# Service difficulty reports: N826US, cancelled Oct 6, 2005 A list on [N826US, cancelled Oct 6, 2005](https://openairdocs.org/deregistered/N826US-2005-10-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD02011](https://openairdocs.org/sdr/USAAD02011.md): Light · inoperative · Feb 22, 2002 · N826US · Doug DC981 · Emergency Lighting > PIT - THE EMERGENCY LIGHT AT THE 1-R DOOR CAME ON LANDING. MAINTENANCE CHECK THE EMERGENCY LIGHT OPERATION, ALL CHECKED NORMAL. REPLACED THE EMERGENCY LIGHT BATTERY AS PRECAUTION. (M) - [SDR USAAD02009](https://openairdocs.org/sdr/USAAD02009.md): Battery · discharged · Feb 9, 2002 · N826US · Doug DC981 · Emergency Lighting > IND - TWO SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD02005](https://openairdocs.org/sdr/USAAD02005.md): Battery · discharged · Feb 6, 2002 · N826US · Doug DC981 · Emergency Lighting > IND - THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD02006](https://openairdocs.org/sdr/USAAD02006.md): Battery · discharged · Feb 6, 2002 · N826US · Doug DC981 · Emergency Lighting > IND - THE AFT ACCESSORY CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD02007](https://openairdocs.org/sdr/USAAD02007.md): Battery · discharged · Feb 6, 2002 · N826US · Doug DC981 · Emergency Lighting > IND - THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT REMOTE RECEIVER BATTERY. (M) - [SDR USAAD01185](https://openairdocs.org/sdr/USAAD01185.md): Duct · disconnected · Dec 4, 2001 · N826US · Doug DC981 · Air Distribution System > PHL-RSW - FLT 415 - DURING CRUISE AT 35,000 FEET, THE CABIN ALTITUDE STARTED TO CLIMB A 300 TO 500 FT/MIN AND THE FLOW LIGHT ILLUMINATED. THE CABIN PRESSURE COULD NOT BE CONTROLLED IN MANUAL AND AN EMERGENCY DESCENT WAS INITIATED. CONTROL OF THE CABIN PRESSU - [SDR USAAD01164](https://openairdocs.org/sdr/USAAD01164.md): Valve · failed · Sep 26, 2001 · N826US · Doug DC981 · Cabin Pressure Control System > MSY-CLT - FLT 1278 - DURING CRUISE, AT THE TOP OF THE DESCENT, THE CABIN FLOW LIGHT ILLUMINATED WITH NO INDICATION OF A FAULT IN THE CABIN PRESSURE CONTROL. THE CREW INITIATED AN EMERGENCY DESCENT FROM 33,000 FEET TO 19,000 FEET. THE AIRCRAFT CONTINUED TO IT - [SDR USAAD01145](https://openairdocs.org/sdr/USAAD01145.md): Sensor · inoperative · Aug 2, 2001 · N826US · Doug DC981 · Landing Gear System > RSW-CLT - FLT 714 - THE RED NOSE GEAR LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. THE CHECK LIST PROCEDURES WERE ACCOMPLISHED, HOWEVER, THE NOSE GEAR LIGHT REMAINED ON FOR THE REST OF THE FLIGHT. THE LANDING GEAR INDICATED NORMAL WHEN THE LANDING GEAR W - [SDR 2001F00215](https://openairdocs.org/sdr/2001F00215.md): Battery · discharged · Jul 29, 2001 · N826US · Doug DC981 · Emergency Lighting > IND - ON LOW LEVEL EMERGENCY LIGHT AND THE LEFT AND RIGHT EXIT PATH LIGHTS A PASSENGER SEAT ROW 19 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01140. (M) - [SDR USAAD01140](https://openairdocs.org/sdr/USAAD01140.md): Battery · inoperative · Jul 29, 2001 · N826US · Doug DC981 · Emergency Lighting > IND - ON LOW LEVEL EMERGENCY LIGHT AND THE LEFT AND RIGHT EXIT PATH LIGHTS A PASSENGER SEAT ROW 19 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD01113](https://openairdocs.org/sdr/USAAD01113.md): Battery · discharged · May 20, 2001 · N826US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 6 WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAA010258](https://openairdocs.org/sdr/USAA010258.md): Shear Tie · corroded · Feb 28, 2001 · N826US · Doug DC981 · Fuselage Main, Structure > BOS - FOUND SHEAR TIE CORRODED.75 INCH BY 2 