N932UP

Part: LIGHT — INOPERATIVE (OVER PAX DOOR)

EMERGENCY EXIT LT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE. REPLACED EMERGENCY EXIT BATTERIES. OPS CK NORMAL PER AMM 33-50-67-2.

Part: LIGHT — INOPERATIVE (CABIN)

N/A ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY REF AMM 33-50-00-0. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT)

FLIGHT COMPARTMENT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY REF AMM 33-50-00-0. OPS CK NORMAL. DISCOVERED UPON INVESTIGATION OF SELF DISCLOSURE.

Part: CHAIN — DETACHED (FWD DOOR SLIDE)

DURING C-CHECK, INSPECTION OF FWD DOOR EMERGENCY ESCAPE SLIDE BUSTLE LATCH CHAIN WAS FOUND DETACHED FROM THE SPLIT RING. THE SPLIT RING HAD BECOME ELONGATED AND THE RING COILS HAD SEPARATED THUS ALLOWING THE CHAIN TO DETACH. THE SLIDE WOULD NOT HAVE INFLATED IF REQUIRED. THE CHAIN AND RING ASSY WILL BE REPLACED. (K)

Part: RING — DISCONNECTED (DOOR SLIDE) · airframe 53,694 hrs · 41,775 cycles

CHAIN DISCONNECTED FROM LATCH ON ESCAPE SLIDE BOX ON FWD ENTRY DOOR. NEW RING FITTED TO LATCH CHAIN IAW MM 25-60-00.

Part: TRUNNION — CRACKED (RT MLG) · airframe 53,694 hrs · 41,775 cycles

INSPECTION TYPE:C ON INSP OF RT TRUNNION, 2 SUSPECT CRACKS DETECTED ON HOLE C I/B FLANGE O/B FACE AND O/B FLANGE I/B FACE. REPAIR CARRIED OUT IAW AAAE EO'S 2005-087-001, 2005-087-006 AND UPS EO 2 B727-5740-20666 APPX F. UPS ENGINEERING FILE NO'S B727-5740-22955-A AND B727-5740-22974-A.

Part: SKIN — DAMAGED (BS 521) · airframe 53,694 hrs · 41,775 cycles

INDICATION OF MATERIAL LOSS AT BS 521 S1L-2L. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-30-3, MM 25-21-33 AND AAAE EO 200 5-087-007. UPS ENGINEERING FILE NR B727-5330-22937.

Part: TRUNNION — CRACKED (LT MLG) · airframe 53,694 hrs · 41,775 cycles

INSPECTION TYPE:C ON INSPECTION OF LT TRUNNION 2 SUSPECT CRACKS DETECTED ON HOLE C ON BOTH I/B SIDES. REPAIR CARRIED OUT IAW AAAE EO'S 2005-087-004, 2005-087-005, UPS EO B7 27-5740-20666 APPX F. UPS ENGINEERING FILE NO'S B727-5740-22955-A AND B727-5740-22975.

Part: FRAME — CORRODED (BS 680) · airframe 53,694 hrs · 41,775 cycles

CORROSION FOUND AROUND ANCHOR NUT ON FRAME UPPER CHORD LWR SIDE AT BS 680 RBL 25. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-10-2 AND 51-40-3.

Part: LAP JOINT — CORRODED (BS 590 SKIN) · airframe 53,694 hrs · 41,775 cycles

SUSPECT CORROSION AT LAP JOINT DUE TO 2 POPPED FASTENER HEADS AT BS 590, S10R. CORROSION ON UPPER SKIN FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-10-06, 53-30-1 & 53-30-3.

Part: FLOORBEAM — CORRODED (BS 340) · airframe 53,694 hrs · 41,775 cycles

CORROSION ON FLOORBEAM TOP ANGLE AT BS 340 RBL 24. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-8 AND 53-10-1.

Part: INTAKE DUCT — CRACKED (NR 2 ENGINE) · airframe 53,694 hrs · 41,775 cycles

NR 2 ENG S-DUCT HAS A CRACKED ON INNER SKIN AT 3 O`CLOCK POS. ON RIB NR 5 REPAIR CARRIED OUT IAW AAAE EO 2005-087-002. UPS ENGINEERING FILE NR 727-54-20024.

Part: CASTING — CRACKED (LT AILERON) · airframe 53,694 hrs · 41,775 cycles

CRACK FOUND ON LT OUTBOARD AILERON LOCKOUT SUPPORT CASTING. LEFT O/B AILERON LOCKOUT SUPPORT CASTING REPLACED IAW MM 27-10-64, 27-1 0-60, 20-10-20, 27-10-00 & SRM 51-30-2.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C NR 1 ENG FWD MOUNT HOLES HAVE PITTING CORROSION IN BOTH IB HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT HOLE HAVE PITTING CORROSION IN BOTH I/B HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592.

