N402FE
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
181 reports on file, 1995-07-13 – 2010-07-16.
Part: SKIN — CORRODED (ZONE 600) · airframe 35,953 hrs · 31,138 cycles
RT WING UPPER SKIN SURFACE 8 INCH AFT OF REAR SPAR AND RIB 4 HAS 4 SQ INCH OF CORROSION COMMON TO FASTNER HEAD. REPAIR ACCOMPLISHED IAW EA 6-5730-135225 IAW APPROVED DATA REF 6, RAS/BAE/1013408/2010, ISSUE A. THE REPAIR IS IAW THE A/B REPAIR RECOMMENDATION WHICH IS TO BLEND THE AREA SMOOTH , OVERSIZE FASTNERS AND REPROTECT WITHOUT REINFORCEMENT.
Part: FRAME — DENTED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
FUSELAGE INTERNAL STRUCTURE AT FR 54.2 HAS (2 EA) AREAS DENTED. AREA NR1=.0781 IN.D X .7500 IN W . AREA NR2 =.0469 IN D X .5 IN W BETWEEN STRINGER 12-15 LT SIDE. REPAIRED FRAME IAW SRM 53-10-12, PARA 5, REPAIR 202, AND EA 6-5310-135243.
Part: FITTING — CORRODED (NR 2 PYLON) · airframe 35,953 hrs · 31,138 cycles
NR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE HAS CORROSION AROUND 4 EA MOUNT HOLES (APPROX 6 SQ IN TOTAL) REMOVED CORROSION FROM NR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE. AROUND 4 EA HOLES IAW SRM 54-51-81 PAGE 101-102 FIG 104 NDT CHECK C/W IAW NTM 51-60-00NO DEFECTS NOTED. REPAIRED NR 2 PYLON IAW EA 6-5450-135226 BY FABRICATING 3 EA BUSHINGS.
Part: FRAME — DENTED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
FUSELAGE INTERNAL STRUCTURE FR 54.3 L HAS A DENT APPROX 3/32 INCH DEEP AND 1.5 IN DIAM. BETWEEN STR 14-13 LT MEASURED DENT ON FR 54.3 AT STR. 13L-14L FOUND TO BE OUT OF LIMIT IAW SRM 53-16-13 . REPAIRED FR 54.3L IAW EA 6-5310-135243 INSTRUCTIONS AND SRM 53-10-12 PAR 5 AND REPAIR 202.
Part: SPAR — CORRODED (VERTICAL STAB) · airframe 35,953 hrs · 31,138 cycles
VERTICAL STAB T/E PANEL ATTACH ANGLEAT RT SIDE HAS APPROX 2 SQ INCH OF VISIBLE CORROSION BETWEEN RIB 9 AND AT RIB 10 AT STA 286 AND 309 (2 EA LOCATIONS) BETWEEN RIB. REMOVED CORROSION FROM VERTICAL STAB T/E PANEL ATTACH ANGLE RT SIDE BETWEEN RIB 9 AND RIB 10 IAW SRM 51-74-10, PAG 201. CHECKED LIMITS IAW SRM 55--30-00, PAGE 104 FOUND TO BE OUT OF LIMITS. REPAIRED VETICAL IAW SRM 55-31-21, FIG 203, PAGE 217/218.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 35,953 hrs · 31,138 cycles
FWD CARGO DOOR HAS DAMAGE STRUCTURE WEB AND HOLE BETWEEN FR 22A AND FR 23 AT BEAM 2. REMOVED DAMAGED AREA OF DOOR SKIN BY CUT OUT OF APPROX 2 IN X 3 IN AND INSTALLED FRAME, STRINGER AND SKIN REPAIR FILLERS AND DOUBLER BETWEEN FR 22 AND FR 23 AT BEAM NR 2 IAW SRM 52-30-00, FIG 20. ALSO REF SNRM N00596.
Part: RIB — DAMAGED (RT KRUEGER FLAP) · airframe 35,953 hrs · 31,138 cycles
RT WING KRUEGER FLAP FWD OTBD CORNER HAS IMPACT DAMAGE TO THE EXTERIOR SKIN & CLOSE OUT RIB. FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, AND INSTALLED ON RT WING KRUEGER FLAP IAW SRM 51-40-21.
Part: RIB — GOUGED (LT KRUEGER FLAP) · airframe 35,953 hrs · 31,138 cycles
LT WING L/E KRUEGER FLAP LOWER LIP OTBD L/E GOUGED, 2 SQ INCHES FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, IAW DWG A57843755 AND INSTALLED ON LT WING KRUEGER FLAP OTBD L/E IAW SRM 51-40-21.
Part: SHEAR TIE — CRACKED (CARGO DOOR) · airframe 35,953 hrs · 31,138 cycles
FWD CARGO DOOR STRUCTURE SKIN SUPPORT ANGLE AFT OF ACTUATOR HINGE FITTING LOWER END HAS 1 IN CRACK REMOVED DAMAGED ANGLE AND STRINGER CLIPS, FABRICATED REPLACEMENT ANGLE AND 2 EA STRINGER CLIPS IAW MFG DWG A52370111 AND DWG A52370142 AND INSTALLED REPLACEMENT PARTS ON LWR FWD CARGO DOOR BETWEEN FR 22 AND FR 23, BEAM NR 2 IAW SRM 51-40-21. ALSO REF SNRM N01901.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MAIN DECK CARGO COMPT FLOORBEAM CORRODED ON UPPER SURFACE,FR 14 AT SEAT TRACK 3 LT REMOVED LEVEL 1CORROSION. REMOVED, FABRICATED REPLACEMENT TRACK SECTION AND REPLACED DAMAGED SECTION OF TRACK NR3 LT BETWEEN FR 10 AND FR 15A IAW SRM 51-72-10 AND SRM 53-12-15.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 5 RT AT FR 34 TO FR 36 HAS CORROSION AT 3 EA LOCATIONS UPPER SURFACE, APPROX 3 SQ IN REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK, FABRICATED REPLACEMENT SECTION OF TRACK IAW DWG 537B1054 AND INSTALLED REPLACEMENT TRACK AT TRACK 5 RT BETWEEN FR 26/32 AND FR 39 IAW SRM 51-72-10.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 6LT INBD SIDE UPPER SURFACE IS CORRODED JUST FWD OF FR 33, APPROX 1 SQ IN REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF SEAT TRACK 6 LT BETWEEN FR 33 AND FR 36 AND INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 53-10-16, FIG 208A, PG 250C/250D.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
CLS AT FR 36 BETWEEN SEAT TRACKS 3 RT AND 2 RT FWD SIDE LWR SURFACE REPAIR ANGLE CRACKED ON RADIUS, APPROX 1.5 IN LONG REMOVED EXISTING REPAIR ANGLE AT FRAME 36 BETWEEN SEAT TRACKS NR 2 RT AND NR 3 RT FWD SIDE FLOORBEAM, FABRICATED NEW REPAIR ANGLE AND INSTALLED IAW SRM 53-10-15, FIG 206 SHEET 3, PAGES 231/232 AND IN REF TO EA 6-5321-29160 PREVIOUSLY REPAIRED. ALSO REF SNRM N01960.
Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
FRAME 26 SEAT TRACK 4 LT OTBD JUST AFT OF CLS, FOUND CORROSION IN FLOOR PANEL, APPROX 1 SQ INCH REMOVED LEVEL 1 CORROSION. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-10-00, FIG 102. R & R SHEAR PLATE BETWEEN FR 26/32 AND FR 36 AND SEAT TRACK 4LT AND SEAT TRACK 5LT IAW SRM 51-72-10.
Part: PLATE — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
SUB FLOOR CORRODED APPROX 1 SQ IN AFT OF FR 25 BETWEEN SEAT TRACKS 4 LT AND TRACK 3 LT REMOVED LEVEL 1 CORROSION. R & R SUB FLOOR THRUST PLATE BETWEEN FR 25 AND FR 26/32 AND BETWEEN SEAT TRACKS 3 LT AND 4 LT IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MAIN DECK CARGO COMPT CROSSOVER BEAM HAS CORROSION ON UPPER SURFACE FR 14, BETWEEN SEAT TRACKS 3 LT AND 4 LT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED BEAM, FABRICATED REPLACEMENT BEAM IAW DWG A53611789 AND INSTALLED REPLACEMENT BEAM IAW SRM 51-75-10.
Part: WEB — DAMAGED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
WEB BETWEEN FRAME 12A AND 14, BENEATH TRACK 3 LT, IS DAMAGED. REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 12A AND FR 14 AT SEAT TRACK 3 LT IAW SRM 51-75-10.
Part: WEB — DAMAGED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
WEB BETWEEN FR 14 AND FR 15 BENEATH TRACK 3 LT IS DAMAGED REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 14 AND FR 15 AT SEAT TRACK 3 LT IAW SRM 51-75-10.
