N922VA

Part: LINE — LEAKING (HYD SYSTEM) · airframe 18,758 hrs · 4,803 cycles

ENROUTE LOSS OF YELLOW HYDRAULIC QUANTITY GROUNDED - YES. PRESSURE ASSEMBLY LEAKING AT FILTER IN LINE "B" NUT CONNECTION. REMOVED PRESSURE ASSY REF AMM 29-13-49-000-813-A. INSTALLED #2 ENG/PYLON PRESSURE LINE AS FOLLOWS PN: D2902083900000 ITEM #2, ITEM #1 AND ITEM #3 IAW AMM 29-13-49-400-813A. INSTALLATION AND LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,587 hrs · 4,762 cycles

L2 DOOR EMERGENCY EXIT OVERHEAD LIGHT INOP. GROUNDED - YES. SECURED TERMINAL CONNECTOR OF CABIN EMERGENCY LIGHT OVERHEAD ON L2 DOOR 35WL A321 AMM 33-51-11-400-001-A. PERFORMED OPS TEST IAW A321 AMM 33-51-11-400-001-A STEP F CHECK GOOD

Part: FLOORBOARD — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,584 hrs · 4,761 cycles

MAIN CAIN FLOOR BOARD 261LG UPPER AND LOWER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD P/N: D5367680500200 261LG AT FR66 TO FR68 RBL 30 TO RBL 50 IAW A321 AMM 53-00-00-400-801-A-01.

Part: FITTING — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

AFT RH PASSENGER DOOR CUTOUT AFT LOWER CORNER HAS CORROSION AT FR68 GROUNDED - YES. REMOVED AND REPLACED AFT RH PASSENGER DOOR CUTOUT AFT LOWER CORNER FITTING AT FR68 IAW A321 SRM 51-42-11.

Part: FLOORBOARD — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOORBOARD 261LG UPPER END LOWER SURFACE HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 261LG IAW A321 AMM 53-00-00-400-801-A-01

Part: FITTING — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

AFT R/H PASSENGER DOOR CUTOUT AFT LOWER CORNER HAS CORROSION AT FR68. GROUNDED - YES. REMOVED AND REPLACED AFT R/H PASSENGER DOOR CUTOUT AFT LOWER CORNER FITTING AT FR68, STR 23R IAW A321 SRM 51-42-11.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOOR R/H OUTBD LATERAL SHEAR PLATE HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE P/N: D5347112420300 AT MAIN CABIN FLOOR R/H OUTBD LATERAL AT FR69 TO FR70, Y=-1732R, STR 23R IAW A321 SRM 51-42-11/001 PARA 2E AND 2M.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOOR SUPPORT UPPER SURFACE IS CORRODED AT RBL 24. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BEAM AT RBL 24, FR66 TO FR70 IAW A321 SRM 51-42-11/001.

Part: FLOORBOARD — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOOR BOARD 221FF UPPER SKIN IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 221FF AT FR16 TO FR20, LBL 52 TO LBL 73 IAW A321 AMM 53-00-00-400-801-A-01.

Part: SEAT TRACK — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOOR SUPPORT L/H SIDE IS CORRODED IN 2EA PLACES BETWEEN FR16 TO FR18. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK P/N: D5313520720000 AT FR21 TO FR24, Y = -1292 IAW A321 SRM 51-42-11/001 REV 29.

Part: FLOORBOARD — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOOR BOARD 222FF UPPER SKIN CORRODED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 222FF P/N: D5367647800100 AT FR16 TO FR20, RBLE22TO RBL73 IAW A321 AMM 53-00-00-400-801-01.

Part: FLOORBOARD — DELAMINATED · airframe 18,583 hrs · 4,761 cycles

MAIN CABIN FLOOR BOARD 222EF UPPER SKIN IS DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOOR BOARD 222EF IAW A321 SRM 53-02-00-283-001, REV. 144 TABLE 3.

Part: BRACKET — CORRODED · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

AFT CARGO LOWER DOOR SILL TORQUE BOX UPPER WEB HAS CORROSION IN MULTIPLE AREAS. GROUNDED - YES. REMOVED AND REPLACED 1EA NEW WEB P/N: D5347556522400 AT AFT CARGO LOWER DOOR SILL TORQUE BOX AT FRAME 52A TO FR56, STR 39R TO STR 41R IAW SRM 51-42-11/001 REV 28.