INCH, STATION 1287 BETWEEN LONGERON 28L TO 28R. CORROSION LEVEL 1. BURNISHED, TREATED AND PRIMED CORROSION. CUT OUT SECTION OF SHEAR TIE AND REPLACED PER OM-26. (M) - [SDR USAAD01035](https://openairdocs.org/sdr/USAAD01035.md): Light · misinstalled · Feb 20, 2001 · N826US · Doug DC981 · Emergency Lighting > PIT - THE EMERGENCY LIGHTS AT ROWS 19, 24, AND 29 WERE INSTALLED AT THE WRONG POSITIONS. INSTALLED THE LIGHT ASSEMBLIES INTO THE CORRECT POSITIONS. (M) - [SDR USAAD01034](https://openairdocs.org/sdr/USAAD01034.md): Battery Pack · discharged · Feb 19, 2001 · N826US · Doug DC981 · Emergency Lighting > PIT - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAD01033](https://openairdocs.org/sdr/USAAD01033.md): Battery · discharged · Feb 18, 2001 · N826US · Doug DC981 · Emergency Lighting > IND - THE INTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED TRANSMITTER BATTERIES. (M) - [SDR USAAD00033](https://openairdocs.org/sdr/USAAD00033.md): Fan · failed · Feb 26, 2000 · N826US · Doug DC981 · Air Distribution Fan > CLT - IND - FLT 1248 - DURING DESCENT, THERE WAS AN UNIDENTIFIED ODOR IN THE CABIN. THE AIRCRAFT LANDED AT ITS DESTINATION WITHOUT INCIDENT. ON ARRIVAL THE FIRE DEPARTMENT SEALED THE AIRCRAFT AND THE HEALTH DEPARTMENT SAMPLED THE AIR IN THE CABIN, AND NOTHIN - [SDR USAAD99175](https://openairdocs.org/sdr/USAAD99175.md): Light · inoperative · Dec 9, 1999 · N826US · Doug DC981 · Emergency Lighting > PHL - THE LEFT AFT OVERWING EXIT IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT AFT OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. (M) - [SDR USAA990860](https://openairdocs.org/sdr/USAA990860.md): Subfloor · corrosion · Sep 1, 1999 · N826US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q1/C4 CHECK, FOUND EXTENSIVE CORROSION OF SUB FLOOR AT STATION 155 AREA BY EPC. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) - [SDR USAA990930](https://openairdocs.org/sdr/USAA990930.md): Cusp · corroded · Aug 25, 1999 · N826US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q1/C4 CHECK, FOUND HOLE IN CUSP MEMBRANE DUE TO CORROSION AT STATION 200, LEFT SIDE. CUSP MEMBRANE REPLACED PER EA 52552 REV A. (M) - [SDR USAA990929](https://openairdocs.org/sdr/USAA990929.md): Longeron · corroded · Aug 25, 1999 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q1/C4 CHECK, FOUND CORROSION.020 DEEP AT LONGERON 296, STATION 427 TO 446, CORROSION TASK NR C51-53300, CORROSION LEVEL 1. SPLICED IN NEW SECTION PER EA 52620 AND SRM 53-02 FIG 4. (M) - [SDR USAA990620](https://openairdocs.org/sdr/USAA990620.md): Web · cracked · Jun 20, 1999 · N826US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - LINE MAINTENANCE REPORT INDICATED 6 INCH CRACK AT RIGHT SIDE CANTED WEB SECTION AT STATION 1463. REMOVED AND REPLACED CRACKED WEB SECTION. (M) - [SDR USAAD98172](https://openairdocs.org/sdr/USAAD98172.md): Air Dist · odor · Oct 5, 1998 · N826US · Doug DC981 · Air Distribution System > PHL-GSP - FLT 273 - AFTER TAKEOFF THE FLIGHT ATTENDANTS NOTICED A BURNING SMELL THROUGH THE AIR CONDITIONING SYSTEM. THE SMELL SUBSIDED A LITTLE THEN RETURNED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE AIR CONDI - [SDR USAA980413](https://openairdocs.org/sdr/USAA980413.md): Skin · cracked · Sep 18, 1998 · N826US · Doug DC981 · Wing, Plate/Skin > PIT - DURING C-CHECK, FOUND 2.25 INCH CRACK ON SKIN AT RT WING LEADING EDGE BETWEEN NR 2 AND NR 3 SLAT PANELS UPPER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER MD-80 SRM 57-06B PAGE 11, FIG 4. (M) - [SDR USAA980412](https://openairdocs.org/sdr/USAA980412.md): Longeron · corroded · Sep 18, 1998 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING C-3 CHECK, FOUND CORROSION ON APPROX 7 INCHES OF LONGERON (1 INCH BY 7 INCH) AT LONGERON 25R STATION 218 TO STATION 225. REPLACED SECTION OF LONGERON (SPLICED IN A SECTION) PER SRM 53-02. (M) - [SDR USAAD98011](https://openairdocs.org/sdr/USAAD98011.md): Window · cracked · Jan 19, 1998 · N826US · Doug DC981 · Flight Compartment Windows > PIT - FLT 1085 - DURING CLIMB-OUT AT 28,000, THE OUTER PANE OF THE CAPTAINS WINDOW CRACKED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDOW. (M) - [SDR USAA970304](https://openairdocs.org/sdr/USAA970304.md): Skin · cracked · Oct 14, 1997 · N826US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING C2 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT STATION 1437 ABOVE LONGERON 4R. INSTALLED DOUBLER PER SRM 53-04 FIG 27. (M) - [SDR USAAD97130](https://openairdocs.org/sdr/USAAD97130.md): Compressor · stalled · Jul 31, 1997 · N826US · Doug DC981 · Turbine Engine Compressor Section > FLT 1899 - BOS-PHL - ON DESCENT INTO PHL, THE RIGHT ENGINE EXPERIENCED A COMPRESSOR STALL. ENGINE READINGS DROPPED, CAPT SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY. FLIGHT LANDED PHL SAFELY. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. (M) - [SDR USAAD96135](https://openairdocs.org/sdr/USAAD96135.md): Gen Contrl Unit · failed · Oct 2, 1996 · N826US · Doug DC981 · AC Regulator > FLIGHT 320 - CLT-SAV - AFTER TAKEOFF, LEFT GENERATOR FAILED, APU WAS ALREADY ON MEL. RETURNED TO CLT. REPLACED LEFT GCU. (M) - [SDR USAAD96055](https://openairdocs.org/sdr/USAAD96055.md): Battery Pack · discharged · May 16, 1996 · N826US · Doug DC981 · Emergency Lighting > SAV - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 3-7 AND 17-20. MX REPLACED THE APPLICABLE BATTERY PACKS. (M) - [SDR USAA960199](https://openairdocs.org/sdr/USAA960199.md): Skin · corroded · Feb 2, 1996 · N826US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING C-6 INSPECTION, FOUND CORROSION AT LONGERON 22R STATION 140 TO STATION 160 BETWEEN SKIN AND LONGERON. REMOVED DAMAGED AREA AND ACCOMPLISHED LONGERON SPLICE REPAIR AND SKIN DOUBLER REPAIR PER SRM 53-04-12B AND 53-02 FIG 2. (M) - [SDR USAA950478](https://openairdocs.org/sdr/USAA950478.md): Skin · corrosion · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-6 CHECK INSPECTION, FOUND CORROSION AT STATION 807 LONGERON 28-30 RIGHT IN SKIN. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53. (W) - [SDR USAA950477](https://openairdocs.org/sdr/USAA950477.md): Cusp Membrane · cracked · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK AT STATION 1305 RT SIDE CUSP MEMBRANE. SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 97. (W) - [SDR USAA950476](https://openairdocs.org/sdr/USAA950476.md): Longeron · cracked · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-6 CHECK INSPECTION, FOUND 2 INCH CRACK AT STATION 1290-1300 CUSP MEMBRANE LEFT SIDE LONGERON 18L. SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 97. (W) - [SDR USAA950475](https://openairdocs.org/sdr/USAA950475.md): Longeron · cracked · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.375 INCH CRACK AT STATION 1322 LONGERON 17 LEFT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-03 FIG 32. (W) - [SDR USAA950474](https://openairdocs.org/sdr/USAA950474.md): Beam · gouged · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-6 CHECK INSPECTION, FOUND A GOUGE BEYOND LIMITS AT STATION 1174 AND 1193 LOWER FLANGE OF BEAM, AFT CARGO CEILING STRUCTURE. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR ANGLES PER SRM 53-05 FIG 86. (W) - [SDR USAA950473](https://openairdocs.org/sdr/USAA950473.md): Frame · cracked · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Frame > PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN FRAME STATION 160 AT CENTER OF AIRCRAFT IN E/E COMPARTMENT. STOP DRILLED CRACK AND INSTALLED SPLICE REPAIR AND DOUBLER PER SRM 53-03 FIG 2A. (W) - [SDR USAA950472](https://openairdocs.org/sdr/USAA950472.md): Longeron · cracked · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT -DURING Q-6 CHECK INSPECTION, FOUND.75 INCH CRACK STATION 160 LONGERON 4 LEFT. SPLICED NEW SECITON OF LONGERON IN PER SRM 53-02 FIG 2. (W) - [SDR USAA950471](https://openairdocs.org/sdr/USAA950471.md): Skin · dented · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH BY 2 INCH BY.030 INCH DEEP DENT STATION 484 BETWEEN LONGERON 21L AND 22L. CUT OUT DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER REPAIR PER SRM 53-04 FIG 38 VIEW L. (W) - [SDR USAA950470](https://openairdocs.org/sdr/USAA950470.md): Skin · dented · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-6 CHECK INSPECTION, FOUND DENT 2.375 INCH BY 1.75 INCH BY.080 INCH DEEP STATION 296 BETWEEN LONGERON 24L AND 23L. CUT OUT DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER REPAIR PER SRM 53-04 FIG 38. (W) - [SDR USAA950469](https://openairdocs.org/sdr/USAA950469.md): Track · elongated · Apr 17, 1995 · N826US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings > PIT - DURING Q-6 CHECK INSPECTION, FOUND HOLES ELONGATED FLIGHT OFFICER AFT OUTBOARD SEAT TRACK. INSTALLED REPAIR KIT PER USAIR TYPICAL REPAIR 53-20-06 REV A. (W) - [SDR USAA950468](https://openairdocs.org/sdr/USAA950468.md): Track · elongated · Apr 17, 1995 · N826US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings > PIT - DURING Q-6 CHECK INSPECTION, FOUND HOLES ELONGATED CAPTAINS AFT OUTBOARD SEAT TRACK. INSTALLED SET TRACK REPAIR KIT PER USAIR TYPICAL REPAIR 53-20-06 REV A. (W) - [SDR USAA950466](https://openairdocs.org/sdr/USAA950466.md): Longeron · chafed · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-6 CHECK INSPECTION, FOUND CHAFED AREA STATION 1401-1418 LONGERON 8 LEFT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2 AND USAIR TYPICAL REPAIR 53-10-17. (W) - [SDR USAA950465](https://openairdocs.org/sdr/USAA950465.md): Longeron · cracked · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-6 CHECK INSPECTION, FOUND.75 INCH CRACK RT AND 1 INCH CRACK LT STATION 1416 LONGERON 4 AND 5 RIGHT AND 4 AND 5 LEFT. INSTALLED TEMPORARY REPAIR PER USAIR EA 30225 AND SRM 53-03 FIG 30. (W) - [SDR USAA950464](https://openairdocs.org/sdr/USAA950464.md): Angle · corrosion · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-6 CHECK INSPECTION, FOUND LEVEL II CORROSION REF CPCP TASK NR C58-53300 FLOORBEAM TOP ANGLE STATION 1338 RIGHT LAV. ACCOMPLISHED SPLICE REPAIR FLOORBEAM AND REPLACED ANGLE PER USAIR TYPICAL REPAIR 53-10-14. (W) - [SDR USAA950463](https://openairdocs.org/sdr/USAA950463.md): Floorbeam · corrosion · Apr 17, 1995 · N826US · Doug DC981 · Fuselage Main, Floor Beam > PIT - DURING Q-6 CHECK INSPECTION, FOUND LEVEL II CORROISON REF CPCP TASK NR C58-5330 STATION 1322 RIGHT LAV FLOORBEAM. REMOVED CORROSION TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER, REPAIR ANGLES AND STRAP PER USAIR TYPICAL REPAIR 53-10-19. (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 = 'N826US' AND deregistration_id = 'N826US-2005-10-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N826US-2005-10-06/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.