N894AA
Registered owner: REGISTRATION PENDING, MI (owner ≠ operator)
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.
93 reports on file, 1996-01-28 – 2004-02-19.
Part: BRACKET — CRACKED (LT EVEVATOR)
LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.
Part: BRACKET — CRACKED (LT ELEVATOR)
LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.
Part: BRACKET — CRACKED (LT ELEVATOR)
LEFT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLES THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES AND CRACKED AND BENT.
Part: BRACKET — CRACKED (LT ELEVATOR)
LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.
Part: BRACKET — CRACKED (LT ELEVATOR)
LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.
Earlier reports · 1996–2002 · 88 reports
2002
Part: WIRE — SHORTED (ELECTRICAL)
UPON ENTRY INTO COCKPIT FOUND RIGHT DUCT PRESSURE NEEDLE FLUCTUATING W/WPU OFF, NR 2 FUEL HEAT VALVE C/B POPPING, NR 2 ENGINE OIL PRESSURE INDICATOR FLUCTUATING. NR 3 WING ANTI-ICE VALVE C/B POPPING. NR F/F AND NR 2 EPR POPS C/B. SHORTED WIRES FOUND BURNED AT AFT PRESSURE BULKHEAD AREA ABOVE ENTRY DOOR RIGHT SIDE JUST AFT OF PRESSURE BULKHEAD. INITIAL INSPECTION REVEALED WIRE BUNDLE W-082 AT PRESSURE BULKHEAD (AFT) ISOLATION COMPLETELY BURNED ON NUMEROUS WIRES IN SAME BUNDLE. ADJACENT WIE BUNDLES AFFECTED ARE W-342, W-350 W-152, W-558, W-843, W-358. REPLACEMETN TO ALL AFFECTED WIRES IN WORK, AND FULL SYSTEMS OPS CHECKS TO FOLLOW ON ALL AFFECTED SYSTEMS. (M)
Part: WIRE HARNESS — BURNED (INSTRUMENT PANEL)
WHEN APPLYING GROUND POWER TO A/C NOTICED FE PANEL INSTRUMENTS FLUCTUATING AND CIRCUIT BREAKERS POPPING. SHUT DOWN GROUND POWER AND UPON INSPECTION FOUND WIRE BUNDLES AFT OF 1183 PRESSURE BULKHEAD BURNED. BUNDLES AFFECTED WERE W-082, W-342, W-350, W-152, W-558, W-843 AND W-358. REPLACED AFFECTED WIRES AND PERFORMED OPERATIONAL CHECKS ON ALL SYSTEMS. OPS CHECKED OK PER MM. SUSPECT WIRE CHAFFING IN BUNDLE W-082. (M)
2001
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEN FIRST CLASS AND COACH CLASS BROKEN. REPLACED EMERGENCY EXIT LIGHT WIRE BETWEEN FIRST CLASS AND COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
BNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SPAR — CORRODED (HORIZONTAL STAB)
TUL - FOUND CORROSION ON LEFT HORIZONTAL STAB AFT SPAR ON TOP APPROX 15 INBOARD OF ELEVATOR PCU. REPAIRED AREA PER ESO 11697 DATED 3-7-2001. (M)
Part: SPAR — CORRODED (HORIZONTAL STAB)
TUL - FOUND CORROSION ON RIGHT HORIZ STABILIZER AFT SPAR ON TOP APPROX 6 INCHES OUTBOARD OF ELEVATOR PCU. REPAIRED AREA PER ESO 11697, DATED 3-7-01. (M)
Part: SPAR — CORRODED (HORIZONTAL STAB)
