N826UA
Registered owner: UNITED AIRLINES INC, IL (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
EMERGENCY LIGHTS TEST FAILS RECEIVED FAULT MESSAGE EPSU UNIT FWD L REMOVED AND REPLACED FWD L EPSU BATTERY OPS CHECK GOOD REF AMM 33-51-38
AUTO BRAKES FAULT ON ECAM. POST FLIGHT REPORTED FAILED BRAKE NORMAL SERVO VALVE 16GG FAILED REMOVED AND REPLACED NORMAL BRAKE SERVO VALVE PER AMM 32-42-48-400-001-A, PERORMED OPS CHECK PER AMM 32-42-00-720-005-A, OPS CHECK GOOD, AND FONCTIONAL TEST OF TECHOMETER PER AMM 32-42-00-720-002-A. TEST PASS. PARTS USED: 31-3244-9-9004,QTY :1 MFG PN ON - C20374000-2 MFG SN ON - 59125 M&E SN ON - 09125 M&E PN ON - 31-3244-9-9004 MFG SN OFF - UNABLE TO IDENT MFG PN OFF - UNABLE TO IDENTIFY ROTABLE PARTS CHG:TT # 1290256 SN OFF 4026 PN OFF 31-3244-9-9004 IPC REFERENCE # DP STATUS UNREADABLE M&E OFF 31-3244-9-9004 SN OFF 4026 - S/N ENTERED IS INVALID VALVE, SERVOVAL OFF 31-3244-9-9004 9515 ON 31-3244-9-9004 9125
EMERGENCY LIGHT BULB NEAR AISLE UNDER SEAT 31C BURNT OUT. REMOVED AND REPLACED LIGHT MODULE. OPS CHECK FAILED. FOUND WIRING PULLED OUT OF CONNECTOR. TERMINATED EMERGENCY LIGHTING WIRE AND MOLEX CONNECTOR IAW ESPM 20-44. REPLACED SEAT MOUNTED EMERGENCY LIGHTING WIRE ASSEMBLY IAW AMM 33-51-19/401 CONFIG 00. OPS CHECKED GOOD.
FUEL CAP MISSING. CHECKED COUPLING FOR LEAKS, NO LEAKS AT THE COUPLING. INSTALLED A FUEL CAP IAW MM 28-25-41. SECURED ATTACHMENT LANYARD, NO DEFECTS NOTED.
CREW REPORTED FUEL CAP MISSING AFTER FUELING. FUEL REPORTS NO CAP ON ARRIVAL TO AIRCRAFT INFO NOTED, SEE LOG PAGE FOR MEL.
UPON INSTALLATION OF LT ELEVATOR OTBD ELEVATOR SERVO. FOUND BROKEN TAB ON ELEVATOR SIDE. TECHNICIAN WAS CLEANING FLUID IN AREA WHEN THE TAB BROKE OFF & FELL INTO THE LIFT. UPON CLOSER INSPECTION GLUE WAS FOUND ON TAB. TAB IS PART OF THE FITTING TO HOLD COTTER PIN. REMOVED LOCKING TAB DAMAGE FLUSH TO SURROUNDING AREA IAW SRM 55-26-47-300-001 STEP 2.A.(4) REMOVAL OF DAMAGE REQUIRES VERIFICATION VERIFIED BLENDED AREA CHECKS OK. IAW SRM 55-26-47-300-001. STEP 2A(4). . ABOVE STATEMENT SHOULD READ PER SRM 55-26-47-300-001. STEP 2A(5) COMPETED UP TO STEP 2(A)8 REF SRM 55-26-47-300-001 VERIFIED MATERIALS AND FABRICATION OF SHIMS AND LOCKING LUG WITH VERIFIED STEPS 2. A. (5-8) ACCOMPLISHED PER SRM 55-26-47-300-001, REPAIR LOCKING LUG MANUFACTURED IN SFO. ACCOMPLISHED IAW GMM 09-25-05. COMPLETED STEPS 2. A. (9) THROUGH (20) OF SRM 55-26-47-300-001. READY FOR VERIFICATION TO INSTALL PARTS. VERIFIED NEW PART AND FIT REF SRM 55-26-47-300-001 STEPS 2A(9) TO(20). COMPLETED STEPS 2. A. (20) THROUGH (28) OF SRM 55-26-47-300-001.
FUELER REPORTS FUEL CAP IS MISSING FROM AIRCRAFT. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41.
CABIN ENTRY LIGHT NEAR DOOR 1R FLASHES RED INTERMITTENTLY RESET LIGHTS FOR FWD ENTRY DOOR, PROFORMED OPS CHECK REF AMM 33-21-00-710-001-A, NO FAULTS NOTED, OK TO CONTINUE.
L/H AILERON HAS COMPOSITE DAMAGE ON TOP T/E. REPAIRED DAMAGED COMPOSITE IAW A319 SRM 51-77-12-911-002 RMVD AND RPLD AILERON TRAILING EDGE CHANNEL IAW A319 SRM 51-42-11 CMM 57-61-21 SRM 51-72-11 CAT A.
EMERGENCY EXIT LIGHTS ONUNABLE TO TURN OFF LIGHT SWITCH WAS IN THE WRONG POSITION. EMERGENCY LIGHTS WORKING NORMALLY OK TO CONT.
FWD AFT LAV TOILET OVERFLOWED DURING CLIMB SENDING WATER INTO AF T AFT LAV AND AFT GALLEY. UPON INITIAL INSPECTION FOUND TOILET FULL OF LIQUID. FLUSHED TOILET TO CHECK FLUSH VALVE, NO EVIDANCE OF LEAKING FROM FLUSH VALVE, SUSPECT FILL SIDE OF SYSTEM. FOUND LAVATORY SHUT OFF VALVE LEAKING, BELIEVE THIS WAS THE MAIN REASON FOR LEAK IN GALLEY/RESTROOM D. OPENED RIGHT PANEL ON RT SIDE AFT CARGO AND DID LEAK CHECK TO SEE IF IT WAS LEAKING AS WE RAN THE TOLIET AND SINK WE SAW NO LEAK AND NO WATER DAMAGE. FROM PREVIOUS LEAK REF AMM 38-10-00-614-001-A. ALSO DID OPS TEST OF TOLIET UNIT, CHECKS OK IAW AMM 38-31-00-710-009-A. WHILE COMPLETING TOILET OPS CHECKS MULTIPLE TIMES THERE WAS NO NOTED TOILET OVERFLOW.
