N782SP
Registered owner: LIBERTY UNIVERSITY INC, VA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
RH UPPER WING CENTER L/E SKIN DOUBLER HAS CORROSION BETWEEN STA.XFS=422.75 AND XS=442.185. REF NRC# B000102.
FORWARD CARGO COMPARTMENT PNEUMATIC DUCT FOUND WITH 6" CRACK. REF NRC# B000386.
RH I/B LEADING EDGE AUX FUEL TANK O/B SPAR UPPER FLANGE ANGLE CRACKED. REF NRC# B000385.
L/ H HORZ. STAB I/B L/E SECTION LOWER RIB IS CRACKED AT STA. SFX.= 47.500, REF NRC B000153
MAIN CABIN FWD. FLOOR AREA R/H SIDE HAS A CRACKED INTERCOSTAL AT STA. 270.000, REF NRC B000331.
MAIN CABIN AFT FUSELAGE INTERCOSTAL SUPPORT HAS CORROSION BETWEEN STA. 1360-1380 LON 18R. REF NRC B000316.
MAIN CABIN SEAT TRACK HAS CORROSION FROM STA. 1100-1120 BL 0". REF NRC# B000312.
MAIN CABIN LWR SURFACE OF DOUBLE WIDE SEAT TRACK HAS CORROSION AT STA. 781 LBL 48. REF NRC# B000293.
AFT CARGO COMP., AFT BULKHEAD L/H PROFINE SUPPORT/INTERCOSTAL HAS MISDRILLED HOLES, REF NRC B000183.
L/H WING O/B L/E UPPER RIB/FORMER IS CRACKED AT STA. XFS.760.000, REF. NRC B000114.
R/H HORZ. STAB L/E I/B SECTION LOWER SURFACE HAS CORROSION AROUND 2 FASTENERS BETWEEN STA. XFS. 122.500 & 128.750, REF NRC B000142.
R/H HORZ. STAB L/E I/B SECTION UPPER SKIN HAS CORROSION AT STA. XFS. 60.000, REF. NRC B000143.
R/H HORZ. STAB L/E O/B SECTION UPPER SURFACE HAS CORROSION AROUND FASTENER HOLE AT STA. XFS. 272.500, REF NRC B000140.
AFT CARGO COMPARTMENT FORWARD BULKHEAD R/H UPPER ATTACH PANEL PROFILE (INTERCOSTAL)CRACKED AT STA. 980. REF NRC B000207.
R/H I/B FLAP O/B SUPPORT RIB IS CRACKED AT LOWER SECTION OF INTERCONNECT FITTING, REF NRC B000168.
FWD. CARGO FWD. BULKHEAD CEILING HAS CRACKED INTERCOSTAL AT STA. 270.00, REF. NRC B000152
R/H HORZ. STAB L/E I/B SECTION LOWER SURFACE SKIN HAS CORROSION AT STA. XFS. 122.5 & 128.750, REF NRC B000142.
L/H WING O/B LOWER RIB IS CRACKED AT STA. XFS.= 622.500, REF. NRC B000111
RT WING UPPER FORWARD SKIN HAS CORROSION AT STA.XRS= 74.869. REF NRC B000098.
RT WING O/B L/E LWR SKIN HAS MULTIPLE AREAS OF CORROSION AT STA. XFS 566.250. REF NRC # B000092.
L/H WING O/B LOWER RIB A IS CRACKED AT STA. XFS.= 616.250, REF. NRC B000110
R/H WING L/E SKIN UPPER SURFACE BETWEEN STA XOLD 67.750 TO STA XW 485, HAS CORROSION ON EXISTING REPAIR DOUBLER. REF NRC B000104
REFERENCE NRC A016593, LT WING CTR LE UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENERS AT XFS 347.750. ITEM REPAIRED IAW EA 008-5730-38-A6009.
REFERENCE NRC A016060, LT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XW 761 & STRINGER 2. ITEM REPAIRED IAW EA 008-5710-38-A5879.
RT WING SKIN CTR LE HOIST POINT AT XFS 385.250 HAS INTERGRANULAR CORROSION. REPAIRED ON EA 008-5730-38-A5966.
AFTER REMOVAL OF LT OTBD LE STUB WING, FOUND SKIN UPPER ATTACH SCREW HOLE COUNTERSINK DAMAGED. REPAIRED IAW EA 008-5730-38-A5967.
REFERENCE NRC A016331, RT WING OTBD LE, OTBD SECTION HAS INTERGRANULAR CORROSION AROUND FASTENERS ON UPPER SKIN, BETWEEN XFS710.000 - 747.500. ITEM REPAIRED ON EA 008-5710-38-5863.
