N937UP

Part: OVERHEAT LOOP — FALSE INDICATION (NR 1 ENGINE)

NR 1 ENGINE 1 STRUT OVERHEAD ILLUMINATED IN FLIGHT. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 1 ENG OVERHEAT DETECT LOOPS PER MM 26-14-12. OPS CHECKS GOOD PER MM 26-14-00. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTION BOX FOR PRECAUTION PER MM 26-14-00.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 63,770 hrs · 48,317 cycles

INSPECTION TYPE: C, RT WING L/E CAVITY SUSPECT CRACK ON RIB ABOVE NR 5 L/E FLAP ACTUATOR ON INVESTIGATION T-SECTION FOUND CRACKED & CORRODED. REPLACED T-SECTION IAW SRM 51-30-02 & DRAWING NR 656268.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,770 hrs · 48,317 cycles

INSPECTION TYPE:C, CRACK INDICATION FOUND AT BS 910 AFT SIDE OF REINFORCING BEAD RBL 52. REPAIRED IAW EO B727-5310-0088 APPDX C.

Part: SHUTOFF VALVE — DEFECTIVE (NR 2 ENGINE) · airframe 63,770 hrs · 48,317 cycles

INSPECTION TYPE: C, DURING TEST OF ENG NR 2 HYD SHUTOFF VALVE FAILED TO OPERATE CORRECTLY. TROUBLESHOOTING CARRIED OUT IAW WDM 29-11-01 AND ENG NR 2, SYS A HYD SHUT OFF VALVE FOUND TO BE DEFECTIVE. INSTALLED REPLACEMENT HYD SHUT OFF VALVE IAW MM 29-11-21 REF NRC 681341 FOR CANNON PLUG INST & TEST. LEAK CHECK CARRIED OUT IAW MM 29-11-21 STEP 5. NO LEAKS FOUND AND REMAINING STEPS COMPLETED IAW MM 29-11-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,770 hrs · 48,317 cycles

INSPECTION TYPE: C, LT BS 740 FITTING CRACKED BEYOND LIMITS. LT BS 740 FITTING REPLACED IAW UPS EO B727-5310-7477-C.

Part: RELAY — INOPERATIVE (E/E BAY)

DURING LANDING ROLLOUT & T/R APPLICATION A PWR LOSS TO THE FLT & ENGINE INSTRUMENTS WAS NOTED. THE COCKPIT WENT MOMENTARILY DARK. APPLIED T/R DURING TAXI IN AND NOTED KW NR 1 JUMPED TO 35 WHILE THE KWNR 2 DROPPED TO ZERO. REMOVED AND REPLACED R58S POWER RELAY AND REPLACED R112 ESSENTIAL POWER RELAY. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT.

Part: SKIN — CRACKED (T/E FLAP)

INSPECTION TYPE:N/A RIGHT INBD AFT FLAP HAS DAMAGE (DENT WITH CRACKED SKIN) JUST OUTBOARD OF INBD CANOE FAIRING. REMOVED DAMAGED SKIN AND CORE, REMOVED INBD AFT FLAP SECTION, REPAIRED FLAP IAW SRM 51-40-20.

Part: LIGHT — NOT SEATED (CABIN)

EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOPERATIVE. RESEATED FWD ENTRY DOOR EMERGENCY EXIT LIGHT OPERATIONAL CKS GOOD.

Part: FLAP — DELAMINATED (RT WING)

INSPECTION TYPE:W/E RIGHT WING I/B T/E MID-FLAP HAS 3 X 15 INCH DELAMINATION. REMOVED AND REPLACED FLAP IAW MM27-51-03 AND TASK CARD 1 259

Part: CONTROL CABLE — LACK OF LUBE (AILERON)

INSPECTION TYPE: IN, AILERON BINDING (REPEAT W/U). TROUBLESHOT PER MM 27-10-00 PAGE 111 INSP CABLE AA & AB NO DEFECT NOTED LUB CABLE, OPS CHECK GOOD.

Part: FITTING — BROKEN (RT AILERON) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, AFTER RIGHT O/B AILERON TAB REMOVAL FOUND O/B FITTING FOR TAB HINGE B-RING BROKEN. REPLACED FITTING IAW DRG 65-21766.

