N893AA
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.
87 reports on file, 1995-05-28 – 2001-04-02.
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION 1 INCH BY 20 INCHES ON STRINGER AND SPLICE STRINGER 27R STATION 1010 TO 1014. INSTALLED REPAIR OF .063 17-7PH CRES, ANGLES AS PER ESO 11697 DATED 3-30-01. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND STRINGER 29L CORRODED OUTBOARD SIDE STATION 1006 TO STATION 1010. INSTALLED NEW STRINGER SPLICE AND STRINGER CLIP PER SRM 53-10-3 AND STRINGER 29L OUTBOARD SIDE STATION 1006-1010. (M)
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND HFEC CRACK AT LOWER AFT CORNER OF DOOR CUTOUT FROM FASTENER TOWARD CUTOUT RADIUS, FS 417-419. CRACK INDICATION IN SKIN. REPAIRED PER BOEING S/B 727-53-188 LISTED ON PATTERN CARD NR 5708 PAGE NR 1. (M)
Part: SKIN — CORRODED (WING CENTER BOX)
TUL - FOUND CORROSION ON LOWER SURFACE OF CENTER WING SKIN RBL 30 BETWEEN S4C AND S5C CORROSION WAS REMOVED BY BLENDOUT AND A REPAIR WAS ACCOMPLISHED WITH DEVIATIONS PER ESO 11697 DATED 2/29/00. REMOVED DOUBLER PER ESO 11697 DATED 2/20/00 AND INSTALLED DOUBLER PER SRM 57-30-03 FIG 10. (M)
Part: SOCKET — INOPERATIVE (OVERWING)
DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE OVERWING EMERGENCY LIGHT DIM. RE-SECURED LEFT SIDE OVERWING EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LAMP — INOPERATIVE (OVERWING)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE OVERWING EMERGENCY LIGHT DIM. RE-SECURED RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PUMP — LEAKING (NR 1 ENGINE)
MIA - FLT 9212 - EN ROUTE MIA-ABQ - DETECTED NR 1 ENGINE SHUT DOWN. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1995–2000 · 80 reports
2000
Part: LIGHT STRIP — DEFECTIVE (CABIN)
MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHT UNDER EXIT PLACARD AT SEAT 3E INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DENTED (FUSELAGE)
TUL - FOUND SKIN DENTED STATION 420, BETWEEN STRINGER 17L AND 18L ADL NR 8930035. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3. (M)
Part: STRUCTURE — CRACKED (FUSELAGE)
TUL - FOUND CRACK EMANATING FROM FASTENER IN W/W STATION 870 BELOW LOAD CONTROL VALVE. REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AS PER ESO 11697 DATED 2/23/2000. (M)
1999
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP CLOSE TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: STRINGER — DAMAGED (BS 1243)
TUL - FOUND STRINGER IN LEFT GOUGED AND FASTENER HOLE ELONGATED JUST FORWARD OF BS 1243. REMOVED DAMAGE ON NR 14 STRINGER LEFT PER SRM 53-10-03. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4C-4E FIG 1. (M)
