N948UP

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES, NO HELP. REMOVED AND REPLACED EMERGENCY EXIT ASSY & NEW BATTERIES INSTALLED. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (L1 EXIT DOOR)

INSPECTION TYPE:N/A, EMERGENCY LIGHTING INOP AT L1 EXIT DOOR. REPLACED EMERGENCY EXIT LIGHT ASSY AT L1 DOOR PER MM 33-50-01, OPS CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C SUPPORT INTERCOSTAL FOR LWR CENTER LINE FAIRING CORRODED AT BS 740 BETWEEN S28L AND S28R. INTERCOSTAL REPLACED WITH FABRICATED INTERCOSTAL IAW SRM 51-30-02 AND 51-20-2.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, VENTRAL STAIRS TORQUE BOX HORIZONTAL WEB PUNCTURED AFT OF BS 1243 RIGHT O/B END. REPAIRED AREA IAW SRM 51-40-02.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, SUPPORT CLIP FOUND CRACKED AT BS 580 BETWEEN S2L AND S3L. SUPPORT CLIP FABRICATED AND INSTALLED IAW 51-20-01 AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, AFT CARGO FLOOR SUPPORT RAIL AT BS 1035 RBL 4 APPROX, CORRODED. SECTION OF FLOOR SUPPORT RAIL REPLACED IAW SRM 53-10-5 & DRAWING 65-19 388.

Part: ANGLE — CRACKED (TE FLAP) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, ANGLE CRACKED AT RT ELEPHANTS EAR. FABRICATED ANGLE IAW SRM 51-30-2, INSTALLED NEW ANGLE IAW SRM 51-20-01 FIG 7 AND BOEING DRG 65-26786.

Part: FLAP TRACK — CORRODED (NR 4 FLAP) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C, NR 4 FLAP TRACK, AFT PAD-B HAS CORROSION IN BORE HOLES F & G. REPAIR CARRIED OUT IAW AAAE EO 2004-061-003.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C, NR 6 L/E SLAT O/B UPSTOP HAS CRACK ON SURROUNDING SKIN. REPAIR CARRIED OUT IAW MM 27-81-11 & SRM 57-30-4 FIG 4.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, ON REMOVAL OF SKIN PANEL CORROSION FOUND ON LWR SKIN PANEL LAP JOINT S4R BETWEEN BS 615 & BS 540. REPAIR CARRIED OUT IAW AAAE 2004-061-006.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, SUPPORT WEB BENEATH STAND-BY PUMP CRACKED AT ACCESS HOLE FOR DRAIN PLUG. STOP DRILLED CRACK AND SUPPORT WEB REPAIRED IAW SRM 51-40-2.

Part: BRACKET — CRACKED (NR 7 SLAT) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C, NR 7 SLAT O/B TRACK TO SKIN ATTACH BRACKETS ARE CRACKED. NEW BRACKETS INSTALLED IAW SRM 51-30-02, OHM 57-51-61.

Part: STRINGER — WORN (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, STR WORN ON BS 1183 AFT SIDE AT WL 208 I/B OF SYS-A PRESSURE MODULE. REPAIR CARRIED OUT IAW AAAE EO 2004-061-004, UPS ENGINEERING FILE NR 727-53-20150 & SRM 51-30-02.

Part: BRACKET — CRACKED (NR 5 SLAT STOP) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C, NR 5 SLAT, O/B UPSTOP BOLT RETAINING BRACKET IS CRACKED. BRACKET REMOVED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-30-01, BRACKET INSTALLED IAW SRM 51-30-1 & MM 20-80-01. STOP ADJUSTED TO WITHIN LIMITS IAW MM 27-81-11.

Part: FLAP TRACK — CORRODED (NR 4 FLAP) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, NR 4 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD-B. REPAIR CARRIED OUT IAW AAAE 2004-061-003.

Part: SKIN — CRACKED (NR 3 LE FLAP) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, NR 3 LEADING EDGE FLAP ANTI ICE SKIN IS CRACKED IN TWO AREAS, ALSO LOOSE RIVETS IN ANTI ICE SKIN. REPAIRED CRACKS IAW EO B727-5750-3082. REPLACED LOOSE RIVETS IAW SRM 51-30-2.

Part: STRUCTURE — CRACKED (NR 3 LE FLAP) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C, NR 3 LEADING EDGE FLAP, O/B BONDING WIRE ATTACH SCREW HOLE IS CRACKED. REPAIR CARRIED OUT IAW AAAE EO 2004-061-002, UPS ENGINEERING FILE NR 727-57-20113.

Part: SKIN — CORRODED (BS - BS) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, SUSPECT CORROSION AT BS 640-680 S1L TO S4L. ON INVESTIGATION CORROSION FOUND INTERNALLY ON SKIN PANEL AT BS 680 - 660 S4R, BS 620 S2L - 1L, BS 540 - 530 S2L REPAIR CARRIED OUT IAW SRM 51-30-2, 33-30-01 DRAWING 65-42370, AAAE EO 2004-61-006, UPS ENGINEERING FILE B727-5330-20718-A.

Part: ATTACH FITTING — CRACKED (RT IB FLAP G/B) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C SUSPECT CRACK ON OFFSET GEARBOX AT ATTACHMENT LUG ON RIGHT I/B FLAPS. HFEC CONFIRMED CRACK ON LUG. OFFSET GEARBOX REPLACED IAW MM 27-51-60 PARA 1-3.

