N939AS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
91 reports on file, 1995-01-21 – 2005-03-06.
Part: ENGINE — MAKING METAL (LEFT)
DFW INFLIGHT T1304/6 MAR LOUD BAND AND SHUTTER. LEFT ENGINE LOST POWER. ROLLED BACK TO IDLE. ENGINE RAN AT IDLE UNTIL AFTER LANDING. ENGINE WAS SHUT DOWN AFTER LANDING. FOUND METAL IN TAILPIPE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - AFT TAIL CONE EMERGENCY LIGHT AND OVERHEAD EMERGENCY AISLE PATH LIGHT INOPERATIVE. REPLACED TWO EACH BATTERY PACKS ABOVE RIGHT HAND AFT LAV FOR TAIL CONE EMERGENCY LIGHT AND OVERHEAD EMERGENCY AISLE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)
DFW - AFT EMERGENCY LIGHTS BETWEEN AFT LAVS INOPERATIVE. REPLACED BATTERY PACKS AND TWO LIGHT BULBS FOR EMERGENCY LIGHTS BETWEEN AFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1995–2004 · 88 reports
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
FIRST CLASS EMERGENCY LIGHTS ON OVERHEAD PANELS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FIRST CLASS EMERGENCY LIGHTS ON OVERHEAD PANELS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - FORWARD CABIN EMERGENCY BYPASS LIGHTING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY BYPASS LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 46,253 hrs · 26,708 cycles
THE EGRESS LIGHTS WERE INOPERATIVE BETWEEN CABIN ROWS 27 AND 30. SECURED LOOSE CONNECTOR AT ROW 30. CHECK-C 11-23-03 STL. --CLOSED---
2002
Part: BRACKET — CRACKED (HORIZONTAL STAB) · airframe 44,189 hrs · 25,408 cycles
BRACKET CRACKED INSIDE HORIZONTAL STABILIZER AT STA 1429 AND RBL 6. REPLACED ANGLE PER SPM 6-70-01 AND DOUGLAS DRAWING 5912188. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED--
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,189 hrs · 25,408 cycles
FLOOR TIE DOWN TRACK BETWEEN STRINGERS 27 AND 28 LT AND STA 1003 AND 1079 IN AFT AUX FUEL TANK HAS CORROSION. REPLACED TRACK SPLICE AND TRACK I.A.W. SRM 53-05-10R. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED--
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,189 hrs · 25,408 cycles
FLOOR SUPPORTS BETWEEN STA 160 AND STA 200 FOUND WITH SURFACE CORROSION. FABRICATED NEW SUPPORTS AND INSTALLED PER SRM 51-03-02. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED--
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,189 hrs · 25,408 cycles
FLOOR TIE BETWEEN STRINGERS 28 AND 27 RT AND FROM STA 1003 TO 1079 IN AFT AUX FUEL TANK CAVITY HAS CORROSION. INSTALLED NEW TRACK FROM STA 1022 TO STA 1079. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED--
Part: TURBINE — FAILED (LT ENGINE) · airframe 43,578 hrs · 24,993 cycles
DURING CLIMB LEFT ENG TURBINE FAILURE. FLT CREW DECLARED EMERGENCY SHUT ENG DOWN PER QRH RESULTING IN UNSCHEDULED LANDING. REPLACED NR 1 ENG, OPS AND LEAK CHECKED NR 1 ENG.
2001
Part: BATTERY — INOPERATIVE (CABIN) · airframe 39,676 hrs · 22,770 cycles
DURING PREFLIGHT, FOUND EGRESS PATH MARKING SYSTEM LIGHTS INOP. REPLACED BATTERIES. OP 00-05 01-31-01 STL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 39,676 hrs · 22,770 cycles
DURING PREFLIGHT, FOUND EGRESS PATH MARKING SYSTEM LIGHTS INOP. REPLACED BATTERYS. OP 00-05 01-31-01 STL.
Part: SOCKET — FAILED (ROW 33) · airframe 39,672 hrs · 22,767 cycles
THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 33. SPLICED IN NEW LIGHT SOCKET. CHECK-C 1-20-01 STL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,471 hrs · 22,657 cycles
THE FWD OVERWING EMERGENCY EXIT SIGN LH AND RH HAND, THE FWD ENTRY PORTABLE EMERGENCY LIGHT, EGRESS LIGHTS ROW 5 THRU 7, AND EGRESS LIGHTS ROW 22 THRU 27 WERE INOPERATIVE. REPLACED BATTERY IN THE BATTERY PACK PN 41B030CF00101 FOR THE EXIT SIGN AND FOR THE ENTRY LIGHT, REPLACED A LIGHT MODULE PN 0105606-005 FOR FWD CABIN EGRESS LIGHTS, AND ADJUSTED BATTERY CONTACTS FOR THE AFT CABIN EGRESS LIGHTS. CHECK-C 11-16-99 MCI.
