# Service difficulty reports: N959U, cancelled Aug 19, 2008 A list on [N959U, cancelled Aug 19, 2008](https://openairdocs.org/deregistered/N959U-2008-08-19.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 · 73 reports - [SDR AALA20060138](https://openairdocs.org/sdr/AALA20060138.md): Smoke · detected · Feb 26, 2006 · N959U · Doug DC982 · Air Distribution System > DEN - FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN ON CLIMBOUT. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. SMOKE HAD DISSIPATED AT LANDING. ACCOMPLISHED WORK CARD 21-96-01. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUSTING PER MAINTENANCE MANUAL 21-2 - [SDR AALA20041063](https://openairdocs.org/sdr/AALA20041063.md): Battery Pack · inoperative · Oct 10, 2004 · N959U · Doug DC982 · Emergency Lighting > DFW - AFT OVERWING EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20041028](https://openairdocs.org/sdr/AALA20041028.md): Switch · inoperative · Oct 7, 2004 · N959U · Doug DC982 · Emergency Lighting > DFW - FLIGHT ATTENDANT SWITCH WILL NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH AND AFT CARGO EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR ZW0A0205601](https://openairdocs.org/sdr/ZW0A0205601.md): Light · defective · May 29, 2002 · N959U · Doug DC982 · Emergency Lighting > MAL-FWD OVERHEAD GALLEY LIGHT PN 293-0077 GETS VERY HOT AND SMELLS OF ELECTRICAL BURNING ODOR. DEACTIVATED AND REMOVED BULB. PLACARDED PER MEDP 33-2. PULLED AND BANDED FWD MIS CABIN AND LAV LT CB. HEAT AND SMELL GONE. LAST CHECK-C STL 6/28/01 - [SDR ZW0A0108801](https://openairdocs.org/sdr/ZW0A0108801.md): Light · contaminated · Sep 18, 2001 · N959U · Doug DC982 · Emergency Lighting > THE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. CLEANED AND DRIED OUT THE LIGHT STRIP. CHECK-C 6-28-01 STL. - [SDR ZW0A0107202](https://openairdocs.org/sdr/ZW0A0107202.md): Light · inoperative · Aug 21, 2001 · N959U · Doug DC982 · Emergency Lighting > THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21 TO 26. REPLACED BROKEN CONTACT ON POWER STRIP AT THE LIGHT TRACK. - [SDR ZW0A0101501](https://openairdocs.org/sdr/ZW0A0101501.md): Light · inoperative · May 10, 2001 · N959U · Doug DC982 · Emergency Lighting > THE EGRESS LIGHTING IN THE FIRST CLASS SECTION WAS INOPERATIVE. REMOVED THE LIGHT STRIP. CLEANED THE TRACK AND ELECTRICAL CONTACTS. PRESERVED CONTACTS WITH MOISTURE LOCKOUT BEFORE RE-INSTALLING. CHECK-C 12-3-00 MCI. - [SDR TWAA0018616](https://openairdocs.org/sdr/TWAA0018616.md): Seat Track · corroded · Nov 21, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND FASTENER HOLES FOR FLOOR AND SIDEWALL PANELS CORRODED AT LT FLOOR TRACK STA 1170 TO STA 1221. REPLACED CORRODED SECTION OF TRACK PER SRM 53-05, FIG 4G. - [SDR TWAA0018615](https://openairdocs.org/sdr/TWAA0018615.md): Casting · corroded · Nov 21, 2000 · N959U · Doug DC982 · Wing, Control Surface Attach Fittings > DURING CHECK-C MAINT ON LT WING THE O/B FLAP I/B MOUNT CASTING ON SPAR TOP I/B STUD WAS EMITTING RUST. REPLACED 2 UPPER STUDS AND INSTALLED NEW HINGE CASTING PER MM 57-40-01. - [SDR TWAA0018419](https://openairdocs.org/sdr/TWAA0018419.md): Beam · corroded · Nov 20, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND DOOR BEAM CORRODED AT STA 1155 TO 1211. REMOVED CORROSION PER SPM 6-80-01. BEAM OUT OF LIMITS AND REPLACED PER DRAWING 5936038-501. INSTALLED PER SRM 51-30-02 AND 51-30-05. TREATED AND PAINTED PER 51-10-3. - [SDR TWAA0018416](https://openairdocs.org/sdr/TWAA0018416.md): Frame · corroded · Nov 20, 2000 · N959U · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT A FORMER WAS CORRODED AT STA 1308, LONGERON 28R TO 23L. REMOVED FRAME FROM LONGERON 18R TO 18L. INSTALLED NEW FRAME. INSTALLED SPLICE BETWEEN LONGERON 25R AND 26R PER SRM 53-03, PAGE 4C, AND FIG 2A FOR THICK - [SDR TWAA0018418](https://openairdocs.org/sdr/TWAA0018418.md): Seat Track · corroded · Nov 19, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND CORROSION ON TRACK AT STA 200 TO 237, RBL 44. REMOVED CORROSION PER SPM 6-80-1. REPLACED 47 INCHES OF TRACK PER SRM 53-08 FIGURE 4F. - [SDR TWAA0018417](https://openairdocs.org/sdr/TWAA0018417.md): Web · cracked · Nov 19, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND MEMBRANE CRACKED AT STA 237, RBL 46. REPLACED CRACKED MEMBRANE WITH SHOP FABRICATED NEW ONE. INSTALLED WITH FASTENERS PER SRM 51-30-02. - [SDR TWAA0018415](https://openairdocs.org/sdr/TWAA0018415.md): Web · corroded · Nov 18, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 170 TO 200, RBL 56 TO 58, AND ON MEMBRANE UNDER FLOOR SUPPORT AT STA 180 TO 200, RBL 53. INSTALLED NEW MEMBRANES FROM STA 160 TO 200, RBL 44 TO 57, PER SRM 53-01 PAGE 9 FIGURE 2, DRAWING 9936534, SRM 51- - [SDR TWAA0018414](https://openairdocs.org/sdr/TWAA0018414.md): Web · corroded · Nov 18, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON CUSP AT STA 170 TO 200, AT FWD SERVICE DOOR SILL AREA. RE-INSTALLED FASTENERS REMOVED FOR CORROSION REMOVAL. REMOVAL PER SRM 51-30-1, 51-30-2, AND 51-30-5. - [SDR TWAA0018413](https://openairdocs.org/sdr/TWAA0018413.md): Web · corroded · Nov 18, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE UNDER RT SERVICE DOOR SILL AT STA 170 AND ON MEMBRANE AT STA 160, RBL 43. INSTALLED NEW MEMBRANE FROM STA 160 TO 200, RBL 44 TO 57 PER SRM 53-01, PAGE 9 FIG 2, DRAWING 9936534, SRM 51-30-2, AND SRM 51-30-5. SE - [SDR TWAA0018412](https://openairdocs.org/sdr/TWAA0018412.md): Floor Support · corroded · Nov 18, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT STA 180, RBL 10 TO RBL 44. NEW FLOOR SUPPORT FABRICATED PER DRAWING 9936534. PAINTED PER SRM 51-10. INSTALLED FASTENERS PER SRM 51-30-2, SRM 51-30-05. SEALED STIFFENER PER SRM 51-20-0. - [SDR