N875AA

Part: STRINGER — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON STRINGER TIE STATION 1133 ON INBOARD SIDE OF STRINGER 27L. CUT OUT CORRODED SECTION OF STRINGER STATION 1116 TO 1134. INSTALLED NEW STRINGER SECTION AND REPAIR SPLICE PER SRM 53-10-3. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SHEAR TIE STATION 700 BETWEEN STRINGER 28R AND 29R. TRIMMED OFF DAMAGED SECTION OF SHEAR TIE AND INSTALLED REPAIR AT SKIN ATTACHMENT AS PER SRM 53-10-4 FIG 15 SHEET 3. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SHEAR TIE STATION 680 BETWEEN STRINGER 28R AND STR 29R. REMOVED CORRODED SHEAR TIE FLANGE AND INSTALLED REPAIR ANGLE PER SRM 53-10-4 FIG 14. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 27 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UPPER CHORD ANGLE AT STATION 1213. REMOVED CORROSION AND INSTALLED .032 17-7PH ANGLE REPAIR WITH .25 INCH HI-LOCK PER ESO 11697 DATED 1/4/01. (M)

Part: FITTING — CRACKED (NR 6 FLAP)

TUL - FOUND NR 6 FLAP TRACK FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING PER 51-10-01. (M)

Part: SKIN — CORRODED (WING)

TUL - FOUND BOTTOM CENTER WING SKIN HAS CORROSION AROUND HI-LOCK IN PLEUM CHAMBER ABOVE RIGHT PRIMARY HEAT EXCHANGER STRINGER 5 RBL 27. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DATED 1108101. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND BULGE IN FUSELAGE SKIN STATION 1013 BETWEEN STRINGER 9R/10R, CORROSION ON SKIN. REPAIRED PER SRM 53-30-3, PART 1 FIG 1 SHEET 4, INSTALLED DOUBLER. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FS 303 FRAME CRACKED .625 INCH AT STRINGER 16L CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SB 727-53-153 R5. (M)

Part: BEAM — CORRODED (HORIZONTAL STAB)

TUL - FOUND CORROSION ON TIE OF LEFT HORIZ STABILIZER OUTBOARD END 6 INCHES INBOARD OF OUTBOARD END, T/E BEAM. REMOVED CORROSION, TREATED AND PRIMED AND INSTALLED DOUBLER OF T3 2024.063 PER SRM 55-10-6. (M)

Part: BEAM — CORRODED (HORIZONTAL STAB)

TUL - FOUND CORROSION ON UPPER LEFT HORIZONTAL TIE (BEAM) 8 INCHES FROM INBOARD END. REMOVED CORROSION, TREATED AND PRIMED AND INSTALLED DOUBLER PER SRM 55-10-6. (M)

Part: TORQUE BOX — CRACKED (FUSLEAGE)

TUL - FOUND LEFT LOWER TORQUE BOX VERTICAL WEB CRACKED AT LIGHTENING HOLE STATION 1283. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 51-40-2. (M)

Part: SPLICE — FAULTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CABIN FLOOR PATH EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH SPLICES AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (VENTRAL STAIR)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD VENTRAL STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD VENTRAL STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PCU — DEFECTIVE (ELEVATOR)

MIA - FLT 331 - ON CLIMB-OUT MIA AT 6500 FEET WITH CLIMB POWER SET, AND 250 KNOTS AIRCRAFT YAWED RIGHT AND DID NOT RESPOND TO YOKE IMPUTS. AS WINGS WERE LEVELED AIRCRAFT PORPOISED VIOLENTLY FOR APPROX 5 SECONDS. DECLARED EMERGENCY AND RETURNED MIA WITHOUT INCIDENT. REPLACED UPPER AND LOWER YAW DAMP COUPLER. REPLACED RIGHT SIDE ELEVATOR POWER CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)

MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT AFT STAIRS INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (COCKPIT)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ASSEMBLY IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AT AFT GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - EMERGENCY EXIT LIGHT INOPERATIVE OVERAFT END OF AFT AIRSTAIRS. REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M)

Part: ANGLE — CRACKED (WS 760)

TUL - RIGHT 760 CHORD ANGLE HFEC INDICATES CRACK BELOW RPR DOUBLER. INSTALLED REPAIR DOUBLER AT STATION 760 RIB CHORD ANGLE IAW SERVICE BULLETIN 727-57-0112, REV 5 AFTER CRACK STOP DRILLED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - AFT CARGO DOOR EMERGENCY EXIT LIGHT ASSEMBLY HAD WIRE THAT WAS INTERMITTENT RT AFT EXT EMERGENCY LT ON AFT CARGO DOOR HAS 1 LAMP OUT. REPLACED LIGHT ASSEMBLY CPN LIE 5844 MPN 30-0593-1 OPS CHECKED OK, (E583093460. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (LT MLG)