LEFT HORIZ STAB INBD LE UPPER SURFACE HAS CORROSION AT OTBD HOIST ATTACH POINT. ITEM REPAIRED IAW EA 008-5530-38-A5938.
REFERENCE NRC A017940, AFTER REMOVING RT CABIN WINDOW AT STATION 1410, FOUND CORROSION ON WINDOW FRAME & INSIDE FASTENER HOLES. ITEM REPAIRED ON EA 008-5320-38-A5955.
REFERENCE NRC A016333, RT WING OTBD LE, OTBD SECTION HAS INTERGRANULAR CORROSION AROUND FASTENERS ON UPPER SKIN BETWEEN XFS 778.750 - XW 761.695. ITEM REPAIRED ON EA 008-5710-38-A5863.
REFERENCE NRC A016797, RT WING CTR LE UPPER SKIN, TE HAS INTERGRANULAR CORROSION AROUND FASTENERS AT XOLD16.225 & XFS 429. REPAIR ACCOMPLISHED IAW EA 008-5730-38-A5993.
REFERENCE NRC A016226, LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 4 & CTR SPAR & XRS 358-393. ITEM REPAIRED IAW EA 008-5710-38-A5882.
REFERENCE NRC A016795, RT WING CTR LE UPPER SKIN, TE HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 385.250. ITEM REPAIRED ON EA 008-5730-38-A5993.
REFERENCE NRC A016224, LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR & AFT SPAR & XRS 393 - 428. ITEM REPAIRED IAW EA 008-5710-38-A5885.
REFERENCE NRC A017180, COCKPIT SUBFLOOR IS EXFOLIATED THROUGH SKIN AT STATION 133 RT CUSP AREA. REPAIR ACCOMPLISHED ON EA 008-5310-38-A5956.
REFERENCE NRC A016101, TAIL CONE SKIN CORRODED AT LOWER TAIL LIGHT ASSEMBLY. ITEM REPAIRED IAW EA 008-5330-38A5869.
REFERENCE NRC A019317, LT WING INBD LE, OTBD SECTION UPPER SKIN HAS SEVERAL CRACKS AT XILD 42. ITEM REPAIRED IAW EA 008-5730-38-A6019.
REFERENCE NRC A016084, EXTERIOR FUSELAGE HAS CORROSION ON SKIN AT WINDOW REPAIR DOUBLER, STATION 1340. REPAIR WAS ACCOMPLISHED ON EA 008-5320-38-A5955.
AFTER REMOVAL OF AFT RT LAVATORY DUMP PAN & FASTENERS. MAIN CABIN FLOORBEAM FOUND EXFOLIATED.
REFERENCE NRC A016695, LT WING INBD AILERON CTR & OTBD BALANCE PANELS HAVE RUST CORROSION. REPAIR ACCOMPLISHED IAW EA 008-5751-38-A5958.
LEFT WING LOWER SURFACE HAS CORROSION AT STRINGER 53 & INBD OF PYLON, 28-023.
EXFOLIATED LOWER FWD STRINGER INBD END, INSIDE FUEL ACCESS PANEL 514D.
REFERENCE NRC A016056, LT WING LOWER SURFACE HAS CORROSION OTBD SIDE OF NR 1 PYLON AT STRINGER 52 28-034.
EXTERIOR FUSELAGE DOUBLER HAS CORROSION AT RT AFT DRAIN MAST, STATION 1552 32-015.
REFERENCE NRC A016097, EXTERIOR FUSELAGE, AFT RT LAVATORY SERVICE PANEL, CUT OUT HAS CORROSION INSIDE. REPAIR ACCOMPLISHED IAW EA 008-5330-38-A6035.
REFERENCE A017940, AFTER REMOVING RT CABIN WINDOW AT FS 1410, FOUND CORROSION ON WINDOW FRAME & INSIDE FASTENER. REPAIR ACCOMPLISHED IAW EA 008-5320-38-A5955.
RIGHT WING, INBD LE, OTBD SECTION LOWER SKIN HAS INTERGRANULAR CORROSION AT XS 250.089. REPAIR ACTION ACCOMPLISHED IAW EA 008-5710-38-A6018.
REFERENCE NRC A016309, LT HORIZONTAL STABILIZER INBD LE, UPPER SURFACE HAS CORROSION AT INBD HOIST ATTACH POINT. ITEM REPAIRED IAW EA 008-5530-38-A5929.
REFERENCE NRC A016448 & A023498 INGRESS & EGRESS DOOR FROM FLIGHT DECK TO UPPER CARGO COMPARTMENT, MAIN CARGO DECK, HAS TORN & COMPRESSED FIRE SUPPRESSION SEALS. THIS ITEM WAS REPAIRED IAW EA AQ56-25-101.
REFERENCE NRC A017102, AFT ACCESSORY COMPARTMENT, FS 1530, LONGERON 28L - 28R, AFT FACING SURFACES CORRODED.
