N493FE
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.
198 reports on file, 1996-03-25 – 2011-07-26.
Part: SKIN — DAMAGED (BS 440) · airframe 42,964 hrs · 28,450 cycles
TRAPPED RIVET AT UPPER AND LOWER BUTT SEAM DOUBLER FOR SURROUND STA 440, STR 21L TO 22L. ACCOMPLISHED TRIM OUT AT BS 440 STR 21L TO 22L IAW EA 3 7-5330-136786.
Part: SKIN — DAMAGED (BS 440 S23L) · airframe 42,964 hrs · 28,450 cycles
PILOT HOLE ON MCD SURROUND DOUBLE BESIDE BLIND FASTENER STA 440, STR 23L. REPAIRED IAW EA 7-5330-136786.
Part: STRUCTURE — CRACKED (TE FLAP) · airframe 42,964 hrs · 28,450 cycles
LT WING INBD MIDFLAP T/E CHORD CRACKED AT INBD AFT FLAP CONTROL ROD CUTOUT DAMAGED AREA OF CHORD EXTRUSION IAW SRM 51-40-4, FIG 1, 4' 9.5" AND FABRICATED SPLICE FROM 7075T6 9.75" IAW SRM 51-40-4, FIG 1. INSTALLED SPLICE IAW SRM 51-30-2 AND FABRICATED REPAIR SECTION CHORD FROM EXTRUSION 7075T6, 57.375" IAW SRM 51-40-4, FIG 1 AND INSTALLED CHORD SECTION IAW SRM 51-30-2.
Part: FRAME — CORRODED (BS 620 S23-26L) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
FWD CARGO FRAME BS 620 BETWEEN STR 23L -STR 26L HAS CORROSION & DOUBLE DRILLED HOLES FOUND DURING REPAIR OF SURROUND DOUBLER. REMOVED DAMAGED FRAME IAW SRM 51-30-2. FABRICATED NEW FRAME SECTION IAW DRAWING 65-15934. INSTALLED FRAME SECTION IAW SRM 51-30-2 AND DRAWING 65-15934.
Part: SEAT TRACK — CORRODED (BS 855) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
SEAT TRACK CORRODED STA 855, LBL 25. REMOVED CORRODED SEAT TRACK SECTION LBL 25 FROM BS 850 - 870. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2, SRM 53-10-2 FIG 7, SRM 51-30-5, SRM 51-10-2.
Part: FRAME SPLICE — CORRODED (BS 620 S26-27L) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
FRAME SPLICE SEGMENT AT BS 620, STRINGER 27- 26 LT IS CORRODED. REMOVED FRAME SPLICE SEGMENT AT BS 620, STR 27L TO 26L IAW SRM 51-30-2. FABRICATED FRAME SEGMENT IAW DWG 51FX521 AND 53FX1497. INSTALLED FRAME SEGMENT IAW SRM 51-30-2.
Part: FAILSAFE — CORRODED (BS 620 S3-26L) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
FWD CARGO BS 620 BETWEEN STRINGER 3L - 26L FRAME FAILSAFE HAS DOUBLE DRILLED HOLES AND LIGHT CORROSION. REMOVED DAMAGED FAILSAFE, FABRICATED & INSTALLED NEW FAILSAFE IAW SRM 51-30-2, SRM 53-10-2 FIG 3, SRM 51-30-5, SRM 51-10-2 & FAS ER 2-37153-801 REV A, AND SRM 51-20-1 FIG 7.
Part: SKIN — MISREPAIRED (BS 620 S25-27L) · airframe 42,964 hrs · 28,450 cycles
FASTENERS WITH INSUFFICIENT ON CENTER SPACING AT STA 620 DOUBLER, STR 27L TO STR 25L. REPAIRED IAW EA 7-5330-136777.
Part: SKIN — DENTED (BS 418 S1-2L) · airframe 42,964 hrs · 28,450 cycles
DENT STA 418, BETWEEN STR 1L- 2L. CUTOUT DAMAGE AREA, FABRICATED REPAIR DOUBLER, AND INSTALLED IAW SRM 53-30-3, FIG 1, SRM 51-10-2, SRM 51-30-8 AT BS 418 BETWEEN STR 1L TO 2L.
Part: DOUBLER — CORRODED (BS 1135) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CCORROSION AT LBL 25 SEAT TRACK, STA 1135 DOUBLER. REMOVED DOUBLER IAW SRM 51-10-3, FABRICATED DOUBLER IAW DWG 53FX939 AND TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2.
Part: FLOORBEAM — GOUGED (BS 950) · airframe 42,964 hrs · 28,450 cycles
STA 950 FLOORBEAM TOP STRAP GOUGED, LBL 50. CUTOUT DAMAGED AREA OF BS 950 FLOORBEAM UPPER STRUCTURE, FABRICATED, AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 11.
Part: STRINGER — CRACKED (BS 640 S26L) · airframe 42,964 hrs · 28,450 cycles
FWD CARGO COMPARTMENT STRINGER 26L CRACKED ON OTBD SIDE AT BS 640. REMOVED DAMAGED AREA OF STRINGER, FABRICATED AND INSTALLED REPAIR IAW SRM 51-30-2, 53-10-3 FIG 1, AND 51-10-2.
Part: SKIN — DENTED (BS 1070-1110) · airframe 42,964 hrs · 28,450 cycles
DENT LOWER FUSELAGE SKIN STA 1070-1110, STR 21L. CUTOUT DAMAGE, FABRICATED, & INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-30-3 FIG 1 & 14, SRM 51-10-2, SRM 51-30-8, & SRM 51-30-2.
Part: FLOORBEAM — DAMAGED (BS 348) · airframe 42,964 hrs · 28,450 cycles
FWD LAV AREA FLOORBEAM STA 348, RBL 12 UNDERSIDE OF TOP TEE ANGLE, REPAIR HAS MISSED DRILLED FASTENER HOLE ALONG BACKSIDE EDGE AND INTO VERTICAL FILLER. FABRICATED REPAIR ANGLE SPLICES, CUTOUT DAMAGED OF TOP TEE, FABRICATED TOP TEE, INSTALLED NEW SECTION OF TOP TEE, HEAT TREATED ANGLES TO 7075T6, AND INSTALLED REPAIR ANGLES IAW SRM 53-10-8 FIG 9 AND SRM 51-30-2 AND FAS ER 2-37153-801 REV A.
Part: SHEAR TIE — CORRODED (BS 700 S28L/R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON SHEAR TIE AT BS 700 (AFT SIDE) BETWEEN STRINGER 28L AND 28R. REMOVED DAMAGED MATERIAL DIM 10" X 2" IAW SRM REV 103, 51-10-1. FABRICATED NEW SHEAR TIE DIM 10" X 2" 7075 T6 .050" IAW SRM 53-10-4. INSTALLED SHEAR TIE IAW SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 700 S28L/R) · airframe 42,964 hrs · 28,450 cycles
CORROSION ON SHEAR TIE AT BS 700 BETWEEN STRINGER 28R AND 28L. REMOVED DAMAGED AREA IAW SRM REV 103, 51-10-1. FABRICATED SHEAR TIE AND DOUBLER IAW SRM 53-10-4. INSTALLED SHEAR TIE & DOUBLER IAW SRM 51-30-2 AND 53-10-4 FIG 13.
