N656GT

Part: ESCAPE REEL — UNSECURE · airframe 62,220 hrs · 43,891 cycles

ESCAPE REEL NOT SECURED. RESECURED DESCENT DEVICE, IAW AIA 25-61-03.

Part: ENGINE — VIBRATION (RIGHT) · airframe 61,603 hrs · 43,477 cycles

HEARD SEVERAL BANGS AND FELT THE AIRFRAME SHUDDER EACH TIME FOLLOWED BY ABNORMAL ENGINE INDICATIONS ON RIGHT ENGINE, WHICH RESULTED IN THE ENGINE SHUTTING DOWN IN FLIGHT. NR 2 ENG REMOVED & REPLACED IAW WORK CARD A-71-999-03-01.

Part: WEB — CORRODED (BS 970-1021) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

CORROSION IN SEVERAL AREAS ON UPPER SURFACE OF KEEL WEB, STA 970-1021 APPROX.(<P>REPAIRED DAMAGE IAW AMES DOCUMENTS 47389REA09 AND 47389REA07, SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #7 PAGES 1-8.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PN: 145T8612-1; KEEL BEAM WEB</P>)

Part: SUPPORT — CORRODED (ROLLER TRAY) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

ROLLER TRAY FRAME SUPPORT IS CORRODED AT STA 720, S 33R.&NBSP;(<P>BLENDED CORROSION ON FLOOR FRAME UPPER CHORD @ STA 720 ST 33R IAW B767 SRM 53-00-07 FIG 101 DET VIII. FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS 103". MATERIAL REMAINING .036". MATERIAL REMOVED .064". REMOVED DAMAGED SECTION. REINSTALLED UPPER CHORD SECTION PN BAC1506-3132-7075-T6511 PO# 0047619 AND SPLICE REPAIR IAW B767 SRM 53-00-09 FIG 201 DET VII. SEE PWA FOR WORK ACCOMPLISHED AND PARTIAL WORKSHEET #41 PG 1.</P>)

Part: BUSHING — LEAKING (RT WG FUEL TANK) · airframe 61,493 hrs · 43,408 cycles

RW MAIN TANK SUMP DRAIN LEAKING.(<P>REMOVED AND REPLACED SUMP DRAIN&NBSP;&AMP; SUMP DRAIN BUSHING IAW B767 AMM 28-11-05 AND AMES ENGINEERING 47389REA03. LEAK CHECK GOOD IAW B767 AMM 28-11-00-206. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET 45 FOR WORK COMPLETED.</P>)

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

RW LES 477 LOWER AIR LOAD RIB CORRODED.(<P>REMOVED AND REPLACED AIR LOAD RIB RW LES 477 IAW B767 SRM 51-40-02 PARAGRAPH 9. SEE PARTIAL WORK ACCOMPLISHED.</P>)

Part: LONGERON — CORRODED (LT OVERWING) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

LEFT SIDE OVERWING LONGERON CORRODED.(<P>REMOVED CORROSION ON LEFT SIDE OVERWING LONGERON IAW B767-200 SRM 51-10-02 AND REPAIRED IAW AMES NO. #47389REA05. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #9, PGS 1 &AMP; 2.</P>)

Part: WEB — CORRODED (BS 955-1021) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

CORROSION IN SEVERAL AREAS OF KEEL WEB IN RWW (M), JUST INBD OF BODY DOOR AT STA 955-1021.(<P>REPAIRED DAMAGE IAW AMES DOCUMENT 47389REA09 AND 47389REA07. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #10 PAGES 1-9 FOR WORK COMPLETED AND 47389REA10.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PART 145T8612-1, KEEL BEAM HORIZONTAL WEB.</P>)

Part: DOOR FRAME — CORRODED (BS 1270) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