REFERENCE NRC A016313, LT WING INBD STUB WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN XILD 42 - XW 257 AT FWD SPAR ATTACHMENT.
REFERENCE NRC A016937, RT INBD AILERON BALANCE PANEL HAS CORROSION. REPAIR ACCOMPLISHED IAW EA 008-5751-38-A5959.
LT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XRS763 & STRINGER 2 28-039.
MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE SAT 590, LBL 24.32-156.
LT INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED & CRACKED RIVETS 28-010.
COCKPIT SUBFLOOR RT SIDE CUSP AREA STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS.
MAIN DECK CARGO COMPARTMENT, SEAT TRACK LUGS DAMAGED 2 PLACES STATION 834, LBL 24.
LT WING INBD LE FUEL TANK UPPER TE TEE CAP HAS INTERGRANULAR CORROSION. BETWEEN XFS 30.000 - 57.000.
LEFT HORIZONTAL STAB TIP HAS CORROSION ON SKIN AT STATIC WICK BASES.
LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 9 & FWD SPAR, BETWEEN XRS 255 - 289.28-063.
FOUND FITTING THAT ATTACHES FRAME TO FLOORBEAM AT STATION 1480 RT SIDE WITH INTERGRANULAR CORROSION. REMOVED FITTING. FABRICATED & INSTALLED NEW FITTING IAW EA 008-5310-38-A6040.
MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE, BS 990, LBL 24, 32-151.
CRACK FOUND AT LT INBD SIDE OF AFT PRESSURE BULKHEAD BETWEEN LONGHORN 10 AND 11 APPROXIMATELY 2.25" IN LENGTH. VERIFIED BY FPI AND HFEDC INSPECTION.
FRAME BS 1060, UPPER CAP CORRODED INCLUDING EXFOLIATION AT SEVERAL PLACES FROM S34L TO S31R.
LT WING CTR UE UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 261.500.
LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR SPAR & STRINGER 11 & XRS 204 & 238.052.
AFTER REMOVAL OF LOWER IFF ANTENNA, FOUND CORROSION, JUST AFT OF NLG INTERNAL STRUCTURE AROUND ANTENNA CUT OUT. GAINED ACCESS TO AREA & FOUND LONGERON 36L WITH ELONGATED HOLES. REMOVED LONGERON 36L. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER, REPLACEMENT ANTENNA PAN FITTING & REPLACEMENT LONGERON IAW SRM.
UPON OK TO CLOSE, FOUND EXFOLIATED LOWER FWD STRINGER INSIDE FUEL ACCESS PANEL 514D, INBOARD END. REMOVED STRINGER 59. FABRICATED STRINGER 59 REPAIR SPLICE FITTING. INSTALLED IAW SRM & EA 008-5710-38-A6042.
FOUND LONGERON 23L, EXFOLIATED IN 2 PLACES. REMOVED SECTION, FABRICATED NEW & INSTALLED IAW SRM.
LONGERON 24 LT, END FITTING EXFOLIATED AT BARREL NUT HOLE, STATION 1530. REMOVED END FITTING, FABRICATED NEW END FITTING & INSTALLED IAW SRM.
LONGERON 28 LT, STATION 1530, END FITTING EXFOLIATED AT BARREL NUT HOLE. REMOVED, FABRICATED NEW & INSTALLED IAW SRM.
LONGERON 30L AT STATION 1530, END FITTING EXFOLIATED AT BARREL NUT HOLE. REMOVED END FITTING, FABRICATED NEW FITTING & INSTALLED IAW SRM.
LONGERON 26 RT, END FITTING EXFOLIATED INSIDE OF BARREL NUT HOLE STATION 1530. REMOVED END FITTING, FABRICATED NEW END FITTING & INSTALLED IAW SRM.
RIGHT END FITTING, FABRICATED NEW END FITTING & INSTALLED IAW SRM.
LONGERON 26 LT, STATION 1530, EXFOLIATED AT BARREL NUT HOLD END FITTING.
WHILE WORKING NR A016127, FOUND LONGERON 36 AT STATION 612 - 712 WITH EXFOLIATION. REMOVED LONGERON 36, 2 EACH EXTRUSION. FABRICATED NEW LONGERON 36 & INSTALLED IAW 008-5310-38-A6024.
FOUND SUBFLOOR WEB EXFOLIATED AT LOWER SURFACE OF WEB, BS 1480, L21R. REMOVED SUBFLOOR WEB, FABRICATED NEW SUBFLOOR WEB & INSTALLED IAW SRM.
FOUND SKIN SPLICE STRAP EXFOLIATED FROM STATION 1530 - 1606, LONGERON 28L. REMOVED STRAP, FABRICATED NEW STRAP & INSTALLED IAW SRM.