TUL - FOUND CORROSION ON RIGHT HORIZ STAB AFT SPAR, ON TOP APPROX 30 INCHES OUTBOARD OF ELEVATOR PCU. REPAIRED AREA PER ESO 11697 DATED 3-7-01. (M)
Part: DOOR FRAME — CRACKED (CARGO BAY)
TUL - FOUND FORWARD CARGO DOOR CRACKED AFT FRAME STATION 620 AT SERVICE LIGHT SWITCH CUTOUT. REPAIRED CRACK IN FRAME WEB STATION 620 FORWARD DOOR CUTOUT PER SRM 51-40-2 FIG 1. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
TUL - FOUND DOUBLER CORRODED STATION 294 RIGHT SIDE OF DOGHOUSE UPPER CHORD. REMOVED AND REPLACED DOUBLER (RADIUS FILLER BLOCK) ON UNDER SIDE OF PREVIOUSLY INSTALLED REPAIR ANGLE 7075-T6 .250 .75 INCH WIDE BY 6 INCHES LONG. RE-INSTALLED EXISTING FASTENERS PER SRM 51-40-4 PAGE 2. (M)
2000
Part: CONTACTOR — LOOSE (LT OVERWING)
DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. TIGHTENED LEFT SIDE OVERWING EMERGENCY EXIT BULB CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — DAMAGED (NR 1 ENGINE)
SJU - FLT 1014 - EN ROUTE SJU-MIA, NR 1 ENGINE FUEL CROSS FEED VALVE STUCK IN THE CLOSED POSITION. RETURNED SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SIDE ENGINE CROSS FEED VALVE. REPAIRED WIRES AT NR 1 SIDE ENGINE CROSS FEED VALVE CANNON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (F/C GALLEY)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - FOUND DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REPLACED LEFT OVERWING EMERGENCY EXIT SLIDE LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: FLASHLIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD VAULT DOOR EMERGENCY EXIT GRAB AND GO LIGHT INOPERATIVE. REPLACED OVERHEAD VAULT DOOR EMERGENCY EXIT GRAB AND GO LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: STRINGER — CORRODED (BS 715-720)
TUL - FOUND CORROSION ON STRINGER 28L BOTTOM SIDE STATION 715-720. CUT OUT DAMAGE AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M)
Part: SKIN — CORRODED (BS 700-720)
TUL - FOUND CORROSION ON SKIN UNDER INTERCOSTAL STATION 700-720, STRINGER 28L. CUT OUT DAMAGE AND INSTALLED DOUBLER PER 51-10-6. (M)
Part: SHEAR TIE — CORRODED (BS 700)
TUL - FOUND SHEAR TIE CORRODED LOWER END STATION 700, STRINGER 26L. REMOVED AND REPLACED SHEAR TIE PER 51-10-1. (M0
1999
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BY AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRINGER — CRACKED (BS 1243)
TUL - FOUND CRACK IN STRINGER 11R AROUND FASTENER JUST AFT OF FS 124. REPAIRED PER ESO 11597 DATED 4/19/99. (M)
Part: STRINGER — CRACKED (BS 1243)
TUL - FOUND CRACKS IN STRINGER 15R AND 17R AT STATION 1243, BOTH CRACKS IN RADIUS, BOTH CRACKS APPROX .75 INCH LONG. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 2. (M)
