N719AA
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.
77 reports on file, 1995-12-04 – 2001-08-23.
Part: CONTACTOR — WORN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH FLOOR LIGHT STRIP AFT OF FIRST CLASS DIM. REPLACED EMERGENCY PATH FLOOR LIGHT CONDUCTOR STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — DAMAGED (FUSELAGE)
TUL - FOUND AREA OF FUSELAGE SKIN HAS DEEP BLEND OUT AREAS OF PREVIOUS GOUGES BETWEEN STRINGER 17 AND 18L AT STATION 1090. INSTALLED DOUBLER OVER DAMAGED AREA PER SRM 53-30-3 FIG 1. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
TUL - FOUND LIGHT INOPERATIVE, EMERGENCY AFT STAIR OVERHEAD. INSTALLED SERVICEABLE LIGHT ASSEMBLY. OPS CHECK OK. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON STRINGER 23R STATION 1165. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 1. (M)
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND CRACK IN SKIN AT FASTENER HOLE AT STATION 328 JUST BELOW STRINGER 20L. INSTALLED REPAIR PER SRM 53-30-3 FIG 13. (M)
Part: SPLICE — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT OF FIRST CLASS DIM. REPLACED EMERGENCY EXIT LIGHT FLOOR SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PROXIMITY LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FLOOR PATH EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FLOOR PATH EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1995–2000 · 69 reports
2000
Part: WARNING LIGHT — ILLUMINATED (COCKPIT)
DFW - FLT 434 - DURING CLIMB THROUGH 17,000 FEET, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ON TAXI TO GATE SMOKE OBSERVED FROM NR 2 ENGINE. ACCOMPLISHED ENGINE HIGH POWER RUN. NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — SHORTED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN FIRST CLASS AND COACH SHORTED. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHTS CONDUCTOR WIRE BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT ROW 3 INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP AT ROW 3. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 74,746 hrs · 52,455 cycles
TUL- LEFT VERTICAL STABILIZER TO FUSELAGE CORD ANGLE CRACKED THROUGH 2 FASTENERS IN VERTICAL LEG STA 1381. REPAIRED CORD ANGLE PER ESO 11697 DATED 4-14-00. (X)
Part: PRESSURE PANEL — CRACKED (RT WHEELWELL) · airframe 74,746 hrs · 52,455 cycles
TUL - RIGHT WHEELWELL PRESSURE DECK CRACKED APPROXIMATELY 1 INCH AT BEND, STA 950 RBL 52 TO RBL 70. INSTALLED REPAIR DOUBLER IN RT WHEELWELL PRESSURE DECK, STA 940 - STA 950, RBL 52 - RBL 70 IAW ESO 11697 DATED 4-11-00. REF: SB 53-149R4 AND DRWING 65-89360 AND 65C 36247. (X)
Part: SKIN — CRACKED (VERTICAL STAB) · airframe 74,746 hrs · 52,455 cycles
TUL- VERTICAL STABILIZER SKIN CRACKED AT STA 1340, LEFT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER BOEING SB 727-55-82. (X)
Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 74,746 hrs · 52,455 cycles
TUL - SKIN BULGING AND RIVET DISHED, LT 580 STR 26L. REMOVED SURFACE CORROSION FROM SKIN AT STA 580 BETWEEN STR 25 AND STR 26L PER SRM 51-10-6. ALODINED AND PRIMED SKIN. INSTALLED SERVICEABLE SHEAR TIE PER SRM 51-10-1. (X)
