# Service difficulty reports: N392US, cancelled Apr 10, 2006 A list on [N392US, cancelled Apr 10, 2006](https://openairdocs.org/deregistered/N392US-2006-04-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAA200507004](https://openairdocs.org/sdr/USAA200507004.md): Skin · cracked · Jul 12, 2005 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > 5 IN CRACK FOUND BETWEEN FRAME 727D AND 727E STR 24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. - [SDR USAA200507003](https://openairdocs.org/sdr/USAA200507003.md): Frame · cracked · Jul 11, 2005 · N392US · Boeing 7373B7 · Fuselage Main, Frame > 1.5 IN CRACK FOUND AT FRAME 767, STR 24L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229. - [SDR SB05059](https://openairdocs.org/sdr/SB05059.md): Battery · discharged · May 11, 2005 · N392US · Boeing 7373B7 · Emergency Lighting > CLT FOUND EXTERIOR EMERGENCY LIGHTS AFT OF THE WINGS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. - [SDR USAA041077](https://openairdocs.org/sdr/USAA041077.md): Skin · delaminated · Dec 10, 2004 · N392US · Boeing 7373B7 · Wing, Plate/Skin > PIT - WALKAROUND- WING T/E, 8 INCH X 12 INCH AREA, DELAMINATION, UPPER PANEL OB RT FIXED T/E OF WING. REPLACED PANEL IAW SRM AND EA. - [SDR SB04142](https://openairdocs.org/sdr/SB04142.md): Light · loose · Oct 10, 2004 · N392US · Boeing 7373B7 · Emergency Lighting > CLT - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE IN SOCKET. SECURED BULB. OPERATIONAL CHECK GOOD. - [SDR USAA040243](https://openairdocs.org/sdr/USAA040243.md): Skin · cracked · Jun 1, 2004 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > SKIN CRACKED (1 INCH X Q.22 INCH) LOWER AFT CORNER FORWARD SERV CUTOUT STA 322, 4 INCH/ 14 INCH. INSTALLED DOUBLERS IAW SRM. - [SDR USA2004F00007](https://openairdocs.org/sdr/USA2004F00007.md): Indicator · failed · Feb 9, 2004 · N392US · Boeing 7373B7 · Attitude and Direction Data System > SHORTLY AFTER TAKEOFF, ENROUTE, THE F/O ADI FAILED. CREW REPORTED THE CIRCUIT BREAKER WAS TRIPPED AND THAT A SLIGHT ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTEN - [SDR USAASB03216](https://openairdocs.org/sdr/USAASB03216.md): Charger · failed · Dec 16, 2003 · N392US · Boeing 7373B7 · Emergency Lighting > MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 22 AND AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND REPLACED ALL BULBS. OPERATIONAL CHECK GOOD. (M) - [SDR USAA030132](https://openairdocs.org/sdr/USAA030132.md): Skin · cracked · Jul 25, 2003 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 2 INCHES, S23L AND BS 727E. INSTALLED DOUBLER PER EA 94536. (M) - [SDR USAA030208](https://openairdocs.org/sdr/USAA030208.md): Skin · corroded · May 15, 2003 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > PIT - FOUND ON WALKAROUND SKIN AND KEEL BEAMS CORRODED 1 FT BY.5 INCH AREA, AT FASTENERS STATION 727, L STR 27 AND R STR 28. REPLACED LEFT AND RIGHT BEAMS SPLICED AT STATION 540 PER TYP REP 53-60-07 AND EA 76192. CORROSION LEVEL 2, TASK NR C53-212-01. (M) - [SDR USAA030028](https://openairdocs.org/sdr/USAA030028.md): Skin · cracked · Mar 21, 2003 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED 1 INCH IN LENGTH, AFT SERVICE DOOR, UPPER HINGE CUTOUT. REMOVED CRACK AND INSTALLED DOUBLER PER TR 52-10-13 AND EA 75742. (M) - [SDR USAASB03019](https://openairdocs.org/sdr/USAASB03019.md): Sensor · malfunctioned · Feb 6, 2003 · N392US · Boeing 7373B7 · Landing Gear Position and Warning > PIT - FLT 1963 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR LEVER WOULD NOT MOVE TO RETRACT GEAR. