N930UP

Part: SKIN — CRACKED (BS 364 STR3L) · airframe 56,817 hrs · 42,732 cycles

SUSPECT SKIN CRACK AT BS 364 STR 3 LT. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 53030-3 FIG 3A.

Part: FRAME — CORRODED (BS 1010 S26R) · airframe 56,817 hrs · 42,732 cycles

BODY FAIRING 3608 AFT FRAME AT ATTACHING ANGLE IS CORRODED AT BS 1010 ADJACENT TO STR 26R. FRAME REPLACED IAW SRM 51-20-1 FIG 7.

Part: CLIP — CRACKED (PANEL 3427) · airframe 56,817 hrs · 42,732 cycles

RT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,817 hrs · 42,732 cycles

SUSPECT SKIN CRACK AT UPPER FWD ENTRY DOOR CUT OUT BETWEEN STR 5 AND 6 L. PLEASE CARRY OUT NDI AND RECIFITY. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5330-1460-D OPT 1.

Part: WEB — CRACKED (BS 290) · airframe 56,817 hrs · 42,732 cycles

INSPECTION TYPE: C, NLG W/W CEILING AT BS 290 LBL 0 HAS SUSPECT CRACKS AT FASTENER HEADS. WEB REPLACED IAW SRM 51-20-1 AND DWG 65-18416.

Part: DOOR — CORRODED (NLG) · airframe 56,817 hrs · 42,732 cycles

NLG FWD LT DOOR HAS CORROSION UNDER SEAL AT I/B END. CORRODED SECTION REPLACED WITH FABRICATED SECTION IAW SRM 51-20-1 AND DWG 65-17563.

Part: STRINGER — CORRODED (BS 304-320 S22R) · airframe 56,817 hrs · 42,732 cycles

AREA OF SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE AT BS 295 STR22R. CORROSION FOUND TO BE ON STRINGER 22R BETWEEN BS 204-316. STRINGER SECTION REPLACED BETWEEN BS 304 AND 320 IAW SRM 53-10-3 FIG 1.

Part: SKIN — SCRATCHED (BS 1263 S5L TO 6) · airframe 56,817 hrs · 42,732 cycles

LIGHT SURFACE SCRATCHES FOUND ON SKIN AT BS 1263 BETWEEN S5L AND 6L. DAMAGED AREA FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13.

Part: PANEL — DELAMINATED (NR 8 SPOILER)

INSPECTION TYPE:N/A NR 8 GROUND SPOILER CENTER HINGE BOTTOM S/M PANEL DELAMINATED. REMOVED AND REPLACED NR 8 GROUND SPOILER PER MM 27-62-01. OPS CHECK NORMAL.

Part: SUPPORT — CRACKED (NLG WW) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT STRUCTURE FABRICATE D IAW SRM 51-20-1, SUPPORT STRUCTURE INSTALLED IAW SRM 51-30-02.

Part: PULLEY BRACKET — CRACKED (RUDDER) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BRACKET, FAB BRACKET IAW SRM 51-20-01, BRACKET INSTALLED.

Part: FRAME — CRACKED · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02

Part: SKIN — CRACKED (ENG.1 THRUST REV) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON THE ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND AND ENDS MARKED. STOP DRILLED CRACKS IAW MM 78-30-01. DYE PENETRANT INSP. CARRIED OUT AROUND STOP DRILLED AREA IAW MIL-STD-6 866. CRACKS CONTAINED WITHIN REPAIR AREA. FABRICATED REPAIR DOUBLER IA W SRM 78-30-01. CARRIED OUT REPAIR IAW SRM 78-30-01

Part: SKIN — CHAFED (FUSELAGE) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REPROTECTED IAW SRM51-10-02. AT BS1070 DAMAGE OUT OF LIMITS IAW SRM 53-30-1. REPAIR CARRIED OUT IAW SRM 53-30-02 FI G.2

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 51-30-2. TIE DOWN RAIL FABRICATED IAW DRG. NO.:66-01573 INSTALLED NEW TIE DOWN RAIL IAW SRM 51-30-2

Part: RIB — CRACKED (MID GALLEY DOOR) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02

Part: RETAINER — CORRODED (NLG WW) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-01

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTICAL INTERNAL STRUCTURE OF NWW RBL 14.6 B STA 314. REMOVED OLD REPAIR. HFEC CW NDF. NEW DOUBLER INSTALLED IAW SRM 51-10-02 AND 51-30-02.

Part: RETAINER — CORRODED (NLG WW) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 20-80-01

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRACKED AREA CUT OUT, HFEC C/O AROUND CUT OUT AREA NDF, REMOVED SUPPORT STRUCTURE TO GAIN ACCESS, FABRICATED REPAIR PARTS, INSTALLED FABRICATED PARTS, REINSTALLED SUPPORT STRUCTURE, REPAIR PAINTED.

Part: WEB — CRACKED (KREGUER FLAP) · airframe 56,319 hrs · 42,328 cycles

INSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30-02

Part: SKIN — CRACKED (BELOW WINDSHIELD)

INSPECTION TYPE: ASV, SKIN PANEL BELOW L1 AND R1 CENTER WINDOW POST HAS .375 INCH CRACK FROM EDGE TO RIVET. CONFIRMED BY DYE PENETRANT INSP. REPLACED SKIN PANEL AS PER SRM ADDENDUM EO B727-5330-5128A.

Part: HINGE — CRACKED (AFT ENTRY DOOR) · airframe 55,788 hrs · 41,899 cycles

UPPER HINGE ARM OF AFT ENTRY DOOR CRACKED. HINGE REPLACED. FUNCTION AND OPERATION CHECK CARRIED OUT IAW MM 52-13-02 AND 52-13-00.

Part: SHEAR TIE — CRACKED (BS1050 STR.5.) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR.SHEAR TIE CRACKED AT STR.5 R/H BS1050. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW 51-20-1+51-40-3

Part: SPAR — CORRODED (WING) · airframe 55,788 hrs · 41,899 cycles

DURING PREPARATION FOR CENTER SECTION REAR SPAR WEB SPLICE REPAIR, ADDITIONAL CORROSION WAS NOTED ON UPPER CHORD INBOARD OF LBL 34.20. WEB, CHORD, SPLICE AND STIFFENERS FABRICATED IAW DRG NR 65C21531 REPAIR COMPLETED IAW SMRO EO 2002-052-013. UPS ENG FILE NR B727-5710-177 09-A.