FLT ATTS REPORTED CABIN AIR SMELLED LIKE ROTTEN EGGS AT BEGINNI NG OFDESCENT AND DOWN PER FLIGHT ATTENDANT DEBRIEF, AT TOP OF DESCENT FWD CABIN ONLY SMELLED STRONGLY OF SULFUR. WENT AWAY AFTER PARKING AT GATE. PER PILOTS NO SMELL NOTED IN FLIGHT DECK AT ANY POINT OF FLIGHT. OPERATED BOTH PACKS, COULD NOT DUPLICATE SMELL. NO SMELL DETECTED IN FWD OR AFT CABIN.
VENT BLOWER/EXTRACT FAULT ON TAKEOFF ROLL. REF L/P 4453445. 21-26-53 SKIN AIR OUTLET VAVLE CALL OUT AFTER AEVC TEST REMOVED AND REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53. PERFORMED OPS CHECK PER AMM 21-26-00-710-001A. TEST OK.
GRINDING NOISE AND HOT FRICTION SMELL FROM FRONT LOWER FRONT OF AIRCRAFT. LASTED 2 MIN THEN UPON INSPECTION FOUND VENT BLOWER FAN 20HQ VIBRATING WITH STRONG ELEC SMELL IN MAIN AVIONICS BAY. ITEM HAD HISTORY OF CB TRIPPING EARLIER THIS MORNING. SMOKE FORM ATTACHED REMOVED AND REPLACED AVIONICS VENT BLOWER IN REF AMM 21-26-51, OPS CHECK TEST OK REF AMM 21-26-00 PARTS USED: 40-0597-3-0412,QTY :1 31-2126-9-9004,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1339814 SN OFF 2242 FAN, AVIONICS F OFF 31-2126-9-9004 2242 ON 31-2126-9-9004 3050
F/A RPTS BURNING RUBBER ODOR FRM AFT GALLEY AFTER PARKING AT GAT E ADDING PICTURES OF FORM. ADD PERFOMED INSPECTIONS ON APU AND ACTIVATED APU BLEED AIR. RAN AIR PACKS, CHILLERS, AND OVENS. ALL FUNCTION NORMALLY. NO CIRCUIT BREAKERS ARE POPPED. THERE WAS NO OIL FOUND IN APU HOUSING OR COWLING. CREW WAS ALREADY ABSENT. COULD NOT DUPLICATE ODOR. OK TO CONTINUE.
PDA 2 REF LOG PAGE 9490433, A PORTION OF THE LEFT WING #2 SLAT INBOARD CLOSING PLATE WAS MISSING ON ARRIVAL INTO RDM ON FLIGHT 2082. THE MISSING PLATE WAS PLACED ON CDL 27B. SEE LOG PAGE 9490433.
TAPE APPLIED CAPT AFT WINDOW SEPARATED, TAPE APPLIED TO CAPT SIDE WINDOW THAT IS COVERING SEALANT HAS COME LOOSE AND IS FLAPPING. NOISE ASSOCIATED. CABIN PRESS OK. NO PRESSURIZATION ISSUES, NOISE ASSOCIATED WITH TAPE. TORQUED, SEALED AND REMOVED TAPE ON L3 WINDOW, DUE TO WINDOW SQUEAL. WINDOW SEALANT CURED. ACFT OK FOR SERVICE.
LEFT & RIGHT WINDSHIELD CONTINUITY FITTINGS FOUND TO BE CRACKED DUR ING HFEC INSPECTION. REMOVED AND REPLACED LT & RT WINDSHIELD CONTINUITY FITTING PER PER EC/RA 5311-03129 PART 1 STEP 2.
AFT FUSELAGE 4EA DENTS AROUND TAIL JACKING POINT, REQUIRING EVALUATIONS. REPAIR 04EA DENTS AROUND TAIL JACKING POINT DOOR FR73 AND FR74 B STA: ST ENG BFM. REF ELB 7404529 FOR DMG. BETWEEN STGRS 31RH AND 31LH PER EC/RA 5351-01220, FOUND REPAIR IS PERMANENT REPAIR, NO MORE ACTION REQUIRED, APPLIED 04 DENT DOT PER GMM 06-35-05 IAW EC/RA 2060-01042. INSPECTED AND FOUND SATISFACTORY.
RIGHT EXTERNAL FUSELAGE SKIN FR25-26 STR 41R-42R HAS 2EA DENTS. REPAIRED RT EXTERNAL FUSELAGE SKIN BETWEEN FR25-26 AND 241R-42R. PER EC/RA # 5321-02124 REV ORIGINAL AND FINAL EA 319-5321-13-A34 55 REV -.
DENT WITH GOUGE FOUND AT FR23 BETWEEN STR42 AND 43RH DURING HMV AT VTAERO ON NR80072. IAW SRM53-11-11-300-041. THIS IS A CAT B REPAIR WITH REINP REQ''D REPAIR EMBODIMENT. WHICHEVER COMES FIRST, SUBSEQUENT INSP TBD. IAW SRI53-11-11-205-037 IN ZONE 1 AT 60000FC OR 120000FH FROM DAMAGE EXCEEDS ALLOWABLE DAMAGE, PERFORMED CUTOUT OF DENT/GOUGE BETWEEN STR 43R-42R 3.5 IN FWD OF FR23, INSTALLED DOUBLER REPAIR
FWD CABIN, L1 DOOR SILL, MID FITTING IS CORRODED AROUND FASTENER S HOLE. () REMOVE CORROSION AROUND FASTENERS HOLES L=.925", W=.875", D=.062 CHED FORM: 44-0008 WORK ACCOMPLISHED AT ST ENGINEE " REWORK 51% OF THICKNESS, REMOVED L1 DOOR SILL, MID FITTING AND RING OF MOBILE AT BFM ON NR#: 80108 REPLACED P/N D531119820006 BATCH# 0002534168. I.A.W SRM 51-74-0 0, SRM 51-44-11/001, SRM 51-42-11/001 AND SRM 51-75-12/001.