&NBSP;ALC DOOR CUTOUT, FWD EDGE FRAME STRAP UPPER SURFACE IS CORRODED AT STA 1270, S32R.(<P>REPAIRED FRAME IAW B767-200 SRM 51-40-02 AND AMES 47389REA06. SEE PARTIAL WORK ACCOMPLISHED AND PWS 46.</P>)

Part: SPLICE PLATE — CORRODED (BS 933-977) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

THE RIGHT OVERWING LONGERON HAS A LARGE AREA OF CORROSION NEAR THE AFT END.(<P>AREA OF CORROSION FOUND TO BE OUT OF LIMITS IAW B767-200 SRM 53-50-05. AREA BEYOND LIMITS, THEREFORE REPLACEMENT OF R/H EXTERIOR LONGERON SPLICE PLATE WAS ACCOMPLISHED IAW AMES DOCUMENT 47389REA11. SEE PARTIAL WORK ACCOMPLISHED AND PWS #40 PG 1 OF 1.</P>)

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

FLOOR FRAME UPPER CHORD CORRODED

Part: KEEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

KEEL CORRODED AT STA 970-1021

Part: FAILSAFE — CORRODED (BS 1270) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

FAILSAFE STRAP ON FRAME AT ALC DOOR CUTOUT WAS CORRODED

Part: SPLICE PLATE — CORRODED (BS 922-933) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

LEFT OVERWING SPLICE PLATE CORRODED.

Part: BUSHING — WORN (RT WING SUMP) · airframe 61,493 hrs · 43,408 cycles

RT WING SUMP DRAIN LEAKING AT BUSHING

Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

RT WING AIRLOAD RIB CORRODED

Part: STRINGER SPLICE — CORRODED (BS 933-977) · airframe 61,493 hrs · 43,408 cycles

RT OVERWING LONGERON SPLICE PLATE CORRODED

Part: WEB — CORRODED (BS 1005) · corrosion level 2 · airframe 61,493 hrs · 43,408 cycles

KEEL WEB IN RWW CORRODED

Part: ACTUATOR — LEAKING (RT MLG) · airframe 59,243 hrs · 42,230 cycles

RH LANDING GEAR AFT SIDE BRACE ACTUATOR LEAKING.(<P>REMOVED AND REPLACED RH MLG SIDE BRACE ACTUATOR ASS. OPS CHECK NORMAL IAW AMM 32-32-02</P>)

Part: CONTROL UNIT — LEAKING (HYD SYSTEM) · airframe 59,243 hrs · 42,230 cycles

LEFT STCM INPUT SHAFT SEAL HAS HYDRAULIC LEAK.(<P>REMOVED AND REPLACED LEFT STCM. OPS CHECK NORMAL IAW AMM 27-41-00-715-014 TASK .</P>)

Part: STARTER — DAMAGED (NR 2 ENGINE) · airframe 59,243 hrs · 42,230 cycles

NO 2 ENGINE STARTER WITH METAL FRAGMENT LARGER THAN 0-1 INCH.(<P>REMOVED AND REPLACED THE #2 ENGINE STARTER IAW AMM 80-11-01. OPS CHECK NORMAL.</P>)

Part: HYDRAULIC SYSTEM — LOW (LEFT) · airframe 58,743 hrs · 41,971 cycles

LEFT HYD SYSTEM QTY WENT TO 0. C/W MTX PROCEDURES DISPATCH YK AT 1849Z DUE DATE 16AUG17.

Part: LINE — LOOSE (RT ENGINE) · airframe 58,315 hrs · 41,724 cycles

DURING TAKE OFF AT 80 KTS, THE RT ENGINE ROLLED BACK TO 96.8 N1, UNABLE TO PUSH BACK TO MATCH, LT ENGINE AT 100.4. ACCOMPLISHED EEC BITE IAW FIM 71-01, 804, NO FAULTS NOTED. FOUND LOOSE CBT LINE ON MEC. RAN ENGINE TO POWER IAW AMM 71-01-00, ALL INDICATIONS NORMAL.

