N906UP

Part: ANGLE — CORRODED (WS 383) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C SMALL AREA OF CORROSION NOTED IN R/H WING T/E STRUCTURE WS 383, ANGL E BETWEEN SUPPORT WEB & UPPER T/E SKIN REMOVED FASTNERS FROM CORRODED AREA AS PER SRM 51-30-02 & CUT AND TR IMMED ANGLE AS PER SRM 51-20-00. FABRICATED REPAIR PARTS IAW SRM 51- 40-04. FABRICATED PARTS INSTALLED IAW SRM 51-30-02

Part: SKIN — CRACKED (UPPER DOOR) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C ENGINE #1 THRUST REVERSER UPPER DOOR INNER SKIN CRACKED AT UPPER I/B CORNER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201

Part: LONGERON — CRACKED (LT NACELLE) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE: C, ENGINE NR 2, LT NACELLE. CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK (DOOR SHEAR). LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON MANUFACTURED IAW SRM 51-20-1. NEW LOGERON INSTALLED IAW SRM 51-30-02 & RE-PROTECTED

Part: LONGERON — CRACKED (#2 R/H) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C ENG. #2 R/H FWD COWL CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK(DOOR SHEAR) LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON FABRICATED IAW SRM 5 1-30-1 NEW LONGERON INSTALLED IAW SRM 51-30-02 & REPORTECTED IAW MM 51-20-01

Part: WEB — CRACKED (NOSE W/W R/H) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C SUSPECT CRACKS IN NOSE WHEEL WELL R/H WEB, JUST BELOW FWD END OF AFT PRESSURE PANEL REPAIR CARRIED OUT IAW SRM 51-40-2 & 51-30-2. REPAIR PARTS LEAK CEHC KED OK IAW MM 5-51-25

Part: SKIN — CRACKED (UPPER DOOR I/B) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C ENG. #1 THRUST REVERSER, UPPER DOOR, INNER SKIN CRACKED AT I/B OF CE NTER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE: C, ENGINE NR 1 & 3 THRUST REVERSER OUTBOARD FAIRING MID SUPPORT BRACKETS CRACKED. REPLACED BRACKETS IAW MM 20-80-01

Part: FITTING — CRACKED (TENSION TIE) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C L/H LWR TENSION TIE FITTING CRACKED AT O/B LUG IN TAILSKID COMPARTME NT INSTALLED NEW L/H LWR TENSION TIE FITTING IAW SRM 51-30-02 & DRAWING 65-25992

Part: FITTING — CRACKED (R/H TENSION TIE) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C TAILSKID BAY RH LWR TENSION TIE AFT FITTING HAS EVIDENCE OF CRACK INSTALLED NEW R/H LWR TENSION TIE FITTING IAW SRM 51-30-02 & DRAWING 65-25992

Part: BULKHEAD — CRACKED (NLG WW) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE: C, SUSPECT CRACKS IN NOSE WHEEL WELL BULKHEAD RT SIDE, BETWEEN FASTENER JUST UNDER CENTER OF FWD RT PRESSURE PANEL REPAIR CARRIED OUT IAW SRM 51-10-1 & SRM 51-40-2 FIG 2

Part: FITTING — CRACKED (TAILSKID BAY RH) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C TAILSKID BAY R/H UPPER TENSION TIE AFT FITTING CRACKED NEW R/H UPPER TENSION TIE AFT FITTING INSTALLED IAW SRM 51-30-02 AND DRAWING 65-25992

Part: FITTING — CRACKED (L/H TENSION TIE) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C TAILSKID BAY L/H UPPER TENSION TIE AFT FITTING CRACKED L/H UPPER TENSION TIE REPLACED IAW SRM 51-30-02 & DRAWING 65-25992

Part: ELEVATOR — CRACKED (ELEV. STA 47) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C X-RAY INSP. SHOWS A CRACK INDICATION ON THE RIGHT ELEVATOR JUST I/B OF THE TAB AT ELEV. STA. 47, APPROX. REPAIR CARRIED OUT IAW SRM 51-30-2,51-10-1, 55-20-3, 51-40-5, 51-10- 2 & DRAWING 65-25638