TWAA0018411](https://openairdocs.org/sdr/TWAA0018411.md): Web · corroded · Nov 18, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT STA 200 RT SIDE, AND UNDER T-ANGLE BOTTOM DOOR FRAME (JAMB) SUPPORT. INSTALLED NEW MEMBRANE FROM STA 160 TO 200, RBL 44 PER SRM 53-01 PAGE 9, FIG 2, DRAWING 993634. - [SDR TWAA0018410](https://openairdocs.org/sdr/TWAA0018410.md): Web · corroded · Nov 18, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 200, RBL 46 TO 50, AND ON MEMBRANE RT SIDE AT SIDEWALL TO FLOOR SUPPORT ANGLE STA 160 TO 180, RBL 53 TO 57. INSTALLED NEW MEMBRANES FROM STA 160 TO 200, RBL 44 TO RBL 57, PER SRM 53-01 PAGE 9 FIGURE 2, D - [SDR TWAA0018614](https://openairdocs.org/sdr/TWAA0018614.md): Seat Track · corroded · Nov 17, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND FASTENER HOLES CORRODED FOR FLOOR AND SIDE WALL PANELS AT LT FLOOR TRACK STA 1221 THRU 1322. REPAIRED PER SRM 53-05, FIG 4G. - [SDR TWAA0018613](https://openairdocs.org/sdr/TWAA0018613.md): Floor Support · corroded · Nov 17, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FLOOR SUPPORT WAS CORRODED AT STA 160 TO 200, RBL 44 IN. NEW FLOOR SUPPORT FABRICATED PER DRAWING 9936534. PAINTED PER SRM 51-10-3. - [SDR TWAA0018612](https://openairdocs.org/sdr/TWAA0018612.md): Floor Support · corroded · Nov 17, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 160 TO 180, RBL 53 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. PAINTED PER SRM 51-10-3. - [SDR TWAA0018409](https://openairdocs.org/sdr/TWAA0018409.md): Floor Support · corroded · Nov 17, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200, RBL 10 IN TO RBL 48 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. PAINTED AND TREATED PER SRM 51-10-3. INSTALLED NEW SUPPORT PER SRM 51-30. - [SDR TWAA0018408](https://openairdocs.org/sdr/TWAA0018408.md): Floorbeam · corroded · Nov 17, 2000 · N959U · Doug DC982 · Fuselage Main, Floor Beam > DURING CHECK-C MAINT, THE CABIN FLOOR AND GALLEY DRAIN PAN SUPPORT WAS CORRODED AT STA 160, RBL 53 INCHES. INSTALLED SUPPORT ANGLE PER SRM 51-30. REMADE FLOOR SUPPORT FROM RAW STOCK. - [SDR TWAA0018407](https://openairdocs.org/sdr/TWAA0018407.md): Frame · corroded · Nov 16, 2000 · N959U · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT FOUND CORROSION AT PREVIOUS REPAIR FWD SIDE OF FORMER STA 1287, LONGERON 29L THRU L29R. FORMER FRAME SEGMENT WAS REPLACED FROM LONGERON 18L TO AND BETWEEN LONGERON 25R AND L26R PER SRM 53-03, FIG 2A, AND DRAWING 9957739. - [SDR TWAA0018406](https://openairdocs.org/sdr/TWAA0018406.md): Frame · corroded · Nov 16, 2000 · N959U · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT FOUND CORROSION AT FORMER FOOT STA 1287, BETWEEN LONGERON 30R AND LONGERON 29R. NEW FORMER FOOT WAS INSTALLED PER DRAWING 9957739. - [SDR TWAA0018405](https://openairdocs.org/sdr/TWAA0018405.md): Splice · corroded · Nov 16, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT FOUND CORROSION ON SPLICE PLATE AFT SIDE OF FORMER STA 1287, LONGERON 30 AND 28L. FORMER FRAME SEGMENT WAS REPLACED FROM LONGERON 18L AND BETWEEN L25R AND L26R PER SRM 53-03, FIG 2A, AND DRAWING 9957739. - [SDR TWAA0018404](https://openairdocs.org/sdr/TWAA0018404.md): Frame · corroded · Nov 16, 2000 · N959U · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1287, FROM LONGERON 30 T0 23L, FWD SIDE. FORMER FRAME SEGMENT WAS REMOVED FROM LONGERON 18L AND BETWEEN L25R AND L26R. NEW FRAME WAS INSTALLED PER SRM 53-03, FIG 2A AND PER DRAWING 9957739. - [SDR TWAA0017907](https://openairdocs.org/sdr/TWAA0017907.md): Skin · damaged · Nov 13, 2000 · N959U · Doug DC982 · Fuselage Main, Plate/Skin > DURING CHECK-C MAINT, THE FUSELAGE SKIN WAS REMOVED TO A THICKNESS OF 0.029 IN AT LT STA 237 BETWEEN LONGERON 17L AND 18L, MEASURED WITH NDT U.T. THICKNESS STRESSTEL INSTRUMENT. REMEASURED SKIN THICKNESS WITH NORTEC 1000 AND KRAUTKRAMER PENCIL THINKNESS PROBE - [SDR TWAA0017906](https://openairdocs.org/sdr/TWAA0017906.md): Skin · delaminated · Nov 13, 2000 · N959U · Doug DC982 · Trailing Edge Flaps > DURING CHECK-C MAINT, ON RT WING T/E THE I/B FLAP T/E WEDGE WAS DELAMINATED APPROX 65 INCHES TO 72 INCHES FROM I/B END OF FLAP. CLEANED DAMAGED AREA AND REPAIRED PER SRM 51-90-0. - [SDR TWAA0017905](https://openairdocs.org/sdr/TWAA0017905.md): Seat Track · corroded · Nov 11, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT, FOUND CORROSION ON TRACK AT LBL 59 AT GALLEY TIE DOWN STA 1208. ALSO CORROSION ON TRACK AT LBL 58 ON FLANGE AND AT GALLEY TIE DOWN STA 1236. CORROSION ALSO FOUND ON TRACK AT LBL 58 AT GALLEY TIE DOWN AT STA 1174. REPLACED TRACK FROM S - [SDR TWAA0017904](https://openairdocs.org/sdr/TWAA0017904.md): Seat Track · corroded · Nov 11, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT, FOUND CORROSION ON NUMBER 2 CHAIR TRACK O/B OF FLOOR PANEL 1 ATTACH FLANGE, STA 1265 TO 1309. ALSO CORROSION ON TRACK FLANGE STA 1193 TO 1212 AT LBL 48. REPLACED CHAIR TRACK FROM STA 1032 TO 1307 PER SPM 6-70-01. INSTALLED SPLICE PER S - [SDR TWAA0102403](https://openairdocs.org/sdr/TWAA0102403.md): Seat Track · corroded · Nov 10, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND CORROSION IN SEAT TRACK AT LBL 24 INCHES, STA 1205 TO 1309. MATERIAL.25 INCH THICK MISSING. REMOVED AND REPLACE CHAIR TRACK AT LBL 24 IN FROM STA 1180 TO 1309 WITH STOCK MATERIAL, SPLICE AND PLATE. ATTACHED WITH HI-LOKS, MS250 WA - [SDR TWAA0017903](https://openairdocs.org/sdr/TWAA0017903.md): Frame · corroded · Nov 10, 2000 · N959U · Doug DC982 · Fuselage Main, Frame > DURING CHECK-C MAINT, FOUND FORMER CORRODED ABOVE LONGERON 29L, AT STA 1193. REMOVED FORMER, FABRICATED, HEAT TREATED AND INSTALLED NEW FORMER PER DRAWING 9936073. - [SDR TWAA0017902](https://openairdocs.org/sdr/TWAA0017902.md): Strap · corroded · Nov 10, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, FOUND STRAP UNDER TRACK AT LBL 59 IN WAS CORRODED FROM STA 1136 TO 1142, AND THE FASTENER HEADS WERE POPPED. REPAIRED, REPLACED NEW STRAP PER SPM 6-70-01. PAINTED PER SRM 51-30-05. INSTALLED FASTENERS PER SRM 51-30-05. - [SDR TWAA0017901](https://openairdocs.org/sdr/TWAA0017901.md): Floor Panel · corroded · Nov 10, 2000 · N959U · Doug DC982 · Fuselage Main, Floor Beam > DURING CHECK-C MAINT, FOUND CORROSION AT BOTTOM OF CABIN FLOOR MEMBRANE, STA 1163, LBL 5 INCHES. REMOVED CORROSION PER SPM 6-80-01. INSTALLED REPAIR PER SRM 53-01-18. PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER SRM 51-30-05. - [SDR TWAA0102402](https://openairdocs.org/sdr/TWAA0102402.md): Seat Track · corroded · Nov 8, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND CORROSION IN THE SEAT TRACK AT RBL 24, AT STA 247 AND FROM STA 206 TO 210. CUT OUT TRACK AT BOTH LOCATIONS AND INSTALLED NEW TRACK PER SRM 53-05, FIG F. - [SDR TWAA0017617](https://openairdocs.org/sdr/TWAA0017617.md): Skin · dented · Nov 8, 2000 · N959U · Doug DC982 · Leading Edge Devices > DURING CHECK-C MAINT, THE LT WING O L/E SLAT HAD DENT IN L/E APPROX CENTER OF SLAT. ACCOMP NDT AND NO CRACK FOUND PER PART 6-51-08-03 HFEC OF AREA IN SHOP PER TWA NDT SPM NUMBER 3 REPAIR PART NUMBER 6, NO CRACK. FOUND OK TO CLOSE LOWER SKIN. REPAIRED L/E PE - [SDR TWAA0017509](https://openairdocs.org/sdr/TWAA0017509.md): Galley Track · corroded · Nov 6, 2000 · N959U · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT FOUND CORROSION ON GALLEY TRACK AT STA 1136 TO 1178. REPLACED 42.75 INCH SECTION OF GALLEY TRACK PER SRM 53-05, PAGE 11, FIG 4H. INSTALLED TRACK PER SRM 51-30-1. - [SDR TWAA0017508](https://openairdocs.org/sdr/TWAA0017508.md): Floorbeam · corroded · Nov 5, 2000 · N959U · Doug DC982 · Fuselage Main, Floor Beam > DURING CHECK-C MAINT FOUND CORROSION ON FLOORBEAM CAP AT STA 1250, LBL 24 IN TO LBL 48 INCHES. REPLACED FLOOR PANEL SUPPORT PER DRAWING 9930612. - [SDR TWAA0017507](https://openairdocs.org/sdr/TWAA0017507.md): Floorbeam · corroded · Nov 5, 2000 · N959U · Doug DC982 · Fuselage Main, Floor Beam > DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM CAP AT STA 1155, LBL 24 TO LBL 47. REMOVED AND REPLACED FLOORBEAM CAP PER SPM 6-70-01, PAGE 2 AND 3. INSTALLED BEAM CAP USING HI-LOKS PER SRM 51-30-5, PAGE 12, AND PER TORQUE VALUES SRM 51-30-1, PAGE 11 - [SDR TWAA0017506](https://openairdocs.org/sdr/TWAA0017506.md): Web · corroded · Nov 3, 2000 · N959U · Doug DC982 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE UNDER END OF SUPPORT AT STA 201, RBL 10 INCHES. REMOVED CORROSION PER SRM 6-80-01. TREATED CORROSION PER SRM 51-10-3. REPAIRED MEMBRANE PER SRM 53-01 PAGE 9. - [SDR TWAA0017505](https://openairdocs.org/sdr/TWAA0017505.md): Skin · cracked · Nov 2, 2000 · N959U · Doug DC982 · Cargo/Baggage Doors > DURING