Part: WEB — DAMAGED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
WEB HAS DAMAGED HOLES AT FR 10 AND FR 12A SEAT TRACK 3 LT REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 10 AND FR 112A AT SEAT TRACK 3 LT IAW SRM 51-75-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
AFT CARGO COMPT BILGE AREA, STR 44 LT HAS CORROSION ON VERTCAL LEG FROM FR 62 TO FR 63,APPROX 10 SQ IN. REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF STR 44 LT AND INSTALLED STRINGER REPAIR AT STR 44 LT BETWEEN FR 62 AND FR 63 IAW SRM 53-10-14, FIG 201, PAGE 203/204.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MDCC FLOORBEAM HAS CORROSION ON UPPER SURFACE AT FR 14 6IN. BETWEEN SEAT TRACK 3L AND 4L. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND CROSSBEAM SECTION OUT OF LIMITS IAW SRM 51-74-10 AND SRM 53-10-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-21.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
MDCC SEAT TRACK 5L HAS A 4 SQ INCH AREA OF CORROSION BENEATH FLOOR PANEL FR 16A. REMOVED CORROSION IAW SRM 51-74-10 , CHECKED LIMITS IAW SRM 53-10-15 FIG 101 FOUND TO BE OUT OF LIMITS . REPLACED SEAT TRACK 5L , AT FR 16A. IAW SRM 51-40- 21 AND 51-72-10.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MAIN DECK FLOORBEAM FWD FACE HAS 0.188 INCH CRACK , ON FR 38 , 67 INCHES FROM CTR LINE, LT SIDE. TRIMMED OUT DAMAGE AREA IAW SRM 53-10-15, FIG 201, NDT CHECK IAW NTM 51-10-08. FOUND CRACK EXTENDS TO 1.0 INCH. CUT OUT CRACK DAMAGE AREA IAW SRM 53-10-15, FIG 203 , NDT CHECK VERIFIED NO CRACK AFTER CUT OUT. REPAIRED CROSSBEAM IAW SRM 53-10-15, FIG 203, PAGE 249/250.
Part: SKIN — CORRODED (RT ELEVATOR) · airframe 35,953 hrs · 31,138 cycles
RT ELEVATOR UPPER SURFACE HAS APPROX 1.5 SQ IN OF CORROSION AT APPROX. ER36 1 IN. FWD OF AFT EDGE REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND UPPER SURFACE 1 IN FWD OF AFT EDGE, OUT OF LIMITS IAW SRM 55-10-00 FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-21-11, PGS 247-252 FIG 209 AND SRM 51-40-21.
Part: SKIN — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
RT ELEVATOR LWR SURFACE SKIN HAS CORROSION 56 INCHES FROM OTBD END, 6 INCHES FWD OF AFT EDGE APPROX 5 SQ IN TOTAL , APPROX ER 34 REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10 , FOUND LOWER SURFACE OUT OF LIMITS IAW SRM 55-10-00. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 55-21-11, FIG 209, PAGES 247-252.
Part: SKIN — CORRODED (RT ELEVATOR) · airframe 35,953 hrs · 31,138 cycles
RT ELEVATOR LWR SURFACE CTR SPLICE HAS CORROSION 8 IN FWD FROM AFT EDGE APPROX 1.5 SQ IN APPROX STA ER21. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND LWR SURFACE CTR SPLICE OUT OF LIMITS IAW SRM 55-10-00. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM55-21-11, PGS 247-252, FIG 209 AND SRM 51-40-21.
Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
BULK CARGO COMPT FLOOR STRUCTURE FRAME 69 RBL 20 FLOORBEAM SUPPORT HAS MISDRILLED HOLE THRU UPPER CHORD FWD SIDE. REMOVED DAMAGE AND FABRICATED SPLICE IAW SRM 53-10-15 PG 241/242 FIG 207. INSTALLED REPAIR IAW SRM 53-10-15 AND SRM 51-40-21
Part: SUPPORT FITTING — CRACKED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
AFT CARGO BILGE AREA- FR 54 BULKHEAD SUPPORT FITTING AT STR 53R HAS A 1 IN. CRACK ON OTBD. SIDE ABOUT 3 IN AFT OF BULKHEAD. REMOVED SPLICE AND 2 EA ATTACH FITTINGS IAW SRM 51-72-10, VERIFIED MATERIAL 7175-T7351 08-101155 IAW SRM 53-15-14, FABBED SPLICE FITTING IAW DWG 53811099, ALODINED FITTING IAW SRM 51-21-10, PRIMED FITTING IAW SRM 51-75-10, PART MARKED 1 EA. FITTING IAW GMM 7-01001, LOCATED AND DRILLED FITTING IAW A310-200 SRM 51-72-10, APPLIED TOP COAT IAW SRM 51-75-10 PARA 3 AND 51-23-10. INSTALLED SUPPORT FITTING AT STR 53R IAW SRM 51-72-10 AT FR 54.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 2L APPROX 18 IN FWD OF FR33 IS CORRODED APPROX 1 SQ IN REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16, FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK 2L BETWEEN FR 32 AND FR 33 IAW SRM 53-10-16 FIG 208.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
5L SEAT TRACK HAS CORROSION AT 7 EA. LOCATIONS BETWEEN FR 33 AND FR38.1 APPROX 15 SQ INCH REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REPAIRED SEAT TRACK IAW DWG R537, B1054, REV B.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
MDCC SEAT TRACK HAS CORROSION 4 EA AREAS ON UPPER SURFACE BETWEEN FR 15 AND FR 16A AT 4L. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REPLACED SEAT TRACK 4L, BETWEEN FR 15 AND FR 16A IAW SRM 51-40-21 AND SRM 51-72-10.
Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 35,953 hrs · 31,138 cycles
LT WING INBD FLAP LWR T/E SURFACE HAS IMPACT DAMAGE MEASURING 6 IN. X 6 IN. X .32 IN. D REPAIRED IMPACT DAMAGE ON LT WING INBD FLAP LWR T/E SURFACE USING COR REPLACMENT WITH EXTERNAL BONDED METAL DOUBLER IAW SRM 57-53-12, PARA 12, A,B,C FIG 208.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 2R INBD SIDE CORRODED AT 4 EA LOCATIONS FROM APPROX 16 IN FWD OF FR33 TO 10 INCHES AFT OF FR 33 APPROX 5 SQ INCH TOTAL. REMOVED CORROSION IAW SRM 51-74-10 , CHECKED LIMITS IAW SRM 53-10-16 PAGE 103, FIG 101 FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK 2R BETWEEN FR 32 AND FR34 IAW SRM 53-10-16 FIG 208, PAGE 247/248.
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
AFT CARGO COMPARTMENT BILGE AREA STR. 45L HAS CORROSION AT FR60 TO FR60 2 INCHES APPROX TOTAL 2 SQ INCHES. REMOVED CORROSION IAW SRM 51-74-10, CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-00 PAGE 106. REPAIRED STR 45LT BETWEEN FR 60 AND FR 61 IAW A310 SRM 53-10-14, PAGE 203/204, FIG 201A.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 6L HAS 7 AREAS OF CORROSION BETWEEN FR 35 TO FR38 APPROX 10 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101 . REPAIRED SEAT TRACK 6L BETWEEN FR35 AND FR38 IAW SRM 53-10-16, FIG 208A PAGE 250A/250B.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 4L IS CORRODED AT 4 EA LOCATIONS FROM FR 33 TO FR 38.1 APPROX 6 SQ IN. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK 4L IAW SRM 53-10-16, FIG 208, PG 247/248.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
AFT CARGO COMPT FLOORBEAM FR63, RBL 45, PRODUCTION SPLICE HAS CORROSION BETWEEN IT AND T-CHORD APPROX. 5" LONG (EXFOLIATION) REMOVED CORROSION ON AFT CARGO COMPT FLOORBEAM FR 63, RBL 45, IAW A310 SRM 51-74-10 PG 205. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00, FIG 102. REPAIRED AFT CARGO FLOORBEAM AT FR 63 IAW SRM 53-10-15, FIG 207, PG 241/242.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK NR1 HAS 2EA LOCATIONS THAT ARE CORRODED FR 33 TO APPROX 18 IN FWD OF FR 33 REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND TRACK SECTION OUT OF LIMITS IAW SRM 53-10-16. FABRICATED AND INSTALLED SEAT TRACK REPAIR IAW SRM 53-10-16, FIG 205, AREA 1.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 6R HAS 5EA AREAS CORRODED APPROX 6 SQ IN FROM FR 34 TO FR 39 REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REPAIRED SEAT TRACK 6R BETWEEN FR 34 AND FR 39 IAW DWG R537 B1054 REV B AND SRM 51-72-10.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 2R HAS 2EA. LOCATIONS CORRODED BETWEEN FR49 TO FR46. CORROSION IS ON THE OTBD UPPER AND LOWER SURFACE APPROX. 4SQ IN. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16 FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 205.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
FLOORBOARD SUPPORT STRUCTURE THAT TURNS INTO THE 5L SEAT TRACK IS CORRODED, FR 14 TO FR 15 APPROX 72 IN LONG. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL, FOUND FLOOR SUPPORT AND SUPPORT FITTING OUT OF LIMITS IAW SRM 53-10-16. R & R FLOOR SUPPORT AND SUPPORT FITTING PN A5361077820000 IAW SRM 51-72-10.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MDCC SEAT TRACK 4R BETWEEN FRAMES 18 & 19 HAS 5 SQ. INCH OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205 , CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 53-12-16, PB 201.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MDCC SEAT TRACK 3R , AT FR 54.2 HAS 1 SQ INCH OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 , CHECKED SEAT TRACK 3R AT FR 54.2 FOUND OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R AT FR 54.2 IAW SRM 51-72-00.
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
FUSELAGE SKIN STRINGER HAS 1" X 1" CORROSION FWD OF AFT PRESSURE BULK HEAD 10" FWD OF FR 80/82 STR 56R REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, FIG 201. CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-14 PAGE 203/204, FIG 201. REPAIRED STR 56R IAW SRM 53-10-14, PARA 4 PAGE 204/205, FIG 201.