Part: SEAT TRACK — CORRODED (BS 950) · airframe 42,964 hrs · 28,450 cycles
LBL 25, SEAT TRACK CORRODED - STA 950 - 950 PLUS 10". REMOVED DAMAGED SEAT TRACK SECTION FROM BS 870 - 950 PLUS 10" LBL 25. FABRICATED NEW SEAT TRACK SECTION. FABRICATED NEW ANGLES SPLICES (2) AND 1 STRAP SPLICE. INSTALLED NEW SEAT TRACK SECTION AND SEAT TRACK SPLICES IAW SRM 53-10-1 FIG 1, SRM 51-30-2, SRM 53-10-5 FIG 1, SRM 51-30-5, SRM 51-10-2 AND SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 720 S28L/R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON SHEAR TIE AT BS 720 BETWEEN STRINGER 28L AND 28R. CUT OUT DAMAGED SHEAR TIE AT BS 720 BETWEEN STR 28L AND 28R IAW SRM REV 103, 51-10-1. FABRICATED SHEAR TIE AND DOUBLER IAW SRM 53-10-4 FIG 13. INSTALLED SHEAR TIE AND DOUBLER IAW SRM 53-10-4 FIG 13 AND 51-30-2.
Part: SEAT TRACK — CRACKED (BS 950-1010) · airframe 42,964 hrs · 28,450 cycles
SEAT TRACK FLANGE SHEARED OFF, MISSING MATERIAL - RBL 45. SEAT TRACK RUN IS STATION 950F -1010 PLUS 10". REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW AND INSTALLED SEAT TRACK IAW SRM 53-10-5 FIG 1.
Part: SEAT TRACK — CORRODED (BS 950C-950F) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION - RBL 45, SEAT TRACK, STA 950C - 950F PLUS 10". REMOVED SEAT TRACK AT 950 PLUS 10" TO 950F RBL 45 IAW B727 SRM 51-30-2. FABRICATED SEAT TRACK SECTION AT 950 PLUS 10" TO 950F RBL 45, IAW SRM 53-10-2 FIG 1 AND SRM 53-10-5 FIG 1. TREATED AND PRIMED SEAT TRACK, IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 870-950) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION - RBL 45, SEAT TRACK, STA 870 - 950, PLUS 10". REMOVED SEAT TRACK RBL 45 STA 870 - 950 PLUS 10" IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, IAW SRM 53-10-5 FIG 1 AND FABRICATED NEW SPLICES AND 2 EACH ANGLES IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED SEAT TRACK AND SPLICE STRAP, 2 EACH ANGLES. INSTALLED SEAT TRACK RBL 45 STA 870 - 950 PLUS 10" AND SPLICE STRAP, 2 EACH ANGLE IAW SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION SEAT TRACK FLANGE, NUMEROUS AREAS, RBL 24 STA 480-360. REMOVED SEAT TRACK SECTION, FABRICATED NEW SECTION OF SEAT TRACK, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 950-1070) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION LBL 25, SEAT TRACK, STA 950 PLUS 10" TO STA 1070 PLUS 10". REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1, TREATED AND PRIMED SEAT TRACK SECTION IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION IAW SRM 51-30- 2.
Part: SEAT TRACK — CORRODED (BS 380-480) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
SEAT TRACK FLANGE CORRODED IN SEVERAL AREAS LBL 24, STA 380 - 480. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON LOWER SPLICE PLATE RBL 25 SEAT TRACK, STA 950, PLUS 10". REMOVED DAMAGED SPLICES STRAP AND ANGLE FROM RBL 25 STA 950 PLUS 10" IAW SRM 51-30-2. FABRICATED NEW STRAP FROM 7075-T6 .250 DIM: 9.25" X 2" AND 2 EA. ANGLES FROM BAC 1503-100122, DIM: 12.9" IN LENGTH IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW SPLICE STRAP AND 2 EA. ANGLES. IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 51-30-2.
Part: FLOORBEAM — GOUGED (BS 950F) · airframe 42,964 hrs · 28,450 cycles
FLOORBEAM UPPER FLANGE UPPER SURFACE IS GOUGED STA 950F, RBL 3- RBL 6. CUTOUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PARTS ON FLOORBEAM UPPER FLANGE IAW SRM 53-10-8 FIG 3.
Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORRODED SEAT TRACK FLANGE NUMEROUS AREA'S LBL 24 STA 690 TO STA 480. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 SRM 53-10-5 FIG 1, SRM 51-10-2 AND SRM 51-30-2.
Part: SKIN — GOUGED (BS 1050 S27-28R) · airframe 42,964 hrs · 28,450 cycles
GOUGE LOWER FUSELAGE STA 1050, STR 27R-28R. CUT OUT DAMAGED SKIN IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER IAW SRM REV 103, 53-30-3 FIG 1 AND 53-30-2 FIG 2. INSTALLED DOUBLER IAW SRM 53-30-3 FIG 1.
Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION, LBL 45, SEAT TRACK STA 950, PLUS 10". REMOVED SEAT TRACK AND SPLICE AND ANGLES STA 950 PLUS 10" - 950E PLUS 10" IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, ANGLES AND STRAP IAW SRM 53-10-5 FIG 1 REV 103. TREATED AND PRIMED SEAT TRACK ANGLE AND STRAP IAW SRM 51-10-2. INSTALLED SEAT TRACK IAW SRM 51-30-2.
Part: SKIN — GOUGED (BS 620 S4L) · airframe 42,964 hrs · 28,450 cycles
INNER SURROUND SKIN GOUGED STA 620, STR 4L. REMOVED DAMAGED MCD INNER SURROUND AFT SKIN, FABRICATED & INSTALLED NEW SKIN IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, & SRM 53-10-2 FIG 3A.
Part: SKIN — CRACKED (BS 413) · airframe 42,964 hrs · 28,450 cycles
R1 DOOR CUTOUT AFT LOWER CORNER BS 413 HAS SKIN CRACKED FROM EDGE TO FASTENER. CUTOUT DAMAGED R1 DOOR AFT CORNER, FABRICATED & INSTALLED REPAIR DOUBLER & FILLER IAW SRM 51-30-2, 51-10-1, 51-10-2, & EO 7-5313-7-2304 P2.
Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION SEAT TRACK FLANGES NUMEROUS AREAS BL 0 BS 360-480. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 720D S25-26R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON SHEAR TIE AT BS 720D BETWEEN STRINGER 26R AND 25R. REMOVED SHEAR TIE IAW SRM REV 103, 51-30-2 FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15 AND 53-10-2 FIG 3 INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15
Part: SKIN — DENTED (NR 5 SLAT) · airframe 42,964 hrs · 28,450 cycles
NR 5 SLAT UPPER SKIN INBD OF FENCE HAS A DENT. CUT OUT DAMAGE 5 3/4" X 3 1/2" IAW SRM 57-50-3 FIG1 REV. 103, FABRICATED FILLER IAW SRM 57-50-3. FABRICATED DOUBLER IAW SRM 57-50-3. INSTALLED FILLER & DOUBLER IAW SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 640 S28L/R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON SHEAR TIE AT BS 640 BETWEEN STRINGER 28L AND 28R. CUT OFF LOWER LEG OF FRAME IAW SRM 53-10-4 FIG 13 REV 103. FABRICATED REPAIR DOUBLER AND SHEAR TIE IAW SRM 53-10-4 FIG 13. INSTALLED DOUBLER AND SHEAR TIE IAW SRM 51-30-2 AND 53-10-4 FIG 13.
Part: SHEAR TIE — CORRODED (BS 620 S28L/R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON SHEAR TIE AT BS 620 BETWEEN STRINGER 28L AND 28R. REMOVED DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED REPAIR PARTS, DOUBLER, & SHIMS IAW SRM 53-10-4 FIG 13. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-4 FIG 13 REV 103.
Part: SHEAR TIE — CORRODED (BS 680 S28L/R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
FWD CARGO COMPT, BS 680 FRAME IS CORRODED ON THE AFT SIDE BETWEEN STR 28L - 28R, BELOW FAILSAFE CHORD. FOUND CORROSION TO BE OUT OF LIMITS ON FRAME SHEAR TIE IAW SRM 51-10-6 AND 53-10-1 FIG 1. CUT OUT DAMAGED SECTION OF SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED REPAIR PARTS IAW SRM 53-10-4 FIG 13. INSTALLED REPAIR PARTS ON FRAME IAW SRM 53-10-4 FIG 13.