Part: FRAME — DENTED (BS 990)
TUL - FOUND UPPER FLANGE OF BELLFRAME 990 DENTED ABOVE STRINGER 26L. INSTALLED DOUBLER PER AARD 53-10-07-3. (M)
Part: SHEAR TIE — CORRODED (BS 1130)
TUL - FOUND BELT FRAME 1130 SHEAR TIE CORRODED AFT SIDE OF BELT FRAME JUST OUTBOARD OF STRINGER 28R. REMOVED AND REPLACED SHEAR TIE STATION 1130 AFT SIDE OF BELT FRAME JUST OUTBOARD OF STRINGER 28R ACCORDING TO SRM 53-10-2 PAGE 28, SEALED PER SRM 51-20-40. (M)
Part: SHEAR TIE — CORRODED (BS 1166)
TUL - FOUND SHEAR TIE CORRODED AT 1166 BELL FRAME STRINGER 29R AND STRINGER 30. REMOVED CORRODED SHEAR TIE, INSTALLED NEW SHEAR TIE. (M)
Part: FRAME — DENTED (BS 1050)
TUL - TOP SECTION OF BELL FRAME DENTED 4 PLACES FS 1050 STRINGER 25R TO 27R. REMOVED DAMAGE, INSTALLED .063 7075T6 DOUBLER WITH 15 MS20470-D-8 RIVETS, 10MS20470-D-6 RIVETS, 10 BACR15CE-6 RIVETS, 1BACB30FP6 HI-LOCKS, 1BACB30FP6 HI-LOCKS PER SRM 51-40-3. (M)
Part: FRAME — BUCKLED (BS 1110)
TUL - BELL FRAME STATION 1110 BENT, WEB AREA BUCKLED ABOVE STRINGER 26L ITEM 2 TOP OF BELL FRAME STATION 1110 GOUGED FROM TOO LONG FAST. CUT OUT DAMAGE, REPAIRED BELL FRAME PER SRM 51-40-3 DOUBLER 7075-T6 .063 BY 20 INCH LONG 2 ROWS 43 BACB30FP8 HI-LOCKS AND 1 ROW OF 19 BACB30FC6 AND 2BACB306F10 HI-LOCKS. (M)
Part: FRAME — GOUGED (BS 1130)
TUL - TOP OF BELL FRAME GOUGED (FROM TOO LONG OF FAST), BELL FRAME STATION 1130 BELOW RT TIEDOWN FIITTING. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER AARD 3-10-07-3 DOUBLER 7075-T6 .063 THICK BY 9.5 INCH LONG, 16 BACB30FP8 AND 17 BACB30FPL HI-LOCKS, 2 ROWS IN WEB AND 1 ROW ON TOP. (M)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND CORROSION ON SKIN AROUND ICE LIGHT STRINGER 14R-17R STATION 720B-C. INSTALLED DOUBLER AT RIGHT ICE LIGHT CUTOUT PER SRM 53-30-3 PAGE 137-140 FIG 22 AND ECO 11697, DATED 3/3/99. (M)
Part: FRAME — CORRODED (BS 720)
TUL - FOUND CORROSION ON 720E FRAME, FORWARD SIDE, FROM STRINGER 7L TO STRINGER 4L, 7 SPOTS (MARKED). REMOVED CORROSION AND INSTALLED FRAME REPAIRS AT STRINGER 4L, 5L, 6L, PER SRM 53-10-4 FIG 2. (M)
Part: FITTING — MISDRILLED (BS 1176)
TUL - RIGHT CREASE BEAM 1183 END FITTING MIS-DRILLED ZERO EDGE DISTANCE ON FORWARD FASTENER, STATION 1176 STRINGER 17R. REMOVED 7 FASTENERS AND INSTALLED DOUBLER AND FILLERS PER ESO 11697 DATED 2-26-99. (M)
Part: FRAME — CORRODED (CARGO DOORWAY)
TUL - FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER FRAME WEB CORRODED STATION 560, STRINGER 26R. INSTALLED DOUBLER ON WEB PER SRM 51-40-2, DOUBLER 5.5 BY 4.25 INCH, 3 ROWS FASTENERS BACB3OMC8-6 W/BACC30M8 COLLARS MATERIAL 2024T3 .080. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND STRINGER 15R CRACKED AT END OF STRINGER FORWARD OF ICE LIGHT. HFEC TO CONFIRM CRACK, REMOVED CRACKED SECTION OF STRINGER 1.25 INCH. HFEC TO CONFIRM CRACK REMOVAL AND INSTALLED REPAIR, FILLER AND CHANNEL PER 53-10-3 PAGE 12-17. (M)