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
AFT CARGO BILGE AREA FR 54 LAST 9 INCHES STR 46 L HAS APPROX 3 SQ IN OF CORROSION. REMOVED CORROSION ON STR 46L AT FR 54 IAW SRM 51-74-10 CHECKED. FOUND OUT OF LIMITS IAW SRM 53-10-14. REPAIRED STR 46L IAW SRM 53-10-14 PAGE 203 AND 204, FIG 201, STRINGER.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
INTERCOSTAL TRACK AT FR 47/48BETWEEN RT NR 2 AND NR 3 SEAT TRACKS HAS CORROSION INSIDE THE SCALLOPS APPROX 1 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10 PAGE 205 , CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-15, FIG 101 . R & R CROSSBEAM IAW SRM 51-75-10, PAGE 1,2,3
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
AFT CARGO COMPT FRAME 58 LT SIDE FLOOR SUPPORT BEAM, LBL 44 UNDER SIDE HAD EXFOLIATION CORROSION APROX 4SQ IN IN TOTAL. REMOVED CORROSION IAW SRM 51-74-10 CHECK AREA FOUND TO BE OUT OF LIMIT IAW SRM 53-10-15. REPAIRED FLOOR SUPPORT BEAM IAW SRM 53-10-15.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
CABIN SEAT TRACK 4L FROM FR 50 TO FR51 HAS APPROX. 8 SQ IN OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 P205. CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 201. REPAIRED SEAT TRACK 4L IAW SRM 53-10-16, FIG 203.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
BULK CARGO COMPT FLOOR STRUCTURE LONGITUDINAL SUPPORT BETWEEN FRAME 65-66, LBL 5. UPPER AND LOWER SURFACES HAVE CORROSION IN AND AROUND FASTENER HOLES, APPROX 10 SQ IN IN TOTAL. REMOVED CORROSION FROM PROFILE IAW SRM 51-74-10 CHECK LIMIT IAW SRM 53-10-00, PG 106 FOUND OUT OF LIMITS. R & R FLOOR PROFILE IAW SRM 51-72-10.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MAIN CABIN FR 54 SEAT TRACK 3R CORROSION ON A FLANGE UPPER SURFACE. REMOVED CORROSION IAW SRM 51-74-10 CHECK LIMIT FOUND OUT OF LIMIT IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 51-40-21.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MAIN DECK CARGO INTERCOSTAL TRACK AT FR 54 BETWEEN RT SEAT TRACKS 2 AND 3 HAS CORROSION INSIDE THE SCALLOPS APPROX 1 SQ IN. REMOVED CORROSION IAW SRM 51-74-10 FOUND OUT OF LIMITS IAW SRM 53-10-15. R & R INTERCOSTAL TRACK AT FR 54 BETWEEN SEAT TRACKS 2 AND 3 R IAW SRM 51-40-21.
Part: ADAPTER — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
INTERCOSTAL TRACK AT FRAME 47/48 BETWEEN LT SEAT TRACKS 2 AND 3 HAS CORROSION INSIDE THE SCALLOPS APPROX .5 SQ IN. REMOVED CORROSION IAW SRM 51-74-10. CHECK LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-15 . R & R ADAPTOR IAW SRM 51-40-21.
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
AFT CARGO COMPT HAS CORROSION AT STRINGER 31 RT FROM FRAME 54.1 TO FRAME 54.1, 12 IN TOTAL AREA APPROX 13 SQ IN. REMOVE CORROSION IAW SRM 51-74-10, CHECK FOUND OUT OF LIMIT IAW WITH SRM 53-10-00, PG 106. REPAIRED STRINGER 31RT IAW SRM 53-10-14.
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
FUSELAGE SKIN STRINGER HAS 1" X 1" CORROSION FWD OF AFT PRESSURE BULKHEAD 10" FWD OF FR 80/82 STR 56L. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, FIG 201, CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-14 PAGE 203/204, FIG 201. REPAIRED STRINGER 56L IAW SRM 53-10-14, PARA 4, FIG 201.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
MDCC SEAT TRACK 2 R FR 54 HAS A 1 SQ IN AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 CHECKED AND FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 101. R & R MDCC SEAT TRACK 2R IAW SRM 51-72-10.
Part: SKIN — DENTED (ZONE 100) · airframe 35,953 hrs · 31,138 cycles
RAMP REPORTED 3 SMALL DENTS 10 IN AFT OF AFT LOWER CARGO COMPT DOOR. REF WRITE UP WRI 53-30 1790. CUT OUT DAMAGE AREA IAW SRM 53-17-12, FIG 205, NDT VERIFIED NO CRACKS IAW NTM 51-10-08. REPAIRED SKIN IAW SRM 53-17-12, FIG 205.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
CORROSION AT MDCC SEAT TRACK 4L BETWEEN FR 54.3 AND FR 58 , DEFECT MEASURES 4 SQ INCHES OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 PAGE 205 , CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101 . R & R SEAT TRACK 4L BETWEEN FR 54.3 AND FR 58 IAW SRM 51-72-10, PAGE 1 TO 3.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
FWD CARGO COMPARTMENT FLOORBEAM HAS 3X1 INCH CORROSION UNDER NR 1L CARGO LOADING ROLLER TRACK AT FR 33. REMOVED CORROSION AND CHECKED MATERIAL LOSS FOUND 100 PERCENT LOSS. REPAIRED FLOORBEAM IAW SRM 53-10-15, PAGE 237.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
AFT CARGO COMPARTMENT BILGE STRINGER 46LT HAS CORROSION AT FRAME 54.3 PLUS 13 IN. REMOVED CORROSION IAW SRM 51-74-10, CHECKED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00 . REPAIRED STRINGER 46 LT IAW SRM 53-10-14, FIG 201.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 4 R BETWEEN FRAMES 74 AND 80/82 HAS 5 EA AREAS OF COROSION, DEFECTS MEASURE 5 SQ IN REMOVED COROSION IAW SRM 51-74-10, PAGE 5. CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-10-16, PAGES 243-245, FIG 208.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 3R BETWEEN FRAMES 53 AND 54 HAS 4 SQ INCHES OF CORROSION IN AND AROUND SCALLOPS. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMIT, FOUND OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK SECTION AND REPAIRED IAW SRM 53-10-16 PARA 7, PAGES 227-232, FIG 205.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
SEAT TRACK 3L, BETWEEN FRAMES 14C & 15B, HAS 2 SQ. INCHES WITH EXFOLIATION CORROSION CHECKED MATERIAL LOSS IAW SRM 53-10-16 FIG 101 AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-10-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,953 hrs · 31,138 cycles
MDCC, SEAT TRACK 3R, HAS 3 SQ. INCHES OF CORROSION AT FR 15B REMOVED CORROSION IAW A310 SRM 51-74-10. CHECKED LIMITS , FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 101. R & R SEAT TRACK 3R BETWEEN FR 15A TO FR 19 IAW SRM 53-10-16 AND SRM 51-72-10.
Earlier reports · 1995–2009 · 118 reports
2009
Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 35,206 hrs · 30,538 cycles
ON TAXI OUT RECEIVED OVERBOARD EXTRACT VALVE FAULT. FOLLOWED MEL BUT WOULD NOT MAINTAIN PRESSURIZATION IN FLIGHT. DIVERT TO ATL PER GOC. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-23-06 CATEGORY: C. VENT OVBD VALVE INOP, VALVE MANUALLY SET PARTIALLY OPEN, FOR GROUND OPERATION OF AVIONICS, CONDITIONED AIR MUST BE AVAILABLE AND USED." REMOVED AND REPLACED OVBD EXTRACT VALVE PER MM 21-23-13-4. OPS CHECKED NORMAL.
2007
Part: SWITCH — MISALIGNED (ZONE 800) · airframe 34,265 hrs · 29,894 cycles
FWD CARGO DOOR UNLOCK WARNING AND ECAM MESSAGE AT 18,000' AND PSID 7.0, SPEED 340 KTS. PREECEDING THE CARGO DOOR UNLOCK WARNING BY LESS THAN 1" WAS A LOUD "THINK" FROM UNDERSIDE OF AIRCRAFT. SLOWED TO 240 KTS, NO CHANGE. DEPRESSURIZED AND DESCENDED AND PSID 4.0 THE WARNING DISAPPEARED. ADJUSTED FWD CARGO DOOR SWITCH 14WS IAW FEDEX A310-200 AMM 52-71-11, AND ACCOMPLISHED AN INSPECTION OF FWD CARGO DOOR SILL AND FRAME AREA. NO DISCREPANCIES NOTED IAW FEDEX A310-200 AMM 52-31-11.
Part: FITTING — GOUGED (ZONE 100) · airframe 34,264 hrs · 29,893 cycles
FWD CARGO COMPARTMENT DOOR LOCK FITTING AT NR 1 POS GOUGED ON BOTH LUGS. RECEIVED NEW DOOR LOCK FITTING P/N A5377293500200 PO NR 597399.1. INSTALLED FITTING IAW A310-200 SRM 51-40 20 AND 53-13-83 PARA 5 SHT 1. FITTING WAS INSTALLED ON FEDEX JOB CARD NON-ROUTINE N00900.