Part: SKIN — WORN (RUDDER) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C, SKIN ON LWR RUDDER L/E WORN IN SEVERAL PLACES ON LT & RT SIDES. LWR RUDDER REPLACED IAW MM 27-20-01, 27-20-11 & SRM 51-30-02.

Part: SKIN — CRACKED (NR 6 LE SLAT) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C NR 6 L/E SLAT UPPER SKIN HAS SCRATCHES 2 OF WHICH ARE SUSPECT CRACKS NR 1 IS 3 INCHES O/B OF ACTUATOR, NR 2 IS 4 INCHES I/B OF ACTUATOR AND FROM PREVIOUS REPAIR CUTOUT. HFEC INSP CARRIED OUT ON THE ABOVE AREAS IAW B727 NDTM PT6 51-00-00 FIG 4. TWO CRACKS CONFIRMED AND ENDS MARKED. SLAT REPLACED IAW MM 27-81-11, 27-81-32 & SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, CRACK IN SKIN FOUND AT WING SCANNING LIGHT CUTOUT LT BS 675. REPAIR CARRIED OUT IAW AAAE EO 2004-061-001, UPS ENGINEERING FILE NR 727-53-20149 & SRM 53-30-3 & MM 33-41-02.

Part: SKIN — DELAMINATED (NR 2 SPOILER) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE: C, NR 2 SPOILER HAS DELAMINATION ON UPPER & LWR SURFACES. REPAIRED IAW SRM 51-40-5.

Part: SKIN — DAMAGED · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C PULLED RIVETS & BULGE ON RT STAB LWR SKIN APPROX 4 INCHES FROM REAR SPAR AND AT STAB STA 66 APPROX. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-10-3 FIG 3, 51-10-1 & MM 51-20 -01 & 27-30-51.

Part: YOKE — CRACKED (TAIL SKID) · airframe 62,960 hrs · 48,304 cycles

INSPECTION TYPE:C TAIL SKID UNIT FOUND CRACKED. TAIL SKID YOKE ASSY REPLACED IAW MM 32-71-41 & 31-71-22 FUNCTION CHECK.

Part: LIGHT — INOPERATIVE (FWD ENTRY)

FWD ENTRY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,469 hrs · 47,867 cycles

INSPECTION TYPE:C MAIN ENTRY DOOR FLOORBEAM T ANGLE SUPPORT SHOWS EVIDENCE OF CORROSION BETWEEN FS 312 AND FS 344. REMOVED AND REPLACED T ANGLE SUPPORT.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 62,469 hrs · 47,867 cycles

INSPECTION TYPE:C MAIN ENTRY DOOR FLOOR PANEL CORRODED BETWEEN FS 312 AND 344. REMOVED AND REPLACED FLOOR PANEL.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PFLT COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY AND CLEANED CONNECTOR TO LIGHT ASSY MOUNTING PLATE, OPS CHECK GOOD PER MM 33-50-67.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A AIR TURNBACK DUE TO SMOKE IN COCKPIT SMELLED SMOKE CLIMBING THROUGH 4000 FT THEN WENT AWAY UNTIL CREW SAW SMOKE AND SMELLED HEAVY ELECTRICAL SMELL AFTER BLOCK IN WITH EXTERNAL POWER CONNECTED. INSPECTED BEHIND PANELS OF F/E PANEL. REMOVED AND REPLACED VOLTAGE REGULATOR, GENERATOR CONTROL PANEL, PERFORMED ADJ TEST PER MM 24-20-00, PERFORMED HIGH POWER RUN. NO SMOKE, NO FAULTS.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT 243.7 TO LOWER CHORD. REMOVED LT SIDE WALL AND FASTENERS AT BS 243.7 IAW SRM 51-30-2. CUT OUT CRACK SECTION PER SRM 51-40-2 FIG 1. APPROX SIZE 7 X 1 INCH, INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT BS 277.5 TO LOWER CHORD. REMOVED NOSE WHEEL WELL ACCESS PANEL LT AFT TO GAIN ACCESS AND REMOVED FASTENERS LT SIDE AT 277.5 S PER B727 SRM 51-30-2. CUT OUT CRACK SECTION AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-4-2 FIG 1.

Part: BEAM — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A VERTICAL BEAM AT BS 1183 CRACKED LBL 26.83 WL 260 APPROX 2 INCH LONG FROM LIGHTENING HOLE. REPAIRED CRACK BY STOP DRILLING. HFEC AREA INSTALLED REPAIR PER B727.

Part: BULKHEAD — CRACKED (FUSELAGE)

INSPECTION TYPE:C PRESSURE BULKHEAD CRACKED RBL 18 AT HAND PUMP LOWER OUTBOARD MOUNT BRACKET. CUT OUT CRACKED AREA AT BS 1183 RBL 18 AS PER SRM 51-10-1. NDI NO CRACK FOUND, INSTALLED DOUBLER PER B727 SRM 53-10-9.

