N912UP

Part: SLIDE — UNSECURE (ENTRY DOOR)

INSPECTION TYPE:N/A ESCAPE SLIDE CAME OFF WHEN CREW CLOSED DOOR. SLIDE RE-INSTALLED NOTE: SLIDE DID NOT DEPLOY.

Part: SLIDE — UNSECURE (DOOR)

INSPECTION TYPE:IN DOOR PARTIALLY OPENED FROM EXTERIOR WITH SLIDE ARMED SLIDE FELL FROM DOOR BUT DID NOT DEPLOY. RESECURED SLIDE ASSY.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C NDI INSP OF MID GALLEY DOOR CUTOUT INDICATES REINFORCING STRAP CRACK AT UPPER FWD CUTOUT. REPAIRED IAW UPS EO B727-5330-2685.

Part: BRACKET — CRACKED (#3 T/R FAIRING) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C #3 THRUST REVERSER O/B LATCH FAIRING MID ANF AFT BRACKETS ARE CRACKE D. BRACKETS REPLACED IAW MM 78-30-01

Part: TRUNNION — CORRODED (NLG) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C ON REMOVAL OF TRUNNION CAPS ON NLG TRUNNION AREA WHERE BUSHINGS WERE INSTALLED HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 53-40-1, 20-20-02, & SMRO EO 2001-044-001.

Part: DRUM — CORRODED (NLG) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C NLG MANUAL EXTENSION AFT DRUM CORRODED. DRUM ASSY REPLACED IAW OHM 32-34-03.

Part: TRUNNION — CORRODED (NLG) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C ON REMOVAL OF NLG TRUNNION CAPS CORROSION WAS FOUND IN ALL FOUR BOLT HOLES FOR CLAMPING OF TRUNNION CAPS. REPAIRED IAW SMRO EO 2001-044-001 UPS 727-53-200032.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C NDT INSPECTION FOUND CRACK INDICATION AT BS 880 LBL18-19. STOP DRILLED AND HFEC, CRACK CONTAINED. REPAIRED IAW EO B727-5310-04 60.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C SUSPECT CRACKS ON LT AND RT 940 SUPPORT FRAME FITTING AT FLOOR BEAM ATTACH FLANGES. HFEC CARRIED OUT LT NDF RT CRACK CONFIRMED ON FWD I/B UPPER FLANGE. REPAIRED IAW UPS EO B727-5310-2954 A.

Part: SPAR — CORRODED (CENTER WING) · airframe 55,552 hrs · 49,278 cycles

INSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRED IAW SRM 51-30-02 RBL 19 TO 31.

Part: BULKHEAD — CRACKED (RH MLG BULKHEAD) · airframe 0 hrs · 0 cycles

INSPECTION TYPE:N/A RT MLG WHEEL WELL FWD BULKHEAD BELOW APU EXHAUST HAS CRACKS AROUND U PPER INBOARD CANNON PLUG RECEPTICLE STA 870 ****MRR FILED AS OPEN*** AIRCRAFT FERRIED TO GSO REPAIR IN PROGRESS FERRY FLIGHT TO GSO

Part: SKIN — CRACKED (RH WHEEL WELL)

INSPECTION TYPE:N/A CRACKS AT RH WHEEL WELL AREA STA 870 ***MRR FILED AS OPEN***

Part: LIGHT — FAILED (COCKPIT)

INSPECTION TYPE:IN COCKPIT EMERGENCY EXIT LIGHT INOP W/OP CHECKED IN FLIGHT. RELAMPED, OPS CHECKS GOOD.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:PFLT 2 INCH CRACK ALONG RT NLG W/W SIDE WALL FWD OF GEAR TRUNNION AT APPROX STA 228 (MARKED). VERIFIED END OF CRACK WITH HFEC. STOP DRILLED RACK IAW 51-40-02 FIG 1. REPAIRED CRACK AS PER SRM 51-40-02 FIG 1. REF LOG PAGE 589676.