Part: BRACKET — CRACKED (L/E SLAT) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE: C BRACKET INSIDE NR 7 SLAT AT OB TRACK CRACKED. REPAIRED IAW SRM 57-50-3.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C MATERIAL LOSS (LAP JOINT CORROSION) AT S-6L BS 685. REPAIRED IAW UPS EO B727-5330-0509 APPX C, AND SRM 53-3 0-1, FIG 5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE: C CRACK IN SKIN AT FWD CARGO DOOR CUTOUT AT FWD LWR CORNER. REPAIRED IAW AAAE EO 2004-050-001. REFERENCE UPS EO B72 7-5330-20497-A.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C CORROSION AT LAP JOINT, STR 6L, BS 695 - BS 718. REPAIRED IAW SRM 53-30-3, FIG 4.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C NWW PRESSURE WEB HAS A CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT BS 290 RT. REPAIRED IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C LT WING LE CAVITY INTERCOSTAL JUST OB OF NR 1 LEADING EDGE FLAP CENTER HINGE CASTING CRACKED AT IB LOWER FASTENER HOLE. REPLACED INTERCOSTAL IAW DRG 65-17356.

Part: RING — DISCONNECTED (EVAC SLIDE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE: C SLIDE LATCH RING ON FWD E DOOR ESCAPE SLIDE AND GIRT BAR TO SLIDE COMPARTMENT LATCH CHAIN FOUND DISCONNECTED. REPLACED RING AND CONNECTED CHAIN TO SLIDE LATCH IAW 25 -60-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C CORROSION ON SEAT TRACK FLANGE AT BS 495, RBL 62.5. REPAIRED IAW SRM 53-10-5, FIG 1.

Part: DOOR — CRACKED (RT MLG) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE: C RT MLG DOOR HAS DEEP INTERGRANULAR CORROSION ON A STRUCTURAL SKIN ELEMENT NEAR THE FWD HINGE AREA. ON REMOVAL OF SKIN, TWO CRACKS FOUND ON TOP AND BOTTOM OF SKIN. REPAIRED IAW SRM 52-80-2 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C CRACK ON FUSELAGE SKIN AT BS235.8, LT SIDE, WL 222. REPAIRED IAW SRM 53-30-3, FIGURE 3.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,286 hrs · 41,405 cycles

INSPECTION TYPE:C 2 DENTS IN SKIN AT BS 1245, STR 19R . REPAIRED IAW SRM 53-30-3, FIG 13A.

Part: BATTERY — DISCHARGED (CARGO BAY)

INSPECTION TYPE:N/A FIRE BELL SOUNDED ON CLIMB, LOWER CARGO LIGHT ON INSPECTED, FOUND TO BE INDICATION INOP DUE TO LOW BATTERY. DEFERRED PER MEL.

Part: PANEL — CRACKED (BS 249.3) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI CRACK SUSPECT ON NLG BAY R/H SIDE PANEL @ BS 249.3 BETWEEN FASTENERS AFT OF R/H FWD PRESSURE PANEL CUTOUT REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1

Part: BEAM — CRACKED (FUSELAGE) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, WHILE REMOVING RT BS 870 FITTING CRACK FOUND IN SIDE LOAD BEAM AT R BBL 54.50 REPAIRED IAW SMRO EO 2002-055-009. UPS ENGINEERING FILE NO. 727-53-2 0084

Part: FRAME — CORRODED (AFT WING) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C &SI, APU EXHAUST, SUSPECT CORROSION ON AFT WING FRAME UNDER TADPOLE SEAL OF UPPER EXHAUST. FRAME CORRODED BEYOND LIMITS. NEW FRAME FABRICATED AND INSTALLED IAW DRAWING 65-31997.

Part: FRAME — CRACKED (BS 990 S29L) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI SUSPECT CRACK AT FUSELAGE FRAME ATTACH POINT AT BS 990 STR. 29L IN A FT CARGO BAY REPAIRED FRAME AS PER SRM 53-10-4 FIG 11

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI AFT CARGO BAY, SEAT TRACK HAS LIGHT SURFACE CORROSION AT 2 AREAS AT BS 1027 LT & BS 1008 RT. CORROSION REMOVED AND FOUND OUTSIDE LIMITS IAW SRM 51-10-06 SEAT TRACK REPAIRED IAW SRM 53-10-5 FIG 8.

Part: SEAT TRACK — CORRODED (AFT CARGO BAY) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, AFT CARGO BAY, SEAT TRACK HAS LIGHT SURFACE CORROSION AT BS 1110 R/H SIDE CORROSION REMOVED IAW SRM 51-10-06 AND FOUND TO BE OUTSIDE LIMITS IA W SRM 53-10-01 FIG 3. SEAT TRACK REPAIRED IAW SRM 53-10-01.

Part: PIN — CORRODED (RT WING) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, RT WING REAR SPAR TO BODY FITTING TERMINAL BOTTLE PIN AT BS 870 HAS EVIDENCE OF PITTING CORROSION. CORROSION OUT OF LIMITS, BOTTLE PIN REPLACED IAW MM 57-41-01.

