N648AA
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.
69 reports on file, 1995-12-12 – 2011-04-30.
Part: PUMP — INOPERATIVE (RT ENGINE) · airframe 61,736 hrs · 21,250 cycles
TUL (REPEAT ITEM) CREW REPORTED DURING FUNCTIONAL CHECK FLIGHT RIGHT ENGINE FAILED TO RESTART (SINGLE ENGINE TIME 23 MIN). NO FUEL WAS DISPLAYED WITH FUEL CONTROL SWITCH IN RUN POSITION. EICAS DISPLAYED RIGHT ENGINE FUEL VALVE. EMERGENCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HIGH PRESSURE FUEL PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: GOVERNOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 61,734 hrs · 21,248 cycles
TUL (REPEAT ITEM) CREW REPORTED DURING FUNCTIONAL CHECK FLIGHT RIGHT ENGINE WAS SHUT DOWN AND ENGINE WOULD NOT RESTART (SINGLE ENGINE TIME 18 MINUTES). EMERGENCY DECLARED FLIGHT LANDED TUL WITHOUT INCIDENT. INSTALLED NUMBER 1 FUEL FLOW GOVERNOR ONTO NUMBER 2 ENGINE THEN REPLACED NUMBER 1 FUEL FLOW GOVERNOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: GOVERNOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 61,733 hrs · 21,247 cycles
TUL - CREW REPORTED DURING FUNCTIONAL CHECK FLIGHT WHEN RIGHT ENGINE WAS SHUT DOWN, ENGINE WOULD NOT RE-START (SINGLE ENGINE TIME 12 MINUTES). INDICATION WAS ENGINE FUEL LIGHT. EMERGENCY DECLARED FLIGHT LANDED TUL WITHOUT INCIDENT. REPLACED FUEL FLOW GOVERNOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FLOORBEAM — GOUGED (BS 1707) · airframe 61,732 hrs · 21,246 cycles
FLOORBEAM GOUGED AT STATION 1707 AT RIGHT BUTTLINES 9 TO 10. INSTALLED REPAIR STRAPS PER SRM 51-10-02-0G WITH MODIFICATIONS PER EA B757-53-016570.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 61,732 hrs · 21,246 cycles
IN THE MAIN EMERGENCY EQUIPMENT BELOW THE CABIN FLOOR AT STATION 418 THE INTERCOSTALS TOP TEE IS CRACKED AT BUTTLINE 0. INSTALLED REPAIR STRAP AND SRM MATING COLLAR WET WITH BMS 5-95 SEALANT PER SRM 51-70-12-0G AND EA B757-53-016550.
Part: FLOORBEAM — CRACKED (BS 700) · airframe 61,732 hrs · 21,246 cycles
REPAIR 700 BEAM ON LEFT SIDE. PERFORMED NECESSARY REPAIR TO LATERAL FLOORBEAM STATION 700 WATERLINE 208, LEFT BUTTLINES 70 TO 0 BY COMPLETING TASK CARD 53-98-01, "STA 700 FLOORBEAM REPAIR" PER SRM 53-00-51-2 REPAIR 3, WITH A DEVIATION AUTHORIZED BY B757-53-016157.
Part: PAN — GOUGED (R4 DOOR) · airframe 61,732 hrs · 21,246 cycles
RIGHT NUMBER 4 DOOR HANDLE PAN GOUGE. INSTALLED NEW HANDLE PAN PER ESO 90108.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
SHEAR TIE STATION 1460 STRINGER 26 CORRODED. ACCOMPLISHED REPAIR PER SRM 51-40-02-0G.
Part: STRUCTURE — MISINSTALLED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
AFT DECK DOUBLERS NOT INSTALLED PER SRM. INSTALLED REPAIR DOUBLER IAW SRM 53-60-51-2R 2 EA B757-53-016339.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
WEB CAP STATION 1480 TO 1500 CORRODED. ACCOMPLISHED REPAIR PER AARD 51-10-05-1.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
STATIONS 1480 TO 1500 OUTBOARD OF STRINGER 27 RIGHT FLOOR INTERCOSTAL CORRODED. INSTALLED FLOOR INTERCOSTAL PER SRM 51-10-02-0G.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
STRINGER SPLICE HAS CORROSION ON INNER SURFACE. REMOVED STRINGER SPLICE AND INSTALLED NEW SPLICE.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 61,732 hrs · 21,246 cycles
THIRD FLOORBOARD SUPPORT FROM RIGHT SIDE HAS GAPS BETWEEN REPAIRS AT STATION 555 AND 580. ACCOMPLISHED REPAIR PER SRM 51-10-02-G9.