Part: DRAG BRACE — CRACKED (NLG)

INSPECTION TYPE:N/A DRAG BRACE SUPPORT BEAM IS CRACKED AT LT AFT CORNER CONFIRMED BY HFEC. STOP DRILLED CRACK PER SRM HFEC INSPECTED AREA FOUND NO CRACKS BEYOND AREA. FOUND CRACK TO BE BEYOND REPAIRABLE LIMITS PER UPS EO B727 -5310-0943. REMOVED AND REPLACED NOSE GEAR DRAG BRACE SUPPORT BEAM AND GEAR ANGLES PER EO AND BOEING DRAWING 65C15725. PERFORMED LEAK CHECK PER B727 MM 21-31-00, NO LEAKS FOUND.

Part: SWITCH — MALFUNCTIONED (LANDING GEAR)

INSPECTION TYPE:IN, RIGHT LDG GEAR LIGHT NOT ILLUMINATED WHILE TAXIING IN RIGHT LDG GEAR LIGHT EXTINGUISHED STOPPED AIRCRAFT WHILE MAINTENANCE PINNED GEAR. LIGHT ILLUMINATED AGAIN BRIEFLY THEN WENT OUT AGAIN. REMOVED AND REPLACED RIGHT LANDING GEAR DOWN AND LOCKED SWITCH AND CANNON PLUG, OPS CKS REQUIRED SEE LOG PAGE 226825 ITEM 3.

Part: SLIDE — DEPLOYED (CABIN)

INSPECTION TYPE:N/A, ESCAPE SLIDE DEPLOYED. *S/D* DEFERRED ESCAPE SLIDE PER MEL 52-15 CONTROL NR M197975 PLACARD INSTALLED.

Part: JACKSCREW — SLIPPED (HORIZONTAL STAB)

STAB TRIM COASTS THREE REVOLUTIONS IN FLIGHT. REMOVED AND REINSTALL JACK SCREW ASSY PER MM 27-40-41 OP CHECKS GOOD .

Part: SEAT TRACK — BROKEN (BS 755)

INSPECTION TYPE:C, CABIN SEAT TRACK BS 755 AT BL 0 HAS BROKEN TANG. REPLACED SECTION OF CABIN SEAT TRACK AT BBL 0 FROM BS 750 TO BS 850 IAW WITH SRM 53-10-5.

Part: SEAT TRACK — BROKEN (BS 610)

CABIN SEAT TRACK LBL 60.0 BS610, ONE EACH SIDE EARS HALF BROKEN OFF. REPLACED DAMAGED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5. MATERIAL USED PART NUMBER BAC1520-1433.

Part: SEAT TRACK — BROKEN (BS 610)

INSPECTION TYPE:C, CABIN SEAT TRACK LBL 60.0 BS 610 ONE SIDE EAR HALF BROKEN OFF. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-5.

Part: FLOORBEAM — CORRODED (BS 600)

INSPECTION TYPE:C, APPROXIMATE FS 600 FLOORBEAM LBL 10 FORWARD LOWER CHORD SECTION HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR IN ACCORDANCE WITH AVITAS ENGINEERING REPAIR ORDER AVHM-101RO-1A AND UPS ENGINEERING FILE NR 727-53 -2229.

Part: FLOORBEAM — CORRODED (BS 600)

INSPECTION TYPE:C APPROXIMATE FS 600 FLOORBEAM RBL 18 FORWARD LOWER CHORD SECTION HAS CORROSION. REMOVED CORROSION, REPAIRED ANGLES IAW AVITAS ENGINEERING REPAIR ORDER NR AVHM-101RO-1A AND UPS ENGINEERING FILE NR 727-53-2229.

Part: FLOORBEAM — CRACKED (BS 870)

INSPECTION TYPE:C, CABIN FS 870 UPPER FLANGE CRACKED IN UPPER RADIUS WHERE IT CONNECTS TO VERTICAL WEB RBL 43-RBL 47 FLOORBEAM UPPER CHORD. REPAIRED IAW WITH AVITAS ENGINEERING REPAIR ORDER NR AVHM-100RO-1 AND UPS EO FILE NR 727-53-2224. REMOVED ASSOCIATED PARTS AND STOP DRILLED CRACK.

Part: STRINGER — CORRODED (BS 440)

INSPECTION TYPE:C, STRINGER 25 LT SPLICE CORRODED AT BS 440 BURNISHED AREA OUT OF LIMITS. REPLACED DAMAGED SECTION AS PER B727 SRM 51-30-2 AND 53-10-2.

Part: STRINGER — CORRODED (BS 440)

INSPECTION TYPE:C, STRINGER 25 LEFT SPLICE CORRODED AT BS440. REPLACED DAMAGED SECTION OF STRINGER 25 LEFT, BS440 IAW B727 SRM 53 -10-2.

Part: ANGLE — CRACKED (LE FLAP)

INSPECTION TYPE:C, NR 3 LEADING EDGE SLAT OUTBOARD TRACK ROLLER SUPPORT WEBS INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES CRACKED AT FRONT SPAR LOWER CHORD. REPLACED INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK ROLLER SUPPORT WEBS, 7075-T6, P/N 57-21207 IAW B727 SRM 57-10-6.

Part: ANGLE — CRACKED (LE FLAP)

INSPECTION TYPE:C, NR 2 LEADING EDGE SLAT INBOARD TRACK ROLLER SUPPORT WEBS INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES CRACKED AT FRONT SPAR LOWER CHORD. REPLACED ANGLES AT NR 2 LEADING EDGE SLAT INBOARD TRACK ROLLER SUPPORT WEB INBOARD AND OUTBOARD MATERIAL USED PART NUMBER AND10133-1403 IAW B727 SRM 51-30-2.

