N729CK

Part: PRESSURE SYSTEM — FAILED · airframe 42,583 hrs · 23,076 cycles

RIGHT PACK FAILED DURING CLIMBOUT - UNABLE TO PRESSURIZE. PERFORMED OPS CHECK OF COOLING PACKS IAW B727 AMM 21-55-00 OPS CHECK GOOD

Part: ACCESSORY UNIT — FAILED (ZONE 100) · airframe 42,140 hrs · 22,946 cycles

GEAR HANDLE WILL NOT GO UP PASS THE OFF POSITION. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: TROUBLESHOOT PER AMM 32-31-00 & 32-31-00. VERIFIED LANDING GEAR CONTROL VALVE IS OPERATING OK, FOUND OK PER AMM 32-31-31.SIMULATED AIRPLANE-IN-AIR CONDITION PER AMM 32-42-00. R&R LDG GEAR ACCESSORY UNIT, PERFORMED GEAR RETRACTION PER AMM 32-33-00 OPS CK GOOD

Part: NONE — NONE · airframe 41,963 hrs · 22,868 cycles

PROBLEM DESCRIPTION: #3 AC GENERATOR DRIVE OIL LOW PRESSURE LIGHT ILLUMINATED DURING CRUISE. ON APPROACH TO TCL #1 AND #2 A/C GENS. TRIPPED WITH ASSOCIATED UNDER EXCITATION FAULTS, SYSTEMS ONE AND TWO , #2 GB AND GF LIGHTS ILLUMINATED, #1 GB ILLUMINATED. #1 BT CLOSED THEN TRIPPED. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: CORRECTIVE ACTION CURRENTLY IN WORK

Part: SENSOR — DIRTY (MLG) · airframe 41,538 hrs · 22,525 cycles

LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, LEVER WOULD NOT GO PAST OFF POSITION. CLEANED, INSPECTED AND ADJUSTED GEAR SAFETY SENSORS IAW B727 AMM 32-09-22, PERFORMED OPS TEST OF NORMAL LANDING GEAR SYSTEM IAW B727 AMM 32-31-00 NO DEFECTS NOTED AT THIS TIME

Part: ENGINE — STALLED (NR 1) · airframe 40,680 hrs · 22,111 cycles

PROBLEM DESCRIPTION: ON CLIMBOUT BETWEEN 9000’ - 10000’ EXPERIENCED A COMPRESSOR STALL EPR INDICATED 1.9 ON NR 2 AND NR 3 AND 1.8 ON NR 1. AT 11000’ EXPERIENCED A SECOND COMPRESSOR STALL AND SUBSEQUENT ENGINE ROLLBACK ON NR 1 ENGINE. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: REMOVE AND REPLACED NR 1 ENGINE. ENGINE SENT TO SHOP FOR FURTHER INSPECTION.

Part: FUEL CONTROL — FAILED (NR 3 ENGINE) · airframe 40,535 hrs · 22,040 cycles

ON TAKEOFF ROLL, NR 3 ENGINE DID NOT PRODUCE FULL THRUST, AIRCRAFT PERFORMED REJECTED TAKEOFF. TROUBLESHOOTING IN WORK AT THIS TIME.

Part: LINKAGE — DISCONNECTED (NLG) · airframe 40,301 hrs · 21,850 cycles

NOSE LANDING GEAR RED WARNING LIGHT REMAINED ON AFTER GEAR EXTENSION, CYCLED GEAR AND UNSAFE INDICATION REMAINED ON. TROUBLESHOT NOSE GEAR UNSAFE INDICATION IAW AMM 32-61-71 FOUND POSITION SWITCH LINKAGE DISCONNECTED FROM THE NOSE LANDING GEAR DRAG BRACE INSTALLED NOSE GEAR POSITION SWITCH OPERATING LINKAGE IAW AMM 32-61-71. OPS CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,714 hrs · 21,560 cycles

MAIN DECK R/H FASTENER HOLE JUST BELOW FLOOR HAS A CRACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,714 hrs · 21,560 cycles

FWD ENTRY DOOR LOWER HINGE CUTOUT FUSELAGE SKIN.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 39,714 hrs · 21,560 cycles

CRACK SEAT TRACK.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,714 hrs · 21,560 cycles

LT WINDOW FRAME HAS CORROSION.

Part: DOOR — CRACKED (CARGO BAY) · airframe 39,714 hrs · 21,560 cycles

MAIN DECK CARGO DOOR FWD UPPER CORNER IS CRACKED.