Part: LINE — BURST (HYDRAULIC SYS) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, PRESSURE LINE IN B SYS HYD SERVICE BAY BURST ON OPERATION. FAILED UNDER P-CLIP AREA. PRESSURE LINE IN B-SYS HYD SERVICE BAY REPLACED IAW MM 20-80-01. LEAK CHECKED OK.

Part: WEB — CRACKED (ELEVATOR) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, WEB BENEATH STAB ACTUATED ELEV TRIM SENSOR CRACKED AT SYS A & SYS B ELEVATOR HYD LINE SUPPORT POINT (PRESS LINES). WEB REPAIRED IAW SRM 51-40-3.

Part: FRAME — CORRODED (VERT STAB) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, CORROSION ON VERT STAB ON T-CHORD AFT OF FEEL COMPUTER. REPLACED T-CHORD IAW SRM 51-30-2. REF IPC 55-30-00, FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, CRACK ON EDGE OF FRAME AT BS 1000 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.

Part: STIFFENER — CORRODED (FAIRING) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, WING TO BODY FAIRING NR 3334 HAS CORRODED STIFFENER AROUND GROUND FAN DOOR CUTOUT (RT). ALSO, CORROSION ON DOOR CUTOUT CORRODED STIFFENER REPAIRED IAW SRM 51-40-3, FIGURE 1. CORROSION FOUND ON CORNER OF DOOR CUTOUT. CORROSION REMOVED, SKIN REPAIRED IAW SRM 51-40-2.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, CRACK ON FLOOR LONGITUDINAL Z SECTION AT BS 1000 AT STR 30 IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-5 FIG 4.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, SUSPECT CRACK FOUND ON TIE DOWN TRACK AT STA 1080, STR 28 RT ADJACENT TO FRAME CUTOUT. REPAIR CARRIED OUT IAW SRM 53-10-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, CRACK ON FRAME AT BS 1070 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.

Part: WEB — CRACKED (FIREWALL) · airframe 54,930 hrs · 48,671 cycles

INSPECTION TYPE:C, LEFT AND RIGHT WEBS AT BS 1387 OVER THE ENGINE 2 HORIZONTAL FIREWALL ARE CRACKED. LT WEB AND BODY SKIN ATTACH TEE REPLACED IAW DRAWING 65-17555.

Part: SUPPORT — CORRODED (LT TE FLAP)

INSPECTION TYPE AD V LEFT SUPPORT ASSY I/B FLAP TRACK FWD CORRODED. LEFT I/B FLAP TRACK FWD SUPPORT ASSY REPLACED IAW MM 27-51-31.

Part: LIGHT — INOP (COCKPIT)

INSPECTION TYPE-N/A, REPEAT WRITE UP WITH EMERGENCY EXIT SWITCH IN THE ARMED POSITION, THE EMERGENCY EXIT LIGHT IN THE COCKPIT IS ON. EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR IS OFF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AS PER MM 33-50-01. OPS CK'D GOOD. (P/N F 10-0067-9) (S/N UP 18500) ON, (20246) OFF.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE:C SURFACE CORROSION ON LOWER RUDDER SKIN PANEL LEFT SIDE BETWEEN FRONT SPAR AND REAR SPAR BY PCU ATTACH POINT. RUDDER REPLACED IAW MM 27-20-1.

Part: FRAME — CRACKED (BS 825.95)

INSPECTION TYPE-C DURING NDT INSPECTION, CRACK FOUND EMANATING FROM FOURTH FASTENER HOLE ABOVE FLOOR LINE AT BS 825.95 RT. REPAIRED IAW APPENDIX C OF EO B727-5310-5474.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AND TYPICAL WEB REPAIRS IAW SRM 51-40-3.

Part: BULKHEAD BEAM — CRACKED (BS 1183)

INSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BEAM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED IAW APPENDIX D OF B727-5311-0631.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE:C CORROSION ON LOWER RUDDER SKIN PANEL RT SIDE FRONT SPAR AREA BY PCU ATTACH POIN. RUDDER REMOVED IAW MM 27-20-11.