Part: RIB — CRACKED (LE FLAP)

INSPECTION TYPE:C, NR 3 LEADING EDGE SLAT ACTUATOR ROD END ATTACH BOLT OUTBOARD SUPPORT RIB CRACKED AT AFT LOWER CORNER. INSTALLED REPAIR AT OUTBOARD SUPPORT RIB FOR NR 3 LEADING EDGE SLAT ACTUATOR ROD END, MATERIAL USED 321.032. 5 BY 3 IAW B727 SRM 57-50-3.

Part: CARGO DOOR — CORROSION (MAIN CARGO)

INSPECTION TYPE:N/A, MAIN CARGO DOOR UPPER AFT STRUCTURE/STRAP HAS CORROSION.

Part: LIGHT — LOOSE (CABIN)

INFLIGHT EMERGENCY EXIT LIGHT CAME ON, TAPPED ON LEN'S COVER, LIGHT WENT OUT. FOUND RIGHT MOUNT LATCH UNSECURED, RESECURED COCKPIT EMERGENCY LIGHT LATCH, LIGHT OPS CHECK GOOD.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE-C, RT WING O/B AILERON ACTUATOR ROD END FITTING IS CORRODED. REMOVED CORROSION FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-2.

Part: HINGE — CORRODED (LT AILERON)

INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER I/B FWD HINGE HALF CORRODED. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.

Part: HINGE — CORRODED (LT AILERON)

INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER O/B FWD HINGE HALF CORRODED. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.

Part: HINGE — CORRODED (LT AILERON)

INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND O/B FWD HINGE HALF CORRODED, LT WING O/B AILERON. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.

Part: WEB — CORRODED (BS 1147)

INSPECTION TYPE-C, CORROSION ON SHEAR WEB BS 1147, LBL 50, WL 208. DAMAGED CLEAN-UP BEYOND ALLOWABLE LIMITS PER SRM 51-10-06. AREA SIZE TO BE .013 X 2.5 X 2.5. DAMAGED AREA REMOVED AND WEB WAS REPAIRED PER SRM 51-40-2.

Part: WEB — CORRODED (BS 1174)

INSPECTION TYPE:C, CORROSION ON SHEAR WEB BS 1174, RBL 45, WL 208. REPAIRED PER SRM 51-40-2.

Part: WEB — CRACKED (BS 1225)

INSPECTION TYPE:C, AFT AIR STAIR AREA, 2 CRACKS IN LIGHTENING HOLE IN TORQUE BOX RT SIDE STATION 1225. REPAIRED PER SRM 51-40-2.

Part: SUPPORT — CORRODED (BS 520-540)

INSPECTION TYPE:C, CORROSION ON FLOOR SUPPORT (C53-113-01.07-01) AT FWD CARGO DOOR THRESHOLD BS 520-540 RBL 21.5 WL 156. REPLACED FLOOR SUPPORT BS 510 TO BS 600 PER 727 SRM 51-30-5 AND 53-10-1.

Part: FLOORBEAM — CORRODED (BS 267)

INSPECTION TYPE:C, CORROSION ON FLOORBEAM UPPER CHORD AT BS 267, LBL 2, COCKPIT FLOOR. CORROSION CLEAN UP WENT BEYOND ACCEPTABLE LIMITS. REMOVED AND REPLACED FLOORBEAM UPPER CHORD.

Part: BULKHEAD — CRACKED (BS 870)

INSPECTION TYPE:C, TRANSFERRED FROM LP 266457 ITEM 3 CRACK IN PRESSURE BULKHEAD LEFT WHEEL WELL STA 870. REMOVED DAMAGED AREA AT 870 BULKHEAD LT WHEEL WELL. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS PER SRM 53-10-9 PGS 10-11 AND SRM 51-40-2 PGS 1-6.

Part: FRAME — CORRODED (BS 420)

INSPECTION TYPE:C CORROSION ON SUPPORTING FRAME AT BS 420 UNDER BATTERY TRAY. TRAY ALSO HAS CORROSION AROUND MOUNTING LUG BRACKETS. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER ON FRAME PER SRM 53-10-1. TRAY AND LUG BRACKETS WERE WITHIN LIMITS, ALL PARTS REINSTALLED PER SRM 51-30-2.

Part: SHEER TIE — CORRODED (BS 306)

INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON SHEER TIE IN TRUNNION TORQUE BOX AT BS 306 RBL 18 WL 148. REMOVED CORROSION, OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-4. INSTALLED LEVELING COMPOUND IAW SRM 51-20-4.

Part: WEB — CORRODED (BS 1225)

INSPECTION TYPE:C, AFT AIR STAIR AREA CRACK IN LIGHTENING HOLE IN TORQUE BOX WEB LT SIDE AT STA 1225. STOP DRILLED AND REPAIRED PER SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE:C, FLOORBEAM UPPER CHORD CORRODED BS 344 RBL 15 WL 208. CORROSION CLEANUP BEYOND ACCEPTABLE LIMITS. REPAIRED FLOORBEAM PER SRM 53-10-8 FIGURE 9.