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE: C. SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL IN AREA ADJACENT TO AFT LOWER CORNER OF AFT PRESS PANEL REPAIR PARTS FABRICATED IAW SRM 51-40-2 FIG 1. REPAIR PARTS PROTECTED AS PER SRM 51-10-02. REPAIR PARTS ASSEMBLED AND FASTNERS INSTALLED AS PER SRM 51-30-02 & SRM 51-40-2 FIG 1 REMAINING FASTNERS INSTA LLED IAW SRM 51-30-02 & 51-40-2 FIG 1

Part: ELEVATOR — CRACKED (ELEV. STA 204) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE:C X-RAY INSPECTION SHOWS A CRACK INDICATION ON THE LEFT ELEVATOR AT EL EV STA. 204, APPROX 5" FWD OF THE TRAILING EDGE REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE: C, SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL AT UPPER FWD EN D OF AFT PRESSURE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2

Part: STRUCTURE — DAMAGED (LEADING EDGE) · airframe 40,622 hrs · 43,789 cycles

INSPECTION TYPE: C, RT LE, REMOVABLE SECTION, SOME SCREWS HAVE PULLED THROUGH ON UPPER SURFACE AT O/B END (INTERSECTION OF NR 6 KREUGER & NR 5 SLAT). REPAIR CARRIED OUT IAW SMRO EO 2002-057-003.

Part: LIGHT — UNSECURE (L1 DOOR)

INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT LENS COVER HANGING BY ONE END. FOUND FWD END OF EMERGENCY EXIT LIGHT ASSY NOT SECURED. SECURED LIGHT ASSY AND LENS. OPS CHECK GOOD.

Part: LENS — LOOSE (ENTRY DOOR)

INSPECTION TYPE:AS PLASTIC LENS FOR ENTRY DOOR EMERGENCY EXIT LIGHT FALLS OFF. REPLACED LIGHT LENS.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:IN ENTRY DOOR EMERGENCY LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT OVER ENTRY DOOR. OPS CHECK GOOD.

Part: GUARD — INOPERATIVE (COCKPIT)

INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS SWITCH GUARD IS INOP; WHEN LIGHTS ARE TURNED ON TO TEST & GUARD IS CLOSED, LIGHTS REMAIN ON INSTEAD OF MOVING TO ARMED POSITION. R&R EMERGENCY EXIT LIGHT SWITCH GUARD. OPS CHECKS NORMAL. PERFORMED EMERGENCY EXIT LIGHT OPS. CHECKS PER MM 33-50-01 CHECKS NORMAL.

Part: SKIN — CRACKED (L/E FLAP) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C, CRACK ON ANTI-ICE SKIN NR 3 L/E FLAP I/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW UPS EO B727-5750-3082.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C STRUCTURE ABOVE NR 2 ENGINE, WEB CRACKED AT BS 1388 APPROX RT SIDE. NEW WEB INSTALLED IAW SRM 51-30-02 & BOEING DRAWING 65-17555.

Part: WEB — CRACKED (L/E SLAT) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C NR 3 SLAT ANTI ICE WEB IS CRACKED AT CUTOUT FOR ANTI ICE DUCT. REPAIRED IAW UPS AUTORIZATION B727-57-20028 AND SMRO EO 2001-016-006.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C, SUSPECT CRACK IN LWR AFT CORNER OF FWD CARGO DOOR FRAME. REPLACED LWR AFT CORNER OF FWD CARGO DOOR FRAME IAW DRAWING 65-18620.