Part: SPLICE — CORRODED (BS 615-619)
TUL - FRAME SPLICE STRIP HEAVILY CORRODED ON UNDERSIDE OF CARGO DOOR FRAME UPPER CHORD AT STATION 615 TO 619 STRINGER 26R, AFT LOWER CORNER OF DOOR OPENING. INSTALLED NEW FRAME SPLICE STRIP ON UNDERSIDE OF CARGO DOOR FRAME 615 TO 619 STRINGER 26R. (M)
Part: FRAME — DENTED (BS 1070)
TUL - STATION 1070 FRAME DENTED ON TOP BETWEEN STRINGER 26R AND 27R. INSTALLED DOUBLER WET AT STATION 1070 BETWEEN STRINGER 26R AND 27R PER SRM 53-10-4. (M)
Part: FLOOR — CORRODED (BS 1166-1162)
TUL - FOUND CORROSION ON LEFT AFT LAV FLOOR STATION 1166-1162 LBL 24-29. REPLACED LEFT LAV FLOOR PAN PER SRM 51-10-1 AND ESO 11697, DATED 1-14-99. (M)
Part: KEEL BEAM — CRACKED (BS 870)
TUL - KEEL BEAM CRACKED AT LOWER CHORD, RIGHT SIDE, SECOND FASTENER AFT OF STATION 870. REMOVED DAMAGED (CRACK) PER ESO 11697 DATED 1/13/99. REPAIRED PER SERVICE BULLETIN 727-53-0208, DETAIL II. (M)
Part: ANGLE — CORRODED (CARGO DOORWAY)
TUL - FOUND CORROSION ON TOP ANGLE AFT CARGO DOR CUTOUT AFT FRAME BETWEEN STRINGER 26R AND 27R. PERFORMED REPAIR OF AIRCRAFT CARGO DOORWAY AFT FRAME UPPER FLANGE IAW ESO 11697, DATED 1/18/99. (M)
Part: SKIN — CORRODED (WS 830)
TUL - FOUND WING LOWER SKIN CORRODED ON LOWER SURFACE STATION 830 LBL 30 INCH TO LBL 32 INCH. REPAIRED CORRODED AREA PER 57-30-3 PAGE 27 FIG 10. (SHEET 3). (M)
Part: FRAME — CRACKED (BS 930)
TUL - FOUND STATION 930 LEFT BELL FRAME CRACKED AT STRINGER 14 LEFT. REPAIRED BELL FRAME AT STATION 930 LEFT, STRINGER 14L PER SRM 53-10-4 FIG 1 USING 1 CHANNEL 5530762 - .080 7075T6 AND 1 DOUBLER 5831870 - .071-7055 PLUS 6 - .25 INCH 1ST OVER HI-LOCKS IN PREVIOUS HOLES AND .375 1ST OVERSIZE INNEW HOLES. (M)
Part: STIFFENER — CORRODED (BS 950)
TUL - FOUND STATION 950 CORROSION AT 2ND VERTICAL STIFFENER FROM KEEL BEAM TOP END. INSTALLED DOUBLER WET PER SRM 53-10-9. (M)
Part: SKIN — CORRODED (WS 830-831)
TUL - FOUND WING LOWER SKIN CORRODED ON LOWER SURFACE. INSTALLED DOUBLER/TRIPLER OVER THE AREA WHERE CORROSION REMOVAL WAS BEYOND LIMITS PER SRM 57-30-3 AND SEALED PER 51-20-4. (M)
Part: CHORD — CORRODED (BS 1183)
TUL - FOUND STATION 1183 LOWER CHORD CORRODED INBOARD STRINGER 27L BULKHEAD FITTING. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 1-13-99. (M)
Part: STIFFENER — CORRODED (BS 1183)
TUL - FOUND LOWER END OF VERTICAL STIFFENER CORRODED STATION 1183, INBOARD STRINGER 27L. REMOVED CORROSION, INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 1-13-99. (M)
Part: FRAME — DENTED (BS 1090)
TUL - FOUND TOP OF BELL FRAME DENTED STATION 1090 STRINGER 27 LEFT. INSTALLED DOUBLER PER SRM 53-10-4. (M)
