N467UA
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
Maintenance disclosures
LEFT AFT EPSU IS FAULTING DURING EMERGENCY LIGHT TEST. R & R EPSU BOX PER AMM33-51-38, OPS CHECKED GOOD.
EXCESSIVE SMOKE COMING FROM NR 1 ENG. APON SHUTDOWN WITH A STRONG SMELL OF OIL. MOTORED NR1 ENG. SMOKE AND OIL SMELL STILL PRESENT AFTER MOTORING SHUTDOWN. RAN ENGINE NR 1 PER AMM 71-00-00-710-043-A FOR 15 MINS. ENGINE OPERATED WITHIN NORMAL PARAMETERS. NO EXCESSIVE SMOKE OR OIL SMELLS UPON ENGINE SHUTDOWN.
WHILE WORKING JOB CARD 18-3351-1-0003 FOUND EPSU EMERGENCY BATTERY LEFT FAULT. REMOVED AND REPLACE EPSU BATTTERY LEFT WITH SERVICEABLE FROM STOCK. REF AIPC 33-51-38-01B. OPS CHECK GOOD.
SURVEY OF THE LT INSP AREA SHOWS EVIDENCE OF A PREVIOUS REPAIR. PERFORMED REPAIR PER PART 1 INTERIM REPAIR IAW EC/RA 5330-07609 AND REO-L25569 REV IR WITH NO DEVIATIONS.
RIGHT WING FUEL PANEL LANDING 604JB HAS 2EA HOLES OUT OF ROUND. REPAIRED 2 EA HOLES AT RT WING FUEL PANEL LANDING 640JB IAW A32 0 SRM 51-21-11-300-002 AND REO L2559B EC/RA 5721-01516 CAT A.
LEFT WINDSHIELD FWD NODE, MOST INBD HOLE FROM CENTER LINE HAS A CRACK INDICATION AT THE 6:O CLOCK POSITION 100% SH. PERFORMED REPAIR IAW PART 1 INTERIM REPAIR IAW EC/RA 5311-03390 AND REO-L25578 REV IR WITH NO DEVIATIONS
RH AFT EMERGENCY HATCH INTERNAL STRUCTURE, ABOVE WINDOW, HAS 2 G OUGES WITH EVIDENCE OF CORROSION. REMOVED & REPLACED BEAM SUPPORT AT R/H AFT EMERGENCY HATCH INTER NAL/STRUCTURE IAW A320 SRM 51-72-11 & 51-42-11.
LEFT WINDSHIELD LOWER NODE AREA, CONTINUITY FITTING CRACKED AT AFT FACE OF HORIZONTAL FLANGE, AFT OF INBD FASTENER. LEFT WINDSHIELD LOWER NODE AREA, CONTINUITY FITTING CRACKED AT AFT FACE OF HORIZONTAL FLANGE, AFT OF INBD FASTENER. R & R CONTINUITY FITTING PER EA 5310-07675 OP 004.
L1 DOOR SILL IS CORRRODED AT UPPER ATTACH HOLES FOR SCUFF PLATE CENTER SHAPE SILL. R & R CORRODED L1 DOOR SILL AS REQUIRED IAW SRM 51- 72-11-911-001.
LEFT AFT EMERGENCY HATCH INTERNAL STRUCTURE ABOVE WINDOW HAS 2 GOUGES WITH EVIDENCE OF CORROSION. REMOVED AND REPLACED L/H AFT EMERGENCY HATCH BEAM SUPPORT IAW A320 SRM 51-42-11.
LH FWD EMERGENCY EXIT HATCH UPPER HORIZONTAL BEAM HAS 2 NOTCHES AND GOUGES FROM CHAFING ON LINER FASTENERS. REMOVED AND REPLACED L/H FWD EMERGENCY HATCH SUPPORT BEAM IAW A320 SRM 51-42-11.
AFT LH EMERGENCY HATCH INTERNAL STRUCTURE HAS CORROSION AT THE SECOND FROM THE BOTTOM SUPPORT STRUCTURE. R & R SUPPORT BEAM AT AFT L/H EMERGENCY HATCH IAW A320 SRM 51-42-11.
RIGHT FWD EMERGENCY HATCH INTERNAL STRUCTURE ABOVE WINDOW HAS 2 GOUGES WITH EVIDENCE OF CORROSION. R AND R BEAM SUPPORT AT RH FWD EMERGENCY HATCH INTERNAL STRUCTURE IAW A320 SRM 51-72-11.
CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS. LEFT WINDSHIELD FWD NODE, MOST INBD HOLE FROM CENTER LINE HAS A CRACK INDICATION AT THE 6:O CLOCK POSITION 100% SH. PERFORM REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 5,600 FLIGHT CYCLES CURRENT HOURS 74772:19 FLIGHT CYCLES 32837.
AFT CARGO FRAME SHEAR TIE AT FR 62 BETWEEN STRINGER 42L AND 43L HAS CORROSION. REMOVED AFT CARGO FRAME SHEAR TIE FR 62 STR 42L & 43L. FABRICATED AND INSTALLED NEW SHEAR TIE AS REQUIRED IAW SRM 51-72-11-911-00 1.
SEAT TRACK Y765 FR 25-35 HAS CORROSION. PERFORMED REPAIR ON SEAT TRACK Y765, FR 25-35 IAW SRM 53-21- 15-300-004.
Y1292 HAS CORROSION FR12-24. SEAT TRACK AT Y1292 FR12-24 FOUND TO BE OUT OF LIMITS WITH A DEP TH OF .041" AND A MAX ALLOWED DEPTH OF .031" IAW A320 SRM 53-11- 14-283-007 REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-11 -911-001 AND SRM 51-42-11.
Y503.2 HAS CORROSION FR12-16. EVALUATED BEAM Y503.2 FOUND TO BE OUT OF LIMITS IAW SRM 53- 11-14-283-001, REMOVED AND REPLACED Y503.2 AS REQUIRED IAW A 320 SRM 51-42-11/001.
-Y1292 HAS CORROSION JUST FWD OF FR 20. EVALUATED FOUND OUT OF LIMITS IAW SRM 53-11-15-283-011 REMOVED A ND REPLACED -Y1292 FR12-FR24 IAW SRM 51-42-11/001.
AFT PIT CORROSION AT 38R PROFILE FR 52. REMOVED AND REPLACED CORRODED PROFILE PANEL AT FR43-FR52A IAW SRM 51-72-11.
FLOOR SUPPORT AT Y765 HAS CORROSION FR12-24. REMOVED AND REPLACED FLOOR SUPPORT Y765 AT FR 12-24 IAW A320 SRM 51 -72-11.
SEAT TRACK AT FR47-FR52 Y1292 MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED SEAT TRACK Y1292 AT FR 47-FR52, INSTALLED SPLICE REPAIR AS REQUIRED IAW A320 SRM 53-41-15-300-003.
LEFT ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 131 IN CHES FROM IB EDGE AND 15 INCHES FROM AFT EDGE, I INCH DIA. REPAIRED L/H ELEVATOR UPPER SURFACE 131IN FROM I/B 15IN FROM T/E 1.38IN DIA ZONE A IAW A320 SRM 55-21-11-300-004 CATEGORY A REPAIR.
AFT CARGO BILGE AREA BETWEEN FR 63 & 64 STRINGER 41R HAS CORROSI ON. REMOVED AND REPLACED STRINGER 41R FR59-61 IAW SRM 51-72-11.
AFT PIT AT FRAME 59RT UNDER STRINGER 41RT WEDGE IS CRACKED. REMOVED AND REPLACED WEDGE IN AFT CARGO PIT FR59RT AT STRINGER 4 1 IAW A320 SRM 51-72-11.
LEFT ELEVATOR NR 4 HINGE HAS A BROKEN TAB. REPAIRED LT ELEVATOR NR 4 HINGE LUG FITTING IAW SRM 55-26-41- 300-002.
R/H ELEVATOR INBD ACTUATOR FITTING LOCKING LUG GOUGED. REPAIRED RH ELEVATOR I/B ACTUATOR FITTING LOCKING LUG IAW A320 S RM 55-26-47-300-001 THIS REPAIR IS CATEGORY A NO FURTHER ACTION REQUIRED.
CABIN FLOOR STRUCTURE L/H SEAT TRACK Y254 CORRODED AT FRS 21, 22 , 23. REMOVED AND REPLACED SEAT TRACK Y254 FR 12-24 LH IAW A320 SRM 51 -72-11-911-001 AND SRM 51-42-11 ACMP BY MECH V937285 INSP BY V89 2429
SEAT TRACK AT FR58 Y765 UPPER FLANGE CROWN GOUGED. REMOVED SEAT TRACK FR58-FR64 Y765 IAW A320 SRM 53-41-15-300-003 REV 154 REPLACED SEAT TRACK FR58-FR64 Y765 IAW A320 SRM 53-41-15 -300-003 REV 154.
FWD CARGO COMPT, FRAME 28 STR33 LH TO 33 RH FLOOR PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR28 STR33 LH TO 33 RH IAW A320 SRM 51-42-11.
AFT CABIN WET AREA FLOOR BEAM Y765 FR 66-70 L/H HAS CORROSION. REMOVED CORRODED FLOOR BEAM AND REPLACED WITH NEW FLOOR BEAM AT Y765 FR 66-70 LH IAW A320 SRM 51-42-11/001.
EXTERNAL RT FUSELAGE FAIRING OUTER VERTICAL SUPPORT AT FR 34 IS CRACKED. REMOVED AND REPLACED FR 34 VERTICAL ANGLE IAW SRM 51-42-11 P 18-25.
R/H WET AREA SEAT TRACK -1292 AT FR64-66 IS CORRODED. REMOVED SEAT TRACK, -1292 FR 64-66 IAW A320 SRM 51-42-11/0 01 REV 154 REPLACED BEAM-SEAT TRACK -1292 FR64-66 IAW A320 SRM 5 1-42-11/001 REV 154
MAIN CABIN AFT WET AREA FLOOR SUPPORT AT FR 68-69 LT Y1292 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM TASK 51-72-11-911-001.
CABIN FLOOR AFT WET AREA AT FR68-70 L/H FLOOR SUPPORT Y254 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-11/001, REV 154.
AFT CABIN WET AREA FLOOR SUPPORT -Y765 RT FR 66-70 SHOWS EVIDENCE OF CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-42-11/001, REV 154.
SHEAR PLATE AT L/H FR69-70 WET AREA HAS SHEARED FASTENERS & POSS IBLE CORROSION. REMOVED AND REPLACED SHEAR PLATE AT LH FR 69-70 WET AREA IAW A32 0 SRM TASK 51-72-11-911-001.
AFT CABIN WET AREA FLOOR BEAM -Y1292 R/H BETWEEN FR68-69 HAS EVI DENCE OF CORROSION. REMOVED AND REPLACED FLOOR BEAM RT - Y1292 RH FR68-69 IAW A320 S RM 51-72-11-911-001.
AFT MAIN CABIN R2 DOOR SILL HAS CORROSION. REPAIRED AFT MAIN CABIN R2 DOOR SILL IAW A320 SRM 53-41-14-300-0 01. CAT A.
WATER CONTINUOUSLY LEAKING FROM FORWARD GALLEY WITH VERY STRONG ODOR. FORWARD GALLEY WATER FAUCET ADJUSTED AND WATER LEAK STOP AND DRAIN WATER FROM SYSTEM DRAIN TWICE AND REFILLED FOT ODOR MM 12-15-38-613-001-A
LAV SMOKE DETECT ACTIVE ON ALL 3 LAVS NO SMOKE OR FIRE INDICATIN S UPON OPS CHECK OF THE LAV SMOKE DETECTORS. FOUND AURUAL AND LIGHT INDICATORS NOT INDICATING WITH TEST. REMOVED AND REPLACED SDCU REF 26-17-34. OPS CHECK GOOD. PARTS USED: 31-2610-9-0001,QTY :1 ADD EMP:412895 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1662349 SN OFF 5476 UNIT, SMOKE DET OFF 31-2610-9-0001 5476 ON 31-2610-9-0001 5228
PDA 2 REF LP 9465269 - FUEL CAP FOUND MISSING AT DFW ENTERED INTO HISTORY FOR SDR ON WALK AROUND FOUND FUEL CAP MISSING. REQUEST CDL REFERENCE # 28 A. NO PARTS AVALIBLE..DFW. COMPLIED WITH CDL 28A. OKAY TO DEFER MISSING FUEL CAP PER CDL 28A CAP, COUPLING R OFF 31-2825-9-0001 0333 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 0333 ON 31-2825-9-0001 0307 R&R FUEL CAP AND LANYARD IAW AMM 28-25-41-000-001-A OPS CHECK GOOD OK FOR SERVICE PARTS USED: 31-2825-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1513314 SN OFF 0333
REJECTED TAKEOFF APPX 95 KTS AIRCRAFT PULLED HARD LEFT. DEBRIEFED CREW. CREW STATES BRAKES WERE NOT DRAGGING. WIND AT TIME OF TAKEOFF WAS 9 KTS. ALL INDICATIONS WERE NORMAL AND NO FAULT MESSAGES DISPLAYED. CREW STATED IT FELT LIKE ENGINE FAILURE. UPON MX ARRIVAL OF AC CYCLED BRAKES TO VERIFY ALL MAIN GEARS JACKED AND TIRES ROTARED. NO BRAKE DRAGGING NOTED ON EITHER GEAR. NO DISCREPENCES NOTED FROM VUSUAL INSPECTION OF BRAKE UNITS. PERFORMED HIGH SPEED TAXI, CONFIRMED AIRCRAFT PULLING TO THE LEFT AFTER 40KTS. PERFORMED TSM STEERING DEVIATION DURING TAXI REF TSM 32-51-00-810-823-A, FOUND N/WS SERVO VALVE FAILING ON CHANNEL 2, REMOVED AND REPLACED N/WS STEERING SERVOVALVE REF AMM BRAKES WORKING PROPERLY. NO DEFECTS NOTED. CYCLED RUDDER AND NO DEFECTS NOTED. FURTHER TROUBLESHOOTING REQUIRED 32-51-51-400-001-A, PERFORMED FUNTIONAL CHECK REF 32-51-00-720-003-A, TEST PASS. NO LEAKS NOTED. PERFORMED HIGH SPEED TAXI UP TO 65KTS, OPS CHECK GOOD NO PULL TO THE LEFT.
INSPECT (GENERAL VISUAL) ENTRY DOOR LININGS, SLIDE BUSTLES, AND SURROUNDING CLOSEOUT TRIM AND SEAL FOR: {A3NB-25-3-6025} - CRACKED L2 DOOR HINGE COVER DECORATIVE ITEM, NO HAZARD FOR PASSENGERS, PLACED UNDER INTERIOR PROGRAM PER GMM 05-30-06
ACFT ARRIVED WITH NO FUEL CAP NOTIFIED TOMC. INSPECT (GENERAL VISUAL) FUEL TANKS FOR: {A3NB-28-3-6004} - AIRCRAFT ARIVED MISSING FUEL CAP. CAP REQUIRED 31-2825-9-0001 NOT AVALIBLE IN SAN. REQUEST TO APPLY MEL 28A VERIFIED TO LEAKAGE FROM CONNECTOR WITH CAP MISSING. CDL APPROVED . INSTALLED NEW FUEL CAP. CAP, COUPLING R OFF 31-2825-9-0001 8384 ON 31-2825-9-0001 2472. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1660484 SN OFF 8384
DAMAGE FOUND ON OUTSIDEOF DOOR 1R AT THE LOWER AREA. SHEETMETAL R IPPED OFF OF DOOR. LOCKING FOR FERRY FLT. LOG PAGE UNLOCKED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN POSSIBLE REPAIR SRM 52-10-00-300-003. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INVESTIGATE PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. LOCAL FBO TO DAMAGE, SEND PHOTO. EVAL DAMAGE AND SEND PICS TO TOMC. CONFIRMED MATERIAL ID FOR NOTED DAMAGE IS WHAT IS CALLED OUT IN VERIFIED PARTS ARE FABRICATED AS PER NOTED SRM. OK TO CONTINUE VERIFIED REPAIR PARTS HAVE BEEN TREATED AND PRIMED.OK TO VERIFIED DVI INSPCTION, NO FURTHER DAMAGE NOTED OTHER THAN ON OK TO INSTALL DOUBLER & FILLER 320SRM 52-10-00-300-003, DOUBLER PO#2008330 (0.125")AND SHIM REPAIR. CONTINUE REPAIR. LWR PLATE AT BEAM #1. PO#2674362 (0.100") REMOVED DAMAGE PER SRM 52-10-00 FIGURE 1. VERIFIED MATERIALS FOR REPAIR AS PER A 320 SRM 52-10-00-300-003 FABRICATED PARTS REFERENCE A320 SRM 52? 10?00?300? 003 OK TO FABRICATED PARTS REFERENCE A320 SRM 52-10-00-300-003 OK TO TREAT FABRICATED PARTS REFERENCE A320 SRM 52-10-00-300-003 OK TO TREAT TREATED AND PRIMED PARTS AND AREA PER REFERENCE A320 SRM TREATED AND PRIMED PARTS AND AREA PER REFERENCE A320 SRM UPON LOOKING AT REPAIR AREA ON R-1 DOOR TO PREP FOR NDT, A PERFORMED DVI AS PER 51-27-11-911-011 STEP 2 A (2) AFTER REMOVAL REQUEST OK TO INSTALL REPAIR DOUBLER AND FILLER REF SRM REQUEST OK TO INSTALL REPAIR DOUBLER AND FILLER REF SRM REQUEST OK TO IN
FLT/CONTRL SPOILERFAULT ON DEPARTURERIGHT INBOARD 1 REMAINEDEXTE NDED..RTB COMPLIED WITH MEL, SPOILER 1 RIGHT SIDE LOCKED OUT, PER MEL. PK PER TOMC ADD EMP:U116706,U167027 DISPATCH DESK: 23 NAME: VS DATE: 13-JUN-22- 2764A APPROVED. TROUBLE SHOT REF FIM 27-60-00-810-814.REPLACED SEC 3 FIN 1CE3 REF AMM 27-94-34. FAULT CONTINUED. SO REPLACED #1 SPOILER SERVO VALE FIN 31CE2. REF AMM 27-94-00. OPS GOOD. ADD EMP:U118140 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1008865 SN OFF 6318 TT # 1228546 SN OFF 1099 IPC REFERENCE # 27-94-00 COMPUTER, SPOIL OFF 31-2794-9-0001 6318 ON 31-2794-9-0001 5115 VALVE, SERVOVAL OFF 31-2763-9-9002 1099 ON 31-2763-9-9002 2501
PDA 3 REF LP7766813 FUEL CAP LANYARD MISSING. PDA 3 NOTED REF LP 7766813 FOR CDL APPLIED.
PDA 3 FOUND 1 SCREW MISSING RIGHT WING PANEL 674BB TOMC BROADSTONE NOTIFIED. PICTURE ADDED ADDED 2 MORE PICTURES, MISSING SCREW NUTPLATE STRIPPED BUT BEHIND WALL. REPLACED SCREW AS REQ REF IPC 57-51-05-34M OK TO CONTINUE
FOUND R/H FR68, DOOR STOP FITTING #1, LOWER I/B HOLE CRACKED IN AREA 2 DURING THE ACCOMPLISHMENT OF EA5340-01724 OPS 002, REV C. REF PEMCO NR.10814.0244 OVERSIZED THE #1 DOOR STOP FITTING LWR I/B HOLE D1 AT R/H FR68 CONCENTRICALLY TO .3890(AREA 2), OVERSIZED HOLE D1 ECCENTRICALLY TO .4970, HOLE D1=.4970(12.62MM), FABBED FREEZE PLUG & INSTALLED REPAIR PART R5342079920101, ACCOMP''D REPAIR OF FR68 R/H #1 DOOR STOP IAW A320 SRM 53-41-12-300-008 AND SRM 53-41-12-300-011. REPAIR REQ''S HFEC RELEVANT FOR EITHER INSPECTION REQUIREMENT PER SRI SUBSEQUENT INSP AT 5800FC INTERVALS, FLIGHT HOURS NOT INSP AT THRESHOLD OF 19500FC FROM REPAIR EMBODIMENT, 53-41-12-205-010 FIGURE 001, TABLE 006, SHT 7 DIP 53-DIP NEEDS UPDATE FOR D2 DIMENSION AND REPAIR PART SRM 53-41-12-300-011, FIGURE 8. PN# R5342079920101, M&E# 31-5341-3-0041, SPLICE, FR68,RH WAS INSTALLED DUE TO REWORK AND BUSH OF HOLE D1, HOLE D1 BUSH DRILLED AND REAMED TO .281 FINAL SIZE HOLE D2 =.281, HOLE D3 = .281, HOLE D4 = .281 D1 ECCENTRICALLY TO .4970, HOLE D1=.4970(12.62MM), R/H FR68 CONCENTRICALLY TO .3890(AREA 2), OVERSIZED HOLE OVERSIZED THE #1 DOOR STOP FITTING LWR I/B HOLE D1 AT FABBED FREEZE PLUG & INSTALLED REPAIR PART R5342079920101, ACCOMP''D REPAIR OF FR68 R/H #1 DOOR STOP IAW A320 SRM 53-41-12-300-008 AND SRM 53-41-12-300-011. REPAIR REQ''S HFEC RELEVANT FOR EITHER INSPECTION REQUIREMENT PER SRI SUBSEQUENT INSP AT 5800FC INTERVALS, FLIGHT HOURS NOT INSP AT THRESHOLD OF 19500FC FROM REPAIR EMBODIMENT, 53-41
AFT CARGO STR 41R CORRODED FROM 61.5-58 REMOVED DAMAGED SECTION OF STR 41R FR 56-FR61 IAW A320 SRM 53-00 -13-300-002. FABRICATED AND INSTALLED REPAIR COMPONENTS/PARTS IA W A320 SRM 53-00-13-300-002 AND 51-72-11-911-002 ADD EMP:V890622
A3NB-05-3-6023, A27-048, FR61 FLOOR SUPPORT BEAM BENT FROM STR 3 8L TO 44 REMOVED FLOOR BEAM SUPPORT IAW A320 SRM 51-72-11-911-001, FABRIC ATED NEW SUPPORT PER MFG DRAWING NO. 17D53470382. HEAT TREATED I AW A320 SRM 51-25-00-801. HARNESS TESTED IAW A320 SRM 51-28-11-9 11-004. INSTALLED NEW BEAM SUPPORT FR61 STR 38L-44 IAW A320 SRM 51-72-11-911-001 ADD EMP:V890622
A3NB-05-3-6023, A27-052, AFT CARGO FR60 CLEAT CORRODED STR 44-41 L QTY 3 CLEATS CORRODED. REMOVED 3 CLEATS FR60 STR 44-41L. (2) CLEATS FR60 STR 44-42L WER E CORRODED. (1) CLEAT 42L-41L DAMAGE LIMITED TO SURFACE PROTECTI ON ONLY. IAW SRM A320 51-42-11-801, IAW SRM A320 51-75-12-911-00 1, AND IAW AIRBUS NTM 51-90-00. FABRICATED, HEAT TREATED AND INS TALLED (2) CLEATS FR60 STR 44-42L ADD EMP:V925673 NITED ER 5100R01017 REV F EATS, FASTENERS AND SKIN IAW SRM A320 51-75-12-911-001 AND IAW U IAW SRM A320 51-72-11-911-002. RESTORED SURFACE PROTECTION TO CL -28-11-911-004 AND IAW NTM 51-10-17.INSTALLED (1) CLEAT 42L-41L IAW AIRBUS DWG 17D534 70854 AND REF NO. ABS5044. IAW SRM A320 51
SKIN HAS CORROSION UNDER BONDING STRAPS AT FR69.5 STR 2L-1L. REPAIRED CORROSION ON SKIN UNDER BONDING STRAPS AT FR69.5 STGR 1-2L IAW ECRA 5341-01181 REV A. CREATE A DTA DIP LOG PAGE TO REA D "ACCOMPLISH THE PERMANENT REPAIR AT FUSELAGE SKIN FR66-70... ..STR 3L-3R AS PER PART 3 OF ECRA 5341-01181 ON OR BEFORE THE AIRCRAFT REACHES 89400 TOTAL FLIGHT CYCLES. CONTACT ENGINEERING AFTER 87000 TOTAL AIRCRAFT FLIGHT CYCLES BUT PRIOR TO 88000 ... ON CRITERIA FROM AIRBUS. WORK PERFORMED ON AAR DLH L/P 9820729. ..TOTAL AIRCRAFT FLIGHT CYCLES IN ORDER TO OBTAIN FINAL INSPECTI DIP 53-DIP ECRA IS FOR STR3LH-3RH. WRITE UP STATES STR2L-1L. INTERIM REPAIR ACCOMPLISHED PER PART 1 OF ECRA 5341-01181 REV A. APPROVED FOR CARRY TO ACP PERMANENT REPAIR PER PART 3 OF ECRA 5341-01181 ON OR BEFORE 89400 FC. CONTACT EG AFTER 87000 FC, BUT PRIOR TO 88000 FC
SKIN HAS CORROSION UNDER BONDING STRAPS AT FR 69.5 STGR 1R-2R. REPAIRED CORROSION ON SKIN UNDER BONDING STARPS AT FR 69.5 STGR 1-2R IAW ECRA 5341-01181 REV. A. CREATED A DTA DIP LOG PAGE TO R EAD "ACCOMPLISH THE PERMANENT REPAIR AT THE FUSELAGE SKIN FR66.. ..-70 STR 3L-3R AS PER PART 3 OF ECRA 5341-01181 ON OR BEFORE THE AIRCRAFT REACHES 89400 TOTAL AIRCRAFT FLIGHT CYCLES. CONTACT ENGINEERING AFTER 87000 TOTAL AIRCRAFT FLIGHT CYCLES, BUT ... L/P 9821067. FINAL INSPECTION CRITERIA FROM AIRBUS. WORK PERFORMED ON AAR DLH ..PRIOR TO 88000 TOTAL AIRCRAFT FLIGHT CYCLES IN ORDER TO OBTAIN DIP 53-DIP ECRA IS FOR STR3LH-3RH, WRITE STATES STR1R-2R. INTERIM REPAIR ACCOMPLISHED PER PART 1 OF ECRA 5341-01178. APPROVED FOR CARRY TO ACP PERMANENT REPAIR PER PART 3 OF ECRA 5341-01181 ON OR BEFORE 89400 FC. CONTACT EG AFTER 87000 FC, BUT PRIOR TO 88000 FC TO OBTAIN FINAL CRITERIA FROM AIRBUS. CORRECTED SOURCE REF. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC QC REVIEW RECORDS UPDATE....TW INIT: PLN/ENG >87,000<88,000 TAFC T/A: 89,400 TAFC....TW
AFT CARGO FR61 CLEAT CORRODED STR 44-43 R REMOVED CORRODED CLEAT AND REPLACED CLEAT(NEW) AFT CARGO FR61 ST R 44-43R IAW SRM A320 51-42-11-80100. RESTORED SURFACE PROTECTIO N TO CLEAT AND RIVETS FR61 STR 44-43R IAW SRM A320 51-75-12-911- 001 AND IAW ER 5100R01017 REV F.
SEVERAL FUZZY FASTENER HEADS AT FR 67-69.5 STR 3L-3R. REPLACED DAMAGED FASTENERS AND REPAIRED CORROSION FOUND UNDER FA STENERS IAW ECRA 5341-01181 REV-A. CREATE DIP TO READ ACCOMPLISH THE PERMANENT REPAIR AT THE FUSELAGE SKIN FR66-70 STR 3L-3R.. ..AS PER PART 3 OF ECRA 5341-01181 ON OR BEFORE THE AIRCRAFT REA CHES 89400TOTAL AIRCRAFT FLIGHT CYCLES. CONTACT ENGINEERING AFTE R 87000 TOTAL AIRCRAFT FLIGHT CYCLES BUT PRIOR TO 88000 TOTAL .. TERIA FROM AIRBUS. WORK PERFORMED ON AAR DLH L/P 9820732. ..AIRCRAFT FLIGHT CYCLES IN ORDER TO OBTAIN FINAL INSPECTION CRI DIP 53-DIP ECRA STATES FR66-70, WRITE UP STATES FR 67-69.5. ADD STATEMENT "ACP''D INTERIM REPAIR PER PART 1 OF ECRA...." INTERIM REPAIR WAS ACCOMPLISHED PER PART 1 OF ECRA 5341-01181 REV A. APPROVED FOR CARRY TO ACP PERMANANENT REPAIR, TO BE DETERMINED, BY EG PER PART 3 OF ECR
AFT CARGO STR 40L C ORREDED FROM FR 59-56 REMOVED AND REPLACED STR 40L FR53 TO FR60 IAW A320 SRM 51-72-11 AND A320 SRM 51-42-11. RE-INSTALLED CLEATS AT STR 40L TO FR60 IA W SRM 51-72-11 AND A320 SRM 51-42-11. PRIMED AND TOPCOATED IAW A 320 SRM 51-75-12-911-001 AND ER5100R01017.
AFT CARGO STR 43L CORRODED FROM FR60-58 REMOVED AND REPLACED STR 43L FR 54 TO FR60 IAW A320 SRM 51-72-11 -911-001 AND A320 SRM 51-42-11-001. REINSTALLED CLEATS STR 43L-4 2L FR54-FR60 IAW A320 SRM 51-72-11-911-001 AND A320-SRM 51-42-11 -001. PRIMED AND TOP COATED IAW A320 SRM 51-75-12-911 AND ER5100 R01017 REV. F.
CRACK INDICATIONS NOTED OUTSIDE THE CUTOUT AREA AT FR35 LT SIDE, HOLES 3, 4 & 20. REPAIRED THE PRESSURE PANEL HOLES IAW ECRA 5331-02417 REV. A,
FOUND EPSU 11WL BAD. REPLACED EPSU IAW AMM 33-51-38-400-001A. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1103608 SN OFF 2897 POWER SUPPLY, C OFF 31-3350-9-9001 2897 ON 31-3350-9-9001 5406 PART UPDATE ONLY ROTABLE PARTS CHANGE WAS INDICATED - TT # 1810908 SN OFF 8316
R1 DOOR EMERGENCY SLIDE CASE CRACKED. PROCURED NEW DOOR SLIDE RI DOOR TO BE INSTALLED ON CARD NR 18-2 562-1-2307/2067.
LT OFF WING SLIDE CONTAINER DELAM AND CRACKED. REMOVED AND REPLACED LT OFF WING SLIDE CONTAINER.
RT OFF WING SLIDE CONTAINER DELAM AND CRACKED. REMOVED AND REPLACED RT OFF WING SLIDE CONTAINER.
R2 DOOR SILL HAS CORROSION AROUND FASTENERS HOLES 5 FWD OF FR68. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001.
L2 DOOR SILL HAS CORROSION AROUND FASTENER HOLE AT FR68. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11-001.
AFT CABIN SHEAR WEB SUPPORT CORRODED JUST FWD OF FRAME 70. REMOVED AND REPLACED THE SHEAR WEB SUPPORT IAW SRM 51-42-11-001, PAR F4, & F2.
EMERGENCY LIGHT TEST FAILS. REPLACED BATTERY AND POWER SUPPLY IAW AMM 33-51-38, REF AMM 33-5 1-39. LIGHTS FUNCTIONED NORMAL.
EMERGENCY LIGHT TEST FAILURE. EPSU BATTERY EMER RT. ACCOMPLISHED TSM TASK 33- 51-00-810-801-A. REPLACED EPSU BATTERY 12WL IAW AMM TASK 33-51-3 8.
2 SERVICE EMER LIGHT TEST FAILED. REPLACED 12WL EPSU & BATTERY IAW MM 33-51-38.
DAMAGE TO ACFT, BELOW AFT LOWER CORNER OF DOOR 2L. DAMAGE IS APPROX 9 INCHES LONG & 2 INCHES WIDE BURNISH AREA IAW SRM 53-41 -11. WILL REQUIRE REPETITIVE INSPECTION IAW SR I53-41-11, TABLE 10 4, BLOCK SSI53-41-31. MUST BE ACCOMPLISHED WITHIN 23,800 FC OR 47,600 FH WHICHEVER COMES FIRST.
INITIAL APU START WAS SLOW WITH LP FUEL VLV FAULT, FAULT CLEARED. DUCT PRESS RECOVERED, ENG STARTS NORMAL, SYS RECOVERED. OPERATIONS NORMAL, OK TO CONTINUE.
AFT CARGO HEAT TEMP ONLY 58F WITH TEMP SEL ON FULL HOT. NO ECAM MSGS OR AMBER IND. REPLACED PRESS REG VLV & TRIM AIR VLV.
ANTI EROSION TAPE IS COMING OFF IN 4 PLACES ON VERTICAL TAIL. TRIMMED LOOSE EROSION TAPE IAW MT 55-003.
G RESERVOIR LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN, HYD. LOSS OF ALL GREEN FLUID. PTU & GREEN HYD PUMP COMMANDED OFF WITHIN 30 SECONDS OF ECAM INSTRUCTIONS. REPLACED LEAKING LINE.
RAMP REPORTED LOOSE FASTENER ON LT VERTICAL STABILIZER. SECURED FASTENER.
F-CTL ELAC 2 FAULT. ELAC 2 SHOWED AS WARNING ON AIRMAN-WEB WITH ELAC 2 FAILURE MESSAGE, RESET NO HELP. SWAPPED NR 1 AND NR 2 ELAC COMPUTERS AND FAULT FOLLOWED, NR 2 TEST OK. NR 1 ELAC NOW INOP AND COMPLIED WITH MEL 2793A.
FWD F/A OXYGEN MASK COMPARTMENT DOOR OPENED ON TAXI OUT AND MASKS HANGING DOWN. ACCOMPLISHED SAT. MASK DROP TEST IAW MM 35-23-00-710-001-A. OPS CHECKED OK.
OXYGEN MASKS DROPPED ROW 7DEF. REPACKED MASKS IAW AMM. PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM, OPS CHECKED GOOD.
MULTIPLE ECAM FAULTS AFTER A-C ARRIVAL. SWINGS REPORTED FAULTS OCCURED DURING POWER SWAP? ECAM FAULTS. LG CUI 2, REVERSER 2, MAIN GALLEY SHED, MAINT MESSAGE ENG 2 EIU, OVERHEAD PBSW FAULT LIGHTS ENG2 YELLOW HYD, BLUE HYD SYS, ENGINE INDICATIONS WITH FADAC OFF NR 2 EPR AND PERCENT RPM AMBER FOR ALL OTHERS. SWAPPED LGCIU, GCU AND SDAC NO HELP, SUSPECT DC ESS BUS. REPLACED LT MAIN LANDING GEAR FWD PROXIMITY SENSOR 23GA IAW AMM 32-31-73 AND INDICATION NORMAL NOW.
LIFE JACKET DOOR ON CENTER OBSERVERS SEAT WILL NOT REMAIN CLOSED. R & R CREW LIFE VEST. DOOR STAYS CLOSED.
ONE FUEL PANEL LATCH INBD, DAMAGED. REPLACED LATCH.
LANDING GEAR STUCK, RETURNED TO FIELD. ADJUSTED PROXIMITY SENSORS 24GA AND 25GA ACCOMPLISHED GEAR SWING. OPS CHECKED NORMAL IAW AMM 32-31-00 AND AMM 32-31-73-820-006-A.
MLG LEFT BRAKE SERVO VALVE MANIFOLD LEAKING AT HOUSING CASTING WHEN PRESSURIZED AND BRAKES APPLIED. REMOVED AND REPLACED THE LEFT NORMAL BRAKE SERVO VALVE MANIFOLD ASSY. OPERATIONAL TESTS PERFORMED NO DEFECTS NOTED REF AMM 32-42-16-400-001-A.
OMC HEADPHONES INOPERATIVE. REPLACED HEADSET.
AFT WATER SERVICE PANEL HAS A DENT AND 1 INCH CRACK 3 INCHES FROM AFT EDGE. REPORTED BY WATER SERVICE. REINSTALLED DOOR IAW MM 52-42-13. SECURITY CHECKED GOOD.
STRONG BURNING ELEC SMELL IN AFT CABIN NOT ABLE TO IDENTIFY SOURCE. DISSIPATED IN FIVE MINUTES. ACCOMPLISHED ELECTRICAL SMELL INSPECTION PER MM 24-00-00-810-823-A. REMOVED VIDEO MONITORS AND INSPECTED WIRING UNDERNEATH SEATS. NO IRREGULARITIES NOTED. NO CIRCUIT BREAKERS TRIPPED OR ECAM MESSAGES. OK TO CONTINUE.
SEAT 30ABC PAX OXYGEN DOOR FELL OPEN, WITH MASKS DEPLOYED.
CREW REPORT: NOSE WHEEL VIBRATION ON TAKEOFF SEEMED EXCESSIVE. REPLACED BOTH NLG TIRES.
RIVET MISSING IN EXHAUST AREA OF NR 1 ENGINE RT C-DUCT LOWER BIFI HAS ONE MISSING FASTENER ON VERTICAL WALL APPROXIMATELY THREE INCHES FROM TRAILING EDGE. REPLACED LOCK FASTENER PER CMM 78-30-00 FIG 31 SHEET 10 ITEM 150.
COCKPIT DOOR FAULT LIGHT DOOR CONTROLLER MID STRIKE LIGHT IS ON. REMOVED AND REPLACED MID STRIKE ELECTRIC LOCK IAW MM, OPS CHECKED GOOD.
LEFT SIDE OF RUDDER IS DELAMINATED AT THE UPPER HOIST POINT AREA ALONG WITH MINOR IMPACT DAMAGE 26 INCHES ABOVE THE UPPER HOIST POINT. BOTH AREAS HAVE BEEN REPAIRED PER ECRA 5540-01330.
L2 DOOR SILL CORRODED AT FRAME 68. CORROSION OUT OF LIMITS. INSTALLED STRAP REPAIR IAW SRM 53-41-14 FIG 201. MAJOR REPAIR.
G1 AND G4 GALLEYS HAVE HEAT DAMAGE BEHIND WORK LIGHTS. GALLEYS WERE REFURBISHED AT HMV2 VISIT PER JD-CE-40-25-30-02-JD1.
NR 2 ENGINE HAS MISSING ACOUSTIC MATERIAL IN ENGINE INLET. PERFORMED REPAIR PER MT71 -006 REF CF9044 FOR PERM REPAIR AT 7 O'CLOCK POSITION.
RAT FAILED FUNCTIONAL TEST. REPLACED RAM AIR TURBINE, OP CKS GOOD.
CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. SWAPPED CAPT'S AND SECOND OBS O2 STORAGE BOXES DUE TO A CHAFED WIRE. CAPT'S MASK NOW OPS CHECKS NORMAL FOR AUDIO AND O2.
SOME EMERGENCY EXIT LIGHTS ON WITH SWITCH IN OFF POSITION EPSU BATT AFT L MESSAGE ON PTP. REPLACED EPSU BATTERY PER MM. OPS CHECK GOOD.
DOOR 1R ESCAPE SLIDE IS IN RED BAND. REPLACED DOOR NR 1 RIGHT SLIDE RAFT ASSY IAW REF AMM.
LEFT WINDSHIELD ANTI ICE DISPLAYED ON UPPER ECAM SCREEN. BOTH SENSORS READ APPROXIMATELY 595 OHMS FROM CONTROLLER. (MATCHES RT WINDSHIELD) LT WINDOW ELEMENT RESISTANCE IS APPROX 11.5 OHMS. (MATCHES RT WINDSHIELD). WIRES ARE NOT SHORTED TO GROUND. WIRES FROM WINDSHIELD TO CONTROLLER, NO FAULTS WITH WINDOW POWERED. RAN 1 HOUR, NO FAULTS. BITE CHECKED OK. PER OPBLM REPLACE LEFT WINDSHIELD. OPS CHECKED GOOD.
INSULATION BLOWING INTO CABIN LEFT SIDE EXIT ROW. REBONDED SEPARATED TWO HALF OF AIR CONDITION DUCT.
NR 1 ENGINE OIL QTY IND, FLIGHT DIVERTED. ENG 1 OIL QUANTITY INDICATION INOP ON ENG ECAM SYSTEM PAGE. OIL PRESSURE AND-OR TEMP ABNORMAL. ENG 1 CREW COMMENTS: OIL QUANTITY DOWN TO 4.0 TO 3.5 SAMC TEXT: PER CAPT ATKINSON, OIL TEMP AND PRESS WERE NORMAL. OIL QTY VERIFIED TO BE FULL. REPLACED ENGINE OIL QTY TRANSMITTER. ECAM OIL QTY INDICATION GOOD.
LIGHTNING STRIKE ON LT NOSE RVSM AREA AND EXITED FROM RT ELEVATOR CAUSING DAMAGE. ALSO HAS RVSM DAMAGE. *SUPPLEMENTAL DATA UPDATE* PLANNING ON REPLACED RT ELEV CAP ASSY. PERFORMED LIGHTNING STRIKE INSP. PERFORM PHASE 2 AND PHASE 3 INSPECTION IN AREAS WITH DAMAGE (ELEVATOR AND RADOME AND RVSM). FOUND DAMAGE TO THE RVSM AREA, RIGHT ELEVATOR TIP AND DAMAGE TO RT ELEVATOR. NO OTHER DEFECTS NOTED. REPLACED RADOME LATCH ON CAPTAIN SIDE AND REPLACED RT ELEVATOR TIP.
AFT NOSE STEERING CYLINDER LEAKING WITH HYD PRESSURE OFF. PACKINGS ON ANTI SHIMMY VALVE. OP CHECKED STEERING, NO LEAKS NOTED.
DURING CABIN EMERGENCY LIGHT TEST (3SV) "EPSU INT LOAD EMER L" MESSAGE. FOUND SEAT EMERGENCY LIGHT AT SEAT 18C INOP. REPLACED & RE-TESTED OKAY.
ENG NR 2 BLEED FAULT, RTFL. THERMOSTAT FAILURE. REPLACED NR 2 ENGINE FAV CONTROL THERMOSTAT. TESTS OKAY DURING HIGH POWER RUN.
BIRDSTRIKE RADOME AREA. MAJOR REPAIR ACCOMPLISHED, BIRDSTRIKE ON RIGHT HAND SIDE OF NOSE IN RVSM AREA AROUND FRAME 4. INSP FOUND NO CRACKS, PLNG DBLR RPR. STARTING TO DRILL HOLES AND FABRICATING REPAIR. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR.
K PANEL NR 527EB LOCATED INBD OF NR 1 PYLON NOT SECURE. PANEL MOUNT DOUBLER CRACKED OFF. PANEL IS ON UNDER SIDE OF WING L/E, PANEL IS 521EB. REPAIRED OUTBD COMPARTMENT FRONT BRACKET ASSY AND AFT LANDING. CENTER AFT LANDING AND SMALL LANDING AT OUTBD TRACK NEED REPAIR. THEN PANEL NEEDS TO BE INSTALLED. COMPLETED REPAIRS AND INSTALLED PANEL ONTO AIRCRAFT.
AVIONICS MSG RCV'D. SUSPECT HUMIDITY SET OFF THE ALARM. MSG WAS NOT PRESENT WHEN MECH ARRIVED. PERFORMED AEVC TEST AND SDCU TEST AND TESTED OK. CHECKED AVIONICS BAYS FOR SMOKE AND NONE FOUND. NO BURNING ODOR EITHER.
AVIONIC SMOKE ECAM, NO SMOKE PERCEPTIBLE. FLIGHT DIVERTED. FOUND NO EVIDENCE OF SMOKE OR ODORS ON MAIN DECK OR E&E COMPARTMENT, ECAM HAD CLEARED UPON ARRIVAL, SUCCESSFULLY TESTED AEVC AND SCDU REF AMM 21-26-00. CHECK PFR REPORT FOR FAILURE MESSAGES, NONE FOUND. TESTED LWR CARGO FIRE SYSTEM - NORMAL, AND RESET FWC'S PRECAUTIONARY.
BOTTOM OF DOOR 1L DAMAGED. AFTER VISUAL INSPECTION FOUND DENT TO BE WITHIN LIMITS THICKER THEN .063 CANNOT BE DRESSED OUT. WILL REQUIRE DOUBLER REPAIR. SCHEDULED FOR A PERMANENT REPAIR.
NR 2 ENGINE IDG POWER FEEDER CONNECTION FAILURE CAUSED DIVERSION. FOUND NR 2 ENG IDG FAILURE. NO IDG FEEDER CABLE ISSUE. REPLACED NR 2 IDG, PERFORMED INSPECTION OF IDG FEEDER CONNECTION AT PYLON AND CKECKED FOR PIN BURNING OR ARCING. AREA OK, NO ISSUES NOTED.
BURNING SMELL IN FWD GALLEY FOR SHORT TIME THEN NOTICED AUDIO INOP WITH C/B-PBS MUSIC LT POPPED.
BURNING ODOR IN FWD GALLEY FOR SHORT TIME THEN NOTICED AUDIO INOPERATIVE W-CB-PBS MUSIC LT POPPED. REPLACED SEU UNDER SEAT 2ABC, MULTIPLEX BOX AT 3ABC AND CB 23MK. AS PRECAUTIONARY. ODOR WAS INTERMITTMENT AND POSSIBLY UNRELATED TO THE MTX PREFORMED. ODOR HAS NOT RETURNED SINCE 7/13/07.
ABORTED TAKEOFF FOR COMPRESSOR STALL AT 100-110 KTS. ALL INDICATIONS NORMAL UP TO THAT POINT. STOPPED THE ACFT WITH TWO BLOWN TIRES. NO INJURIES. BOROSCOPE INSPECTION FOUND 2 BLADES DAMAGED WITH PARTS OF THE MIDSPAN SHROUD MISSING, 1 ALSO HAS LEADING DAMAGE SPANING APROX. ONE THIRD THE LENGTH AND A RADIAL CREASE THE SAME LENGTH IN STAGE 3 COMPRESSOR. ON STAGE 6 COMP. COUNTED 26 BLADES WITH LEADING EDGE DAMAGE OF VARRIS DEGREES OF SEVERITY. ALL DAMAGE IS BEYOND SERVICEABLE LIMITS. REPLACED #1 ENGINE, SERIAL NUMBER REMOVED V10856.
WITH NO SMOKING SWITCH IN THE ON POSITION, EMERGENGY EXIT SIGNS WERE ILLUMINATED DURING TAXI & FOR THE FIRST 30 MIN OF FLIGHT. FLIGHT ATTENDANT CALLED TO REPORT THAT ALL EMERGENCY EXIT SIGNS EXTINGUISHED AT SAME TIME WITH NO CHANGE IN COCKPIT SWITCH POSITION.
CABIN FLOOR STRUCTURE FRAME 12+2, LBL 9 TRANSVERSE FLOORBEAM CRACKED FWD FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF TRANSVERSE FLOORBEAM WITH 4EA NESTED ANGLES.
SKIN IS DAMAGED FROM STRINGER 41R TO 40L, FRAMES 58 THROUGH 61. MAJOR REPAIR ACCOMPLISHED. REPLACED DAMAGED SKIN SECTION.
AIRCRAFT SUSTAINED DAMAGE TO AFT LWR BELLY SKIN BETWEEN FRAME 58 AND 64 BETWEEN STRINGER 41R AND 40L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKINS AND DOUBLER.
AFT CARGO DOOR CUT OUT LOWER SILL 3RD FROM FRONT LUG HAS GOUGE AFT LOWER END. MAJOR REPAIR ACCOMPLISHED. 3RD FROM FRONT LOWER LUG BLENDED & ROTO PEENED.
AFT PIT FRAME 58 AT STRINGER 41L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED NEW SHEAR TIE. REPLACED BENT SHEAR TIE.
AFT PIT FRAME 59 AT STRINGER 42L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. REPLACED SHEAR TIE.
AFT PIT FRAME 59 AT STRINGER 43L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. SHEAR TIE REPLACED.
AFT PIT FRAME 59 AT STRINGER 41L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. SHEAR TIE REPLACED.
FUSELAGE SKIN DAMAGED AT FRAME 67 TO FRAME 70 FROM STRINGER 42L TO 42R. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO DOUBLERS AND FILLERS.