N436FE
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.
97 reports on file, 2006-12-16 – 2013-11-28.
Part: UNKNOWN — ABNORMAL (AUTOTHRUST SYS) · airframe 44,193 hrs · 19,759 cycles
WHEN TAKEOFF THRUST APPLIED & TOGA SELECTED ATS LEVER TRIPPED OFF. LOW SPEED REJECT ACCOMPLISHED ECAM ATTEMPTED NO HELP. REMOVED AND REPLACED THRUST CONTROL COMPUTER PRECAUTIONARY PER A310-200 M/M REF 22-35-34 -04-01. PERFORMED SUCCESSFUL AFS/LAND TEST PER A310-200 M/M REF 22-40-00-5.
Earlier reports · 2006–2012 · 96 reports
2012
Part: COMPUTER — INOPERATIVE (TE FLAPS) · airframe 42,930 hrs · 18,844 cycles
FLAP SYS 1 FAULT LIGHT IN FLIGHT RELEASED FOR SERVICE IAW MEL: 27-51-01-01 CATEGORY: C, "MEL 27-51-01-01: NR 2 SLATS/ FLAPS CONTROL COMPUTER - INOP. SLAT/FLAP WING TIP BRAKE TEST HAS BEEN ACCOMPLISHED." SFCC PN 49-079-05 (SYS NR 1) GOOD. SFCC PN 49-079-05 (SYS NR 2) INOP NR1 SFCC WOULD NOT PERFORM A BITE TEST, SWAPPED NR 2 SFCC INTO NR 1 SFCC POSITION. PERFORMED BITE TEST. TEST WAS GOOD IAW AMM 27-51-00-05. SFCC SYS NR 1 HAS PN 49-079-05 SN 405. SYS NR 2 HAS PN THIS SYS IS INOP. REFERENCE MEL 27-51-01-01. SWAPED BACK TO ORIGINAL POSITIONS, CONFIRMED PN ARE THE SAME 49-079-05 R & R NR1 SFCC IAW MM 27-51-00-05-0. OPS CK GOOD.
2011
Part: FLAP SYSTEM — STICKING (K FLAPS) · airframe 42,616 hrs · 18,653 cycles
ON CLIMB OUT, AFTER SLATS RETRACT, KRUGER FLAP DID NOT RETRACT. RE-CYCLED AND KRUGER WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST AND RETURNED TO DEPARTURE. BITE TESTED SFCC 1. FAULTED LT RETRACT SWITCH. FOUND LT RETRACT SWITCH TO BE STICKING FREED STUCK SWITCH IAW SMP. OPS CHECKED IAW AMM 27-89-12-04-0. SYS CHECKS NORMAL ALL INDICATIONS NORMAL AT THIS TIME.
Part: SKIN — DENTED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
LOWER FUSELAGE DENT 17 INCHES AFT OF LOWER CARGO DOOR. SKIN TRIMMED-OFF BETWEEN FR 26/32 TO FR 33, STR 32R TO 34R PER SRM 53-10-12 REV 79, FIG 225. HFEC INSPECTION CARRIED OUT PER NTM 51-10-08 REV 74 FOUND NO CRACKED EVIDENT. REPAIR DOUBLER FABRICATED AND REPAIR PARTS INSTALLED PER SRM 53-10-12 REV 79, FIG 225. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOOR PANEL RT AT FRAME 36, 37, X = -35 FOUND DAMAGED. REMOVED AND REPLACED BY FABRICATION PER DWG SRZ-25-005, REV J. AND AS PER AMM 53-10-25 REV 30.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOORBEAM AT FRAME 36, RBL 27 FOUND WITH 0.25 INCH CRACK. TRIMMED OUT IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOORBEAM AT FRAME 34, RBL 27 FOUND WITH A 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203, SHT 1. REPAIR PROFILE FABRICATED AND INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOORBEAM AT FRAME 37, RBL 67 FOUND WITH 0.28 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15 REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SRM 53-10-15, REV 18, FIG 203 SHEET 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOORBEAM AT FRAME 37, RBL 27 FOUND WITH 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOORBEAM AT FRAME 37, RBL 27 FOUND WITH 0.25 INCH CRACK. TRIMMED OUT IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK FLOORBEAM AT FRAME 58, RBL 67 FOUND WITH A 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203 SHT 1 & 2. REPAIR PROFILE FABRICATED AND INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1 & 2. ACCOMPLISHED EA 6-5310-143632. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 60 - 62, X= -55 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT AT FRAME 54 - 54.2, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT AT FRAME 62 - 65, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT FRAME 55/58 - 60, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: SKIN — MISREPAIRED (ZONE 500) · airframe 42,376 hrs · 18,523 cycles
