.md): Stiffener · corroded · Jul 27, 2011 · N722CK · Boeing 7272H3 · Wing Miscellaneous Structure > L/W FRONT SPAR STIFFENER CORROSION, 1X4 INCHES. - [SDR K11A2011083072203](https://openairdocs.org/sdr/K11A2011083072203.md): Stringer · corroded · Jul 26, 2011 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > AFT PIT STRINGER CORROSION, 1X6 INCHES. - [SDR K11A2011083072202](https://openairdocs.org/sdr/K11A2011083072202.md): Stringer · corroded · Jul 19, 2011 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > AFT PIT STRINGER CORROSION, 1X8 INCHES. - [SDR K11A2011090772203](https://openairdocs.org/sdr/K11A2011090772203.md): Support Fitting · cracked · Jul 17, 2011 · N722CK · Boeing 7272H3 · Drag Control Actuator > SPOILER ACTUATOR I/B SUPPORT FITTING CRACKED, 1X3 INCHES. - [SDR K11A2011090772202](https://openairdocs.org/sdr/K11A2011090772202.md): Stiffener · corroded · Jul 15, 2011 · N722CK · Boeing 7272H3 · Wing Spar > WING FRONT SPAR STIFFENER CORROSION, 1X4 INCHES AND.5X1 INCHES. - [SDR K11A2011090772201](https://openairdocs.org/sdr/K11A2011090772201.md): Stiffener · corroded · Jul 15, 2011 · N722CK · Boeing 7272H3 · Wing Spar > WING FRONT SPAR STIFFENER CORROSION, 1X3 INCHES. - [SDR K11A2011082672202](https://openairdocs.org/sdr/K11A2011082672202.md): Fitting · corroded · Jul 13, 2011 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER END FITTING CORROSION, 1X1 INCHES. - [SDR K11A2011082672201](https://openairdocs.org/sdr/K11A2011082672201.md): Fitting · corroded · Jul 13, 2011 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER END FITTING CORROSION, 1X1 INCHES. - [SDR K11A2011050572201](https://openairdocs.org/sdr/K11A2011050572201.md): Frame · cracked · May 5, 2011 · N722CK · Boeing 7272H3 · Fuselage Main, Frame > DURING AD INSPECTION FOUND FRAME 1148 CRACKED IN 2 AREAS BETWEEN STRINGERS 30L AND 28L. - [SDR K11A2010072472202](https://openairdocs.org/sdr/K11A2010072472202.md): Stringer · corroded · Aug 12, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER CORROSION. - [SDR K11A2010081172201](https://openairdocs.org/sdr/K11A2010081172201.md): Frame · cracked · Aug 11, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Frame > FRAME CRACKED ABOVE R1 DOOR. - [SDR K11A2010080372201](https://openairdocs.org/sdr/K11A2010080372201.md): Door Frame · corroded · Aug 3, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Structure > AFT ENTRY DOOR FRAME CORRODED UPPER DOOR FRAME (20 INCHES). - [SDR K11A2010071372203](https://openairdocs.org/sdr/K11A2010071372203.md): Stiffener · corroded · Aug 3, 2010 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > VERT STIFFENER CORRODED 5 INCHES. - [SDR K11A2010070872205](https://openairdocs.org/sdr/K11A2010070872205.md): Sill · cracked · Aug 3, 2010 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > L2 DOOR LOWER SILL HAS 1 INCH CRACK. - [SDR K11A2010072472203](https://openairdocs.org/sdr/K11A2010072472203.md): Shear Tie · corroded · Aug 1, 2010 · N724CK · Boeing 7272H3 · Fuselage Internal Mounting Structure > FRAME SHEAR TIE CORROSION 5 INCHES. - [SDR K11A2010072972201](https://openairdocs.org/sdr/K11A2010072972201.md): Frame · dented · Jul 29, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Frame > FRAME DAMAGE (2 INCH DENT). - [SDR K11A2010070872206](https://openairdocs.org/sdr/K11A2010070872206.md): Shear Web · corroded · Jul 28, 2010 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > SHEAR WEB CORROSION, CORROSION 10 INCHES. - [SDR K11A2010072872201](https://openairdocs.org/sdr/K11A2010072872201.md): Intercostal · damaged · Jul 28, 2010 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > INTERCOSTAL DAMAGED 24 INCHES. - [SDR K11A2010071072202](https://openairdocs.org/sdr/K11A2010071072202.md): Seat Track · corroded · Jul 28, 2010 · N722CK · Boeing 7272H3 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK CORROSION. - [SDR K11A2010071072201](https://openairdocs.org/sdr/K11A2010071072201.md): Seat Track · corroded · Jul 28, 2010 · N722CK · Boeing 7272H3 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK CORROSION. - [SDR K11A2010070272201](https://openairdocs.org/sdr/K11A2010070272201.md): Frame · corroded · Jul 28, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Frame > FRAME WEB CORROSION AT RT HORIZONTAL WALKWAY. - [SDR K11A2010072672201](https://openairdocs.org/sdr/K11A2010072672201.md): Stringer · corroded · Jul 26, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER HAS CORROSION, 12 INCHES. - [SDR K11A2010072572202](https://openairdocs.org/sdr/K11A2010072572202.md): Tank · corroded · Jul 25, 2010 · N722CK · Boeing 7272H3 · Fuel Storage > UPPER SURFACE CENTER TANK CORROSION (CORROSION 1 X 2 INCHES). - [SDR K11A2010072572201](https://openairdocs.org/sdr/K11A2010072572201.md): Web · corroded · Jul 25, 2010 · N722CK · Boeing 7272H3 · Fuselage Miscellaneous Structure > WEB HAS HOLE CORRODED THRU ENTIRE WEB, 6 INCHES. - [SDR K11A2010072472201](https://openairdocs.org/sdr/K11A2010072472201.md): Floorbeam · corroded · Jul 24, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Floor Beam > FLOORBEAM UPPER CHORD CORROSION 10 INCHES. - [SDR K11A2010070872204](https://openairdocs.org/sdr/K11A2010070872204.md): Stringer · cracked · Jul 22, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Longeron/Stringer > STRINGER CRACKED. - [SDR K11A2010071872201](https://openairdocs.org/sdr/K11A2010071872201.md): Door Frame · corroded · Jul 18, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Structure > AFT ENTRY DOOR CUROUT AFT SIDE CORRODED DOUBLER STRAP (40 INCHES). - [SDR K11A2010071472201](https://openairdocs.org/sdr/K11A2010071472201.md): Door Frame · corroded · Jul 14, 2010 · N722CK · Boeing 7272H3 · Fuselage Main, Structure > AFT ENTRY DOOR CUTOUT FRAME CORROSION RIGHT SIDE (20 INCHES OF CORROSION). Next page: https://openairdocs.org/model/boeing-727-2h3/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 aircraft_model_key = '7272H3' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-727-2h3/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.