Part: ROD — CORRODED (BLEED DUCT) · airframe 58,177 hrs · 41,643 cycles

APU BLEED AIR DUCT SUPPORT ROD FACING LEFT & RIGHT CORRODED LOCATED IN AFT HORIZONTAL STAB ACCESS AREA. REMOVED APU BLEED AIR DUCT SOPPORT ROD AND INSTALLED A NEW ONE IAW AMM 20-11-00.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,177 hrs · 41,643 cycles

RIGHT HORIZONTAL STAB OTBD END, AFT OTBD CHORDWISE ATTACH FLANGE FOR THE STAB TIP HAS CORROSION ON THE UPPER SURFACE. REMOVED AND REPLACED THE ATTACH FLANGE IAW SRM 51-40-2, PARAGRAPH 4.

Part: HOUSING — CORRODED (BOOST PUMP) · airframe 58,177 hrs · 41,643 cycles

RIGHT WING BOOST PUMP HOUSING SHUT OFF SLEEVE HAS CORROSION.

Part: WINDOW FRAME — CORRODED (BS 720-740) · corrosion level 2 · airframe 58,177 hrs · 41,643 cycles

CABIN WINDOW FRAME, STRINGER 16R, IS CORRODED AT LOWER EDGE. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02-0G-0 AND DRAWING 143T3410.

Part: ATTACH FITTING — CORRODED (BS 1437-1461) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1437 TO 1461, LBL 48 TO 72. FOUR BAT WINGS CARGO LOCKS ATTACH FITTINGS FOUND CORRODED AFTER REMOVAL OF BAT WING CARGO LOCKS. CLEANED & EVALUATED THE AREAS UNDER CARGO LOCKS ATTACH FITTINGS IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 58,177 hrs · 41,643 cycles

RIGHT HORIZONTAL STAB INBD END, INBD ATTACH FLANGE FOR PANEL 345CB HAS CORROSION ON THE UPPER & LOWER SURFACE OF HORIZONTAL FLANGE. REMOVED CORROSION IAW SRM 55-10-09 AND REINSTALLED IAW SRM 51-40-02- & 02.

Part: FITTING — CORRODED (BS 1395-1417) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS1395 TO 1417, LBL 72, FOUR BAT WING CARGO LOCKS ATTACH FITTINGS FOUND CORRODED. FITTINGS LOCATED UNDER REMOVED BAT WING CARGO LOCKS. REF NRI 3280. CLEANED AND EVALUATED MAIN DECK CARGO IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94. TREATED, PRIMED, & PAINTED THE AREAS IAW SRM 51-20-01-OG-0.

Part: FITTING — CORRODED (BS 1217-1237) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BAY BS 1237 - 1217, LBL 48 TO 72. FITTING LOCATED UNDER REMOVED BATWINGS CORRODED. CLEANED & EVALUATED IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94. TREATED & PRIMED IAW SRM 51-20-01-OG-0.

Part: LOCK — CORRODED (BS 1307-1327) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1307 - 1327, LBL 48 - 72. FOUR BAT WINGS CARGO LOCKS CORRODDED. REMOVED THE CORROSION IAW SRM 51-10-02, AND FOUND TO BE IN LIMITS IAW CMM 25-50-99.

Part: ATTACH FITTING — CORRODED (BS 1177-1197) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1177 - 1197, LBL 48 AND 72, FOUR BAT WING CARGO LOCK FITTINGS ARE CORRODED. CLEANED & EVALUATED THE AREAS UNDER CARGO LOCKS IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94.

Part: TEE FITTING — CORRODED (HORIZONTAL STAB) · airframe 58,177 hrs · 41,643 cycles

LEFT HORIZONTAL STAB, OTBD END RIB 17, UPPER ATTACH TEE FITTING FOR STAB TIP HAS CORROSION AT THE FWD END, BOTH INBD AND OTBD SIDES, FWD 3 INCHES. REMOVED CORROSION IAW AMM 51-10-02-0G-0. FOUND TO BE IN LIMITS IAW SRM 55-10-09-1A-1, FIGURE 101, DETAIL 1.