Part: BUSHING — CRACKED (ENGINE MOUNTS) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, ENGINE NR 2 MOUNTS LEFT ADAPTER FITTING UPPER LUG LWR BUSH FOUND CRACKED ON FLANGE. BUSHING REPLACED IAW MM 20-10-07 & MM 21-21-12.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, DURING SKIN RETIFACTION WORK AT BS 1180 STRINGER TIE END AT S5L WAS FOUND CORRODED. STRINGER TIE END REPLACED IAW DWG 65-19690 AND SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, INTERCOSTAL BETWEEN FLOORBEAM BS 294.5 TO BS 312R CRACKED RBL 46 APPR OX. STOP DRILLED CRACK ON INTERCOSTAL BETWEEN BS 294.5 & 312 RBL 46 APPROX IAW SRM 51-40-03, 51-10-01. HFEC C/O POST STOP DRILL IAW B727 NDTM PT6 51-00-00 FIG 4. CRACK CONTAINED WITHIN STOP DRILL HOLE. REPAIRED IAW SRM 51-40-03 FIG 1.

Part: SUPPORT BRACKET — CRACKED (MLG DOOR) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, RT GEAR MAIN DOOR AFT DOOR STOP LWR SUPPORT BRACKETS CRACKED. REMOVED SUPPORT BRACKETS IAW SRM 21-30-02. ON REMOVAL ATTACH FRAME I/B AND O/B LWR SECTIONS CRACKED. DAMAGED AREA REMOVED IAW SRM 51-10-06. CRACKED AREA REPAIRED IAW SRM 51-20-01. DAMAGED BRACKETS REPLACED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, TO FACILITATE ACCESS TO FASTENERS IN AREA AT BS 1183 AND STR 4L REMOVAL OF STRINGER END IS REQD, ON REMOVAL OF STRINGER IT WAS FOUND TO BE CRACKED. REPAIR CARRIED IAW SRM 51-30-2 SRM 53-11-00 & MM 20-50-1.

Part: FRAME — CRACKED (RT MLG WW) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CRACK BS 910 FRAME RT W/WELL. REPAIRED CRACK AT BS 910 FRAME IAW EO B727-5310-1896B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, BS 930 FRAME IN LT WHEEL WELL HAS SUSPECT CRACKS BETWEEN FASTENER HOLES AT AFT FLANGE. REPAIR CARRIED OUT IAW SMRO EO 2000-041-005 UPS ENGINEERING FILE NO 727-53-2301.

Part: CASTING — CRACKED (RT MLG DOOR) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, RIGHT MAIN GEAR WING DOOR AFT HINGE CASTING CRACKED IN TWO PLACES. RT WING DOOR REPLACED IAW MM 32-12-11 AND ADJ/TESTED IAW 32-12-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION ON STR 24R AT BS 470. REPAIRED STR 24R AT BS 470 IAW SRM 53-10-3 FIG 1.

Part: FRAME — CRACKED (LT MLG WW) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, BS 930 FRAME IN LT WHEEL WELL HAS SUSPECT CRACKS BETWEEN THE FASTENER HOLES AT AFT FLANGE. CRACKS CONFIRMED. AREA REPAIRED IAW UPS EO B727-5310-2611 AND SMRO EO 2000-041-005, UPS ENG FILE NUMBER 727-53-2301.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION ON STR 21R AT BS 480. REPAIRED IAW SRM 53-10-3 FIG 1.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, AFT CARGO DOOR FWD FRAME BENEATH NR 1 STOP FITTING CRACKED. REPLACED LWR FORWARD FRAME ON AFT CARGO DOOR IAW SRM 51-30-2 AND DRAWING 65-18625.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, SUSPECT CRACK BS 950L AT FWD LUG OF SWING LINK ON 950 FRAME. HFEC INSPECTION C/O ON ABOVE LUG IAW B727 NDTM PT6 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REPAIR C/O PER SMRO EO 2000-041-004. UPS FILE 727-53-2296.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION ON LT AT BS 312 APPROX VERTICAL WEB OF TORQUE BOX. VERTICAL WEB FOUND TO BE CRACKED BEYOND LIMITS IAW SRM 51-10-10. REPLACED VERTICAL WEB 65-18415-49 IAW DRW 65-18415 AND SRM 51-30-3. TO AID WITH REPLACEMENT OF VERTICAL WEB 65-18415-49, CHORD ANGLE REMOVED AND REINSTALLED IAW DRW 65-18415 AND SRM 51-30-2.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, FWD CARGO DOOR NET SUPPORT BRACKET CRACKED AT AFT END. CRACK REPAIRED IAW SRM 51-40-2.

