N378AX

Part: CABLE — FRAYED (FLT CONTROLS) · airframe 94,644 hrs · 15,000 cycles

ON APPROACH FLIGHT CONTROLS FELT AS THOUGH THEY WERE BINDING. FLIGHT CONTROLS ASYMETRY IS INDICATED ON INDICATOR.

Part: UNKNOWN — BURNED (ZONE 800) · airframe 92,768 hrs · 14,638 cycles

ODOR OF SMOKE DETECTED AFTER TAKE OFF SHORTLY THEREAFTER THE FLIGHT DECK LOCK CIRCUIT BREAKER WAS DISCOVERED TO HAVE POPPED. CORRECTIVE ACTION: REMOVED AND REPLACED FLIGHT DECK DOOR ELECTRIC STRIKE PER B767 AMM 52-51

Part: NONE — NONE · airframe 91,374 hrs · 14,300 cycles

CRACK FOUND ON LH WING ON ANGLE AT WING STA 802 UNDER SLAT. CORRECTIVE ACTION: CRACK LOWER CHORD OF AIRLOAD RIB AT L/H WING STA 820 REMOVED AND REPLACED WITH MADE REPAIR PART IAW BOEING DOC# 114T2219 PL REV E INSTALLED IAW BOEING DOC# 114T2219 ID 001 REV A

Part: NONE — NONE · airframe 91,374 hrs · 14,300 cycles

CRACKED STIFFNER ON LH WING STA 982 FORWARD SPAR. CORRECTIVE ACTION: CRACKED STIFFINER ON L/H WING STA 982 FROMT SPAR REMOVED AND REPLACED WTIH PART IAW BOEING DOC. #112T2253 PL REV. NON AND INSTALLED IAW BOEING DOC.# 112T200:ID21 REV D. CRACKED LOWER CHORD OF AIRLOAD RIB LOC. AR STA 982 REMOVED AND REPLACED WITH MADE REPAIR PART IAW BOEING DOC.#114T2225 PL REV F. AND INSTALLED IAW BOEING DOC.# 114T2225 DWG 001 REV A.

Part: NONE — NONE · airframe 91,374 hrs · 14,300 cycles

CRACK FOUND BOTH L/H & R/H SIDES OF THE VERTICAL CHORD. CORRECTIVE ACTION: NLG WHEEL WELL VERT CHORD REPAIRED AT BS 287 AND LBL 25 PER SB 767-53A0110 PT 3 REV 00 & 767-300 SRM 51-70-12-0G-0 FIG 1 REV 119 REF Q1 AVIATION WO 139170-5 FOR HFEC INSP WITH NFF NOTE: REPAIRED CHORD IS A PERMANENT REPAIR AND NO FURTHER INSPECTION PER SB 53A0110 ARE REQUIRED AS THIS IS A TERMINATING ACTION

Part: NONE — NONE · airframe 91,374 hrs · 14,300 cycles

HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN WAS FOUND TO HAVE CORROSION DAMAGE AT 2EA AREAS ALONG S-4 TO THE LH SIDE OF THE BL 0. CORRECTIVE ACTION: HORIZONTAL STAB CENTER SECTION UPPER SKIN REPAIRED FROM LBL 3.4-7.9 AT S-4 PER STS EA 72-2022-114 REV 1R REF Q1 AVIATION WO 139170 FOR HFEC, BHEC, AND UT RESULTS NFF FOR HFEC SCANS NOTE: THIS IS A CAT B REPAIR WITH STAGE ONE APPROVAL SUBMITTAL OF DT DATA MUST BE SUBMITTED NO LATER THEN 13 JUL 2023 (12 MONTHS) FROM THE DATE OF 8110-3 SEE ALSO: OMNI EO B7655-09 REV INITIAL ISSUE (ATTACHED)

Part: STABILIZER — CORRODED (ZONE 300) · airframe 91,374 hrs · 14,300 cycles

HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN WAS FOUND TO HAVE CORROSION DAMAGE AT 2EA AREAS ALONG S-4 TO THE LH SIDE OF THE BL 0. CORRECTIVE ACTION: COMPLIED WITH EO B7655-09 INCORPORATING STS EA 72-2022-114 DATED 7/13/22.