Part: VALVE — FAILED (FUEL CROSSFEED) · airframe 39,576 hrs · 21,505 cycles

FUEL VALVE ON NUMBER 1 TANK FAILED CLOSED OR WOULD NOT OPEN ALL THE WAY. UNABLE TO BALANCE FUEL FOR THE SCHEDULED 4 HOUR FLIGHT PILOT OPTED TO RETURN TO KYIP. NOTIFIED OPS VIA SAT PHONE & RETURNED UNEVENTFULLY. R&R #1 FUEL CROSS FEED MANIFOLD VALVE IAW B727 AMM 28-22-01. LEAK AND OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,937 hrs · 37,982 cycles

FRAME CRACK @ SUPPORT BRACKET STA 380 BETWEEN STR 8 - 9R.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 39,302 hrs · 21,346 cycles

FO'S ALTIMETER INOP SHORTLY AFTER TAKEOFF, THE POINTER DROPPED TO THE 6 O'CLOCK POSITION, THE SCREEN WENT BLANK AND THE BACKLIGHT STOPPED WORKING. CONSIDERING THE LOW WEATHER/FORECAST AT DESTINATION PILOT ELECTED TO RETURN TO KLRD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 38,585 hrs · 20,947 cycles

DURING PRE-FLIGHT, FOUND COCKPIT PORTABLE EMERGENCY LIGHT INOPERATIVE. R & R THE PORTABLE EMERGENCY LIGHT IAW AMM 33-50-92, OPS CHECKED GOOD.

Part: WINDOW FRAME — CORRODED (BS 730C) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 730C RT, HAD EXTERNAL CORROSION.

Part: BULKHEAD WEB — CORRODED (BS 1183) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

CORROSION ON AFT SIDE OF PRESSURE BULKHEAD BS 1183 ABOVE STRINGER 14L.

Part: WINDOW FRAME — CORRODED (BS 960F) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 960F RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 530) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 530 RT HAD EXTERNAL CORROSION.

Part: SKIN — CORRODED (WINDOW FRAME) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 470 RT EXTERNAL, CORRODED.

Part: WINDOW FRAME — CORRODED (BS 570) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 570 RT HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 450) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 450 LT, HAD EXTERNAL CORROSION.

Part: BUSHING — CORRODED (LT TRUNNION) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

LEFT AFT TRUNNION BUSHING CORRODED.

Part: WINDOW FRAME — CORRODED (BS 730A) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 730A RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 730F) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 730F, HAD EXTERNAL CORROSION.

Part: SUPPORT — CORRODED (ELEVATOR) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

ELEVATOR CONTROL QUADRANT UPPER SUPPORT ASSY RIGHT SIDE FITTING

Part: MOUNT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

RIGHT WING INBD FLAP OTBD FLAP TRACK AFT MOUNT CORRODED.

Part: WINDOW FRAME — CORRODED (BS 900) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 900 RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 710) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 710 RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 980) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME BS 980 RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 590) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 590 RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 510) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME BS 510, RT EXTERNAL.

Part: WINDOW FRAME — CORRODED (BS 610) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 610 RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 550) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 550 RT HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 670) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME AT BS 670 RT, HAD EXTERNAL CORROSION.

Part: WINDOW FRAME — CORRODED (BS 730F) · corrosion level 2 · airframe 38,312 hrs · 20,784 cycles

WINDOW FRAME BS 730F LT CORRODED.

Part: SUPPORT RIB — CRACKED (LE SLAT) · airframe 37,897 hrs · 20,509 cycles

NR 3 SLAT NR 10 SUPPORT RIB CRACKED.

Part: WEB — CRACKED (LE SLAT) · airframe 37,897 hrs · 20,509 cycles

NR 3 SLAT INBD ACTUATOR SUPPORT WEB CRACKED.

Part: STIFFENER — CORRODED (RT WING) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

RIGHT WING WEB STIFFENER IS CORRODED AT STA 140.

Part: STRUCTURE — CORRODED (NLG WW) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

IN NOSE WHEEL WELL, T-CHORD IS CORRODED AT STA 351, LBL 17 TO RBL 17.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

RT WALKWAY BEAM HAS CORROSION, STA 351 AFT END.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

RIGHT INBD WEB COMMON TO NOSE WW FWD OF ELECTRONICS EQUIPMENT BAY HAS CORROSION STA 350, RBL 20.

Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

CORROSION ON LT HORIZONTAL STABILIZER T/E UPPER EXTERNAL SURFACE, STA 62.

Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

CORROSION ON LEFT HORIZONTAL STABILIZER T/E UPPER EXTERNAL SURFACE STA 32.08.

Part: SHEAR TIE — CORRODED (BS 600) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

FRAME SHEAR TIE AT BS 600 AT RBL 2 CORRODED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

LEFT WALKWAY WEB ATTACH ANGLE AT NOSE W/W HAS CORROSION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

AFT PIT DOOR SILL WEB HAS CORROSION STA 986, STR 27R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

STRINGER CORRODED STR 29L, STA 950B AND STA 950E.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

FRAME SHEAR TIE HAS EVIDENCE OF CORROSION, STA 720F BETWEEN STR 29R & STR 28R.

Part: FRAME — CORRODED (BS 500) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

FRAME LOWER CHORD AT BS 500, BL 0 HAS CORROSION.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

LEFT WALKWAY WEB ATTACH ANGLE CORRODED STA 302, LBL 32.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

STRINGER CORRODED AT STA 990, STR 29R.

Part: STRINGER — CORRODED (BS 723) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

STRINGER 27L HAS CORROSION AT BS 723.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

FORWARD PIT DOOR HAS PULLING FASTENERS.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

RT WING FWD SPAR LOWER CHORD SPLICE PLATE HAS CORROSION AT WING STA 466.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

SKIN CORRODED BELOW SKUFF PLATE OF AFT CARGO DOOR STA 970 & STA 974, STR 27R.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 37,224 hrs · 20,151 cycles

CAPTAIN`S WINDSHIELD STARTED ARCING FOLLOWED BY WINDSHIELD SHATTERING. R & R WINDSHIELD AND TEMP CONTROLLER.

Part: ANGLE — CRACKED (PYLON) · airframe 37,176 hrs · 20,117 cycles

NR 1 PYLON INBD CHORD ANGLE HAS CRACK INDICATION IN FWD FASTENER HOLE COMMON TO FWD ENGINE MOUNT, HOLE "A" LISTED IN SB 727-54A0010, R6, FIG 1.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORROSION STA 930-950 LEFT.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORROSION STA 620-640 RIGHT.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORROSION STA 1090-1110 RIGHT.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORROSION STA 950D-950E LEFT.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORRODED STA 950D-950E RIGHT.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORROSION STA 970-990 LEFT.

Part: PLUG — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

WINDOW PLUG CORROSION STA 720A-720B LEFT.

Part: FRAME — CHAFED (FUSELAGE) · airframe 36,020 hrs · 19,470 cycles

FRAME DAMAGE WHERE FLOOR SUPPORT SITS STA 640 RBL 1 TO RBL 2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

STRINGER CORROSION FWD CARGO PIT.

Part: FRAME — BENT (FUSELAGE)

FRAME IS BENT.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2

CIRCUMFERENTIAL FRAME CORRODED AT SKIN FASTENER.

Part: SPAR — DAMAGED (ELEVATOR) · airframe 36,020 hrs · 47,291 cycles

ELEVATOR FORWARD SPAR DAMAGED STA 187 LEFT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

CORROSION ON TOP CHORD STA 328 RBL 14.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

CORROSION ON ANGLE BELOW LEFT COCKPIT WINDOW, (NR 49296).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

COCKPIT LEFT FRAME WEB HAD CORROSION (NR49298).

Part: WINDOW FRAME — CORRODED (CABIN) · corrosion level 2 · airframe 36,060 hrs · 19,470 cycles

CORROSION 1X1 INCHES, AROUND WINDOW PLUG RIGHT BS 640-660 (NR 49244).

Part: WINDOW FRAME — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

CORROSION AROUND WINDOW PLUG RIGHT, 1X1 (NR 49237).

Part: WINDOW FRAME — CORRODED (CABIN) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

CORROSION AROUND WINDOW PLUG, 1X1 INCHES (NR 49258).

Part: WEB — GOUGED (FUSELAGE) · airframe 36,020 hrs · 19,470 cycles

AFT PIT BILGE WEB AND ANGLE DAMAGED AT BS 970 TO 990 STRINGER 30 RIGHT (NR 49132).

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

SHEAR TIE CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

MAIN DECK SEAT TRACK HAS SPOTS OF CORROSION (NR49081).

