N922UP

Part: SMOKE GOGGLES — SCRATCHED (COCKPIT)

INSPECTION TYPE:N/A 2ND OBSERVER SMOKE GOGGLES BADLY SCRATCHED. REMOVED AND REPLACED 2ND OBSERVER SMOKE GOGGLES.

Part: SLAT TRACK — CORRODED (NR 6 SLAT) · airframe 49,681 hrs · 37,104 cycles

ON REMOVAL OF NR 6 SLAT I/B TRACK SKIN SUPPORT BRACKET, CORROSION ON TEE TRACK FOUND BENEATH BRACKET. NR 6 SLAT TRACK REPLACED IAW MM 27-81-11.

Part: LAP JOINT — CORRODED (BS 1139 STR 4 RT) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C 2 BULGES FOUND ON LAP JOINT AT STRINGER 4R BS 1139. DAMAGED AREA CUT OUT IAW SRM 53-30-3 FIG 5 AND REPAIRED IAW SRM 53-30-3 FIG 5.

Part: BUSHING — CORRODED (NR 1 PYLON) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C NR 1 ENGINE FWD ENGINE MOUNT PITTING CORROSION IN BORE OF MOUNT HOLES (TW O/B HOLES). BUSHINGS REPLACED IAW SOPM 20-50-03 AND EO B727-5440-1592 APNDX-A.

Part: RIB — CRACKED (NR 8 SLAT) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C-CRACK ON NR 8 SLAT O/B RIB AT I/B TRACK ATTACHMENT AREA. SLAT STOP DRILLED IAW AAAE EO 2005-081-004 REV 1 (UPS ENG FILE NR 727- 57-20133).

Part: BULKHEAD — CORRODED (BS 870) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE: C, CORROSION ON LT WHEEL WELL BULKHEAD AT BS 870 - FWD FACE 25 INCH FROM O/B EDGE AND 20 INCH FROM BOTTOM EDGE. REPAIR CARRIED OUT IAW AAAE RO 2005-081-2 -UPS ENG FILE NUMBER 727-53 -20190.

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C SURFACE CORRSION AT BS 1130 JOINT BETWEEN FLOORBEAM TOP AND CREASE WEB AT RBL 62. REPAIR PARTS FABRICATED IAW AAAE EO 2005-081-003 - UPS ENG FILE 72 7-53-20189. DOUBLER INSTALLED IAW SRM 51-30-02.

Part: ATTACH FITTING — CRACKED (BS 1050 LBL 21) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE: C, CRACK IN ZEE SECTION ATTACHED TO FRAME AT BS 1050 LBL 21. Z-SECTION REPAIRED IAW SRM 51-40-4 FIG 2.

Part: SHEAR TIE — CRACKED (BS 740 LBL 25.08) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C SUSPECT CRACK IN CENTER TANK FRONT SPAR TO STIFFENER SHEAR TIE CLIP O/B AFT RADIUS LBL 25-08. SHEAR TIE CLIP REPLACED IAW 51-30-02.

Part: FLAP TRACK — CORRODED (NR 4 FLAP) · airframe 496,813 hrs · 7,104 cycles

INSPECTION TYPE:C-CORROSION FOUND ON FWD MOUNTING PAD OF NR 4 FLAP TRACK. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K. SURFACE TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10.

Part: FLAP TRACK — CORRODED (NR 4 FLAP) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK AFT MOUNT PAD CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K & TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10.

Part: FLAP TRACK — CORRODED (NR 4 FLAP) · airframe 496,813 hrs · 7,104 cycles

INSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK FWD MOUNTING UPPER AND LWR, ALSO INNER RADIUS OF HOLES. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K AND TEMPER ETCHED IAW SOPM 20-10-01.

Part: FITTING — CORRODED (NLG TRUNNION) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C CORROSION ON NLG TRUNNION FITTINGS LT AND RT. CORROSION REMOVED FROM LT & RT TRUNNION FITTINGS IAW SRM 53-40-01. NEW BUSHINGS FABRICATED AND INSTALLED IAW MM 53-40-01 AND 53-40-01 FIG 2.

Part: STIFFENER — CRACKED (LT WING) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C-CRACK IN VERTICAL STIFFENER LT WING FRONT SPAR AT STA 557. STIFFENER REPLACED IAW SRM 51-30-2 AND DRW NR 65-16200.

Part: CHANNEL — CRACKED (RT ELEVATOR.) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C SUPPORT CHANNEL CRACKED AT TOP END, JUST I/B OF RT ELEVATOR NR 1 HINGE BEAM, AFT OF ELEVATOR I/B INPUT ROD. CHANNEL FABRICATED IAW SRM 51-20-1 FIG 7. CHANNEL REPLACED IAW SRM 51-30-02.

Part: STIFFENER — CORRODED (BS 870) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE:C HORIZONTAL STIFFENER CORRODED IN CABIN AT BS 870 FWD SIDE, RBL 19. REPLACEMENT STIFFENER FABRICATE IAW SRM 51-20-10 AND DRAWING 65-23114. STIFFENER INSTALLED IAW SRM 51-30-02 AND DRAWING 65-16328.

Part: FITTING — LEAKING (FUEL SYSTEM) · airframe 49,681 hrs · 37,104 cycles

INSPECTION TYPE: C+SI, FUEL LEAK FROM UNDERNEATH LT LANDING GEAR FWD TRUNNION SUPPORT SITTING SEEMS TO BE COMING FROM LWR LARGE BOLTS. LWR I/B FASTENERS (X2) REMOVED IAW TRUNNION REMOVED AND CORROSION FOUND SRM 51-30-02 AND BOTH HOLES REAMED TO 1ST OVERSIZE DUE TO CORROSION. CORROSION STILL EVIDENT. FITTING REMOVED IAW AAAE EO 2005-081-001 AND REWORKED. TRUNNION RESEALED IAW MM28-11-00. UPS FILE NUMBER = B727-5 330-22949.