Part: FRAME — WORN (BS 1090)
TUL - TOP OF BELT FRAME HAS 2 EACH WORN SPOTS ABOVE STRINGER 27L FROM FASTENER PROTRUSION AT CARGO TIEDOWN CASTING, STATION 1090 AND 27L STRINGER. INSTALLED DOUBLER .071 INCH WITH 19 EACH .25 INCH HI-LOCKS PER SRM 51-40-3 PAGE 3 AND 9 .1875 INCH HI-LOCKS. THE DOUBLER IS 8.5 INCH BY 4 INCH, NO CUTOUT OF MATERIAL, JUST WEAR. (M)
Part: FRAME — CRACKED (BS 420)
TUL - FOUND STATION 420 FRAME CRACKED AT STRINGER 10L. REPAIRED DAMAGED FRAME STATION 420 STRINGER 10L WITH DOUBLER AS PER SRM 53-10-4 PAGE 3-6 FIG 1 SHEET 4. INSTALLED DOUBLER ONE GAUGE HEAVIER THAN ORIGINAL AND USED HI-LOCK .15625 DIAMETER. (M)
Part: WEB — CRACKED (BS 1213)
TUL - FOUND CORROSION AND CRACKS ON UPPE RLOWER SIDE ANGLES AND WEB OF TAIL SKID ACT MOUNT RIB STATION 1213 LBL 18 TO RBL 18, LBL 30 TO RBL 30. REMOVED AND INSTALLED NEW ANGLES AND WEB PER SRM 51-10-1. (M)
Part: CASTING — CRACKED (BS 760)
TUL - FOUND CRACK IN RADIUS AND VERTICAL AREA OF LEFT 760 CASTING (BEHIND RIB). REPAIRED LEFT 760 CASTING PER BOEING SERVICE BULLETIN 727-57-0112 REV 5 LARGE REPAIR. (M)
Part: SEAT TRACK — CORRODED (BS 480)
TUL - FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK STATION 480 INBOARD, OUTBOARD LEGS AT FASTENER HOLES. REMOVED CORRODED SECTION OF SEAT TRACK. SPLICED IN NEW SECTION PER SRM 53-10-5 FROM STATION 480-560 RIGHT. (M)
Part: SKIN — CORRODED (BS 708)
TUL - FOUND STATION 708 BETWEEN STRINGER 27L AND 28L FUSELAGE SKIN HAS CORROSION. REPAIRED FUSELAGE SKIN PER SRM 53-30-3. (M)
Part: STRINGER — CORRODED (BS 702)
TUL - FOUND CORROSION DOWN INSIDE STRINGER 27L AROUND DOME NUT, NUT PLATE STATION 702. REPAIRED FUSELAGE STRINGER PER SRM 53-10-3. (M)
Part: STRINGER — CORRODED (BS 708)
TUL - FOUND HEAVY CORROSION ON STRINGER 28L, STATION 708. REPAIRED FUSELAGE STRINGER PER SRM 53-10-3. (M)
Part: STRINGER — CORRODED (BS 1030-1070)
TUL - FOUND STRINGER 28R HAS CORROSION ON BOTTOM SURFACE AT FS 1040 TO 1070. REPAIRED STRINGER ACCORDING TO SRM 53-10-3. (M)
Part: SKIN — CORRODED (BS 708)
TUL - FOUND CORROSION ON EXTERIOR SKIN, STATION 708 STRINGER 28L. REPAIRED FUSELAGE SKIN PER SRM 53-30-3. (M)
Part: STRINGER — CORRODED (BS 1040-1070)
TUL - FOUND STRINGER 28R HAS CORROSION ON BOTTOM SURFACE AT FS 1040 TO 1070. REPAIRED STRINGER ACCORDING TO SRM 53-10-3. (M)
Part: SKIN — CORRODED (BS 1055-1095)
TUL - FOUND SKIN CORRODED ON EXTERIOR OF AIRCRAFT. REPAIRED CORRODED THROUGH PORTION OF SKIN PER SRM 53-30-3. ALODINED AND PRIMED SKIN, PATCH AND SURFACE ON EXTERIOR OF SKIN PER SRM 51-10-2. (M)