Part: SEAT TRACK — CORRODED (BS 950A-950F) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION RBL 25, SEAT TRACK STA 950A - 950F, 10". REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM BAC 1520-7178-T6511 IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW SEAT TRACK, IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2
Part: SEAT TRACK — CORRODED (BS 690) · corrosion level 2 · airframe 41,441 hrs · 28,748 cycles
CORROSION SEAT TRACK MAIN CABIN STA 690, RBL 24. REMOVED DAMAGE SEAT TRACK & FABRICATED NEW SEAT TRACK SECTION & FABRICATED NEW SPLICES, ANGLES, & STRAP. INSTALLED NEW PARTS IAW SRM 53-10-1, FIG 3 & 51-30-2.
Part: SEAT TRACK — CORRODED (BS 720E) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORRODED SEAT TRACK FLANGE NUMEROUS AREAS MAIN CABIN STA 720E, PLUS 10", BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2, REMOVED & FABRICATED INTERCOSTAL IAW SRM 51-30-2, SRM 53-10-2 , & SRM 51-20-1. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7A & 53-10-5, TREATED & PRIMED INTERCOSTAL & SEAT TRACK IAW SRM 51-10-2, INSTALLED SEAT TRACK & INTERCOSTAL IAW SRM 51-30-2.
Part: STRINGER — CORRODED (BS 740 S27R) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION ON STRINGER 27R AT BS 740 BULKHEAD. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1 REV 103. FABRICATED STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER AND SPLICE IAW SRM 51-30-2 & 53-10-3 FIG 1.
Part: SEAT TRACK — CORRODED (BS 785-850) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
SEAT TRACK CORRODED STA 785-850 LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK IAW SRM 51-30-2, SRM 51-10-2 & DWG 65-16279 REV G.
Part: FLANGE — CORRODED (BS 690-740) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
SEAT TRACK FLANGE CORRODED, NUMEROUS AREAS STA 740 - STA 690, LBL 24. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION. FABRICATED ANGLE SPLICES (2) AND STRAP SPLICE. INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW SRM 51-30-2, SRM 53-10-5 FIG 1, SRM 51-10-2 AND SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
CORROSION SEAT TRACK FLANGE NUMEROUS AREAS MAIN CABIN STA 690 -STA 480, LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED & INSTALLED NEW SEAT TRACK IAW SRM 51-30-2, SRM 51-10-2 & SRM 53-10-5 FIG 1.
Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 42,964 hrs · 28,450 cycles
FLOORBEAM CORRODED STA 620 BL 0 TO LBL 24. CUTOUT DAMAGED AREA IAW SRM 51-10-2. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 3. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 51-30-2.
Part: MOUNT — CRACKED (NR 8 SLAT) · airframe 42,964 hrs · 28,450 cycles
NR 8 SLAT INBD TRACK MOUNT OTBD CORNER IS CRACKED IN RADIUS. STOP DRILLED CRACK, FABRICATED & INSTALLED REPAIR DOUBLER AT NR 8 SLAT IB TRACK MOUNT IAW SRM 51-10-2, SRM 51-10-1, SRM 51-30-2, & DWG SR27-57-034 & EA 7-5750-136792.
Part: SKIN — DENTED (BS 720 S18L) · airframe 42,964 hrs · 28,450 cycles
DENT EXTERIOR FUSELAGE STA 720, STR 18L. CUT OUT DAMAGED SECTION OF SKIN AT BS 720 STR 18L IAW B727 SRM REV 103, 53-30-3 FIG 3. FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3. INSTALLED DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3.
Part: STRUCTURE — MISINSTALLED (FUSELAGE) · airframe 42,964 hrs · 28,450 cycles
RAIN GUTTER ABOVE L-1 DOOR HAS IMPROPER FASTENERS INSTALLED. REPAIRED FUSELAGE SKIN COMMON TO L1 DOOR RAIN GUTTER IAW EA 7-5330-136775.
Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 42,964 hrs · 28,450 cycles
LT WING INBD FOREFLAP L/E GOUGE AT REPAIR. REMOVED REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND INSTALLED NEW DOUBLER IAW SRM 51-30-2 & EA 7-5750-153124.
Part: ENGINE — OVERTEMP (NR 2) · airframe 42,854 hrs · 28,356 cycles
RT WINDSHEAR WARNING ON APPROACH TO RWY 14, MISSED APPROACH WITH FIREWALL POWER AT 640MSL & WENT TO CLIMB AT 1100MSL. NO ENGINE PAREMETERS OBSERVED. ANALYSIS CONFIRMED THE NR 1 & NR 3 ENG EGT, N1 & N2 WERE WITHIN LIMITS. NR 2 ENG EXPERIENCED & EGT OVERTEMP OVER 630 DEGREES C FOR APPROX 29 SECOND IAW REF 5. 1 & NR 3 DID NOT EXCEED EGT, N1, OR N2 OPERATION LIMITS. BORESCOPE OF HOT SECTION, & 1ST STAGE TURBINE REF MM 72-00-00, INSPECTION CHECKED 01. NO DEFECTS, DISCOLORATION OR OTHER INDICATION OF OVERTEMP DAMAGE NOTED. PERFORMED BORESCOPE OF NR 2 ENGINE HOT SECTION AND 1ST STAGE TURBINE BLADES. NO DEFECTS, DISCOLORATION OR OTHER DEFECTS NOTED. COMPLIED WITH EA 7-7100-149350.
Earlier reports · 1996–2009 · 148 reports
2009
Part: OIL SYSTEM — LOW PRESSURE (NR 3 ENGINE) · airframe 42,035 hrs · 27,680 cycles
DURING CLIMB OUT OF MEM LOST NR 3 OIL PRESS AND OIL TEMP. C/B FOR OIL TEMP AND PRES HOT TO TOUCH AFTER APPROX 5 MINS, WOULD NOT RESET. PERFORMED PRECAUTIONARY SHUTDOWN ENG NR 3 IAW QRH RAN ENG AT IDLE 3 MINUTES PRIOR TO SHUTDOWN.
2008
Part: SKIN — CORRODED (ZONE 100) · airframe 41,466 hrs · 27,228 cycles
LWR FUSELAGE SKIN BETWEEN STA 950B AND 950C AT BL0 IS BULDGING WITH 2 EACH RIVET HEADS POPPED. COMPLIED WITH EA 7-5330-124049 PART 1 BY MANUFACTURING FILLER, DOUBLER AND TRIPLER OUT OF2024T3 180/90/100C. REMOVED DAMAGE AND INSTALLED PARTS ALL IAW EA 7- 5330-124049 PART 1. MAJOR REPAIR RII.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,466 hrs · 27,228 cycles
UPPER CARGO COMPARTMENT STA 770 BL24L SEAT TRACK LOBE CORRODED REMOVED PANEL TO GAIN ACCESS IAW 51-30-2 AND REMOVED CORRODED SEAT TRACK AT STA 760-848; BL 24L IAW SRM 53-10-5. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5. TREATED AND PRIMED IAW SRM 51-10-2, AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-5. INSTALLED FLOOR PANEL IAW SRM 51-30-2. MAJOR REPAIR RII.