Part: BRACKET — CRACKED (NO. 13 SPOILER) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI NO. 13 SPOILER SUPPORT CASTING, I/B SUPPORT BRACKET IS CRACKED AT LW R ATTACH HOLE BRACKET REPLACED IAW SB 57-84 & DRAWING 65-17351

Part: BRACKET — CRACKED (NO.2 SPOILER) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI NO. 2 SPOILER SUPPORT CASTING, I/B REAR SPAR ATTACH BRACKET IS CRACK ED AT LWR ATTACH HOLE BRACKET REPLACED IAW SB 57-84 & DRAWING 65-17351

Part: SKIN — CORRODED (AFT AIRSTAIRS) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, CORROSION ON OUTER SURFACE OF NR 6 RISER SKIN OF AFT AIR STAIRS CORROSION REMOVED IAW SRM 51-10-06, FOUND TO BE OUT OF LIMITS IAW SR M 52-00-2. REPAIRED IAW EO B727-5260-7551-A

Part: FLAP TRACK — CORRODED (FWD ATTACH LUG) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C+SI #7 FLAP TRACK HAS SURFACE CORROSION ON THE I/B FWD ATTACH LUG. SURFA CE CORROSION ALSO FOUND ON THE FWD ATTACH PAD AND ON THE ON THE I/B FACE OF THE WING ATTACH FITTING. REPAIR CARRIED OUT IAW SMRO EO 20025507. REF. UPS ENGINEERING FILE N O. 727-57-20078. NOTE THAT POST HEAT TREATMENT, A CRACK WAS FOUND AN D THE FLAP TRACK WAS REPLACED. REF. NRC 605735.

Part: FITTING — CRACKED (BS 870 R/H) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI WHILE CARRYING OUT NDT ON R/H 870 FITTING CRACKS WERE FOUND IN 3 FAS TENER HOLES IN ROW 3, 1ST HOLE FROM BOTTOM AND 3RD & 4TH HOLES FROM BOTTOM R/H 870 FITTING REPLACED IAW EO B727-5310-3057 & DRAWING 65C13724

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, CRACKS FOUND ON FWD OUTBOARD FLANGE OF LT BS 950 FITTING. REPAIRED CRACKS IAW SMRO EO'S 2002-055-002 AND 2002-055-012. REF. UP S EO B727-5310-17901 AND UPS FILE NO. 727-53-20088.

Part: FITTING — CRACKED (RT MLG) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, RT MAIN GEAR DOOR ACTUATOR SUPPORT FITTING LUG CRACKED. LUG REPLACED IAW EO B727-3210-2583

Part: BRACKET — CRACKED (NR 12 SPOILER) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE: C & SI, NR 12 SPOILER SUPPORT CASTING I/B & O/B BRACKETS ARE CRACKED AT LWR ATTACH HOLES. BRACKETS REPLACED IAW DRAWING 65-17351 & SB 57-84

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHTS WILL NOT COME ON. REPLACED BATTERIES, OPS CHECKS GOOD.

Part: FITTING — CRACKED (BS 870 L/H) · airframe 52,741 hrs · 40,885 cycles

INSPECTION TYPE:C&SI WHILE CARRYING OUT NDT INSP. OF L/H 870 FTG, RECENT CRACK FOUND FROM HOLE COMMON TO STR. END AT 1ST ROW, ALSO 2 OTHER HOLES HAVE CORROSI ON INDICATIONS L/H 870 REPLACED IAW EO B727-5310-3056-F & DRAWING 65C13724

Part: SPAR — CRACKED (CENTER WING)

INSPECTION TYPE: C, WING CENTER SECTION FRONT SPAR T FITTING CRACKED LWR CHORD STA 740 LBL 42. REPLACED WING CENTER SECTION FRONT SPAR T FITTING T LWR CHORD STA 74 0 LBL 42 IAW B727 SRM 51-30-2

Part: FITTING — CRACKED (RT MLG WW)

INSPECTION TYPE: C, RT WHEEL WELL BS 940 FRAME FITTING LWR HALF CRACKED INBD AFT SIDE INSTALLED UPPER AND LOWER BACK TO BACK BATH TUB FITTINGS. AS PER REF UPSMIA-01-0003F AND DRAWING 65-16337 AT RH STA 940 FITTING FLANGE

Part: SWITCH — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A ENG FIRE WARNING BELL WILL NOT SOUND REMOVED AND REPLACED SWITCH

Part: BATTERY — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, ON PREFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT MODULE OVER COCKPIT ENTRY DOOR. PERFORMED OPS TEST PER MM 33-50-01.

Part: BATTERY — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, COCKPIT EMERGENCY EXIT LIGHT INOP DURING TEST. REPLACED THE BATTERIES IN THE COCKPIT EMERGENCY EXIT LIGHT. OPS CK NORMAL.

Part: TE FLAP — INOPERATIVE (WING)

ATB - FLAPS WOULD NOT RETRACT UPON RETRACTION ATTEMPT.

Part: WINDOW — OPEN (COCKPIT)

ATB - LOUD SQUEAL FROM F/O WINDOW AND AIRCRAFT WILL NOT PRESSURIZE. REMOVED LODGED CONDENSATION DRAIN TUBE FROM WINDOW.

Part: ANGLE — CORRODED (BS 950)

INSPECTION TYPE:C SURFACE CORROSION ON BKLD BS 950 LWR CHORD LBL 6 TO RBL 6 IN AFT CAR GO BAY LWR CHORD ANGLE REMOVED IAW SRM 51-30-02 LWR CHORD ANGLE REPLACED IAW DRAWING # 66-12639-0 ***CPCP***

Part: FRAME — CRACKED (BS 990)

INSPECTION TYPE:C, FRAME CRACKED AT BS 990 LWR LEG LBL 17. REPAIR CARRIED OUT IAW SRM 53-10-4 FIG 4.

