N845AA

Boeing 727-223 Minor injury Part 121 — operator not named in the NTSB record

Boeing 727-223 Serious injury Part 121 — operator not named in the NTSB record

ATA 5711

Part: SPAR WEB — CRACKED (BS 870)

TUL - FOUND CRACK INDICATION APPROX RBL 5 INCHES ON UPPER REAR SPAR WEB. STOP DRILLED CRACK AND INSTALLED REPAIR STRAP AND FILLER PER ESO 11697, DATED 11/11/97. (M)

ATA 5311

Part: FRAME — MISDRILLED (BS 760.95)

TUL - INBOARD FRAME FLANGE AT STATION 760.95 RIGHT HAS MISDRILLED HOLE AT APPROX WL 212. OPENED HOLE AND INSTALLED FREEZE PLUG PER SRM 51-10-7. INSTALLED REPAIR DOUBLER AND STRAPS PER BOEING SERVICE BULLETIN 727-53-0197 AND DWG NR 65C36279. (M)

ATA 5320

Part: SHEAR TIE — CORRODED (BS 599)

TUL - FUSELAGE SKIN HAS BULGE JUST ABOVE STRINGER 26L SKIN LAP AT STATION 599 TO 601. REMOVED CORRODED SHEAR TIE AT STATION 600 , STRINGER 25L-26L AND REPLACED WITH NEW PER SRM 53-10-4. (M)

ATA 5311

Part: FRAME — BROKEN (BS 950)

TUL - BELTFRAME ON LOWER FORWARD CORNER OF AFT CARGO DOOR BROKEN. CUT OUT DAMAGE AND INSTALLED STAINLESS FORMER REPAIR PER SRM 51-40-3. (M)

ATA 3397

Part: WIRE — DELAMINATED (CABIN)

TUL - FLAT CONDUCTOR WAS DELAMINATED PRODUCING AN OPEN CIRCUIT. AFT SECTION OF EMERGENCY AISLE LIGHTS INOP. REPLACED P/N A3-06-0720-204, LIGHTS OPS CHECK OK. (M)

ATA 5312

Part: BULKHEAD WEB — CRACKED (BS 870)

TUL - STATION 870 BULKHEAD CRACKED AT CUTOUT FOR APU LOAD CONTROL VALVE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-2 PAGE 261 (C). (M)

ATA 5330

Part: SKIN — CORRODED (BS 1180)

TUL - SKIN BULGED AT AFT EDGE OF THE AFT LAV SERVICE PANEL AT STATION 1180, STRINGER 20L TO 21L (FUSELAGE SKIN). REMOVED CORRODED SECTION OF SKIN AND INNER DOUBLER (AREA PREVIOUSLY WORKED). INSTALLED NEW INNER DOUBLER AND REPAIR DOUBLER WITH FILLER PER SRM 53-30-3 FIG 3. (M)

ATA 2120

Part: AIR DISTR — ODOR (CABIN)

ATL - FLT 1503 - AFTER TAKEOFF ATL DURING CLIMB-OUT, UNIDENTIFIABLE FUMES/ODOR NOTED IN AFT CABIN. AIRCRAFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED BOTH PACKS WITH NO DEFECTS OR FUMES/ODOR NOTED. CHECKED ALL CARGO COMPARTMENTS AND VENTRAL STAIR AREA WITH NO DEFECTS FOUND. OPERATED ALL GALLEY OVENS WITH NO DEFECTS FUOND. UNABLE TO DUPLICATE PROBLEM. PRECAUTIONARY CLEANED FORWARD GALLEY OVENS AND AIRCRAFT REDEPARTED. (M)

ATA 3350

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

ATA 5743

Part: PIVOT PIN — CRACKED (MLG BEAM)

TUL - FOUND REQ TORQUE VALUE TO HAVE STRETCHED AND CRACKED PIVOT PIN AT THREADED END. FOUND WHILE ATTEMPTING TO REMOVE (NUT). POSSIBLE OVER TORQUE VALUE IN 'FT LBS' SHOULD BE 'IN LBS'. (M)

ATA 5330

Part: SKIN — WORN (BS 720)

TUL - FOUND FUSELAGE SKIN HAS HEAVY WEAR MARKS FROM LEFT WING ROOT LE FAIRING AT STRINGER 19 LAP JOINT. INSTALLED DOUBLER AND FILLER PER 53-30-3 SRM. (M)

ATA 5330

Part: SKIN — CRACKED (BS 1097)

TUL - FOUND FUSELAGE SKIN HAS VISUAL INDICATION OF CRACK (APPROX 1 INCH LONG) EXTENDING FROM RIVET HEAD STRINGER 1 AT STATION 1097. INSTALLED DOUBLER AND FILLER WITH 870B2 PER SB53A0204 AND SRM 53-30-3 FIG 3. (M)

ATA 5330

Part: SKIN — CORRODED (BS 1183)

TUL - SKIN BULGING AND RIVET HEADS PULLED UNDER AFT LAV SERVICE PANEL. REMOVED DAMAGED AREA AND CORROSION AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1 SHEET 1-4. (M)

ATA 5713

Part: STRINGER — CRACKED (WS 686.5)

TUL - UPPER WING STRINGER CRACKED AT WS 686.5, FIRST STRINGER FORWARD OF JETTISON TUBE, INSIDE WING. STOP DRILLED CRACK. FABRICATED 3 SMALL DOUBLERS. INSTALLED DOUBLERS PER SRM 57-10-4. (M)