Part: STRUCTURE — GOUGED (LT TE FLAP)

INSPECTION TYPE: ASV, LEFT O/B TRAILING EDGE FLAP HAS A GOUGE AT LEADING EDGE O/B ATTACH POINT (I/B OF ATTACH POINT). INSTALLED REPAIR DOUBLER PER SRM 57-50-4 FIG 9. REMOVED AND REINSTALLED LEFT O/B TRAILING EDGE AFT FLAP TO FACILITATE REPAIR IAW MM 27-51-12.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERIES REPLACED. INSPECTED/TESTED SERVICEABLE IAW B727 MM 33-50-01.

Part: TRUNNION — CORRODED (LT MLG) · airframe 49,153 hrs · 36,634 cycles

INSPECTION TYPE:C LT MLG TRUNNION LINK FWD TRUNNION CORRODED. LT MLG TRUNNION LINK REPLACED IAW MM 32-11-01.

Part: WEB — CRACKED (#4 SLAT RIB) · airframe 49,153 hrs · 36,634 cycles

INSPECTION TYPE:C SUSPECT CRACK #4 SLAT RIB I/B OF ACTUATOR ROD END CARRIED OUT WEB REPAIR IAW SRM 51-40-2

Part: FLANGE — WORN (BS 1183 BLKD) · airframe 49,153 hrs · 36,634 cycles

INSPECTION TYPE:C BS 1183 BULKHEAD THE AFT FLANGE OF HOIZ. STIFFENER P/N 65-16350-240 IS WORN AT LBL 32 APPROX DUE CHAFFING OFF HYDRAULIC PIPE FLANGE REPAIRED IAW SMRO EO 2002-015-001 UPS ENGINEERING FILE NO. 727-53-20048

Part: FLAP — CRACKED (WING) · airframe 49,153 hrs · 36,634 cycles

INSPECTION TYPE:C NR 5 L/E FLAP HAS CRACK AT I/B LOWER BONDING WIRE ATTACH POINT (BULLNOSE). REPAIR CARRIED OUT IAW SMRO EO 2002-015-002 UPS ENGINEERING FILE 727-57-20052.

Part: SKIN — CRACKED (ELEV. STA 130) · airframe 49,153 hrs · 36,634 cycles

INSPECTION TYPE:C R/H ELEVATOR SUSPECT CRACK IN ELEVATOR BEADED SKIN ELEV. STA. 130 AP PROX. REPAIR CARRIED OUT IAW SRM 51-30-2, 55-20-3, 51-40-5, 51-80-7

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 49,107 hrs · 36,604 cycles

INSPECTION TYPE:N/A NR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE (4 PSI). REPLACED ENGINE NR 3 IAW TC 1273 AND TC 1276. ENGINE RUN SATISFACTORY.

Part: STOP FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE:N/A AFT CARGO DOOR AFT NR 1 STOP FITTING CRACKED. AFT CARGO DOOR NR 1 STOP FITTING REPLACED IAW EO B727-5230-0032 APP C AND DRAWING 65-18625.

Part: SLIDE — OUT OF POSITION (CABIN)

INSPECTION TYPE:N/A, SLIDE FELL OUT OF CONTAINER. ITEM DEFFERRED IAW MEL 52-15, NOT REQUIRED FOR FLIGHT.

Part: MODULE — FAILED (HYDRAULIC SYS)

INSPECTION TYPE:N/A ON CLIMBOUT OF WAW A-SYS HYD PRESS DROPPED TO ZERO. NO FLUID LOSS. INADVERTANT DEPLOYMENT OF NR 1 THRUST REVERSER ON TOUCH DOWN. REPLACED A-HYD SYS PRESSURE MODULE DEACTIVATED NR1 T-R PER MEL. SUSPECT OUT OF RIG.

Part: BATTERY — DISCHARGED (AFT BULKHEAD)

INSPECTION TYPE:N/A, FLASHLIGHT ON BULKHEAD AFT OF LAV NEEDS NEW BATTERIES. REMOVED AND REPLACED BATTERIES IN FLASHLIGHT REAR BULKHEAD TOILET COMPARTMENT. OPS CHECK SATISFACTORY.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A ON SHUTDOWN, DISCOVERED COCKPIT EMERGENCY EXIT LIGHT DOES NOT WORK- BULBS CHECK GOOD-EXTREMELY DIM WHEN SWITCHED TO ON POSITION - BATTERY APPEARS BAD R/R EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00 OPS CHECK SATIS. PN/ OFF/ON 10-0067-9 SN OFF 26744 SN ON UP10498

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C DURING 950 FITTING REPLACEMENT TIE DOWN ATTACH POINT AT FLOOR LEVEL ON BEAM AT BS 950 FOUND CRACKED. TIE DOWN REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C ON REMOVAL OF S18A RT SECTION AND NR 1 INSP OF ALL ACCESSED FASTENER HOLES CORROSION AND SUSPECT CRACKS FOUND IN SKIN REPAIR CARRIED IAW SRM 51-10-6 AND SMRO EO 2000-036-003 UPS ENGINEERING FILE NR 727-53-2289.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C, ON REMOVAL OF BODY FITTING 940 RT CORROSION FOUND ON LWR SURFACE OF STR 18 A AROUND FASTENER HOLES COMMON TO BS 940. REPAIR CARRIED OUT IAW SRM 51-30-2 UPS EO B727-5330-3815 & SMRO EO 2 000-036-003 UPS ENGINEERING FILE 727-53-2289.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C, POSSIBLE CRACK INDICATION ON STR 15L, BS 1213 IN AFT AIRSTAIRS AREA. REPAIRED STRINGER IAW SRM 53-10-03 FIG 1.

Part: CASTING — CRACKED (TAIL SKID) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C TAIL SKID SUPPORT STRUCTURE IN TAIL SKID CAVITY AREA, UPPER CASTING TIE ROD, LEFT HAND SIDE, CASTING CRACKED BETWEEN TWO FASTENER HOLES. CASTING REPLACED IAW SRM 51-30-2.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C SUSPECT CRACK NR 4 SLAT ACTUATOR O/B RIB PREVIOUS (AFT) RADIUS OF ANGLE. REPAIR CARRIED OUT IAW MM 27-81-32 SRM 51-40-02 & MM 27-81-32.

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C, CORROSION EVIDENT IN NR 1 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW UPS EO B727-5440-11592.