Part: STRINGER — CORRODED (BS 1015)
TUL - FOUND CORROSION ON OUTBOARD LEG OF STRINGER 29R AROUND 5 EACH FASTENERS STATION 1000-1015. REMOVED CORROSION INSTALLED STRAP REPAIR PER ESO 11697, DATED 1-19-99. (M)
Part: STIFFENER — WORN (BS 870)
TUL - FOUND STATION 870 VERTICAL STIFFENER, NEXT TO APU LOAD CONTROL VALUE HAS DEEP WEAR MARKS. INSTALLED DOUBLER (.050 STAINLESS) PER SRM 51-40-4. (M)
Part: STRINGER — CRACKED (BS 1090)
TUL - FOUND STRINGER 1 STATION 1090, CRACKED AROUND FASTENER HOLE ON RIGHT SIDE FORWARD HOLE AT STRINGER CLIP. CUTOUT DAMAGE STRINGER FROM STATION 1082 TO STATION 1096. HAD NEW PIECE FABRICATED FROM 7075-T6 .040 THICK. INSTALLED STRINGER AND CHANNEL STRAP (TAPERED FROM .125) TO SKIN WITH 23 EACH STANDARD .375 INCH HI-LOCKS. INSTALLED 4 .080 STRAPS TO OUTBOARD ENDS OF STRINGER CHANNEL SPLICE WITH 40 EACH .15625 INCH HI-LOCKS. INSTALLED 4 EACH .080 STRAPS TO THE LOWER FLANGE OF STRINGER AT SPLICED WITH 40 EACH .15625 INCH HI-LOCKS. REPAIR IS PER SRM 53-10-3 FIG 3. (M)
Part: SUPPORT — CORRODED (BS 1213)
TUL - FOUND CORROSION ON UPPER TAIL SKID ACTUATOR SUPPORT BEAM STATION 1213, RBL 6 TO LBL 6. INSTALLED NEW SUPPORT BEAM. (M)
Part: FLOORBEAM — CORRODED (BS 1130)
TUL - FOUND CORROSION ON FLOORBEAM STATION 1130 RBL 27 INCH. INSTALLED REPAIR PER ESO 11697, DATED 1-5-99. (M)
Part: SUPPORT — CORRODED (BS 1213)
TUL - FOUND CORROSION ON LOWER TAIL SKID ACTUATOR SUPPORT BEAM STATION 1213 LBL 6 FORWARD SIDE. INSTALLED NEW SUPPORT BEAM. (M)
Part: FRAME — DENTED (BS 1030)
TUL - FOUND STATION 1030 FRAME DENTED AT STRINGER 25L. CUT OUT DAMAGED AREA OF FRAME. INSTALLED DOUBLER REPAIR PER SRM 53-10-4. (M)
Part: CLIP — CRACKED (BS 1090)
TUL - FOUND STRINGER 1 TO BELT FRAME CLIP IMPROPERLY INSTALLED AND CRACKED STATION 1090. REMOVED AND REPLACED WITH SERVICEABLE (NEW) CLIP PER SRM. (M)
Part: FRAME — CRACKED (CARGO DOORWAY)
TUL - UPPER DOOR FRAME TORQUE BOX LOWER WEB AND ANGLE CRACKED, THREE PLACES, STATION 570-580 BELOW STRINGER 17R. REMOVED AND REPLACED CRACKED SUPPORT ANGLE AND CUT OUT 2.75 INCH BY .75 INCH DAMAGED WEB. INSTALLED DOUBLER REPAIR PER SRM 51-40-2 PAGE 1-6 .040 7075-T6 DOUBLER .032 7075-T6 FILLER, 20 FP6 HI-LOCK . (M)
Part: SHEAR TIE — CORRODED (BS 1166)
TUL - FOUND STATION 1166 BELL FRAME SHEAR TIE CORRODED, AFT SIDE BETWEEN STRINGER 28L AND 29L. REPLACED SHEAR TIE PER SRM 51-10-01, TREATED AND PRIMED PER MM 51-20-0. (M)
Part: SHEAR TIE — CORRODED (BS 1166)
TUL - AT STATION 1166 BELL FRAME SHEAR TIE CORRODED, AFT SIDE, BETWEEN STRINGER 29L AND 30L. REPLACED SHEAR TIE PER SRM 51-10-01, TREATED, PRIMED AND PAINTED PER MM 51-20-0. (M)
Part: FRAME — CRACKED (BS 930)