PHL - FLT 1845 - AFTER TAKEOFF PHL/MIA - ALL 3 RED GEAR WARNING LIGHTS AND TAIL SKID LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO LGA. REPLACED LANDING GEAR HANDLE DOWN SWITCH. ALSO, REPLACED LEFT MAIN LANDING GEAR DOWNLOCK PROXIMITY SENSOR. ACCOMPLISHED GEAR RETRACTION CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: UNIT — DEFECTIVE (E/E COMP)

PHL - FLT 0880 - AFTER TAKEOFF MIA/PHL - GEAR AND TAIL SKID UNSAFE LIGHTS REMAINED ILLUMINATED WHEN GEAR HANDLE WAS IN UP AND OFF POSITION. GEAR OPERATION WAS NORMAL. AIRCRAFT LANDED PHL WITHOUT INCIDENT. REPLACED LANDING GEAR ACTUATION UNIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP FORWARD OF FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP FORWARD OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (AFT AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (NR 1 ENGINE)

MIA - FLT 808 - EN ROUTE POP, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. CREW FOLLOWED CHECKLIST AND SHUTDOWN NR 1 ENGINE. ENGINE WINDMILL TIME WAS 1 HOUR AND 15 MINUTES. FLIGHT CONTINUED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED SCREENS AND CHIP DETECTOR. NO DEBRIS NOTED. REPLACED OIL FILTER ELEMENT AND OIL BYPASS SWITCH. GROUND RAN ENGINE WITH ALL INDICATIONS NORMAL. LEAK CHECK WAS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (GALLEY DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER AFT LEFT GALLEY DOOR INOPERATIVE. REPLACED OVERHEAD GALLEY DOOR LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TPA - EMERGENCY EXIT LIGHT OVERHEAD IN AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ABOVE LEFT ENTRY DOOR IN AFT GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY ABOVE LEFT ENTRY DOOR IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT SIGN HAD TWO BULBS INOPERATIVE. REPLACED AFT EMERGENCY EXIT SIGN LIGHT STRIP ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 340)

TUL - UNDERSIDE OF FLOORBEAM AT SEAT TRACK JUNCT, HOLES CORRODED, RIGHT OUTBOARD SEAT TRACK. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-6 OUT OF LIMITS. REPAIRED IAW AARD 53-10-07-2 FIG 1. (M)

Part: FRAME — CRACKED (BS 950)

TUL - BELL FRAME CRACKED AT FLOORBOARD SUPPORT STATION 950B RBL 4 INCH. CRACK WAS CUT OUT. REPAIRED BELL FRAME STATION 950B RBL 4 INCH IAW SRM 51-40-3. (M)

Part: FRAME — CORRODED (BS 416-417)

TUL - BOTTOM INBOARD END FRAME 416 CORODED AT STRINGER 17R ABOVE AND BELOW SILL PLATE. BLENDED CORROSION, OUT OF LIMITS PER SRM. INSTALLED DOUBLER IAW SRM 51-40-3, PAGE 1-5. (M)

Part: SILL — CORRODED (BS 414)

TUL - BELOW CREASE ANGLE STATION 414R SILL WEB CORRODED, BOTTOM SIDE AROUND DRAIN LINE HOSE, FORWARD GALLEY DOOR CUTOUT. REMOVED AND REPLACED WEB IAW SRM 51-10-01. (M)

Part: FRAME — CORRODED (BS 375-377)

TUL - FORWARD RIGHT GALLEY DOOR LOWER FRAME CORRODED INBOARD OF STRINGER 17R. CUT OUT CORRODED AREA AND INSTALLED DOUBLER IAW SRM 51-40-3 PAGES 1-5. (M)

Part: STRINGER — CORROSION (BS 707-710)

TUL - SKIN BULGED UNDER STRINGER 28 LEFT STATION 707-710, CORROSION ON STRINGER 28L, STATION 700-720, NO CORROSION ON SKIN. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN A NEW ONE PER SRM 53-10-3 FIG 1 SEC 4. (M)

Part: FRAME — CORRODED (BS 370)

TUL- FOUND CORROSION ON LOWER FRAME STA 370 RIGHT LOWER END AT STR 17R INBOARD. CUT OUT CORRODED AREA. INSTALLED DOUBLER IAW SRM 51-40-3 PAGES 1 THROUGH 5.