Part: BUTT JOINT — CORRODED (FUSELAGE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C, SUSPECT CORROSION AT BUTT JOINT BS 441, S5L. REPAIR CARRIED OUT IAW UPS EO B727-5310-1371 APPENDIX 8.5 AND BOEING DRAWING 69-62161.

Part: FITTING — CORRODED (NR 3 PYLON) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C CORROSION EVIDENT IN NR 3 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C, NR 6 SLAT INNER SKIN CRACKED AROUND CTR FASTENER I/B OF ACTUATOR. REPAIRED INNER SKIN IAW UPS EO B727-5750-3082.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C ON INSP PER APPENDIX 8.2 SUSPECT MATERIAL LOSS OF 20 PERCENT AT BS 360 BETWEEN STR 23 & 24R. REPAIR CARRIED OUT IAW APPENDIX 8.5 UPS EO B727-5310-1371 AND DRAWING 69-62161.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C ON INSP PER APPENDIX 8.2 SUSPECT MATERIAL LOSS OF 20 PERCENT AT BS 360 AND STR 21L. REPAIR CARRIED OUT IAW EO B727-5310-1371 APPENDIX 8.5.

Part: BEAM — CRACKED (BULKHEAD) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C CRACK FOUND ON AFT PRESSURE BULKHEAD VERTICAL BEAM BS 1183 LBL 26.83 AT WL 262 WEB. REPAIR CARRIED OUT IAW WITH UPS EO B727-5311-0631 APPENDIX D.

Part: BEAM — CRACKED (BULKHEAD) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C, 3 CRACKS FOUND ON AFT PRESSURE BULKHEAD VERT BEAM BS 1183 RBL 26.83 AT WL 260 WEB. REPAIR CARRIED OUT IAW UPS EO B727-5311-0631 APPENDIX D.

Part: BOLT — DAMAGED (NR 3 ENGINE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C TO AID NDI REMOVE ENGINE NR 3 FWD AND AFT CRANE BEAM SHOULDER BOLTS. REPAIR CARRIED OUT IAW MM 71-21-03.

Part: BOLT — DAMAGED (NR 1 ENGINE) · airframe 48,329 hrs · 35,956 cycles

INSPECTION TYPE:C TO AID NDI REMOVE ENG NR 1 FWD & AFT CRANE BEAM SHOULDER BOLTS. REPAIR CARRIED OUT IAW MM 71-21-03.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHT IN COCKPIT CAME LOOSE DURING TAXI.. REINSTALLED COCKPIT EMERGENCY EXIT LIGHT AND CHECKED LATCH SECURITY. TESTED PER MM 33-50-01, OPS CHECK GOOD.

Part: RETRACT MECH — INOP (TE FLAPS)

FLAPS FAILED TO DEPLOY.

Part: HINGE — CORRODED (RT AILERON)

INSPECTION TYPE:C+SI, RT I/B AILERON CENTERING HINGE CORRODED. CENTERING HINGE REMOVED AND REPLACED IAW 27-10-01.

Part: FITTING — CRACKED (BS 1183)

INSPECTION TYPE:C+SI, STRINGER 8 AFT OF BS 1183 LT LOWER FITTING FOUND CRACKED. FITTING REMOVED AND NEW FITTING INSTALLED IAW SRM 51-30-2 AND MM 53-11-00.

Part: STRINGER — DAMAGED (BS 700)

INSPECTION TYPE:C+SI, DAMAGE STR 22 BS 700 RT AT FRAME ATTACH POINT. STRINGER REPAIRED AS PER SRM 53-10-3 FIG 1 DETAIL 2.

Part: PANEL — CORRODED (WS 550)

INSPECTION TYPE:C+SI, ACCESS PANEL NR 8 FOR NR 3 FUEL TANK CORRODED. PANEL REPLACED PER MM 28-11-21.

Part: STRINGER — CRACKED (BS 380)

INSPECTION TYPE:C+SI, STR 23 RT CRACKED AT FRAME ATTACH POINTS BS 380 STR 23 RT. REPLACED BETWEEN BS 360 AND 440 IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 400)

INSPECTION TYPE:C+SI, STR 23 LT CRACKED AT FRAME ATTACH POINT BS 400 STR 23 LT. REPLACED IAW SRM 53-10-2 BETWEEN BS 360 AND BS 440.

Part: STRINGER — CRACKED (BS 420)

INSPECTION TYPE:C+SI, STR 25 LT DAMAGED AT FRAME ATTACH POINTS BS 420 LT. CRACKED STRINGER REPAIRED IAW SRM 53-10-2 FIG 1 DETAIL 2.

Part: STRINGER — CRACKED (BS 380)

INSPECTION TYPE:C+SI, STR 21 RT CRACKED AT FRAME ATTACH POINTS BS 380. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.

Part: CASTING — WORN (TE FLAPS)

INSPECTION TYPE:C+SI, NR 5 JACKSCREW FAIRING, AFT BEARING WORN. BEARING CASTING REPLACED PER DWG 65-26786 AND SRM 51-30-2.

Part: STRINGER — CRACKED (BS 400)

INSPECTION TYPE:C+SI, STR 22 LT DAMAGED AT FRAME ATTACH POINT BS 400. CRACKED STR 22 LT SECTION REPLACED BETWEEN BS 390 AND BS 440 IAW SRM 53-10-2.

Part: STRINGER — CRACKED (BS 420)

INSPECTION TYPE:C+SI, STR 24 LT CRACKED AT FRAME ATTACH POINTS. BS 420 STR 24L REPLACED BETWEEN BS 360 AND BS 440 IAW SRM 51-30-2.

Part: PANEL — CORRODED (WS 180)

INSPECTION TYPE:C+SI, NR 1 ACCESS PANEL RHS FOR NR 2 INTEGRAL SECTION CORRODED. PANEL REPLACED IAW MM 28-11-21.