Part: STRINGER — CORRODED (BS 1050-1070)
TUL - FOUND STRINGER 28L CORRODED FROM STATIN 1050 TO 1070. CUT OUT DAMAGED STRINGER SECTION, AND INSTALLED STRINGER SPLICE PER SRM 53-10-3, FIGURE 1. (M)
Part: SKIN — CORRODED (BS 1060-1067)
TUL - FOUND SKIN CORRODED ON EXTERIOR OF AIRCRAFT FROM STATION 1060 TO 1067 AT STRINGER 28L. CUTOUT DAMAGED SKIN. REPAIRED WITH DOUBLER PER SRM 53-30-3 FIG 3. (M)
Part: FRAME — DENTED (BS 680)
TUL - STATION 680 BELL FRAME DENTED AT STRINGER 23L. INSTALLED DOUBLER PER SRM 51-40-3 7075T6.063, 3 ROWS OF RIVETS 1 ROW TOP 2 ROWS SIDE 20 .1875 D-RIVETS. (M)
Part: FRAME — DENTED (BS 950)
TUL - FOUND TOP OF BELL FRAME DENTED AT STAITON 950F 5 INCHES ABOVE STRINGER 26L. CUTOUT DAMAGED AREA, DUE CHECKED, FABRICATED DOUBLER, AND INSTALLED PER SRM 53-10-4 PAGE 4 FIG 1. (M)
Part: FRAME — DENTED (BS 600)
TUL - UPPER FLANGE OF BELL FRAME DENTED AT STATION 600 AND STRINGER 24 TO 25L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 7075T6 .063 SEVEN INCHES LONG, 3 ROWS RIVETS 1 TOP, 2 ON SIDE, NINTEEN .1875 INCH D-RIVETS, ONE .25 INCH D-RIVETS. (M)
Part: FRAME — DENTED (BS 680)
TUL - SMALL DENT, UPPER FLANGE OF STATION 680 BELL FRAME, BELOW STRINGER 24L. INSTALLED DOUBLER PER SRM 51-40-3 7075T6.063, 3 ROWS OF RIVETS 2 ROWS SIDE SIXTEEN .1875 D-RIVETS, FOUR .25 INCH D-RIVETS. (M)
Part: FRAME — DENTED (BS 620)
TUL - FOUND UPPER FLANGE OF BELL FRAME IS DENTED AT STATION 620 AT STATION 24L TO 25L. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 7075T6 .063, 16.5 INCH LONG, 3 ROWS RIVETS 1 ON TOP 2 ON SIDE WITH FORTY-EIGHT .1875 INCH D-RIVETS, FOUR .25 INCH D-RIVETS. (M)
Part: UNKNOWN
TUL - FOUND STATION 344 LBL 30 TOP FLANGE OF FLOORBEAM CRACKED AT FASTENER HOLE. CUT OUT DAMAGED SECTION OF TOP FLANGE. INSTALLED DOUBLER REPAIR PER SRM 53-10-8 FIG 9 SHEETS 1-5. (M)
Part: FRAME — DENTED (BS 660)
TUL - FOUND STATION 660 BELT FRAME DENTED AT 24L. INSTALLED DOUBLER (7075T-6, .063, 7.5 INCH LONG) 3 ROWS OF RIVETS (1 ROW TOP, 2 ROWS SIDE) WITH 20 EACH .1875 D-RIVETS PER SRM 51-40-3. (M)
Part: CASTING — CORRODED (WS 385)
TUL - INBOARD AILERON QUAD MOUNT CASTING CORRODED ON CASTING AND AROUND BEARING BORES. REMOVED AND REPLACED CORRODED CASTING PER SRM 51-10-1 PAGE 4. (M)
Part: SKIN — CRACKED (RT WING)
TUL - FOUND CRACK IN LEADING EDGE SKIN OUTBOARD EDGE OF INBOARD ROLLER, CUTOUT AT BOTTOM FLANGE NR 8 SLAT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 57-30-4. (M)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND CORROSION ON SKIN AROUND LEFT ICE LIGHT HOUSING BETWEEN STRINGER 14L AND 16L STATION 720B-720C. REMOVED CORROSION AND BLENDED CORRODED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 137-140 ALODINED AND PRIMED ALL PARTS PER SRM 51-10-2. (M)