REPAIR FOUND AT LT WING T/E FLAP LOWER SURFACE OTBD AREA RIB 9 & RIB 10. FOUND PREVIOUSLY NOT REPAIRED IAW ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED IAW SRM 57-52-12 REV 79, FIGURE 205. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 51 - 54, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT AT FRAME 54.2 - 55/58, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 54 - 55, X= -35, FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT AT FRAME 43 - 46, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT AT FRAME 60 - 62, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 37 - 38.2, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL AT FRAME 61, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 58 - 60, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. AND INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 54 -55, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 43 - 46, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL AT LT FRAME 40/41-43, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 40/41 - 43, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 35 - 36, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 46 - 51, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: SKIN — DENTED (PAX DOOR) · airframe 42,376 hrs · 18,523 cycles
RT AFT PAX DOOR EXTERIOR SURFACE AFT LOWER EDGE FOUND WITH DENT. REPAIR CARRIED OUT IAW EA 6-5210-14361.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL LT AT FRAME 46 - 51, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR PANEL — DAMAGED (CARGO DECK) · airframe 42,376 hrs · 18,523 cycles
MAIN DECK CARGO FLOOR PANEL RT AT FRAME 38.2 - 40/41, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: SKIN — DENTED (ZONE 100) · airframe 42,376 hrs · 18,523 cycles
RAMP REPORTED DENT 17 IN AFT OF FWD LOWER CARGO DOOR AND APPROX 57 IN UP FROM BOTTOM OF DOOR OPENING. INSP IAW SRM 53-10-12 DIAGRAM 109 WITIN LIMITS OF "B" NO REPAIR REQUIRED. REINSPECT WITHIN 3000 FC. ACFT OK TO CONTINUE. NO RESTRICTION REF: SRM 53-10-12 AFT OF THE FWD CARGO DOOR MX REPORTED A DENT, 17 IN. AFT AND 57 IN ABOVE THE BOTTOM OF THE DOOR OPENING. REF: SRM 53-10-12 INTERMEDIATE ACTION REQUIRED AT OR BEFORE: SPEC: 3,000 CYCLES. EXPIRATION: 21,517 CYCLES, TERMINATING ACTION REQUIRED AT OR BEFORE: NEXT: C-CHECK. DENT FUSELAGE SKIN TRIMMED-OFF BETWEEN FR 26/32 TO FR 33, STR 32R TO 34R IAW SRM 53-10-12, REV 79, FIG 225. HFEC INSP CARRIED OUT IAW NTM 51-10-08, REV 74 FOUND NO CRACKED EVIDENT. REPAIR DOUBLER FABRICATED USING 2024 T3-0.071" AND REPAIR PARTS INSTALLED IAW SRM 53-10-12, REV 79, FIG 225.
2009
Part: BUSHING — MIGRATED (ATTACH FITTING) · airframe 40,379 hrs · 17,175 cycles
NR 2 PYLON TO WING ATTACHMENT FITTING LINK HAS A MIGRATED BUSHING AND IS GOUGED. REMOVED AND REPLACED THE BUSHING IAW A310-200 AMM 54-51-75-8. THE GOUGE IS WITHIN LIMITS IAW AIRBUS DWG A54611761 ON THE NR 2 PYLON TO WING ATTACHMENT FITTING.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOOR SUPPORT STRAP AT FR 65-70 APPROX RBL 20 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT STRAP IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 100 PERCENT MATERIAL LOSS MAT ID LN9497-130 PO NR 0 IAW SRM 53-17-15. ALODINED IAW A310-200 SRM 51-21-10 PRIMED AND PAINTED IAW SRM 51-23-10 PART MARKED FXA5397426320200 IAW GMM 7-0-1001.
