N727AA
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, 1996-02-16 – 2001-04-09.
Part: MODULE — INOPERATIVE (L2 DOOR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR DIM. TIGHTENED EMERGENCY EXIT LIGHT BATTERY PACK AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — DISCHARGED (COCKPIT)
DFW - DURING OVERNIGHT MAINTENANCE, FOUND COCKPIT EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: MODULE — DEFECTIVE (CABIN)
IAD - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRAP — CRACKED (BULKHEAD)
TUL - FOUND THE STRAP ON VERTICAL STIFFENER RBL 26.83 WL 273 AT 1183 BULKHEAD WAS GOUGED UPON REMOVAL OF STRAP FASTENER HOLE AND FOUND CRACKED FROM HOLE. STRAP WAS REMOVED AND NEW STRAP INSTALLED SRM 51-10-1 DOUBLERS ON BOTH SIDE OF VERTICAL STIFFENER WERE INSTALLED WITH STEEL FASTENERS SRM 51-42-4. (M)
Part: FLOORBEAM — CRACKED (FUSELAGE)
TUL - FOUND FS 825.95 FLOOR FRAME WEB IS CRACKED THROUGH BOTH SIDES OF LIGHTENING HOLE NEXT TO BL 48 RT SEAT TRACK. STOP DRILLED CRACKS. INSTALLED DOUBLER PER SRM 51-402. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND LIGHT TO MODERATE CORROSION ON BOTTOM OF STRINGER, ABOVE LEFT PRIMARY HEAT EXCHANGER AFT INBOARD SECTION. INSTALLED REPAIR PER SRM 57-30-3 FIG 9. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
TUL - FOUND CABIN FLOOR BEAM CORRODED BOTTOM FLANGE PLATE HOLES, STATION 1130. REPAIRED PER ESO11697 DATED 1/30/01. (M)
Part: DOOR FRAME — CRACKED (GALLEY DOOR)
TUL - FOUND LOWER AFT CORNER OF FORWARD GALLEY DOOR HAS TWO SKIN CRACKS DOOR CUTOUT. STRIPED PAINT INSTALLED DOUBLER PER SERVICE BULLETIN 727-53-0188. (M)
Earlier reports · 1996–2000 · 68 reports
2000
Part: LANDING GEAR — LACK OF LUBE (NOSE)
MCI - FLT 1379 - DURING LANDING MCI, NOSE GEAR LANDING GEAR FAILED TO FULLY EXTEND. RECYCLED GEAR AND GEAR EXTENDED NORMALLY. LANDED MCI WITHOUT INCIDENT. LUBED NOSE LANDING GEAR, SWUNG NOSE GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 73,050 hrs · 47,075 cycles
TUL - CORROSION ON STA 1070 FLOORBEAM LOWER FLANGE AROUND 2 NDT PLATES, RBL 10 AND LBL 10. INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 4-21-00. (X)
1999
Part: SHEAR TIE — CORRODED (BS 680)
TUL - CORROSION ON SHEAR TIES BETWEEN BL ZERO AND STR 26L. INSTALLED REPAIRS BETWEEN STR 28L AND STR 27L PER SRM 53-10-4 FIG 15 SHEET 3 REPAIR 3. INSTALLED NEW SHEAR TIE BETWEEN STR 27L AND STR 26L PER SRM 51-10-1. TST: 72,089 HOURS. CYCLES: 46,585. (X)
Part: SKIN — DENTED (VERT STABILIZER)
TUL - VERTICAL STABILIZER DENT IN SKIN 34 INCHES AFT OF RIGHT AMERICAN FLAG IN SKIN STA 1223 WITH CRACK IN DENT. INSTALLED DOUBLER PER SRM 54-10-3. TST: 72,089.43 HOURS. CYCLES: 46,585. (X)
Part: FRAME — CRACKED (BS 783)
TUL - CRACK IN FRAME AT STA 783 LEFT FRAME. INSTALLED REPAIR ANGLES PER DWG 65C36280 AND PER SB 727-53-0197. TST: 72,089.5 HOURS. CYCLES: 46,585. (X)
Part: SHEAR TIE — CORRODED (BS 720)
TUL - SHEAR TIE IN FORWARD CARGO CORRODED STA 720 STR 28L TO STR 28R. REMOVED CORRODED SHEAR TIE AND FABRICATED AND INSTALLED NEW SHEAR TIE SRM 51-10-1. TST: 72,089.43 HOURS. CYCLES: 46,585. (X)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
BNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIPS FROM FRONT OF COACH TO FRONT OF FIRST CLASS INOPERATIVE. REPLACED CONNECTOR BETWEEN FIRST CLASS AND COACH EMERGENCY EXIT FLOOR PATH LIGHTS STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 6D AND 28D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BULKHEAD — CRACKED (BS 870)
TUL - 870 BULKHEAD CRACKED AT THE LOAD CONTROL VALVE CUT OUT, 5 O'CLOCK POSITION. STOP DRILLED CRACK TO .250 INCH FABRICATED AND INSTALLED DOUBLER AND TRIPLER AROUND CUT OUT PER SRM 53-10-2 PAG 26. (M)
Part: BRACKET — CORRODED (WS 513)