TUL - FOUND CRACK IN FRAME INBOARD TO OUTBOARD RADIUS. FRAME WAS CUT ABOVE STRINGER 13 RT NEW FRAME SPLICED IAW SRM 53-10-4 FIG 1. (M)
Part: STIFFENER — CORRODED (BS 303.9)
TUL - FOUND HORIZONTAL STIFFENER CORRODED RIGHT STATION 303.9 OUTBOARD OF RIGHT GEAR TRUNNION FITTING. INSTALLED NEW HORIZONTAL STIFFENER RIGHT SIDE STATION 303.9. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND STRINGER 15L CRACKED JUST FORWARD OF LEFT WING ICE LIGHTS. REMOVED DAMAGE SECTION OF STRINGER COMPLETED STRINGER REPAIR PER SRM 53-10-3 FIG 1 DETAIL II. (M)
Part: WEB — CORRODED (BS 1213)
TUL - FOUND CORROSION ON WEB STATION 1213 LBL 4, AT TAIL SKID ACTUATOR MOUNTS. REMOVED AND REPLACED CORRODED WEB (7075-T6 .125) PER SRM 51-10-1 PAG 4. (M)
Part: STIFFENER — CORRODED (BS 307)
TUL - FOUND HORIZONTAL STIFFENER CORRODED RIGHT STATION 307 JUST OUTBOARD OF RIGHT NOSE GEAR TRUNNION FITTING AT FORWARD END. INSTALLED NEW HORIZONTAL STIFFENER RIGHT SIDE STATION 307. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - 15R STRINGER END CRACKED JUST FORWARD OF RIGHT WING ICE LIGHT. REMOVED DAMAGED SECTION OF STRINGER, COMPLETED REPAIR OF STRINGER PER SRM 53-10-3 FIG 1 DETAIL II. (M)
Part: STRINGER — CRACKED (BS 280)
TUL - 5TH STRINGER UP FROM LINE RIGHT SIDE, STATION 280 CENTER OF STRINGER CHANNEL HAS VISUAL INDICATION OF CRACK AT TOOLING MARK. DYE CHECKED, NO CRACK FOUND. BLENDED TOOLING MARK PER SRM 51-10-1, INSTALLED DOUBLER IN STRINGER PER SRM 53-10-3. (M)
Part: SHEAR TIE — CORRODED (BS 990)
TUL - FOUND CORROSION ON SHEAR TIE AT STATION 990 INBOARD OF STRINGER 29R 1 INCH - 2 INCH FORWARD SIDE. CUT OFF DAMAGED SECTION AND SPLICED IN NEW SHEAR TIE PER SRM 53-10-04 FIG 13. (M)
Part: STRAP — CORRODED (BS 1004-995)
TUL - FOUND CORROSION ON STRINGER 29L REPAIR STRAP OUTBOARD LEG STATION 1004-995. FABRICATED AND INSTALLED NEW REPAIR STRAP ON STRINGER 29L. (M)
Part: SKIN — CORRODED (WS 830)
TUL - WING LOWER SKIN CORRODED ON LOWER SURFACE STATION 830 LBL 30 INCHES TO LBL 32 INCHES. REPAIRED CORRODED AREA PER 57-30-3 PAGE 27 FIG 10 (SHEET 3). (M)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND CORROSION ON FUSE AT LEFT OVERWING ICE LIGHT INSIDE. REMOVED CORROSION AROUND LEFT ICE LIGHT CUTOUT, STRINGER 15L BS 720B AND C, DIGITAL THICKNESS HIGH.168, .132. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 137-140. (M)
Part: STRINGER — BENT (BS 388)
TUL - FOUND UPPER LEG OF STRINGER 24R AT STATION 388 BENT. REFORMED SMALL DENT AND INSTALLED DOUBLER PER SRM 53-10-3 FIG 2. (M)
Part: FRAME — DENTED (BS 1030)