Part: FRAME — CORRODED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FRAME 64 " TEE CAP IS CORRODED AT APPORX RBL 42 INCHES. REMOVED & REPLACED FRAME CAP IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. FABRICATED TEE CAP REF DWG A53974220 & A53974290. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10 PART MARKED REF GMM 7-0-1001 REMOVED & REINSTALLED FLOOR PANELS REF AMM 53-10-35-4.
Part: FRAME — CORRODED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FRAME 67, AT APPROX RBL 42 INCHES IS CORRODED ON THE FRAME CAP. REMOVED & REPLACED FRAME CAP IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. PART MARKED IAW GMM 7-0-1001.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOOR SUPPORT IS CORRODED AT FRAME 66; APPROX RBL 42". REMOVED & REPLACED FLOOR SUPPORT STRAP IAW SRM 51-40-21. SUPPORT STRAP FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED & REINSTALLED FLOOR PANELS REF AMM53-10-35-4.
Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 40,324 hrs · 17,147 cycles
THE CAPTAINS WINDSHIELD HEAT SENSOR IS DISBONDED FROM THE WINDSHIELD AT THE LOWER LEFT CORNER. REMOVED & REPLACED CAPTAINS WINDSHIELD PANEL & PERFORMED OPS CHECK REF. MM 56-11-11-4 & 30-42-00-5.
Part: ROLLER TRAY — CORRODED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
THE ROLLER TRAY AT FRAME 29; LBL 12 INCHES IS CORRODED. REMOVED CORROSION IAW A310-200 SRM 51-74-10 & FOUND TO BE OUT IF LIMITS IAW SRM 53-10-15; PG 8; FIG 108. REMOVED & RE-INSTALLED THE LATCHES IAW AMM 25-52-57-4; PG 2; PARA B&D. REMOVED & RE-INSTALLED ROLLER TRAY IAW SRM 51-40-21; PG 7; PARA 5. ALODINED ROLLER TRAY & DOUBLER IAW SRM 51-21-40; PG 8; PARA 5-C. PRIMED & PAINTED ROLLER TRAY & DOUBLER IAW SRM 51-23-10; PG 24; PARA 3B & 3C.
Part: PANEL — DELAMINATED (ZONE 100) · airframe 40,324 hrs · 17,147 cycles
MAIN LANDING GEAR WHEEL WELL PANEL 143 DF IS DISBONDED. FABBED NEW PANEL IAW FEDEX DWG SRZ25-005; REV "G". PART MARKED IAW GMM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
LEFT AFT PAX/CREW DOOR HAS A 5.5 INCH BY .5 INCH AREA OF FRETTING CORROSION ON THE AIRCRAFT SKIN, AT THE UPPER AFT CORNER OF THE DOOR CUT OUT, JUST FWD OF FRAME 75A. ALODINED AREA IAW SRM 51-21-10. PRIMED AREA IAW SRM 51-23-10. PAINTED AREA IAW SRM 51-23-10. FAILSAFE RING INSTALLED ON NON-ROUTINE N01000.
Part: FAILSAFE — CORRODED (PAX DOOR) · airframe 40,324 hrs · 17,147 cycles
RIGHT AFT CREW/PAX DOOR HAS CORROSION ON THE FACE OF THE FAIL SAFE RING, LOWER PORTION OF THE CUT OUT, (23 PLACES). REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-18-12. REMOVED & REPLACED FAILSAFE IAW DWG R53970136. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10.