CABIN FOOR SEAT TRACK Y1292 FRAME 24 TO 35 SEVERIAL POINTS OF CORROSION. () REMOVED AND REPLACED SEAT TRACK Y1292 AT MAIN CABIN BETWEEN LH FR24 TO FR35 IAW SRM 51-42-11.
MAIN CABIN THRESHOLD AT R1 DOOR CUT OUT, FLOOR PANEL SUPPORT STR HAS CORROSION AT FASTENER HOLES. DOT 102-252 () REPLACED CENTER FITTING P/N: D5311219820106 BTCH: 0002527532 IAW A319 SRM 51-42-11.
UNDER R1 SCUFF PLATE FR 16 CORNER STR HAS CORROSION. DOT 102-141 () REPLACED FWD CORNER FITTING P/N D5311222320104 BTCH: 0004192306 IAW A319 SRM 51-42-11
RIGHT WING O/B FLAP T/E AFT OF #3 TRACK LOWER EDGE HAS EXFOILATI NG CORROSION AT PREVIOUS REPAIR. DOT 102-139 () REPAIRED R/H O/B FLAP T/E AFT OF #3 TRACK, LOWER SKIN, I.A.W. SR M 57-53-00-300-120 AND SRM 51-77-11-911 SEE FORM: 44-0008
DURING THERMOGRAPHIC INSPECTION AND TAP TEST OF LH ELEVATOR NDT NOTED INDICATION OF WATER INGRESS AROUND THE 12TH FASTENER FROM I/B EDGE. AREA OF CONCERN IS CIRCLED IN RED AND MARKED WITH AN '' X''. () REPAIRED L/H ELEVATOR T/E, I.A.W. SRM 55-21-11-300-005, AND SRM 51-77-11-911 #44-0008 ATTACHED
DURING THERMOGRAPHIC INSPECTION AND TAP TEST OF RH ELEVATOR NDT NOTED INDICATION OF WATER INGRESS AROUND A TRAILING EDGE FASTENE R AT THE 6TH FROM OUTBOARD. WATER INDICATION CIRCLED IN RED WITH A ''X'' DRAWN THROUGH IT. () REPAIRED R/H ELEVATOR T/E I.A.W. SRM 55-21-11-300-005, AND SRM 5 1-77-11-911 #44-0008 ATTACHED.
FWD CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION LOC. FR 16, +Y 1 300. () FWD CABIN FLOOR SUPPORT FOUND DAMAGE OUT OF LIMITS, REMOVED, REP LACED FLOOR SUPPORT P/N D5311281300251 BTCH 0003979250 IAW SRM 5 1-42-11.
FWD CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION LOC. FR 16, +Y40 0. () REMOVED AND REPLACED 1EA FLOOR BEAM BETWEEN LH FR 12 TO FR 16 IA W SRM 51-42-11 ATTACHED FORM 44-0008 EMP#: V935975 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 79858
CABIN FOOR SEAT TRACK -Y765 FRAME 24 TO 35 SEVERAL POINTS OF CORROSION. () REMOVED CORROSION ON AREA AND FOUND OUT OF LIMITS I.A.W SRM 53-2 1-15-283-004. REMOVED AND REPLACED SEAT TRACK -Y765 FR 24 TO 35 I.A.W SRM 51-72-11 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 79845
FWD CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION LOC. FR16 +Y 600 . REMOVED AND REPLACED SEAT TRACK Y765 BETWEEN FR12 TO FR24 IAW SR M 51-42-11. EMP: V935975 WC: 79857 STA: ST ENG BFM
THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/16/22. PDA 3 FUELER REPORTS FUEL CAP LANYARD IS MISSING. REPLACED FUEL CAP LANYARD.
THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER GENERATED ON 5/25/22. SERVICING CHART RH MAIN LANDING GEAR MISSING GEAR SHOCK STRUT. REMOVED AND REPLACED WITH SERVICEABLE PLACARD.
DENT ALONG STRINGER 22L BETWEEN FRAME 21 AND 23 REQUIRES REPAIR PER 9290286/44286 GEN BY V079529 REPAIRED DENT ALONG STRINGER 22L BTWN FRAME 21 AND 23 IAW A319 S V079529 INSP BY V898117 RM 53-11-11-300-041 FIG.002 SHEET 01 THIS REPAIR IS CONSIDER CAT EGORY B PERMANENT REPAIR INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 60,000 FC/120,000 FH WHICHEVER VALUE OCCURS FIRST SUB SEQUENT INSPECTION AT INTERVALS OF N/A INSP METHOD N/A BY MECH V ADD EMP:V079319
R/H EMER EXIT AFT AND FWD FRAME WEB CRACKED PER 9290245/44245 GE N BY V077960 REMOVED AND REPLACED R/H EMERGENCY EXIT FWD AND AFT FRAME WEB TO P COATED AND CIC''D IAW A319 SRM 51-72-11-911-001,51-44-11/001,51 -75-12-911-002 BY MECH V079529 INSP BY V898117
L/H EMER. EXIT AFT AND FWD FRAME WEB CRACKED PER 9290244/44244 G EN BY V077960 REMOVED AND REPLACED LOCATED DRILLED DEBURRED INSTALLED AND TOP COATED LEFT HAND EMERGENCY EXIT FWD AND AFT FRAME WEB IAW SRM 51 -72-11-911-001,51-44-11,51-21-11,51-75-12-911-002 BY MECH V07952 9 INSP BY V898117
ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD AFTER TAKEOFF GOTHYD Y RSVR LO LVL ECAM. COULD NOT DUPLICATE ECAM Y RSVR LO LVL WITH YELLOW ELE PUMP. RAN #2 ENG YELLOW HYD PUMP PER TSM 52-36-00-810-805-A OPS CHECK GOOD. R&R LOW LEVEL SWITCH AND QUANTITY IND AS PRECAUTIONARY PER TSM 29-13-00-810-801-A OPS CHECK GOOD.