Part: SEAT TRACK — CRACKED (BS 760)

INSPECTION TYPE:C SEAT TRACK AT STA 760 LBL 65 WL 208 CRACKED AT O/B FLANGE. REPLACED TRACK IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1166)

INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BS 1166, LBL 20, WHERE IT ATTACHES TO AFT BULKHEAD OF AFT CARGO BAY. REMOVED CORROSION ON SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 53-10-05.

Part: WEB — CORRODED (FUSELAGE)

INSPECTION TYPE-C, CORROSION (C53-132-02-01-01) 870.5 WEB RBL WL 153 AROUND CANNON PLUG CONNECTORS (MARKED). REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS PER SRM 53-10-9.

Part: FITTING — CORRODED (ELEVATOR)

INSPECTION TYPE:C, CORROSION (C55-391-30.02-01) ON ELEVATOR CENTERING UNIT SPRING FWD ATTACH FITTING AROUND FASTENER HOLES. FITITNG OUT OF LIMITS, REMOVED OLD FITTING, INSTALLED NEW FITTING PER MM 27-30-11 AND SRM 51-30-02.

Part: RIB — CORRODED (NR 1 LE FLAP)

INSPECTION TYPE-C, CORROSION (C57-562-01.00-01) LT WING NR 1 K-FLAP CORRODED AROUND BONDING JUMPER BOLT HOLE ON BOTH SIDES OF RIB. CORROSION OUT OF LIMITS. REMOVED AND INSTALLED NEW K-FLAP. WORK DONE IAW SRM 57-50-1, MM 27-81-01.

Part: BULKHEAD — CRACKED (BS 870)

INSPECTION TYPE:N/A, 2 X 3 INCH CRACK IN PRESSURE BULKHEAD STA 870, LEFT WHEEL WELL FACING FORWARD. *S/D* REMOVED 4 X 8 INCH SECTION IAW SRM 53-10-1, FABRICATED REPAIR IAW 53-10-9. INSTALLED DOUBLERS, FILLERS AND STRAP IAW 53-10-9.

Part: SWITCH — INTERMITTENT (RT MLG DOOR)

RIGHT MAIN GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION COMPLETE. CYCLED GEAR ONCE AND LIGHT WENT OUT. FOUND RT MLG DOOR WARNING SWITCH TO BE INTERMITTENT. REMOVED AND REPLACED RT MLG DOOR SWITCH PER MM-32-62-11. ADJ/TEST PERFORMED PER MM 32-62-11 OPS CKS GOOD.

Part: BATTERIES — DISCHARGED (CABIN)

EMER EXIT LIGHT BY MAIN CABIN DOOR INOP. REMOVED AND REPLACED EMER EXIT BATTERIES AT MAIN CABIN DOOR, OPS CHKS GOOD.

Part: CABLE — BROKEN (RT TE MIDFLAP)

FOL UNEVENTFUL 340 KT CLIMB, .80M/330 IAS SET. AFTER APROX 10 MIN, MOD VIBS STARTED AND WERE AIRSPEED. A/S REDUCED 263 KTS BEFORE VIBS ABATED. FLR COMPLIED BELOW 260 KTS. FOUND CABLE BROKEN IN MID FLAP TO AFT FLAP ASSY RT INBD T/E FLAP SEE LOG PAGE 267071 ITEM 1 FOR REPAIR.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, COCKPIT AND ENTRY DOOR EMERGENCY EXIT LIGHTS HAVE DEAD BATTERIES. REPLACED COCKPIT AND ENTRY DOOR EMERGENCY EXIT LIGHTS IAW 33-50-01, OPS CHECKED GOOD.

Part: PANEL — CRACKED (LT WING)

INSPECTION TYPE-N/A, SMALL PANEL CRACKED ON BOTTOM LEFT WING FWD OF LEFT GEAR STRUT WELL EO NR B727-5720-9615-B ASSIGNED FOR INTERIM REPAIR OF SPEED TAPE OVER AREA DMI OPENED PER EO PERM. REPAIR DUE BY 8/16/97.

Part: ACCESSORY UNIT — MALFUNCTIONED (NLG)

ON GEAR EXTENSION, THE NOSE GEAR DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. RECYCLED GEAR AND CHECKED LIGHTS AND C/B'S. THE PROBLEM STILL EXISTS. ACCOMPLISHED PROCEDURES AND CONFIRMED NOSE WHEEL RED STRIPES WERE ALIGNED AND LANDED. DID NOTICE ACRID SMELL WITH GEAR EXTENSION. REPLACED LANDING GEAR ANNUNCIATOR PANEL AND LANDING GEAR ACCESSORY UNIT PER MM 32-09-11, OPS CK OK.

Part: ANGLE — CORRODED (BS 1766)

INSPECTION TYPE-D, LT FLOOR SUPPORT ANGLE TO AFT BLKD IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED REPLACEMENT ANGLE AND INSTALLED IAW SRM 53-7-1 AND SRM 51-1-20.

Part: CHANNEL — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 CENTER CHANNEL IS CORRODED. REMOVED AND REPLACED CHANNEL NR 65-22551-7 IAW BAC DWG 65-22551 AND UPS EO B727-5530-4601-B.

Part: FRAME — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT LWR FRAME CHORD RBL 24 WL 220 STA 1342 IS CORRODED. REMOVED AND REPLACED LWR FRAME CHORD NR 65-17508-224 IAW UPS EO 727-5530-4601-B AND BAC DWG 65-17508.