Part: STRAP — CRACKED (FUSELAGE) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C CRACK INDICATIONS IN REINFORCING STRAP AT MID GALLEY DOOR FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-2685.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C, CRACK ON AFT UPPER SECTION OF GALLEY DOOR FRAME. REPAIR CARRIED OUT IAW UPS EO B727-5240-4626.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C NDI ON BS 950 RT FITTING CONFIRMED CRACK ON OUTBOARD FLANGE BETWEEN S9R AND 10R. RT 950 FRAME FITTING REPLACED IAW UPS EO B727-5310-3011.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C MCD UPPER BEAM AND UPPER BEAM DOUBLER CORRODED. DOOR REMOVED AND UPPER BEAM AND UPPER BEAM DOUBLER REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C, FUSELAGE SKIN FOUND TO HAVE WEAR HOLE AT BS 1187 BETWEEN S24 LT & S26 LT SECT 48. REPAIR CARRIED OUT IAW SRM 53-30-3, 51-30-1, 51-20-00, 51-10-2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C, AREA OF SUSPECT CORROSION AT S4L BS 1185. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-00, 51-30-4.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 40,116 hrs · 43,207 cycles

INSPECTION TYPE:C, WING TO BODY FAIRING ATTACH BRACKET BS 945 S18A LT CRACKED. NEW BRACKET FABRICATED

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PFLT, ON PREDEPT CK FOUND COCKPIT EMERGENCY EXIT ASSY INOP IN ARM OR ON. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:IN ON PREFLIGHT CHECK EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WOULD NOT TEST WITH EMERGENCY EXIT LIGHT SWITCH ON O/H. LIGHTS WORK OK AT LIGHT ASSY W/SWITCH ON. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT COCKPIT DOOR. OPS CHECK OK PER MM 33-50-101.

Part: LIGHT — DETACHED (CABIN)

INSPECTION TYPE:PFLT CREW REPORTS MAIN ENTRY EMERGENCY EXIT LIGHT FELL OFF AT LANDING. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS NORMAL.

Part: GENERATOR — OVERHEATED (NR 3)

INSPECTION TYPE:N/A, A/C DECLARED EMERGENCY WITH SMOKE IN THE COCKPIT WITH A CORRESPONDING TRIP ON THE NR 3 GENERATOR BREAKER. AIRCRAFT DIVERTED TO KMDT. MAINTENANCE FOUND THE NR 3 GENERATOR VOLTAGE REGULATOR VERY HOT AND A DOMINATE ELECTRICAL SMELL IN THE AREA. AFTER CONSULTING WITH CAPTAIN DEFERRED THE NR 3 GENERATOR IAW MEL 24-1.

Part: CARTRIDGE — OUT OF ADJ (AILERON)

INSPECTION TYPE:N/A ATB-AILERON BINDING T/S PER MM CHAPT 27-10-00 PG 102,106,AND 107 ADJUSTED AILERON SPRING CARTRIDGE PER MM 27-10-00 OPS CHECKS GOOD ***SUPPLEMENTAL MRR***

Part: LIGHT — MALFUNCTIONED (CABIN)

L-1 DOOR EMERGENCY LIGHTS DIM. RESEATED L-1 DOOR EMERGENCY LIGHT PACK, LIGHT CHECKS NORMAL PER MM 3 3-50-01.

Part: SUPPORT — CRACKED (LT WING)

INSPECTION TYPE:C LEFT WING FIXED LEADING EDGE CAVITY VERTICLE OUTBOARD SUPPORT IS CRACKED FOR THE NR 2 SLAT INBOARD TRACK, INBOARD SUPPORT RIB. REPLACED LEFT WING FIXED LEADING EDGE CAVITY VERTICAL OUTBOARD SUPPORT AS PER SRM 57-20-03 FIG 2. MATERIAL USED 7075-T6.

Part: ENGINE — MALFUNCTIONED (NR 2)

INSPECTION TYPE:N/A ON TEST FLIGHT, PERFORMED TEST EVENT SHUT DOWN OF NR 2 ENGINE. ENGINE NR 2 WAS THEN RESTARTED WITH ALL PARAMETERS NORMAL. MINUTES LATER AS NR 2 ENGINE WAS ADVANCED TO CRUISE SETTING, ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. PRECAUTIONARY SHUTDOWN ACCOMPLISHED.