Part: SUPPORT ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
AT FRAME 26 SUPPORT ANGLE UNDERNEATH T-CAP AT RBL59 HAS CORROSION. REMOVED GUIDE AND FITTING IAW A310 SRM 51-40-02 PG 7. RECIEVED NEW FITTING P/N A5377364420100. DRILLED AND LOCATED FITTING IAW A310 SRM 51-40-44 PG 16 AND INSTALLED FITTING AND GUIDE IAW A310 SRM 51-40-21.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
FWD CARGO COMPARTMENT DOOR SILL LOWER/AFT CORNER CORRODED. REMOVED NR 10 LATCH FITTING AND ANGLE IN AFT CORNER. REMOVED CORROSION IAW A310-200 SRM 51-74-10-8. MAT THICKNESS .243 LOWEST SPOT REMOVED 0.110 FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR IAW A310-200 SRM 53-13-83 FIG 203 SHEET 1. ALODINED REPAIR PARTS AND SILL AREA IAW A310-200 SRM 51-21-10. PRIMED AND PAINTED REPAIR PARTS AND DOOR SILL AREA IAW A310-200 SRM 51-23-10. INSTALLED NEW CORNER ANGLE IAW A310-200 SRM 51-40-21. INSTALLED DOUBLER AND NR 10 DOOR LATCH FITTING IAW A310-200 SRM 53-13-83 FIG 203 SHT.1
Part: SKIN — MISREPAIRED (LT WING) · airframe 34,264 hrs · 29,893 cycles
LEFT WING EXTERNAL REPAIR DOUBLER ON TRAILING EDGE END RIB, APPROXIMATE WING STATION 1278 BETWEEN WING RIBS 20 AND 21 REAR SPAR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR, FOUND NOT TO BE WITHIN APPROVED DATA. REMOVED DAMAGED RIB AND REPLACED WITH NEW PART. FABED ON FEDEX NR N01216 AND N01215. INSTALLED I/A/W A310- 200 SRM 51-40-21 PG. 25.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
AT FRAME 26 FLOOR SUPPORT T-CAP HAS CORROSION AT RBL 59. CUT DAMAGE IAW A310 SRM 53-10-15. MATERIAL ID LN 9497-420 AND LN 9496-310 IAW A310 SRM 53-10-15. FABRICATED REPAIR PARTS IAW A310 SRM 53-10-15, ALODINED AND PRIMED IAW A310 SRM 51-21-10. PAINTED IAW A310 SRM 51-23-10 AND INSTALLED IAW A310 SRM 53-10-15.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
FWD CARGO COMPARTMENT DOOR LOCK FITTING AT NR 1 POSITION CORRODED. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR NR 1 LOCK FITTING IAW A310-200 SRM 51-40-20.
Part: CROSSBEAM — DAMAGED (ZONE 100) · airframe 34,264 hrs · 29,893 cycles
FWD E/E BAY FRAME 14 RT CROSS MEMBER VERTICAL LEG HOLE LABELED "A" DAMAGED. THIS SDR WAS GENERATED TO REPLACE SDR 07-4770. THIS SDR IS TO MAKE CORRECTIONS IN THE FOLLOWING BLOCKS 5A, 5C, 5D, 5F.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
CORROSION ON STRINGER 56R FROM FRAME 60 TO 61 ALSO ON FRAME SHEAR TIE IN AFT PIT. REMOVED SHEAR TIE IAW A310-200 SRM 53-10-14 PARA. 4.A (2) (A) AND DAMAGE STRINGER AT FRAME 60-61 S56R IAW A310-200SRM 53-10-14 PARA. 4.A (2) (A). REMOVED CORROSION IN SHEAR TIE, NO MATERIAL LOSS IAW A310-200 SRM 51-74-10. INSTALLED REPAIR SPLICES, STRINGER AND SHEAR TIE IAW A310-200 SRM 53-10-14 PARA. 4.A (2) (A).
Part: BEAM — CRACKED (PAX DOOR) · airframe 34,264 hrs · 29,893 cycles
NR 3 HOLE ON FIGURE 8, AREA ON RT PAX DOOR INDICATED AS CRACKED WHEN CHECKED BY BHEC IAW NDT MANUAL 53-30-53 USING MACHINE T8209A. REAMED HOLE IN REF TO SRM 51-40-51. PERFORMED BHEC IAW NTM 53-30-53-NO CRACKS FOUND. FABRICATED REPAIR BUSHING, PRIMED, PAINTED AND INSTALLED REPAIR BUSHING AND FASTENER IN REF TO EA 6-5310-112988 PT1, "FUSELAGE-AD2007-11-12, SB A310-53-2037, SB A310-53-2017, EO 6-5310-7-3318, RI DOOR UPPER HEADER AT FR14C-REPAIR"
Part: BULKHEAD — CORRODED (ZONE 100) · airframe 34,264 hrs · 29,893 cycles
FWD PIT, 3 INCHES AFT FRAME 39 LEFT, 3 INCHES ABOVE STRINGER 30 LEFT, HORIZONTAL BULKHEAD LT FWD CORNER, SEVERE EXFOLIATION CORROSION. COMPLIED WITH EA 6-5310-109221
Part: FRAME — CRACKED (ZONE 600) · airframe 34,264 hrs · 29,893 cycles
FRAME 47 FASTENER HOLE INSPECTION, NR 4 RT HOLE HAS INDICATION OF DEFECT. REAMED HOLE TO TRANSITION FITTING IAW FED EX A310-200 SRM 51-40-40 PG14. INSTALLED FASTENER IAW A310-200 SRM 51-40-21 PG 24. BHEC NR 4 HOLE REF EA 6-5710-112994. NO CRACK INDICATION NOTED
Part: TRUNNION — CRACKED (RT MLG) · airframe 34,264 hrs · 29,893 cycles
RT MLG TRUNNION RIB 5 FWD LUG AFT FACE APPEARS TO BE CRACKED. SPOT FACE AND CHAMFERED ON E.O. 6-5710-7-5010 PT8 - NO CRACKS FOUND.
Part: ADAPTER — CRACKED (SEAT TRACK) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FR 46 RT SIDE, ADAPTER CRACKED (OVER WING BOX) BS 2553 RBL 60. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW SRM 51-40-21 PG7.
Part: FRAME — DAMAGED · airframe 34,264 hrs · 29,893 cycles
FWD E/E BAY FRAME 14 RT VERTICAL LEG HOLE LABELED "A" DAMAGED FABRICATED AND INSTALLED 2. REPAIR BUSHINGS IAW FED EX EA 6-5310-109224 "FUSELAGE-MAINFRAME-O.S. HOLES IN NLG WHEEL WELL CROSSMEMBER-REPAIR" BY TIMCO EMP NR 110294/QC254.
Part: FRAME — GOUGED (ZONE 200) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FR55 AT APPROX L15L HAS A PUNCTURE IN FLANGE OF FRAME. CUTOUT DAMAGE AND REPAIRED WITH REINFORCING PLATE/REPAIR DOUBLER IAW A310 SRM 53-10-13 PAGE 206-209 FIGURE 202.
Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 34,264 hrs · 29,893 cycles
AGING AIRCRAFT DETERMINATION OF EXTERNAL DOUBLER ON FUSELAGE SKIN AT FRAME 40 STRINGER 16 TO 18 RT REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR FOUND NOT TO BE WITHIN SRM REQUIREMENTS. REMOVED DOUBLER, REPAIRED HOLES AND INSTALLED FASTENERS IAW EA 6-5330-112990 FUSELAGE-SKIN PANEL AT FR 40 AND S-17R- REPAIR. REMOVED AND REPLACED STRINGER SPLICE AT FS 2294- S-17R IAW A310 SRM 51-40-21 PG 22 AND PG 24.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
BULK PIT BELOW FLOOR, CORROSION ON FLOOR FRAME 67 UNDER NUTPLATE AT RBL 38. REMOVED CORROSION IAW A310 SRM 51-22-00 PG 11, CHECKED LIMITS, ORIG MAT 0.130, MAT. REMOVED .040, MAT REMAINING .090. FOUND OUT OF LIMITS IAW A310 SRM 53-10-15 PG 101 UTG NR 8225-B. REMOVED BEAM IAW A310 SRM 51-40-21 PG 7, RECEIVED NEW BEAM P/N A5397826720400 PO 594281.3. DRILLED AND LOCATED IAW A310 SRM 51-40-40 AND INSTALLED IAW A310 SRM 51-40-21 PG 7.
Part: ARM — CORRODED (ZONE 300) · airframe 34,264 hrs · 29,893 cycles
NR 5 RUDDER HINGE ARM (3EA) BEARINGS WORN, CORROSION ON LUG FACE REMOVED CORROSION FROM LUG FACE IAW A310-200 MM 51-24-10-8 LUG THICKNESS OUT OF LIMITS IAW A310-200 SRM 55-30-00. ORDERED AND RECEIVED SERVICEABLE NR 5 HINGE ARM S/N776235. HINGE ARM WAS INSTALLED ON FEDX CARD 43S2082 STEP 5G.3.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
INTERGRANULAR CORROSION ON TOP OF MAIN CABIN FLOORBEAM AND AROUND FLOOR PANEL HOLES, LONGITUDINAL FLOORBEAM UNDER LT FWD LAV MARKED. REMOVED CORROSION IAW A310 SRM 51-74-10. ORIGINAL THICKNESS .079, REMOVED .040, .039 REMAINING. MATERIAL LOSS BEYOND ALLOWABLE LIMITS IAW A310 SRM 53-10-00. UT GAUGE NR T82530. REMOVED CORRODED BEAM IAW A310 SRM 51-40-21. LOCATED AND DRILLED HOLES IN NEW BEAM IAW A310 SRM 51-40-44, PART NR 5361164422000 PO 593006.1. INSTALLED NEW BEAM IAW A310 SRM 51-40-21.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FLOORBEAM STRUCTURE BENEATH LT FWD LAV BETWEEN FR 14 AND 14B HAS INTERGRANULAR CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10. ORIGINAL THICKNESS .079. REMOVED .045. REMAINING MATERIAL NOT WITHIN ALLOWABLE LIMITS IAW A310 SRM 53-10-00. UT GAUGE NR 8225I. REMOVED CORRODED FLOORBEAM IAW A310 SRM 51-40-21. LOCATED AND DRILLED HOLES IN NEW FLOORBEAM PART NR A5361079723100, PO NR 593163.1 IAW A310 SRM 51-40-40. INSTALLED NEW FLOORBEAM IAW A310 SRM 51-40-21.