Part: FORGING — CRACKED (VERT STAB)

INSPECTION TYPE C-HFEC INSP, DET CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT FIRST HOLE AFT OF STA 1233 TOP ROW OF FASTENERS. CRACK IS .5 INCH LONG RUNS AFT OF HOLE. STOP DRILLED CRACK, REPAIRED VERT STAB CRACK PER DRAWING 65-62346 AND SRM 51-30-2.

Part: FORGING — CRACKED (VERT STAB)

INSPECTION TYPE C-NFEC, DET A CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT 1ST HOLE OF STA 1233 BOTTOM ROW OF FASTENERS. CRACK IS 1 INCH LONG AND RUNS A FT OF HOLE. STOP DRILLED CRACK, REPAIRED PER DRAWING 65-62346 AND SRM 51-30-2.

Part: RIB — CRACKED (FS 1367 LT)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT RIB CRACKD AT FS 1367 BL 22.5. REMOVED DAMAGED AREA PER SRM 51-40-3, FAB AND INSTALLED REPAIR ANGLE PER SRM 51-40-3.

Part: SKIN — CORRODED (WS 870)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING NR 5 SLAT CRACK GOING PAST DRILL HOLE AT BOTTOM OF SLAT. REMOVED DAMAGED SECTION SKIN PER SRM 57-30-3. FAB AND INSTALLED REPAIR PARTS PER SRM 57-50-3 FIG 1.

Part: RIB — CRACKED (FS 1367 RT)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT RIB CRACKED AT FS 1367 BL 22.5. REMOVED DAMAGED AREA PER SRM 51-40-3, FAB AND INSTALLED REPAIR ANGLE PER SRM 51-40-3.

Part: FITTING — CORRODED (BS 870)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FITTING AT RT WHEEL WELL STA 870 HAS HEAVY CORROSION ON LWR END. REMOVED CORROSION IAW SRM 53-10-9 FIG NR 6 HFEC INSP PER B727NTM PT 6 51-00-00 FIG 23, DETECTED NO CRACKS AND REPAIRED IAW SRM 53-10-9.

Part: FRAME — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT LWR FRAME CHORD LBL 24 WL 220 STA 1342 IS CORRODED. REMOVED AND REPLACED FRAME CHORD IAW SRM 51-17508 SRM 51-30-2.

Part: TEE CHORD — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT O/B CHORD AT FS 1342 RBL 30 WL 250 IAW BAC 65-19532 DWG AND UPS EO B727-5530-4601 B.

Part: TEE CHORD — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT O/B CHORD FS 1342 LBL 30 WL 250 IS CORRODED. REMOVED AND REPLACED O/B CHORD IAW BAC 65-19532 AND UPS EO B727-5530-4601 B.

Part: TEE CHORD — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 WL 270 UPPER T-CHORD IS CORRODED. REMOVED AND REPLACED T-CHORD 65-17508-2 IAW 51-30-2, 51-10-1 AND BAC DWG 65-17508.

Part: CHORD — CRACKED (VERT FIN)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FIN STA 13.74 CHORD FOUND TO BE CRACKED. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: SPAR SKIN — CORRODED (FS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 LT INTERSPAR SKIN IS CORRODED BEYOND LIMITS. CUTOUT DAMAGED AREA, FAB AND INSTALLED REPAIR PARTS IAW BAC DRWG 65C29055.

Part: SPAR SKIN — CORRODED (FS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 RT INTERSPAR SKIN IS CORRODED BEYOND LIMITS AT TERMINAL FITTING. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PARTS IAW BAC DRWG 65C29055 AND SRM 51-30-2.

Part: STIFFENER — CORROSION (FS 351)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 351 STA 19L, FRAME TEE STIFFENER HAS HEAVY CORROSION. REMOVED AND FABRICATED AND INSTALLED FRAME TEE STIFFENER AT FS 351, STR 19L PER SRM 51-10-1 AND 51-30-2.

Part: SPAR WEB — CRACKED (FS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 WL 260 VERT FIN SPAR WEB IS CRACKED. CUT OUT DAMAGED CENTER WEB, FABRICATED REPLACEMENT SECTION AND REPAIRED PER SRM 55-30-6.

Part: SHEAR WEB — CORRODED (FS 1185)

INSPECTION TYPE: C. STA 1185, LBL 65 SHEAR WEB CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA IAW SRM 51-40-2 AND FABRICATED AND INSTALLED REPAIR DOUBLER IAW 51-40-2 AND 51-30-2.

Part: ANGLE — CRACKED (FS 1345)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT SKIN SUPPORT ANGLE IS CRACKED AT FS 1345 AND FIN STA 22.5. REMOVED DAMAGED SECTION IAW SRM 51-40-3, FAB AND INSTALLED REPAIR IAW SRM 51-40-3.

Part: SKIN — CORRODED (BS 360)

INSPECTION TYPE: C. LFEC INSPECTION REVEALED MATERIAL LOSS OF GREATER THAN 10 PERCENT, BUT LESS THAN 20 PERCENT ON AFT SIDE BS 360, BETWEEN STR 25L AND STR 26L. CUT OUT DAMAGED AREA AT AFT STA 360 BETWEEN STR 25L AND STR 26L. REPAIRED SKIN PER DRAWING NR 69-62161 AND SRM 51-30-2 AND EO B727-5310-1371.

