# Service difficulty reports: N17984 A list on [N17984](https://openairdocs.org/aircraft/N17984.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 2 · 72 reports - [SDR ASOA201909063045](https://openairdocs.org/sdr/ASOA201909063045.md): Light · inoperative · Sep 6, 2019 · N17984 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP @ ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10. - [SDR ASOA201905077042](https://openairdocs.org/sdr/ASOA201905077042.md): Trunnion · cracked · May 4, 2019 · N17984 · Emb EMB145LR · Wing, Landing Gear Attach Fittings > RT AFT MLG TRUNNION CRACKED. REMOVED AND REPLACED RT AFT MLG TRUNNION. AIRCRAFT STILL IN C CHECK. - [SDR ASOA201905037041](https://openairdocs.org/sdr/ASOA201905037041.md): Structure · gouged · May 3, 2019 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE APU FIREWALL MOUNTING STRUCTURE AT THE 06:00 POSITION WITH A GOUGE AND POSSIBLE CRACK. MAINTENANCE BLENDED OUT THE DAMAGE AND NO CRACK FOUND, THEN INSTALL A INTERNAL AND EXTERNAL DOUBLER WITH SHIMS FOR THE APU CO - [SDR ASOA201905167047](https://openairdocs.org/sdr/ASOA201905167047.md): Skin · cracked · Apr 29, 2019 · N17984 · Emb EMB145LR · Fuselage Main, Plate/Skin > EXTERIOR SKIN CRACKED AT FRAME 75 STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLERS. AIRCRAFT WAS IN C CHECK AND IS NOW RELEASED AND RETURNED TO SERVICE. - [SDR ASOA201905017040](https://openairdocs.org/sdr/ASOA201905017040.md): Stringer · cracked · Apr 29, 2019 · N17984 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > STRINGER 2L CRACKED AT FRAME 75. CUT OUT DAMAGED AREA AND INSTALLED J-SECTION PER ETD2019-145-055731. AIRCRAFT STILL IN C CHECK. - [SDR ASOA201904237037](https://openairdocs.org/sdr/ASOA201904237037.md): Skin · cracked · Apr 23, 2019 · N17984 · Emb EMB145LR · Fuselage Main, Plate/Skin > A/C IS IN C-CHECK WHEN INSPECTION FOUND THE EXTERIOR SKIN CRACKED AT FRAME 75,STRINGER 2R. MAINTENANCE REPAIRED THE SKIN AT FRAME 75 IAW EMB SRM 53-31-01 REF. FIGURE #219-FUR 53-00-016-72. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA201808231054](https://openairdocs.org/sdr/ASOA201808231054.md): Engine · odor · Aug 21, 2018 · N17984 · Emb EMB145LR · Engine (Turbine/Turboprop) > THE CREW REPORTED A STRONG OIL ODOR FROM THE PACKS AFTER TAKEOFF. MAINTNENACE INSPECTED AND REPLACED THE NR 1 ENGINE IAW TASK CARD 6271001. OPS CHECKED GOOD. - [SDR ASOA201705043132](https://openairdocs.org/sdr/ASOA201705043132.md): Channel · corroded · May 4, 2017 · N17984 · Emb EMB145LR · Service Doors > SERVICE DOOR LOWER CHANNEL CORRODED AROUND ANCHOR NUTS. SERVICE DOOR LOWER CHANNEL REPLACED IAW SRM 51-40-02. - [SDR ASOA201705033130](https://openairdocs.org/sdr/ASOA201705033130.md): Beam · corroded · May 3, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Structure > CARGO DOOR SURROUND STRUCTURE, LOWER BEAM FOUND CORRODED. OUT OF TOLERANCE. THE LOWER BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR ASOA201705033129](https://openairdocs.org/sdr/ASOA201705033129.md): Door Frame · corroded · May 3, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Structure > CORROSION ON PAX DOOR LOWER FRAME AROUND NUT PLATE HOLES. REPAIRED IAW ETD 2017-145-035391. - [SDR ASOA201705013126](https://openairdocs.org/sdr/ASOA201705013126.md): Channel · cracked · May 1, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Bulkhead > RIGHT CHANNEL CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEEL WELL. THE CHANNEL WAS REPLACED IAW SRM 51-40-02. - [SDR ASOA201705013125](https://openairdocs.org/sdr/ASOA201705013125.md): Support · corroded · May 1, 2017 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > SURFACE CORROSION FOUND ON WASTE DRAIN VALVE SUPPORT. WASTE DRAIN VALVE SUPPORT REPLACED IAW SRM 51-40-02. - [SDR ASOA201705013124](https://openairdocs.org/sdr/ASOA201705013124.md): Floorbeam · corroded · May 1, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Floor Beam > FLOORBEAM CORRODED UNDER GUSSET AROUND ANCHOR NUT. THE FLOORBEAM WAS