PDA 3 REF LOG PAGE 6736380. LEFT OVERWING SLIDE PANEL HAS PIECE OF THE SKIN MISSING. CLOSED PARENT LOG PAGE. NO NEED FOR DUPLICATE LOG. UPDATING THIS LOG PAGE WITH PICTURES OF DAMAGE TO LEFT OVER WING SLIDE. REPLACED L-H OFFWING ESCAPE SLIDE AND OPS CK''D GOOD. REF: AMM 25-62-42-400-001-A ADD EMP:U181010,U181223,U181191 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1936245 SN OFF 0891 IPC REFERENCE # 25-62-04-16 INSPECTED INSTALLATION OF SLIDE, REF AMM 25-62-42 SLIDE, RAMP-OFF OFF 31-2561-9-0001 5891 ON 31-2561-9-0001 7999
RH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE #7 IS CRACKED IN FITT ING ABOVE PRESSURE PANEL CONTACT ENGINEERING FOR REPAIR BEFORE N EXT FLIGHT AD 2018-06-04 PER LCQ NON ROUTINE 9292328. REMOVED AND REPLACED R/H CORNER FITTING FR36 IAW A319 SRM 51-42- 11 PARA 2F, EA 5330-05216 003, ECRA 5331-02481.
LH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE #7 IS CRACKED IN THE FITTING ABOVE THE PRESSURE PANEL CONTACT ENGINEERING FOR INSTRUC TIONS AND REPAIR BEFORE NEXT FLIGHT AD 2018-06-04 PER LCQ NON ROUTINE 9292325. REMOVED AND REPLACED L/H CORNER FITTING FR36 IAW A319 SRM 51-42- 11 PARA 2F, EA 5330-05216 002.
LH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE 2,4,13,14,15,16,21,23 ,24,25,26,27 AND 28 ARE CRACKED IN THE PRESSURE PANEL CONTACT EN GINEERING FOR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT AD 2018 -06-04 PER LCQ NON ROUTINE 9292324. LH PRESSURE PANEL AT FR35-36 REPAIRED PER ECRA 5331-02480 PART 1 STEP 1. DTA DIP REQUIRED PER PART 1 STEP 2 TO ACCOMPLISH PERMAN ENT REPAIR PER PART 3 OF ECRA 5331-02480 ON OR BEFORE 11 APR 20. PLANNING TO CONTACT ENGINEERING AFTER 11 MAR 2020 BUT BEFORE 26 MAR 2020 FOR THE PERMANENT REPAIR. APPROVED TO CARRY REF ECRA 5331-02480 PERMANENT REPAIR TO BE ACCOMPLISHED PER ECRA 5331-02480 PART 3 ON OR BEFORE 11APR2020 PLANNING TO CONTACT ENGINEERING AFTER 11MAR2020 BUT BEFORE 26MAR2020. TOMC-APPROVAL FROM SC1ELBYC COMMENT Q/C REVIEWED. Q/C REVIEWED. RECORDS UPD
AFT UPPER L/H TAIL SECTION OF FUSELAGE HAS DENT/CREASE ON SURFAC E BETWEEN FR 72-FR73 STRGRS 6L-8L A3NB-05-3-6062 PER HAECO LCQ N R 9292189 GENERATED BY V901665 DURING C-2 HAECO LCQ TECHNICIAN V892069 AND QC LC-32 REPAIRED DE NT INSTALLING REPAIR DOUBLER L=1.5"X W=1.5" FR72-FR73 STR6 L-STR8L IAW SRM 53-00-11-300-042 REPAIR CATEGORY B. INSPECTION P ADD EMP:V892069 ER SRI53-00-11-205-052 TABLE 004 FROM TIME OF REPAIR EMBODIMENT 60000FC/120000FH. SUBSEQUENT INSPECTIONS TBD, METHOD TBD. APPROVED. PER SRM 53-00-11-300-042 INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 60000FC OR 120000 FH SUBSEQUENT INSPECTIONS AND METHOD TBD. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED RECORDS UPDATE ..JF T/A: 60,000 FC OR 120,000 FC ..JF
RH FR68 ON 3RD GUSSET FROM THE TOP ON BOTTOM HOLE HAS REJECTABLE DAMAGE INDICATION. REPAIR REQUIRED PRIOR TO NEXT FLIGHT CYCLE S UPPORT TASK AD RELATED (2015-05-02) PER HAECO LCQ NR 9292205 GEN ERATED BY V916887 REPLACED GUSSET ON R2 PASSENGER DOOR AT FR68 STR 14 IAW A319 SRM 51-42-11-801 AND SRM 51-44-11-801.
RH FR16 DOOR STOP 7 LOWER INBOARD HOLE HAS CRACK INDICATION SUSP ECTED TO BE IN INTERCOSTAL REPAIR REQUIRED PRIOR TO NEXT FLIGHT CYCLE A3NB--53-4-6304 AS RELATED TASK (2018-25-02) PER HAECO LCQ NR 9292191 GENERATED REMOVED NAD REPLACED #7 DOOR STOP INTERCOSTAL IAW A319 SRM 51-72 -11-911-001 WORK ACCOMPLISHED
(SUPPORT TASK) REMOVE AND REPLACE THE THSA. REFER TO N/R: 96 17583. CHANGED DUE TO A LEAK. REMOVED & REPLACED THSA IAW AMM 27-44-51-000-001-A & 27-44- 51-400-001. OPS CHECK GOOD NO DEFECTS NOTED IAW AMM 27-41-0 0-730-001. REFER TO N/R: 9617583. WORK PERFORMED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1271165 SN OFF 1508 ACTUATOR, TRIMM OFF 31-2743-9-0001 1508 ON 31-2743-9-0001 1413.
WITH EMERGENCY LIGHT SWITCH ARMED, AND POWER OFF AIRCRAFT, EMERGENCY LIGHTS BY DOOR 1L AND 1R DO NOT ILLUMINATE. REPLACED THE BATTERY. OPS GOOD.
RT OVERWING EPSU FAILED TO TEST. FOUND RIGHT POWER SUPPLY AT FAULT. REPLACED THE EPSU IAW AMM 33-51-38-400-001. PERFORMED BITE TEST AND FOUND EMERGENCY LIGHTS OPS CKS GOOD.
RIGHT OVERWING SLIDE RESERVOIR CYLINDER PRESSURE IN THE RED BAND. REMOVED AND REPLACED THE CYLINDER IAW AMM 25-62-46-000-001-A, AND 25-62-46-400-001-A. OP CHECKED GOOD.
FWD CARGO POTABLE WATER VALVE INTERNAL HOUSING, FRAMES 28 - 29 STRINGERS 42 - 44L HAS CORROSION. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW DWG D53230935. REMOVED AND REPLACED THE HOUSING IAW SRM 51-42-11-001, AND 51-44-11-0 01.