Part: ANGLE — CRACKED (FS 1345)

INSPECTION TYPE: C. LEFT SKIN SUPPORT ANGLE IS CRACKED AT FS 1345 AND FIN STA 22.5. REMOVED DAMAGED AREA IAW SRM 51-40-3 AND FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3.

Part: STRINGER — CORROSION (BS 300)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 300 AT STR 23R HAS CORROSION AT FRAME ATTACH POINT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2, 53-10-3 AND 51-30-2.

Part: FRAME — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT FRAME CHORD AT STA 1342 RBL 20 WL 238 IS CORRODED. REPLACED LT I/B CHORD PER SRM 51-10-1.

Part: FRAME — CORRODED (BS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRAME CHORD AT STA 1342 RBL 20 WL 238 IS CORRODED. REPLACED RT I/B CHORD PER SRM 51-10-1.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 RT CHANNEL WL 247 RBL 18 IS CORRODED AFT SIDE OF 1342 FRAME. REMOVED AND REPLACED CHANNEL IAW BAC DWG 65-93155 B727-5530-4601 AND SRM 51-30-2.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 LT CHANNEL WL 247 LBL 18 IS CORRODED AFT SIDE OF 1342 FRAME. REMOVED AND REPLACED CHANNEL IAW BAC DWG 65-93155 B727-5530-4601 AND SRM 51-30-2.

Part: FITTING — CRACKED (NR 7 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 7 SPOILER I/B HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-10-1 AND 51-30-2.

Part: FRAME — CRACKED (BS 351)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 351 LT SIDE 2 INCHES AFT OF FWD AIR STAIR CUTOUT AT STR 18L, FRAME HAS LARGE AREA OF CORROSION AND LARGE CRACK. REMOVED DAMAGED AREA PER SRM 51-40-2, FABRICATED PARTS AND INSTALLED PER SRM 51-40-2. INSTALLED ATTACHING PARTS PER SRM 51-30-2.

Part: WEB — CRACKED (BS 279)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOG HOUSE TUNNEL AREA RT SIDE APPROX STA 279, WALL OF NOSE W/W CUTOUT HAS 4 INCH CRACK IN WEB. REMOVED DAMAGED SECTION PER SRM 51-40-2 AND FAB DOUBLER AND FILLER AND INSTALLLED PER SRM 51-40-2.

Part: FLOOR BEAM — CORROSION (FS 312)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 312, LBL 26 FLOOR BEAM UPPER FLANGE AFT BOTTOM SIDE FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED PER SRM 53-10-8, FIG 7.

Part: SKIN — CRACKED (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON LOWER FUEL CELL SKIN AT STA 740, RBL 1-15. REPAIRED IAW E.O. B727-5710-7079A.

Part: SPAR CHORD — CORRODED (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER FRONT SPAR CHORD AT STA. 740, WL 166.5, BL 0. REPLACED CHORD IAW E.O. B727-5710-7078A.

Part: SKIN — CORRODED (NR 6 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND RT WING NR 6 K-FLAP BULLNOSE O/B HINGE UPPER SURFACE OF UPPER ATTACH POINTS HAVE CORROSION. INSTALLED FABRICATED PARTS IAW SRM 57-50-1, 51-10-6, 51-10-1, 51-20-04.

Part: TE WEDGE — DELAMINATED (RT TE MID FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B MID FLAP T/E WEDGE ON O/B CORNER. REPAIRED IAW SRM 51-40-6.

Part: WEB — CORRODED (FS 1170)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR WEB STA 1170, RBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-40-2, 51-30-8, 51-10-2, 51-30-2, M/M 51-20-151.

Part: SEAT TRACK — CORRODED (BS 697-703)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK WELL B.S. 697-703, LBL 65, WL 208. INSTALLED NEW TRACK STA. 620-740 IAW SRM 53-10-1, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1130-1135)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK WELL AND TABS B.S. 1130-1135, RBL 45, WL 208. REPLACED TRACK IAW SRM 53-10-5, 53-10-2, 51-30-2, M/M 51-20-151.

Part: TE WEDGE — DELAMINATED (RT TE MID FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B MID FLAP T/E WEDGE 27 INCHES FROM I/B END. REPAIRED IAW SRM 51-40-6.

Part: TE WEDGE — DELAMINATED (RT TE MID FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B MID FLAP T/E WEDGE 7 INCHES FROM O/B END ON LOWER SURFACE. REPAIRED IAW SRM 51-40-6.

Part: CHORD — CORRODED (FS 294-350)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD B.S. 294-350, LBL 15, WL 169. REPLACED IAW SRM 51-30-5, 51-30-2.

Part: TAB — DELAMINATION (RT AILERON)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B AILERON TAB. REPAIRED IAW SRM 51-40-6.

Part: SKIN — CRACKED (FS 259.5-272)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS AROUND FASTENERS (HIGH FREQUENCY EDDY CURRENT INSPECTION) AT B.S. 259.5 TO 272, STR 9R, WINDSHIELD UPPER SILL. REPAIRED IAW SRM 51-30-2, 53-30-3.

Part: SKIN — CORROSION (BS 850-870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FUEL CELL SKIN B.S. 850-870, RBL 45-65. REPAIRED IAW E.O. 727-57-1385.

