N942UP

Part: ACTUATOR — WORN (NR 6 SLAT)

LED NR 6 DOES NOT RETRACT. THE AMBER LT CAME ON DURING CLIMB TO 310. COULD NOT DUPLICATE FAULT ON GROUND. AS PRECAUTION REPLACED NR 6 L/E SLAT ACTUATOR. OPS CHECK GOOD, REF MM 27-81-32-4.

Part: RING — ELONGATED (EVAC SLIDE)

DURING ROUTINE C-CHECK INSPECTION OF FORWARD DOOR EMERGENCY ESCAPE SLIDE, THE 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 SPLIT RING HAS BEEN REPLACED. (K)

Part: HINGE — CRACKED (LT AILERON) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE:C CRACK FOUND AFT FASTENER HOLE OF LT O/B AILERON 2ND FROM I/B FIXED W WING HINGE CASTING UPPER O/B FLANGE. REPLACE HINGE ASSY. HINGE ASSY REPLACED IAW SRM 51-30-2, 51-30-5 AND MM 27-10-14, 21-80-01 AND BOEING DRAWING 65-19275. REF NRC 100803 FOR AILERON CONTROL SYS ADJUSTMENT.

Part: FAIRING — CORRODED (FUSELAGE) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE:C BODY FAIRING 3430 HAS AREA OF LIGHT SURFACE CORROSION LWR DOOR CUTOUT FRAME. PLEASE REMOVE ANCHOR NUTS, REMOVE CORROSION, REINSPECT AND RECTIFY AS NECESSARY. FRAME AND SUPPORT BRACKET REPAIRED IAW SRM 51-40-04 AND 51-30-02.

Part: BRACKET — CRACKED (BULKHEAD) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF LT 870 FITTING AT LWR CORNER, CRACK IDENTIFIED ON BRACKET REMOVED BRACKET IAW SRM 51-30-02. NEW BRACKET INSTALLED IAW SRM 51-30-02 AND DRAWING NR 65-25370.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON REPAIR BUSHING IN AFT OB HOLE FITTING REPAIR BUSHING REMOVED IAW SOPM 20-50-03. REPAIR CARRIED OUT IAW APPX B.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE:C SCRATCH ON FUSELAGE SKIN BETWEEN BS 1186 AND 1193 S19R. PAINTSTRIP AREA A RE-INSPECT AND RECTIFY AREA PAINT STRIPPED IAW MM 51-20-01. SCRATCH OUTSIDE LIMITS IAW SRM 5 3-30-1. REPAIR CARRIED OUT IAW SRM 53-30-03 AND 51-30-02.

Part: RING — BROKEN (ESCAPE SLIDE) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE-C ON SLIDE LATCH CHAIN AND RING BROKEN ON FWD ENTRY DOOR ESCAPE SLIDE. REPLACE RING AND CHAIN ON FURTHER INVESTIGATION CHAIN FOUND NOT TO BE BROKEN, BUT RING WAS DEFORMED AND DETACHED. RING REPLACED IAW MM 25-60-14. NOTE: RING SOLDERED W/NO DEFECTS. FOLLOWING PROCESS USED: CLEANED IAW STANDARD PRACTICES MANUAL 20-30-03. ENTIRE RING SOLDERED.

Part: SKIN — CRACKED (FOREFLAP) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE-C CRACK ON RT OB FORE FLAP LE AT CUTOUT OB OF IB SEQUENCE CARRIAGE ATTACH BRACKET DAMAGE OUTSIDE LIMITS IAW SRM 57-50-1. CRACK STOP DRILLED IAW SRM 57-5 0-4. HFEC CARRIED OUT IAW NDTM 51-00-00 PT 6 FIG 4 CRACK CONTAINE D. REPAIR CARRIED OUT IAW SRM 57-50-4.

Part: SUPPORT — CRACKED (NR 2 NACELLE) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE-C ENGINE NR 2 SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL HAS SUSPECT CRACK ON RT CHORD BETWEEN AFT CONE BOLT HOUSING AND REAR SPAR AT 2 FOOT FROM TOP OF CHORD HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. CRACK CONFIRMED. CHORD REPLACED IAW DRWG 65-17551 AND 65-17561.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE-C CORROSION AT BS 344 OUTSIDE LIMITS, PLEASE REPAIR IAW SRM FLOORBEAM TOP CHORD REMOVED IAW SRM 51-30-02. SPLICE ANGLES AND TOP CHORD FABRICATED IAW SRM 53-10-08. PARTS REPROTECTED IAW SRM 51-10-02. PARTS INSTALLED IAW SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE: C, ON REMOVAL OF FLOOR PANEL AT ENTRANCE TO COCKPIT. CORROSION FOUND ON FLOORBEAM TOP CAP BS 344 LBL 10 TO RBL 12. AREA FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1.

Part: PRESSURE PANEL — CRACKED (BS 286) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE:C SUSPECT CRACK ON NLG SIDE WALL AT WL 184 BS 276. CRACK REPAIRED IAW SRM 51-40-02.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE: C, DURING PRESSURIZATION CHECK LEAK WAS FOUND IN NOSE WW PRESSURE DECK CE CEILING. WEB CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-02, 51-10-02 & 51-10-01.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:ASE FLIGHT STAT EMERGENCY LIGHT INOP. REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY IAW 33-50-01-2. OPS CHECK GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,713 hrs · 40,516 cycles

INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF RT 870 FITTING AT LWR CORNER. CRACK IDENTIFIED ON BRACKET, REMOVED BRACKET IAW SRM 51-30-02. NEW BR BRACKET INSTALLED IAW SRM 51-30-02 AND DRAWING NR 65-25370.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C AREAS OF LITE SURFACE CORROSION FOUND ON INNER FUSELAGE SKIN SURFACE OF LWR SURFACE OF INTERNAL DOUBLER BETWEEN S3L & S2L BS 630 TO 660 AT VARIOUS LOCATIONS. REPAIR CARRIED OUT IAW SRM 53-30-03.

Part: FITTING — CRACKED (RT TRUNNION) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C EXTENSIVE CRACKING SROUND BOTH I/B B & C HOLES FOR A LARGE AREA OF THE RT TRUNNION FITTING ON RT REAR SPAR. REMOVED MLG FWD TRUNNION HOUSING ATTACHMENT FITTING ON REAR SPAR IAW SRM 51-30-2. REPAIR CARRIED OUT IAW SRM 51-30-2, DRAWING 65-19297 & AAA E EO 2005-021-001.

Part: BRACKET — CRACKED (NR 1 ENGINE T/R) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C ENGINE NR 1 THRUST REVERSER O/B FAIRING MID AND AFT SUPPORT BRACKET ARE CRACKED. BRACKETS REPLACED IAW MM 78-30-01.