2007
Part: WARNING HORN — FALSE ACTIVATION · airframe 40,432 hrs · 26,385 cycles
REJECTED TAKEOFF AT 75 KTS, ACFT WEIGHT 130,000 DUE TO UNSCHEDULED AIRSPEED/MACH AURAL WARNING SYSTEM MEL 12MAY07 03:27, BFM R ACN RELEASED FOR SERVICE PER MEL/CDL: 34-04-03 CATEGORY: B EXPIRATION: 15MAY07. MEM R PERFORMED MACH AURAL WARN TEST IAW 727-200 M/M 34-14-002-5 AND NO FAULTS FOUND, UNABLE TO DUPLICATE REPORTED DISCREPANCY. REMOVED AND REPLACED BOTH CAPT'S AND F/O'S MACH AIRSPEED INDICATORS IAW 727-200 M/M 34-12-021-4.
Part: OIL SYSTEM — UNKNOWN (NR 1 ENGINE) · airframe 40,221 hrs · 26,229 cycles
NR 1 ENG OIL QUANTITY BEGAN TO DECREASE SHORTLY AFTER T/O WITH ASSOCIATED NOTICEABLE DECREASE IN OIL TEMP, (OUT OF LIMITS) PRECAUTIONARY ENGINE SHUTDOWN. OIL QTY DECREASED TO BELOW 1 GAL. AFTER SHUTDOWN OIL QTY ROSE AGAIN TO 4 GALS. DUE TO THE FACT THAT THE AIRCREW SHUT DOWN THE ENG INFLIGHT AND WINDMILLED. THE FLIGHT CREW WAS UNABLE TO ID HOW MUCH OIL PRESSURE THEY HAD DURING WIND-MILLING PER AMM MIN OIL PRESSURE 10 PSI.
2006
Part: TIRE — UNKNOWN (NLG) · airframe 39,887 hrs · 25,968 cycles
REJECTED TAKEOFF 40-50 KTS, DUE TO AIRCRAFT SHUDDER SUSPECTED COMPRESSOR STALLS. NO ABNORMALS NOTED ON ANY ENGINES AFTER THROTTLES RETARDED. RAN APPROPRIATE QRH PROCEDURES. INSPECTED ENG'S FOR HIGH PWR STALL IAW MM 71-00-000-6 1 WITH NO FAULTS FOUND. DURING DEBRIEF FLT CREW REPORTED THAT THEY SAW NO ABNORMAL PARAMETERS BUT FELT MORE OF A SHUDDER IN THE NOSE AREA OF THE AIRCRAFT. INSP NOSE GEAR TO FIND RT N/WHEEL SEVERELY OUT OF ROUND. REMOVED AND REPLACED BOTH LT AND RT NOSE WHEELS IAW M/M 32-45-011-4.
Part: GASPER FAN — FAILED (CABIN) · airframe 39,769 hrs · 25,878 cycles
NOXIOUS ODORS IN THE COCKPIT. EXECUTED PHASE ONE PROCEDURES FOR FUMES IN THE COCKPIT. AFTER REMOVAL OF GASPER FAN, VERIFIED FAN WAS BAD. REMOVED AND REPLACED GASPER FAN IAW M/M 21-23-011-4. ALSO, REMOVED AND REPLACED GASPER FAN C/B C818 PER SMP AND WDM 21-11-01. GASPER FAN OPS CHECKS NORMAL IAW MM 21-23-011-4.
Part: HYDRAULIC SYSTEM — MALFUNCTIONED (A SYSTEM) · airframe 39,653 hrs · 25,790 cycles
THE FLIGHT CREW PERFORMED AIR TURNBACK, INVOKED BY LOSS OF A-SYSTEM HYDRAULIC FLUID INFLIGHT, DURING CLIMBOUT FOR SCHEDULED FLIGHT 0307 FROM MEM, ON 07/28/2006.
Part: FITTING — CORRODED (T/E FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 6 FLAP TRACK FORWARD FITTING IS CORRODED ON INBOARD FACE. REPAIRED PER STANDARD REWORK DRAWING SR 27-57-020A.
Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 1 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REPAIRED PER FED EX EA 7-5740-102247.
Part: ATTACH FITTING — CORRODED (T/E FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 8 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED ON INBOARD FACE. REPAIRED PER FED EX EA 7-5740-102247.
Part: STRUCTURE — MISDRILLED (HORIZ STAB) · airframe 39,586 hrs · 25,731 cycles
MIS-DRILLED HOLE IN PANEL SUPPORT AT FWD, CENTER, LT SIDE OF HORIZONTAL STAB JACKSCREW COMPARTMENT. REPAIRED PANEL SUPPORT PER SRM 51-40-4 FIG 1
Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
STRINGER CLIP AT BS 950A STR 7 RT HAS 2 EA EXTRANEOUS HOLES. REMOVED STRINGER CLIP AT BS950A STR 7 RT AND REPLACED WITH REPLACEMENT STRINGER CLIP AT BS 950A STR 7 RT PER SRM 51-30-2 AND SRM 51-30-5.
Part: HINGE FITTING — DAMAGED (LT AILERON) · airframe 39,586 hrs · 25,731 cycles
LEFT WING OUTBOARD AILERON OUTBOARD BALANCE BAY, FWD HINGE HALF ATTACH POINT IS ABRAIDED AT THE OUTBOARD AND INBOARD EDGES AT THE APEX OF THE BENDS. REPAIRED PER FED EX EA 7-5710-100548.
Part: SUPPORT ANGLE — CHAFED (LT AILERON) · airframe 39,586 hrs · 25,731 cycles
LEFT O/B AILERON I/B BALANCE PANEL FWD HINGE SUPPORT ANGLE HAS CHAFING DAMAGE AT I/B AND O/B ENDS. REPAIRED PER FED EX EA 7-5710-100548.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
WHILE WORKING FOUND CORROSION ON FLOORBEAM LOWER FLANGE BS 720 RBL 30 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER SRM 53-10-8.
Part: STRUCTURE — CORRODED (KRUEGER FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 1 K-FLAP CORRODED AT O/B BONDING JUMPER ATTACH POINT. REPAIRED NR 1 K-FLAP PER FED EX EA 7-5710-100544.
Part: STOP FITTING — GOUGED (SERVICE DOOR) · airframe 39,586 hrs · 25,731 cycles
LEFT AFT SERVICE DOOR FWD LOWER STOP PIN FITTING IS GOUGED. REPAIRED PER FED EX EA 7-5240-100541.
Part: STIFFENER — CHAFED (LT WING) · airframe 39,586 hrs · 25,731 cycles
LEFT WING BRACKET LOOSE AND CHAFING ON NR 8 VERTICAL STIFFENER, INBOARD SIDE OF WS 192.01. REPAIRED VERTICAL STIFFENER IAW FED EA 7-5710-100545.
Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP AT BS 480 STRINGER 7RT. REMOVED AND REPLACED STR AND SPLICE AT BS 480 STR 7RT.
Part: BEAM — CORRODED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
FOUND DELTA BEAM WEB, UPPER SURFACE, ACCESSED THOUGH LIGHTNING HOLE, BS 867, LBL 4 - RBL 4 WL 137 TO BE CORRODED. REPAIRED DAMAGE PER SRM 51-40-2.
Part: SKIN — GOUGED (LT FOREFLAP) · airframe 39,586 hrs · 25,731 cycles
FOUND LT OB FOREFLAP LE IS GOUGED 3 INCHES FROM IB END. ACCOMPLISHED FED EX EA 7-5750-100934.
Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 6 FLAP TRACK IS CORRODED ON SPOILER BEAM MOUNT PAD AREA ON FLAP TRACK ITSELF. REPLACED NR 6 FLAP TRACK, FLAP TRACK WILL BE INSTALLED ON FED-EX CARD 27X5708-03.
Part: NONE — NONE (CARGO DOOR) · airframe 39,586 hrs · 25,731 cycles
EXTERNAL DOUBLER ON RT FUSELAGE AFT CARGO COMPARTMENT DOOR, AFT LOWER CORNER BS 980 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED AFT CARGO DOOR IAW MM 52-35-011-4.