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

MAIN DECK STA 312 TO STA 320, LBL 30 FLOOR SUPPORT HAS CORROSION (NR 49123).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

MAIN DECK SEAT TRACK HAS CORROSION 1X1 INCHES (NR49096).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

CORROSION ON TOP CHORD STA 344 RBL 3 TO LBL 12.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

AFT ENTRY DOOR FRAME LEFT SIDE WL 273.25 NUMBER 7 DOORSTOP RE-INFORCEMENT ANGLE CORROSION AT CUTOUT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

SEAT TRACK HAS CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

MAIN DECK SEAT TRACK CORROSION (NR49089).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

MAIN DECK DECK HAS CORROSION 1X1 INCHES (NR49082).

Part: SKIN — CRACKED (L1 DOOR) · airframe 36,020 hrs · 19,470 cycles

L1 DOOR BOTTOM SKIN CRACKED.

Part: REPAIR — SEPARATED (LT WING) · airframe 36,020 hrs · 19,470 cycles

PREVIOUS REPAIR ON LEFT WING L/E LOWER SPAR CAP SEPARATING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 47,291 cycles

FLOORBEAM CORROSION ON TOP CAP STA 1130 LBL 29.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

SEAT TRACK CORRODED 1X1 INCHES. (NR 49055)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,020 hrs · 47,291 cycles

MISSDRILLED HOLE IN FRAME CAP STA 480 STR 26R.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,020 hrs · 19,470 cycles

MAIN DECK FRAME HAS ELONGATED HOLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,020 hrs · 47,291 cycles

CORROSION ON TOP CHORD STA 1110 LBL 24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

SEAT TRACK FASTENER HAS CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

SEAT TRACK CORROSION 1X1 INCHES (NR49043).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

SEAT TRACK CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

SEAT TRACK CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,020 hrs · 19,470 cycles

CORROSION ON SEAT TRACK AROUND NUT PLATE, 1X1 INCH (NR 49051).

Part: AIR DISTR — ODOR (COCKPIT)

PRIOR TO DESCENT, FUMES PRESENT ON FLT DECK. CAPT AND F/E EXPERIENCED IRRITATIONS. A/C HAD HAZMAT ABOARD NOT PREVIOUSLY IDENTIFIED BY SHIPPER. A/C WAS DOWN LOADED AND SECURED FOR SHUTDOWN. CHECKED AREA WITH GAS ANALYZER PROBE, NO SIGN OF CONTAMINATION. ALL CARGO THAT WAS ON BOARD WAS CHECKED BY BDL FIRE DEPARTMENT, NO CONTAMINATION. COULD NOT DUPLICATE. DEFERRED PER MEL 30-7 CAT D DMI NR 88110798. INSPECTED REPELLANT SYSTEM FOR LEAKAGE, NO LEAKS FOUND. PLACARDS INSTALLED, OPS CHECKED GOOD. THIS CLEARS DMI NR 88110798, PLACARDS REMOVED.

Part: SILL — DAMAGED (CARGO DOOR)

AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION AT FL310. CABIN ALTITUDE CONTINUED TO CLIMB 150 TO 300 FPM AT CRUISE. CARGO HEAT OUTFLOW VALVE CLOSED AND CABIN RATE INCREASED TO 1500 FPM UNCONTROLLABLY. AIRCRAFT DESCENDED FROM FL310 TO FL240, CABIN PRESSURE BEGAN TO RESPOND BELOW FL290, FLIGHT CONTINUED AT FL240, PRESSURIZATION CONTROL MANUAL. TRANSFERRED TO DMI LIST NR 88109098 IAW MEL 21-16-1A, PLACARDS INSTALLED. AUTO CONTROL IS WORKING FINE AFTER MAIN CARGO DOOR SILL REPAIR. CLEARED DMI NR 88109098 AUTO PRESSURIZATION PER FLT CREW INFORMATION ON PRESSURIZATION SATISFACTORY.

Part: GUSSET — CRACKED (BS 825.95)

DURING ACCOMPLISHMENT OF AD 94-02-04 SB 727-53-0197 PARA (C) OF AD PART IV OF SB, FOUND LT LOWER FRAME GUSSET (BELOW CABIN FLOOR) AT BS825.95 HAS A CRACK ON LOWER INBD FASTENER HOLE TO THE BOTTOM EDGE OF GUSSET (.5 CRACK). REMOVED AND REPLACED GUSSET IAW SB 727-53-0197. NON-ROUTINE TASK CARD NUMBER 003232.

Part: BULKHEAD — CRACKED (FWD PRESS BLKHD)

DURING ROUTINE CPCP INSPECTION, FOUND FWD BULKHEAD CRACKED AROUND RIVETHEAD. INSTALLED REPAIR IAW B727 SRM 53-10-9 FIG 4. CORROSION TASK CARD NUMBER C53-100-01 PART 4 OF 6. NON-ROUTINE TASK CARD NUMBER 003115.

