N919UP

Part: SKIN — CRACKED (BS 348)

3 INCH CRACK ON FUSELAGE SKIN AT 10 O'CLOCK POSITION RUNNING FWD AND AFT AT STA 348.2, BETWEEN STRINGERS 5L & 6L. ADDITIONAL DISBONDING APPROXIMATELY 4 X 4 INCHES. C/W EO B727-5330-25585A TO FERRY A/C TO BFM 9014 D337794 ISSUED.

Part: SLIDE — DISLODGED (CABIN)

FOUND DOOR SLIDE ON FLOOR. RE-INSTALLED ESCAPE SLIDE PER 25-60-14-2.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS ABOVE THE MAIN ENTRY DOOR AND ABOVE THE COCKPIT ENTRY DOOR ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON MAIN ENTRY DOOR PER MM 33-50-90-2. REMOVED AND REPLACED BATTERIES ON COCKPIT ENTRY DOOR. OPS CHECK GOOD.

Part: SLIDE — DISLODGED (MAIN PAX DOOR)

INSPECTION TYPE: NA ESCAPE SLIDE FELL OUT OF CASE ON MAIN ENTRY DOOR REPLACED ENTRY DOOR EVACUATION SLIDE IAW MM 25-60-14-2.

Part: BATTERY — INOPERATIVE (LIGHT)

INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CK NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AS REQUIRED.

Part: FAIRING — DELAMINATED (LT WING)

DELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERRED FOR REPEAT INSPECTION EVERY 30 DAYS AND PERM BY C-CK. NR D 325051 ASSIGNED INSTALLATION OF PANEL IN ON L/P 543424 #3.

Part: SKIN — CORRODED (BS 1385 TO 1485) · airframe 49,748 hrs · 51,314 cycles

INSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND CORRODED AND CHORD REMOVED. NEW CHORD SPLICE IN WITH REPAIR ANGLES AND SKIN REPLACED IAW UPS AUTH 727-53-20187 AND 727-55-20049.

Part: STIFFENER — CORRODED (BS 870) · airframe 49,748 hrs · 51,314 cycles

LT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1.

Part: STIFFENER — CORRODED (BS 870) · airframe 49,748 hrs · 51,314 cycles

RT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 49,748 hrs · 51,314 cycles

FLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2.

Part: INTERCOSTAL — CORRODED (BS 294.5 - 312) · airframe 49,748 hrs · 51,314 cycles

INSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02.

Part: SUPPORT — CORRODED (BS 302-344) · airframe 49,748 hrs · 51,314 cycles

INSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW SRM 51-10-2, 51-20- 2 & 51-30-2.

Part: SKIN — CORRODED (BS 355 S8-10) · airframe 49,748 hrs · 51,314 cycles

AREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30-1 MM 25-21-2 AND AAAE EO 200 5-077-001 UPS ENGINEERING FILE NO. B727-5330-22744-A.

Part: ATTACH ANGLE — CORRODED (BS 294.5) · airframe 49,748 hrs · 51,314 cycles

RT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2.

Part: WEB — CORRODED (BS 294.5) · airframe 49,748 hrs · 51,314 cycles

INSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40-2.

Part: LIGHT — INOPERATIVE (L1 DOOR)

L1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8.

Part: DOOR FRAME — CORRODED (TAIL SKID) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61.

Part: SUPPORT — CORRODED (NR 12 SPOILER) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.

Part: SKIN — BULGED (FUSELAGE) · airframe 49,254 hrs · 50,915 cycles

INSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOSS OF 15-20 PERCENT. DUE TO EXCESS MATERIAL LOSS IND ON SKIN PNL ABOVE & GOUGE IN SAME SKIN PNL BEYOND LIMITS REPLACED SKIN PNL BETWEEN BS 259.5 & BS 360, 19L - 24L IAW SRM 51-30-02.