Part: FITTING — CORRODED (NR 5 FLAP TRACK) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C NR 5 FLAP TRACK FWD SUPPORT FITTING P/N 65-21651 HAS PITTING CORROSION ON HOLE FOR SPECIAL STUD. REPAIR CARRIED OUT IAW AAAE EO 2005-021-003.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C CARGO TIE DOWN TRACK CRACKED AT BS 1030 RBL 14. REPAIR CARRIED OUT IAW SRM 53-10-5, 51-30-2, 51-20-1 & 53-10-5.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C FLOOR SUPPORT CRACKED AT BS 1070 LBL 14. REPLACED FLOOR SUPPORT FROM 1100 - 1060 IAW SRM 53-10-5 FIG 4.

Part: SPINDLE — CORRODED (4 FLAP CARRIAGE) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C SURFACE CORROSION ON 4 FLAP CARRIAGE SPINDLE INNER SURFACE. CORROSION REMOVED IAW SRM 51-00-06, WITHIN LIMITS OHM 57-52-01. AREA PROTECTED IAW SRM 51-10-02.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIP RACK CRACKED AT BS 400 BS 420 AND BS 460 LBL 17. REPAIRED CRACKS ON UPPER SUPPORT CHANNEL AT BS 400, 420, 460 LBL 17 IAW SRM 51-40-3.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE: C FWD CARGO DOOR CRACKED AT AFT UPPER FRAME BETWEEN LWR ATTACH BOLT FOR BALANCE MECHANISM. REPAIR CARRIED OUT IAW AAAE EO 2005-021-002.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIPMENT RACK CRACKED AT BS 420 AND 460 RBL 22. REPAIRED CRACKED UPPER SUPPORT CHANNEL IAW SRM 51-90-3 AT BS 420 TO 460.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C AFT CARGO DOOR, CRACKED IN 1ST FRAME FROM TOP IN O/B RADIUS BENEATH FWD HINGE. REPAIR CARRIED OUT IAW MM 52-31-01 & SRM 51-10-01, 51-40-3, 51-10-02 & 51-30-02. REF NRC 768566 FOR INSTALLATION OF AFT CARGO DOOR.

Part: PANEL — DELAMINATED (NR 8 SPOILER) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C DELAMINATION ON NR 8 SPOILER AT I/B END. NR 8 SPOILER PANEL REPLACED IAW MM 27-62-01 AND SPOILER LINK REPLACED IAW MM 27-62-91.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 51,199 hrs · 40,063 cycles

INSPECTION TYPE:C EVIDENCE OF DELAMINATION TO RT ELEVATOR TAB UPPER INBOARD SURFACE. TAB REPLACED IAW MM 27-30-11 & 27-30-00.

Part: LIFE RAFT — MALFUNCTIONED (AFT OF LAV)

LIFE RAFT LOCATED AFT OF LAV EXPERIENCED AN UNCOMMANDED INFLATION. NO DAMAGE TO THE A/C WAS NOTICED. A/C NOW IN HEAVY MAINTENANCE IN SNN. INSTALLED SERVICEABLE LIFE RAFT MM 25-60-00 LOG PAGE 333531 THIS WAS TRANSFERRED TO NRC768041 AT SNN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C PARTIAL REPLACEMENT OF SKIN LOCATED AT BS 360-390 S4L-4R. REPLACED IAW UPS AUTHORIZATION B727-5330-19967-A.

Part: RIB — CRACKED (WING) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLACED IAW SRM 51-30-2 & SPOILER OPERATION WITH STOP TESTED SATISFACTORY IAW MM 27-61-00.

Part: BRACKET — CRACKED (BATTERY CHARGER) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, BATTERY CHARGER FWD MOUNTING BRACKET CRACKED ON E3 RACK LOWER RT SIDE. REMOVED CRACKED BRACKET IAW SRM 51-30-02. FABRICATED NEW BRACKET IAW SRM 51-20-01. NEW BRACKET REPROTECTED IAW SRM 51-10-02, AND RE-INSTALLED IAW SRM 51-30-02.

Part: BRACKET — DAMAGED (WING-BDY FAIRING) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, SUSPECT CORROSION WHERE 259.5 RT STIFFENER AND TOP LEFT HAND CORNER OF NWW TORQUE BOX MEET BRACKET. REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. FASTENERS INSTALLED IAW SRM 51-30-2 & APPLIED SEALANT IAW SRM 51-20-04. BRACKET REPROTECTED IAW SRM 51-10-02.

Part: WEB — CRACKED (RT TORQUE BOX) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CARRIED OUT IAW EO B727-5310-1239-E & MM 20-10-05.

Part: HINGE — CRACKED (MLG DOOR) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 NDF. REPAIR CARRIED OUT IAW SRM 51-40-04.

Part: SUPPORT FITTING — DAMAGED (NR 3 SPOILER) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C REPAIR PLATES ON NR 3 SPOILER PCU SUPPORT FITTING, REAR SPAR ATTACH ANGLES DO NOT CONFORM TO REQUIREMENTS OF SRM REPAIR 51-40-4 FIG 1 OR S/B 57-84 R1 CRITERIA. REPAIR CARRIED OUT IAW DRAWING 65-16201 & MM 28-11-20 & 28-11-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C PRESENCE OF INTERGRANULAR CORROSION FOUND ON VARIOUS HOLES AND THE LOWER I-BEAM AT BS 1110 RBL 31 AS MARKED. REPAIRED IAW UPS AUTHORIZATION B727-53-21034.

Part: FITTING — CRACKED (RT MLG WW) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C RIGHT MLG WHEEL WELL, EVIDENCE OF CORROSION ON BS 870 FITTING O/B FLANGE AREA ABOVE STR 18A. FITTING REPLACED IAW DWG65C23231 AND 2BOF65-72710 AND UPS EO B727-5310-3056G.

Part: SOLENOID VALVE — STICKING (NR 1 ENG EXTING) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, ENGINE NR 1 FIRE EXTINGUISHING SOLENOID STICKS DURING OPERATION. ENGINE NR 1 FIRE SOLENOID VALVE REPLACED IAW MM 26-21-21. TEST AND FOUND SATISFACTORY IAW MM 21-21-00.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FLAP CARRIAGE NR 1 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. REMOVAL OF HARDWARE CORROSION FOUND ON SPINDLE SMALL BEARING SEAT. CORROSION FOUND TO BE OUTSIDE LIMITS OF OHM 57-58-01. FLAP CARRIAGE REPLACED IAW MM27-51-13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI DURING RECTIFICATION UPPER LT AFT TENSION TIE FITTING FOUND CRACKED IN TAIL SKID UNIT CAVITY. UPPER LT TENSION TIE REMOVED IAW SRM 51-30-02 UPPER LT TENSION TIE INSTALLED IAW 51-30-02.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SUSPECT CRACKS ON 2 FRAMES AND FRAME ATTACH ANGLES ON OUTER FACE OF AFT CARGO DOOR. FRAMES AND ANGLES REPLACED IAW DWG 65-18625, LOWER FRAME REPAIRED IAW SRM 51-40-2 FIG 1.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SEVERAL MAIN HINGES CORRODED ON MAIN CARGO DOOR. HINGES REPLACED IAW OHM 20-50-01.