1999
Part: RIB — CRACKED (WS 760)
TUL - LEFT BS 760 RIB CHORD, HFEC SHOWS CRACK INDICATION APPROX .75 INCH AFT OF FLOORBEAM WEB AT LOWER EDGE OF REPAIR DOUBLER. REPAIRED PER SB 727-57-0112 FIG 12 SRM 57-10-5 PAGE 1, E589069177. (M)
Part: SKIN — DENTED (BS 1305)
TUL - SMALL DENT, FORWARD OF EXT POWER PANEL AND CRACK EXTENDING FROM RIVET. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER PER 53-30-3 FIG 5. (M)
Part: SKIN — LIGHTNING STRIKE (BS 227.8)
TUL - LIGHTNING STRIKE STATION 227.8 JUST BELOW STRINGER 17R. CUT OUT DAMAGE. INSTALLED DOUBLER PER SRM 53-30-3 FIG 13A WITH PERMANENT FASTENERS. (M)
1998
Part: DOUBLER — CORRODED (BS 720)
TUL - LIGHT HOUSING AND SKIN DOUBLER CORRODED. TREATED AND PRIMED DOUBLER PER SRM 51-20-0, INSTALLED NEW LIGHT HOUSING PER SRM 51-10-1. (M)
Part: STRINGER — CRACKED (WS 656)
TUL - TOP FORWARD STRINGER CRACKED AT STATION 656.5 OUTBOARD SIDE. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER SB 727-57A159 REV 5. (M)
Part: STRINGER — CRACKED (WS 656)
TUL - FOUND STRINGER CRACKED 4TH TAB AFT OUTBOARD SIDE STATION 656.5. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER SB 727-57A 159 REV 5. (M)
Part: STRINGER — CORRODED (BS 620)
TUL - FOUND CORROSION ON STRINGER 27R OUTBOARD LEG (VERTICAL) AT STATION 620. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PGS 4C-4E. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED AREA. (M)
Part: SKIN — CORRODED (BS 1143-1149)
TUL - RIVETS PULLING THROUGH, HEADS CRACKED, STA 1143 TO STA 1149, STR 23L, 4 EACH FASTENERS. FOUND CORROSION BETWEEN DOUBLER SKIN (WHEN REMOVING FASTENERS). REMOVED CORROSION, REPAIRED AREA, INSTALLED DOUBLER AND TRIPLER PER ECO 11697 DATED 6-24-98, REVISED 6-25-98. TST: 70,062 HOURS. CYCLES: 49,889. (X)
Part: ANGLE — CRACKED (BS 950)
TUL - NR 2 CARGO DOOR FRAME UPPER CHORD ANGLE WORN AND CRACKED JUST AFT STR 26R (MARKED) (FORWARD EDGE OF DOOR). STOP DRILLED CRACK, FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM 51-40-4. (X)
Part: ANGLE — CRACKED (FUSELAGE)
TUL - FOUND CRACK IN CORNER ANGLE INBOARD OF APU AIR BOX FLANGE. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)
Part: FRAME — CRACKED (BS 950)
TUL - FOUND CRACK IN BELTFRAME AT 950F BETWEEN STRINGER 26L AND 27L. STOP DRILLED CRACK. INSTALLED DOUBLER PER AARD 53-10-07-3. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER CRACKED 15L STA 720B FORWARD OF ICE LIGHT HOUSING AT END OF STRINGER. REPAIRED STR 15L FORWARD OF ICE LIGHT STA 720B PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X)
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER CRACKED 15L STA 720C AFT SIDE OF ICE LIGHT AT END OF STRINGER. REPAIRED STR 15 LT AFT SIDE OF ICE LIGHT STA 720C PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X)
Part: STRINGER — CRACKED (WS 656)
TUL - TOP AFT STRINGER CRACKED, STA 656.56 AT FLANGE HOLE. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SB 727-57 A 159 REV 5. TST: 70,062 HOURS. CYCLES: 49,889. (X)
Part: STRINGER — CRACKED (WS 656)