Part: FITTING — CRACKED (FUSELAGE) · airframe 34,264 hrs · 29,893 cycles
RIGHT SIDE CRACK INDICATION IN FR43A LOWER HOLE AT APPROX 12 O'CLOCK AND 6 O'CLOCK IN FRAME FITTING ONLY REMOVED LOWER FRAME FITTING AT FR 43A, THAT IS CRACKED. INSTALLED NEW FITTING IAW A31 SRM 51-40-21 PG 24 AND 51-40-40 PG 17.
Part: FITTING — CRACKED (FUSELAGE) · airframe 34,264 hrs · 29,893 cycles
LEFT SIDE CRACK INDICATION IN FR 43A LOWER HOLE APPROX 12 O'CLOCK IN FRAME FITTING ONLY REMOVED LOWER FRAME FITTING AT FR 43A THAT IS CRACKED. INSTALLED NEW FITTING IAW A310 51-40-40, 51-40-21 PG 24.
Part: ADAPTER — CRACKED (MAIN CABIN) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FR 43 RT SIDE, ADAPTER CRACKED OVERWING BOX REPLACED FR 43 RT SIDE ADAPTER IAW A310-200 SRM 51-40-21 P7 AND MA310-200 AMM 20-21-12 BY TIMCO EMP NR 5252/QC204.
Part: ATTACH FITTING — CRACKED (BS 2506) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FR45 RT SIDE ADAPTER CRACKED OVER WING BOX REPLACED FR45 ADAPTER IAW SRM 51-40-21 P7 AND AMM 20-21-12.
Part: ADAPTER — CRACKED (MAIN CABIN) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FR44, RT SIDE, ADAPTER CRACKED OVERWING BOX REPLACED FR 44 RT SIDE ADAPTER IAW SRM 51-40-21 P7 AND A310-200 AMM 20-21-12.
Part: ATTACH FITTING — CRACKED (MAIN CABIN) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FS 42 RT SIDE ADAPTER CRACKED OVERWING BOX REPLACED FR 42 RT SIDE ADAPTER IAW A310-200 SRM 51-40-21 P7 AND A310-200 AMM 20-21-12.
Part: ADAPTER — CRACKED (MAIN CABIN) · airframe 34,264 hrs · 29,893 cycles
MAIN CABIN FR 42 LT SIDE, ADAPTER CRACKED OVERWING BOX REMOVED CRACKED ADAPTER IAW SRM 51-40-21 PAR 7. INSTALLED NEW ADAPTER IAW SRM 51-40-21 AND AMM 20-21-12-0.
2005
Part: FILTER — CLOGGED (FUEL SYSTEM) · airframe 31,989 hrs · 28,466 cycles
REJECTED TAKE OFF AS 95 KNOTS DUE TO ECAM WARNING 'ENG FUEL FILTER CLOG' WARNING WAS RESOLVED AS SOON AS THROTTLES WERE RETARDED. TOGA POWER WAS USED (104.7 PERCENT N1) MESSAGE DISAPPEARED QUICKLY AND WE WERE UNC ERTAIN OF WHICH ENGINE WAS AFFECTED. PULLED BOTH MAIN FUEL FILTERS. BOTH WERE CLEANED. REPLACED WITH NEW FILTERS, RAN BOTH ENGS FOR LEAK CHECK AND TO CHECK CLOG LIGHTS. NO LEAK,NO LIGHTS, RELEASED A/C FOR SERVICE. AMM 73-12-03 REMOVED & REPLACED FUEL FILTERS.
Part: O-RING — CUT (HYDRAULIC SYS) · airframe 31,888 hrs · 28,393 cycles
ECAM ALERTED HYD RSVR LO LEVEL ON GREEN SYSTEM. ALL INDICATIONS (GAUGE, ECAM SYNOPTIC) SHOWED AND VERIFIED. QRH CONSULTED AND COMPLIED WITH MANUAL GEAR GRAVITY EXT PROCEDURES ACCOMPLISHED. TOWED TO GATE DUE NO NOSE WHEEL STEERING. T/S FOUND HYD LEAK FROM GREEN HYD MANIFOLD FITTING FOUND O-RING CUT. REPLACED O-RING PER SMP. LEAK CHECK GOOD. RESTORED LANDING GEAR FREEFALL SYSTEM TO NORMAL OPERATING CONDITION PER A310MM CHP 32-33-00-2 PG 201-202.
Part: STRINGER — CORRODED (FUSLEAGE) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 46- FR 47 ON STG 51L HAS AREA OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10 C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 39 - FR 40/41 ON STR 45 L HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784, FOUND ALL AREAS TO BE WITH IN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12 INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 46 - FR 47 ON STR 46 L HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10 C/W EA 6-5310- 87784, FOUND ALL AREAS TO BE WITH IN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21, RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: RIB — CRACKED (RT WING) · airframe 31,806 hrs · 28,327 cycles
TOP OF RIGHT WING AT RIB 20 SKIN JOINT I/B SIDE OF SPLICE HAS 4 FASTENERS SHOWING CRACK INDICATION USING NDT METHOD. REMOVED CRACKS IAW EA 6-5720--87800.
Part: RIB — CRACKED (LT WING) · airframe 31,806 hrs · 28,327 cycles
LEFT WING LOWER SURFACE T/E SKIN HAS INDICATION OF CRACK RIB 11 AT PANEL 581 AB. REPAIRED IAW EA 6-5710-87138.
Part: SKIN — DAMAGED (RT WING) · airframe 31,806 hrs · 28,327 cycles
RIGHT WING BOTTOM SKIN CUTOUT FOR PANEL 650 GB HAS 1 EA ELONGATED SCREW HOLE. COMPLIED EA 6-5710-87212.
Part: WEB — CRACKED (THRUST REVERSER) · airframe 31,806 hrs · 28,327 cycles
NR 2 ENG O/B REVERSER COWL HAS A CRACKED WEB, ON UPPER ANGLE GEAR BOX ACTUATOR HOLE, REV DEPLOYED). REMOVED NR 2 ENG O/B T/R GEAR BOX ASSY IAW A310-200 MM 78-31-03-2-B, AND FAB FILLER AND REPAIRED DOUBLER IAW EA 6-7830-87417 AND REINSTALLED UPPER GEAR BOX IAW A310-200 MM 78-31-03-2-B. OPS CHECK GOOD.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
CORROSION ON SKIN IN A/C BAY BETWEEN FRAMES 45 AND 46, BETWEEN VAPOR BARRIER AND PACK CUTOUT. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
CORROSION ON SKIN IN A/C BAY BETWEEN FRAMES 39 TO 40/41 AND STRINGERS 43L TO 47L. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — CORRODED (FUSELAGE) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY, ALL SKIN AREAS WHICH HAVE HAD CORROSION REMOVED REQUIRE FLAP PEENING. FLAP PEENED ALL EFFECTED SKIN AREAS IN ACM BAY IAW A310-200 SRM 51-29-00. THIS NR COVERS THE ACM AREA FROM FRAME 39 TO FRAME 47, FROM STRINGER 33L TO 33R, FOR CORROSION REPAIRS THAT WERE WITHIN SRM LIMITS. ALL DOCUMENTS ON FILE AT EADS, W/O 00028159, 0510-0201-0192.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY SKIN BETWEEN STR39R AND STR40R AND FR46 TO FR47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS PER A310 SRM 53-15-12 AND EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. C/W EA 6-5310-87784.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY SKIN BETWEEN STR 38R TO 39R AND FR44 TO FR45 HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-15-12. FLAP PEENED IAW A310-200 SRM 51-29-00. TREATED AND PRIMED AND TOPCOATED IAW A310-200 SRM 51-23-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
BULK CARGO COMPT, JUST FWD OF FR68 ON LT STR 50 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED STR 50L.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN A/C BAY, FROM FRAME 45 TO FRAME 46 AND STR 46R TO 41R AREA HAS NUMEROUS SPOTS OF CORROSION ON SKIN. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS PER A310 SRM 53- 15-12. INSTALLED FASTENERS PER A310-SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310-SRM 51-75-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY STR 42R HAS AREAS OF CORROSION BETWEEN FRAME 40/41 TO FRAME 44. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784 AND A310 SRM 53-15-12. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: VANE — CHAFED (LE FLAPS) · airframe 31,806 hrs · 28,327 cycles
RIGHT FLAP VANE LEADING EDGE HAS 2 CHAFED AREAS. REMOVED RT WING FLAP VANE IAW A310-200 AMM 27-50-15-4. COMPLIED WITH EA 6-5750-87216. INSTALLED RT FLAP VANE IAW A310-200 AMM 27-50-15-4. OPS CHECKED GOOD IAW A310-200 AMM 27-54-00-5.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT, ABOUT STGR 57 FWD SIDE OF FR 59 AROUND BASE OF RADIO ALT. TRANSMISSION ANTENNA HAS AREA OF CORROSION. REMOVED FASTENERS AROUND BASE OF ANTENNA IAW A310-200 SRM 51-40-21. REMOVED LIGHT CORROSION IAW A310-200 SRM 51-74-10. INSTALLED FASTENERS IAW A310-200 SRM 51-40-21. TREATED, PRIMED, AND TOPCOATED AREA IAW A310-200 SRM 51-21-10, AND APPLIED SEALING IAW A310-200 AMM 34-42-11-4-01.
