N943UP

Part: FLAP — CORRODED (RT WING) · airframe 52,842 hrs · 41,031 cycles

INSPECTION TYPE:AD SUSPECT CORROSION BETWEEN SKIN MIDSPAR OF RT INBD MIDFLAP WBL130 APPROX. CORROSION FOUND TO BE OUT OF LIMITS, FLAP REPLACED IAW TC 1259

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 52,842 hrs · 41,031 cycles

INSPECTION TYPE:C CRACK FOUND ON DOOR STOP AT LWR AFT CORNER OF FWD PIT DOOR. REPLACED CRACKED FITTING IAW B727-5230-0032.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, CORROSION ON STR 19 L AT BS 360 IN E & E BAY. STR 19L REPLACED IAW DRAWING 65-18420.

Part: WEB — CRACKED (LT MLG WW) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, LT MLG WHEEL WELL, SUSPECT CRACKS IN KEEL BEAM WEB, AREA FWD OF APU CUTOUT COVERED BY REPAIR PLATE. REPAIR CARRIED OUT IAW EO B727-5330-1995-B.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, CRACK ON FWD LT CORNER OF FWD LWR NOSE ACCESS DOOR ON INNER LIP OF DOOR FRAME. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, RT MLG WHEEL WELL SUSPECT CRACK TO VERT CHORD AT BS 870 TO KEEL BEAM JOINT, 16.5 INCHES FROM BOTTOM OF CHORD. REPAIR CARRIED OUT IAW B727-5330-1995-B.

Part: SUPPORT BRACKET — CORRODED (VERTICAL STAB) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, VERT STAB, FAIRING SUPPORT AT JUNCTION OF TENSION TIE RIB AND VERT STAB FRONT SPAR IS WORN DUE TO FRETTING CORROSION LT. REPLACED FAIRING SUPPORT STRUCTURE IAW BOEING INST DRG 65-17485 & SRM 51-30-02.

Part: FLANGE — CORRODED (FAIRING) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, FAIRING 3608 AFT SUPPORT FRAME AFT FLANGE CORRODED. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, ON INSP HORIZ STIFFENER ON LWR BODY 740 FRAME FOUND CORRODED AT BBL 0. STIFFENER REMOVED IAW SRM 51-30-02, STIFFENER REPLACED IAW SRM 51-10-02.

Part: JACKSCREW — CORRODED (TE FLAPS) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, NR 5 TRANSMISSION YOKE ASSY & JACKSCREW ARE BADLY CORRODED. JACKSCREW REPLACED IAW MM 27-51-41.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, CRACK IN FUSELAGE SKIN AT BS 243.7 LT. REPAIR CARRIED OUT IAW SRM 51-30-03.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, SUSPECT CRACK IN UPPER LIGHTENING HOLE 6 O CLOCK POSITION BS 1300 LT. CRACK STOPPED DRILLED IAW SRM 51-10-1, CRACK FOUND TO BE WITHIN LIMITS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, CORROSION ON STR 18L AT BS 360. REPAIR CARRIED OUT IAW SRM 51-10-54 AND SRM 51-30-2.

Part: FRAME — CORRODED (CENTER WING) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, RIVET POPPED AND EVIDENCE OF CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870. REPAIR CARRIED OUT IAW SRM 51-30-02 & SRM 51-20-4 AND DRAWING 65C215 66.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 52,306 hrs · 40,474 cycles

INSPECTION TYPE:C, SUSPECT CRACK IN UPPER LIGHTENING HOLE 70 C POS BS 1243 LT AFT AIRSTAIRS AREA. REPAIR CARRIED OUT IAW SRM 51-10-1.

Part: BRACKET — CRACKED (TE FLAPS)

INSPECTION TYPE:C, NR 7 FLAP TRACK MID FAIRING AFT SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW DRAWING 65-21796.

Part: FAIRING — CRACKED (TE FLAPS)

INSPECTION TYPE:C, NR 7 FLAP TRACK MID FAIRING OUTBOARD TRACK CRACKED. TRACK REPLACED IAW DRAWING 65-21796.