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ADJUSTED THE GROUND SPOILER BYPASS/GROUND SENSE TELE - [SDR USAASB03018](https://openairdocs.org/sdr/USAASB03018.md): Sensor · malfunctioned · Feb 5, 2003 · N392US · Boeing 7373B7 · Landing Gear Position and Warning > PIT - FLT 231 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR LEVER WOULD NOT MOVE TO RETRACT GEAR. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED - [SDR USAASB02229](https://openairdocs.org/sdr/USAASB02229.md): Iru · failed · Dec 23, 2002 · N392US · Boeing 7373B7 · Inertial Guidance System > PIT - FLT 1004 - AFTER TAKEOFF FROM PIT, EN ROUTE TO MKE, THE LEFT IRS FAILED IN FLIGHT. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT INERTIAL REF - [SDR USAA020106](https://openairdocs.org/sdr/USAA020106.md): Angle · cracked · Feb 17, 2002 · N392US · Boeing 7373B7 · Fuselage Miscellaneous Structure > PIT - FOUND ANGLE CRACKED 2 INCHES, FORWARD OF STATION 345. REPLACED ANGLE PER SRM 31-70-12. (M) - [SDR USAA020107](https://openairdocs.org/sdr/USAA020107.md): Skin · cracked · Feb 17, 2002 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E PLUS 3 INCHES AT S18R. INSTALLED DOUBLER PER SRM 53-00-01 AND 51-20-05. (M) - [SDR USAA020108](https://openairdocs.org/sdr/USAA020108.md): Floorbeam · broken · Feb 17, 2002 · N392US · Boeing 7373B7 · Fuselage Main, Floor Beam > PIT - FOUND WEB BROKEN IN HALF, MAIN FRAME BROKE IN HALF STATION 639 FLOOR LEVEL. REMOVED AND REPLACED WEB PER EA 73114. (M) - [SDR USAA020103](https://openairdocs.org/sdr/USAA020103.md): Frame · corroded · Feb 4, 2002 · N392US · Boeing 7373B7 · Fuselage Main, Frame > PIT - FOUND FRAME CORRODED 6 INCHES BY.5 INCHES, RBL 8.10 BETWEEN STATION 727E AND 772. CORROSION LEVEL 1. REPAIRED PER TYPICAL REPAIR 53-10-06B. (M) - [SDR USAA020070](https://openairdocs.org/sdr/USAA020070.md): Doubler · cracked · Jan 24, 2002 · N392US · Boeing 7373B7 · Fuselage Main, Structure > PIT - FOUND DOUBLER CRACKED.5 INCHES AREA AND 1 INCH AREA BENT, LIP FOR A/C DOOR, STATION 490 BL 0. INSTALLED DOUBLER PER TR 53-30-05 AND EA 73180. (M) - [SDR USAA020071](https://openairdocs.org/sdr/USAA020071.md): Web · corroded · Jan 24, 2002 · N392US · Boeing 7373B7 · Fuselage Miscellaneous Structure > FOUND SUPPORTS AND WEB CORRODED 36 INCHES BY 3 INCHES AREA, STATION 300-340 MAIN ENTRY THRESHOLD. CORROSION LEVEL 2, TASK NR C53-107-0. REMOVED AND REPLACED SUPPORTS AND WEB PER SRM 53-10-15. (M) - [SDR USAA020105](https://openairdocs.org/sdr/USAA020105.md): Channel · cracked · Dec 30, 2001 · N392US · Boeing 7373B7 · Nacelle/Pylon Structure > PIT - FOUND CHANNEL CRACKED 12 INCHES, STATION 345-363. DEFECTIVE PART REPLACED WITH IDENTICAL P/N, REPLACED CHANNEL PER NR 313A1355. (M) - [SDR USAASB00146](https://openairdocs.org/sdr/USAASB00146.md): Relief Valve · misinstalled · May 21, 2000 · N392US · Boeing 7373B7 · Hydraulic Pressure Relief Valve, Main > CLT - WHILE ON THE GATE AT CLT, THE A SYSTEM HYDRAULIC RESERVOIR EXPLODED. MAINTENANCE FOUND THE PRESSURE RELIEF VALVE INSTALLED IMPROPERLY. THE VALVE AND RESERVOIR WERE REPLACED. (M) - [SDR USAA990622](https://openairdocs.org/sdr/USAA990622.md): Skin · cracked · Jun 21, 1999 · N392US · Boeing 7373B7 · Fuselage Main, Plate/Skin > CLT - DURING METRO MOD, FOUND 2 INCH LONG CRACK ON SKIN AT STATION 727B STRINGER 16L. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAASB99079](https://openairdocs.org/sdr/USAASB99079.md): Engine · failed · Mar 21, 1999 · N392US · Boeing 7373B7 · Engine (Turbine/Turboprop) > CLT - FLT 858 - FLIGHT RETURNED TO FIELD AT CLT DUE TO A 6 INCH THROTTLE SPLIT AND A NR 1 EGINE OVERTEMP. DURING TAKEOFF ROLL, THE CREW GOT THE THROTTLE SPLIT AS THEY APPROACHDED TAKEOFF SPEED. CREW CONTINUED THE TAKEOFF BECAUSE THEY HAD GOOD TAKEOFF POWER. - [SDR USAASB98311](https://openairdocs.org/sdr/USAASB98311.md): Light · inoperative · Nov 23, 1998 · N392US · Boeing 7373B7 · Emergency Lighting > GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT THE FORWARD SERVICE DOOR AND THE CHARGER ASSEMBLY AND M1134 BATTERY PACK FOR - [SDR 98ZZZM948](https://openairdocs.org/sdr/98ZZZM948.md): Battery Pack · discharged · Nov 23, 1998 · N392US · Boeing 7373B7 · Emergency Lighting > GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT THE FORWARD SERVICE DOOR AND THE CHARGER ASSEMBLY AND M1134 BATTERY PACK FOR - [SDR 98ZZZM947](https://openairdocs.org/sdr/98ZZZM947.md): Charger · inoperative · Nov 23, 1998 · N392US · Boeing 7373B7 · Emergency Lighting > GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT THE FORWARD SERVICE DOOR AND THE CHARGER ASSEMBLY AND M1134 BATTERY PACK FOR - [SDR USAA980320](https://openairdocs.org/sdr/USAA980320.md): Floorbeam · corroded · Jul 26, 1998 · N392US · Boeing 7373B7 · Fuselage Main, Floor Beam > CLT - DURING Q-3 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 4 INCH CORROSION TOP OF FLANGE STA 312 CENTERLINE FLOORBEAM. CORROSION TASK NR C 53-107-01. INSTALLED SPLICE PER REPAIR DOCUMENT SRM 53-10-03. (X) - [SDR USAA980319](https://openairdocs.org/sdr/USAA980319.md): Floorbeam · corroded · Jul 26, 1998 · N392US · Boeing 7373B7 · Fuselage Main, Floor Beam > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION TOP OF FLANGE FLOORBEAM AT STA 312 RBL 30. CORROSION TASK NR C53-107-01. INSTALLED SPLICE PER SRM 53-10-03. (X) - [SDR USAA980318](https://openairdocs.org/sdr/USAA980318.md): Frame · cracked · Jul 26, 1998 · N392US · Boeing 7373B7 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1.50 INCH CRACK 727D BETWEEN STRINGERS 27 LT AND RT OF FRAME. INSTALLED DOUBLER, NEW SHEAR TIES AND FLOOR ANGLE SUPPORTS PER SRM 53-00-07 FIG 203. (X) - [SDR USAASB98149](https://openairdocs.org/sdr/USAASB98149.md): Battery Pack · discharged · Jun 12, 1998 · N392US · Boeing 7373B7 · Emergency Lighting > PIT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97029](https://openairdocs.org/sdr/USAASB97029.md): Tr Unit · failed · Jan 25, 1997 · N392US · Boeing 7373B7 · DC Rectifier/Converter > ILM - FL 1505 - EN ROUTE FROM BOS-FLL OVER ILM, AT FL 310, FLT LOST A TRANSFORMER/RECTIFIER. RESULT WAS COMPLETE INSTRUMENTATION LOSS ON CAPTAINS SIDE AND PARTIAL LOSS ON F/O'S SIDE. ALSO, LOST AUTO AND STANDBY PRESSURIZATION CONTROL, MANUAL MODE WAS OK. AT - [SDR USAASB95016](https://openairdocs.org/sdr/USAASB95016.md): Bleed Vlv · failed · Nov 19, 1995 · N392US · Boeing 7373B7 · Compressor Bleed Control > MCO - FLT NR 378 - NR 2 ENGINE OVERTEMPED ON TAKEOFF TO 944 DEGREES FOR 2 SECONDS. FLIGHT CREW REDUCED POWER AFTER TAKEOFF TO BELOW RED LINE. CREW COULD NOT SELECT NORMAL CLIMB N1 WITHOUT EGT EXCEEDANCE. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTEN ## 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 = 'N392US' AND deregistration_id = 'N392US-2006-04-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N392US-2006-04-10/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.