Part: COWLING — CHAFED (NR 1 ENGINE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, ENGINE NR 1 NOSE COWL EXTERNAL SKIN WORN DUE CHAFING OFF PYLON NOSE. NOSE COWL REPAIRED IAW SMRO EO 2000-041-001 UPS FILE 727-71-0095.

Part: FITTING — CRACKED (NR 3 FLAP TRACK) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON O/B AFT NR 3 TRAP TRACK SUPPORT FITTING ATTACH TO SPOILER SUPPORT BEAM AT BARREL NUT HOLE. REMOVED FITTING IAW SRM 51-31-00 AND INSTALLED FITTING IAW SRM 51-30 -02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 1180 S4L. REPAIRED AREA FROM BS 1163 - 1183 IAW SRM 53-30-3 FIG 14.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT, PITTING CORROSION IN AFT I/B HOLE. REPAIR CARRIED OUT IAW UPS EO B727-5440-11592 APP B.

Part: SKIN — CRACKED (NR 12 SPOLIER) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, RT WING T/E UPPER AT NR 12 SPOLIER CTRL I/B HINGE SKIN CRACKED. SKIN REPAIRED IAW 57-30-4.

Part: FITTING — CRACKED (RT TE FLAP) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, RIGHT O/B FLAP O/B JACKSCREW FAIRING LWR ATTACH FITTING IS CRACKED AND SEVERAL FASTENERS ARE LOOSE AT UPPER ATTACH POINT. FITTING INSTALLED AND LOOSE FASTENERS REPLACED IAW SRM 51-30-2.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION AT LAP JOINT S19R BS 500 - 481 AT VARIOUS LOCATIONS. LFEC INSP OF LAP JOINT BS 440 - 520 S19R IAW B727 NDTM. RESULT 15 - 20 PERCENT CORROSION. OTHER AREAS NDF. HFEC INSP LAP JOINT IAW B727 NDTM NO DEFECTS FOUND. REPAIR CARRIED OUT IAW UPS EO B727-5330 0509 APPX 8.3 SRM 53-30-3 FIG 14 AND SMRO EO 2000-041-010 WITH UPPER SKIN CUT OUT BETWEEN BS 498 AND 485. UPS FILE 727-53-2300.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION AT LAP JOINT S19R BS 500 TO BS 481 AT VARIOUS LOCATIONS. HFEC AND LFEC CARRIED OUT LFEC FOUND 15 - 20 PERCENT CORROSION BS 485 - 498. OTHER AREAS NO DEFECTS FOUND. HFEC RESULTS NO DEFECTS FOUND. FASTENERS REMOVED IN CRITICAL AREA IAW SRM 51-30-00 NDF. REPAIR CARRIED OUT IAW UPS EO B727-5330-0509 APPIX 8.3 SRM 53-30-3 FIG 14 AND SMRO EO 2000-0 41-010 WITH UPPER SKIN CUTOUT BETWEEN BS 498 AND 485. UPS FILE NO727-53 -2300.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, ENG NR 3 FWD MOUNT, PITTING CORROSION IN ALL 4 MOUNT HOLES. REPAIR C/O IAW EO B727-5440-11592 APP B.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, SUSPECT CORROSION ON SKIN AT BS 1140 BETWEEN STR 3R AND STR 4R. AREA REPAIRED FROM BS 1140 - BS 1160 IAW SRM 53-30-3.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, NR 5 KRUEGER FLAP INNER SKIN CRACKED JUST I/B OF ACTUATOR X2. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC C/O IAW B727 NDTM PT.6 51-0 0-00 FIG 4. CRACK FOUND TO BE CONTAINED WITHIN STOP DRILL HOLE. REPAIR C/O IAW EO B727-5750-3082.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION AT VARIOUS MARKED LOCATIONS S4L LWR SKIN BETWEEN BS 750 AND BS 870. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, SUSPECT CRACK FROM FASTENER HOLE IN SKIN AT NR 3 RT COCKPIT WINDOW AFT VERTICAL CUT OUT. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CRACK IN SKIN AT L/WING ICE LIGHT UPPER FWD CUTOUT. CRACK STOP DRILLED IAW SRM 51-10-01. HFEC INSP C/O ON ABOVE AREA IAW B727 NDTM PT.6 FIG 4. RESULT: CRACK CONTAINED WITHIN STOP DRILL. AREA REPAIRED IAW SRM 53-30-3 FIG 22 AND SMRO EO 2000-041-003. UPS FILE 727-53-2295.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,985 hrs · 47,549 cycles

