# Service difficulty reports: N827US, cancelled May 16, 2006 A list on [N827US, cancelled May 16, 2006](https://openairdocs.org/deregistered/N827US-2006-05-16.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 · 53 reports - [SDR USAAD02012](https://openairdocs.org/sdr/USAAD02012.md): Battery · inoperative · Mar 13, 2002 · N827US · Doug DC981 · Emergency Lighting > IND - SOME OF THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD02010](https://openairdocs.org/sdr/USAAD02010.md): Light · inoperative · Feb 19, 2002 · N827US · Doug DC981 · Emergency Lighting > IND - SEVERAL SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR 2001F00740](https://openairdocs.org/sdr/2001F00740.md): Light · inoperative · Dec 6, 2001 · N827US · Doug DC981 · Emergency Lighting > IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHTS AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EME - [SDR 2001F00739](https://openairdocs.org/sdr/2001F00739.md): Battery · discharged · Dec 6, 2001 · N827US · Doug DC981 · Emergency Lighting > IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHTS AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EME - [SDR USAAD01186](https://openairdocs.org/sdr/USAAD01186.md): Battery · discharged · Dec 6, 2001 · N827US · Doug DC981 · Emergency Lighting > IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHTS AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EME - [SDR USAA010921](https://openairdocs.org/sdr/USAA010921.md): Fitting · cracked · Jun 29, 2001 · N827US · Doug DC981 · Doors > PIT - FOUND FITTING CRACKED 4.5 INCHES, MAIN ENTRY DOOR UPPER HINGE FITTING BROKEN AT BASE. REPLACED WITH IDENTICAL PART NR. (M) - [SDR USAA010808](https://openairdocs.org/sdr/USAA010808.md): Frame · cracked · Jun 27, 2001 · N827US · Doug DC981 · Fuselage Main, Structure > PIT - FOUND FRAME CRACKED 2 INCHES, CANTED STATION 1485 AT LONGERON 3L. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M) - [SDR 2001F00000](https://openairdocs.org/sdr/2001F00000.md): Battery · discharged · May 14, 2001 · N827US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01103. (M) - [SDR USA2001F00003](https://openairdocs.org/sdr/USA2001F00003.md): Battery · discharged · May 14, 2001 · N827US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01103. (M) - [SDR USAAD01103](https://openairdocs.org/sdr/USAAD01103.md): Battery · discharged · May 14, 2001 · N827US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD01030](https://openairdocs.org/sdr/USAAD01030.md): Battery · discharged · Feb 16, 2001 · N827US · Doug DC981 · Emergency Lighting > TPA - DURING A TEST OF THE EMERGENCY LIGHTS, ROW 25 UNDER SEAT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. A BATTERY WAS REPLACED. OPERATIONALLY CHECKED OK. (M) - [SDR USAAD00188](https://openairdocs.org/sdr/USAAD00188.md): Duct · cracked · Dec 29, 2000 · N827US · Doug DC981 · Air Distribution System > PIT-PBI - FLT 1947 - AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED A LOUD BANG FROM THE TAIL AREA, ALSO SMOKE IN THE TAIL CONE AND CABIN. NO UNUSUAL COCKPIT INDICATIONS WERE NOTED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE R - [SDR USAAD00184](https://openairdocs.org/sdr/USAAD00184.md): Bottle · discharged · Dec 1, 2000 · N827US · Doug DC981 · Escape Slide > MCO - THE TAILCONE SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE TAILCONE SLIDE ASSY. (M) - [SDR USAAD00163](https://openairdocs.org/sdr/USAAD00163.md): Strut · leaking · Oct 6, 2000 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > PIT-AVP - FLT 671 - AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY. (M) - [SDR USAAD00159](https://openairdocs.org/sdr/USAAD00159.md): Strut · damaged · Oct 6, 2000 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > BNA-PIT - FLT 548 - AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RAISED, THE NOSE GEAR LIGHT INDICATED UNSAFE AND A LOUD NOISE WAS HEARD. AT THE SAME TIME, THE AIRCRAFT DEPRESSURIZED. THE FLIGHT DECLARED AND EMERGENCY AND RETURNED TO THE FIELD TO MAKE AND UNEVEN - [SDR USAAD00083](https://openairdocs.org/sdr/USAAD00083.md): Valve · leaking · May 25, 2000 · N827US · Doug DC981 · Drag Control System > BNA-PHL - FLT 478 - DURING CLIMB-OUT, THE RIGHT HYDRAULIC SYSTEM QUANTITY WAS LOST. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. A MANUAL LANDING GEAR EXTENSION WAS REQUIRED. MAINTENANCE REPLACED THE RIGHT SPOILER CONTROL VALVE. (M) - [SDR USAAD00027](https://openairdocs.org/sdr/USAAD00027.md): Seal · leaking · Feb 9, 2000 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > MSP-CLT - FLT 1631 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR STRUT SEALS. (M) - [SDR USAAD00004](https://openairdocs.org/sdr/USAAD00004.md): Unknown · odor · Jan 15, 2000 · N827US · Doug DC981 · Air Distribution System > MKE-PIT - FLT 1845 - AFTER ARRIVAL IN PIT, THE FLIGHT ATTENDANTS REPORTED SMELLING FUMES, THE ODOR OF FUEL AND EXHAUST DURING FLIGHT. MAINTENANCE RAN THE ENGINES AND THE APU TO CHECK FOR FUEL LEAKS. NO LEAKS WERE FOUND. THE ACM OIL LEVELS CHECKED NORMAL. B - [SDR USAAD99176](https://openairdocs.org/sdr/USAAD99176.md): Actuator · failed · Dec 11, 1999 · N827US · Doug DC981 · Pressure Regulator/Outflow Valve > PIT/TPA - FLT 1845 - WHILE CRUISING AT 35,000 FEET, THE CABIN ALTITUDE SLOWLY CLIMBED TO 10,000. AFTER CREW WAS UNABLE TO CONTROL THE CABIN ALTITUDE MANUALLY, AN EMERGENCY DESCENT WAS INITIATED AND THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MA - [SDR USAAD99100](https://openairdocs.org/sdr/USAAD99100.md): Power Supply · failed · Jul 22, 1999 · N827US · Doug DC981 · Emergency Lighting > IND - THE CEILING EMERGENCY LIGHTS ADJACENT TO THE AFT SERVICE DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY. (X) - [SDR USAA990253](https://openairdocs.org/sdr/USAA990253.md): Frame · corroded · Mar 11, 1999 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURIGN C5 CHECK, FOUND 1 INCH AREA OF CORROSION ON AND AROUND FASTENER HOLE AT AFT CARGO DOOR FRAME, FORWARD STRAP FASTENER HOLE IN LINE WITH LONGERON 28R. INSTALLED STRAP ASSEMBLY PER EA NR 51730. (M) - [SDR USAA990252](https://openairdocs.org/sdr/USAA990252.md): Frame · corroded · Mar 11, 1999 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING C5 CHECK, FOUND 1 INCH AREA OF CORROSION ON AND AROUND FASTENER HOLE AT AFT CARGO DOOR FRAME, AFT STRAP FASTENER HOLE LONGERON 28R. INSTALLED STRAP ASSEMBLY PER EA NR 51730. (M) - [SDR USAA990251](https://openairdocs.org/sdr/USAA990251.md): Skin · corroded · Mar 11, 1999 · N827US · Doug DC981 · Trailing Edge Flaps > PIT - DURING C5 CHECK, FOUND 1 INCH LONG, 1 INCH WIDE,.011 DENT AND 1 INCH LONG, 1 INCH WIDE,.009 DEEP DENT AT RIGHT WING INBOARD FLAP, AFT SIDE, MIDDLE OF TOP CENTER SKIN PANEL. CORROSION LEVEL 1. CLEANED AND TREATED CORROSION PER SRM CHAP 51. (M) - [SDR USAAD99029](https://openairdocs.org/sdr/USAAD99029.md): Coalescer Bag · dirty · Feb 18, 1999 · N827US · Doug DC981 · Humidity Control System > BOS-BUF - FLT 1022 - AFTER LANDING AT BUF THE FLIGHT CREW REPORTED FUMES IN THE FORWARD GALLEY AND COCKPIT 25 MINUTES AFTER TAKEOFF. SUSPECTED THE LEFT AIR CONDITIONING PACK AS THE SOURCE. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND REPLACED THE WATE - [SDR USAAD98139](https://openairdocs.org/sdr/USAAD98139.md): Sensor · malfunctioned · Aug 6, 1998 · N827US · Doug DC981 · Landing Gear Door Retract Section > CLT - FLT 995 - AFTER TAKEOFF FROM CLT AND GEAR RETRACTION, THE GEARS DOOR LIGHTS REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR AND RECEIVED THE SAME INDICATION. THE FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT - [SDR USAAD98097](https://openairdocs.org/sdr/USAAD98097.md): Engine · failed · May 30, 1998 · N827US · Doug DC981 · Engine (Turbine/Turboprop) > MCO - FLT 2292 - DURING CLIMB-OUT, THERE WAS A LOUD BANG FROM THE LEFT ENGINE AND THE N1 INDICATION DECREASED. THE VIBRATION INDICATION WENT OFF SCALE ON THE HIGH SIDE. THE ENGINE THROTTLE WAS RETURNED TO IDLE, THE AIRCRAFT RETURNED TO THE FIELD AND LANDED W - [SDR USAAD97224](https://openairdocs.org/sdr/USAAD97224.md): Power Supply · inoperative · Nov 24, 1997 · N827US · Doug DC981 · Emergency Lighting > PHL - EMERGENCY LIGHTS INOPERATIVE AT ROWS 27 THROUGH 30. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) - [SDR USAAD97168](https://openairdocs.org/sdr/USAAD97168.md): Bulbs · failed · Sep 28, 1997 · N827US · Doug DC981 · Landing Gear Position and Warning > PIT - FL 1640 - ON APPROACH, CREW DID NOT RECEIVE THE LEFT MAIN LANDING GEAR DOWN AND LOCKED LIGHT. CREW CYCLED THE GEAR WITH SAME RESULT. CREW SUBSTITUED SIMILAR LIGHTS FROM AND FOUND THAT THE ORIGINAL LIGHT BULBS WERE BURNED OUT. FLIGHT LANDED NORMALLY AT - [SDR USAAD97108](https://openairdocs.org/sdr/USAAD97108.md): Duct · failed · Jun 21, 1997 · N827US · Doug DC981 · Cabin Cooling System > PIT/MDT - FLT 1672 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO FIELD. REPLACED 4 INCH RUBBER DUCT ON BOTH PACKS. (X) - [SDR USAAD97091](https://openairdocs.org/sdr/USAAD97091.md): Strut · req'd service · May 19, 1997 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/Axle > FLT 441 - PIT-ORD - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR, AND NOSE STILL WOULD NOT RETRACT. RETURNED TO PIT. SERVICED NOSE STRUT WITH NITROGEN. (M) - [SDR USAAD97087](https://openairdocs.org/sdr/USAAD97087.md): Power Supply · failed · May 18, 1997 · N827US · Doug DC981 · Emergency Lighting > IND - FOUND LAST ROW OF EMERGENCY TRACK LIGHTING INOPERATIVE. REPLACED POWER SUPPLY. (M) - [SDR USAAD96145](https://openairdocs.org/sdr/USAAD96145.md): Battery Pack · discharged · Sep 27, 1996 · N827US · Doug DC981 · Emergency Lighting > TAIL COMPARTMENT EMERGENCY LIGHTS DIM. REPLACED BOTH BATTERY PACKS IN RIGHT AFT LAVATORY. (M) - [SDR USAA950968](https://openairdocs.org/sdr/USAA950968.md): Fitting · corroded · Aug 24, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND 3 INCH BY 6 INCH AREA OF CORROSION LEVEL 2 IN CUSP ANGLE AT MED FRAME LOWER ATTACH FITTING STATION 200. CORROSION TASK NR C46-53303. REMOVED CORRODED SECTION AND SPLICED NEW SECTION IN PER USAIR EA 31153. (M) - [SDR USAA950988](https://openairdocs.org/sdr/USAA950988.md): Jamb · corroded · Aug 23, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED FORWARD CARGO DOOR JAMB PAN ALONG BOTTOM EDGE BETWEEN PAN AND FUSELAGE SKIN CORROSION REF C51-53300. REMOVED LOWER SECTION OF DOOR JAMB AND SPLICED IN NEW SECTION PER SRM 53-05 FIG - [SDR USAA950969](https://openairdocs.org/sdr/USAA950969.md): Frame · corroded · Aug 23, 1995 · N827US · Doug DC981 · Fuselage Main, Frame > PIT - DURING Q-5 CHECK INSPECTION, FOUND 3 AREAS 2 INCHES BY 3 INCHES OF LEVEL 2 CORROSION AFT SIDE OF FRAME AT STATION 1250 FROM LONGERON 28L TO 28R. CORROSION TASK NR C57-53300. CLEANED CORRODED SECTION AND INSTALLED DOUBLERS PER SRM 53-03 FIG 2A. (M) - [SDR USAA950984](https://openairdocs.org/sdr/USAA950984.md): Longeron · corroded · Aug 18, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH BY 20 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED AT LONGERON 28L, STATION 1211 TO 1231 CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) - [SDR USAA950967](https://openairdocs.org/sdr/USAA950967.md): Longeron · corroded · Aug 18, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 29R AT STATION 1297 CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) - [SDR USAA950966](https://openairdocs.org/sdr/USAA950966.md): Longeron · corroded · Aug 18, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 28R AT STATION 1287. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) - [SDR USAA950986](https://openairdocs.org/sdr/USAA950986.md): Beltframe · corroded · Aug 16, 1995 · N827US · Doug DC981 · Fuselage Main, Frame > PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN BELTFRAME BETWEEN LONGERON 28R AND 28L BELTFRAME 180. CORROSION TASK NR C45-53300. REMOVED SECTION OF BELTFRAME AND SPLICED IN NEW SECTION PER SRM 53-03 FIG 2A. (M) - [SDR USAA950983](https://openairdocs.org/sdr/USAA950983.md): Angle · cracked · Aug 16, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND.25 INCH CRACK LEFT SIDE STATION 1463, DRAG ANGLE. INSTALLED FILLER AND DOUBLER PER SRM 53-05 FIG 23. (M) - [SDR USAA950982](https://openairdocs.org/sdr/USAA950982.md): Cusp Membrane · cracked · Aug 16, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND 12 INCH CRACK IN CUSP MEMBRANE STATION 1231, LONGERON 18L. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 96. (M) - [SDR USAA950981](https://openairdocs.org/sdr/USAA950981.md): Longeron · cracked · Aug 16, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND 5 CRACKS.125 INCH TO.375 INCH LONG, BELTFRAME 256 TO 408 IN LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) - [SDR USAA950987](https://openairdocs.org/sdr/USAA950987.md): Track · corroded · Aug 14, 1995 · N827US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings > PIT - DURING Q-5 CHECK INSPECTION, FOUND CORROSION 1 INCH BY 6 INCHES LEFT INBOARD SEAT TRACK MOUNT HOLES AT STATION 1205. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) - [SDR USAA950985](https://openairdocs.org/sdr/USAA950985.md): Angle · corroded · Aug 12, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCH BY 29 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED RIGHT LAV T-CUSP ANGLE FROM STATION 1309 TO 1338 LONGERON 18R. CORROSION TASK NR C58-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 25. (M) - [SDR USAA950970](https://openairdocs.org/sdr/USAA950970.md): Doubler · corroded · Aug 11, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION 2 INCHES BY 35 INCHES STATION 1338, JACK PAD DOUBLER AFT CARGO AREA. CORROSION TASK NR C57-53300. REPLACED DOUBLER, CUT OUT DAMAGED AREA AND SPLICED IN NEW SECTION PER USAIR TYPICAL REPAIR 53-30-10. - [SDR USAA950980](https://openairdocs.org/sdr/USAA950980.md): Longeron · cracked · Aug 10, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND 6 CRACKS APPROXIMATELY.125 INCH TO.25 INCH IN LONGERON 17L AT BELTFRAME 237, 275, 295, 332, 370 AND 389. SPLICED IN NEW SECTION OF LONGERON BETWEEN STATION 237 TO 408 PER SRM 53-02 FIG 2. (M) - [SDR USAA950979](https://openairdocs.org/sdr/USAA950979.md): Longeron · cracked · Aug 10, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND.75 INCH CRACK LONGERON 4L AT STATION 160. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) - [SDR USAA950978](https://openairdocs.org/sdr/USAA950978.md): Jamb · cracked · Aug 10, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND.75 INCH CRACK UPPER FORWARD CORNER OF MED JAMB. INSTALLED INTERNAL AND EXTERNAL DOUBLER PER SRM 53-05 FIG 2B. (M) - [SDR USAA950649](https://openairdocs.org/sdr/USAA950649.md): Pump · inoperative · Jun 29, 1995 · N827US · Doug DC981 · Hydraulic Pump (Electric/Engine), Main > MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE F - [SDR 95ZZZW813](https://openairdocs.org/sdr/95ZZZW813.md): Rtn Line Filter · inoperative · Jun 29, 1995 · N827US · Doug DC981 · Hydraulic Filter, Main > MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE F Next page: https://openairdocs.org/deregistered/N827US-2006-05-16/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 = 'N827US' AND deregistration_id = 'N827US-2006-05-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N827US-2006-05-16/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.