Part: BEAM — CORRODED (RT WING) · airframe 55,788 hrs · 41,899 cycles

DURING REMOVAL OF T/E PANEL ATTACHED TO LOWER SURFACE OF RT MLG SUPPORT BEAM, CORROSION NOTED AROUND MLG SUPPORT BEAM FASTENER HOLE. CORROSION REMOVED AROUND HOLE IAW SRM 51-10-06. HFEC C/O ON FASTENER HOLE AND COUNTER BORE IN THE ABOVE AREA IAW B727 N DTM PT 6 51-00-00 FIG 4 AND FIG 16 - NDF. FREEZE PLUG INSTALLED IAW SRM 51-10-019 AND SMRO EO 2002-052-019. UPS ENGINEERING FILE NR 727-57-20063.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

PRESS WEB AT BS 740 BULKHEAD DAMAGED AT LWR END WHERE IT ATTACHS TO 740 RT FITTING. DAMAGE BLENDED OUT AND REPAIRED PER SRM 53-10-9 FIG 4.

Part: FRAME — DAMAGED (S5 - 6R) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI DURING REPAIR OF FRAME BS 560 STR. 7R DAMAGE WAS FOUND ON EXISTING R EPAIR ABOVE AT S5R - 6R REPAIR TO FRAME CARRIED OUT IAW SRM 53-10-4 FIG 2

Part: HINGE PIN — CORRODED (HORIZ STAB) · airframe 55,788 hrs · 41,899 cycles

HORIZONTAL STAB HINGE LEFT OUTER PIN HAS EVIDENCE OF PITTING CORROSION ADJACENT TO RELIEF RADIUS. HORIZONTAL STABILIZER HINGE PIN LEFT OUTER REPLACED IAW MM 55-10-01 STEPS 3 AND 4.

Part: RISER — CORRODED (RISER #8) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CORROSION ON RISER #8 ON AFT AIRSTAIRS DOOR FOUND TO BE OUTSIDE LIMI TS REF. NRC 480122 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-A

Part: RISER — CORRODED (AFT AIRSTAIR) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI CORROSION ON RISER #5 FOUND TO BE OUTSIDE LIMITS- REF NRC 480122.(AI RSTAIR DOOR) RISER REPLACED IAW SRM ADDENDIUM EO B727-5260-1551-A.

Part: RISER — CORRODED (#6 RISER) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CORROSION ON RISER #6 ON AFT AIRSTAIRS FOUND TO BE OUTSIDE LIMITS RE F. NRC 480122 #6 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-A

Part: PIN — CORRODED (HORIZ. STAB.) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI HORIZ. STAB. HINGE R/H OUTER PIN HAS EVIDENCE OF PITTING CORROSION A DJACENT TO RELIEF RADIUS HORIZ. STAB HINGE R/H O/B PIN REPLACED IAW MM 55-10-01

Part: PANEL — CRACKED (BS 250) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL SIDE PANEL RH SIDE ALONG ROW OF FASTENERS AF T OF FWD RH PANEL BS 250 FASTNERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-02. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2

Part: PANEL — CRACKED (BS 239) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL PANEL RH SIDE ALONG ROW OF FASTNERS BELOW FW D RH PRESSURE PANEL BS 239 FASTENERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-2. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2 & SRM 51-30-2

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

BS 740 BULKHEAD LWR CHORD FOUND CORRODED DURING REMOVAL TO FACILITATE FITTING REPLACEMENT. SECTION OF CHORD REPLACED IAW DRAWING 65C13724.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

CRACKS RT KEEL BEAM VERTICAL WEB FWD OF APU CUT OUT. REPAIR IAW EO B727-5330-1995-B.

Part: INTERCOSTAL — CRACKED (BS 294 & 284) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI COCKPIT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 294 & 284 LBL 5 REMOVED INTERCOSTAL IAW SRM 51-30-2 FABRICATED INTERCOSTAL IAW SRM 53-10-2 & SRM 51-20-4 INSTALLED INTERCOSTAL IAW SRM 51-30-2

Part: RIB — CRACKED (BS519 LWR STR.) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI SUSPECT CRACK AT RIB BS 519 AT LWR. STR. ATTACH POINT AFT OF ACCESS PNL. STOP DRILLED CRACK IAW 51-10-1. PAGE 12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

CORROSION AROUND NUT BS 380 LBL 45.5 ON SEAT TRACK. REMOVED DAMAGED SECTION IAW SRM 51-30-2, REPAIRED IAW SRM 53-10-5.

Part: FRAME — DENTED (BS 560 STR7 R/H) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI DENT IN FRAME BS 560 STR7 R/H REPAIRED IAW SRM 53-10-4 FIG 1

Part: STIFFENER — CORRODED (WING CENTER BOX) · airframe 55,788 hrs · 41,899 cycles

BULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202.

Part: FRAME — CRACKED (BS 930 R/H) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CRACK ON LWR AFT FLANGE OF FRAME BS 930 R/H AT MLG PRESS. WEB REPAIRS TO S15 & S16 CARRIED OUT IAW SRM 53-10-3. FRAME REPAIR BS 9 20 SPLICE FABRICATED IAW SRM 51-10-3 NEW 930 FITTING INSTALLED IAW D RG 65-16336 &65-18383 SRM 51-30-3 & SMRO EO 2002-052-021 UPS ENG. FI LE NO. 727-53-20080. FRAME BS 920 REPAIR CARRIED OUT IAW SRM 51-40-3

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

ON INVESTIGATION OF BS 360 BOLTS AND BOLT HOLES, BOLT HOLE IMMEDIATELY BELOW STR 24L HAS EXCESSIVE CORROSION INSIDE HOLE BORE. REPAIR CARRIED OUT IAW SRM 51-10-06, SRM 51-30-02 AND SMRO EO 2002-052-004 UPS ENGINEERING FILE NR 727-53-20077.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

LWR AFT CARGO BAY, FRAME SUPPORT IS CRACKED AT STR 25 ATTACH POINT FRAME IS LOCATED AT BS 1093 LEFT. FRAME SUPPORT ANGLE REPAIRED IAW SRM 51-40-3 FIG 1.