Part: STRINGER — CRACKED (BS 460 STR8L) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI STR NO8 L/H HAS EVIDENCE OF CRACKING ON ROOT OF INSIDE LOWER FLANGE AT BS 460 REPAIR CARRIED OUT IAW SRM 53-10-3 FIGURE 3.

Part: INTERCOSTAL — CRACKED (BS520 RBL15) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACKED BRACKET ON INTERCOSTAL BS520 RBL15, CABIN FLOOR. BRACKET REPAIRED IAW SRM 51-40-03 FIG 1 TYP FORMED SECTION REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FLOOR TIE LUG CRACKED AT BS 1180 RBL 38 AFT CARGO BAY. FABRICATED TWO NEW ANGLES IAW DRAWING NR 65-19606 AND SRM 51-20-1 FIG 7. INSTALLED BOTH ANGLES IAW SRM 51-30-2 AND DRAWING NR 65-19606.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI LIGHT SURFACE CORROSION AROUND ANCHOR NUT AT BS 480 LBL 8 FLOORBEAM. CORROSION REMOVED AND FOUND OUTSIDE ALLOWABLE LIMITS OF SRM53-10-1 FIG 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON TOP OF FLOORBEAM BS 540 LBL12. REPAIRED IAW SRM 53-10-8 FIGURE 5

Part: INTERCOSTAL — CRACKED (BS950 LBL 6.) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI BS 950 LBL 6 ANGLE CRACKED AT FLOOR BEAM INTERCOSTEL. NEW ANGLE FABRICATED IAW SRM 51-20-1 FIG.7 ANGLE INSTALLED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON TOP OF FLOOR BEAM BS 560 LBL 40. REPAIR CARRIED OUT IAW SRM 53-10-08 FIGURE 5

Part: SEAT TRACK — CORRODED (BS 360 BLO) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON SEAT TRACK FLANGE AT BS 360 BLO. CORROSION BLENDED AND FOUND TO BE OUTSIDE LIMITS, TRACK CUT AT BS 41 0 AND NEW SECTION SPLICED IN IAW SRV-SNN-02-00124H AND 00134H UPS AU THORISATION 727-53-20064

Part: DOUBLER — CORRODED (DELTA BEAM BS747) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI BULGING ON EXTERNAL DOUBLER ATTACHED TO DELTA BEAM BS 747 Y/H DOUBLER REMOVED IAW SRM 51-30-2, CORROSION FOUND ON UDERSIDE OF DOUB LER, DELTA BEAM FAYING SURFACE INSPECTED AND LIGHT SURFACE CORROSION FOUND, REMOVED AND FOUND WITHIN LIMITS, REPROTECTED IAW SRM 51-10-2 . CORROSION ON DOUBLER OUTSIDE OF LIMITS, NEW DOUBLER FABRICATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-2

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI LIGHT SURFACE CORROSION FOUND ON TOP CAP OF FLOORBEAM AT BS 344 BETWEEN LBL 4 TO RBL 30. CORROSION BLENDED BETWEEN LBL 4 AND RBL 30, FOUND TO BE OUTSIDE LIMITS. REPLACED TOP CAP OF FLOORBEAM AT BS 344 IAW DWG 65-16316 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON UNDER SIDE OF FLOORBEAM TOP CAP BS 560 LBL12. REPAIRED IAW SRM 53-10-8 FIGURE 5 .

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI DURING EDDY CURRENT INSP 5 HOLES WERE FOUND TO CONTAIN CORROSION AT LT BS 870 FITTING. REPAIRED IAW SMRO EO 2002-035-004

Part: FRAME — CRACKED (BS338-STR.13R.) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FRAME CRACKED AT BS338-STR.13R FRAME REPAIRED IAW SRM 53-10-4 FIG 1.

Part: SPAR — CORRODED (WING) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI DURING INSPECTIONS OF THE WING CENTER SECTION AFT SPAR AREA AIR CON, TWO FASTENERS FOUND POPPED ON THE WING CENTER SECTION REAR SPAR LOWER CHORD VERTICAL FLANGE AT BS 870 LBL38. NDT CONFIRMS CORROSION PRESENCE. REAR SPAR CHORD AND ASSOCIATED STRUCTURE REMOVED. LWR CHORD REPLACED IAW DWG 65-16202 AND DWG 65C21566.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM WEB AFT SURFACE AT BS 890 RBL25. CORROSION REMOVED AND FOUND TO BE WITHIN LIMITS IAW 51-10-6

Part: BRACKET — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI DUCT WEB BRACKET CRACKED BS 1090 LBL 45.5. DUCT WEB BRACKET REPLACED IAW SRM 51-20-1, 51-10-02 AND 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI AFT STR END AT BS 950 STR 9 RT CRACKED. REPLACED STR END IAW SRM 51-30-2.

Part: BEARING — CRACKED (MLG SUPPORT BEAM) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI L/H MLG AFT TRUNNION BEARING CRACKED L/H MLG AFT TRUNNION REPLACED IAW 32-11-00 PARA 4AA(2) TO (4) PARA 5 (3) A TO E.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM LOWER CHORD BS 1030 LBL 52. REPAIRED IAW BOEING INSTRUCTIONS SRV-SNN-02-00112H AND 00132H B727-53-20058

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI, NLG W/W RIGHT CEILING PANEL CORRODED. REMOVED AND REPLACED AFT CORNER . MATERIAL REMOVED IAW SRM 51-10-01. CARRIED OUT REPAIR OF AFFECTED AREA IAW SMRO EO 2002-035-016.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM WEB AFT SURFACE AT BS890 RBL 34, CORROSION REMOVED IAW 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK ON SHEAR WEB LOCATED AT BS1130 LBL24.5. REPAIR CARRIED OUT IAW SRM51-40- 2 FIG1.