Part: FITTING — CORRODED (LT MLG)
TUL - FOUND CORROSION ON FORWARD LEFT MLG TRUNNION FITTING BEARING ATTACHMENT BORES 4 EACH. REAMED HOLES AND INSTALLED OVERSIZE BUSHING PER ESO 11697 (2-22-97) AND SB 727-57-132. (M)
Part: SKIN — CRACKED (BS 1097)
TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HOLE STATION 1097 RIGHT SIDE OF STRINGER 1. INSTALLED REPAIR PER SB NR 727-53-A0204 PARB, P615 (SRM 53-30-3 F 16.3). (M)
Part: SKIN — CRACKED (RT WING)
TUL - FOUND CRACK IN LEADING EDGE SKIN AT INBOARD ROLLER TRACK CUTOUT FOR NR 6 SLAT. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 57-30-4. (M)
Part: FITTING — CORRODED (WS 224)
TUL - FORWARD TRUNNION FITTING BEARING BORES CORRODED. REPLACED RMG FORWARD TRUNNION FITTING PER SRM 51-10-1. (M)
Part: S-DUCT — DAMAGED (NR 2 ENGINE)
TUL - NR 2 ENGINE S-DUCT INNER SKIN BLISTERED AROUND 2 RIVETS APPROX 2 INCH DIAMETER LOCATED 2 SKIN LAPS PLUS RIVET ROWS UP FROM AFT END BETWEEN 6 AND 7 O'CLOCK POSITION. BLENDED CORROSION PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 54-10-3. (M)
Part: BEAM — CORRODED (WS 36-60)
TUL - FOUND CORROSION IN 16 EACH FASTENER HOLE OUTBOARD NR 4 FLAPTRACK IN LEFT MLG GEAR BEAM. REAMED HOLES TO REMOVED CORROSION AND INSTALLED BUSHINGS IN HOLES PER ESO 11697, DATED 2-19-99. (M)
Part: CLIP — CORRODED (BS 660)
TUL - FOUND CORROSION ON STRINGER CLIP TO FRAME AT FS 660 STRINGER 15R. REPLACED STRINGER CLIP. (M)
Part: ANGLE — CORRODED (BS 323-326)
TUL - FOUND CORROSION AT TOP OF NLG DOGHOUSE AT TOP WALL TO SIDE WALL JOINT (CORNER) LEFT SIDE. INSTALLED DOUBLER REPAIR IAW SRM 51-40-3 FIG 1. (M)
Part: ANGLE — CORRODED (BS 334-337)
TUL - FOUND CORROSION AT TOP OF NLG DOGHOUSE AT TOP WALL TO SIDE WALL JOINT CORNER. INSTALLED DOUBLER REPAIR IAW SRM 51-40-3 FIG 1. (M)
Part: STRINGER — CRACKED (BS 660)
TUL - FOUND STRINGER CRACKED AT PREVIOUS RADIUS AREA, FS 660 STRINGER 15R. STOP DRILLED CRACK, HFEC. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)
Part: FRAME — DENTED (BS 680)
TUL - FOUND STATION 680 BELL FRAME DENTED ABOVE STRINGER 24R. INSTALLED DOUBLER (7075 T-6 .063) 3 ROWS OF RIVETS, 1 ROW TOP, 2 ROWS SIDE WITH SEVENTEEN .1875 D-RIVETS AND FOUR .25 INCH RIVETS, DOUBLE 7.5 INCH LONG PER SRM 51-40-3. (M)
Part: FRAME — DENTED (BS 700)
TUL - FOUND STATION 700 BELL FRAME DENTED ABOVE STRINGER 24R. INSTALLED DOUBLER (7075T-6 .063) 3 ROW OF RIVETS, 1 ROW TOP, 2 ROWS SIDE WITH EIGHTTEEN .1875 D-RIVETS, DOUBLER 7.5 INCH LONG PER SRM 51-40-3. (M)
Part: FRAME — DENTED (BS 580)