Part: NONE — NONE · airframe 90,690 hrs · 14,142 cycles

LE SLAT LIGHT (EICAS) MESSAGE ILLUMINATED. CORRECTIVE ACTION: BIT FSEU, M548 OUTBOARD SLAT PDU RVDT MISRIG MESSAGE FOUND. PERFORMED PSEU SENSOR (SLATS) CHECKS, NO FAULTS FOUND. ACCESSED OUTBD SLAT PDU RVDT CONNECTORS, CLEANED THEM, SECURED THEM. RUN SLATS UP AND DOWN, CHECKED FSEU FOR FAULTS, NO FAULTS. RUN FLAPS/SLATS SEVERAL TIMES, NO DEFECTS NOTED. VERIFY FSEU FOR FAULTS, NONE FOUND. OK FOR SERVICE (REF FIM 27-51 FAULT TREE 810).

Part: PSEU — FAILED · airframe 90,257 hrs · 14,048 cycles

MASTER CAUTION ACCESS DOORS CARGO DOORS ENTRY DOORS L/R CABIN ALTITUDE WAS RISING FROM 8,500 FT TOWARDS 9,200 FT AT A RATE OF 500 FT / ??? WE EXECUTED AN IMMEDIATE DESCENT TO 14,000 FT AT WHICH POINT ALL EICAS MESSAGES CLEARED MAX CABIN DIFFERENCIAL REACHED 8.7 CABIN ALTITUDE MASTER WARNING LIGHT AND EICAS MESSAGE DID NOT ILLUMINATE CABIN OXYGEN MASKS DID NOT DEPLOY CABIN ALTITUDE STABILIZED BRIEFLY AT 14,000 THEN BEGAN TO CLIMB AGAIN TOWARDS 9,500 FT THUS WE INDICATED FURTHER DESCENT TO 9,000 FT WE COMPLETED THE CARGO DOORS QRH (PAGE 1.4) AS THE FWD CARGO DOOR WAS THE HIGHEST PRIORITY COMPANY DIRECTED DIVERSION TO LBBG REST OF FLIGHT WAS COMPLETED UNEVENFULLY. CORRECTIVE ACTION: PERFORMED MANUAL MODE CONTROL TEST - CABIN PRESSURE CONTROL AMM 21-31 REPLICATED IN FLIGHT EXT DOOR MESSAGES ON GROUND WITH TEST REMOVED AND REPLACED PSEU PER AMM 32-09 PSEU TEST OPS CHECK GOOD NO FAULTS PERFORMED MMLT - CABIN PRESSURE CONTROL SYSTEM AMM 21-31 NO FAULTS OPS CHECK GOOD

Part: MODULATING VALVE — DEFECTIVE (RT ENGINE) · airframe 89,334 hrs · 13,861 cycles

RT ENGINE BLEED OVERHEAT RT ENGINE BLEED OFF R1 PACK AFT EICAS OCCURED AT HIGH & LOW TRUST SETTING ~ R&R FAMV PER B767-300 FIM 36-10 FT 835 SHT 3 BLK 4+47 & AMM 36-11 P.CASAS 13013 R&R "R" ENG BLEED AIR CONT CARD PER FIM 36-10 FT 835 SHT 3 BLK 44 & AMM 36-11 P.CASAS 13013 R&R THE PRSOV PER AMM 36-11 & FIM 36-10 FT 835 SHT 3 BLK 3 D.F. 14232 PERFORMED ENGINE RUN IAW AMM 71-00 OPS CHECKED PRSOV & FAMV BOTH FOUND GOOD

Part: THERMAL SWITCH — DEFECTIVE (RT ENGINE) · airframe 89,275 hrs · 13,850 cycles

R ENG BLEED OVERHEAT (EICAS MSG) EARLY ON CLIMB OUT ~ REMOVED AND ATTACHED WIRES IAW WDM 36-11 AND UNLOCKED FAMV FOR OPS CHECK IAW AMM 36-10. OPS CHECK OKAY.