Part: FRAME — CRACKED (BS 1030 S25-26LH) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI LWR AFT CARGO BAY, FRAME (BS1030)TO FUSELAGE SKIN ATTACH POINT IS CR ACKED IN BEND RADIUS BETWEEN STR 25 AND STR. 26L/H FRAME REPAIRED IAW SRM 53-10-4 FIG 11

Part: SUPPORT FITTING — CORRODED · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI CORROSION ON INNER FACE OF RH MLG TRUNNION SUPPORT FITTING. RH MLG TRUNNION SUPPORT FITTING REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

AREAS OF LIGHT SURFACE CORROSION ON UPPER CHORD OF FLOORBEAM BS 344 BETWEEN LBL 15 TO RBL 35. FLOORBEAM SECTION REPLACED IAW SRM 53-10-8 FIG 7 WITH REF TO BOEING DRG 65-16316.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

AREA OF LIGHT SURFACE CORROSION ON UPPER CHORD OF FLOORBEAM BS 312 AT LBL 4. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND TO BE OUSIDE LIMITS. REPAIR THEN CARRIED OUT IAW SRM 53-10-8 FIG 9.

Part: STRINGER — CORRODED (VENTRAL STAIRWAY) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI VENTRAL STAIRWAY MID STRINGER CORRODED UNDER #1 TREAD STRINGER REPAIRED IAW SRM 53-10-3 FIG 1

Part: SKIN — CORRODED (VENTRAL STAIRWAY) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI VENTRAL STAIRWAY INNER SKIN UNDER #1 TREAD HAS SURFACE CORROSION CORROSION REMOVED IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 52-1 0-2 FIG 5. PAINTED IAW SRM 51-20-91

Part: SKIN — DELAMINATED (RUDDER) · airframe 55,788 hrs · 41,899 cycles

LWR RUDDER LEFT SKIN CORRODED AT TS 141.6. CORROSION AND DELAMINATION FOUND ON LOWER RUDDER, LEFT SIDE, UPPER PANEL, AFT UPPER CORNER. REPLACED RUDDER IAW MM 27-20-01.

Part: STRINGER — CRACKED (BS 400 STR.15R) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR.15R FOUND CRACKED AT BS400 STRINGER REPAIRED IAW SRM 53-10-3 FIG.1 DETAIL 2

Part: RISER — CORRODED (AFT AIRSTAIRS) · airframe 55,788 hrs · 41,899 cycles

VENTRAL STAIRWAY NR 1 TREAD RIZER LOWER CHORD EVIDENCE OF CORROSION. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.

Part: RIB — CRACKED (VENTRAL STAIRS) · airframe 55,788 hrs · 41,899 cycles

EXFOLIATION CORROSION AND CRACK ON NR 10 VENTRAL STAIRWAY RISER LWR RIB CRACKED. LOWER RIB WEB REMOVED IAW SRM 51-30-2. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 52-00-02. RIB WEB FABRICATED AS PER DRG NR 65-19809. RIB WEB INSTALLED IAW SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (BS1183LBL26WL280) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI CRACK ON VERT. BEAM INTERCOSTAL AT BS 1183 LBL26 AT WL 280. FABRICATED NEW INTERCOSTAL IAW SRM 53-10-2 FIG 5. INTERCOSTAL INSTALLED IAW SRM 51-30-2.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 55,788 hrs · 41,899 cycles

NR 6 FLAP CARRIAGE SPINDLE BOLT HOLE AND UPPER AIR LOAD ROLLER BOLT HOLES ARE CORRODED. INSTALLED FABRICATED BUSHINGS IN CARRIAGE IAW SPOM 20-50-03. CORROSION REMOVED FROM HOLES IAW OHM 57-58-02. BUSHINGS FOR HOLES FABRICATED IAW OHM 57-58-02. NR 6 FLAP CARRIAGE REPAIRED IAW OHM 57-58-02.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 55,788 hrs · 41,899 cycles

NR 7 FLAP CARRIAGE AFT DEAD WEIGHT ROLLER BRACKET BOLT HOLE AND CARRIAGE SPINDLE BOLTS HOLE IS CORRODED. CORROSION REMOVED FOR BOLT HOLES IAW OHM 57-58-01. BUSHINGS FOR HOLES IN CARRIAGES FABRICATED IAW OHM 57-58-01. INSTALLED BUSHINGS IAW OHM 57-58-01. NR 7 FLAP CARRIAGE REPAIRED IAW OHM 57-58-01.

Part: FORK — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

STRINGER TIE CRACKED BS 870 STRINGER 1 FWD SIDE. NEW STRINGER TUNING FORK INSTALLED IAW SRM 51-30-02.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 55,788 hrs · 41,899 cycles

NR 3 FLAP CARRIAGE HAS EXCESSIVE CORROSION ON SPINDLE SHAFT SURFACE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03.

Part: SUPPORT FITTING — CRACKED (R/H MLG W/W) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI R/H MLG WING DOOR ACTUATOR SUPPORT FITTING CRACKED FITTING REMOVED AND REPLACED IAW EO B727-3210-2583

Part: CONTROL QUADRANT — CRACKED · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI NO. 5 SPOILER CONTROL QUADRANT CRACKED. NEW QUADRANT FITTED IAW MM 27-61-91

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 55,788 hrs · 41,899 cycles

NR 1 FLAP CARRIAGE HAS EVIDENCE OF CORROSION IN SPINDLE BORE HOLE. NR 1 FLAP CARRIAGE REPLACED IAW MM 27-51-13.

Part: STRINGER — CRACKED (BS 1000 STR6R) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR 6R FOUND CRACKED AT BS 1000 STRINGER REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 11

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

CORROSION ON INNER SURFACE OF INTERNAL DOUBLER (SUSPECT CORROSION BETWEEN SKIN AND DOUBLER) BETWEEN BS 481 AND 475 BETWEEN STINGERS 7L AND 6L. REPAIR CARRIED OUT IAW UPS AUTHORIZATION 727-53-20082.