Part: SUPPORT — CRACKED (BS 990)

INSPECTION TYPE:C, CARGO FLOOR SUPPORT CRACKED AT BS 990 RBL 3 AFT CARGO BAY. CARGO FLOOR SUPPORT REPLACED IAW SRM 53-10-05 FIG 4.

Part: INTERCOSTAL — CRACKED (BS 1148)

INSPECTION TYPE:C, INTERCOSTAL CRACKED ON LWR LEG AT BS 1148 BENEATH LT TIE DOWN TRACK. REPAIRED INTERCOSTAL IAW SRM 51-20-02.

Part: FRAME — CRACKED (BS 1010)

INSPECTION TYPE:C, FRAME AT BS 1010 LWR LEG CRACKED STR 29R. REPAIRED IAW SRM 53-10-4.

Part: FLOORBEAM — CRACKED (BS 294.5)

INSPECTION TYPE:C, CRACK AT BS 294.5 ON FLOORBEAM WEB RBL 44.5. REPAIRED CRACK IAW SRM 51-40-2 FIG 1.

Part: FLOORBEAM — CRACKED (BS B1110)

INSPECTION TYPE:C WHILE INSTALLING SMOKE DETECTOR UNIT AT BS 1110 A SUSPECT CRACK FOUN D ON LWR CHORD OF FLOOR BEAM BS 1110 LBL 19 APPROX REPAIR CARRIED OUT IAW SMRO EO. 99-37-005 UPS ENGINEERING FILE NO 727-53-2195

Part: FLOORBEAM — CORRODED (BS 1050)

INSPECTION TYPE:C, CORROSION FOUND ON FLOORBEAM LWR CAP AT BS 1050 BL 0 - RBL 20. REPAIR CARRIED OUT IAW SMRO EO 99-37-004 UPS ENGINEERING FILE NR 77-53-2197.

Part: HINGE — CRACKED (NR 4 TE FLAP)

INSPECTION TYPE:C, NR 4 FLAP TRACK, AFT HINGE FITTING FOR WING DOOR CRACKED. REPLACED AFT DOOR HINGE ON FLAP TRACK IAW SRM 51-10-01 AND 51-30-02.

Part: WEB — CRACKED (BS 275)

INSPECTION TYPE:C, 2 CRACKS CONFIRMED ON NOSE LANDING GEAR CEILING PRESSURE WEB AT BS 275 RBL 12 & LBL 16. PRESSURE WEB REPLACED IAW DRAWING NR 65-18416.

Part: BRACKET — CRACKED (LT MLG WW)

INSPECTION TYPE:C, LT WHEEL WELL, BRACKET CRACKED AT FWD FACE OF 940 FITTING. FABRICATED AND INSTALLED BRACKET IAW DRAWING 65C15732.

Part: PLATE — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, FWD CARGO DOOR AFT CORNER SCUFF PLATE CRACKED. SCUFF PLATE REPLACED IAW DRAWING NR 65-18621.

Part: SILL — CORRODED (BS 460 -640)

INSPECTION TYPE:C, AREAS OF CORROSION AT MAIN CARGO DOOR SILL LBL 64 BETWEEN BS 460 - BS 640. REPAIR CARRIED OUT IAW SMRO EO 99-37-03 UPS ENGINEERING FILE NR 727-53-2194.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE:C, EVIDENCE OF CORROSION AND CRACK ON BS 740 RT FITTING LWR WEB VERTICAL FLANGE. FITTING REPLACED IAW EO B727-5310-7477-E.

Part: BRACKET — CRACKED (BS 940)

INSPECTION TYPE:C, RT WHEEL WELL, BRACKET CRACKED AT FWD SIDE OF BS 940 FITTING. FABRICATED AND INSTALLED BRACKET IAW DRAWING NR 65C15732.

Part: SKIN — CORRODED (BS 1163)

INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1163 S20L & S22L. ALL CORROSION REMOVED FROM SKIN AREA IAW SRM 51-30-2 AND FOUND TO BE WITHIN LIMITS PER SRM 53-30-1.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, PREFLIGHT COCKPIT EMERGENCY EXIT LIGHT OPS CHECK BAD. REPLACED BATT PACK, OPS CK GOOD.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS GO DIM. REPLACED DRAINED BATTERIES.

Part: FRAME — CRACKED (FRAME 400)

INSPECTION TYPE-C, OUTER CHORD OF FRAME 400 CRACKED AT STR 20 TO 21. FRAME REPAIR CARRIED OUT IAW SRM 53-10-4.

Part: SKIN — DAMAGED (CARGO DOOR)

INSPECTION TYPE-C, NUMEROUS SCRATCHES AND GOUGES OUTSIDE LIMITS IN AFT CARGO DOOR ALSO PATCHES ON INSIDE SKIN. DOOR REPLACED IAW MM 52-30-00 REF N/R 704898 FOR RIG AND OPERATION OF DOOR.

Part: SILL — CRACKED (BS 620)

INSPECTION TYPE-C, CREASE BEAM SILL CHORD WEB CRACKED AT BS 620 LT. WEB REPAIRED IAW SRM 51-40-2.

