N391HA
Registered owner: HAWAIIAN AIRLINES INC, HI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
4R DOOR SAFETY PIN IS CROOKED. DIFFICULT TO REMOVE. GROUNDED - YES. INSPECTED 4R DOOR SAFETY PIN. PIN CONDITION FOUND OK. READJUSTED AND LUBRICATED SAFETY PIN AND OPS CHECK OK. OK FOR SVC.
ETOPS - NR 2 PACK OUTLET TEMP "XX". REMOVED AND REPLACED NR 2 PACK OUTLET TEMP SENSOR PER AMM 21-53-18. OPS/LEAK CHECK GOOD. OK FOR SVC.
ETOPS - 1L PA INTERPHONE HANDSET INOP/BROKEN. REMOVED AND REPLACED 1L HANDSET ASSY PER AMM 23-73-44. OK FOR SVC.
ETOPS - DURING INSTALLATION OF #1 ENG EDP FOUND HYD SUCTION LINE CHAFED. REQUIRES REPLACEMENT. REPLACED #1 ENG GREEN HYD PUMP SUCTION LINE PER AMM 29-11-49-000-809-A/400-809-A. LEAK CHECK OF SUCTION LINE NO LEAKS DETECTED. OK FOR SVC.
ETOPS - ECAM APU FUEL LOW PRESSURE FAULT. REMOVED AND REPLACED AFT FUEL FEED PUMP IAW AMM 28-22-52-000-801-A AND 28-22-52-400-802-A, LEAK CHECK GOOD, OPS CHECK GOOD, OK FOR SERVICE
ETOPS - INFO TO MAINT: ECAM FUEL APU PUMP FAULT CAME ON AFTER START ON TAXI 1N THEN LEEPED. REMOVED LOW PRESSURE SWITCH PER AMM 49-34-11-000-801-A. INSTALLED SWITCH AS NEEDED PER AMM 49-34-11-400-801-A. LEAK CHECK GOOD. OPS CHECK GOOD. OK FOR SVC.
ETOPS - DURING FLIGHT F. USED 1 AND F. USED 1+2 STOPPED COUNTING UP. LAST 3 DIGITS SHOWED AMBER DASHES. F. USED 2 NORMAL. REMOVED AND REPLACED FCMC 2 PER AMM 28-51-34. TEST OK. RAN BOTH ENGINES AT IDLE PER AMM 31-00-00. NO DEFECTS NOTED. OK FOR SVC.
ATB - ECAM AIR ENG 2 BLEED FAULT NOTED. ENG 2 BLEED SW PER ECAM PROCEDURE. REMOVED & REPLACED ENG 2 PRV PER AMM 36-11-52. OPS CHECK/LEAK CHECK OK. REMOVED & REPLACED PACK 2 FLOW CONTROL VALVE PER AMM 21-51-51. OPS CHECK/LEAK CHECK OK. OK FOR SVC.
SEAT TRACK CORROSION FR67, -Y953
SEAT TRACK CORRODED AT FR 33 Y1552.5
SEAT TRACK CORRODED BETWEEN FR 14 AND 15 Y-953
SEAT TRACK CORRODED BETWEEN FR 19 TO FR 20 Y 1456
SEAT TRACK CORRODED BETWEEN FR 13 TO FR 14, DR 1R CUT OUT FWD EDGE
SEAT TRACK CORROSION FR74, Y450 AND FR 72 Y450
SEAT TRACK CORROSION FR74/75, Y-450
SEAT TRACK CORROSION AT FR 70/71 , Y-450
SEAT TRACK CORROSION AT FR74,-YC1
SEAT TRACK CORROSION AT FR66/67, Y450.
SEAT TRACK CORROSION FR33 Y1959.
SEAT TRACK CORROSION Y-450 FR 53.1.
SEAT TRACK CORROSION FR77/78 Y0 AND Y450
SEAT TRACK CORROSION FR 80/82 -Y450
SEAT TRACK CORROSION FR75 -Y450.
SEAT TRACK CORROSION FR74, Y794.3
SEAT TRACK CORROSION FR34 -Y1552.5
SEAT TRACK CORROSION AT FR78 Y0
SEAT TRACK MATERIAL CHIPPED OFF AT FR54 Y-953
SEAT TRACK CORROSION FR35 TO FR 36 Y-2462.
SEAT TRACK CORROSION FR70, Y450
SEAT TRACK CORROSION FR53,1 TO 53,2 Y1959.
SEAT TRACK CORROSION F52 Y-1959
OTHER - ARR, #2 BRAKE OVERHEAT & SMOKE CONDITION. PERFORMED OVERHEAT CONDITION CHECK & NORMAL, CLEANED AREA AS PER AMM 05-51-16--200-801-A AND REMOVED AND REPLACED #2 MAIN WHEEL AS PER AMM 32-41-11-000-801-A.