Part: FAIRING — CRACKED (TE FLAPS)

INSPECTION TYPE:C, NR 8 FLAP TRACK MID FAIRING INBOARD TRACK CRACKED. TRACK REPLACED IAW DRAWING 65-21796.

Part: BRACKET — CRACKED (TE FLAPS)

INSPECTION TYPE:C, NR 1 FLAP TRACK MID FAIRING AFT SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 AND DRAWING 65-21796.

Part: BRACKET — CRACKED (NR 3 TR UNIT)

INSPECTION TYPE:C, NR 3 ENGINE THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 AND MM 78-30-00.

Part: ANGLE — CRACKED (BS 500)

INSPECTION TYPE:C, CRACKED FRAME ANGLE AT FWD SIDE OF LATCH SUPPORT FITTING AT BS500 FWD CARGO BAY. FRAME ANGLE REPAIRED IAW SRM 53-10-4.

Part: ANGLE — CRACKED (RT WING)

INSPECTION TYPE:C, RT WING TE PANEL OUTBOARD OF NR 7 FLAP TRACK, ATTACH ANGLE CRACKED. ANGLES REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 1090)

INSPECTION TYPE-D, CORROSION BETWEEN INTERNAL STRUCTURE AND SKIN DOUBLER BS 1090 STR 18R. CORROSION REMOVED IAW SRM 51-10-6. REPAIR CARRIED OUT IAW SRS EO 98 -01-025 R1.

Part: TEE — CRACKED (BS 1409)

INSPECTION TYPE-D, CRACK ON ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL AT STATION 1409 RT SIDE (NR 2 ENG AFT MOUNT SUPPORT RIB CHORD). SUPPORT RIB TEE CHORD REPLACED IAW DRAWING 65-22913 AND 65-17551.

Part: SKIN — CORRODED (BS 1115)

INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND STRUCTURE AT BS 1115 BETWEEN S18R AND S19R. REPAIRED IAW SRS EO 98-01-025R1.

Part: WEB — CORRODED (CARGO COMPT)

INSPECTION TYPE-D, ON FURTHER INSPECTION OF DAMAGED ANCHOR NUTS EXTRUSION WAS CORRODED AND WEB DAMAGED. REPLACED EXTRUSION WITH 65-24258-1 IAW DRAWING 65C33855.

Part: CASTING — CORRODED (LT AILERON)

INSPECTION TYPE-D, LT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. CASTING REPLACED IAW SRM 51-10-1 AND MM 20-80-1.

Part: BOLT — CORRODED (CARGO DOOR)

INSPECTION TYPE-D, MAIN CARGO DOOR AFT HINGE BOLT ON PRESS RELIEF DOOR BADLY CORRODED. MAIN CARGO DOOR BOLT AND BUSHING REPLACED PER STANDARD PRACTICES 20- 50-01.

Part: TEE — CRACKED (NR 2 ENGINE)

INSPECTION TYPE-D, CRACK ON VERTICAL ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, LT SIDE AT STATION 1409 NR 2 ENGINE AFT MOUNT SUPPORT RIB CHORD. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-01-012R1.

Part: REAR SPAR — CRACKED (LT ELEVATOR)

INSPECTION TYPE-D, LT ELEVATOR HAS CRACKED REAR SPAR, CRACKED HINGE LUG, AND CRACKED LOWER SKIN. REPLACEMENT ELEVATOR INSTALLED IAW MM27-30-01.

Part: CARRIAGE — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE-D, NR 3 FLAP CARRIAGE IS CORRODED IN SPINDLE BORE AND AROUND LARGE BEARING. SEAT CARRIAGE REPLACED IAW OHM 57-58-01.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-D, RT BS 740 FUSELAGE FITTING HAS NEW CRACK ON LOWER OUTBD WEB FLANGE (VERTICAL). FITTING REMOVED AND NEW FITTING INSTALLED PER UPS ENGINEERING ORDER B727-5310-7477C.