TUL - UPPER STRINGER CRACKED, 3RD TAB AFT OUTBOARD SIDE STATION 656.5. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER SB 727-57 A159 REV 5. (M)
Part: FITTING — CORRODED (BS 1183)
TUL - STRINGER END FITTING CORRODED, STRINGER 5R STATION 1183. REPLACED END FITTING 65-24276-10, STRINGER 5 NEW END FITTING PER SRM 51-10-1. (M)
Part: BEAM — CORRODED (BS 744)
TUL - FOUND LOWER SKIN ON DELTA BEAM CORRODED AND BLOWN OUT STATION 744 FWD END. REMOVED DAMAGED WEB. INSTALLED WEB REPAIR PER SRM 51-40-2 FIG 1. (M)
Part: FLOORBEAM — CORRODED (BS 360)
TUL - FOUND CORROSION ON TOP FLANGE OF FLOORBEAM STATION 360 LBL 10 INCHES AT NUTCLIP HOLE. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-10-8. (M)
Part: FRAME — DENTED (BS 950)
TUL - DENT IN FRAME AT 950F STRINGER 25 AND 24 RT. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER AARD 53-10-07-3. (M)
Part: WEB — CRACKED (BS 874)
TUL - TWO EACH CRACKS IN WEB SKIN FORWARD END RT APU CUT-OUT. STOP DRILLED CRACKS. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2. TST: 70,062 HOURS. CYCLES: 49,889. (X)
Part: WEB — CORRODED (BS 1183)
TUL - FOUND CORROSION ON CHORD STATION 1183 RBL 20. FOUDN AFTER FASTENER REMOVAL OF CHORD ANGLE, CHORD ANGLE DISPLACED. REPLACED ALL FASTENERS TO RESTORE STRUCTURE AT HAT CHANNEL FLOOR PANS AND CHORD ANGLE. REPLACED FLOOR PAN AREA COMMON TO CHORD ANGLE IAW 51-40-2, 16 BY 12 AREA. (M)
Part: SKIN — GOUGED (BS 1130-1150)
TUL - SKIN DENTED AND GOUGED BETWEEN STA 1130 - STA 1150, STR 3R - STR 4R (DUE TO DOCK STRIKE). INSTALLED REPAIR DOUBLER PER SRM 53-30-3 CUTTING OUT DAMAGE AND INSTALLING FILLER WITH SCAB EXT DOUBLER. (X)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND CORROSION ON INNER SKIN JUST INBOARD OF STRINGER 28L, STATION 720C TO STATION 720C PLUS 5 INCHES. INSTALLED DOUBLER AS PER SRM 53-30-3 AND 51-20-1 AND PER AARD 53-30-03-3 PAGE 1. (M)
Part: STRINGER — CORRODED (BS 678)
TUL - FOUND STRINGER 25R CORRODED ON LOWER VERTICAL LEG AT STATION 678. REMOVED STRINGER FROM STATION 675 TO 690 AND INSTALLED NEW STRINGER SPLICE PER ESO 11697, DATED 6-4-98 TITLED BS 680, STRINGER 25R REPAIR RT SIDE. (M)
Part: SKIN — DENTED (BS 420)
TUL - FOUND SCRATCH AND DENT IN FUSELAGE STATION 420. REMOVED DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-30-3 FIG 3 PAGE 12. (M)
Part: LIGHT — INOPERATIVE (COCKPIT)
DFW - DURING OVERNIGHT CHECK, DISCOVERED COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR LIGHTS IN FORWARD PASSENGER CABIN NOT OPERATING PROPERLY. REPLACED JUMPER WIRE AT FORWARD PASSENGER CABIN FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: T-CHORD — MIS-DRILLED (BS 265)
AFW - FOUND T-CHORD HAS 3 MIS-DRILLED HOLES. REPAIRED PER MRB 727-0044. (M)
Part: STRAP — CORRODED (BS 684-689)
AFW - TEAR STRAP CORRODED AT STATION 684-689 STRINGER 26R. CUT OUT CORRODED TEAR STRAP INSTALLED DOUBLER PER SRM 53-30-3. (M)
Part: BEAM — CORRODED (BS 780-790)
AFW - LEFT DELTA BEAM CORRODED AT STATION 780-790 OUTBOARD OF PANEL 3358. REMOVED AND REPLACED BEAM PER SRM 51-40. (M)
Part: FRAME — CORRODED (BS 480)
AFW - FOUND FRAME CORRODED AT STA 480. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10.