Part: TIE — CRACKED (BS950 STR9) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI STRINGER TIE CRACKED BS 950 STR 6L. STRINGER TIE REPLACED IAW SRM 51-30-02.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI HORIZONTAL STAB RT SIDE FRONT SPAR LOWER CHORD IS CRACKED AT STAB STA 60.28. FRONT SPAR WEB SECTION CUT FROM ST 82.16 AND 44.6 IAW SRM 51-10-0, DAMAGED SECTION OF CHORD REMOVED IAW SRM 51-10-01, REPAIR PARTS FABRICATED IAW BOEING TELEX SRV-SNN-02-00101H 00102H 00116H AND UPS AUTHORIZATION 727-55-20008.

Part: STRINGER — CORRODED (BS448) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SURFACE CORROSION STRINGER 21R BS 448 APPROX SURFACE CORROSION FOUND TO BE OUTSIDE LIMITS I.A.W SRM 53-10-1. STRINGER 21 R REPAIRED I.A.W SRM 53-10-3 FIG1.

Part: FLOOR SUPPORT — CORRODED (BS343 RBL 15) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT BS 343 RBL 15. TOILET PARTITION REMOVED FOR ACCESS IAW MM25-40-00, CORROSION REMOVE D IAW SRM 51-10-6 , FOUND OUTSIDE LIMITS IAW SRM 53-10-1, PARTS FABV RICATED IAW DWG 65-26173. INSTALLED PARTS IAW DWG 65-26173 AND SRM 5 1-30-2. PARTITION REINSTALLED IAW MM25-40-00 AND OHM 20-50-01.

Part: STRINGER — CORRODED (BS460-440 S19L) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI INTERGRANULAR CORROSION S19L BS 460-440, CORROSION FOUND TO BE OUTSIDE LIMITS OF SRM 51-10-1. STRINGER REPAIR ED IAW SRM 53-10-3.

Part: BRACKET — CRACKED (BS720 S17R) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI BRACKET CRACKED AT RIVET HOLE(UPP FASTENER) AT I/B LEG OF FRAME BS72 0" STR 17R 4" ABOVE FLOOR LEVEL. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1.

Part: HINGE FITTING — CRACKED (MID GALLEY DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SUSPECT CRACKS ON FWD.(FRAME)LWR. HINGE CUTOUT FITTING(MID GALLEY DO OR) REMOVED FITTING IAW SRM 51-30-2. INSTALLED NEW FITTING IAW DRG.65-16722.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI AFT CARGO DOOR HAS SUSPECT CRACKS AT FWD END AFT HINGE ATTACH POINTS FRAME ANGLES. CRACKED BRACKETS REMOVED IAW SRM 51-30-2, TWO NEW BRACKETS FABRICATED IAW SRM 51-20-1 F7. TWO NEW BRACKETS INSTALLED IAW DWG NR 65-18625 AND SRM 51-30-2.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI LT SLIDING WINDOW SILL CHORD CORRODED BETWEEN BS236 AND 244L. REMOVED SLIDING WINDOW IAW 56-12-11, REMOVED CHORD IAW DWG 5-71775 A ND SRM 51-30-02, NEW CHORD FABRICATED IAW SRM 51-20-1 FIG 7, CHORD INSTALLED IAW DWG 5-71775 AND SRM 51-30-2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON FAIRING SUPPORT ANGLE BS 760 AIR CONDITIONING BAY AT LBL 10 AND RBL 10. ANGLE SECTION REPLACED IAW SRM 51-30-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI INTERGRANULAR CORROSION ON FRAME ANGLE BS 328 AT ATTACH POINT TO S22R. FRAME ANGLE REPLACED IAW SRM 51-40-3 FIG 1 FROM BELOW S21R TO BETWEEN S22R AND S23R.

Part: RIB — CRACKED (HOR-STAB L/H+R/H) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI INSPECT REMOVED STAB.RIBS. FOR CRACKS AND FORWARD FINDING TO ENGINEE RING(RETAIN CRACKED RIBS) DVI INSPECTION PERFORMED IAW CUSTOMER REQUEST :CRACKS NOTED @ L/H RI BS 17:20 AND 136:50 AND R/H RIBS 17:20 AND 66:50 AND 99:79.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1080 TO BS 1110 STR 11RT TO STR 13 RT. AREA OPENED UP IAW SRM 51-10-1, FOUND CORROSION BS1080-1100 AND AROUND SKIN CUTOUT TOP AFT CORNER WINDOW AT BS 1090 BETWEEN STRINGERS 11 AND 13 RT. FOUND OUTSIDE LIMITS REPAIRED IAW SRV-SNN-02-00109H AND 00129H AND UPS AUTHORIZATION 727-53-20061

Part: SUPPORT FITTING — CORRODED (R/HMLG WING DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI R/H MLG WING DOOR ACTUATOR SUPPORT FITTING CRACKED. FITTING REPLACED IAW EO B727-3210-2583 APP D,E,F,G.

Part: CASTING — CRACKED (SPOILER) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI NR 12 SPOILER SUPPORT CASTING O/B ATTACH ANGLE LWR HOLE HAS CRACK INDICATION. SUPPORT CASTING REPLACED IAW SRM 51-30-02

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK ON STRINGER FLANGE S21R BS 580-BS600. UPON FURTHER INVESTIGATION STRINGER CRACKED DUE TO CORROSION. CORRODED SECTION CUT AWAY AND STRINGER REPAIRED IAW SRM 53-10-3 FIG 1

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK ON FRAME BS 540 AT CARGO DOOR FITTING. CRACKED LUG OF BS 540 FRAME AT MCD LATCH SUPPORT FITTING CUT AWAY IAW SRM 51-40-3. REPAIR PARTS FABRICATED IAW SRM 51-40-3. PARTS INSTALLED IAW SRM 51-30-02 AND SRM 51-40-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM AT BS 480 AT RBL 27.39. CORRODED FLANGES CUTOUT AT STA 480 RBL 27-31 AS CORROSION NOT ALLOWED AND AT RBL 35-39 IAW SRM 53-10-8. FLOORBEAM REPAIR IAW SRM 53-10-8 FIGURE 5.

Part: SUPPORT FITTING — CORRODED (LT MLG DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI LT WING LANDING GEAR DOOR ACTUATOR SUPPORT FITTING HAS EVIDENCE OF CORROSION. CORROSION FOUND TO BE OUT OF LIMITS, OLD FITTING WAS REMOVED AND NEW FITTING INSTALLED IAW UPS EO B727-3210-2583 APP D,E,F,G.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI NR 3 ENG, FWD MOUNT FITTING HAS PITTING CORROSION IN BOLT HOLES. REPAIR CARRIED OUT IAW EOB727-5440-11592 APPENDIX B.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI 1 INCH CRACK FOUND ON FWD DOOR AFT FRAME AT LOWER LATCH ROLLER TORQUE SHAFT CUTOUT. CRACKING STOP DRILLED PREVIOUSLY. DOOR FRAME REPAIRED IAW BOEING INSTRUCTION SRV-SNN-02-00135H 00100H.