Part: TORQUE TUBE — LOOSE (RT MLG)

INSPECTION TYPE:N/A ATB-AFTER T/O, LG RAISED AND RIGHT MAIN GEAR STAYED DOWN. RED GEAR LIGHT AND DOORS LIGHT REMAINED ON. GEAR CAME DOWN NORMALLY. REPLACED 6 EA SHEARED RIVETS ON UPLOCK TORQUE TUBE, OPS CHECKS GOOD PER MM 32-30-00.

Part: BATTERY — DISCHARGED (COCKPIT)

COCKPIT EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERIES, OPS CHECKS GOOD, BATTERIES IAW MM 33-50-01.

Part: CONTACTOR — DIRTY (CABIN)

EMERGENCY EXIT LIGHTS INOP. REMOVED LIGHT ASSY OVER CREW CABIN DOOR, CLEANED CONTACTS, OPS CK OK IAW MM 33-50-01.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT L1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT COCKPIT. REPLACED BATTERIES, OPS CHECK GOOD.

Part: LIGHT — NOT SEATED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE CABIN DOOR INOP. SEATED EXIT LIGHT ASSY OPS CHECKS GOOD

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM 33-50-01.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN FWD EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OP CHECK GOOD IAW MM 33-50-01.

Part: COVER — LOOSE (CABIN)

INSPECTION TYPE:PFLT CABIN EXIT LIGHT COVER OVER CABIN DOOR IS LOOSE. CHECK SECURITY OF EXIT LIGHT ASSY PER MAINT PRACTICES MM 33-50-01 AND INSTALLED LIGHT COVER, NO DEFECTS NOTED.

Part: LIGHT — NOT SEATED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS DIM, RESEATED LIGHT ASSY. OPS CHECKS GOOD PER MM 33-50-101.

Part: FAIRING — CRACKED (T/E FLAP)

INSPECTION TYPE:PFLT LT INBD FLAP LT OUTBD CANOE FIXED FAIRING HAS A CRACK ON AFT UPPER CORNER OF PREVIOUS REPAIR. DEFFERRED PER MMOC

Part: ACTUATOR — LEAKING

INSPECTION TYPE:N/A RIGHT MAIN GEAR DOOR OPENED ENROUTE GEAR HANDLE PLACED TO "UP" POSIT ION DOOR CLOSED GEAR HANDLE RETURNED TO "OFF" POSITION OPS NORMAL ****SUPPLEMENTAL MRR*** REMOVED AND REPLACED GEAR DOOR ACTUATOR R/H PER MM 32-32-81 ADJ TEST GROUND DOOR MECHANISM PER 32-34-00 ADJ DOOR WARNING SWITCH REF 32-62 -11. JACKED AIRCRAFT PER MM 7-11-00. SWUNG GEAR. OPS CHECK NORMAL

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C-CK, CRACK AT FUSELAGE FRAME BS 930 ABOVE STR 13L. CUT OUT DAMAGE SECTION OF FRAME BETWEEN STR 12L & 13L. INSTALLED FORMED ANGLE REPAIR, HEAT TREATED.

Part: STRINGER — CORRODED (FUSELAGE)

INSPECTION TYPE:C-CK, STRINGER 18 LEFT CORRODED BETWEEN BS 440 TO BS 460. REMOVED CORROSION ON STRINGER FLANGE. FOUND OUT OF UNIT. INSTALLED STRINGER REPAIR.

Part: FITTING — CRACKED (L WING SPAR)

INSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CRACK MIGRATING FROM OB BOLT. REMOVED FITTING LT WING FRONT SPAR INTERIOR LBL 70.5 V SHAPE. INSTALLED LT WING UPPER FRONT SPAR CONER NEW FITTING & TORQUE BOLTS.

Part: DUCT — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS. 1 EA 4 INCH CRACK 93 INCHES FROM AFT EDGE 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR.