Part: FRAME — CORRODED (ZONE 700) · airframe 31,806 hrs · 28,327 cycles
CORROSION ON FRAME IN RT WHEEL WELL AFT OF FRAME 47 ON DIAGONAL FRAME. REMOVED CORROSION AND REPROTECTED SURFACE IAW A310-200 SRM 51-74-10 AND 51-23-10. MATERIAL LOSS WITHIN LIMITS PER FEDEX EA 6-5310-87818.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT, BETWEEN FR 54.2 AND FR 54.3 ON STR 56 RT HAS 3 AREAS OF CORROSION. REF FEDEX EA 6-5310-88741, REMOVED SHEAR TIE, REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION, CHECK MATERIAL LOSS IAW A310-200 SRM 53-10-00 PG 123 ITEM 24. FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED, AND TOPCOATED AREA IAW A310-200 SRM 51-23-20. REINSTALLED SHEAR TIE AND FASTENERS IAW A310-200 SRM 51-40-21.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN A/C BAY, FROM FRAME 46 TO 47, STRINGER 46R TO 43R HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND ALL AREAS TO BE WITHIN LIMITS IN AREA STR 44R BETWEEN FR 46 AND 47. C/W EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT BETWEEN FR 60 AND FR 61 ON STR 50 RT HAS AREA OF CORROSION. REMOVED FASTENERS AND REMOVED CORROSION FROM STG50 BETWEEN FR60 AND FR61 IAW A310-200 SRM 51-40-21 AND SRM 51-74-10; CHECKED LIMITS AND FOUND MATERIAL THICKNESS TO BE WITHIN LIMITS, TREATED, PRIMED, AND TOPCOATED AREA IAW A310-200 SRM 53-10-00 PG 123 ITEM NR4 AND SRM 51-23-10. REF FEDEX EA 6-5310-88741 FOR APPROVAL FOR RETURN TO SERVICE.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY SKIN BETWEEN STR 39R TO STR 40R HAS AREAS OF CORROSION BETWEEN FR 44 TO FR 45. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-15-12. FLAP PEENED IAW A310-200 SRM 51-29-00. TREATED PRIMED AND TOPCOATED IAW A310-200 SRM 51-23-10.
Part: SKIN — DAMAGED (LT WING) · airframe 31,806 hrs · 28,327 cycles
WHILE WORKING EO 6-5710-7-5008PT3, LT WING FOR LANDING ASSY FOR PANEL 575CB 4 EA HOLES NOTED ARE LARGER THAN DRAWING SIZE. THIS IS AN INCOMING CONDITION. HOLE NR 9 .263 INCH, EM PLANK .6 INCH, NR 10 .328 INCH, EM RIB .610 INCH, EM PLANK .760 INCH, NR17 .328 INCH, EM RIB .570 INCH, EM PLANK .840 INCH, NR 21 .263 INCH, EM PLANK .5 INCH. SHOULD BE NR 9 AND 21 AT .187 INCH, NR 10 AND 17 AT .310 INCH. NOTE HOLES NEED COLDWORKING. REPAIRED HOLES IAW EA 6-5730-79121.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 31,806 hrs · 28,327 cycles
CLS ADAPTER AT FR 37 TRACK L3 IS GOUGED. REMOVED AND REPLACED CLS ADAPTER AT FR 37 TRACK L4, L3 MDC IAW A310-200 SRM 53-10- 16.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 43 TO FR 44 BETWEEN STR 40L AND STR 41L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10, WITHIN LIMITS, FLAP PEENED IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10 ON SKIN FR 43 TO FR 44 BETWEEN STR 40L AND 41L.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 46 TO FR 47 BETWEEN STR 44L AND STR 45L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 WITHIN LIMITS. FLAP PEENED IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY STR 46 RT BETWEEN FR 43 TO FR 47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER A310 SRM 53-10-00 AND EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN AC BAY, FROM FRAME 41 TO 42 AND STGR 51R TO 47R, AREA HAS CORROSION ON SKIN. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL REMOVED WITHIN LIMITS IAW A310-200 SRM 53-10-00. FLAP PEENED AS REQUIRED IAW A310-200 51-29-00, TREATED, PRIMED, AND APPLIED TOP COAT IAW A310-200 SRM 51-75-10. REINSTALLED FASTENERS IAW A310-200 SRM 51-40-21.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 40/41 BETWEEN STR 44L AND STR 45L, SKIN HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10, REF FEDEX EA 6-5310-88751.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN AC BAY, FRAME 39 TO 40 AND STGR 47R TO 43R HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND ALL AREAS TO BE WITHIN LIMITS IN AREA FR 39 TO 40 AND STR 45R TO 44R AND STR 47R TO 46R. C/W EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 44 TO FR45 BETWEEN STR 37L AND 38L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 WITHIN LIMITS. FLAP PEENED AREA IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10 ON SKIN FR44 TO FR45 BETWEEN STR 37L TO STR 38L.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT, AT FR 54.3 FWD AND AFT SIDE, ON R-STR 48 HAS AREAS OF CORROSION. REMOVED FASTENERS AND STRINGER TIE TO FOM IAW A310 SRM 51-40-21 AND 51-72-10. REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-00 TABLE 102. REINSTALLED FASTENERS AND STRINGER TIE IAW A310 SRM 51-40-21 AND 51-72-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN AC BAY, FROM FRAME 39 TO 40 AND FROM STR 55-51 RT HAS AREAS OF CORROSION ON SKIN. REMOVED CORROSION PER SRM 51-74-10. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA6-5310-87784. C/W EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN A/C BAY, FROM FRAME 46 TO 47, STGR 43R TO 38R HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — DAMAGED (LT WING) · airframe 31,806 hrs · 28,327 cycles
L/WING, 550JB HAS ONE EACH ELONGATED HOLE. COMPLIED WITH EA 6-5710-87121.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR46 TO FR47 BETWEEN STR 50R AND STR 51R, SKIN HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310-SRM 51-75-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN A/C COMPARTMENT STRINGER 44L FROM FRAME 39 TO 47 HAS AREAS OF CORROSION ON STRINGER AND AROUND FASTENERS. REMOVED FASTENERS IAW A310-200 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10, FOUND SECTION OUT OF LIMITS IAW A310-200 SRM 53-10-00, CUTOUT DAMAGED SECTION, FAB REPAIR PARTS, AND INSTALLED REPAIR IAW A310-200 SRM 51-40-21 AND EA 6-5310-87227. REINSTALLED FASTENERS IAW A310-200 SRM 51-40-21.
Part: SKIN — DAMAGED (ZONE 500) · airframe 31,806 hrs · 28,327 cycles
LT WING, 560CB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5710-87212.
Part: FRAME — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN A/C BAY, FRAME 47 AFT SIDE FROM STGR40R TO 47R HAS CORROSION. REMOVED AND REINSTALLED FASTENERS IAW A310 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. ROTOTESTED HOLES AND CLEARED DEFECTS IAW A310 NTM 51-10-01. ALL WORK WAS PERFORMED AND LIMITS ARE GOOD IAW FEDEX EA 6-5310-87236.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY FR 43 TO FR 44 BETWEEN STR 39L AND 40L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10. WITHIN LIMITS, FLAP PEENED IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10 ON SKIN FR 43 TO FR 44 BETWEEN STR 39L AND 40L.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
BULK CARGO COMPT, BETWEEN FR 63 AND FR 64 LT SIDE STR 54 AND STR 55 LT HAS CORROSION AROUND FASTENERS AREA. REMOVED AND REPLACED FASTENERS IAW A310 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10, NDT FOR MAT LOSS IAW A310-200 SRM 53-17-12 AND 53-10-00. RETURNED TO SERVICE PER FEDEX EA 6-5310-88741.