Part: MOUNT — CORRODED (NR 3 ENGINE)

INSPECTION TYPE-C, NR 3 ENG PITTING CORROSION ON BORE OF HOLES ON FWD ENG MOUNT FITTING = 2 O/B HOLES. REPAIR CARRIED OUT PER SRS EO 98-14-002 AND 98-14-005 REF CPT 049-8 AND 052-98 FOR BUSHING MANUFACTURE.

Part: MOUNT — CORROSION (NR 1 ENGINE)

INSPECTION TYPE-C, NR 1 ENG PITTING CORROSION ON BORE OF HOLES FWD ENG MOUNT FITTING TWO O/B HOLES AND I/B AFT HOLE. REPAIR CARRIED OUT PER SRS EO 98-14-003 AND 98-14-004 REF CPT 006/98 056/98 AND 055/98 FOR BUSHING MANUFACTURE.

Part: SKIN — CRACKED (LT MLG DOOR)

INSPECTION TYPE-C, LT WING MLG WING DOOR HAS CRACK ON EXISTING REPAIR ON OUTER SKIN. HIFEC INSPECTION CARRIED OUT IAW B727 NDT MANUAL D6-48875 PART 6 51-00-00 FIG 4 AND 16 CRACKS CONFIRMED AND STOPPED DRILL.

Part: WEB — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-C, CRACK IN WEB AFT OF AFT CARGO DOOR CUTOUT EXTENDING BEYOND EXISTING REPAIR. REMOVED EXISTING PATCH AND REPAIRED WEB. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: SKIN — CRACKED (BS 243)

INSPECTION TYPE-C, CRACKS IN FUSELAGE SKIN BS 243.7 BETWEEN 212 AND 215 RT. AREA REPAIRED PER SRM 53-30-3 FIG 3 AT BS 243.7 BETWEEN 212 AND 215 RT.

Part: SKIN — CRACKED (BS 188)

INSPECTION TYPE-C, SUSPECT SKIN CRACKS BS 188 WL 207 RT SIDE. AREA REPAIRED PER SRM 53-30-3 FIG 3 AT BS 188 WL 207 RT.

Part: BULKHEAD — CRACKED (BS 178)

INSPECTION TYPE-C, CRACK ON FWD PRESSURE BULKHEAD, BS 178 AT WL 207.5, RBL 5. BULKHEAD REPAIRED IAW UPS EO B727-5310-4290.

Part: PACK — MALFUNCTIONED (CARGO COMP)

AT DEPARTURE, HEARD A LOUD BOOM. ALL COCKPIT INDICATIONS NORMAL. OPENED COCKPIT DOOR, FOUND CARGO COMPARTMENT FULL OF SMOKE. DI NUMBER 125957. INSPECTED PACK SYSTEM FOR OPERATION AND OIL LEAKS, NONE FOUND. OPERATED LT PACK IAW MM21-00-00, NO FAULTS OR EVIDENCE OF SMOKE FOUND.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE-SI, CORROSION ON STA 344 FLOORBEAM UPPER CHORD LBL 55 TO RBL 45 WL 207. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED UPPER CHORD, FABRICATED NEW UPPER CHORD AND INSTALLED UPPER CHORD. ALL WORK DONE IAW SRM 53-10-1, 51-10-1, 51-30-2, 53-10-8 AND MM 51-20-151.

Part: FLOORBEAM — CORRODED (BS 1030)

INSPECTION TYPE-SI, CORROSION STA 1030 FLOORBEAM LBL 5 TO 61 AND RBL 5 TO 30 FWD AFT FLANGES RBL 48 TO 55 FWD FLANGE WL 208 AT NUTPLATE HOLES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 96-2563.

Part: EXPANSION LINK — CORRODED (BS 740)

INSPECTION TYPE-SI, EXPANSION LINKS ARE CORRODED AT BS 740 WL 162.5 LBL 36 RBL 12. REMOVED CORRODED LINKS WHICH WERE FOUND TO BE OUT OF LIMITS, INSTALLED NEW EXPANSION LINKS IAW SRM 51-10-1, 51-30-2.

Part: STRINGER — CORRODED (BS 435-475)

INSPECTION TYPE-SI, CORROSION ON STRINGER AND SPLICE STR 24R 435 TO 475. REMOVED CORROSION ON STRINGER AND SPLICE, FOUND TO BE OUT OF LIMITS. REMOVED OLD STR 24R BS 435 TO 475, INSTALLED NEW STR AND SPLICE ALL WORK DONE IAW SRM 53-10-2, 53-10-3, 51-30-2, 51-40-3, 51-10-06.

Part: STIFFENER — CORRODED (BS 219.8)

INSPECTION TYPE-SI, CORROSION ON STIFFENER BS 219.8 LBL 15 WL 165. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENER PER SRM 51-30-2.

Part: EXPANSION LINK — CORRODED (BS 858-870)

INSPECTION TYPE: SI. CORROSION ON EXPANSION LINK STA 858-870 LBL 25 AROUND EACH NUTPLATE. CORROSION OUT OF LIMITS IAW 53-10-1. REPLACED EXPANSION LINK IAW SRM'S 51-10-1, 51-30-5 OHM 20-50-01 MM 20-50-02, 20-50-03.