TUL - FOUND CORROSION ON INBOARD SIDE OF OUTBOARD MOUNT BRACKET FOR NR 3 LE SLAT ACTUATOR. INSTALLED NEW MOUNT BRACKET ON INBOARD SIDE OF OUTBOARD MOUNT BRACKET NR 3 SLAT ACTUATOR. (M)
1998
Part: LIGHT — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE CEHCK, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT COACH INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WEB — CRACKED (BS 1363)
TUL - APPROX .75 INCH CRACK IN WEB RADIUS AT UPPER CORNER ATTACH TO VERTICLE FIN RT SIDE STATION 1363. STOP DRILLED CRACK, INSTALLED WEB ANGLE DOUBLER REPAIR PER SRM 51-40-2 FIG 1. (M)
Part: STRINGER — CORRODED (BS 1030-1040)
TUL - CORROSION ON STR 27R STA 1030 - STA 1040 AND SKIN UNDER STRINGER. REMOVED CORROSION, REPAIRED PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SHEAR TIE — CORRODED (BS 720)
TUL - FOUND CORROSION ON SHEAR TIE STRINGER 26R AT STATION 720. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1. (M)
Part: STRINGER — CORRODED (BS 720)
TUL - CORROSION AT STR 23L, STA 720E TO 720F. REPAIRED STRINGER PER SRM 53-10-3, FIG 1, SHEET 4, DETAIL NR 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (WS 431)
TUL - AREA OF BULGED AND DISTORTED SKIN UPPER FIXED LEADING EDGE JUST ABOVE INBOARD END OF FUELING PANEL, POSSIBLE CORROSION. REMOVED DAMAGED AREA, INSTALLED FLUSH REPAIR PER SRM 57-30-4. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: FLOOR BEAM — CORRODED (BS 1130)
TUL - APPROXIMATELY ONE-HALF DIAMETER OF DEEP CORROSION ON TOP OF FLOOR BEAM STA 1130 RBL 2411. REPAIRED AFFECTED AREA WITH STRAP DOUBLER PER ESO 11697 DATED 12-12-97. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 840-826)
TUL - CORROSION EMANATING FROM LONGITUDINAL SKIN LAP. INSTALLED EXTERNAL DOUBLER 11 INCHES BY 14 INCHES PER SRM 53-30-3 FIG 14 SHEETS 1 THROUGH 6. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CRACKED (BS 580)
TUL - STR 28L CRACKED, DAMAGED OUTBOARD LEG STA 580. REPAIRED STR PER SRM 53-10-3, FIG 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SHEAR TIE — CORRODED (BS 680)
TUL - FOUND CORROSION AT SHEAR TIE STATION 680 BETWEEN STRINGER 26L AND STRINGER 27L. REPLACED SHEAR TIE PER SRM 51-10-1. (M)
Part: SKIN — CORRODED (BS 580)
TUL - SKIN BULGED OUT AT THE FLUSH REPAIR STA 580, STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CORRODED (BS 680-700)
TUL - CORROSION AT STR 26L BETWEEN STA 680 AND STA 700 (MKD). REPAIRED STRINGER PER SRM 53-10-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 1030-1040)
TUL - CORROSION COMING OUT AROUND FASTENERS AND SKIN AND BETWEEN SKIN AND STRINGER. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CRACKED (BS 720)
TUL - STR 15L CRACKED IN U-CHANNEL FROM END TO FIRST FASTENER AT 720C. REPAIRED STA PER 53-10-3, FIG 5, SHEET 2. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: WEB — CORRODED (BS 1130-1183)
TUL - RIGHT AFT LAV FLOOR WEB HAS SEVERAL AREAS OF CORROSION ON TOP SIDE. INSTALLED NEW FLOOR WEB PER SRM 51-10-1 PAGE 4. (M)
Part: SKIN — CORRODED (BS 500)
TUL - LOWER SKIN BULGED AT STR 27R STA 500. INSTALLED EXTERNAL DOUBLER AT STR 27R STA 500 PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 990-1010)
TUL - CORROSION IN SEALANT AT STR 10R STA 990 - STA 1010 AT SKIN LAP. REPAIRED PER SRM 53-30-3 FIG 5 PER ESO 11697 DATED 12-8-97. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 708)
TUL - SKIN BULGING AROUND FASTENER HOLE STA 708 OUTBOARD STR 26R. REPLACED DAMAGED SKIN PER SRM 53-30-3 FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SHEAR TIE — CRACKED (BS 720)
TUL - STA 720, ABOVE STR 18L, BELT FRAME SHEAR TIE IS CRACKED. REPAIRED PER SRM 51-40-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: BEAM — CRACKED (BS 1183)