Part: STRINGER — CRACKED (BS 420)

INSPECTION TYPE:C+SI, STRINGER 24 RT CRACKED AT FRAME ATTACH POINTS. STR 24 RT REPLACED BETWEEN BS 360 AND BS 440 IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 420)

INSPECTION TYPE:C+SI, STRINGER 25 RT DAMAGED BS 420 AT FRAME ATTACH POINTS. CRACKED STRINGER 25 RT REPLACED BETWEEN BS 360 AND BS 440 IAW SRM 51-30-2.

Part: FRAME — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:C+SI, AFT CARGO DOOR MOVABLE FAIRING IS CRACKED AT THE LOWER RAIL FWD FRAME ATTACH POINT. REPAIRED FRAME IAW SRM 51-40-3 FIG 1.

Part: PANEL — CORRODED (NR 3 TANK)

INSPECTION TYPE:C+SI, NR 3 TANK I/B AND O/B BOOST PANELS CORRODED. PANELS REPLACED IAW MM 12-30-06.

Part: RING — CORRODED (WS 400-725)

INSPECTION TYPE:C+SI, RT WING NR 3 FUEL TANK ACCESS PANEL CLAMP UP RINGS CORRODED ON NR 2 THRU NR 14. CLAMP UP RINGS REPLACED IAW MM 28-11-21.

Part: STRINGER — CORRODED (BS 700)

INSPECTION TYPE:C+SI, CORROSION IN STR 23, BS 700 RHS. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 1.

Part: CASTING — WORN (NR 8 SPOILER)

INSPECTION TYPE:C+SI, NR 8 SPOILER O/B HINGE CASTING WORN ON RT WING T/E. CASTING REPLACED IAW DWG 65-16216.

Part: HINGE — WORN (NR 9 SPOILER)

INSPECTION TYPE:C+SI, NR 9 SPOILER I/B AND O/B HINGE CASTINGS WORN ON RT WING TRAILING EDGE. WORN CASTINGS REMOVED AND REPLACED WITH NEW CASTINGS IAW SRM 51-30-2 & DRAWING 65-16216.

Part: SKIN — CORRODED (BS 670)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON LAP STR 19 BETWEEN BS 660 AND 680 RT SIDE. LAP REPAIRED IAW UPS EO B727-5330-0509 APP 8.3.

Part: BRACKET — CRACKED (TE FLAP FAIRING)

INSPECTION TYPE:C+SI, NR 3 FLAP TRACK MID FAIRING ANGLE BRACKET CRACKED AT FWD END OF O/B ROLLER TRACK. CRACKED ANGLE BRACKET REPLACED PER SRM 51-10-1 AND SRM 57-20-2 FIG 4.

Part: CASTING — CORRODED (TE FLAPS)

INSPECTION TYPE:C+SI, NR 6 FLAP TRACK MID FAIRING FWD HINGE CASTING CORRODED AT LUGS. CASTING REPLACED IAW DWG 65-21795.

Part: CASTING — CRACKED (NR 1 FLAP TRACK)

INSPECTION TYPE:C+SI, NR 1 FLAP TRACK MID FAIRING FWD ATTACH CASTING CRACKED. CASTING REPLACED IAW SRM 51-30-2.

Part: CHANNEL — CRACKED (TE FLAPS)

INSPECTION TYPE:C+SI, NR 5 FLAP TRACK AFT FAIRING CRACK IN CHANNEL SECTION AT UPPER O/B ATTACH POINT. CHANNEL SECTION REPLACED IAW SRM 51-20-1 FIG 7 AND SRM 57-20-2 FIG 4.

Part: SKIN — CORRODED (BS 600-620)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON LAP AT BS 600-620 STR 19 RT SIDE INTERNAL SURFACE. LAP REPAIRED IAW UPS EO B727-5330-0509 APPENDIX 8.3/8.4 FROM BS 600-700 STR 19 RT.

Part: CASTING — CORRODED (NR 8 FLAP TRACK)

INSPECTION TYPE:C+SI, NR 8 FLAP TRACK MID FAIRING FWD ATTACH CASTING CORRODED. CASTING REPLACED IAW SRM 51-30-02.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-C+SI, SUSPECT CRACK CARGO DOOR (FWD) FWD HINGE FRAME (DOOR INTERIOR). FWD HINGE FRAME REPLACED IAW DWG 69-18203.

Part: PANEL — CORRODED (WS 230)

INSPECTION TYPE:C+SI NR 1 FUEL TANK INBD BOOST PUMP ACCESS PANEL CORRODED. PANEL REPLACED IAW MM 28-22-21.

Part: ANGLE — CRACKED (CARGO DOOR)

INSPECTION TYPE-C+SI, SUSPECT CRACK FWD CARGO DOOR (LWR) FWD HINGE AT FRAME SUPPORT ANGLE. SUPPORT ANGLE FABRICATED AND INSTALLED PER DWG 69-18203.

Part: PANEL — CORRODED (WS 280)

INSPECTION TYPE:C+SI NR 1 FUEL TANK OB BOOST PUMP ACCESS PANEL CORRODED. PANEL REPLACED PER MM 28-22-21.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON NR 6 FLAP TRACK FWD ATTACH LUG. REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (FILE NR 727-57-2052).

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:C+SI, NR 3 FLAP TRACK FWD ATTACH LUG HAS LIGHT SURFACE CORROSION ON I/B FACE (ON WING). REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (UPS FILE NR 727-57-2052).

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON NR 7 FLAP TRACK FWD ATTACH LUG I/B AND O/B. REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (FILE NR 727-57-2052).

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:C+SI, NR 4 FLAP TRACK FWD ATTACH LUG ON WING HAS LIGHT SURFACE CORROSION. REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (UPS FILE NO 727-57-2052).

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:C+SI, SURFACE CORROSION ON NR 5 FLAP TRACK FWD ATTACH LUG. REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (FILE NR 727-57-2052).

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON NR 8 FLAP TRACK FWD ATTACH LUG I/B SIDE. REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (FILE NR 727-57-2052).

Part: SKIN — CRACKED (NR 3 LE FLAP)

INSPECTION TYPE:C+SI, NR 3 LE FLAP HAS CRACK AROUND RIVET ON ANTI-ICE SKIN CENTER SKIN BETWEEN CENTER HINGE AND INBOARD HINGE. ANTI-ICE SKIN REPAIRED PER EO B727-5750-3082.