Part: INTAKE DUCT — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 6 INCH CIRCUMFERENTIAL CRACK AT 4 O''CLK APPROX 30 INCHES AFT OF WHERE S-DUCT ATTACHES TO INLET. CUT OUT DAMAGED AREA APPROX 7 X 1 INCHES. PERFORMED NDT AND NO CRACK INDICATIONS. INSTALLED SKIN DOUBLER AND RIB REPAIR.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C-CK, LOW FREQ EDDY CURRENT INSP OF SKIN AT BS 441 BETWEEN STRG 18R & 19R HAS INDICATION OF CORROSION LOSS GREATER THAN 10 PERCENT. REMOVED EQUIPMENT TO ACCESS REPAIR, CUT DAMAGED AREA AND INSTALLED REPAIR PER EO -1371.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:C-CK, FUSELAGE SKIN HAS CORROSION BULGE AND APPROX 3 INCH LATERAL CRACK. REMOVED FASTENERS, REMOVED CORROSION. NDT INSP C/W CUT DAMAGE AREA AND INSTALL DOUBLER REPAIR AT FUSE SKIN.

Part: DUCT — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS 2 EA APPX 100-104 INCH FROM AFT EDGE. 1 EA 7 INCH Y SHAPED CRACK & 1 EA 1.5 INCH CRACK APPX 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR. HEAT TREATED.

Part: DUCT — CRACKED (NR 2 ENG)

INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AFT EDGE AT 3 O''CLOCK. CUT OUT DAMAGE AREA. INSTALLED REPAIR.

Part: LAP JOINT — BULGED (FUSELAGE)

INSPECTION TYPE:C CK LAP JOINT 19RT HAS SKIN BULGE AT BS 620. CUT OUT DAMAGED SKIN LWR & UPPER AREA. INSTALLED REPAIR PART AT LAP JOINT STR 19 BS 620.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C CHECK LT W/W LWR SECTION OF BS 930 FRAME SHOWS CRACK TO AFT CENTER SECTION WHERE REPAIR NOT INSTALLED. ACCOMPLISHED STA 930 RT & LT FRAME REMOVAL & REPLACEMENT.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PFLT EMER. EXIT LITE INOP. REPLACED COCKPIT EMER. LIGHT ASSY. OPS NORMAL.

Part: SLAT — MALFUNCTIONED (NR 6)

ATB - NR 6 SLAT FAILED TO RETRACT RETURNED TO BFI. REPLACED NR 5, NR 6 AND NR 7 SLAT AND ADJUSTED PER M/M27-81-11 PAGE 401 NR 6 P/N ON 65-16222-92, OFF 65-16222-2, S/N ON BN81, OFF 319.

Part: SKIN — CORRODED (BS 620)

INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN IS BULGED FROM STR 1 TO STR 4 RT BS 620. REMOVED AND REPLACED UPPER FUSELAGE EXTERIOR SKIN FROM BS 520 TO BS 740 FROM STR 6 LT TO 4 RT AS PER AVITAS REPAIR ORDER 99 AVHM 048RO- 1. PREVIOUSLY ACCOMPLISHED WITH N/R 985901 AND 985502.

Part: SKIN — CORRODED (BS 620)

INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN AT SKIN LAP STR 4 RT BS 620 IS BULGED. REMOVED AND REPLACED UPPER FUSELAGE EXTERNAL SKIN FROM BS 520 TO BS 740 FROM STR 6 LT TO 4 RT AS PER AVITAS REPAIR ORDER 99 AVNM 048RO-1, PREVIOSLY ACCOMPLISHED WITH N/R 985901 AND 985502.

Part: SKIN — DENTED (CARGO DOOR)

INSPECTION TYPE:C, MAIN CARGO DOOR EXTERIOR SKIN IS DENTED 6 INCHES BELOW THE DOOR HINGE BS 548. REWORKED MAIN CARGO DOOR EXTERIOR SKIN BS 548 AS PER SRM 51-40-1, DENT OUT OF LIMITS. CUT OUT SKIN DAMAGED AREA AS PER B727 SRM 52-00-3, INSTALLED DOUBLER PER B727 SRM 52-00-3 PAGE 1.

