# Service difficulty reports: N13988 A list on [N13988](https://openairdocs.org/aircraft/N13988.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 127 reports - [SDR ASOA201906117059](https://openairdocs.org/sdr/ASOA201906117059.md): Handle · cracked · Jun 11, 2019 · N13988 · Emb EMB145LR · Fuselage Miscellaneous Structure > A/C WAS IN C-CHECK WHEN INSPECTION FOUND THE R/H COCKPIT GRAB HANDLE CRACKED FWD. OF FUSELAGE II. MAINTENANCE REPAIRED AREA IAW ETD 2019-145-074630 BY REMOVING THE DAMAGED AREA AND MANUFACTURED A FILLER AND DOUBLER. ALL WORK ACCOMPLISHED AND WILL BE RELEASED A - [SDR ASOA201906117058](https://openairdocs.org/sdr/ASOA201906117058.md): Fitting · cracked · Jun 11, 2019 · N13988 · Emb EMB145LR · Trailing Edge Flaps > A/C WAS IN C-CHECK WHEN INSPECTION FOUND THE RT OUTBOARD FLAP INBD SIDE FITTING CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALL A DOUBLER REIN-ENFORCEMENT PLATE IAW ETD2019-145-069108. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CH - [SDR ASOA201906087055](https://openairdocs.org/sdr/ASOA201906087055.md): Window Post · cracked · Jun 7, 2019 · N13988 · Emb EMB145LR · Fuselage Main, Structure > L/H WINDSHIELD LATERAL POST CRACKED AT UPPER O/B CORNER AROUND RIVET. REMOVED RIVETS, BOLTS AND SUPPORTS TO FACILITATE INSTALLATION OF REINFORCEMENT FOR L/H WINDSHIELD PILLAR. DRILLED REINFORCEMENT, CUT OUT PILLAR SKIN CRACKED SECTION, COLD WORKED 14 HOLES ON - [SDR ASOA201906087056](https://openairdocs.org/sdr/ASOA201906087056.md): Window Post · cracked · Jun 6, 2019 · N13988 · Emb EMB145LR · Fuselage Main, Structure > L/H FUSELAGE WINDSHIELD REINFORCEMENT PILLAR 2 SKIN HOLES FOUND CRACKED. REMOVED AND REPLACED L/H FUSELAGE WINDSHIELD REINFORCEMENT PILLAR. AIRCRAFT STILL IN C CHECK. - [SDR ASOA201905317054](https://openairdocs.org/sdr/ASOA201905317054.md): Floor Support · corroded · May 31, 2019 · N13988 · Emb EMB145LR · Fuselage Miscellaneous Structure > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE RT OMEGA BEAM FORWARD OF NUT PLATE. MAINTENANCE CUTOUT THE CORROSION AND FABRICATED AN EXTERNAL DOUBLER IAW SRM 53-24-10 AND CPM 51-21-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE - [SDR ASOA201905317053](https://openairdocs.org/sdr/ASOA201905317053.md): Floor Support · corroded · May 31, 2019 · N13988 · Emb EMB145LR · Fuselage Miscellaneous Structure > TYS A/CIS IN C-CHECK WHEN INSPECTION FOUND CORROSION AT AFT NUTPLATE OF RT OMEGA BEAM IN THE LAV. MAINTENANCE CUTOUT THE CORROSION, FAB. A DOUBLER IAW SRM 53-24-10 AND CPM 51-21-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA201905317052](https://openairdocs.org/sdr/ASOA201905317052.md): Trunnion · cracked · May 31, 2019 · N13988 · Emb EMB145LR · Main Landing Gear Attach Section > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE LT MLG AFT TRUNION CRACKED. MAINTENANCE REMOVED AND REPLACED THE LT TRUNION IAW ECTC ETD2019-145-072657.ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA2018120314068](https://openairdocs.org/sdr/ASOA2018120314068.md): Acm · frozen · Dec 1, 2018 · N13988 · Emb EMB145LR · Cabin Cooling System > DFW - FLIGHT 3999 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PLANE AND PLACED THE NUMBER ONE PACK ON MEL 21-51-00-2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 1 - [SDR ASOA201806035150](https://openairdocs.org/sdr/ASOA201806035150.md): Control Module · failed · Jun 3, 2018 · N13988 · Emb EMB145LR · Passenger Compartment Lighting > PILOT REPORTED AN ODOR, CABIN LIGHT WAS GETTING TOO HOT. MX PERFORMED AN INSPECTION OF THE CABIN LIGHTING AND FOUND CABIN LIGHTING CONTROL MODULE AND 1A LIGHT BALLAST BAD. REMOVED AND REPLACED LIGHT CONTROL MODULE AND BALLAST, OPS CHECKED GOOD. ACFT WAS A - [SDR ASOA2018051605126](https://openairdocs.org/sdr/ASOA2018051605126.md): Transducer · faulty · May 12, 2018 · N13988 · Emb EMB145ER · Landing Gear Brake System > CREW REPORTED