TUL - FOUND LOWER LOBE BELL FRAME DENTED ON TOP FLANGE OF FRAME, STATION 1030 BETWEEN STRINGER 26R AND 25R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER 53-10-4 PAGE 1-4. (M)
Part: FRAME — DENTED (BS 560)
TUL - FOUND DENT AT BELL FRAME STATION 560 BETWEEN 24L AND 25L. INSTALLED DOUBLER 8 INCHES LONG, 7075-T6 .050 WITH 3 ROWS OF FASTENERS, 1 ROW ON TOP, 2 ROWS ON SIDE, 39 .1875 D RIVETS, 4.25 INCH D RIVETS. (M)
Part: FRAME — DENTED (BS 660)
TUL - FOUND DENTS AT BELL FRAME STATION 660 BETWEEN STRINGER 24R AND 25R. REMOVED DAMAGED AREA 1 INCH BY 2 INCH, INSTALLED 7075-T6 .063 DOUBLER 8 INCHES LONG, RIVETS ARE MS 20470D, 19 EACH .1875 AND 4 EACH .25 , 3 ROWS TOTAL IAW SRM 51-40-3 PAGE 3 FIG 1. (M)
Part: FRAME — DENTED (BS 1010)
TUL - FOUND STATION 1010 FRAME DENTED TWO PLACES ABOVE 26L. INSTALLED DOUBLER 7075 T-6 .050, 14.5 INCHES LONG WITH 2 ROWS FASTENERS ON SIDE, ONE ROW TOP PER SRM 53-10-4. (M)
Part: FRAME — DENTED (BS 680)
TUL - FOUND DENTS IN BELL FRAME AT BS 680 BETWEEN STRINGER 22R AND 23R. REMOVED DAMAGED AREA 1.25 INCH BY 1 INCH AND 1 INCH BY 1 INCH. INSTALLED 7075-T6 .063 DOUBLER 14 INCHES LONG, RIVETS ARE MS20470D, 34 EACH .1875, 3 ROWS TOTAL IAW SRM 51-40-3 PAGE 3 FIG 1. (M)
Part: FRAME — DENTED (BS 620)
TUL - FOUND BELL FRAME 620 DENTED BETWEEN STRINGERS 24L AND 25L, AND DENTED ABOVE STRINGER 25L. CUT OUT AREA 1 INCH BY 5 INCH, INSTALLED DOUBLER 13 INCH LONG 7075T6 AND .063, 39 UNIVERSAL .375 D RIVETS AND 4 UNIVERSAL HEAD .25 D RIVETS INSTALLED. (M)
Part: FRAME — DENTED (BS 990)
TUL - FOUND STATION 990 FRAME DENTED STRINGER 26L TO 25L. INSTALLED DOUBLER AT STATION 990 STRINGER 26L TO 25L WET IAW SRM 53-10-4. (M)
Part: FRAME — CRACKED (BS 600)
TUL - BELL FRAME STATION 600 BETWEEN STRINGER 4R AND 5R CRACKED. REMOVED DAMAGED AREA 1..875 INCH. INSTALLED DOUBLER 15 INCHES LONG .071 7075-T6 INNER 15 INCH .080 7075-T6 OUTER, .050 2024-T3 FILLER 4 ROWS OF FASTENER 51 BACB30FA16. (M)
Part: TRUNNION — CRACKED (WS 736)
TUL - FOUND NR 1 SLAT ACT OUTBOARD TRUNNION MOUNT HAS VISABLE INDICATION OF CRACK AT TOP BOLT. REMOVED DOUBLER PLATE WITH CRACK IN IT AND INSTALLED NEW DOUBLER PER SRM 51-10-1. ALODINED AND PRIMED DOUBLER. (M)
Part: CLIP — CORRODED (BS 566)
TUL - STRINGER CLIP CORRODED INSIDE STRINGER 26L AT STATION 566. REMOVED CORROSION ON STRINGER CLIP PER SRM 51-10-6, BEYOND MANUAL LIMITS. REPLACED STRINGER CLIP AT STATION 26L, STATION 566. (M)
Part: FRAME — CORRODED (BS 376)
TUL - FOUND FORWARD DOOR OPENING FRAME CORRODED AT BOTTOM GOING UNDER FLOORBOARD TO SIDE CREASE ANGLE AT STATION 376. REPAIRED PER SRM 51-40-3, MATERIAL USED 2024-T3 OF .063 THICKNESS FASTENERS USED WERE BACB30FM6, BACB30EN6, NAS6204 BOLTS. (M)
Part: ANGLE — CORRODED (BS 950-990)