Part: WEB — CRACKED (BS 1380)

INSPECTION TYPE:D, FOUND CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL LT SIDE, BS1380 CRACKED WEB REMOVED. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65 -17555.

Part: HINGE LUG — CRACKED (RT ELEVATOR)

INSPECTION TYPE-D, RT ELEVATOR NR 3 HINGE LUG ES 66.50 CRACKED. HINGE LUG FITTING REPAIRED IAW SRS ENGINEERING ORDER 98-01-014.

Part: ANGLE — CORRODED (BS 740)

INSPECTION TYPE:D UPPER CHORD ANGLE OF BS 740 LOWER SECTION WL 170.5, BETWEEN LBL 40 AND RBL40, FOUND CORRODED AT VARIOUS LOCATIONS. CORRODED UPPER CHORD ANGLE REMOVED AND NEW CHORD ANGLE FITTED IAW DRAWING 65-15940.

Part: FRAME — CORRODED (NLG DOOR)

INSPECTION TYPE-D, CORROSION FOUND ON INBOARD SKIN FRAME LT DOOR OF NOSE WHEEL WELL. LT NLG FWD WHEEL DOOR I/B FRAME REPLACED PER SRM 52-80-1 FIG 1 SRM 51-10-1 AND DRAWING 65-17563.

Part: FITTING — CORRODED (WS 357)

INSPECTION TYPE-D, RT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. RT I/B AILERON TURNAROUND FITTING REPLACED IAW SRM 51-10-1 ADN MM20 -80-1.

Part: FRAME — CRACKED (BS 783.95)

INSPECTION TYPE:, ON INSPECTION FOUND CRACK ON FRAME BS 783.958 RT AT FOURTH FASTENER ABOVE FLOOR. REPAIR CARRIED OUT IAW APPENDIX C OF EO B727-5310-5474 AND SRS ENGINEERING ORDER 98-01-021.

Part: CARRIAGE — CORRODED (NR 4 TE FLAP)

INSPECTION TYPE-D, NR 4 FLAP CARRIAGE DEAD WEIGHT ROLLER HOLES ON I/B AND O/B SIDES ARE CORRODED. HOLES OVERSIZED PER OHM 57-58-02. BUSHINGS MANUFACTURED AND INSTALLED PER OHM 57-58-02.

Part: ANGLE — CRACKED (BS 880)

INSPECTION TYPE-D, TWO CRACKS AT TOP FASTENER HOLES IN FRAME ANGLE BS 880 RT AT STRINGER 15. REPAIR CARRIED OUT WITH NEWLY FABRICATED REPAIR ANGLE PER SRM 51-40- 3 FIGURE 1.

Part: ACCESS PANEL — CORRODED (NR 1)

INSPECTION TYPE-D, NR 1 FUEL ACCESS PANEL HAS CORROSION RT WING. FUEL ACCESS PANEL REPLACED IAW MM 28-11-21.

Part: STRINGER — DAMAGED (BS 740)

INSPECTION TYPE-D, STRINGER END FOUND DAMAGED ON REMOVAL TO AID BS 740 FITTING REPLACEMENT, DUE TO INCORRECT FITMENT INTO STRINGER 16R AT BS 740. STRINGER END AND STRINGER SECTION BETWEEN BS 740 AND 760 REPLACED IAW DRG NR 65C13724.

Part: FLAP TRACK — CORRODED (WS 442)

INSPECTION TYPE-D, WING LUG FOR NR 8 FLAP TRACK WBL 442 HAS CORROSION. CORROSION REMOVED AND THEN REPAIRED PER SRS ENGINEERING ORDER 98-01- 023.

Part: INTERCOSTAL — CRACKED (DOORSTOP)

INSPECTION TYPE-D, DOOR STOP INTERCOSTAL FOUND CRACKED. INTERCOSTAL FABRICATED FROM 7075-0, 0.050 INCH THICK AND INSTALLED IAW SRM 51-30-2.