Part: SKIN — CORRODED (BS 1080)

INSPECTION TYPE-S, CORROSION BEYOND LIMITS FS 1080 STR 17R EXTERNAL FUSELAGE SKIN. REPAIRED IAW SRM 53-30-3.

Part: LIGHT — INOP (PAX DOOR)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT AT MAIN PAX DOOR INOP. RELAMPED, OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 760-848)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM ON AND AT NUT PLATES BS 760 TO 848 LBL 45 WL 208. CORRODED PART OUT OF LIMITS. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2, 51-10-2, 51-20-21, 51-20-151, 51-30-4.

Part: BULKHEAD — CORRODED (BS 1183)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON BS 1183 BULKHEAD RBL 15 WL 178. REMOVED CORROSION AND ACCOMPLISHED EO B727-5311-0635 WITH THE ADDITION OF EXTENDING THE RBL 8 BULKHEAD DOUBLER TO ENCOMPASS THE CORRODED AREA.

Part: BRACKET — CORRODED (FUSELAGE)

INSPECTION TYPE:SI, CORROSION AROUND EXPANSION LINK BRACKET. REPLACED BRACKET PER SRM 53-10-1.

Part: SKIN — CORRODED (BS 1120-1150)

INSPECTION TYPE-SI, DISHED RIVETS AND PILLOWED SKIN STA 1120 TO 1150 LT 3 STR TO STR 4 LT AND 3 STR RT TO 4 STR RT. REPLACED SKIN PER EO 98-2608.

Part: SEAT TRACK — CORRODED (BS 760-785)

INSPECTION TYPE:SI, SEAT TRACK CORRODED BS 760-785 RBL 25. REPLACED TRACK PER SRM 53-10-5.

Part: LINK — CORRODED (BS 870)

INSPECTION TYPE:SI, CORROSION ON EXPANSION LINK BS 870 RBL 25. REPLACED PER DRAWING 65-34144.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION TYPE:SI CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM. REPLACED PER DWG 65-34144.

Part: FLOORBEAM — CORRODED (BS 740)

INSPECTION TYPE:SI CORROSION (C53-224-01.05-02) AND CHAFFING ON UPPER BS 740 FLOORBEAM UPPER FLANGE, RBL 0-45, WL 208, MARKED. REMOVED COROSION FOUND TO BE OUT OF LIMITS, REPLACED CHORD AS PER SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 336)

INSPECTION TYPE-SI, WHILE WORKING FUSELAGE 88 CUSTOMER ID NR 832295 FOUND CORROSION ON NLG WHEEL WELL STIFFENER BS 336, LBL 14, WL 158. OUT OF LIMITS. REPAIRED PER SRM 51-10-6, 53-10-1, 53-10-2, 51-30-2, 51-20-151.

Part: TRACK — CORRODED (NR 7 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-06.00-04) NR 7 FLAP TRACK FWD LUG HAS RUST AROUND BOLT HOLE. REMOVED FLAP TRACK AND SENT TO OUTSIDE SERVICES FOR REPAIR AND REINSTALLED AFTER REPAIR.

Part: TRACK — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE-SI, NR 3 FLAP TRACK CENTER MOUNT BOLT IS CORRODED ON THE AFT SIDE CORROSION (C57-581-06.00-03) AND CORROSION (C57-581-06.00-03) NR 3 FLAP TRACK IS CORRODED ON THE SPOILER BEAM MOUNT PAD. FLAP TRACK REMOVED AND SENT TO OUTSIDE SERVICES FOR REPAIR. REINSTALLED AFTER REPAIR.

Part: TRACK — CORRODED (NR 1 TE FLAP)

INSPECTION TYPE-SI, NR 1 FLAP TRACK FWD MOUNT BOLT LUGS ARE CORRODED. REMOVED FLAP TRACK AND SENT TO OUTSIDE SERVICES FOR REPAIR AND REINSTALLED AFTER REPAIR.

Part: RIB — CRACKED (WS 6565)

INSPECTION TYPE-SI, CRACK INDICATION NOTED ON LT WING RIB AT WS 6565 STR 6 LOWER. REMOVED CRACKED RIB REPLACED WITH NEW RIB IAW EO B727-5710-1325D.