INSPECTION TYPE:C, CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 475 BETWEEN S7L AND S6L. REPAIR C/O IAW SMRO EO 2000-041-006. UPS EO B727-5330-13568.

Part: VALVE — INOPERATIVE (RT A/C PACK)

INSPECTION TYPE:N/A, AIRCRAFT WILL NOT MAINTAIN PRESSURIZATION. REMOVED AND REPLACED RIGHT PACK FLOW SENSING VENTURA VALVE IAW DC8 MM 21-51-62, OPS CHECKS GOOD. (P/N 106892-1-1) (S/N P-501) ON, (S/N P-444) OFF.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE: C, STRINGER 24 RT CRACKED AT BS 290. INSTALLED STRINGER REPAIR IN ACCORDANCE WITH B727 SRM 53-10-3 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE: C, CORRODED AND CRACKED STRINGER 24 RT LAP JOINT STA 296 UPPER OUTER SKIN. INSTALLED LAP SKIN REPAIR IN ACCORDANCE WITH UPS EO B727-5330-0509 A PPENDIX 8.3

Part: BRACKET — CRACKED (NR 8 LE SLAT)

INSPECTION TYPE:SI, NR 8 SLAT ATTACHMENT BRACKET AT I/B TRACK CRACKED. REPLACED BRACKET PER OHM 20-50-01.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE:SI, NR 4 SLAT RIB CRACKED AT ACTUATOR ROD END BOLT O/B SIDE. REPLACED RIB PER SRM 51-30-5.

Part: BRACKET — CRACKED (NR 6 LE FLAP)

INSPECTION TYPE:SI, CRACKED NR 6 K-FLAP ACTUATOR I/B MOUNT BRACKET, LWR FWD RADIUS. FABRICATED AND REPLACED MOUNT BRACKET PER SRM 51-20-1.

Part: SKIN — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE:SI, CRACK RUNNING FROM NR 6 SLAT O/B GUIDE HOOK MOUNT HOLE TO O/B RIVET HOLE. REMOVED AND REPLACED NR 6 SLAT PER MM 27-81-11.

Part: CLIP — CRACKED (BS 1090)

INSPECTION TYPE-SI, CRACK IN STRINGER CLIP STA 1090 STR 3 RT. REPLACED CLIP IAW SRM 51-30-2.

Part: CLIP — CRACKED (BS 1030)

INSPECTION TYPE:SI, CRACKED STRINGER CLIP STA 9 LT STA 1030. REPLACED CLIP IAW SRM 51-30-2.

Part: BEAM — CORRODED (BS 1052)

INSPECTION TYPE:SI, CORROSION ON TRANSVERSE BEAM BL 0 STA 1052, WL 208. REPAIRED PER SRM 51-10-1.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581.04.00-03) ON NR 1 FLAP CARRIAGE SPINDLE FORWARD OF THRUST WASHER. REPLACED CARRIAGE ASSEMBLY.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, NR 5 FLAP CARRIAGE CORRODED ON I/B OF SPINDLE CORROSION (C57-581-04.00-04). REPLACED CARRIAGE ASSEMBLY.

Part: CARRIAGE — CORRODED (TE FLAPS)

INSPECTION TYPE:SI, CORROSION (C57-581-04-00-03) ON NR 3 FLAP CARRIAGE INNER AND OUTER SURFACE OF SPINDLE AND NUMEROUS AREAS ON REST OF CARRIAGE. REPLACED CARRIAGE ASSEMBLY.

Part: BEAM — CORRODED (BS 1180)

INSPECTION TYPE:SI, CRACK IN VERTICAL BEAM WEB BS 1180 WL 281 RBL 26.83. INSTALLED REPAIR KIT PER UPS EO B727-5310-1137.