CABIN CREW ADVISED A STRONG BURNED PLASTIC SMELL LASTING TWO MINUTES WAS EVIDENT AFTER TAKEOFFF. THE SMELL DISSIPATED. FUMES FORM ATTACHED TO THIS WRITEUP. POSITION 2 DOORS TO AFT OF AIRCRAFT. FOUND #2 OVEN IN MID GALLEY FAILURE, (MOTOR STARTUP FAILURE), BURNING SMALL ASSOCIATED WITH OVEN. SEE LP 0982690/1 FOR SDL OF OVEN. AC OKAY TO CONTINUE.
ETOPS - OBSERVED ENGINE #1 ABOVE AVERAGE OIL CONSUMPTION. MINIMUM OBSERVED INFLIGHT 10.0 QTS. ALL OTHER INDICATIONS NORMAL. FOUND #1 ENG PRESSURE OIL FILTER ELEMENT HOUSING LEAKING. REMOVE & REPLACE HOUSING SEAL RING PER AMM 79-22-43, LEAK CK OK. SVC ENG OIL TO FULL, 10 PINTS ADDED.
ETOPS - ECAM ENG 2 FUEL FILTER CLOG. PERFORMED TSM 73-21-79-810-804-A. REMOVED AND REPLACED FUEL FILTER. NO DEFECTS NOTED. PERFORMED ENG 2 RUN, OPS CHECK GOOD NO FAULTS NOTED
ETOPS - AFTER LANDING ENG 1 CTL SYS FAULT. EEC1 VSV TEST FAULTED VSV CONTROL UNIT (4081KS). REMOVED & REPLACED VSV CONTROL PER AMM 75-33-51.HIGH POWER RUN OK. NO LEAKS NOTED. SYSTEM CHECK OK.
ATB - AIR TURN BACK MAJOR HAZMAT LEAK LAV G. LOCK LAV G - TOILET INOP - NOT USABLE. AREA CLEANED & SECURED BY CABIN SERVICE. REMOVED & REPLACED LAV G TOILET ASSY PER AMM 38-31-41-801-A. OPS & LEAK TEST GOOD. PLACARD REMOVED, MIC SHEET UPDATED.
ETOPS-ON CLIMBOUT BELOW 1000FT, ECAM: "AIR ENG 2 BLEED FAULT" AND "AIR ABNORM BLEED CONFIG" AFTER LEVEL OFF, RESET SUCCESSFUL. REMOVED & REPLACED #2 ENG PRV PER AMM 36-11-52-000/400-804A. OPS AND LEAK CHECK OK. OK FOR SVC. VALVE, BLEED, P OFF 33-3611-9-0002 02376 ON 33-3611-9-0002 03245
SHIP 391 BUSH ROTATION WAS OBSERVED ON THE OUTBOARD LUG BUSH ON THE MLG SIDE STAY FITTING ON THE LEFT HAND WING. UPON BUSH REMOVAL, CORROSION WAS FOUND IN THE OUTBOARD LUG BORE AND OUTBOARD SPOTFACE. CORRECTIVE ACTION:DAMAGE REMOVAL, INSPECTION AND MAJOR REPAIRE WERE DONE PER ER/A 601934-14. (2400655)
SHIP 391 CORROSION WAS FOUND FWD LUG OF RH MLG RIB 6. CORRECTIVE ACTION: CORROSION/DAMAGE REMOVAL, INSPECTION AND MAJOR REPAIRE WERE DONE PER ER/A 601674-14. (2401047)
SHIP 391 CORROSION WAS FOUND FWD LUG OF LH MLG RIB 6. CORRECTIVE ACTION: CORROSION HAS BEEN REMOVED BY OVERSIZING THE FWD LUG BORE. AND MAJOR REPAIRE WAS DONE PER ER/A 601775-14. (2401041)
SHIP 391 DURING WALK AROUND, MAINTENANCE NOTED THAT THE SILICONE PROTECTIVE LAYER MATERIAL WAS MISSING FROM LH UPPER TRIMMABLE HORIZONTAL STABILIZER APRON FAIRING FIN: 333AT. THE DAMAGE MEASURES APPROXIMATELY 68.5" WIDE AND 17.5" LONG. DAMAGE IS ISOLATED TO THE SILICONE LAYER ONLY. CORRECTIVE ACTION: MAINTENANCE PERFORMED REF ER/A 601267-14. (7268979)
ETOPS - FUELER REPORTS DIFFICULTY FUELING // FOUND OUTER TANK INLET VALVE 1 (500QU1) FAULTING. REMOVED AND REPLACED PER AMM 28-25-57. OPS CHECK OK. ACTUATOR, SINGL OFF 43-2826-9-0002 S/N 40125 ON 43-2826-9-0001 S/N 90702
SHIP 391 EXIT SIGN ABOVE 3L DOOR FELL OFF. CORRECTIVE ACTION: RESECURED SIGN. (8456199)
ETOPS - ON PDC FOUND #1 ENG DRIPPING FUEL FROM DRAIN MAST // REMOVED AND REPLACED #1 ENG FUEL DRAIN EJECTOR PER AMM 71-71-42. OPS AND LEAK CHECK OK. A/C OK FOR SVC.