RIGHT OTBD FLAP FRONT SPAR FWD FACE HAS CORROSION OTBD OF THE NR 3 FLAP TRACK INSIDE CAVITY PANEL NR 2. BLENDED CORROSION AND OUT OF LIMITS IAW SRM 51-73-11. REMOVED AND REPLACED THE RT OTBD FLAP FRONT SPAR WEB AT THE FLAP TRACK IAW SRM 57-53-21-300-004.
AFT CARGO UNDER FLOOR AREA, FLOOR SUPPORT BRACKETS LOCATED ON TOP OF FR59 BETWEEN STR41R-38L HAS SPOTS OF UPPER SURFACE CORROSION AND DOUBLE DRILLED HOLE. BLEND CORROSION AT FR59 STR41R-38L SUPPORT BRACKET FOUND TO BE O UT OF LIMITS, ALSO DOUBLE DRILL HOLE IAW A319 DAN 11304, RECEIVED CROSSBEAM AND ANGLE AND INSTALLED IAW A319 SRM 51-72-11-911-00 1
CORROSION STRINGER 31R FRAMES 65-66 BELOW OUTFLOW VALVE. REMOVED AND REPLACED STR31R PN D5348004 721201 PO NO. 1035886.2 IAW A319 SRM 51-72-11
FWD CARGO UNDER FLOOR AREA HAS SURFACE CORROSION ON THE SHEAR TIE LOCATED ON FRAME 29 BETWEEN STRINGERS 43-44R. EVALUATED AND REMOVED CORROSION FRO M CLEAT MATERIAL REMOVED WAS NOT WITHIN LIMITS IAW NSA2110. REPLACED SHEAR TIE WITH NEW CLEAT IAW SRM 51-72-11-911-001, AND SRM 51-42-11-001
FWD CARGO BILGE SHEAR TIE FRAME 26, STRINGERS 43-44R HAS CORROSION. EVALUATED & REMOVED CORROSION FROM THE SHEAR TIE. MATERIAL REMOVED WAS NOT WITHIN LIMITS IAW NSA2110. REPLACED THE SHEAR TIE IAW 51-72-11-911-001, AND SRM 51-42-11-001
RT OVER WING SLIDE HAS DELAM. 625 PROCURED NEW RT OVERWING SLIDE TO BE INSTALLED ON CARD 17-2562- 1-9912 OP 565.
LEFT OW SLIDE HAS CORROSION AND DELAMINATION ALONG TOP EDGE. PROCURED NEW LT OW SLIDE TO BE INSTALLED ON CARD 17-2562-1-9911 OP 564.
CORROSION ON R-2 DOOR SILL WHERE AFT GIRT BAR FITTING ATTACHES. REMOVED AND REPLACED DOOR SILL IAW SRM 51-72-11-911-001 REV 119, SRM 51-42-11-001 REV 119 RECEIVED NEW SILL PN D53480043207 01 IAW SRM 53-41-14-001.
CORROSION AROUND TWO NUT PLATES L2 DOOR SILL AT FRAME. REPAIRED IAW SRM 53-41-14-300-001, PARA 2A.
PLASTIC COVER FOR EMERGENCY EXIT LIGHTS IN AFT CABIN MISSING. REPLACED THE COVER.
L2 DOOR SLIDE NOT ARMED, DISPLAYED WITH DOOR PRESSURE LIGHT FLASHING. CREW REPORTED NO PRESSURIZATION ISSUES AND NO DOOR HANDLE MOVEMENT. FLT CREW REPORTS L2 DOOR ARMING HANDLE DID MOVE UP SLIGHTLY. FLT ATTENDENT RESET HANDLE AND THE L2 DOOR DID ARM AND PRESSURE LIGHT EXTINGUISHED. REMOVED DEBRIS FROM AFT PORTION OF THE L2 DOOR SILL.
ECAM COMPRESSOR VANE FOLLOWED BY ENGINE STALL ECAM, AND ENGINE FAIL ECAM. SHUTDOWN ENGINE. RESTART SUCCESSFUL. UNEVENTFUL LANDING WITH BOTH ENGINES AND APU ON. REPLACED THE NR 2 ENGINE DUE CHRONIC VSV CHANNEL A FAULTS.
SMOKE DETECTOR FAULT. IAW AMM 26-10-00 RESET SDCU CBS. ALL INDICATIONS NORMAL.
FLIGHT HAD WINDOW HEAT FAIL EN-ROUTE.
EMERGENCY LIGHT TEST FAILED EPSU BATTERY FWD LT. REPLACED FWD LT EMER LIGHT BATTERY IAW MM33-51-39. OPERATIONS CHECKED NORMAL. BATTERY PN AD-3214-30.
CORROSION PRESENT ON R2 DOOR SILL ATTACH HOLES AT FRAME 68. INSTALLED REPAIR STRAP AT DOOR SILL AT FRAME 68 IAW SRM 53-41-14, REPAIR PRINCIPAL 4, FIG 201.
LEFT NAV LIGHT COVER HAS 3 INCH CRACK. STOP DRILLED & TAPED OVER IAW AMM33-4199-350-001-A.
EMERGENCY LIGHT TEST FAILED AT EMERGENCY EXIT LT. REPLACED BATTERY AT EMERGENCY EXIT LT IAW AMM 33-51-38, EMERGENCY LIGHT TEST PASSED ON GND.
DURING NR 2 ENG START ATTEMPT, START VLV FAILED TO OPEN. CREW GOT THE ASSOCIATED ECAM MESSAGE. CONFIRMED NO DUCT PSI DROP & NO N2 ROTATION. ACCOMPLISHED A SECOND START ATTEMPT USING CROSS BLEED AIR FROM NR 1 ENG START VLV FUNCTIONED NORMALLY. NR 2 ENG GOOD START, OK. TO CONTINUE.
UNABLE TO ARM DOOR 2L. REF SEQ 4812004, ARMING CABLE REPLACED IAW AMM 52-13-22.
RAMP REPORTS BROKEN STANCHION AT FWD SIDE OF AFT CARGO PIT DOOR. R & R STANCHION IAW AMM, OPERATIONS CHECKED GOOD.