Part: STRINGER — CORRODED (FWD CARGO BAY) · airframe 39,586 hrs · 25,731 cycles
WHILE WORKING FORWARD CARGO COMPARTMENT CLOSE CARD 714515 FUSELAGE 106 71C201-02, FOUND CORROSION EMANATING FROM FASTENERS HOLES AT BS 510 STR 27L. REPAIRED STRINGER PER SRM 53-10-3 FIG 3.
Part: FLOORBEAM — CORRODED (BS 1110) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON FLOORBEAM STA 1110 RBL 24 - LBL 24 WL 208. REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3.
Part: STRINGER — MISREPAIRED (BS 1101 S29L) · airframe 39,586 hrs · 25,731 cycles
REWORK REQUIRED, REJECTED FOR WRONG REPAIR USED AT BS 1101, STR 29L, REF CARD N01221. REPAIRED STRINGER PER SRM 53-10-3 FIG 1.
Part: PANEL — DAMAGED · airframe 39,586 hrs · 25,731 cycles
FOUND SEVERAL DAMAGED CAMLOCK FASTENER HOLES ON PANEL 9115. REPAIRED PANEL 9115 IAW FED-EX EA 7-5510-100550.
Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 39,586 hrs · 25,731 cycles
FOUND DRILL STARTS IN VERTICAL STAB SKIN AT TOP 2 HOLES THROUGH STAB SKIN BEHIND RT FWD LOWER SLIDE SEAL TRACK. REPAIRED STAB SKIN PER SRM 55-30-3 FIG 2.
Part: FLOORBEAM — MISREPAIRED (BS 400) · airframe 39,586 hrs · 25,731 cycles
IMPROPER REPAIR ON FLOORBEAM AT BS 400, RBL 18 WL 208. REPAIRED FLOORBEAM PER SRM 53-10-8.
Part: ATTACH ANGLE — CRACKED (BS 1183) · airframe 39,586 hrs · 25,731 cycles
FOUND DITCHING PAN ATTACH ANGLE CRACKED BS 1183 RBL 48-64 WL 208. REPAIRED PER FED EX EA 7-5310-100552.
Part: BEAM — CRACKED (RT WING SPOILER) · airframe 39,586 hrs · 25,731 cycles
RIGHT WING SPOILER BEAM IS CRACKED AT NR 8 SPOILER ACTUATOR FITTING. REPAIRED RIGHT WING SPOILER BEAM AT NR 8 SPOILER ACTUATOR FITTING PER SR 27-57-038.
Part: CREASE BEAM — DENTED (BS 925) · airframe 39,586 hrs · 25,731 cycles
FOUND CREASE BEAM WEB DENTED ON THE LIGHTENING HOLE, BS 925, LBL 66, WL 208. REPLACED WEB PER SRM 51-40-5, 51-30-2.
Part: PANEL — CORRODED · airframe 39,586 hrs · 25,731 cycles
FOUND RIGHT NR 5 BALANCE BAY PANEL AFT ATTACH POINTS HAVE CORROSION IN VARIOUS AREAS. REPLACED NR 5 RT BALANCE PANEL AFT ATTACH DOUBLER IAW FED EX MM 27-30-021-4.
Part: PIN — CORRODED (LT WING) · airframe 39,586 hrs · 25,731 cycles
FOUND LEFT WING FORWARD TERMINAL PIN IS CORRODED. REPLACED TERMINAL PIN ON FED EX CARD 75C011-00.
Part: FRAME — MAINT ERROR (BS 640 S6R) · airframe 39,586 hrs · 25,731 cycles
FOUND BS 640 FRAME HAS BEEN CHAIN DRILLED AT STRINGER 6 RIGHT. REPAIRED FRAME PER SRM 53-10-4 FIG 1.
Part: FLOORBEAM — CORRODED (BS 680) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON FLOORBEAM AT BS 680, RBL 49, WL 208. REPAIRED FLOORBEAM PER SRM 53-10-8.
Part: STRINGER — CORRODED (BS 1070-1110) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION IN STRINGER CHANNEL STA 1070-1110 STR 29 L. REPAIR TO BE ACCOMPLISHED ON CUSTOMER ID NR N01854.
Part: FRAME — DENTED (BS 1010 S25L) · airframe 39,586 hrs · 25,731 cycles
FOUND DENT ON FRAME INNER FLANGE STA 1010 STR 25L. REMOVED DENTS, FABRICATED REPAIR DOUBLER FROM .070 7075T6 LOT NR 169810. LOCATED AND DRILLED. ALODINED AND PRIMED REPAIR DOUBLER AND INSTALLED IAW SRM 51-40-3.
Part: STRINGER CLIP — CRACKED (BS 540 S24L) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP AT STA 540 LT STR 24 CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: FRAME — CRACKED (BS 540) · airframe 39,586 hrs · 25,731 cycles
FOUND FWD CARGO BAY, UPPER SECTION OF FRAME AT BS 540 LBL 2, CRACKED. REPAIRED FRAME PER SRM 51-40-3.
Part: FRAME — CRACKED (BS 1303 S5L) · airframe 39,586 hrs · 25,731 cycles
FOUND VERTICAL FIN FRAME AT BS 1303, LT UPPER STRUCTURE STRAP CRACKED. REPAIRED FRAME PER SRM 53-30-3.
Part: STRINGER — CRACKED (BS 620) · airframe 39,586 hrs · 25,731 cycles
FOUND FASTENER HOLE IN STRINGER COMMON TO STRINGER CLIP AT BS 620 STR 27L IS CRACKED. REPAIRED STRINGER PER SRM 53-10-3.
Part: STRINGER — DAMAGED (BS 363 S3R) · airframe 39,586 hrs · 25,731 cycles
OPEN HOLES BS 363 IN STRINGER 3 RT. OPEN HOLES AT BS363 STR 3RT WAS FOUND TO BE OUT OF LIMITS REPAIRED STR 3 RT AT BS 363 PER FED EX EA 7-5310-102251 PT 1.
Part: STRINGER CLIP — DAMAGED (BS 950C S7L) · airframe 39,586 hrs · 25,731 cycles
STRINGER CLIP BS 950C STR 7LT HAS 2 EXTRANEOUS HOLES. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: SPAR — CHAFED (VERTICAL STAB) · airframe 39,586 hrs · 25,731 cycles
VERT FIN, LT MID SPAR HAS CHAFING DAMAGE AT FIN STA 225.71. REPAIRED PER FED EX EA 7-5530-100551,
Part: FRAME — DENTED (BS 580) · airframe 39,586 hrs · 25,731 cycles
FOUND DENT IN FRAME AT BS 580 STRINGER 10 RT. REPAIRED FRAME PER SRM 51-40-3 FIG 1.
Part: STRINGER CLIP — DAMAGED (BS 680 S5L) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 5 LEFT. REMOVED AND REPLACED STRINGER CLIP AS PER SRM 51-30-02.
Part: STRINGER CLIP — CRACKED (BS 440 S8L) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP CRACKED BS 440 STRINGER 8 LT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 39,586 hrs · 25,731 cycles
FOUND NR 2 FLAP TRACK MOUNT PAD IS CORRODED. REPLACED NR 2 FLAP TRACK ON 27X5706-03.
Part: FRAME — DENTED (BS 560 S23-25L) · airframe 39,586 hrs · 25,731 cycles
FOUND FRAME AT BS 560 HAS DENT BETWEEN STR 23L-25L. REPAIRED FRAME PER SRM 51-40-3.
Part: SKIN — DAMAGED (BS 480-620) · airframe 39,586 hrs · 25,731 cycles
FOUND OPEN HOLES IN SKIN BETWEEN STRINGER 2 LT AND STRINGER 4 LT BS 480 AND BS 620. INSTALLED FASTENERS IN SKIN PER FED EX EA 7-5330-99515.
Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 39,586 hrs · 25,731 cycles
NR 5 BALANCE BAY PANEL AFT STRAP CORRODED AROUND FASTENER HOLES FOR ENTIRE LENGTH, LT HORIZONTAL STAB. REPAIRED NR 5 BALANCE PANEL PER SRM 51-80 AND DRAWING 65-27917.
Part: FRAME — CRACKED (BS 804) · airframe 39,586 hrs · 25,731 cycles
FOUND CRACK IN FRAME AT BS 804.5, STR 14R. REMOVED CRACKED FRAME AT VS 804.5, FABRICATED ALODINE, PRIMED AND INSTALLED FRAME IAW SRM 51-30-2 AND BOEING DWG NR 65-16327.
Part: FLAP TRACK — CORRODED (NR 8 FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 8 FLAP TRACK IS CORRODED ON FORWARD INBOARD CLEVIS O/B FACE. REPLACED FLAP TRACK ON 27X5710-03.
Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 7 FLAP TRACK HAS CORROSION AT FWD END ON I/B CLEVIS O/B FACE. REPLACED FLAP TRACK ON 27X5709-03.
Part: SHEAR TIE — TOOL DAMAGE (BS 720A) · airframe 39,586 hrs · 25,731 cycles
DRILL START ON LOWER SHEAR TIE AT BS 720A BETWEEN STR 20L, STR 21L. REPAIRED SHEAR TIE PER SRM 53-10-1.
Part: STRINGER — DAMAGED (BS 678) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER 6 LEFT AT BS 678. REMOVED MECHANICAL DAMAGE FOUND TO BE IN LIMITS PER SRM 53-10-1 ALODINED AND PRIMED AREA.
Part: STRINGER — CORRODED (BS 527) · airframe 39,586 hrs · 25,731 cycles
FOUND FWD CARGO BAY, STRINGER L28 CORRODED AT BS 527. REPAIRED STRINGER PER SRM 53-10-3.
Part: STRINGER — DAMAGED (BS 783) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE ON STR 7 LT AT BS 783. REPAIRED STR 7 LT AT BS 783 IAW SRM 53-10-3 FIG 3.
Part: FRAME — DENTED (BS 720) · airframe 39,586 hrs · 25,731 cycles
FOUND FRAME AT BS 720 BETWEEN STR 23L -24L HAS 2 DENTS. REPAIRED FRAME PER SRM 51-40-3.
Part: STRINGER CLIP — DAMAGED (BS 680) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 3 LEFT. REMOVED AND REPLACED STRINGER CLIP BS 680, STRINGER 3 LEFT PER SRM 51-30-2.
Part: WEB — CORRODED (BS 1166) · corrosion level 2 · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON FLOOR WEB STA 1166 RBL 16 WL 208. REMOVED CORROSION 7 BY 3 BY .008 INCHES, FOUND OUT OF LIMITS. REMOVED DAMAGE, FABRICATED, INSTALLED REPAIR PLATE IAW SRM 51-40-2 AND SRM 51-10-1.
Part: STRINGER CLIP — CRACKED (BS 540) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP AT BS 540 LT STR 23 CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: STRINGER CLIP — CRACKED (BS 440) · corrosion level 2 · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP CRACKED BS 440 STRINGER 16 LT. REMOVED AND REPLACED STRINGER CLIP BS 440 STRINGER 16 LEFT.
Part: STRINGER CLIP — DAMAGED (BS 680) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 6 LEFT. REMOVED AND REPLACED DAMAGE STRINGER CLIP BS 680 STRINGER 6 LEFT PER SRM 51-30-2.
Part: FLOORBEAM — CORRODED (BS 440) · airframe 39,586 hrs · 25,731 cycles
ELONGATED HOLE ON FLOORBEAM AT BS 440 LBL 19 WL 208. CUT OUT DAMAGE FLOORBEAM AT BS 440 LBL 11.5 - LBL 20.5 WL 208 AND INSTALLED REPAIR PER SRM 53-10-8.
Part: STRINGER CLIP — DAMAGED (BS 680) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 4 LEFT. REMOVED AND REPLACED STRINGER CLIP BS 680, STRINGER 4 LEFT PER SRM 51-30-2.
Part: STRINGER CLIP — CRACKED (BS 440) · corrosion level 2 · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP CRACKED BS 440 STRINGER 15 LT. REMOVED AND REPLACED STRINGER CLIP BS 440, STRINGER 15 LEFT PER SRM 51-30-2.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 660 STRINGER 5 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: STRUCTURE — CORRODED (BS 336) · airframe 39,586 hrs · 25,731 cycles
FOUND FUSELAGE BS 336 LBL 18 WL 148, LONGITUDINAL CHORD ATTACH CLIP CORRODED. REPLACED ATTACH ANGLE PER SRM 51-30-2.
Part: STRINGER CLIP — DAMAGED (BS 680) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 9 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: FRAME — DENTED (BS 580 S22-24L) · airframe 39,586 hrs · 25,731 cycles
FOUND FRAME AT BS 580 BETWEEN STR 22L-24L HAS DENT. REPAIRED FRAME PER SRM 51-40-3.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
FOUND UPPER RUDDER, RT T/E WEDGE CHAFED APPROX 69" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 69" FROM BOTTOM IAW FED EX EA 7- 5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 7.75 INCHES FROM UPPER T/E. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 7.75" FROM UPPER EDGE IAW FEDEX EA 7-5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 52 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 52" FROM BOTTOM IAW FED EX EA 7- 5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
FOUND UPPER RUDDER, LT T/E WEDGE CHAFED APPROX 12" FROM UPPER T/E. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX. 12" FROM UPPER EDGE IAW FEDEX EA 7-5530-100549.
Part: FRAME — DENTED (BS 720) · airframe 39,586 hrs · 25,731 cycles
FOUND FRAME DENT AT BS 720 LBL 8 WL 156. REPAIRED FRAME BS 720 LBL 8 IAW SRM 51-40-3.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER LEFT T/E WEDGE CHAFED APPROX 28.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX 28.5" FROM BOTTOM IAW FEDEX EA 7-5530-100549.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP AT BS 660, STRINGER 2 RIGHT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 24 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX. 24" FROM BOTTOM IAW FED EX EA 7-5530-100549.
Part: FRAME — DENTED (BS 540 S22-24L) · airframe 39,586 hrs · 25,731 cycles
FOUND FRAME AT BS 540 IS DENTED AND GOUGE BETWEEN STR 22-24LT. REPARIED FRAME PER SRM 51-40-3.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
FOUND UPPER RUDDER, LT T/E WEDGE CHAFED APPROX 24" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE APPROX 24" FROM BOTTOM IAW FED EX EA 7-5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, LEFT T/E WEDGE CHAFED APPROX 2 INCHES FROM BOTTOM EDGE.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 43.75 INCH FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 43.75" FROM BOTTOM IAW FEDEX EA 7-5530-100549.
Part: SHEAR TIE — CORRODED (BS 990 S29-30L) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON FRAME SHEAR TIE STA 990 BETWEEN STR 29L - 30. REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4.
Part: REPAIR — UNKNOWN · airframe 39,586 hrs · 25,731 cycles
FOUND EXTERNAL DOUBLER AT BS 360-380, STR 24R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED NEW REPAIR PER SRM 53-30-3 FIG 3A.
Part: ATTACH FITTING — CORRODED (BS 336) · airframe 39,586 hrs · 25,731 cycles
FOUND FUSELAGE BS 336 RBL 18 WL 148, LONGITUDINAL CHORD AND SUPPORT ANGLE ATTACH CLIP CORRODED. REPLACED ATTACH CLIP PER SRM 51-30-2.