Part: BRACKET — CORRODED (UNKNOWN) · corrosion level 2 · airframe 18,583 hrs · 4,761 cycles

AFT CARGO LOWER DOOR SILL TORQUE BOX UPPER WEB HAS CORROSION IN MULTIPLE AREAS. GROUNDED - YES. REMOVED AND REPLACED 1EA NEW WEB P/N: D5347556522400 AT AFT CARGO LOWER DOOR SILL TORQUE BOXT AT FRAME 52A TO FR56, STR 39R TO STR 41R IAW A321 SRM 51-42-11/001 REV 28.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,958 hrs · 4,344 cycles

EMERGENCY LIGHT EXIT R2 LOWER LIGHT BULBS OUT. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT EXIT R2 LOWER IAW A321 AMM 33-21-13-00/400-001-A. PERFORMED OP'S CHECK PER A321 AMM 33-51-13-710-050-A. OP'S CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR SYS) · airframe 8,217 hrs · 2,172 cycles

AIR BLEED CLASS II MSG GROUNDED - YES. RESET AIR BLEED MSG, ALL CLEARED. REF AMM 36-11-00-740-001.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR SYS) · airframe 7,217 hrs · 2,172 cycles

AIR BLEED CLASS II MSG GROUNDED - YES. RESET AIR BLEED MSG, ALL CLEARED. REF AMM 36-11-00-740-001.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR SYS) · airframe 8,217 hrs · 2,172 cycles

CLASS 2 MAINT MSG ON FOR "AIR BLEED" GROUNDED - YES. VERIFIED PFR SHOWS AIR BLEED CLASS 2 MSG. L WING LOOP B INOP. NO CURRENT FAULTS. BMC 2 SOURCE IN PFR. BMC 2 ELEC TEST GOOD, GROUND REPORT NO FAULTS, BMC #2 GROUND SCAN NO FAULTS. REF TSM 36-22-00-810-907-A. FAULT CONF. RESET CLASS 2 FAULT. FWC #1 & #2 C/B RESET. NO CURRENT FAULTS. REF AMM 36-11-00-710-002 A

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 FADEC) · airframe 8,139 hrs · 2,153 cycles

ENGINE 1 FADEC FAULT GROUNDED - YES. PEFORMED FADEC TEST NON-MOTORING NO FAULTS FOUND REF AMM 73-29-00 A.C OK FOR SVC

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 8,129 hrs · 2,150 cycles

ENGINE 2 REV MINOR FAULT GROUNDED - YES. PER TSM 78-37-00-810-839-A PRFORMED TR CYCLING TEST. NO FAULT FOUND. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 8,137 hrs · 2,152 cycles

ENG 1 TLA FAULT. GROUNDED - YES. ACCOMP. OPS TEST OF THROTTLE CONT. UNIT FOR TEST OPEN 18C/B'S & INST. 18 MIG51A'S ACCOMP. TEST, TEST PASS NO FAULTS.CLOSED 18C/B'S & REMOVED 18 MIG51A'S. REF. M/M 76-11-00-710-805 & 22-96-00-740-050.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,258 hrs · 1,938 cycles

AIR BLEED MESSAGE ON ECAM STATUS PAGE GROUNDED - YES. RESET RMCS AND TEST OK PER AMM 36-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,162 hrs · 1,908 cycles

INTERMITTENT ENG 1 HP TIP CONTROL FAULT GROUNDED - YES. PERFORMED TSM 75-22-00-810-819-A AND IDLE TEST AMM 73-29-00-740-803-A TEST OK NO MAINT ACTION REQUIRED PER TSM 75-22-00-810-819-A. A/C OK FOR SERVICE

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 7,135 hrs · 1,900 cycles

CLASS 2 AIRBLEED MESSAGE ON ECAM GROUNDED - YES. APPLIED MEL 36-36-00-04 OPENED MDDR 68627 MCC NOTIFIED . NO MAINT PROCEDURE REQUIRED MEL LIST UPDATED PLACARD INSTALLED.

Part: COMPUTER — FAILED (BLEED AIR SYS) · airframe 7,043 hrs · 1,876 cycles

AIR BLEED CLASS 2 MESSAGE GROUNDED - YES. PER TSM 36-22-00-810-887-A R+R BMC 1 REF AMM 36-11-34 OPS CK GOOD. AIR BLEED FAULT NO LONGER APPEARS, AIRCRAFT RELEASED FROM MEL 36-36-00-04. MDDR 68361 REMOVED. MCC NOTIFIED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,027 hrs · 1,870 cycles

CLASS II MX MSG: AIR BLEED GROUNDED - YES. PERFORMED POWER RESET PER TSM 24-00-00-810-818

Part: WARNING MESSAGE — ILLUMINATED (BLEED AIR) · airframe 6,919 hrs · 1,838 cycles