HOT BRAKES, REPLACED NR 3 MLG BRAKE IAW A319 AMM 32-42-27-000-001-C AND 32-42-27-400-001-A.
UNABLE TO DESELECT VHF 2 AUDIO ON FIRST OFFICER`S SIDE. R & R FIRST OFFICER`S AUDIO CONTROL PANEL.
COCKPIT 4TH OCCUPANT OXYGEN MASK LENS IS SCRATCHED. REPLACED ON WU B9223T.
TWO SCREWS MISSING ON RT SIDE VERTICAL STABILIZER. THREE EACH SCREWS MISSING ON RT SIDE VERTICAL STABILIZER PANEL 323AR. INSTALLED ONE EACH SCREW, REMAINING TWO ARE MISSING RECEPTACLES. REPLACED TWO EACH MISSING FASTENERS AT AFT END OF PANEL 323AR.
SCREW MISSING AT AFT INBD CORNER OF PANEL 191KB NEAR LOWER ROT BEACON. R & R FAULTY RECEPTACLE AND INSTALLED MISSING STUD, WASHER AND WASHER-TAB IAW IPC 53-35-12-01A AND AMM 53-35-13-400-002-A.
ON WALK-AROUND. FOUND A 3 INCH DENT ON L/E OF LT WING JUST ABOVE AND LT OF ENGINE. SUP: DENT IS .070" DEEP AND 3.5" WIDE AND HEIGHT IS 1.35" DENT HAS PREVIOUS REPAIR AND WILL NEED PERM REPAIR IN 150 HR IAW ECRA 5720-02391. REPAIRED LT OTBD L/E IAW REF SRM.
R2 DOOR SLIDE DECORATIVE COVER HAS A 14 INCH CRACK HORIZONTALLY IN OUTER LAYER 4 INCHES FROM BOTTOM. ALSO, HAS 4 INCH CRACK IN OUTER LAYER EXTENDING 4 INCHES VERTICALLY. VISUAL INSPECTION ACCOMPLISHED, NO ADDITIONAL DAMAGE. BUSTLE IS RIGID. INSTALLED ONE 841-0482 AND ONE 841-0483 PATCH TO INNER SURFACE AND RESIN COVERED WITH TAPE. DOOR BUSTLE. INSTALLED SECURELY AND WILL NOT INTERFERE WITH INTERNAL SLIDE OR OPERATION.
NO RADAR DISPLAY CAPT ND F-O IS WORKING FINE. WEATHER RADAR T-R UNIT PER MM.
BLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. NOISE QUIT WHEN SELECTED OVERRIDE. REMOVED AND REPLACED BLOWER FAN IAW AMM. OPS CHECK OKAY. OK TO CONTINUE.
CAPTAIN`S OXYGEN MASK COMPARTMENT DOOR UNHINGED. REPAIRED THE HINGE OPS CHECKED GOOD.
CREW REPORTS FLT CONTROL ELEVATOR SERVO FAULT: FOR NR 2 ELAC RESET. RESET ELACS CB'S AND PERFORMED EFCS TEST, ALL SYSTEMS NORMAL.
ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. CREW CYCLED B11 FAULT CLEARED. REPLACED ELAC 1 REF AMM. FAULT CLEARED. OPS TEST GOOD NO FAULTS.
EMERGENCY LIGHT TEST FAILED. FAULTS EPSU AFT LEFT BATTERY. REPLACED AFT EPSU BATTERY. EMERGENCY LIGHT TEST OPS. CHECKED NORMAL.
NR 3 RT FIXED COCKPIT WINDOW HAS HEAT DAMAGE AND IS CRACKED ALONG FWD EDGE MIDPOINT OF WINDOW. INSPECTED DEPT VERIFIED CRACK PER AMM, MIDDLE PLY CRACKED, PCN 110-3206, AOG R1897.
CIDS FAULTS, ESPU BATT FWD L, DURING EMERGENCY LIGHT TEST. REPLACED BATTERY AT DOOR 1L TEST NORMAL AS PER AMM.
COCKPIT DOOR STOPPER BROKEN. REPLACED DOOR ARRESTOR.
CREW REPORTED, 8DEF OXYGEN MASKS ARE DEPLOYED. MASKS REPACKED. OPS CHECK PER MM, OPS CHECK OK.
F/A REPORTS LOUD PRESSURE LEAK AT FWD JUMPSEAT, LOUDEST MIDWAY BETWEEN 1L AND 1R. FLT ATTD NOTICED A HUM AT 10,000 FT, WHEN SHE GOT THE 2 DINGS FROM FLT DECK, THAT ITS OK FOR HER TO GET UP. SITTING DOWN SHE COULD NOT HEAR THE HUM. HUM IS COMING FROM TOP OF A-C, BY 2000VU CB PNL. HUM WENT AWAY AS AIRCRAFT SPEEDED UP. SHE SAID, THAT IT WAS THE LOUDEST AT CTR OF A-C AND GOT LESS AS YOU WENT TO DOOR 1L AND 1R. IT DID NOT SOUND LIKE A DOOR LEAK. NUMBER ONE VHF ANTENNA GIVES HOWL FROM CF0315. NOISE NOTICEABLE BTWN 240-270 KNOTS 35,000FT. REPLACED THE NR 1 (TOP) VHF ANTENNA IAW AMM.
IN CRUISE LOUD HUMMING DEVELOPED IN CEILING ABOVE DOOR 1R. VIEWED ABOVE DUCTS AND FOUND NO OBSTRUCTIONS OR DETERIORATED DUCTING. RE-ATTACHED DUCTS. ACCMP'D CH2296, NOTHING FOUND. SEALANT ON UPPER GPS ANTENNAS DETERIORATED. REPLACED ANTENNAS AND RESEALED.
RAMP REPORTED SKID PLATE METAL UP IN AFT CARGO PIT. REPLACED DAMAGED SKID PLATE IN AFT CARGO PIT REF MT 53-016.
HUMMING-AIR NOISE FROM DOOR 1L. DOOR 1L FOUND FWD CORNER OF RUBSTRIP LOSE, REMOVED LOOSE SECTION AND TAPED PER MT. REPAIR RUB STRIP REF MT 52-0 32.P RESS A-C TO 5.1 DPSI NO AIR LEAKS NOTED AT DOOR 1L OR 2L, INSP ABOVE CEILING & E&E BAYS DEFECTS, NONE NOTED.