TUL - FOUND CRACK RIGHT SIDE 1183 BEAM FORWARD SIDE 24 INCHES OUTBOARD FROM VAULT DOOR FRAME STRINGER 13 AREA. INSTALLED SERVICEABLE BEAM PREVENT MOD AND REPAIR PER BOEING BWG 65C34406 (S/B 727-53-0192). (M)
Part: SKIN — CORRODED (BS 700)
TUL - SKIN BULGED OUT AND FRONT BROKEN IN SKIN LAP AND DOUBLER, STR 26R, STA 700. DAMAGED AREA REPAIRED PER SRM 53-30-3, FIG 4. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 715)
TUL - CORROSION UNDER STR 26R FROM STA 696 TO STA 715. REPAIRED PER SRM 53-30-3 FIG 14. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 720)
TUL - CORROSION UNDER STR 26R BETWEEN STA 720C TO STA 720D. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: FLOORBEAM — CORRODED (BS 328)
TUL - FOUND STATION 328, 52LBL FLOORBEAM CORROSION. INSTALLED DOUBLER ON FLOORBEAM PER SRM 53-10-08 PAGE 49-53. (M)
Part: SKIN — CORRODED (BS 681)
TUL - FUSELAGE SKIN BULGED STA 681 BETWEEN STR 28L AND STR 28R. REPLACED DAMAGED SKIN PER SRM 53-30-3 FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CORRODED (BS 720)
TUL - CORROSION AT STR 23L STA 720E TO STA 720F. REPAIRED STRINGER PER SRM 53-10-3, FIG 1, SHEET 4, DETAIL NR 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 720)
TUL - CORROSION UNDER STR 26R BETWEEN STA 720C TO STA 720D. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — DENTED (BS 332)
TUL - 3 INCH DENT AND GOUGE BELOW STR 24R, STA 332. REPAIRED MINOR DENT IN SKIN PER SRM 53-30-3 PAGE 154 FIG 24 SHEET 4. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: SKIN — CORRODED (BS 552)
TUL - SKIN BULGED OUT AT THE REPAIR STA 552, STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CRACKED (BS 720)
TUL - STR 15L CRACKED IN U-CHANNEL FROM END TO FIRST FASTENER STA 720B. REPAIRED STR PER SRM 53-10-3 FIG 5, SHEET 2. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CORRODED (BS 552/555)
TUL - STR 27L HAS CORROSION ON BOTTOM AT STA 552 TO STA 555. REPAIRED STR PER SRM 53-10-3 FIG 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: BEAM — CORRODED (HORIZ STABILIZER)
TUL - SEVERAL AREAS OF CORROSION ON AFT EDGE OF RT HORIZONTAL REAR UPPER CHORD. REPLACED RT AFT HORIZONTAL BEAM. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: FRAME — CRACKED (BS 277)
TUL - BELL FRAME CRACKED STA 277 AT STR 16 LEFT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CORRODED (BS 680-700)
TUL - CORROSION UNDER STRINGER BETWEEN STA 680 - STA 700. REPAIRED DAMAGED AREA PER SRM 53-10-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
Part: STRINGER — CRACKED (BS 720)
TUL - STR 15R CHANNEL CRACKED STA 720B AT RIGHT ZEE LIGHT. INSTALLED REPAIR PER SRM 53-10-3, FIG 5. TST: 67,236. CYCLES: 44,034. (X)
1997
Part: ACCESSORY UNIT — DEFECTIVE (E/E COMPT)
MIA - FLT 631 - DURING APPROACH TO MIA WHEN LANDING GEAR EXTENDED, RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHED MANUAL GEAR EXTENSION AND VISUALLY CONFIRMED RIGHT MAIN LANDING GEAR EXTENDED. AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL. (M)
Part: LIGHT — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT RIGHT FORWARD OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT RIGHT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — DAMAGED (BS 1100)
TUL - HOLE AND DENT IN FUSELAGE SKIN AT STA 1100 BETWEEN STA 21 - STA 22R. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 2. TST: 66,625 HOURS. CYCLES: 43,709. (X)
Part: SKIN — CORRODED (BS 740)
AFW - CORROSION REMOVED FORWARD OF STA 740, S26L AND S27L. REMAINING METAL BEYOND LIMITS. ADDED DOUBLER PER MRB 727-0035. TST: 66,102.09. CYCLES: 43,435. (X)
Part: SKIN — CORRODED (BS 720)
AFW - FUSELAGE SKIN HAS CORROSION REMOVAL BEYOND SRM LIMITS. ADDED DOUBLER PER MRB 727-0034. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: SKIN — CORRODED (BS 740)