BRAKES WERE SLOW TO REPOND ON LANDING ROLLOUT FOR LANDING. BRAKING WAS NORMAL ON BOTH SIDES ON TAXI TO GATE. REMOVED AND REPLACED THE NR 3 WHEEL SPEED TRANDSDUCER IAW MM 32-41-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201704305071](https://openairdocs.org/sdr/ASOA201704305071.md): Control Unit · faulty · Apr 30, 2017 · N13988 · Emb EMB145LR · Landing Gear Brake System > PILOT REPORTED BRAKES ARE NOT EFFECTIVE AT HIGH SPEEDS, FINE AT IDLE SPEED. LITTLE OR NO BRAKING ACTION ON LANDING. MX REMOVED AND REPLACED THE BRAKE CONTROL UNIT AND OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201704273120](https://openairdocs.org/sdr/ASOA201704273120.md): Stringer · cracked · Apr 27, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > CRACK ON LT REAR STRINGER 2L AT FRAME 75. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, ITEM 3, FIG 202. - [SDR ASOA201704273119](https://openairdocs.org/sdr/ASOA201704273119.md): Skin · cracked · Apr 27, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > LEFT REAR FUSELAGE SKIN CRACKED AT TWO PLACES AT FRAME 75, STRINGER 21L. REPAIRED THE SKIN IAW SRM 53-31-01, PARA 11, FIG 219, SHEET 2. - [SDR ASOA201704273118](https://openairdocs.org/sdr/ASOA201704273118.md): Door Sill · corroded · Apr 27, 2017 · N13988 · Emb EMB145LR · Fuselage Miscellaneous Structure > SERVICE DOOR FRAME FORWARD SILL CUT OUT CORRODED. SILL REPLACED AS PER SRM 51-40-02. - [SDR ASOA201704263117](https://openairdocs.org/sdr/ASOA201704263117.md): Trunnion · corroded · Apr 26, 2017 · N13988 · Emb EMB145LR · Fuselage, Landing Gear Attach Fittings > RIGHT MLG FORWARD LOWER TRUNNION CAP CORRODED. THE TRUNNION CAP WAS REPLACED IAW CARD 57-26-00-220-C02-A00. - [SDR ASOA201704263116](https://openairdocs.org/sdr/ASOA201704263116.md): Bearing Race · corroded · Apr 26, 2017 · N13988 · Emb EMB145LR · Fuselage, Landing Gear Attach Fittings > CORROSION FOUND ON THE RT MLG FWD UPPER TRUNNION BEARING RACE. THE CORROSION WAS BLENDED OUT IAW 51-10-03 AND ETD2017-145-032710. NDT INSPECTION PERFORMED WITH NO FAULTS. - [SDR ASOA201704253115](https://openairdocs.org/sdr/ASOA201704253115.md): Skin · cracked · Apr 25, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > AFT FUSELAGE SKIN CRACKED AT FRAME 65, AFT RADIO ALTIMETER ANTENNA MOUNT HOLES. REPAIRED IAW ETD2017-145-032887. - [SDR ASOA201704253114](https://openairdocs.org/sdr/ASOA201704253114.md): Skin · corroded · Apr 25, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > AFT FUSELAGE FRAMES 65 AND 68 CORRODED UNDER RADIO ALTIMETER ANTENNA. CORROOSION REMOVED IAW ETD2017-145-032887. - [SDR ASOA201704253113](https://openairdocs.org/sdr/ASOA201704253113.md): Beam · corroded · Apr 25, 2017 · N13988 · Emb EMB145LR · Cargo/Baggage Doors > CARGO DOOR LOWER BEAM CORRODED. CARGO DOOR ENTRY LOWER BEAM REPLACED IAW SRM 51-40-02. - [SDR ASOA201704253112](https://openairdocs.org/sdr/ASOA201704253112.md): Support · corroded · Apr 25, 2017 · N13988 · Emb EMB145LR · Fuselage Miscellaneous Structure > RIGHT OTBD LAVATORY SUPPORT CORRODED. THE SUPPORT REPLACED IAW SRM 51-40-02 - [SDR ASOA201704243111](https://openairdocs.org/sdr/ASOA201704243111.md): Doubler · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > RIGHT CENTER FUSELAGE CORROSION AROUND POTABLE WATER HEATED NIPPLE. DOUBLER BLENDED IAW SRM 51-10-05 - [SDR ASOA201704243110](https://openairdocs.org/sdr/ASOA201704243110.md): Seat Track · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > CABIN LT OTBD SEAT TRACK NR 6 CORRODED. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06-400-801-A. - [SDR ASOA201704243109](https://openairdocs.org/sdr/ASOA201704243109.md): Seat Track · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > CABIN RT OUTBOARD SEAT TRACK NR 4 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801-A. - [SDR ASOA201704243108](https://openairdocs.org/sdr/ASOA201704243108.md): Seat Track · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > CABIN RT OUTBOARD SEAT TRACK 3 CORRODED. SEAT TRACKED 3 REPLACED IAW AMM 53-01-06-400-801-A - [SDR ASOA201704243107](https://openairdocs.org/sdr/ASOA201704243107.md): Seat Track · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > RT CABIN SEAT TRACK NR 1 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801A - [SDR ASOA201704243106](https://openairdocs.org/sdr/ASOA201704243106.md): Shear Tie · cracked · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Internal Mounting Structure > FRAME 80 RT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02 - [SDR ASOA201704243105](https://openairdocs.org/sdr/ASOA201704243105.md): Shear Tie · cracked · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Internal Mounting Structure > FRAME 80 LT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02. - [SDR ASOA201704243103](https://openairdocs.org/sdr/ASOA201704243103.md): Bushing · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Horizontal Stabilizer Structure > HORIZONTAL STAB RT PIN BUSHING CORRODED. PIN BUSHING REPLACED. - [SDR ASOA201704243104](https://openairdocs.org/sdr/ASOA201704243104.md): Pin · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Horizontal Stabilizer Structure > HORIZONTAL STAB RT PIN CORRODED. PIN REPLACED IAW MM 55-10-01 - [SDR ASOA201704243102](https://openairdocs.org/sdr/ASOA201704243102.md): Bushing · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Horizontal Stabilizer Structure > HORIZONTAL STAB LT PIN BUSHING CORRODED. BUSHING REPLACED IAW MM 55-10-01. - [SDR ASOA201704243101](https://openairdocs.org/sdr/ASOA201704243101.md): Channel · corroded · Apr 24, 2017 · N13988 · Emb EMB145LR · Service Doors > SERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02. - [SDR ASOA201704243100](https://openairdocs.org/sdr/ASOA201704243100.md): Angle · cracked · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Miscellaneous Structure > COCKPIT LT FRAME 10, UPPER ANGLE CRACKED. THE FRAME ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR ASOA201704243099](https://openairdocs.org/sdr/ASOA201704243099.md): Frame · cracked · Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Frame > COCKPIT RT FRAME 10 CRACKED. THE FRAME WAS REPLACED IAW SRM 51-40-02. - [SDR ASOA201704203098](https://openairdocs.org/sdr/ASOA201704203098.md): Crossbeam · cracked · Apr 20, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Structure > NLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50. - [SDR ASOA201704203097](https://openairdocs.org/sdr/ASOA201704203097.md): Crossbeam · cracked · Apr 20, 2017 · N13988 · Emb EMB145LR · Fuselage Main, Structure > NLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50. - [SDR ASOA20161001056](https://openairdocs.org/sdr/ASOA20161001056.md): Flapper Valve · leaking · Oct 1, 2016 · N13988 · Emb EMB145LR · Fuel Storage > THE CREW REPORTED FUEL STREAMING FROM THE LEFT WING INFLIGHT. MAINTENANCE INSPECTED AND FOUND RIGHT WING FLAPPER VALVE DAMAGED. REPLACED THE FLAPPER VALVE AND OPERATIONAL CHECKS WERE GOOD. - [SDR ASOA20140515064](https://openairdocs.org/sdr/ASOA20140515064.md): Control Panel · inoperative · May 13, 2014 · N13988 · Emb EMB145LR · Emergency Lighting > DURING CRUISE, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE EMERGENCY LIGHTS WERE NOT ARMED. MAINTENANCE R & R THE F/A LIGHTING CONTROL PANEL. THE EMERGENCY LIGHTING SYSTEM OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140513070H](https://openairdocs.org/sdr/ASOA20140513070H.md): Module · inoperative · May 13, 2014 · N13988 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED AN EMERGENCY LIGHTS NOT ARMED EICAS MESSAGE IN FLIGHT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND R & R THE OVERHEAD LIGHT CONTROL MODULE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131126447](https://openairdocs.org/sdr/ASOA20131126447.md): Bleed Valve · stuck · Nov 25, 2013 · N13988 · Emb EMB145LR · Compressor Bleed Valve > AIRCRAFT MADE AN AIR RETURN WHEN THE ENGINE NR 1 SHOWED THAT THE ENGINE 1 BLEED VALVE WAS CLOSED. MAINTENANCE R & R THE NR 1 ENGINE BLEED VALVE REF AMM 36-11-05 AND IPC REF 36-11-05, FIGURE 1A ITEM. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE. - [SDR ASOA20130903066](https://openairdocs.org/sdr/ASOA20130903066.md): Windshield · failed · Sep 3, 2013 · N13988 · Emb EMB145LR · Flight Compartment Windows > THE CREW REPORTED A NR 1 WINDSHIELD FAILED IN FLIGHT ALONG WITH A ELECTRICAL BURNING SMELL. MX INSPECTED AND REPLACED THE NR 1 WINDSHIELD. OPS CHECKS WERE GOOD. THEY ALSO REPLACED THE NR 1 HEAT CONTROLLER AND THE NR 1 WINDSHIELD HEAT CONTACTOR. - [SDR ASOA20130901068](https://openairdocs.org/sdr/ASOA20130901068.md): Unknown · odor · Sep 1, 2013 · N13988 · Emb EMB145LR · Air Distribution System > THE CREW REPORTED A ELECTRICAL BURNING ODOR AFTER WINDSHIELD NR 1 FAIL INFLIGHT. MX INSPECTED AND FOUND NO ELECTRICAL BURNING ODOR. PERFORMED OPS CHECK OF WINDSHIELD HEAT AND NO DEFECTS WERE FOUND. THE ACFT WAS RELEASED FOR SERVICE. - [SDR ASOA20130830065](https://openairdocs.org/sdr/ASOA20130830065.md): Controller · faulty · Aug 30, 2013 · N13988 · Emb EMB145LR · Windshield/Door Rain/Ice Removal > THE CREW REPORTED A BURNING SMELL WHEN WINDSHIELD HEAT NR 2 IS ON. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPS CHECKS WERE GOOD. - [SDR ASOA20130830064C](https://openairdocs.org/sdr/ASOA20130830064C.md): Controller · faulty · Aug 30, 2013 · N13988 · Emb EMB145LR · Windshield/Door Rain/Ice Removal > THE CREW REPORTED BURNING ODOR WITH WINDSHIELD HEAT NR 1 ON. MX INSPECTED AND REPLACED THE NR 1 WINDSHIELD HEAT CONTROLLER. OPS CHECKED GOOD. - [SDR ASOA20130712072R](https://openairdocs.org/sdr/ASOA20130712072R.md): Duct · loose · Jul 12, 2013 · N13988 · Emb EMB145LR · Air Distribution System > CREW REPORTED PACK NR 2 VALVE CLOSED ON EICAS MESSAGE IN FLIGHT WHICH RESULTED IN LOSS OF BOTH AIR CONDITIONING PACKS AND PRESSURIZATION DUE TO NR 1 PACK BEING ON MEL. MX PERFORMED SERVERAL OPERATIONAL CHECKS OF THE PACK NR 2 SYS SUCCESSFUL WITH NO MESSAGES NO - [SDR ASOA20130513075](https://openairdocs.org/sdr/ASOA20130513075.md): Skin · cracked · May 13, 2013 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING A-CK INSPECTION THE AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 6L ON FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR R - [SDR ASOA20130513074](https://openairdocs.org/sdr/ASOA20130513074.md): Skin · cracked · May 13, 2013 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET EBLOW STR 8L AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED F - [SDR ASOA20130513073](https://openairdocs.org/sdr/ASOA20130513073.md): Skin · cracked · May 13, 2013 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 2R AT FR75. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED - [SDR ASOA20130513072](https://openairdocs.org/sdr/ASOA20130513072.md): Skin · cracked · May 13, 2013 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 8R AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FO - [SDR ASOA20130513071](https://openairdocs.org/sdr/ASOA20130513071.md): Skin · cracked · May 13, 2013 · N13988 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STRINGER 4R AT FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPRO - [SDR ASOA20130505034](https://openairdocs.org/sdr/ASOA20130505034.md): Relay · faulty · May 5, 2013 · N13988 · Emb EMB145LR · Emergency Lighting > MX REPORTED THE EMERGENCY LIGHTS WOULD NOT ARM. REPLACED RELAY K0275. OPS CHECKED GOOD. Next page: https://openairdocs.org/aircraft/N13988/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 n_number = 'N13988' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N13988/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.