Part: FLAP CARRIAGE — CORRODED (NR 7 TE FLAP)

INSPECTION TYPE-D, NR 7 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BARE AND AROUND LARGE BEARING SEAT. NR 7 FLAP CARRIAGE REPLACED IAW OHM 57-52-11 AND 27-51-13.

Part: FLAP TRACK — CORRODED (WS 348)

INSPECTION TYPE-D, WING LUG FOR NR 7 FLAP TRACK WBL 348 APPROX HAS CORROSION. CORROSION REMOVED AND LUG REPAIRED IAW SRS ENGINEERING ORDER 98-01-0 22.

Part: ANGLE — CRACKED (FRONT SPAR)

INSPECTION TYPE-D, TEE ANGLE AT FRONT SPAR UPPER CHORD BBL 24.5 RT CRACKED (WING CENTER SECTION INTERIOR). TEE ANGLE REPLACED IAW EO B727-5710-4575.

Part: SHEAR TIE — CRACKED (CARGO COMPT)

INSPECTION TYPE-D, LOWER FWD CARGO COMPARTMENT SHEAR TIE AT FRAME 540 ABOVE STRINGER 18L IS CRACKED. SHEAR TIE REPAIRED IAW SRM 51-40-03 FIGURE 1.

Part: DOOR STOP — CRACKED (CARGO DOOR)

INSPECTION TYPE-D, LOWER AFT CARGO DOOR, NR 1 FWD STRUCTURAL STOP CRACKED. STOP REPLACED IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 580)

INSPECTION TYPE-D, LOWER FWD CARGO COMPARTMENT STRINGER 19L BETWEEN BS 580 AND 600 IS CRACKED. STRINGER REPAIRED IAW SRM 53-10-3.

Part: WEB — CORRODED (BS 220)

INSPECTION TYPE-D, CORROSION ON WEB OF AFT LT CORNER OF LOWER FORWARD NOSE CUTOUT, BS 220 APPROX, WL 156 APPROX. WEB REPLACED IAW SRM 57-30-2.

Part: CLEAT — CRACKED (BS 1010)

INSPECTION TYPE-D, CRACKED CLEAT BS 1010, STRINGER 3L. REPLACED STRINEGR CLIP IAW SRM 51-30-2.

Part: FLAP CARRIAGE — CORRODED (NR 8 TE FLAP)

INSPECTION TYPE-D, NR 8 FLAP CARRIAGE IS CORRODED INSIDE SPINDLE BARE AND AROUND LARGE BEARING SEAT AREA. NR 8 FLAP CARRIAGE REPLACED IAW OHM 57-52-11 AND MM 27-51-13.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE-D, SEVERAL AREAS OF CORROSION ON UPPER CHORD OF FLOORBEAM, BS 344 BL 0 TO LBL 50. ALSO, EXISTING SPLICE FROM LBL 54 TO RBL 16. NEW UPPER CHORD OF BS 344 FLOORBEAM REPLACED IAW SRM 51-30-02 AND DRAWING 65-16316.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE-D, CORROSION IN FLOORBEAM UPPER CHORD AT BS 312 LBL 46 AT EXISTING BLENDOUT. AREA REPAIRED IAW SRM 53-10-8.

Part: SEAT TRACK — CRACKED (BS 344-360)

INSPECTION TYPE-D, SHORT SECTION OF SEAT TRACK BETWEEN BS 344 AND BS 360 AT RBL 62 IS CRACKED. SECTION OF SEAT RAIL REPLACED IAW IAW SRM 51-30-2.

Part: BOTTLE PIN — PITTED (BS 870)

INSPECTION TYPE-D, RIGHT HAND REAR BOTTLE PIN HAS WEAR AND LIGHT PITTING. RIGHT HAND AFT BOTTLE PIN REPLACED IAW MM 57-41-01.

Part: BOTTLE PIN — PITTED (LT WING/FUS)

INSPECTION TYPE-D, LT REAR SPAR BOTTLE PIN HAS WEAR AND LIGHT PITTING. LT AFT BOTTLE PIN REPLACED IAW MM 57-41-01.