Part: PANEL — DAMAGED (RT WING) · airframe 31,806 hrs · 28,327 cycles
RT WING FAIRING 633BB 2 MOUNTED BRACKETS REQUIRES INSTALLATION. NOTE 7 EA HOLES IN WING PLANK ARE COUNTERSUNK. RT WING BRACKETS FOR FAIRING 633BB REAMED HOLES TO 2ND OVERSIZE, SEALED FITTINGS (2EA.). INSTALLED CONICAL WASHERS, AND FITTINGS IAW A310 SRM 51-40-44, SRM 51-71-70, SRM 51-40-21 AND FEDEX EA 6-5720-57820.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN A/C BAY, FRAME 44 TO 45, STR 46R TO 43R HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
IN ACM BAY STR 50R BETWEEN FR43 TO FR47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 57-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT JUST AFT OF FR 54.3 ON STR 51 RT HAS 1EA AREA OF CORROSION. REMOVED CORROSION FROM AFT OF FR 54.3 RT STG 51 IAW A310-200 SRM. FOUND MATERIAL TO BE WITHIN LIMITS IAW A310-200 SRM 53-10-00 PG 123 ITEM 24. INSTALLED REMOVED PARTS AND FASTENERS IAW A310-200 SRM 51-40-21. REF FEDEX EA 6-5310-88741 FOR APPROVAL FOR RETURN TO SERVICE.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT, BETWEEN FR59 AND FR60 ON R STGR 54 HAS AREA OF CORROSION. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MEASURED MATERIAL LOSS IAW A310-200 SRM 53-17-12. VERIFIED MATERIAL IS WITHIN LIMITS IAW A310-200 SRM 53-10-00. INSTALLED FASTENERS IAW A310-200 SRM 51-40-21. APPLIED PROTECTIVE FINISH IAW A310-200 SRM 53-21-10.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT PIT FRAME 67 STR 50L STRINGER HAS 2SQ INCH OF CORROSION. STR 50L FR 67 AFT, SECTION OF STRINGER REMOVED AND REPLACED.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT, BETWEEN FR 54.1 AND FR 54.2 ON STR 56 RT HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED WITH NEW STRINGER SECTION BETWEEN FRAMES 54.2 AND 54.1 IAW A310 SRM 53-10-14, CUT AND SPLICED FRAME 54.2 IAW A310 SRM 53-10-13 REF EA 6-5320-87234.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 31,806 hrs · 28,327 cycles
FLOOR PANEL 231NH HAS 3 EA CRACKS AND 7 EA MISSING/BROKEN INSERTS. FABBED REPLACEMENT PANEL 231NH IAW FED EX DWG NR SRZ-25-005 REV E.
Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 31,806 hrs · 28,327 cycles
NR 2 ENGINE FWD MOUNT FITTING HAS PITTED CORROSION ON BOLT HOLES, SPIGOT HOLE, LOWER AND UPPER MATING SURFACE. REMOVED CORROSION IN ALL AREAS LISTED. FABBED AND INSTALLED 3 EA BUSHINGS AND REPROTECTED SURFACES IAW A310 SRM 54-51-81 AND FEDEX EA 6-5450-87748.
Part: FLAP TRACK — DAMAGED (WINGS) · airframe 31,806 hrs · 28,327 cycles
COMPLY WITH EA 6-5720-86138 REV NO POS P2 WING INSPECTION FLAP TRACK MOVABLE FAIRING. LT NR 2, 4, 5 AND RT NR 3,5. COMPLIED WITH EAN 6-5720-86138 AND REPORTED FINDINGS TO FED EX VIA MAXI MERLIN.
Part: SKIN — DAMAGED (ZONE 600) · airframe 31,806 hrs · 28,327 cycles
WHILE WORKING EO 6-5710-7-5004 PT 4, RT WING FOR LANDING ASSY FOR PANEL 675CB, 2 EA HOLES NOTED ARE LARGER THAN DRAWING SIZE. THIS IS AN INCOMING CONDITION. HOLE NR 10 .390", EDGE MARGIN RIB .610", PLANK .760", NR 17 .390", EDGE MARGIN RIB .570", PLANK .840". HOLE SIZE SHOULD BE .310". REPAIRED HOLES IAW EA 6-5730-79121
Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
VERT STAB FRONT SPAR ANTENNA HAS PITTING CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED 1 EA ANTENNA IAW A310-200 AMM 23-11-11-4. OPS CHECK NOT REQUIRED HF SYSTEM IS DEACTIVATED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
CORROSION ALONG STRINGER 52L BETWEEN FRAMES 60 AND 61, AFT CARGO UNDER FLOOR. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL THICKNESS AFTER WENT OUT OF LIMITS IAW A310-200 SRM 51-10-04. CUT AND SPLICED STRINGER 52L AT FRAMES 60 AND 61 IAW A310-200 SRM 53-10-14. RESTORED PROTECTIVE COATING IAW A310-200 SRM 51-21-10.
Part: BRACKET — WORN (ZONE 400) · airframe 31,806 hrs · 28,327 cycles
NR 2 ENGINE RT CORE COWL DOOR HOLD OPEN ROD SUPPORT BRACKET ON ENGINE IS WORN. REMOVED AND REPLACED BRACKET, INSTALLING IAW A310-200 AMM 20-21-12.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AREA BEHIND BULK CARGO BETWEEN FRAMES 72-74 LEFT SIDE AT STRINGER 48 HAS 15 SQ INCHES OF CORROSION. REMOVED CORROSION FR 72-74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED AND REPLACED STRINGER SECTION 48L FR 72 TO 78 IAW A310-200 SRM 53-10-14.
Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
OFF AIRCRAFT PART, NR 1 PYLON ACCESS PANEL NR 413BL HAS MODERATE CORROSION AROUND ALL FASTENERS HOLES INTERIOR SIDE OF PANEL. REPLACED PANEL ASSY IAW A310-200 SRM 51-72-10.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AREA BEHIND BULK CARGO AT FRAME 72 LEFT SIDE APPROX STR 41L, STRINGER HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION, AREA OUT OF LIMITS, REMOVED DAMAGED STRINGER SECTION AND REPLACED WITH NEW SECTION PER A310-200 SRM 51-74-10 AND 53-10-14.
Part: DOOR FRAME — CORRODED (FUSLAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AREA BEHIND BULK CARGO BETWEEN FRAMES 72-74 LEFT SIDE AT STRINGER 49 HAS 15 SQ" OF CORROSION. REMOVED CORROSION FR 72-74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED AND REPLACED STRINGER SECTION 49L FR 72 TO 78 IAW A310-200 SRM 53-10-14.
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
MAIN DECK CARGO CLS ADAPTER BETWEEN R1 AND R2 AT FRAME 50 IS CORRODED. REMOVED AND REPLACED BEAM IAW A310-200 SRM 51-72-10.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AFT CARGO COMPT, AFT OF FS 54 ON R-STRINGER 51 HAS AREA OF CORROSION. REMOVED STRINGER END FITTING AT FS 54 ON STRINGER 51R IAW A310-200 SRM 51-74-21. REMOVED CORROSION FROM STRINGER 51 AFT OF FS 54 IAW A310-200 SRM 51-74-10. VERIFIED ALLOWABLE LIMITS AND MATERIAL LOSS IAW A310-200 SRM 53-10-00 AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE ANGLE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED END FITTING, SPLICE ANGLE AND NEW STRINGER 51 SECTION IAW A310-200 SRM 51-40-21 AND 53-10-14.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AREA BEHIND AFT CARGO COMPARTMENT FRAME 77 LEFT SIDE APPROX STR 49L STR HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION AT FRAME 77 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104 TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FR 72-78 IAW A310-200 SRM 53-10-14.
Part: BRACKET — CRACKED (ZONE 400) · airframe 31,806 hrs · 28,327 cycles
NR 1 PYLON AFT END AT APPROX RIB 18 1 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10.
Part: ADAPTER — BROKEN (FUSELAGE) · airframe 31,806 hrs · 28,327 cycles
CLS ADAPTER AT FS 74 TRACK L4 HAS BROKEN CLEVIS. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.
Part: STRINGER — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AREA BEHIND BULK CARGO BETWEEN FRAME 75 AND 76 APPROX AREA STR 49L, STRINGER HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION AFT OF FRAME 75 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104, TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FR 72 TO 78 IAW A310-200 SRM 53-10-14.
Part: STRAP — CRACKED (ZONE 400) · airframe 31,806 hrs · 28,327 cycles
NR 1 PYLON OUTBD SIDE FWD OF PRECOOLER STRAP IS CRACKED. REMOVED AND REPLACED ANGLE IAW A310-200 SRM 51-72-10.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
MAIN CABIN FRAME 61/62, SCALLOPS ARE WORN ON TRACK '0'. REMOVED FLOOR PANELS FOR ACCESS IAW A310-200 SRM 51-40-21. REMOVED AND REPLACED SEAT TRACK SECTION IAW A310-200 SRM 51-72-10 AND 53-10-16. REINSTALLED FLOOR PANELS IAW A310-200 SRM 51-40-21.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
SEAT TRACK '0' AT FR 75A AND 76 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK. REINSTALLED FLOORBOARDS IAW A310-200 SRM 51-72-10 AND 51-40-21.
Part: ACCESS PANEL — CORRODED (ZONE 400) · airframe 31,806 hrs · 28,327 cycles
NR 2 PYLON ACCESS PANEL NR 423EL HAS MODERATE CORROSION AROUND INTERIOR SIDE OF ALL FASTENER HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10, VERIFIED THREE AREAS OUT OF LIMITS. VERIFIED REPAIR MATERIAL, FABBED THREE EA. REPAIR DOUBLERS AND FILLERS IAW A310-200 SRM 54- 52-51. CUT OUT DAMAGED AREAS IAW A310-200 SRM 54-52-51. APPLIED PROTECTIVE TREATMENT TO FABBED PARTS AND ACCESS PANEL IAW A310-200 SRM 51-21-10. INSTALLED THREE EACH REPAIR DOUBLER AND FILLERS IAW A310-200 SRM 54-52-51.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AFT OF BULK CARGO BILGE AREA STGR 53 LT HAS 2 AREAS OF CORROSION BETWEEN FR 70-71. REMOVED REQUIRED FASTENERS AND REMOVED CORROSION IAW A310-200 SRM 51-40-21 AND SRM 51-74-10. MATERIAL LOSS AFTER CORROSION REMOVAL WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00. CUT OUT DAMAGED STRINGER SECTION AND FABBED REPAIR STRINGER AND SPLICE IAW A310-200 SRM 53-10-14. RESTORED SURFACE PROTECTIVE COATING IAW A310-200 SRM 51-21-10. INSTALLED STRINGER REPAIR IAW A310-200 SRM 53-10-14.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,806 hrs · 28,327 cycles
FLOORBEAM IS CRACKED 66 INCH RIGHT OF CENTER LINE AT FRAME 54.3 UNDER CEILING PANEL 152BC IN AFT CARGO, (PANEL NOT REMOVED FOR C-CHECK). REMOVED FLOOR PANEL 252DF AND CEILING PANEL 152BC FOR ACCESS IAW A310-200 SRM 51- 40-21. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLES AND INSTALLED ANGLES ON AIRCRAFT IAW A310-200 SRM 53-10-15 FIG 201. REINSTALLED FLOOR AND CEILING PANELS IAW A310-200 SRM 51-40-21 AND AMM 53-10-25-4.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
BULK CARGO COMPT, JUST AFT FS 63 ON R STRINGER 53 1 AREA OF CORROSION. REMOVED DISCREPANT SECTION OF STRINGER AND REPLACED PER A310-200 SRM 51-10-14 IN BULK CARGO COMPARTMENT AFT OF FRAME 63 ON R STRINGER 53.