Part: ANGLE — CORRODED (LT ELEVATOR)

TUL - FOUND CORROSION ON TOP OF HORIZONTAL STAB T/E ALONG LT ELEVATOR HINGE LINE, APPROX 5 INCHES LONG 2 INCHES WIDE. INSTALLED DOUBLER PER ESO 11697. (M)

Part: FRAME — DENTED (BS 950)

TUL - FOUND STATION 950B BELL FRAME DENTED STRINGER 26R. REPAIRED STATION 950B BELL FRAME AT STRINGER 26R IAW SRM 51-40-3. (M)

Part: FLOORBEAM — CORRODED (BS 380)

TUL - STATION 380 FLOORBEAM 12 INCHES RBL TO RIGHT FWD SERVICE DOOR FRAME HAS CORROSION. INSTALLED REPAIR PER 53-10-6 ON FLOORBEAM. (M)

Part: FLOORBEAM — CORRODED (BS 1177)

TUL - CHORD ANGLE AT STATION 1177 CORRODED TOP AND BOTTOM RBL 27, SEE E58 0093393. REMOVED AND REPLACED CHORD ANGLE RBL 66 TO LBL 19 PER SRM 51-10-1, SEE E58 009 3393. (M)

Part: SPLICE — CORRODED (BS 1008)

TUL - STRINGER 26L, UPPER SIDE CORRODED AT STATION 1008. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3. (M)

Part: WEB — CORRODED (BS 373-377)

TUL - LOWER WEB CORRODED INBOARD STRINGER 17R STATION 373-377 AT CREASE ANGLE. REMOVED AND REPLACED WEB IAW SRM 51-10-1. (M)

Part: DOUBLER — CORRODED (BS 1010)

TUL - FOUND CORROSION ON SKIN SPLICE DOUBLER ABOVE STRINGER 26R, STATION 1010. INSTALLED DOUBLER SPLICE REPAIR, ESO 11697, DATED 14 NOV. (M)

Part: FRAME — CORRODED (BS 370)

TUL - FOUND CORROSION ON LWER FRAME STATION 370 RIGHT LOWER END AT STRINGER 17R INBOARD. CUT OUT CORRODED AREA. INSTALLED DOUBLER IAW SRM 51-40-3 PAGE 1 THROUGH 5. (M)

Part: MOTOR — LEAKING (TE FLAPS)

MIA - FLT 919 - AFTER TAKEOFF MIA DURING CLIMB-OUT, SYSTEM 'A' QTY BEGAN TO DECREASE BELOW 2. ACCOMP LOSS OF SYSTEM A ABNORMAL PROCEDURE AND AIRCRAFT RETURNED TO MIA, LANDING WITHOUT INCIDENT. REPLACED HYDRAULIC FLAP POWER UNIT MOTOR. ALSO, REPLACED 1/2 HYD PUMP FILTERS. SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED LEAK CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 950-990)

TUL - FOUND CORROSION ON STRINGER 29 LEFT FROM STATION 950F TO 990. REMOVED CORROSION, PRIMED AND TREATED AREA, INSTALLED REPAIR DOUBLER PER ESO 11697, DATED 2-27-97 AND SRM 53-10-03. (M)

Part: RETRACT MECH — MALFUNCTIONED (NLG)

MIA - FLT 2157 - AFTER TAKEOFF MIA WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEAR AND ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO MIA LANDED WITHOUT INCIDENT. ACCOMPLISHED LANDING GEAR RETRACTION AND FREE FALL CHECKS WITH NO DEFECTS FOUND. CYCLED LANDING GEAR MULTIPLE CYCLES AND OPERATION AND ALL LIGHTS INDICATE NORMAL. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYD MOTOR — DEFECTIVE (TE FLAPS)

MIA - FLT 1791 - AFTER TAKEOFF MIA DURING CLIMB-OUT, LOST SYSTEM A HYDRAULIC SYSTEM. MANUALLY LOWERED LANDING GEAR AND AIRCRAFT RETURNED TO MIA, LANDING WITHOUT INCIDENT. REPLACED FLAP HYDRAULIC MOTOR. PRECAUTIONARY REPLACED BOTH ENGINE DRIVE HYDRAULIC PUMPS. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — OUT OF ADJUST (RT MLG)

MIA - FLT 1791 - AFTER TAKEOFF MIA WITH LANDING GEAR RETRACTED, RIGHT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ADJUSTED RIGHT MAIN LANDING GEAR DOOR SWITCH. OPERATED DOOR AND SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT REDEPARTED MIA. (M)