Part: CHORD — CRACKED (BS 171.5)

INSPECTION TYPE:SI, UPPER RIB FLANGE CRACKED AT LT WING (FUEL TANK) UPPER STRINGER NR 16 WS 171.5. REMOVED AND REPLACED CHORD PER SRM 51-30-2. CHORD REPLACEMENT LOCATED AT UPPER STRINGER 16 WS 171.5 AT LT WING.

Part: CHORD — CRACKED (BS 171.5)

INSPECTION TYPE:SI, RT WING TANK UPPER CHORD CRACKED AT STRINGER 21 STA 171.5. REMOVED AND REPLACED THE CHORD IAW SRM 51-30-2. CHORD REPLACEMENT LOCATED AT RT WING, STRINGER 21 WS 171.5.

Part: FRAME — DENTED (BS 1010)

INSPECTION TYPE:SI, AFT CARGO BAY FRAME DENTED STA 1010 STR 25L-26L. REPAIRED FRAME AT STA 1010 STR 25L-26L PER SRM 51-40-3.

Part: TENSION STRAP — CRACKED (BS 720)

INSPECTION TYPE:SI, LWR FLOORBEAM TENSION STRAP CRACKED STA 720, RBL 25, WL 200. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR TO TENSION STRAP AT LWR FLOORBEAM TENSION STAP AT STA 720, RBL 25, WL 200 PER SRM 53-10-8, 51-30-2.

Part: SHEAR TIE — CRACKED (BS 720)

INSPECTION TYPE:SI, SHEAR TIE CRACKED AND FASTENER SHEARED STA 720 BETWEEN STR 20R AND 21R. REPAIRED SHEAR TIE AT STA 720 BETWEEN STR 20R AND 21R PER SRM 53-10-4 AND 51-20-1.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON STA 328 FLOORBEAM UPPER CHORD LBL 50. REPAIRED FLOORBEAM AT STA 328 PER SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION TYPE:SI, CORROSION ON FLOORBEAM UPPER FLANGE LBL 50 TO RBL 50. REPAIRED FLOORBEAM SRM 53-10-8.

Part: CLIP — CRACKED (BS 990)

INSPECTION TYPE:SI, CRACK IN STRINGER CLIPS STA 990 STR 6 AND 8 RT. REMOVED CRACKED STRINGER CLIPS STA 990 STR 6 AND 8 RT AND INSTALLED NEW STRINGER CLIPS IAW SRM 51-10-1 AND 51-30-2.

Part: SHEAR TIE — CRACKED (BS 680)

INSPECTION TYPE:SI, SHEAR TIE CRACKED STA 680 BETWEEN STR 17R AND 18R. REPAIRED SHEAR TIE AT STA 680 BETWEEN STR 17R AND 18R PER SRM 51-20-1.

Part: SEAT TRACK — CORRODED (BS 782-788)

INSPECTION TYPE:SI, DAMAGE TO SEAT TRACK IN WELL AT BS 782 TO 788 LBL 62 WL 208. ALSO, FOUND CORROSION ON O/B FLANGE BS 760- LBL 66 FOUND OUT OF LIMITS. REPLACED SEAT TRACK FROM BS 750 TO BS 850 PER SRM 51-30-2 AND 53-10-5.

Part: FRAME — CRACKED (BS 277)

INSPECTION TYPE:SI, CRACK ON FRAME AT STA 277 JUST ABOVE STR 26 RT. STOP DRILLED CRACK IN FRAME, FABRICATED REPAIR DOUBLER, FABRICATED STIFFENER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02, 51-10-02, MM 51-20-151.

Part: CLIPS — CRACKED (BS 1050)

INSPECTION TYPE:SI, CRACK IN STRINGER CLIPS STA 1050 RT STRINGERS 5 AND 6. REPLACED BOTH CLIPS PER 727 SRM 51-30-2 AND 51-30-5.

Part: CLIP — CRACKED (BS 1070)

INSPECTION TYPE:SI, CRACK IN STRINGER CLIP STA 1070 STR 9 RT. REMOVED CRACKED STRINGER CLIP AT BS 1070 AND INSTALLED NEW STR CLIP IAW SRM 51-30-02, 51-10-01, 51-20-01.