Part: CASTING — CORRODED (WS304) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI #6 SPOILER CENTRE HINGE SUPPORT CASTING O/B FACE OF I/B HINGE LUG HA S EVIDENCE OF CORROSION. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND OUT OF LIMITS IAW SRM 5 1-10-01. HINGE CASTING REPLACED IAW DWG 65-16216

Part: WEB — CRACKED (BS1182 LBL54) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK TO WEB AT BS 1182 LBL54 APPROX AT ACCESS HOLE FOR PIPE WORK WEB REPLACED IAW SRM 51-20-1 FIG7 AND SRM 51-30-2

Part: ANGLE — CRACKED (BS1180 RBL30) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI ANGLE CRACKED AT BS1180 RBL 30 APPROX IN LWR AFT CARGO BAY. CRACKED ANGLE REMOVED IAW SRM 51-30-2 NEW ANGLE FAB. IAW SRM 51-20-1 FIG7 AND SRM 53-10-2 FIG 5 NEW ANGLE INSTALLED IAW SRM 51-30-2.

Part: FLAP TRACK — CORRODED (WS304) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI PITTING CORROSION IN BORE OF HOLES F+G ON NO3 FLAP TRACK TRACK REPLACED REF NRC 541795 FOR REPLACMENT DETAILS.

Part: BRACKET — CRACKED (BS178) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK ON SUPPORT ANGLE AT BS 178 BULKHEAD RBL24 SUPPORT BRAKET REPLACED IAW SRM 53-10-2 FIG1 ABD SRM 51-20-1 FIG 7 A ND SRM 51-30-2.

Part: FRAME — CORRODED (BS218 LBL24) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI INTERGRANULAR CORROSION ON FRAME WEB BS 218 LBL24 FASTENERS REMOVED, CORRODED SECTION OF FRAME WEB CUT OUT IAW 51-40-2 FIG1. PARTS FABRICATE, FRAME REPAIRED IAW SRM 51-40-2 FIGURE 1.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FLAP CARRIAGE NR 8 HAS SUSPECT CORROSION INSIDE SPINDLE BORE HOLE. CORROSION FOUND TO BE OUTSIDE LIMITS IAW OHM 57-58-01. REPLACED FLAP CARRIAGE IAW MM 27-51-13.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK FOUND ON KEELBEAM WEB FWD OF APU CUTOUT IN RIGHT HAND WHEEL WELL. KEEL BEAM REPAIRED IAW SRM ADDENDUM EO B727-5330-1995.

Part: HINGE — CORRODED (LH ELEV #5 BL.PL) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FOUND ON #5 BALANCE PANEL(LH ELEV) 1.LIGHT SURFACE CORROSION ON AFT HINGE ASSY. 2.LIGHT SURFACE CORROSION WHERE AFT HINGE MATES WITH BAL ANCE PANEL. UPON INVESTIGATION FOUND HALF OF AFT HINGE ASSY CORRODED BEYOND LIMI TS IAW SRM 51-80-7-AFT HINGE REPLACED.

Part: PIN — CORRODED (RT WING) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION ON RT WING FRONT SPAR BOTTLE PIN HEAD AFT FLANGE. BOTTLE PIN REPLACED IAW MM57-41-01.

Part: CAP — CORRODED (NLG) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI NOSE LANDING GEAR LT TRUNNION CAPS CORRODED. TRUNNION CAPS REWORKED IAW SRM 53-40-01. FLUORESCENT PENETRANT INSPECTION COMPLIED WITH NDF. NEW BEARINGS FABRICATED IAW SOPM AND OHM.

Part: INTERCOSTAL — CORRODED (BS219-211) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SURFACE CORROSION ON INTERCOSTAL BETWEEN BS219+BS211 LBL 24 L/H. INTERCOSTAL FABRICATED IAW SRM 51-20-1 INTERCOSTAL INSTALLED IAW SRM 53-30-2

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FLAP CARRIAGE NR 2 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. CORROSION FOUND TO BE OUTSIDE LIMITS IAW OHM 57-58-01. REPLACED FLAP CARRIAGE IAW MM 27-51-13.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FLAP CARRIAGE NR 7 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. FLAP CARRIAGE REPLACED AS CORROSION OUTSIDE LIMITS.

Part: BUTT JOINT — CORRODED (1080 S4L TO S6L) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI LFEC INSPECTION INDICATES MATERIAL LOSS AT BS 1080 BETWEEN S4L AND 6 L AREA REPAIRED IAW UPS ENGINEERING ORDER B727-5330-1177 APPEDIX 7.BET WEEN STRINGER 5L AND 6L AT BS 1080. BUTT JOINT RESEALED AND FASTENED IAW SRM 51-30-02.

Part: CLEVIS — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CORROSION AT RT BS 870 FRAME SPLICE ON WW WALL WBL 60 APPROX. CORROSION LOCATED ON HORIZONTAL CLEVIS FLANGES, CRACKS ALSO LOCATED. CORROSION AND CRACKS BEYOND LIMITS. 870 RT CLEVIS REPAIRED IAW SB 727-53-0077 R2 AND BOEING INSTRUCTIONS SRV-SNN-02-00105H, 00133H AND UPS AUTHORIZATION 727-53-20063.

Part: SKIN — CORRODED (BS441-521 S1 TO7) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SUSPECT MATERIAL LOSS ON CROWN SKIN AT BS 500 TO 519 BETWEEN STRINGE R 1 L TO STRINGER 3L SKIN DERIVETED BETWEEN BS441 AND 521 S2L TO 10L IAW SRM 51-10-2, COR ROSION FOUND OUT OF LIMITS, SKIN CUT BETWEEN BS441 BS521 BETWEEN S1L AND S2L AND REMOVED. NEW SKIN SPLICED IN RUNNING BETWEEN BS 441 TO BS 481(MCD CUTOUT) AT STRINGER 7L AND 441 TO 521 BETWEEN S1L AND S2 L. IAW UPS AUTHORISATION 727-53-20065

Part: TORQUE BOX — CRACKED (ENTRY DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI CRACK IN TORQUE BOX OF FWD ENTRY DOOR WHERE LATCH ROD GOES THROUGH T-BOX. REPAIRED IAW SMRO EO2002-035-001 UPS ENG FILE NR 727-52-20010.