Part: FLOORBEAM — CORRODED (BS 1070) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON FLOORBEAM LWR FLANGE BS 1070 LBL 52 - RBL 52 WL 200. REPAIRED FLOORBEAM PER SRM 53-10-8.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 46.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE APPROX 46.5" FROM BOTTOM IAW FED EX EA 7-5530- 100549.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 660 STRINGER 6 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: STRINGER CLIP — DAMAGED (BS 680) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 2 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER RIGHT T/E WEDGE CHAFED APPROX 28.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX. 28.5 " FROM BOTTOM IAW FED EX EA 7-5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER LEFT T/E WEDGE CHAFED APPROX 24 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE APPROX 24" FROM BOTTOME IAW FED EX EA 7-5530-100549.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP AT BS 660, STRINGER 3 RIGHT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
FOUND UPPER RUDDER, RT T/E WEDGE CHAFED APPROX 12" FROM UPPER T/E EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 12" FROM UPPER EDGE IAW FED EX EA 7-5530-100549.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 660 STRINGER 3 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
FOUND UPPER RUDDER, LT T/E WEDGE CHAFED APPROX 69" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX 69" FROM BOTTOM IAW FED EX EA 7- 5530-100549.
Part: SHEAR TIE — CORRODED (BS 990) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON FRAME SHEAR TIE STA 990 BETWEEN STR 28L - 29L. REPLACED FRAME SHEAR TIE PER SRM 53-10-1, 53-10-4.
Part: SUPPORT ANGLE — CORRODED (BS 336) · airframe 39,586 hrs · 25,731 cycles
FOUND FUSELAGE BS 336 RBL 9 WL 148, LONGITUDINAL CHORD SUPPORT L ANGLE CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-30-2.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 660 STRINGER 7 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, RT TIE WEDGE CHAFED APPROX 2 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RH T.E. WEDGE CHAFF APPROX 2" FROM BOTTOM EDGE IAW FED EX EA 7-5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
UPPER RUDDER, LEFT T/E WEDGE CHAFED APPROX 7.75 INCHES FROM UPPER T/E EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFED APPROX. 7.75" FROM UPPER EDGE UAW FED EX EA 7-5530-100549.
Part: WEDGE — CHAFED (RUDDER) · airframe 39,586 hrs · 25,731 cycles
FOUND UPPER RUDDER, RT T/E WEDGE CHAFED APPROX 39" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE APPROX. 39" FROM BOTTOM IAW FED EX EA 7-5530-100549.
Part: FRAME — DAMAGED (BS 990 S26R) · airframe 39,586 hrs · 25,731 cycles
FOUND AFT CARGO BAY DOUBLE HOLE IN FRAME WEB STA 990 2" ABOVE STR 26R. REPAIRED DOUBLE HOLE IN FRAME IAW FED EX EA 7-5310-100553.
Part: STRINGER CLIP — DAMAGED (BS 660) · airframe 39,586 hrs · 25,731 cycles
FOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 660 STRINGER 4 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: FRAME — DENTED (BS 680 S24-25L) · airframe 39,586 hrs · 25,731 cycles
FRAME AT BS 680 BETWEEN STR 24L - 25L HAS DENT. *S/D* REPAIRED FRAME PER SRM 51-40-3.
Part: STRINGER CLIP — DAMAGED (BS 1010 S7L) · airframe 39,586 hrs · 25,731 cycles
STRINGER CLIP BS 1010 STR 7 LT HAS 2 EXTRANEOUS HOLES AND DAMAGE. *S/D* REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: SKIN — CORRODED (BS 676 S27R) · corrosion level 2 · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION EMANATING FROM UNDER STRINGER R027 AT BS 676, ALSO FASTENER HEAD IS DISHED. REMOVED AND REPLACED STR 27R BS 673-680 PER SRM 53-10-3.
Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 39,586 hrs · 25,731 cycles
NR 7 FLAP TRACK FORWARD SUPPORT FITTING HAS CORROSION PITTING ON INBOARD FACE. REMOVED FITTING, REPAIRED IAW FED EX DWG SR27-57-020 REV A AND SOPM 20-10-03 AND REINSTALLED FITTING IAW OHM 20-50-01.
Part: STRINGER CLIP — DAMAGED (BS 680 S7L) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 7 LEFT. *S/D* REMOVED DAMAGED STR CLIP, AND INSTALLED NEW CLIP IAW SRM 53-10-1 AND SRM 51-30-2.
Part: FLOORBEAM — CORRODED (BS 1130) · airframe 39,586 hrs · 25,731 cycles
FOUND CORROSION ON LWR FLANGE OF FLOORBEAM BS 1130 BETWEEN RBL 6 - 53 WL 200. REPAIRED LOWER CHORD OF FLOOR BEAM IAW FED EX EA 7-5310-102253.
Part: STRINGER CLIP — CRACKED (BS 600 S23L) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP AT BS 600 LT STR 23 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-5 .
Part: STRINGER CLIP — DAMAGED (BS 680 S8L) · airframe 39,586 hrs · 25,731 cycles
MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 8 LEFT. *S/D* FOUND STRINGER CLIP OUT OF LIMITS. REMOVED AND INSTALLED NEW STR CLIP IAW SRM 53-10-1 AND SRM 51-30-2.
Part: STRINGER — CRACKED (BS 600 S24L) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP AT BS 600 LT STR 24 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-5.
Part: STRINGER CLIP — CRACKED (BS 600 S23L) · airframe 39,586 hrs · 25,731 cycles
STRINGER CLIP AT BS 600 LT STR 23 CRACKED. *S/D* REPLACED STR CLIP PER SRM 53-10-1, 51-30-5.
Part: STRINGER CLIP — CRACKED (BS 560 S23L) · airframe 39,586 hrs · 25,731 cycles
STRINGER CLIP AT BS 560 LT STR 23 CRACKED. REMOVED CRACKED STR CLIP AT BS 560 LT STR 23 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. OBTAINED NEW CLIP LOCATED AND DRILLED PER SRM 51-30-5 AND INSTALLED PER SRM 51-30-2.
Part: STRINGER CLIP — CRACKED (BS 540 S23L) · airframe 39,586 hrs · 25,731 cycles
STRINGER CLIP AT BS 540 LT STR 23 CRACKED. *S/D* REMOVED CRACKED STR CLIP. INSTALLED NEW CLIP IAW SRM 53-10-1, 51-30-5 AND SRM 51-30-2.
Part: SKIN — OUT OF LIMITS (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N01803 WHILE WORKING N01403. BLENDED EXTERNAL SKIN AT BS950E PLUS 13 TO BS9503 PLUS 17 BTWN STR27-26 LT REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 1.
Part: SKIN — OUT OF LIMITS (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N01804 WHILE WORKING N01403. BLENDED EXTERNAL SKIN BTWN BS979 TO BS983 BELOW AND AT STR 25LT. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 3.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N00610 STRINGER CLIP AT BS 580 LT STR. 24 CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N00602 STRINGER CLIP AT BS 580 LT STR. 22 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-2.
Part: SKIN — OUT OF LIMITS (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N01802 WHILE WORKING N01403, BLENDED EXTERNAL SKIN AT BS 950D PLUS 15 STR26LH REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 14.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N00605 STRINGER CLIP AT BS 580 LT STR. 23 CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
EXTERIOR FUSELAGE BS 1148 BETWEEN STR 5R AND 6R, SKIN IS DENTED. FOUND DENT TO BE BEYOND LIMITS. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED REF SRM 53-30-3.
Part: STRINGER — CORRODED (BS 1070-1110) · airframe 39,586 hrs · 25,731 cycles
CORROSION IN STRINGER CHANNEL STA 1070 - 1110 STR 29R. INSTALLED REPAIR HAT SPLICE SECTIONS BETWEEN 1080-1120 IAW SRM 53-10-3.