ETOPS - ENGINE - DURING FILTER CHANGE PER TASK CARD 7923-6017-01-HAL FOUND #1 PRESSURE FILTER (4041KS) DIFFERENTIAL PRESSURE SWITCH CONNECTOR BACK SHELL LOOSE. // REMOVED & REPLACED BACKSHELL ON CONNECTOR 4041KS PER ROLLS ROYCE CMM 70-00-20-400-800.(357297 M. DEINER 12/21/21) OPS CHECK & LEAK CHECK GOOD. OK FOR SVC.
ETOPS - #1 ENG FUEL DRAINS COLLECTOR TANK LEAKING EXTERNALLY // REMOVED AND REPLACED #1 ENG DRAIN COLLECTOR TANK PER AMM 71-71- 41-400-803-A. 1754836 LEAK AND OPS CHK PENDING. OPERATED #1 ENG @ IDLE. NO LEAKS NOTED OK FOR SVC.
BLOCK TURN BACK ENG 2 CTL SYS FAULT ECAM ACTIONS COMPLETED // PERFORMED TSM 71-00-00-810-924-A PERFORMED VSV SYSTEM TEST NO FAULTS NOTED. PERFORMED ENGINE RUN PER 71-00-00-860-875-A. NO FAULTS NOTED. OK FOR SVC
SHIP 391 3L EXIT SIGN PLACARD NEEDS TO BE REATTACHED. CORRECTIVE ACTION: RE-ATTACHED 3L EXIT SIGN. (7742300)
AIR TURN BACK. UNABLE TO MAINTAIN CABIN ALTITUDE. FOUND AUX FLAP PARTIALY OPEN, MAIN FLAP CLOSED IAW MEL 21-26-2. PERFORMED TSM 21-31-00-810-888-A. NO DAMAGE FOUND. TESTED GOOD. PRESSURIZED A/C TO 5.8 DPS. PRESSURE HOLD PER AMM 2131-00-710-802-A. OK FOR SVC.
SHIP 391 3R DOOR EXIT SIGN KEEPS FALLING OFF. CORRECTIVE ACTION: RE-SECURED 3R DOOR EXIT SIGN. (4525793)
SHIP 391 3R EXIT SIGN COVER UNSECURE. CORRECTIVE ACTION: RESECURED COVER. (4525777)
SHIP 391 EXIT SIGN INOP AT 3R. CORRECTIVE ACTION: REINSTALLED EXIT SIGN LENS. (4084623)
ETOPS - #2 ENGINE INLET COWL EXTERNAL SKIN IS CRACKED/PUNCTURED @ APPROX. 5:30 POSITION 1" FROM AFT EDGE EXTENDING 9 1/4" FWD. // REMOVED #2 AIR INTAKE COWL PER AMM 71-61-41-000-802-A. 1724236 3/3/21 REPLACED AND INSTALLED #2 AIR INTAKE COWL PER AMM 71-61-41-400-802-A. OPS CHECK, LEAK CHECK GOOD. OK FOR SVC. COWL, NOSE; AIR OFF 43-7111-9-0003 02478 ON 43-7111-9-0003 02144
ETOPS - DUE TO REPEAT AIR ENGINE 2 BLEED NOT CLOSED ECAM MESSAGE. REMOVED AND REPLACED NR 2 ENGINE PRV, PER AMM 36-11-52-400-804-A, IPC 36-11-52-01. OFF P/N: 43-3611-9-0002 S/N:02642 ON P/N:43-3611-9-0002 S/N:02376. LEAK CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - AIR APU BLEED FAULT. // NO CURRENT FAULT SHOWING CYCLED APU BLEED WITH APU RUNNING WITH NO FAULT APU BLEED VLV HAS 4 PREV LAST LEG FAULTS RPLCD APU BLEED VLV AS PRECAUTION PER A330 AMM 49-51-51. A/C OK FOR SVC.