2000
Part: LANDING GEAR — DAMAGED (LEFT) · airframe 37,564 hrs · 21,608 cycles
AFTER TAKEOFF GOT A RED LEFT MAIN LIGHT AND DOOR LIGHT ILLUMINATED. REPLACED LEFT MAIN GEAR ASSEMBLY. 0001 4-10-00 DFW.
1999
Part: FLOORBEAM — CORRODED (BS 1149 - 1169)
DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE BETWEEN STA 1149L AND 1169L, AT LONGERON 18L. ACCOMP NDT PER 51-00-01 PART 4.. REMOVED LIGHT AND MODERATE CORROSION ON LT FLOOR MEMBRANE BETWEEN STA 1149 AND 1169 AT LONGERON 18, PER SPM 6-80-01 PAGE 1 TO 3. REPAIRED AREA AT 1155-115 PER SRM 53-01, FIG 4 SHEET 3 PAGE 18 DOUBLER REPAIR. TREATED AREA FROM STA 1145L TO 1169L AT LONGERON 18 PER SRM 51-10-3(C)(1)AND (3), PAGE 45 AND 46.
Part: FLOOR PAN — CORRODED (BS 1107 - 1149)
DURING CHECK-C MAINT, FOUND CORROSION AT MEMBRANE FLOOR PAN ALONG LONGERON 18L, FROM STA 1107 THROUGH 1149. REMOVED LIGHT AND MODERATE CORROSION ON THE LT FLOOR MEMBRANE, LONGERON 18L FROM STA 1107 TO 1149 PER SPM 6-80-01, PAGE 1-3. REPAIRED AREA STA 1118 TO 1123 PER SRM 53- 01, FIG 4 SHEET 3 PAGE 18. TREATED AREA FROM STA 1107 TO 1149 LONGERON 18L FLOOR MEMBRANE PER SRM 51-10-3.
Part: LONGERON — CORRODED (BS 1031)
DURING CHECK-C MAINT, FOUND CORROSION AT STA 1031R, LONGERON 18. REMOVED CORROSION PER SRM 6-80-01. INSTALLED DOUBLER PER SRM 53-01, FIG 4.
Part: MEMBRANE — CORRODED (BS 439)
DURING CHECK-C MAINT, FOUND CORROSION AND PILLOWING AT STA 439, LONGERON 18L MEMBRANE. REMOVED CORRODED SECTIONS OF MEMBRANE PER SPM 6-80-01, PAGE 1. REPAIRED PER SRM 53-01, PAGE 18.
Part: MEMBRANE — CORRODED (BS 57)
DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT STA 57R, LONGERON 18. CORROSION REMOVED PER SRM 53-01. INSTALLED DOUBLER PER 53-01.
Part: LONGERON — CORRODED (BS 1102)
DURING CHECK-C MAINT, FOUND CORROSION AT STA 1102R, LONGERON 18. CORRECTED PER SRM 53-01. TREATED AND PAINTED PER 51-10-B.
Part: LIGHT — INOPERATIVE (ROWS 19-22)
PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19 THROUGH 22. REPLACED PACK BATTERIES AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT FLICKERS ON AND OFF WITH ELECTRICAL POWER OFF. REPLACED THE BATTERIRES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)
Part: LIGHT — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (ROW 23-27)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: PIN — LOOSE (RT COCKPIT)
SEA - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED AND SECURED UPPER HINGE PIN ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M)
1998
Part: WIRE — DISCONNECTED (CABIN)
ONT - PRIOR TO DEPARTURE OF FLIGHT 555, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 137, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY AND GALLEY AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 137, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WOULD NOT EXTINGUISH WHEN CONTROL SWITCH PLACED TO OFF POSITION, WOULD EXTINGUISH WHEN SWITCH PLACED TO ARMED POSITION. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: PIN — OUT OF ADJUST (RT COCKPIT)
SEA - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT RT SLIDING WINDOW WAS FOUND DIFFICULT TO OPEN. ADJUSTED THE WINDOW GUIDE PIN AND OPERATED NORMALLY. (M)
Part: PANEL — MISALIGNED (COCKPIT)
ANC - AFTER ARRIVAL OF FLT 104, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN COMPLETELY. REPOSITIONED THE WINDOW TRIM PANEL AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: FUSE — FAILED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE FUSE IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 3 WAS FOUND PULLED UP AND THE 2ND FORWARD LIGHT WAS INOPERATIVE. RECONNECTED THE CONNECTOR TO THE LIGHT ASSEMBLY AND REINSTALLED THE TRACK COVER AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