Part: STRINGER — CORRODED (BS 735)

INSPECTION TYPE-D, CORROSION ON STRINGER 21R BS 735. STRINGER REPAIR CARRIED IAW SRM 53-10-3 FIG 1.

Part: ANGLE — CRACKED (BS 900)

INSPECTION TYPE-D, TWO CRACKS DISCOVERED AT TOP FASTENER HOLES IN FRAME ANGLE BS 900 LT AT STRINGER 15. REPAIR CARRIED OUT IAW SRM 51-40-3, FIGURE 1.

Part: SKIN — CRACKED (WS 105)

INSPECTION TYPE-D, CRACK ON INNER SKIN L/E STN 105 (RIGHT HAND WING LEADING EDGE). DAMAGE REPAIRED IAW SRM 57-30-4.

Part: ANGLE — CRACKED (BS 920)

INSPECTION TYPE-D, TWO CRACKS DISCOVERED AT TOP FASTENER HOLES IN FRAME ANGLE BS 920 LT AT STRINGER 15. REPAIR CARRIED OUT IAW SRM 51-40-3 FIGURE 1.

Part: INTERCOSTAL — CRACKED (BS 304)

INSPECTION TYPE-D, INTERCOSTAL TO BEAM TIE CRACKED AT BS 304, LBL 12. NEW BRACKET INSTALLED IAW SRM 51-30-02.

Part: STRINGER — CRACKED (BS 880)

INSPECTION TYPE:D ON REMOVAL OF DAMAGE ON OUTER CHORD OF FRAME AT BS 880 RT STRINGER 15R, SUSPECT CRACK FOUND IN LOWER HOLE STRINGER. REPAIR CARRIED IAW SRM 53-10-3

Part: STIFFENER — CRACKED (RT ELEVATOR)

INSPECTION TYPE-D, RIGHT HAND ELEVATOR ES 103.5 HAS CRACK IN LOWER SKIN STIFFENER IN REPAIRED AREA 19 FWD OF TRAILING EDGE. REPAIR CARRIED OUT IAW SRS EO 98-01-008.

Part: FLAP TRACK — CORRODED (TE FLAP)

INSPECTION TYPE-D, ON REMOVAL OF BUSHINGS FROM NR 4 AND NR 5 FLAP TRACK WING LUGS, CORROSION WAS FOUND IN THE BORE AREA REWORKED IAW SRS ENGINEERING ORDER 98-01-024.

Part: FLAP TRACK — CORRODED (WS 203)

INSPECTION TYPE-D, NR 3 FLAP TRACK WING LUG WBL 203 HAS CORROSION. CORROSION REMOVED AND REPAIR THEN CARRIED OUT PER SRS ENGINEERING OR DER 98-01-018.

Part: FLAP TRACK — CORRODED (WS 203)

INSPECTION TYPE-D, NR 6 FLAP TRACK WING LUG, WBL 203 APPROX, HAS CORROSION. CORROSION REMOVED AND REPAIR THEN CARRIED OUT PER SRS ENGINEERING OR DER 98-01-012.

Part: FLAP TRACK — CORRODED (NR 3 FLAP TRACK)

INSPECTION TYPE-D, NR 3 FLAP TRACK CORROSION PAD B. CORROSION REMOVED AND REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 9 8-01-015.

Part: FLAP TRACK — CORRODED (WS 224)

INSPECTION TYPE-D, NR 6 FLAP TRACK PAD B HAS CORROSION. CORROSION REMOVED AND PAD REPAIRED IAW SRS ENGINEERING ORDER 98-01-0 16.

Part: ANGLE — CRACKED (BS 880)

INSPECTION TYPE-D, 2 CRACKS FOUND AROUND TOP FASTENER HOLES IN FRAME ANGLE BS 880 LT AT STRINGER 15. REPAIRED IAW SRM 51-40-3 FIGURE 1.

Part: FITTING — CORRODED (NLG)

INSPECTION TYPE-D, ON REMOVAL OF NLG DRAG BRACE SUPPORT FITTING, CORROSION WAS DISCOVERED ON THE DRAG BRACE SUPPORT BEAM. BEAM REPAIRED IAW SRS ENGINEERING ORDER 98-01-004.