EMERGENCY LIGHT ABOVE 3R INOP. // REPLACED LIGHT BULB ABOVE 3R. OPS CHECK GOOD. OK FOR SVC
ENG 2 FUEL FILTER CLOG//PER TSM 73-21-79-810-804-A CONNECTOR 403KS-A IS A STRAIGHT METALLIC BACKSHELL. CONTINUITY CHECK BETWEEN 4034KS PIN1 1 + 4000KS-JA1 PIN 49, 4034KS PIN 3 + 4000KS-JA1 PIN 48 GOOD. INSULATION RESISTANCE CHECK BETWEEN 4034KS-A + 4000KS-JA1 GOOD. NO SHORT TO GROUND. REMOVED AND REPLACED #2 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-11. LEAK CHECK GOOD. OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - L/H ENG FUEL LEAK FROM DRAIN MAST VSVA/TCC EGR 10 MINS C/O LEAK INCREASED FROM 12DPM TO 50DPM IAW TASK 71-71-00-200-805A PT 1-8. 1 TSM TASK 71-00-00-810-914-A C/O LEAK ISOLATED TO AOHE CONFIRMED BEYOND DISPATCH LIMITS OF AMM 71-71-00-200-801-A DURING 10 MIN RUN APPROXIMATELY 15ML IN 10 MINS (15CC) DISTURBED DRAIN LINES RECONNECTED IAW AMM 50-51-00 TORQUE WRENCH #40054002. L/H ENG AIR OIL HEAT EX CHANGER REMOVED AND REPLACED IAW TASK 71-21-51000-803-A AND 71-21-400-803-A.
ETOPS SIGNIFICANT SYSTEM - L/H ENG FUEL LEAK FROM DRAIN MAST VSVA/TCC EGR 10 MINS C/O LEAK INCREASED FROM 12DPM TO 50DPM IAW TASK 71-71-00-200-805A PT 1-8. 1 TSM TASK 71-00-00-810-914-A C/O LEAK ISOLATED TO AOHE CONFIRMED BEYOND DISPATCH LIMITS OF AMM 71-71-00-200-801-A DURING 10 MIN RUN APPROXIMATELY 15ML IN 10 MINS (15CC) DISTURBED DRAIN LINES RECONNECTED IAW AMM 50-51-00 TORQUE WRENCH #40054002. L/H ENG AIR OIL HEAT EX CHANGER REMOVED AND REPLACED IAW TASK 71-21-51000-803-A AND 71-21-400-803-A.
AFTER ENGINE START, RECEIVED NOTICE FROM THE AFT GALLEY OF A CAMP FIRE ODOR NEAR THE L4 DOOR THAT DID NOT DISSIPATE. WITH ENGINE 1 & 2 & APU OPERATION. ISOLATION OF PACKS APU & ENGINE. NO CAMP FIRE ODOR NOTED. SMELL CHECK OK AT 4L. NO SMELL NOTED. AFT GALLEY & AFT LAVS NO SMELL NOTED. OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - DURING PDC, FOUND #2 ENG LP COMPRESSOR BLADE ATTRITION LINING TO BE DISBANDED FROM LP COMPRESSOR FRONT CASE.// REMOVED AND REPLACED ENGINE #2 PER TASK CARD 7100-9401-02-HAL. OPS AND LEAK CHECK OK. OK FOR SERVICE. FUNCTIONAL CHECK FLIGHT, CHECKED GOOD.
EMERGENCY EXIT LIGHTS REMAINING ILLUMINATED IN ARM AND OFF POSITIONS. RESET CIDS SYSTEM 1 AND 2. EMERGENCY EXIT LIGHTS OPS CHECK GOOD. OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - IN CRUISE ECAM FUEL - T TANK XFR FAULT. // T/S PER A330 TSM 28-27-00-810-823-A. FOUND TRIM TANK TRANSFER PUMP 709QN DEFECTIVE. ELECTRICAL CONNECTOR STILL OPEN. ALL WORK IN ACCORDANCE WITH SFAR 88 AND CDCCL. PULLED & COLLARED C/B E40 AT 722VU. INSTALLED CAP ON ELECTRICAL CONNECTOR FOR TRIM TANK XFER PUMP. C/W SFAR 88. REMOVED AND REPLACED TRIM TANK TRANSFER PUMP 709QN PER A330 AMM 28-27-48. OPS CHK OK. OK FOR SVC.
ETOPS SIGNIFICANT SYSTEM - AIR APU BLEED FAULT.// PERFORMED BITE TEST OF BMC 1&2 PER A330 AMM 36-11-00. NO FAULT NOTED. PERFORMED ECS BITE, TEST OK. OK FOR SVC.
ETOPS SIGNIFICANT SYSTEM, ENG NR 2 LEAKING FUEL FROM DRAIN MAST WHILE AT IDLE. REMOVED AND REPLACED NR 2 ENG FMU PER AMM 73-21-52-000-802-A AND 73-21-52-400-802-A. OK FOR SVC.
ATB - ETOPS SIGNIFICANT SYSTEM - AFTER TAKEOFF WE GOT AN ELEC IDG 2 OIL LO PR. REMOVED NR 2 IDG PER AMM 24-21-51-000-804-A. INSTALLED IDG PER AMM 24-21-51-400-804-A. INSPECTED IDG OIL FILTER BEFORE REMOVAL FOUND NO METAL PARTICLES. SERVICED IDG RAN NR 2 ENG. NO LEAKS NOTED. A/C OK FOR SVC.