EXISTING REPAIR ON LONGERON SECTION 32 RT AFT OF STATION 1530, HAS CORROSION & DAMAGED FASTENER HOLES. REMOVED REPAIRED SECTION. FABRICATED NEW REPAIR & INSTALLED IAW SRM.
SKIN SPLICE STRAP FOUND EXFOLIATED FROM STATION 1530 - 1606, LONGERON 28R. REMOVED STRAP, FABRICATED NEW STRAP & INSTALLED IAW SRM.
FOUND LT SUBFLOOR CRACKED, BELOW AFT LT ENTRY DOOR, STATION 1480 - 1520. GAINED ACCESS TO AREA. REMOVED WEB, FABRICATED INTERCOSTAL & INSTALLED IAW SRM.
AFTER REMOVAL OF RT WING UPPER PANEL, ABOVE AILERON BAY FOUND GOUGE MARKS ON UPPER SKIN. CUT OUT DAMAGED AREA. HFEC SURFACE INSPECTION, NO CRACKS NOTED. FABRICATED REPLACEMENT DOUBLER & FILLER IAW EA 008-5730-38-A6021 & INSTALLED.
FOUND CRACKED WEB, BETWEEN STATION 1520 - 1540, RBL 24, MAIN CABIN. REMOVED WEB, FABRICATED NEW WEB & INSTALLED IAW SRM.
MAIN CABIN SEAT TRACK IS CORRODED AT LOWER FLANGE, STATION 1480, BL0. CORROSION IS OUT OF LIMITS. CUT OUT DAMAGED SECTION. FABRICATED REPLACEMENT SEAT TRACK & INSTALLED IAW SRM.
MAIN CABIN LT OTBD SEAT TRACK, LOWER REPAIR STRAP IS EXFOLIATED AT LOWER SURFACE IN AFT ACCESSORY COMPARTMENT, STATION 1420. REMOVED CORROSION, OUT OF LIMITS. FABRICATED SPLICE PLATE & INSTALLED IAW SRM.
LEFT WING LOWER SURFACE HAS INTERGRANULER CORROSION AROUND FASTENERS AT XW 761. REMOVED FASTENERS & REMOVED CORROSION. UT INSPECTION. OPEN HOLE INSPECTION, BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & FILLER. INSTALLED IAW EA 008-5730-38-A6020.
AFTER REMOVAL OF AFT RT DUMP PAN FOUND FUSELAGE FLOOR FRAME EXFOLIATED AT STATION 1500, LONGERON 23R - 24R. PERFORMED BLEND, BLEND OUT OF LIMITS. FABRICATED REPAIR ANGLE & FILLER. INSTALLED IAW EA 008-5310-38-A6007.
WHILE WORKING NR A016589, FOUND INTERNAL PRODUCTION DOUBLER EXFOLIATED, LT WING LE STATION XFS 304.000. REMOVED DOUBLER & REMOVED SURFACE CORROSION. FABRICATED & INSTALLED REPLACEMENT DOUBLER IAW SRM.
FOUND CORROSION ON SKIN LT WW, STATION 980, BETWEEN STRINGERS 25 - 30. GAINED ACCESS, CUT OUT DAMAGED LONGERON. FABRICATED LONGERON & INSTALLED IAW SRM.
MAIN CARGO DOOR ACTUATOR HINGE FITTING, PN 5777788-1, CORRODED. REMOVED HINGE FITTING, REMOVED CORROSION, FABRICATED 4 EACH BUSHINGS & INSTALLED IAW EA 008-5310-38-A6014.
CRACK FOUND AT RT OTBD SIDE OF AFT PRESS BULKHEAD WEB, BETWEEN LONGERON 10 & 11. APPROX 2 INCHES IN LENGTH. CUT OUT DAMAGED AREA. HFEC SURFACE INSPECTION. FABRICATED REPAIR DOUBLER & FILLER. INSTALLED REPAIR DOUBLER & FILLER IAW SRM.
RIGHT FWD FUSELAGE AT AFT PRIMARY HEAT EXCHANGER, FUSELAGE FRAME AT STATION 148, LONGERON 23R HAS HEAVY CORROSION. REMOVED FRAME, FABRICATED NEW FRAME & INSTALLED IAW SRM.
MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BS 1420, LBL 59. REPLACED SEAT TRACK.
ON OK TO INSTALL LE PANELS ON RT ELEVATOR GEAR TAB, FOUND SMALL ROUND ACCESS HOLE BENT & CRACKED. NDT VERIFIED 2 EACH CRACKS. BLENDED CRACKED AREAS. HFEC SURFACE INSPECTION PERFORMED. ACCOMPLISHED REPAIR TO RT ELEVATOR GEAR TAB ACCESS HOLE IAW EA 008-5510-38-A6034.