Part: STRINGER — CRACKED (BS 462-466)

INSPECTION TYPE: SI. STR 26L CRACKED AND DENTED BS 462-466. REPAIRED STR 26L STA 462-466 IAW SRM 53-10-3.

Part: FITTING — CORRODED (NR 1 SPOILER)

INSPECTION TYPE: SI. WHILE WORKING WINGS 499 CUSTOMER ID NR 598179 FOUND NR 1 SPOILER FITTING TO BE CORRODED. REMOVED AND REPLACED NR 1 SPOILER FITTING IAW MM 27-51-131, 27-61-81. TO BE OPS CHECKED ON NRC 597706.

Part: INTERCOSTAL — CRACKED (CARGO DOOR)

INSPECTION TYPE: SI. FWD CARGO DOOR AFT HINGE FWD INTERCOSTAL CRACKED. REMOVED AND REPLACED FWD CARGO DOOR AFT HINGE FWD INTERCOSTAL PER SRM 51-30-2.

Part: HINGE — CORRODED (LT AILERON)

INSPECTION TYPE: SI. L/W I/B AILERON CENTER (WING SIDE) HINGE FITTING IS CORRODED. REPLACED L/W I/B AILERON CENTER (WING SIDE) HINGE FITTING IAW MM 27-10-01.

Part: SPAR — CORRODED (LT WING)

INSPECTION TYPE: SI. CORROSION L/W LOWER SPAR CHORD IS CORRODED 28 TO 30 OF I/B END AT OUTER RADIUS. REPAIRED SPAR CHORD (LOWER) IAW TRAMCO EWO 96-2549 (UPS EO FILE NR 727-57-1745).

Part: CASTING — CRACKED (OVER WING EXIT)

INSPECTION TYPE: SI. CORROSION ON RT AFT OVERWING EXIT HANDLE FRAME ASSY CASTING. BEGAN REMOVING CORROSION AND FOUND FRAME CRACKED, REMOVED AND REPLACED FRAME IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 740-783)

INSPECTION TYPE: SI. CORROSION ON STR 7 LEFT FROM BS 740-783. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER SRM'S 51-20-51, 51-20-151, 51-30-2.

Part: CARRIAGE — CORRODED (NR 1 TE FLAP)

INSPECTION TYPE: SI. CORROSION AROUND THE THRUST WASHER ON NR 1 CARRIAGE. CORROSION FOUND BEYOND ECONOMICAL REPAIR, RECEIVED REPLACEMENT CARRIAGE, WILL ADVISE OF REPAIRS.

Part: CARRIAGE — CORRODED (NR 8 TE FLAP)

INSPECTION TYPE:SI CORROSION ON NO 8 FLAP CARRIAGE HAS BARE METAL AND CORROSION INSIDE SPINDLE CARRIAGE FOUND TO BE BEYOND ECONOMICAL REPAIR, RECEIVED REPLACEMENT CARRIAGE, WILL BE REPLACED ON TC C57-581-04-4D

Part: CARRIAGE — CORRODED (NR 4 TE FLAP)

INSPECTION TYPE: SI. CORROSION NR 4 CARRIAGE HAS CORROSION INSIDE SPINDLE. CORROSION BEYOND ECONOMIC REPAIR, RECEIVED REPLACEMENT CARRIAGE, WILL ADVISE OF REPAIRS.

Part: FRAME — CORRODED (BS 675)

INSPECTION TYPE: SI. CORROSION AT BS 675 ON FRAME AT STR 20A. REMOVED CORRSION, REWORK DEEMED OUT OF LIMITS, IAW SRM 53-10-1, REPAIRED FRAME STA 20 IAW SRM 51-40-2, STR CLIP AT STR 20 ALSO REPLACED. IAW SRM'S 51-30-2, 51-20-1.

Part: FLOOR BEAM — CORRODED (BS 680)

INSPECTION TYPE: SI. CORROSION ON STA 680 FLOORBEAM BOTTOM SIDE OF UPPER CHORD LBL 25-RBL 25 WL 207. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED, WILL ADVISE OF REPAIRS.

Part: SEAT TRACK — EXFOLIATED (BS 872)

INSPECTION TYPE: SI. SEAT TRACK STA 872 LBL 25 WL 208 IS EXFOLIATED. REMOVED AND REPLACED SEAT TRACK FROM 870-1020 LBL 25 WL 208 IAW 53-10-1, 51-10-1, 51-10-2.

Part: STRAP — CORRODED (BS 385)

INSPECTION TYPE: SI. I/B SEAT TRACK SPLICE STRAP CORRODED STA 385 RBL 60.5 WL 206. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-8. REPLACED STRAP PER SRM'S 51-20-1, 51-10-2.

Part: STRINGER — CORRODED (BS 377)

INSPECTION TYPE: SI. CORROSION ON STR 22R BS 377. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, REPLACED STR PER SRM'S 51-40-3, 53-10-3, 53-10-2, 51-40-3, 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 328)

INSPECTION TYPE: SI. CORROSION ON STA 328 FLOORBEAM LBL 3 AND LNL 44 WL 207. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. REPLACED UPPER CHORD FLOOR BEAM PER SRM'S 53-10-8, 51-10-2, 53-10-8.