ATB BACK TO HNL DUE ELEC IDG 2 OIL LO PR MESSAGE APPEARED AFTER TAKEOFF. REPLACED THE IDG.
DURING H CHECK, SEAT TRACK BETWEEN FR 26 AND 37.4, -Y 2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FR 47 AND 53.2, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53312812.
DURING H CHECK, SEAT TRACK BETWEEN FR 47 AND 53.2, +Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53312813.
DURING H CHECK, ACCESS DOOR 313AL AFT FRAME FR 94A IS CORRODED. REPLACED FRAME ASSEMBLY AT FR 94A PER SRM 51-42-11 AND DRAWING F53589325.
DURING H CHECK, AFT CABIN AUX FLOOR SUPPORT BEAMS BETWEEN FR 75 AND 78, +Y380 AND -Y380 FOUND CORRODED. REPLACED AUX FLOOR SUPPORT BEAM PER SRM 51-72-11 AND DRAWINGS F53478040.
DURING H CHECK, SEAT TRACK BETWEEN FR 40 AND 47, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F57112821.
DURING H CHECK, SEAT TRACK BETWEEN FR 47 AND 53.2, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53312812.
DURING H CHECK, SEAT TRACK SPLICE PLATE FR 54, -Y450 FOUND CORRODED. REPLACED SEAT TRACK SPLICE PLATE PER SRM 51-72-11 AND DRAWINGS F53329385002.
DURING H CHECK, SEAT TRACK BETWEEN FR 26 AND 37.4, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FR 37.4 AND 39.2, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53311114.
DURING H CHECK, SEAT TRACK BETWEEN FR 37.4 AND 39.2, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53311114.
DURING H CHECK, SEAT TRACK BETWEEN FR 53.2 AND 55, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53326941.
DURING HCK CORROSION WAS FOUND ON THE FUSELAGE SKIN, P/N F5358948020000, AT FR 92 JUST FORWARD OF THE 313AL ACCESS DOOR. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLERS AND DOUBLER PER ER/A 571769-14.
DURING H CHECK, SEAT TRACK BETWEEN FR 26 AND 37.4, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FR 26 AND 37.4, +Y1453 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FR 47 AND 53.2, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53334771.
DURING H CHECK, SEAT TRACK BETWEEN FR 40 AND 47, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F57112824.
DURING H CHECK, SEAT TRACK BETWEEN FR 40 AND 47, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F57112819.
DURING H CHECK, SEAT TRACK BETWEEN FR 26 AND 37.4, +Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FR 26 AND 37.4, +Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWINGS F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 47 AND 53.2, +Y450 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53334771.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 47 AND 53.2, -Y2462 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53312813.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 62 AND 72, -Y1959 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53477040.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 31 AND 35, -Y1552.5 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53275878.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 40 AND 47, +Y450 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F57112816.
SEAT TRACK BETWEEN FRAME 40 AND 47, -Y2462 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F57112826.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 26 AND 37.4 , +Y1959 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53276421.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 53.2 AND 55, +Y1959 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53326941.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 58 AND 62, -Y1959, WAS FOUND CORRODED. THE SEAT TRACKAWAS REPLACED IAW SRM 51-72-11, AND DRAWING F53477040.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 55 AND 58, -Y450, WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53476200.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 55 AND 58, +Y450, WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53476200.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 55 AND 58, +Y1959 FOUND CORRODED. SEAT TRACK REPLACED PER SRM 51-72-11 AND DRAWING F53476200.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 58 AND 68, +Y450 WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53477044.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 58 AND 62, -Y1959, WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53477040.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 58 AND 68, -Y450, WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53477040.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 53.2 AND 53.4, -Y450 FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53326973.
DURING H CHECK, THE SEAT TRACK BETWEEN FRAME 53.2 AND 53.4, +Y450, FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, AND DRAWING F53326973.
DURING H CHECK, SEAT TRACK BETWEEN FRAME 11 AND 18, -Y953 FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-11-15-283-001, FIG 10101.
AFTER TAKEOFF, TANK WAS DONE TRANSFERRING FORWARD, RECEIVED A FUEL TANK TRANSFER FAULT ECAM. PERFORMED LEVEL SENSE TEST ON FCMC 1 & 2 IAW TSM 28-27-00-810-828- A. TEST PASSED, NO FAULTS NOTED. ALSO PERFORMED FUEL VALVES TEST IAW TSM 28-27-00-810-816-A, TEST PASSED, OK FOR SERVICE.