Part: RIB — CRACKED (WS 656.5)

INSPECTION TYPE-SI, CRACK INDICATION NOTED ON RT WING RIB AT WS 656.5 STR 6 LOWER. REPLACED CRACKED RIB WITH NEW RIB PER EO B727-5710-1325.

Part: STRINGER — CORRODED (BS 291)

INSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON STR 1 AT STA 291. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED AREA OF STRINGER AND FABRICATED REPAIR PARTS IAW SRM 53-10-3 SRM 53-10-4.

Part: FLOORBEAM — CORRODED (BS 740)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON NUT PLATES AT BS 740 FLOORBEAM RBL 60 TO LBL 60 WL 208. REMOVED FLOORBEAM AT BS 740 LBL 6, RBL 60, INSTALLED FABRICATED FLOORBEAM IAW SRM 51-30-2, 53-104.

Part: ANGLE — CRACKED (BS 804)

INSPECTION TYPE-SI, POSSIBLE CRACK IN FLOORBEAM SUPPORT ANGLE BS 804, LBL 46, WL 206. FLOORBEAM SUPPORT CRACKED, VERIFIED BY NDI. REPLACED SUPPORT ANGLE PER 727 SRM 51-30-2 AND 51-10-1.

Part: SEAT TRACK — CORRODED (BS 760-850)

INSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 850 LBL 65 BL 208. REPLACED SEAT TRACK EXTRUSION BS 760 TO 850 LBL 65 WL 208 PER 727 SRM 51-30-2. ALSO, REFERENCE NRC 832521 REPLACED L-ANGLES PER SRM 51-20-1 AT BS 804.

Part: ANGLE — CRACKED (BS 804)

INSPECTION TYPE-SI, POSSIBLE CRACK IN FLOORBEAM SUPPORT ANGLE BS 804, LBL 46, WL 206. FLOORBEAM SUPPORT CRACKED, VERIFIED BY NDI. REPLACED SUPPORT ANGLE PER 727 SRM 51-30-2 AND 51-10-1.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE:SI CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 344 FROM LBL 25 TO RBL 15. REMOVED AND REPLACED UPPER CHORD AT FLOOR BEAM IAW SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 760-848)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760 TO 848, WL 208 RBL 45. REPLACED LONGITUDINAL FLOORBEAM AND SEAT TRACK (NRC 832504) BS 760 TO 848 PER SRM 51-30-2.

Part: SKIN — CORRODED (BS 679)

INSPECTION TYPE:SI CORROSION (C53-111-01.01-02) ON INTERNAL SKIN SURFACE OF LWR LAP JOINT AT BS 679 ABOVE STR 19L. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLERS PER 727 SRM 53-30-3.

Part: EXPANSION LINK — CORRODED (BS 860)

INSPECTION TYPE:SI, WHILE WORKING INTERIOR 140 CUST NR 832471 FOUND STA 860 RBL 45 EXPANSION LINK CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1.

Part: SEAT TRACK — CORRODED (BS 760-848)

INSPECTION TYPE:SI CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760-848, WL 208 RBL 45. REPLACED LONGITUDINAL FLOORBEAM AND SEAT TRACK (NRC 832504) BS 700 TO 848 PER SRM 51-30-2.

Part: DOUBLER — CRACKED (BS 305)

INSPECTION TYPE:SI BONDED DOUBLER ON TOP SURFACE OF NLG (DOGHOUSE) IS CRACKED AT BS 305 LBL 2 WI L181. REPLACED DOUBLER 16.5 BY 24.5 LBL 14 TO RBL 14 PER 727 SRM 51-40-2, 51-30-2, 51-40-2. BONDED PER BAC5514-551 AND 5514-5101 AND DRAWING 65-18417 AND REPLACED STIFFENER BS 306 LBL 15 TO RBL 15 DUE TO OUT OF LIMITS CORROSION.