Part: HINGE FITTING — CRACKED (AILERON) · airframe 55,788 hrs · 41,899 cycles

SUSPECT CRACK ON LEFT O/B AILERON NR 3 HINGE FITTING ON WING. LEFT O/B AILERON REMOVED IAW MM 27-10-10. HINGE FITTING NR 3 REMOVED IAW SRM 51-30-02. NEW HINGE FITTING INSTALLED IAW DRAWING 65-19275.

Part: BRACKET — CRACKED (BS 500 S26L) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI SMALL BRACKET ATTACHING AFT END OF INTERCOSTAL TO FRAME AT BS 500 IS CRACKED, INTERCOSTAL IS LOCATED ABOVE STR. 26L IN LWR FWD CARGO BAY BRACKET REPLACED IAW SRM 51-20-1, FIG 7 & SRM 51-30-02

Part: STRINGER — CRACKED (S5L BS 1030) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI STR. 5L FOUND CRACKED AT BS 1030 REPAIR CARRIED OUT IAW SRM 53-10-3 FIG 2

Part: PLUG — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

CORROSION FOUND ON 3RD WINDOW PANEL BLANK FROM AFT END LEFT SIDE EXTERIOR SURFACE LOWER ENDS AND 7TH FRAME FROM AFT END ABOVE STR 14L. WINDOW PLUG REPLACED IAW MM 56-20-00. WINDOW PLUG REPLACED DUE TO CORROSION EXCESSIVE, HOWEVER NO LIMITS EXIST PER SRM. CORROSION EXCEEDS 10 PERCENT MATERIAL THICKNESS IAW STANDARD PRACTICES.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 55,788 hrs · 41,899 cycles

NR 8 FLAP CARRIAGE LEFT AFT DEAD WEIGHT ROLLER BRACKET BOLT HOLE IS CORRODED. CORROSION REMOVED IAW OHM 57-58-01. BUSHINGS FABRICATED AND INSTALLED IAW OHM 57-58-01. NR 8 FLAP CARRIAGE REPAIRED IAW OHM 57-58-01.

Part: SHEAR TIE — CRACKED (S5L BS 990) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI STR. SHEAR TIE CRACKED AT S5L BS 990 SHEAR TIE REPLACED IAW SRM 51-20-1 & 51-40-3

Part: SHEAR TIE — CRACKED (BS990 STR.6 R/H) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.6 R/H B.S.990. STRINGER SHEAR TIE REMOVED IAW SRM 51-30-2. STR.SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-40-3.

Part: SHEAR TIE — CRACKED (BS1010 STR.4L) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR. 4 L BS 1010. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW SRM 51-20-1+51-40-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

STRINGER SHEAR TIE CRACKED AT S3L BS 990. CRACKED STRINGER SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-30-2.

Part: SKIN — CORRODED (BS 1178 - 1181) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CORROSION EVIDENT ON FUSELAGE SKIN EXTERNALLY AT BS 1178 STR. 10L & 9L, BS 1181 BETWEEN STR 9L & 8L, BS 1179 BETWEEN STR. 7L & 6L REPAIR CARRIED OUT IAW SMRO EO 2002-052-012. UPS ENGINEERING FILE N O. 727-53-20081

Part: BALLSCREW — CORRODED (T/E FLAP) · airframe 55,788 hrs · 41,899 cycles

NR 4 BALLSCREW AND NUT ASSY ARE BADLY CORRODED AT YOKE ATTACH POINT. NR 4 BALLSCREW AND NUT ASSY REPLACED AS REQ`D IAW MM 27-51-36 AND OHM 57- 54-04.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

STRINGER SHEAR TIE CRACKED AT STRINGER 6 RT BS 1050. SHEAR TIE REMOVED IAW SRM 51-30-2. SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-40-3.

Part: SHEAR TIE — CRACKED (BS1030 STR.8 R/H) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.8 R/H BS 1030. SHEAR TIE REMOVED IAW SRM 51-30-2. SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-40-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

STRINGER SHEAR TIE CRACKED AT STR 5 RT BS 1010. SHEAR TIE REPLACED IAW SRM 51-20-1, 51-40-3.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

CRACK ON NLG WHEEL WELL CEILING AT BS 284 BBL 6L. CRACKED AREA TRIMMED OUT IAW SRM 51-40-2 FIG 1. HFEC AROUND THE EDGE OF CUTOUT CARRIED OUT IAW SRM 51-40-2 PT 6 51-00-00 FIG 4, RESULTS NDF.

Part: SHEAR TIE — CRACKED (BS990 STR.5 R/H) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.5 R/H BS 990. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-40-3.

Part: SHEAR TIE — CRACKED (BS1010 STR.6) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.6 R/H BS 1010. SHEAR TIE REMOVED IAW SRM 51-30-2. SHEAR TIE REPLACED IAW SRM 51-20-1+51-40-3.

Part: SUPPORT BRACKET — CRACKED (AFT ENTRY DOOR) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI CRACK ON AFT ENTRY DOOR LONGITUIDINAL SUPPORT BRACKET AT RBL 8 WL 23 8 DOOR REMOVED IAW MM 52-13-00. SUPPORT BRACKET REMOVED IAW SRM 51-30- 2. NEW BRACKET FABRICATED IAW SRM 51-20-1 & 52-10-1.AFT ENTRY RE-INS TALLED IAW MM 52-13-00 FUNCTION CHECKED IAW MM 52-13-00. LEAK CHECKE D IAW MM 21-30-00 - NO LEAKS

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 55,788 hrs · 41,899 cycles

SUSPECT CRACK ON AFT LWR CARGO DOOR, CRACK IS LOCATED ON LOWER AFT CORNER JUST INSIDE NR 1 AFT DOOR STOP. HFEC CONFORMS CRACK, CARGO LOWER AFT FRAME REPLACED IAW DWG 65-18625.