NR 2 ENGINE OIL CHIP DETECTED ILLUMINATED DURING TAXI TO GATE. PERFORMED FIM 79-20-00, FOUND NO DEBRIS. PERFORMED BITE TEST OF EMDC IAW AMM 73-21-00-740-823. TEST PASSED. OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED ECAM AFTER LANDING. UPON ARR, NO FAULT MSG FOUND. CKD PFR FOUND "OIL SYS DEBRIS" CLASS 1 SOURCE EEC 2A PER TSM TASK 79-20-00-810-824-A. PERFORMED EMCD TEST PER AMM 73-21-10. FOUND TEST OK. NO FAULT MSG FOUND. A/C OK FOR SVC.
UPON REMOVING #02 WHEEL ASSY FOR REPLACEMENT FOUND NR 02 BRAKES DAMAGED AND MISSING MULTIPLE RIVETS AND BRACKETS. R&R NR 02 BRAKE ASSY PER AMM 32-42. OPS AND LEAK CHECKS GOOD. OK FOR SVC.
F/A REPORTED A PUNGENT ODOR DURING CRUISE AND DESCENT FROM VENTS. PERFORMED A NR 1 AND 2 ENGINE RUNS, OPERATIONAL CHECKED PACKS, OPS CHECKED GOOD. NO ODORS DETECTED. OK FOR SERVICE.
NR 2 ENGINE ECAM, MINOR ENGINE FAULT. TROUBLESHOT IAW 73-21-71-810-952-A. NO LAST LEG CLASS 3 FAULTS FOUND. NO ECAM MESSAGED. OK FOR SERVICE.
CREW REST SMOKE ALARM TRIGGERED AT BUNK 3, FALSE ALARM. PERFORMED AN OPERATIONAL CHECK OF THE SMOKE DETECTOR IAW AMM 26-18-00, NO DEFECTS NOTED, OK FOR SERVICE
NR 2 ENGINE FUEL FLOW AND FUEL USED IS SIGNIFICANTLY HIGHER THAN THE NR 1 ENGINE. NR 1 FUEL USED IS 10000 LBS NR 2 FUEL FLOW 3000 LBS HIGHER. ACMS SHOWED HIGHER FUEL FLOW ON NR 2 ENGINE. ALL OTHER PARAMETERS NORMAL. REMOVED & REPLACED FUEL FLOW TRANSMITTER.
FLOOR EMERGENCY LIGHT MISSING 1 FOOT PIECE BETWEEN ROWS 28-29A. REPLACED THE LIGHT STRIP.
EXIT LIGHTS ABOVE DOOR 3L AND 3R IS ILLUMINATED. RE-CYCLED LIGHT SWITCH BUT LIGHTS STILL ILLUMINATED. RESET CIDS.
ATB, CHEMICAL SMELL IN COCKPIT AND CABIN. NR 1 ENG & NR 2 ENG BOROSCOPE INSP COMPLETED, NO ABNORMALITIES NOTED. INSP HP6 IP8 & BLEED VLV, NO DEFECTS NOTED / AFT RECIRC FILTERS REPLACED.
AIR TURN BACK DUE TO FUMES IN FLT DECK AND CABIN. INSPECTED APU PER TSM 21-00-00-810-801A. NO DEFECTS NOTED. CONTINUE TO TSM 71-00-81-810-805A. CHK BOTH ENG OIL ENG 1 AT 19.8 AND ENG 2 AT 19.1. DRAINED ENG 1 OIL OK AND RAN ENG 1 & 2 TO VERIFIED OIL AT PROPER LEVEL. VISUAL INSPECTED ENG 1 & 2 NO OIL LEAK NOTED. CONTINUED T/S PER TSM 71-00-81-810-805. PERFORMED 1 AND 2 BOROSCOPES PER AMM 72-00-00-200-812 NO DEFECTS NOTED. PER MCC REQUEST, INSPECTED HP6 IP8 PER AMM 36-11. NO DEFECTS NOTED. AS PRECAUTIONARY REPLACED 8 EA. RECIRC FILTERS PER AMM 21-21 E. C/W 1 AND 2 ENG BOROSCOPE IAW AMM 72-00-00-200-812 NO DEFECTS NOTED. R&R RT OZONE CONVERTER IAW AMM 21-58 OPS CK GOOD. WORK STILL IN PROGRESS. RAN PACKS WITH APU NO ISSUES. RAN PACKS FULL HOT AND COLD WITH EACH ENGINE INDIVIDUALLY AT IDLE AND TOGETHER AT 94% N3 NO ISSUES. A/C OK FOR SVC.
FLOORING LIGHTNING LIFTING OFF THE FLOOR AT ROWS 28 AND 29AB. RE-SECURED FLOOR LIGHTING AT ROW 28 AND 29 / AB.
EMERGENCY LIGHT SIGN ABOVE SEAT 16H MISSING IT'S COVER. REPLACED EMERGENCY LIGHT AT SEAT 16H.