Part: LAP JOINT — CORRODED (BS465-497 STR19R) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SUSPECT CORROSION AT LAP JOINT BS 490 TO 470 AT S19R/H LFEC INDICATES MATERIAL LOSS 15-20% BS 498-465 AT STR 19R.CORROSION REMOVED FROM LAP JOINT AT BS470-480, FOUND WITHIN LIMITS AND LAP CLO SED IAW SRM 51-40-5 AND 51-30-2. AREA BETWEEN BS 485-497 FOUND OUTSI DE LIMITS AND DAMAGE CUT AWAY, REPAIRED IAW UPS EO 5330-0509 APP 8.3 AND UPS EO 727-53-20059

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI NOSE LANDING GEAR BAY, EVIDENCE OF CORROSION IN TORQUE BOX AREA. ARE A JUST AFT OF LT FWD NLG DOOR AT BS 288 LT. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. OLD CHORD REMOVED IAW SRM 51-30-2 AND NEW CHORD DRILLED OFF IAW DWG 6 5-18415. NEW CHORD INSTALLED IAW DWG 65-18415 AND SRM 51-30-2. CRACK WAS THEN FOUND AT SKIN BS 350 LBL 18, NEW REPAIR INSTALLED IAW SRM 53-30-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI SUSPECT CRACK IN FUSELAGE SKIN FROM FASTENER HOLE AT FWD UPPER CORNER OF FWD ENTRY DOOR CUT OUT. HEFC INSP CARRIED OUT IAW NDT MANUAL PT 6 51-00-00 FIG 4, CRACK CONFIRMED AND MEASURED AS 5MM IN LENGTH. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460C.

Part: CASTING — CORRODED (FUSELAGE) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI NLG FWD WHEEL WELL BS 227, BULKHEAD FITTING FOR NLG DOOR OPERATION CORRODED AT OUTBOARD UPPER SURFACE, ATTACHES TO RADIUS ROD. CASTING REMOVED IAW SRM 51-30-02, NEW CASTING INSTALLED IAW DWG 65-1 6306 AND SRM 51-30-02.

Part: GATE — CRACKED (ENTRY DOOR) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FWD ENTRY DOOR GATE STOP LUG CRACKED ON UPPER GATE. GATE REMOVED IAW MM 52-11-01, GATE REPLACED IAW MM52-11-01 AND SRM 51-30-2.

Part: WEB — CRACKED (FWD CRG.DR.STP.) · airframe 50,347 hrs · 39,291 cycles

INSPECTION TYPE:C+SI FWD CARGO DOOR AFT LWR.STOP ON FUSELAGE HAS A CRACKED SUPPORT WEB. WEB REMOVED IAW SRM 51-30-02. NEW WEB FABRICATED IAW SRM 53-10-2 FIG.3 AND SRM 51-20-1 FIG 7. WEB INSTALLED IAW SRM 51-30-02.

Part: DAMPENER — FAILED (RUDDER)

INSPECTION TYPE:N/A 2 RUDDER HARD OVERS IN FLIGHT PILOT NOTICED LOWER YAW DAMPENER INDICATOR MOVED LEFT. LOWER YAW DAMPENER SWITCH WAS TURNED OFF AND FLIGHT CONTINUED WITH NO FURTHER PROBLEMS. R&R LOWER YAW DAMPENER COUPLER PER MM 22-11-131 FAILED YAW DAMPENER CHANNEL. OPS CHECK G14 SWITCH POSITION 5 TRANSFER VALVE BALANCE MM 22-00 -00 P 507 14818 7/28/01 R/R YAW DAMPENER PER 22-11-131 NO DEFECTS NOTED OK FOR SERVICE.

Part: TRANSFORMER — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A, SMELLED SMOKE IN THE COCKPIT THEN FOUND NR 1 TR BREAKER POPPED. *S/D* REMOVED AND REPLACED NR 1 TR CHECKS GOOD IAW MM 24-30-51. THIS CLEARS M218279.

Part: SEAT — DEFECTIVE (COCKPIT)

INSPECTION TYPE:N/A, CAPT''S SEAT W/N LOCK INTO POSITION. CLEANED AND LUBED HORIZONTAL MECHANISM ON CAPT''S SEAT O/C IAW M/M 25-10-42. SEAT CHECKS OK.

Part: BEAM — CORRODED (LT MLG)

INSPECTION TYPE:C, CORROSION ON LOWER SURFACE OF LT WING LANDING GEAR BEAM AT NR 4 FLAP TRACK MOUNT. REPAIRED LANDING GEAR BEAM AT NR 4 FLAP TRACK IAW ER 99-5716 (UPS FILE 727-57-2091).

Part: BULKHEAD BEAM — CRACKED (BS 1183)

INSPECTION TYPE:C INSP 1183 BULKHEAD BL 3683 L AND RT VERTICAL BEAMS & BL 26.83 LT AND RT VERTICAL BEAM AT WL 238 FOUND RBL 26.83 CRACKED. REPAIRED RBL 26.83 VERTICAL BEAM PER ESR 0008 AND EO B727-5310-1116 APPENX E.

Part: SEAT TRACK — CORRODED (BS 358)

INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BS 358, LBL 23, WL 208. REMOVED CORROSION IN A 2' X 8 AREA, REMOVED .038 FROM ORIGINAL THICKNESS OF .100 FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA OF SEAT TRACK, FABRICATED NEW SECTION OF TRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-5, SRM 51-30-2.

Part: MASK — LEAKED (FLIGHT DECK)

INSPECTION TYPE:N/A, DURING CREW PREFLIGHT-CAPTAINS O2 MASK FAILED NEGATIVE PRESSURE CHECK AND ALTERNATE PREFLIGHT CHECK. REMOVED AND REPLACED CAPTAINS O2 MASK. SYSTEM CHECKS GOOD, LEAK CHECKS GOOD, REGULATORS CHECK GOOD.

Part: STRINGER — CORRODED (BS 420)

INSPECTION TYPE-C, WHILE WORKING NRC FUSELAGE 70 CUSTOMER NR 677615 DISCOVERED STRINGER AND STRINGER TIE CORRODED BS 420 STR 23R. REPAIRED STRINGER FROM BS 416 TO 440 PER 727 SRM 53-10-3 AND REPAIRED STRINGER TIE PER SRM 53-10-3, 51-30-2 AND 53-10-1.

Part: BATTERIES — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT, CK OK.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, FOUND EMER LIGHTS INOP. ROBBED 2 EMER LIGHTS FROM ACFT 948, INSTALLED AND OPS CK GOOD.

Part: SHUT OFF VALVE — FAILED (LT PACK)

INSPECTION TYPE-N/A, SMOKE IN FLIGHT DECK. FOUND LEFT PACK SOV, FAILED OPEN AND PACK COOLING FAN CB PULLED DUE TO DI 126385. REMOVED AND REPLACED LEFT PACK SOV PER MM 21-51-61. REMOVED AND REPLACED LEFT ACM PER MM 21-51-11, PRECAUTIONARY. INSPECTED SYSTEM AS REQUIRED NO DEFECTS NOTED. OPS CHECK, LEAK CHECK NORMAL SOV P/N ON 398540-2-1, OFF 321674-41, SN ON P2343.

Part: FLAP TRACK — CORRODED (LT TE FLAP)

INSPECTION TYPE-D, LEFT I/B FLAP O/B FLAP TRACK NR 3 HAS RUST IN AREA OF AFT MOUNT PAD AND ON MOUNT PAD ON FALSE SPAR. REMOVED CORROSION PER EO B727-57-0178.

Part: STRINGER — CRACKED (BS 940)

INSPECTION TYPE-D, FUSELAGE STR 18A, RT SIDE CRACKED IN OUTER FLANGE AT BRACKET ATTACH HOLE AT BS 940. REPAIRED STRINGER PER UPS EO B727-53-1830.

Part: FRAME — CORRODED (BS 360)

INSPECTION TYPE-D, TENSION BOLTS CORRODED AT BS 360 FRAME BELOW STR 21. REPAIRED PER UPS EO B727-53-1827.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-D, FUSELAGE BS 940 FITTING, HFEC SHOWS CRACK INDICATIONS IN OUTER PORTION OF FITTING BETWEEN UPPER AND LOWER FASTENER HOLES SECOND ROW FROM FRONT AND LOWER FASTENER HOLE IN THIRD ROW FROM FRONT. REPLACED RT SIDE 940 FITTING, INSTALLED REPLACEMENT MOUNT PER UPS E O B727-5310-4501E.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE-D, STA 334 FLOORBEAM UPPER CHORD HAS CORROSION FROM LBL 65 TO RBL 24. REPLACED DAMAGED SECTION OF FLOORBEAM PER SRM 51-10-1, 51-30-2.

Part: SKIN — CORRODED (BS 259.5)

INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259.5 FWD PANEL, FROM STR 19L TO STR 24L. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E.

Part: FLAP CARRIAGE — CORRODED (RT TE FLAP)

INSPECTION TYPE-D, RIGHT O/B FLAP I/B CARRIAGE, NR 7, HAS RUST AROUND SPINDLE. REMOVED AND REPLACED WITH OVERHAULED CARRIAGE PER MM 27-51-13.

Part: SKIN — CORRODED (BS 259)

INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259, FWD PANEL, FROM STR 19R TO 24R. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E.

Part: SKIN — CORRODED (BS 259.5)

INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259.5 AFT PANEL FROM STR 6L TO STR 10L. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E.

Part: FLAP CARRIAGE — CORRODED (LT TE FLAP)

INSPECTION TYPE-D, RUST ON EXTERNAL SURFACE AND ON SPINDLE OF I/B FLAP I/B CARRIAGE. REMOVED AND REPLACED WITH OVERHAULED CARRIAGE MM 27-51-03.

Part: CARRIAGE — CORRODED (LT TE FLAP)

INSPECTION TYPE-D, RUST ON EXTERNAL SURFACE OF LEFT I/B FLAP, O/B CARRIAGE. REPLACED WITH OVERHAULED CARRIAGE PER MM 27-51-03.

Part: FLAP CARRIAGE — CORRODED (LT TE FLAP)

INSPECTION TYPE-D, RUST ON EXTERNAL SURFACES OF LEFT O/B FLAP, I/B CARRIAGE NR 2. REPLACED WITH OVERHAULED CARRIAGE IAW MM 27-51-13.

Part: FLAP CARRIAGE — CORRODED (LT TE FLAP)

INSPECTION TYP-D, RUST ON EXTERNAL SURFACE AND INSIDE SPINDLE OF AFT O/B FLAP, O/B CARRIAGE NR 1. REMOVED AND REPLACED WITH OVERHAUL CARRIAGE ASSY IAW MM 27-51-13.

Part: RIB — CRACKED (WS 686)

INSPECTION TYPE-D, RIB AT LEFT WING STA 686 CRACKED AT LOWER STR 8 ATTACH HOLE. REPLACED RIB ASSY STA 686 PER EO B727-5710-1325 APPENDIX C.

Part: SKIN — CORRODED (BS 360)

INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 360 FWD PANEL FROM STR 10R TO STR 14R. CUT OUT CORRODED SECTION OF FWD SKIN PANEL, INSTALLED FILLER AND EXTERNAL DOUBLER PER DRAWING 69-62161 AND PER UPS EO B727-5310-1371E.

Part: STRINGER — CORRODED (BS 360)

INSPECTION TYPE-D, HFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 360 FROM STR 17L TO STR 19L FWD PANEL. CUT OUT DAMAGED SKIN FWD PANEL. REPLACED STR TIE FITTING (P/N 65-29889-13) AT STR 19L. INSTALLED REPAIR DOUBLER PER DRAWING 69-62161 AND PER UPS EO B727-5310-1371E.

Part: STRINGER — CRACKED (BS 720)

INSPECTION TYPE-D, STR 15L CRACKED AT BS 720. REMOVED DAMAGED SECTION OF STRINGER 15L AT BS 720, 13 INCHES LONG. INSTALLED SECTION, BAC 1498-144 PER SRM 53-10-03 FIG 1.

Part: SPLICE — CRACKED (BS 870)

INSPECTION TYPE-D, EDDY CURRENT INSPECTION SHOWS CRACK INDICATION AT BS 870 LT STR 9 SPLICE AFT ROW TOP HOLE AT ABOUT 12 O'CLOCK POSITION. ACCOMPLISHED REPAIR ACC UPS EO B727-5310-8735A.

Part: SKIN — CORRODED (BS 303)

INSPECTION TYPE-D, FUSELAGE SKIN CORRODED AT FUSELAGE LAP SEAT AT BS 303, STR 24L. LFEC REVEALED MORE THAN 10 PERCENT MATERIAL LOSS AT BS 295. CUT OUT SECTION OF SKIN 5 BY 3. INSTALLED DOUBLER REPAIR IAW SRM 53-30-03 FIG 14.

Part: BATTERIES — DISCHARGED (COCKPIT DOOR)

MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR DIM. REPLACED BOTH BATTERIES. RELAMPED, TEST NORMAL PER MM 33-50-101.

Part: ACCUMULATOR — LEAKING (A HYD SYST)

ON DESCENT OUT OF 24,000 FEET 85 MILES NORTHWEST OF JAX, THE A-HYDRAULIC QTY GAUGE WENT TO ZERO. THE LEFT A-HYD LOW PRESSURE LIGHT CAME ON FOLLOWED BY THE RIGHT ONE. PILOT CALLED FOR THE A-HYDRAULIC LEAK OR LOSS CHECK LIST. MANUAL GEAR EXTENSION WAS INITIATED. NORMAL LANDING WAS MADE. NOSE PIN WAS INSTALLED, AND THE AIRCRAFT WAS TOWED INTO PARKING. MAINTENANCE REPAIRED THE LEAK AT A-SYS. ACCUMULATOR, SERVICED RESERVOIR. LUBRICATED NOSE GEAR. OPERATED ALL 3 LANDING GEARS MANUALLY AND HYDRAUCIALLY OPERATED NORMALLY IAW MM 32-34-00.