CHECK-C MAINT, THE FWD CARGO DOOR INTERNAL DOOR SKIN HAD A 2 INCH CRACK IN THE RADIUS OUTBOARD SIDE OF AFT BOTTOM LATCH AND.5 INCH CRACK BETWEEN ADJACENT FASTENER HOLE. CRACK CONTAINED PER EDDY CURRENT PART L 51-00-03. INSTALLED DOUBLER PER SRM 52-05 - [SDR TWAA0017303](https://openairdocs.org/sdr/TWAA0017303.md): Structure · dented · Oct 24, 2000 · N959U · Doug DC982 · Leading Edge Devices > DURING CHECK-C MAINT, THE LT WING L/E NUMBER 3 SLAT INBOARD L/E HAD WIND EROSION ON DENT FILLER IN DENT APPROX 2 FEET FROM INBOARD END. ACCOMP NDT AND NO CRACK FOUND PER PART 6 OF 51-00-03. SANDED OUT OLD FILLER AND REPLACED WITH NEW PER SRM 57-03 PAGE 20A. - [SDR TWAA0008403](https://openairdocs.org/sdr/TWAA0008403.md): Battery Pack · inoperative · May 25, 2000 · N959U · Doug DC982 · Emergency Lighting > DURING OVERNIGHT INSPECTION FOUND EGRESS FLOOR LIGHTING AND FORWARD ENTRY DOOR EMERGENCY EXIT SIGNS INOP. REPLACED EGRESS BATTERY PACK. AC04 04-30-00 DFW. - [SDR TWAA9913602](https://openairdocs.org/sdr/TWAA9913602.md): Battery Pack · discharged · Sep 24, 1999 · N959U · Doug DC982 · Emergency Lighting > THE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 7, 8, 11 AND 33, AND THE AIRSTAIRS. REPLACED THE BATTERY PACK, PART NR 5822-2, IN THE CABIN AND REPAIRED WIRING IN THE AIRSTAIRS. CHECK-C 7-6-99 JFK. - [SDR TWAA9908703](https://openairdocs.org/sdr/TWAA9908703.md): Battery Pack · discharged · Jun 22, 1999 · N959U · Doug DC982 · Emergency Lighting > THE EGRESS LIGHTS AT ROWS 15 TO 21 CAME ON IN FLIGHT AND WOULD NOT RESET. REPLACED THE BATTERY PACK AT ROW 20. CHECK-C 10-10-98 STL. - [SDR TWAA9908705](https://openairdocs.org/sdr/TWAA9908705.md): Battery Pack · discharged · Jun 21, 1999 · N959U · Doug DC982 · Emergency Lighting > THE CABIN EGRESS LIGHTS AT ROW 15 TO 20 ILLUMINATED INTERMITTENTLY IN FLIGHT. REPLACED THE MID CABIN EGRESS LIGHT BATTERIES. CHECK-C 10-10-98 STL. - [SDR TWAA9820002](https://openairdocs.org/sdr/TWAA9820002.md): Excitor · shorted · Dec 22, 1998 · N959U · Doug DC982 · APU Start/Ignition System > THE LT CSD TEMP WAS HIGH AND CREW DISCONNECTED THE CSD. ATTEMPTED TO START APU FOR GENERATOR BUT APU WOULD NOT START. CORRECTED THE APU BY REPLACING THE OIL PRESS SEQUENCE SWITCH, MFG 692525-9, THE IGNITION COIL, MFG 10-381175-9, AND THE IGNITOR PLUG MFG CH31 - [SDR TWAA9816601](https://openairdocs.org/sdr/TWAA9816601.md): Battery · discharged · Oct 14, 1998 · N959U · Doug DC982 · Emergency Lighting > EGRESS LIGHTS IN FLOOR AFT OF ROW 29 CAME ON IN FLIGHT AND REMAINED ON. REPLACED BATTERIES IN POWER SUPPLY. CHECK-C 10-1-98 STL. Next page: https://openairdocs.org/deregistered/N959U-2008-08-19/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 = 'N959U' AND deregistration_id = 'N959U-2008-08-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N959U-2008-08-19/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.