ENG 2 OIL CHIP DETECTED AFTER ENG SHUTDOWN REPEAT. REMOVED AND REPLACED SCAVENGE OIL FILTER ELEMENT PER AMM 79-22-45. OPS CHECK LEAK CHECK GOOD. OK FOR SERVICE.
LAVATORY SMOKE DETECTOR FAULT. RESET CIDS 1 AND 2 IAW AMM 23-35-00. OPS CHECKED GOOD.
AFT CARGO DOOR DAMAGED FROM AFT DOOR SILL ANTI ROLL OUT LATCH BETWEEN FR 61 & 61A, 62 & 62A, 63 & 63A, BEAM 4&5. NO CRACKS NOTED ON DAMAGED AREA VERIFIED WITH EDDY CURRENT CHECK. BLEND "A" REMAINING MATERIAL .040" CHORD: .250" SPAN .250 INSP. BLEND "B" REMAINING MATERIAL .041" CHORD .250" SPAN .250". REMOVED 4EA FASTENERS NEAR BURNISHED AREA. ACCOMPLISHED INTERNAL/EXTERNAL DETAILED INSPECTION AND INSTALLED REMOVED FASTENERS, INSTALLED SILVER DOT PER PRI. CUTOUT DAMAGE HFEC OK. INSTALLED IAW PRI 559603-14.
AFT CARGO DOOR DAMAGED FROM FWD & MID & AFT DOOR SILL LATCHES BETWEEN FRAMES 61 & 61A 62 & 62A 63 & 63A BEAMS 4 & 5. CUTOUT DAMAGE, HFEC OK. FABRICATED DOUBLER AND FILLER. NO CRACKS NOTED ON DAMAGED AREA VERIFIED WITH EDDY CURRENT CHECK. INSTALLED DOUBLER & FILLER IAW PRI 559603-14.
RETURNED TO DEPARTURE DUE TO AIR BLEED LOW TEMP ON BLEED 2 ECAM MESSAGE DURING CLIMB OUT. REPLACED NR 2 ENGINE FAN CONTROL THERMOSTAT, AND EXCHANGER OUTLET TEMP SENSOR, AND FAN AIR VALVE.
FUEL FLOW NR 2 ENG ERRATIC ON T/O CLIMB THRUST 3-400 FLOW DIFF FUEL USED DURING THOSE OPS. NORMAL, ALL OTHER THRUST REQUIREMENTS. NORM IE: CRUISE DESCENT AND APPROACH. ALSO ALL OTHER PARAMETERS NORM. ACCOMPLISHED TSM 73-21-52. FOUND FMU FAULT. REMOVED AND REPLACED FMU ON NR 2 ENG PER AMM 73-21-52. LEAK AND OPS CHECK GOOD. NO DEFECT NOTED. OK FOR SERVICE. METER, FUEL; PO OFF 43-7321-9-0012 12153 ON 43-7321-9-0012 12284
UPON APU START UP, AFTER LANDING, ECAM CAUTION "FUEL APU AFT PUMP FAULT. CAUTION CONDITION INTERMITTENT. FOUND APU AFT PUMP FAULT ON FCMC GRD REPORT. REMOVED AND REPLACED APU AFT PUMP (3QC) PER AMM 28-22-52-400-801-A. OPS CHK OK. A/C OK FOR SVC. PUMP, FUEL FEED OFF 33-2822-9-0002 67096 ON 33-2822-9-0002 14455. UPON APU START ECAM FUEL APU AFT PUMP FAULT. T/S PER TSM 28-22-00 MSG CLEARED APU OPS NORMAL.
DURING TAXI IN WHEN APU BLEED SELECTED ON OBSERVED ECAM FOR AIR APU BLEED FAULT, RESET APU BLEED AND NO HELP. VALVE OPENED AFTER 4 MINUTES, FAULT CLEARED. PERFORMED BITE TEST OF BMC 1 AND 2 IAW AMM 36-11-00-740-802-A. TEST OK. CYCLED APU BLEED P/B SEVERAL TIMES, OPS NORMAL, OK FOR SERVICE.
ABORTED TAKEOFF DUE TO CAPTAIN'S FLUCTUATING AIRSPEED AT ABOUT 140 KNOTS. FLUSHED PITOT LINES IAW AMM 34-11-00-170-801A, LEAK TESTED SYSTEM, AND REPLACED CAPTAIN'S PITOT PROBE.
DUE TO FLUCTUATING AIRSPEED AT ABOUT 140 KTS, ON CAPT SIDE. FLUSHED PITOT LINES IAW AMM 34-11-00-170-801-A. PERFORMED FUNCTIONAL TEST OF AIRSPEED DATA IAW AMM 34-13-00. CHECK OK. LEAK TEST OF CAPT, F/O, AUX PITOTS IAW AMM 34-11-00-790-801-A, OK. R & R CAPTAIN PITOT PROBE IAW AMM34-11-15. OPS CHECK OK. OK FOR SERVICE.