Part: ANGLE — CRACKED (BS 180.6)

INSPECTION TYPE:SI, VERTICAL FIN STA 180.6, STR 7, ANGLE IS CRACKED AT FASTENER HOLE. REMOVED FASTENERS COMMON TO REPAIR, FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED REPAIR PARTS IAW SRM 55-30-02, 55-30-05.

Part: STRINGER — CORRODED (BS 360)

INSPECTION TYPE-N/A, EVIDENCE OF CORROSION LEFT SIDE STA 360 APPROX S24-S25. DEFERRED CORROSION AT STATION 360 STRINGER 24 AND 25 IN ACCORDANCE WITH FERRY PERMIT NR 9052. REMOVED FASTENER TO INVESTIGATE, VISUALLY INSPECTED FASTENER HOLES. NO CORROSION FOUND, ILLEGIBLE 66193 12 AUG 98. INSP ALL INTERNAL STRUCTURE NO CORROSION NOTED ILLEGIBLE 90851. INSTALL FASTENERS, THIS CLEARS D-157185.

Part: WEB — CORRODED (BS 1170-1176)

INSPECTION TYPE-C, CORROSION ON SHEAR WEB FLOOR STA 1170 TO 1176 LBL 25 WL 208 CORROSION SDN C53-224-04.00-01. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-1, SRM 51-10-6. DAMAGED AREA WAS REMOVED AND REPAIRED ON CARD NR 740159.

Part: BEAR STRAP — CORRODED (BS 1070-1085)

INSPECTION TYPE-C, CORROSION (C53-100-01.00-04) EXTERNAL SKIN PILLOWED WITH (5) DISHED RIVET HEAD ABOVE AFT CARGO DOOR AREA (MARKED). REPAIRED EXTERNAL SKIN PER UPS EO NO 727-53-1963 TRAMCO EO 97-2560.

Part: SILL — CORRODED (BS 1135)

INSPECTION TYPE-C, CORROSION ON MOP SILL STA 1135 LBL 65 WL 208 CORROSION SDN C53-224-04.00-01. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED OLD MOP SILL, FABRICATED AND INSTALLED NEW MOP SILL ALL WORK PER SRM 51-10-6, SRM 53-10-1, SRM 51-30-2, SRM 51-20-1.

Part: CHANNEL — CRACKED (BS 336)

INSPECTION TYPE-C, CRACK ON NLG DRAG BRACE SHELF FWD SUPPORT ANGLE RBL 18 WL 154 BS 336. REPLACED SUPPORT ANGLE (SHELF) IAW SRM 51-30-2, 51-10-1, 51-10-2 AND DWG 65-50411.

Part: CHANNEL — CORRODED (BS 325-340)

INSPECTION TYPE-C, CORROSION (C53-224-03.00-01) ON HAT CHANNEL STA 325 TO 340 RBL 15 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT. REMOVED OLD HAT CHANNEL AND INSTALLED NEW HAT CHANNEL PER SRM 53-10-1, SRM 51-30-2, SRM 51-10-6.

Part: TAB — DELAMINATED (RT AILERON)

INSPECTION TYPE-C, O/B AILERON TAB LOWER SURFACE HAS TWO AREAS OF DELAMINATION, ONE 30 FROM I/B END AND ONE 17 FROM I/B END T/E. REPAIRED AILERON TAB PER SRM 51-40-06.

Part: WEB — CORRODED (BS 1176)

INSPECTION TYPE-C, WHILE WORKING ON CUSTOMER CARD 740177 FOUND CORROSION ON SHEAR WEB BS 1176 LBL 40 TO 50 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR WEB AT STA 1176 LBL 40 TO 50 WL 208 IAW SRM 51-40-2.

Part: CHORD — CORRODED (BS 1176)

INSPECTION TYPE-C, CORROSION ON 1176 CHORD LBL 40 TO 50 WL 208 (CORROSION SDN 224-04.00-01). CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED 1176 CHORD LBL 67 RBL 67 IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-20-4.