Part: HOUSING — CORRODED (BOOST PUMP) · corrosion level 2 · airframe 58,177 hrs · 41,643 cycles

LEFT WING BOOST PUMP HOUSING SHUT OFF SLEEVE HAS CORROSION TO THE INSIDE FUEL PATH SURFACE. REMOVED AND REPLACED THE BOOST FUEL PUMP HOUSING IAW AMM 28-92-03-404-027.

Part: SUPPORT CHANNEL — CORRODED (RT WING) · corrosion level 2 · airframe 58,177 hrs · 41,643 cycles

RT WINE TE PANEL SUPPORT CHANNEL AT PANEL 661PB HAS CORROSION BETWEEN NUT PLATE HOLES. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-40-05 & DWG 113T1912, SHEET 1, REV D.

Part: LOCK — CORRODED (BS 1480-1500) · corrosion level 2 · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1480 - 1500, LBL 48 - 72. TWO BROKEN BAT WING CARGO LOCKS ARE CORRODDED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 25-50-99.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 58,177 hrs · 41,643 cycles

RIGHT HORIZONTAL STAB OTBD END, AFT SPANWISE ATTACH FLANGE FOR THE HORIZONTAL TIP HAS CORROSION ON THE TOP SURFACE. REMOVED CORROSION IAW51-10-02-OG-0 PARA 14 & 15, FIG 1. FOUND TO BE WITHIN LIMITS IAW SRM 55-10-09 .

Part: INLET — CORRODED (NR 2 ENGINE) · airframe 58,177 hrs · 41,643 cycles

NR 2 ENGINE INLET LOWER TWO BOLT HOLES HAVE CORROSION. FREEZE PLUGS FABRICATED AND INSTALLED IAW SRM 51-20-07, PARA B, FIG 5 & FIG C, AND PARA 3B AND RDR PMO-TLS-17-007-14B.

Part: SHIM — CORRODED (CARGO DOOR) · airframe 58,177 hrs · 41,643 cycles

FWD CARGO DOOR AFT HOOK APPEARS TO HAVE CORROSION UNDER MOUNT SURFACE. INSPECTION REVEALED CORROSION IS ON LIMITED SHIMS. REPLACED AND REMOVED THE HOOK IAW SRM 51-20-11-0G-0, AND AMM 20-11-00-910-802.

Part: ATTACH BRACKET — CORRODED (BS 1257-1277) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1257 TO 1277 LBL 48 TO 72. FOUR EACH BAT WING CARGO LOCKS ATTACH BRACKETS CORRODED. CLEANED & EVALUATED IAW SRM 51-10-02. FOUND TO BE IN LIMITS IAW CMM 25-50-94.

Part: ATTACH BRACKET — CORRODED (BS 1510-1570) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1510 TO 1570, LBL 4. ONE BUMPER RAIL ATTACH BRACKET CORRODED. REMOVED & REINSTALLED THE BUMPER RAIL IAW SRM 51-40-02. CLEANED THE BUMPER RAIL IAW SOPM 20-30-03, NO CORROSION NOTED.

Part: ATTACH FITTING — CORRODED (BS 1349-1369) · airframe 58,177 hrs · 41,643 cycles

MAIN DECK CARGO BS 1349 - 1369, LBL 48 - 70. FOUR BAT WINGS CARGO LOCKS ATTACH FITTINGS FOUND CORRODED AFTER REMOVAL OF BAT WING CARGO LOCKS. CLEANED & EVALUATED THE AREAS UNDER CARGO LOCKS ATTACH FITTING IAW SRM 51-10-02, FOUND IN LIMITS IAW CMM 25-50-94.