Part: SHEAR TIE — CRACKED (BS 1070 STR.5 LH) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C+SI STR.5 L/H SHEAR TIE FOUND CRACKED AT BS 1070. STR. SHEAR TIE REMOVED IAW 51-30-2. STR. SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-40-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

TAILSKID COMPT LEFT UPPER TENSION TIE AFT FITTING CRACKED. REPLACED TENSION TIE FITTING IAW DRAWING 65-25992 AND SRM 51-30-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,788 hrs · 41,899 cycles

CORROSION ON RT BS 740 FRAME O/B WEB FLANGE. CORROSION REMOVED WAS OUTSIDE OF LIMITS OF EO B727-5310-7477. FITTING REPLACED IAW EO B727-5310-7477-E.

Part: FRAME — CORRODED (BS 740) · airframe 55,788 hrs · 41,899 cycles

INSPECTION TYPE:C&SI EVIDENCE OF CORROSION ON L/H BS 740 FRAME O/B WEB FLANGE REFER TO FI G 2 ITEM 3 (WEB SEPERATION) BS 740 FITTING REPLACED IAW SRM 51-30-2 DRG 65C13724 & EO B727-5310- 7477-E

Part: CONTROL PANEL — FAULTY (COCKPIT)

INSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT INDICATION ON TAKEOFF. RAN CHECKLIST FOR WW, FIRE LIGHT EXTINGUISHED. RETURNED FOR LANDING. AFTER LANDING WHEEL WELL FIRE INDICATIONS RESUMED. NO FIRE OBSERVED. LANDED 1300 LBS OVER LANDING WEIGHT. REMOVED AND REPLACED FIRE DETECTION PANEL OPS CHECKS GOOD IAW 26-11-02.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE: C, EVIDENCE OF CORROSION, NOSE WHEEL WELL TORQUE BOX WDF PANHEL BS 294 - 309 . REPAIR CARRIED OUT IAW SRM 53-10-9

Part: CASTING — CORRODED (AILERONS) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C, LT O/B AILERON LOCKOUT MECHANISM, MAIN SUPPORT CASTING HAS EVIDENCE OF CORROSION ON NUMEROUS BUSHING AREAS. CASTING REPLACED IAW SRM 51-30-02 & DRAWINGS 65-21776 & 65-21779

Part: CASTING — CRACKED (LT GEAR) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C, LT GEAR OPERATED DOOR SEQUENCE VALVE SUPPORT CASTING CRACKED. CASTING REPLACED IAW MM 32-32-31

Part: HINGE — CORRODED (SPOILER PANEL) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C BOTH END HINGES ON NR 7 SPOILER PANEL ARE CORRODED BEYOND LIMITS. REPLACED HINGES IAW SRM 51-30-02

Part: CASTING — CORRODED (WING) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C, NR 7 SPOILER SUPPORT CASTING IS CORRODED BEYOND LIMITS. NR 7 SPOILER CASTING REMOVED & REPLACED IAW DRW 65-16216 & IAW SRM 51- 10-2

Part: SUPPORT — CORRODED (NR 7 SPOILER) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C, NR 7 SPOILER, I/B END HINGE SUPPORT ATTACHED TO SPOILER SUPPORT BEAM I S CORRODED BEYOND LIMITS. /BEND HINGE REPLACED IAW SRM 51-30-02

Part: SUPPORT — CORRODED (AILERON) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C, O/B AILERON LT WING, ALL HINGE SUPPORTS ON REAR SPAR OF AILERON SHOW EVIDENCE OF CORROSION. LT O/B AILERON REMOVED IAW MM 27-10-31, NEW AILERON INSTALLED IAW MM 27-10-31.

Part: CASTING — CORRODED (AILERON GEARBOX) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE: C, EVIDENCE OF CORROSION ON LEFT OUTBOARD AILERON TURNAROUND GEARBOX CASTING. REPLACED GEARBOX CASTING IAW 27-10-131

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE: C, ON HFEC INSPECTION CRACKS FOUND ON FUSELAGE SKIN AT BS 235.8 BETWEEN SL 223 & 225 LT. SKIN REPAIR CARRIED OUT IAW SRM 530 FIG 3

Part: RIB — CORRODED (WING) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C, NR 7 SPOILER, SUPPORT RIB ON I/B SIDE ATACHED TO MLG BEAM IS CORRODED BEYOND LIMITS. REPLACED SUPPORT RIB IAW SRM 51-30-2

Part: WEB — CORRODED (FUSELAGE) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE: C, SURFACE CORROSION FOUND ON LOWER SURFACE OF HORIZONTAL WEB S18A RT, BETWEEN BS 880 & 950. ALL REPAIRS CARRIED OUT IAW SRM 51-10-6, 51-10-1, 51-10-2, 51-30-2 & SMRO EO 2001-013-001 UPS ENGINEERING FILE NO 727-53-20015

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE: C, CORROSION FOUND AT BS 870 LT ON S18A LWR AFT ATTACH BOLT LOCATION. REPAIR CARRIED OUT IAW SRM 51-10-6 & SHANNON MRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE:C CORROSION FOUND ON S18A LT AT BS 890 TO 940 HORIZ. FLANGE AT BODY F AIRING SUPPORT. REPAIR CARRIED OUT IAW SRM 51-30-2 51-30-6 & SMRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016

Part: HOUSING — CORRODED (RT EMERG. EXIT) · airframe 55,039 hrs · 41,300 cycles

INSPECTION TYPE: C, CORROSION ON OPERATING HANDLE HOUSING ON AFT RT EMERGENCY EXIT. OPERATING HOUSING REPLACED IAW SRM 51-30-2 & PER DRW 50-7978

Part: BRACKET — CRACKED (LT&RT ELEVATOR)

INSPECTION TYPE:C, LT AND RT ELEVATOR POSITION SENSOR BRACKETS CRACKED. LT AND RT ELEVATOR POSITION SENSOR BRACKETS REPLACED IAW MM 20- 80-01.

Part: SEAT TRACK — CRACKED (BS 560)

INSPECTION TYPE:C, SEAT TRACK CRACKED AT BS 560 RT SIDE. REPAIRED IAW SRM 53-10-5 FIG 5.