TUL - STATION 580 BELL FRAME HAS TWO DENTS AT STRINGER 23L TO STRINGER 24L. INSTALLED DOUBLER 7075T6 .063, 3 ROWS OF RIVETS 1 ROW IN TOP, 2 ROWS ON SIDE WITH THIRTY .1875 D-RIVETS AND FOUR EACH HI-LOCKS IN SHEAR TIE, STD .15625 ATTACHING TO STRINGER PER SRM 51-40-3. (M)
Part: FITTING — CORRODED (BS 740)
TUL - FOUND STRINGER 27L OUTBOARD END FITTING HEAVILY CORRODED. INSTALLED NEW END FITTING CPN5624412. (M)
Part: STRINGER — CORRODED (BS 740)
TUL - FOUND CORROSION AFT END STRINGER 27R, STATION 740. PERFORMED STRINGER SPLICE REPAIR PER SRM 53-10-3. (M)
Part: SKIN — GOUGED (BS 9505)
TUL - FOUND STATION 9505 PLUS 16, APPROX 3 INCHES BELOW STRINGER 25L, SKIN HAS DEEP GOUGE. BLENDED GOUGE, ALODINED AND PRIMED AREA, BLEND OUT OF LIMITS. REPAIRED WITH DOUBLER PER SRM 53-30-3 PAGE 5, 6, 7, 8. (M)
Part: FRAME — DENTED (BS 500)
TUL - STATION 500 BELL FRAME HAS 3 DENTS ON UPPER LEG FROM STR 22R TO 25R. CUTOUT DAMAGED AREA, REPAIRED BELT FRAME AT STATION 500, STRINGER 22R TO 25R PER SRM 51-40-3 FIG 1, PAGE 3. 1 DOUBLER 8 INCHES LONG .0637075-T6 20 EACH .1875 MS20470D RIVETS 3 ROWS, 2ND DOUBLER 20 INCHES LONG .063 7075-6, 2 EACH .1875 AND 4 EACH .25 MS20470D RIVETS 3 ROWS. (M)
1998
Part: ANGLE — CORRODED (BS 303)
TUL - FORWARD ENTRY DOOR SILL INBOARD CHORD ANGLE HORIZONTAL AND VERTICAL FLANGES HAVE INTERGRANULAR CORROSION. INSTALLED NEW CHORD ANGLE STA 303 - STA 460. TST: 49,071 HOURS. CYCLES: 24,653. (X)
Part: STIFFENER — CORRODED (WS 230)
TUL - VERTICAL STIFFENER CORRODED RT WING FRONT SPAR STA 230. (ABOVE NR 5 L/E FLAP ACTUATOR.) REMOVED AND REPLACED CORRODED VERTICAL STIFFENER AT STA 230 ABOVE NR 5 L/E FLAP ACTUATOR. PRIMED, PAINTED, AND SEALED IAW SRM 53-10-01. TST: 49,071 HOURS. CYCLES: 24,653. (X)
1997
Part: SKIN — CORRODED (BS 720)
AFW - FOUND CORROSION ON SKIN ABOVE STRINGER 18L. REMOVED CORROSION, TREATED AND PRIMED PER MRB 727-0046. (M)
Part: WEB — CORRODED (BS 760)
AFW - FOUND CORROSION ON WEB AROUND OPENING FOR PANEL 3210R. ADDED DOUBLER PER MRB 727-0047. (M)
Part: PANEL — CORRODED (BS 795)
AFW - PANELS 3346 AND 3218 LEFT LOWER ATTACH LANDING CORRODED. REPLACED LANDING IAW SRM 51-40-4. (M)
Part: ANGLE — CORRODED (BS 772)
AFW - FOUND PANEL 5458 ATTACH ANGLE CORRODED AT BL 0. INSTALLED NEW PANEL LANDING. (M)
Part: ANGLE — CORRODED (BS 740)
AFW - FOUND CORROSION ON PANEL SUPPORT ANGLE AT RBL 3. REMOVED AND REPLACED CORRODED ANGLES. (M)
Part: PANEL — CORRODED (BS 772)
AFW - LOWER FAIRING PANEL 3450 LANDING CORRODED. REMOVED AND REPLACED LANDING AS PER SRM 53-10. (M)
Part: PANEL — CORRODED (BS 846)
AFW - FOUND PANELS 3453 AND 3353 LOWER ATTACH LANDINGS CORRODED. REPLACED LANDING IAW SRM REF 51-40-4. (M)
Part: SKIN — CORRODED (BS 720)
AFW - FRETTING CORROSION ON FUSELAGE FROM STATION 720D PLUS 10 INCHES TO 720E STRINGER 17R TO 19R. REMOVED CORROSION AND INSTALLED DOUBLERS PER SRM 53-30-3. (M)
Part: FRAME — CORRODED (CARGO DOORWAY)
AFW - FOUND CORROSION ON FORWARD FRAME NR 2 DOOR AT HOLD OPER SETTING. REMOVED CORROSION INSTALLED DOUBLER PER SRM 51-40-02, AARD 51-20-01. (M)
Part: PANEL — CORRODED (BS 720)
AFW - FOUND PANEL 3458R CORRODED AT HINGE AREA. REMOVED AND REPLACED PANEL. (M)
Part: ANGLE — CORRODED (BS 760)
AFW - FOUND CORROSION ON PANEL SUPPORT ANGLE AT NUT PLATE. REMOVED AND REPLACED CORRODED ANGLES. (M)
Part: SKIN — CORRODED (BS 500)
TUL - SKIN BULGING BETWEEN STR 26L AND STR 27L, STA 500. REMOVED SECTION OF SKIN, INSTALLED DOUBLER PER SRM 53-30-3 FIG 24, 51-10-1. TST: 46,546 HOURS. CYCLES, 23,428. (X)
Part: FLOOR — CORRODED (BS 1175)
TUL - CORROSION ON FLOOR WEB STA 1175 BL 6L (JUST FORWARD END OF VAULT DOOR THRESHOLD JOINT). REPLACED FLOOR SHEET METAL SECTION IN FRONT OF VAULT DOOR (REPAIRED PER 51-40-2) SRM. TST: 46,546 HOURS. CYCLES, 23,428. (X)
Part: FRAME — CORRODED (BS 580)
TUL - CORROSION ON FRAME BETWEEN STA 26L AND STA 27L AT STA 580. INSTALLED FRAME REPAIR PER SRM 53-10-4 FIG 11. TST: 46,544.32 HOURS. CYCLES, 23,433. (X)
Part: STRINGER — CORRODED (BS 720/730)
TUL - CORROSION ON STR 27L AT STA 720+10. REMOVED CORRODED SECTION OF STR 27L BETWEEN STA 720 - STA 720A AND INSTALLED REPAIR PER SRM 53-10-7. FIG 1. TST: 46,546 HOURS. CYCLES, 23,428. (X)
Part: SHEAR TIE — CORRODED (BS 580)
TUL - CORROSION ON SHEAR TIE BETWEEN STR 26L AND STR 27L AT STA 580. INSTALLED NEW SHEAR TIE PER SRM 51-30-2. TST: 46,544.32. CYCLES: 23,433. (X)
Part: SKIN — CORRODED (BS 520)
TUL - SKIN BULGING BETWEEN STR 26L AND STR 25L STA 520. REMOVED AND INSTALLED SECTION OF SHEAR TIE. TST: 46,546 HOURS. CYCLES, 23.428. (X)
1996
Part: STRINGER — CORRODED (BS 560)
CORROSION ON DOUBLER AND STRINGER, STA 560, STR 28R. CUT OUT DAMAGED SECTION OF STR 28R, UNDER STA 560 FRAME. INSTALLED STRINGER SPLICE REPAIR AT STA 550 AND STA 570 (SRM 53-10-3). TST: 44,049 HRS. CYCLES: 22,196. (X)
Part: SKIN — CORRODED (BS 560)
TUL - SKIN CORRODED BELOW STR 28R, STA 560 TO STA 565. INSTALLED FILLER AND DOUBLER PER SRM 53-30-3. TST: 44,049. CYCLES: 22,196. (X)
Part: SKIN — CORRODED (FUSELAGE)
TUL - SKIN CORROSION ON BOTTOM OF STR 27R. COMPLETED REPAIR DOUBLER PER ESO 11697. TST: 44,049 HRS. CYCLES: 22,196. (X)
1995
Part: EEL WIRE — NEED REPAIR (CABIN)
DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD SECTION OF MAIN CABIN DIM. REPAIRED EMERGENCY EXIT FLOOR PATH WIRING AT FORWARD SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)