Part: SKIN — CORRODED (BS 480)

INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN IS BULGED AT STR 4 RT TO STR 5 RT BS 480. REMOVED AND REPLACED SKIN FROM BS 440 TO BS 520 FROM STR 10 LT TO 4 RT AND INSTALLED SKIN REPAIR FROM BS 440 TO BS 540 AND FROM STR 4 RT TO STR 5 RT AS PER AVITAS REPAIR ORDER 99AVHM049RO-1, PREVIOUSLY ACCOMPLISHED WITH N/R 985901 AND 985502.

Part: SKIN — CORRODED (BS 477)

INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR REPAIR DOUBLER IS BULGED AT STR 5 RT BS 477. REMOVED AND REPLACED UPPER FUSELAGE EXTERIOR SKIN FROM BS 440 TO BS 520 FROM STR 10 LT TO 4 RT AND INSTALLED SKIN REPAIR FROM BS 440 TO BS 540 FROM STR 4 RT TO 5 RT AS PER AVITAS 99 AVM 048 RO-1 PREVIOUSLY ACCOMPLISHED WITH NR'S 985901 AND 985502.

Part: LIGHT — MISSING (FLIGHT DECK)

INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT PACK IAW MM 33-50-01, OPS CKS GOOD PER MM 33-50-01. (P/N 10-0067-9), (S/N 10894) INSTALLED.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR ANNUNCIATOR ILLUMINATED INLIGHT. AIRCRAFT PRESSURIZATION NORMAL. ATB 0245Z DOOR WARNING SYSTEM DEFERRED. CONTROL NR M171685, MEL 5-2-4. DOOR VISUALLY CHECKED BY RFD MX. AT SDF, ADJUSTED FWD CARGO DOOR SWITCH PER M/M 52-70-01. OPS CHECK NORMAL. DEFFERAL CLOSED.

Part: BATTERIES — DISCHARGED (CABIN)

EMER EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN BOTH EMER EXIT LIGHT ASSY. OPS NORMAL.

Part: MIX VALVE — INOPERATIVE (LT PACK)

INSPECTION TYPE-N/A, FUMES SMELLED IN COCKPIT LIKE BURNING RUBBER. CHECKED CARGO AREA AND NO FUMES DETECTED. *S/D* REMOVED AND REPLACED LEFT PACK MIX VALVE DUCT (P/N 65-23579-2) OPS CHECK LEFT PACK OK. THIS CLEARS M120048 PLACARD REMOVED.

Part: BLEED AIR SO VLV — INOPERATIVE (NR 2 ENGINE)

INSPECTION TYPE-N/A, SMELL/ODOR OF BURNT OIL/RUBBER WHEN USING NR 1 BLEED AIR FOR LEFT PACK SMELL GOES AWAY WHEN AIR SOURCE SWITCHED TO ENG NR 2. NR 1 ENG BLEED AIR S/O VALVE INOP, PER MEL 36-6-1-2 M-116899.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE: C. 940 FRAME FITTING RT SIDE IS CRACKED IN 3 PLACES, 1 ON FRONT AND 2 ON AFT SIDE. REPAIRED 940 FITTING RT SIDE IAW EO'S B727-5310-3737A, B727-5310-1001A.

Part: CLIP — CORRODED (BS 312)

INSPECTION TYPE: C. CORROSION ON FRAME CLIP, NOSE W/W LOWER LOBE, STA 312 RT SIDE ON FLOOR SKIN. REMOVED, FAB'D AND INSTALLED REPLACEMENT ANGLES PER SRM 51-10-01 AND SRM 51-30-02.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: C. LOWER RUDDER SKIN AT FRONT SPAR IS CORRODED. REMOVED AND REPLACED RUDDER (LOWER) IAW M/M 27-20-11 AND MM 27-20-20.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: C. UPPER RUDDER SKIN RT SIDE HAS CORROSION AT RUDDER FRONT SPAR. REMOVED AND REPLACED UPPER RUDDER M/M 27-20-01 AND MM 27-20-00.