RT WING CENTER L/E UPPER CENTER SLOT PANEL HAS INTERGRANULER CORROSION.
AFTER REMOVAL OF LONGERON 24R, FOUND CORROSION ON AFT WALL RT WW AT STATION 980, LONGERON 24R. CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA FROM STATION 980 BULKHEAD SKIN. FABRICATED WEB SKIN & SPLICE. INSTALLED IAW EA 008-5310-38-A5925.
FOUND CORROSION ON COPILOT FLOOR WEB. REMOVED WEB, FABRICATED NEW WEB & INSTALLED WEB IAW SRM.
AFTER REMOVAL OF LONGERON 24R, FOUND BRACKET CRACKED AT STATION 940. FABRICATED ANGLE FLAP SUPPORT BRACKET LOCATED AT STATION 940, LONGERON 24R. REQUIRE MATERIAL SUBSTITUTION AS 7075-T651 CLAD PLATE IS NOT AVAILABLE TO PURCHASE. ACCOMPLISHED REPAIR TO LONGERON 24R, BRACKET STATION 940 IAW EA 008-5300-38-A6023.
FOUND LT ELEVATOR CONTROL TAB UPPER SURFACE DELAMINATED IN SEVERAL AREAS. CUT OUT DAMAGE, FABRICATED FILLERS & DOUBLERS. BONDED FILLERS & DOUBLERS IAW SRM. TO BE BALANCED ON NR A020022.
FOUND RT ELEVATOR CONTROL TAB UPPER SURFACE DELAMINATED IN SEVERAL AREAS. CUT OUT DELAMINATED AREAS, FABRICATED FILLERS & DOUBLERS, BONDED FILLERS & DOUBLER IAW SRM.
AFTER REMOVAL OF MAIN CARGO DOOR, FWD UPPER HINGE FITTING, FOUND CORROSION ON OUTER SKIN INTERNAL SURFACE. BLENDED AREA, BLEND OUT OF LIMITS, CUT OUT DAMAGED AREA. HFEC SURFACE & OPEN HOLE INSPECTION. ACCOMPLISHED REPAIR IAW EA 008-5230-38-A6016.
WHILE WORKING NR A016629 ON RT WING UPPER SURFACE FOUND AN EXISTING REPAIR DOUBLER WITH MULTIPLE CORROSION AREAS STATION XRS 74.8 FROM FWD SPAR TO CTR SPAR. UT INSPECTION PERFORMED. REMOVED EXISTING REPAIR DOUBLER & REMOVED CORROSION. DP INSPECTION PERFORMED. BLEND WITHIN LIMITS. PERFORMED HFEC OPEN HOLE INSPECTION. FOUND 2 EACH CRACKS. REMOVED CRACKS IAW SRM. ACCOMPLISHED REPAIR IAW EA 008-5730-38-A612.
AFTER REMOVING LT CABIN WINDOW AT STATION 1290, FOUND CORROSION ON WINDOW FRAME. REMOVED CORROSION. FABRICATED WINDOW REPAIR DOUBLER & INSTALLED IAW EA 008-5320-38-A5955.
AFTER REMOVING RT SIDE CABIN WINDOW AT STATION 1250, FOUND CORROSION ON WINDOW FRAME. REMOVED 2 EA OLD REPAIR DOUBLERS. REMOVED CORROSION. PERFORMED HFEC OPEN HOLE INSPECTION. FABRICATED NEW DOUBLER & INSTALLED IAW EA 008-5320-38-A5955.
FUSELAGE EXTERIOR, AFTER REMOVAL OF LOWER STRESS PANELS, CTR SECTION KEEL BEAM HAS CORROSION, GAINED ACCESS. REMOVED KEEL BEAM SECTION. FABRICATED NEW KEEL BEAM SECTION & INSTALLED IAW EA 008-5302-38-A5957.
AFTER REMOVAL OF LT NOSE TUNNEL INSULATION BLANKETS FOUND COCKPIT SUBFLOOR HEAVILY CORRODED AT STATION 173 - 188. CUT OUT CORROSION FROM COCKPIT SUBFLOOR PANEL & FLOORBEAM. ACCOMPLISHED REPAIR IAW 008-5310-38-A5962.
LT WING CENTER L/E LOWER SKIN IS CRACKED AT 2 FASTENERS AT XOLDI 6.225.
NLG REMOVED, FOUND RT TRUNNION PIVOT BORE WITH PITTING IN SEVERAL AREAS. REPAIRED NLG TRUNNION PIVOT BORE IAW EA 008-5310-38-A5945.
RT WING OTBD L/E INBD SECTION LOWER SKIN HAS INTERGRANULER CORROSION AROUND FASTENERS.