REPAIRED IAW SRM 53-24-10, PAR 3, FIG 202, SHEET 3. - [SDR ASOA201704283123](https://openairdocs.org/sdr/ASOA201704283123.md): Angle · cracked · Apr 28, 2017 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > COCKPIT LEFT FRAME 10, UPPER ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-40-02. - [SDR ASOA201704283122](https://openairdocs.org/sdr/ASOA201704283122.md): Shear Tie · corroded · Apr 28, 2017 · N17984 · Emb EMB145LR · Fuselage Internal Mounting Structure > CARGO DOOR SURROUND STRUCTURE SHEAR TIE CORRODED AT FRAME 65. THE SHEAR TIE WAS REPAIRED IAW SRM 53-31-04, STEP 4F. - [SDR ASOA201704203094](https://openairdocs.org/sdr/ASOA201704203094.md): Crossbeam · cracked · Apr 20, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Structure > NLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50. - [SDR ASOA201704203093](https://openairdocs.org/sdr/ASOA201704203093.md): Crossbeam · cracked · Apr 20, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Structure > NLG UPLOCK FORWARD CROSSBEAM CRACKED. FORWARD CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50. - [SDR ASOA20151021083H](https://openairdocs.org/sdr/ASOA20151021083H.md): Firewall · cracked · Oct 21, 2015 · N17984 · Emb EMB145LR · APU Cowling/Containment > DURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE APU FIREWALL AT APPROXIMATELY THE 2 O'CLOCK POSITION NEAR AN EXISTING DOUBLER. MAINTENANCE REMOVED THE EXISTING DOUBLER AND PERFORMED A COMBINATION REPAIR IAW SRM 53-32-13 AND THE ACFT WAS APPROVED FOR R - [SDR ASOA20150421024C](https://openairdocs.org/sdr/ASOA20150421024C.md): Inverter · inoperative · Apr 21, 2015 · N17984 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS 2-8 AND EXIT SIGN BY MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD. - [SDR ASOA20130901102](https://openairdocs.org/sdr/ASOA20130901102.md): Computer · shorted · Sep 1, 2013 · N17984 · Emb EMB145LR · Independent Position Determining System > ELECTRICAL ODOR REPORTED IN COCKPIT WITH TERRAIN MESSAGE ON EICAS. MX R & R THE EGPWS COMPUTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130731086](https://openairdocs.org/sdr/ASOA20130731086.md): Bracket · unsecure · Jul 31, 2013 · N17984 · Emb EMB145LR · Passenger/Crew Doors > MX REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MX SECURED THE MAIN DOOR HANDLE BRACKET. OPS CHECK OF THE MAIN DOOR SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130730085](https://openairdocs.org/sdr/ASOA20130730085.md): Ground Stud · damaged · Jul 30, 2013 · N17984 · Emb EMB145LR · Light System Wiring > MX REPORTED THE EMERGENCY LIGHTS CAME ON WITH THE CEILING AND SIDEWALL LIGHTS ACTIVATION AND LIGHTS IN ARM POSITION. MX FOUND GROUND STUD GS8008DC TO HAVE BAD GROUND CONNECTION. CLEANED THE SURFACE AND OPS CHECK OF THE EMERGENCY LIGHTS SUCCESSFUL. ACFT WAS - [SDR ASOA20130726082](https://openairdocs.org/sdr/ASOA20130726082.md): Battery Pack · discharged · Jul 26, 2013 · N17984 · Emb EMB145LR · Emergency Lighting > PILOT REPORTED EMERGENCY LIGHTS INOPERATIVE. MX R & R THE NR 3 AND NR 4 EMERGENCY LIGHT SYS BATTERY PACKS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20121230124](https://openairdocs.org/sdr/ASOA20121230124.md): Sensor · faulty · Dec 30, 2012 · N17984 · Emb EMB145LR · Engine Oil Pressure > FLIGHT DIVERTED, CREW REPORTED NR 1 ENGINE OIL PRESSURE IN FLIGHT FLUCTUATED BETWEEN 98-151 PSI. CREW SHUTDOWN ENGINE IN FLIGHT. MX R & R NR1 ENGINE OIL PRESSURE/TEMP SENSOR WITH OPS AND LEAK CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20121015150](https://openairdocs.org/sdr/ASOA20121015150.md): Inverter · inoperative · Oct 11, 2012 · N17984 · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHT FLOOR STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA20120918077](https://openairdocs.org/sdr/ASOA20120918077.md): Inverter · inoperative · Sep 18, 2012 · N17984 · Emb EMB145 · Emergency Lighting > DURING ROUTINE INSPECTION, MX THE FORWARD 3 EMERGENCY AILSE PATH LIGHT STRIPS WERE INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. - [SDR ASOA20120504043](https://openairdocs.org/sdr/ASOA20120504043.md): Fan · odor · May 4, 2012 · N17984 · Emb EMB145LR · Air Distribution Fan > CREW REPORTED AN ELECTRICAL ODOR. INSPECTED AVIONICS BAY AND FOUND RECIRCULATION FANS INOPERATIVE. THE SYS WAS RESET AND OPS CHECKED GOOD. NO ELECTRICAL ODOR WAS FOUND. - [SDR C2XA11IA160](https://openairdocs.org/sdr/C2XA11IA160.md): Light · inoperative · Jul 25, 2011 · N17984 · Emb EMB145LR · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATOINALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11CL148](https://openairdocs.org/sdr/C2XA11CL148.md): Inverter · faulty · Jun 20, 2011 · N17984 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY EXIT SIGN AT THE OVERWING ESCAPE HATCH WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11SH073](https://openairdocs.org/sdr/C2XA11SH073.md): Fitting · loose · Mar 26, 2011 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK VERTICAL STAB SPAR 1 ATTACHMENT AT FRAME 75 SHOWS SIGNS OF MOVEMENT AT O/B AREAS (INSIDE AFT AVIONICS BAY). MAINTENANCE PERFORMED REPAIR OF FRAME 75 FITTING IAW EMB-145 EC5310-01317 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH072](https://openairdocs.org/sdr/C2XA11SH072.md): Structure · damaged · Mar 26, 2011 · N17984 · Emb EMB145LR · Cargo/Baggage Doors > SHV - DURING C-CHECK CARGO DOOR INNER STRUCTURE BELOW FWD PULLEY HAS MISS DRILL DAMAGE. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR INNER STRUCTURE AND RESTORED TO ORIGINAL FINISH IAW EMB-145 EC5230-01208 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV - [SDR C2XA11SH071](https://openairdocs.org/sdr/C2XA11SH071.md): Hinge · gouged · Mar 26, 2011 · N17984 · Emb EMB145LR · Rudder Structure > SHV - DURING C-CHECK RUDDER II LOWER CENTER HINGE HAS A GOUGE. MAINTENANCE REMOVED AND REPLACED RUDDER II LOWER CENTER HINGE IAW EC5540-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH070](https://openairdocs.org/sdr/C2XA11SH070.md): Door Frame · corroded · Mar 23, 2011 · N17984 · Emb EMB145LR · Fuselage Main, Structure > SHV - DURING C-CHECK SERVICE DOOR AFT CUTOUT HAS CORROSION AT LOWER NUT PLATE HOLE. REPAIRED FRAME IAW EC5310-01548. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH069](https://openairdocs.org/sdr/C2XA11SH069.md): Frame · corroded · Mar 23, 2011 · N17984 · Emb EMB145LR · Fuselage Main, Frame > SHV - DURING C-CHECK FRAME 65 HAS AREAS OF CORROSION. REPAIRED FRAME IAW EC5310-01505. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10CL169](https://openairdocs.org/sdr/C2XA10CL169.md): Computer · faulty · Nov 13, 2010 · N17984 · Emb EMB145LR · Integrated Flight System > EWR FLT 2940 THE CREW REPORTED GLIDESLOPE ISSUES GOING INTO DTW. REPORTED A 1/2 DOT DIFFERENCE BETWEEN GLIDESLOPE INDICATIONS DURING CAT II GS COMPARATIVE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR - [SDR C2XA09IA272](https://openairdocs.org/sdr/C2XA09IA272.md): Sealant · odor · Oct 27, 2009 · N17984 · Emb EMB145LR · Pitot/Static System > IAH - FLIGHT 2886, THE CREW REPORTED A BURNING SMELL WHILE TAXIING IN AND WAS STRONGER IN INTENSITY AS THE PARKING BRAKE WAS SET, AND WAS FOUND TO BE STRONGER IN THE MAIN CABIN DOOR / GALLEY AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SMELL TO BE C - [SDR C2XA09SH070](https://openairdocs.org/sdr/C2XA09SH070.md): Door Frame · corroded · Mar 1, 2009 · N17984 · Emb EMB145 · Fuselage Main, Structure > SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM AREA CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07CL093](https://openairdocs.org/sdr/C2XA07CL093.md): Uplock · faulty · Nov 3, 2007 · N17984 · Emb EMB145LR · Landing Gear Retraction/Extension System > CLE FLIGHT 2251 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING IN FLIGHT. THE AIRCRAFT DIVERTED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA07RI069](https://openairdocs.org/sdr/C2XA07RI069.md): Light · inoperative · Aug 16, 2007 · N17984 · Emb EMB145LR · Emergency Lighting > RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LIGHTS AT ROW 3 AND ROW 14 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS IAW EMB145 AMM 33-50-08 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07IA131](https://openairdocs.org/sdr/C2XA07IA131.md): Proximity Switch · inoperative · Jun 5, 2007 · N17984 · Emb EMB145LR · Landing Gear Position and Warning > IAH - FLIGHT 2598, THE CREW REPORTED A LOUD NOISE AND VIBRATION IN THE NOSE ARE DURING CRUISE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND - [SDR C2XA07IA120](https://openairdocs.org/sdr/C2XA07IA120.md): Brake Assy · malfunctioned · May 18, 2007 · N17984 · Emb EMB145LR · Landing Gear Brake System > IAH - FLIGHT 2528, THE CREW REPORTED A -BRK OUTBD- MESSAGE ON EICAS ON FINAL APPROACH, AND THAT THE OUTBOARD BRAKES DID NOT WORK ON ROLLOUT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BRAKES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPRO - [SDR C2A07SH028](https://openairdocs.org/sdr/C2A07SH028.md): Floor Support · corroded · May 13, 2007 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM FROM FR 20 TO 23. MX REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA06CL063](https://openairdocs.org/sdr/C2XA06CL063.md): Proximity Switch · faulty · Jun 27, 2006 · N17984 · Emb EMB145LR · Landing Gear Position and Warning > CLE FLIGHT 3245 THE CREW REPORTED LOUD NOISE FROM NOSE GEAR AREA DURING CLIMBOUT ABOVE 1700 AND DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT. THE NLG DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECKS WE - [SDR C2XA05RI017](https://openairdocs.org/sdr/C2XA05RI017.md): Wire Harness · burned · Aug 8, 2005 · N17984 · Emb EMB145LR · Light System Wiring > FLT 2969 - RIC - PRE-FLIGHT - DURING PRE-FLIGHT INSPECTION, SIDE WALL LIGHT AT SEAT 2A WAS SMOKING. RIC MAINTANACE REMOVED AND REPLACED LAMP HARNESS ASSY AND PERFORMED OPERATIONAL TESTS. OPS TEST GOOD. ACFT WAS APPROVED TO RETURNED TO SERVICE. - [SDR C2XA05SH041](https://openairdocs.org/sdr/C2XA05SH041.md): Floor Support · corroded · May 23, 2005 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C CHECK, PREVIOUS REPAIR TO LT OMEGA BEAM AT FS 20 WAS FOUND TO BE CORRODED. MX REMOVED DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-40-02, EC5320-01140 AND EC 5320-01137. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR C2XA05SH042](https://openairdocs.org/sdr/C2XA05SH042.md): Floor Support · corroded · May 23, 2005 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK THE RT OMEGA BEAM NUT PLATE IS CORRODED JUST AFT OF FRAME 23. MAINTENANCE INSTALLED HAT BEAM REPAIR ON RT OMEGA BEAM AT NUT PLATE HOLE AFT OF FR 23 IAW EMB SRM 53-21-10 FIG 206. INSTALLED NUT PLATE IAW EC 5320-01137. THE AIRCRAFT WAS AP - [SDR C2XA05RI001](https://openairdocs.org/sdr/C2XA05RI001.md): Light · burned out · Jan 13, 2005 · N17984 · Emb EMB145LR · Emergency Lighting > RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT FLOOR STRIP, BY SEAT 6A, INOP. MAINTENANCE REMOVED AND REPLACED STRIP. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA04BT091](https://openairdocs.org/sdr/C2XA04BT091.md): Odor · detected · Aug 15, 2004 · N17984 · Emb EMB145LR · Air Distribution System > CREW REPORTED, (STRONG FUEL ODOR IN AIRCRAFT WHILE APU IS RUNNING.) MAINTENANCE TROUBLESHOT NO DEFECTS FOUND AND PLACED THE AIRCRAFT ON MEL FOR FURTHER FOLLOWUP. STL MAINTENANCE OPS. CHECKED THE APU WITH BOTH PACKS NR 1 AND NR 2 RUNNING FOR 30 MINUTES, NO - [SDR C2XA03TY073](https://openairdocs.org/sdr/C2XA03TY073.md): Angle · corroded · May 20, 2003 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLE - [SDR C2XA03TY072](https://openairdocs.org/sdr/C2XA03TY072.md): Angle · corroded · May 20, 2003 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT C Next page: https://openairdocs.org/aircraft/N17984/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 = 'N17984' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N17984/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.