Part: WIRE — CHAFED (NR 2 ENGINE)

INSPECTION TYPE-N/A, CLIMB POWER 250 KTS ENG NR 2 OVERHEAT LT ON INFLIGHT 10,000 FT. ALL OTHER INDICATIONS NORMAL, ENGINE NR 2 SHUTDOWN PER CHECKLIST PROCEDURES. RETURNED AND LANDED MEM. UNEVENTFUL PREVIOUS FLIGHT BUT DIFFERENT CREW, SAME PROBLEM. PERFORMED ENG OVERHEAT WARNING SYSTEM T/S PER MM 75-41-00, NO DEFECTS NOTED. FOUND WIRE W9281-E9201-20 CHAFING AGAINST MOTOR MOUNT SUPPORT BRACKET. REPAIRED SAME, RAN ENG AND SYSTEM OPS CHECK OK.

Part: WIRE — CHAFED (NR 2 ENGINE)

INSPECTION TYPE-N/A, CLIMB POWER 250 KTS ENG 2 OVERHEAT LIGHT ON INFLIGHT 10,000 FT. ALL OTHER INDICATIONS NORMAL, ENG 2 SHUTDOWN PER CHECKLIST PROCEDURES. PERFORMED ENG OVERHEAT WARNING T/S PER MM 75-41-00, NO DEFECTS NOTED. FOUND WIRE W9281-E9201-20 CHAFING AGAINST MOTOR MT SUPPORT BRACKET. REPAIRED SAME, RAN ENG AND SYSTEM OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: P/D. ON PREDEPARTURE CK FOUND ENTRY DOOR EMERGENCY EXIT LIGHT NOT WORKING FROM ARM SWITCH, BUT WORKS FROM SWITCH ON LIGHT ASSY ITSELF. REMOVED AND REPLACED ENTRY DOOR EMER EXIT LIGHT ASSY IAW MM 33-50-00 EMER EXIT LIGHTS. OPS CK NORMAL. P/N ON 10-0067-9, P/N OFF SAME. S/N ON 20195, S/N OFF 4249.

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE DURING WEEKEND CHECK, LIGHT ASSY JARRED LOOSE DURING LAST LEG. REMOVED BATTERY PACK AND CHARGED BATTERY OVER THE WEEKEND, OPS CK'ED NORMAL.

Part: STIFFENER — CORRODED (LT WING)

INSPECTION TYPE 'C', CORROSION ON LT WING FRONT SPAR VERT STIFFENER 5TH STIFFENER O/B FROM ACCESS CUTOUT 7340. REMOVED CORRODED STIFFENER, INSTALLED NEW SIFFENER PER SRM 51-3-2, 57-10-4 AND MM 28-11-0.

Part: NOSE — CORRODED (AILERON)

INSPECTION TYPE 'C' AILERON SERVO HOUSING IN FWD NOSE COMP IS CORRODED. REMOVED CORRODED HOUSING, INSTALLED NEW HOUSING PER MM 22-11-11.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE 'C', CENTER HINGE 0N RT WING AILERON TAB AILERON SIDE IS CORRODED. REMOVED CORRODED HINGE FITTING AND INSTALLED NEW HINGE FITTING PER SRM 51-30-2 AND MM 27-10-11.

Part: DOOR GATE — CRACKED (GALLEY DOOR)

INSPECTION TYPE 'C', MID GALLEY DOOR UPPER GATE BEAM CRACKED ON I/B RADIUS ALL AFT SIDE. REMOVED AND REPLACED BEAM IAW SRM 51-30-2, 51-20-4 AND MM 52-12-11.

Part: INTERCOSTAL — CORRODED (BS 1045)

INSPECTION TYPE 'C', CORROSION ON THE INTERCOSTAL AT BS 1045, RBL 6 WL 146. REMOVED CORROSION AND REPAIRED INTERCOSTAL IAW SRM 51-30-2, 51-10-2 AND MM 51-20-15.

Part: BATTERY — DISCHARGED (CABIN)

MAINTENANCE REPORTED, DURING WEEKEND CHECK EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLIGHT DECK)

WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPAIRED BATTERY (BOTH) EMERGENCY LIGHTS. OPS CHECK O.K.

Part: BATTERY — DISCHARGED (FLIGHT DECK)

WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHTS WILL NOT ILLUMIATE. REPLACED BATTERY. OP CHECK GOOD.