Part: ENGINE — POWER LOSS (RIGHT) · airframe 57,772 hrs · 41,414 cycles

RTO ON TAKEOFF RT ENGINE DID NOT PRODUCE TAKEOFF THRUST, RTO BELOW 80 KNOTS. COMPLIED WITH GROUND TEST NR 4 VERIFIED BOTH ENGINE MAKE T/O POWER 108.6 NO THROTTLE SPLIT ELECTRONIC ENGINE CONTROL OFF REF AMM 71-00-00. TRANSFERED TO MDDR 70393 IAW MEL 73-21-01-01B, CAT C.

Part: ESCAPE ROPE — UNSERVICEABLE (CABIN) · airframe 56,852 hrs · 40,937 cycles

COCKPIT DESCENT DEVICE CABLE EXTENDED. R & R DEFECTIVE DESCENT DEVICE IAW AMM 25-61-03.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 56,716 hrs · 40,853 cycles

TRAILING EDGE FLAP DISAGREE MSG DISPLAYED & APPROACH LANDING FLAPS 20. TROUBLE SHOT IAW FIM 27-51 FIM FAULT TREE, NO FAULTS NOTED. PERFORMED BITE CHECK OF FSEU, NO FAULTS REPORTED, OK FOR SERVICE.

Part: BEAM — CORRODED (DOOR)

FLC DOOR, CORROSION UNDER NUTPLATE AFT OF UPPER END OF DOOR LIGHT. FABRICATED, R & R BEAM NR 6 IAW DOCUMENT 47169FAB03.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 56,319 hrs · 40,615 cycles

LEFT WING NR 1 OTBD FLAP ACTUATOR SUPPORT, RIB 1 HOLE HAS CRACK. REPAIRED SUPPORT RIB NR 1 HOLE IAW REA 47169REA02.

Part: SUPPORT BRACKET — DAMAGED (RT WING) · airframe 56,319 hrs · 40,615 cycles

THE FWD ATTACH SUPPORT BRACKET FOR RT TRANSFER CYLINDER ACTUATOR IS CORRODED & SPLITTING, INSIDE ACCESS 652CB OPENING. R & R BRACKET WITH A SERVICEABLE BRACKET IAW SRM 51-40-02. SEE PARTIAL WORK ACCOMPLISHED FOR WORK PERFORMED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

LEFT FAILSAFE CRACKED AT STATION 955. REPAIRED IAW EO 06753A070, TRIMMED.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

LONGITUDINAL BEAM IN CTR WING TANK HAS CRACKED SUPPORT BRACKET AT AFT BULKHEAD LBL 24. R & R BRACKET AT AFT BULKHEAD IAW SRM 51-40-02.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 56,319 hrs · 40,615 cycles

RIGHT WING NR 8 OTBD FLAP SUPPORT, RIB 3 HOLE HAS CRACK. REAMED HOLE 3 IAW REA 47169REA02.

Part: STRUCTURE — CORRODED (DOOR) · airframe 56,319 hrs · 40,615 cycles

FLC DOOR CORROSION UNDER LIGHT ASSEMBLY LOWER CTR NUTPLATE. R & R CHORD BELOW LIGHT ASSEMBLY ON FLC DOOR IAW SRM 51-40-02 PARA 7D, 4B & DOCUMENT 47169 FAB 04.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

RIGHT SIDE FAILSAFE CRACKED AT STATION 955. REPAIRED IAW EO 06753A070, TRIMMED.

Part: SPLICE PLATE — CORRODED (LT WING) · airframe 56,319 hrs · 4,065 cycles

CORROSION ON LT WING UPPER SPICE PLATE AT LES 574. REPAIRED UPPER SPLICE PLATE IAW REA 147169 REA01. SPLICED IN NEW SECTION FROM LES 549 TO LES 595.