Part: FAILSAFE — CORRODED (PAX DOOR FRAME) · airframe 40,324 hrs · 17,147 cycles
RIGHT AFT CREW/PAX DOOR CUT OUT HAS 24.5 INCH OF FRETTING CORROSION ON THE OUTER FACE OF THE FAILSAFE RING AT THE UPPER PORTION OF THE CUT OUT, BETWEEN FRAME 73A AND FRAME 75A. ONE SPOT IS AT THE AFT CORNER AND IS 1.250 INCH BY 0.250 INCH BEGINNING AT THE FWD UPPER CORNER. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-18-12. FAILSAFE REPLACED ON FEDEX NON-ROUTINE N01023.
Part: HINGE — SHEARED (CARGO DOOR) · airframe 40,324 hrs · 17,147 cycles
FWD MAIN CARGO DOOR MAIN HINGE, 2ND FROM THE AFT, HINGE HAS 6 ATTACHMENT BOLTS SHEARED. REMOVED AND REPLACED HINGE HASP IN REF TO AMM SUPPLEMENT 52-36-12; PG 401.
Part: STRINGER SPLICE — CORRODED (HORIZONTAL STAB) · airframe 40,324 hrs · 17,147 cycles
LEFT HORIZONTAL STAB FRONT SPAR INBD END OF THE INTERNAL STRUCTURAL STRINGER NR 1 SPLICE IS CORRODED. REMOVED CORROSION REF SRM 51-74-10. OUT OF LIMITS REF SRM 55-11-28. REMOVED APRON SUPPORT FITTING & STRINGER SPLICE REF SRM 51-40-21; PARAGRAPH 7. MACHINED NEW SPLICE REF DWG A55171538. ALODINED; PRIMED & PAINTED SPLICE REF AMM 51-23-10-0. PART MARKED SPLICE P/N A55171538-201 REF GMM 7-0-1001. LOCATED HOLES IN SPLICE REF SRM 51-40-44. INSTALLED SPLICE & APRON FITTING REF SRM 51-40-21; PARAGRAPH 7.
Part: FAILSAFE — CORRODED (PAX DOOR FRAME) · airframe 40,324 hrs · 17,147 cycles
LEFT AFT PAX/CREW DOOR HAS APPROX 30 PLACED OF CORROSION ON THE FACE OF THE FAILSAFE RING, LOWER PORTION OF THE CUT OUT. 2 PLACES OF CORROSION ON THE EDGE OF THE INNER PLATE, JUST FWD OF FRAME 75A, INBD OF THE FAILSAFE RING. REMOVED CORROSION FROM INNER PLATE IAW SRM 57-74-10. REMOVED & REPLACED THE FAILSAFE RING IAW DWG R53970136. FOUND OUT OF LIMITS IAW SRM 53-18-12; FIG 102. INNER PLATE IS WITHIN LIMITS REF SRM 53-10-00. ALODINED REF SRM 51-21-10. PRIMED REF SRM 51-23-10.
Part: FRAME — GOUGED (BS 1870) · airframe 40,324 hrs · 17,147 cycles
MAIN CABIN FRAME 34 L IS GOUGED AT APPROX STRINGER 13 L. BLENDED AREA IN RF TO A310-200 SRM 51-73-10. ORIGINAL MATERIAL 0.236. MATERIAL REMOVED 0.040. MATERIAL REMAINING 0.196 WITHIN LIMITS IN REF TO DAN 26. ALODINED IN REF TO SRM 51-21-10. PRIMED & PAINTED IN REF TO SRM 51-23-10.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
LEFT FWD ENTRY DOOR CUT OUT, LOWER AFT CORNER, CORNER STRAP HAS CORROSION. BLENDED OUT STRAP & FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10. REMOVED & REPLACED STRAP IAW SRM 51-40-21, PG 7.
Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
FWD LOWER CARGO COMPARTMENT DOOR CUT OUT FWD FRAME IS GOUGED ON THE AFT SIDE OF FRAME 20 BETWEEN STRINGER 34R AND 35R. COMPLIED WITH E.A. 6-5310-127915.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 40,324 hrs · 17,147 cycles
CABIN FLOOR PANEL IS BROKEN BETWEEN FRAMES 19 AND 22, RBL 64. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-008; REV "G". MART MARKED IAW GMM 7-0-1000.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
FLOOR PANEL IS CRACKED AT FRAME 54.1, LBL 54.1 AND 70.0. FABRICATED NEW FLOOR PANEL IAW DWG SRZ25-005; REV "G". PART MARKED IAW GMM 7-0-1000.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS CRACKED BETWEEN FRAMES 53 AND 54, RBL 79.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS DAMAGED BETWEEN FRAMES 41 AND 43, RBL 31.0. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "G". PART MARKED PANEL IAW GMM 7-0-1000.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS CRACKED BETWEEN FRAMES 41 42; RBL 87.0. FABRICATED A NEW PANEL FROM FRAME 41 TO 42, RBL 87.0 IAW DWG SRX25-005; REV "G".
Part: FRAME — CRACKED (ZONE 200) · airframe 40,324 hrs · 17,147 cycles
HOLE NR 10 SHOWS A CRACK INDICATION IN THE FRAME ON THE RIGHT SIDE OF THE COCKPIT. REAMED HOLE TO .310 IAW SRM 51-40-44. PERFORMED BHEC INSPECTION OF HOLE NR 10, IAW NTM 51-10-01 A6, INDICATION STILL PRESENT. CLEANED HOLE NR 10 IAW AMM 12-21-13-7, ACCOMPLISHED BHEC OF HOLE NR 10 IAW NTM 51-10-01 A6. NO CRACK FOUND.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS CRACKED BETWEEN FRAMES 53 AND 54, LBL 79. FABRICATED NEW PANEL IAW DWG SRZ25-005; REV "G". PART MARKED IAW GMM 7-0-1000.
Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOORBOARD IS CRACKED AT FRAME 68, LBL 60. FABRICATED NEW PANEL IAW DWG SRZ25-005; REV "G". PART MARKED IAW GMM.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN CARGO COMPARTMENT FLOOR PANEL RIGHT 251 BF IS DAMAGED IN THE AREA OF THE TIE DOWN. FABRICATED NEW PANEL IAW FEDEX DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7-0-1000.
Part: FLOOR PANEL — CRACKED (FUELAGE) · airframe 40,324 hrs · 17,147 cycles
FLOOR PANEL IS CRACKED BETWEEN FRAMES 51 AND 50, RBL 17.0 TO RBL 37. FABRICATED NEW FLOOR PANEL AT FRAME 50 - 51 IAW DWG SRZ 25-005; REV " G ". PART MARKED IAW GMM 7-0-1000.
Part: PANEL — DENTED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT SLANT PANEL 161 CW IS DENTED.
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 132 YF IS DELAMINATED AND THE EDGES ARE DAMAGED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV " G ". PART MARKED PANEL IAW GMM 7-0-1000.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 152 EF IS PUNCTURED AND DELAMINATED. REPAIRED FLOOR PANEL IAW SRM 53-10-20.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT SLANT PANEL 161 AW IS DENTED AND PUNCTURED. FABRICATED NEW PANEL IAW DWG SRZ 25-005, REV G. FABRICATED TOP SHEET IAW DWG 25-011, REV C. PART MARKED IAW GMM 7-0-1000.
Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOORBOARD 161 BF IS DENTED, PUNCTURED AND DELAMINATED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV G. FABRICATED TOP SHEET IAW DWG 25-011, REV C.
Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOORBOARD 161 AFT IS DENTED, PUNCTURED AND THE BOTTOM IS CORRODED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV G. FABRICATED TOP SHEET IAW DWG 25-011, REV " C ".
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOORBOARD 162 HF IS DENTED AND DELAMINATED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV " G ". FABRICATED TOP SHEET IAW DWG 25-011, REV " C ".
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOORBOARD 161 GF IS DENTED AND DELAMINATED. FABRICATED NEW PANEL IAW DWG SRZ 25-005, REV G. FABBED TOP SHEET IAW DWG SRZ 25-011, REV C. PART MARKED IAW GMM 7-0-1000.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
AFT CARGO COMPARTMENT FLOORBOARD 151 EF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV " G ". PART MARKED PANEL IAW GMM 7-0-1000.
Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOORBOARD 162 EF IS DENTED. REPAIRED IAW DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1001.
Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
BULK CARGO COMPARTMENT FLOORBOARD 161 HF IS DENTED, PUNCTURED AND THE TOP IS CORRODED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV G. FABRICATED TOP SHEET IAW DWG SRZ 25-011, REV C. BONDED TOP SHEET IAW DWG SRZ 25-011, REV C.
Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 131 HG HAS EDGE DAMAGE. REPAIRED FLOOR PANEL 131 HG IAW DWG SRZ 25-005; REV "G".
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
AFT CARGO COMPARTMENT FLOORBOARD 151 CF CORNERS ARE BROKEN AND DELAMINATED. FABRICATED NEW FLOOR PANEL 151 CF IAW DWG SRZ 25-005; REV " G ". PART MARKED PANEL IAW GMM 7-0-1000.
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 131 QF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV " G ". PART MARKED PANEL IAW GMM 7-0-1000.
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 132 QF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV " G ". PART MARKED PANEL IAW GMM 7-0-1000.
Part: FLOORBOARD — BROKEN (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 132 RF EDGE IS BROKEN AT A SCREW HOLE.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN CARGO COMPARTMENT FLOOR PANEL 251 BF IS DAMAGED IN THE AREA OF THE TIE DOWN BEAM.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 40,324 hrs · 17,147 cycles
AFT CARGO COMPARTMENT FLOORBOARD 152 FF HAS MULTIPLE PUNCTURES. REPAIRED IAW SRM 53-10-20.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 40,324 hrs · 17,147 cycles
FWD CARGO COMPARTMENT FLOORBOARD 132 ZF IS BROKEN. REPAIRED FWD CARGO COMPARTMENT FLOORBOARD 132 ZF IAW DWG SRZ25-005, REV "G".
Part: RIB — BROKEN (VERTICAL STAB) · airframe 40,324 hrs · 17,147 cycles
VERTICAL STABILIZER RIB NR 8 IS BROKEN AT THE LEFT REAR EDGE AT THE ATTACHMENT POINT TO THE REAR SPAR. COMPLIED WITH E.A. 6-5530-127910 REV. A.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 40,324 hrs · 17,147 cycles
MAIN CABIN FLOOR PANEL IS BROKEN BETWEEN FRAME 19 AND FRAME 22, RBL 64 INCHES.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT IS CRACKED AT FRAME 45, RBL 35.0. REMOVED & REPLACED THE FLOOR PANEL SUPPORT IAW A310-200 SRM 51-40-21.
Part: SKIN — GOUGED (LT WING) · airframe 40,324 hrs · 17,147 cycles
LT WING LWR SKIN LOWER SURFACE IS GOUGED AT THE FWD SPAR ATTACHMENT BETWEEN THE PRESSURE FUELING CAPS.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
THE SEAT TRACK AT FRAME 54.2 IS GOUGED LBL 54.0. BLENDED OUT DAMAGE IN REF TO SRM 53-10-16; FIG 101. REMOVED DAMAGED SEAT TRACK SECTION & 3 EA FITTINGS IN REF TO SRM 53-10-16; FIG 208. FABRICATED A NEW SEAT TRACK SECTION & SPLICES IN REF TO SRM 53-10-16; FIG 208. ALODINED; PRIMED & PAINTED IN FRE TO SRM 51-21-10. INSTALLED SEAT TRACK SECTION; SPLICES & THREE FITTINGS IN REF TO SRM 53-10-16; FIG 208.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT IS CRACKED AT FRAME 43, RBL 34.0. REMOVED & REPLACED THE FLOOR PANEL SUPPORT IAW A310-200 SRM 51-40-21.
Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS CRACKED BETWEEN FRAME 53 AND FRAME 54; LBL 79.
Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS CRACKED BETWEEN FRAME 53 AND FRAME 54; RBL 79.
Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS CRACKED BETWEEN FRAME 41 AND FRAME 42; RBL 87.0.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
THE FLOORBOARD IS CRACKED AT FRAME 54.1; LBL 54.1 AND LBL 70.0.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT IS CRACKED AT FRAME 44, RBL 34.0. REMOVED & REPLACED THE FLOOR PANEL SUPPORT IAW A310-200 SRM 51-40-21.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 40,324 hrs · 17,147 cycles
MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS DAMAGED BETWEEN FRAME 41 AND FRAME 43; RBL 31.0.
Part: SKIN — DENTED (L1 DOOR) · airframe 40,324 hrs · 17,147 cycles
THE L-3 DOOR OUTER SKIN HAS 1 SMALL DENT; AFT OF FRAME 74 AND STRINGER 26L. CHECKED DENT & FOUND IT TO BE OUT OF LIMITS IN REF TO SRM 52-10-00; FIG 102. REMOVED DAMAGED AREA & FABRICATED A REPAIR DOUBLER IN REF TO SRM 52-10-00; FIG 206. ALODINED REPAIR DOUBLER IN REF TO SRM 51-21-10. PRIMED DOUBLER IN REF TO SRM 51-23-10. INSTALLED REPAIR DOUBLER IN REF TO SRM 52-10-00; FIG 206. TOPCOATED REPAIR DOUBLER IN REF TO SRM 51-23-10.
Part: SKIN — DENTED (L3 DOOR) · airframe 40,324 hrs · 17,147 cycles
THE L-3 DOOR OUTER SKIN HAS 1 DENT AT FRAME 75 AND STR 25L. CHECKED DENT & FOUND IT TO BE OUT OF LIMITS IN REF TO SRM 52-10-00; FIG 102. REMOVED DAMAGED AREA & FABRICATED A REPAIR DOUBLER IN REF TO SRM 52-10-00; FIG 206. ALODINED REPAIR DOUBLER IN REF TO SRM 51-21-10. PRIMED DOUBLER IN REF TO SRM 51-23-10. INSTALLED REPAIR DOUBLER IN REF TO SRM 52-10-00; FIG 206. TOPCOATED REPAIR DOUBLER IN REF TO SRM 51-23-10.
Part: FLOORBEAM — BENT (ZONE 200) · airframe 40,324 hrs · 17,147 cycles
MAIN CARGO COMPARTMENT FLOOR SUPPORT BEAM AT FRAME 54.1 BETWEEN RBL 17 TO RBL 37 IS BENT. REMOVED & INSTALLED BEAM IN REF TO SRM 51-40-21; PARA 5. DRILLED & DEBURRED NEW BEAM IN REF TO SRM 51-40-21; PARA 5.
2008
Part: SUPPORT — CRACKED (PRECOOLER) · airframe 40,324 hrs · 17,147 cycles
NR 1 PRECOOLER SUPPORT IS CRACKED. MATERIAL ID PER ASTME-1476-01 & WELD PER P.S. 01-04-21.
2006
Part: SLAT SYSTEM — MALFUNCTIONED (LE SLATS) · airframe 38,215 hrs · 15,891 cycles
TURNING FINAL AT 3000' SELECTED SLATS EXTEND. NO SLAT EXTENSION NOTED AND ECAM INDICATED SLATS FAULT LIGHT. CYCLED HANDLE FOUR TIMES NO IMPROVEMENT. EMERGENCY DECLARED, LANDED WITH NO SLATS FLAPS 40 APPROACH, FOLLOWING RED TABS. AFTER TOUCHDOWN HANDLE WAS RECYCLED AND SLATS EXTENDED NORMALLY CHECKED SFCC AND FOUND SLAT JAM ON BOTH SFCC'S, RESET SFCC'S AND OPERATED SLATS NUMEROUS TIMES AND NO FAULTS. CHECKED SYSTEM TORQUE LIMITERS AND SCREW JACK LOCK, OUT INDICATORS AND NONE WERE TRIPPED, REF M/M 27-84-00-5 AND 27-84-00-0. NO HISTORY NINTY DAYS. A/C OK FOR SERVICE.