AFTER REMOVAL OF RT WING LONGERON 24 BARREL NUT & BOLT. FOUND LONGERON 24 CRACKED IN 2 PLACES IN BOLT HOLE AT RT WW STATION 857. ACCOMPLISHED REPAIR TO RT LONGERON 24 IAW EA 008-5300-38-A5915.
EXTERNAL FUSELAGE SKIN HAS POCKET OF CORROSION AT BS 1600, LONGERON 32L.
RT OTBD LE STUB WING, UPPER SKIN HAS SEVERAL NICKS & SCRATCHES. BLENDED, BLEND OUT OF LIMITS. ACCOMPLISHED REPAIR IAW EA 008-5730-38-A5982.
CAPTAINS CONTROL COLUMN, LOWER END IS CORRODED. GAINED ACCESS. REPLACED CAPTAINS CONTROL COLUMN PN 5614272-501.
COPILOT'S CONTROL COLUMN IS EXFOLIATED THROUGHOUT. GAINED ACCESS TO CONTROL COLUMN. REPLACED COPILOT'S CONTROL COLUMN IAW AMM.
COCKPIT SUBFLOOR RT CUSP AREA, STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS. REMOVED DOUBLER FITTING & ATTACHMENT. FABRICATED TWO EACH FINGER DOUBLERS & INSTALLED IAW SRM.
AFT CABIN FLOOR SUPPORT EXTRUSION FS 1589, LBL 35 TO RBL 35, HAS BARE METAL, PREVIOUS REWORKED AREAS & CORROSION. REMOVED FLOOR SUPPORT ASSEMBLY, FABRICATED NEW FLOOR SUPPORT & INSTALLED IAW SRM.
AFT CABIN SEAT TRACK BL 0, FS 1520 - 1547 IS CORRODED. GAINED ACCESS & REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM.
AFT CABIN SEAT TRACK FS 1520 - 1547, RBL 24 IS CORRODED. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM.
NR A017107, AFT ACCESSORY COMPARTMENT S32R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.
AFT ACCESSORY COMPARTMENT S34L END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.
AFT ACCESSORY COMPARTMENT, STRINGER 30R, END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED. INSTALLED REPLACEMENT FITTING IAW SRM.
AFT ACCESSORY COMPARTMENT S36 END FITTING AFT AFT SIDE OF FRAME FS 1530 IS CORRODED.
AFT ACCESSORY COMPARTMENT S32L END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.
NR A017106, AFT ACCESSORY COMPARTMENT S34R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.
AFT ACCESSORY COMPARTMENT, STRINGER 28R, END FITTING AT AFT SIDE OF FRAME, FS 1530 IS CORRODED. REMOVED FITTING, FABRICATED NEW FITTING & INSTALLED FITTING IAW SRM.
AFT ACCESSORY COMPARTMENT, FS 1586, CANTED FRAME IS CORRODED STRINGER 30L - 30R. REMOVED DAMAGED SECTION, FABRICATED NEW SECTION FRAME & INSTALLED IAW SRM.
RT INBD, CTR INBD BALANCE PANEL, HAS RUST CORROSION ON LOWER SURFACE. REPAIRED IAW EA 008-5751-38-A5959.
NR A016891, MAIN DECK CARGO COMPARTMENT HAS SEAT TRACK CORROSION AT SPLICE. BS 1300, RBL 49. 32-164. REPLACED SEAT TRACK.
RT WING AILERON BAY CONTROL QUADRANT, ACTUATOR MOUNT FITTING IS GOUGED IN MULTIPLE AREAS. ACCOMPLISHED REPAIR IAW EA 008-5740-38-A6027.
RIGHT WING, LOWER SKIN HAS CORROSION AROUND FASTENERS AT STRINGER 58 & FWD SPAR & XRS 763. PERFORMED UT INSPECTION. REMOVED FASTENERS & REMOVED CORROSION. PERFORMED OPEN HOLE HFEC, BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6028.
RT INBD AILERON, INBD BALANCE PANEL HAS CORROSION. REMOVED CORROSION. REPAIRED IAW EA 008-5751-38-A5959.
RT INBD AILERON, CTR INBD BALANCE PANEL HAS CORROSION. REPAIRED IAW EA 008-5751-38-A5959.
RT INBD AILERON, CTR OTBD BALANCE PANEL HAS CORROSION. REPAIRED IAW EA 008-5751-38-A5959.
RT INBD AILERON, OTBD BALANCE PANEL HAS CORROSION. REPAIRED IAW EA 008-5751-38-A5959.
RIGHT WING LOWER SKIN HAS CORROSION AROUND FASTENERS AT STRINGER 57 & FWD SPAR & XRS 795. REMOVED CORROSION, PERFORMED UT, REMOVED FASTENERS, PERFORMED HFEC OPEN HOLE INSPECTION, NO CRACKS. CHECKED MATERIAL THICKNESS, OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6022.