Part: STRINGER — CORRODED (BS 480)

INSPECTION TYPE:C, STRINGER CORRODED AT BS 480 STR 28L. STRINGER SPLICE SECTION REPAIRED IAW SRM 51-20-1 FIG 7.

Part: PANEL — CRACKED (RT AILERON)

INSPECTION TYPE:C, RT OUTBOARD AILERON LOWER SURFACE ACCESS PANEL T/E EXTRUSION CRACKED. EXTRUSION REPLACED IAW SRM 51-30-02.

Part: WEB — CRACKED (BS 277)

INSPECTION TYPE:C, NOSE WHEEL WELL, CEILING WEB HAD SUSPECT CRACK AT BS 277 APPROX AND RBL 14. DAMAGED AREA TRIMMED OUT IAW SRM 51-40-2, ALL EXISTING FASTENER HOLES IN PERIMETER ROW OF DOUBLER ZERO-TIMED PER SRM 51-10-1. WEB REPAIRED IAW SRM 51-40-02.

Part: SKIN — NICKED (CARGO DOOR)

INSPECTION TYPE:C, FWD CARGO DOOR LWR AFT CORNER SKIN NICKED. NICKED SKIN FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. SKIN BLENDED OUT LIMITS IAW SRM 52-00-2 FIG 1. FWD CARGO DOOR REPAIRED IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4.

Part: INTERCOSTAL — CRACKED (BS 1148)

INSPECTION TYPE:C, WEB CRACKED ON LWR LEG AFT OF BS 1148 LBL 3 INTERCOSTAL. INTERCOSTAL REPAIRED IAW SRM 51-40-03 FIG 1.

Part: BEAM — CORRODED (CARGO DOOR)

INSPECTION TYPE:C, ON REMOVAL OF ACCORDION SEAL, CORROSION FOUND ON UPPER BEAM OF MAIN CARGO DOOR. CORROSION REMOVED FROM UPPER BEAM, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. BEAM REPLACED IAW SRM 51-30-2, WITH REF TO BOEING DWG NR 65-25337. ALL AREA RE-PROTECTED AND SEALED REF SRM 51-10-2.

Part: BRACKET — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, AFT CARGO DOOR AFT HINGE AFT BRACKET CRACKED. REPLACED AFT CARGO AFT HINGE BRACKET IAW DRAWING NR 65-18625.

Part: HINGE — CRACKED (RT AILERON)

INSPECTION TYPE:C, RT OUTBOARD AILERON OUTBOARD HINGE SUPPORT CRACKED. REPLACED AILERON HINGE CASTING IAW DWG NR 65-19277.

Part: WEB — CRACKED (AFT AIRSTAIRS)

INSPECTION TYPE:C, CRACK ON WEB AT FWD LOWER LIGHTNING HOLE RT TORQUE BOX AFT AIRSTAIRS. REPAIRED AREAS IAW SRM 51-40-3.

Part: WEB — CRACKED (AFT AIRSTAIRS)

INSPECTION TYPE:C, CRACK ON WEB AT LIGHTNING HOLE (UPPER ROW 2ND FROM AFT) RT TORQUE BOX AFT AIRSTAIRS. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIRED AREA IAW SRM 51-40-2.

Part: CASTING — CRACKED (NR 3 LE FLAP)

INSPECTION TYPE:C, SUSPECT CRACK ON NR 3 L/E FLAP I/B ATTACH CASTING. NR 3 L/E FLAP REPLACED IAW MM 27-81-01.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE:C, CRACK FOUND ON 940 FRAME FITTING UPPER FWD FLANGE BELOW FLOOR LEVEL NDT. COFIRMED CRACK, REPAIRED PER EO B727-5310-3787.

Part: ANGLE — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, CRACK IN AFT CARGO DOOR FWD HINGE FWD ANGLE. REPLACED ANGLE IAW DRAWING NR 65-18625.

Part: FITTING — CRACKED (BS 520)

INSPECTION TYPE:AD, DURING NDT INSPECTION OF MAIN CARGO DOOR CAM SUPPORT FITTINGS. CRACK FOUND ON FITTING AT BS 520. FITTING BS 520 REPLACED IAW UPS EO B727-5230-0005 APPENDIX B.

Part: TR UNIT — MALFUNCTIONED (NR 3 ENGINE)

INSPECTION TYPE-N/A, ON CLIMBOUT NR 3 THRUST LEVER RAPIDLY RETARD TO IDLE A/C YAWED, T/R WARNING LIGHT CAME ON, PERFORMED APPROPRIATE CHECKLIST AND SECURED THE ENGINE. PERFORMED E/O B727-7100-10130 C/W, NO DEFECTS FOUND.

Part: BULB — FAILED (COCKPIT)

INSPECTION TYPE-N/A, COCKPIT EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY F/C OK (P/N 10-0067-9), (S/N 14867) ON, (S/N 32U) OFF.

Part: SKIN — CRACKED (LT ELEVATOR)

INSPECTION TYPE-C, LT ELEVATOR TRAILING EDGE FASTENER HOLES FOUND CRACKED AND DAMAGED. DAMAGE BLENDED OUT AND REPAIR CARRIED OUT IAW SRM 55-20-3, FIG 2.

Part: FITTING — DAMAGED (NR 3 TRUNNION)

INSPECTION TYPE-C, NR 3 TRUNNION FITTING FOUND TO HAVE A SURFACE IRREGULARITY DURING NDT PROCESS (FLUORESCENT DYE PENETRANT). NR 3 TRUNNION FITTING REPLACED IAW MM 71-21-01.

Part: HINGE — CRACKED (RT AILERON)

INSPECTION TYPE-C, RT OUTBD AILERON HINGE IS CRACKED, SECOND FROM INBD HINGE FITTING. REPLACED IAW 65-19275.

Part: SKIN — CRACKED (BS 251.6)

INSPECTION TYPE-C, CRACK FOUND ON FUSELAGE SKIN BS 251.6, WL 221.5. SKIN REPAIRED IAW SRM 53-30-3 FIG 3.