Part: ANGLE — CRACKED (THRUST REVERSER) · airframe 31,806 hrs · 28,327 cycles
NR 1 ENGINE OUTBD T/R COWL LOWER FWD CORNER ANGLE IS CRACKED. REMOVED RIVETS IAW A310-200 SRM 51-40-21. CUTOUT CRACKED FLANGE IAW ROHR CF6-80A SRM 54-05-02. VERIFIED REPAIR FILLER AND ANGLE IAW ROHR CF6-80A SRM 54-05-02. FABBED FILLER AND REPAIR IAW ROHR CF6-80A SRM 54-05-02. APPLIED PROTECTIVE COATING IAW A310-200 SRM 51-21-10. INSTALLED REPAIR ANGLE AND FILLER IAW ROHR CF6-80A SRM 54-05-02 FIG 1.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AVIONICS COMPARTMENT LEFT SIDE AT FRAME 12 TO 12A AT FLOOR BOARD LEVEL, AREA HAS CORROSION APPROX 8 INCHES BY 8 INCHES ON RIBS AND STRINGER, STR 44L. REMOVED SKIN STIFFENER AT LT AVIONICS COMPARTMENT BETWEEN FR 12 AND 12A STR 44L IAW A310-200 DRAWING A536-10873. INSTALLED REPLACEMENT STIFFENER IAW A310-200 DRAWING A536-10873.
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
MAIN CABIN FRAME 62 TO 73 SEAT TRACK '0' HAS SEVERAL AREAS OF CORROSION IN ZONE 250. REMOVED AND REPLACED SEAT TRACK FROM FRAME 62 TO FRAME73 IAW A310-200 SRM 51-72-10.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
N00674 AREA BEHIND BULK CARGO AT FRAME 74 LEFT SIDE APPROX FR 49L HAS 7 SQ IN OF CORROSION. REMOVED CORROSION AFT OF FRAME 74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104, TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FS 72-78 IAW SRM 53-10-14.
Part: GUSSET — CORRODED (ZONE 400) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
NR 1 PYLON OUTBD SIDE AT RIB 17 ANGLE HAS CORROSION AROUND 4 HOLES. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
AFT OF BULK CARGO AT BILGE AREA, STRINGER 56 LT HAS NUMEROUS CORROSION ON STRINGER'S. RUNS THROUGH FRAME 70-71 AND FRAME 72, AS MARKED. REMOVED FASTENERS ON STR 56 LT AT FR 70-71 AND 72 IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL LOSS OUT OF LIMITS. REMOVED STR 56 LT AT FR 69.5 TO FR 72 IAW A310-200 SRM 51-40-21. MATERIAL ID FOR REPAIR PARTS VERIFIED IAW A310-200 SRM 53-17-14. FABRICATED REPAIR PARTS IAW A310-200 SRM 53-10-14. TREATED, PRIMED AND TOP COATED REPAIR PARTS IAW A310-200 SRM 51-74-10. INSTALLED REPAIR PARTS IAW A310-200 SRM 51-40-21.
Part: GUSSET — CORRODED (ZONE 400) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
NR 1 PYLON OUTBD SIDE AT RIB 15 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310200 SRM 51-72-10.
Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
BULK CARGO COMPT, BETWEEN FR 64 AND 65 ABOUT RT STRINGER 46 FLOOR PANEL ATTACH BRACKET HAS 3 SCREW HOLE CORRODED BENEATH NUTPLATE AREA. REMOVED AND REPLACED PROFILE IAW A310-200 SRM 51-72-10.
Part: GUSSET — CORRODED (ZONE 400) · corrosion level 2 · airframe 31,806 hrs · 28,327 cycles
NR 1 PYLON OUTBD SIDE AT RIB 16 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10.
2004
Part: CIRCUIT BREAKER — MALFUNCTIONED (LIGHT) · airframe 31,652 hrs · 28,226 cycles
DURING FLT, HEARD CRACKING & ARCING SOUND COMING FROM REAR OF COCKPIT (CB PANEL), FOLLOWED BY ACRID ELECTRICAL ODOR. DONNED O2 & DIVERTED INTO MCO. NO APPARENT EQUIP PROBLEMS DURING APPROACH & LANDING. LANDED 18R MCO UNEVENTFULLY. FOUND LANDING GEAR AND AIR COND COMPARTMENT DOME LIGHT C/B POPPED AND WOULD NOT RESET. CYCLED A/C COMPARTMENT DOME SWITCH TO OFF AND THEN C/B RESET. PULLED AND COLLARED C/B. MEL 33-45-01. ALL WHEEL WELL DOME LIGHT(S) INOP. REMOVED AND REPLACED CIRCUIT BREAKER 4LM, AND SWITCH 33LS PER AWM 33-37-01 AND AWM 33-35-01 RESPECTIVLEY. PERFORMED SATISFACTORY OPERATIONAL CHECK OF A/C BAY AND LANDING GEAR BAY LIGHTING PER AMM 33-32-00-5.
2002
Part: PROXIMITY SENSOR — MALFUNCTIONED (LANDING GEAR) · airframe 29,351 hrs · 26,747 cycles
COULD NOT RETRACT GEAR ON POSITION 1 SELECTED POSITION 2 THE GEAR CAME UP (REPEAT WRITEUP) SUBSEQUENT INDICATIONS WERE PITCH TRIM INOP, ATS 2 OFF CAPT TAT INOP, (HEAT FAILURE) & CABIN PRESS REG 1 FAIL & NR 1 TRANSPONDER, NO ALTITUDE READOUT. REMOVED AND REPLACED PROX DETECTOR UNIT PER M/M 32-31-71-4. GEAR SWING CHECKS OK IN BOTH SYSTEM 1 AND 2. EXTENSION AND RETRACTION PERFORMED PER M/M 32-30-00-6. A/C OK FOR CONTINUED SERVICE.
2000
Part: INDICATOR — READS LOW (COCKPIT) · airframe 27,707 hrs · 25,657 cycles
T/O ROLL, CAPT A/S IND BELOW 40 KTS WHEN F/O AS IND 80 KTS. FLUSH CAPT TOTAL PRESSURE LINE PER IAW AIRBUS MM CHAPTER 34-10-00-3. PERF FUNCTIONAL TEST PER MM 34-10-00-5-01. TEST CK NORMAL.
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 27,543 hrs · 25,517 cycles
CABIN RATE OF CLIMB WAS GREATER THAN 1500 FT/MIN. THEN GOT NR 2 CAB PRESS REG FAULT, NR 1 WOULD NOT HOLD PRESS. REMOVED AND REPLACED NR 2 CABIN SYS CONTROLLER PER MM 21-31-11/4. OPS CK GOOD PER 21-31-00/5.
1997
Part: DUCT — FAILED (NR 1 ENGINE)
ACFT DEPARTED BDL HAD AN AIR TURNBACK, NR 1 ENG ECAM ADVISORY NACELLE TEMP ADVISORY OCCURRED AFTER T/O CK LIST. FLASHING GREEN 230C AND THEN CRC/ECAM FOR NR 1 ENG FIRE HANDLE RED HANDLE AND BOTH LOOP LT ON. ATS DISCONNECTED. # 1 THROTTLE PLACED TO IDLE, FIRE WARNING CEASED ENG ABLE TO BE USED FOR LANDING. FOUND HIGH PRESSURE RECOUP DUCT ELBOW BLOWN ON RT SIDE OF ENGINE. REMOVED AND REPLACED HPT RECOUP AIR TUBING. ELBOW MOUNTED ON COMP CASE. PERFORMED ENG RUN IAW JRH, OPS CK NORMAL.
1995
Part: MECHANISM — NOT LATCHED (CABIN DOOR)
AT FL 220, RECEIVED ECAM WARNING L FWD DOOR NOT CLOSED. ALSO, GOT AUDIBLE WARNING FROM DOOR SIREN. A/C WAS DEPRESSURIZED AND WARNING CONTINUED. DURING DESCENT THROUGH 15,000, ECAM AND AUDIBLE WARNING CLEARED ITSELF. A/C WAS UNPRESSURIZED AT 15,000, WHEN PROBLEM CLEARED. INSPECTED CLOSE AND LOCK MECH OF L-1 ENTRY DOOR, NO FAULTS. DOOR OPENED AND CLOSEDNORMAL. CHECKED FOR FAIR, ALL NORMAL. OK TO CONTINUE FLIGHT PER MEL 52-8. CLOSED AND LOCK WARNING DEF, MX PROC 52-8 C/W CONT NR 0713034, EXP 7-23-95.