Part: SKIN — CORRODED (BS 693)
AFW - FOUND CORROSION ON SKIN AT STRINGER 26R. REMOVED CORRODED SECTION OF SKIN. INSTALLED REPAIR IAW SRM 53-30-3. (M)
Part: ANGLE — CORRODED (BS 770)
AFW - FOUND SUPPORT ANGLE AT STATION 770, RBL 10 HAS CORROSION. FABRICATED DOUBLER FOR CORRODED AREA AND INSTALLED AS PER SRM. (M)
Part: STRINGER — CORRODED (BS 670)
AFW - FOUND CORROSION ON SKIN AT STRINGER SPLICE STRINGER 27R STATION 670-690. (M)
Part: SKIN — CORRODED (BS 684)
AFW - FOUND CORROSION ON SKIN STRINGER 28R. REMOVED CORRODED SECTION OF SKIN, INSTALLED REPAIR IAW SRM 53-30-3. (M)
Part: STRINGER — CORRODED (BS 700)
AFW - FOUND CORROSION AROUND FASTENERS IN STRINGER. REPLACED STRINGER IAW SRM 53-10-3. (M)
Part: STRINGER — CRACKED (BS 367)
AFW - FOUND STRINGER 19R CRACKED AND CORRODED AT FORWARD END. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-10-3. (M)
Part: ANGLE — CORRODED (BS 740-760)
AFW - T-ANGLE AT STATION 740-760 RBL 10 CORRODED. REMOVED CORRODED ANGLE AND INSTALLED WITH NEW 'T' ANGLE. (M)
Part: STRINGER — CORRODED (BS 670)
AFW - FOUND STRINGER SPLICE CORRODED 27R STATION 670-690. REPLACED STRINGER SPLICE IAW SRM 53-10-3. (M)
Part: STRINGER — CORRODED (BS 720)
AFW - FOUND STRINGER CORRODED 26R STATION 720E-720F. FABRICATED AND INSTALLED STRINGER REPAIR ON STRINGER 26R AT STATION 720E TO STATION 720F PER SRM 53-10-3. (M)
Part: FRAME — CORRODED (BS 600)
AFW - FOUND FORWARD AND AFT SIDE OF BELTFRAME CORROSION BETWEEN STRINGER 28R AND 27R, STATION 600. FABRICATED NEW SHEAR TIE, INSTALLED IAW 51-10-1. (M)
Part: SKIN — CORRODED (BS 600)
AFW - CORROSION ON FRAME TO SKIN AT STA 600 STR 27R - STR 28R. REMOVED CORROSION IAW SRM 51-10-6, FOUND OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-10-4. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: SKIN — CORRODED (BS 580)
AFW - INNER SURFACE OF SKIN CORRODED AT STATION 580-595, STRINGER 28R. CUT OUT DAMAGED AREA, FABRICATED DOUBLER PER SRM 53-30-3. (M)
Part: INTERCOSTAL — CORRODED (BS 600)
AFW - FOUND CORROSION UNDER INTERCOSTAL BETWEEN STATION 580-600, STRINGER 27R-28R. REMOVED AND REPLACED PART IAW SRM 51-10-1. (M)
Part: BRACKET — CORRODED (BS 620)
AFW - FOUND CORRODED CLIP NUT BRACKET. INSTALLED NEW CLIP BRACKET. (M)
Part: STRINGER — CORRODED (BS 950)
AFW - FOUND CORRODED STRINGER, STATION 950 STRINGER 27R. REPAIRED STRINGER PER SRM 51-40-4. (M)
Part: STRINGER — CORRODED (BS 686)
AFW - FOUND CORROSION PRESENT AROUND FASTENERS IN CENTER OF STRINGER 26R. REMOVED AND REPLACED CORRODED SECTION OF STRINGER PER SRM 53-10-3. (M)
Part: WEB — CORRODED (BS 790)
AFW - FOUND CORROSION ON ANGLE AND WEB AFT OF PANEL LANDING FOR PANEL 3448. ADDED DOUBLER AND FILLER. (M)
Part: STRINGER — CORRODED (BS 680-684)
AFW - CORROSION AT STRINGER SPLICE STA 680 - STA 684, STR 20R. REMOVED CORROSION, TREATED AND PRIMED. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: SKIN — CORRODED (BS 720)