Part: SILL — CRACKED (BS 480-600)

INSPECTION TYPE-C, TO AID IN CORROSION REMOVAL PLEASE DISPLACE DOOR SILL WEB BS 480 TO 600 DOOR SILL WEB DERIVETED, INSPECTED AND FOUND CRACKED AND CORRODED. NEW WEB FABRICATED IN TWO SECTIONS IAW SRM 53-10-2, FIG 3 AND SPLICED AT BS 525 IAW SRM 51-40-2 FIG 1. WEB INSTALLED IAW DRAWING 65-40507.

Part: ANGLE — CRACKED (NR SPOILER ACT)

INSPECTION TYPE-C, NR 2 SPOILER ACTUATOR SUPPORT CASTING, ATTACH ANGLE ON REAR SPAR I/B CRACKED. ATTACH ANGLE REPLACED IAW SRM 51-30-2.

Part: SKIN — SCRATCHED (BS 530)

INSPECTION TYPE-C, FOUND SCRATCH 3 INCHES LONG NEAR OF FWD CARGO COMPARTMENT, RT SIDE STN 530 WL 188 SECTION 43. REMOVED SCRATCH AND REPAIRED IAW SRM 53-30-3, FIG 3.

Part: FRAME — CRACKED (BS 481)

INSPECTION TYPE-C, CRACK FOUND ON FUSELAGE FRAME AT BS 481 AT SEAT TRACK ATTACH HOLE LBL 62. CRACK REMOVED PER SRM 51-10-6 AND REPAIR CARRIED OUT IAW SRS EO 98-10-007.

Part: FITTING — CRACKED (BS 520)

INSPECTION TYPE-C, ON REMOVAL OF MAIN CARGO DOOR LATCH SUPPORT FITTING, FITTING FOUND CRACKED. NEW MAIN CARGO DOOR FITTING REPLACED IAW EO B727-5310-0437.

Part: BRACKET — CRACKED (RT ELEVATOR)

INSPECTION TYPE-C, RT ELEVATOR TRAILING EDGE CAVITY BRACKET CRACKED A FS 60 (ABOVE TAB ROD). BRACKET REPLACED IAW DRAWING NR 69-19144.

Part: FRAME — CRACKED (BS 490)

INSPECTION TYPE-C, TOE ON FRAME AT BS 490 FWD SIDE CRACKED AT LATCH SUPPORT FITTING OF MAIN CARGO DOOR. FRAME REPAIRED IAW SRM 53-10-4.

Part: FITTING — CORRODED (BS 487)

INSPECTION TYPE-C, ON REMOVAL OF BS 487 MAIN CARGO DOOR LATCH SUPPORT FITTING, CORROSION FOUND ON FITTING. NEW MAIN CARGO DOOR LATCH SUPPORT FITTING REAPLACED IAW EO B727-5310 -0437 APPENDIX 8.6 AND 8.7.

Part: WEB — CRACKED (BS 870)

INSPECTION TYPE-C, CRACK FOUND ON RT WHEEL WELL, FWD WALL BS 870. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: SKIN — DELAMINATED (LT TE FLAP)

INSPECTION TYPE-C, LT INBD AFT FLAP HAS DELAMINATION OUTBD LOWER SURFACE. REPAIRED IAW SRM 51-40-9.

Part: RIB — CRACKED (LT ELEVATOR)

INSPECTION TYPE-C, RESULTS OF X-RAY INSPECTION ON LT ELEVATOR SHOWS CRACK IN LOWER RIB REPAIR AREA BETWEEN ES 66.79 AND 69.79 AT 23 INCHES FWD OF TRAILING EDGE. DAMAGED AREA OF RIB TRIMMED OUT AND REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-10-006, UPS ENGINEERING FILE NUMBER 727-55-0369.

Part: RIB — CRACKED (LT ELEVATOR)

INSPECTION TYPE-C, RESULTS OF X-RAY ON LT ELEVATOR SHOWS CRACK IN LOWER RIB AREA BETWEEN ES 66.79 AND ES 71.79, 23 INCHES FWD OF TRAILING EDGE. DAMAGE TRIMMED OUT IAW SRM 55-20-1 AND REPAIR CARRIED IAW SRS ENGINEERING ORDER 98-10-006, REF UPS ENGINEERING FILE NUMBER 727-55-0369.

Part: WEB — CRACKED (BS 1380)

INSPECTION TYPE-C, SUSPECT CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1380. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: FRAME — CRACKED (BS 500)

INSPECTION TYPE-C, CRACK IN TOE OF FRAME AT BS 500 LT AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4, FIG 11.

Part: FRAME — CRACKED (BS 490)

INSPECTION TYPE-C, CRACK IN TOE OF FRAME AT STATION 490 LT AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4 FIGURE 11.

Part: FRAME — CRACKED (BS 580)

INSPECTION TYPE-C, CRACK IN TOE OF FRAME AT BS 580 LEFT HAND AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4 FIGURE 11.

Part: EXTRUSION — CORRODED (BS 480-600)

INSPECTION TYPE-C, CORROSION UNDER REMOVED TEFLON STRIP. ALL CORROSION REMOVED IAW SRM 51-10-6, ALL AREAS INSPECTED AND REPAIRED IAW SRS ENGINEERING ORDER 98-10-005, UPS FILE NUMBER 727-53-2017.

Part: PRESSURE WEB — CRACKED (BS 938)

INSPECTION TYPE-C, CRACK DETECTED IN CEILING OF RT WHEEL WELL AT BS 938 RBL 36. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIR COMPLETED PER EO B727-5 310-0460-L.

Part: PRESSURE WEB — CRACKED (BS 938)

INSPECTION TYPE-C, CRACK DETECTED IN CEILING OF LT WHEEL WELL AT BS 938 LBL 55. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIR CARRIED OUT IAW EO B72 7-5310-0460, APPENDIX C.

Part: CASTING — CORRODED (RT AILERON)

INSPECTION TYPE-C, RT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. CASTING REPLACED IAW SRM 51-30-2.

Part: CASTING — CORRODED (LT AILERON)

INSPECTION TYPE-C, LT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. REPLACED CASTING WITH NEW ONE IAW SRM 51-30-2.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE:C CRACKS FOUND ON BS 740 FITTING OUTBD FLANGE BETWEEN S18R AND S20R AND LOWER END OF FITTING. FITTING REPAIRED IAW UPS ENGINEERING ORDER B727-5310-7497.