AFW - SKIN AT STA 740, STR 26L IS CORRODED. INSTALLED DOUBLER PER MRB 727-0035. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: SKIN — CORRODED (BS 720)
AFW - CORROSION ON SKIN ADJACENT TO STR 26R FORWARD OF BS 720F. REPAIRED PER MRB 727-0034. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: ANGLE — CORRODED (BS 738)
AFW - CORROSION ON SUPPORT ANGLE ON LOWER FUSELAGE. REMOVED AND RE-INSTALLED NEW SUPPORT ANGLE. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: SHEAR TIE — CORRODED (BS 540)
AFW - SHEAR TIE CORRODED OUTBOARD STR 27R AFT FRAME AT STA 540. REMOVED DAMAGED SHEAR TIE, INSTALLED NEW SHEAR TIE PER SRM 53-10-2. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: STRINGER — CORRODED (BS 740)
AFW - STRINGER END CORRODED A STA 740, STR 27R. REMOVED AND CORROSION AND REPAIRED PER SRM 53-10-3. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: STRINGER — CORRODED (BS 720-740)
AFW - STR 27R FROM STA 720F + 10 TO 740 SEVERELY CORRODED. REMOVED CORROSION AND REPAIRED STRINGER PER SRM 53-10-3. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: INTERCOSTAL — CORRODED (BS 950)
AFW - WEB CORRODED. REMOVED AND REINSTALLED NEW INTERCOSTAL WEB PER SRM 53-10. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: STRINGER — CORRODED (BS 720-740)
AFW - CORROSION ON TOP AND SIDE OF STRINGER AT STA 720F - STA 740. REPLACED CORRODED STRINGER PER SRM 53-10-3. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: STRINGER — CORRODED (BS 675)
AFW - CORROSION IN AREAS AS MARKED STA 675, 27R. REMOVED FASTENERS FROM 660 TO 680. REMOVED CORROSION ON STR 27R. INSTALLED STRINGER. REPAIRED DAMAGE AT STA 670 PER RM 53-10-3. ALODINED, PRIMED, AND PAINTED AREA AND REINSTALLED NEW FASTENERS. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: STRINGER — CORRODED (BS 640-670)
AFW - CORROSION INSIDE STR 27R FROM STA 640 - STA 670. REMOVED FASTENERS FROM STA 640 TO STA 670. REMOVED CORROSION ON STR 27R. INSTALLED STRINGER, REPAIRED DAMAGE AT STA 670 PER 53-10-3, AND RE-INSTALLED NEW FASTENERS FROM STA 640 - STA 670. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: STRINGER — CORRODED (BS 720)
AFW - CORROSION ON STR 27L, STA 720F. REPLACED CORRODED STRINGER AT 720F PER SRM 53-10-3. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
Part: WEB — CORRODED (BS 990)
AFW - CORROSION ON WEB, FRONT AND BACK SIDES FORWARD OF STA 990 AND OUTBOARD OF 529R. TST: 66,102.09 HOURS. CYCLES, 43,435. (X)
1996
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE R1 DOOR INOPERATIVE. REPLACED THE EMERGENCY EXIT LIGHT ABOVE R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONTROL UNIT — DEFECTIVE (E/E COMPT)
RDU - FLT 1880 - EN ROUTE MIA/DTW DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT BEGAN TO FLICKER. SHORTLY AFTER BEGINNING QRH PROCEDURE, LIGHTS STOPPED FLICKERING AND SYSTEM WOULD NOT TEST. AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. REPLACED FIRE DETECTION ACCESSORY CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FRAME — CRACKED (BS 825.95)
TUL - CRACK IN FRAME WEB, STA 825.95, LT STR 16 CUT-OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2, PAGES 1-8, AND SRM 51-40, PAGE 1. TST: 62,953 HRS. CYCLES: 41,811. (X)
Part: SKIN — CRACKED (BS 248)
TUL - CRACK IN FUSELAGE SKIN AT STA 243 AND STR 222. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-30-3, PAGES 5-8. TST: 62,953 HRS. CYCLES 41,211. (X)
Part: SKIN — CORRODED (BS 684)
TUL - SMALL HOLE IN BELLY SKIN BELOW FORWARD CARGO AREA CAUSED BY CORROSION. CUT OUT CORROSION, REPLACED CUT OUT PER SRM 53-30-3, PAGES 14B, 14C, AND 14D. INSTALLED 2024-T3 0.071 DOUBLER. TST: 62,772 HRS. CYCLES, 41,734. (X)