TUL - FOUND AFT CARGO DOOR CUTOUT FRAME, LOWER CHORD OF FRAME HAS CORROSION IN SEVERAL PLACES AROUND NUTPLATE. SLIGHTLY SPOT FACED AREAS, TREATED AND PRIMED AREA AND REINSTALLED NUTPLATES PER ESO 11697. (M)
Part: STRINGER — CORRODED (BS 443)
TUL - FOUND CORROSION ON STRINGER 27R STATION 435-445. INSTALLED DOUBLER PER SRM 51-40-3. (M)
Part: FRAME — DENTED (BS 580)
TUL - FOUND DENTS IN BELT FRAME UPPER FLANGE ABOVE STRINGER 23L AND ABOVE STRINGER 24L. INSTALLED DOUBLER ON BELT FRAME STATION 580 STRINGER 22L - 24L. DOUBLER 18 INCH LONG MADE OF 7075T6 .050 USING 3 ROWS, 2 ON THE SIDE AND 1 ON TOP, USED 44 MS20470D .375 RIVETS AND 4MS20470D .25 INCH RIVETS. (M)
Part: FRAME — DENTED (BS 680)
TUL - DENT AT BELL FRAME STATION 680 BETWEEN 24L AND 25L. CUT OUT DAMAGED AREA 10 INCH BY .5 INCH. INSTALLED DOUBLER 7075-T6 .050 15 INCHES LONG INSTALLED THREE ROWS OF RIVETS, 1 ON TOP, 2 ON SIDE, 33 D UNIVERSAL .1875 RIVETS AND 3 D UNIVERSAL .25 RIVETS. (M)
Part: FRAME — DENTED (BS 600)
TUL - FOUND DENT AT BELL FRAME STATION 600 ABOVE STRINGER 24L DENT AT BELL FRAME STATION 600 ABOVE STRINGER 25L. REMOVED DAMAGE AREA 1 INCH AND 1 INCH ABOVE 24L 1 INCH BY 1 INCH ABOVE STRINGER 25L. INSTALLED 20 INCH DOUBLER, 7075-T6 .063 INSTALLED 53 RIVETS .1875 AND FOUR .25 3 ROWS TOTAL PER SRM 51-40-3 PAGE 3 FIG 1. (M)
Part: FRAME — DENTED (BS 600)
TUL - FOUND DENT AT BELL FRAME ABOVE STRINGER 23L. REMOVED DAMAGED AREA ABOVE STRINGER. REMOVED DAMAGED AREA ABOVE STRINGER 23L STATION 600 CUTOUT 1 INCH BY 1 INCH AREA. INSTALLED 8 INCH DOUBLER 7075-T6 .063 INSTALLED 21 RIVETS MS20470D 3 ROWS TOTAL PER SRM 51-40-3 PAGE 3 FIG 1. (M)
Part: FRAME — DENTED (BS 560)
TUL - FOUND DENT AT BELL FRAME STATION 500 BETWEEN STRINGER 22L AND 23L. DENT AT BELL FRAME STATION 500 BETWEEN STRINGER 23L AND 24L. CUTOUT SECTION .75 INCH BY 2 INCH BETWEEN STRINGER 22L AND 23L, .75 INCH BY 1 INCH AND .75 INCH AND .5 INCH STRINGER 23L AND 24L. INSTALLED DOUBLER 14.5 INCH LONG, 7075-T6 .050 INSTALLED 35 .1875 UNIVERSAL HEAD D RIVETS 3 ROWS TOTAL 2 ON SIDE 1 ON TOP PER SRM 51-40-3 PAGE 3 FIG 1. (M)
Part: FRAME — DENTED (BS 1110)
TUL - STATION 1110 FRAME DENTED ON TOP 2 PLACES AT STRINGER 26L. REMOVED DAMAGE. INSTALLED 7075-T6 .071 DOUBLER 13 INCHES LONG PER SRM 51-40-3 FIG 1. REFERRED FROM AARD 53-10-7-3 PAGE 1, 3 ROWS AD RIVETS ON WEB, R ROW .1875 RIVETS TOP FLANGE 10 FASTENERS 21 EACH .1875 TWO ROWS, 11 EACH .25 ON ONE ROW. (M)
1998
Part: STRINGER — CORRODED (BS 560)
TUL - CORROSION INSIDE STR 17R STA 560 - STA 563 INBOARD SIDE. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED STRINGER REPAIR SPLICE IAW SRM 53-10-3 FIG 1. TST: 48,697 HOURS. CYCLES: 24,206. (X)