APU AUTO SHUTDOWN. REMOVED APU GENERATOR IAW AMM 24-23-51. INSTALLED APU GENERATOR IAW AMM 24-23-51. STILL NEEDS TO BE TORQUED AND REINSTALL INTAKE DUCT. APU GENERATOR TORQUED AND INSTALL DUCT. OPS CHECK NORMAL.
DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS BAT/EPSU, 13WL, DOOR 2, CLASS 1 MESSAGE APPEARED. REPLACED EPSU DOOR 02L BATTERY, 13WL IAW AMM 33-51-38. OK FOR SERVICE.
FOD DAMAGE NR 2 ENGINE INLET COWL AT 12 O'CLOCK POSITION, 1" ROUND. THE COWL WAS REPAIRED IAW CMM TASK 71-60-00-300-813-A01, AND REPLACED IAW CMM TASK 71-60-00-300-813-A01.
AIRCRAFT ABORTED TAKEOFF AT 65 KTS DUE TO F/O AIRSPEED INDICATION ERROR. REPLACED F/O PITOT TUBE, NR 2 ADM AND HOSE. OPS CHECK OK.
DURING NR 1 FIRE LOOP INSPECTION, FOUND CRACK IN WELD ON FIRE LOOP BELOW OIL COOLER AND ADEL CLAMP CHAFED. R & R FIRE LOOP IAW AMM 26-12-15-000-802-A. FDU 1 & 2 BITE TEST PASSED. OK FOR SERVICE.
HYD YELLOW SYS QUANTITY LOW. FOUND YELLOW ENGINE MOUNTED HYD PULSATION DAMPER O-RING LEAKING. REPLACED O-RING IAW AMM 29-13-54-400-801-A. ENGINE IDLE RUN. NO LEAKS NOTED. CYCLED FLIGHT CONTROLS. OPS CHECK GOOD. HYD FLUID SERVICED-RESERVOIR STILL HAD FLUID WHEN A/C BLOCKED IN. ACFT OK FOR SERVICE.
ECAM ENGINE FAULT FOR NR 1 ENGINE STALL, AUTO RESTART-NORMAL. NR 1 ENGINE, INLET EXHAUST CHECKED GOOD. PERFORMED TSM, OK FOR SERVICE IAW TSM80-00-00-810-899-A.
INBD SIDE OF AFT CARGO DOOR .5" X .7500" AREA DENTED + GOUGED BET. FR63 + FR63A AT BEAM 5. DEPTH OF BLEND, DENT .049, AREA OF BLEND .7500" X 1.2500", NO CRACKS NOTED. .005 MATERIAL REMOVED W/ BLEND. BLENDED GOUGE IAW SRM 51-11-00. TREAT, PRIMED, + PAINTED IAW SRM 51-21-00. ACCOMPLISHED E1 05-391000-TEMP, ENG APP TEMP REPAIR IAW PS 900-5-1, NR 4. OK FOR SERVICE.
INSIDE OF AFT CARGO DOOR SKIN DENTED AND GOUGED BETWEEN FRAMES 63 & 63A ABOVE BEAM 4 & 5. THE GOUGE BLENDED AND HFEC INSPECTED WITH NO CRACKS NOTED. ACFT IS OK FOR SERVICE.
EPSU BATTERY FOUND INOPERATIVE DURING OPS CHECK,. R & R ESPU BATTERY IAW AMM 33-51-38-400-802-A, OPS CHECKED OK, OK FOR SERVICE.
DURING TAKE OFF ROLL, CREW FELT A YAW, AND FELT THE ENGINE SURGE THREE TIMES. ABORTED TAKE OFF. RAN BOTH ENGINES AND PERFORMED LOW POWER SURGE MARGIN DEMONSTRATION TEST PER RI 43-528033-14 REV. ORIGINAL. NO SURGES WERE DETECTED. NO STALL MESSAGES WERE DISPLAYED. ACFT IS OK FOR SERVICE.
SMOKE DETECTOR CONTROL PANEL WILL NOT PUSH TO TEST. R & R SMOKE DETECTOR CONTROL PANEL IAW AMM 26-18-34. REMOVED CONNECTOR FROM CONTROLLER AND INSTALL IT ON THE NEW CONTROLLER IAW AMM 27-70-25. OPS NORMAL.
IAW FUELER ACFT WOULD NOT ACCEPT FUEL. RESET MANUAL OVER RIDE BUTTON ON FUELING MANIFOLD. ACFT WILL ACCEPT FUEL, OK FOR SERVICE. PERFORMED HIGH LEVEL TEST IAW MCC CHECKS GOOD.