LT EXTERIOR FUSELAGE SKIN IS GOUGED AT FS 960, APPROXIMATELY LONGERON 25L.
RT WING INBD LE FUEL TANK, AFT SKIN IS CHAFED AT XFS 26.250. BLENDED AREAS, BLEND IS OUT OF LIMITS. GAINED ACCESS. PERFORMED OPEN HOLE INSPECTION, NO CRACKS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6013.
NR 4 PYLON ACCESS PANEL 492A, HAS 2 EACH SCREW HOLES ELONGATED. FOUND HOLES WORN & COUNTERSINK DAMAGED. FABRICATED REPAIR DOUBLER & FILLER . INSTALLED IAW EA 008-5430-38-A6032.
RT WING CTR LE UPPER SKIN HAS INTERGRANULER CORROSION AROUND FASTENER AT XFS 341.500. PERFORMED UT INSPECTION, CORROSION MARKED AS DETECTED, GAINED ACCESS. REMOVED CORROSION, BLEND OUT OF LIMITS. ACCOMPLISHED REPAIR IAW EA 008-5730-38-A5987.
RT WING FWD SPAR UPPER FLANGE HAS A DAMAGED FASTENER HOLE AT APPROX XFS 188.750. GAINED ACCESS. REAMED HOLE TO ROUND. PERFORMED HFEC SURFACE & OPEN HOLE INSPECTION. INSTALLED 2 EACH FREEZE PLUGS IAW EA 008-5720-38-A6015.
RIGHT WING CTR LE LOWER SKIN HAS CORROSION AROUND INBD FUELING GND POINT. PERFORMED UT INSPECTION. REMOVED CORROSION. HFEC SURFACE INSPECTION PERFORMED. BLEND OUT OF LIMITS. REPAIRED IAW EA 008-5730-38-A5992.
NR 2 PYLON PANEL 293B IS CHAFED. BLENDED DAMAGED AREA, GAINED ACCESS. PERFORMED UT INSPECTION. ACCOMPLISHED REPAIR IAW EA 008-5430-38-A6001.
LEFT WING INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED AND CRACKED RIVETS. FOUND EXFOLIATED SKIN UNDER PLATE.
STATION 1606, LONGERON 3L & 3R, CHORD ANGLE CRACKED IN RADIUS AT STATION 1606. VIEWED THRU NR 60 ACCESS DOOR. HFEC VERIFIED 2 EACH CRACKS. FABRICATED 3 EACH ANGLES & FILLERS. INSTALLED IAW EA 008-5310-38-A5980.
LEFT WING INBD LE, OTBD SECTION LOWER AFT SKIN HAS INTERGRANULER CORROSION AT XFS 245. PERFORMED UT INSPECTION, REMOVED FASTENERS. REMOVED CORROSION & BLENDED AREA IS OUT OF LIMITS. HFEC SURFACE INSPECTION. FABRICATED EXTERNAL SPLICE REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6017.
LT HORIZONTAL STABILIZER UPPER SKIN HAS POCKETS OF CORROSION, BETWEEN STATION XFS 47 & 65, INCLUDING AREA UNDER UPPER SLIDING FAIRING, FROM LE TO CLOSING SPAR. ACCOMPLISHED REPAIR TO LT HORIZONTAL STABILIZER UPPER SURFACE, XFS 47 - 65 IAW EA 008-5510-38-A6037.
RIGHT HORIZONTAL STABILIZER UPPER SKIN HAS POCKETS OF CORROSION, BETWEEN STATION XFS-47 & 65, INCLUDING AREA UNDER UPPER SLIDING FAIRING, FROM LE TO CLOSING SPAR. REMOVED CORROSION & PERFORMED UT. ACCOMPLISHED REPAIR IAW EA 008-5510-38-A6038.
LT WING INBD AILERON IS CHAFED & GOUGED JUST AFT OF CTR OTBD BALANCE PANEL, GAINED ACCESS & BLENDED. BLEND IS OUT OF LIMITS. OPEN HOLE HFEC INSPECTION PERFORMED, NO CRACKS. FABRICATED SHIM & EXTERNAL SPLICE DOUBLER & INSTALLED IAW EA 008-5720-38-5989.
RT WING UPPER SURFACE, FROM XW 240 - XW 467, HAS SURFACE CORROSION IN MULTIPLE AREAS. PERFORMED UT INSPECTION, CORROSION DETECTED. GAINED ACCESS, BLENDED. DPI PERFORMED & HFEC OPEN HOLE PERFORMED. ALL BLENDED AREAS ARE WITHIN LIMITS. SEVERAL FASTENER HOLES HAVE CRACKS DETECTED. REAMED HOLES, HFEC REAMED HOLES, NO CRACKS NOTED. TREATED, PRIMED & FABRICATED REPAIR DOUBLER, TRIPLER & FILLERS. INSTALLED IAW EA 008-5710-38-A6026.