1997
Part: CONNECTOR — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RECONNECTED CONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN AND LOWER TAILCONE AREA ILLUMINATE AND REMAIN ILLUMINATED WITH MAIN BATTERY SWITCH OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED CONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: JAMB — CORRODED (BS 180-200)
BFM - DURING 30K CHECK, CORROSION WAS FOUND ON R1 DOOR JAMB LOWER FORWARD CORNER. REPLACED LOWER SECTION OF R1 DOOR JAMB IAW DC9 SRM 53-05, FIG 55. TT: 29,023 HOURS. TC: 17,222. (X)
Part: SKIN — CREASED (RT LE FLAP)
BFM - DURNG 30K CHECK, CREASE WAS FOUND ON RT WING OUTBOARD FLAP INBOARD FIXED VANE. REPAIRED WITH BONDED DOUBLER IAW ASA EA 5750-01254. TT: 29,023 HOURS. TC: 17,222. (X)
Part: WEB — CORRODED (BS 927-946)
BFM - DURING 30K CHECK, CORROSION WAS FOUND ON CUSP MEMBRANE AT LONGERON 18L AND FS 930. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW ASA EA 5310-01556. TT: 29,023 HOURS. TC: 17,222. (X)
Part: HINGE ARM — GALLED (LT TE FLAP)
BFM - DURING 30K CHECK, GALLED BUSHINGS WERE FOUND ON LT WING OUTBOARD FLAP INBOARD HINGE ARM LOWER MOUNT BOLT AND CORROSION ON INBOARD LUG. REPAIRED IAW ASA EA 5750-01256. (X)
Part: HINGE ARM — GROOVED (RT TE FLAP)
BFM - DURING 30K CHECK, GROOVED BUSHINGS WERE FOUND ON RT WING OUTBOARD FLAP INBOARD HINGE ARM PIVOT AND CORROSION IN BORE. REPAIRED IAW ASA EA 5750-01256. TT: 29,023 HOURS. TC: 17222. (X)
Part: SKIN — CRACKED (RT TE FLAP)
BFM - DURING 30K CHECK, PUNCTURE WAS FOUND IN RT WING INBOARD FLAP OUTBOARD VANE ON INBOARD LOWER SURFACE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW DC9 SRM 51-70-02. (M)
Part: SEAT TRACK — CORRODED (BS 1032-1309)
BFM - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK FROM FS 1032 TO 1309. REPLACED SEAT TRACK IAW DC9 SRM 51-30-00. (M)
Part: WEB — CRACKED (BS 1170-1276)
BFM - DURING 30K CHECK, CRACK WAS FOUND ON CUSP WEB AND ELONGATED HOLES FROM FS 1170 TO FS 1276. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW DC9 SRM 53-05, PG 3, FIG 96. (M)
Part: FLOORBEAM — GOUGED (BS 1338)
BFM - DURING 30K CHECK, GOUGE WAS FOUND ON AFT LAVATORY FLOORBEAM AT FS 1338. REMOVED AND REPLACED TOP ANGLE OF FLOORBEAM AT FS 1338 IAW DC9 SRM 51-10-04 AND 51-30-02. (M)
Part: SKIN — CRACKED (NR 2 LE SLAT)
BFM - DURING 30K CHECK, CRACKS AND BROKEN RIVETS WERE FOUND IN LEFT WING NR 2 L/E SLAT LOWER SKIN. SPLICED SKIN IAW DC9 SRM 57-09, FIG 10. (M)
Part: SILL — CRACKED (BS 46)
BFM - DURING 30K CHECK, CRACK WAS FOUND ON NLG WHEEL WELL DOOR SILL FRAME AT FS 46, LBL 18. REMOVED AND REPLACED FRAME IAW DC9 ARM 51-30-02 AND 51-30-05. (M)
Part: WEB — PUNCTURED (BS 206)
BFM - DURING 30K CHECK, PUNCTURE WAS FOUND ON MAIN CABIN FLOOR WEB AT FS 206, RBL 56. REPAIRED PUNCTURE IN WEB IAW DC9 SRM 53-01, FIG 4. (M)
Part: FRAME — CRACKED (BS 47)
BFM - DURING 30K CHECK, CRACKS AT FASTENER HOLES WERE FOUND ON NLG WHEEL WELL FRAME AT FS 47, LBL 30. REPAIRED FRAME IAW DC9 SRM 53-30, PAGE 85. (M)
Part: CHANNEL — CRACKED (BS 1338)
BFM - DURING 30K CHECK, CRACK WAS FOUND ON AFT CABIN ENTRY DOOR UPPER LEFT CHANNEL UNDER HINGE. REMOVED AND REPLACED CHANNEL IAW DC9 SRM 51-30-02. (M)
Part: WEB — CORRODED (BS 200-220)
BFM - DURING 30K CHECK, CORROSION WAS FOUND ON MAIN CABIN CUSP WEB AROUND NUT PLATE HOLES FROM FS 200 TO FS 220, RBL 22. REPAIRED WEB IW DC9 SRM 53-01, PAGE 3, FIG 4. (M)