AFW - FRETTING CORROSION ON FUSELAGE SKIN AT STATION 720D PLUS 10 INCHES. REPAIRED DAMAGED AREA PER SRM 53-30-3. (M)
Part: SKIN — CORRODED (BS 720)
AFW - FRETTING CORROSION ON FUSELAGE SKIN FROM STA 720D + 10 INCHES TO STA 720E + 10 INCHES, STR 17L TO STR 19L. REPAIRED PER MRB 727-0043. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: SKIN — CORRODED (BS 504)
AFW - CORROSION AT STA 504, STR 24R AND SKIN. REMOVED CORROSION AND INSTALLED DOUBLERS IAW SRM 53-10-3. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: ANGLE — CORRODED (BS 720)
AFW - CORROSION UNDER TWO NUTPLATES AT INBOARD END OF WING-TO-BODY FAIRING SUPPORT ANGLE STA 720 AND STR 28L - STR 28R. ALODINED AND PRIMED NEW PART PER SRM. INSTALLED WITH NEW NUTPLATES. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: ANGLE — CORRODED (BS 720)
AFW - CORROSION ON SUPPORT ANGLE AROUND GROUND WIRES AT STA 720B, BL ZERO. REMOVED DAMAGED SECTION OF ANGLE AND REPAIRED PER SRM 51-40-3. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: ANGLE — CORRODED (BS 720)
AFW - CORROSION UNDER 2 NUTPLATES AT INBOARD END OF WING-TO-BODY FAIRING SUPPORT ANGLE AT STA 720 + 10 INCHES AND STR 28R. ALODINED AND PRIMED PER SRM, INSTALLED NEW ANGLE SUPPORT AND NUTPLATES. TST: 68,096.30 HOURS. CYCLES: 48,857. (X)
Part: STRINGER — CORRODED (BS 670-690)
TUL - SKIN CORRODED, RIVETS PULLED, STR 27L STA 670 TO STA 690. REMOVED CORRODED SECTION OF STR 27L, FOUND NO CORROSION ON SKIN. INSTALLED NEW STRINGER SPLICE PER SRM 53-10-3. TST: 67,283. CYCLES: 48,400. (X)
Part: CONNECTOR — BROKEN (CABIN)
RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING INOPERATIVE. AIRCRAFT MAINTENANCE FERRY RDU/DFW. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: WIRE — BROKEN (L1 DOOR)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT SYSTEM SIDEWALL LIGHT AT L1 DOOR INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT SYSTEM SIDEWALL LIGHT WIRE AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — CRACKED (LT TE MID FLAP)
TUL - OUTBOARD LEFT MID FLAP TOP SKIN IS CRACKED APPROXIMATELY ON TOP OF TRAILING EDGE FLAP OUTBOARD SPRING ROD END (MARKED ON FLAP) STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-50-4. EDGE SEALED, TREATED, PRIMED AND PAINTED. (M)
Part: BLKHD SKIN — CRACKED (BS 1183)
TUL - CRACK IN FORWARD SKIN OF TAIL SKID, LT SIDE, AT ANGLE BRACKET, STA 1183. INSTALLED DOUBLER PER SRM 53-10-2, PAGE 28. TST: 64,360. CYCLES: 46,865. (X)
Part: SKIN — CORRODED (BS 483)
TUL - CORROSION OUT OF LIMITS ON FUSELAGE SKIN. REPLACED PER SRM 53-30-3, FIGURE 3A (SHEET 3). TST: 64,356. CYCLES: 46,864. (X)
1995
Part: LIGHT — DEFECTIVE (GALLEY DOORS)
DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS OVER FORWARD GALLEY AND AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER FORWARD AND AFT GALLEY DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)