RT WING UPPER SURFACE, FROM XW 69 - XW 240, HAS SURFACE CORROSION FORMING IN MULTIPLE AREAS. UT INSPECTION PERFORMED, PERFORMED OPEN HOLE INSPECTION. BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6029.
RT WING UPPER SURFACE FROM XW 468 TO WING TIP, HAS SURFACE CORROSION FORMING IN MULTIPLE AREAS. PERFORMED UT INSPECTION & CORROSION DETECTED. PERFORMED BLEND OUT. PERFORMED NDT, DP & HFEC OPEN HOLE INSPECTIONS. BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6030.
SURFACE CORROSION ON LOWER SURFACE OF MIDDLE INTERCOSTAL INSIDE STRUCTURAL BOX AT AFT OTBD CORNER OF LT MLW WW. GAINED ACCESS, FOUND 4 EA INTERCOSTALS CORRODED. REMOVED CORROSION & BLEND IS OUT OF LIMITS. FABRICATED REPLACEMENT INTERCOSTALS & INSTALLED IAW SRM.
LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS AND VORTEX GENERATORS AT CENTER SPAR BETWEEN XW 408 AND XW 485.28-49.
RT NOSE TUNNEL ACCESS DOOR 91D, CUT OUT HAS 3 BROKEN & WORN STRIKER PLATES. REMOVED 3 EACH STRIKER PLATES. FABRICATED 3 EACH STRIKER PLATES & INSTALLED IAW EA 008-5310-38-A6031.
LEFT HORIZONTAL STABILIZER INBD L/E UPPER SURFACE HAS CORROSION AT INBD SCREW HOLE. REMOVED CORROSION IAW SRM. FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 55-2-1.
LEFT WING OTBD LE, OTBD SECTION HAS INTERGRANULER CORROSION AROUND FASTENERS ON UPPER SKIN, BETWEEN XFS 841.250 - 860.000.. BLENDED DAMAGED AREA. BLEND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FILLER & INSTALLED IAW SRM.
LT WING OTBD SLOT DOOR, UPPER INBD PANEL HAS EXFOLIATION CORROSION. UT INSPECTION CONFIRM CORROSION, GAINED ACCESS. FABRICATED REPLACEMENT PANEL & INSTALLED IAW SRM.
LEFT WING OTBD SLOT DOOR CTR PANEL HAS EXFOLIATION CORROSION. FABRICATED REPLACEMENT DOOR IAW DWG. INSTALLED DOOR IAW SRM.
LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR SPAR, STRINGER 14 & XRS 172 - 204. PERFORMED UT INSPECTION. GAINED ACCESS & BLENDED. BLEND OUT OF LIMITS. ACCOMPLISHED EA 008-5710-38-A5990.
LT WING UPPER SKIN HAS CORROSION AT AFT SPAR, BETWEEN XRS139 - 172. PERFORMED BLEND OUT. PERFORMED UT INSPECTION. POSSIBLE CORROSION EXIST UNDERNEATH STRAP, FAIRING. REMOVED STRAP & ADDITIONAL CORROSION. BLENDED AREAS OUT OF LIMITS. FABRICATED FILLER & REPAIRED DOUBLER IAW EA 008-5730-38-A5922.
EXTERIOR FUSELAGE AFT LT LAVATORY, SERVICE PANEL CUT OUT WORN & GOUGED AT LATCH CONTACT POINTS. FOUND GOUGE TO BE OUT OF LIMITS & FOUND CRACK ON FRAME. REPAIRED IAW SRM.
EXTERIOR FUSELAGE, CORROSION ON LOWER SKIN, BETWEEN STRESS PANELS, STATION 680, LONGERON 36. REMOVED CORROSION. PERFORMED UT INSPECTION. BLEND OUT OF LIMITS. UPON GAINING ACCESS, FOUND CORROSION ON INNER SKIN & SURROUND STRUCTURE, BETWEEN STATION 683 - 718, LONGERON 36. GAINED ACCESS. FABRICATED NEW SKIN PANEL, 4 EACH REPAIR DOUBLERS & 4 EACH FINGER DOUBLERS & INSTALLED IAW EA 008-5300-38-A5865.
LEFT WING, OTBD FLAP UPPER SURFACE, INBD OF STATION 219, FLAP TRACK IS CHAFED & GOUGED. BLENDED OUT DAMAGED AREA, MATERIAL LOSS OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW 008-5700-38-A5864.