Part: WARNING LIGHT — FALSE INDICATION (MLG) · airframe 84,938 hrs · 12,890 cycles

AFTER T.O. WITH NORMAL GEAR RETRACTION STARTED AFTER T.O. CHK LIST. WHILE MOVING LANDING GEAR LEVER TO THE OFF POSITION, HEARD UNUSUAL NOISE WITH AMBER GEAR AND DOOR LIGHTS WITH GREEN NOSE GEAR DOWN AND LOCKED INDICATION. FOLLOWING QRH PROCEDURES MOVED GEAR LEVER TO THE UP POSITION. IN THE UP POSITION ALL LIGHTS PREVIOUSLY METIONED EXTINGUISHED. AFTER DUMPING FUEL AND MAX LANDING WEIGHT EXTENDED GEAR HANDLE TO THE DN POSITION. NORMAL EXTENSION WITH 3 GEAR DOWN AND LOCKED, NO AMBER INDICATIONS. PROCEEDED TO LAND WITH A NORMAL LANDING. JACKED AIRCRAFT PER B767 AMM 07-11-01. PERFORMED MULTIPLE LANDING GEAR EXTENSIONS AND RETRACTIONS IAW B767 AMM 32-32-00. NO DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE MALFUNCTION.

Part: ENGINE — VIBRATION (RIGHT) · airframe 81,127 hrs · 12,070 cycles

AT 25000 FT STILL CLIMBING RIGHT ENGINE GAVE OUT A LOUD BANG FOLLOWED BY HIGH VIBRATION , LOW N1 AND HIGH N2. EGT APPEARED TO BE NORMAL. CORRECTIVE ACTION:RIGHT ENGINE REMOVED & REPLACED IAW OAI WC 71-R07-R

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,057 hrs · 11,849 cycles

AFTER PUSHBACK AND BOTH ENGINES STARTED, RECIEVED NOTIFICATION FROM FROM FA LOCATED IN AFT CABIN THAT THERE WAS THE ODOR OF SMOKE. DURING THIS TIME A HIGH PITCH NOISE WAS HEARD THROUGHOUT CABIN. ENGINE SHUTDOWN AND NOISE ENDED. RAN BOTH ENGINES AND OPERATED HYDRALIC SYSTEM AND OPERATED AC PACK SYSTEM INSPECTED ALL SYSTEMS FOR SIGNS OF SMOKE OR ODOR. NO DEFECTES NOTED AT THIS TIME.

Part: FUEL FILTER — CLOGGED (RT ENGINE) · airframe 76,488 hrs · 11,121 cycles

DURING FLIGHT, STATUS MESSAGE, RT ENGINE FUEL FILTER. DURING POWER REDUCTION AT TOP OF DECENT, EICAS MESSAGE WENT AWAY. R & R RT ENGINE FUEL FILTER LEAK AND OPS CK IAW AMM 73-11. OPS CK GOOD. PREFORMED ENGINE RUN IAW AMM 71-00. OPS CK GOOD. MSG'S CLEARED.

Part: SLIDE — BINDING (RT OVERWING) · airframe 65,593 hrs · 8,957 cycles

RIGHT OVERWING ESCAPE SLIDE AFT UPPER CORNER JAMBING AND BINDING. EVALUATION: SLIDE ON DOOR UPPER AFT CORNER IS GETTING STUCK ON DOOR LATCH ACTUATOR. R & R SLIDE PACK ASSEMBLY DUE TO BEING IMPROPERLY PACKED.