Part: FRAME — CORRODED (BS 870)

INSPECTION TYPE-D, CORROSION ON BS 870 FRAME, FWD LOWER TANG AT SEAL OF STR 18A. REMOVED CORROSION AND REPAIRED.

Part: ANGLE — CRACKED (AFT CARGO DOOR)

INSPECTION TYPE-D, THREE WEBS AND AN ATTACH ANGLE WERE FOUND CRACKED ON THE INTERNAL OF THE AFT CARGO DOOR. REPLACED WEBS AND ANGLE.

Part: SEAT TRACK — CORRODED (BS 620)

INSPECTION TYPE-D, SEAT TRACK FLANGE AT BS 620, LBL 62.5 CORRODED. REPAIRED PER SRM 53-10-5.

Part: FITTING — CRACKED (LT TE MID FLAP)

INSPECTION TYPE-D, FLANGE OF FLAP CARRIAGE FITTING ON LT O/B MID FLAP AT STATION 442 CO RRODED AND CRACKED. REPAIRED PER BOEING INSTRUCTIONS SRS EO 96-33-03.

Part: FRAME — CRACKED (BS 880)

INSPECTION TYPE-D, CREASE BEAM CRACKED AT BS 880, STRINGER 15L. REPLACED FRAME CHORD AT BS 880 PER SRM 51-30-2.

Part: FRAME — CRACKED (FWD ENTRY DOOR)

INSPECTION TYPE-D, CRACK IN FWD ENTRY DOOR FWD FRAME. REPAIRED PER BOEING INSTRUCTIONS SRS EO 96-33-05.

Part: SILL — CORRODED (BS 310-350)

INSPECTION TYPE-D, DOOR SILL TOP HAT SECTION CORRODED AT BS 310 TO 350, RBL 14. REPLACED DOOR SILL EXTRUSION.

Part: SEAT TRACK — CRACKED (BS 950)

INSPECTION TYPE-D, SEAT TRACK CRACKED AT BS 950, LBL 63. REPAIRED PER SRM 53-10-1.

Part: SPAR — CRACKED (WS 290)

INSPECTION TYPE-D, CRACK IN REAR SPAR UPPER CHORD AT WS 290 RT. REPAIRED PER BOEING INSTRUCTIONS SRS EO 96-33-01.

Part: HINGE FITTING — CRACKED (LT AILERON)

INSPECTION TYPE-D, LT AILERON HINGE FITTING ON WING T/E IS CRACKED. REPLACED FITTING PER DRAWING 65-19276.

Part: WINDOW FRAME — CORRODED (BS 227.8-235.8)

INSPECTION TYPE-D, SURFACE CORROSION ON UNDERSIDE OF RT SLIDING WINDOW FRAME AT STA 227 .78 TO 235.8. REPLACED WEB.

Part: RIB — CRACKED (LT TE MIDFLAP)

INSPECTION TYPE-D, LT WING O/B MID FLAP INTERSPAR RIB CRACKED AT STATION 319. REPLACED RIB.

Part: STIFFENER — CORRODED (BS 243.7)

INSPECTION TYPE-D, CORROSION ON STIFFENER ANGLE ON FRAME AT STA 243.7, STRINGER 14R. STIFFENER REPLACED PER SRM 51-30-2.

Part: FRAME — CRACKED (AFT CARGO DOOR)

INSPECTION TYPE-D, CRACK ON AFT CARGO DOOR MAIN FRAME RADIUS BELOW UPPER FWD DOOR STOP. REPLACED PER BOEING DRAWING 65-18625.

Part: STRINGER — CORRODED (BS 860)

INSPECTION TYPE-D, STRINGER 18A, BS 860 CORRODED. REPAIRED PER SRS EO 96-33-02.

Part: RIB — CRACKED (LT TE MIDFLAP)

INSPECTION TYPE-D, LT WING O/B MID FLAP INTERSPAR RIB CRACKED AT STA 321. REPLACED RIB.

Part: RIB — CRACKED (LT TE MIDFLAP)

INSPECTION TYPE-D, LT O/B MID FLAP O/B INTERSPAR RIB CRACKED. REPLACED RIB.

Part: FLOORBEAM — CORRODED (BS 560)

INSPECTION TYPE-D, CORROSION UNDER ANCHOR NUT ON FLOORBEAM AT BS 560, LBL 55. FLOORBEAM REPAIRED SRS EO 96-33-015.

Part: ANGLE — CRACKED (BS 720-740)

INSPECTION TYPE-D, CRACK IN INTERCOSTAL AND ATTACH ANGLE BETWEEN FLOORBEAMS 720 AND 740. REPLACED ANGLE AND REPAIRED WEB PER SRM 51-10-1, 53-10-2.

Part: FLOORBEAM — CORRODED (BS 560)

INSPECTION TYPE-D, CORROSION UNDER ANCHOR NUT ON FLOORBEAM AT BS 560, LBL 35. REPAIRED FLOORBEAM.

Part: RIB — CRACKED (LT TE MIDFLAP)

INSPECTION TYPE-D, LT O/B MID FLAP INTERSPAR RIB CRACKED AT STA 388. REPLACED RIB.

Part: EEL — MALFUNCTION (CABIN)

WHILE ON GROUND AT CGN, MAINTENANCE FOUND DURING TESTING, LIGHTS GOING DIM RAPIDLY. MAINTENANCE REPLACED ASSY, F/C GOOD.

Part: HYD FLUID — LOSS (A HYD SYST)

AFTER TAKEOFF FROM VIE TO NUE DURING GEAR RETRACTION, THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1.8 GALLONS. A-SYSTEM LOSS CHECKLIST ACCOMPLISHED AND AFTER MANUAL GEAR EXTENSION, THE A-SYSTEM QUAN. RETURNED TO 3.4 GALS. UNEVENTFUL EMERGENCY LANDING PERFORMED IN NUE. SERVICED HYD SYSTEM BY 1.5 GALLONS, PRESSURIZED ALL HYD SYSTEMS AND ENGINES, RAN ALL HYD SYSTEMS, NOTHING FOUND ABNORMAL.