Part: STRAP — CORRODED (BS 950-1166)

INSPECTION TYPE: SI. CORROSION AROUND NUTPLATE HOLES ON THE BL ZERO STABILIZER STRAP FROM BS 970-1166 WL 199-203. REMOVED CORRODED STABILIZER STRAP FROM BS 950-1160 AND INSTALLED NEW STABILIZER STRAP FROM BS 950-1160, ALL WORK DONE, IAW SRM'S 53-10-1, 51-30-8, 51-30-5, 51-30-2, 51-10-2, 51-10-6, MM 51-20-31.

Part: FRAME — CORRODED (BS 251)

INSPECTION TYPE: SI. CORROSION ON FRAME WEB STA 251 RBL 48 WL 208 TO 228. REMOVED CORROSION. REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPAIRED 251 FRAME IAW SRM'S 51-40-2 AND 51-30-2.

Part: FRAME — CORRODED (BS 227)

INSPECTION TYPE: SI. CORROSION ON FRAME WEB STA 227 RBL 44 WL 208 TO 234. CORROSION WAS FOUND OUT OF LIMITS IAW SRM 53-10-1, REPAIRED FRAME WEB AT STA 227 IAW SRM 51-40-2.

Part: STRINGER — CRACKED (BS 863)

INSPECTION TYPE: SI. STR 4R CRACKED STA 863 RT FLANGE LIP. REPAIRED STR 4R STA 863 IAW SRM 51-30-2, 53-10-1, 53-10-3, AND MM 51-20-21, 51-20-31.

Part: STRINGER — CORRODED (BS 1110-1130)

INSPECTION TYPE: SI. CORROSION ON BACKSIDE OF STRINGER 12 TOP FLANGE STA 1110-1130 LT WL 246. REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 12L IAW SRM 53-10-3.

Part: STRAP — CORRODED (2-24)

INSPECTION TYPE: SI. CORROSION ON OUTBOARD SEAT TRACK SPLICE STRAP STA 380 RBL 56 WL 207. REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED SPLICE STRAP AT STA 380 RBL 56 IAW SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 745)

INSPECTION TYPE: SI. CORROSION AT BS 745 RBL 11 WL 168 AROUND FASTENER IN UPPER DELTA BEAM BOX. FOUND STIFFENER TO BE OUT OF LIMITS PER SRM 51-10-1, REMOVED AND REPLACED STIFFENER PER SRM 51-30-2.

Part: STRINGER — CORRODED (BS 990-1148)

INSPECTION TYPE: SI. CORROSION ON STR 3 LT STA 990-1148. FOUND CORROSION OUT OF LIMITS AT STR 3 LT BS 1037 AND 104. REPAIRED PER SRM 51-10-1, 51-40-02, 51-30-2, 51-10-2, MM 51-20-151.

Part: STIFFENER — CORRODED (BS 211.8)

INSPECTION TYPE: SI. CORROSION ON STIFFENER BS 211.8 LBL 19 WL 165. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-1, REPLACED STIFFENER PER SRM'S 51-30-5, 51-30-2, 51-10-6, 51-10-2, 51-20-1.

Part: FITTING — CRACKED (VERT STAB)

INSPECTION TYPE: SI. POSSIBLE CRACK IN ATTACH FITTING COMMON TO STR 11 UNDER PANEL 9780 RT VERT STAB (MARKED). REMOVED AND REPLACED ATTACH FITTING AT RT VERT STAB STR 11 PER 51-30-2 OF THE SRM.

Part: STRINGER — CORRODED (BS 680-700)

INSPECTION TYPE: SI. CORROSION AT STRINGER 12 RIGHT HAND BETWEEN BS 680-700. FOUND CORROSION TO BE OUT OF LIMITS, REPLACED STRINGER PER SRM'S 53-10-1, 51-10-2, 51-10-6, 53-10-2, 53-10-3.

Part: INTERCOSTAL — CORRODED (BS 211.8-219.8)

INSPECTION TYPE: SI. CORROSION ON INTERCOSTAL BS 211.8-219.8 LBL 25 WL 190. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED INTERCOSTAL PER SRM 53-30-2.

Part: STRINGER — CRACKED (BS 863)

INSPECTION TYPE: SI. STR 5R CRACKED ON LOWER FLANGE LIP STA 863. REPAIRED PER SRM'S 53-10-3, 51-10-2, 51-30-2, 53-10-3, 51-30-15.

Part: FRAME — CORRODED (BS 211.8)

INSPECTION TYPE: SI. CORROSION ON FRAME WEB BS 211.8 LBL 15-26 WL 165. REMOVED CORROSION FROM 211.8 FRAME WEB DOUBLER, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPLACED DOUBLER IAW SRM'S 51-30-5, 51-30-2, 51-20-1, ALSO, FOUND STIFFENERS TO BE CORRODED. REPLACED STIFFENERS IAW SAME ABOVE REFERENCES.

Part: STRINGER — CORRODED (BS 1070-1090)

INSPECTION TYPE: SI. CORROSION ON STR 4R STA 1070-1090 AND FRAME 1110-1130. REMOVED CORROSION FROM STR 4R STA 1070-1090, STA 1110-1130. ALL REWORK WITHIN LIMITS EXCEPT STA 1121-1123, REPAIRED STR 4R 1121-1123 IAW SRM 53-10-3.