LOUD HUMMING IN DESCENT . SOUNDS LIKE IT IS COMING FROM ABOVE THE FRONT GALLEY IN MIDDLE. FOUND PRELOAD ON UPPER DOOR LOOSE AND TEFLON SEAL PEELING OFF, REPAIRED PER MT52-020 AND 52-10-00MM.
SAME SQUEAL NOISE IN FWD CABIN AT CRUISE. PRESSURIZED CABIN WITH CEILING PANELS DOWN, NO LEAKS NOTED. TURNED ON CHILLER AND STARTED CHECKING CART VALVES AND FOUND ONE CART VALVE ACCORDION SEAL MISSING FROM CHILLER INLET TO CARD MAKING NORMAL HIGH PITCH SOUND. REPLACED ACCORDION SEAL.
PRESSURIZATION ISSUE, RTFL. SKIN AIR VALVE FAULT ON ECAM, RETURNED TO FIELD. CFDS SHOW SKIN AIR OUTLET VALVE 22HQ. DETERMINED AN INTERMITTENT FAULT WITH THE OUTFLOW VALVE. REPLACED SKIN AIR OUTFLOW VALVE IAW MM. BITE TESTED OK.
F-CTL ELAC 2 PITCH FAULT. ELAC 2 PITCH FAULT DURING ENG RAN. REPLACED ELAC 2 COMPUTER, NO HELP (SEE PTT SEQ 9506001 FOR MR AND DASH INFO). SAMC TEXT: CHANGE PTA 565-9210 PER AMM 27-44-57. PFR & EFCS1 FAULTED PITCH TRIM ACT (THS) MOT1 9CE, RPLCD THS-MOT1 ELECT MODULE. RAN BOTH ENGS 5 MINUTES IDLE, OP CK'D GOOD, NO FAULTS. CAT-3 CHK ACPD -PASSED REF MM 22-97-00 & 22-96-00-501.
PICTURE MONITOR POOR PICTURE QUALITY AT 31A. CREW COMMENTS: PICTURE DIM (MONITOR INOP'D POS 31A). ADJUSTED MONTOR AT 31ABC. OPS NORMAL.
NR 2 ENGINE IGNITION SYSTEM 'A' INOPERATIVE. FOUND ARCING ON THE IGNITER PLUG AND LEAD, REPLACED LEAD, IGNITER PLUG AND EXCITER BOX, OP CHECK GOOD.
SEAT 7F ARMREST HAS SHARP EDGES. NEEDS TAPE JOB. MADE INTERIM REPAIR WITH TAPE ARM CAP COVER MISSING. REPLACED ARM REST.
F/O SLIDING WINDOW CRACKED. REPLACED F-O SLIDING WINDOW. ACP OPS TEST OF ANTI-ICING & DEFOGGING. OPS CHECKS GOOD.
RIGHT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. FOUND KNOTTED EIGHTH INCH DIA. STRING ENTANGLED IN AFT END OF GIRT BAR PREVENTING AFT END OF GIRT BAR FROM FULL ENGAGEMENT. REMOVED STRING. CYCLED ARMING LEVER THROUGH SEVERAL CYCLES. CHECKED GOOD. ECAM CONCURRED WITH ARMING LEVER. PRESSURIZED CABIN AND CHECKED FOR ARMING INDICATION ISSUES. ALL INDICATIONS NORMAL.
LIFE VESTS MISSING AT SEATS 11D, 19D & 22C. REPLACED MISSING LIFE VESTS AT SEATS 11D, 19D & 22C.
RIGHT OVERWING SLIDE BLOW OUT DOOR AFT FRAME AREA 2 CRACKED 6 INCHES. CARRIED FWD PER MT TO BE RECHECKED EVERY 3 SVC, CRACK WITHIN LIMITS 6 INCHES AT THIS TIME. ACP PER MT 25-018. CRACK IS WITHIN LIMITS AREA 2.
APU ON AT GATE, EXCESSIVE SMOKE OUT EXHAUST, FUEL PRESS REG LOW ON ECAM. APU OVERTEMP-AUTO SHUTDOWN. APU OFF, NO SMOKE OUT EXHAUST AFTER SHUTDOWN. NO SMOKE OR ODOR IN CABIN. APU SWITCH TO OFF, APU INLET DOOR VISUAL CHECKED CLOSED. REF: TSM 490000-810 & IAW TSK 921. R & R AS NEEDED & INCLUDED FINDINGS IN ACP W-U. REPLACED APU IAW AMM. OPS CHECKS GOOD NO LEAKS NOTED.
DURING O2 MASK DROP AT C4 VISIT ROWS 6, 8, 13, 15ABC-11 BC-17,19, 21, 23DEF AND LT FWD ATTENDANT DID NOT DROP AND BREAKERS HA 5,6 POPPED. REPAIRED AND OPS CHECKED THE SHORED TERMINAL AT TERMINAL BLOCK 7201VT, AFT CABIN, BLOCK 13 PIN WIRED-1346. OPS CHECKED GOOD.
CAPTAIN'S O2 MIC INOPERATIVE. REPLACED CAPTAIN'S OXYGEN MASK. OPS CHECKS NORMAL.
MAINTENANCE PROBLEM INCURRED. FLIGHT DIVERTED. NR 1 EPR BLUE ARC INDICATION FLUCTUATING. ALL OTHER ENGINE PARAMETERS NORMAL. REPLACED NR 1 EIU, NR 1 FWC, NR 1 LGCIU (P/N 664700500A4D - 274). ALL CHECK OK. ACCOMPLISHED AIRCRAFT TAXI CHECK, NO MESSAGES.
SMOKE LAVATORY DETECTOR FAULT. REPLACED LAV 'A' DETECTOR.
DOOR 2R, PER INBOARD CREW, OK ON GRD WHEN PRESSURIZED SLIDE ARMING HANDLE MOVES OUT APPROX ONE-HALF IN. RE-RIGGED DOOR ARMING LEVER. DOOR ARMS/DISARMS NORMALLY.
HARD CONT TEMP PACK 1 WILL NOT GO TO HIGH FLOW. OPERATED NR 1 PACK THROUGH ALL PARAMETERS AND GROUND CHECKS NORMAL. PACK WENT TO HIGH FLOW WITH NO DELAY OR MESSAGES.