Part: BULKHEAD — DAMAGED (BS 178)

INSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-5310-4290 USING REPAIR KIT 65C36289-1.

Part: INTERCOSTAL — DAMAGED (BS 760)

INSPECTION TYPE-C, INTERCOSTAL DAMAGED BS 760 LBL 45 LBL 62. REPAIR CARRIED OUT IAW SRM 51-20-1.

Part: SUPPORT — CORRODED (BS 780)

INSPECTION TYPE-C, CORROSION ON ANGLE SUPPORT FOR FRONT NET TIE DOWN BS 780 LBL 60.00. ANGLE SUPPORT REPLACED IAW SRM 51-30-2.

Part: OVERHEAT LOOP — LOOSE (ENGINE)

ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLT. ENGINE WAS SHUTDOWN FOR REMAINDER OF FLIGHT. FOUND BACKSHELL LOOSE ON OVERHEAT LOOP AT STATION NR 48. RAN ENGINE AND OPS CKS OK.

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY LIGHT ABOVE COCKPIT DOOR ILLUMINATES WITH EMERGENCY LIGHT SWITCH IN THE ARM POSITION. RESEATED EMERGENCY EXIT LIGHT. OPS CK OK.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR ILLUMINATED AT START OF DESCENT. RESEATED AND TESTED EMERGENCY EXIT LIGHT PER M/M 33-50-101, OPS CK NORMAL.

Part: BULKHEAD FTG — CRACKED (BS 870)

INSPECTION TYPE-D, CRACK FOUND IN RT BS 870 FTG. REPAIRED IAW B727-5310-3057 APP 8.3.

Part: FLAP CARRIAGE — CORRODED (LT TE FLAP)

INSPECTION TYPE-D, LT O/B FLAP I/B CARRIAGE HAS PITTING CORROSION. REPLACED IAW 57-58-01.

Part: BUNGEE ASSY — FAILED (AFT AIRSTAIR)

WHEN PARKED AT FWA, AFT AIRSTAIR WAS ALL THE WAY DOWN. REMOVED AND REPLACED AFT AIRSTAIR TORQUE TUBE BUNGEE ASSY PER MM 52-60-01, OPS CHK GOOD PER MM 52-62-01. P/N ON/OFF 69-21112-1 S/N ON TAG 215194A S/N OFF UNKNOWN.

Part: STRINGER — CORRODED (FS 740)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, F.S. 740 STRINGER SKIN HAS CORROSION. REPAIRED I.A.W. DHC SK 912-788.

Part: OVERHEAT MODULE — MALFUNCTION (NR 1 ENGINE)

CREW REPORTED NR 1 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. APPROPRIATE CHECKLIST WAS PERFORMED AND ENGINE WAS SHUTDOWN. ACT NOTIFIED, EMERGENCY DECLARED AND FLIGHT PROCEEDED WITHOUT FURTHER EVENT TO DFW. REMOVED AND REPLACED OVERHEAT DETECTION MODULE PER MM 26-14-00, OPS TEST GOOD. REPAIRED CHAFED WIRE AT FWD PYLON LOOP FWD CONNECTOR IN STAIRWELL AREA, OPS CK NORMAL.

Part: SKIN — DELAMINATED (LT TE MIDFLAP)

WHILE ON GROUND, MAINTENANCE FOUND LEFT INBOARD MIDFLAP TRAILING EDGE DELAMINATED IN SEVERAL PLACES. REPAIRED DELAMINATION IAW B-727 SRM 51-40-6 PAGE 20.

Part: EEL — INOP (FLIGHT DECK)

(SUPPLEMENTAL MRR) FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMER. EXIT LIGHT ASSY AS PER MM 33-50-01. OPS CHECKED GOOD.

Part: EEL BATTERIES — DISCHARGED (FLIGHT DECK)

DURING PREDEPARTURE CHECK, EMERGENCY EXIT SIGN DIM AT FORWARD ENTRY DOOR. REPALCED BATTERIES, CHECKS OK. MFG P/N 5106.