# Service difficulty reports: N385US, cancelled Sep 6, 2006

A list on [N385US, cancelled Sep 6, 2006](https://openairdocs.org/deregistered/N385US-2006-09-06.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR PIDR2006023](https://openairdocs.org/sdr/PIDR2006023.md): Floorbeam · corroded · Jan 5, 2006 · N385US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > BS 986.5 FLOORBEAM CORRODED AT A PREVIOUS REPAIR FROM RBL14 TO RBL18. REPLACED UPPER T CAP OF FLOORBEAM IAW EA NR 53-264.
- [SDR USAA200507001](https://openairdocs.org/sdr/USAA200507001.md): Skin · cracked · Jul 9, 2005 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CRACK AT BS 767 BETWEEN STRINGERS 21 RT AND 22 RT ON FUSELAGE SKIN. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229, DETAIL X.
- [SDR USAA041075](https://openairdocs.org/sdr/USAA041075.md): Skin · cracked · Dec 12, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - A-CHECK - SKIN, 2 INCH CRACK, STA 760, STR 19R, INSTALLED DOUBLER IAW SRM.
- [SDR SB04159](https://openairdocs.org/sdr/SB04159.md): Odor · detected · Nov 27, 2004 · N385US · Boeing 7373B7 · Cabin Cooling System
  > PHL - FLT1227, EN ROUTE FROM BTV TO PHL, CREW REPORTED A STRONG OIL SMELL IN CABIN. CREW WAS ABLE TO ISOLATE SOURCE TO LEFT PACK/LEFT ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FAULT ISOLATION STEPS FROM MM 21-00-01, PRO
- [SDR USAA040829](https://openairdocs.org/sdr/USAA040829.md): Skin · delaminated · Oct 19, 2004 · N385US · Boeing 7373B7 · Trailing Edge Flaps
  > PIT - C4, IB AFT FLAP SKIN, 3 INCHES BY 2.5 INCH AREA, DELAMINATION, IB AFT FLAP OB T/E LEFT WING. REMOVED SKIN AND CORE, INSTALLED REPAIR AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10.
- [SDR USAA040837](https://openairdocs.org/sdr/USAA040837.md): Skin · delaminated · Oct 19, 2004 · N385US · Boeing 7373B7 · Trailing Edge Flaps
  > PIT - C4, IB AFT FLAP SKIN, 3 INCHES X 2.5 INCHES AREA, DELAMINATION. IB AFT FLAP OB T/E LT WING. REMOVED DELAMINATION, INSTALLED REPAIR CORE, SKIN AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10.
- [SDR USAA040750](https://openairdocs.org/sdr/USAA040750.md): Skin · cracked · Oct 15, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT, C3; SKIN,.2500 INCH CRACK, BETWEEN STR 13/16R AND FRA 947.5. 11 INCH W X 9.5 INCH H FILLER, ALONG WITH 10 INCH W X 13.5 H DOUBLER IAW SRM 53-60-01, FIG 207.
- [SDR USAA040748](https://openairdocs.org/sdr/USAA040748.md): Bulkhead · cracked · Oct 7, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT, C1; SKIN WITH.5 INCH LONG CRACK AT AFT PRESSURE BULKHEAD AT BL0 AND 10 INCHES ABOVE CENTER. INSTALLED DOUBLER IAW SRM 53-80-08.
- [SDR USAA040749](https://openairdocs.org/sdr/USAA040749.md): Skin · cracked · Oct 6, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT, C3; SKIN, (3 EA) CRACKS; 1 INCH, 2.7 INCHES AND 1 INCH, AFT OF 727E-747, S18R. INSTALLED REPAIRS IAW SRM 53-00-01, FIG 228.