Part: SKIN — CRACKED (NR 3 LE FLAP)

INSPECTION TYPE:C+SI, NR 3 LEADING EDGE FLAP HAS A CRACK AROUND RIVET ON ANTI ICE SKIN. ANTI-ICE SKIN REPAIRED IAW EOB727-5750-3082.

Part: CLEAT — CRACKED (BS 560)

INSPECTION TYPE:C+SI, CRACKED CLEAT DETECTED AT BS 560 BELOW MAIN CARGO DOOR SUPPORT FITTING. REPAIRED ANGLES IAW SRM 51-40-3.

Part: SUPPORT — CRACKED (BS 1090)

INSPECTION TYPE:C+SI DUCT SUPPORT CRACKED BS1090 LBL 45.5. NEW STRAP FABRICATED PER SRM 51-20-1 AND FITTED PER SRM 51-30-2.

Part: CLEAT — CRACKED (BS 487.1)

INSPECTION TYPE:C+SI, CRACKED CLEAT DETECTED AT BS 487.1 BELOW MAIN CARGO DOOR SUPPORT FITTING. CLEAT STOP DRILLED PER SRM 51-10-1.

Part: SEAT TRACK — GOUGED (BS 910)

INSPECTION TYPE:C+SI, SEAT TRACK AT BS 910 LBL 45.5 BADLY GOUGED. NEW SEAT TRACK SPLICED IN IAW SRM 53-10-5.

Part: SKIN — CRACKED (BS 243.7)

INSPECTION TYPE:C+SI, CRACK FOUND ON FUSELAGE SKIN BS 243.7 AFT ROW 6TH FASTENER DOWN (BET WEEN S14 AND S15 LH). REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3.

Part: CLEAT — CRACKED (BS 520)

INSPECTION TYPE:C+SI, CRACKED CLEAT FOUND AT BS 520 BELOW MAIN CARGO DOOR SUPPORT FITTING. CRACK STOP DRILLED PER SRM 51-10-1, REPAIRED ANGLES IAW SRM 51-20-3.

Part: POST — CRACKED (LT WINDOW)

INSPECTION TYPE:C+SI, CRACK FOUND IN INTERNAL DOUBLER LT WINDOW POST 5 INCHES ABOVE POINT F. WINDOW POST REPAIRED IAW UPS EO B727-5310-0012 APP D.

Part: STAIR — CORRODED (AIRSTAIRS)

INSPECTION TYPE:C+SI, CORROSION EVIDENT ABOVE NR 7 STAIRTHREAD FORWARD SUPPORT ANGLE ON RISER LOWER SURFACE. REPAIRED IAW SRM ADDENDUM EO 10-26-95.

Part: TRACK — CRACKED (NR 5 FLAP TRACK)

INSPECTION TYPE:C+SI, CRACK ON NR 5 FLAP TRACK. TRACK REPLACED, REF TC C57-581-04-4D FOR INSTALLATION.

Part: TRACK — CRACKED (TE FLAPS)

INSPECTION TYPE:C+SI, NR 3 FLAP TRACK SUSPECT CRACK AT AFT END OF TRACK. FLAP TRACK REMOVED AND REPLACED IAW TC C57-581-04-03.

Part: SKIN — CORRODED (BS 1175)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON SKIN BS 1175 STR 6L. SKIN REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1 BETWEEN STR 5L AND STR 8L BS 1183 TO 1170.

Part: SKIN — CORRODED (BS 1160-1183)

INSPECTION TYPE:C+SI, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 1160 TO 1183 BETWEEN S18L AND 19L. REPAIR CARRIED OUT IAW SMRO EO 99-08-009 (UPS FILE NR 727-53-2120).

Part: SKIN — CORRODED (BS 1323-1342)

INSPECTION TYPE:C+SI, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1323 & 1342 S9L. REPAIR CARRIED OUT IAW SMRO EO 99-08-004 (FILE NR 727-53-2117).

Part: HINGE HALF — WORN (BS 480-620)

INSPECTION TYPE:C+SI TO FACILITATE CLEANING OF MAIN CARGO DOOR HINGES, REMOVE HINGES FROM CARGO DOOR AND FUSELAGE. REFIT S HINGES 6 OF 8 HINGES FOUND OUT OF LIMITS ON INSPECTION. 6 HINGE SECTIONS REPLACED. HINGE SECTIONS ON DOOR CLEANED AND PROTECTED IAW OHM52-36-62 AND SRM 51-30-2.

Part: FRAME — CORRODED (BS 740-870)

INSPECTION TYPE:C+SI, ON INSPECTION OF UNDERWING FAIRING NR 3430 HAS SUSPECT CORROSION ON FWD FRAME. FWD FRAME REPAIRED IAW SRM 51-40-3 FIG 1.

Part: WEB — CRACKED (BS 1376)

INSPECTION TYPE:C+SI, WEB CRACKED ABOVE NR 2 ENGINE BS1376 LT. REPLACED WEB IAW BOEING DWG 65-17555.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE:C+SI, DURING INSPECTION OF BS 870 TERMINAL FITTING CRACK WAS FOUND BY NDT METHOD ON STRINGER TO FRAME TIE END STRINGER 10 AFT RT. NEW TIE END INSTALLED IAW SRM 51-30-2.

Part: FAIRING — CORRODED (WING/FUSELAGE)

INSPECTION TYPE:C+SI ON INSPECTION OF FAIRINGS, NR 3335 UPPER SIDE OF FAIRING EXTRUSION FOUND TO BE CORRODED. INTERCOSTAL REPLACED PER SRM 51-10-6 AND 51-30-2.

Part: BEAM — CORRODED (BS 480-620)

INSPECTION TYPE:C+SI DURING REMOVAL OF ACCORDIAN SEAL FOR HINGE INSPECTION TOP BEAM OF MA IN CARGO DOOR FOUND CORRODED IN SEVERAL AREAS. UPPER BEAM REMOVED AND REPLACED IAW BOEING DRAWING 65-25337.