Part: SEAT TRACK — CORRODED (BS 200-579)
BFM - DURING 30K CHECK, CORROSION AND GOUGES WERE FOUND ON RT INBOARD SEAT TRACK FROM FS 200 TO FS 579, RBL 22. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 51-30-01, 51-30-02, 51-30-05 AND 53-05. (M)
Part: SKIN — CRACKED (LT TE FLAP)
BFM - DURING 30K CHECK, CRACK WAS FOUND LEFT OUTBOARD FLAP TE 14 INCHES OUTBOARD OF CENTER FLEX JOINT. REMOVED DAMAGED MATERIAL AND REPAIRED WITH FIBERGLASS DOUBLER IAW DC9 SRM 57-03, FIG 8. (M)
Part: SILL — CRACKED (BS 46-83)
BFM - DURING 30K CHECK, CRACK WAS FOUND ON NLG WHEEL WELL DOOR SILL FRAME AT FS 46, RBL 18. REMOVED AND REPLACED FRAME IAW DC9 SRM 51-30-02 AND 51-30-05. (M)
Part: SEAT TRACK — CORRODED (BS 1145-1271)
BFM - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK NR 2 FROM FS 1145 TO 1271. REPLACED SEAT TRACK IAW DC9 SRM 51-30-01 AND 53-05, FIG 4. (M)
Part: SKIN — DAMAGED (RT TE FLAP VANE)
BFM - DURING 30K CHECK, THE RT WING OUTBOARD FLAP VANE LEADING EDGE SKIN WAS FOUND DAMAGED AT 4 LOCATIONS. REPAIRED IAW ASA EA 5750-01254. (M)
Part: SKIN — GOUGED (BS 788)
BFM - DURING 30K CHECK, THE FUSELAGE SKIN WAS FOUND GOUGED ON OUTER SURFACE AT FS 788 BETWEEN LONGERON 17R AND 18R. REPAIRED IAW DC9 SRM 53-04, PG 22, FIG 38. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: SKIN — CRACKED (RT WING)
SEA - RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5730-01052. (M)
1996
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND OPERATED NORMALLY. (M)
Part: INFLATION BOTTLE — LOW PRESSURE (L2 DOOR)
OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE EMERGENCY EVACUATION SLIDE. (M)
Part: SLIDE — FAILED (TAIL CONE)
OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M)
Part: SLIDE — OUT OF POSITION (L2 DOOR)
LAX - AFTER ARRIVAL OF FLT 255 - CREW REPORTED THE L2 DOOR DIFFICULT TO OPEN, APPEARS TO BE STICKING AT LOWER AFT CORNER. FOUND THE EMERGENCY EVACUATION SLIDE COVER HOLDING THE DOOR TRIM OUT OF POSITION AND INTERFERRING WITH DOOR FRAME. REPLACED THE EMERGENCY EVACUATION SLIDE ASSEMBLY AND DOOR OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTNENANCE CHECK, THE 0VERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 6 WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DEFECTIVE (TAILCONE)
LAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: SLIDE BOTTLE — LOWPRESSURE (TAILCONE)
SEA - DURING MAINTENACNE CHECK, THE TAILCONE EMERGENCY EVACUATIONSLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE TAILCONEEMERGENCY EVACUATION SLIDE. (M)
1995
Part: EVAC SLIDE — FAILED TEST (R1 DOOR)
OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 20 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 20 REMAINED ILLUMINATED WITH THE SWITCH IN THE OFF POSITION. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FWD OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPAIRED WIRING, REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATTERY — LOOSE (CABIN)
ONT - FLT 531 - PRIOR TO DEPARTURE, CREW REPORTED ROW 13 EMERGENCY EXIT FLOOR TRACK LIGHTS WILL NOT TEST. RESEATED BATTERY IN PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FWD RT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHT OPERATED NORMALLY. (W)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM 16 TO 20 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 1 TO 3 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATTERY — DISCHARGED (CABIN)
SEA - CHECK, 3 CEILING LIGHTS INOP AT ROWS 24 AND 25. MAINTENANCE REPLACED BATTERIES AND SYSTEM OPS CHECKED NORMAL. (W)