Part: BATTERY — DISCHARGED (FLIGHT DECK)

WHILE ON GROUND, MAINT FOUND FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BOTH EMERGENCY LIGHT BATTERIES, OPS CHECK OK.

Part: BATTERY — DISCHARGED (COCKPIT)

WHILE ON GROUND, MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED N1-CAD BATTERIES, OPS CHECK GOOD.

Part: PANEL — CRACKED (NR 4 SPOILER)

WHILE ON GROUND, MAINTENANCE FOUND NR 4 SPOILER PANEL CRACKED AT ACTUATOR ATTACH POINTS.

Part: PANELS — CRACKED (SPOILER)

WHILE ON GROUND, MAINTENANCE FOUND 34 SPOILER PANEL CRACKED AT ACTUATOR ATTACH POINTS.

Part: ACTUATOR — MALFUNCTIONED (RT MLG DOOR)

PILOT REPORTED, THAT RIGHT MAIN GEAR DOOR LIGHT CAME ON WHEN GEAR HANDLE WAS PLACED IN OFF. LANDING GEAR RECYCLED WITH NO EFFECT. MAINTENANCE REPLACED THE RIGHT MAIN DOOR ACTUATOR.

Part: CHORD — CORRODED (VERT FIN)

DURING C-CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN TORQUE BOX RT HORIZONTAL CHORD, RBL 19 FIN STA 0. INSTALLED REPAIR PER UPS ENGINEERING FILE NR 727-55-0273.

Part: CHORD — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT O/B CHORD AT RBL 30, WL 250 IS CORRODED. REPLACED CHORD PER SRM 51-30-2.

Part: FRAME — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT FRAME CHORD CORRODED AT LBL 20, WL 228. REPLACED CHORD PER SRM 51-30-2.

Part: ANGLE — CRACKED (FS 1345)

DURING 'C' CHECK, MAINTENANCE FOUND LEFT SKIN SUPPORT ANGLE CRACKED AT FS 1345, FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3, 51-30-2.

Part: CHORD — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 FWD CHORD CORRODED. REPLACED FWD CHORD PER SRM 51-30-2.

Part: CHORD — CORRODED (STA 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT O/B CHORD CORRODED AT LBL 30, WL 250. REPLACED CHORD PER SRM 51-30-2.

Part: SKIN — CORRODED (FS 1283-1342)

DURING 'C' CHECK, MAINTENANCE FOUND SKIN LAP AT STR 14L FROM STA 1283-1342 IS CORRODED. REPAIRED PER SRM 53-30-3.

Part: SPAR CHORD — CRACKED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND REAR SPAR BULKHEAD CHORD HAS A CRACKED ANGLE ON THE RT SIDE AT F/S 1342, RBL 16. REPLACED ANGLE PER BOEING DRAWING 65-19104 AND SRM 51-10-1, 51-30-2.

Part: FRAME — CORRODED (STA 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT FRAME CHORD CORRODED AT RBL 20, WL 238. REPLACED CHORD PER UPS EO B727-5530-4601B.

Part: CHORD — CORRODED (FIN STA 22.5)

DURING 'C' CHECK, MAINTENANCE FOUND RT INNER CHORD FIN CRACKED AND CORRODED AT FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER BOEING DRAWING 65C20296 AND 65C20381.

Part: CHANNEL — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 CENTER CHANNEL CORRODED AT WL 247. REPLACED CENTER CHANNEL PER SRM 51-30-2.

Part: FRAME — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT LOWER FRAME CHORD CORRODED AT LBL 24, WL 220. REPLACED CHORD PER SRM 51-30-2.

Part: CHANNEL — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT AFT CHANNEL CORRODED AT RBL 18, WL 247. REPLACED CHANNEL PER SRM 51-30-2.

Part: FRAME — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT LOWER FRAME CHORD CORRODED AT RBL 24, WL 220. REPLACED LOWER CHORD PER SRM 51-30-2, AND UPS EO B727-5530-4001.

Part: CHANNEL — CORRODED (FS 1342)

DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT CHANNEL CORRODED AT LBL 18, WL 247. REPLACED CHANNEL PER SRM 51-30-2.

Part: ANGLE — CRACKED (FS 1345)

DURING 'C' CHECK, MAINTENANCE FOUND RT SKIN SUPPORT ANGLE CRACKED AT FS 1345, FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-3.