Part: SKIN — DAMAGED (BS 294.5)

DURING ROUTINE CPCP INSPECTION, FOUND BS 294.5 S-14LT, SKIN DAMAGED. REMOVED DAMAGED AREA AND REPAIRED IAW B727 SRM 53-30-3 FIG 15A. CORROSION TASK CARD NUMBER C53-100-01 PART 5 OF 6. NON-ROUTINE TASK CARD NUMBER 003047.

Part: SPAR — CRACKED (HORIZ STAB)

DURING ROUTINE CPCP INSPECTION, FOUND RT HORIZONTAL STAB STA 32.108 OUTSIDE OF REAR SPAR LONG. FRAME FORWARD TOP PART HAS 2.5 INCH CRACK COVERING 3 FASTENERS MOST FORWARD EDGE. NDT VERIFIED CRACK. INSTALLED REPAIR IAW AIA/E/2643, EDR B2-05517. CORROSION TASK CARD NUMBER C55-391-10 PART 2 OF 2. NON-ROUTINE TASK CARD NUMBER 003109.

Part: ANGLE — CORRODED (BS 720)

DURING ROUTINE CPCP INSPECTION, FOUND FS 720 FRAME ATTACH ANGLE CORRODED BETWEEN S27 AND S28R. REMOVED ATTACH ANGLE FOUND TO BE OUT OF LIMITS B727 SRM 53-10-1. INSTALLED ANGLE IAW SRM 51-10-1. CORROSION TASK CARD NUMBER C53-113-01 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 003100.

Part: FRAME — CORRODED (BS 1070)

DURING ROUTINE CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, BS 1070 LOWER FRAME CORRODED AT STOP. INSTALLED REPAIR IAW B727 SRM 51-40-3. CORROSION TASK CARD NUMBER C53-111-02 PART 2 OF 2. NON-ROUTINE TASK CARD NUMBER 003123.

Part: SKIN — CORRODED (BS 990)

DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION ON LT SIDE OF FUSELAGE AT FS990 FROM S24L TO S21L AROUND SCREW HOLES AND UNDER PANEL MEETING AREA. REMOVED CORROSION IAW B727 SRM 51-10-6. TWO INCH BY TWO INCH AREA AT FS 990 BETWEEN STR 23 AND 24 FOUND TO BE OUT OF LIMITS IAW 53-30-1. REPAIRED DAMAGE IAW SRM 53-30-3 FIG 3. CORROSION TASK CARD NUMBER C53-100-02 PART 4 OF 6. NON-ROUTINE TASK CARD NUMBER 003099.

Part: BULKHEAD — CRACKED (FWD PRESS BLKHD)

DURING ROUTINE CPCP INSPECTION, FOUND 2 CRACKS FROM RIVET HOLES ON FWD FUSELAGE BULKHEAD 6 TO 8 DOWN AND 12 TO 18 FROM RIGHT SIDE. INSTALLED REPAIR DOUBLER IAW SB 727-53146. CORROSION TASK CARD NUMBER C53-100-01 PART 4 OF 6. NON-ROUTINE TASK CARD NUMBER 003034.

Part: SEAL — TORN (CARGO DOOR)

CABIN SET AT FL 370 AND 6000 FEET, CARGO HEAT OUTFLOW VALVE CLOSED, CABIN CONTINUES TO CLIMB 100 FEET PER MINUTE EVEN WITH RATE KNOB FULL INCREASE AND MANUAL CONTROLLER FULL INCREASE. AIRCRAFT HAD TO BE DESCENDED BELOW FL 280 TO REGAIN CONTROL OF CABIN. REPAIRED SEAL AROUND MAIN CARGO DOOR. OPS CHECK OK ON GROUND PER B727 MM 52-31-0.

Part: CONNECTOR — DIRTY (NLG)

HUF/IAH - FLT 72669 - ON EXTENSION, NOSE GEAR DID NOT GO GREEN UNTIL THIRD ATTEMPT. INSPECTED NOSE GEAR, FOUND NO DEFECTS. LUBED ALL GREASE FITTINGS IN NOSE. CLEANED AND RE-SECURED CANNON PLUGS ON BOTH SWITCHES. JACKED NOSE GEAR IAW 727 MM 7-11-0. PERFORMED NOSE GEAR RETRACTION TEST IAW 32-33-0. CYCLED 15 TIMES. POSITON AND WARNING SYSTEMS. OPS CHECK GOOD IAW 32-61-0. (X)