Part: WEB — CORRODED (AILERON) · airframe 61,732 hrs · 21,246 cycles
CORROSION ON OUTBOARD HINGE WEB OF LEFT AILERON UNDER BONDING STRAP. REMOVED WEB AND INSTALLED NEW WEB.
Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 61,732 hrs · 21,246 cycles
NUMBER 1 PYLON MID BULKHEAD CRACKED. ACCOMPLISHED REPAIR PER EA 016326.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON CREASE BEAM STATIONS 1588 TO 1591. REPLACED CREASE BEAM.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON AFT DECK STIFFENER STATION 1715 BUTTLINE 0. CORROSION REMOVED AND INSTALLED SHIMS AND A NEW HAT CHANNEL AS PER SRM 51-10-02-0G SECTION 9.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON Z-BRACE STIFFENER STATIONS 1712 TO 1685 LEFT BUTTLINE 50. INSTALLED NEW Z-BRACE STIFFENER STATIONS 1712 TO 1685 LEFT BUTTLINE 50 PER SRM 51-10-02-0G.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
NUMBER 4 SEAT TRACK STATIONS 667 TO 780 CORRODED. REPLACED SEAT TRACK PER SRM 53-01-02-25.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON TOP AND UNDERSIDE OF WEBBING OF RIGHT NUMBER 1 DOOR THRESHOLD/ DITCHING PANEL BELOW THE CREASE ANGLE, FRAME STATIONS 334 TO 365 RIGHT BUTTLINES 63 TO 70, WATERLINE 208 INBOARD OF STRINGER 17 RIGHT. REPLACED RIGHT NUMBER 1 DOOR WEB FROM STATIONS 324 TO 365 PER SRM 51-10-02-0G, 9, AND EA B757-53-016109.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
NUMBER 3 SEAT TRACK CORRODED. REPLACED SEAT TRACK.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
THE Z-ANGLE INBOARD OF THE RIGHT NUMBER 2 DOOR THRESHOLD IS CORRODED BETWEEN STATIONS 680 TO 740. REPLACED CREASE ANGLE STATIONS 655 TO 760 RIGHT SIDE PER SRM 51-10-02-0G.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON TOP OF RIGHT FLOOR BOARD SUPPORT. REPLACED CREASE BEAM.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON GALLEY TIE DOWN STATION 1686 RIGHT BUTTLINE 52. REPLACED GALLEY FLOOR FITTING PER SRM 51-10-02-0G.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON GALLEY TIE DOWN STATION 1715 RIGHT BUTTLINE 52. REMOVED CORRODED GALLEY TIE DOWN AT STATION 1715 RIGHT BUTTLINE 52 AND INSTALLED NEW MOUNT IAW SRM 51-10-02-0G.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
THE CABIN LONGITUDAL FLOOR BOARD SUPPORT AT STATION 406 IS CORRODED ON TOP AT 66 INCHES RIGHT BUTTLINE. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-02-0G.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,732 hrs · 21,246 cycles
INTERCOSTAL CRACKED BELOW CABIN FLOOR STATIONS 1320 TO 1340. REPLACED INTERCOSTAL.
Part: DOOR — DAMAGED (L4) · airframe 61,732 hrs · 21,246 cycles
LEFT NUMBER 4 DOOR INTERIM REPAIR TO INNER SKIN BY THE HINGE ARM. INSTALLED DOUBLER REPAIR PER SRM 51-70-13-0G AND EA COMP-52-016002.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CREASE ANGLE STATIONS 665 TO 760 CORRODED. REPLACED CREASE ANGLE PER SRM 51-10-2-G9.
Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
FORWARD CARGO DOOR LOWER EDGE BEAM IS CORRODED AND DAMAGED ALONG ENTIRE LENGTH. REMOVED DAMAGED AND CORRODED EDGE BEAM ,LOCATED AND DRILLED NEW EDGE BEAM AND INSTALLED NEW BEAM PER ESO 90114.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
CORROSION ON FLOOR SUPPORT STATIONS 1640 TO 1661 BUTTLINE 0. CORROSION WAS REMOVED BY INSTALLING NEW FLOORBOARD SUPPORT AND INSTALLING NEW FASTENERS PER SRM 51-10-02-0G PARAGRAPH 9.