Part: FRAME — CORRODED (WING/FUSELAGE)

INSPECTION TYPE:C+SI ON INSPECTION OF UNDERWING FAIRINGS, NR 3430 FOUND TO HAVE A NUMBER OF SMALL GOUGES ON MAIN CENTER FRAME AND CORROSION ON FWD FRAME LOWER CHORD I/B. SMALL GOUGES BLENDED OUT AND FOUND WITHIN LIMITS. FWD FRAME LOWER CHORD REPAIRED IAW SRM 51-40-4 FIG 3.

Part: PRESSURE WEB — CRACKED (BS 920)

INSPECTION TYPE:C+SI 3 CRACKS ON RT MLG WHEEL WELL PRESSURE FLOOR BBL10 TO BBL12 APPROX A T BS920. CRACKS REPAIRED IAW EO B727-5310-0088-K APPX C.

Part: SKIN — WORN (NR 3 TR UNIT)

INSPECTION TYPE:C+SI, NR3 ENGINE THRUST REVERSER LOWER DOOR SKIN (INNER) HAS WEAR. REPAIR CARRIED OUT PER SRM 54-10-03 FIG 203.

Part: ANGLE — CRACKED (BS 178)

INSPECTION TYPE:C+SI SUSPECT CRACK ON ANGLE BS178 RT FLOOR LEVEL. HFEC CONFIRMED CRACK. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1.

Part: WINDOW FRAME — CRACKED (BS 1090)

INSPECTION TYPE:C+SI, ON REMOVAL OF WINDOW FRAME TWO SUSPECT CRACKS FOUND AT BS 1090 RT. WINDOW FRAME REPLACED IAW DRG 65-18384 AND SMRO EO 99-08-002R1 UPS ENG FILE NR 727-53-2119.

Part: SKIN — DELAMINATED (RUDDER TAB)

INSPECTION TYPE:C+SI, LOWER RUDDER TAB HAS NUMEROUS PREVIOUS REPAIRS WITH DELAMINATION. REPAIRED IAW SRM 51-40-10 FIG 1.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON TOP FLOORBEAM CAP BS 344 LBL 25.75 TO 0. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7.

Part: SKIN — DAMAGED (LEFT AILERON)

INSPECTION TYPE:C+SI, LT I/B AILERON HAS DAMAGE ON UPPER SKIN AT FWD O/B END. DAMAGED AREA TRIMMED IAW SRM 57-50-5.

Part: FRAME — DAMAGED (BS 848.95)

INSPECTION TYPE:C+SI FRAME 848.95 LT 2ND FASTENER HOLE ABOVE FLOORLINE IS AT 0.341 AFTER CLEAN UP OF MECHANICAL DAMAGE. THIS IS OUTSIDE LIMITS OF MAX 0.313. REPAIR CARRIED OUT IAW APPENDIX B OF EO B727-5310-5474 AND SMRO EO 9 9-08-001 (UPS FILE NO 727-53-2115).

Part: SKIN — CORRODED (BS 441)

INSPECTION TYPE:C+SI, SUSPECT CORROSION AT BUTT JOINT BS 441 BETWEEN S20R TO S21R. REPAIR CARRIED OUT IAW EO B727-5310-1371 APPX 8.5.

Part: BRACKET — CRACKED (NR 1 TR UNIT)

INSPECTION TYPE:C+SI, NR 1 ENGINE THRUST REVERSER ACTUATOR FAIRING HAS 2 CRACKED MOUNT BRACKETS. BRACKETS REPLACED IAW MM 20-80-01.

Part: PLUG — CORRODED (BS 600)

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON WINDOW PLUG BS 600 S13L. WINDOW PLUG REPLACED IAW MM 52-30-00.

Part: FRAME — CRACKED (BS 740)

INSPECTION TYPE:C+SI, CRACKS ON O/B FLANGE BS 740 RT BETWEEN S18 R AND S24R. CRACKS CONFIRMED BY HFEC. REPAIR CARRIED OUT IAW UPS EO B727-5310-74 97.

Part: RIB — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE:C+SI, SUSPECT CRACK IN NR 3 LE SLAT RIB AT SLAT STA 200 APPROX. CRACK CONFIRMED BY HFEC. SLAT RIB REPAIRED IAW SRM 57-50-3 FIG 9.

Part: BRACKET — CRACKED (NR 3 TR UNIT)

INSPECTION TYPE:C+SI, NR 3 ENGINE THRUST REVERSER FAIRING MOUNT BRACKET CRACKED. BRACKET REPLACED IAW MM 20-80-01.

Part: CASTING — CRACKED (TE FLAPS)

INSPECTION TYPE:C+SI, CRACK ON OUTBOARD FLAP CONTROL VALVE SUPPORT CASTING IN ROOF OF RT MLG WHEEL WELL. REPLACED HOUSING IAW MM 27-51-51 AND OHM 20-50-02.

Part: BULLNOSE — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE:C+SI, CORROSION ON NR 4 LEADING EDGE FLAP BULLNOSE. BULLNOSE REMOVED AND REPLACED IAW MM 27-81-01.

Part: SKIN — CRACKED (BS 294.5)

INSPECTION TYPE:C+SI, CORROSION AT LAP S24R BS 294.5. CRACK CONFIRMED IN FASTENER HOLE. REPAIR CARRIED OUT PER EO B727-533 0-0509 APPX 8.3 AND DWG 69-61590.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C+S1, LIGHT SURFACE CORROSION ON SKIN UNDER NR 2 ADF ANTENNA (LWR AFT). CORROSION CONFIRMED ON EXTRUDED STIFFENER. STIFFENER REPLACED PER SRM 51-30-2.

Part: SKIN — CORRODED (BS 1100)

INSPECTION TYPE:C+SI, CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 1090 TO 1110, STR 10R STR 14R. REPAIR CARRIED OUT IAW SMRO EO 99-08-002R1 UPS ENG FILE NR 727-53-211 9.

Part: BRACKET — CORRODED (BS 740)

INSPECTION TYPE:C+SI, BULKHEAD BS 740 TENSION TIE BRACKET FOUND CORRODED. REMOVED BRACKET IAW SRM 51-30-02 IAW SRM, RE-INSTALLED NEW BRACKET IAW SRM 51-30-02, RE-INSTALLED BOLTS IAW MM 20-80-01.