Part: FLOORBEAM — CORRODED (BS 760-848)

INSPECTION TYPE:SI CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760-848 LBL 25 WL 208. REPLACED LONG FLOORBEAM BS 760 TO 840 LBL 25 WL 208 AND EXPANSION LINK FROM 850 TO BS 870 PER 727 SRM 53-10-1 AND 51-30-2 EXPANSION LINK BS 850 TO 870 WILL BE REPLACED ON NRC 832520.

Part: STRINGER — CORRODED (BS 480-500)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-02) ON STR 22R BS 480-500. REPLACED 22R STR CHANNEL BS 480 TO 500 PER 727 SRM 53-10-3.

Part: FITTING — CRACKED (BS 1183)

INSPECTION TYPE:SI CRACK IN LT INBOARD 3A BOLT FITTING BS 1183 STRINGER 3A LT INBRD FITTING FWD FITTING. REPLACED FITTING 65-25591-9 PER SRM 51-10-1 AND MM 51-20-31.

Part: STRINGER — CORRODED (BS 312)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 21R BS 312. REPLACED STRINGER CHANNEL FROM BS 292 TO 315 IAW SRM 51-10-7, 53-10-1 AND 53-10-3.

Part: FLOOR TRACK — CORRODED (BS 568-582)

INSPECTION TYPE:SI SEAT TRACK HAS CORROSION UNDER NUT CLIPS BS 568-582 LBL 25 WL 208. REPLACED SEAT TRACK EXTRUSION FROM 540 TO 615 PER SRM 53-10-5, 53-10-2, 51-20-151, 51-30-2.

Part: SEAT TRACK — CORROSION (BS 599-607)

INSPECTION TYPE:SI SEAT TRACK HAS CORROSION BS 599 TO 607 LBL 25 WL 208. REPLACED SEAT TRACK BS 540 TO 615 LBL 25 PER 727 SRM 53-10-5, 51-30-2, 53-10-1.

Part: FRAME — CORRODED (BS 294)

INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) ON FRAME AT STA 294 LBL 57 WL 236-239. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-40-3.

Part: FRAME — CORRODED (BS 294)

INSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON FRAME AT STA 294 LBL 57 WL 236 TO 239. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-40-3.

Part: STRINGER — CORRODED (BS 474)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 24F BS 474. REPLACED STRINGER FROM BS 470 TO BS 490. INSTALLED STRINGER SECTION AND SPLICE PLATES PER 727 SRM 53-10-1, 53-10-3.

Part: FITTING — CORRODED (WING/FUSELAGE)

INSPECTION TYPE:SI RIGHT WING REAR SPARS BOTTLE PIN AND BODY SIDE ARE DAMAGED (CORROSION C53-100-05-4B). REMOVED BUSHING FOUND CORROSION OUT OF LIMITS IAW SRM 53-40-1 AND HAD BOEING REPAIR IAW DRAWING 65C36301 AND BOEING AGREEMENT NR 6-1171-TA954.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT FASTENER HOLE BS 312, LBL 3, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8, 51-30-5, 51-30-2 AND MM 51-20-151.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT FASTENER HOLE BS 312, LBL 3, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8, 51-30-5, 51-30-2, AND MM 51-20-151.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT BS 328 LBL 45. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGE FROM BEAM AND INSTALLED STANDARD REPAIR PER SRM 53-10-8, 53-10-2 AND 51-30-2.

Part: BRACKET — CORRODED (BS 203.8)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON NOSE COMPARTMENT DOOR STOP BRACKET, FWD SIDE OF BS 203.8 BRACKET, LBL 8. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. NEW FITTING INSTALLED IAW SRM 52-40-21 AND SRM 51-30-2.

Part: SPLICE — CORRODED (BS 443)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 25R SPLICE AT BS 443. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-5, 51-30-2, AND MM 51-30-00.

Part: SPLICE — CORRODED (BS 443)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 25R SPLICE AT BS 443. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-5, 51-30-2 AND MM 51-30-00.