Part: DOOR — DENTED (CARGO BAY) · airframe 61,732 hrs · 21,246 cycles
DENT ON FORWARD CARGO DOOR 6 INCHES FROM BOTTOM AND 18 INCHES FROM FORWARD EDGE IS BEYOND MANUAL LIMITS. TRIMMED OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 52-30-01-2R.
Part: BEAM — DAMAGED (CARGO DOOR) · airframe 61,732 hrs · 21,246 cycles
NUMBER 2 CARGO DOOR LOWER EDGE BEAM IS BENT AND GOUGED IN MULTIPLE AREAS. INSTALLED NEW LOWER EDGE BEAM ON NUMBER 2 CARGO DOOR PER ESO 90121.
Part: PAN — GOUGED (CARGO DOOR) · airframe 61,732 hrs · 21,246 cycles
RIGHT NUMBER 1 DOOR HANDLE PAN GOUGED. REPLACED HANDLE PAN PER ESO 90284.
Part: SUPPORT ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
FORWARD CARGO DOOR LOWER AFT EDGE BEAM SUPPORT ANGLE CORRODED. REMOVED CORRODED SUPPORT ANGLE, LOCATED AND DRILLED NEW SUPPORT ANGLE AND INSTALLED PER ESO 90114.
Part: INTERCOSTAL — BENT (CARGO DOOR) · airframe 61,732 hrs · 21,246 cycles
NUMBER 2 CARGO DOOR 2ND FROM FORWARD EDGE BEAM SUPPORT INTERCOSTAL IS BENT. REMOVED BENT INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PER ESO 90121.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
GALLEY MOUNT STATION 329 RIGHT BUTTLINE 44 CORRODED. REPLACED MOUNT PER SRM 51-10-02-G14.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
AFT INBOARD LAVATORY MOUNT CORRODED. REPLACED MOUNT PER SRM 51-10-02-0G.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,732 hrs · 21,246 cycles
AFT LAVATORY MOUNT CORRODED. REPLACED MOUNT PER SRM 51-10-02-0G.
Earlier reports · 1995–2010 · 30 reports
2010
Part: COMPUTER — INOPERATIVE (EICAS) · airframe 60,198 hrs · 20,711 cycles
MIA - CREW REPORTED EICAS DISPLAYS INOPERATIVE WHEN LEFT COMPUTER SELECTED AND BOTH ENGINES FUEL FLOW ERRATIC. EMERGENCY DECLARED, RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EICAS SWITCHING MODULE AND LEFT EICAS COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: DUCT — BLOWN (CABIN) · airframe 59,064 hrs · 20,303 cycles
MIA - CREW REPORTED AFTER TAKEOFF AIR CONDITIONING DISTRIBUTION DUCT AT ROWS 12 TO 14 BLEW. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT FERRIED TO MCI FOR DUCT REPLACEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: ACM — MALFUNCTIONED (RIGHT) · airframe 58,878 hrs · 20,240 cycles
DEN - INFLIGHT DFW-HDN - CREW REPORTED HAD SMOKE IN AFT PORTION OF MAIN CABIN. EMERGENCY DECLARED, DIVERTED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT AIR CYCLE MACHINE INOPERATIVE. REPLACED AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,644 hrs · 19,802 cycles
EMERGENCY LIGHTS INOPERATIVE ROWS 16-25 RIGHT SIDE. REMOVED AND REPLACED BATTERY PACK AND CHARGER M10800 PER M/M. OPS CHECK OK.
Part: COVER — MISSING (CABIN) · airframe 57,078 hrs
JFK LEFT NUMBER FOUR DOOR EXIT SIGN MISSING COVER. REINSTALLED LEFT NUMBER FOUR DOOR EXIT SIGN COVER.