CLASS II MESSAGE AIR BLEED AFTER SHUTDOWN GROUNDED - YES. DEFERRED

Part: WARNING MESSAGE — ILLUMINATED · airframe 6,772 hrs · 1,801 cycles

AIR BLEED CLASS 2 MESSAGE GROUNDED - YES. DEFERRED

Part: WARNING MESSAGE — ILLUMINATED · airframe 6,756 hrs · 1,798 cycles

ECAM : CLASS II - EIU 1 & 2 GROUNDED - YES. DEFERRED

Part: COMPUTER — FAILED (BLEED AIR SYS) · airframe 6,754 hrs · 1,796 cycles

AIR BLEED CALSS 2 MESSAGE GROUNDED - YES. REPLACED #1 BMC IAW AMM 36-11-34-04. NO FAULTAS NOTED. BITE TEST GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED SYSTEM) · airframe 6,656 hrs · 1,771 cycles

CLASS II AIR BLEED MESSAGE GROUNDED - YES. RESET CB`S REF AMM 36-20-00 OPS CHECK GOOD NO FAULT. THIS CLEARS MDDR 66051 AND MEL 36-36-00-04, MEL LIST UPDATED PLACARD REMOVED, MCC WILL NOTIFIED

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 6,640 hrs · 1,768 cycles

CLASS II AIR BLEED FAULT MSG ON ECAM GROUNDED - YES. RESET C/BS CHECK GOOD PER AMM36-11-00, T

Part: COMPUTER — MALFUNCTIONED (BLEED AIR SYS) · airframe 6,330 hrs · 1,694 cycles

AIR BLEED CLASS II MAINT MSG GROUNDED - YES. R/R BMC NR 1 IAW 36-11-34, OPS CHECK GOOD. PLACARD REMOVED, LIST UPDATED, MCC NOTIFIED. NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,239 hrs · 1,672 cycles

ON ENGINE SHUTDOWN AT GATE GOT: ENG 1 ONE TLA FAULT, ENG 1 REV MINOR FAULT ECAM MSGS GROUNDED - YES. PERFORMED TS 76-11-00-810-831-A & TS 78-31-00-810-A23-A.OPS CHECKS GOOD NO MSG ON GRD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,030 hrs · 1,619 cycles

ENGINE 1 OVTHR PROT FAULT ECAM GROUNDED - YES. PERFORMED OPS ENGINE 1 IDLE TEST ON CH A PER TSM 73-21-01-810-928-A, IAW AMM 73-29-00-740-803-A, TEST OKAY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,940 hrs · 1,600 cycles

CLASS II MX MSG - AIR BLEED GROUNDED - YES. DEFERRED. ETOPS RESTRICTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,878 hrs · 1,583 cycles

AIRBLEED MAINTENANCE STATUS MESSAGE DISPLAYED GROUNDED - YES. RESET C/B PER TSM 36-00-00 OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR) · airframe 5,509 hrs · 1,464 cycles

CLASS II AIR BLEED MSG. GROUNDED - YES. RESET FWC 1 AND 2. MSG CLEARED. OK FOR SVC. BMC TEST OK.

Part: WARNING MESSAGE — ILLUMINATED (BLEED AIR) · airframe 5,312 hrs · 1,391 cycles

CLASS II MAINT STATUS MESSAGE DISPLAYED AFTER SHUTDOWN 'AIR BLEED'. GROUNDED - YES. ON DEFERRAL

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,289 hrs · 1,386 cycles

APU FIRE LOOP 'B' - FAULT GROUNDED - YES. NO FAULT FOUND ON PFR & FAULT HISTORY SYSTEM TESTED IAW AMM 26-13-00 AND SYSTEM FOUND OK.

Part: STATUS MESSAGE — FALSE ACTIVATION (AIR BLEED) · airframe 5,278 hrs · 1,384 cycles

AIR BLEED MTNCE STATUS MESSAGE IN WHITE ON SD PAGE GROUNDED - YES. COMPLETED BITE TEST BMC 1+2 AMM 36-00-00 TEST PASSED AND CLASS II MSG CLEARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,123 hrs · 1,346 cycles

CLASS II" MAINTENANCE" " AIRBLEED" ON ECAM (WORK WITH RMA 2519) GROUNDED - YES. ON DEFERRAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,117 hrs · 1,344 cycles

AIR BLEED CLASS II MAINTENANCE MESSAGE GROUNDED - YES. PERFORMED BMC TEST PER AMM 36-11-00. AIR BLEED MSG CLEARS. OK FOR CONT SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,024 hrs · 1,324 cycles

CLASS II AIR BLEED STATUS MESSAGE GROUNDED - YES. DEFERRED.