Part: STRUCTURE — CORRODED (BS 580-600)
TUL - CORROSION ON SKIN STR 28L AND INTERCOSTAL STA 580 - STA 600. REMOVED CORROSION AND INSTALLED SKIN DOUBLER PER SRM 53-30-3 FIG 3 AND SPLICED IN NEW SECTION FO STR 28L PER SRM 53-10-3 FIG 1 AND REPLACED INTERCOSTAL. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
Part: FRAME — DENTED (BS 700)
TUL - FOUND DENT BELL FRAME STATION 700 BETWEEN STRINGER 21R AND STRINGER 22R. REPAIRED PER SRM AARD 53-10-7-3 PAGE 1. (M)
Part: FRAME — DENTED (BS 520)
TUL - FOUND DENTS AT BELL FRAME STATION 520 BETWEEN STRINGER 23L AND 24L. REMOVED A 2 INCH BY 1.63 INCH WIDTH AND 1 SQUARE INCH SECTION OF DAMAGE MATERIAL 13.5 INCH 7075T-6 .063 THICK 'J' DOUBLER USED 30MS20470D-6 RIVETS, 3 FAST PAST DAMAGE 2 ROWS ON SIDE 1 ROW ON TOP. (M)
1997
Part: SKIN — CRACKED (BS 1213)
TUL - FOUND CRACK IN LEFT LOWER TORQUE BOX SKIN STATION 1213. STOPPED DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2, PAGE 1-6. (M)
Part: SPAR CHORD — CORRODED (FSS 385)
TUL - FOUND CORROSION FORWARD SPAR LOWER CHORD FSS 385, BELOW FUEL SHUTOFF. REMOVED CORROSION, REPAIRED LOWER SPAR CHORD PER ESO 11697, DATED 7-19-95. (M)
Part: FLOOR PAN — CORRODED (BS 1155)
TUL - FOUND CORROSION BEYOND LIMITS 6 INCHES INBOARD OF LAV SINK DRAIN TUBE. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2 PAGE 1-6. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 7 TO 28 INOPERATIVE. SECURED CONNECTORS AT ROW 7 AND 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: BATTERY — DIRTY (CABIN)
RDU - DURING OVERNIGHT CHECK, FOUND THE AFT STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — CORRODED (BS 680)
TUL - CORROSION ON SKIN AND SKIN BUTT SPLICE DOUBLER. BLENDED OUT CORROSION PER SRM 51-10-6, AND INSTALLED DOUBLER OVER DAMAGED AREA PER ESO 11697 (AS REVISED 02-21-96) . TST: 43,536 HRS. CYCLES, 21,736. (X)
Part: WEB — CORRODED (BS 950)
TUL - CORROSION ON WEB AT FWD LWR CORNER OF NR 2 CARGO DOOR OPENING, CORRODED AFT OF FWD FITTING. REMOVED (CUT OUT) 6 INCH SECTION OF CORRODED WEB AT BOTTOM FWD CARGO DOOR OPENING AND SPLICED IN NEW SECTION OF WEB PER SRM 51-40-2, PAGE 5 (TYP WEB REPAIR). TST: 43,536 HRS. CYCLES, 21,736. (X)
Part: SKIN — CORRODED (BS 1011)
TUL - STA 1011 - SKIN IS CORRODED BETWEEN STR 29L AND STR 30. REPAIRED WITH DOUBLER PER SRM 53-30-3. TST: 43,536. CYCLES 21,736. (X)
Part: SKIN — CORRODED (BS 1148-1166)
TUL - SKIN CORRODED AND BULGED OUT BOTTOM OF THE AFT LAV PANEL. INSTALLED DOUBLER PER ESO 11697, DATED 2-16-96. TST: 43,536. CYCLES, 21,736. (X)
Part: STRIP — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)