Part: SPLICE — CORRODED (BS 436)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 25L SPLICE AT BS 442, BS 436. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, INSTALLED NEW SPLICE PER SRM 51-30-2, 51-30-5 AND SRM 51-30-6.

Part: SPLICE — CORRODED (BS 442-436)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 25L SPLICE AT BS 442, BS 436. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-2, 51-30-5, AND SRM 51-30-6.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY, BOTH BATTERY PACK WITH SERVICEABLE PACKS ROBBED FROM A/C 907.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERG LIGHT STAYS ON. REPLACED LIGHT ASSY, CHECKS OK (P/N 10-0067-9), (S/N 4249) ON, (S/N UPS1730) OFF.

Part: TRUNNION — WORN (RT MLG)

INSPECTION TYPE: SP. RIGHT MLG TRUNNION FITTING HAS 4 EACH OUT OF ROUND HOLES AT LOWER REAR SPAR STA. 224.5. HOLES GO THROUGH FITTING, LOWER REAR SPAR AND REAR SPAR WEB. ITEM FOUND WHEN FITTING WAS REMOVED FOR FUEL LEAK. OVERSIZED HOLES IAW DHC SK-906-848. REF. ENRG FILE NR 727-57-1786.

Part: SEAT TRACK — CORRODED (BS 480-500)

INSPECTION TYPE-C, BS 480 TO 500 RBL 65 WL 208 THERE IS CORROSION IN THE SEAT TRACK WELL. REPLACED SEAT TRACK PER SRM 53-10-5, 51-30-2.

Part: THRESHOLD — CRACKED (BS 676)

INSPECTION TYPE-C, AFT CORNER THRESHOLD, AFT FRAME IS CRACKED AT BS 676 WL 215 RBL 67. REPLACED WITH NEW PART IAW SRM 51-30-3, 51-30-2, 51-20-4.

Part: FITTING — CORRODED (BS 364)

INSPECTION TYPE-C, CARGO NET ATTACHMENT FITTING CORRODED AT BS 364 RBL 56 WL 206. REPLACED WITH NEW PART IAW SRM 51-30-2, 51-20-1, 51-30-5.

Part: FITTING — CORRODED (BS 364)

INSPECTION TYPE-C, CARGO NET ATTACHMENT FITTING CORRODED AT BS 364 LBL 39 WL 206. REPLACED WITH NEW PART IAW SRM 51-30-2, 51-10-2, 51-20-151.

Part: SPAR — CRACKED (NR 4 SLAT)

INSPECTION TYPE-C, NR 4 SLAT AFT SPAR CRACKED AT O/B END. INSTALLED DOUBLERS PER SRM 51-40-4.

Part: THRESHOLD — CORRODED (PAX DOOR)

INSPECTION TYPE-C, CORROSION AROUND THE UPPER AND LOWER NUTPLATE AREA ON THE FWD ENTRY DOOR LOWER SILL THRESHOLD ATTACH ANGLES WL 208 LBL 60 TO 67. REMOVED ALL CORROSION TO WITHIN LIMITS. REMOVED AND REPLACED AFFECTED PARTS SRM 53-10-01, 51-30-02.

Part: FITTING — CORRODED (BS 364)

INSPECTION TYPE-C, CARGO NET ATTACH FITTING CORRODED AT BS 364 LBL 5 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED FITTING IAW SRM 51-10-1, 51-10-2, 51-10-6, 51-30-2, 51-30-5.

Part: RIBS — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE-C, R/W NR 6 SLAT ACTUATOR RIBS CRACKED AT AFT FASTENER HOLE BOTH SIDES OF ACTUATOR. SLAT WAS REPLACED ON NRC 494364 IAW M/M 27-81-11.