Part: FUEL STRAINER — CLOGGED (NR 2 ENGINE) · airframe 5,011 hrs · 1,315 cycles

ENG 2 FUEL STRAINER CLOG ECAM. GROUNDED - YES. R&R FUEL STRAINER ON NR 2 ENG PER AMM 73-34-10. OPS & LEAK CHECK GOOD. OK FOR SERVICE.

Part: COMPUTER — FAILED (BLEED AIR SYS) · airframe 4,991 hrs · 1,300 cycles

CLASS II AIR BLEED MSG ON ECAM STS PAGE GROUNDED - YES. R/R BMC1 REF AMM 36-11-34 PB401 AND PERFORMED BITE TEST REF AMM 36-11-00. NO FAUTLS NOTED. PLACARD REMOVED. MEL LIST UPDATED. MCC NOTIFIED. THIS CLEARS MDDR 60674.

Part: FILTER — UNKNOWN (NR 2 ENGINE) · airframe 4,960 hrs · 1,294 cycles

ITEM 1. ENG 2 FUEL STRAINER FAULT FUEL STRAINER SNSR GROUNDED - YES. ITEM 2 - DEFERRED. REF ITEM NR 1: PER MEL REQUIREMENT P/R ENG 2 FUEL FILTER PER AMM 73-11-10 PB 401 LEAK CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,945 hrs · 1,291 cycles

PACK 2 REGULATOR FAULT GROUNDED - YES. PREFORMED OPS TEST OF PACK TEMP CONTROL SYS REF AMM 21-61-00-710-001-A NO FAULTS NOTED. MDDR 60544 CLEARED MEL LIST UPDATED MCC.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,718 hrs · 1,209 cycles

ENG 2 REV MINOR FAULT ECAM MSG ON ENGINE START. GROUNDED - YES. DEFERRED.

Part: FAULT MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 4,537 hrs · 1,142 cycles

PACK 1 REGULATOR FAULT. GROUNDED - YES. NO FAULT ON ECAM, RESET PACK 1 & PERFORMED BITE TEST, TEST OKAY REF AMM 21-61-00.

Part: COMPUTER — MALFUNCTIONED (BLEED AIR SYS) · airframe 4,542 hrs · 1,143 cycles

CLASS II AIRBLEED MSG GROUNDED - YES. RESET BMC1 & BMC2 IAW AMM 36-11-00-740-001.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR) · airframe 4,500 hrs · 1,132 cycles

CLASS II MAINTENANCE MESSAGE FOR THE AIR BLEED DISPLAYED, A & P 3687395. ACFT GROUNDED. RESET BOTH BMC IAW AMM 36-11-00, NO FAULT FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED) · airframe 4,287 hrs · 1,072 cycles

BLEED AIR CLASS 2 MX MESSAGE. ACFT GROUNDED. PERFORMED BMC NR 1 BITE TEST IAW AMM 36-11-00, OPS CHECKED GOOD, NO FAULTS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,038 hrs · 988 cycles

PRESSURE LIGHTS AT ALL EXIT DOORS WERE FLASHING RED PRIOR TO PUSHBACK GROUNDED - YES. PERFORMED CPC SYSTEM TESTS. NO FAULTS FOUND. TEST OK. REF AMM 21-31-00-710-002-A.

Part: UNKNOWN — SPALLED (NR 2 ENGINE) · airframe 3,712 hrs · 901 cycles

PER MAINT CONTROL, AIRCRAFT PLACED IN ETOPS RESTRICTED STATUS DUE TO NR 2 ENGINE EBC SPALL. GROUNDED - YES. *DEFERRED* *ETOPS RESTRICTED*

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 3,507 hrs · 845 cycles

ENG 2 FADEC SYS FAULT UPON LANDING. GROUNDED - YES. PERFORMED TSM OPERATIONAL ENGINE IDLE TEST ON CHANNELS A&B ON ENG NR 2 IAW AMM 73-29-00-740-803. NO FAULTS FOUND TEST OK NO ECAM FAULTS NOTED. OK FOR SERVICE.

Part: THRUST REVERSER — MALFUNCTIONED (NR 2) · airframe 3,449 hrs · 829 cycles

NR 2 ENGINE THRUST REVERSER, MINOR FAULT, ACFT GROUNDED. PERFORMED A THRUST REVERSER CYCLING TEST IAW AMM 73-29-09-740-804-A. OPS CHECKED GOOD. NO FAULTS.