Part: RIB — CRACKED (NR 1 LE FLAP)

INSPECTION TYPE: SI. NR 1 SLAT FIRST RIB INBOARD OF TAIL DUCT CRACKED AT T/E CHORD ATTACH POINT. REPAIRED NR 1 SLAT FIRST RIB INBOARD OF TAIL DUCT PER SRM 57-30-3.

Part: RIB — CRACKED (NR 1 LE SLAT)

INSPECTION TYPE: SI. NR 1 SLAT, NR 2 RIB FROM INBOARD OF TAIL DUCT CRACKED AT T/E CHORD ATTACH POINT. REPAIRED NR 1 SLAT NR 2 RIB FROM INBOARD OF TAIL DUCT PER SRM 57-50-3.

Part: RIB — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE: SI. NR 3 SLAT OUTBOARD END RIB IS CRACKED IN RADIUS. REMOVED AND REPLACED NR 3 SLAT O/B END RIB IAW SRM 51-30-2, 51-10-1.

Part: JUMPER — CORRODED (NR 6 LE SLAY)

INSPECTION TYPE: SI. NR 6 K-FLAP BULLNOSE BONDING JUMPER O/B UPPER ATTACH BOLT HAS PITTING AROUND BOLT HEAD. BLEND CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-50-0. K-FLAP ASSY WAS REPLACED ON NRC 597765.

Part: RIB — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE: SI. NR 3 SLAT 3RD RIB O/B OF ROD END ATTACH RIBS IS CRACKED IN RADIUS AT EXTRUDED CHORD ATTACH POINT. REMOVED AND REPLACED DOUBLER IAW SRM 57-50-3, 57-50-30.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE: SI NR 4 SLAT INBD TRACK INBD RIB HAS TEMPORARY STOP DRILLED CRACK IN FLANGE. REMOVED AND REPLACED SRM 51-30-2, 51-30-5, OHM 57-51-61.

Part: EEL ASSY — INOPERATIVE (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT WOULD NOT TEST DURING PREFLIGHT. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY.

Part: LE SKIN — CRACKED (LT ELEVATOR)

WHILE ON GROUND, MAINTENANCE FOUND REF D97427 LT ELEVATOR L/E 2 CRACKED. REPAIRED LT REV IAW 55-20-3 FIG 4. CALCULATED REPAIR WEIGHT TO BE 20 GRAMS AT O MOMENT, REPAIR WEIGHT WITHIN SRM 57-80-7.

Part: TEE — CORRODED (FS 760)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TEE AT FS 760, LBL 70.5, WL 200. REPAIRED IAW SRM 51-10-1, 51-30-2.

Part: WEB — CORRODED (FS 1175)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SHEAR WEB AT STA 1175, AT RBL 40. REPAIRED IAW SRM 51-40-2, 51-30-2.

Part: TEE — CORRODED (FS 760)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TEE AT FS 760, RBL 70.5, WL 200 ON THE I/B FLANGE. REPAIRED IAW SRM 51-10-1, 51-30-2.

Part: INTERCOSTAL — CRACKED (FS 303)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT STR 15L, FS 303. REPAIRED IAW SRM 51-40-3, 51-30-2.

Part: INTERCOSTAL — CRACKED (FS 303)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT STA 303, STR 16L. REPAIRED IAW SRM 51-40-3, 51-30-2.

Part: SHEAR TIE — DAMAGED (FS 294)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BROKEN SHEAR TIE FS 294, STR 9 TO 10L. REPAIRED IAW SRM 51-40-3, 51-30-2.

Part: SHEAR TIE — CRACKED (FS 294)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT FS 294 BETWEEN STRINGER 10L AND 11L. REPAIRED IAW SRM 51-30-2.

Part: WEB — CRACKED (FS 227)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED WEB AT STA 277 AT STR 14L AND 16L. REPAIRED IAW SRM 51-40-3, 51-30-2.

Part: SHEAR TIE — CRACKED (FS 294)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT FS 294, STA 8 TO 9L. REPAIRED IAW SRM 51-40-3, 51-30-2, B727-5310-1259.

Part: SEAT TRACK — CORRODED (FS 580-680)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LWR CARGO RT SEAT TRACK AT FS 580 TO 680. REPAIRED IAW SRM 51-10-1, 51-30-2.

Part: DOOR SWITCH — MALFUNCTION (RT MLG DOOR)

PILOT REPORTED RT GEAR DOOR LIGHT ON WITH HANDLE IN OFF POSITION. CYCLED GEAR, NO HELP. REMOVED AND REPLACED MAIN GEAR DOOR WARNING SWITCH IAW MM 32-62-11, OPS CHECK NORMAL.

Part: RETRACT MECH — MALFUNCTION (RT MLG)

PILOT REPORTED, RT MLG DOOR FAILED TO CLOSE AFTER TAKEOFF, CYCLED GEAR, SECOND TIME DOOR CLOSED, BUT SLOWLY. TESTED RT MAIN GEAR DOOR PER MM 32-12-01, CHECKS GOOD. NO PROBLEMS NOTED.