Part: STRAP — CORRODED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

CORROSION ON STRAP ON FLC DOOR CUT OUT UNDER SLOPING PANEL, UPPER ATTACH BRACKET. REMOVED CORROSION IAW REA 47169REA10.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

STRINGER 25L CRACKED AT SPLICE AFT OF FS 676. SPLICED NEW STRINGER SECTION IAW REA 47169REA05 & SRM 53-00-03 FIG 201 REPAIR 2.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 56,319 hrs · 40,615 cycles

VERTICAL STAB ACCESS PANEL 324 AL AUX STRUCTURE FWD OTBD ANGLE END CRACKED. COMPLETED RAM FORM AS REQUESTED, ATTACHED TO JC A-06-056-01. REF SIGN STEP 1 B 4. REMOVED & INSTALLED NEW ANGLE IAW 51-40-02 PARA 5A & 5B PARA 7D.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 56,319 hrs · 40,615 cycles

LEFT WING NR 1 OTBD FLAP SUPPORT, RIB 3 HOLE HAS CRACK. REPAIRED RIB 3 & 4 IAW REA 47169REA02.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 56,319 hrs · 40,615 cycles

RIGHT WING NR 8 OTBD FLAP SUPPORT, RIB 4 HOLE HAS CRACK. REAMED HOLE 4 IAW REA 47169REA02.

Part: STRINGER SPLICE — TORN (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

STRINGER 32L, SPLICE AFT OF STATION 434 TORN. REPLACED SPLICE IAW SRM 51-40-02 SEC 4.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

ELONGATED HOLE THROUGH FAILSAFE STRAP & FRAME CHORD. REPAIRED IAW REA 47169 REA 10.

Part: STRUCTURE — CORRODED (DOOR) · airframe 56,319 hrs · 40,615 cycles

FLC DOOR, LOWER CHORD, 1 INCH FROM FWD END & 8 INCHES FROM BOTTOM IS EXFOLIATED UNDER NUTPLATE. R & R LOWER CHORD ON FLC DOOR IAW SRM 51-40-02 PARA 4B PARA 7D & DOCUMENT 47169FAB02.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 56,319 hrs · 40,615 cycles

LEFT WING FLAP ACTUATOR SUPPORT, RIB NR 2 HOLE HAS CRACK. REPAIRED SUPPORT RIB HOLE IAW REA 47169REA02.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 56,319 hrs · 40,615 cycles

STRINGER SPLICE AT FS 434 & STRINGER 34R CORRODED. INSTALLED NEW SPLICE IAW SRM 51-40-02 PARA 4.

Part: SKIN — CORRODED (DOOR) · airframe 56,319 hrs · 40,615 cycles

FLC DOOR, CORROSION ON INNER LOWER SURFACE PANEL & NUTPLATES. R & R INNER LOWER WEB ON FLC DOOR IAW SRM 51-40-02 PARA 7D PARA 4B & DOCUMENT 47169REA08 REV A.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 56,321 hrs · 40,618 cycles

RIGHT WING NR 8 OTBD FLAP SUPPORT, RIB 2 HOLE HAS CRACK. REAMED HOLE IAW REA 47169REA02.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 56,319 hrs · 40,615 cycles

RIGHT WING NR 8 OTBD FLAP SUPPORT, RIB 1 HOLE HAS CRACK. REAMED HOLE IAW REA 47169REA02.

Part: SKIN — CORRODED (RT WING) · airframe 56,015 hrs · 40,376 cycles

RIGHT WING OVERWING FILL PORT FAILED BONDING RESISTANCE CHECK, READS INFINITE RESISTANCE IAW JC A-28-018-04. REMOVED & REINSTALLED FILL PORT IAW AMM 28-11-04. REMOVED CORROSION IAW SRM 27-20-01.

Part: SKIN — CORRODED (LT WING) · airframe 56,015 hrs · 40,376 cycles

LEFT WING OVERWING FILL PORT FAILED BONDING RESISTANCE CHECK, READ INFINITE RESISTANCE IAW JC A-028-018-03. REMOVED FILL PORT, CLEANED CORROSION & REINSTALLED FILL PORT IAW SRM 57-20-01 & AMM 28-11-04 REA 47135REA02 A.