Part: PACK — FAILED (LT PACK)

CREW REPORTED, DURING TAKEOFF THRUST AND CLIMBOUT INCREASINGLY BAD FUMES AND SMELL. TURNED OFF NR 1 BLEED AND NR 1 PACK, SMELL WENT AWAY. LATER USED NR 2 BLEED TO SUPPLY NR 1 PACK AND SMELL AND FUMES WERE NOT EXISTANT. DEFERRED MAINTENANCE ITEM ASSIGNED PER MEL 21-1-2, LEFT PACK INOP DUE TO SIGNIFICANT OIL RESIDUE IN COLD AIR DUCTING DOWNSTREAM OF AIR CYCLE MACHINE UP TO AND THROUGH THE WATER SEPARATOR. ALSO, OIL RESIDUE IN 35 DEGREE VALVE DUCTING.

Part: ACM — MALFUNCTIONED (LEFT)

CREW REPORTED, BTB DUE TO SMOKE IN FLIGHT DECK. RAN ENG 1 AT A TIME, ISOLATED PROBLEM TO LT PACK AND DEFERRED PACK PER MEL. REMOVED AND REPLACED LT AIR CYCLE MACHINE PER MM 21-51-12 PG 401. OPS CHECK OFF APU AND ALL ENGS DURING TAXI, NO DEFECTS NOTED.

Part: FITTING — CRACKED (RT MLG)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK INDICATION DURING INSPECTION OF RT MLG FWD TRUNNION BEARING SUPPORT FITTING. INSTALLED NEW TRUNNION SUPPORT FITTING IAW OHM 32-10-13, MM 32-11-51, MM 32-11-01.

Part: FITTING — CRACKED (FS 941)

WHILE IN C-CHECK, MAINTENANCE FOUND LINE OF CORROSION BETWEEN FASTENERS STATION 941, RBL 58 TO 59, WL 207 TOP FLANGE OF FRAME FITTING, POSSIBLE CRACK. REPAIRED PER EWO 95-2805 AND UPS EO B727-5310-7200-A.

Part: INTERCOSTAL — CRACKED (BS 1110-1130)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT BS 1110 TO 1130 RBL 6 WL 152. REPLACED IAW SRM 53-10-2, 51-20-21, 51-10-2, M/M 51-20-00.

Part: END CAP — CRACKED (RT TE FOREFLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RIGHT WING O/B FOREFLAP I/B END CAP CRACKED ON UPPER SURFACE. REPLACED IAW SRM 51-30-2, 51-10-2.

Part: ANGLE — CORRODED (BS 296)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SUPPORT ANGLE AT BS 296 LBL 14 WL 180. REPLACED IAW SRM 51-10-6, 53-10-1, 51-30-5, 51-10-2, 51-30-2, 51-20-4.

Part: SKIN — DELAMINATED (NR 13 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 13 SPOILER DELAMINATED ON THE UPPER SURFACE LEADING EDGE AT CENTER HINGE FITTING. REPAIRED WITH FIBERGLASS AND RESIN IAW SRM 57-50-6.

Part: FITTING — CRACKED (LT MLG)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK INDICATION DURING INSPECTION OF LT MLG FWD TRUNNION BEARING SUPPORT. INSTALLED NEW TRUNNION SUPPORT FITTING IAW MM 32-11-01, MM 32-11-01, MM 32-32-11.

Part: EEL — INOP (FLIGHT DECK)

PILOT REPORTED EMERGENCY EXIT UNARMED. INDICATOR LIGHT WILL NOT TEST OR ILLUMINATE WHEN DISARMED. CHANGED LIGHT BULB, NO HELP. RELAMPED, OPS CHECKED OK.

Part: LT PACK — SMOKE (CABIN)

PILOT REPORTED, FUMES IN FLIGHT DECK AFTER T/O (SIMILAR TO PREVIOUS PROBLEM) LEFT PACK WAS SHUT OFF AND FUMES DIMINISHED. INSTALLED REPAIR. RAN PACKS, OPS CHECK GOOD. OK FOR SERVICE.

Part: HYD SYST — OVERSERVICED (LWR FUSELAGE)

PILOT REPORTED, AIR CONDITIONING FUMES STILL EVIDENT ESPECIALLY AT HIGH POWER SETTING. FOUND HYDRAULIC SYSTEM OVERSERVICED. DRAINED HYD FLUID TO PROPER LEVEL.