Part: OIL SYSTEM — OVERTEMP (NR 2 ENGINE) · airframe 3,444 hrs · 828 cycles

NR 2 ENGINE SHUTDOWN DUE TO A HIGH OIL TEMP. DIVERTED. THE NR 2 ENGINE OIL TEMPERATURE LIMIT EXCEEDED. ACFT GROUNDED. TROUBLESHOT IAW TSM 79-32-00-810-853-A. NO FINDINGS NOTED. IAW ENGINEERING REQUEST, R & R THE OIL PRESSURE TEMP SENSOR IAW AMM 79-32-05 PB 401. ACCOMPLISHED ENGINE HIGH POWER RUN ALL PARAMETERS NORMAL. A/C OK TO PROCEED. AT THE END OF A FLIGHT, ON REACHING BINGO FUEL, PROCEEDED TO THE ALTERNATE. NEARLY AT FINAL APPROACH, AT APPROXIMATELY 4000 FEET, RECEIVED AN ECAM MESSAGE FOR THE NR 2 ENG OIL TEMP EXCEEDING LIMITS. THE PILOT TROUBLESHOT THE ISSUE, REDUCED THE ENGINE TO IDLE AND NOTICED THAT THE NR 2 ENG OIL TEMPERATURE HAD RETURNED TO NORMAL. BOTH PILOTS OBSERVED THAT THE NR 2 ENG OIL TEMPERATURE WAS FLUCTUATING CONSIDERABLY AND REACHED APPROXIMATELY 195C. THE PILOTS AGREED TO CONTINUE FOLLOWING THE ECAM PROCEDURE AND SHUTDOWN THE ENG. DECLARED AN EMERGENCY. FIRST OFFICER PROCEEDED TO FINISH THE ECAM AND QRH PROCEDURES. PERFORMED AN UNEVENTFUL SINGLE-ENGINE LANDING.

Part: REGULATOR — MALFUNCTIONED (NR 1 A/C PACK) · airframe 3,176 hrs · 751 cycles

NR 1 A/C PACK REGULATOR FAULTED. ACFT GROUNDED. RESET THE CIRCUIT BREAKER AND PERFORMED AN OPS CHECK, OPS CHECKED GOOD, NO DEFECT NOTED IAW AMM 21-61-00.

Part: ANTI-ICE SYSTEM — INTERMITTENT (NR 2 ENGINE) · airframe 3,264 hrs · 747 cycles

NR 2 ENGINE ANTI ICE INTERMITTENT FAULT. ACFT GROUNDED. RAN ENGINE, OPERATED THE ANTI-ICE, NO FAULTS IAW AMM 30-21-00-810-857A.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR) · airframe 3,143 hrs · 743 cycles

BLEED AIR CLASS II MAINTENANCE STATUS MESSAGE, ACFT GROUNDED. PERFORMED BMC 1, AND 2 TEST IAW AMM 36-11-00. OPS CHECKED GOOD. NO FAULTS FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,468 hrs · 260 cycles

AIR PACK 1 REGUL FAULT GROUNDED - YES. REF TSM 24-00-00-810-818-A, RESET AIR COND SYS CTL FAULT CLEARED, PERFORMED CAB TEMP CTL SYS IAW AMM 21-63-00 NO FAULT NOTED.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 2,625 hrs · 610 cycles

NR 1 ENGINE START VALVE FAULTED. START VALVE NOT OPEN. ACFT GROUNDED. R & R THE NR 1 ENGINE START VALVE IAW AMM 80-11-15. OPS CHECKED GOOD IAW AMM 73-29-00,

Part: START VALVE — FAILED (NR 2 ENGINE) · airframe 2,555 hrs · 590 cycles

NR 2 ENGINE START VALVE FAULTED. START VALVE NOT OPEN. ACFT GROUNDED. R & R THE NR 2 ENGINE START VALVE OPS CHECKED GOOD IAW AMM 80-11-15

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 2,474 hrs · 561 cycles

NR 2 ENGINE ANTI-ICE FAULT, VALVE NOT OPEN. ACFT GROUNDED. IAW AMM 30-21-51 REPLACED THE AIR INTAKE ANTI ICE VALVES. NR 2 ENGINE IDLE TEST SATISFACTORY. NO FAULTS NOTED. LEAK TEST OK. FOUND SENSE LINE ON PRSOV 2 LOOSE. SECURED THE LINE. FOUND PRSOV 1 VALVE BUTTERFLY STICKING.