Part: LIGHT — INOP (PAX DOOR)

FWD ENTRY DOOR EMERGENCY EXIT LIGHT ON WITH POWER OFF SWITCH/OFF. REMOVED AND REPLACED EMERG EXIT LIGHT ASSY, OPS GOOD PER MM 3350-01.

Part: LIGHT — INOP (PAX DOOR)

INSPECTION TYPE AS-E, FWD ENTRY DOOR EMERGENCY EXIT LIGHT COMES ON WHEN AIRCRAFT POWER TURNED OFF AND EMER EXIT LIGHT SWITCH IS IN OFF POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CHECKS GOOD PER M/ M 33-50-01 (P/N 10-0067-9), (S/N 32U) ON, (S/N 6155) OFF.

Part: RUDDER — SPLIT (EMPENNAGE)

DURING EACH LEG, THE RUDDER TRIES TO SPLIT AT VARIOUS SPEEDS AND ALTITUDES. INSPECTED RUDDER SYSTEM FOR LOOSE TABS OR COMPONENTS, NONE FOUND. COULD NOT DUPLICATE ON GROUND, ALL WORK DONE IAW MM 27-20 AND 27-30-143. NO FAULTS NOTED. ALL OPS CHECKS NORMAL, A/C OK FOR SERVICE.

Part: SKIN — CORRODED (L1 DOORWAY)

CORROSION DAMAGE JUST FWD OF L1 DOOR APPROX 12 IN EXT SKIN 5X 2 REF DMI 140558. REMOVED AND REPLACED LEFT SIDE FUSELAGE SKIN PANEL FROM STA 259.5 TO STA 312 AND S-10L TO S-14L AS PER UPS EO B727-5330-9847-A DATED 10/31/97. (REF N/R 731755).

Part: SLAT — CRACKED (NR 5 LE FLAP)

INSPECTION TYPE-N/A, NR 5 SLAT CRACKED AT OUTBOARD STOP THROUGH STOP MOUNTING POINTS. REPLACED NR 5 LEADING EDGE SLAT WITH A BORROWED PART FROM DELTA AIRLINES. WITH REF TO M/M 27-81-11. GRND CHKS GOOD. REMOVED (P/N 65-1 6221-2) (S/N BN46) OFF, (P/N 65-16221-88) (S/N BN4) ON.

Part: SKIN — CORRODED (BS 1108)

INSPECTION TYPE: C. CORROSION ON EXTERIOR FUSELAGE SKIN ABOVE AFT CARGO DOOR. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW 53-10-1. REMOVED DAMAGED SKIN AND FABRICATED REPAIR PARTS IAW TRANCO EWO - 96-2307, SRM'S 53-30-0, 51-10-2, 51-20-1.

Part: HINGE FITTING — PITTED (NR 4 LE FLAP)

INSPECTION TYPE-C, R/W NR 4 K-FLAP FIXED L/E CTR HINGE FITTING IS PITTIED. REMOVED AND REPLACED NR 4 K-FLAP CENTER HINGE FITTING IAW OHM 57-51-21.

Part: BULLNOSE LUGS — CORRODED (NR 2 LE FLAP)

INSPECTION TYPE-C, NR 2 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 2 K-FLAP BULLNOSE IAW OHM 57-51-21 AND M/M 27-81-01.

Part: BULLNOSE LUGS — CORRODED (NR 3 LE FLAP)

INSPECTION TYPE-C, NR 3 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 3 BULLNOSE IAW 57-51-21.

Part: BULKHEAD FITTING — CRACKED (BS 1183)

INSPECTION TYPE-C, FOUND BULKHEAD FITTINGS TO BE CORRODED AND CRACKED STR 20R BS 1183 WL 190. REMOVED AND REPLACED CRACKED AND CORRODED FITTINGS STA 1183 STR 20R IAW 51-10-1, 51-10-2, 51-30-5.

Part: BULLNOSE LUGS — CORRODED (NR 1 LE FLAP)

INSPECTION TYPE-C, NR 1 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED BULLNOSE LUGS IAW M/M 27-81-01 AND OHM 57-51-01.

Part: STRINGER — CRACKED (BS 1125-1180)

INSPECTION TYPE-C, FOUND STRINGER 15R CRACKED AT SEVERAL LOCATIONS FROM STA 1125 TO 1180. REMOVED AND REPLACED STRINGER SECTION NR 15R STATION 1125 TO 1180 IAW 53-10-03.

Part: SKIN — DISBONDED (RT TE FLAP)

INSPECTION TYPE-C, RIGHT WING I/B AFT FLAP UPPER SIDE 17 O/B FROM I/B END AND 13 FWD FROM T/E IS DISBONDED. REMOVED DAMAGE AND REPAIRED DISBONDED IAW SRM 51-40-06.

Part: GATE BEAM — CORRODED (MID GALLEY DOOR)

INSPECTION TYPE-C, CORROSION ON MID GALLEY LOWER GATE BEAM FORWARD SIDE INSIDE ON DOOR UNDER LEVELING COMPOUND STA 642, WL 217, RBL 69. CORROSION REMOVAL ON BEAM WAS OUT OF LIMITS, RELOCATED MID GALLEY LOWER GATE BEAM PER SRM 51-30-02.

Part: SKIN — CORRODED (BS 705-713)

INSPECTION TYPE-C, CORROSION ON INNER SKIN AT BS 705 TO 713, RBL 27 WL 153 UNDER RIGHT HAND WATER SEPARATOR. MECHANICALLY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-01 AND 53-30-01. REPAIRED SKIN STA 705 TO 713 RBL 27, WL 153, IAW SRM 53-30-03.

Part: FITTING — CRACKED (RT VERT STAB)

INSPECTION TYPE-C, CRACKED L-EXTRUSION AT RT FIN REAR SPAN CLOSURE RIB FITTING, ACCESS UNDER PANEL 9780. REMOVED AND REPLACED FITTING IAW SRM 51-30-2, 51-30-5.