- [SDR SB04137](https://openairdocs.org/sdr/SB04137.md): Proximity Sensor · faulty · Oct 2, 2004 · N385US · Boeing 7373B7 · Leading Edge Slat Position Indicating System
  > EWR - FLT 2164 - ON DESCENT INTO LGA FROM DCA, CREW RECEIVED A NR 4 LEADING EDGE KRUGER FLAP AMBER LIGHT ALONG WITH A LEADING EDGE TRANSIT AMBER LIGHT DURING SLAT EXTENSION. CREW RECYCLED FLAPS IN HOPES OF CLEARING THE PROBLEM WITH NO HELP. CREW DECIDED TO D
- [SDR USAA040506](https://openairdocs.org/sdr/USAA040506.md): Beam · cracked · Aug 24, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT - FOUND VERTICAL BEAM CRACKED, VERT CHORD 5.7 LEFT WL 184 STATION 178 FPBH. REMOVED DEFECTIVE PARTS, INSTALLED REPAIR ANGLE PER EO 5300V155. (M)
- [SDR USAASB04077](https://openairdocs.org/sdr/USAASB04077.md): Uplock Sensor · malfunctioned · Jun 25, 2004 · N385US · Boeing 7373B7 · Landing Gear Position and Warning
  > AFTER TAKEOFF FROM GSO, CREW RECEIVED A RIGHT MLG RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW LOWERED GEAR PER QUICK REF HANDBOOK PROCEDURES AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS AND NO RED LIGHTS. FLIGHT LANDED WITHOUT INCIDENT AT CLT
- [SDR USA2004F00050](https://openairdocs.org/sdr/USA2004F00050.md): Flap · malfunctioned · May 17, 2004 · N385US · Boeing 7373B7 · Leading Edge Slat Control System
  > ON APPROACH, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ASSOCIATED WITH A YELLOW TRANSIT LIGHT ON THE NR 3 LEADING EDGE SLAT. CAPTAIN REPORTED THE FLAPS WOULD NOT EXTEND PAST 15 UNITS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AN
- [SDR USAASB04012](https://openairdocs.org/sdr/USAASB04012.md): Controller · malfunctioned · Jan 26, 2004 · N385US · Boeing 7373B7 · Cabin Pressure Controller
  > PIT - FLT 385 - EN ROUTE FROM PHL-MSY, AT FL250, THE CABIN ALTITUDE BEGAN TO CLIMB MODERATELY. FLIGHT DESCENED TO 10,000 FEET WHERE CABIN WAS REGAINED. FLIGHT THEN DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN
- [SDR USAA030318](https://openairdocs.org/sdr/USAA030318.md): Skin · cracked · Dec 11, 2003 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN WRINKLE CRACK 2.5 INCHES LONG, STATION 747 STRINGER 22R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 PG 205, FIG 202. (M)
- [SDR USAASB03206](https://openairdocs.org/sdr/USAASB03206.md): Engine · failed · Nov 23, 2003 · N385US · Boeing 7373B7 · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH 16,000 FT OUT OF BOS, EN ROUTE TO DCA, THE NR 1 ENGINE EXPERIENCED A LOUD BANG. THE AIRCRAFT STARTED TRACKING TO THE LT. CREW DETERMINED NO THRUST WAS BEING PRODUCED FROM THE NR 1 ENGINE, SO THEY FOLLOWED CHECKLIST AND SHUTDOWN THE NR 1 ENGI
- [SDR USAASB03031](https://openairdocs.org/sdr/USAASB03031.md): Light · failed · Feb 28, 2003 · N385US · Boeing 7373B7 · Emergency Lighting
  > ATL - MAINTENANCE REPORTED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACD THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT/SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA020477](https://openairdocs.org/sdr/USAA020477.md): Skin · cracked · Dec 27, 2002 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 3 INCHES LONG, RIGHT SIDE STATION 867 STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAASB02125](https://openairdocs.org/sdr/USAASB02125.md): Wire · pinched · Jun 26, 2002 · N385US · Boeing 7373B7 · Light System Wiring
  > RDU - MAINTENANCE FOUND THE SIDEWALL EMERGENCY EXIT LIGHTS AT THE FORWARD FLIGHT ATTENDANT POSITION AND FORWARD GALLEY POSITION INOPERATIVE. ALSO, FOUND THE AISLE EMERGENCY LIGHTS IN SEAT ROWS 1 THROUGH 4 INOPERATIVE. MAINTENANCE REPAIRED A PINCHED WIRE AT T
- [SDR USAA011376](https://openairdocs.org/sdr/USAA011376.md): Skin · cracked · Nov 19, 2001 · N385US · Boeing 7373B7 · Wing, Plate/Skin
  > PIT - FOUND SKIN CRACKED.5 INCH HOLE, LEFT UPPER WING T/E JUST OUTBOARD OF AILERON. REPLACED PANEL PER SRM 57-51-01 AND EA 72942. (M)
- [SDR USAA011375](https://openairdocs.org/sdr/USAA011375.md): Web · cracked · Nov 19, 2001 · N385US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND DOOR REINFORCING WEB CRACKED 1 INCH, STATION 921, 1 INCH BELOW S11R IN DOOR REINFORCING WEB. REPAIR DOUBLER INSTALLED PER SRM 51-70-13 AND EA 72800. (M)
- [SDR USAA011373](https://openairdocs.org/sdr/USAA011373.md): Skin · cracked · Nov 19, 2001 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.045 INCH DEEP, 3 INCHES LONG BY 2 INCHES WIDE, STATION 420 43 INCHES FORWARD OF CARGO BETWEEN 22R AND 23R. DOUBLER INSTALLED PER SRM 53-00-01. (M)
- [SDR USAA011363](https://openairdocs.org/sdr/USAA011363.md): Skin · delaminated · Nov 12, 2001 · N385US · Boeing 7373B7 · Elevator, Plate/Skin
  > PIT - FOUND RIGHT ELEVATOR HAS DELAMINATION TOP SKIN PEELING 2 SPOTS 7.5 INCHES LONG BY 1 INCH WIDE, INBOARD EDGE 84 INCHES OUTBOARD FROM INBOARD 7.5 INCHES LONG BY 1 INCH WIDE. TRAILING EDGE DAMAGE, DELAMINATED AND TOP SKIN TAPE PEELING IN 2 SPOTS REPAIRED P
- [SDR USAA011377](https://openairdocs.org/sdr/USAA011377.md): Skin · cracked · Nov 5, 2001 · N385US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.5 INCH, STATION 952 STRINGER 11L. INSTALLED DOUBLER PER EA 72801. (M)
- [SDR USAA011374](https://openairdocs.org/sdr/USAA011374.md): Frame · cracked · Oct 26, 2001 · N385US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED 2 INCHES, AT STATION 847 BETWEEN STRINGER 8L-9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAASB01246](https://openairdocs.org/sdr/USAASB01246.md): Battery Pack · inoperative · Sep 2, 2001 · N385US · Boeing 7373B7 · Emergency Lighting
  > LGA- MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY (P/N 11-0049) AND BATTERY PACK ALONG WITH THE FORWARD AND RIGHT FORWARCD BATTERY PACKS. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA011146](https://openairdocs.org/sdr/USAA011146.md): Pressure Panel · cracked · Aug 23, 2001 · N385US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED 1.5 INCH, MAIN W/W PRESSURE DECK AT 664 RBL 40. INSTALLED DOUBLER PER TR 53-60-04. (M)
- [SDR USAA011129](https://openairdocs.org/sdr/USAA011129.md): Web · cracked · Aug 21, 2001 · N385US · Boeing 7373B7 · Wing Structure
  > CLT - FOUND ON WALKAROUND, WEB CRACKED.5 INCH AND.125 INCH, WHEEL WELL CEILING AT LBL 30 BS 685. INSTALLED DOUBLER PER TR 53-60-04. (M)
- [SDR USAASB01124](https://openairdocs.org/sdr/USAASB01124.md): Uplock Sensor · faulty · May 1, 2001 · N385US · Boeing 7373B7 · Landing Gear Position and Warning
  > IAH - FLT 1620 - AFTER TAKEOFF FROM IAH, WHEN THE LANDING GEAR WAS RAISED, CREW RECEIVED TWO GREEN LIGHTS AND A LEFT MLG RED LIGHT. AN UNUSUAL RUMBLE WAS ALSO NOTICED WHILE GEAR WAS BEING RETRACTED. CREW RECYCLED GEAR AND GOT THREE GREEN LIGHTS WHEN GEAR WAS
- [SDR USAASB00363](https://openairdocs.org/sdr/USAASB00363.md): Circuit Breaker · faulty · Dec 30, 2000 · N385US · Boeing 7373B7 · Windshield/Door Rain/Ice Removal
  > CLT - FLT 1775 - EN ROUTE FROM PHL-ORD - THE LEFT FORWARD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES BUT LIGHT REMAINED ILLUMINATED. ICE BEGAN TO FORM ON THE WINDSHIELD SO THE CREW DIVERTED TO CLT. FLIGHT L
- [SDR USAASB00194](https://openairdocs.org/sdr/USAASB00194.md): Downlock Sensor · faulty · Jul 21, 2000 · N385US · Boeing 7373B7 · Landing Gear Position and Warning
  > CLT - FLT 250 - ON PREPARATION FOR LANDING AT CLT FROM PNS, THE RIGHT MLG GREEN LIGHT FLICKERED. WHEN GEAR WAS EXTENDED, THE RED UNSAFE LIGHT ILLUMINATED AND NO GREEN LIGHT. CREW ACCOMPLISHED A GO-AROUND AND MADE A VISUAL CHECK TO CONFIRM THAT THE GEAR WAS D
- [SDR USAA000780](https://openairdocs.org/sdr/USAA000780.md): Strap · cracked · Jun 2, 2000 · N385US · Boeing 7373B7 · Passenger/Crew Doors
  > TPA - FOUND STRIP CRACKED.25 INCH, MAIN ENTRY DOOR, INNER STRUCTURE UPPER HINGE WEB. REPLACED STRAP PER SRM 51-10-2. (M)
- [SDR USAASB00109](https://openairdocs.org/sdr/USAASB00109.md): Valve · failed · Apr 9, 2000 · N385US · Boeing 7373B7 · Cabin Cooling System
  > CLT - FLT 1930 - EN ROUTE FROM PHL TO PBI, CREW NOTIFIED DISPATCH VIA ACARS THATY THEY WERE LOSING CABIN PRESSURE ALTITUDE AND UNABLE TO CONTROL THE PRESSURE LOSS. FLIGHT DESCENDED TO FL140 AND WAS MAINTAINING PRESSURE FOR AWHILE, BUT CABIN BEGAN LOSING PRESS
- [SDR USAA990864](https://openairdocs.org/sdr/USAA990864.md): Stiffener · cracked · Aug 8, 1999 · N385US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - DURING CX3 CONV CHECK, FOUND.5 INCH CRACK IN STIFFENER AT STATION 344 INTERCOSTAL. REPLACED ANGLES PER EA 52604. (M)
- [SDR USAA990863](https://openairdocs.org/sdr/USAA990863.md): Skin · cracked · Aug 8, 1999 · N385US · Boeing 7373B7 · Cargo/Baggage Doors
  > PIT - DURING CX3 CONV CHECK, FOUND CRACK APPROX.500 INCH IN AFT CARGO DOOR, FLAPPER DOOR CUT OUT (A/C SKIN) UPPER AFT CORNER. REPAIRED PER TYPICAL REPAIR 52-10-01 'A' FIG 1. (M)
- [SDR USAA990862](https://openairdocs.org/sdr/USAA990862.md): Floorbeam · cracked · Aug 8, 1999 · N385US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > PIT - DURING CX 3 CONV CHECK, FOUND CRACK APPROX.500 INCH FLOORBEAM AT FS 344 AT LBL 11. REPAIRED PER SRM 53-10-51 AND EA 52604. (M)
- [SDR USAASB99198](https://openairdocs.org/sdr/USAASB99198.md): Charger · failed · Jul 28, 1999 · N385US · Boeing 7373B7 · Emergency Lighting
  > EWR - PILOT REPORTED THAT THE FORWARD ENTRY DOOR EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99163](https://openairdocs.org/sdr/USAASB99163.md): Yaw Damper · failed · Jul 5, 1999 · N385US · Boeing 7373B7 · Autopilot System
  > SDF - FLT 1548 - ON TAKEOFF ROLL FROM SDF, AT APPROX 125 KNOTS, AIRCRAFT EXPERIENCED A BRIEF UNCOMMANDED YAW TO THE RIGHT WITH NO FEEDBACK THROUGH RUDDER PEDALS. AFTER MOMENTARY YAW, REST OF TAKEOFF WAS NORMAL. FLIGHT CONTINUED ON TO PIT WITHOUT FURTHER INCI
- [SDR USAASB99156](https://openairdocs.org/sdr/USAASB99156.md): Battery Pack · discharged · Jun 28, 1999 · N385US · Boeing 7373B7 · Emergency Lighting
  > LGA - FLT 528 - PILOT REPORTED PRIOR TO DEPARTURE, THE FORWARD ENTRY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. BATTERY PACK, P/N 2013-1ALP.
- [SDR 99ZZZX2961](https://openairdocs.org/sdr/99ZZZX2961.md): Charger · inoperable · Jun 28, 1999 · N385US · Boeing 7373B7 · Emergency Lighting
  > LGA - FLT 528 - PILOT REPORTED PRIOR TO DEPARTURE, THE FORWARD ENTRY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. BATTERY PACK, P/N 2013-1ALP.
- [SDR USAA970293](https://openairdocs.org/sdr/USAA970293.md): Skin · cracked · Oct 10, 1997 · N385US · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > CLT - DURING EDDY CURRENT Q-3 CHECK INSPECTION, FOUND 2 CRACKS EACH LESS THAN 2 INCHES LONG NR 2 PYLON AT PANEL 5824R CUT OUT AT PYLON SKIN DOUBLER. INSTALLED DOUBLER PER REPAIR DOCUMENT 54-50-04C. (X)
- [SDR USAA970292](https://openairdocs.org/sdr/USAA970292.md): Floor Beam · corrosion · Oct 10, 1997 · N385US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON STA FLOOR BEAM COVERING APPROXIMATELY 124 INCHES BY 2 INCHES LONG AT 328 FLOOR BEAM FROM LBL 36 TO RBL 58 ON UPPER AND LOWER SURFACE OF T-CAP. INSTALLED T-CAP PER REPAIR DOCUMENT T/R 53-10-03. (X)
- [SDR USAA970291](https://openairdocs.org/sdr/USAA970291.md): Bulkhead · corrosion · Oct 10, 1997 · N385US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT ALL SCREW HOLES.50 INCH BY.50 INCH AT STA 294 ENTIRE LENGTH UPPER CHORD SECTION 41, BULKHEAD. CORROSION TASK NR C53-107-01. INSTALLED SPLICE PER REPAIR DOCUMENT SRM 51-10-51. (X)
- [SDR 97ZZZX4561](https://openairdocs.org/sdr/97ZZZX4561.md): Skin · cracked · Oct 10, 1997 · N385US · Boeing 7373B7 · Cargo/Baggage Doors
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK FROM THE EDGE OF LIGHTENING HOLE ON INTERIOR OF FORWARD CARGO DOOR SKIN IN THE CENTER OF THE DOOR. INSTALLED REPAIR DOUBLERS PER E.A. 60459. (X)
- [SDR USAASB97237](https://openairdocs.org/sdr/USAASB97237.md): Battery Pack · discharged · Aug 23, 1997 · N385US · Boeing 7373B7 · Emergency Lighting
  > CLT - SEVERAL CABIN EMERGENCY LIGHTS EXTINGUISHED PREMATURELY WHEN TESTED ON AN OVERNIGHT CHECK. REPLACED BATTERY ASSEMBLIES AT CHARGERS (M1136) AND (M1197) FOR LOW CAPACITY. (M)
- [SDR USAASB97093](https://openairdocs.org/sdr/USAASB97093.md): Air Distribution · odor · Mar 29, 1997 · N385US · Boeing 7373B7 · Air Distribution System
  > CLT - FL 2314 - AT FL 280, A SMOKE/BURNING ODOR WAS NOTED IN THE MID CABIN. THE ODOR WOULD COME AND GO. CREW COULD NOT ISOLATE ODOR WITH ALTERNATE PACKS OR GALLEY POWER. DECISION WAS MADE TO DIVERT TO CLT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WI
- [SDR USAASB97040](https://openairdocs.org/sdr/USAASB97040.md): Battery Pack · discharged · Feb 5, 1997 · N385US · Boeing 7373B7 · Emergency Lighting
  > ROC - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS WOULD ONLY REMAIN ILLUMINATED FOR APPROXIMATELY 45 SECONDS, FOLLOWING OPERATIONAL CHECK, AT THE FOLLOWING LOCATIONS; MID CABIN BULLNOSE, RIGHT OVERWING HATCH SIGN AND LEFT OVERWING EXTERIOR. MAINTENANCE REMOVE
- [SDR USAASB95028](https://openairdocs.org/sdr/USAASB95028.md): Pressurization · malfunctioned · Dec 17, 1995 · N385US · Boeing 7373B7 · Cabin Pressure Control System
  > FLT 2301 - SYR - ON TAKEOFF, AUTO PRESSURIZATION FAILED. STANDBY WOULD NOT PRESSURIZE THE AIRCRAFT. LEVELED OFF AT 8000 FEET AND RETURNED TO SYR. (M)
- [SDR USAA950971](https://openairdocs.org/sdr/USAA950971.md): Stringer · corroded · Aug 23, 1995 · N385US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - DURING DROP-IN CHECK INSPECTION, VISUALLY FOUND A 5 INCH BY 2 INCH CORRODED AREA LOCATED AT S-25RT FROM STATION 352 TO STATION 357. DROP IN AIRCRAFT. CORROSION LEVEL 2. INSTALLED REPAIR ANGLES. (M)
- [SDR USAA950603](https://openairdocs.org/sdr/USAA950603.md): Actuator · failed · Jun 8, 1995 · N385US · Boeing 7373B7 · Stabilizer Actuator
  > PIT - FLT 1662 - AFTER DEPARTURE, CREW WAS UNABLE TO TRIM STABLIZER WITH THE YOKE SWITCHS. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED STAB TRIM MAIN ELECTRIC ACTUATOR. OPS CHECK NORMAL. (W)

## 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 = 'N385US' AND deregistration_id = 'N385US-2006-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N385US-2006-09-06/reports

---
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