CREW REPORT: IN FLIGHT, DOOR 2R SHOWS DISARMED ON DOORS PAGE. DOOR INDICATES ARMED AT DOOR. FOUND DOOR OUT OF ADJUSTMENT. PERFORMED DOOR ADJUSTMENT, ALL OPERATIONS ARE NORMAL.. NO REPEATS SINCE ORIGINAL.
BOTH FWD EMERGENCY FLASHLIGHTS DEAD. REPLACED BOTH BATTERIES. OPS CHECKED NORMAL.
EMERGENCY LIGHTS TEST FAILS PER 3SVC PAPERWORK. FAULTS EPSU EXT LOAD FWD L. ELECTRICAL SHORT INSIDE SLIDE 1L. REPLACED SLIDE PACK 1L, OPS CHECKED NORMALLY.
NR 1 ENGINE FIRE HANDLE HAS FOUR OUT OF EIGHT LIGHTS INOP. RELAMPED AND SWAPPED LGCIU AND ENG/APU FIRE IND PANEL.
LEFT MAIN LANDING GEAR, OUTER CYLINDER, FOUND CORROSION ON INNER SURFACE. REPLACED THE LT GEAR AND SENT UNIT TO SHOP FOR COMPLETE OVERHAUL.
GEAR HANDLE WOULD NOT GO UP AFTER TAKEOFF UNTIL ABOVE ABOUT 150 FEET. FOUND SENSOR 22GA OUT OF ADJUSTMENT/TOLERANCE. ADJUSTED SENSOR 22GA AND ADJUSTED UPPER TORQUE LINKS. FAC1 AND FAC2 WERE ALSO REPLACED AS PRECAUTIONARY. NO REPEATS,,
APU SMOKING UPON ARRIVAL INTO SFO AT GATE WITH OIL COMING OUT OF TAILPIPE. REPLACED APU. MANUFACTURER CHANGED EPOXY IN '06. UAL'S 1ST INCIDENT OCCURRED 12/23/06 AND HAS HAD 6 ADDITIONAL INCIDENTS SINCE. 4026 WAS THE 1ST SDR AND THE LAST OCCURRANCE. MANUFACTURER HAS SINCE ADDRESSED THE PROBLEM FOR ANY ESV'S AS OF 20070607. THE MTBF IS 2005 HRS, MCBF 2306. EP HAS REQUESTED A RESEARCH AS TO WHICH ENGINES HAVE THE OLD REPAIR METHOD APPLIED, CURRENTLY UNKNOWN.
ECAM MESSAGE SMOKE DETECTOR MESSAGE DOOR 1L FWD. SMOKE DETECTOR DIRTY. REMOVED, CLEANED AND REINSTALLED SMOKE DETECTOR IN FWD LAV A. OPS CHECK NORMAL.
LOW BOTTLE PRESSURE. *S/D* GAUGE LEAKING AT TEFLON TAPE. REMOVED GAUGE & INSTALLED NEW TEFLON TAPE. RETESTED & CHECKS OK.
CREW REPORTED DOOR 2R SLIDE BLOWN. REPLACED DOOR 2R SLIDE.
LT AFT MAIN ENTRY DOOR EVACUATION ESCAPE SLIDE GAUGE DISLODGED AND OUT OF VIEW CAN NOT VERIFY BOTTLE PRESSURE UNLESS COVERING IS REMOVED. REPLACED WITH SERVICEABLE EVACUATION ESCAPE SLIDE.
EEL AT 6C IS BROKE AND HANGING OUT. REPLACED EEL LIGHT ASSY, LIGHT OPS NORMAL.
EMERGENCY FLOOR LIGHT AT SEAT 15ABC INOP WHEN EMERGENCY LIGHTS COMMANDED ON. REPLACED SEAT 15ABC EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD.
CABIN LIGHTS STAYING ON BRIGHT AND EMERGENCY EXIT LIGHTS GOING ON AND OFF WITH THE DOUBLE CHIME. ACCOMPLISHED CFDS TEST ON NUMBER 1 AND 2 CPC WITH NO FAULTS. ALSO SWAPPED NUMBER 1 AND 2 CPC. ACCOMPLISHED CFDS TEST WITH NO FAULTS.
DOOR 1L SLIDE AFT LWR MOUNT BRACKET BROKEN. THE STEP BRACKETS OF SLIDE (LH & RH) ARE THE TWO BOTTOM ATTACHMENT POINTS THAT HOLD THE SLIDE ASSEMBLY ONTO THE AIRCRAFT DOOR. THESE PARTS ARE STICKING OUT OF THE WHOLE ASSEMBLY AND ARE LIABLE TO DAMAGE ESPECIALLY DURING TRANSPORTATION AND HANDLING. WHEN THE ASSEMBLY IS DROPPED ACCIDENTALLY THE BRACKETS ARE THE IMPACT POINTS. BRACKETS ARE ROUTINELY REPLACED WHEN FOUND BROKEN IN THE SHOP.
STRINGER 7L WAS DENTED JUST FORWARD OF FRAME 7. MAJOR REPAIRED ACCOMPLISHED. REPLACED STRINGER.
CREW REPORTS NOISE-VIBRATION-DRONING IN FORWARD CABIN COCKPIT AREA. NOISE REDUCED UPON REACHING CRUISE ALTITUDE. VIBRATION COULD BE FELT IN COCKPIT FLOOR. GROUND ELECTRICAL CONNECTION DOOR VERY LOOSE. ADJUSTED LATCH DOOR.
BLUE SYSTEM HYDRAULIC LOW PRESSURE ELECTRIC CENTRALIZED AIRCRAFT MONITORING MESSAGE. *S/D* FINAL FIX WAS A RETERMINATION OF THE WIRES CONNECTING TO THE PUMP PUSHBUTTON SWITCH IN THE COCKPIT. ALL OTHER WIRING CHECKS WERE COMPLETED WITHOUT FINDINGS.
EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. *S/D* AFT CHARGER AND BATTERY WERE REPLACED. (P/N 11-0049) CHARGER, BATTERY (P/N 3214-30). AIRCRAFT HAS BEEN GOOD SINCE REPLACEMENTS.