Part: WATER SEP BAG — DIRTY (LT PACK)

DIRTY WATER SEPARATOR BAG CAUSING ODOR IN FLIGHT DECK. REPLACED BAG.

Part: FLAP — CORRODED (NR 2 LE FLAP)

WHILE IN SI CHECK MAINTENANCE FOUND NR 2 K-FLAP HAS CORROSION. REMOVED AND REPLACED NR 2 K-FLAP IAW M/M 27-81-01.

Part: SKIN — CORRODED (WING)

WHILE IN SI CHECK MAINTENANCE FOUND CORROSION INSIDE BREATHER WEB ON SKIN SURFACE OF LOWER CENTER FUEL CELL. REPAIRED IAW E.O. B727-5710-7042A AND SRM 57-30-3.

Part: FITTING — CORRODED (NR 9 SPOILER)

WHILE IN SI CHECK MAINTENANCE FOUND NR 9 SPOILER SUPPORT FITTING CORRODED. REPLACED FITTING IAW SRM 51-30-2.

Part: CHANNEL — CRACKED (NR 2 LE FLAP)

WHILE IN SI CHECK MAINTENANCE FOUND NR 2 K-FLAP O/B ACTUATOR SUPPORT CHANNEL CRACKED. INSTALLED FABRICATED PARTS IAW SRM 57-20-2, 51-20-1, 51-30-2, M/M 20-50-21.

Part: FLOORBEAM — CORRODED (BS 480)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM OF AFT UPPER FLANGE OF FLOORBEAM STA 480, LBL 60. INSTALLED REPAIR ANGLE IAW B727-5310-7006A.

Part: FITTING — CORRODED (BS 870)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON I/B FLANGE RT AFT BOTTLE PIN FITTING STA 870, RBL 60 TO 70.5, WL 192 TO 178. REPLACED FITTING IAW 727-57-1372.

Part: FITTING — CRACKED (FS 1183)

WHILE IN SI CHECK, MAINTENANCE FOUND STRINGER 3A LT AT STA 1183 I/B FWD FITTING HAS CRACK INDICATION. REMOVED FITTING AND REPLACED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 760-780)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AT STA 760 TO 780, BL 0, WL 208. INSTALLED NEW TRACK IAW SRM 53-10-1.

Part: SKIN — CRACKED (NR 2 SLAT)

WHILE IN SI CHECK, MAINTENANCE FOUND NR 2 SLAT HAS 2 GOUGES ON T/E ABOVE THE I/B GUIDE HOOK. REPLACED SLAT IAW B727-5750-1235.

Part: TIES — CORRODED (BS 1183)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER TIES STR 20L, BS 1183, WL 185. INSTALLED FABRICATED TIES IAW SRM 51-30-2, 51-20-1.

Part: WEB — DELAMINATED (FUSELAGE)

WHILE IN SI CHECK, MAINTENANCE FOUND WALKWAY PANEL, UPPER TORQUE BOX WEB, LEFT SIDE DELAMINATING. INSTALLED FABRICATED PARTS IAW 53-10-2, 51-10-2.

Part: FITTING — CORRODED (BS 870)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON I/B FLANGE LT AFT BOTTLE PIN FITTING STA 870, RBL 60 TO 70.5, WL 194 TO 184. REPLACED FITTING IAW 727-57-1372.

Part: SPAR — CORRODED (X 70.5)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON I/B SIDE RT UPPER SPAR CHORD BETWEEN WEB AND SPAR CHORD 70.5, BS 870. REPLACED CHORD IAW B727-5710-7020A.

Part: STRINGER — CORRODED (BS 390-400)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 25 LT BS 390 TO 400. REPAIRED STRINGER IAW SRM 53-10-1, 53-10-3, 53-10-2.

Part: RIB — CRACKED (X 70.5)

WHILE IN SI CHECK, MAINTENANCE FOUND LEFT AND RIGHT 70.5 RIB CHORDS CRACKED. REPAIRED IAW B727-5710-7024A, B727-5710-7023A.