Part: SKIN — CHAFED (BS 950D-990) · airframe 39,586 hrs · 25,731 cycles
FUSELAGE SKIN CHAFED FROM BODY FAIRINGS BS 950D PLUS 10 BS 990 BTWN STR 27L AND 23L. REPAIRED CHAFFED SKIN IAW SRM 53-30-01.
Part: STRINGER CLIP — CRACKED (BS 500 S23L) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP AT BS 500 LT STR 23 CRACKED. REMOVED AND REPLACED STR CLIP BS 500 STR 23L IAW SRM 51-30-02.
Part: STRINGER CLIP — CRACKED (BS 500 S22L) · airframe 39,586 hrs · 25,731 cycles
FOUND STRINGER CLIP AT BS 500 LT STR 22 CRACKED. REMOVED AND REPLACED STR CLIP BS 500 STR 22L IAW SRM 51-30-02.
Part: REPAIR — UNKNOWN · airframe 39,586 hrs · 25,731 cycles
EXTERNAL DOUBLER AT BS 695, STR 28L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPAIRED EXTERNAL DOUBLER AT BS 695 STR 28L IAW SRM 53-30-3 FIG 3A.
Part: SKIN — GOUGED (BS 720D S19L) · airframe 39,586 hrs · 25,731 cycles
FOUND FUSELAGE SKIN GOUGED, BS 720D PLUS 12, STR 19L, MARKED. REPAIRED SKIN PER SRM 53-30-3 FIG 14.
Part: REPAIR — MISREPAIRED (BS 660) · airframe 39,586 hrs · 25,731 cycles
EXTERNAL DOUBLER AT BS 660, STR 30 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXTERNAL DOUBLER AT BS 660, STR 30 WAS FOUND NOT TO BE ACCOMPLISHED IAW APPROVED DATA. REMOVED DOUBLER, REPAIRED IAW SRM 53-30-3, FIG 1. THIS IS A MAJOR REPAIR.
Part: KEELBEAM — CRACKED (BS 872-874) · airframe 39,586 hrs · 25,731 cycles
KEEL BEAM CRACKED, RIGHT SIDE BS 872-B2 874, 2 EA FASTENER HOLES, MARKED, 4 INCHES ABOVE BOTTOM SURFACE OF BEAM. REPAIRED KEEL BEAM UPPER CHORD R/H SIDE AT BS 872-874 IAW FEDEX EA 7-5310-99517.
Part: RIB — GOUGED (VERTICAL FIN) · airframe 39,586 hrs · 25,731 cycles
N00712 WHILE WORKING CARD NO. 73C023-00 (TAIL 43), FOUND VERT. FIN TENSION TIE RIB, LT VERT AFT BOLT HOLE HAS A GOUGE. REPAIRED BOLT HOLE IAW EA 7-5530-100866.
Part: RIB — GOUGED (VERTICAL STAB) · airframe 39,586 hrs · 25,731 cycles
N00638, WHILE WORKING CARD NR 73C023-00 (TAIL 43). FOUND VERT FIN TENSION TIE RIB. RT AFT VERT BOLT HOLE HAS GOUGE. REPAIRED BOLT HOLE PER FED EX EA 7-5530-100866.
Part: FLOORBEAM — CUT (BS 1010) · airframe 39,586 hrs · 25,731 cycles
CUT MARK INTO VERTICAL FLANGE OF FLOORBEAM JUST BELOW UPPER FLANGE BS 1010 RBL 57 WL 207 AFT SIDE. REPAIRED FLOORBEAM PER SR27-53-034 SHEET 5.
Part: FLOORBEAM — CUT (BS 990) · airframe 39,586 hrs · 25,731 cycles
CUT MARK INTO VERTICAL FLANGE OF FLOORBEAM JUST BELOW UPPER FLANGE BS 990 RBL 57 WL 207 AFT SIDE. REPAIRED FLOOR BEAM PER SR27-53-034 REV F.
2005
Part: SKIN — OUT OF LIMITS (FUSELAGE) · airframe 39,586 hrs · 25,731 cycles
N01804 WHILE WORKING N01403. BLENDED EXTERNAL SKIN BTWN BS979 TO BS983 BELOW AND AT STR 25LT. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 3.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 38,635 hrs · 24,984 cycles
WHILE ACCESSING FOR BARRIER MOD FOUND REPAIR ON FLOORBEAM BL 0 NEEDS REWORK TO ACCOMPLISH INSTALLATION OF EXTENDED SEAT TRACK. REPAIRED PER SRM 53-10-8
2003
Part: SUPPORT BEAM — CORRODED (NLG) · corrosion level 2 · airframe 37,303 hrs · 23,935 cycles
CORROSION AROUND NOSE GEAR SUPPORT BEAM PANEL ATTACHMENT FLANGE CORROSION ON TEE CHORD FLANGE AT NOSE GEAR SUPPORT BEAM PANEL ATTACHMENT FLANGE FOUND TO BE OUT OF LIMITS. REMOVED TEE CHORD AND SENT OUT FOR FABRICATION. INSTALLED NEW TEE CHORD IN PLACE OF CORRODED TEE CHORD PER 727 SRM 51-30-2, 51-30-5, 51-20-4, FED EX M/M 51-20-151-7, SRM 51-10-1, 51-10-2.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,303 hrs · 23,935 cycles
CORROSION FOUND ON AIRCRAFT SKIN, UNDER STRINGER 28 LT AT BS 950E, 950E+9, AND 950F+6. FOUND SKIN TO BE OUT OF LIMITS AT 950E, 950E 9 AND 950F 6. CUT OUT CORRODED SKIN AND REPAIRED PER 727 SRM 53-30-3 FIG 3
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,303 hrs · 23,935 cycles
CORROSION ON STRINGER 28 LT, BS 950E 3, OUTBOARD SIDE OF STRINGER.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,303 hrs · 23,935 cycles
CORROSION (C53-113-01(2) ON EXTERNAL SKIN BS 1054 AT STR 28L. COMING CUT OUT & REMOVED DAMAGED SKIN B/S 1054. FABRICATED & INSTALLED REPAIR IAW SRM 53- 30-3 FIG 3. (STR 28L).
Part: STRINGER — BULGED (FUSELAGE) · airframe 37,303 hrs · 23,935 cycles
BULGE ON EXTERNAL SKIN BS 1050 AT STR 27L. CUT OUT & REMOVED DAMAGED STRINGER BS 1040-1060 STR 27L. FABRICATED & INSTALLED REPAIR IAW SRM 53-10-3 FIG 1.
1999
Part: ENGINE — FAILED (NR 2)
99-88 - OIL PRESSURE ON NR AND ENGINE HI (57 PSI). RUN OIL PRESSURE HI CKLIST AND OIL QUANTITY INCREASE ENG WAS SHUTDOWN ACCORD TO CKLIST. REMOVED AND REPLACED NR 2 ENG PER WC 70T0002 AND PERF ENG RUNS PER WC 70T0301. NO LEAKS. AC OK FOR SERVICE
1996
Part: FLOOR BEAM — CORRODED (BS 380)
CABIN FLOOR BEAM CORRODED ON BOTTOM SIDE STA 380 RBL 23 TO 42. REMOVED CORROSION, INSTALLED REPAIR PER SRM 53-10-8 FIG 3.
Part: FLOOR BEAM — CORRODED (BS 360)
CORROSION REMOVED AT FLOOR BEAM STA 360 LBL 3, AREA NOW BELOW SRM LIMITS FOR THICKNESS. TRANSFERRED FROM NR 0958. CORRODED AREA REMOVED AND FLOOR BEAM REPAIRED PER SRM 53-10-8 FIG 8.
Part: STRINGER — CORROSION (BS 1155)
AFT CARGO STA 1155 STR 30 HEAVY CORROSION ON STRINGER. CUT OUT CORRODED AREA, INSTALLED STRINGER REPAIR PER 53-10-3.