2008
Part: SHROUD — DAMAGED (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT FORWARD SEAT 5E HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT FORWARD SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PLACARD — DAMAGED (CABIN)
DFW - EMERGENCY LIGHT EXIT PLACARD AT RIGHT FORWARD OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT PLACARD AT RIGHT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (CABIN)
DFW - EMERGENCY LIGHT ADJACENT TO RIGHT AFT LAVATORY MISSING LENS. REPLACED LENS COVER FOR EMERGENCY LIGHT ADJACENT TO RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: PLACARD — DAMAGED (CABIN)
DFW - EMERGENCY LIGHT EXIT PLACARD AT LEFT FORWARD OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT PLACARD AT LEFT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
LAX - EMERGENCY EXIT LIGHT AT LEFT WING INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT WING. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: INTERCOSTAL — CORRODED (FUSELAGE)
TUL - RIGHT NUMBER 4 DOOR DRAIN LINE SUPPORT CORRODED BETWEEN STATION 1640 AND 1661. REPLACED DRAIN LINE SUPPORT INTERCOSTAL WITH A NEW INTERCOSTAL BETWEEN STATIONS 1640 AND 1661 PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - COFFEE BAR TIE DOWN SEAT TRACK NUMBER 3 AT STATION 686 TO 690 CORRODED. REPLACED COFFEE BAR TIE DOWN SEAT TRACK, ALODINED, PRIMED, AND PAINTED.
2002
Part: LIGHT — INOPERATIVE (CABIN)
BDL - FOUND SEAT MOUNTED ESCAPE PATH LIGHT ASSEMBLY ON SEAT 14D INOPERATIVE. INSTALLED NEW LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: BATTERY PACK (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS ROWS 15 THROUGH 23 DIM. REPLACED BATTERY PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: DUCT — LEAKING (CABIN)
BGI - FLT 984 - EN ROUTE BGI-MIA - DETECTED LOUD NOISE IN CABIN. RETURNED BGI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED AIR CONDITIONING DUCT. ACCOMPLISHED LEAK CHECK. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: LIGHT ASSY — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED AFT RIGHT EMERGENCY EXIT LIGHT ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: LIGHT ASSY — FAILED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT LIGHT AT FORWARD COACH CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN FORWARD COACH CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: LIGHT — BROKEN (R4 DOOR)
ORD - DURING OVERNIGHT CHECK, R4 EMERGENCY EXIT DOOR LIGHT BROKEN. REPLACED R4 EMERGENCY EXIT DOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT FORWARD EDGE OF R1 DOOR FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT AT FORWARD EDGE OF R1 DOOR. SYSTEM FOUND CHECKED, NORMAL OPERATION. (X)
1996
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 9 THROUGH 16 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOOR BEAM — CORRODED (BS 1640)
AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED AT VARIOUS LOCATIONS MATERIAL REMOVED IS BEYOND SRM LIMITS. MRB 757-778. (M)
Part: PAN — GOUGED (L-4 DOOR)
AFW - FOUND L-4 DOOR HANDLE PAN HAS A GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-781. (M)
Part: SURROUND STRUCT — CORRODED (BS 1440)
AFW - FOUND AFT CARGO DOOR SURROUND STRUCTURE UPPER CHORD HAS CORROSION BLENDED OFF BEYOND SRM LIMITS. PER MRB 757-783. (M)
Part: FLOOR BEAM — CORRODED (BS 324)
AFW - FLOOR BEAM AT STATION 324 RBL 42 AND RBL 62 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-777. (M)
Part: PAN — GOUGED (R-4 DOOR)
AFW - FOUND R-4 DOOR HAS A SMALL GOUGE AFTER BLENDING. BLENDED AREA IS BEYOND SRM LIMITS. PER MRB 757-775. (M)
Part: DECK PLATE — CORRODED (BS 1680)
AFW - DECK PLATE HAS CORROSION REMOVAL ON UPPER SURFACE MATERIAL REMAINING AT VARIOUS LOCATIONS ARE BEYOND SRM LIMITS. PER MRB 757-779. (M)
Part: FLOOR BEAM — MISDRILLED (BS 345)
AFW - FLOOR BEAM AT STATION 345 LBL HAS A MISDRILLED HOLE. PER MRB 757-788. (M)
1995
Part: SKIN — GOUGED (BS 1094)
AFW - FOUND FUSELAGE SKIN HAS A SMALL BUT DEEP GOUGE AT STATION 1094 AT S10R. PER MRB 757-673, BLENDED PER MRB. PERMANENT REPAIR REQUIRED AT NEXT 'C' CHECK. (M)