Part: EXPANSON LINK — CORRODED (BS 740-760)

WHILE IN C-CHECK, MAINTENANCE FOUND EXPANSION LINK STA 740 TO 760, BL 0, WL 208 CORRODED. REMOVED AND REPLACED EXPANSION LINK IAW SRM 51-10-1.

Part: FITTINGS — CRACKED (BS 1183)

WHILE IN C-CHECK, MAINTENANCE FOUND STRINGER 3A RT AT STA 1183 I/B AND O/B FITTINGS, (PN 65-22547-5, 65-25591-8), CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 51-10-1, 51-30-2.

Part: SPAR — CORRODED (HORIZ STAB)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON LT HORIZ STAB UPPER FWD SPAR CHORD, VERT FLANGE AFT SIDE AT SPAR STA 16.08. REPAIRED IAW SRM 55-10-5, 55-10-4.

Part: SPAR — CORRODED (HORIZ STAB)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON RT HORIZ STAB FRONT SPAR UPPER CHORD, STAB STA 114, AROUND FASTENER HOLE AFT HORIZ FLANGE. REPAIRED IAW SRM 51-30-2, 55-10-1, 51-10-6, OHM 20-10-3.

Part: SEAT TRACK — CRACKED (BS 948-952)

WHILE IN C-CHECK, MAINTENANCE FOUND SEAT TRACK CRACKED STA 948 TO 952, RBL 61, WL 207. INSTALLED FABRICATED PARTS IAW SRM 53-10-5, 51-30-2.

Part: FLOORBEAM — CORRODED (BS 344)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER SURFACE OF TOP CHORD STA 344, BL 0, RBL 45. INSTALLED FABRICATED PARTS IAW SRM 51-30-2, 51-20-151, 51-10-2.

Part: SKIN — CORRODED (BS 1386)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN PANEL AT BS 1386, RBL 20, WL 255. REMOVED CORROSION AND INSTALLED NEW CHORD IAW SRM 51-30-2, 51-10-1, 53-10-1.

Part: SEAT TRACK — CORRODED (BS 1100-1110)

WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK UNDERSIDE BS 1100 TO 1110, LBL 55, WL 204. INSTALLED FABRICATED PARTS IAW SRM 53-10-5.

Part: LOCK ACT — MALFUNCTIONED (LT MLG)

(SUPPLEMENTAL MRR) PILOT REPORTED WHEN LOWERED LANDING GEAR, NO LEFT MAIN GEAR CAME DOWN, CYCLED GEAR 3-4 TIMES, NO LEFT MAIN LANDING GEAR. ATTEMPT TO LOWER LT MAIN GEAR MANUALLY AND DID NOT WORK PROPERLY. TURNED HANDLE C/W 2-3 TURNS AND GOT DOOR LIGHT, WAIT 5 SECONDS AND TRIED TO CONTINUE TURN TO STOP, BUT HANDLE WOULD NOT MOVE. IT FELT BOUND. FINALLY, FORCED HANDLE UNTIL HEARD A CABLE BREAK. LEFT GEAR CAME DOWN AT THAT TIME. CHECK LEFT MANUAL EXTENSION FOR BROKEN CABLE OR SOMETHING. REPLACED LT MAIN GEAR LOCK ACTUATOR PER MM 32-30-00. REPLACED MLG CABLES PER 32-34-41. REPLACED MANUAL EXTENSION DRUM PER 32-34-71.

Part: GEAR ASSY BOX — MALFUNCTION (LANDING GEAR)

(SUPPLEMENTAL MRR) PILOT REPORTED LEFT MAIN GEAR LIGHT WOULD NOT INDICATE GREEN WHEELS. RECYCLED THEN BOTH LEFT AND RIGHT MAIN GEAR WOULD NOT INDICATE GREEN WHEELS. ON THE THIRD RECYCLE BOTH LEFT AND RIGHT MAIN GEAR GREEN LIGHTS INDICATED SAFE CONDITION. REPLACED GEAR ASSY BOX IAW MM 32-09-11. SYS CHECKS GOOD.