Part: EEL CB — TRIPPED (CABIN)

WHILE ON GROUND, MAINTENANCE PREFLIGHT CREW FOUND EMERGENCY LIGHTS CHARGER C/B POPPED. A/C 214 COVERED FLT W/E PHL.

Part: EEL — INOPERATIVE (COCKPIT)

PILOT REPORTED, ON TAKEOFF ROLL EMERGENCY EXIT LIGHT OVER CABIN ENTRY DOOR AND FWD ENTRY DOOR ILLUMINATED. CYCLED SWITCHES ON OVERHEAD PANEL, UNDER COVER, NO CHANGE AND HAD TO TURN OFF FOR LIGHTS TO EXTINGUISH. FOUND EMERGENCY LIGHT C/B POPPED, RESET D/B. FOUND COCKPIT ENTRY DOOR LIGHT ASSY INOP. REMOVED AND REPLACED COCKPIT ENTRY DOOR EMERGENCY LIGHT ASSY AND OPS CHECKS GOOD.

Part: EEL CB — OPEN (FLIGHT DECK)

WHILE ON THE GROUND, CREW FOUND EMERGENCY EXIT LIGHT IN COCKPIT IS ON IN ARMED POSITION. FOUND EMERGENCY EXIT LIGHT BATTERY CHARGER CB OPEN. RESET AND NO FURTHER PROBLEMS NOTED. OPERATIONAL TEST GOOD PER MM 33-50-01.

Part: EEL — MALFUNCTION (CABIN)

PILOT REPORTED EMERGENCY, CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. CYCLED EMERGENCY LIGHT SWITCH NUMEROUS TIMES. COULD NOT DUPLICATE. REPLACED EMERGENCY LIGHT OVER ENTRANCE DOOR, PRECAUTIONARY.

Part: SKIN — CRACKED (LT ELEVATOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT ELEVATOR UPPER SKIN BEADED DOUBLER AT STA 40 HAS A 1 INCH CRACK FROM DRAIN HOLE. REPAIRED IAW SRM 55-20-3.

Part: RIB — CRACKED (FS 1367)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND F.S. 1367 RT RIB CRACKED. REPAIRED IAW SRM 51-30-2.

Part: LE RIB — CRACKED (RT WING)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT THE O/B END OF THE NR 6 SLAT UPPER FLANGE CRACKED IN 3 PLACES. REPAIRED IAW SRM 51-40-3.

Part: SKIN — CORRODED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN INNER SURFACE AT THE AFT LOWER CORNER OF THE RT AFT EMERGENCY EXIT. REPAIRED IAW SRM 53-30-3.

Part: WEB — CRACKED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND .50 INCH CRACK ON LT SIDE OF AFT AIRSTAIRS, TOP ROW OF LIGHTENING HOLES, 4TH FROM FRONT. REPAIRED IAW SRM 51-10-1, 51-30-2.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL B.S. 1342. REPLACED IAW E.O. B727-5530-4601.

Part: FRAME — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LT LOWER FRAME CHORD B.S. 1342, LBL 24, WL 220. REPLACED IAW E.O. B727-5530-4601.

Part: FRAME — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND LT FRAME CHORD CORRODED B.S. 1342, LBL 20, WL 238. REPLACED IAW E.O. B727-5530-4601.

Part: SEAT TRACK — CRACKED (FS 598-603)

WHILE IN C-CHECK, MAINTENANCE FOUND MAIN CABIN SEAT TRACK CRACKED, STA 598-603, LBL 48. INSTALLED FABRICATED PARTS IAW SRM 51-30-2, 53-10-5.

Part: ENGINE RING — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND ENGINE RING CORRODED AT STA 1342. REPLACED IAW SRM 51-10-1, 51-30-2.

Part: WEB — CRACKED (FS 1283)

WHILE IN C-CHECK, MAINTENANCE FOUND .50 INCH CRACK ON UPPER TORQUE BOX WEB, STA 1283, RBL 27.8, WL 201.3. REPAIRED IAW SRM 51-40-2.

Part: SKIN — CRACKED (RT AILERON)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED SKIN ON THE LOWER I/B SIDE OF RT AILERON. REPAIRED IAW SRM 57-50-5.

Part: FRAME — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON RT LOWER FRAME CHORD B.S. 1342, RBL 24, WL 220. REPLACED IAW E.O. B727-5530-4601.

Part: SPAR CHORD — CRACKED (VERT STAB)

WHILE IN C-CHECK, MAINTENANCE FOUND RT VERTICAL FIN REAR SPAR CHORD CRACKED AT STA 22.5, F.S. 1342. REPAIRED IAW E.O. B727-5530-4601.

Part: SPAR CHORD — CRACKED (VERT STAB)

WHILE IN C-CHECK, MAINTENANCE FOUND LT VERTICAL FIN REAR SPAR CHORD CRACKED STA 22.5, F.S. 1342. REPAIRED IAW SRM 51-10-3.

Part: CHORD — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD B.S. 1342, LBL 30, WL 250. REPLACED IAW E.O. B727-5530-4601.

Part: CHANNEL — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL B.S. 1342, RBL 18, WL 247. REPLACED IAW E.O. B727-5530-4601.

Part: FRAME — CORRODED (VERT STAB)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON RT FRAME CHORD B.S. 1342, RBL 20, WL 238. REPLACED IAW E.O. B727-5530-4601.

Part: CHORD — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CENTER FWD CHORD CORRODED B.S. 1342. REPLACED IAW E.O. B727-5530-4601.

Part: ANGLE — CRACKED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND LT SKIN SUPPORT ANGLE CRACKED AT F.S. 1345. INSTALLED FABRICATED PARTS IAW SRM 51-40-3, 51-30-2.

Part: CHORD — CORRODED (FS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD B.S. 1342, RBL 30, WL 250. REPLACED IAW E.O. B727-5530-4601.

Part: WEB — CRACKED (FUSELAGE)

WHILE IN C-CHECK, MAINTENANCE FOUND .50 INCH CRACK ON RT SIDE OF AFT AIRSTAIRS, TOP ROW OF LIGHTENING HOLES, 2ND FROM FRONT. REPAIRED IAW SRM 51-10-1, 51-30-2.