Part: SPAR — CORRODED (WS 349)

INSPECTION TYPE: C. WHILE CARRYING OUT REPAIR TO LEADING EDGE AT WS 349 ON RT WING, CORROSION FOUND ON UPPER SURFACE OF FRONT SPAR UPPER CHORD. REPAIR CARRIED OUT PER BOEING INSTRUCTIONS. SEE SRS EO 96-35-005 REFERENCE UPS REPAIR AUTHORIZATION ENGINEERING FILE NUMBER 727-57-17 43.

Part: FLAP TRACK — CORRODED (RT TE FLAP)

INSPECTION TYPE-C, RT I/B FLAP TRACK IS CORRODED AT ATTACHMENT TO MLG SUPPORT BEAM. REPAIRED IAW B727-5742-0651.

Part: RIB — CRACKED (RT TE MID FLAP)

INSPECTION TYPE: C. RT INBD MID-FLAP CRACK ON INTERSPAR RIB AT WBL 226. REPAIR CARRIED OUT IAW SRM 57-50-4 FIG 6.

Part: RIB — CRACKED (RT TE MID FLAP)

INSPECTION TYPE: C. CRACK ON INTERNAL TE RIB AT WBL 210 OF THE RT INBD MID-FLAP. REPAIR PER SRM 51-40-04 FIG 1.

Part: RIB — CRACKED (RT TE MID FLAP)

INSPECTION TYPE: C. RT INBD MID-FLAP CRACK ON INTER SPAR RIB AT STA 230 WBL. REPAIRED PER SRM 57-50-4 FIG 6.

Part: RIB — CRACKED (RT TE MID FLAP)

INSPECTION TYPE: C. RT INBD MID FLAP CRACKED IN INTER SPAR RIB AT STA 154. REPAIRED PER SRM 57-50-4 FIG 6.

Part: RIB — CRACKED (RT TE MID FLAP)

INSPECTION TYPE: C. RT INBD MID FLAP CRACKED AT STA WBL 150. REPAIRED PER SRM 57-50-4 FIG 6.

Part: SKIN — CRACKED (CARGO DR CUTOUT)

INSPECTION TYPE: C. CRACK IN SKIN AT FWD CARGO DOOR (LWR) CUT OUT AFT LWR CORNER. REPAIR CARRIED OUT PER BOEING INSTRUCTIONS (SEE SRS EO 96-35-006) UPS EO B727-5330-8728-A.

Part: FITTING — CRACKED (BS 500)

INSPECTION TYPE: C. MAIN CARGO DOOR LATCH SUPPORT FITTING BS 500 LT FOUND CRACKED. REPLACED PER UPS EO B727-5310-0437.

Part: STOP FITTING — CRACKED (AFT CARGO DOOR)

INSPECTION TYPE: C. LOWER AFT CARGO DOOR STOP CUT OUT. DOOR STOP CRACKED AT AFT FRAME MID STOP. REPLACED PER SRM 51-30-2.

Part: DOOR STOP — CRACKED (CARGO DOOR)

INSPECTION TYPE: C. LOWER AFT CARGO DOOR CUT OUT. DOOR STOP CRACKED AT AFT FRAME MID STOP. STOP REPLACED IAW SRM 51-30-2.

Part: SKIN — OIL CANNING (BS 440)

INSPECTION TYPE: C. FUSELAGE AT BS 440 BETWEEN S21-S22L SKIN IS PANTING ( OIL CANNING). REPAIRED PER SRM 53-30-3 FIG 1.

Part: TR DOOR — CRACKED (NR 3 ENGINE)

INSPECTION TYPE: C. NR 3 ENGINE TR LOWER DOOR CRACK 2.5 INCHES LONG LOCATED FWD RT SIDE IN A FORE/AFT DIRECTION. REPAIRED PER DEE HOWARD SRM SUPPLEMENT 78-30-01.