Part: RIB — CRACKED (RT ELEVATOR)

WHILE IN C-CHECK, MAINTENANCE FOUND RT ELEVATOR SUPPORT RIB AT STA 99.79 IS CRACKED. REPLACED RIB IAW SRM 51-30-2.

Part: K-FLAP — CORRODED (NR 1 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 K-FLAP. REPLACED IAW M/M 27-81-1.

Part: STIFFENER — CORRODED (BS 301)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER B.S. 301, LBL 12 TO RBL 12 WL 180. REPLACED STIFFENER IAW SRM 53-10-1, 51-10-1, 51-30-2.

Part: STIFFENER — CORRODED (BS 308)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER B.S. 308, LBL 12 TO RBL 12 WL 180. REPLACED STIFFENER IAW SRM 53-10-1, 51-10-1.

Part: SEAT TRACK — CORRODED (BS 580)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN SEAT TRACK B.S. 580, RBL 65, WL 208. REPLACED TRACK IAW SRM 51-30-2.

Part: WEB — CORRODED (FS 259.5)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AROUND LOCKBOLT STA 259.5, LBL 21, WL 192.5. REPAIRED IAW SRM 51-40-2, 51-10-2, 51-30-2, 53-10-2.

Part: EXPANSION LINK — CORROSION (BS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSEAGE TO WING CENTER SECTION EXPANSION LINKS (LT AND RT) AT B.S. 740, RBL 13, LBL 13, WL 150.

Part: K-FLAP — CORROSION (NR 3 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP. REPLACED IAW M/M 27-81-1.

Part: SKIN — CORROSION (BS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER FUEL CELL SKIN STA. 740, LBL 39 AND 45. REPAIRED IAW E.O. 727-5710-7079A.

Part: ANGLE — CORRODED (BS 280)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ANGLE AT B.S. 280, WL 177 NOSE WHEELWELL. INSTALLED FABRICATED PARTS IAW SRM 53-10-1, 51-20-1, 53-30-2.

Part: HAT CHANNEL — CORRODED (FS 1145-1148)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON HAT CHANNEL STA 1145-1148, RBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-10-2, 51-20-4, 51-30-6, 51-10-1.

Part: TE WEDGE — DELAMINATED (RT TE MID FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B MID FLAP T/E WEDGE 36 INCHES FROM I/B END. REPAIRED IAW SRM 51-40-6.

Part: WEB — CORRODED (BS 294-350)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT B.S. 294-350, LBL 14, WL 180-160. INSTALLED FABRICATED PARTS IAW E.O 727-53-1612.

Part: K-FLAP — CORRODED (NR 2 LE FLAP)

WHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP. REPLACED IAW M/M 27-81-1.

Part: TAB — DELAMINATION (RT AILERON)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B AILERON TAB. REPAIRED IAW SRM 51-40-6.

Part: SPAR CHORD — CORROSION (BS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SPAR CHORD B.S. 870, RBL 35, WL 188. REPAIRED IAW E.O. B727-5710-7063A.

Part: SKIN — CORROSION (BS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FUEL SKIN AT B.S. 870, RBL 32-39, WL 188. REPAIRED IAW E.O. 727-57-1386.

Part: SEAT TRACK — CORRODED (FS 595-600)

WHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON SEAT TRACK TABS I/B AND O/B B.S. 595 TO 600, LBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 53-10-1, 53-10-5.

Part: UPLOCK SWITCH — MALFUNCTION (NLG)

PILOT REPORTED WHEN HE EXTENDED THE GEAR THE FIRST TIME, THE TWO MAIN GEAR INDICATED DOWN WITH GREEN LIGHTS, BUT NOSE DIDN'T. RECYCLED THE GEAR AND SAME THING HAPPENED. THE NOSE GEAR VISUAL HOLE CONFIRMED NOSE GEAR DOWN (STRIPES ALIGNED). WHEN NOSE GEAR TOUCHED DOWN ON LANDING, NOSE GEAR GREEN LIGHT CAME ON. DETERMINED THAT THE NOSE GEAR LOCK SWITCH BAD. WHILE TAPPING ON SWITCH, LIGHT WOULD FLICKER. REMOVED AND REPLACED SWITCH PER 32-64-01, GROUND TEST GOOD.

Part: CONNECTOR — DIRTY (NLG)

PILOT REPORTED ON APPROACH INTO ELP WHEN GEAR WAS EXTENDED, THE GREEN NOSE GEAR DOWN AND LOCK LIGHT WAS BEARLY VISIBLE. FLIGHT TEST PERFORMED, OPS GOOD. CYCLED L/G AFTER GO AROUND ONCE, GEAR CYCLED. LIGHT DIM THEN AFTER TEN SECONDS, FULL BRIGHT. A/C LANDED WITHOUT INCIDENT. INSPECTED NLG, FOUND DOWNLOCK SWITCHES CANNON PLUGS DIRTY. CLEANED CONNECTORS AND INSURE PROPER BULBS INSTALLED IN ANNUNCIATOR PANEL. N/G LIGHTS OPERATE NORMAL.

Part: EEL — INOP (FLIGHT DECK)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHT INOP. INSTALLED SERVICEABLE EMERGENCY LIGHT ASSY. OPS CHECK GOOD.