Part: HAT CHANNEL — CORRODED (BS 344)

INSPECTION TYPE-C, CORROSION ON HAT CHANNEL AT STA 344, RBL 25 TO 35 WL 208. CORROSION REMOVAL OUT OF LIMITS, REMOVED CHANNEL, FABRICATED NEW PART, INSTALLED IAW SRM 53-10-1, 51-30-2.

Part: HAT CHANNEL — CORRDED (BS 304-344)

INSPECTION TYPE-C, CHANNEL AT BS 304 TO 344 RBL 17, WL 708 WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED HAT CHANNEL, FABRICATED NEW CHANNEL, REINSTALLED IAW SRM 53-10-01, 51-30-2.

Part: BEAM — CORRODED (BS 344)

INSPECTION TYPE-C, CORROSION ON TOP DOGHOUSE BEAM AT BS 344, LBL 15. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-02.

Part: SHEAR TIE — CORRODED (BS 660)

INSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 660 LBL 11 WL 150. REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-01. REPAIRED FRAME SHEAR TIE STA 660 IAW SRM 51-40-03.

Part: AILERON HINGE — CORRODED (RT AILERON)

INSPECTION TYPE-C, R/W, O/B AILERON O/B CENTER HINGE FITTING IS CORRODED AILERON SIDE. REMOVED AND REPLACED R/W, O/B AILERON O/B CENTER HINGE FITTING ON AILERON SIDE IAW SRM 51-30-05, 51-30-02 OHM 20-50-03 AND M/M 57-50-11.

Part: SKIN — CORRODED (BS 1180)

INSPECTION TYPE-C, CORROSION ON SKIN AT STA 1180 STR 7 LT WL 260. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1180 STR 7 LT WL 260 IAW SRM 53-30-1.

Part: HINGE — CORRODED (RT AILERON)

INSPECTION TYPE-C, R/W I/B AILERON CENTER AND O/B TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED CENTER AND O/B TAB FITTINGS ON R/W, I/B AILERON IAW SRM 51-30-02.

Part: STIFFENER — CORRODED (BS 336)

INSPECTION TYPE-C, CORROSION ON TOP DOGHOUSE BEAM AT BS 336 LBL 15. REMOVED CORROSION, REWORKED OUT OF LIMITS IAW SRM 53-10-1, REMOVED AND REPLACED STIFFENER, BEAM IAW SRM 51-30-2.

Part: EEL ASSY — INOPERATIVE (FLIGHT DECK)

WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: EEL — MALFUNCTION (CABIN)

PILOT REPORTED, EMERGENCY EXIT LIGHTS ILLUMINATED ON TAXI OUT WITH ARMING SWITCH ARMED. LIGHT WENT OUT WHEN SWITCH PLACED IN OFF POSITION, THEN ON WHEN ARMED. RESECURED EMERGENCY EXIT LIGHT ASSY, CHECK OK.

Part: CHANNEL — CORRODED (FS 342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD SIDE AND BASE OF THE FLOOR SUPPORT IN THE LAV AREA AT STATION 342 FROM RBL 13 TO 20. MAINTENANCE FABRICATED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-30-2 AND 51-10-1.

Part: SPAR — CRACKED (VERT STAB)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL STABILIZER RIGHT HAND REAR SPAR CHORD AT STATION 0 TO 12. MAINTENANCE REPAIRED THE ONE INCH CRACK STOP AT FASTENER HOLE.

Part: CHORD — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CENTER CHORD AT STATION 1342 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-10-1, 51-30-2 AND UPS EO 727-5530-4601B.

Part: CHORD — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND OUTBOARD CHORD AT STATION 1342, RBL 30 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHORD PER SRM 51-30-2.

Part: CHORD — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND OUTBOARD CHORD AT STATION 1342, LBL 30 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-30-02.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT CENTER CHANNEL AT STATION 1342 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHANNEL IAW SRM 51-10-1, 51-30-2 AND UPS EO 727-5530-4601B.

Part: WEB — CRACKED (FS 1223)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WEB AT THE INBOARD CHORD AT STATION 1223 AND WL 230. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-2.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND CHANNEL AT STATION 1342, LBL 18 AND WL 247. MAINTENANCE REMOVED AND REPLACED THE CHANNEL PER SRM 51-30-2.

Part: RIB — CRACKED (FS 760.95)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIB UPPER CHORD AT BL 70.5 AND STATION 760.95. MAINTENANCE CUT OUT DAMAGE AND REPAIRED IAW SRM 51-10-6 AND UPS EO 727-5710-1271F AND UPS EO 727-5710-6865A.

Part: SPAR — CRACKED (VERT STAB)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL STABILIZER REAR SPAR LEFT HAND CHORD AT STATION 0 TO 12. MAINTENANCE STOP DRILLED AND INSTALLED THE REPAIR KIT.

Part: FRAME — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND LOWER FRAME CHORD AT STATION 1342 AND LBL 24. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-30-2.

Part: FRAME — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND LOWER FRAME CHORD AT STATION 1342 AND RBL 24. MAINTENANCE REMOVED AND REPLACED THE CHORD PER SRM 51-30-2.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND CHANNEL AT STATION 1342, RBL 18 AND WL 247. MAINTENANCE REMOVED AND REPLACED THE CHANNEL PER SRM 51-30-2.

Part: FRAME — CORRODED (FS 1342, LBL 20)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND FRAME CHORD AT STATION 1342 AND LBL 20. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-30-2.

Part: RIB — CRACKED (FS 1365)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND RIB FLANGE AT STATION 1365 AND WL 250. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PART PER SRM 57-40-3 AND 51-30-2.

Part: FRAME — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND FRAME CHORD AT STATION 1342 AND RBL 20. MAINTENANCE REMOVED AND REPLACED THE CHORD.

Part: ANGLE — CRACKED (FS 1345)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND SKIN SUPPORT ANGLE AT FS 1345 AND FIN STATION 22.5. MAINTENANCE CUT OUT THE DAMAGED AREA AND INSTALLED FABRICATED SECTION AND SPLICE IAW SRM 51-40-3 AND 51-30-2.

Part: EEL — INOP (CABIN)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD.