N173UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED PARCEL SERVICE CO. (IPXA) | Operator | 2011-03-22 – 2011-03-22 | Operator named in NTSB report |
| UNITED PARCEL SERVICE CO | Operator | 2011-03-22 – 2011-03-22 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EXTREMELY LOUD SQUEAL EMANATING FROM MAIN DOOR ON AIRCRAFT. SOUND IS COMING FROM AREA OF LOWER DOOR HINGE OR FLOOR. INSTALLED NEW ENTRY DOOR SEAL PER AMM 52-10-18.
EXTREMELY LOUD SQUEAL EMANATING FROM MAIN DOOR ON AIRCRAFT. SOUND IS COMING FROM AREA OF LOWER DOOR HINGE OR FLOOR. INSTALLED NEW ENTRY DOOR SEAL PER AMM 52-10-18. AWAITING SEALANT CURE TIME AND PRESSURIZATION LEAK CHECK. PERFORMED PRESSURIZATION OF ACFT PER AMM 21-31-00. NO LEAKS NOTED. NO LOUD SQUEAL NOTED. ACFT OKAY FOR SERVICE.
FUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. REF[T3F18E0080U8N]. REQUESTED FAULT BE DERRERD FOR 6 MONTHS IAW EO 96143 REQ1
FUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. VERIFY DAMAGE AND REPORT FINDINGS TO SDF LIAISON ENGINEERING PRIOR TO STARTING INITIAL CUTOUT. FOUND 24Ãâ¬? LONG DENT FWD AND AFT OF FRAME 54.2. WIDTH OF DENT MEASURES FROM 3Ãâ¬? TO 6Ãâ¬? MAXIMUM. DEPTH OF SKIN DENT FROM .030 TO .300 WITH A .9Ãâ¬? LONG CRACK AT INTERSECTION OF FRAME AND STR 42L. THERE IS MAX OF .200 DEFLECTION OF FRAME FITTING AT UPPER FWD CORNER. THE STRINGER S42L IS ALSO DEFLECTED .080 X 9Ãâ¬? FWD & AFT OF FRAME.
FUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. REPLACEMENT STRINGER WAS FABRICATED IAW SRM 53-10-14 AND EO-96143-PRELIM4 STEP 6.
MAIN DECK-CLS ADAPTER CRACKED FR38.1 BETWEEN -Y1959 AND -Y2462-RT SIDE-109. REMOVED 01 CLS ADAPTER. IAW SRM 51-40-21. INSTALLED CLS ADAPTER. IAW SRM 51-40-21.
FAULT-STR-Z400- #2 ENG PYLON LOWER SPAR LOWER SURFACE LH/RH ANGLE CRACKED PROJECTION RIB 18. DOT 139-2. REMOVED 02 EA ANGLE CRAKED AT #2 ENG PYLON LOWER SPAR LOWER SURFACE LH/RH, IAW A300-600 SRM 51-40-21. INSTALLED NEW 01EA ANGLE SECTION LH P/N A5451506320400 BATCH 0003654319, AT #2 ENG PYLON LOWER SPAR PROJECTION RIB 18, IAW A300-600 SRM 51-40 21. INSTALLED NEW ANGLE SECTION RH (01EA), AT #2 ENG PYLON LOWER SPAR PROJECTION RIB 18, IAW SRM 51-40 21.
ENGINE NR 1 OTBD THRUST REVERSER INTERNAL STRUCTURE, AFT UPPER CORNER HAD A CRACK. PERFORMED SURFACE HFEC INSPECTION IN THE CRACKED AREA TO THE NR 1 THRUST REVERSER INTERNAL STRUCTURE AFT UPPER CORNER. FOUND AND VERIFIED CRACK WITH AN EST. LENGTH OF 31.75MM (1.25"). ACCOMPLISHED INSPECTION IAW NTM 51-10-08 PART 6. INSP ONLY. T91269. CRACK WAS REPAIRED ON TRAVELER T25/1838644.
MDC FLOOR, R/H SIDE, BTW FR 38.1 AND FR 38.2, DOG BONE SUPPORT BROKEN. REMOVED AND REPLACED THE DOG BONE SUPPORT BTW FR 38.1 AND FR 38.2 R/H SIDE IAW SRM 51-40-21.
MDC FLOOR, R/H SIDE, BTW FR 37 AND FR 38, DOG BONE SUPPORT BROKEN. REMOVED AND REPLACED THE DOG BONE SUPPORT BTW FR 37 AND FR 38 R/H SIDE IAW A300-600 SRM 51-40-21.
MDC FLOOR PANEL 251 LJ IS DAMAGED. FABRICATION OF PANEL 251LJ IS COMPLETE IAW SREO-16407-REQ001((APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)). VERIFIED FABRICATION 251LJ
FLOOR PANEL 252 PG IS DAMAGED. FLOOR PANEL 252PG FABRICATION COMPLETED IAW SREO-16407-REQ001.
LH WING, UPPER SURFACE, WTB, THROUGH FAIRING 577DT, CLOSE TO FALSE REAR SPAR, BRACKET SUPPORT HAS GOUGE. REMOVED BRACKET SUPPORT AT LH WING, UPPER SURFACE, WTB IAW A300-600 SRM 51-40-21. ++INSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21.
FAULT - STR - Z600 - R/H WING, KRUEGER MOVABLE VANE, EXTERNAL LOWER CENTER SKIN WITH GOUGE.REMOVED GAUGE ON EXTERNAL SKIN R/H KRUEGER IAW A300-600 SRM 51-73-10.RECEIVED SERVICEABLE RH KRUEGER FLAP FOLDING FAIRING P/N: A5351028500500 AND IT IS APPLICABLE TO USE ON A/C N173UP I.A.W. A300 AIPC 27-87-03-04. ITEM 140.INSTALLED R/H WING, KRUEGER FLAP MOVABLE VANE I.A.W. A300 AMM 27-87-12/401
R/H WING, KRUEGER MOVABLE VANE, EXTERNAL LOWER O/B SKIN WITH GOUGE. REMOVED GAUGE ON EXTERNAL SKIN R/H KRUEGER IAW SRM 51-73-10, ORIGINAL THICKNESS .090", REMAINING THICKNESS .065", MAX MATERIAL LOSS .025" FOUND OUT OF LIMITS IAW A300-600 SRM 51-73-11. REMOVED R/H WING, KRUEGER FLAP MOVABLE VANE I.A.W. A300 AMM 27-87-12/401. ++INSTALLED R/H WING, KRUEGER FLAP MOVABLE VANE I.A.W. A300 AMM 27-87-12/401.
RIGHT KRUEGER MOVABLE VANE, EXTERNAL SKIN WITH SCRATCH.EMOVED SCRATCH ON EXTERNAL SKIN R/H KRUEGER IAW A300-600 SRM 51-73-10.RECEIVED SERVICEABLE RH KRUEGER FLAP FOLDING FAIRING.INSTALLED R/H WING, KRUEGER FLAP MOVABLE VANE I.A.W. A300 AMM 27-87-12/401
R/H WING, KRUEGER MOVABLE VANE, INTERNAL STRUCTURE, INBOARD LOWER SECTION WITH GOUGE.REMOVED GOUGE ON INTERNAL STRUCTURE SKIN R/H KRUEGER IAW A300-600 SRM 51-73-10.RECEIVED SERVICEABLE RH KRUEGER FLAP FOLDING FAIRING P/N: A5351028500500 AND IT IS APPLICABLE TO USE ON A/C N173UP I.A.W. A300 AIPC 27-87-03-04. ITEM 140.INSTALLED R/H WING, KRUEGER FLAP MOVABLE VANE I.A.W. A300 AMM 27-87-12/401
MDC, LH SIDE, FLOOR AREA, FR36 HAS CLS ADAPTER BROKEN (BY CORROSION). DOT 103-41. REMOVED 01 CLS ADAPTER. IAW SRM 51-40-21. IAW STEP 9. INSTALLED CLS ADAPTER. IAW SRM 51-40-21.
MDC, LH SIDE, FLOOR PANEL241BF, LOWER SURFACE HAS A PUCTURE AND MATERIAL DAMAGED. DOT 103-52 JOB COMPLETED
MDC, LH SIDE, FLOOR PANEL241BF, LOWER SURFACE HAS A PUCTURE AND MATERIAL DAMAGED. FLOOR PANEL 241BF FABRICATION COMPLETE IAW SREO-16407-REQ001.
FWD CARGO, FR 38.2, BULKHEAD PANEL UPPER SUPPORT HAS BRACKETS CRACKED (6EA). SAW THROUGH FLOOR PANELS). REMOVED (6EA) BRACKETS SUPPORT I.A.W SRM 51-40-21. INSTALLED 6 EA NEW BRACKETS IAW A300-600 SRM 51-40-21.
MDC, LH SIDE, FLOOR PANEL 241HF HAS INSERT OUT OFF POSITION AND LOWER SURFACE DAMAGED. FLOOR PANEL 241HF FAB COMPLETED IAW SREO-16407-REQ001.
MDC, LH SIDE, FLOOR PANEL 241EF, LOWER SURFACE HAS AFT EDGE DAMAGED. DOT 103-48 APPROVED
MDC, LT SIDE, FLOOR PANEL 241EF, LOWER SURFACE HAS AFT EDGE DAMAGED. FLOOR PANEL 241EF FABRICATION COMPLETE IAW SREO-16407-REQ001.
MDC, LH SIDE, FLOOR AREA, FR38.1 TO FR38.2 HAS CROSS WEB (DOG BONE) BROKEN. DOT 103-39.REMOVED SUPPORT CROOS WEB (DOG BONE) LOCATED AT Z200, MDC, LH SIDE, FLOOR AREA, FR38.1 TO FR38.2 IAW A300-600 SRM 51-40-21.RECEIVED NEW CROSS WEB (DOG BONE) IAW A300-600 SRM 53-14-15 FIG #2 ITEM #1. P/N: A5378103821400, B/N:0004431402.INSTALLED NEW CROSS WEB (DOG BONE) ON Z200, MDC, LH SIDE, FLOOR AREA, FR38.1 TO FR38.2
RIGHT MAIN DECK DOG BONE IS LOOSE BETWEEN FR 37-38. REPLACED DOG BONE BETWEEN FR 37-38 IAW SRM 51-40-21.
RIGHT MAIN DECK DOGBONE BROKEN AT FR 38.1 - 38.2. REPLACED DOG BONE BETWEEN FR 38.1 - 38.2 IAW SRM 51-40-21.
FAULT: INT-200- MCC FLOORBOARD 232SG HAS DAMAGE. 33-035. FLOOR PANEL 232SG FAB COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY-1 TOP INSERTS P/N G2001B-3P B/N 0004418941 QTY-50 BOTTOM INSERTS P/N PG2002B-3S B/N 0004392380 QTY-50 GLUE P/N 04-001-0012 B/N 0004348393 QTY 1KIT EDGE FEEL P/N 04-009-0018 B/N004376925 QTY 1KIT REVIEWED
FAULT: INT-200- MCC FLOORBOARD 232WG HAS AN OVERSIZE SCREW HOLE. 33-038. FLOOR PANEL 232WG FAB COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY-1 TOP INSERTS P/N G2001B-3P B/N 0004418941 QTY-50 BOTTOM INSERTS P/N PG2002B-3S B/N 0004392380 QTY-50 GLUE P/N 04-001-0012 B/N 0004348393 QTY 1 KIT EDGE FEEL P/N 04-009-0018 B/N 004376925 QTY 1KIT.
FAULT-STR-ZONE 300. VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, LH #2 UPPER PANEL SUPPORT BRACKET (1EA) BROKEN. REMOVED THE BROKE UPPER BRACKET AT 300. VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, LH IAW A300-600 SRM 51-40-21 IT. ++INSTALLED SUPPORT BRACKET AT ZONE 300. VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, LH IAW A300-600 SRM 51-40-21.
MCC FLOOR BOARD 231MJ IS BROKEN. 33-033. FLOOR BOARD 231MJ FABRICATION COMPLETE IAW SREO-16407-REQ 001 INSERT QUANTITY 40 INSERT, EDGE FILL, KIT INSERT GLUE. MAJOR.
MCC FWD FLOORBOARD 221CG HAS FWD EDGE DAMAGE. 33-032. FLOOR PANEL FABRICATION COMPLETE IAW SREO-16407-REQ001.
VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, RH #3 PANEL SUPPORT BRACKET (1EA) BROKEN. REMOVED SUPPORT BRACKET (1EA)I.A.W A300-600 SRM 51-40-21. ++INSTALLED NEW PART IAW A300-600 SRM 51-40-21. RIVET P/N CR3213-4-06, BATCH #0004279158, QTY 2EA
MAIN DECK FLOOR STRUCTURE, FR 10, -Y1456, FITTING PICK-UP WITH CRACK.REMOVED FITTING IN MAIN DECK FLOOR STRUCTURE, FR 10, -Y1456. IAW AIRBUS A300-600 SRM 51-40-21.FABRICATED, LOCATED AND DRILL NEW FITTING PICK-UP P/N: 2024-T3 .063, BATCH: 0004410262 IAWAIRBUSA300-600 GMM 09-08, AND SRM 51-40-40.INSTALLED NEW FITTING PICK-UP ON MAIN DECK FLOOR STRUCTURE, FR 10, -Y1456 IAW A300-600 SRM 51-40-21
FR 80, BTW -Y1137.1 AND -Y1580.5, Z ANGLE WITH CRACK.REMOVED AND REPLACED PROFILE-T P/N A53988140120100 BATCH 0004429452, AT MDC, FR 80, BTW -Y1137.1 AND -Y1580.5, IAW A300-600 SRM 51-40-21
MDC, LH SIDE, FLOOR AREA, THROUGH PANEL 241YK, BTWN FR38.1 TO 38.2 HAS CLS ADAPTER BROKEN (BY CORROSION). REMOVED 02 EA CLS ADAPTER LOCATED IN FR38.1 AND FR38.2. IAW SRM 51-40-21. IAW STEP 9. INSTALLED 02 EA CLS ADAPTERS. IAW SRM 51-40-21.
CREW DOOR, EXTERNAL SURFACE, ALONG OF THE FWD EDGE HAS BARE METAL. PREPPED AND PAINTED CREW DOOR EXTERNAL SURFACE ,ALONG OF THE FWD EDGE IAW SRM 51-75 10.
CREW DOOR, EXTERNAL HANDLE INNER SIDE, LOWER EDGE HAS A GOUGE.
MAIN DECK FLOOR PANEL 241JN DELAMINATED. FLOOR BOARD 231MJ FABRICATION COMPLETE IAW SREO-16407-REQ00.
CREW DOOR, EXTERNAL HANDLE INNER SIDE, LOWER EDGE HAS A GOUGE. REMOVED MINOR GOUGE AT CREW DOOR, EXTERNAL HANDLE INNER SIDE, LOWER IAW SRM 51-73-10 AND ORIGINAL THICKNESS IS 0.135" AND MATERIAL LOSS IS 0.001 AND REMAINING THICKNESS IS 0.134" AND FOUND WITH IN LIMITS IAW SRM 51-73-11. APPLIED SURFACE PROTECTION AT CREW DOOR, EXTERNAL HANDLE INNER SIDE, LOWER EDGE IAW SRM 51-75-10.
CREW DOOR CUT-OUT, FWD AND AFT FRAMES, ROLLER RAILS (4EA) HAVE GOUGES. REMOVED MINOR GOUDES AT FWD AND AFT FRAMES, ROLLER RAILS (4EA) IAW SRM 51-73-10 AND THE ORIGINAL THICKNESS IS 0.095" AND MATERIAL LOSS 0.002 AND REMAINING THICKESS IS 0.093" AND FOUND WITHIN LIMITS IAW SRM 51-73-11. APPLIED SURFACE PROTECTION AT CREW DOOR AFT ROLLER RAILS IAW SRM 51-75-10.
MDC FLOOR, FR 59, BTW Y0 AND -Y450, CLS ADAPTER CORRODED. REWORKED CLS ADAPTER AT FR59 BTW Y0 AND Y-450 BY TOOL AND IS OUT OF LIMITS. ACCOMPLISHED STEP 11 EA#300-5317-27-A4163 PRELIMINARY 1. INSTALL CLS ADAPTER PER DRAWING A53275514.
MDC FLOOR STRUCTURE, FR 63, -Y1959 HAS CLS ADAPTER BROKEN.. REMOVED CLS ADAPTER AT MDC FLOOR STRUCTURE, FR 63, -Y1959, IAW SRM 51-40-21. ACCOMPLISH PERMANENT REPAIR IAW EO-95271-REQ1 AND VT-MAE EA 300-5317-27-A4164.
MDC, FR 48, BTW -Y450 AND -Y953, CROSSBEAM BENT. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
MDC, FR 49, BTW -Y450 AND -Y953, CROSSBEAM BENT. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
MAIN DECK FLOOR PANEL 251DN, CORNER DAMAGED. FLOOR PANEL 251CN FAB COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY-1 TOP INSERTS P/N G2001B-3P B/N 0004418941 QTY-50 BOTTOM INSERTS P/N PG2002B-3S B/N 0004392380 QTY-50 GLUE P/N 04-001-0012 B/N 0004348393 QTY 1KIT EDGE FEEL P/N 04-009-0018 B/N004376925 QTY 1KIT.
MAIN DECK FLOOR PANEL 251CN HAS COMPOSITE DAMAGE. PANEL 251CN FABRICATION COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY1 TOP INSERT P/N G2001B-3P B/N 0004418941 QTY 50 BOTTOM INSERT P/N G2002B-3S B/N 0004392380 QTY 50 EDGE FEEL PN 04-009-0018 B/N 0004376925 QTY 1 KIT ADHESIVE P/N 04-001-0012 B/N 0004348393 QTY 1KIT. REVIEWED
MDC, FR 50, BTW -Y450 AND -Y953, CROSSBEAM BENT. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
MDC, FR 51, BTW -Y450 AND -Y953, CROSSBEAM CRACKED. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
CREW DOOR CUT-OUT, FWD AND AFT FRAMES, FOUR ROLLER RAILS HAVE GOUGES.
MAIN DECK FOOR PANEL 262GH EDGE DAMAGED. FLOOR BOARD 262GH FABRICATION COMPLETE IAW SREO-16407-REQ001. MAJOR REPAIR.
FAULT - STR - Z200 - MDC FLOOR STRUCTURE, FR 74, -Y2127.5 Z ANGLE CRACKED DOT 1/026.REMOVED Z-PROFILE AT MDC FLOOR STRUCTURE, FR 74, -Y2127.5, IAW A300-600 SRM 51-40-21.FABRICATED NEW Z-PROFILE, IAW A300-600 SRM 53-18-18 AND GMM 09-08-01-04.INATALLED NEW Z-PROFILE AT MDC FLOOR STRUCTURE, FR 74, -Y2127.5, IAW A300-600 SRM 51-40-21
MAIN DECK FLOOR PANEL AREA, LT Z-ANGLE HAVE 2 CRACKS AT FR74 AND FR75. VERIFIED STEP 8. INSTALLED NEW Z-ANGLE LT BTW FR73 TO FR76 MAIN DECK FLOOR PANEL AREA IAW SRM 51-40-21. JOB COMPLETE
CREW DOOR, EXTERNAL SURFACE, ALONG OF THE FWD EDGE HAS BARE METAL.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 12. CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.
MAJOR REPAIR - RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, TWO CRACKS INDICATION NOTED AT RIB 11. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 & VT-MAE EA 300-5750-27-A4159, REV -.
LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE. ONE CRACK NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-95368-REQ1 AND VT-MAE EA 300-5750-27-A4158.
LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE. TWO CRACKS NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-95368-REQ1 AND VT-MAE EA 300-5750-27-A4158.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, THREE CRACK INDICATION NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 25. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 19. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 18. ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, ONE CRACK INDICATION NOTED AT RIB 17. PERFORMED 2X CUTOUTS AT RIB 17 TO RIB 19 FROM REAR SAPR TO STR 2.1 IAW SRM-57-50-00 PARA 4E FIG 205 AND EA 300-5750-27-A4159, STEP 15. .ACCOMPLISHED PERMANENT REPAIR IAW EO-95369-REQ1 AND VT-MAE EA 300-5750-27-A4159.
RIGHT WING, CENTER FLAP, TOP SKIN FLANGE, THREE CRACK INDICATIONS NOTED AT RIB 27. ACCOMPLISH PERMANENT REPAIR IAW EO-95120-REQ1 AND VT-MAE EA 300-5750-27-A4111.
NR 2 ENG NOSE COWL RH EXTERNAL SURFACE HAVE 7EA CRACKS, MARKED AREA (1, 2 O'CLOCK POSITION). REMOVED SKIN DAMAGE WITH CRACK, IAW PRATT & WHITNEY SRM 54-10-00 REPAIR 11 FIG 204. ++INSTALLED DOUBLER AND FILLERS AT ENG #2 NOSE COWL RH EXTERNAL SURFACE, IAW A300-600 SRM 51-40-21 AND PRATT & WHITNEY SRM 54-10-00 REPAIR 11 FIG 204.
NR 2 PYLON OTBD SIDE AT RIB 3A HAD 2 CRACKS. REMOVED PLATE PYLON #2 O/B SIDE AT RIB 3A IAW A300-600 SRM 51-40-21. INSTALLED PLATE P\N A5461237120000 PYLON #2 O/B SIDE AT RIB 3A, IAW SRM 51-40-21. AND 54-52-21.
MAIN DECK FLOOR PANEL 262AH HAS COMP DAMAGE DOT 1/024. FLOOR PANEL 262AH FABRICATION COMPLETED IAW SREO-16407-REQ001.
ENG NR 2 NOSE COWL BULKHEAD AREA LH SIDE, HAS 2 CRACKS (9 O'CLOCK POSITION). REMOVE PART ENG #2 NOSE COWL BULKHEAD AREA LH SIDE IAW SRM 51-40-21. INSTALLED PART ENG NR 2 NOSE COWL BULKHEAD AREA LT SIDE, IAW SRM 54-10-00 AND SRM 51-40-21. PART FABRICATED AFT BULKHEAD WEB, BECAUSE FOR TWO BREAKS, WITH DIMENSIONS OF 2 INCHES IN LENGTH EACH, IAW PW 54-10-00.
ENG #2, INBD FAN COWL, UPPER AFT ATTACH FITTING DAMAGED. REWORKED WITH ABRASION BY HAND UPPER AFT ATTACH FITTING WITH DAMAGE AT NR 2 ENG, INBD FAN COWL, IAW SRM 51-73-10, AFTER REWORK ORIGINAL THICKNESS: .100", MATERIAL LOSS: .068", MAX ALLOWABLE DAMAGE: 0.0039", FOUND OUT OF LIMITS IAW SRM 51-73-11. INSTALLED NEW ATTACH BRACKET USING EXISTING FASTENERS, AT NR 2 ENG, INBD FAN COWL, IAW SRM 51-40-23.
PYLON NR 2 UPPER SURFACE AT RIB 3A HAVE A CRACK. RIB 3A REMOVED IN IAW SRM 51-40-21, WELDED. RE-INSTALLED RIB 3A AT PYLON NR 2 UPPER SURFACE, IAW SRM 51-40-21.
PYLON #2 I/B SIDE AT RIB 3A HAVE A CRACK. DOT 90-080. RIB 3A REMOVED IN IAW A300-600 SRM51-40-21, READY TO WELD. ++RE-INSTALLED RIB 3A AT PYLON #2 UPPER SURFACE, IAW A300-600 SRM 51-40-21.
FAULT-Z200-STR MAIN DECK FLOOR STRUCTURE AT FRAME 80/82 SEAT TRACK CORRODED, -Y852.4 DOT 1/019.CUT SEAT TRACK SECTION AT FR 80.10 -Y794 TO REMOVE DAMAGE IAW A300-600-SRM-53-10-16 FIG 201.FABRICATED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201 WITH SEAT TRACK SECTION P/N: R5307007120600 BACHT#: 0004423880.INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW A300-600 SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201 AND SRM 51-40-21 WITH SEALANT 1 KIT P/N: 04-001-0109 BATCH# 0004410103
FAULT - STR Z400 - ENG #2 O/B T/R UPPER INTERNAL STRUCTURE, RUB STRIP HAS A GOUGE. MARKED AREA. DOT 90-066.REMOVED UPPER AFT RUB STRIP #2 ENGINE T/R IAW A300-600 SRM 51-40-21.FABRICATED RUB STRIP AND AFT BRACKET ENGINE #2 L/H T/R UPPER IAW GMM 09.08 PARAGRAPH 09.08.RUB STRIP AND AFT BRACKET ENGINE #2 L/H T/R UPPER INSTALLED IAW A300-600 SRM51-40-21
MAIN DECK FLOOR STRUCTURE AT FRAME 79, -Y1580.5 ANGLE CRACKED. REMOVED CRACKED ANGLE. IAW SRM 51-40-21-001. INSTALLED ANGLE IAW SRM 51-40-21-001.
MAIN DECK FLOOR STRUCTURE AT FRAME 79 AT Y1580.5 ANGLE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-40-21-001. INSTALLED ANGLE IAW SRM 51-40-21-001.
MAIN DECK FLOOR STRUCTURE AT FRAME 80/82 HAS SEAT TRACK CORRODED, -Y450 DOT 1/018. REMOVED CORROSION IAW SRM 51-22-00 AND AFTER FURTHER EVALUATION FOUND STILL SHOWS UP EXFOLIATED CORROSION. FOUND OUT OF LIMITS IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201 AND SRM 51-40-21 WITH SEALANT.
MAJOR REPAIR, FLOOR PANEL 147BF OIL SOAKED. FLOOR PANEL FABRICATION COMPLETE IAW SREO-16407-REQ 001.
NR 1 ENG, R/H T/R. UPPER AFT RUB STRIP WITH GOUGE AND MISSING RIVETS.REMOVED RUB STRIP AT #1 ENG, R/H T/R. UPPER AFT.FABRICATED RUB STRIP FWD COVER, #1 ENG, R/H T/R, UPPER. IAW GMM 09.08 PARAGRAPH 09.08.01.04.INSTALLED RUB STRIP FWD COVER, #1 ENG, R/H T/R, UPPER. IAW A300-600 SRM 51-40-21
LEFT WING, LOWER SURFACE, ACCESS PANEL 575DB, CUT-OUT HAS A CRACK. .ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95281-REQ1 REV. 2 AND VT-MAE EA 300-5751-27-A4155
FAULT - STR Z400 - ENG #2 I/B T/R INTERNAL UPPER STRUCTURE DAMAGED. PLATE BROKEN. DOT 90-031.REMOVED PLATE IN ENG #2 I/B T/R INTERNAL UPPER IAW A300-600 SRM 51-42-11. REMOVED PLATE IN ENG#2 I/B T/R INTERNAL UPPER IAW A300-600 SRM 51-40-2O. FABRICATED NEW PART IAW GMM 09.08.01.04.INSTALLED NEW PART IAW A300-600 SRM 51-40-21
FAULT - STR - Z400 - #1 ENG, L/H T/R, UPPER AFT RUB STRIP FWD COVER WITH GOUGE.REMOVED UPPER AFT RUB STRIP #1 ENG, T/R. IAW SRM A300-600 51-40-21.FABRICATED RUB STRIP FWD COVER, #1 ENG, L/H T/R, UPPER. IAW GMM 09.08 PARAGRAPH 09.08.01.04.INSTALLED RUB STRIP FWD COVER, #1 ENG, L/H T/R, UPPER. IAW A300-600 SRM 51-40-21
FAULT - STR - Z400 - #1 ENG, R/H T/R, UPPER AFT RUB STRIP FWD COVER WITH CRACK.REMOVED DAMAGED RUB STRIP FWD COVER IAW A300 SRM 51-40-21.FABRICATED RUB STRIP FWD COVER, #1 ENG, R/H T/R, UPPER. IAW GMM 09.08 PARAGRAPH 09.08.01.04.INSTALLED RUB STRIP FWD COVER, #1 ENG, R/H T/R, UPPER. IAW A300-600 SRM 51-40-21
FAULT - STR - Z400 - #1 ENG, L/H T/R. UPPER AFT RUB STRIP WITH GOUGE.REMOVED UPPER AFT RUB STRIP, #1 ENG, T/R. IAW A300-600 SRM 51-40-21.FABRICATED RUB STRIP FWD COVER, #1 ENG, L/H T/R, UPPER. IAW GMM 09.08 PARAGRAPH 09.08.01.04.INSTALLED RUB STRIP FWD COVER, #1 ENG, L/H T/R, UPPER. IAW A300-600 SRM 51-40-21
ENG #2 I/B T/R AFT UPPER RUB STRIP HAVE GOUGES. MARKED AREA. DOT 90-030 .REMOVED UPPER AFT RUB STRIP #2 ENGINE T/R IAW A300-600 SRM 51-40-21.FABRICATED RUB STRIP AND AFT BRACKET ENGINE #2 R/H T/R UPPER IAW GMM 09.08 PARAGRAPH 09.08.RUB STRIP INSTALLED IAW A300-600, SRM51-40-21
FLOOR PANEL 143DF OIL SOAKED INTERNAL SIDE AND DISBONDED CUSHION TAPE. FLOOR PANEL FABRICATION COMPLETE IAW SREO-16407-REQ 001, MAJOR.
NR 1 PYLON PANEL 413BL AFT SUPPORT FRAME LH SIDE END WORN THRU. REMOVED AFT SUPPORT FRAME LH SIDE #1 PYLON-ZONE400 IAW SRM 51-40-21. INSTALLED FRAME SUPPORT WITH THE SAME FASTENER AT #1 PYLON-ZONE400: NO.1 PYLON PANEL 413BL AFT IAW A300-600 SRM 51-40-21.
FAULT-STR-#1 PYLON-ZONE400: NO.1 PYLON PANEL 413BL FWD SUPPORT FRAME CRACKED. REMOVE SUPPORT FRAME PYLON N.1 PANEL 413BL -ZONE400 IAW A300-600 SRM 51-40-21. ++INSTALLED FRAME SUPPORT WITH THE SAME FASTENER AT -#1 PYLON-ZONE400: NO.1 PYLON PANEL 413BL FWD IAW A300-600 SRM 51-40-21.
AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE CRACKED AT Y1456 O/B SIDE-109-22 VWV 91195430. REMOVED AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE IAW A300-600 SRM 51-40-21.FABRICATED NEW ANGLE, IAW UPS GMM 09-08 AND A300-600F SRM 53-15-18.INSTALLED NEW ANGLE IAW A300-600 SRM 51-40-21
AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE CRACKED AT -Y1456 O/B SIDE-109-24 VWV 91195430.REMOVED AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE AT -Y1456 O/B SIDE, IAW A300-600 SRM 51-40-21.FABRICATED NEW ANGLE IAW UPS GMM 09-08 PARAGRAPH 09.08.01.04 AND A300-600F SRM 53-15-18.INSTALLED NEW ANGLE IAW A300-600 SRM 51-40-21
AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE CRACKED AT Y0-109-20 VWV 91195430.REMOVED AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE AT -Y1456 I/B SIDE, IAW A300-600 SRM 51-40-21.FABRICATED NEW ANGLE IAW UPS GMM 09-08 PARAGRAPH 09.08.01.04 AND A300-600F SRM 53-15-18.INSTALLED NEW ANGLE IAW A300-600 SRM 51-40-21
AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE CRACKED AT -Y1456 I/B SIDE-109-23 VWV 91195430.REMOVED AFT CARGO-AFT REAR BULKHEAD FR54 1EA ANGLE AT Y0, IAW A300-600 SRM 51-40-21. FABRICATED NEW ANGLE, IAW UPS GMM 09-08 AND A300-600F SRM 53-15-18.INSTALLED NEW ANGLE IAW A300-600 SRM 51-40-21
LEFT PACK EXTERNAL SURFACE, AFT BRACKET HAS A CRACK. REMOVED AND REPLACED 1 EA AFT BRACKET IAW SRM 51-40-21.USED SAME FASTENERS REMOVED.VERIFIED NEW PART INSTALLED.JOB COMPLETE
L1 DOOR SLIDE WOULD NOT ARM. COULD NOT MOVE DOOR SLIDE ARM TO RIGHT. CLEARED DEBRIS FROM FLOOR FITTINGS AND GRIT BAR AND ACCOMPLISHED FUNCTIONAL TEST F REF AMM 52-10-30/501. OP'S CHECK GOOD. ITEM HAS NO HISTORY. OSD: 1/28/2025
DURING PREFLIGHT EMG DOOR SLIDE PRESSURE IN RED LEVEL ZONE. VERIFIED SAFETY PIN REMOVED , SAFETY BAR ENGAGED , ALL LIGHTS NORMAL , NO FAULT AT THIS TIME .. REF AMM , 52-10-00.
EVACUATION SLIDE WARNING SYSTEM LIGHT INOP. REMOVED AND REINSTALLED LAMPS IN LIGHT IRW AMM 52-73-11/401. OPS CHECK GOOD. THIS CLEARS MEL. PLACARD REMOVED.
INSPECTION TYPE:NA*ATB* SLAT SYS 1 FAULT AFTER T/D. MAINTAINED 220 KTS CYCLED SWAT IAW QRH. SLATS SLOW ON STATUS PAGE. LANDED 30/40 NORMALLYFAULT CODE ON SFCC 1 WAS 11101 FOR SLATS, NO RELATED COMPONENT LISTED ON BOX. RESET SFCC & NO FAULTS DETECTED R/R #1 SFCC AS A PRE-CAUTION PER AMM 27-51-18-0401. OP CKS GOOD. RAN SLATS USING GREEN & BLUE PRESSURE. ESR: IPC 27-51-08-02A-010A
INSPECTION TYPE:NAPASSENGER/CREW DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW.SERVICED WITH NITROGEN AS REQUIRED REF: A300 AMM 52-10-14-0301.
INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** SLIDE WARNING LIGHT INOP. SOUND ACTIVATES NORMALLY. ORDERED ESCAPE SLIDE INDICATION LIGHT ON REQ #420610. DEFERRED SLIDE WARNING LIGHT PER MEL 52-73-01-1. PLACARD INSTALLEDPERFORMED OPS CHECK OF SLIDE WARNING LIGHT AND BUZZER REF A300 AMM 52-73-11-0401. LIGHT AND BUZZER OPS CHECK NORMAL. THIS CLEARS M794563
INSPECTION TYPE:N/ALAV EMERG LIGHT (DIM) IS BURNT OUTRELAMPED OPS CK GOOD REF MM 33-51-21
INSPECTION TYPE:N/AA/C LOST POWER DURING LIGHTNING STORM AND WILL NOT FULLY START BACK UP. BURNING ELECTRICAL SMELL ON FLIGHT DECK. TWO ECAM MSG'S "AC ESS BUS OFF" & "AC EMER BUS OFF".R/R RECTIFIER UNITS 3XD & 5XH PER ESPM 20-46-50. ACCOMPLISHED OPERATIONAL TEST OF A/C MONITORING & INDICATION IAW AMM 24-27-00-0501. OPS CK NORMAL. NO FAULTS NOTED REF IPC 24-52-0802B & 24-53-08-02A
INSPECTION TYPE:N/AL1 DOOR DAMPERR/R'D DOOR DAMPER CYLINDER IAW AMM 52-10-14-0401. SERVICED IAW AMM 52-10-14-0301 OPS CK OK. PLACARD REMOVED AND SAFETY PIN REMOVED AMM 52-10-14-0601. THIS CLEARS M758608
INSPECTION TYPE:N/A**SUPPLEMENTAL SDR ** EXIT SLIDE PRESSURE GAUGE IS OUT OF PLACE & CANT BE READ. DEFERRED DOOR SLIDE PER MEL 52 11 01 2 3 GIRT BAR SLIDER AND SLIPS IN PFM BOXR/R L1 DOOR EVAC SLIDE REF AMM 25-61-21-0401. OPS CK NORMAL. THIS CLEARS M758313
INSPECTION TYPE:N/ASLIDE PRESSURE INDICATOR IN REF BANK. DEFERRED L1 SLIDE PER MEL 52-11-01-2-3 CW DMP 52-11-01-2-3.REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW A300 AMM 25 61 21 0401. PRESSURE CHECK GOOD THIS CLEARS M 755239. PLACARD REMOVED.
INSPECTION TYPE:NAEMERGENCY EXIT LIGHTS BURNED OUTREMOVED AND REPLACED EMERGENCY EXIT LIGHTS IAW AMM 33-51-13-0401 OPS CHECK GOOD ESR: IPC 33-51-04-09B ITEM 50
INSPECTION TYPE:NA**SUPPLEMENTAL SDR ** SLIDE ARMING NEEDS TO BE RIGGED GIRT BAR CATCHES ON AFT GIRT FITTING DURING ENGAGEMENT. TRANSFERED TO NRC 198654.DISARMED DOOR DAMPER IAW AMM 52-10-00-301. REMOVED L1 DOOR SLIDE IAW AMM 25-61-21-0401. INSTALLED L1 SLIDE IAW AMM 25-61-21-0401. ADJUSTED SLIDE ARMING ON GIRT BAR FITTINGS IAW AMM 52-10-11-0501. ADJUSTMENT CHECK GOOD.
INSPECTION TYPE:SEGONL 161KF DAMAGED. FABBED PER SREO A300-5320-16407-E
INSPECTION TYPE: SEG FWD CARGO COMPARTMENT FLOORBOARD NUMBER 131AH IS PUNCTURED. C/W SREO A300-5320-42722.
INSPECTION TYPE: SEG FWD CARGO COMPARTMENT FLOORBOARD NUMBER 131MG IS PUNCTURED. C/W SREO A300-5320-42722.
INSPECTION TYPE:SEGPANEL 162LF IS DAMAGED. FABBED PER SREO A300-5320-16407-E
INSPECTION TYPE:SEGPNL 161LF DAMAGEDFABBED PER SREO A300-5320-16407-E
INSPECTION TYPE:SEGPNL 161MF CRACKEDFABBED PER SREO A300-5320-16407-E
INSPECTION TYPE:SEGPNL 162MF DAMAGEDFABBED PER SREO A300-5320-16407-E
INSPECTION TYPE:SEGPNL 161KF DAMAGEDFABBED PER SREO A300-5320-16407-E
INSPECTION TYPE: C PNL 222DG BROKEN. FABBED IAW SREO A300-5320-40552-B.
INSPECTION TYPE:SEGMAIN FORWARD CABIN BAY AT FR20 RH SIDE -Y1959 ADAPTER IS CRACKED.INSTALLED REPLACEMENT CLS ADAPTOR USING B5377413820200 SERIAL NUMBER TAG 713693 THAT WAS ROBBED FROM TAIL NUMBER N174UP IAW A300-600 SRM 51-40-21.
INSPECTION TYPE:SEGAFT CARGO DOOR AT FR 60A UPPER FWD HOLE IS DAMAGED THROUGH SKIN AND FRAME FORK.REMOVED AND REPLACED FRAME FORK AT 60A USING P/N F5237230220000 S/N TAG 1498879 IAW EO# 300-5230-27-A2553 STEP 12.
INSPECTION TYPE:SEGMDC FLOOR SEAT TRACK BETWEEN FR79 AND FR80 AT Y-0 HAS INTERGRANULAR MEASURING 2.40" LONG AND .90"WIDE ON THE RH FLANGE AND 1.80"LONG BY 1.2" WIDE ON UPPER CROWN AREA. THE FLANGE IS CORRODED 100% THROUGH AND THE CROWN IS EXFOLIATED BEYONG MEASURE. SEAT TRACK P/N IS A5327923920200.REPAIR SEAT TRACK IAW SRM 53-10-16 FIG 201 USING R5307007120600 BATCH0003720709 SEAT TRACK AND R5327049020000 BATCH 0003719244 SPLICED
INSPECTION TYPE:SEGBULK CARGO COMP. FLOOR PANEL 162HF HAS PUNCTURECOMPLIED WITH SREO A300-5320-42722
INSPECTION TYPE: SEG BULK CARGO COMP FLOOR PANEL 161JF HAS SEVERAL DENTS SREO A300-5320-42722.
INSPECTION TYPE: SEG FWD CARGO FLOOR PANEL 132PG FWD CORNER HAS DAMAGE SREO A300-5320-42722.
INSPECTION TYPE: SEG AFT CARGO COMPARTMENT AFT BULKHEAD WALL AT -Y953 SUPPORT ANGLE HAS A .875" CRACK ON THE UPPER FLANGE. REMOVE AND REPLACE IAW A300 SRM 51-40-54.
LEFT WING TE FLAP 536BB INTERNAL ANGLE WAS CRACKED. REPAIRED IAW REO G21546, REV IR.
LEFT WING CENTER FLAP WAS DENTED BETWEEN RIBS 14 AND 15, -10.5 FROM FRONT SPAR AND 79 INCHES FROM FLAP INBD EDGE. REPAIRED THE FLAP IAW REO-G20545, REV IR.
LEFT WING TIP LOWER SURFACE WAS DENTED AND CRACKED AFT OF THE WING TIP. REPAIRED IAW SRM 57-30-11.
FWD CARGO DOOR CUTOUT, FWD UPPER END DEPRESSOR SEAL WAS DAMAGED. REMOVED & REPLACED THE SEAL DEPRESSOR IAW SRM 51-40-21.
INSPECTION TYPE:12YRLEFT WING CENTER FLAP LOWER SURFACE HAS NUMEROUS DENTSREPAIRED IAW UPS EO A300-5750-69637-A AND HAECO REO G21541 REV IR BY CUTOUT OF DAMAGE AND INSTALLATION OF REPAIR DOUBLER.
FUSELAGE SKIN DOUBLER GOUGED BETWEEN FRAMES 84 AND 86, STRINGER 44L AND 44R. REFABRICATED THE DOUBLER IAW SRM 53-10-12, REPAIR 13
FWD CARGO BAY AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, RBL 40 WAS CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.
LEFT WING CENTER FLAP TRAILING EDGE, LOWER SKIN BETWEEN RIB 17 AND 18, DENTED. REPAIRED THE LT WING FLAP IAW EO A300-5750-69636-A, AND REO G21540 REV IR.
FWD CARGO BAY AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, LBL 40 WAS CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.
FWD CARGO BAY AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, LBL 22 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT FRAME IAW SRM 51-40-21.
FWD CARGO BAY AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, RBL 22. REMOVED AND REPLACED IAW SRM 51-40-21.
FWD CARGO BAY AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, LBL 62 WAS CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.
AVIONICS COMPARTMENT FLOOR SUPPORT ANGLE WAS CRACKED AT FRAME 10, RBL 37. REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IAW SRM 51-40-21.
LAVATORY MIRROR AUX LIGHT INOPERATIVE. REPLACED THE LAMPS LAVATORY MIRROR LIGHT IAW AMM 33-51-21-0401. OPS CHECKED GOOD.
ENTRY DOOR SLIDE WILL NOT ARM. THIS ARMING LEVER WILL ONLY MOVE SLIGHTLY AND THEN BINDS. DOOR OPENS & CLOSES NORMALLY. DOOR VERIFIED CLOSED & LOCKED. ADJUSTED SLIDE SLEEVE TO GIRT BAR IAW AMM 52-10-00. ARM LEVER HAS FULL TRAVEL.
STRINGER 38L IS DAMAGED BETWEEN FRAMES 20 & 21. THIS IS CONSIDERED MAJOJR REPAIR. REPAIRED IAW SRM 53-10-14, FIG 210.
STRINGER 39L FOUND DAMAGED BETWEEN FRAMES 20 & 21. THIS IS CONSIDERED A MAJOR REPAIR. REPAIRED IAW SRM 53-10-14, FIGURE 210.
HOLE IN FUSELAGE SKIN AT FRAME 20, STRINGERS 30 - 39L. SKIN DAMAGED CONSIDERED A MAJOR REPAIR. REPAIRED IAW SRM 53-10-12.
CABIN PRESSURE REGULATOR NR 2 FAILED IN FLIGHT. NR 1 SYSTEM WAS ON DEFFERAL, THEN NR 2 FAILED. EMERGENCY DECLARED. REPLACED THE NR 2 CABIN PRESSURE CONTROLLER IAW MM 21-31-11-0401. ACCOMPLISHED REQUIRED TESTS. OPS CHECKED GOOD.
LAVATORY EMERGENCY LIGHT IS BURNED OUT. R & R THE LIGHT IAW MM 33-51-21-0401. OPS OK.
GOUGE AND DENT TO UPPER FACE SHEET OF FLOOR PANEL MAIN CARGO DECK. FABRICATED NEW PANEL IAW EO A300-5320-40552.
MAIN CARGO DECK FLOOR PANEL GOUGED AND DENTED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552B
MAIN CARGO DECK FLOOR PANEL GOUGED AND DENTEDFABRICATED NEW PANEL PER EO A300-5320-40552B
INSPECTION TYPE:10YR, NR 1 PYLON RIB 18 FWD AND AFT SHACKLE HAVE CORROSION, NICKS, AND CHAFING. REPLACED SHACKLE.
INSPECTION TYPE: 10 YR, NR 1 PYLON RUB 18 FWD AND AFT SHACKLES HAVE CORROSION, NICKS, AND SCRATCHES. REPLACED SHACKLE.
INSPECTION TYPE:1C, 2AFT PIT FWD BULKHEAD LT SIDE PANEL SUPPORT CORRODED AT FRAME 54. REMOVED BRACKET, FABRICATED AND REINSTALLED IAW AB DWG A53440767202, SRM 53-15-18 AND SRM 51-40-21.
INSPECTION TYPE:123C, SIDEWALL PANEL 132HW DAMAGED AROUND SEVERAL FASTENER HOLES. REPAIRED IAW AMM 25-00-00.
INSPECTION TYPE:124CRH, ELEVATOR UPPER SURFACE T/E SHOWS INDICATIONS OF WATER BETWEEN ER 10 & ER 13. AREA IS AROUND SCREW 21 FROM OTBD SIDE OF ELEVATOR AND MARKED IN RED. EVALUATED AREA AND REPAIRED WITNESS HOLES IAW SREO A300-5500-43303-B.
INSPECTION TYPE:124CRH, ELEVATOR UPPER SURFACE SKIN T/E SHOWS INDICATION OF WATER BETWEEN ER 10 & ER 13. AREA IS AROUND SCREW 22 FROM OTBD OF ELEVATOR AND MARKED IN RED. EVALUATED AREA & REPAIRED WITNESS HOLES IAW SREO A300-5500-43303-B.
INSPECTION TYPE:124CRH, ELEVATOR UPPER SKIN T/E SHOWS INDICATIONS OF WATER BETWEEN ER 10 & ER 13. AREA IS AROUND SCREW 23 FROM OTBD SIDE OF ELEVATOR AND MARKED IN RED. EVALUATED AREA AND REPAIRED WITNESS HOLES IAW SREO A300-5500-43303-B.
INSPECTION TYPE:124C, RT ELEVATOR UPPER SKIN T/E SHOWS INDICATIONS OF WATER BETWEEN ER 10 & ER 13. AREA INCLUDES SCREWS 17 AND 18 FROM OTBD SIDE OF ELEVATOR AND MARKED IN RED. EVALUATED WATER INDICATIONS AND REPAIRED WITNESS HOLES IAW IAW SREO A300-5500-43303-B.
INSPECTION TYPE: 123C, SIDEWALL PANEL 131HW DAMAGED AROUND SEVERAL FASTENER HOLES. REPAIRED IAW AMM 25-00-00.
INSPECTION TYPE: 10YR, FWD CARGO CEILING PANEL 132LC DEBONDED AT CORNER. REPAIRED IAW SRM 51-77-11.
INSPECTION TYPE:10YR, BULK CARGO SLOPE PANEL 161-GW HAS DENTS ON THE TOP SIDE. REPAIRED THE DENTS IAW SRM 51-77-10, 51-77-11.
INSPECTION TYPE:10YR, CABIN OVERWING AREA FR 49 CROSSBEAM AT -Y450 TO -Y953 IS BOWED REPLACED CROSSBEAM SRM 51-40-21.
INSPECTION TYPE:10YR, CABIN OVERWING AREA FR 48 CROSSBEAM AT -Y450 TO -Y953 IS BOWED REPLACED CROSSBEAM IAW SRM 51-40-21.
INSPECTION TYPE:10YR, CABIN OVERWING AREA FR 50 AT -Y450 TO -Y953 IS BOWED. REPLACED CROSSBEAM IAW SRM 51-40-21.
INSPECTION TYPE:10YR, CABIN OVERWING AREA FRAME 51 AT -Y450 TO -Y953 IS CRACKED. REPLACED CROSSBEAM IAW A300, SRM 51-40-21.
INSPECTION TYPE:10YR, PANEL NR 162-CW HAS SEVERAL DENTS ON THE TOP SURFACE. REPAIRED THE DENTS IAW SRM 51-77-10, 51-77-11.
INSPECTION TYPE:10YR, PANEL 161 CW HAS SEVERAL DENTS ON TOP SURFACE REPAIRED DENTS IAW SRM 51-77-10, 51-77-11.
INSPECTION TYPE: 10YR, AFT CARGO COMPARTMENT BULKHEAD, FR 54, LT UPPER PANEL SUPPORT BRACKETS. R & R IAW DWG.
INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FWD BULKHEAD, FRAME 54, LT UPPER PANEL SUPPORT BRACKETS CRACKED. R & R IAW DWG A5341012301, REV J.
INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 161LFF HAS DENTS. REPAIR IAW EO A300-5320-42722-E AND SRM 53-10-20-202, 51-77-10, 51-77-11.
INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL NR 161-JF HAS PUNCTURE ON TOP SIDE. REPAIRED IAW EO 5320-42722-E, SRM 51-77-10, 51-77-11, AND 51-21-10.
INSPECTION TYPE:10YR, PANEL 161 DW CRACKED IN CENTER OF PANEL. REMOVED DAMAGED, PREPARED AREA, FILLED AREA, SMOOTHED REPAIR IAW SRM 51-77-10 AND 51-77-11, TOPCOATED IAW SRM 51-21-10.
INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 162MF HAS DENTS. REPAIR IAW EO A300-5320-A2722-E AND SRM 53-10-20-201, 51-77-10, 51-77-11.
INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 161 MF HAS DENTS REPAIR IAW EO A300-5320-42722-E AND SRM 53-10-20-201, 51-77-10, 51-77-11.
INSPECTION TYPE:1C2C, INTERNAL EMPENAGE, BETWEEN FRAME 86 AND FRAME 87, BL3OR DEFORMED. INTER COSTAL REMOVED, FABRICATED, INSTALLED WEBPLATE IAW DWG A53986733000, SRM 51-40-21, 57-21-10, 51-23-10.
INSPECTION TYPE:1C2C, INTERNAL EMPENAGE, BETWEEN FRAME 86 AND FRAME 87, BL 30R DEFORMED INTERCOSTAL. REMOVED, FABRICATED, INSTALLED STIFFENER IAW DWG A53986733000, SRM 51-21-10, 51-23-10, AND 51-40-21.
INSPECTION TYPE:10YR, FWD PIT SIDEWALL PANEL 131FW HAS 2 EA CRACKS ON BACKSIDE NEXT TO BLOWOUT PANEL. REMOVED DAMAGED AREA PREPARED AREAS, FILLED AREA SMOOTHED AREA IAW SRM 51-77-10 AND 51-77-11. TOPCOATED AREAS IAW SRM 51-21-10.
INSPECTION TYPE:10YR, DOOR LINER 813A2 CRACKED. PREPARED AREA, MAT:ID WET LAY UP, CURED, ABRADED, IAW SRM 51-77-10 AND 51-77-11. TOPCOATED IAW SRM 51-21-10.
INSPECTION TYPE:10YR, FWD PIT SIDEWALL PANEL 131 MW HAS PUNCTURES ON TOP SIDE REMOVED DAMAGED, FILLED, SMOOTHED IAW SRM 51-77-11 TOPCOATED IAW SRM 51-21-10.
INSPECTION TYPE:10YR, FWD PIT SIDEWALL PANEL 131TW HAS PUNCTURED ON TOP SIDE REMOVED DAMAGED, PREPARED AREA FILLED AREA, SMOOTHED AREA IAW SRM 51-77-10 AND 51-77-11. TOPCOATED REPAIR AREA IAW SRM 51-21-10.
INSPECTION TYPE:1C,2BULK CARGO SIDEWALL PANEL 161MW HAS PUNCTURE ON TOP SIDE, REPAIRED IAW SRM 51-77-10 AND 51-77-11.
INSPECTION TYPE:1C, 2 FWD BULKHEAD PANEL 151DW HAS PUNCTURE ON TOP SIDE, REPAIRED IAW SRM 51-77-10 AND 51-77-11.
INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL 151VF HAS A PUNCTURE ON BACK SIDE. REPAIRED IAW E0 A300-5320-42722-E.
INSPECTION TYPE:10YR, AFT FLOOR PANEL 151TF HAS PUNCTURE ON BACK SIDE REPAIR IAW EO NR 5320-42722-E AND SRM 53-10-20-201, 51-77-10 / 51-77-11.
INSPECTION TYPE:1C2C, LEFT ALL SPEED AILERON INBD AFT CORNER DELAMINATED. REPAIRED IAW SRM 57-61-11, PARA 4E AND 51-77-12, PARA 4.D, FIG 222 USING DOUBLER .020 2024-T3 CLAD, HONEYCOMB CORE F0N1-4309-70 5056, PASTE ADHESIVE.
INSPECTION TYPE: 1C2C, PANEL 323AR ATTACH BRACKET BROKEN. R & R BRACKET.
INSPECTION TYPE:1C2C, SUPERNUMERARY FLOOR PANEL 222KG IS CRACKED. REPAIRED FLOOR PANEL 222KG IAW SREO A300-5320-42721-F.
INSPECTION TYPE:1C2C, AFT CARGO FLOOR PANEL 161KF HAS 2 BAD INSERTS AND DELAMINATION BOTTOM SIDE. REPAIRED THE FLOOR PANEL IAW SREO A300-5320-42721-F.
INSPECTION TYPE:C1C2, 2 RADIO ALTIMETER ANTENNA DAMAGED. R & R IAW SRM 51-40-21.
INSPECTION TYPE: 10YR, FWD CARGO DOOR CUTOUT UPPER FWD JAM WIRE BUNDLE CLAMP MOUNT BRACKET BENT AND CRACKED. REMOVED BROKEN WIRE BUNDLE BRACKET AND INSTALLED NEW BRACKET IAW SRM 51-40-21.
INSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 1315G HAS CRACK ON BACK SIDE. REMOVED DAMAGED AREA, FILLED AREA WITH EPOXY EA934 A/B IAW SRM 51-77-11.
INSPECTION TYPE:10YR, PANEL 132PG HAS EDGE DAMAGE. REPAIRED PANEL IAW EO A300-5320-42721-F.
INSPECTION TYPE:10YR, PANEL 132QG IS PUNCTURED. REPAIRED PANEL IAW EO A300-5320-42721-F.
INSPECTION TYPE:1C2C, PANEL 131MG HAS SEVERAL PUNCTURES. REPAIRED FLOOR PANEL IAW EA A300-5320-42721-F.
INSPECTION TYPE:1C, 2 MAIN CABIN FLOORBEAM LT AT FRAME 79, Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-59902-B.
INSPECTION TYPE:1C, 2 MAIN CABIN FLOOR CROSSBEAM RT AT FRAME 79-Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-59902-B.
MAIN CABIN DOOR SLIDE WILL NOT ARM, CLEANED AND LUBED GIRT BAR FLOOR FITTINGS AND SLIDERS. OPS CK GOOD, AMM 25-61-20. THIS CLEARS M535049.
AFTER TAKE OFF LANDING GEAR FAILED TO RETRACT, ECAM DIRECTED GEAR DOWN ALL GEAR DOWN LOCKED INDICATIONS NORMAL. R & R LANDING GEAR CONTROL SWITCH IAW MM 32-31-11-0401. GROUND CHECKED NORMAL. OK FOR SERVICE. PERFORMED OPS CHECK OF LANDING GEAR SELECTOR VALVE IAW MM 32-31-12-0601. GROUND CHECKED NORMAL. OK FOR SERVICE.
EMERGENCY LIGHT WILL NOT TEST PROPERLY, LIGHTS STAYED ON AFTER TEST. R & R POWER SUPPLY.
EMERGENCY DECLARED -45 MINS FROM LANDING GREEN SYS HYD QTY SLOW LOSS OF QTY IN FLIGHT. FOUND GREEN HYD SYS TRANSMITTER INTERMITTENT. REPLACED GREEN RES HYD QTY TRANSMITTER IAW MM 29-31-11-0401. OPS CHECK GOOD.
INSPECTION TYPE:3C BULK CARGO FLOORBOARD 161GF HAS CRUSHED COMPOSITE MATERIAL AND MISSING TOP LAYER. FABRICATED BULK CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.
ON CLIMBOUT NR 2 ENGINE OIL PRESSURE WAS LOST. DIDN'T APPEAR TO GO TO ZERO, BUT WENT DOWN TO 8 PSI. SHUTDOWN NR 2 ENGINE IN FLIGHT. TROUBLESHOT IAW TSM 79-00-40. R & R OIL PRESSURE TRANSMITTER. IAW AMM 79-33-11-401. OPS CHECKED NORMAL ON GROUND.
INSPECTION TYPE: SV, MAIN DECK CARGO FLOOR PANEL 231WG PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B PARA 6A.
INSPECTION TYPE: SV, MAIN DECK CARGO FLOOR PANEL 222AG BROKEN. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX B.
INSPECTION TYPE:5YR, FLOOR PANEL 251JF IS DELAMINATED. FABRICATED NEW FLOOR PANEL 251JF IAW EO A300-5320-40552-A.
INSPECTION TYPE:5YR, FLOOR PANEL 251KM IS DELAMINATED. FABRICATED NEW FLOOR PANEL 251KM IAW EO A300-5320-40552-A.
INSPECTION TYPE:5YR, FLOOR PANEL 231KG IS CRACKED. FABRICATED NEW FLOOR PANEL 231KG IAW EO A300-5320-40552-A.
INSPECTION TYPE:5YR, MAIN CABIN COMPT, ZONE 230, FLOORBOARD 231KH IS CRACKED ON LOWER SURFACE AROUND INSERT. REPAIRED DAMAGED MAIN DECK FLOORBOARD 231KH REF EO A300-5320-43099-A AND STA, SA, EA 300-5320-01-A3124.
INSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR242NK IS BROKEN AT EDGE. FABRICATED MAIN CABIN FLOORBOARD NR242NK IAW EO A300-5320-40552-A, APPENDIX B.
INSPECTION TYPE:5YR, MAIN CABIN OVER WING FLOOR SUPPORT IS BENT AT FR 49 BETWEEN -Y450 AND -Y953. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SUPPORT AT FR 49 BETWEEN -Y450 AND -Y953 IAW EO A300-5310-42744-A AND STA-SA EA 300-5310-01-A3110 IR DATED 05/19/11.
INSPECTION TYPE:5YR, MDCC FLOOR PANEL 241RM IS CRACKED. FABRICATED NEW MDCC FLOOR PANEL 241RM IAW EO A300-5320-40552-A.
INSPECTION TYPE:5YR, MAIN CARGO COMPT ZONE 252, FLOORBOARD 252HJ IS CRACKED ON LOWER SURFACE AT INBD FWD AREA. REPAIRED MAIN DECK FLOORBOARD 252HJ REF EO A300-5320-43100-A AND STA, SA, EA 300-5320-01-A3126.
INSPECTION TYPE:5YR, MAIN CARGO COMPT ZONE 252, FLOORBOARD 252RG IS CRACKED ON LOWER SURFACE FWD INBD CORNER. REPAIRED MAIN DECK FLOORBOARD 252RG REF EO A300-5320-43102-A AND STA, SA, EA 300-5320-01-A3125 REV I/R.
INSPECTION TYPE:5YR, MAIN CABIN COMPT ZONE 241, FLOORBOARD 241ZK IS CRACKED ON LOWER SURFACE AT INBD FWD AREA. REPAIRED MAIN DECK FLOOROARD 241 ZK REF EO A300-5320-43103A AND STA, SA, EA 300-5320-01-A3124 REV I/R.
INSPECTION TYPE:5YR, MAIN CABIN OVERWING FLOOR SUPPORT IS BENT AT FR48 BETWEEN -Y450 AND -Y 953 AS MARKED. REMOVED, FABRICATED AND INSTALLED MAIN CABIN OVERWING FLOOR SUPPORT CROSSBEAM AT FR48 BETWEEN -Y450 AND -Y953 REF STA, SA, EA 300-5310- 01-A3110 I/R AND EO A300-5310-42744-A.
INSPECTION TYPE:5YR, MAIN CABIN OVERWING FLOOR SUPPORT IS BENT AT FR50 BETWEEN -Y450 AND Y9 53 AS MARKED. REMOVED, FABRICATED AND INSTALLED MAIN CABIN FLOOR SUPPORT CROSSBEAM BETWEEN -Y450 AND -Y953 REF STA, SA, EA 300-5310-01-A3110 I/R AND EO A300-5310-42744-A.
REPAIR OF BULK CARGO FLOORBOARD NR161HF. FABRICATED BULK CARGO FLOORBOARD NR161HF IAW EO A300-5320-16407-E, APPENDIX D.
ON POST FLIGHT WALKAROUND, FOUND TAIL SKID AND DRAIN PIPE DAMAGED. TAIL STRIKE REPAIR DAMAGE PERFORMED IAW WOTD M-303681-EMBOD & EO A300-5100-43246-A.
ON POST FLIGHT WALKAROUND FOUND TAIL SKID AND DRAIN PIPE DAMAGED. (OPEN)
INSPECTION TYPE:N/A EVACUATION SLIDE WARNING SYSTEM LIGHT ON CABIN DOOR INOP. BUZZER DOES NOT WORK. DEFERRED EVACUATION SLIDE WARNING SYSTEM LIGHT IAW MEL 52-73-001-1. REMOVED AND REPLACED AUTONOMOUS PWR SUPPLY UNIT IAW MM 52-73-18-04. OPS CHECK GOOD IAW 52-73-00-05. THIS CLEARS M369580.
FUEL MIGRATION IN FLIGHT. EMERGENCY DECLARED. UPON LANDING, CAPT NOTIFIED DISPATCHER HAD OBSERVED AN ABNORMAL DECREASE IN THE FUEL QUANTITY OF HIS LEFT OUTER TANK. R&R LT. O/B REFUEL/DEFUEL VALVE IAW 28-25-12-04 OPS & LK CHECK GOOD. AFTER REPEATED ATTEMPTS WITH DIFFERENT FUEL CONFIGURATIONS DID NOT GET ANY LOSS OF MIGRATION OF ANY FUEL.